{"info":{"_postman_id":"7e7b5c63-1636-43fe-88db-e4722539b23f","name":"Engineer Component","description":"Engineer Component collection for SIA App Challenge 2019.","schema":"https://schema.getpostman.com/json/collection/v2.0.0/collection.json"},"item":[{"name":"RepairLog","id":"da93eede-fd4d-457e-bc01-be8620b68422","protocolProfileBehavior":{"disableBodyPruning":true},"request":{"method":"GET","header":[],"url":"{{url}}/repairlog","description":"A sample repair log / history of various aircraft components.<br>\n(Do note: the values used are not actual values, but fictitious examples of the types of records/inputs captured)"},"response":[{"id":"14638438-0c65-4290-b3b6-b28c8062ad85","name":"Get RepairLog By ComponentID = 873421-361-91:89AB2","originalRequest":{"method":"GET","header":[],"url":{"raw":"{{url}}/repairlog?ComponentID=873421-361-91:89AB2","host":["{{url}}"],"path":["repairlog"],"query":[{"key":"ComponentID","value":"873421-361-91:89AB2"}]}},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"data\": {\n        \"Component\": \"Duct Assy Clamp\",\n        \"ComponentID\": \"873421-361-91:89AB2\",\n        \"serial no\": \"86509253\",\n        \"history\": [\n            {\n                \"index\": \"0\",\n                \"equipment\": \"886240\",\n                \"flying hours TSI\": \"10951.87\",\n                \"flying cycles TSI\": \"1396\",\n                \"installed days TSI\": \"809\",\n                \"flying hours TSN\": \"10951.87\",\n                \"flying cycles TSN\": \"1396\",\n                \"installed days TSN\": \"809\",\n                \"flying hours TSO\": \"10951.87\",\n                \"flying cycles TSO\": \"1396\",\n                \"installed days TSO\": \"809\",\n                \"install date\": \"02/11/2015\",\n                \"A/C reg\": \"9V-SWI\",\n                \"A/C posn\": \"EMA_JCL_22K\",\n                \"removal date\": \"27/09/2018\",\n                \"fail/NFF\": \"NDEC\",\n                \"defect\": \"null\",\n                \"action taken\": \"null\",\n                \"reason for removal\": \"Reason for dismantle: EMA TEST FAILED\",\n                \"order\": \"1320908653094\",\n                \"vendor\": \"STARTECH SOLUTIONS\"\n            }\n        ]\n    }\n}"},{"id":"9025e52c-b02d-45da-8612-962095055a4c","name":"Get RepairLog By ComponentID = 347892-837-42:88GF2","originalRequest":{"method":"GET","header":[],"url":{"raw":"{{url}}/repairlog?ComponentID=347892-837-42:88GF2","host":["{{url}}"],"path":["repairlog"],"query":[{"key":"ComponentID","value":"347892-837-42:88GF2"}]}},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"data\": {\n        \"Component\": \"Avi OHDS Connectors\",\n        \"ComponentID\": \"347892-837-42:88GF2\",\n        \"serial no\": \"86809002\",\n        \"history\": [\n            {\n                \"index\": \"0\",\n                \"equipment\": \"885848\",\n                \"flying hours TSI\": \"10951.87\",\n                \"flying cycles TSI\": \"1396\",\n                \"installed days TSI\": \"809\",\n                \"flying hours TSN\": \"10951.87\",\n                \"flying cycles TSN\": \"1396\",\n                \"installed days TSN\": \"809\",\n                \"flying hours TSO\": \"10951.87\",\n                \"flying cycles TSO\": \"1396\",\n                \"installed days TSO\": \"809\",\n                \"install date\": \"16/05/2019\",\n                \"A/C reg\": \"9V-SWI\",\n                \"A/C posn\": \"EMA_JCL_22K\",\n                \"removal date\": \"10/09/2019\",\n                \"fail/NFF\": \"NDEC\",\n                \"defect\": \"FOUND EMA AT SEAT 23K NIL OUTPUT WHEN PUSH TO TESTnP/N OFF: 511959-407-42nS/N OFF: A24MAY16-46(EX STORE)\",\n                \"action taken\": \"SAID EMA REPLACED TO NO AVAIL. FOUND EX-STORE.nX-REF TO SVO 36284893 FOR NEXT WORK DETAILS.\",\n                \"reason for removal\": \"FOUND EMA AT SEAT 23K NIL OUTPUT WHEN PUSH TO TESTnP/N OFF: 511959-407-42nS/N OFF: A24MAY16-46(EX STORE)\",\n                \"order\": \"13214868021212\",\n                \"vendor\": \"SENG HIP ENG INC\"\n            },\n            {\n                \"index\": \"1\",\n                \"equipment\": \"885853\",\n                \"flying hours TSI\": \"12880.24\",\n                \"flying cycles TSI\": \"1396\",\n                \"installed days TSI\": \"809\",\n                \"flying hours TSN\": \"12880.24\",\n                \"flying cycles TSN\": \"1396\",\n                \"installed days TSN\": \"809\",\n                \"flying hours TSO\": \"12880.24\",\n                \"flying cycles TSO\": \"1628\",\n                \"installed days TSO\": \"956\",\n                \"install date\": \"16/05/2019\",\n                \"A/C reg\": \"9V-SWI\",\n                \"A/C posn\": \"EMA_JCL_17F\",\n                \"removal date\": \"16/05/2019\",\n                \"fail/NFF\": \"NDEC\",\n                \"defect\": \"FOUND EMA AT SEAT 17F NIL OUTPUT WHEN PUSH TO TEST.nP/N OFF: 511959-401-42nS/N OFF: A28OCT15-268\",\n                \"action taken\": \"SAID EMA REPLACEMENT CARRIED OUT. INSTALLATION TEST FOUND SATISFACTORY.\",\n                \"reason for removal\": \"null\",\n                \"order\": \"null\",\n                \"vendor\": \"STARTECH SOLUTIONS\"\n            },\n            {\n                \"index\": \"2\",\n                \"equipment\": \"885848\",\n                \"flying hours\": \"10951.87\",\n                \"flying cycle\": \"1396\",\n                \"installed days\": \"809\",\n                \"install date\": \"24/05/2016\",\n                \"A/C reg\": \"9V-SWF\",\n                \"A/C posn\": \"EMA_FCL_1D\",\n                \"removal date\": \"10/08/2018\",\n                \"fail/NFF\": \"NDEC\",\n                \"defect\": \"null\",\n                \"action taken\": \"null\",\n                \"reason for removal\": \"Reason for dismantle:EMA TEST FAILED\",\n                \"order\": \"null\",\n                \"vendor\": \"STARTECH SOLUTIONS\"\n            }\n        ]\n    }\n}"},{"id":"95fa6a1c-133b-425c-8d92-01a6132f0878","name":"Get RepairLog By ComponentID = 912312-129-11:32ND2","originalRequest":{"method":"GET","header":[],"url":{"raw":"{{url}}/repairlog?ComponentID=912312-129-11:32ND2","host":["{{url}}"],"path":["repairlog"],"query":[{"key":"ComponentID","value":"912312-129-11:32ND2"}]}},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"data\": {\n        \"Component\": \"Run Controller Plug\",\n        \"ComponentID\": \"912312-129-11:32ND2\",\n        \"serial no\": \"843092493\",\n        \"history\": [\n            {\n                \"index\": \"0\",\n                \"equipment\": \"922115\",\n                \"flying hours TSI\": \"7212.20\",\n                \"flying cycles TSI\": \"1219\",\n                \"installed days TSI\": \"730\",\n                \"flying hours TSN\": \"7212.20\",\n                \"flying cycles TSN\": \"1219\",\n                \"installed days TSN\": \"730\",\n                \"flying hours TSO\": \"7212.20\",\n                \"flying cycles TSO\": \"1219\",\n                \"installed days TSO\": \"730\",\n                \"install date\": \"16/01/2017\",\n                \"A/C reg\": \"9V-SWI\",\n                \"A/C posn\": \"EMA_JCL_11D\",\n                \"removal date\": \"15/01/2019\",\n                \"fail/NFF\": \"NDEC\",\n                \"defect\": \"ALL B/C SEATS EMA FAILED DURING OPERATION TESTn(QTY: 48) P/N: 912312-129-11\",\n                \"action taken\": \"SEATS 16K,17A,17D,17F,17K,18A,18F,18K,19A,19D,19F,19K,20A,20D,20F,20K,21A,21D,21FF,21K,22A,22D,22D,22F,22K,23A,23F AND 23K EMA REPLACED AND TESTED AS PER AMSAFE ICAW E512322 CMM 25-20-01 FOUND SATISFACTORY SEATS 11A,11D,11K,12A,12D,12F,12K,14A<(>,<)> 14D,14F,14K,15A,15D,15F,15K,16A,6D AND 16F EMA REPLACED AND TESTED AS PER AMSAFE ICAW E512322 CMM 25-20-01. FOUND SATISFACTORY. CMM 25-20-01\",\n                \"reason for removal\": \"null\",\n                \"order\": \"null\",\n                \"vendor\": \"null\"\n            },\n            {\n                \"index\": \"1\",\n                \"equipment\": \"922151\",\n                \"flying hours TSI\": \"7212.20\",\n                \"flying cycles TSI\": \"1219\",\n                \"installed days TSI\": \"730\",\n                \"flying hours TSN\": \"7212.20\",\n                \"flying cycles TSN\": \"1219\",\n                \"installed days TSN\": \"730\",\n                \"flying hours TSO\": \"7212.20\",\n                \"flying cycles TSO\": \"1219\",\n                \"installed days TSO\": \"730\",\n                \"install date\": \"16/01/2017\",\n                \"A/C reg\": \"9V-SWI\",\n                \"A/C posn\": \"EMA_JCL_11F\",\n                \"removal date\": \"15/01/2019\",\n                \"fail/NFF\": \"NDEC\",\n                \"defect\": \"ALL B/C SEATS EMA FAILED DURING OPERATION TEST (QTY: 48) P/N: 912312-129-11\",\n                \"action taken\": \"SEATS 16K,17A,17D,17F,17K,18A,18F,18K,19A,19D,19F,19K,20A,20D,20F,20K,21A,21D,21FF,21K,22A,22D,22D,22F,22K,23A,23F AND 23K EMA REPLACED AND TESTED AS PER AMSAFE ICAW E512322 CMM 25-20-01 FOUND SATISFACTORY SEATS 11A,11D,11K,12A,12D,12F,12K,14A<(>,<)> 14D,14F,14K,15A,15D,15F,15K,16A,6D AND 16F EMA REPLACED AND TESTED AS PER AMSAFE ICAW E512322 CMM 25-20-01. FOUND SATISFACTORY. CMM 25-20-01\",\n                \"reason for removal\": \"null\",\n                \"order\": \"null\",\n                \"vendor\": \"STARTECH SOLUTIONS\"\n            }\n        ]\n    }\n}"},{"id":"a00186bc-6e8c-490c-9e83-0e22507d8fdf","name":"Get RepairLog By ComponentID = 829323-120-82:78YU2","originalRequest":{"method":"GET","header":[],"url":{"raw":"{{url}}/repairlog?ComponentID=829323-120-82:78YU2","host":["{{url}}"],"path":["repairlog"],"query":[{"key":"ComponentID","value":"829323-120-82:78YU2"}]}},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"data\": {\n        \"Component\": \"Dynamic Shark Bus Cable\",\n        \"ComponentID\": \"829323-120-82:78YU2\",\n        \"serial no\": \"88310910\",\n        \"history\": [\n            {\n                \"index\": \"0\",\n                \"equipment\": \"956057\",\n                \"flying hours TSI\": \"257.39\",\n                \"flying cycles TSI\": \"1612\",\n                \"installed days TSI\": \"852\",\n                \"flying hours TSN\": \"257.39\",\n                \"flying cycles TSN\": \"1612\",\n                \"installed days TSN\": \"852\",\n                \"flying hours TSO\": \"257.39\",\n                \"flying cycles TSO\": \"1612\",\n                \"installed days TSO\": \"852\",\n                \"install date\": \"24/01/2017\",\n                \"A/C reg\": \"9V-SWS\",\n                \"A/C posn\": \"EMA_FCL_1D\",\n                \"removal date\": \"25/05/2019\",\n                \"fail/NFF\": \"NDEC\",\n                \"defect\": \"X-829323-120-82-FOUND SEAT 1D EMA SHOWING '3 RED LIGHTS'\",\n                \"action taken\": \"PN OFF 829323-120-82 SN OFF A24JAN17-281 PN ON 829323-120-82 SN ON A24JAN17-281\",\n                \"reason for removal\": \"X-829323-120-82-FOUND SEAT 1D EMA SHOWING '3 RED LIGHTS'\",\n                \"order\": \"1321463153067\",\n                \"vendor\": \"SENG HIP ENG INC\"\n            },\n            {\n                \"index\": \"1\",\n                \"equipment\": \"961847\",\n                \"flying hours TSI\": \"48.76\",\n                \"flying cycles TSI\": \"8\",\n                \"installed days TSI\": \"5\",\n                \"flying hours TSN\": \"48.76\",\n                \"flying cycles TSN\": \"8\",\n                \"installed days TSN\": \"5\",\n                \"flying hours TSO\": \"48.76\",\n                \"flying cycles TSO\": \"8\",\n                \"installed days TSO\": \"5\",\n                \"install date\": \"14/06/2019\",\n                \"A/C reg\": \"9V-SWK\",\n                \"A/C posn\": \"EMA_JCL_11F\",\n                \"removal date\": \"19/06/2019\",\n                \"fail/NFF\": \"NDEC\",\n                \"defect\": \"X-ELECTRONIC MODULE PN 829323-120-82 SN A10JAN19-247 FAILED INFLATABLE SEAT BELT TEST.\",\n                \"action taken\": \"null\",\n                \"reason for removal\": \"X-ELECTRONIC MODULE PN 829323-120-82 SN A10JAN19-247 FAILED INFLATABLE SEAT BELT TEST.\",\n                \"order\": \"1321520943216\",\n                \"vendor\": \"SENG HIP ENG INC\"\n            }\n        ]\n    }\n}"},{"id":"e4c6aa22-02b2-453c-91eb-bb32864627bc","name":"Get RepairLog By ComponentID = 511959-407-42:35FB9","originalRequest":{"method":"GET","header":[],"url":{"raw":"{{url}}/repairlog?ComponentID=511959-407-42:35FB9","host":["{{url}}"],"path":["repairlog"],"query":[{"key":"ComponentID","value":"511959-407-42:35FB9"}]}},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"data\": {\n        \"Component\": \"Engine Precooler\",\n        \"ComponentID\": \"511959-407-42:35FB9\",\n        \"serial no\": \"84220948\",\n        \"history\": [\n            {\n                \"index\": \"0\",\n                \"equipment\": \"null\",\n                \"flying hours TSI\": \"null\",\n                \"flying cycles TSI\": \"null\",\n                \"installed days TSI\": \"null\",\n                \"flying hours TSN\": \"null\",\n                \"flying cycles TSN\": \"null\",\n                \"installed days TSN\": \"null\",\n                \"flying hours TSO\": \"null\",\n                \"flying cycles TSO\": \"null\",\n                \"installed days TSO\": \"null\",\n                \"install date\": \"null\",\n                \"A/C reg\": \"null\",\n                \"A/C posn\": \"null\",\n                \"removal date\": \"10/09/2019\",\n                \"fail/NFF\": \"No fault found\",\n                \"defect\": \"null\",\n                \"action taken\": \"null\",\n                \"reason for removal\": \"(Dismantle) EMA BIT TEST C/OUT EMA FAILED\",\n                \"order\": \"1320861600012\",\n                \"vendor\": \"SECENG INC\"\n            },\n            {\n                \"index\": \"1\",\n                \"equipment\": \"null\",\n                \"flying hours TSI\": \"null\",\n                \"flying cycles TSI\": \"null\",\n                \"installed days TSI\": \"null\",\n                \"flying hours TSN\": \"null\",\n                \"flying cycles TSN\": \"null\",\n                \"installed days TSN\": \"null\",\n                \"flying hours TSO\": \"null\",\n                \"flying cycles TSO\": \"null\",\n                \"installed days TSO\": \"null\",\n                \"install date\": \"null\",\n                \"A/C reg\": \"null\",\n                \"A/C posn\": \"null\",\n                \"removal date\": \"08/08/2018\",\n                \"fail/NFF\": \"NDEC\",\n                \"defect\": \"null\",\n                \"action taken\": \"null\",\n                \"reason for removal\": \"(Dismantle) SEAT 45G ELECTRONIC MODULE ASSY PUSH TO TEST FAILED DURING OPERATIONAL CHECK\",\n                \"order\": \"1320779037854\",\n                \"vendor\": \"SENG HIP ENG INC\"\n            },\n            {\n                \"index\": \"2\",\n                \"flying hours TSI\": \"null\",\n                \"flying cycles TSI\": \"null\",\n                \"installed days TSI\": \"null\",\n                \"flying hours TSN\": \"null\",\n                \"flying cycles TSN\": \"null\",\n                \"installed days TSN\": \"null\",\n                \"flying hours TSO\": \"null\",\n                \"flying cycles TSO\": \"null\",\n                \"installed days TSO\": \"null\",\n                \"install date\": \"null\",\n                \"A/C reg\": \"null\",\n                \"A/C posn\": \"null\",\n                \"removal date\": \"07/08/2018\",\n                \"fail/NFF\": \"NDEC\",\n                \"defect\": \"null\",\n                \"action taken\": \"null\",\n                \"reason for removal\": \"(Dismantle) EMA TEST CARRIED OUT, BATTERY FAILURE DETECTED\",\n                \"order\": \"1320680974309\",\n                \"vendor\": \"SECENG INC\"\n            },\n            {\n                \"index\": \"3\",\n                \"equipment\": \"null\",\n                \"flying hours TSI\": \"null\",\n                \"flying cycles TSI\": \"null\",\n                \"installed days TSI\": \"null\",\n                \"flying hours TSN\": \"null\",\n                \"flying cycles TSN\": \"null\",\n                \"installed days TSN\": \"null\",\n                \"flying hours TSO\": \"null\",\n                \"flying cycles TSO\": \"null\",\n                \"installed days TSO\": \"null\",\n                \"install date\": \"null\",\n                \"A/C reg\": \"null\",\n                \"A/C posn\": \"null\",\n                \"removal date\": \"21/06/2018\",\n                \"fail/NFF\": \"NDEC\",\n                \"defect\": \"null\",\n                \"action taken\": \"null\",\n                \"reason for removal\": \"ELECTRONIC MODULE ASSY SN A06AUG15-207 QTY 01 REMOVED DUE SELF TEST FAILED DURING OPERATIONAL CHECK.\",\n                \"order\": \"1320642985098\",\n                \"vendor\": \"SECENG INC\"\n            },\n            {\n                \"index\": \"4\",\n                \"equipment\": \"null\",\n                \"flying hours TSI\": \"null\",\n                \"flying cycles TSI\": \"null\",\n                \"installed days TSI\": \"null\",\n                \"flying hours TSN\": \"null\",\n                \"flying cycles TSN\": \"null\",\n                \"installed days TSN\": \"null\",\n                \"flying hours TSO\": \"null\",\n                \"flying cycles TSO\": \"null\",\n                \"installed days TSO\": \"null\",\n                \"install date\": \"null\",\n                \"A/C reg\": \"null\",\n                \"A/C posn\": \"null\",\n                \"removal date\": \"20/06/2018\",\n                \"fail/NFF\": \"NDEC\",\n                \"defect\": \"SEAT 11F FAILED TO INFLATABLE SEAT RESTRAINT SYSTEM OPERATIONAL CHECK.nPN: 511959-407-42nQTY: 01 OFF\",\n                \"action taken\": \"SEAT 11F EMA REPLACED, INSTALLATION TEST C/OUT FOUND SATIS\",\n                \"reason for removal\": \"SEAT 11F FAILED TO INFLATABLE SEAT RESTRAINT SYSTEM OPERATIONAL CHECK.nPN: 511959-407-42nQTY: 01 OFF\",\n                \"order\": \"1320596554113\",\n                \"vendor\": \"SECENG INC\"\n            }\n        ]\n    }\n}"},{"id":"ea519d9f-6351-4968-8a97-ce047e88ad75","name":"Get All Repair Logs","originalRequest":{"method":"GET","header":[],"url":"{{url}}/repairlog"},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"reports\": [\n        {\n            \"Component\": \"Engine Precooler\",\n            \"ComponentID\": \"511959-407-42:35FB9\",\n            \"serial no\": \"84220948\",\n            \"history\": [\n                {\n                    \"index\": \"0\",\n                    \"equipment\": \"null\",\n                    \"flying hours TSI\": \"null\",\n                    \"flying cycles TSI\": \"null\",\n                    \"installed days TSI\": \"null\",\n                    \"flying hours TSN\": \"null\",\n                    \"flying cycles TSN\": \"null\",\n                    \"installed days TSN\": \"null\",\n                    \"flying hours TSO\": \"null\",\n                    \"flying cycles TSO\": \"null\",\n                    \"installed days TSO\": \"null\",\n                    \"install date\": \"null\",\n                    \"A/C reg\": \"null\",\n                    \"A/C posn\": \"null\",\n                    \"removal date\": \"10/09/2019\",\n                    \"fail/NFF\": \"No fault found\",\n                    \"defect\": \"null\",\n                    \"action taken\": \"null\",\n                    \"reason for removal\": \"(Dismantle) EMA BIT TEST C/OUT EMA FAILED\",\n                    \"order\": \"1320861600012\",\n                    \"vendor\": \"SECENG INC\"\n                },\n                {\n                    \"index\": \"1\",\n                    \"equipment\": \"null\",\n                    \"flying hours TSI\": \"null\",\n                    \"flying cycles TSI\": \"null\",\n                    \"installed days TSI\": \"null\",\n                    \"flying hours TSN\": \"null\",\n                    \"flying cycles TSN\": \"null\",\n                    \"installed days TSN\": \"null\",\n                    \"flying hours TSO\": \"null\",\n                    \"flying cycles TSO\": \"null\",\n                    \"installed days TSO\": \"null\",\n                    \"install date\": \"null\",\n                    \"A/C reg\": \"null\",\n                    \"A/C posn\": \"null\",\n                    \"removal date\": \"08/08/2018\",\n                    \"fail/NFF\": \"NDEC\",\n                    \"defect\": \"null\",\n                    \"action taken\": \"null\",\n                    \"reason for removal\": \"(Dismantle) SEAT 45G ELECTRONIC MODULE ASSY PUSH TO TEST FAILED DURING OPERATIONAL CHECK\",\n                    \"order\": \"1320779037854\",\n                    \"vendor\": \"SENG HIP ENG INC\"\n                },\n                {\n                    \"index\": \"2\",\n                    \"flying hours TSI\": \"null\",\n                    \"flying cycles TSI\": \"null\",\n                    \"installed days TSI\": \"null\",\n                    \"flying hours TSN\": \"null\",\n                    \"flying cycles TSN\": \"null\",\n                    \"installed days TSN\": \"null\",\n                    \"flying hours TSO\": \"null\",\n                    \"flying cycles TSO\": \"null\",\n                    \"installed days TSO\": \"null\",\n                    \"install date\": \"null\",\n                    \"A/C reg\": \"null\",\n                    \"A/C posn\": \"null\",\n                    \"removal date\": \"07/08/2018\",\n                    \"fail/NFF\": \"NDEC\",\n                    \"defect\": \"null\",\n                    \"action taken\": \"null\",\n                    \"reason for removal\": \"(Dismantle) EMA TEST CARRIED OUT, BATTERY FAILURE DETECTED\",\n                    \"order\": \"1320680974309\",\n                    \"vendor\": \"SECENG INC\"\n                },\n                {\n                    \"index\": \"3\",\n                    \"equipment\": \"null\",\n                    \"flying hours TSI\": \"null\",\n                    \"flying cycles TSI\": \"null\",\n                    \"installed days TSI\": \"null\",\n                    \"flying hours TSN\": \"null\",\n                    \"flying cycles TSN\": \"null\",\n                    \"installed days TSN\": \"null\",\n                    \"flying hours TSO\": \"null\",\n                    \"flying cycles TSO\": \"null\",\n                    \"installed days TSO\": \"null\",\n                    \"install date\": \"null\",\n                    \"A/C reg\": \"null\",\n                    \"A/C posn\": \"null\",\n                    \"removal date\": \"21/06/2018\",\n                    \"fail/NFF\": \"NDEC\",\n                    \"defect\": \"null\",\n                    \"action taken\": \"null\",\n                    \"reason for removal\": \"ELECTRONIC MODULE ASSY SN A06AUG15-207 QTY 01 REMOVED DUE SELF TEST FAILED DURING OPERATIONAL CHECK.\",\n                    \"order\": \"1320642985098\",\n                    \"vendor\": \"SECENG INC\"\n                },\n                {\n                    \"index\": \"4\",\n                    \"equipment\": \"null\",\n                    \"flying hours TSI\": \"null\",\n                    \"flying cycles TSI\": \"null\",\n                    \"installed days TSI\": \"null\",\n                    \"flying hours TSN\": \"null\",\n                    \"flying cycles TSN\": \"null\",\n                    \"installed days TSN\": \"null\",\n                    \"flying hours TSO\": \"null\",\n                    \"flying cycles TSO\": \"null\",\n                    \"installed days TSO\": \"null\",\n                    \"install date\": \"null\",\n                    \"A/C reg\": \"null\",\n                    \"A/C posn\": \"null\",\n                    \"removal date\": \"20/06/2018\",\n                    \"fail/NFF\": \"NDEC\",\n                    \"defect\": \"SEAT 11F FAILED TO INFLATABLE SEAT RESTRAINT SYSTEM OPERATIONAL CHECK.nPN: 511959-407-42nQTY: 01 OFF\",\n                    \"action taken\": \"SEAT 11F EMA REPLACED, INSTALLATION TEST C/OUT FOUND SATIS\",\n                    \"reason for removal\": \"SEAT 11F FAILED TO INFLATABLE SEAT RESTRAINT SYSTEM OPERATIONAL CHECK.nPN: 511959-407-42nQTY: 01 OFF\",\n                    \"order\": \"1320596554113\",\n                    \"vendor\": \"SECENG INC\"\n                }\n            ]\n        },\n        {\n            \"Component\": \"Avi OHDS Connectors\",\n            \"ComponentID\": \"347892-837-42:88GF2\",\n            \"serial no\": \"86809002\",\n            \"history\": [\n                {\n                    \"index\": \"0\",\n                    \"equipment\": \"885848\",\n                    \"flying hours TSI\": \"10951.87\",\n                    \"flying cycles TSI\": \"1396\",\n                    \"installed days TSI\": \"809\",\n                    \"flying hours TSN\": \"10951.87\",\n                    \"flying cycles TSN\": \"1396\",\n                    \"installed days TSN\": \"809\",\n                    \"flying hours TSO\": \"10951.87\",\n                    \"flying cycles TSO\": \"1396\",\n                    \"installed days TSO\": \"809\",\n                    \"install date\": \"16/05/2019\",\n                    \"A/C reg\": \"9V-SWI\",\n                    \"A/C posn\": \"EMA_JCL_22K\",\n                    \"removal date\": \"10/09/2019\",\n                    \"fail/NFF\": \"NDEC\",\n                    \"defect\": \"FOUND EMA AT SEAT 23K NIL OUTPUT WHEN PUSH TO TESTnP/N OFF: 511959-407-42nS/N OFF: A24MAY16-46(EX STORE)\",\n                    \"action taken\": \"SAID EMA REPLACED TO NO AVAIL. FOUND EX-STORE.nX-REF TO SVO 36284893 FOR NEXT WORK DETAILS.\",\n                    \"reason for removal\": \"FOUND EMA AT SEAT 23K NIL OUTPUT WHEN PUSH TO TESTnP/N OFF: 511959-407-42nS/N OFF: A24MAY16-46(EX STORE)\",\n                    \"order\": \"13214868021212\",\n                    \"vendor\": \"SENG HIP ENG INC\"\n                },\n                {\n                    \"index\": \"1\",\n                    \"equipment\": \"885853\",\n                    \"flying hours TSI\": \"12880.24\",\n                    \"flying cycles TSI\": \"1396\",\n                    \"installed days TSI\": \"809\",\n                    \"flying hours TSN\": \"12880.24\",\n                    \"flying cycles TSN\": \"1396\",\n                    \"installed days TSN\": \"809\",\n                    \"flying hours TSO\": \"12880.24\",\n                    \"flying cycles TSO\": \"1628\",\n                    \"installed days TSO\": \"956\",\n                    \"install date\": \"16/05/2019\",\n                    \"A/C reg\": \"9V-SWI\",\n                    \"A/C posn\": \"EMA_JCL_17F\",\n                    \"removal date\": \"16/05/2019\",\n                    \"fail/NFF\": \"NDEC\",\n                    \"defect\": \"FOUND EMA AT SEAT 17F NIL OUTPUT WHEN PUSH TO TEST.nP/N OFF: 511959-401-42nS/N OFF: A28OCT15-268\",\n                    \"action taken\": \"SAID EMA REPLACEMENT CARRIED OUT. INSTALLATION TEST FOUND SATISFACTORY.\",\n                    \"reason for removal\": \"null\",\n                    \"order\": \"null\",\n                    \"vendor\": \"STARTECH SOLUTIONS\"\n                },\n                {\n                    \"index\": \"2\",\n                    \"equipment\": \"885848\",\n                    \"flying hours\": \"10951.87\",\n                    \"flying cycle\": \"1396\",\n                    \"installed days\": \"809\",\n                    \"install date\": \"24/05/2016\",\n                    \"A/C reg\": \"9V-SWF\",\n                    \"A/C posn\": \"EMA_FCL_1D\",\n                    \"removal date\": \"10/08/2018\",\n                    \"fail/NFF\": \"NDEC\",\n                    \"defect\": \"null\",\n                    \"action taken\": \"null\",\n                    \"reason for removal\": \"Reason for dismantle:EMA TEST FAILED\",\n                    \"order\": \"null\",\n                    \"vendor\": \"STARTECH SOLUTIONS\"\n                }\n            ]\n        },\n        {\n            \"Component\": \"Duct Assy Clamp\",\n            \"ComponentID\": \"873421-361-91:89AB2\",\n            \"serial no\": \"86509253\",\n            \"history\": [\n                {\n                    \"index\": \"0\",\n                    \"equipment\": \"886240\",\n                    \"flying hours TSI\": \"10951.87\",\n                    \"flying cycles TSI\": \"1396\",\n                    \"installed days TSI\": \"809\",\n                    \"flying hours TSN\": \"10951.87\",\n                    \"flying cycles TSN\": \"1396\",\n                    \"installed days TSN\": \"809\",\n                    \"flying hours TSO\": \"10951.87\",\n                    \"flying cycles TSO\": \"1396\",\n                    \"installed days TSO\": \"809\",\n                    \"install date\": \"02/11/2015\",\n                    \"A/C reg\": \"9V-SWI\",\n                    \"A/C posn\": \"EMA_JCL_22K\",\n                    \"removal date\": \"27/09/2018\",\n                    \"fail/NFF\": \"NDEC\",\n                    \"defect\": \"null\",\n                    \"action taken\": \"null\",\n                    \"reason for removal\": \"Reason for dismantle: EMA TEST FAILED\",\n                    \"order\": \"1320908653094\",\n                    \"vendor\": \"STARTECH SOLUTIONS\"\n                }\n            ]\n        },\n        {\n            \"Component\": \"Run Controller Plug\",\n            \"ComponentID\": \"912312-129-11:32ND2\",\n            \"serial no\": \"843092493\",\n            \"history\": [\n                {\n                    \"index\": \"0\",\n                    \"equipment\": \"922115\",\n                    \"flying hours TSI\": \"7212.20\",\n                    \"flying cycles TSI\": \"1219\",\n                    \"installed days TSI\": \"730\",\n                    \"flying hours TSN\": \"7212.20\",\n                    \"flying cycles TSN\": \"1219\",\n                    \"installed days TSN\": \"730\",\n                    \"flying hours TSO\": \"7212.20\",\n                    \"flying cycles TSO\": \"1219\",\n                    \"installed days TSO\": \"730\",\n                    \"install date\": \"16/01/2017\",\n                    \"A/C reg\": \"9V-SWI\",\n                    \"A/C posn\": \"EMA_JCL_11D\",\n                    \"removal date\": \"15/01/2019\",\n                    \"fail/NFF\": \"NDEC\",\n                    \"defect\": \"ALL B/C SEATS EMA FAILED DURING OPERATION TESTn(QTY: 48) P/N: 912312-129-11\",\n                    \"action taken\": \"SEATS 16K,17A,17D,17F,17K,18A,18F,18K,19A,19D,19F,19K,20A,20D,20F,20K,21A,21D,21FF,21K,22A,22D,22D,22F,22K,23A,23F AND 23K EMA REPLACED AND TESTED AS PER AMSAFE ICAW E512322 CMM 25-20-01 FOUND SATISFACTORY SEATS 11A,11D,11K,12A,12D,12F,12K,14A<(>,<)> 14D,14F,14K,15A,15D,15F,15K,16A,6D AND 16F EMA REPLACED AND TESTED AS PER AMSAFE ICAW E512322 CMM 25-20-01. FOUND SATISFACTORY. CMM 25-20-01\",\n                    \"reason for removal\": \"null\",\n                    \"order\": \"null\",\n                    \"vendor\": \"null\"\n                },\n                {\n                    \"index\": \"1\",\n                    \"equipment\": \"922151\",\n                    \"flying hours TSI\": \"7212.20\",\n                    \"flying cycles TSI\": \"1219\",\n                    \"installed days TSI\": \"730\",\n                    \"flying hours TSN\": \"7212.20\",\n                    \"flying cycles TSN\": \"1219\",\n                    \"installed days TSN\": \"730\",\n                    \"flying hours TSO\": \"7212.20\",\n                    \"flying cycles TSO\": \"1219\",\n                    \"installed days TSO\": \"730\",\n                    \"install date\": \"16/01/2017\",\n                    \"A/C reg\": \"9V-SWI\",\n                    \"A/C posn\": \"EMA_JCL_11F\",\n                    \"removal date\": \"15/01/2019\",\n                    \"fail/NFF\": \"NDEC\",\n                    \"defect\": \"ALL B/C SEATS EMA FAILED DURING OPERATION TEST (QTY: 48) P/N: 912312-129-11\",\n                    \"action taken\": \"SEATS 16K,17A,17D,17F,17K,18A,18F,18K,19A,19D,19F,19K,20A,20D,20F,20K,21A,21D,21FF,21K,22A,22D,22D,22F,22K,23A,23F AND 23K EMA REPLACED AND TESTED AS PER AMSAFE ICAW E512322 CMM 25-20-01 FOUND SATISFACTORY SEATS 11A,11D,11K,12A,12D,12F,12K,14A<(>,<)> 14D,14F,14K,15A,15D,15F,15K,16A,6D AND 16F EMA REPLACED AND TESTED AS PER AMSAFE ICAW E512322 CMM 25-20-01. FOUND SATISFACTORY. CMM 25-20-01\",\n                    \"reason for removal\": \"null\",\n                    \"order\": \"null\",\n                    \"vendor\": \"STARTECH SOLUTIONS\"\n                }\n            ]\n        },\n        {\n            \"Component\": \"Dynamic Shark Bus Cable\",\n            \"ComponentID\": \"829323-120-82:78YU2\",\n            \"serial no\": \"88310910\",\n            \"history\": [\n                {\n                    \"index\": \"0\",\n                    \"equipment\": \"956057\",\n                    \"flying hours TSI\": \"257.39\",\n                    \"flying cycles TSI\": \"1612\",\n                    \"installed days TSI\": \"852\",\n                    \"flying hours TSN\": \"257.39\",\n                    \"flying cycles TSN\": \"1612\",\n                    \"installed days TSN\": \"852\",\n                    \"flying hours TSO\": \"257.39\",\n                    \"flying cycles TSO\": \"1612\",\n                    \"installed days TSO\": \"852\",\n                    \"install date\": \"24/01/2017\",\n                    \"A/C reg\": \"9V-SWS\",\n                    \"A/C posn\": \"EMA_FCL_1D\",\n                    \"removal date\": \"25/05/2019\",\n                    \"fail/NFF\": \"NDEC\",\n                    \"defect\": \"X-829323-120-82-FOUND SEAT 1D EMA SHOWING '3 RED LIGHTS'\",\n                    \"action taken\": \"PN OFF 829323-120-82 SN OFF A24JAN17-281 PN ON 829323-120-82 SN ON A24JAN17-281\",\n                    \"reason for removal\": \"X-829323-120-82-FOUND SEAT 1D EMA SHOWING '3 RED LIGHTS'\",\n                    \"order\": \"1321463153067\",\n                    \"vendor\": \"SENG HIP ENG INC\"\n                },\n                {\n                    \"index\": \"1\",\n                    \"equipment\": \"961847\",\n                    \"flying hours TSI\": \"48.76\",\n                    \"flying cycles TSI\": \"8\",\n                    \"installed days TSI\": \"5\",\n                    \"flying hours TSN\": \"48.76\",\n                    \"flying cycles TSN\": \"8\",\n                    \"installed days TSN\": \"5\",\n                    \"flying hours TSO\": \"48.76\",\n                    \"flying cycles TSO\": \"8\",\n                    \"installed days TSO\": \"5\",\n                    \"install date\": \"14/06/2019\",\n                    \"A/C reg\": \"9V-SWK\",\n                    \"A/C posn\": \"EMA_JCL_11F\",\n                    \"removal date\": \"19/06/2019\",\n                    \"fail/NFF\": \"NDEC\",\n                    \"defect\": \"X-ELECTRONIC MODULE PN 829323-120-82 SN A10JAN19-247 FAILED INFLATABLE SEAT BELT TEST.\",\n                    \"action taken\": \"null\",\n                    \"reason for removal\": \"X-ELECTRONIC MODULE PN 829323-120-82 SN A10JAN19-247 FAILED INFLATABLE SEAT BELT TEST.\",\n                    \"order\": \"1321520943216\",\n                    \"vendor\": \"SENG HIP ENG INC\"\n                }\n            ]\n        }\n    ]\n}"}],"_postman_id":"da93eede-fd4d-457e-bc01-be8620b68422"},{"name":"FlightLog","id":"8051a58b-2531-49eb-a7e3-c39d5d8ea147","protocolProfileBehavior":{"disableBodyPruning":true},"request":{"method":"GET","header":[],"url":"{{url}}/flightlog","description":"A sample repair log / history of various aircrafts. Entries may correspond to the repair log for the various components.<br> \n(Do note: the values used are not actual values, but fictitious examples of the types of records/inputs captured)"},"response":[{"id":"0f7badfe-5d8e-4d9c-be11-f0d312cf2e58","name":"Get Flight Log By Flight Number 861","originalRequest":{"method":"GET","header":[],"url":{"raw":"{{url}}/flightlog?flightNumber=861","host":["{{url}}"],"path":["flightlog"],"query":[{"key":"flightNumber","value":"861"}]}},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"data\": {\n        \"tail\": \"8U-PK2\",\n        \"flight number\": \"861\",\n        \"history\": [\n            {\n                \"defect type\": \"engine issue\",\n                \"defect text\": \"MAINT ENTRY DUCT ASSY PN: L9871230AZ IPC 36-12-42-01 ITEM 300B CANNIBALIZED TOSERVICE 2Q-QK7.\",\n                \"action\": \"DUCT ASSY P/N: L9871230AZ IPC: 36-12-42 (ITEM 300A) REPLACED LEAK CHECK FOUND SATISFACTORY NIL ECAM AND SYSTEM MONITORING MSGS\",\n                \"date\": \"18/10/2015\",\n                \"from\": \"HGK\",\n                \"to\": \"SIN\",\n                \"check type\": \"line\",\n                \"description\": \"TL2372134-010 @@\",\n                \"defective components\": [\n                    \"19820\",\n                    \"17727\"\n                ],\n                \"priority\": \"low\",\n                \"notification\": \"200025204166\",\n                \"equipment affected\": \"null\",\n                \"completion by date\": \"24/10/2015\"\n            },\n            {\n                \"defect type\": \"engine issue\",\n                \"defect text\": \"WRT TL 2372134 FOUND MISSING CLAMP AT DUCT ASSY PN: L9871230AZ. IPC-12-42-01 ITEM 300B.\",\n                \"action\": \"CLAMPS FOR SAID DUCT ASSY INSTALLED AS PER AMM 36-22-18 C/O OHDS TEST AS PER AMM 36-22-00-710-801-A. TEST PASSED. NIL ECAM MSG\",\n                \"date\": \"22/10/2015\",\n                \"from\": \"HKG\",\n                \"to\": \"SIN\",\n                \"check type\": \"line\",\n                \"description\": \"SJS359948\",\n                \"defective components\": [\n                    \"02293\",\n                    \"01928\"\n                ],\n                \"priority\": \"low\",\n                \"notification\": \"200025251309\",\n                \"equipment affected\": \"null\",\n                \"completion by date\": \"24/10/2015\"\n            }\n        ]\n    }\n}"},{"id":"43e11b20-7326-41cb-9234-c6b6dab43817","name":"Get Flight Log By Flight Number 807","originalRequest":{"method":"GET","header":[],"url":{"raw":"{{url}}/flightlog?flightNumber=807","host":["{{url}}"],"path":["flightlog"],"query":[{"key":"flightNumber","value":"807"}]}},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"data\": {\n        \"tail\": \"6H-KJ9\",\n        \"flight number\": \"807\",\n        \"history\": [\n            {\n                \"defect type\": \"stress defect\",\n                \"defect text\": \"1) WRT RSDA00655KM2168A, OPEN R X FEED A.\",\n                \"action\": \"IAW AMM 36-22-00-760-801-A LWR RIGHT X-FEED A WAS MEASURED, CWR RIGHT XFEED A: 55.1OHM RDG OUT OF LIMITS. IAW AMM 36-22-00-760-802-A. CWR OF INDIVIDUAL ELEMENT 573HF - 0.21OHM, 552HF - 6.78OHM, 551HF - 8.31OHM, ALL READINGS LIMITS. IAW AMM 36-22-00-100-801A. DC4 & CLEANING OF CONNECTORS. DONE & RESTORED. IAW AMM 36-22-00-600-801, WETTING CURRENT DONE & CWR RIGHT XFEED A MEASURED AGAIN. CWR RIGHT XFFED, A - 37.1OH. READINGS W/LIMITS. IAW AMM 36-22-18-000/400-801. VISUAL CHK OF ELEMENTS 573HF, 551AF, 552HF DONE AND NO DAMAGES FOUND. CONNECTORS & BRACKETS RETORQUED & RESTORED (TORQUE AS1511 - 5516IN) IAW AMM 36-22-00-740-801. BITE TEST OF THE OHDS DONE & TEST PASSED.\",\n                \"date\": \"15/01/2016\",\n                \"from\": \"LHR\",\n                \"to\": \"SIN\",\n                \"check type\": \"line\",\n                \"description\": \"SJS368242\",\n                \"defective components\": [\n                    \"10092\",\n                    \"09232\",\n                    \"01823\"\n                ],\n                \"priority\": \"medium\",\n                \"notification\": \"200025407716\",\n                \"equipment affected\": \"null\",\n                \"completion by date\": \"21/01/2016\"\n            }\n        ]\n    }\n}"},{"id":"4cbf6e94-a957-4bf0-b749-711458c76058","name":"Get Flight Log By Flight Number 308","originalRequest":{"method":"GET","header":[],"url":{"raw":"{{url}}/flightlog?flightNumber=308","host":["{{url}}"],"path":["flightlog"],"query":[{"key":"flightNumber","value":"308"}]}},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"data\": {\n        \"tail\": \"3E-TU5\",\n        \"flight number\": \"308\",\n        \"history\": [\n            {\n                \"defect type\": \"engine issue\",\n                \"defect text\": \"AFTER PERFORMING ECAM ACTION. ECAM MSG 'AIR ENG 3 BLEED FAULT'.\",\n                \"action\": \"3611ABCD - PLF MSG VLV HP BLEED ENG 3 NOT CONFIRMED. NIL ACTIVE MSG. REF 2363909 ITEM 1. REF ENG GRD RUN.\",\n                \"date\": \"29/10/2015\",\n                \"from\": \"SIN\",\n                \"to\": \"LHR\",\n                \"check type\": \"line\",\n                \"description\": \"TL2363909-2\",\n                \"defective components\": [\n                    \"22567\",\n                    \"13898\"\n                ],\n                \"priority\": \"low\",\n                \"notification\": \"200025107299\",\n                \"equipment affected\": \"null\",\n                \"completion by date\": \"31/10/2015\"\n            }\n        ]\n    }\n}"},{"id":"b3728f59-a89f-4acb-bcd9-21a400a28dc2","name":"Get All FLight Log","originalRequest":{"method":"GET","header":[],"url":"{{url}}/flightlog"},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"results\": [\n        {\n            \"tail\": \"2Q-QK9\",\n            \"flight number\": \"025\",\n            \"history\": [\n                {\n                    \"defect type\": \"engine issue\",\n                    \"defect text\": \"AIR ENG 2 BLEED FAULT ABNORM BLEED (ON DESCENT) \",\n                    \"action\": \"IN ACC WITH MCC PERFORMED EBAS RESET FOUND OK PLS CHK BLEED SYSTEM AT NEXT FLIGHT AND REPORT AGAIN\",\n                    \"date\": \"12/07/2015\",\n                    \"from\": \"JFK\",\n                    \"to\": \"FRA\",\n                    \"check type\": \"line\",\n                    \"description\": \"TL2349079-1\",\n                    \"defective components\": [\n                        \"10092\",\n                        \"09232\",\n                        \"01823\",\n                        \"92223\",\n                        \"10922\"\n                    ],\n                    \"priority\": \"high\",\n                    \"notification\": \"200024626923\",\n                    \"equipment affected\": \"null\",\n                    \"completion by date\": \"15/07/2015\"\n                },\n                {\n                    \"defect type\": \"engine issue\",\n                    \"defect text\": \"DURING DESCENT ECAM AIR ENG 2 BLEED FAULT\",\n                    \"action\": \"ENG #2 PRECOOLER REPLACED AS PER AMM 36-11-42-000/400-801A. LEAK CHECK CARRIED OUT NIL LEAK OBSERVED. EGR CARRIED OUT NIL FAULT OBSERVED PN:XXYY12345 SN OFF: XXYY-00892 SN ON: XXYY-00182\",\n                    \"date\": \"12/07/2015\",\n                    \"from\": \"FRA\",\n                    \"to\": \"SIN\",\n                    \"check type\": \"line\",\n                    \"description\": \"TL2349080-1 \",\n                    \"defective components\": [\n                        \"22567\",\n                        \"13898\",\n                        \"11370\",\n                        \"03912\",\n                        \"83901\"\n                    ],\n                    \"priority\": \"high\",\n                    \"notification\": \"200024210554\",\n                    \"equipment affected\": \"null\",\n                    \"completion by date\": \"23/07/2015\"\n                },\n                {\n                    \"defect type\": \"engine issue\",\n                    \"defect text\": \"MAINT ENTRY - REFER TO ITEM 01 AIR ENG 2 BLEED FAULT. TO C/OUT REPLACEMENT OF FAN AIR VLV ACTUATOR ENG 2 12HA2\",\n                    \"action\": \"SAID ACTUATOR REPLACED IAW AMM 36-11-57-000-801 BITE TEST OF EBAS C/OUT OK. FUNCTIONAL TEST OF FAV C/OUT OK (L9453, SIN, 13/07/18) PN:AABBCC98765 SN OFF: AABB-00272 SN ON: AABB-00304\",\n                    \"date\": \"12/07/2015\",\n                    \"from\": \"FRA\",\n                    \"to\": \"SIN\",\n                    \"check type\": \"null\",\n                    \"description\": \"TL2349085-016 @@\",\n                    \"defective components\": [\n                        \"04457\",\n                        \"04490\",\n                        \"01289\",\n                        \"80203\",\n                        \"92929\"\n                    ],\n                    \"priority\": \"high\",\n                    \"notification\": \"200024626450\",\n                    \"equipment affected\": \"null\",\n                    \"completion by date\": \"15/07/2015\"\n                },\n                {\n                    \"defect type\": \"engine issue\",\n                    \"defect text\": \"TO PERFORM PRESSURE SENSOR DIRFT FOR ENG #3 & 4\",\n                    \"action\": \"PRESSURE SENSOR DRIFT TEST FOR ENG #3 & 4 C/O. BOTH TEST OK\",\n                    \"date\": \"30/03/2016\",\n                    \"from\": \"FRA\",\n                    \"to\": \"SIN\",\n                    \"check type\": \"line\",\n                    \"description\": \"SJS378105\",\n                    \"defective components\": [\n                        \"08891\",\n                        \"13898\",\n                        \"33124\"\n                    ],\n                    \"priority\": \"medium\",\n                    \"notification\": \"200026102123\",\n                    \"equipment affected\": \"null\",\n                    \"completion by date\": \"01/04/2016\"\n                },\n                {\n                    \"defect type\": \"avionics issue\",\n                    \"defect text\": \"1) TO MEASURE CWR OF ELEMENTS 746HF,747HF. 2) TO CLEAN AND APPLY DC4 TO THE OHDS  CONNECTORS LISTED ABOVE. 3) TO C/O BITE TEST OF THE OHDS. \",\n                    \"action\": \"1) MEASURED AS PER AMM 36-22-00, 746HFl CWR - 8.78OHM, RP: O.L, 747HF: CWR: 6.593OHM, RP: O.L. BOTH WITHIN LIMIT.2) CONNECTORS CLEANED AS PER 36-22-00-100-801. 3) BITE TEST C/O AS PER AMM 36-22-00-710-801. ALL TEST OK.\",\n                    \"date\": \"30/03/2016\",\n                    \"from\": \"JFK\",\n                    \"to\": \"FRA\",\n                    \"check type\": \"line\",\n                    \"description\": \"SJS378107\",\n                    \"defective components\": [\n                        \"92094\",\n                        \"51266\",\n                        \"11370\"\n                    ],\n                    \"priority\": \"medium\",\n                    \"notification\": \"200026095924\",\n                    \"equipment affected\": \"null\",\n                    \"completion by date\": \"01/04/2016\"\n                }\n            ]\n        },\n        {\n            \"tail\": \"7J-KU4\",\n            \"flight number\": \"322\",\n            \"history\": [\n                {\n                    \"defect type\": \"engine issue\",\n                    \"defect text\": \"DURING DESCENT PHASE ECAM AIR ENG 2 BLEED FAULT\",\n                    \"action\": \"ENG #2 PRECOOLER REPLACED AS PER AMM 36-11-42-000/400-801A. LEAK CHECK CARRIED OUT NIL LEAK OBSERVED. EGR CARRIED OUT NIL FAULT OBSERVED PN: XXYY12345 SN OFF: XXYY-00182 SN ON: XXYY-00189\",\n                    \"date\": \"12/09/2015\",\n                    \"from\": \"SIN\",\n                    \"to\": \"LHR\",\n                    \"check type\": \"line\",\n                    \"description\": \"TL2349088-1\",\n                    \"defective components\": [\n                        \"03321\",\n                        \"09122\"\n                    ],\n                    \"priority\": \"low\",\n                    \"notification\": \"200024210554\",\n                    \"equipment affected\": \"null\",\n                    \"completion by date\": \"15/07/2015\"\n                }\n            ]\n        },\n        {\n            \"tail\": \"8U-PK2\",\n            \"flight number\": \"861\",\n            \"history\": [\n                {\n                    \"defect type\": \"engine issue\",\n                    \"defect text\": \"MAINT ENTRY DUCT ASSY PN: L9871230AZ IPC 36-12-42-01 ITEM 300B CANNIBALIZED TOSERVICE 2Q-QK7.\",\n                    \"action\": \"DUCT ASSY P/N: L9871230AZ IPC: 36-12-42 (ITEM 300A) REPLACED LEAK CHECK FOUND SATISFACTORY NIL ECAM AND SYSTEM MONITORING MSGS\",\n                    \"date\": \"18/10/2015\",\n                    \"from\": \"HGK\",\n                    \"to\": \"SIN\",\n                    \"check type\": \"line\",\n                    \"description\": \"TL2372134-010 @@\",\n                    \"defective components\": [\n                        \"19820\",\n                        \"17727\"\n                    ],\n                    \"priority\": \"low\",\n                    \"notification\": \"200025204166\",\n                    \"equipment affected\": \"null\",\n                    \"completion by date\": \"24/10/2015\"\n                },\n                {\n                    \"defect type\": \"engine issue\",\n                    \"defect text\": \"WRT TL 2372134 FOUND MISSING CLAMP AT DUCT ASSY PN: L9871230AZ. IPC-12-42-01 ITEM 300B.\",\n                    \"action\": \"CLAMPS FOR SAID DUCT ASSY INSTALLED AS PER AMM 36-22-18 C/O OHDS TEST AS PER AMM 36-22-00-710-801-A. TEST PASSED. NIL ECAM MSG\",\n                    \"date\": \"22/10/2015\",\n                    \"from\": \"HKG\",\n                    \"to\": \"SIN\",\n                    \"check type\": \"line\",\n                    \"description\": \"SJS359948\",\n                    \"defective components\": [\n                        \"02293\",\n                        \"01928\"\n                    ],\n                    \"priority\": \"low\",\n                    \"notification\": \"200025251309\",\n                    \"equipment affected\": \"null\",\n                    \"completion by date\": \"24/10/2015\"\n                }\n            ]\n        },\n        {\n            \"tail\": \"3E-TU5\",\n            \"flight number\": \"308\",\n            \"history\": [\n                {\n                    \"defect type\": \"engine issue\",\n                    \"defect text\": \"AFTER PERFORMING ECAM ACTION. ECAM MSG 'AIR ENG 3 BLEED FAULT'.\",\n                    \"action\": \"3611ABCD - PLF MSG VLV HP BLEED ENG 3 NOT CONFIRMED. NIL ACTIVE MSG. REF 2363909 ITEM 1. REF ENG GRD RUN.\",\n                    \"date\": \"29/10/2015\",\n                    \"from\": \"SIN\",\n                    \"to\": \"LHR\",\n                    \"check type\": \"line\",\n                    \"description\": \"TL2363909-2\",\n                    \"defective components\": [\n                        \"22567\",\n                        \"13898\"\n                    ],\n                    \"priority\": \"low\",\n                    \"notification\": \"200025107299\",\n                    \"equipment affected\": \"null\",\n                    \"completion by date\": \"31/10/2015\"\n                }\n            ]\n        },\n        {\n            \"tail\": \"8Y-PK1\",\n            \"flight number\": \"321\",\n            \"history\": [\n                {\n                    \"defect type\": \"engine issue\",\n                    \"defect text\": \"DUE TO PFR, SUSPECTED PREDURE SENSOR DRIFT ON ENG 2,3 & 4.\",\n                    \"action\": \"C/O FAULT ISOLATION AS PER TSM 36-11-00-810-99 PRESS SENSOR DRIFT TEST AS EPR AMM 36-11-00-740-803, ALL TEST OK. FAULTS NOT FOUND. \",\n                    \"date\": \"19/11/2015\",\n                    \"from\": \"LHR\",\n                    \"to\": \"SIN\",\n                    \"check type\": \"line\",\n                    \"description\": \"SJS368242\",\n                    \"defective components\": [\n                        \"19820\",\n                        \"17727\",\n                        \"11109\",\n                        \"109292\",\n                        \"94320\"\n                    ],\n                    \"priority\": \"high\",\n                    \"notification\": \"200025407716\",\n                    \"equipment affected\": \"null\",\n                    \"completion by date\": \"19/11/2015\"\n                }\n            ]\n        },\n        {\n            \"tail\": \"6H-KJ9\",\n            \"flight number\": \"807\",\n            \"history\": [\n                {\n                    \"defect type\": \"stress defect\",\n                    \"defect text\": \"1) WRT RSDA00655KM2168A, OPEN R X FEED A.\",\n                    \"action\": \"IAW AMM 36-22-00-760-801-A LWR RIGHT X-FEED A WAS MEASURED, CWR RIGHT XFEED A: 55.1OHM RDG OUT OF LIMITS. IAW AMM 36-22-00-760-802-A. CWR OF INDIVIDUAL ELEMENT 573HF - 0.21OHM, 552HF - 6.78OHM, 551HF - 8.31OHM, ALL READINGS LIMITS. IAW AMM 36-22-00-100-801A. DC4 & CLEANING OF CONNECTORS. DONE & RESTORED. IAW AMM 36-22-00-600-801, WETTING CURRENT DONE & CWR RIGHT XFEED A MEASURED AGAIN. CWR RIGHT XFFED, A - 37.1OH. READINGS W/LIMITS. IAW AMM 36-22-18-000/400-801. VISUAL CHK OF ELEMENTS 573HF, 551AF, 552HF DONE AND NO DAMAGES FOUND. CONNECTORS & BRACKETS RETORQUED & RESTORED (TORQUE AS1511 - 5516IN) IAW AMM 36-22-00-740-801. BITE TEST OF THE OHDS DONE & TEST PASSED.\",\n                    \"date\": \"15/01/2016\",\n                    \"from\": \"LHR\",\n                    \"to\": \"SIN\",\n                    \"check type\": \"line\",\n                    \"description\": \"SJS368242\",\n                    \"defective components\": [\n                        \"10092\",\n                        \"09232\",\n                        \"01823\"\n                    ],\n                    \"priority\": \"medium\",\n                    \"notification\": \"200025407716\",\n                    \"equipment affected\": \"null\",\n                    \"completion by date\": \"21/01/2016\"\n                }\n            ]\n        }\n    ]\n}"},{"id":"dbabfd7e-ddb5-4403-85dd-feaa20db9d4c","name":"Get Flight Log By Flight Number 322","originalRequest":{"method":"GET","header":[],"url":{"raw":"{{url}}/flightlog?flightNumber=322","host":["{{url}}"],"path":["flightlog"],"query":[{"key":"flightNumber","value":"322"}]}},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"data\": {\n        \"tail\": \"7J-KU4\",\n        \"flight number\": \"322\",\n        \"history\": [\n            {\n                \"defect type\": \"engine issue\",\n                \"defect text\": \"DURING DESCENT PHASE ECAM AIR ENG 2 BLEED FAULT\",\n                \"action\": \"ENG #2 PRECOOLER REPLACED AS PER AMM 36-11-42-000/400-801A. LEAK CHECK CARRIED OUT NIL LEAK OBSERVED. EGR CARRIED OUT NIL FAULT OBSERVED PN: XXYY12345 SN OFF: XXYY-00182 SN ON: XXYY-00189\",\n                \"date\": \"12/09/2015\",\n                \"from\": \"SIN\",\n                \"to\": \"LHR\",\n                \"check type\": \"line\",\n                \"description\": \"TL2349088-1\",\n                \"defective components\": [\n                    \"03321\",\n                    \"09122\"\n                ],\n                \"priority\": \"low\",\n                \"notification\": \"200024210554\",\n                \"equipment affected\": \"null\",\n                \"completion by date\": \"15/07/2015\"\n            }\n        ]\n    }\n}"},{"id":"e2ae9483-6774-4cc7-b595-52b49fefdc01","name":"Get Flight Log By Flight Number 321","originalRequest":{"method":"GET","header":[],"url":{"raw":"{{url}}/flightlog?flightNumber=321","host":["{{url}}"],"path":["flightlog"],"query":[{"key":"flightNumber","value":"321"}]}},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"data\": {\n        \"tail\": \"8Y-PK1\",\n        \"flight number\": \"321\",\n        \"history\": [\n            {\n                \"defect type\": \"engine issue\",\n                \"defect text\": \"DUE TO PFR, SUSPECTED PREDURE SENSOR DRIFT ON ENG 2,3 & 4.\",\n                \"action\": \"C/O FAULT ISOLATION AS PER TSM 36-11-00-810-99 PRESS SENSOR DRIFT TEST AS EPR AMM 36-11-00-740-803, ALL TEST OK. FAULTS NOT FOUND. \",\n                \"date\": \"19/11/2015\",\n                \"from\": \"LHR\",\n                \"to\": \"SIN\",\n                \"check type\": \"line\",\n                \"description\": \"SJS368242\",\n                \"defective components\": [\n                    \"19820\",\n                    \"17727\",\n                    \"11109\",\n                    \"109292\",\n                    \"94320\"\n                ],\n                \"priority\": \"high\",\n                \"notification\": \"200025407716\",\n                \"equipment affected\": \"null\",\n                \"completion by date\": \"19/11/2015\"\n            }\n        ]\n    }\n}"},{"id":"e4531080-08c9-49a5-903d-bfbde63150ba","name":"Get Flight Log By Flight Number 025","originalRequest":{"method":"GET","header":[],"url":{"raw":"{{url}}/flightlog?flightNumber=025","host":["{{url}}"],"path":["flightlog"],"query":[{"key":"flightNumber","value":"025"}]}},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"data\": {\n        \"tail\": \"2Q-QK9\",\n        \"flight number\": \"025\",\n        \"history\": [\n            {\n                \"defect type\": \"engine issue\",\n                \"defect text\": \"AIR ENG 2 BLEED FAULT ABNORM BLEED (ON DESCENT) \",\n                \"action\": \"IN ACC WITH MCC PERFORMED EBAS RESET FOUND OK PLS CHK BLEED SYSTEM AT NEXT FLIGHT AND REPORT AGAIN\",\n                \"date\": \"12/07/2015\",\n                \"from\": \"JFK\",\n                \"to\": \"FRA\",\n                \"check type\": \"line\",\n                \"description\": \"TL2349079-1\",\n                \"defective components\": [\n                    \"10092\",\n                    \"09232\",\n                    \"01823\",\n                    \"92223\",\n                    \"10922\"\n                ],\n                \"priority\": \"high\",\n                \"notification\": \"200024626923\",\n                \"equipment affected\": \"null\",\n                \"completion by date\": \"15/07/2015\"\n            },\n            {\n                \"defect type\": \"engine issue\",\n                \"defect text\": \"DURING DESCENT ECAM AIR ENG 2 BLEED FAULT\",\n                \"action\": \"ENG #2 PRECOOLER REPLACED AS PER AMM 36-11-42-000/400-801A. LEAK CHECK CARRIED OUT NIL LEAK OBSERVED. EGR CARRIED OUT NIL FAULT OBSERVED PN:XXYY12345 SN OFF: XXYY-00892 SN ON: XXYY-00182\",\n                \"date\": \"12/07/2015\",\n                \"from\": \"FRA\",\n                \"to\": \"SIN\",\n                \"check type\": \"line\",\n                \"description\": \"TL2349080-1 \",\n                \"defective components\": [\n                    \"22567\",\n                    \"13898\",\n                    \"11370\",\n                    \"03912\",\n                    \"83901\"\n                ],\n                \"priority\": \"high\",\n                \"notification\": \"200024210554\",\n                \"equipment affected\": \"null\",\n                \"completion by date\": \"23/07/2015\"\n            },\n            {\n                \"defect type\": \"engine issue\",\n                \"defect text\": \"MAINT ENTRY - REFER TO ITEM 01 AIR ENG 2 BLEED FAULT. TO C/OUT REPLACEMENT OF FAN AIR VLV ACTUATOR ENG 2 12HA2\",\n                \"action\": \"SAID ACTUATOR REPLACED IAW AMM 36-11-57-000-801 BITE TEST OF EBAS C/OUT OK. FUNCTIONAL TEST OF FAV C/OUT OK (L9453, SIN, 13/07/18) PN:AABBCC98765 SN OFF: AABB-00272 SN ON: AABB-00304\",\n                \"date\": \"12/07/2015\",\n                \"from\": \"FRA\",\n                \"to\": \"SIN\",\n                \"check type\": \"null\",\n                \"description\": \"TL2349085-016 @@\",\n                \"defective components\": [\n                    \"04457\",\n                    \"04490\",\n                    \"01289\",\n                    \"80203\",\n                    \"92929\"\n                ],\n                \"priority\": \"high\",\n                \"notification\": \"200024626450\",\n                \"equipment affected\": \"null\",\n                \"completion by date\": \"15/07/2015\"\n            },\n            {\n                \"defect type\": \"engine issue\",\n                \"defect text\": \"TO PERFORM PRESSURE SENSOR DIRFT FOR ENG #3 & 4\",\n                \"action\": \"PRESSURE SENSOR DRIFT TEST FOR ENG #3 & 4 C/O. BOTH TEST OK\",\n                \"date\": \"30/03/2016\",\n                \"from\": \"FRA\",\n                \"to\": \"SIN\",\n                \"check type\": \"line\",\n                \"description\": \"SJS378105\",\n                \"defective components\": [\n                    \"08891\",\n                    \"13898\",\n                    \"33124\"\n                ],\n                \"priority\": \"medium\",\n                \"notification\": \"200026102123\",\n                \"equipment affected\": \"null\",\n                \"completion by date\": \"01/04/2016\"\n            },\n            {\n                \"defect type\": \"avionics issue\",\n                \"defect text\": \"1) TO MEASURE CWR OF ELEMENTS 746HF,747HF. 2) TO CLEAN AND APPLY DC4 TO THE OHDS  CONNECTORS LISTED ABOVE. 3) TO C/O BITE TEST OF THE OHDS. \",\n                \"action\": \"1) MEASURED AS PER AMM 36-22-00, 746HFl CWR - 8.78OHM, RP: O.L, 747HF: CWR: 6.593OHM, RP: O.L. BOTH WITHIN LIMIT.2) CONNECTORS CLEANED AS PER 36-22-00-100-801. 3) BITE TEST C/O AS PER AMM 36-22-00-710-801. ALL TEST OK.\",\n                \"date\": \"30/03/2016\",\n                \"from\": \"JFK\",\n                \"to\": \"FRA\",\n                \"check type\": \"line\",\n                \"description\": \"SJS378107\",\n                \"defective components\": [\n                    \"92094\",\n                    \"51266\",\n                    \"11370\"\n                ],\n                \"priority\": \"medium\",\n                \"notification\": \"200026095924\",\n                \"equipment affected\": \"null\",\n                \"completion by date\": \"01/04/2016\"\n            }\n        ]\n    }\n}"}],"_postman_id":"8051a58b-2531-49eb-a7e3-c39d5d8ea147"},{"name":"ProductManual","id":"a628ce0d-d513-4bdd-9a51-c2d2d5e94003","protocolProfileBehavior":{"disableBodyPruning":true},"request":{"method":"GET","header":[],"url":"{{url}}/manualproduct","description":"An extraction of the some of the relevant fields from the aircraft maintenance manual and parts catalogue that could be used for identifying specific components and repairs."},"response":[{"id":"01511680-e8f1-4931-b43c-50a054351ef9","name":"Get Manual Product By Id = 10000","originalRequest":{"method":"GET","header":[],"url":{"raw":"{{url}}/manualproduct?id=10000","host":["{{url}}"],"path":["manualproduct"],"query":[{"key":"id","value":"10000"}]}},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"data\": {\n        \"id\": 10000,\n        \"component\": \"WING GEAR SHOCK STRUT DOORS\",\n        \"location\": \"Wing Gear Doors\",\n        \"AMM section\": \"32-12-00\",\n        \"IPC section\": \"45-11-21\",\n        \"subcomponents\": [\n            \"1001,1002,1003\"\n        ],\n        \"component image\": \"https://drive.google.com/drive/folders/16XJbnATQKAOTeoouLfTgczDWvKiYmBIy\",\n        \"AMM pages\": [\n            \"514\",\n            \"508\",\n            \"535\"\n        ],\n        \"IPC pages\": [\n            \"235\",\n            \"220\",\n            \"246\"\n        ],\n        \"test_procedure\": \"Multiple\",\n        \"dimension\": \"400x200x50mm\",\n        \"weight\": \"55kg\"\n    }\n}"},{"id":"0defacb8-44f6-4971-8687-bc6b2daa59a6","name":"Get Manual Product By Id = 20004","originalRequest":{"method":"GET","header":[],"url":{"raw":"{{url}}/manualproduct?id=20004","host":["{{url}}"],"path":["manualproduct"],"query":[{"key":"id","value":"20004"}]}},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"data\": {\n        \"id\": 20004,\n        \"component\": \"SHOCK STRUT INBOARD DOOR\",\n        \"location\": \"Wing Gear Doors\",\n        \"AMM section\": \"32-00-00\",\n        \"IPC section\": \"32-08-01\",\n        \"subcomponents\": [],\n        \"component image\": \"https://drive.google.com/drive/folders/1xhYl6pjkgrz0cyltBjvLPRKCDbNipJdy\",\n        \"test_procedure\": \"General\\nA. This procedure contains two task:\\n(1)  The removal of the inboard door of the shock strut on the wing landing gear.\\n(2)  The installation of the indoor door of the shock strut on the wing landing gear.\",\n        \"AMM pages\": [\n            \"204\"\n        ],\n        \"IPC pages\": [\n            \"155\"\n        ],\n        \"dimension\": \"303x118x44x31mm\",\n        \"weight\": \"13kg\"\n    }\n}"},{"id":"2d7a088a-868a-4b75-a76e-bf440629dfb2","name":"Get Manual Product By Id = 20000","originalRequest":{"method":"GET","header":[],"url":{"raw":"{{url}}/manualproduct?id=20000","host":["{{url}}"],"path":["manualproduct"],"query":[{"key":"id","value":"20000"}]}},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"data\": {\n        \"id\": 20000,\n        \"component\": \"Ground Lock for Air Dispatch\",\n        \"location\": \"Body Gear Doors\",\n        \"AMM section\": \"32-00-00\",\n        \"IPC section\": \"32-08-01\",\n        \"subcomponents\": [\n            \"20001\",\n            \"20002\",\n            \"20003\",\n            \"20004\"\n        ],\n        \"component image\": \"https://drive.google.com/drive/folders/1xhYl6pjkgrz0cyltBjvLPRKCDbNipJdy\",\n        \"AMM pages\": [\n            \"201\",\n            \"202\",\n            \"203\",\n            \"204\"\n        ],\n        \"IPC pages\": [\n            \"145\",\n            \"158\",\n            \"152\",\n            \"155\"\n        ],\n        \"test_procedure\": \"Multiple\",\n        \"dimension\": \"500x200x45x50mm\",\n        \"weight\": \"70kg\"\n    }\n}"},{"id":"4ef4fb09-5df3-4531-8ae2-283cbd7f40a9","name":"Get All Manual Product","originalRequest":{"method":"GET","header":[],"url":"{{url}}/manualproduct"},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"results\": [\n        {\n            \"id\": 10000,\n            \"component\": \"WING GEAR SHOCK STRUT DOORS\",\n            \"location\": \"Wing Gear Doors\",\n            \"AMM section\": \"32-12-00\",\n            \"IPC section\": \"45-11-21\",\n            \"subcomponents\": [\n                \"1001,1002,1003\"\n            ],\n            \"component image\": \"https://drive.google.com/drive/folders/16XJbnATQKAOTeoouLfTgczDWvKiYmBIy\",\n            \"AMM pages\": [\n                \"514\",\n                \"508\",\n                \"535\"\n            ],\n            \"IPC pages\": [\n                \"235\",\n                \"220\",\n                \"246\"\n            ],\n            \"test_procedure\": \"Multiple\",\n            \"dimension\": \"400x200x50mm\",\n            \"weight\": \"55kg\"\n        },\n        {\n            \"id\": 10001,\n            \"component\": \"WING GEAR SHOCK STRUT OUTBOARD DOOR\",\n            \"location\": \"Wing Gear Doors\",\n            \"AMM section\": \"32-12-00\",\n            \"IPC section\": \"45-11-21\",\n            \"subcomponents\": [],\n            \"component image\": \"https://drive.google.com/drive/folders/16XJbnATQKAOTeoouLfTgczDWvKiYmBIy\",\n            \"AMM pages\": [\n                \"514\"\n            ],\n            \"IPC pages\": [\n                \"235\"\n            ],\n            \"test_procedure\": \"General\\nA. This procedure contains two tasks:\\n(1)  The removal of the outboard door of the shock strut on the wing landing gear.\\n(2)  The installation of the outboard door of the shock strut on the wing landing gear.\",\n            \"dimension\": \"312x103x54mm\",\n            \"weight\": \"13kg\"\n        },\n        {\n            \"id\": 10002,\n            \"component\": \"WING GEAR SHOCK STRUT INBOARD DOOR\",\n            \"location\": \"Wing Gear Doors\",\n            \"AMM section\": \"32-12-00\",\n            \"IPC section\": \"45-11-21\",\n            \"subcomponents\": [],\n            \"component image\": \"https://drive.google.com/drive/folders/16XJbnATQKAOTeoouLfTgczDWvKiYmBIy\",\n            \"AMM pages\": [\n                \"508\"\n            ],\n            \"IPC pages\": [\n                \"220\"\n            ],\n            \"test_procedure\": \"General\\nA. This procedure contains a task to examine the linkage rod assemblies and hinge assemblies of the inboard door for worn parts.\\nB. To do this procedure, you must remove the inboard door of the shock strut on the wing landing gear.\",\n            \"dimension\": \"340x102x43 mm\",\n            \"weight\": \"10kg\"\n        },\n        {\n            \"id\": 10003,\n            \"component\": \"WING GEAR SHOCK STRUT DOOR FAIRING\",\n            \"location\": \"Wing Gear Doors\",\n            \"AMM section\": \"32-12-00\",\n            \"IPC section\": \"45-11-21\",\n            \"subcomponents\": [],\n            \"component image\": \"https://drive.google.com/drive/folders/16XJbnATQKAOTeoouLfTgczDWvKiYmBIy\",\n            \"AMM pages\": [\n                \"535\"\n            ],\n            \"IPC pages\": [\n                \"246\"\n            ],\n            \"test_procedure\": \"General\\nA. This procedure has these tasks:/n(1)  The removal of the door fairing of the shock strut for the wing landing gear (referred to as the door fairing)\\n(2)  The installation of the door fairing (recommended procedure)\\n(3)  The installation of the door fairing (alternative procedure)\\nB.  Use the recommended installation procedure when you install a door fairing on a new inboard door\\nC.  Use the alternative installation procedure to replace a door fairing on the door which is on the airplane.\\nD.  After the adjustment and the installation of a door fairing, you set the position of the fairing to the door.  No subsequent adjustment of the fairing is possible.  This is because you drilled the inboard door after the adjustment to align the pilot holes in the door fairing.  The door fairing is then installed to the inboard door.  If you replace the fairing (without the replacement of the inboard door), you must install the new fairing in the same position as the installed fairing.\",\n            \"dimension\": \"320x110x50mm\",\n            \"weight\": \"30kg\"\n        },\n        {\n            \"id\": 20000,\n            \"component\": \"Ground Lock for Air Dispatch\",\n            \"location\": \"Body Gear Doors\",\n            \"AMM section\": \"32-00-00\",\n            \"IPC section\": \"32-08-01\",\n            \"subcomponents\": [\n                \"20001\",\n                \"20002\",\n                \"20003\",\n                \"20004\"\n            ],\n            \"component image\": \"https://drive.google.com/drive/folders/1xhYl6pjkgrz0cyltBjvLPRKCDbNipJdy\",\n            \"AMM pages\": [\n                \"201\",\n                \"202\",\n                \"203\",\n                \"204\"\n            ],\n            \"IPC pages\": [\n                \"145\",\n                \"158\",\n                \"152\",\n                \"155\"\n            ],\n            \"test_procedure\": \"Multiple\",\n            \"dimension\": \"500x200x45x50mm\",\n            \"weight\": \"70kg\"\n        },\n        {\n            \"id\": 20001,\n            \"component\": \"BODY GEAR DOORS\",\n            \"location\": \"Body Gear Doors\",\n            \"AMM section\": \"32-00-00\",\n            \"IPC section\": \"32-08-01\",\n            \"subcomponents\": [],\n            \"component image\": \"https://drive.google.com/drive/folders/1xhYl6pjkgrz0cyltBjvLPRKCDbNipJdy\",\n            \"AMM pages\": [\n                \"201\"\n            ],\n            \"IPC pages\": [\n                \"145\"\n            ],\n            \"test_procedure\": \"1. General\\nA. This procedure has two tasks:\\n(1)  The adjustment of the doors for the body landing gear.\\n(2)  The adjustment of the doors for the body landing gear after the door actuator replacement.\\nB.  When you replace the door for the body landing gear, you must adjust the door.  It is necessary to close the door to check the actuator for the fully locked position or for rig pin installation of the sequence valve. If the actuator cannot be locked fully or the rig pin cannot be put in freely, you must adjust the door.\\nC.  When you close the doors, make sure the landing gear control handle is in the off position.  This will port the hydraulic pressure in the door actuator to return and ensure the door is mechanically locked.\\nD.  You can adjust the forward doors for the body landing gear with the airplane on the ground.  You must lift the airplane clear of the ground to adjust the shock strut door.  If you do not have jacks, you can do a temporary door adjustment with the steps that follow.\\nE.  This task is applicable to the left body landing gear doors and the right body landing gear doors.\",\n            \"dimension\": \"340x102x43x22mm\",\n            \"weight\": \"10kg\"\n        },\n        {\n            \"id\": 20002,\n            \"component\": \"WING GEAR SHOCK STRUT DOOR FAIRING\",\n            \"location\": \"Wing Gear Doors\",\n            \"AMM section\": \"32-00-00\",\n            \"IPC section\": \"32-08-01\",\n            \"subcomponents\": [],\n            \"component image\": \"https://drive.google.com/drive/folders/1xhYl6pjkgrz0cyltBjvLPRKCDbNipJdy\",\n            \"AMM pages\": [\n                \"202\"\n            ],\n            \"IPC pages\": [\n                \"148\"\n            ],\n            \"test_procedure\": \"General\\nA. This procedure has these tasks:\\n(1)  The removal of the door fairing of the shock strut for the wing landing gear (referred to as the door fairing)\\n(2)  The installation of the door fairing (recommended procedure)\\n(3)  The installation of the door fairing (alternative procedure)\\nB.  Use the recommended installation procedure when you install a door fairing on a new inboard door.\\nC.  Use the alternative installation procedure to replace a door fairing on the door which is on the airplane.\\nD.  After the adjustment and the installation of a door fairing, you set the position of the fairing to the door.  No subsequent adjustment of the fairing is possible.  This is because you drilled the inboard door after the adjustment to align the pilot holes in the door fairing.  The door fairing is then installed to the inboard door.  If you replace the fairing (without the replacement of the inboard door), you must install the new fairing in the same position as the installed fairing.\",\n            \"dimension\": \"342x101x52x33mm\",\n            \"weight\": \"30kg\"\n        },\n        {\n            \"id\": 20003,\n            \"component\": \"WING GEAR SHOCK STRUT OUTBOARD DOOR\",\n            \"location\": \"Wing Gear Doors\",\n            \"AMM section\": \"32-00-00\",\n            \"IPC section\": \"32-08-01\",\n            \"subcomponents\": [],\n            \"component image\": \"https://drive.google.com/drive/folders/1xhYl6pjkgrz0cyltBjvLPRKCDbNipJdy\",\n            \"AMM pages\": [\n                \"203\"\n            ],\n            \"IPC pages\": [\n                \"152\"\n            ],\n            \"test_procedure\": \"General\\nA. This procedure contains two task:\\n(1)  The removal of the outboard door of the shock strut on the wing landing gear.\\n(2)  The installation of the outboard door of the shock strut on the wing landing gear.\",\n            \"dimension\": \"303x118x44x31mm\",\n            \"weight\": \"13kg\"\n        },\n        {\n            \"id\": 20004,\n            \"component\": \"SHOCK STRUT INBOARD DOOR\",\n            \"location\": \"Wing Gear Doors\",\n            \"AMM section\": \"32-00-00\",\n            \"IPC section\": \"32-08-01\",\n            \"subcomponents\": [],\n            \"component image\": \"https://drive.google.com/drive/folders/1xhYl6pjkgrz0cyltBjvLPRKCDbNipJdy\",\n            \"test_procedure\": \"General\\nA. This procedure contains two task:\\n(1)  The removal of the inboard door of the shock strut on the wing landing gear.\\n(2)  The installation of the indoor door of the shock strut on the wing landing gear.\",\n            \"AMM pages\": [\n                \"204\"\n            ],\n            \"IPC pages\": [\n                \"155\"\n            ],\n            \"dimension\": \"303x118x44x31mm\",\n            \"weight\": \"13kg\"\n        }\n    ]\n}"},{"id":"6c8b9960-e5c4-49c1-945e-eddc41df9985","name":"Get Manual Product By Id = 10002","originalRequest":{"method":"GET","header":[],"url":{"raw":"{{url}}/manualproduct?id=10002","host":["{{url}}"],"path":["manualproduct"],"query":[{"key":"id","value":"10002"}]}},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"data\": {\n        \"id\": 10002,\n        \"component\": \"WING GEAR SHOCK STRUT INBOARD DOOR\",\n        \"location\": \"Wing Gear Doors\",\n        \"AMM section\": \"32-12-00\",\n        \"IPC section\": \"45-11-21\",\n        \"subcomponents\": [],\n        \"component image\": \"https://drive.google.com/drive/folders/16XJbnATQKAOTeoouLfTgczDWvKiYmBIy\",\n        \"AMM pages\": [\n            \"508\"\n        ],\n        \"IPC pages\": [\n            \"220\"\n        ],\n        \"test_procedure\": \"General\\nA. This procedure contains a task to examine the linkage rod assemblies and hinge assemblies of the inboard door for worn parts.\\nB. To do this procedure, you must remove the inboard door of the shock strut on the wing landing gear.\",\n        \"dimension\": \"340x102x43 mm\",\n        \"weight\": \"10kg\"\n    }\n}"},{"id":"6d953295-d1aa-4eff-9609-24da6399e3a2","name":"Get Manual Product By Id = 10003","originalRequest":{"method":"GET","header":[],"url":{"raw":"{{url}}/manualproduct?id=10003","host":["{{url}}"],"path":["manualproduct"],"query":[{"key":"id","value":"10003"}]}},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"data\": {\n        \"id\": 10003,\n        \"component\": \"WING GEAR SHOCK STRUT DOOR FAIRING\",\n        \"location\": \"Wing Gear Doors\",\n        \"AMM section\": \"32-12-00\",\n        \"IPC section\": \"45-11-21\",\n        \"subcomponents\": [],\n        \"component image\": \"https://drive.google.com/drive/folders/16XJbnATQKAOTeoouLfTgczDWvKiYmBIy\",\n        \"AMM pages\": [\n            \"535\"\n        ],\n        \"IPC pages\": [\n            \"246\"\n        ],\n        \"test_procedure\": \"General\\nA. This procedure has these tasks:/n(1)  The removal of the door fairing of the shock strut for the wing landing gear (referred to as the door fairing)\\n(2)  The installation of the door fairing (recommended procedure)\\n(3)  The installation of the door fairing (alternative procedure)\\nB.  Use the recommended installation procedure when you install a door fairing on a new inboard door\\nC.  Use the alternative installation procedure to replace a door fairing on the door which is on the airplane.\\nD.  After the adjustment and the installation of a door fairing, you set the position of the fairing to the door.  No subsequent adjustment of the fairing is possible.  This is because you drilled the inboard door after the adjustment to align the pilot holes in the door fairing.  The door fairing is then installed to the inboard door.  If you replace the fairing (without the replacement of the inboard door), you must install the new fairing in the same position as the installed fairing.\",\n        \"dimension\": \"320x110x50mm\",\n        \"weight\": \"30kg\"\n    }\n}"},{"id":"a02bd739-c040-4f1a-866e-1c0c29920707","name":"Get Manual Product By Id = 20002","originalRequest":{"method":"GET","header":[],"url":{"raw":"{{url}}/manualproduct?id=20002","host":["{{url}}"],"path":["manualproduct"],"query":[{"key":"id","value":"20002"}]}},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"data\": {\n        \"id\": 20002,\n        \"component\": \"WING GEAR SHOCK STRUT DOOR FAIRING\",\n        \"location\": \"Wing Gear Doors\",\n        \"AMM section\": \"32-00-00\",\n        \"IPC section\": \"32-08-01\",\n        \"subcomponents\": [],\n        \"component image\": \"https://drive.google.com/drive/folders/1xhYl6pjkgrz0cyltBjvLPRKCDbNipJdy\",\n        \"AMM pages\": [\n            \"202\"\n        ],\n        \"IPC pages\": [\n            \"148\"\n        ],\n        \"test_procedure\": \"General\\nA. This procedure has these tasks:\\n(1)  The removal of the door fairing of the shock strut for the wing landing gear (referred to as the door fairing)\\n(2)  The installation of the door fairing (recommended procedure)\\n(3)  The installation of the door fairing (alternative procedure)\\nB.  Use the recommended installation procedure when you install a door fairing on a new inboard door.\\nC.  Use the alternative installation procedure to replace a door fairing on the door which is on the airplane.\\nD.  After the adjustment and the installation of a door fairing, you set the position of the fairing to the door.  No subsequent adjustment of the fairing is possible.  This is because you drilled the inboard door after the adjustment to align the pilot holes in the door fairing.  The door fairing is then installed to the inboard door.  If you replace the fairing (without the replacement of the inboard door), you must install the new fairing in the same position as the installed fairing.\",\n        \"dimension\": \"342x101x52x33mm\",\n        \"weight\": \"30kg\"\n    }\n}"},{"id":"c3115c04-fa61-4a51-b0d5-1e41e4f24588","name":"Get Manual Product By Id = 10001","originalRequest":{"method":"GET","header":[],"url":{"raw":"{{url}}/manualproduct?id=10001","host":["{{url}}"],"path":["manualproduct"],"query":[{"key":"id","value":"10001"}]}},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"data\": {\n        \"id\": 10001,\n        \"component\": \"WING GEAR SHOCK STRUT OUTBOARD DOOR\",\n        \"location\": \"Wing Gear Doors\",\n        \"AMM section\": \"32-12-00\",\n        \"IPC section\": \"45-11-21\",\n        \"subcomponents\": [],\n        \"component image\": \"https://drive.google.com/drive/folders/16XJbnATQKAOTeoouLfTgczDWvKiYmBIy\",\n        \"AMM pages\": [\n            \"514\"\n        ],\n        \"IPC pages\": [\n            \"235\"\n        ],\n        \"test_procedure\": \"General\\nA. This procedure contains two tasks:\\n(1)  The removal of the outboard door of the shock strut on the wing landing gear.\\n(2)  The installation of the outboard door of the shock strut on the wing landing gear.\",\n        \"dimension\": \"312x103x54mm\",\n        \"weight\": \"13kg\"\n    }\n}"},{"id":"d2e352be-8a15-47ad-8134-ab6f08ef729a","name":"Get Manual Product By Id = 20001","originalRequest":{"method":"GET","header":[],"url":{"raw":"{{url}}/manualproduct?id=20001","host":["{{url}}"],"path":["manualproduct"],"query":[{"key":"id","value":"20001"}]}},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"data\": {\n        \"id\": 20001,\n        \"component\": \"BODY GEAR DOORS\",\n        \"location\": \"Body Gear Doors\",\n        \"AMM section\": \"32-00-00\",\n        \"IPC section\": \"32-08-01\",\n        \"subcomponents\": [],\n        \"component image\": \"https://drive.google.com/drive/folders/1xhYl6pjkgrz0cyltBjvLPRKCDbNipJdy\",\n        \"AMM pages\": [\n            \"201\"\n        ],\n        \"IPC pages\": [\n            \"145\"\n        ],\n        \"test_procedure\": \"1. General\\nA. This procedure has two tasks:\\n(1)  The adjustment of the doors for the body landing gear.\\n(2)  The adjustment of the doors for the body landing gear after the door actuator replacement.\\nB.  When you replace the door for the body landing gear, you must adjust the door.  It is necessary to close the door to check the actuator for the fully locked position or for rig pin installation of the sequence valve. If the actuator cannot be locked fully or the rig pin cannot be put in freely, you must adjust the door.\\nC.  When you close the doors, make sure the landing gear control handle is in the off position.  This will port the hydraulic pressure in the door actuator to return and ensure the door is mechanically locked.\\nD.  You can adjust the forward doors for the body landing gear with the airplane on the ground.  You must lift the airplane clear of the ground to adjust the shock strut door.  If you do not have jacks, you can do a temporary door adjustment with the steps that follow.\\nE.  This task is applicable to the left body landing gear doors and the right body landing gear doors.\",\n        \"dimension\": \"340x102x43x22mm\",\n        \"weight\": \"10kg\"\n    }\n}"},{"id":"f1e7bd9d-ec7d-4383-accd-e89805ab809f","name":"Get Manual Product By Id = 20003","originalRequest":{"method":"GET","header":[],"url":{"raw":"{{url}}/manualproduct?id=20003","host":["{{url}}"],"path":["manualproduct"],"query":[{"key":"id","value":"20003"}]}},"_postman_previewlanguage":"json","header":[],"cookie":[],"responseTime":null,"body":"{\n    \"status\": \"SUCCESS\",\n    \"data\": {\n        \"id\": 20003,\n        \"component\": \"WING GEAR SHOCK STRUT OUTBOARD DOOR\",\n        \"location\": \"Wing Gear Doors\",\n        \"AMM section\": \"32-00-00\",\n        \"IPC section\": \"32-08-01\",\n        \"subcomponents\": [],\n        \"component image\": \"https://drive.google.com/drive/folders/1xhYl6pjkgrz0cyltBjvLPRKCDbNipJdy\",\n        \"AMM pages\": [\n            \"203\"\n        ],\n        \"IPC pages\": [\n            \"152\"\n        ],\n        \"test_procedure\": \"General\\nA. This procedure contains two task:\\n(1)  The removal of the outboard door of the shock strut on the wing landing gear.\\n(2)  The installation of the outboard door of the shock strut on the wing landing gear.\",\n        \"dimension\": \"303x118x44x31mm\",\n        \"weight\": \"13kg\"\n    }\n}"}],"_postman_id":"a628ce0d-d513-4bdd-9a51-c2d2d5e94003"}]}