N913JB
Registered owner: JETBLUE AIRWAYS CORP, NY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| JetBlue | Operator | on 2016-07-28 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
38 reports on file, 2014-03-19 – 2026-03-01.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,835 hrs · 13,772 cycles
DURING HEAVY MAINTENANCE: CPCP TASK MULTIPLE AREAS OF CORROSION ON FLOOR BEAM Y1292, FR 66-68 (L4 DOOR); REMOVED AND REPLACED FLOOR BEAM Y1292 FR 66 TO FR 68 (L4 DOOR) IAW A321 SRM 51-42-11 AND SRM 51-72-11 ALL WORK ACCOMPLISHED ON STS WO W004054 NR N0521.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,835 hrs · 13,772 cycles
DURING HEAVY MAINTENANCE: CPCP TASK CABIN FLOOR BEAM Y -512.5 CONOSION DAMAGE ON AT FR67; FLOORBEAM Y-512.5 BETWEEN FR67 AND FR70 REMOVED AND REPLACED IAW A321 SRM 51-11-911-001 ALL WORK ACCOMPLISHED ON STS WO W004054 NR N0907.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,835 hrs · 13,772 cycles
DURING HEAVY MAINTENANCE: CPCP TASK EVIDONCE OT CORROSION ON CENTRAL LINE FLOOR BEAM UPPER SURFACE TROM FR. '16 TO '18; ALL WORK ACCOMPLISHED ON STS WO W004054 NR N00492 REPLACED FLOORBEAM Y254 BTWN FR 12 TO FR 24 IAW A321 SRM 51-42-11 PAR 2E AND 2F.
Part: MOUNT — CORRODED (ZONE 900) · corrosion level 2 · airframe 43,835 hrs · 13,772 cycles
DURING HEAVY MAINTENANCE: CPCP TASK FWD GALLEY MOUNTING POST @FR 14 ON Y-81 FLOOR BEAM CORRODED; REMOVED AND REPLACED FLOOR BEAM Y-81 AT FR 12 TO FR 16 IAW A321 SRTM 51-42-11 AND SRM 53-11-14-10-C ALL WORK ACCOMPLISHED ON STS WO W004054 NR N0496.
Part: BATTERY — FAULTED (ZONE 200) · airframe 43,835 hrs · 13,772 cycles
DURING HEAVY MAINTENANCE, 13WL BATTERY FAULTED. REMOVED AND REPLACED THE BATTERY OF EPSU 13WL IAW AMM 33-51-38-00-002-A/400-002-A. PERFORMED AN OPS CHECK OF EPSU IAW 33-51-00-710-001-A BITE CHECKED OK. PERFORMED INTERFACE & POWER UP TEST OF THE CIDS IAW AMM 23-73-00-740-005-B, TESTED OK. WORK ACCOMPLISHED ON WO W004054 NR N1078.
Part: BATTERY — FAULTED (ZONE 200) · airframe 43,835 hrs · 13,772 cycles
DURING HEAVY MAINTENANCE: 11WL BATTERY FAULTED. REMOVED AND REPLACED THE BATTERY IAW AMM 33-51-38-00-002-A/400-002-A. PERFORMED AN OPS CHECK IAW 33-51-00-710-001-A. CHECKED OK, PERFORMED INTERFACE & POWER UP TEST OF THE CIDS IAW AMM 23-73-00-740-005-B. TESTED OK. WORK ACCOMPLISHED ON WO W004054 NR N1077.
Part: BATTERY — FAULTED (ZONE 200) · airframe 43,835 hrs · 13,772 cycles
DURING HEAVY MAINTENANCE: 15WL BATTERY FAULTED. REMOVED AND REPLACED THE BATTERY IAW AMM 33-51-38-000-002-A/ 400-002-A. PERFORMED AN OPS CHECK IAW AMM 33-51-00-710-001-A. OPS CHECKED OK. PERFORMED CIDS IAW 23-73-00-740-005-B. TESTED OK. WORK ACCOMPLISHED ON WO W004054 NR N1076.
Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 43,835 hrs · 13,772 cycles
DURING HEAVY MAINTENANCE: 10WL POWER SUPPLY FAULTED. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51-38, OPS CHECKED IAW AMM 33-51-00-710-001-A, CIDS INTERFACE AND POWER UP TEST DONE IAW AMM 23-73-00-740-003, BOTH TESTED OK. NO FAULT. WORK ACCOMPLISHED ON WO W004054 NR N1075.
Part: WEB — CORRODED (ZONE 100) · airframe 43,835 hrs · 13,772 cycles
DURING HEAVY MAINTENANCE: AFT CARGO DOOR, AFT ENTRANCE WAY WEB HAD LIGHT SURFACE CORROSION. REMOVED AND REPLACED THE SILL BEAM WEB IAW SRM 51-42-11, AND SRM 51-72-11-911-001.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 43,835 hrs · 13,772 cycles
DURING HEAVY MAINTENANCE: CORRODED FLOOR SUPPORT Y-81, FR 16. REMOVED AND REPLACED THE FLOOR SUPPORT BTWN FR 12 - 16. WORK ACCOMPLISHED ON STS WO W004054 NR N0501.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 43,835 hrs · 13,772 cycles
DURING HEAVY MAINTENANCE: EVIDENCE OF CORROSION ON FLOOR BEAM Y765 UPPER SURFACE @ FR.16; REMOVED AND REPLACED FLOOR BEAM Y765 IAW SRM 51-72-11-911-001 SRM 51-42-11 ALL WORK ACCOMPLISHED ON STS WO W004054 NR N0491.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,835 hrs · 13,772 cycles
DURING HEAVY MAINTENANCE: FLOORBEAM Y765, FRAME 66.6 TO 70' A321 SRI, 53.41-14-16-H (ITEM 410) CORRODED BEYOND LIMITS; (RESOLVED ON W/O: 1402917 TASKCARD: NR-00048) FLOORBEAM Y765 BTW FR 66 AND FR 70 REMOVED AND REPLACED IAW A321 51-72-11-911-001 ALL WORK ACCOMPLISHED ON STS WO W004054 NR N0732.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,835 hrs · 13,772 cycles
DURING HEAVY MAINTENANCE: FLOOR BEAM Y-160.5, FRAME 67 TO 70, A321 SRM 53-41-14-15-H (|TEM 400); REMOVED AND REPLACED FLOOR BEAM Y-160.5 IAW A321 SRM 51-22-11-*901-001 AND EA 160-2025-008 REV IR RDAF# 81712104/002/2025#A JETBLUE EC # A25-1103-01 ALL WORK ACCOMPLISHED ON STS WO W004054 NR N0731.
Part: FILLET — CORRODED (ZONE 400) · airframe 43,835 hrs · 13,772 cycles
DURING HEAVY MAINTENANCE: LT PYLON, PYLON TO WING CENTER FILLETS, INBD STRIP RIB 7A & RIB 10A, CORRODED. EA 160-2025-011 REV IR /2/ AIRBUS RDAF 81708156/003/2025#A /3/ REPAIR INSTRUCTIONS TD/81708156/012/2025#A. DESCRIPTION: DURING CURRENT (01/2026) M1 CHECK ON N913JB (MSN: 05909) @ MLB, STS REPORTED CORROSION DAMAGE ON THE LH PYLON TO WING CENTER FILLET INBD STRIP (PN: D5451804820000)- FABRICATED FROM ASNA3051-8600 AT RIB 7A AND RIB 10A. DAMAGE WAS BLENDED IAW A321 SRM AND WAS EVALUATED IAW SRM 54-53-12 BUT WAS OOL DUE TO NO ADL BEING AVAILABLE. SEE REF /1/ FOR FULL DETAILS. STS REQUESTED PERMANENT REPAIR DISPOSITION FROM AIRBUS WHO PROVIDED REF /3/ TD, WHICH DEFINES A REPAIR CONSISTING OF PERFORMING A CUTOUT, NDT INSPECTION, DOUBLER AND FILLER FABRICATION AND INSTALLATION, AND NEW FASTENER WET INSTALLATION. THIS REPAIR WAS AUTHORIZED BY AIRBUS VIA REF /2/ RDAF. EC A26-030-01 IS ISSUED TO ACCOMPLISH THIS PERMANENT REPAIR PER REF /1/ EA. SUBSTANTIATION: THIS PERMANENT REPAIR IS APPROVED PER REF /2/, RDAF AND IS CLASSIFIED AS MAJOR. (E/C: A26-030-01)
Part: FILLET — CRACKED (ZONE400) · airframe 43,835 hrs · 13,772 cycles
DURING HEAVY MAINTENANCE: PYLONS / LH PYLON / PYLON TO WING CENTER FILLETS / OUTBD STRIP RIB 7A AND RIB 10A / CRACK AND CORROSION â PERMANENT REPAIR; REFERENCES: /1/ STS EA 160-2026-001 REV IR /2/ AIRBUS RDAF 81708168/003/2025#A /3/ REPAIR INSTRUCTIONS TD/81708168/011/2025#A. DESCRIPTION: DURING CURRENT (01/2026) M1 CHECK ON N913JB (MSN: 05909) @ MLB, STS REPORTED ONE (1) CRACK AND SEVEN (7) CORROSION DAMAGES ON THE LH PYLON TO WING CENTER FILLET OUTBD STRIP (PN: D5451804720400 - FABRICATED FROM ASNA3051-8600 [7075-T6 CLAD AL]) AT RIB 7A AND RIB 10A. DAMAGE WAS BLENDED IAW A321 SRM AND WAS EVALUATED IAW SRM 54-53-12 BUT WAS OOL DUE TO NO ADL BEING AVAILABLE. SEE REF /1/ FOR FULL DETAILS. STS REQUESTED PERMANENT REPAIR DISPOSITION FROM AIRBUS WHO PROVIDED REF /3/ TD, WHICH DEFINES A REPAIR CONSISTING OF PERFORMING A CUTOUT, NDT INSPECTION, DOUBLER AND FILLER FABRICATION AND INSTALLATION, AND NEW FASTENER WET INSTALLATION. THIS REPAIR WAS AUTHORIZED BY AIRBUS VIA REF /2/ RDAF. EC A26-028-01 IS ISSUED TO ACCOMPLISH THIS PERMANENT REPAIR PER REF /1/ STS EA. SUBSTANTIATION: THIS PERMANENT REPAIR IS APPROVED PER REF /2/, RDAF AND IS CLASSIFIED AS MAJOR. (E/C: A26-028-01)
Part: BARRIER — FAULTED (ZONE 200) · airframe 43,835 hrs · 13,772 cycles
DURING HEAVY MAINTENANCE: 14WL BATTERY FAULT. R & R 90WL4 EMERGENCY EXIT MARKER IAW AMM 33-51-13 ALSO REMOVED AND REPLACED 14WL EPSU IAW A321 AMM 33-51-38 EPSU OPERATIONAL CHECK DONE IAW A321 AMM 33-54-00-710-001-A 14WL NO FAULT AND WORKED GOOD OPS INTERFACE AND POWER UP TEST IAW A321 AMM 23-73-00-740-005-B DONE TEST OK ALL WORK ACCOMPLISHED ON WO W004054 NR N1079.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,835 hrs · 13,772 cycles
DURING HEAVY MAINTENANCE: CPCP TASK MULTIPLE AREAS OF CORROSION ON FLOOR BEAM .Y765, FR66, FLOORBEAM -Y765 BETWEEN FR 66 AND FR 70 REMOVED AND REPLACED IAW A321 SRM 51-72-11-900-001 ALL WORK ACCOMPLISHED ON STS WO W004054 NR N 0525.
Earlier reports · 2014–2025 · 21 reports
2025
Part: UNKNOWN — ODOR (CABIN) · airframe 43,770 hrs · 13,753 cycles
FLT#904, SJU-JFK. "CABIN CREW ADVISED OF TRANSIENT FUME SMELL ROW 28-30 AFTER TAKEOFF; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A ISOLATED FAULT TO TYPE 10 (CABIN C). INSPECTED APU FOR OIL AND OPERATED PACKS TO REPLICATE ODOR. NO ODODR PER TSM 05-50-00-810-085-B/ TSM 05-50-00-810-085-D. AIRCRAFT IS OK FOR CONT SERVICE"
Part: SLIDE RAFT — UNWANTED DEPLOY (ZONE 800) · airframe 43,263 hrs · 13,610 cycles
FLT#8361, CUN-SJU."L1 SLIDE BLOWN DURING DISARMING; PERFORMED REMOVED AND REPLACED SLIDE RAFT FWD LEFT SIDE AND SECURED AS PER AMM 25-62-44-400-007-A PERFORMED OPS OPEN AND CLOSE ALSO ECAM PAGE DOOR ARM AND DISARMED WORKING NORMAL A/C OKAY FOR RETURN TO SERVICE MCC NOTIFED."
2024
Part: UNKNOWN — ODOR (CABIN) · airframe 40,581 hrs · 12,787 cycles
FLT#1696, SJO-MCO. 'DIRTY SOCK ODOR ON ARRIVAL AT LOW POWER SETTINGS; PERFORMED APU COMPARTMENT INSP NO FOUND INDICATION OIL LEAK. REPLACED RECIRCULATOR FILTER AND PACK BURN OPERATED SYSTEM AND NO FOUND ANY ODOR ON CABIN AND FLIGHT DECK IAW INFO NOTED 2017-T015K A/C OK FOR SVC.'
Part: UNKNOWN — ODOR (CABIN) · airframe 39,448 hrs · 12,457 cycles
FLT#1668, PUJ-JFK. 'DURING DESCENT THROUGH 4000 : SLIGHT ODOR NOTICED IN FLT DECK . ODOR NOTICED LATER IN FWD CABIN. ODOR CLEANED AFTER 5 MINUTES * NOTE * ENG #1 HP BLD OPEN, ENG # 2 HP BLD VALVE CLSD; REF LP 4068219, ITEM 1 (REF INFO NOTICE 2017-T015K. ODOR EVENT IS CONSIDER TO BE A TRANSIENT EVENT. PERFORMED LEVEL B DECON IAW TSM 05-50-00-810-831A. REF SMMS 36-10-00 & 21-00-00. NO ODOR PRESENT.), ODOR EVENT CONSIDERED TRANSIENT EVENT. LEVEL B DECON ACCOMPLISHED. RECIRCULATION FILTERS REPLACED. NO ODOR PRESENT. NO DEFECTS NOTED. A/V OK FOR SVC.'
Part: UNKNOWN — ODOR (CABIN) · airframe 39,445 hrs · 12,456 cycles
FLT#1669, JFK-PUJ. 'ODOR REPORTED BY INFLIGHT CREW. ODOR DESCRIBED AS MILDY THROUGHOUT CABIN DURING TAXI IN. FLIGHT DECK CREW ALSO NOTED ODOR THROUGHOUT CABIN DURING PREFLIGHT ODOR DESCRIBED AS MOLDY & ACRID ( APU SYSTEM ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)
Part: UNKNOWN — ODOR (CABIN) · airframe 39,287 hrs · 12,415 cycles
FLT#1936, STI-JFK. 'DESCENDING THROUGH 6000 FEET STRONG SMELL "DIRTY SOCK" SMELL LASTED FOR ABOUT 5 MIN THAN SLOWLY WENT AWAY. FAH REPORTED THE SMELL AS WELL JUST BELOW 10,000 FEET DING; ACCOMPLISHED DECONTAMINATION OF PACK 1 AND 2 PER TSM TASK 05-50-00-810-831A. NO DEFECTS/ODOR NOTED. RECIR FILTER REPLACED ON L/P 3958772-2 (REPLACED BOTH RECIR FILTERS IAW AMM 21-21-00). APU MEL DEFERRED ON L/P 3958763-1. OK FOR SVC.'
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 36,675 hrs · 11,604 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / AFT FUSELAGE / FR65-66 & STGR23L-26L / DENTS AND GOUGES â TIME LIMITED REPAIR (CONSIDERED A MAJOR REPAIR)
2022
Part: A/C PACK — ODOR · airframe 33,508 hrs · 10,671 cycles
FLT#327, EWR-MCO. 'PASSING 10,000 FOR STRONG ODOR/ FUME. SLIGHTLY DIASPATED AROUND 2000 FT; ACCOMPLISH GVI OF THE APU AIR-INLET PLENUM AND APU AIR INTAKE. ALSO, PERFORM LEVEL A DECONTAMINATION OF THE ECS. COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A, ISOLATED FAULT TO TYPE 10 (A) 1, C PER TSM 05-30-00-810-085-B. AIRCRAFT IS OK FOR SERVICE.'
Part: NONE — NONE · airframe 32,237 hrs · 10,260 cycles
FLT#1405, MCO-SDQ. (AIRCRAFT DECLARED AN EMERGENCY) 'BRAKES ALTN LET RELEASED; RESET BSCU IAW AMM 32-42-00. CLEARED ECAM MSG ALL IS OPERATING NORMALLY. A/C OK FOR SERVICE MCC SAI NOTIFIED.'
2021
Part: WIRE HARNESS — ARCED (LTV UNIT) · airframe 28,507 hrs · 9,061 cycles
FLT 1904, SJU-JFK. SMOKE + ELECT ARC NEAR C ( SEEN BETWEEN 22+23); AFTER INSPECTION PERFORMED PER AMM 5-50-00-810-813-A FOUND LTV BOX/HARNESS ELEC ARC/BURN. NO OTHER DEFECTS NOTED AT THIS TIME. LTV SYS PLACED ON MEL SE LOG PG 3161289 ITEM 1 A/C OKAY TO RTS AT THIS TIME (AFECT ROW 21ABC).
2020
Part: BATTERY — FAILED (CABIN) · airframe 24,699 hrs · 7,834 cycles
FT # 1852, CUN-JFK. WHILE PERFORMING EPSU BATTERY CAPACITY TEST, FOUND EPSU 10WL AND 15WL BATTERIES INOP; R & R 10WL AND 15WL BATTERIES IAW AMM 33-51-38. OPS CHK GOOD.
Part: BATTERY — FAILED (CABIN) · airframe 24,699 hrs · 7,834 cycles
FT # 1852, CUN-JFK. WHILE PERFORMING EPSU BATTERY CAPACITY TEST, FOUND EPSU 10WL AND 15WL BATTERIES INOP; R & R 10WL AND 15WL BATTERIES IAW AMM 33-51-38. OPS CHK GOOD.
2019
Part: DOOR SILL — CORRODED (FRAMES 66-68) · airframe 23,016 hrs · 7,280 cycles
DURING HEAVY MAINTENANCE, FOUND R/H DOOR SILL BTW FR 66-68 CORRODED AT FLOOR ATTACHMENT ANCHOR NUTS, ANGLE REPAIR IS REQUIRED IAW SRM 53-41-14-300-001 PRINCIPLE 5 REV 129; R/H DOOR SILL BTW FR 66-68 AT FLOOR ATTACHMENT ANCHOR NUTS REPAIRED IAW SRM 53-41-14-300-001 PRINCIPLE 5 REV 129 ALL WORK ACCOMPLISHED ON LUFTHANSA NR 5000933006-0010 WO 999902.
Part: DOOR SILL — CORRODED (FRAMES 66-68) · airframe 23,016 hrs · 7,280 cycles
DURING HEAVY MAINTENANCE, FOUND LH DOOR SILL BTW FR 66-68 CORRODED AT FLOOR ATTACHMENT ANCHOR NUTS.ANGLE REPAIR IS REQUIRED IAW SRM 53-41-14-300-001 PRINCIPLE 5 REV. 129; LH DOOR SILL BTW FR 66-68 AT FLOOR ATTACHMENT ANCHOR NUTS REPAIRED IAW SRM 53-41-14-300-001 PRINCIPLE 5 REV 129 ALL WORK ACCOMPLISHED ON WO/999902 LUFTHANSA NR50000936572-0010. THIS REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — DENTED (FRAMES 14-16) · airframe 23,016 hrs · 7,280 cycles
DURING HEAVY MAINTENANCE, WHILE PERFORMING EVALUATION TO CONVERT TO PERMANENT A TEMPORARY REPAIR IAW REF/2/ RDAS ADDITIONAL DAMAGES WERE FOUND IN THE SURROUNDING AREA TO THE DENT. DENTS AND GOUGES WERE FOUND BETWEEN FR 14-16 & STGR 36RH OF THE FWD AVIONICS BAY CUTOUT. SEE REF/1/ LHT EO FOR MORE DETAILS. AIRBUS WAS CONTACTED FOR ASSESSMENT AND PROVIDED REPAIR INSTRUCTIONS VIA REF/4/ TD CONSISTING OF A CUTOUT REPAIR WITH DOUBLER INSTALLATION. FOR GOUGE DAMAGE #A, #C, #D, #E A SMOOTH REWORK HAS BEEN PERFORMED IN ORDER TO REMOVE THE GOUGE DAMAGE COMPLETELY & NDT INSPECTION HAS BEEN PERFORMED WITH NIL FINDINGS. FOR DAMAGE #B, CUT-OUT HAS BEEN PERFORMED IN ORDER TO REMOVE THE DAMAGE COMPLETELY. SEE REF/3/ RDAS FOR MORE DETAILS. LHT ISSUED THE REF/1/ EO DOCUMENTING THIS REPAIR AS PER THE REF/3/ RDAS. THIS REPAIR REQUIRES A POST REPAIR INSPECTION AT 53300FC, WHERE THE METHOD OF INSPECTION & INTERVAL ARE TBD PER THE REF/3/ RDAS. EC A19-924-01 IS ISSUED TO TRACK THIS REPAIR PER THE REF/1/ LHT EO & THE REF/3/ RDAS WITHOUT DEVIATION. EC A19-924-02 IS ISSUED TO TRACK THE POST REPAIR INSPECTIONS PER THE REF/3/ RDAS WHERE IT IS DUE AT 53300FC FROM REPAIR EMBODIMENT (EMBODIED AT 7280FC / 23016FH ON 11/14/2019). THE METHOD OF INSPECTION AND INTERVAL ARE TBD; THIS REPAIR HAS BEEN APPROVED BY THE REF/3/ AIRBUS RDAS. THIS REPAIR IS CLASSIFIED AS CATEGORY B AND âMAJORâ.
2018
Part: UNKNOWN — ODOR (CABIN) · airframe 17,903 hrs · 5,648 cycles
CRUISING AT FL330, AT APPROXIMATELY ONE HOUR AND 40 MINS FLT TIME, INFORMED BY FLT ATT OF A STRONG ODOR OF ELECTRICAL BETWEEN 10 AND 11. DEACTIVATED THE RACK POWER TO ISOLATE ENTERTAINMENT SYSTEM . AFTER 5 MINS THE ODOR WAS GONE. RE-ACTIVATED LTV SYS. PERFORMED TASK 44-20-00-210-802, AT ROWS 10-13 LEFT AND RIGHT SIDE. SYS LEFT ON FOR ADDITIONAL 30 MIN, NO ODOR NOTED, ALL OPS OK.
2017
Part: UNKNOWN — ODOR (GALLEY) · airframe 11,577 hrs · 3,581 cycles
DURING DESCENT, AFT GALLEY SMELLED OF BURNING WIRE. LASTED 5 MINUTES. NO VISIBLE SMOKE. PERFORMED INSPECTION IAW TSM TASK 24-00-00-810-823A. NO BURNING ODOR NOTED AND NO POSITIVE ID OF THE SOURCE OF ODOR. DUE TO SUSPECT ELECTRICAL BURNING ODOR IN CABIN, LTV SYSTEM WAS DEACTIVATED. PERFORMED CABIN AIR QUALITY, ODOR INSPECTION IAW LTV AMM 521 44-20-00-210-802. NO FAULTS FOUND. OPS CHECK PERFORMED. ALL OPS CHECK FOUND TO BE NORMAL.
2016
Part: CONNECTOR — OUT OF POSITION (EMERGENCY LIGHT) · airframe 11,113 hrs · 3,408 cycles
REJECTED TAKEOFF. L1 EMERGENCY EXIT LIGHT INOPERATIVE; FOUND ALL EMERGENCY LIGHTS CHECK NORMAL FROM COCKPIT AND FAP. FOUND WHEN CREW ARMED EMERGENCY LIGHT SWITCH. L1 DOOR RED EMERGENCY LIGHT OFF. CABIN WHITE LIGHT ON. SHOULD BE OPPOSITE IAW AWD 33-51-03. FOUND HARNESS ASSY SWAPPED FROM DISC PLUG 2761VC. CORRECTED. PERFORMED OPS CHECK. OPS CHECK PASSED PER AMM 33-51-01.
2014
Part: COFFEEMAKER — FAILED (GALLEY) · airframe 3,205 hrs · 919 cycles
F/A REPORTED BURNING PLASTIC ODOR IN FWD GALLEY WHEN COFFEE POTS TURNED ON. ALSO PANEL ABOVE COFFEE POTS FELT EXTREMELY HOT. TURNED COFFEE POTS OFF & ODOR WENT AWAY. ACCOMPLISHED INSP OF ACFT IAW TSM 05-50-00-810-831, FOUND FWD COFFEE MAKER 105 INOPERATIVE. R & R NR 105 COFFEEMAKER IAW AMM 25-35-15. OPS CHECK NORMAL.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 733 hrs · 201 cycles
FLIGHT CREW REPORTED THAT THREE FORWARD EXIT EMERGENCY SIGNS INOPERATIVE. CABIN EMERGENCY LIGHTING TEST CARRIED OUT IAW 33-51-00 AND THAT EMERGENCY SIGNS FUNCTIONED NORMALLY.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 729 hrs · 200 cycles
EMERGENCY LIGHTS ILLUMINATED IN FLIGHT AND WOULD NOT EXTINGUISH. DURING TROUBLESHOOTING THE FAULT WAS NOT PRESENT. FOLLOWED TSM 33-51-00-810-881-A, NO FAULTS NOTED. EMERGENCY LIGHTING CHECKED NORMAL. ACFT OK FOR SERVICE.