N337JB
Registered owner: WILMINGTON TRUST CO TRUSTEE, DE (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| JETBLUE AIRWAYS CORPORATION (YENA) | Operator | on 2023-02-24 | Operator named in NTSB report |
Accident & incident history
Operated by JETBLUE AIRWAYS CORP (per NTSB report)
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.
35 reports on file, 2012-02-07 – 2023-09-29.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 30,748 hrs · 20,935 cycles
FLT#105, JFK-ORD. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) ' DURING CLIMB AND CRUISE #1 ENG LP VIBES REACHED 4.0 AT N1 OF 90.5% VIBES REDUCED WHEN THRUST REDUCED. VIBES FELT IN CABIN; PERFORMED FAN TRIM BALANCE IEVM IAW AMM GE LMM 72-21-00-800-802. PERFORMED POWER RUN, HIGHEST NOTED VIB INDICATION WAS .7 AT 91.6 N1. A/C OK FOR CONT SVC.'
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 30,575 hrs · 20,790 cycles
FLT#1026, BWI-BOS. 'MAIN CABIN ( L1 ) DOOR WILL NOT ARM THE ARMING LEVER WILL NOT ARM; FOUND THE L1 GRIT BAR LOOSE. SECURED GRIT BAR BACK TO POSITION. A/C OK FOR FURTHER SVC. OPS CHECK GOOD PER AMM 52-11-00.'
Earlier reports · 2012–2022 · 33 reports
2022
Part: SEAT TRACK — CORRODED (FRAME 84) · airframe 28,661 hrs · 19,353 cycles
DURING HEAVY MAINTENANCE, CORROSION FOUND ON SEAT TRACK, FRAME 84 AND Y=300 RT. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-12-01, 51-10-03, AND SRM 53-23-10/AD54. REPAIRED IAW SRM 53-23-10/R54. MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 28,661 hrs · 19,353 cycles
DURING HEAVY MAINTENACE, FWD FUSELAGE FLOOR STRUCTURE, RT SEAT TRACK CORRODED. COMPLIED WITH A PERMANENT REPAIR. MAJOR REPAIR.
Part: FLOOR SUPPORT — CORRODED (FRMS 12-15) · corrosion level 2 · airframe 28,661 hrs · 19,353 cycles
DURING HEAVY MAINTENANCE, CORRODED FLOOR SUPPORT REPAIR DOUBLER BTW FR 12 - 15, Y280 RT. REPLACED THE FLOOR SUPPORT DOUBLER IAW ETD 2015-190-027057 AND ETI-190-22-704 REV. ORIGINAL. MAJOR REPAIR.
Part: SHEAR TIE — CORRODED (FRM 88 S28R) · airframe 28,661 hrs · 19,353 cycles
DURING HEAVY MAINTENANCE, CORROSION FOUND ON SHEAR TIE, FRAME 88, S28R. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-12-01, SRM 51-10-03, AND SRM 51-75-16. REPLACED THE SHEAR TIE IAW SRM 51-41-02, AND SRM 51-41-01. MAJOR REPAIR.
Part: SKIN — CORRODED (FRM 88 S27R) · airframe 28,661 hrs · 19,353 cycles
DURING HEAVY MAINTENANCE, CORROSION FOUND ON WASTE ACCESS CUT OUT. CORROSION REMOVED IAW SRM 51-12-03, SRM 51-10-03, FOUND OUT OF LIMITS IAW SRM 53-23-60/AD51. REPAIRED IAW SRM 53-23-60, REP 51. MAJOR REPAIR.
Part: FLOORBEAM — CORRODED (FRAME 87) · airframe 28,661 hrs · 19,353 cycles
DURING HEAVY MAINTENANCE, CORROSION FOUND FLOORBEAM FRAME 87, Y=260 LH. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-12-01, SRM 51-10-03, AND SRM 53-23-10/AD52. REPAIRED IAW SRM 53-23-10/R53. MAJOR REPAIR.
Part: SHEAR TIE — CORRODED (FRM 87 S27-28R) · airframe 28,661 hrs · 19,353 cycles
DURING HEAVY MAINTENANCE, . AFTER FASTENER REMOVAL, CORROSION FOUND ON THE SHEAR TIE, FRAME 87, STRINGERS 27-28R. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-12-01, 51-10-03, AND SRM 51-75-16, FABRICATED AND REPLACED IAW DWG 170-66041-001, REV A, SRM SRM 51-41-02, AND SRM 51-41-01.
Part: FLOOR SUPPORT — CORRODED (FRMS 12-16) · airframe 28,661 hrs · 19,353 cycles
DURING HEAVY MAINTENANCE, CORROSION FOUND ON FLOOR SUPPORT BTW FRAMES 12- 16. Y= 280. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-12-01, SRM 51-1003, AND SRM 53-10-10 AD/51. REPAIRED IAW SRM 53-10-10 R51. MAJOR REPAIR.
Part: SHEAR TIE — CORRODED (FRM 85 S28L) · airframe 28,661 hrs · 19,353 cycles
DURING HEAVY MAINTENANCE, CORROSION FOUND ON SHEAR TIE, FRAME 85, S28L. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-12-01, SRM 51-10-03, AND SRM 51-75-16. REPLACED THE SHEAR TIE IAW SRM 51-41- 01 AND SRM 51-41-02. MAJOR REPAIR.
Part: SHEAR TIE — CORRODED (FRM 82 S25L) · airframe 28,661 hrs · 19,353 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS FOUND ON THE SHEAR TIE, FRAME 82, S25L. THE CORROSION WAS REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-12- 01, SRM 51-10-03 AND SRM 51-75-16. REPLACED THE SHEAR TIE IAW SRM 51-41-02, AND SRM 51-41-01. MAJOR REPAIR.
Part: SHEAR TIE — CORRODED (FRM 89 S20-21L) · airframe 28,661 hrs · 19,353 cycles
DURING HEAVY MAINTENANCE, CORROSION FOUND ON THE SHEAR TIE, FRAME 89, STRINGERS 20-21L AFTER WATER TANK REMOVAL. CORROSION REMOVED IAW SRM 51-12-01, SRM 51-10-03, FOUND OUT OF LIMITS IAW SRM 51-75-16, REPLACED THE SHEAR TIE IAW SRM 51-41-01, AND SRM 51-41-02.
Part: SHEAR TIE — CORRODED (FRM 82 S22-23L) · airframe 28,661 hrs · 19,353 cycles
DURING HEAVY MAINTENANCE, CORROSION FOUND ON SHEAR TIE, FRAME 82, STRINGERS 22-23L. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-12-01, SRM 51-10-03, AND SRM 51-75-16. REPLACED IAW SRM 51-41-02, AND SRM 51-41-0.
Part: PRESSURE SWITCH — WARNING LIGHT · airframe 27,923 hrs · 18,747 cycles
FLT#1019, JFK-DTW. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) ' BLEED 1 OVERPRESSURE ON TAKEOFF - WOULD NOT RESET PER QRH; T/S PER FIM 36-14-00-810-817-A. REMOVED AND REPLACED BLEED OVER PRESSURE SWITCH IAW AMM 36-14-01. OPS CHECK GOOD WITH ENGINE AT IDLE. A/C OKAY FOR CONTINED SERVICE.'
2020
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 24,822 hrs · 16,760 cycles
FLT 685, ROC-JFK. COCKPIT CEILING EMERGENCY LIGHT NOT ILLUMINATING. R & R ELPU AT L1 PASSENGER DOOR, IAW AMM 33-50-01. OPERATIONS CHECK GOOD. A/C OK FOR SERVICE.
2019
Part: SKIN — CRACKED (RT WING) · airframe 23,175 hrs · 15,594 cycles
DURING HEAVY MAINTENANCE, CRACK TRAILING EDGE BETWEEN RIB 9 - RIB 10 RT WING (1 EA); ACCOMPLISHED REPAIR OF THE CRACK DAMAGE ON THE RT WING REAR LOWER SKIN AT THE AFT REAR SPAR BETWEEN RIB 9-11 IAW EA 57-0370-19 REV 0 AND EC E19-639-01, ETD2019-190-107926 REV C REF NR: 2019-255002.
Part: LIFE RAFT — UNSECURE (CABIN) · airframe 21,790 hrs · 14,612 cycles
FLT 1853, JAX-FLL. FORWARDED LIFE RAFT IS OPEN AND NOT SECURED. INSTALLED NEW FWD LIFE RAFT PER AMM 25-66-01.
2017
Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 18,295 hrs · 12,072 cycles
FT # 2080, FLL-DCA. ALL 6 EMERGENCY LIGHT POWER UNITS FAILED TO STAY ON MORE THAN 15 MINUTES PER FUNCTIONAL TEST STEP 8 OF TASK CARD E190-33-50-01-720-801-M. R & R EMERGENCY-LIGHT POWER UNIT 1 & 2 IAW AMM 33-50-01. OPS CHECK NORMAL. R & R EMERGENCY-LIGHT POWER UNITS 3 & 4 IAW AMM 33-50-01. OPS CHECK NORMAL. R & R EMERGENCY-LIGHT POWER UNIT # 5 & 6 IAW AMM 33-50-01. OPS CHECK NORMAL.
Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 18,295 hrs · 12,072 cycles
FT # 2080, FLL-DCA. ALL 6 EMERGENCY LIGHT POWER UNITS FAILED TO STAY ON MORE THAN 15 MINUTES PER FUNCTIONAL TEST STEP 8 OF TASK CARD E190-33-50-01-720-801-M. R & R EMERGENCY-LIGHT POWER UNIT 1 & 2 IAW AMM 33-50-01. OPS CHECK NORMAL. R & R EMERGENCY-LIGHT POWER UNITS 3 & 4 IAW AMM 33-50-01. OPS CHECK NORMAL. R & R EMERGENCY-LIGHT POWER UNIT # 5 & 6 IAW AMM 33-50-01. OPS CHECK NORMAL.
Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 18,295 hrs · 12,072 cycles
FT # 2080, FLL-DCA. ALL 6 EMERGENCY LIGHT POWER UNITS FAILED TO STAY ON MORE THAN 15 MINUTES PER FUNCTIONAL TEST STEP 8 OF TASK CARD E190-33-50-01-720-801-M. R & R EMERGENCY-LIGHT POWER UNIT 1 & 2 IAW AMM 33-50-01. OPS CHECK NORMAL. R & R EMERGENCY-LIGHT POWER UNITS 3 & 4 IAW AMM 33-50-01. OPS CHECK NORMAL. R & R EMERGENCY-LIGHT POWER UNIT # 5 & 6 IAW AMM 33-50-01. OPS CHECK NORMAL.
Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 18,295 hrs · 12,072 cycles
FT # 2080, FLL-DCA. ALL 6 EMERGENCY LIGHT POWER UNITS FAILED TO STAY ON MORE THAN 15 MINUTES PER FUNCTIONAL TEST STEP 8 OF TASK CARD E190-33-50-01-720-801-M. R & R EMERGENCY-LIGHT POWER UNIT 1 & 2 IAW AMM 33-50-01. OPS CHECK NORMAL. R & R EMERGENCY-LIGHT POWER UNITS 3 & 4 IAW AMM 33-50-01. OPS CHECK NORMAL. R & R EMERGENCY-LIGHT POWER UNIT # 5 & 6 IAW AMM 33-50-01. OPS CHECK NORMAL.
Part: BEAM — CORRODED (FRAMES 24-25) · corrosion level 2 · airframe 17,122 hrs · 11,205 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CARGO DOOR CUT OUT LOWER THRESHOLD BEAM BETWEEN FRAMES 24 AND 27, RBL 15. REMOVED AND REPLACED THE LOWER THRESHOLD BEAM IAW SRM 51-43-03, AND 51-43-04, REV 35.
Part: FINGER DOUBLER — CORRODED (FRAMES 24-25) · corrosion level 2 · airframe 17,122 hrs · 11,205 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CARGO CUT OUT FWD FINGER DOUBLER BETWEEN FRAMES 24 AND 25, RBL 8 - 15. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-41-02, AND 51-43-04.
Part: FINGER DOUBLER — CORRODED (FRAMES 77-78) · corrosion level 2 · airframe 17,122 hrs · 11,205 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CARGO DOOR CUT OUT FWD FINGER DOUBLER BETWEEN FRAMES 77 AND 78, RBL 12 - 14. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-42-02, AND SRM 51-43-04.
Part: BEAM — CORRODED (FRAME 87) · corrosion level 2 · airframe 17,122 hrs · 11,205 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON PASSENGER CABIN LONGITUDINAL BEAM, FRAME 87 AND RBL 11. REMOVED AND REPLACED THE LONGITUDINAL BEAM IAW SRM 51-41-01 ,51-42-02, AND 51-43-03.
Part: FINGER DOUBLER — CORRODED (FRAMES 26-27) · corrosion level 2 · airframe 17,122 hrs · 11,205 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CARGO DOOR CUT OUT AFT FINGER DOUBLER BETWEEN FRAMES 26 AND 27 AND, RBL 11 - 15. REMOVED AND REPLACED FINGER DOUBLER IAW SRM 51-41-02 AND 51-43-04.
2015
Part: MODULE — FAILED · airframe 10,589 hrs · 6,762 cycles
ON SHORT FINAL APPROACH, NOTICED A FLICKER OF THE FIRE INDICATION ON NR 1 ITT GAUGE, NO EICAS MESSAGE LIGHTS OR WARNING BELLS. FLICKER REOCCURED AT ENGINE IDLE/LOW POWER ABOUT ONCE EVEERY 20 SECONDS. THE EICAS ENGINE 1 FIRE LATCHED ENGINE WITH ASSOCIATED WARNING BELL, BUT NO LIGHT IN THE "T" HANDLE. WARNING BELL QUIT AFTER 2 SECONDS. NO OTHER VISUAL INDICATIONS FROM ENGINE. NO INFLIGHT SHUTDOWN OCCURRED AND SHUTDOWN WAS NORMAL, NO QRH PROCEDURE. AFTER SHUTDOWN REVIEWED CMC CURRENT LEGS MAINTENANCE MESSAGES WITH MECHANIC SHOWED ENGINE 1 FIRE (2) WITH NO CORRELATIONS FAULT NAME OR OTHER TYPE OF CODE, NO LRU AT FAULT. 30 MINUTES LATER WITH ENGINES STILL OFF, RECHECKED PAGE AND SHOWED ENGINE 1 FIRE (3) AND ENGINE 2 FIRES (1). STILL NO CORRELATION OR CODES RELATED TO EITHER ENGINE. PERFORMED DETAILED VISUAL INSPECTION OF ENGINE 1 FIRE LOOPS FOR INTEGRITY AND DEFECTS IAW AMM 26-11-00 NO DESCREPANCIES IAW FIM 26-11-00-810-807-A. NO CORRELATED FAULTS FOUND. R & R GENERIC I/O MODULE IAW AMM 31-41-06.
Part: FLOORBEAM — CORRODED (FRAME 17) · airframe 10,445 hrs · 6,665 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS FOUND AT THE FORWARD CABIN FR 17 CROSSBEAM CENTER LINE AND 3 RBL HAS BARE PAINT. REMOVED CORROSION ON CROSSBEAM IAW SRM PART II 51-12-01 AND BLENDED PROCEDURES APPLIED. ACCOMPLISHED A DYE PENETRANT TYPE 1 INSPECTION. MANUFACTURED SEVERAL REPAIR REINFORCEMENTS, DRILLED AND SHIMED THE AREAS. APPLIED CHEMICAL CONVERSION COMPOUND AND HIGH SOLID EPOXY PRIMER. FILLED THE REWORKED AREAS. INSTALLED THE REPAIRED PARTS AND APPLIED FILLET SEAL IAW SRM PART II 51-21-02. RESTORED TO THE ORIGINAL FINISH IAW E15-300-01.
Part: BEAM — CORRODED (SERVICE DOOR) · corrosion level 1 · airframe 10,445 hrs · 6,665 cycles
DURING HEAVY MAINTENANCE, AFT SERVICE DOOR HAS A GOUGE/CORROSION ON THE INTERNAL SIDE AT BEAM NR 4. ACCOMPLISHED DETAIL VISUAL INSPECTION OF THE IMMEDIATE AREA IAW NDT INTRODUCTION PARA 5.B TO ENSURE DAMAGE IS AS REPORTED AND NO CRACKS EXIST. BLEND AND REWORKED NOTED DAMAGE IAW SRM 51-10-03 REMOVING THE MINIMUM MATERIAL REQUIRED. PERFORMED HFEC INSPECTION TO ENSURE NO CRACKS EXIST AND THE STRUCTURE IS DAMAGE FREE.APPLIED CHEMICAL CONVERSION COMPOUND AND EPOXY TO THE AREA. APPLIED TOPCOAT TO THE REWORKED AREA. RESTORE ALL TO NORMAL CONFIGURATION.
Part: BEAM — CORRODED (CARGO BAY) · corrosion level 1 · airframe 10,445 hrs · 6,665 cycles
DURING HEAVY MAINTENANCE, FOUND FORWARD CARGO BEAM WITH CORROSION. PERFORMED A DETAILED VISUAL INSPECTION OF THE AREA. BLEND AND REWORK IAW SRM 51-10-03. PERFORMED HFEC INSPECTION ALONG ON ALL THE EFFECTED AREAS IAW NDT PART 1 51-00-00-916-803. APPLIED SURFACE PROTECTION TO THE REWORKED AREA IAW SRM 51-23-04. RESTORE TO NORMAL CONFIGURATION.
Part: FLOOR SUPPORT — CORRODED (FRAMES 12-13) · airframe 10,445 hrs · 6,665 cycles
DURING HEAVY MAINTENANCE, CORROSION FOUND AT THE FORWARD RT SIDE SILL RBL 37 BETWEEN FR 12-13. BLENDED OUT CORROSION AND APPLIED ALODINE TO THE REWORKED AREA, AND EPOXY PRIMER IAW SRM PART II 51-23-05. ACCOMPLISHED HFEC INSPECTION AT THE BLEND OUT AREA IAW E190 NDT PART 1 51-00-00-916-803 TO ENSURE NO CRACKS EXIST. RESTORE TO THE ORIGINAL FINISH IAW SRM PART II 51-23-06 AND E15-284-01. THIS IS LEVEL 1 CORROSION.
2013
Part: CIRCUIT CARD — FAILED (NR 2 MAU) · airframe 4,597 hrs · 2,897 cycles
FLT 590 PBI-HPN, CREW DECLARED AN EMERGENCY AND AIRCRAFT DIVERTED TO JFK. AT CRUISE ALT, 45 MINUTES IN TO FLIGHT AVNX MAU2A FAIL AND ASSOCIATED MSGS APPEARED ON EICAS. RAN QRH 45 MINUTES LATER IT DISAPPEARED. REMOVED AND REPLACED MAU2 NIC/PROC NR 1 CARD PER AMM 31-41-04.
2012
Part: SERVO — MALFUNCTIONED (AUTOPILOT SYS) · airframe 2,144 hrs · 1,374 cycles
FLT 1229 BOS-RDU, AT FLIGHT 280 A/P BEGAN UNCOMMANDED ROLL TO RIGHT DISCONNECTED AUTOPILOT. MANUALLY FLEW AIRCRAFT TO TOUCHDOWN. REMOVED AND REPLACED AUTO PILOT AILERON SERVO IAW AMM 22-11-04. CHECK OK. NOTE: THIS AIRCRAFT HAD THE SAME ITEM REPORTED ON 6/5/12, FIM WAS ACCOMPLISHED AND WAS CONSIDERED A TRANSITORY CONDITION.
Part: PRESSURE SWITCH — FAILED (NR 2 ENGINE) · airframe 1,109 hrs · 694 cycles
FLT 1211 BOS-BUF, AIR TURNBACK, CREW DECLARED EMERGENCY DUE TO ON CLIMBOUT THROUGH FL 270 ENG 2 FUEL LO PRESS AND ENGINE 2 FUEL FEED FAULT COME ON. CREW FOLLOWED QRH PROCEDURES. TROUBLESHOOTING PER FIM 73-31-00-810-804A FOUND NR 2 ENGINE LOW PRESSURE SWITCH FAULTED. REMOVED AND REPLACED FUEL LOW PRESSURE SWITCH PER AMM 73-31-01. LEAK AND OPS CHECK NORMAL DURING HIGH POWER RUN UP.