N980JT
Registered owner: JETBLUE AIRWAYS CORP, NY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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.
8 reports on file, 2021-04-12 – 2023-11-20.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 26,699 hrs · 5,239 cycles
FLT#577, FLL-SFO. (AIRCRAFT DIVERTED TO AUS) ' ENG 2 OIL LEVEL DECREASED FROM 11QTS TO AT CRUISE TO AS LOW AS 2.5 QTS ON FINAL TO DIVERT CITY.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
Part: NONE — NONE · airframe 23,418 hrs · 4,587 cycles
DURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE BOTTOM SKIN BTW RIB 17 TO RIB 18 AT STRINGER 8 ON LH WING; REF AEROMAN NR 2023-120182 WO 2023 87/1 PERFORMED REPAIR ON LOWER SURFACE BOTTOM SKIN BTW RIB 17 TO RIB 18 AT STRINGER 8 ON LH WING AS PER EA # 57-3003-23 PART #1 AND EC #.A23-166-01, AIRBUS APPROVED THE REPAIR WITH A REPAIR DESIGN LIFE LIMITATION BASED ON A PRELIMINARY FATIGUE AND DAMAGE TOLERANCE EVALUATION. THIS ALLOWS THE AIRCRAFT TO RETURN TO SERVICE. THE MAXIMUM PERIOD IS CURRENTLY SET TO SIX MONTHS. LIMITATIONS ARE FROM THE TIME OF SOLUTION EMBODIMENT AS PER RDAF 81185067/003/2023#A. TOOL USED ELECTRONIC CALIPER P/N: 500-752-20, S/N: B16101278 DUE DATE: NOV-05-2023, ULTRASONIC THICKNESS GAGE P/N: 45MG S/N: 221859911 DUE DATE: NOV-07-2023, EDDY CURRENT INSTRUMENT P/N: NORTEC 600D, S/N: 210138103, DUE DATE: APR-11-2023, ULTRASONIC EQUIPMENT PN: 45MG, SN: 221861811, DUE DATE: NOV 08 2023, SMALL HOLE GAUGES PN:154-901, SN: AE-412976, DUE DATE SEP-05-2023, AND CALIPER PN:500-196-30, SN: A20226522, DUE DATE SEP-12-2023, TORQUE P/N: QD1200A; S/N:0821122946; DUE DATE: SEP-17-2023, SCALE P/N: CL5000; S/N: ARE-37099; DUE DATE: AUG-22-2023 ACCOMPLISHED BY AEROMAN NR 8612111.
Part: NONE — NONE · airframe 23,418 hrs · 4,587 cycles
DURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE BOTTOM SKIN BTW RIB 17 TO RIB 18 AT STRINGER 1 1 ON LH WING; REF AEROMAN NR 2023-120181 WO 2023 87/1 PERFORMED REPAIR ON LOWER SURFACE BOTTOM SKIN BTW RIB 17 TO RIB 18 AT STRINGER 11 ON LH WING AS PER EA # 57-3003-23 PART #1 AND EC #.A23-166-01, AIRBUS APPROVED THE REPAIR WITH A REPAIR DESIGN LIFE LIMITATION BASED ON A PRELIMINARY FATIGUE AND DAMAGE TOLERANCE EVALUATION. THIS ALLOWS THE AIRCRAFT TO RETURN TO SERVICE. THE MAXIMUM PERIOD IS CURRENTLY SET TO SIX MONTHS. LIMITATIONS ARE FROM THE TIME OF SOLUTION EMBODIMENT AS PER RDAF 81185067/003/2023#A. TOOL USED ELECTRONIC CALIPER P/N: 500-752-20, S/N B16101278 DUE DATE: NOV-05-2023, EDDY CURRENT INSTRUMENT P/N: NORTEC 600D, S/N: 210138103, DUE DATE: APR-11-2023, ULTRASONIC THICKNESS GAGE P/N: 45MG S/N: 221859911 DUE DATE: NOV-07-2023, ULTRASONIC EQUIPMENT PN: 45MG, SN: 221861811, DUE DATE: NOV 08 2023, SMALL HOLE GAUGES PN:154-901, SN: AE-412976, DUE DATE SEP-05-2023, AND CALIPER PN:500-196-30, SN: A20226522, DUE DATE SEP-12-2023, TORQUE P/N: QD1200A; S/N:0821122946; DUE DATE: SEP-17-2023., SCALE P/N: CL5000; S/N: AE-37099; DUE DATE: AUG-22-2023 ACCOMPLISHED BY AEROMAN TECH 8612111.
Part: NONE — NONE · airframe 23,418 hrs · 4,587 cycles
DURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE BOTTOM SKIN BTW RIB 18 TO RIB 19 ON LH WING; REF AEROMAN NR 2023-120178 WO 2023 87/1 PERFORMED REPAIR ON LOWER SURFACE BOTTOM SKIN BTW RIB 18 TO RIB 19 AT STRINGER 11 ON LH WING AS PER EA # 57-3003-23 PART#1 AND EC # A23-166-01, AIRBUS APPROVED THE REPAIR WITH A REPAIR DESIGN LIFE LIMITATION BASED ON A PRELIMINARY FATIGUE AND DAMAGE TOLERANCE EVALUATION. THIS ALLOWS THE AIRCRAFT TO RETURN TO SERVICE. THE MAXIMUM PERIOD IS CURRENTLY SET TO SIX MONTHS. LIMITATIONS ARE FROM THE TIME OF SOLUTION EMBODIMENT AS PER RDAF 81185067/003/2023#A. TOOL USED ELECTRONIC CALIPER P/N: 500-197-30 S/N A18109103 DUE DATE: NOV-05-2023, CALIPER P/N: 700-113-10, S/N: 0033158, DUE DATE: NOV-08-2023, ULTRASONIC EQUIPMENT, P/N: 45MG, S/N: 130063701, DUE DATE: JUN-16-2023, EDDY CURRENT EQUIPMENT, P/N: NORTEC 500D, S/N: N500X12101V022235, DUE DATE: AUG-03-2023, ULTRASONIC EQUIPMENT PN: 45MG, SN: 221861811, DUE DATE: NOV 08 2023, SMALL HOLE GAUGES PN:154-901, SN: AE-412976, DUE DATE SEP-05-2023, CALIPER PN:500-196-30, SN: A20226522, DUE DATE SEP-12-2023, SCALE P/N: CL5000; S/N: AE-37099; DUE DATE: AUG-22-2023 ACCOMPLISHED BY AEROMAN TECH 8612111.
Part: WARNING MESSAGE — FALSE INDICATION (RT WING FUEL) · airframe 16,895 hrs · 3,293 cycles
FLT 482, SFO-EWR. FUEL R WING TANK OVERFLOW ON ECAM; PERFORMED TRANSFER FUEL FROM RIGHT TANK TO CENTER TANK IAW AMM 28-21-00-710-007-A, AND SPILLAGE IN NACA VENT DURING RE-FUEL IAW AMM 28-25-00-810-816-A.
Part: OVEN — SMOKE (FWD GALLEY) · airframe 15,898 hrs · 3,092 cycles
FLT 177, BOS LAS. DURING CRUISE FLIGHT, CABIN CREW ADVISED SMOKE IN THE FWD GALLEY COMMING FROM OVEN. THEY SHUTT OFF OVEN AND SMOKE DISAPPATED, PER MCC PULLED BOTH CB FOR OVEN 103 AND 104 WERE PULLED AS A PRECAUTION. FLIGHT ATTENDANT BELIEVED SMOKE TO BE ELECTRICAL IN NATURE; R & R LH OVEN IAW AMM 25-30-00. OPS CHECK GOOD. THIS ACTION CLEARS MDDR # 438339. MX-4 UPDATED, PLACARD REMOVED, MCC NOTIFIED.
Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 15,550 hrs · 3,021 cycles
DURING HEAVY MAINTENANCE, DURING EMERGENCY LIGHT TEST FAILED BAT/EPSU (14WL) ON PASSENGER CABIN. R & R BATTERY OF THE (EPSU) 14WL ON PASSENGER CABIN IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A AND PERFORMED OPERATIONAL TEST OF (EPSU ) IAW AMM 33-51-00-710-001-A. TEST IS OK.
Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 15,550 hrs · 3,021 cycles
DURING HEAVY MAINTENANCE, DURING EMERGENCY LIGHT TEST FAILED BAT/EPSU (11WL) ON PASSENGER CABIN. R & R BATTERY OF THE (EPSU) 11 WL ON PASSENGER CABIN IAW AMM 33-51-38-00-002-A AND 33-51-28-400-002-A AND PERFORMED OPS TEST (EPSU) IAW AMM 33-51-00-710-001-A. TEST IS OK