N47280

BOEING 737-8 · 2022 · Valid Registration

Registered owner: UNITED AIRLINES INC, IL (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
UNITED AIRLINES INCOperator2024-02-06 – 2024-02-06Operator named in NTSB report
UNITED AIRLINES, INC. (CALA)Operator2024-02-06 – 2024-02-06Operator named in NTSB report

Accident & incident history

Inc · 2024-02-06 Operator named in NTSB report
BOEING 737-8 None injury Part 121UNITED AIRLINES, INC. Not yet finalized — may be revised.
Source: NTSB case DCA24LA094

Maintenance disclosures

F J · 2026-05-04 Matched by certificate designator
ATA 3422

LEFT IRS FAULT LIGHT ON NON NORMAL COMP DEBRIEFED WITH CREW, CHECKED FOR FAULTS IN DFCS, REPLACE L ADIRU. REF FIM 34-21 TASK 839 REPLACED L ADIRU, OPS CHECK GOOD REF AMM 34-21-00.

Source: SDR CALA2026050516011 · FAA SDRS
O · 2025-02-24 Matched by certificate designator
ATA 2560

DOOR 1R SLIDE FABRIC IS TOO CLOSE RIGHT COLLAR. NEEDS ADJUSTMENT ADJUSTED GIRT BAR MATERIAL REF AMM TASK 25-66-01-601-804. NO FURTHER DEFECTS NOTED.

Source: SDR CALA2025022602490 · FAA SDRS
O · 2025-02-03 Matched by certificate designator
ATA 3350

36C EMERGENCY EXIT PATH LIGHTING TRIM FALLEN OFF EMERGENCY LIGHT HOUSING DETACHED FROM SEAT AT ATTACH POINT INSERTS. REQUESTED MEL 3351A SEAT LOCATION IS 37A NOT 36A MEL 3351A NO MEL AVAILABLE, WILL HAVE TO GET WITH ESC FOR POSSIBLE RELIEF. REMOVED AND REPLACED BROKEN EMER LIGHT SHROUD 42-2521-3-0092. CKD NORMAL @ 37C

Source: SDR CALA2025020402193 · FAA SDRS
O · 2024-02-06 Matched by certificate designator
ATA 2721

RUDDER PEDALS WERE LOCKED OUT IN NEUTRAL POSITION SPOKE TO CREW AND CONFIRMED BOTH PILOTS AND F/O SIDE RUDDER PEDALS WERE VERY HHRD TO MOVE AND THEY NEEDED TO APPLY ALOT OF FORCE TO FREE UP PEDALS. REMOVED LEFT NOSE WHEEL WELL CEILING PANEL ASSEMBLY # 14A7901-7 FOR INSPECTION ASSEMBLY # 141A790-7. REMOVED RIGHT NOSE WHEEL WELL CEILING PANEL ASSEMBLY # 141A7901-8 FOR INSPECTION PERFORMED RUDDER PEDAL DO NOT MOVE FREELY (CAPTAINS) FAULT ISOLATION FIM TASK 27-21 TASK 813 : STEPS (D1-D3) UP TO STEP (D4) AS PER FIM TASK 27-21 TASK 813 COMPLETED STEP (D-4). STEP (D-5) TO COMPLETION REQUIRED. COMPLIED WITH VISUAL INSPECTION OF RUDDER AFT QUADRANT AS PER FIM TASK 27-21 TASK 813 STEP (D-4) NO DISCREPANCIES NOTED. LEAK CK''S GOOD PER MM 53-14-01.

Source: SDR CALA2024021400419 · FAA SDRS