N27290
Registered owner: UNITED AIRLINES INC, IL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| UNITED AIRLINES, INC. (CALA) | Operator | on 2024-03-08 | Operator named in NTSB report |
Accident & incident history
Operated by UNITED AIRLINES INC (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.
9 reports on file, 2023-06-29 – 2025-11-16.
Part: LIGHT — FAULTED (ZONE 200) · airframe 7,415 hrs · 2,570 cycles
EMERGENCY EXIT LIGHT FLICKING AC LEFT ROW 20 PULLED AND COLLARED C/B E12 ON P92 PANEL COLLARED CB , REF ATTACHED PIC. PLACED ON MEL 3321A . TOMC APPROVED MEL 3321A APPROVED *DM* ASSIST: {LT ASSY/60-3321-3-0004 PREV ORDERED.} REF WDM 33-21-12-1.1: PRECAUTIONARILY ADDED OWE LT ASSY'S M2837 & M2838 TO ENSURE AVAIL. ADJ M&L TO 6 TO ALLOW FOR DISTURBANCE OF OWE HATCH R/R LIGHT ASSY AT LEFT ROW 20. LOADED DATABASE SOFTWARE, OPS CHKD OK.
Part: SKIN — SCRATCHED (ZONE 200) · airframe 5,325 hrs · 1,883 cycles
FOUND SCRACH LINE ON EXTERIOR FUSELAGE R/H BTW STA.400 AND STA. 420 AND S-14R. PERFORMED REPAIR PER EO 250100 REV P1, P2, P3, P4, P5, AND P6 IAW EO 250100 REV IR AND EC/RA 5330-07509. REF ELB LOGS 4571389 AND 4571342 FOR DIP REQUIREMENTS PER ECRA5330-07509.
Part: LENS — MISSING (ZONE 200) · airframe 5,190 hrs · 1,842 cycles
EMERGENCY LIGHTS DAMAGED 21F EMER EXIT LIGHTS 21F DO NOT ILLUMINATE CREW REPORTED EXIT LIGHT COVER WITH WORD EXIT LENS COVER IS MISSING. LIGHT IS OPERATIONAL REPLACED EMERGENCY EXIT LIGHT COVER AND OPS CHECKED GOOD AT THIS TIME PER AMM 25-21-00
Part: FLOOR SUPPORT — BENT (BS 847-867 LBL21) · airframe 2,635 hrs · 993 cycles
STA 847-867 LBL 21 WL 160, INTERCOSTAL P/N 149A8109-127 WAS REPLACED BY BOEING REF CONTRACT UAL-RE-2401657 AND FRR-111-3. THE PURPOSE OF THIS LP IS TO COMPLY WITH GMM 4-20-05 AND COMPLTE AN SFR. SFR COMPLETE.
Part: STIFFENER — BENT (BS 847 RBL 19-28) · airframe 2,635 hrs · 993 cycles
STA 847 RBL 19-28 WL 162, STIFFENER WAS REPLACED BY BOEING REF CONTRACT #UAL-RE-2401657 AND FRR 149-3. THE PURPOSE OF THIS LP IS TO COMPLY WITH GMM 4-20-05 AND COMPLETE AN SFR. SFR COMPLETE.
Part: FRAME — DENTED (BS 727) · airframe 2,635 hrs · 993 cycles
STA 727+20 WL 169 LBL 72, FRAME ASSY REPLACED BY BOEING REF CONTRACT UAL-RE-2401657 AND FRR 16-1. THE PURPOSE OF THIS LP IS TO COMPLY WITH GMM 4-20-05 AND COMPLETE AN SFR. SFR COMPLETE.
Part: LANDING GEAR — SHEARED (LEFT) · airframe 2,632 hrs · 992 cycles
THIS LOGPAGE IS GENERATED FOR SDR REPORTING PURPOSES IAW GMM 04-20-16, REF LOGPAGE 7288541. LEFT MAIN LANDING SHEARED OFF DUE TO AIRCRAFT VEERED OF THE HARD SURFACE. LOG PAGE GENERATED FOR SDR REPORTING PURPOSES, ALL WORK PERFORMED BY THE BOEING COMPANY FAA REPAIR STATION BACR668L UNDER UNITED CONTRACT UAL-RE-2401657
Part: LANDING GEAR — COLLAPSED (LEFT) · airframe 2,632 hrs · 992 cycles
PER CREW REPORT: LEFT THE HARD SURFACE ON DECELERATION, ACFT SKIDDED. LEFT MAIN WENT INTO DIRT AND COLLAPSED. POSSIBLE FUEL LEAK ON LEFT WING REPORTED.
Part: SENSOR — WARNING MESSAGE (NO 4 FLAP) · airframe 177 hrs · 77 cycles
TAKEOFF CONFIG WARNING ACCOMPANIED BY HIGH SPEED REJECT FLIGHT DECK EFFECT SHOWS NO 4 FLAP SENSOR DISAGREEMENT INFO PER FIM TASK 27-81-00-810-829 ACCOMPLISHED INITIAL EVALUATION 27-51-00-740-801. OMF SHOWS NOT ACTIVE FOR MAINTENANCE MESSAGE STEPS. ACCOMPLISHED LEADING EDGE FLAP AND SLAT SYSTEM OPERATION 27-81223. PER FIM FAULT WAS INTERMITTANT. WITH PRIMARY CONTROL, AMM TASK 27-81-00-860-801 AND ACCOMPLISHED FSEU DISPLAY AND EXISTING FAULTS TEST, AMM TASK