N27266
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 |
|---|---|---|---|
| UNITED AIRLINES, INC. (CALA) | Operator | on 2025-06-08 | Operator named in NTSB report |
Accident & incident history
Operated by United Airlines (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.
5 reports on file, 2023-07-26 – 2026-03-02.
Part: LIGHT — DETACHED (ZONE 200) · airframe 15,095 hrs · 5,100 cycles
EMERGENCY LIGHT 29C HANGING DOWN. REQUESTED MEL FOR EMERGENCY LIGHT 29C. MEL 3351A REJECTED. SECURED THE HOUSING TO SEAT FRAME AS REQUIRED, CHECKED ISLE PATH LIGHTING, OPS CHECKED GOOD. OK TO CONTINUE.
Part: SLIDE — LOOSE (ZONE 800) · airframe 14,817 hrs · 5,017 cycles
R1 DOOR EMERGENCY SLIDE IS LOOSE AND NEEDS TO BE REPACKED. VERIFIED Z FOLD IS PREVELENT AND GIRT MATERIAL DOES NOT INTERFERE WITH DOOR OPERATION IAW AMM 25-66-01.
Part: SEAL — BROKEN (LIFE RAFT) · airframe 13,686 hrs · 4,654 cycles
AFT LIFE RAFT SEAL BROKEN REQUEST MEL 3810A, REFERRAL IS DO LAV SMELLING TO BADLY, ALL SYSTEMS OPERATE NORALLY, PLACARD INSTALLED ON DOOR. MEL 3810A REJECTED INSPECTED LIFE RAFT AND RESEALED BIN.
Part: ANTI-ICE VALVE — FAILED (ENG#2) · airframe 7,198 hrs · 2,578 cycles
ENG ANTI-ICE COWL VALVE LIGHT IS ON AT MORE THAN 28000 FEET ENG 2 COWL VALVE LIGHT REMAINS ILLUMINATED WHEN SWITCHED TO ON AT FL300 T/S PER FIM 30-21 TASK 810 FOUND #2 ENG ANTI ICE VALVE FAILED, REMOVED AND REPLACE VALVE REF AMM 30-21-11-000-801 AND 30-21-11-400-801 UPTO AND INCLUDING STEP H.(6)(C). REQUIRES INSTALLATION TEST PER STEP I. PARTS USED: 42-3021-9-0001,QTY VALVE, ANTI-ICE OFF 42-3021-9-0001 0474 ON 42-3021-9-0001 0424 VALVE, ANTI-ICE OFF 42-3021-9-0001 0474 ON 0000 :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1040632 SN OFF 0474 PERFORMED #2 ENG COWL ANTI ICE VALVE INSTALLATION TEST PER AMM 30-21-11-400-801 STEP I, OPS AND LEAK CHECKS GOOD. #2 ENG COWL VALVE LIGHT WORKS NORMAL.
Part: HEADSET — UNKNOWN (EXT PWR DR) · airframe 5,664 hrs · 2,029 cycles
PDA 3 PILOT REPORT OF SOUND HEARD RIGHT FORWARD FUSELAGE DURING FLIGHT. AIRCRAFT ON T0209 HEADED BACK TO IAH. DURING INSPECTION FOUND JACK AND WIRE HANGING OUT OF EXTERNAL POWER DOOR. HEADSET CONNECTED TO JACK ON EXTERNAL POWER DOOR ATTACHED TO AIRCRAFT. AIRCRAFT AIR RETURNED TO IAH GOING TO BOG. WHEN AIRCRAFT ARRIVED JACK WAS ATTACHED BUT HEADSET WAS MISSING. PDA CATEGORY 3 PER GMM 02-30-95. {COMPLETE LP NBRS ADDED TO ENABLE HYPERLINK BENEFIT} THE DENTS/ABNORMALITIES WERE ANNOTATED. INFO UPDATE"GRND HANDLING EQUIP DEPARTS ACFT" CONDITIONAL INSP PERFORMED BY EMPL U219918 PER AMM 05-51-59 AFTER THE AIR RTN OF T209/25JUL. ADD EMP:U219918. FOUND DENT STA 245.5 R APPROX STR 20.53-00-01-1A -1. APPLIED DENT DOT. FOUND DENT AT STA 245.5 AND INBTWEEN STR 19 AND 20. DENT IS 2.5X 2.5 X .020 DEEP AND W/ Y 125 IS ALLOWABLE LIMITS REF SRM. FOUND MULTIPLE SMALL DENTS APPROX STA 309 R BETWEEN STR 20 AND 22 R. FOUND SMALL DENTS WITHIN SRM ALLOWABLE DAMAGE REF SRM 53-00-01-1A-1, APPLIED DENT DOT. AIRCRAFT RELEASED FROM REPAIR STATION WAS MAINTAINED IAW FAA REGS. AND UNITED SPECIFICATIONS AND PROCEDURES AND IS AIRWORTHY WITH RESPECT TO WORK PERFORMED. PERTINENT DETAILS ARE ON FILE AT THE REPAIR STA. IN THE SIGNOFF, LIST THE VISIT TYPE,CERTIFICATE #, AND DESCRIPTION OF WORK PERFORMED. PAC MAINT ACCOMPLISHED UA PMC ON LINE MAINT CHECKS REF IFC2459X.