- Registered owner
- United Airlines Inc
- Location
- Chicago, IL
- Owner type
- Corporation
- Serial number
- 36408
- Year built
- 2015
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- October 29, 2015
- Certificate issued
- November 5, 2015
- Expires
- November 30, 2028
- Mode S code
- A2A3AF
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every GE GENX-1B74/75/ model are included below.
On this page
Airworthiness directives that may apply · 98
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2012 | 1 |
|---|---|
| 2015 | 3 |
| 2016 | 8 |
| 2017 | 6 |
| 2018 | 15 |
| 2019 | 6 |
| 2020 | 11 |
| 2021 | 8 |
| 2022 | 13 |
| 2023 | 10 |
| 2024 | 8 |
| 2025 | 9 |
| 2026 | 18 |
See all 116 ADs
Information bulletins that may apply · 9
Advisory, not mandatory.
Airframe · Boeing 787-9
SAIB 2025-09INSTRUMENT PANEL, Potential Installation of Lockwire on Switch Guards that May Restrict Access to Passenger Oxygen and Ram Air Turbine (RAT) SwitchesSAIB AIR-22-09R1AUTOPILOT FLIGHT DIRECTOR SYSTEM: ALT HOLD Engaged on Takeoff on Boeing Model 777/787 common fleets.SAIB AIR-20-19Flight Management Computing Software SystemSAIB AIR-20-15Navigation Localizer SystemSAIB NM-20-07Navigation - Glideslope SystemSAIB NM-20-06Electrical Power System: Lug Terminal TracksSAIB NM-18-33Engine Fuel and ControlSAIB NM-17-15Equipment/Furnishings - Inflatable Airbag AssemblySAIB NM-15-03Flight ControlsNTSB investigations
No NTSB investigations matched to N26960Matched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Boeing 787-9 aircraft
FAA incident reports
No FAA accident or incident reports matched to N26960Matched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Boeing 787-9 aircraft
Reports on N26960 not matched to an aircraft · 1
They name N26960, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CALA2026092219679Flashlight · inoperativeFLASHLIGHT OF FA SEAT 1L IS INOPERATIVE. COMPLIED WITH MEL 2564B, INOP STICKER INSTALLED. REPLACED THE FLASHLIGHT. DIP CLOSED.SDR CALA2026052016392Acm · faultedAT GATE RETURN FLIGHT CREW REPORTED BURNING ODOR SMELL IN CABIN. FOUND 3 STATUS MESSAGES REF LP 8941702, 8941648 AND 8941641. RT PACK WOULD NOT TURN ON. PRESSED PACK RESET SWITCH WHICH CLEARED THE MESSAGES THEN CYCLED PACK SWITCH ON. WITHIN 1 MIN OF PACK RUNNISDR CALA2026020213486Bypass Valve · faultedCONDENSER INLET SENSOR R STATUS MSG DISPLAYED, DUE TO LOW LIMIT VALVE R HAS BEEN DEACTIVED IN OPEN POSITION AS REQUIRED PER DDG 21- 52-05. ACPD AS REQUIRED PER DDG 21-52-05. REQUESTING MEL CARD 2152BL. TOMC APPROVES MEL 2152BL FOR RH PACK CONDENSOR INLET SENSSDR CALA2026010712747Lens · broken3D AND 4D PROXIMITY LIGHT LENS BROKEN. R & R THE LIGHT ASSY, GOOD FOR SVC, IAW IFM 25-26-36, AND DWG 2500DD15922.SDR CALA2025042204104Switch · out of positionDOOR 4L EPAS BATTERY IN SAFE POSITION RETURNED DOOR 4L EPAS SAFETY SWITCH TO NORMAL POSITION REF AMM 25-66-01-01B-720ASDR CALA2025031402838Circuit Breaker · pulledPULLED CBS FOR DOOR RH2 EPAS-DOOR 2R A CE5211821, EPAS-DOOR 2R B CE5211824 REF AMM DOOR-MOUNTED ESCAPE SLIDE PACK ASSEMBLY - REMOVAL REFERENCE: DMC-B787-A-25-66-01-01B-520A-A REACTIVATED CB'S FOR DOOR RH2 EPAS-DOOR 2R A CE5211821, EPAS-DOOR 2R B CE5211824SDR CALA2023042401218Unknown · unknownAFTER TAKE OFF STRONG HEAVY ACRID ODOR IN PILOT CREW REST THAT WOULD NOT DISSIPATE. DEBRIEFED CREW,CREW TRIED TO ISOLATE WITH TURN OF LEFT RECIRC AN D LEFT PACK- NO CHANGE, RT RECIRC AND RT PACK NO INCREASE OR DEC REASE IN SMELL. ACCESSED CREW REST RESIDUAL SSDR CALA2022042901104None · noneDURING O2 SERVICING OF CREW OXYGEN, THE VERTICAL O2 BOTTLE SPARKED AND FLAMED ELECTRICALLY AT OPEN/CLOSE VALVE CAUSING BURNS TO LOCAL MATERIALS AND DESTROYING THE VALVE. DUE TO HEAT DAMAGE ACCOMPLISH THE FOLLOWING INSPECTIONS SRM 51-11-03-00A-284A-A SRM 51-13-
STCs that may be installed · 56
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.