# N771CK: 2006 Boeing 777-36NER

- Status: Valid registration
- Airframe: [Boeing 777-36NER](https://openairdocs.org/model/boeing-777-36ner) (registry code 1385253, 552 seats)
- Engine: [GE GE90-115B](https://openairdocs.org/engine/ge-ge90-115b) (registry code 30048)
- Data sheets: [TCDS E00049EN](https://openairdocs.org/tcds/E00049EN) (General Electric Company GE Aviation) (OpenAirDocs)
- Serial number: 32791
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 26, 2025
- Certificate issued: January 18, 2023
- Expires: January 31, 2030
- Mode S code: AA6CFA
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=771CK
- Page: https://openairdocs.org/aircraft/N771CK

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 22 in force

### Matched by airframe (Boeing 777-36NER)

None in force.

### Matched by engine (GE GE90-115B)

- [AD 2025-25-07](https://openairdocs.org/ad/2025-25-07): Turbine Section · General Electric Company GE GE90-90B, GE90-94B, GE90-110B1 and 1 more. Effective Feb 6, 2026
- [AD 2025-07-10](https://openairdocs.org/ad/2025-07-10): Fuel Controlling System · General Electric Company GE GE90-110B1 and GE90-115B. Effective May 21, 2025
- [AD 2024-06-15](https://openairdocs.org/ad/2024-06-15): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective May 14, 2024
- [AD 2023-26-07](https://openairdocs.org/ad/2023-26-07): Turbine Section · General Electric GE90-90B, GE90-94B, GE90-110B1 and 1 more. Effective Feb 27, 2024
- [AD 2023-04-19](https://openairdocs.org/ad/2023-04-19): Turbine Engine Compressor Section · General Electric GE90-110B1 and GE90-115B. Effective Mar 27, 2023
- [AD 2022-23-09](https://openairdocs.org/ad/2022-23-09): Turbine Engine Compressor Section, Turbine Section · General Electric GE90-90B, GE90-94B, GE90-110B1 and 1 more. Effective Jan 17, 2023
- [AD 2022-18-06](https://openairdocs.org/ad/2022-18-06): Turbine Engine Compressor Section, Turbine Section · General Electric GE90-110B1, GE90-115B, GE90-76B and 3 more. Effective Oct 26, 2022
- [AD 2021-26-06](https://openairdocs.org/ad/2021-26-06): Turbine Engine Accessory Drive · General Electric GE90-76B, GE90-85B, GE90-90B and 3 more. Effective Feb 15, 2022
- [AD 2020-21-13](https://openairdocs.org/ad/2020-21-13): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective Nov 17, 2020
- [AD 2020-18-14](https://openairdocs.org/ad/2020-18-14): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective Oct 21, 2020
- [AD 2020-10-04](https://openairdocs.org/ad/2020-10-04): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective May 27, 2020
- [AD 2020-01-55](https://openairdocs.org/ad/2020-01-55): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective Mar 2, 2020
- [AD 2019-21-51](https://openairdocs.org/ad/2019-21-51): Turbine Section · General Electric GE90-115B. Effective Dec 6, 2019
- [AD 2018-20-23](https://openairdocs.org/ad/2018-20-23): Turbine Engine Compressor Section · General Electric GE90-110B1 and GE90-115B. Effective Nov 30, 2018
- [AD 2018-20-22](https://openairdocs.org/ad/2018-20-22): Turbine Section · General Electric GE90-110B1, GE90-113B and GE90-115B. Effective Nov 13, 2018
- [AD 2017-08-06](https://openairdocs.org/ad/2017-08-06): Engine Oil Cooler · General Electric GE90-110B1, GE90-115B, GE90-76B and 3 more. Effective May 22, 2017
- [AD 2013-23-18](https://openairdocs.org/ad/2013-23-18): Variable bypass valve (VBV) actuator fuel supply tube · General Electric GE90-110B1 and GE90-115B. Effective Jan 7, 2014
- [AD 2013-17-07](https://openairdocs.org/ad/2013-17-07): Stage 1 high-pressure turbine (HPT) stator shrouds · General Electric GE90-110B1, GE90-115B, GE90-76B and 3 more. Effective Oct 18, 2013
- [AD 2013-15-20](https://openairdocs.org/ad/2013-15-20): Transfer gearbox assembly (TGB) radial gearshafts · General Electric GE90-110B1, GE90-113B, GE90-115B and 5 more. Effective Aug 21, 2013
- [AD 2011-26-11](https://openairdocs.org/ad/2011-26-11): HPC stages 1-2 seal teeth · General Electric GE90-110B1 and GE90-115B. Effective Feb 3, 2012
- [AD 2009-25-14](https://openairdocs.org/ad/2009-25-14): Blade · General Electric GE90-110B1, GE90-113B and GE90-115B. Effective Jan 19, 2010
- [AD 2007-10-05](https://openairdocs.org/ad/2007-10-05): Turbine Center Frames (TCFs) · General Electric GE90-110B1, GE90-113B and GE90-115B. Effective Jun 14, 2007

### Historical (superseded or no longer in force)

- [AD 2021-15-05](https://openairdocs.org/ad/2021-15-05) (historical): Engine Controls · General Electric GE90-110B1 and GE90-115B. Effective Sep 13, 2021
- [AD 2020-20-17](https://openairdocs.org/ad/2020-20-17) (historical): Engine Controls · General Electric GE90-110B1 and GE90-115B. Effective Oct 23, 2020
- [AD 2017-07-04](https://openairdocs.org/ad/2017-07-04) (historical): Compressor Section · General Electric GE90-110B1 and GE90-115B. Effective Apr 21, 2017
- [AD 2013-24-17](https://openairdocs.org/ad/2013-24-17) (historical): High pressure compressor (HPC) rotor stage 2-5 spools · General Electric GE90-110B1 and GE90-115B. Effective Dec 31, 2013
- [AD 2013-14-51](https://openairdocs.org/ad/2013-14-51) (historical): Failure of a transfer gearbox assembly radial gearshaft · General Electric GE90-110B1 and GE90-115B
- [AD 2013-10-52](https://openairdocs.org/ad/2013-10-52) (historical): Transfer gearbox assemblies (TGBs) · General Electric GE90-110B1 and GE90-115B. Effective Jun 26, 2013

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N771CK.

## FAA accident and incident reports

None matched to N771CK.

## Service difficulty reports (14)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR KCSA2026092456](https://openairdocs.org/sdr/KCSA2026092456), Sep 24, 2026: UNKNOWN. ODOR. ON SHORT FINAL ODOR OF OIL OR OTHER FLUID. CONTINUED AFTER ENGINE SHUTDOWN. SMELL OF DIRTY SOCKS. TRANSFERRED TO DMI 100354336 IAW KA B777 MEL 49-52-01 CAT C DU
- [SDR KCSA2026040820](https://openairdocs.org/sdr/KCSA2026040820), Apr 8, 2026: BRAKE SYS. ABNORMAL. RIGHT BRAKES TOO SENSITIVE WHEN EQUAL MANUAL BRAKING IS APPLIED, CAUSES THE AIRPLANE TO VEER RIGHT. AUTOBRAKING IS NORMAL BEHAVIOR. CORRECTIVE ACTION: PERFORMED
- [SDR KCSA2026021209](https://openairdocs.org/sdr/KCSA2026021209), Feb 12, 2026: LIGHT. NO DISCREPANCY. EMERGENCY LIGHTS ADVISORY A/T. PERFORMED AN OPS TEST OF EMERGENCY LIGHTS CONTROL SWITCHES IAW AMM 33-51-00, TEST PASSED, OPS NORMAL.
- [SDR KCSA2026020308](https://openairdocs.org/sdr/KCSA2026020308), Feb 3, 2026: FITTING. DAMAGED. L1 DOOR WAS VERY DIFFICULT TO OPEN. HANDLE WILL STOP HALF WAY UP. TRANSFERRED TO DMI 100305587 IAW B777 KA MELB 25-10 52-11-01-01B, CAT C, DUE 02-13-26, (M) PRO
- [SDR KCSA202602170308](https://openairdocs.org/sdr/KCSA202602170308), Feb 3, 2026: DOOR. BINDING. L1 DOOR WAS VERY DIFFICULT TO OPEN. HANDLE WILL STOP HALF WAY UP. IAW B777 KA MELB 25-10 52-11-01-01B, CAT C, DUE 02-13-26, (M) PROCEDURE C/W. INSTALLED PLACARD
- [SDR KCSA2026010801](https://openairdocs.org/sdr/KCSA2026010801), Jan 8, 2026: SNUBBER. DAMAGED. L1 DOOR WILL NOT OPEN, R1 DOOR OUT OF ADJUST. FOUND SNUBBER LEAKING ON L1, R & R L1 DOOR LINEAR SNUBBER IAW AMM 52-12-08, OPS CHKD GOOD, DOOR OPS CHKD GOOD IAW 
- [SDR KCSA2026020201380](https://openairdocs.org/sdr/KCSA2026020201380), Dec 13, 2025: DOOR. NO DISCREPANCY. L1 DOOR WILL NOT OPEN A/T: TRANSFERRED TO DMI 100281653 IAW MEL B 25-10 AND 52-11-01-01B CAT C DUE 12-23-25 PLACARD INSTALLED (M) PROCEDURES C/W 100281674: REF 
- [SDR KCSA2025101453](https://openairdocs.org/sdr/KCSA2025101453), Oct 14, 2025: TANK UNIT. UNSERVICEABLE. FUEL IMBALANCE EICAS MESSAGE PRESENTED ON APPROACH TO LLBG NON-NORMAL EICAS CHECKLIST COMPLETED. ACTION TAKEN: TROUBLESHOT IAW B777 FIM 28-22 TASK 847 AND B777 
- [SDR KCSA202510231453](https://openairdocs.org/sdr/KCSA202510231453), Oct 14, 2025: FUEL SYS. MALFUNCTIONED. DECLARED EMERGENCY FOR PRIORITY HANDLING TO LAND RUNWAY 26, 3200 LBS OF FUEL INDICATED IN RIGHT WING TANK. TRANSFERRED TO DMI #100275603 IAW KAL MEL 28-41-1-2-2
- [SDR KCSA202510071177](https://openairdocs.org/sdr/KCSA202510071177), Oct 7, 2025: BATTERY. INOPERATIVE. FOUND EMERGENCY EXIT SIGN FOR L1 DOOR INOP
- [SDR KCSA202510071176](https://openairdocs.org/sdr/KCSA202510071176), Oct 7, 2025: LIGHT. INOPERATIVE. FOUND EMERGENCY LIGHT INOP ON PANEL ABOVE THE L1 DOOR.
- [SDR KCSA202510071175](https://openairdocs.org/sdr/KCSA202510071175), Oct 7, 2025: BRACKET. DAMAGED. L1 EMERGENCY EXIT SIGN LENS HOLDING BRACKET DAMAGED
- [SDR KCSA202510071174](https://openairdocs.org/sdr/KCSA202510071174), Oct 7, 2025: SKIN. CRACKED. WHILE PERFORMING BOEING SB 777-57A0125 CRACK INDICATIONS FOUND AT FASTENERS #5 L/H WING T/E UPPER SKIN
- [SDR KCSA202510071173](https://openairdocs.org/sdr/KCSA202510071173), Oct 7, 2025: SKIN. CRACKED. WHILE PERFORMING BOEING SB 777-57A0125 CRACK INDICATIONS FOUND ON FASTENER #5 R/H WING T/E UPPER SKIN

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Boeing 777-36NER aircraft: https://openairdocs.org/model/boeing-777-36ner/aircraft.md
- The GE GE90-115B engine: https://openairdocs.org/engine/ge-ge90-115b.md

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