# N772CK: 2009 Boeing 777F1H

- Status: Valid registration
- Airframe: [Boeing 777F1H](https://openairdocs.org/model/boeing-777f1h) (registry code 138527D, 2 seats)
- Engine: [GE GE90-110B1](https://openairdocs.org/engine/ge-ge90-110b1) (registry code 30046)
- Data sheets: [TCDS E00049EN](https://openairdocs.org/tcds/E00049EN) (General Electric Company GE Aviation) (OpenAirDocs)
- Serial number: 35607
- Year built: 2009
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 23, 2019
- Certificate issued: June 12, 2019
- Expires: June 30, 2029
- Mode S code: AA70B1
- Registered owner: [Dae 35607 Trust](https://openairdocs.org/faa-owner/DAE%2035607%20TRUST)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=772CK
- Page: https://openairdocs.org/aircraft/N772CK

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): 21 in force

### Matched by airframe (Boeing 777F1H)

None in force.

### Matched by engine (GE GE90-110B1)

- [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 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 N772CK.

## FAA accident and incident reports

None matched to N772CK.

## Service difficulty reports (50)

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 KCSA2026040819](https://openairdocs.org/sdr/KCSA2026040819), Apr 8, 2026: LAMP. INOPERATIVE. R1 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED PER B777 AMM 33-50-00. OPS CHECK GOOD / NO DEFECTS NOTED.
- [SDR KCSA202510231221](https://openairdocs.org/sdr/KCSA202510231221), Oct 23, 2025: BATTERY. NO TEST. LOG BOOK ENTRY # 100211059 R1, EPAS FAILS BATTERY CHECK
- [SDR KCSA202510231220](https://openairdocs.org/sdr/KCSA202510231220), Oct 23, 2025: SKIN. CRACKED. DURING OPEN HOLE INSPECTION FOR BOEING SB 777-57A0125, FASTENER #5 ON L/H WING UPPER SKIN HAS A CRACK INDICATION
- [SDR KCSA202510231219](https://openairdocs.org/sdr/KCSA202510231219), Oct 23, 2025: SKIN. CRACKED. DURING OPEN HOLE INSPECTION FOR BOEING SB 777-57A0125 FASTENERS #5 & #6 ON R/H WING UPPER SKIN HAVE CRACK INDICATIONS
- [SDR KCSA202510231218](https://openairdocs.org/sdr/KCSA202510231218), Oct 23, 2025: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT FITTING STA 1769 APPROX RBL 92 HAS CORROSION
- [SDR KCSA202510231217](https://openairdocs.org/sdr/KCSA202510231217), Oct 23, 2025: FLOOR SUPPORT. CORRODED. MAIN DECK FLOOR SUPPORT FITTING @ BS 1370 LBL 92.5 HAS EVIDENCE OF DAMAGE
- [SDR KCSA202510231216](https://openairdocs.org/sdr/KCSA202510231216), Oct 23, 2025: SHEAR WEB. CORRODED. MAIN DECK SHEAR WEB PANEL 152W1209-25, HAS SEVERAL AREAS WITH EVIDENCE OF CORROSION.
- [SDR KCSA202510231015](https://openairdocs.org/sdr/KCSA202510231015), Oct 23, 2025: SHEAR WEB. CORRODED. MAIN DECK SHEAR WEB PANEL # 152W1209-24, HAS SEVERAL AREAS WITH EVIDENCE OF CORROSION.
- [SDR KCSA202510161214](https://openairdocs.org/sdr/KCSA202510161214), Oct 16, 2025: SHEAR WEB. CORRODED. MAIN DECK SHEAR WEB PANEL # 152W1209-21, HAS SEVERAL AREAS WITH EVIDENCE OF CORROSION
- [SDR KCSA202510161213](https://openairdocs.org/sdr/KCSA202510161213), Oct 16, 2025: SHEAR WEB. CORRODED. MAIN DECK SHEAR WEB PANEL # 152W1209-20, HAS SEVERAL AREAS WITH EVIDENCE OF CORROSION
- [SDR KCSA202510161212](https://openairdocs.org/sdr/KCSA202510161212), Oct 16, 2025: SHEAR WEB. CORRODED. MAIN DECK SHEAR WEB PANEL 152W1209-23, HAS SEVERAL AREAS WITH EVIDENCE OF CORROSION
- [SDR KCSA202510161211](https://openairdocs.org/sdr/KCSA202510161211), Oct 16, 2025: SUPPORT. CRACKED. R/H A/C BAY DOOR ( PANEL # 196ER) AFT LATCH SUPPORT STRUCTURE CHAFFING
- [SDR KCSA202510161210](https://openairdocs.org/sdr/KCSA202510161210), Oct 16, 2025: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK @ STA 403 RBL 5, HAS SEVERAL AREAS WITH EVIDENCE OF CORROSION
- [SDR KCSA202510161209](https://openairdocs.org/sdr/KCSA202510161209), Oct 16, 2025: SHEAR WEB. CORRODED. MAIN DECK SHEAR WEB PANEL # 152W1209-19, HAS SEVERAL AREAS WITH EVIDENCE OF CORROSION
- [SDR KCSA202510161208](https://openairdocs.org/sdr/KCSA202510161208), Oct 16, 2025: RIB. CRACKED. RIGHT WING L/E RIB AT APPROX ISS 356 CRACKED.
- [SDR KCSA202510161207](https://openairdocs.org/sdr/KCSA202510161207), Oct 16, 2025: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT FITTING AT BS 1790, APPROX RBL 92 HAS EVIDENCE OF CORROSION.
- [SDR KCSA202510151206](https://openairdocs.org/sdr/KCSA202510151206), Oct 15, 2025: SHEAR WEB. CORRODED. MAIN DECK SHEAR WEB PANEL 152W1209-22, HAS SEVERAL AREAS WITH EVIDENCE OF CORROSION.
- [SDR KCSA202510151205](https://openairdocs.org/sdr/KCSA202510151205), Oct 15, 2025: FITTING. CRACKED. BS 1119 - 1140, LBL 96 MAIN DECK CARGO HANDLING FITTING HAS DAMAGE.
- [SDR KCSA202510151204](https://openairdocs.org/sdr/KCSA202510151204), Oct 15, 2025: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT FITTING AT BS 1622, APPROX RBL 92 HAS EVIDENCE OF CORROSION.
- [SDR KCSA202510151203](https://openairdocs.org/sdr/KCSA202510151203), Oct 15, 2025: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT FITTING AT STA 1664, APPROX RBL 92 HAS EVIDENCE OF CORROSION.
- [SDR KCSA202510151202](https://openairdocs.org/sdr/KCSA202510151202), Oct 15, 2025: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT FITTING AT STA 1685, APPROX RBL 92 HAS EVIDENCE OF CORROSION.
- [SDR KCSA202510151201](https://openairdocs.org/sdr/KCSA202510151201), Oct 15, 2025: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT FITTING AT STA 1706 RBL 92 HAS EVIDENCE OF CORROSION
- [SDR KCSA202510151200](https://openairdocs.org/sdr/KCSA202510151200), Oct 15, 2025: FITTING. CRACKED. STA 1140 TO STA 1161 LBL 96 MAIN DECK CARGO HANDLING FITTING HAS DAMAGE
- [SDR KCSA202510151199](https://openairdocs.org/sdr/KCSA202510151199), Oct 15, 2025: FLOOR SUPPORT. CORRODED. MAIN DECK CARGO FLOOR SUPPORT FITTING @ BS 1434 LBL 6.5 HAS EVIDENCE OF CORROSION
- [SDR KCSA202510141196](https://openairdocs.org/sdr/KCSA202510141196), Oct 14, 2025: FLOOR SUPPORT. CORRODED. MAIN DECK CARGO FLOOR SUPPORT FITTING @ BS 1410 LBL 6.5 HAS EVIDENCE OF DAMAGE.
- [SDR KCSA202510141195](https://openairdocs.org/sdr/KCSA202510141195), Oct 14, 2025: FLOOR SUPPORT. CORRODED. MAIN DECK FLOOR SUPPORT FITTING @ STA 1390 LBL 6.5 HAS EVIDENCE OF DAMAGE
- [SDR KCSA202510141194](https://openairdocs.org/sdr/KCSA202510141194), Oct 14, 2025: FLOOR SUPPORT. CORRODED. MAIN DECK FLOOR SUPPORT FITTING @ STA 1370 LBL 6.5 HAS EVIDENCE OF DAMAGE.
- [SDR KCSA202510141193](https://openairdocs.org/sdr/KCSA202510141193), Oct 14, 2025: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT FITTING @ STA 1601 APPROX RBL 92 HAS EVIDENCE OF CORROSION
- [SDR KCSA202510141192](https://openairdocs.org/sdr/KCSA202510141192), Oct 14, 2025: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT FITTING @ STA 1748 APPROX RBL 92 HAS EVIDENCE OF CORROSION
- [SDR KCSA202510141191](https://openairdocs.org/sdr/KCSA202510141191), Oct 14, 2025: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT FITTING @ STA 1727 APPROX RBL 92 HAS EVIDENCE OF CORROSION
- [SDR KCSA202510141190](https://openairdocs.org/sdr/KCSA202510141190), Oct 14, 2025: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT FITTING @ STA 1643 APPROX RBL 92 HAS EVIDENCE OF CORROSION
- [SDR KCSA202601211002](https://openairdocs.org/sdr/KCSA202601211002), Oct 13, 2025: SIGN. DAMAGED. FOUND L1 EMERGENCY EXIT SIGN DAMAGED
- [SDR KCSA202510111189](https://openairdocs.org/sdr/KCSA202510111189), Oct 11, 2025: BULKHEAD. CORRODED. MAIN DECK RIGID CARGO BARRIER, HAS SEVERAL AREAS WITH EVIDENCE OF CORROSION
- [SDR KCSA202510111188](https://openairdocs.org/sdr/KCSA202510111188), Oct 11, 2025: SHEAR WEB. CORRODED. MAIN DECK SHEAR WEB PANEL # 152W1209-33, HAS SEVERAL AREAS WITH EVIDENCE OF CORROSION
- [SDR KCSA202510111187](https://openairdocs.org/sdr/KCSA202510111187), Oct 11, 2025: SHEAR WEB. CORRODED. MAIN DECK SHEAR WEB PANEL # 152W1209-34, HAS SEVERAL AREAS WITH EVIDENCE OF CORROSION
- [SDR KCSA202510111186](https://openairdocs.org/sdr/KCSA202510111186), Oct 11, 2025: SHEAR WEB. CORRODED. MAIN DECK SHEAR WEB PANEL # 152W1209-17 HAS SEVERAL AREAS WITH EVIDENCE OF CORROSION
- [SDR KCSA202510111185](https://openairdocs.org/sdr/KCSA202510111185), Oct 11, 2025: FITTING. CRACKED. STA 1287 TO STA 1303 RBL 80 MAIN DECK CARGO HANDLING FITTING HAS DAMAGE.
- [SDR KCSA202510111184](https://openairdocs.org/sdr/KCSA202510111184), Oct 11, 2025: SKIN. DAMAGED. POSSIBLE LIGHTNING STRIKE STA 550 L/H SIDE BETWEEN S-7L AND S-6L
- [SDR KCSA202510101183](https://openairdocs.org/sdr/KCSA202510101183), Oct 10, 2025: SKIN. DAMAGED. FASTENER DAMAGED ON TOP OF UPPER FUSELAGE EXTERIOR AT S-2 L, APPROX STA 697
- [SDR KCSA202510101182](https://openairdocs.org/sdr/KCSA202510101182), Oct 10, 2025: SHEAR WEB. CORRODED. MAIN DECK SHEAR WEB AT STA 382- 403, RBL 6- 56.80 HAS CORROSION
- [SDR KCSA202510101181](https://openairdocs.org/sdr/KCSA202510101181), Oct 10, 2025: SKIN. DAMAGED. LIGHTNING STRIKE DAMAGE ON THE FUSELAGE SKIN LAP SEAM EXTERNAL SURFACE AT STATION 2072 AT STRINGER 5L
- [SDR KCSA202510101180](https://openairdocs.org/sdr/KCSA202510101180), Oct 10, 2025: SKIN. DAMAGED. LIGHTNING STRIKE DAMAGE ON R/H HORIZONTAL TIP AFT SIDE
- [SDR KCSA202510101179](https://openairdocs.org/sdr/KCSA202510101179), Oct 10, 2025: SKIN. DAMAGED. LIGHTNING STRIKE DAMAGE FOUND ON TOP OF UPPER FUSELAGE AT S-1L APPROX STA 772.
- [SDR KCSA202510101178](https://openairdocs.org/sdr/KCSA202510101178), Oct 10, 2025: SKIN. DAMAGED. R/H LOWER FUSELAGE APPROX STA 1951 APPROX STRINGER 42 EXTERNAL SKIN HAS EVIDENCE OF LIGHTNING STRIKE
- [SDR KCSA2025050620](https://openairdocs.org/sdr/KCSA2025050620), May 6, 2025: FAN. CONTAMINATED. CLIMBING THROUGH APPROX 360 HAD SMOKE IN COCKPIT, UNKNOWN SOURCE. T-SHOT IAW FIM 21-00 TASK 808, RAN ENGS 1 & 2. COULD NOT DUPLICATE, FOUND NO BURNING OF EXTERI
- [SDR KCSA2023030809](https://openairdocs.org/sdr/KCSA2023030809), Mar 8, 2023: NONE. NONE. EMERGENCY FLASHLIGHT STRAP BY R1 DOOR BROKEN. REMOVED AND REPLACED EMERGENCY FLASHLIGHT STRAP BY R1 DOOR IAW B777 AMM 25-64-01. ALL CHECKS GOOD.
- [SDR KCSA2022110627](https://openairdocs.org/sdr/KCSA2022110627), Nov 6, 2022: NONE. NONE. FIRST OFFICERS EMERGENCY FLASHLIGHT HOLDER BROKEN FLASHLIGHT BRACKET REPLACED AND CHECKS GOOD PER AMM 25-64-01
- [SDR KCSA2022082820](https://openairdocs.org/sdr/KCSA2022082820), Aug 28, 2022: NONE. UNSERVICEABLE. FOUND RIGHT HAND SIDE EMERGENCY LIGHTS INOPERATIVE WHILE PREFORMING TASK CARD (777) 33-060-00-01 REMOVED AND REPLACED RIGHT HAND EMERGENCY LIGHT BATTERY PACK IA
- [SDR KCSA2022070911](https://openairdocs.org/sdr/KCSA2022070911), Jul 9, 2022: BATTERY. INOPERATIVE. CAPTAINS SIDE EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED CAPTAINS SIDE EMERGENCY FLASHLIGHT BATTERY IAW B777-200 AMM 25-64-01, OPERATIONS CHECK GOOD
- [SDR KCSA2022070213](https://openairdocs.org/sdr/KCSA2022070213), Jul 2, 2022: BATTERY. INOPERATIVE. FOUND COPILOT SIDE EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY IAW B777-200 AMM 25-64-01. OPERATIONS CHECK GOOD.

## Service difficulty reports on N772CK not matched to an aircraft (1)

They name N772CK, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR K11A2010070872202](https://openairdocs.org/sdr/K11A2010070872202), Jul 8, 2010: SKIN. CORRODED. MAIN CABIN CORROSION BETWEEN STRINGER AND SKIN, 5 INCHES.

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Boeing 777F1H aircraft: https://openairdocs.org/model/boeing-777f1h/aircraft.md
- The GE GE90-110B1 engine: https://openairdocs.org/engine/ge-ge90-110b1.md

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