# N782CK: 2009 Boeing 747-4HQF

- Status: Valid registration
- Airframe: [Boeing 747-4HQF](https://openairdocs.org/model/boeing-747-4hqf) (registry code 138488I, 8 seats)
- Engine: [GE CF6-80C2B5F](https://openairdocs.org/engine/ge-cf6-80c2b5f) (registry code 30117)
- Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 37304
- Year built: 2009
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 6, 2009
- Certificate issued: November 29, 2011
- Expires: November 30, 2027
- Mode S code: AA9830
- Registered owner: [Kalitta Air LLC](https://openairdocs.org/faa-owner/KALITTA%20AIR%20LLC)
- Location: [Ypsilanti, MI](https://openairdocs.org/faa-place/MI/Ypsilanti)
- Owner type: LLC
- Owner's area on the map: 42.2751° N, 83.5863° W: Placed by OpenAirDocs at the center of ZIP code 48198, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=782CK
- Page: https://openairdocs.org/aircraft/N782CK

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): 29 in force

### Matched by airframe (Boeing 747-4HQF)

None in force.

### Matched by engine (GE CF6-80C2B5F)

- [AD 2023-20-08](https://openairdocs.org/ad/2023-20-08): Engine (Turbine/Turboprop) · General Electric CF6-80C2B1F, CF6-80C2B2F, CF6-80C2B4F and 4 more. Effective Oct 19, 2023
- [AD 2021-26-22](https://openairdocs.org/ad/2021-26-22): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 14, 2022
- [AD 2021-14-11](https://openairdocs.org/ad/2021-14-11): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 25 more. Effective Aug 27, 2021
- [AD 2021-03-02](https://openairdocs.org/ad/2021-03-02): Fuel Control/Turbine Engines · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Mar 31, 2021
- [AD 2020-22-02](https://openairdocs.org/ad/2020-22-02): Engine Fuel and Control · General Electric CF6-80C2A5F, CF6-80C2B1F, CF6-80C2B2F and 13 more. Effective Dec 3, 2020
- [AD 2016-08-10](https://openairdocs.org/ad/2016-08-10): Accessory heat shield · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Jun 1, 2016
- [AD 2014-21-01](https://openairdocs.org/ad/2014-21-01): Fuel manifold · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Nov 28, 2014
- [AD 2013-08-20](https://openairdocs.org/ad/2013-08-20): Fuel tube · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 14 more. Effective May 31, 2013
- [AD 2012-03-12](https://openairdocs.org/ad/2012-03-12): No. 3 bearing packing · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Apr 5, 2012
- [AD 2012-04-05](https://openairdocs.org/ad/2012-04-05): Electronic control unit (ECU) · General Electric CF6-80C2B1F, CF6-80C2B1F1, CF6-80C2B1F2 and 8 more. Effective Mar 30, 2012
- [AD 2009-21-07](https://openairdocs.org/ad/2009-21-07): Thrust and thrust control · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Dec 1, 2009
- [AD 2009-14-08](https://openairdocs.org/ad/2009-14-08): High-pressure compressor rotor (HPCR) stages 11-14 spool/ shafts · General Electric CF6-80C2B5F. Effective Aug 5, 2009
- [AD 2009-07-03](https://openairdocs.org/ad/2009-07-03): Eddy current inspection (ECI) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Apr 30, 2009
- [AD 2009-04-10](https://openairdocs.org/ad/2009-04-10): Critical life-limited parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 30 more. Effective Mar 30, 2009
- [AD 2008-21-11](https://openairdocs.org/ad/2008-21-11): Low-pressure turbine (LPT) cases · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Nov 28, 2008
- [AD 2007-11-20](https://openairdocs.org/ad/2007-11-20): Fuel shroud retaining rings · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 22 more. Effective Jul 10, 2007
- [AD 2007-05-14](https://openairdocs.org/ad/2007-05-14): Cast titanium weld- repaired forward engine mount platforms · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 9, 2007
- [AD 2006-16-06](https://openairdocs.org/ad/2006-16-06): Certain stage 1 high- pressure turbine (HPT) rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Sep 5, 2006
- [AD 2005-17-05](https://openairdocs.org/ad/2005-17-05): High pressure compressor rotor (HPCR) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Sep 27, 2005
- [AD 2004-22-07](https://openairdocs.org/ad/2004-22-07): Stage 2 nozzle guide vanes (HPT S2 NGVs) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 1, 2004
- [AD 2004-07-13](https://openairdocs.org/ad/2004-07-13): High pressure turbine (HPT) stage 1 disks · General Electric CF6-80C2A5F, CF6-80C2B5F, CF6-80C2B7F and 1 more. Effective May 6, 2004
- [AD 2003-02-07](https://openairdocs.org/ad/2003-02-07): Low pressure turbine (LPT) shrouds · General Electric CF6-50A, CF6-50C, CF6-50C1 and 30 more. Effective Mar 3, 2003
- [AD 2002-25-08](https://openairdocs.org/ad/2002-25-08): High pressure compressor rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Jan 23, 2003
- [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002
- [AD 2000-03-04](https://openairdocs.org/ad/2000-03-04): General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Apr 10, 2000
- [AD 99-01-01](https://openairdocs.org/ad/99-01-01): Accessory Gearbox (AGB) idler adapters · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jan 21, 1999
- [AD 98-22-06](https://openairdocs.org/ad/98-22-06): Fan Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 41 more. Effective Nov 23, 1998
- [AD 97-22-14](https://openairdocs.org/ad/97-22-14): (HPCR) 3-9 Spool · General Electric CF6-50A, CF6-50C, CF6-50C1 and 29 more. Effective Nov 17, 1997
- [AD 93-14-18](https://openairdocs.org/ad/93-14-18): High pressure turbine (HPT) thermal shields · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Oct 4, 1993

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

- [AD 2020-20-13](https://openairdocs.org/ad/2020-20-13) (historical): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Nov 12, 2020
- [AD 2018-15-04](https://openairdocs.org/ad/2018-15-04) (historical): Turbine/Turboprop Engine--Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Oct 2, 2018
- [AD 2009-05-02](https://openairdocs.org/ad/2009-05-02) (historical): Drainless fuel manifold assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Mar 31, 2009
- [AD 2007-12-07](https://openairdocs.org/ad/2007-12-07) (historical): Electronic control units (ECUs) · General Electric CF6-80C2B1F, CF6-80C2B2F, CF6-80C2B4F and 5 more. Effective Jul 11, 2007
- [AD 2004-04-07](https://openairdocs.org/ad/2004-04-07) (historical): Stage 1 HPT rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 12, 2004
- [AD 2002-07-12](https://openairdocs.org/ad/2002-07-12) (historical): Life Limits Section of Continued Airworthiness (ICA) - Selected Critical Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 27 more. Effective May 15, 2002
- [AD 2001-10-07](https://openairdocs.org/ad/2001-10-07) (historical): High Pressure Turbine Rotor Disks · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jun 18, 2001
- [AD 2000-16-12](https://openairdocs.org/ad/2000-16-12) (historical): High Pressure Compressor Rotor Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Sep 5, 2000
- [AD 99-24-15](https://openairdocs.org/ad/99-24-15) (historical): High Pressure Compressor Rotor (HPCR) Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Jan 28, 2000
- [AD 99-08-13](https://openairdocs.org/ad/99-08-13) (historical): General Electric CF6-80A, CF6-80A1, CF6-80A2 and 26 more. Effective May 13, 1999

## Information bulletins (advisory) (5 in force)

- [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023
- [SAIB NE-11-27](https://openairdocs.org/saib/NE-11-27): Fuel Injector Nozzle - CF6-80 Improperly Welded Fuel Nozzles. Issued Apr 5, 2011
- [SAIB NE-10-37](https://openairdocs.org/saib/NE-10-37): Engine Fuel and Control: FADEC Fuel Metering Valve Resolver Feedback Faults. Issued Jul 12, 2010
- [SAIB NE-08-44](https://openairdocs.org/saib/NE-08-44): Engine Thrust Reverser  Transcowl Clevis Pin. Issued Sep 3, 2008
- [SAIB NE-07-01](https://openairdocs.org/saib/NE-07-01): Dual engine flameouts on twin engine airplanes. Issued Oct 12, 2006

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA24LA293](https://openairdocs.org/ntsb/DCA24LA293), Aug 17, 2024: Boeing 747-4HQF (N782CK), Istanbul, Türkiye, substantial damage. Probable cause: The fatigue failure of multiple hinge ribs associated with the right outboard aileron, which resulted in abnormal aileron movement and airframe vibration. Contributing to the failure was the…

## FAA accident and incident reports

None matched to N782CK.

## Service difficulty reports (25)

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 KCSA2026102163](https://openairdocs.org/sdr/KCSA2026102163), Oct 21, 2026: FUEL NOZZLE. UNSECURE. 100371542: JETT NOZZLE L - NO FUEL COMING OUT LEFT NOZZLE FOR 20 MIN. THEN WORKED BUT WOULD NOT STOP DUMPING AFTER CLOSED FOR ALMOST 10 MINUTES. CORRECTIVE ACTI
- [SDR KCSA202509251170](https://openairdocs.org/sdr/KCSA202509251170), Sep 25, 2025: LONGERON FITTING. CRACKED. TWO CRACKS WERE FOUND AT RT LONGERON EXTENSION FITTING.
- [SDR KCSA202509251169](https://openairdocs.org/sdr/KCSA202509251169), Sep 25, 2025: LONGERON FITTING. CRACKED. ONE CRACK WAS FOUND AT LT LONGERON EXTENSION FITTING.
- [SDR KCSA202509201167](https://openairdocs.org/sdr/KCSA202509201167), Sep 20, 2025: BATTERY PACK. INOPERATIVE. UPPER DECK STA 410 EXIT SIGN FOUND INOP.
- [SDR KCSA202509181166](https://openairdocs.org/sdr/KCSA202509181166), Sep 18, 2025: FITTING. CRACKED. CRACK FOUND AT STA 1000 INTERCOSTAL LUG FITTING AT LBL 11.33
- [SDR KCSA202509181165](https://openairdocs.org/sdr/KCSA202509181165), Sep 18, 2025: FITTING. CRACKED. CRACK FOUND AT BS 1000 INTERCOSTAL LUG FITTING AT RBL 11.33
- [SDR KCSA202509181164](https://openairdocs.org/sdr/KCSA202509181164), Sep 18, 2025: POWERPACK. NO TEST. EMERGENCY LIGHT POWER PACK ( M5169) CAN NOT STAY ON FOR 15 MINS
- [SDR KCSA202509181163](https://openairdocs.org/sdr/KCSA202509181163), Sep 18, 2025: POWERPACK. NO TEST. EMERGENCY LIGHT POWER PACK ( M5168) CAN NOT STAY ON FOR 15 MINS.
- [SDR KCSA202509181162](https://openairdocs.org/sdr/KCSA202509181162), Sep 18, 2025: LIGHT. FAILED INSP. M/D L1 DOOR AFT SELF ILLUMINATED EXIT SIGN LIGHT INTENSITY BELOW MINIMUM LIMIT
- [SDR KCSA202407101085](https://openairdocs.org/sdr/KCSA202407101085), Jul 10, 2024: LIGHT. INOPERATIVE. EXTERIOR SLIDE EMERGENCY LIGHT, L1533, ON R/H UPPER FUSELAGE INOP
- [SDR KCSA202404231054](https://openairdocs.org/sdr/KCSA202404231054), Apr 23, 2024: LIGHT. INOPERATIVE. U/D CREW REST EMERGENCY LIGHT INOP APPROX STA 590
- [SDR KCSA202401221003](https://openairdocs.org/sdr/KCSA202401221003), Jan 22, 2024: LIGHT. INOPERATIVE. U/D CEILING EMERGENCY LIGHTS AT APPROX STA 520
- [SDR KCSA202311161142](https://openairdocs.org/sdr/KCSA202311161142), Nov 16, 2023: LIGHT. INOPERATIVE. MULTIPLE EMERGENCY LIGHTS INOP
- [SDR KCSA202311141140](https://openairdocs.org/sdr/KCSA202311141140), Nov 14, 2023: DOUBLER. CRACKED. CRACKED DOUBLER AT STA. 1220 LBL 77 ON CANTED PRESSURE WEB
- [SDR KCSA202311141139](https://openairdocs.org/sdr/KCSA202311141139), Nov 14, 2023: BULKHEAD. CRACKED. MAIN DECK BILGE/CANTED PRESSURE DECK AT TRIM AIR DUCT BULKHEAD LOCATION PANEL HAS EVIDENCE OF CRACKING STA 1240 LBL 90
- [SDR KCSA202311141138](https://openairdocs.org/sdr/KCSA202311141138), Nov 14, 2023: FIREWALL. CRACKED. APU FIRE WALL BOTTOM L/H SIDE AT STA. 2657 WL 265 HAS CRACK
- [SDR KCSA202310201127](https://openairdocs.org/sdr/KCSA202310201127), Oct 20, 2023: SHEAR TIE. CRACKED. SHEAR TIE AT STA 1000 LBL 33.99 IS CRACKED.
- [SDR KCSA2023020306](https://openairdocs.org/sdr/KCSA2023020306), Feb 3, 2023: NOT REPORTED. NOT REPORTED. PER COMPANY CONVENIENCE REMOVED EMERGENCY DECENT DEVICE COMPARTMENT DOOR ASSEMBLY FOR AIRCRAFT N403KZ. INSTALLED EMERGENCY DECENT DEVICE COMPARTMENT DOOR ASSEMB
- [SDR KCSA202111221126](https://openairdocs.org/sdr/KCSA202111221126), Nov 22, 2021: LIGHT. INOPERATIVE. TRANSFER FROM LOG BOOK #782-6112: ITEM #3 MAIN AISLE EMERGENCY INOP
- [SDR KCSA202103221025](https://openairdocs.org/sdr/KCSA202103221025), Mar 22, 2021: LIGHT. INOPERATIVE. L1 OVER DOOR EMERGENCY LIGHT INOP
- [SDR KCSA20190226301](https://openairdocs.org/sdr/KCSA20190226301), Feb 23, 2019: FIRE WARNING. FALSE ACTIVATION. FIRE MAIN DECK AFT. PERFORMED OPERATIONS CHECK IAW AMM 26-14-00. NO FAULTS FOUND AT THIS TIME.
- [SDR KCSA201710231072](https://openairdocs.org/sdr/KCSA201710231072), Oct 23, 2017: LIGHT. INOPERATIVE. MAIN DECK DOOR L1 THRESHOLD OVERHEAD EMERGENCY LAMP IS INOP AT STA 464 ON CEILING IN THE MAIN CARGO DECK.
- [SDR KCSA2015081310](https://openairdocs.org/sdr/KCSA2015081310), Aug 13, 2015: DOOR. DAMAGED. DISCOVERED DAMAGE ON AFT APU SECTION DOORS. REPAIRED IAW DWG'S 53301516-1, 53301517-1 AND SRM 53-80-08, FIG 201.
- [SDR KCSA2015051705](https://openairdocs.org/sdr/KCSA2015051705), May 17, 2015: HOSE. MISROUTED. UPPER DECK SERVICE DOOR RT SLIDE SUPPLY HOSE MISROUTED. REROUTED SUPPLY HOSE IAW AMM 25-68-00, CONFIGURE 2.
- [SDR KCSA201212131211](https://openairdocs.org/sdr/KCSA201212131211), Dec 13, 2012: LIGHT. INOPERATIVE. L1 MAIN ENTRY DOOR EMERGENCY SILL LIGHT DOES NOT COME ON DURING TEST.

## STCs that may be installed (OpenAirDocs) (4)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (GE CF6-80C2B5F)

- [STC SE01543CH](https://openairdocs.org/stc/SE01543CH): Replace Hamilton Sundstrand P/N 778839-13, 778839-14, 778839-19, 778839-20, 778839-37, 778839-38, 816682-1, 840618-2, 880724 carbon bushings with Cook Airtomic P/N AIR22947 Slotted Entry Busing in the High Pressure Shutoff Valve. Cook Airtomic
- [STC SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic
- [STC SE01471AT](https://openairdocs.org/stc/SE01471AT): Replace right and left side Rohr, Inc. fire detection harness on GE CF6-80C2 engine. Unison Industries. Lists CF6-80C2 Series
- [STC SA2227SO](https://openairdocs.org/stc/SA2227SO): Installation of wiring and associated components for utilization of the Rolls Royce, Inc., ARINC, interface/readers UT1317 or UT1317/1, for the purpose of acquisition, recording, and analysis in real time of engine/aircraft/ systems. (767 SERIES POWERED BY RR RB-11-524 SERIES. Rolls Royce, Inc. Lists CF6-80 Series

## Related

- Other Boeing 747-4HQF aircraft: https://openairdocs.org/model/boeing-747-4hqf/aircraft.md
- The GE CF6-80C2B5F engine: https://openairdocs.org/engine/ge-cf6-80c2b5f.md

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