# N740CK: 1989 Boeing 747-4H6

- Status: Valid registration
- Airframe: [Boeing 747-4H6](https://openairdocs.org/model/boeing-747-4h6) (registry code 13848BE, 660 seats)
- Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025)
- Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 24405
- Year built: 1989
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 15, 2003
- Certificate issued: March 20, 2008
- Expires: November 30, 2029
- Mode S code: A9F2C6
- 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=740CK
- Page: https://openairdocs.org/aircraft/N740CK

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. The registry lists only the engine series, so ADs for every GE CF6-80 model are included.

## ADs that may apply (OpenAirDocs): 61 in force

### Matched by airframe (Boeing 747-4H6)

None in force.

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

- [AD 2024-24-03](https://openairdocs.org/ad/2024-24-03): Engine Exhaust · Boeing MD-11, MD-11F and CF6-80C2D1F. Effective Jan 13, 2025
- [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 2022-02-18](https://openairdocs.org/ad/2022-02-18): Engine Mount Section · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 3 more. Effective Feb 25, 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 2018-07-05](https://openairdocs.org/ad/2018-07-05): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 11, 2018
- [AD 2017-11-15](https://openairdocs.org/ad/2017-11-15): Turbine/ Turboprop Engine--Turbine Section · General Electric CF6-80C2L1F. Effective Jul 13, 2017
- [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 2011-23-04](https://openairdocs.org/ad/2011-23-04): Forward engine mount assembly side links · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Dec 12, 2011
- [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 2009-08-06](https://openairdocs.org/ad/2009-08-06): Stage 1 high-pressure turbine (HPT) rotor  
 disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 18, 2009
- [AD 2009-07-10](https://openairdocs.org/ad/2009-07-10): High-pressure turbine rotor (HPTR) · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 6, 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 2008-02-17](https://openairdocs.org/ad/2008-02-17): Thrust reverser actuation systems · General Electric CF6-50A, CF6-50C, CF6-50C1 and 16 more. Effective Feb 28, 2008
- [AD 2007-24-07](https://openairdocs.org/ad/2007-24-07): Thermal spray coating on certain stage 1 fan disks · General Electric CF6-80C2B1. Effective Jan 2, 2008
- [AD 2007-22-07](https://openairdocs.org/ad/2007-22-07): Electronic control unit (ECU) · General Electric CF6-80C2D1F. Effective Nov 28, 2007
- [AD 2007-21-06](https://openairdocs.org/ad/2007-21-06): Electronic control unit (ECU) · General Electric CF6-80C2A5F. Effective Nov 15, 2007
- [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 2006-06-08](https://openairdocs.org/ad/2006-06-08): Latching system of the fan reverser · General Electric CF6-80C2D1F. Effective Apr 25, 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 2005-06-07](https://openairdocs.org/ad/2005-06-07): Directional pilot valve (DPV) assembly · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Apr 25, 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 2003-12-08](https://openairdocs.org/ad/2003-12-08): Directional pilot valve · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Jul 23, 2003
- [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 2001-06-09](https://openairdocs.org/ad/2001-06-09): Aft Engine Mount Link Assemblies · General Electric CF6-80A3. Effective May 1, 2001
- [AD 2000-12-08](https://openairdocs.org/ad/2000-12-08): Mount Link Assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 4 more. Effective Aug 28, 2000
- [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 96-16-07](https://openairdocs.org/ad/96-16-07): Rear Right Hand Mount Link · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective Aug 28, 1996
- [AD 95-17-16](https://openairdocs.org/ad/95-17-16): Compressor Rear Frame · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Nov 7, 1995
- [AD 95-10-11](https://openairdocs.org/ad/95-10-11): Fan Reversers · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective May 31, 1995
- [AD 94-20-06](https://openairdocs.org/ad/94-20-06): Oil System · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 27, 1994
- [AD 94-07-04](https://openairdocs.org/ad/94-07-04): High Pressure Turbine Disk · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 23, 1994
- [AD 94-06-03](https://openairdocs.org/ad/94-06-03): High Pressure Turbine Disk · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 29, 1994

### 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 2006-12-24](https://openairdocs.org/ad/2006-12-24) (historical): Five-link forward mount assembly · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Jul 21, 2006
- [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 2003-01-05](https://openairdocs.org/ad/2003-01-05) (historical): Dovetail slots · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Jan 28, 2003
- [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 2000-08-12](https://openairdocs.org/ad/2000-08-12) (historical): Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 10 more. Effective Oct 23, 2000
- [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 2000-04-14](https://openairdocs.org/ad/2000-04-14) (historical): Fuel tube flange seating · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective May 1, 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 99-18-20](https://openairdocs.org/ad/99-18-20) (historical): Inadvertent In-flight Thrust Reverser · General Electric Aircraft Engines CF6-50 Series (all), CF6-80A1, CF6-80A3 and 6 more. Effective Nov 2, 1999
- [AD 99-18-19](https://openairdocs.org/ad/99-18-19) (historical): Inadvertent Thrust Reverser · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 7 more. Effective Sep 24, 1999
- [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
- [AD 98-15-17](https://openairdocs.org/ad/98-15-17) (historical): Link Assembly · General Electric CF6-80A3. Effective Aug 7, 1998
- [AD 91-20-02](https://openairdocs.org/ad/91-20-02) (historical): Fuel Manifolds · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective Nov 25, 1991
- [AD 90-26-01](https://openairdocs.org/ad/90-26-01) (historical): Fuel Manifold Systems · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 11 more. Effective Dec 20, 1990

All 80: https://openairdocs.org/aircraft/N740CK/ads.md

## 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

None matched to N740CK.

## FAA accident and incident reports

None matched to N740CK.

## Service difficulty reports (146, newest 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 KCSA2026100859](https://openairdocs.org/sdr/KCSA2026100859), Oct 8, 2026: FIRE WARNING. FALSE ACTIVATION. CARGO FIRE AFT. CORRECTIVE ACTION: NO SIGNS FIRE NOTED AND SUSPECTED ISSUE WAS DRY ICE CARRIED IAW CONDITIONAL INSPECTION B747 AMM 05-51-56, FIM 21-00 TASK 810 
- [SDR KCSA2026093058](https://openairdocs.org/sdr/KCSA2026093058), Sep 30, 2026: DOOR. DAMAGED. GEAR DOOR EICAS. INSP & TROUBLESHOT IAW AMM 05-41-07, FIM 32-61, & AMM 32-61-00. DAMAGED LT BLG INBD DOOR & HARDWARE. ALL CHKD GOOD IAW AMM 32-61-00. NO DEFECTS
- [SDR KCSA202605271039](https://openairdocs.org/sdr/KCSA202605271039), May 27, 2026: WEB. CORRODED. CORROSION FOUND ON FORWARD CARGO TORQUE BOX AT STA 660 APPROX
- [SDR KCSA202512121244](https://openairdocs.org/sdr/KCSA202512121244), Dec 12, 2025: WEB. CRACKED. AFTER NDT INSPECTION A DEFECT NOTED ON HOLE AT BONDED WEB ASSEMBLY STA 2598 WL 265 AND RBL 39
- [SDR KCSA202512121243](https://openairdocs.org/sdr/KCSA202512121243), Dec 12, 2025: TENSION TIE. CRACKED. AFTER NDT ACCOMPLISHED A HFEC OPEN INSPECTION ON TENSION TIE STA 1180 L/H SIDE FOUND 3 EA FASTENER HOLE WITH DEFECT INDICATION
- [SDR KCSA202512121242](https://openairdocs.org/sdr/KCSA202512121242), Dec 12, 2025: TENSION TIE. CRACKED. AFTER NDT INSPECTION 3 EA FASTENER HOLES FOUND WITH DEFECT INDICATION ON TENSION TIE BS 1140 LT.
- [SDR KCSA202512121241](https://openairdocs.org/sdr/KCSA202512121241), Dec 12, 2025: SEAT TRACK. CORRODED. DURING " OK TO INSTALL " FOUND SEAT TRACK AT FUSELAGE STA 1960 RBL 11.33 WITH EXFOLIATION CORROSION AT THE LOWER SURFACE FLANGE
- [SDR KCSA202512121240](https://openairdocs.org/sdr/KCSA202512121240), Dec 12, 2025: TENSION TIE. CRACKED. AFTER NDT INSPECTION FOUND TWO CRACKS ON TWO FASTENER HOLES AT TENSION TIE 1120 LT SIDE.
- [SDR KCSA202512121239](https://openairdocs.org/sdr/KCSA202512121239), Dec 12, 2025: INTERCOSTAL. CRACKED. A CRACK INDICATION WAS IDENTIFIED BETWEEN FASTENERS AT BL 0 BETWEEN STA 320 AND STA 340
- [SDR KCSA202512101238](https://openairdocs.org/sdr/KCSA202512101238), Dec 10, 2025: FUEL TANK. CORRODED. CORROSION FOUND ON FUEL CTR TANK BETWEEN UPPER SKIN EDGE AND CANTED AREA MAIN DECK STA 1241, BL 0, NWL 175
- [SDR KCSA202512091237](https://openairdocs.org/sdr/KCSA202512091237), Dec 9, 2025: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS L5734 STA 498, L1382 STA 360, L5604 STA 470 WONT TURN ON.
- [SDR KCSA202512091236](https://openairdocs.org/sdr/KCSA202512091236), Dec 9, 2025: SKIN. CORRODED. CORROSION FOUND ON FUEL CTR TANK ON UPPER SKIN MAIN W/W UPPER SURFACE MAIN DECK STA 1241 LBL 2
- [SDR KCSA202512091235](https://openairdocs.org/sdr/KCSA202512091235), Dec 9, 2025: RESERVOIR. DISCHARGED. EMERGENCY POWER RESEVOIR DISCHARGED (LH)
- [SDR KCSA202512051234](https://openairdocs.org/sdr/KCSA202512051234), Dec 5, 2025: LONGERON FITTING. CRACKED. AFTER NDT INSPECTION PER W/O 740037417 EO 5313-23-02 FOUND 1 EA FASTENER HOLE WITH CRACK INDICATION ON STA 2598 STR 11 LONGERON L/H SIDE UPPER FITTING
- [SDR KCSA202512051233](https://openairdocs.org/sdr/KCSA202512051233), Dec 5, 2025: TENSION TIE. CRACKED. AFTER TENSION TIE NDT INSPECTION FOUND 7 EA FASTENER HOLES WITH CRACK INDICATION ON STEEL PLATE STA 1180 R/H
- [SDR KCSA202512051232](https://openairdocs.org/sdr/KCSA202512051232), Dec 5, 2025: PLATE. CRACKED. AFTER TENSION TIE NDT INSPECTION FOUND 8 EA FASTENER HOLES WITH CRACK INDICATION ON STEEL PLATE BS 1140 RT.
- [SDR KCSA202512051231](https://openairdocs.org/sdr/KCSA202512051231), Dec 5, 2025: PLATE. CRACKED. AFTER TENSION TIE NDT INSPECTION FOUND 7 EA FASTENER HOLES WITH CRACK INDICATION ON STEEL PLATE BS 1220 RT.
- [SDR KCSA202512051230](https://openairdocs.org/sdr/KCSA202512051230), Dec 5, 2025: PLATE. CRACKED. AFTER TENSION TIE NDT INSPECTION FOUND 7 EA FASTENER HOLES WITH CRACK INDICATIONS ON STEEL PLATE BS 1180 LT.
- [SDR KCSA202512051229](https://openairdocs.org/sdr/KCSA202512051229), Dec 5, 2025: WEB. CRACKED. SEVERAL CRACKED PANELS IN AREA INSIDE OF THE FUSELAGE FWD OF NOSE GEAR WELL STA 140-180 L/H AND R/H LOCATIONS. 4 EA. WEBS
- [SDR KCSA202504261076](https://openairdocs.org/sdr/KCSA202504261076), Apr 26, 2025: BULB. INOPERATIVE. MULTIPLE EMERGENCY LIGHTS ARE INOP ON UPPER DECK
- [SDR KCSA202501241003](https://openairdocs.org/sdr/KCSA202501241003), Jan 24, 2025: LIGHT. NO TEST. MULTIPLE UPPER DECK EMERGENCY LIGHTS TURN OFF AFTER 3 SECONDS OF OPERATION.
- [SDR KCSA202411091115](https://openairdocs.org/sdr/KCSA202411091115), Nov 9, 2024: LIGHT. INOPERATIVE. U/D L/H EMERGENCY DOOR EMERGENCY LIGHTS INOP
- [SDR KCSA2024052417](https://openairdocs.org/sdr/KCSA2024052417), May 24, 2024: SMOKE DETECTOR. FAULTED. ON FINAL FOR 8R, AIRCRAFT LOWER CARGO FIRE WARNING ANNUNCIATED. FOLLOWED QRH AND DISCHARGED FIRE BOTTLES. PER B747-400 AMM 05-51-95 CONDITIONAL INSPECTION COMPL
- [SDR KCSA202311141137](https://openairdocs.org/sdr/KCSA202311141137), Nov 14, 2023: BATTERY. INOPERATIVE. PERFORMED EMERGENCY POWER RESERVOIR CHECK OPS CHECK FAILED R/H UPPER DOOR BATTERY INOP
- [SDR KCSA2023092736](https://openairdocs.org/sdr/KCSA2023092736), Sep 27, 2023: SNUBBER. FAILED. L1 DOOR DIFFICULT TO OPEN AND CLOSE. FOUND ROTARY SNUBBER TO BE BAD, REMOVED AND REPLACED ROTARY SNUBBER IAW 747-400 AMM 52-11-10, OPERATIONS CHECKS NORMAL.
- [SDR KCSA202309151111](https://openairdocs.org/sdr/KCSA202309151111), Sep 15, 2023: BATTERY. INOPERATIVE. LH UPPER DECK EMERGENCY ESCAPE DOOR BATTERY IS DEAD
- [SDR KCSA202309141110](https://openairdocs.org/sdr/KCSA202309141110), Sep 14, 2023: SEAT TRACK. CORRODED. POSSIBLE CORROSION ON SEAT TRACK AT STA 1670 RBL 12.
- [SDR KCSA202309141109](https://openairdocs.org/sdr/KCSA202309141109), Sep 14, 2023: SUPPORT FITTING. CORRODED. LH OB ELEVATOR REACTION HINGE SUPPORT FITTING IS CORRODED.
- [SDR KCSA202309141108](https://openairdocs.org/sdr/KCSA202309141108), Sep 14, 2023: BULKHEAD. CRACKED. STA 2598 BLKHD R/H FWD INNER CHORD CRACKED AT 1 EA. LOCATION
- [SDR KCSA202309141107](https://openairdocs.org/sdr/KCSA202309141107), Sep 14, 2023: STIFFENER. CRACKED. TOP STIFFENER CRACKED @ STATION 300 L/H SIDE AS MARKED
- [SDR KCSA202309141106](https://openairdocs.org/sdr/KCSA202309141106), Sep 14, 2023: BULKHEAD. CRACKED. CRACK FOUND STA 2598 R/H SIDE IN INNER CHORD ADJACENT TO LOWEST INBOARD FASTENER HOLE AT INTERIM REPAIR
- [SDR KCSA202309141105](https://openairdocs.org/sdr/KCSA202309141105), Sep 14, 2023: ATTACH ANGLE. CRACKED. #3 PYLON I/B SKIRT FAIRING ATTACH ANGLE HAS POSSIBLE CRACK
- [SDR KCSA202309141104](https://openairdocs.org/sdr/KCSA202309141104), Sep 14, 2023: ANGLE. CRACKED. AFT LOWER L-ANGLE CRACKED AT STA 440, STR 26 FWD SIDE OF R1 DOOR OPENING.
- [SDR KCSA202306261072](https://openairdocs.org/sdr/KCSA202306261072), Jun 26, 2023: BOTTLE. LOW PRESSURE. L/H UPPER DECK ESCAPE SLIDE AFT BOTTLE LOW AFTER SERVICING.
- [SDR KCSA2023013102](https://openairdocs.org/sdr/KCSA2023013102), Jan 31, 2023: COVER. DAMAGED. COVER HAS FALLEN OFF AND SHATTERED FROM FLIGHT DECK EMERGENCY ACCESS LIGHT AIRCRAFT OF P7. REMOVED AND REPLACED SHATTERED COVER ASSEMBLY IN ACCORDANCE WITH B747
- [SDR KCSA202211211213](https://openairdocs.org/sdr/KCSA202211211213), Nov 21, 2022: LIGHT. INOPERATIVE. MULTIPLE EMERGENCY LIGHTS INOP
- [SDR KCSA202206271081](https://openairdocs.org/sdr/KCSA202206271081), Jun 27, 2022: LIGHT. INOPERATIVE. R/H UPPER DECK DOOR EMERGENCY LIGHTS INOP
- [SDR KCSA202206271080](https://openairdocs.org/sdr/KCSA202206271080), Jun 27, 2022: LIGHT. INOPERATIVE. L/H UPPER DECK DOOR EMERGENCY LIGHTS INOP
- [SDR KCSA202201061000](https://openairdocs.org/sdr/KCSA202201061000), Jan 6, 2022: LIGHT. INOPERATIVE. RH UPPER DECK EMERGENCY ESCAPE DOOR EMERGENCY LIGHTS INOP
- [SDR KCSA202107301086](https://openairdocs.org/sdr/KCSA202107301086), Jul 30, 2021: SUPPORT BRACKET. CORRODED. RIGHT HAND ELEVATOR INBOARD ACTUATOR UPPER HINGE OUTBOARD SUPPORT BRACKET HAS EVIDENCE OF CORROSION
- [SDR KCSA202107301085](https://openairdocs.org/sdr/KCSA202107301085), Jul 30, 2021: SUPPORT BRACKET. CORRODED. RIGHT HAND ELEVATOR INBOARD ACTUATOR UPPER HINGE INBOARD SUPPORT BRACKETS HAS EVIDENCE OF CORROSION
- [SDR KCSA202107211084](https://openairdocs.org/sdr/KCSA202107211084), Jul 21, 2021: STIFFENER. CRACKED. CRACKED STIFFENER ON NWW STA 310 RBL 10
- [SDR KCSA202107211083](https://openairdocs.org/sdr/KCSA202107211083), Jul 21, 2021: STIFFENER. CRACKED. CRACKED STIFFENER ON NWW STA 310 LBL 10
- [SDR KCSA202107131082](https://openairdocs.org/sdr/KCSA202107131082), Jul 13, 2021: FRAME. CORRODED. FOUND EVIDENCE OF CORROSION ON MAIN DECK UNDER FLOOR BOARD STA 1480 LBL 20
- [SDR KCSA202106301078](https://openairdocs.org/sdr/KCSA202106301078), Jun 30, 2021: STIFFENER. CRACKED. 3 EA. CRACK INDICATIONS ON NWW AT STA 310 R/H WL 130, RADIUS OF STIFFENER
- [SDR KCSA202103031013](https://openairdocs.org/sdr/KCSA202103031013), Mar 3, 2021: LIGHT. INOPERATIVE. UPPER DECK EMERGENCY LIGHT STA 644 INOP
- [SDR KCSA202005201064](https://openairdocs.org/sdr/KCSA202005201064), May 20, 2020: LIGHT. INOPERATIVE. UPPER DECK AFT EMERGENCY LIGHT INOP
- [SDR KCSA202003041022](https://openairdocs.org/sdr/KCSA202003041022), Mar 4, 2020: LIGHT. INOPERATIVE. L/H UPPER DECK DOOR EMERGENCY SLIDE LIGHTS INOP L2927 AND L2930
- [SDR KCSA202003041021](https://openairdocs.org/sdr/KCSA202003041021), Mar 4, 2020: LIGHT. INOPERATIVE. R/H UPPER DECK DOOR EMERGENCY SLIDE LIGHTS INOP L2927 AND L2930
- [SDR KCSA201908281203](https://openairdocs.org/sdr/KCSA201908281203), Aug 28, 2019: ANGLE. CORRODED. LOWER INSIDE ANGLE OF AFT PIT CARGO DOOR HAS CORROSION IN MULTIPLE SPOTS

All 146: https://openairdocs.org/aircraft/N740CK/reports.md

## STCs that may be installed (OpenAirDocs) (6)

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 CF6-80 series)

- [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. Lists CF6-80A
- [STC SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic. Lists CF6-80C2 Series
- [STC SE00969CH](https://openairdocs.org/stc/SE00969CH): Install AeroControlex P/N 2605290-001 variable stator feedback control cable. AeroControlex Group TransDigm Inc. Lists CF6-80A
- [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 SE00463LA](https://openairdocs.org/stc/SE00463LA): Install fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. This STC is jointly by owned by Hi Temp Insulation and MRA Systems acting through Middle River Aircraft Systems, 103 Chesapeake Park Plaza, Baltimore, MD 21220. Hi Temp Insulation Inc. Lists CF6-80C2A1
- [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

## Earlier aircraft with N740CK

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N740CK before.

- [Cancelled 2008-04-10](https://openairdocs.org/deregistered/N740CK-2008-04-10): Boeing 747-200B, S/N 22064. Owner: [Kalitta Air LLC](https://openairdocs.org/faa-owner/KALITTA%20AIR%20LLC), [Ypsilanti, MI](https://openairdocs.org/faa-place/MI/Ypsilanti)

## Related

- Other Boeing 747-4H6 aircraft: https://openairdocs.org/model/boeing-747-4h6/aircraft.md
- The GE CF6-80 series engine: https://openairdocs.org/engine/ge-cf6-80-series.md

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