# N700CK: 1997 Boeing 747-4R7F

- Status: Valid registration
- Airframe: [Boeing 747-4R7F](https://openairdocs.org/model/boeing-747-4r7f) (registry code 13848BP, 490 seats)
- Engine: [GE CF6-80C2B1F](https://openairdocs.org/engine/ge-cf6-80c2b1f) (registry code 30106)
- Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 25868
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 4, 2013
- Certificate issued: May 15, 2026
- Expires: May 31, 2033
- Mode S code: A954CA
- 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=700CK
- Page: https://openairdocs.org/aircraft/N700CK

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): 33 in force

### Matched by airframe (Boeing 747-4R7F)

None in force.

### Matched by engine (GE CF6-80C2B1F)

- [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 2009-07-03](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 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 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 95-10-11](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 94-06-03](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
- [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
- [AD 91-15-25](https://openairdocs.org/ad/91-15-25): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Sep 6, 1991
- [AD 91-11-05](https://openairdocs.org/ad/91-11-05): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Jul 5, 1991

### 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 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 99-08-13](https://openairdocs.org/ad/99-08-13) (historical): General Electric CF6-80A, CF6-80A1, CF6-80A2 and 26 more. Effective May 13, 1999
- [AD 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

## 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 N700CK.

## FAA accident and incident reports

None matched to N700CK.

## Service difficulty reports (136, 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 KCSA202610091225](https://openairdocs.org/sdr/KCSA202610091225), Oct 9, 2026: RIB. CRACKED. RIGHT WING L/E RIB CRACKED AT ILES 756.95 APPROX. JUST AFT OF L/E BULLNOSE IN UNDERWING CAVITY ON LONGERON ATTACH POINT.
- [SDR KCSA202510251222](https://openairdocs.org/sdr/KCSA202510251222), Oct 25, 2025: LIGHT. INOPERATIVE. L1 DOOR SILL & M/D CEILING EMERGENCY LIGHTS INOP.
- [SDR KCSA202506101093](https://openairdocs.org/sdr/KCSA202506101093), Jun 10, 2025: RIB. CRACKED. LEFT WING LEADING EDGE MACHINED RIB CRACKED AT LOWER FORWARD FASTENER HOLE AT APPROX ILES 964.55
- [SDR KCSA202506101092](https://openairdocs.org/sdr/KCSA202506101092), Jun 10, 2025: RIB. CRACKED. LEFT WING LEADING EDGE MACHINED RIB CRACKED AT LOWER FORWARD FASTENER HOLE AT APPROX ILES 1014.95
- [SDR KCSA202506101091](https://openairdocs.org/sdr/KCSA202506101091), Jun 10, 2025: FITTING. CORRODED. R/H WING L/E FITTING CORRODED AT STA. ILES 1536
- [SDR KCSA202506101090](https://openairdocs.org/sdr/KCSA202506101090), Jun 10, 2025: FITTING. CORRODED. R/H WING L/E FITTING CORRODED STA. ILES 1524
- [SDR KCSA202506101089](https://openairdocs.org/sdr/KCSA202506101089), Jun 10, 2025: FITTING. CORRODED. R/H WING L/E FITTING CORRODED STA ILES 1494
- [SDR KCSA202506101088](https://openairdocs.org/sdr/KCSA202506101088), Jun 10, 2025: FITTING. CORRODED. L/H FITTING ASSY AT STA 1000 APPROX LBL11 HAS CORROSION AROUND FASTENER HOLE BUSHINGS.
- [SDR KCSA202506061087](https://openairdocs.org/sdr/KCSA202506061087), Jun 6, 2025: FLOOR SUPPORT. CRACKED. MAIN DECK FLOOR STRUCTURE FITTING AT APPROX STA 1880 LBL 98 IS CRACKED
- [SDR KCSA202506061086](https://openairdocs.org/sdr/KCSA202506061086), Jun 6, 2025: LONGERON. CRACKED. CRACK FOUND IN L/H LONGERON EXTENSION FITTING AT STA 1480 DURING NDT HFEC INSPECTION.
- [SDR KCSA202506061085](https://openairdocs.org/sdr/KCSA202506061085), Jun 6, 2025: SUPPORT RIB. CRACKED. RH HORIZONTAL STABILIZER TIP RIB HAS CRACK ON FAIRING SUPPORT STRUCTURE AT APPROX STAB BL 420
- [SDR KCSA202506061084](https://openairdocs.org/sdr/KCSA202506061084), Jun 6, 2025: SHEAR TIE. CRACKED. CRACK INDICATION FOUND AT STA 1000 FRONT SPAR SHEAR TIE AT RBL 33.99
- [SDR KCSA202506061083](https://openairdocs.org/sdr/KCSA202506061083), Jun 6, 2025: SKIN. CORRODED. FUSELAGE SKIN AT STA 1476 BETWEEN STR 4L AND 5L HAS CORROSION
- [SDR KCSA202506061082](https://openairdocs.org/sdr/KCSA202506061082), Jun 6, 2025: SKIN. CORRODED. FUSELAGE SKIN AT STA 1476 BETWEEN STR 7L& 8L HAS CORROSION
- [SDR KCSA202506061081](https://openairdocs.org/sdr/KCSA202506061081), Jun 6, 2025: SKIN. CORRODED. FUSELAGE SKIN AT STA 1476, STR 2L & 3L HAS CORROSION
- [SDR KCSA202506061080](https://openairdocs.org/sdr/KCSA202506061080), Jun 6, 2025: FITTING. CRACKED. CRACK INDICATION FOUND IN INTERCOSTAL LUG FITTING AT STA 1000, LBL 11.33 AND WL 197
- [SDR KCSA2024060118](https://openairdocs.org/sdr/KCSA2024060118), Jun 1, 2024: ESCAPE REEL. UNWANTED DEPLOY. NRS 1, 2, 3, 4, 5, & 6 ESCAPE REEL DEPLOYED. REMOVED AND REPLACED DECENT DEVICE IAW B747-400 AMM 25-61-01. NR 7 ESCAPE REEL DEPLOYED. TRANSFERRED TO DMI 1001724
- [SDR KCSA2024012805](https://openairdocs.org/sdr/KCSA2024012805), Jan 28, 2024: LAMP. INOPERATIVE. FIRST OFFICER VERY HIGH FREQUENCY LEFT LIGHT OUT. RELAMPED IAW B747 AMM 33-51-11 OPERATIONS GOOD.
- [SDR KCSA202307111075](https://openairdocs.org/sdr/KCSA202307111075), Jul 11, 2023: ESCAPE REEL. PARTIAL DEPLOY. EMERGENCY DECENT DEVICE #2 P/N 379103D-23 S/N 27728 SHOWS EVIDENCE OF DEPLOYMENT
- [SDR KCSA202307111074](https://openairdocs.org/sdr/KCSA202307111074), Jul 11, 2023: ESCAPE REEL. PARTIAL DEPLOY. EMERGENCY DECENT DEVICE #3 P/N 379103D-23 S/N 27727 SHOWS EVIDENCE OF DEPLOYMENT
- [SDR KCSA202306221070](https://openairdocs.org/sdr/KCSA202306221070), Jun 22, 2023: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK EVIDENCE OF CORROSION STA 2220-2280 LBL 34
- [SDR KCSA202305311065](https://openairdocs.org/sdr/KCSA202305311065), May 31, 2023: SEAT TRACK. DAMAGED. SEAT TRACK DAMAGED IN FWD PIT STA. 580 RBL 20
- [SDR KCSA202305311064](https://openairdocs.org/sdr/KCSA202305311064), May 31, 2023: FRAME. CRACKED. L-5 CLOSE OUT FRAME CRACKED STA-2230/S-25L
- [SDR KCSA202305241057](https://openairdocs.org/sdr/KCSA202305241057), May 24, 2023: BEAM. CRACKED. NWW R/H SIDE UPPER FWD CORNER HAS CRACKED BEAM WL 185 STA 280
- [SDR KCSA202305241056](https://openairdocs.org/sdr/KCSA202305241056), May 24, 2023: TEE FITTING. CRACKED. FWD VERTICAL TEE CHORD ON R/H SIDE OF NOSE WHEEL WELL AT STA. 250 WL 155 TO WL 200 FOUND TO BE CRACKED
- [SDR KCSA202305241055](https://openairdocs.org/sdr/KCSA202305241055), May 24, 2023: SHEAR TIE. CRACKED. BS 1000 FRONT SPAR SHEAR TIE CRACKED RBL 75.92
- [SDR KCSA202305241054](https://openairdocs.org/sdr/KCSA202305241054), May 24, 2023: BULKHEAD. CRACKED. CRACK FOUND ON BULK HEAD BELOW LONGERON FITTING AT STA 1480 WL 150 LBL 109
- [SDR KCSA202110011111](https://openairdocs.org/sdr/KCSA202110011111), Oct 1, 2021: LIGHT. INOPERATIVE. SLIDE EMERGENCY LIGHT INOP
- [SDR KCSA202104271053](https://openairdocs.org/sdr/KCSA202104271053), Apr 27, 2021: LIGHT. INOPERATIVE. EMERGENCY LIGHT L5733 INOP
- [SDR KCSA202104261052](https://openairdocs.org/sdr/KCSA202104261052), Apr 26, 2021: STIFFENER. CRACKED. MAIN DECK FLOOR TRUSS ANGLE STIFFENER HAS POSSIBLE CRACK AT APPROX STA 2360 AND LBL 40 ON AFT SIDE OF TRUSS
- [SDR KCSA202104231051](https://openairdocs.org/sdr/KCSA202104231051), Apr 23, 2021: SHEAR WEB. CORRODED. POSSIBLE CORROSION ON UPPER DECK FLOOR SHEAR WEB AT STA 460-500
- [SDR KCSA202104231050](https://openairdocs.org/sdr/KCSA202104231050), Apr 23, 2021: FLOOR SUPPORT. CORRODED. POSSIBLE CORROSION ON UPPER DECK FLOOR STRUCTURE STA 500, AT TOP OF CREW LADDER
- [SDR KCSA202104191046](https://openairdocs.org/sdr/KCSA202104191046), Apr 19, 2021: SKIN. DAMAGED. SKIN DAMAGE AT APPROX STR 37 L AND APPROX STA 750 ON EXTERNAL SIDE
- [SDR KCSA202104151045](https://openairdocs.org/sdr/KCSA202104151045), Apr 15, 2021: FLOORBEAM. CRACKED. MAIN DECK LATERAL FLOOR BEAM SUPPORT CRACKED AT STA 1080 RBL 98
- [SDR KCSA202104121035](https://openairdocs.org/sdr/KCSA202104121035), Apr 12, 2021: TENSION TIE. CRACKED. CRACK NOTED AT STA 740 TENSION TIE R/H SIDE IN FASTENER HOLE AS MARKED
- [SDR KCSA202103261031](https://openairdocs.org/sdr/KCSA202103261031), Mar 26, 2021: TENSION TIE. CRACKED. CRACK ON END OF TENSION TIE AT STA 720 S-13 L
- [SDR KCSA202103261030](https://openairdocs.org/sdr/KCSA202103261030), Mar 26, 2021: TENSION TIE. CRACKED. CRACK ON END OF TENSION TIE AT STA 720 S13R
- [SDR KCSA202103261029](https://openairdocs.org/sdr/KCSA202103261029), Mar 26, 2021: PRESSURE DECK. CRACKED. 2 INCH CRACK IN CANTED PRESSURE DECK AT STA 1244 RBL 100
- [SDR KCSA202103261028](https://openairdocs.org/sdr/KCSA202103261028), Mar 26, 2021: PRESSURE DECK. CRACKED. 2 INCH CRACK IN CANTED PRESSURE DECK AT STA 1242 LBL 100
- [SDR KCSA202103261027](https://openairdocs.org/sdr/KCSA202103261027), Mar 26, 2021: STIFFENER. CRACKED. CRACK NOTED ON STIFFENER AT APPROX. RBL 10 STA 310 ON NWW INT.
- [SDR KCSA202103261026](https://openairdocs.org/sdr/KCSA202103261026), Mar 26, 2021: STIFFENER. CRACKED. CRACK NOTED ON STIFFENER AT APPROX. LBL 10 STA 310 ON NWW INT.
- [SDR KCSA201905211132](https://openairdocs.org/sdr/KCSA201905211132), May 21, 2019: SKIN PANEL. CORRODED. AFT FLAP UPPER SKIN PANEL AFT FASTENERS HAS CORROSION ALONG INTIRE AFT FLAP OF LT INBD.
- [SDR KCSA201905151129](https://openairdocs.org/sdr/KCSA201905151129), May 15, 2019: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK AT STA 710 RBL 11.33 IS CORRODED.
- [SDR KCSA201905151128](https://openairdocs.org/sdr/KCSA201905151128), May 15, 2019: FLOORBEAM. CORRODED. CORROSION ON MAIN DECK FLOOR BEAM AT STA 2280 RBL 42 AFT SIDE.
- [SDR KCSA201905151127](https://openairdocs.org/sdr/KCSA201905151127), May 15, 2019: SEAT TRACK. CORRODED. EVIDENCE OF CORROSION ON MAIN DECK SEAT TRACK STA 2038 LBL 100.
- [SDR KCSA201905151126](https://openairdocs.org/sdr/KCSA201905151126), May 15, 2019: SEAT TRACK. CORRODED. EVIDENCE OF CORROSION ON SEAT TRACK IN FASTENER HOLES AT STA 2100 LBL 100.
- [SDR KCSA201905151125](https://openairdocs.org/sdr/KCSA201905151125), May 15, 2019: SEAT TRACK. CORRODED. EVIDENCE OF CORROSION IN MULTIPLE FASTENER HOLES ON SEAT TRACK AT STA 2140 TO 2120 LBL 100.
- [SDR KCSA201905151124](https://openairdocs.org/sdr/KCSA201905151124), May 15, 2019: FLOORBEAM. CORRODED. EVIDENCE OF CORROSION ON TOP OF MAIN DECK FLOORBEAM STA 2160 LBL 12.
- [SDR KCSA201905091123](https://openairdocs.org/sdr/KCSA201905091123), May 9, 2019: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM AT STA 580 RBL 24 (MAIN DECK).
- [SDR KCSA201905091122](https://openairdocs.org/sdr/KCSA201905091122), May 9, 2019: SEAT TRACK. CORRODED. EVIDENCE OF CORROSION ON BOTTOM OF MAIN DECK SEAT TRACK STA 1045 LBL 76.

All 136: https://openairdocs.org/aircraft/N700CK/reports.md

## STCs that may be installed (OpenAirDocs) (5)

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 CF6-80C2B1F)

- [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 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
- [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

## Earlier aircraft with N700CK

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N700CK before.

- [Cancelled 2014-07-22](https://openairdocs.org/deregistered/N700CK-2014-07-22): Boeing 747-246B, S/N 22990. Owner: [Kalitta Air LLC](https://openairdocs.org/faa-owner/KALITTA%20AIR%20LLC), [Ypsilanti, MI](https://openairdocs.org/faa-place/MI/Ypsilanti)
- [Cancelled 2004-11-17](https://openairdocs.org/deregistered/N700CK-2004-11-17): Cameron Balloons US V-77, S/N 5162, built 1986. Triennial form not returned. Owner: [Johnson David M](https://openairdocs.org/faa-owner/JOHNSON%20DAVID%20M), [Temecula, CA](https://openairdocs.org/faa-place/CA/Temecula)

## Related

- Other Boeing 747-4R7F aircraft: https://openairdocs.org/model/boeing-747-4r7f/aircraft.md
- The GE CF6-80C2B1F engine: https://openairdocs.org/engine/ge-cf6-80c2b1f.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.