# N765CK: 1992 Boeing 767-3P6

- Status: Valid registration
- Airframe: [Boeing 767-3P6](https://openairdocs.org/model/boeing-767-3p6) (registry code 1385105, 290 seats)
- Engine: [GE CF6-80C2B6](https://openairdocs.org/engine/ge-cf6-80c2b6) (registry code 30103)
- Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 26238
- Year built: 1992
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 12, 2018
- Certificate issued: May 18, 2018
- Expires: May 31, 2028
- Mode S code: AA5457
- 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=765CK
- Page: https://openairdocs.org/aircraft/N765CK

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): 31 in force

### Matched by airframe (Boeing 767-3P6)

None in force.

### Matched by engine (GE CF6-80C2B6)

- [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 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 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
- [AD 91-05-21](https://openairdocs.org/ad/91-05-21): High Pressure Turbine · General Electric CF6-80C2A5, CF6-80C2B6, CF6-80C2B6F and 1 more. Effective Mar 27, 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 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 N765CK.

## FAA accident and incident reports

None matched to N765CK.

## Service difficulty reports (124, 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 21GA202504160002](https://openairdocs.org/sdr/21GA202504160002), Apr 11, 2025: FITTING. DAMAGED. RH FAIRING SUPPORT #7 FLAP REPAIR.
- [SDR 21GA202504161010](https://openairdocs.org/sdr/21GA202504161010), Apr 11, 2025: FITTING. CRACKED. RH FAIRING IB #7 FLAP SUPPORT CRACK REPAIR.
- [SDR 21GA20250411008](https://openairdocs.org/sdr/21GA20250411008), Apr 11, 2025: SPLICE ANGLE. DAMAGED. R1 DOOR CUTOUT REPAIR FASTENER HOLE OVAL.
- [SDR 21GA20250411007](https://openairdocs.org/sdr/21GA20250411007), Apr 11, 2025: SUPPORT FITTING. DAMAGED. #1 FLAP SUPPORT FITTING FASTNER HOLE DAMAGED.
- [SDR 21GA20250411006](https://openairdocs.org/sdr/21GA20250411006), Apr 11, 2025: SHEAR TIE. CORRODED. ANGLE CONNECTING FRAME TO SKIN IN LH NOSE WHEEL WELL CORRODED.
- [SDR 21GA20250411005](https://openairdocs.org/sdr/21GA20250411005), Apr 11, 2025: SUPPORT FITTING. DAMAGED. LH FAIRING SUPPORT #1 FLAP FITTING ASSY DAMAGED.
- [SDR 21GA20230911012](https://openairdocs.org/sdr/21GA20230911012), Sep 11, 2023: STRINGER. CORRODED. CORROSION FOUND ON SURFACE HFEC AT HORZ STAB UPPER STRINGER S-9L AND LBL 39 ON LOWER AFT FLANGE UPPER SURFACE.
- [SDR 21GA20230911011](https://openairdocs.org/sdr/21GA20230911011), Sep 11, 2023: STRINGER. CORRODED. CORROSION FOUN DURING SURFACE HFEC AT HORZ STAB UPPER STRINGER S-5L AND LBL 39 ON LOWER AFT FLANGE UPPER SURFACE. REPAIRED PER KALITTA DWG 55102302-1 OR.
- [SDR 21GA20230911010](https://openairdocs.org/sdr/21GA20230911010), Sep 11, 2023: STRINGER. CORRODED. FOUND SURFACE CORROSION ON HORIZONTAL STABILIZER UPPER STRINGER S-10R AND RBL 39 ON LOWER FLANGE. REPAIRED PER KALITTA DWG 55102304-1.
- [SDR 21GA20230911009](https://openairdocs.org/sdr/21GA20230911009), Sep 11, 2023: FRAME. CORRODED. CORROSION FOUND ON AFT LOWER SIDE OF PRESSURE DECK FRAME AT STA 977, RBL 97. REPAIRED PER KALITTA DWG 53502301.1-OR
- [SDR 21GA20230911008](https://openairdocs.org/sdr/21GA20230911008), Sep 11, 2023: STIFFENER. CRACKED. DURING ACCOMPLISHMENT OF AD 2005-02-02. CRACK INDICATION WAS FOUND EXTENDING BELOW WL 160. REPAIR WAS ACCOMPLISHED PER BOEING.
- [SDR 21GA20230803007](https://openairdocs.org/sdr/21GA20230803007), Jul 31, 2023: LAMP. BLOWN. FLIGHT DECK EMERGENCY LIGHT INOPERATIVE.
- [SDR 21GA20230614006](https://openairdocs.org/sdr/21GA20230614006), Jun 14, 2023: UNKNOWN. UNKNOWN. AFTER TAKEOFF, TCAS FAILED AND CB POPPED. RESET CB. ONE HOUR INTO FLIGHT GOT MESSAGE FWD EQUIP COOLING AND SMELLED SMOKE. PULLED TCAS CB AND SMELL SLOWLY DISSIP
- [SDR 21GA20221227006](https://openairdocs.org/sdr/21GA20221227006), Dec 22, 2022: SKIN. CORRODED. CORROSION AND CRACK FOUND ON LOWER FUSELAGE SECTION 46 SKIN, BS 1210, S39R.
- [SDR KCSA202202091014](https://openairdocs.org/sdr/KCSA202202091014), Feb 9, 2022: LIGHT. INOPERATIVE. L1 DOOR WINDOW SILL EMERGENCY LAMP (L313) FAILS TO ILLUMINATE
- [SDR KCSA202202091013](https://openairdocs.org/sdr/KCSA202202091013), Feb 9, 2022: LIGHT. INOPERATIVE. L1 DOOR EXIT SIGN FAILS TO ILLUMINATE
- [SDR KCSA202202091012](https://openairdocs.org/sdr/KCSA202202091012), Feb 9, 2022: LIGHT. INOPERATIVE. RIGHT OVERHEAD EMERGENCY LAMP ON FLIGHT DCK FAILS TO ILLUMINATE
- [SDR KCSA202201311011](https://openairdocs.org/sdr/KCSA202201311011), Jan 31, 2022: WEB. DAMAGED. WEB FLOOR DAMAGED AT APPROX STA. 548-566 RBL 31-38
- [SDR KCSA202201311010](https://openairdocs.org/sdr/KCSA202201311010), Jan 31, 2022: INTERCOSTAL. DAMAGED. INTERCOSTAL DAMAGED AT APPROX STA. 510 RB2 46-54
- [SDR KCSA202201311009](https://openairdocs.org/sdr/KCSA202201311009), Jan 31, 2022: DOOR SILL. CORRODED. FORWARD CARGO COMPARTMENT DOOR CUTOUT SURROUND - LWR SILL AREA @ APPROX. STA 585 HAS EVIDENCE OF CORROSION
- [SDR KCSA202201311008](https://openairdocs.org/sdr/KCSA202201311008), Jan 31, 2022: SEAT TRACK. CRACKED. CAPTAIN`S FWD INBOARD SEAT TRACK IS CRACKED ON FWD END
- [SDR KCSA2020112419](https://openairdocs.org/sdr/KCSA2020112419), Nov 24, 2020: TARGET. INCORRECT. LEADING EDGE ASYMMETRIC. FOUND INBOARD AND OUTBOARD LEADING EDGE SLAT SENSOR TARGETS SWAPPED. REPOSITIONED TO CORRECT POSITIONS, IAW B767 AMM 20-11-00. OPERATIO
- [SDR KCSA202007011106](https://openairdocs.org/sdr/KCSA202007011106), Jul 1, 2020: FUEL TANK. CORRODED. EVIDENCE OF CORROSION AROUND FASTENER HEADS OF TOP SURFACE OF CENTER FUEL TANK AT APPROX STA 958 LBL 18.
- [SDR KCSA202006221093](https://openairdocs.org/sdr/KCSA202006221093), Jun 22, 2020: FITTING. CHAFED. RIGHT INBOARD AILERON, OUTBOARD FAIL-SAFE FITTING HAS CHAFING DAMAGE.
- [SDR KCSA202006221092](https://openairdocs.org/sdr/KCSA202006221092), Jun 22, 2020: FITTING. CORRODED. EVIDENCE OF CORROSION INSIDE THE BORE OF MDCD LATCH PIN FITTING NR 7 P/N 95345-203.
- [SDR KCSA202006221091](https://openairdocs.org/sdr/KCSA202006221091), Jun 22, 2020: FITTING. CORRODED. EVIDENCE OF CORROSION INSIDE THE BORE OF MDCD LATCH PIN FITTING NR 4 P/N 95345-204.
- [SDR KCSA202006171088](https://openairdocs.org/sdr/KCSA202006171088), Jun 17, 2020: KEELBEAM. CORRODED. EVIDENCE OF CORROSION TOP SIDE OF LT LOWER KEEL BEAM CHORD APPROX STA 795.
- [SDR KCSA202006111087](https://openairdocs.org/sdr/KCSA202006111087), Jun 11, 2020: KEELBEAM. CORRODED. EVIDENCE OF CORROSION TOP SIDE OF L/H LOWER KEEL BEAM CHORD APPROX STA 898
- [SDR KCSA202006111086](https://openairdocs.org/sdr/KCSA202006111086), Jun 11, 2020: KEELBEAM. CORRODED. EVIDENCE OF CORROSION TOP SIDE OF L/H LOWER KEEL BEAM CHORD APPROX STA 921
- [SDR KCSA202006111085](https://openairdocs.org/sdr/KCSA202006111085), Jun 11, 2020: KEELBEAM. CORRODED. EVIDENCE OF CORROSION TOP SIDE OF R/H LOWER KEEL BEAM CHORD APPROX STA 911
- [SDR KCSA202006111084](https://openairdocs.org/sdr/KCSA202006111084), Jun 11, 2020: KEELBEAM. CORRODED. EVIDENCE OF CORROSION TOP SIDE OF R/H LOWER KEEL BEAM CHORD APPROX STA 914
- [SDR KCSA202006111083](https://openairdocs.org/sdr/KCSA202006111083), Jun 11, 2020: KEELBEAM. CORRODED. EVIDENCE OF CORROSION TOP SIDE OF R/H LOWER KEEL BEAM CHORD APPROX STA 954
- [SDR KCSA201812061338](https://openairdocs.org/sdr/KCSA201812061338), Dec 6, 2018: STOP FITTING. CORRODED. AFT CARGO DOOR AFT HOOK STOP FITTING CORRODED.
- [SDR KCSA201812061337](https://openairdocs.org/sdr/KCSA201812061337), Dec 6, 2018: MOUNT FITTING. CORRODED. LT O/B FLAP SUPPORT MECHANISM FLAP SUPPORT TO WING REAR SPAR FITTING ON O/B MOUNT INSIDE BORE HAS CORROSION.
- [SDR KCSA201811291336](https://openairdocs.org/sdr/KCSA201811291336), Nov 29, 2018: FRAME. CORRODED. FRAME UPPER CHORD HAS CORROSION AT STA 1285 RBL 35.
- [SDR KCSA201811291335](https://openairdocs.org/sdr/KCSA201811291335), Nov 29, 2018: TORQUE BOX. CORRODED. EVIDENCE OF CORROSION ON TORQUE BOX WEB IN AFT CARGO COMPARTMENT AT STA 1272 - 1280, RBL 11 - 16.
- [SDR KCSA201811291334](https://openairdocs.org/sdr/KCSA201811291334), Nov 29, 2018: DOOR SILL. CORRODED. EVIDENCE OF CORROSION ON AFT CARGO COMPARTMENT DOOR LOWER SILL WEB AT STA 1367 RBL 45.
- [SDR KCSA201811291333](https://openairdocs.org/sdr/KCSA201811291333), Nov 29, 2018: TORQUE BOX. CORRODED. TORQUE BOX WEB BS 1263 - 1285 RBL 38 SHOWS EVIDENCE OF CORROSION.
- [SDR KCSA201811291332](https://openairdocs.org/sdr/KCSA201811291332), Nov 29, 2018: INTERCOSTAL. CORRODED. FWD PIT TORQUE BOX INTERCOSTAL HAS EVIDENCE OF CORROSION AT STA 610 RBL 24.
- [SDR KCSA201811271331](https://openairdocs.org/sdr/KCSA201811271331), Nov 27, 2018: ACCESS PANEL. CORRODED. WEB ACCESS PANEL HAS CORROSION AT STA 1263 - 1285 LBL 32 - 39.
- [SDR KCSA201811271330](https://openairdocs.org/sdr/KCSA201811271330), Nov 27, 2018: ACCESS PANEL. CORRODED. WEB ACCESS PANEL HAS CORROSION AT STA 1263 TO 1285 RBL 17 - 33.
- [SDR KCSA201811261329](https://openairdocs.org/sdr/KCSA201811261329), Nov 26, 2018: SUPPORT. CORRODED. CORROSION ON SUPPORT AT STA 1263-1285 LBL 33.
- [SDR KCSA201811261328](https://openairdocs.org/sdr/KCSA201811261328), Nov 26, 2018: FRAME. CORRODED. EVIDENCE OF CORROSION ON UPPER CHORD IN AFT PIT FLOOR, STA 1285 APPROX RBL 25.
- [SDR KCSA201811261327](https://openairdocs.org/sdr/KCSA201811261327), Nov 26, 2018: FRAME. CORRODED. FWD PIT LWR FRAME UPPER CHORD HAS EVIDENCE OF CORROSION STA 654 +44 LBL 20.
- [SDR KCSA201811261326](https://openairdocs.org/sdr/KCSA201811261326), Nov 26, 2018: INTERCOSTAL. CORRODED. EVIDENCE OF CORROSION ON AFT CARGO FLOOR INTERCOSTAL STA 1329 LBL 25.
- [SDR KCSA201811211325](https://openairdocs.org/sdr/KCSA201811211325), Nov 21, 2018: FRAME. CORRODED. FRAME UPPER CHORD HAS CORROSION @ STA 1197 +22
- [SDR KCSA201811201324](https://openairdocs.org/sdr/KCSA201811201324), Nov 20, 2018: FRAME. CORRODED. EVIDENCE OF CORROSION ON AFT CORGO COMPARTMENT FLOOR FRAME UPPER CHORD AT STA 1263 RBL 22
- [SDR KCSA201811201323](https://openairdocs.org/sdr/KCSA201811201323), Nov 20, 2018: WEB. CORRODED. EVIDENCE OF CORROSION ON TORQUE BOX WEB @ STA 630 RBL 30 IN FWD PIT
- [SDR KCSA201811191322](https://openairdocs.org/sdr/KCSA201811191322), Nov 19, 2018: STIFFENER. CORRODED. EVIDENCE OF CORROSION ON STIFFENER AT STA 1809.5 BULKHEAD RBL 5
- [SDR KCSA201811161318](https://openairdocs.org/sdr/KCSA201811161318), Nov 16, 2018: INTERCOSTAL. CORRODED. FWD PIT TORQUE BOX INTERCOSTAL HAS EVIDENCE OF CORROSION @ STA 610 RBL 27

All 124: https://openairdocs.org/aircraft/N765CK/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 CF6-80C2B6)

- [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 SE00969CH](https://openairdocs.org/stc/SE00969CH): Install AeroControlex P/N 2605290-001 variable stator feedback control cable. AeroControlex Group TransDigm Inc
- [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

## Related

- Other Boeing 767-3P6 aircraft: https://openairdocs.org/model/boeing-767-3p6/aircraft.md
- The GE CF6-80C2B6 engine: https://openairdocs.org/engine/ge-cf6-80c2b6.md

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