# N747CK: Boeing 747-221F, registration cancelled 2021-09-27 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 27, 2021 - Status when cancelled: Valid registration - Airframe: [Boeing 747-221F](https://openairdocs.org/model/boeing-747-221f) (registry code 13848A2) - Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE) (OpenAirDocs) - Serial number: 21743 - Type of aircraft: Fixed wing multi engine - Certificate issued: May 1, 2007 - Last registry action: November 13, 2019 - Mode S code: AA0CC7 - Owner when cancelled: [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 was based - The mark today: https://openairdocs.org/aircraft/N747CK - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=747CK - Page: https://openairdocs.org/deregistered/N747CK-2021-09-27 From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 747-221F: https://openairdocs.org/model/boeing-747-221f.md ## Service difficulty reports (55, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR KCSA111229](https://openairdocs.org/sdr/KCSA111229), Oct 4, 2011: ANGLE. CORRODED. CORROSION ON ANGLE BOTTOM OF KEEL BEAM BOX TOP WEB AT BS 1264, LBL 10 TO RBL 10. - [SDR KCSA111222](https://openairdocs.org/sdr/KCSA111222), Sep 29, 2011: SKIN. CORRODED. CORROSION ON FUSELAGE SKIN AT BS 2385, STR 35R. - [SDR KCSA111215](https://openairdocs.org/sdr/KCSA111215), Sep 23, 2011: STIFFENER. CORRODED. STIFFENER ANGLE CORRODED IN RT WLG W/W AT STA 1255 RBL 130 BWL 175. - [SDR KCSA111211](https://openairdocs.org/sdr/KCSA111211), Sep 20, 2011: DOUBLER. CORRODED. LEFT WING L/E CAVITY INTERIOR , FSSO 1530: LWR WING SKIN INTERIOR DOUBLER HAS SUSPECT CORROSION NEXT TO 1 FASTENER. - [SDR KCSA11025](https://openairdocs.org/sdr/KCSA11025), May 17, 2011: CLAMP. LOOSE. NR 4 ENGINE FIRE WARNING LIGHT AND BELL LIGHT ILLUMINATED - EXTINGUISHED WHEN ENGINE SHUT DOWN. NO BOTTLE DISCHARGED. ENGINE WINDMILLED 53 MINUTES, 33 MINUTES A - [SDR KCSA111064](https://openairdocs.org/sdr/KCSA111064), Mar 5, 2011: SKIN. CORRODED. STA 1241, CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STR. 14L & 15L FORWARD SIDE. - [SDR KCSA111063](https://openairdocs.org/sdr/KCSA111063), Mar 5, 2011: SKIN. CORRODED. CORROSION ON INTERNAL FUSELAGE SKIN FORWARD SIDE OF STA 1241 BETWEEN STR 14R & 15R. - [SDR KCSA101177](https://openairdocs.org/sdr/KCSA101177), Nov 4, 2010: LIGHT. INOPERATIVE. UPPER DECK EMERGENCY DOOR AISLE LIGHT INOPERATIVE. - [SDR KCSA091137](https://openairdocs.org/sdr/KCSA091137), Dec 14, 2009: LIGHT. INOPERATIVE. UPPER DECK EMERGENCY LIGHT ABOVE SLIDE INOP. - [SDR KCSA091122](https://openairdocs.org/sdr/KCSA091122), Oct 26, 2009: CHANNEL. CORRODED. CORROSION ON U-CHANNEL ON BOTTOM OF RT WING MLG WHEEL WELL PRESSURE DECK AT BS 1335 FUSELAGE FRAME. - [SDR KCSA091121](https://openairdocs.org/sdr/KCSA091121), Oct 26, 2009: FRAME. CORRODED. CORROSION ON AFT LOWER SIDE OF BS 1335 FUSELAGE FRAME JUST ABOVE OVERWING LONGERON. - [SDR KCSA091120](https://openairdocs.org/sdr/KCSA091120), Oct 23, 2009: STIFFENER. CRACKED. NR 2 PYLON STIFFENER CRACKED .5 INCH AT STA 221 LOWER WEB. - [SDR KCSA091119](https://openairdocs.org/sdr/KCSA091119), Oct 23, 2009: STIFFENER. DAMAGED. PYLON NR 1 STIFFENER DAMAGED AT LOWER SPAR WEB STA 221. - [SDR KCSA091118](https://openairdocs.org/sdr/KCSA091118), Oct 23, 2009: SEAT TRACK. CORRODED. STA 760 LBL 99 SEAT TRACK CORRODED. - [SDR KCSA091117](https://openairdocs.org/sdr/KCSA091117), Oct 23, 2009: STRINGER CLIP. CRACKED. FUSELAGE STRINGER CLIP IS CRACKED AT STA 1820, STR 11R. - [SDR KCSA091116](https://openairdocs.org/sdr/KCSA091116), Oct 23, 2009: STRINGER CLIP. CRACKED. FUSELAGE STRINGER CLIP IS CRACKED AT STA 1820, STR 12R. - [SDR KCSA091115](https://openairdocs.org/sdr/KCSA091115), Oct 22, 2009: SKIN. CORRODED. FUSELAGE SKIN CORRODED AT BS 2460, STR 21L. - [SDR KCSA091114](https://openairdocs.org/sdr/KCSA091114), Oct 22, 2009: SPAR. CRACKED. NR 3 PYLON LOWER MID SPAR WEB CHORD CRACKED ON I/B END. - [SDR KCSA091113](https://openairdocs.org/sdr/KCSA091113), Oct 22, 2009: SKIN. CORRODED. FUSELAGE SKIN CORRODED AT BS 985 BETWEEN STR 42L AND STR 43L. - [SDR KCSA091112](https://openairdocs.org/sdr/KCSA091112), Oct 17, 2009: LIGHT. INOPERATIVE. UPPER DECK EXIT EMERGENCY LIGHT IS INOP. - [SDR KCSA091111](https://openairdocs.org/sdr/KCSA091111), Oct 15, 2009: LIGHT. INOPERATIVE. EMERGENCY LIGHT OVER U/D RIGHT SERVICE DOOR INOP. - [SDR KCSA091110](https://openairdocs.org/sdr/KCSA091110), Oct 15, 2009: LIGHT. INOPERATIVE. STA 610 U/D EMERGENCY LIGHT INOP. - [SDR KCSA091109](https://openairdocs.org/sdr/KCSA091109), Oct 15, 2009: SHEAR TIE. CRACKED. FUSELAGE STA 860 LT FRAME SHEAR TIE CRACKED IN RADIUS, AFT SIDE OF FRAME BETWEEN STR 9L AND STR 10L. - [SDR KCSA091026](https://openairdocs.org/sdr/KCSA091026), Mar 24, 2009: BULKHEAD. CANNING. BS 2360 AFT PRESSURE BULKHEAD WEB OIL CANNED AT WL 330 LBL 40. - [SDR KCSA081342](https://openairdocs.org/sdr/KCSA081342), Jul 24, 2008: FRAME. CRACKED. NR 4 PYLON NAC STA 221.90 OUTBOARD AFT FRAME IS CRACKED .500" AT SKIN ATTACHMENT. (A) - [SDR KCSA081254](https://openairdocs.org/sdr/KCSA081254), May 20, 2008: LIGHT. INOPERATIVE. EMERGENCY LIGHT ON RIGHT UPPER DECK SLIDE HAS ONE BULB BURNED OUT. - [SDR KCSA081088](https://openairdocs.org/sdr/KCSA081088), Feb 19, 2008: STIFFENER. CRACKED. NR 3 PYLON LT UPPER STIFFENER CRACKED AT ATTACH POINT OF THE FWD ENG MOUNT BULKHEAD INTERNAL ANGLE. - [SDR KCSA081087](https://openairdocs.org/sdr/KCSA081087), Feb 19, 2008: STIFFENER. CRACKED. NR 3 PYLON RT UPPER STIFFENER CRACKED AT ATTACH ANGLE OF THE FWD ENG MOUNT BULKHEAD INTERNAL ANGLE. - [SDR KCSA071199](https://openairdocs.org/sdr/KCSA071199), Jun 29, 2007: FITTING. CRACKED. LEFT SIDE NOSE CARGO DOOR PORTAL C-3 FRAME UPPER CLOSER FITTING FASTENER HOLE IS CRACKED AT STA 285.5, WL 323. - [SDR KCSA071196](https://openairdocs.org/sdr/KCSA071196), Jun 26, 2007: STANCHION. CORRODED. AFT PIT SIDEWALL STANCHION CORRODED AT BS 1920, RBL 61. - [SDR KCSA071190](https://openairdocs.org/sdr/KCSA071190), Jun 13, 2007: FLOORBEAM. CRACKED. FLOORBEAM WEB DAMAGED AT LBL 109 TO 117 STA 1180 CRACKED 1 INCH. - [SDR KCSA071189](https://openairdocs.org/sdr/KCSA071189), Jun 11, 2007: FITTING. GOUGED. RIGHT BS 1820 FLOORBEAM END FITTING, FWD TWO FASTENERS HOLES GOUGED AND ELONGATED. - [SDR KCSA071188](https://openairdocs.org/sdr/KCSA071188), Jun 11, 2007: FLOORBEAM. CORRODED. MAIN DECK FLOORBEAM CORRODED AT BS 440, LBL 59. - [SDR KCSA071187](https://openairdocs.org/sdr/KCSA071187), Jun 7, 2007: FRAME. CORRODED. FUSELAGE FRAME AFT CHORD IS CORRODED AT STA 2598, STR 8L. - [SDR KCSA071186](https://openairdocs.org/sdr/KCSA071186), Jun 7, 2007: FITTING. CORRODED. FUSELAGE STRINGER END FITTING IS CORRODED AT STA 2598, STR 8L. - [SDR KCSA071185](https://openairdocs.org/sdr/KCSA071185), Jun 6, 2007: FLOORBEAM. CORRODED. STA 1920 RBL 60 EVIDENCE OF CORROSION ON FUSELAGE DOOR LOCK BEAM WEB. - [SDR KCSA071184](https://openairdocs.org/sdr/KCSA071184), Jun 5, 2007: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK IS CORRODED AT LBL 74 STA 1152. - [SDR KCSA071183](https://openairdocs.org/sdr/KCSA071183), Jun 5, 2007: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK IS CORRODED AT O/B FLANGE RBL 83 FROM STA 390 TO 402. - [SDR KCSA071182](https://openairdocs.org/sdr/KCSA071182), Jun 5, 2007: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK IS CORRODED AT LBL 11 FROM STA 1770 TO 1815. - [SDR KCSA071181](https://openairdocs.org/sdr/KCSA071181), Jun 4, 2007: STRINGER. DAMAGED. FUSELAGE STR 21L DAMAGED BETWEEN BS 2160 AND 2180. - [SDR KCSA071180](https://openairdocs.org/sdr/KCSA071180), Jun 4, 2007: STRINGER. BENT. FUSELAGE STR 50L HAS A BENT FLANGE BETWEEN BS 2160 AND 2180. - [SDR KCSA071179](https://openairdocs.org/sdr/KCSA071179), Jun 4, 2007: STRINGER. BENT. FUSELAGE STR 48L HAS A BENT FLANGE BETWEEN BS 2160 AND 2180. - [SDR KCSA071178](https://openairdocs.org/sdr/KCSA071178), Jun 4, 2007: STRINGER. BENT. FUSELAGE STR 49L HAS A BENT FLANGE BETWEEN BS 2160 AND 2180. - [SDR KCSA071177](https://openairdocs.org/sdr/KCSA071177), Jun 4, 2007: STRINGER. BENT. FUSELAGE STR 47L IS BENT BETWEEN BS 2160 AND 2180. - [SDR KCSA071176](https://openairdocs.org/sdr/KCSA071176), Jun 4, 2007: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK CORRODED AT BS 1152, LBL 74. - [SDR KCSA071175](https://openairdocs.org/sdr/KCSA071175), Jun 4, 2007: SPAR. CORRODED. RIGHT WING FRONT SPAR LOWER CHORD STRAP CORRODED AT FSSO 1520. - [SDR KCSA071174](https://openairdocs.org/sdr/KCSA071174), May 31, 2007: FRAME. CRACKED. STA 434 FRAME CRACKED LBL 49 WL 121 APROX .75 INCH. - [SDR KCSA071173](https://openairdocs.org/sdr/KCSA071173), May 31, 2007: CHANNEL. CHAFED. AFT BILGE FUSELAGE FRAME WEB SUPPORT CHANNEL IS CHAFFED AT STA 1680 RBL40. - [SDR KCSA071172](https://openairdocs.org/sdr/KCSA071172), May 31, 2007: ANGLE. CRACKED. NR 1 PYLON NAC STA-221 O/B ANGLE CRACKED FWD SIDE OF BULKHEAD. - [SDR KCSA071171](https://openairdocs.org/sdr/KCSA071171), May 30, 2007: FRAME. CRACKED. AFT BILGE FUSELAGE FRAME UPPER CHORD IS CRACKED AT STA 1820 AT RBL 48 1 INCH. All 55: https://openairdocs.org/deregistered/N747CK-2021-09-27/reports.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.