# N713CK: 2003 Boeing 747-4B5F

- Status: Valid registration
- Airframe: [Boeing 747-4B5F](https://openairdocs.org/model/boeing-747-4b5f) (registry code 13848BH, 490 seats)
- Engine: [Pratt & Whitney PW4056](https://openairdocs.org/engine/pratt-whitney-pw4056) (registry code 51665)
- Data sheets: [TCDS E24NE](https://openairdocs.org/tcds/E24NE) (Pratt & Whitney Division) (OpenAirDocs)
- Serial number: 32808
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 18, 2018
- Certificate issued: March 29, 2018
- Expires: March 31, 2028
- Mode S code: A9876E
- 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=713CK
- Page: https://openairdocs.org/aircraft/N713CK

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): 25 in force

### Matched by airframe (Boeing 747-4B5F)

None in force.

### Matched by engine (Pratt & Whitney PW4056)

- [AD 2026-21-06](https://openairdocs.org/ad/2026-21-06): Engine Fuel and Control · Pratt & Whitney Division PW4052, PW4056, PW4060 and 10 more. Effective Nov 23, 2026
- [AD 2018-13-02](https://openairdocs.org/ad/2018-13-02): Turbine Engine Combustion Section · Pratt & Whitney Division PW4052, PW4056, PW4060 and 7 more. Effective Jul 20, 2018
- [AD 2016-08-09](https://openairdocs.org/ad/2016-08-09): HPC 10th stage disk · Pratt & Whitney Division PW4050, PW4052, PW4056 and 24 more. Effective Jun 1, 2016
- [AD 2015-22-03](https://openairdocs.org/ad/2015-22-03): LPT 4th stage IAS · Pratt & Whitney Division PW4050, PW4052, PW4056 and 24 more. Effective Dec 1, 2015
- [AD 2012-22-16](https://openairdocs.org/ad/2012-22-16): 3rd stage LPT duct segments · Pratt & Whitney Division PW4050, PW4052, PW4056 and 13 more. Effective Dec 19, 2012
- [AD 2012-14-09](https://openairdocs.org/ad/2012-14-09): 3rd and 4th stage vane fractures · Pratt & Whitney Division PW4050, PW4052, PW4056 and 24 more. Effective Nov 7, 2012
- [AD 2012-18-17](https://openairdocs.org/ad/2012-18-17): HPC drum rotor disk assembly · Pratt & Whitney Division PW4052, PW4056, PW4060 and 16 more. Effective Oct 22, 2012
- [AD 2012-18-03](https://openairdocs.org/ad/2012-18-03): 1st stage HPT air seal rings · Pratt & Whitney Division PW4050, PW4052, PW4056 and 18 more. Effective Oct 11, 2012
- [AD 2012-16-01](https://openairdocs.org/ad/2012-16-01): High-pressure turbine (HPT) stage 1 front hubs · Pratt & Whitney Division PW4052, PW4056, PW4060 and 14 more. Effective Sep 28, 2012
- [AD 2012-06-18](https://openairdocs.org/ad/2012-06-18): Engine · Pratt & Whitney Division PW4050, PW4052, PW4056 and 13 more. Effective Apr 27, 2012
- [AD 2012-04-04](https://openairdocs.org/ad/2012-04-04): fuel metering units (FMUs) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 13 more. Effective Apr 5, 2012
- [AD 2011-25-09](https://openairdocs.org/ad/2011-25-09): PW4000 turbofan engines · Pratt & Whitney Division PW4050, PW4052, PW4056 and 18 more. Effective Jan 10, 2012
- [AD 2010-24-14](https://openairdocs.org/ad/2010-24-14): HPC 10th stage disk · Pratt & Whitney Division PW4050, PW4052, PW4056 and 17 more. Effective Jan 21, 2011
- [AD 2010-24-09](https://openairdocs.org/ad/2010-24-09): No. 3 bearing oil pressure tubes · Pratt & Whitney Division PW4050, PW4052, PW4056 and 34 more. Effective Dec 28, 2010
- [AD 2008-24-13](https://openairdocs.org/ad/2008-24-13): Electronic engine controls (EECs) · Pratt & Whitney Division PW4052, PW4056, PW4060 and 6 more. Effective Jan 8, 2009
- [AD 2005-25-09](https://openairdocs.org/ad/2005-25-09): Engine manufacturer's time limits section (TLS) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 26 more. Effective Jun 12, 2006
- [AD 2003-19-15](https://openairdocs.org/ad/2003-19-15): High-Pressure-Compressor (HPC) Surges · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Oct 30, 2003
- [AD 2002-12-15](https://openairdocs.org/ad/2002-12-15): Front Drum Rotors · Pratt & Whitney Division PW4052, PW4056, PW4060 and 6 more. Effective Jul 31, 2002
- [AD 2001-05-07](https://openairdocs.org/ad/2001-05-07): Low Pressure Turbine (LPT) 4th Stage Air Seal · Pratt & Whitney Division PW4052, PW4056, PW4060 and 11 more. Effective Mar 30, 2001
- [AD 99-15-01](https://openairdocs.org/ad/99-15-01): Low Pressure Turbine Disks · Pratt & Whitney Division PW4056, PW4152, PW4156A and 3 more. Effective Sep 14, 1999
- [AD 98-23-08](https://openairdocs.org/ad/98-23-08): High Pressure Compressor  Blade Tips · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Jan 12, 1999
- [AD 98-19-03](https://openairdocs.org/ad/98-19-03): High Pressure Turbine Rotating Airseals · Pratt & Whitney Division PW4052, PW4056, PW4060 and 9 more. Effective Nov 9, 1998
- [AD 96-13-08](https://openairdocs.org/ad/96-13-08): AFT Cascade Support Frame Assembly · Pratt & Whitney assembly Part Number 221D5015, Revision A (STC SE744NE). Effective Aug 1, 1996
- [AD 93-08-16](https://openairdocs.org/ad/93-08-16): Fuel Pump · Pratt & Whitney Division PW4050, PW4052, PW4056 and 2 more. Effective Jul 12, 1993
- [AD 90-22-02](https://openairdocs.org/ad/90-22-02): Low Pressure Turbine Shaft · Pratt & Whitney Division PW4050, PW4052, PW4056 and 6 more. Effective Oct 18, 1990

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

- [AD 2010-18-13](https://openairdocs.org/ad/2010-18-13) (historical): Blade · Pratt & Whitney Division PW4052, PW4056, PW4060 and 16 more. Effective Oct 18, 2010
- [AD 2003-11-18](https://openairdocs.org/ad/2003-11-18) (historical): High-Pressure-Compressor (HPC) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Jul 7, 2003
- [AD 2002-21-10](https://openairdocs.org/ad/2002-21-10) (historical): High pressure compressor (HPC) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Nov 12, 2002
- [AD 2002-03-08](https://openairdocs.org/ad/2002-03-08) (historical): Time Limits Section of Engine Manuals (EM's) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 25 more. Effective Apr 16, 2002
- [AD 2001-25-11](https://openairdocs.org/ad/2001-25-11) (historical): Compressor Surges · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Jan 17, 2002
- [AD 2001-20-13](https://openairdocs.org/ad/2001-20-13) (historical): High Pressure Compressor Front Drum Rotors · Pratt & Whitney Division PW4052, PW4056, PW4060 and 6 more. Effective Nov 16, 2001
- [AD 2001-15-12](https://openairdocs.org/ad/2001-15-12) (historical): High Pressure Compressors (HPC) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Aug 10, 2001
- [AD 2001-09-07](https://openairdocs.org/ad/2001-09-07) (historical): High Pressure Compressor (HPC) Surge · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective May 14, 2001
- [AD 2001-08-52](https://openairdocs.org/ad/2001-08-52) (historical): Multiple-engine power loss due to HPC surges · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more
- [AD 2000-25-06](https://openairdocs.org/ad/2000-25-06) (historical): Low Pressure Turbine (LPT) 4th Stage Air Seal · Pratt & Whitney Division PW4052, PW4056, PW4060 and 11 more. Effective Dec 29, 2000
- [AD 2000-22-01](https://openairdocs.org/ad/2000-22-01) (historical): High Pressure Compressor Cutback Stator · Pratt & Whitney Division PW4050, PW4052, PW4056 and 6 more. Effective Nov 9, 2000
- [AD 2000-12-02](https://openairdocs.org/ad/2000-12-02) (historical): Critical Life-Limited Part · Pratt & Whitney Division PW4050, PW4052, PW4056 and 24 more. Effective Sep 13, 2000
- [AD 99-17-16](https://openairdocs.org/ad/99-17-16) (historical): Pratt & Whitney Division PW4050, PW4052, PW4056 and 11 more. Effective Sep 24, 1999
- [AD 99-08-15](https://openairdocs.org/ad/99-08-15) (historical): Pratt & Whitney Division PW4050, PW4052, PW4056 and 20 more. Effective May 13, 1999

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

- [SAIB 2025-06](https://openairdocs.org/saib/2025-06): High Pressure Turbines. Issued Jul 22, 2025
- [SAIB NE-19-02](https://openairdocs.org/saib/NE-19-02): Turbine Engine Compressor Section -- Low-pressure turbine uncontainment. Issued Feb 19, 2019
- [SAIB NE-16-01R1](https://openairdocs.org/saib/NE-16-01R1): Turbine Section. Issued Jan 14, 2016
- [SAIB NE-15-19](https://openairdocs.org/saib/NE-15-19): Turbine Section. Issued Jul 14, 2015
- [SAIB NE-13-31](https://openairdocs.org/saib/NE-13-31): Turbine Engine Oil System  Scavenge Oil Tube Coking and Proper Cleaning at Overhaul. Issued May 9, 2013
- [SAIB NE-16-01](https://openairdocs.org/saib/NE-16-01) (historical): Turbine Section. Issued Oct 5, 2015

## NTSB investigations

None matched to N713CK.

## FAA accident and incident reports

None matched to N713CK.

## Service difficulty reports (45)

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 KCSA2026092757](https://openairdocs.org/sdr/KCSA2026092757), Sep 27, 2026: BEARING. FAULTED. FLAPS DRIVE EICAS QRH. R & R TORQUE TUBE SUPPORT BEARING ASSY ON RT WING BETWEEN WS 128.45-515 IAW AMM 27-51-20. OPS CHECK IAW AMM 27-51-00. OPS CHECK GOOD NO D
- [SDR KCSA202609091207](https://openairdocs.org/sdr/KCSA202609091207), Sep 9, 2026: WEB. CRACKED. DURING W/O 713028794 SURFACE HFEC INSPECTION AT RT WBL 432.65 FIXED RIB WB, CRACK FOUND.
- [SDR KCSA202609091206](https://openairdocs.org/sdr/KCSA202609091206), Sep 9, 2026: SKIN. DAMAGED. FOUND LIGHTNING STRIKE DAMAGES ON THE UPPER FUSELAGE AREA BS 600 S-0 TO S-1L ( 2 SPOTS).
- [SDR KCSA202609091205](https://openairdocs.org/sdr/KCSA202609091205), Sep 9, 2026: SKIN. DAMAGED. FOUND A LIGHTNING STRIKE DAMAGE ON THE UPPER FUSELAGE AREA. STA 680 TO 700, S-0 TO S-1R
- [SDR KCSA202609091204](https://openairdocs.org/sdr/KCSA202609091204), Sep 9, 2026: FRAME. CRACKED. DURING EO 5312-21-02 OPEN HOLE HFEC INSPECTION, A CRACK SIGNAL INDICATION ON FRAME AT BS 860 RT 3 EA HOLE.
- [SDR KCSA202609091203](https://openairdocs.org/sdr/KCSA202609091203), Sep 9, 2026: TENSION TIE. CRACKED. DURING EO 5312-21-02 INSPECTION, A CRACK WAS FOUND IN THE RT 860 TENSION TIE FWD CHANNEL.
- [SDR KCSA202609091202](https://openairdocs.org/sdr/KCSA202609091202), Sep 9, 2026: TENSION TIE. CRACKED. DURING OPEN HOLE INSPECTION, EO 5312-21-02, CRACK SIGNAL INDICATION AT L/H STA 860 3 EA FRAME HOLE
- [SDR KCSA202609091201](https://openairdocs.org/sdr/KCSA202609091201), Sep 9, 2026: FRAME. CRACKED. DURING OPEN HOLE HFEC INSPECTION, CRACK SIGNAL INDICATIONAT LT BS 840 FRAME AND CHORD 3EA, FWD DOUBLER 1 EA, AFT DOUBLER 1 EA.
- [SDR KCSA202609091200](https://openairdocs.org/sdr/KCSA202609091200), Sep 9, 2026: TENSION TIE. CRACKED. DURING EO 5312-21-02 INSPECTION, A CRACK WAS FOUND IN THE LT BS 860 TENSION TIE FWD CHANNEL
- [SDR KCSA202609091199](https://openairdocs.org/sdr/KCSA202609091199), Sep 9, 2026: TENSION TIE. CRACKED. DURING EO 5312-21-02 INSPECTION, A CRACK WAS FOUND IN THE LT 840 TENSION TIE FWD CHANNEL.
- [SDR KCSA202609091198](https://openairdocs.org/sdr/KCSA202609091198), Sep 9, 2026: TENSION TIE. CRACKED. ONE HOLE CRACK INDICATION FOUND DURING OPEN HOLE HFEC INSPECTION OF THE LT BS 820 AFT CHANNEL.
- [SDR KCSA202609091197](https://openairdocs.org/sdr/KCSA202609091197), Sep 9, 2026: TENSION TIE. CRACKED. DURING OPEN HOLE HFEC INSPECTION, CRACK SIGNAL INDICATIONAT LT BS 720 FWD CHANNEL.
- [SDR KCSA2026090854](https://openairdocs.org/sdr/KCSA2026090854), Sep 8, 2026: BATTERY. INOPERATIVE. TWO EMERGENCY LIGHTS INOPERATIVE ON CEILING TOWARDS REAR OF CABIN AREA. REMOVED & REPLACED BATTERY POWER SUPPLY, ALL CHECKS GOOD IAW AMM 33-51-04.
- [SDR KCSA202507081109](https://openairdocs.org/sdr/KCSA202507081109), Jul 8, 2025: FRAME. GOUGED. R/H ELEVATOR STA 231 HAS GOUGE ON THE COUNTER BALANCE FRAME
- [SDR KCSA202408151107](https://openairdocs.org/sdr/KCSA202408151107), Aug 15, 2024: HINGE BRACKET. CRACKED. FWD LOWER CARGO DOOR AFT HINGE MECHANISM DOOR MOUNT BRACKET HAS EVIDENCE OF A CRACK
- [SDR KCSA202408151106](https://openairdocs.org/sdr/KCSA202408151106), Aug 15, 2024: ANGLE. CRACKED. FWD CARGO DOOR FWD HINGE HAS CRACKED ANGLE ON DOOR SIDE
- [SDR KCSA202408151105](https://openairdocs.org/sdr/KCSA202408151105), Aug 15, 2024: ATTACH FITTING. CRACKED. #1 PYLON TURBINE DRIVE OTBD MOUNT STRUCTURE IS CRACKED.
- [SDR KCSA2024032111](https://openairdocs.org/sdr/KCSA2024032111), Mar 21, 2024: GASKET. LOOSE. L1 DOOR GASKET HAS LOOSE SECTION. REINSTALLED ACOUSTIC AND THERMAL SEAL IAW AMM 52-09-06 ALL CHECKS GOOD NO DEFECTS NOTED.
- [SDR KCSA2023112048](https://openairdocs.org/sdr/KCSA2023112048), Nov 20, 2023: ESCAPE REEL. UNSERVICEABLE. ESCAPE REEL #6 REMOVED FOR COMPANY CONVENIENCE IAW AMM 25-61-01. TRANSFERRED TO DMI #100051381 IAW MEL 25-61-1-1-1 CATEGORY C DUE 11-30-2023 "MAINTENANCE" PROCE
- [SDR KCSA20231121048](https://openairdocs.org/sdr/KCSA20231121048), Nov 20, 2023: ESCAPE REEL. UNSERVICEABLE. ESCAPE REEL #6 REMOVED FOR COMPANY CONVENIENCE IAW AMM 25-61-01. TRANSFERRED TO DMI #100051381 IAW MEL 25-61-1-1-1 CATEGORY C DUE 11-30-2023 "MAINTENANCE" PROCE
- [SDR KCSA202309221114](https://openairdocs.org/sdr/KCSA202309221114), Sep 22, 2023: ESCAPE REEL. DEFECTIVE. UPPER DECK DESCENT DEVICE #8 SEAL BROKEN P/N 3790103 D-23 S/N 19691
- [SDR KCSA202309221113](https://openairdocs.org/sdr/KCSA202309221113), Sep 22, 2023: ESCAPE REEL. DEFECTIVE. UPPER DECK DESCENT DEVICE #1 SEAL BROKEN P/N 379103 D-23 S/N 0001
- [SDR KCSA202309221112](https://openairdocs.org/sdr/KCSA202309221112), Sep 22, 2023: LIGHT. INOPERATIVE. EMERGENCY LIGHT ABOVE L1 DOOR INOP
- [SDR KCSA202306231071](https://openairdocs.org/sdr/KCSA202306231071), Jun 23, 2023: LIGHT. INOPERATIVE. CREW BUNK AREA EMERGENCY LIGHT INOP
- [SDR KCSA202301031001](https://openairdocs.org/sdr/KCSA202301031001), Jan 3, 2023: STRUCTURE. DAMAGED. L/H WING O/B AFT FLAP DAMAGED AT SITE OF PREVIOUS REPAIR AT WBL 786.5
- [SDR KCSA202301031000](https://openairdocs.org/sdr/KCSA202301031000), Jan 3, 2023: STRUCTURE. DAMAGED. L/H WING O/B AFT FLAP DAMAGED AT SITE OF PREVIOUS REPAIR AT WBL 807.5.
- [SDR KCSA2022073116](https://openairdocs.org/sdr/KCSA2022073116), Jul 31, 2022: FAN. FAILED. CREW ADVISED OF BURNT ELECTRICAL SMELL IN COCKPIT ON DESCENT. ACCOMPISHED CONDITIONAL INSPECTION 05-51-56 PER SMOKE OR FUMES IN CABIN. ACCOMPLISHED FIM 21-00 TA
- [SDR KCSA2021032208](https://openairdocs.org/sdr/KCSA2021032208), Mar 22, 2021: EEC. MALFUNCTIONED. IN CRUISE #2 ENGINE ENGINE PRESSURE RATIO, N1, N2 & FUEL FLOW FLUCTUATIONS. REMOVE AND REPLACE #2 ENGINE ELECTRONIC ENGINE CONTROL IAW B747-400 AMM 73-21-04. OP
- [SDR KCSA2020090214](https://openairdocs.org/sdr/KCSA2020090214), Sep 2, 2020: FIRE DETECTOR. DEFECTIVE. FIRE WHEEL WELL. PER FIM 26-17 801. CHECKED WIRING FOR DAMAGE, CHAFFING, AND CORROSION. NO DEFECTS NOTED. CHECKED FOR CONTINUITY AT PIN 10 OF RELAY TO GROUND, F
- [SDR KCSA202008191135](https://openairdocs.org/sdr/KCSA202008191135), Aug 19, 2020: HINGE FITTING. CRACKED. CRACK FOUND AT UPPER OUTBOARD FASTENER HOLE HINGE FITTING RBL 43.50 REAR SPAR UPPER CHORD RT HORIZONTAL STAB BOX, SEE R.E.S 2016068-043 FIG #1 SHEET 2 FOR REF.
- [SDR KCSA202007151124](https://openairdocs.org/sdr/KCSA202007151124), Jul 15, 2020: FITTING. CRACKED. CRACK NOTED WHILE DOING HFEC EXTERNAL INSP AT RIGHT LONGERON EXTENTION FITTING (APPROX LENGTH 0.400" AT 4 O'CLOCK POS) AT STA 1480.
- [SDR KCSA202007151123](https://openairdocs.org/sdr/KCSA202007151123), Jul 15, 2020: FITTING. CRACKED. CRACK NOTED WHILE DOING HFEC EXTERNAL INSP AT LEFT LONGERON EXTENTION FITTING (APPROX LENGTH 0.500" AT 8 O'CLOCK POS) AT STA 1480.
- [SDR KCSA202005281072](https://openairdocs.org/sdr/KCSA202005281072), May 28, 2020: FRAME. DAMAGED. FRAME DAMAGE AT STA 2669 INTERCOSTAL ATTACHMENT POINT WL 310.
- [SDR KCSA202005281071](https://openairdocs.org/sdr/KCSA202005281071), May 28, 2020: FASTENER. LOOSE. MULTIPLE LOOSE FASTENERS ON RT SIDE OF EMPENNAGE B, STA 2680-2700 AND WL 292.5.
- [SDR KCSA20190625007](https://openairdocs.org/sdr/KCSA20190625007), Jun 20, 2019: FIRE WARNING. ACTIVATED. FIRE WHEEL WELL EICAS WARNING AT APPROXIMATELY 3800', FLAPS 1.
- [SDR KCSA201810100507](https://openairdocs.org/sdr/KCSA201810100507), Oct 5, 2018: ESCAPE REEL. UNSECURE. 3 ESCAPE REELS FELL OUT OF SPOT. INSTALLED THE 3 MISSING ESCAPE REELS IAW AMM 25-61-01. POSITION NR 6 PN: 379103D-23 SN: 22966, POSITION NR 7 PN: 379103D-23 SN:
- [SDR KCSA201807121195](https://openairdocs.org/sdr/KCSA201807121195), Jul 12, 2018: FLAP TRACK. CORRODED. NR 8 T/E FLAP TRACK I/B SIDE LOAD BEARING AREA WORN AND CORRODED.
- [SDR KCSA201807121194](https://openairdocs.org/sdr/KCSA201807121194), Jul 12, 2018: FLAP TRACK. CORRODED. NR 7 T/E FLAP TRACK I/B SIDE LOAD BEARING AREA WORN AND CORRODED.
- [SDR KCSA201807121193](https://openairdocs.org/sdr/KCSA201807121193), Jul 12, 2018: FLAP TRACK. CORRODED. NR 6 T/E FLAP TRACK I/B SIDE LOAD BEARING AREA WORN AND CORRODED.
- [SDR KCSA201807121192](https://openairdocs.org/sdr/KCSA201807121192), Jul 12, 2018: FLAP TRACK. CORRODED. NR 3 T/E FLAP TRACK I/B SIDE LOAD BEARING AREA WORN AND CORRODED.
- [SDR KCSA201807121191](https://openairdocs.org/sdr/KCSA201807121191), Jul 12, 2018: FLAP TRACK. CORRODED. NR 2 FLAP TRACK I/B SIDE LOAD BEARING AREA WORN AND CORRODED.
- [SDR KCSA201807121190](https://openairdocs.org/sdr/KCSA201807121190), Jul 12, 2018: FLAP TRACK. CORRODED. NR 1 T/E FLAP TRACK, I/B SIDE LOAD BEARING AREA WORN AND CORRODED.
- [SDR KCSA201806121146](https://openairdocs.org/sdr/KCSA201806121146), Jun 12, 2018: KEELBEAM. CORRODED. KEEL BEAM STA 1010 RBL 9 O/B END OF KEEL BEAM HAS CORROSION.
- [SDR KCSA201805181129](https://openairdocs.org/sdr/KCSA201805181129), May 18, 2018: FUSE PIN. CRACKED. DURING MPI INSPECTION OF LT WING LANDING GEAR SUPPORT BEAM END FITTING FUSE PIN IAW SB 747-57A2360, CRACK DETECTED IN GREASE HOLE.
- [SDR KCSA201805181128](https://openairdocs.org/sdr/KCSA201805181128), May 18, 2018: REVEAL. CRACKED. BS 2231 REVEAL CRACKED BETWEEN STR 21 - 22L.

## STCs that may be installed (OpenAirDocs) (3)

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 (Pratt & Whitney PW4056)

- [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 SE00053AT-D](https://openairdocs.org/stc/SE00053AT-D): Modification of fan exit guide vane, to line replaceable unit configuration. Chromalloy Gas Turbine Corp
- [STC SE00131LA](https://openairdocs.org/stc/SE00131LA): Modification of the subject engines to incorporate an oil tank reservoir insulation blanket in accordance with Hi Temp Insulation Inc. Drawing List 46M1024-301, Revision N/C, dated December 5, 1995, or later FAA approved revision as an acceptable alternate to Pratt & Whitney part number 50R280-01 or 51R059-01 insulation blankets. Hi Temp Insulation Inc

## Earlier aircraft with N713CK

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N713CK before.

- [Cancelled 2013-07-19](https://openairdocs.org/deregistered/N713CK-2013-07-19): Boeing 747-2B4B, S/N 21099, built 1975. Owner: [Kalitta Air LLC](https://openairdocs.org/faa-owner/KALITTA%20AIR%20LLC), [Ypsilanti, MI](https://openairdocs.org/faa-place/MI/Ypsilanti)

## Related

- Other Boeing 747-4B5F aircraft: https://openairdocs.org/model/boeing-747-4b5f/aircraft.md
- The Pratt & Whitney PW4056 engine: https://openairdocs.org/engine/pratt-whitney-pw4056.md

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