# N701CK: 2000 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: 26416
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 30, 2017
- Certificate issued: August 17, 2022
- Expires: August 31, 2029
- Mode S code: A95881
- 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=701CK
- Page: https://openairdocs.org/aircraft/N701CK

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 N701CK.

## FAA accident and incident reports

None matched to N701CK.

## Service difficulty reports (80, 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 KCSA2026072744](https://openairdocs.org/sdr/KCSA2026072744), Jul 27, 2026: ELEC CONNECTOR. LOOSE. DOOR ENTRY L5 ADVISORY IN FLIGHT ACCOMPLISHED QRH PROCEDURE. PRESSURIZATION NORMAL. TRANSFERRED TO DMI 100338109 IAW KA MEL 52-73-01. CAT C. DUE 8.6.26. M PROCE
- [SDR KCSA2026072643](https://openairdocs.org/sdr/KCSA2026072643), Jul 26, 2026: DOOR. NO DISCREPANCY. DOOR ENTRY L5. VERIFIED #5 ENTRY DOOR WARN SWITCH IAW B747-400 AMM 52-11-01. OPS CHECK GOOD.
- [SDR KCSA202604281037](https://openairdocs.org/sdr/KCSA202604281037), Apr 28, 2026: FRAME. CRACKED. CRACKED FRAME WEB AT STA 1480 IN R/H BODY GEAR WHEEL WELL.
- [SDR KCSA202505131078](https://openairdocs.org/sdr/KCSA202505131078), May 13, 2025: POWER SUPPLY. INOPERATIVE. UPPER DECK LADDER SURROUND EMERGENCY LIGHTING IS INOP.
- [SDR KCSA2025042418](https://openairdocs.org/sdr/KCSA2025042418), Apr 24, 2025: DOOR. FALSE INDICATION. DOOR FLIGHT DECK OVERHEAD. BLANKED AFTER TWO MINUTES. PERFORMED DOOR OPERATION IAW B747-400 AMM 52-71-01 OPERATIONS CHECK GOOD. DOOR REMAIN CLOSE.
- [SDR KCSA2025041917](https://openairdocs.org/sdr/KCSA2025041917), Apr 19, 2025: INDICATION SYS. FALSE INDICATION. 100242157- DOOR FLIGHT DECK OVERHEAD INDICATION ONLY. PERFORMED OVERHEAD INSPECTION AND OPERATION IAW B747-400 AMM 52-21-00 OPERATION CHECK GOOD.
- [SDR KCSA2025041213](https://openairdocs.org/sdr/KCSA2025041213), Apr 12, 2025: HANDLE. UNSECURE. DOOR FLIGHT DECK OVERHEAD ENGINE-INDICATING AND CREW-ALERTING MESSAGE - MESSAGE CLEARED BEFORE QUICK REFERENCE HANDBOOK IS COMPLETED. VERIFIED FLIGHT DECK ESCAP
- [SDR KCSA202504051074](https://openairdocs.org/sdr/KCSA202504051074), Apr 5, 2025: ANGLE. CRACKED. CRACKED ANGLE ON RW AFT OF REAR APPROX WBL 412
- [SDR KCSA202504051073](https://openairdocs.org/sdr/KCSA202504051073), Apr 5, 2025: DOUBLER. CORRODED. CORROSION FOUND IN L/H SIDE UPPER LOBE DOUBLER NEAR RADIUS AND VERTICAL STABILIZER ATTACHMENT AT STATION 2521 DURING EXTERNAL SURFACE INSPECTION
- [SDR KCSA202504051072](https://openairdocs.org/sdr/KCSA202504051072), Apr 5, 2025: SPAR. CRACKED. L/H WING T/E AUXILARY SPAR UPPER CHORD AT WBL 429.5 HAS POSSIBLE CRACK
- [SDR KCSA202504051071](https://openairdocs.org/sdr/KCSA202504051071), Apr 5, 2025: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK @ STA 2140 RBL 89 CORRODED
- [SDR KCSA202504051070](https://openairdocs.org/sdr/KCSA202504051070), Apr 5, 2025: FLOORBEAM. CORRODED. MAIN DECK FLOOR BEAM CORRODED AT STA 1620 RBL 13-32
- [SDR KCSA202504051069](https://openairdocs.org/sdr/KCSA202504051069), Apr 5, 2025: TEE ANGLE. CRACKED. R/H WING AUX SPAR VERTICAL "T" CHORD IS CRACKED WBL 429.5
- [SDR KCSA202504051068](https://openairdocs.org/sdr/KCSA202504051068), Apr 5, 2025: FLOORBEAM. CRACKED. E/E BAY FLOOR SUPPORT ANGLE CRACKED AT STA 400 RBL 19
- [SDR KCSA202504051067](https://openairdocs.org/sdr/KCSA202504051067), Apr 5, 2025: FLOORBEAM. CRACKED. E/E BAY FLOOR SUPPORT ANGLE CRACKED AT STA 400 LBL 15
- [SDR KCSA202504051066](https://openairdocs.org/sdr/KCSA202504051066), Apr 5, 2025: FLOORBEAM. CRACKED. E/E BAY FLOOR SUPPORT ANGLE CRACKED AT STA 400 RBL 6
- [SDR KCSA202504041065](https://openairdocs.org/sdr/KCSA202504041065), Apr 4, 2025: STIFFENER. CRACKED. CRACKED STIFFENER ON L/H WING T/E AUX SPAR AT WBL 429.5
- [SDR KCSA202504041064](https://openairdocs.org/sdr/KCSA202504041064), Apr 4, 2025: WEB. CRACKED. OB OF THE #5 SPOILER, WEB CRACK IN THE AREA OF THE 3 UPPER WING SURFACE SUPPORT ROD ENDS
- [SDR KCSA202504041063](https://openairdocs.org/sdr/KCSA202504041063), Apr 4, 2025: ATTACH ANGLE. CRACKED. L-1 DOOR CUTOUT UPPER FORWARD CORNER HAS A CRACKED (3/4") ATTACH ANGLE AT STATION 440 AT STRINGER 16L
- [SDR KCSA202504041062](https://openairdocs.org/sdr/KCSA202504041062), Apr 4, 2025: HINGE. CRACKED. AFT CARGO DOOR FWD HINGE HAS EVIDENCE OF CRACKING IN RADIUS OF ANGLE
- [SDR KCSA202504041061](https://openairdocs.org/sdr/KCSA202504041061), Apr 4, 2025: ATTACH ANGLE. CRACKED. E/E BAY L/H SILL FWD ATTACH ANGLE CRACKED AT STA 400 LBL 26
- [SDR KCSA202504041060](https://openairdocs.org/sdr/KCSA202504041060), Apr 4, 2025: ATTACH ANGLE. CRACKED. E/E BAY R/H AUX FWD SILL ATTACH ANGLE CRACKED AT STA 400 RBL 26
- [SDR KCSA202504041059](https://openairdocs.org/sdr/KCSA202504041059), Apr 4, 2025: SKIN. CRACKED. 2EA. CRACKS FOUND EXTENDING BEYOND 2EA. EXISTING STOP DRILL HOLES IN R/H SIDE UPPER LOBE DOUBLER NEAR VERTICAL STAB. ATTACHMENT AT APPROX. STA. 2515 AND 2521 DU
- [SDR KCSA202504021058](https://openairdocs.org/sdr/KCSA202504021058), Apr 2, 2025: ATTACH ANGLE. CRACKED. E/E BAY SILL FWD ATTACH ANGLE CRACKED AT STA 400 BL 0
- [SDR KCSA202504021056](https://openairdocs.org/sdr/KCSA202504021056), Apr 2, 2025: STIFFENER. CRACKED. CRACK FOUND IN NWW TOP PANEL STIFFENER AT STA 270 AND RBL 20
- [SDR KCSA202504021055](https://openairdocs.org/sdr/KCSA202504021055), Apr 2, 2025: BRACKET. CRACKED. MAIN DECK, OVER PRESSURE DECK, STA 1080, RBL 100, POSSIBLE CRACK IN BRACKET UNDER THE FLOOR
- [SDR KCSA202504021054](https://openairdocs.org/sdr/KCSA202504021054), Apr 2, 2025: STIFFENER. CRACKED. CRACK FOUND IN NWW TOP PANEL STIFFENER AT STA 310 AND LBL 10
- [SDR KCSA202504021053](https://openairdocs.org/sdr/KCSA202504021053), Apr 2, 2025: STIFFENER. CRACKED. CRACK FOUND IN NWW TOP PANEL STIFFENER AT STA 310 AND RBL 10
- [SDR KCSA202504021052](https://openairdocs.org/sdr/KCSA202504021052), Apr 2, 2025: STIFFENER. CRACKED. VERTICAL STIFFENER IS CRACKED ( 1") ON THE AFT SIDE OF THE MAIN DECK FLOORBEAM AT STATION 2360 AT LBL 32
- [SDR KCSA202504021051](https://openairdocs.org/sdr/KCSA202504021051), Apr 2, 2025: STIFFENER. CRACKED. VERTICAL STIFFENER IS CRACKED ( 1") ON THE AFT SIDE OF THE MAIN DECK FLOORBEAM AT STATION 2360 AT LBL 13
- [SDR KCSA202504021050](https://openairdocs.org/sdr/KCSA202504021050), Apr 2, 2025: STIFFENER. CRACKED. VERTICAL STIFFENER IS CRACKED ( 1") ON THE AFT SIDE OF THE MAIN DECK FLOORBEAM AT STATION 2360 AT RBL 32
- [SDR KCSA202504011049](https://openairdocs.org/sdr/KCSA202504011049), Apr 1, 2025: STIFFENER. CRACKED. CRACK FOUND IN NWW TOP PANEL STIFFENER AT STA 270 AND LBL 20
- [SDR KCSA202504011048](https://openairdocs.org/sdr/KCSA202504011048), Apr 1, 2025: PRESSURE DECK. CRACKED. L/H COMPOSITE CLOSE OUT PANEL AT STA. 1240 LBL 75-98 CRACKED.
- [SDR KCSA202504011047](https://openairdocs.org/sdr/KCSA202504011047), Apr 1, 2025: LIGHT. NO TEST. MAIN DECK SELF ILLUMINATING EXIT SIGNS FAIL OPS CHECK
- [SDR KCSA2025012803](https://openairdocs.org/sdr/KCSA2025012803), Jan 28, 2025: WARNING MESSAGE. FALSE ACTIVATION. DOOR FLIGHT DECK OVER HEAD ADVISORY MESSAGE. PERFORMED GROUND OPERATION OF FLIGHT DECK DOOR OVERHEAD IAW B747-400 AMM 52-71-01. OPERATIONS CHECK GOOD.
- [SDR KCSA2025012002](https://openairdocs.org/sdr/KCSA2025012002), Jan 20, 2025: INDICATION SYS. FALSE ACTIVATION. DOOR FLIGHT DECK OVERHEAD ADVISORY ON CLIMB OUT. PERFORMED GROUND OPERATION ON FIRST OFFICER OVER HEAD IAW B747-400 AMM 52-71-01. OPERATIONS CHECK GOOD.
- [SDR KCSA2024122932](https://openairdocs.org/sdr/KCSA2024122932), Dec 29, 2024: ESCAPE HATCH. NOT REPORTED. DOOR FLIGHT DECK OVERHEAD. PERFORMED HATCH OPERATIONAL AND INSPECTION IAW B747-400 AMM 52-21-00 OPERATIONAL CHECK GOOD.
- [SDR KCSA2024111829](https://openairdocs.org/sdr/KCSA2024111829), Nov 17, 2024: HANDLE. NOT SEATED. DOOR FLIGHT DECK ENGINE INDICATION AND CREW ALERTING SYSTEM. NO PRESSURIZATION ISSUES. FOUND DOOR HANDLE SLIGHTLY AJAR. RESECURED INNER DOOR HANDLE IAW B747-400
- [SDR KCSA2024091528](https://openairdocs.org/sdr/KCSA2024091528), Sep 15, 2024: HANDLE. UNSECURE. PER LOGPAGE 100198873, DOOR FLIGHT DECK OVERHEAD. DUE TO TURBULENCE FOUND THE INNER HANDLE SLIGHTLY AJAR. RESECURED INNER HANDLE IAW B747-400 AMM 52-21-00. INDI
- [SDR KCSA202311021131](https://openairdocs.org/sdr/KCSA202311021131), Nov 2, 2023: COVER. BROKEN. MDSS BLUE LIGHT COVER IS BROKEN
- [SDR KCSA2023101900340](https://openairdocs.org/sdr/KCSA2023101900340), Oct 13, 2023: UNKNOWN. UNKNOWN. DOOR FLIGHT DECK OVERHEAD. FOUND FLIGHT DECK OVERHEAD DOOR INNER HANDLE HAD BEEN BUMPED OR WASN'T LATCHED COMPLETELY RELATCHED FLIGHT DECK OVERHEAD DOOR IAW B74
- [SDR KCSA202303131018](https://openairdocs.org/sdr/KCSA202303131018), Mar 13, 2023: FRAME. CRACKED. CRACK FOUND ON FRAME SEGMENT AT LOWER FORWARD CORNER OF L5 DOOR CUTOUT
- [SDR ERKR1110032326416](https://openairdocs.org/sdr/ERKR1110032326416), Mar 10, 2023: FRAME. CRACKED. CRACK FOUND ON FRAME SEGMENT AT LOWER FORWARD CORNER OF L5 DOOR CUTOUT.
- [SDR ERKR1010032326416](https://openairdocs.org/sdr/ERKR1010032326416), Mar 10, 2023: SEAT TRACK. CORRODED. AFTER REMOVAL OF FLOORBOARDS TO GAIN ACCESS FOR SEAT TRACK REPAIR AT STA. 998 RBL 11.33, FOUND CORROSION ON SEAT TRACK I/B FLANGE AT STA. 980 APPROX. RBL 11.33
- [SDR ERKR0910032326416](https://openairdocs.org/sdr/ERKR0910032326416), Mar 10, 2023: NONE. CRACKED. WHILE ACCOMPLISHING SB 747-53A2427 FIG. 2 AT STA. 2598 R/H SIDE, FOUND 2EA FASTENER HOLES WITH CRACK INDICATION COMMON TO FWD INNER CHORD AND UPPER SPLICE FITTI
- [SDR ERKR0810032326416](https://openairdocs.org/sdr/ERKR0810032326416), Mar 10, 2023: SHEAR TIE. CRACKED. WHILE ACCOMPLISHING DVI OF STA. 1000 FRONT SPAR SHEAR TIE, FOUND 1EA FRONT SHEAR TIE CRACKED AT RBL 75.9, REPLACEMENT OF PART REQUIRED PER EO 5312-22-01 G2 COND
- [SDR ERKR0710032326416](https://openairdocs.org/sdr/ERKR0710032326416), Mar 10, 2023: SHEAR TIE. BROKEN. WHILE ACCOMPLISHING DVI AT STA. 1000 FRONT SPAR SHEAR TIE, FOUND 1EA FRONT SHEAR TIE CRACKED AT LBL 33.99, REPLACEMENT OF PART REQUIRED PER EO 5312-22-01 G2 CON
- [SDR ERKR0610032326416](https://openairdocs.org/sdr/ERKR0610032326416), Mar 10, 2023: SHEAR TIE. BROKEN. WHILE ACCOMPLISHING DVI OF STA. 1000 FRONT SPAR SHEAR TIE, FOUND 1EA SHEAR TIE BROKEN AT RBL57.5., REPLACEMENT OF THE PART IS REQUIRED PER EO 5312-22-01-G2 COND
- [SDR KCSA202303101017](https://openairdocs.org/sdr/KCSA202303101017), Mar 10, 2023: SHEAR TIE. CRACKED. WHILE ACCOMPLISHING DVI OF STA 1000 FRONT SPAR SHEAR TIE FOUND 1 EA FRONT SHEAR TIE CRACKED AT LBL 33.99 REPLACEMENT OF PART REQUIRED PER EO 5312-22-01 G2 CONDI
- [SDR ERKR0510032326416](https://openairdocs.org/sdr/ERKR0510032326416), Mar 10, 2023: INTERCOSTAL. BROKEN. WHILE ACCOMPLISHED DVI OF STA. 1000 FRONT SPAR SHEAR TIE, FOUND 1EA INTERCOSTAL LUG FITTING BROKEN AT LBL 11.33, REPLACEMENT OF THE PART IS REQUIRED PER EO 5312

All 80: https://openairdocs.org/aircraft/N701CK/reports.md

## 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 N701CK

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N701CK before.

- [Cancelled 2016-10-04](https://openairdocs.org/deregistered/N701CK-2016-10-04): Boeing 747-259B, S/N 21730, built 1979. First renewal notice. 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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