# N63CK: 1967 Learjet 24A, registration cancelled 2013-04-26

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 26, 2013
- Status when cancelled: Sale reported, pending cancellation
- Airframe: [Learjet 24A](https://openairdocs.org/model/learjet-24a) (registry code 5170304)
- Engine: [GE CJ610-SER series](https://openairdocs.org/engine/ge-cj610-ser-series) (registry code 30006)
- Data sheets: [TCDS A10CE](https://openairdocs.org/tcds/A10CE), [TCDS 1E16](https://openairdocs.org/tcds/1E16) (OpenAirDocs)
- Serial number: 119
- Year built: 1967
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: June 23, 1969
- Last registry action: June 24, 2002
- Mode S code: A83B9F
- Location: [Okla City, OK](https://openairdocs.org/faa-place/OK/Okla%20City)
- Owner type: Individual
- Owner's area on the map: 35.4676° N, 97.5164° W: Placed by OpenAirDocs: center of Oklahoma City, OK, within about 14 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N63CK
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=63CK
- Page: https://openairdocs.org/deregistered/N63CK-2013-04-26

From the FAA registry file of October 29, 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 Learjet 24A: https://openairdocs.org/model/learjet-24a.md

## Service difficulty reports (7)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR KKF2001F00000](https://openairdocs.org/sdr/KKF2001F00000), Jun 21, 2001: SOCKET. FAILED. PRIMARY PITCH TRIM FAILED, WILL TRIM NOSE UP BUT NOT NOSE DOWN. REPLACED 3 SOCKETS IN CONNECTOR P1023 AT 2 SPEED TRIM BOX PINS B,C, AND D. PERFORMED TRIM SYSTEM
- [SDR 99ZZZX485](https://openairdocs.org/sdr/99ZZZX485), Jan 8, 1999: FUEL CONTROL. MALFUNCTIONED. LEFT ENGINE COMPRESSOR STALLNG FROM ROTATION TO 2,000 FEET. REPLACED LEFT FUEL CONTROL UNIT. GROUND RUN, LEAK CHECKED, AND TEST FLEW AIRCRAFT, OPS CHECKED GOOD.
- [SDR 99ZZZX455](https://openairdocs.org/sdr/99ZZZX455), Jan 8, 1999: FITTING. LOOSE. HYDRAULIC SYSTEM PRESSURE LOSS. FOUND LOOSE LINE ON LEFT GEAR ACTUATOR. TIGHTENED LINE. REPLACED BOTH ENGINE HYDRAULIC PUMPS AND FILTERS. C/W RETRACTION CHECK. 
- [SDR 97ZZZX1061](https://openairdocs.org/sdr/97ZZZX1061), Jan 30, 1997: SWITCH. ICE PACKED. LANDING GEAR WOULD NOT RETRACT AFTER DEPARTURE. FOUND GEAR SQUAT SWITCHES FROZEN AND PACKED WITH ICE. CLEANED GEAR OF ALL SNOW AND ICE, LUBED, AND PERFORMED SAT
- [SDR 131963CK](https://openairdocs.org/sdr/131963CK), Feb 1, 1996: SWITCH. FAILED. DURING GEAR EXTENSION, RT MAIN DOWN AND LOCK LIGHT FAILED TO ILLUMINATE IMMEDIATELY. AFTER SEVERAL ATTEMPTS, IT CAME ON, NORMAL LANDING MADE. LANDING GEAR INDIC
- [SDR 1239563CK](https://openairdocs.org/sdr/1239563CK), Dec 6, 1995: O-RING. LEAK. ON APPROACH TO LANDING, HYDRAULIC PRESSURE WAS NOTED TO BE ZERO. LANDING GEAR WAS EXTENDED USING EMERGENCY AIR SYSTEM AND A NORMAL LANDING WAS MADE. EXAMINATION
- [SDR 95ZZZX2825](https://openairdocs.org/sdr/95ZZZX2825), May 12, 1995: ACTUATOR. O-RING FAILED. HYDRAULIC SYSTEM PRESSURE WENT TO ZERO. UNEVENTFUL LANDING ACCOMPLISHED. O-RING LT MAIN GEAR ACTUATOR LEAKING. INSTALLED NEW O-RING, LANDING GEAR HYDRAULIC RESE

## Other aircraft with N63CK

- [Registered now](https://openairdocs.org/aircraft/N63CK): C K ING Adventure CCX-2000, S/N CCX-2000-0120
- [Cancelled 1988-12-01](https://openairdocs.org/deregistered/N63CK-1988-12-01): Teft PITTS S-1S, S/N 23P. N-number assigned, not yet registered

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