# N445CT: 2007 Hawker Beechcraft 400A, registration cancelled 2024-06-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 18, 2024
- Status when cancelled: Valid registration
- Airframe: [Hawker Beechcraft 400A](https://openairdocs.org/model/hawker-beechcraft-400a) (registry code 4220001)
- Engine: [Pratt & Whitney Canada JT15D-5](https://openairdocs.org/engine/pratt-whitney-canada-jt15d-5) (registry code 52197)
- Data sheets: [TCDS A16SW](https://openairdocs.org/tcds/A16SW), [TCDS E25EA](https://openairdocs.org/tcds/E25EA) (OpenAirDocs)
- Serial number: RK-535
- Year built: 2007
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 1, 2007
- Certificate issued: July 28, 2022
- Last registry action: August 18, 2023
- Mode S code: A55D74
- Owner when cancelled: [Wheels Up Partners LLC](https://openairdocs.org/faa-owner/WHEELS%20UP%20PARTNERS%20LLC)
- Location: [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)
- Owner type: LLC
- Owner's area on the map: 40.7506° N, 73.9973° W: Placed by OpenAirDocs at the center of ZIP code 10001, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N445CT
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=445CT
- Page: https://openairdocs.org/deregistered/N445CT-2024-06-18

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 Hawker Beechcraft 400A: https://openairdocs.org/model/hawker-beechcraft-400a.md

## Service difficulty reports (13)

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

- [SDR T17A2020030521004](https://openairdocs.org/sdr/T17A2020030521004), Feb 22, 2020: CLOSEOUT PANEL. CRACKED. R/H UPPER INBOARD PYLON PANEL IS CRACKING AT REAR ATTACH POINT
- [SDR T17A2020030521003](https://openairdocs.org/sdr/T17A2020030521003), Feb 22, 2020: SKIN. CRACKED. R/H UPPER TR DOOR SKIN CRACKED
- [SDR T17A2020030521002](https://openairdocs.org/sdr/T17A2020030521002), Feb 22, 2020: SKIN. CRACKED. L/H UPPER TR DOOR SKIN CRACKED
- [SDR T17A2020031821004](https://openairdocs.org/sdr/T17A2020031821004), Feb 21, 2020: CLOSEOUT PANEL. CRACKED. DURING SCHEDULED INSPECTION MX FOUND A CRACK ON THE RH INBOARD UPPER PYLON PANEL AT THE REAR ATTACH POINT. MX PERFORMED A REPAIR TO THE PANEL IAW BEECHJET 400XP
- [SDR T17A2020031821003](https://openairdocs.org/sdr/T17A2020031821003), Feb 21, 2020: THRUST REVERSER. CRACKED. DURING SCHEDULED INSPECTION MX FOUND THE LH UPPER THRUST REVERSER DOOR SKIN CRACKED. MX REMOVED AND THEN INSTALLED A SERVICEABLE LH UPPER TR BUCKET.
- [SDR T17A2020031821002](https://openairdocs.org/sdr/T17A2020031821002), Feb 21, 2020: THRUST REVERSER. CRACKED. DURING SCHEDULED INSPECTION MX FOUND THE RH UPPER THRUST REVERSER DOOR SKIN CRACKED. MX REMOVED THE RH UPPER THRUST REVERSER BUCKET AND REPLACED IT WITH A SERVI
- [SDR T17A2020031821007](https://openairdocs.org/sdr/T17A2020031821007), Feb 21, 2020: BEAM. CRACKED. DURING SCHEDULED INSPECTION MX FOUND A CRACK ON THE FWD BEAM THE RH MAIN LANDING GEAR DOOR. MX REMOVED AND REPLACED THE RIGHT INBOARD GEAR DOOR FORWARD BEAM WIT
- [SDR T17A2020031721006](https://openairdocs.org/sdr/T17A2020031721006), Feb 21, 2020: BRACKET. CRACKED. 2 EA DOORLAND REINFORCMENT BRACKETS ON THE MAIN ENTRY DOOR FOUND CRACKED DURING VISUAL INSPECTION, MX REPLACED THE BRACKETS WITH NEW
- [SDR T17A201710314027](https://openairdocs.org/sdr/T17A201710314027), Oct 26, 2017: SKIN. SCRATCHED. AREA ABOVE MAIN ENTRY DOOR STEP PADS HAS SEVERAL SCRATCHES. FUSELAGE SKIN BELOW MED, PERFORMED NDT, REPAIR, PAINT, AND SEALED IAW FIELD REPAIR DRAWING FR-RK-535
- [SDR T17A201710314026](https://openairdocs.org/sdr/T17A201710314026), Oct 24, 2017: RIB. CRACKED. CRACKS FOUND IN DOUBLERS IN HORIZONTAL STABILIZER REAR SPAR WHILE COMPLETING SB 55-4162. REPLACED RIBS ON H-STAB IAW AIR SERVICES DRAWING NR CAS-128-6200 REV B,
- [SDR T17A201311074003](https://openairdocs.org/sdr/T17A201311074003), Nov 4, 2013: LANDING GEAR. MALFUNCTIONED. DURING DESCENT AT FL330, UNCOMMANDED NOSE GEAR EXTENSION. AIRSPEED AT THE TIME OF EXTENSION WAS + 280 KTS AND TOTAL TIME ABOVE 200KTS APPROX 5-10 MINUTES. MAINT
- [SDR E81RJT227916B](https://openairdocs.org/sdr/E81RJT227916B), Apr 8, 2010: TIRE. WRONG PART. (E81R) DURING REPLACEMENT OF WORN NOSE WHEEL TIRE, NOTED PN OF INSTALLED NOSEWHEEL TIRE INCORRECT IAW THE ACFT MFG IPC (32-40-05-01). IAW MFG TIRE APPLICATION D
- [SDR E81RJT227916A](https://openairdocs.org/sdr/E81RJT227916A), Apr 8, 2010: WHEEL HALF. CORRODED. (E81R) DURING DISASSEMBLY OF NOSEWHEEL FOR TIRE REPLACEMENT NOTED CORROSION PITTING IN BOLT HOLES. PITTING WAS DEEPER THAN FIELD REPAIRABLE SERVICE LIMITS. THIS

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