# N316NT: 1966 North American NA-265-40, registration cancelled 2003-10-29

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 29, 2003
- Status when cancelled: Triennial form not returned
- Airframe: [North American NA-265-40](https://openairdocs.org/model/north-american-na-265-40) (registry code 6402608)
- Engine: [Pratt & Whitney JT12A-6 6A](https://openairdocs.org/engine/pratt-whitney-jt12a-6-6a) (registry code 52042)
- Data sheets: [TCDS A2WE](https://openairdocs.org/tcds/A2WE) (OpenAirDocs)
- Serial number: 282-60
- Year built: 1966
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: February 28, 1966
- Certificate issued: September 13, 1991
- Last registry action: January 16, 2001
- Mode S code: A35E59
- Owner when cancelled: [Sabreliner Corp](https://openairdocs.org/faa-owner/SABRELINER%20CORP)
- Location: [St Louis, MO](https://openairdocs.org/faa-place/MO/St%20Louis)
- Owner type: Corporation
- Owner's area on the map: 38.6443° N, 90.3281° W: Placed by OpenAirDocs at the center of ZIP code 63105, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N316NT
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=316NT
- Page: https://openairdocs.org/deregistered/N316NT-2003-10-29

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 North American NA-265-40: https://openairdocs.org/model/north-american-na-265-40.md

## Service difficulty reports (4)

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

- [SDR 97ZZZX3783](https://openairdocs.org/sdr/97ZZZX3783), Jul 17, 1997: PUMP. SEAL DAMAGED. HYDRAULIC PUMP WAS REMOVED AFTER 7.9 HOURS TIME IN SERVICE DUE TO SHAFT SEAL FAILURE AND EXCESSIVE FLUID LEAKAGE. PUMP, SN MX193803A, REJECTED FOR INSTALLATION 
- [SDR 97ZZZX3782](https://openairdocs.org/sdr/97ZZZX3782), Jul 17, 1997: PUMP. SEAL DAMAGED. HYDRAULIC PUMP WAS REMOVED AFTER 7.9 HOURS TIME IN SERVICE DUE TO SHAFT SEAL FAILURE AND EXCESSIVE FLUID LEAKAGE. PUMP, SN MX193803A, REJECTED FOR INSTALLATION 
- [SDR 97ZZZX2939](https://openairdocs.org/sdr/97ZZZX2939), Jun 5, 1997: LINE ASSY. CHAFED. DURING PYLON MATCHING ANGLES AND FUSELAGE SKIN INSPECTION, NOTED AN ADEL CLAMP, PN MS21919DG6, WAS BROKEN ON THE RIGHT HAND SIDE FS 367. FURTHER INSPECTION REVE
- [SDR 96ZZZX5145](https://openairdocs.org/sdr/96ZZZX5145), Sep 23, 1996: CONTROL CABLE. FRAYED. LOWER AFT ELEVATOR CONTROL CABLE FS 388 TO FS 457, SHOWED SIGNS OF CORROSION ON UPPER SURFACE 'ONLY' JUST AFT OF FIBERGLASS PROTECTIVE CABLE SHROUD PN 265-54042

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