# N915HA: Dehavilland DHC-8-102, registration cancelled 2003-06-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 18, 2003
- Exported to: Canada
- Status when cancelled: Valid registration
- Airframe: [Dehavilland DHC-8-102](https://openairdocs.org/model/dehavilland-dhc-8-102) (registry code 2809003)
- Engine: [NONE](https://openairdocs.org/engine/none) (registry code 00000)
- Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM) (OpenAirDocs)
- Serial number: 69
- Type of aircraft: Fixed wing multi engine
- Engine type: None
- Certificate issued: April 18, 2003
- Last registry action: April 18, 2003
- Mode S code: ACA9EE
- Owner when cancelled: [Westinghouse Aircraft Leasing Inc](https://openairdocs.org/faa-owner/WESTINGHOUSE%20AIRCRAFT%20LEASING%20INC)
- Location: [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)
- Owner type: Corporation
- Owner's area on the map: 40.7598° N, 73.9907° W: Placed by OpenAirDocs at the center of ZIP code 10036, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N915HA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=915HA
- Page: https://openairdocs.org/deregistered/N915HA-2003-06-18

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 Dehavilland DHC-8-102: https://openairdocs.org/model/dehavilland-dhc-8-102.md

## Service difficulty reports (3)

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

- [SDR HNAA0100041](https://openairdocs.org/sdr/HNAA0100041), Jul 11, 2001: SENSOR. BROKEN. ON BOTH NORMAL AND ALTERNATE GEAR EXTENSION THE NLG UNSAFE LIGHTS REMAINED ILLUMINATED. FOUND BROKEN WIRE ON NLG DOWNLOCK PROXIMITY SENSOR. REPLACED SENSOR.
- [SDR HNAA0100014](https://openairdocs.org/sdr/HNAA0100014), Feb 9, 2001: CONTROL CABLE. OUT OF TOLERANCE. UPON RELEASE OF AUTO PILOT, NOTED ROLL CONTROL VERY STIFF, SEEMS TO REDUCE WITH REDUCTION IN AIR SPEED. INSPECTED AILERONS AND ROLL SPOILERS, FOUND AILERON CONT
- [SDR HNAA9900106](https://openairdocs.org/sdr/HNAA9900106), Jul 21, 1999: SKIN. CRACKED. EXHAUST OUTLET SHROUD INNER SKIN CRACKED AT FORWARD O/B END. REPAIRED IAW RD8-54-331 AND EO8-54-99-255.

## Other aircraft with N915HA

- [Registered now](https://openairdocs.org/aircraft/N915HA): Thrush S2R-G10, S/N G10-176, built 2013

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.