# N801MX: Dehavilland DHC-8-102, registration cancelled 2000-06-27

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 27, 2000
- Exported to: Australia
- Status when cancelled: Valid registration
- Airframe: [Dehavilland DHC-8-102](https://openairdocs.org/model/dehavilland-dhc-8-102) (registry code 2809003)
- Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM) (OpenAirDocs)
- Serial number: 008
- Type of aircraft: Fixed wing multi engine
- Certificate issued: April 20, 2000
- Last registry action: April 20, 2000
- Mode S code: AAE6BD
- Owner when cancelled: [First Security Bank Na Trustee](https://openairdocs.org/faa-owner/FIRST%20SECURITY%20BANK%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N801MX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=801MX
- Page: https://openairdocs.org/deregistered/N801MX-2000-06-27

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 (6)

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

- [SDR PCAA9600291](https://openairdocs.org/sdr/PCAA9600291), Jun 30, 1996: BOLT. CRACKED. DHC TASK 5310/08F DUE. PERFORMED ULTRASONIC TEST OF RIGHT BOLT, TEST REVEALED 30 PERCENT BACK REFLECTION. REMOVED AND REPLACED BOTH LEFT AND RIGHT FORWARD BOLTS
- [SDR PCAA9600280](https://openairdocs.org/sdr/PCAA9600280), Apr 7, 1996: UPPER ARM ASSY. WORN. DURING A SCHEDULED RUDDER CHANGE, THE VERTICAL STABILIZER UPPER AND LOWER CENTER HINGE FITTING RUDDER ATTACH POINTS WERE FOUND WORN. THE BUSHINGS WOULD NOT INST
- [SDR 96ZZZM881](https://openairdocs.org/sdr/96ZZZM881), Apr 7, 1996: LOWER ARM ASSY. WORN. DURING A SCHEDULED RUDDER CHANGE, THE VERTICAL STABILIZER UPPER AND LOWER CENTER HINGE FITTING RUDDER ATTACH POINTS WERE FOUND WORN. THE BUSHINGS WOULD NOT INST
- [SDR PCAA9500206](https://openairdocs.org/sdr/PCAA9500206), Mar 17, 1995: SEQ VALVE. FAILED. WHEN LANDING GEAR WAS RETRACTED, NOSE GEAR ADVISORY LIGHT REMAINED ON. THE GEAR WAS SELECTED DOWN PER THE CHECK LIST; THE MAIN GEAR CAME DOWN AND LOCKED, THE NO
- [SDR PCAA9500204](https://openairdocs.org/sdr/PCAA9500204), Mar 8, 1995: PROX CONT BOX. FAILED. AFTER DEPARTURE AND SELECTING GEAR UP, NOSE GEAR DOOR AMBER LIGHT STAYED LIT, FOLLOWED CHECK LIST, RECYCLED GEAR, NOSE WHEEL DID NOT COME DOWN. PERFORMED ALT GE
- [SDR PCAA9500196](https://openairdocs.org/sdr/PCAA9500196), Feb 8, 1995: PROX CONT BOX. FAILED. THE LT DOOR OPEN ADVISORY LIGHT ILLUMINATED IN FLIGHT. CREW VERIFIED DOOR IS CLOSED. REMOVED AND REPLACED LT FWD GEAR DOOR ACTUATOR AND PSEU IAW MM, OPERATIONAL

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19940109004629I](https://openairdocs.org/incident/19940109004629I), Jan 9, 1994: Dhav DHC8102 (N801MX), Middletown, PA. Narrative: while on a ferry flight from wilkes-barre, PA to Middletown, PA, allegheny flight 801, with no passengers on board, had a #1 hydraulic system…

---
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.