# N89068: 1982 Dehavilland DHC-7-102, registration cancelled 2022-11-05

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 5, 2022
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Dehavilland DHC-7-102](https://openairdocs.org/model/dehavilland-dhc-7-102) (registry code 2802708)
- Engine: [Pratt & Whitney Canada PT6A-50](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-50) (registry code 52272)
- Data sheets: [TCDS A20EA](https://openairdocs.org/tcds/A20EA), [TCDS E4EA](https://openairdocs.org/tcds/E4EA) (OpenAirDocs)
- Serial number: 88
- Year built: 1982
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: March 13, 1997
- Certificate issued: January 29, 1998
- Last registry action: February 15, 2019
- Mode S code: AC489F
- Owners when cancelled: [Department Of Defense](https://openairdocs.org/faa-owner/DEPARTMENT%20OF%20DEFENSE), [Cecom Acquisition Center](https://openairdocs.org/faa-owner/CECOM%20ACQUISITION%20CENTER), [E](https://openairdocs.org/faa-owner/E)
- Location: [Fort Belvoir, VA](https://openairdocs.org/faa-place/VA/Fort%20Belvoir)
- Owner type: Government
- Owner's area on the map: 38.6994° N, 77.1575° W: Placed by OpenAirDocs at the center of ZIP code 22060, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N89068
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=89068
- Page: https://openairdocs.org/deregistered/N89068-2022-11-05

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 Dehavilland DHC-7-102: https://openairdocs.org/model/dehavilland-dhc-7-102.md

## Service difficulty reports (10)

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

- [SDR QM7R201906142502](https://openairdocs.org/sdr/QM7R201906142502), Jun 14, 2019: BRACKET. CRACKED. ONE TIME INSPECTION FOR CRACK/BREAK OF THE RUDDER CONTROL MECHANISM BRACKET. THE INSPECTION RESULTED IN IDENTIFYING A CRACK AT BOTTOM OF RADIUS.
- [SDR 96ZZZX2896](https://openairdocs.org/sdr/96ZZZX2896), Apr 30, 1996: WIRE. CHAFED. ON TEST FLIGHT, AC NR 2 GENERATOR LIGHT CAME ON. DURING TROUBLESHOOTING OF SYSTEM, FOUND WIRE 2420-20001E12A-1 GROUNDED OUT. CONDUIT PASSES BETWEEN REAR SPAR AN
- [SDR 95ZZZX5850](https://openairdocs.org/sdr/95ZZZX5850), Oct 10, 1995: FOREFLAP. CORRODED. ON D-INSPECTION, NDT DEBOND CHECK OF RIGHT FOREFLAP FOUND CORROSION OF STR 14 AT STA YW257.35. SUBMITTER STATED REAR FOREFLAP PANELS NEED REMOVAL AT INSPECTION 
- [SDR 95ZZZX5849](https://openairdocs.org/sdr/95ZZZX5849), Oct 10, 1995: FOREFLAP. ARM CORRODED. ON D-INSPECTION OF FLIGHT CONTROLS, FOUND CORROSION ON INBD FORFLAP HINGE ARM UNDER PANEL COVER. PANELS ARE NOT REQUIRED TO BE REMOVED ON INSPECTION. PANELS NEE
- [SDR 95ZZZX5848](https://openairdocs.org/sdr/95ZZZX5848), Oct 10, 1995: STRUT PIN. CORRODED. ON A D-INSPECTION, REPLACED HARDWARE FOR UPPER DRAG STRUT AND WHEN STRUT PINS WERE REMOVED, THEY HAD CORROSION AND PITTING. SUBMITTER STATED WHEN HARDWARE IS SH
- [SDR 95ZZZX5847](https://openairdocs.org/sdr/95ZZZX5847), Oct 10, 1995: STRUT PIN. CORRODED. ON A D-INSPECTION, REPLACED HARDWARE FOR UPPER DRAG STRUT AND WHEN STRUT PINS WERE REMOVED, THEY HAD CORROSION AND PITTING. SUBMITTER STATED WHEN HARDWARE IS SH
- [SDR 95ZZZX5846](https://openairdocs.org/sdr/95ZZZX5846), Oct 10, 1995: FOREFLAP. CORRODED. ON D-INSPECTION OF FLIGHT CONTROLS, FOUND A HINGE ARM WITH CORROSION AND, WITH THE OTHER FLAP PANELS OPEN, FOUND CORROSION AROUND PANEL NUTPLATES, STA YW367.90 
- [SDR 95ZZZX5845](https://openairdocs.org/sdr/95ZZZX5845), Oct 10, 1995: FOREFLAP. CORRODED. ON D-INSPECTION OF FLIGHT CONTROLS OF LEFT FOREFLAP, FOUND CORROSION ON BOTTOM STR 12 AND STR 14 WITH BORESCOPE, STA YW242.17 TO YW257.35. FOREFLAP PANELS ARE N
- [SDR 95ZZZX5868](https://openairdocs.org/sdr/95ZZZX5868), Sep 29, 1995: PIN. CORRODED. DURING D-INSPECTION, RIGHT MLG UPPER DRAG STRUT PINS WERE REMOVED AND FOUND TO HAVE CORROSION AND PITTING. SUBMITTER STATED NEED TO INSPECT BY REMOVING PINS. PI
- [SDR 95ZZZX5867](https://openairdocs.org/sdr/95ZZZX5867), Sep 29, 1995: PIN. CORRODED. DURING D-INSPECTION, RIGHT MLG UPPER DRAG STRUT PINS WERE REMOVED AND FOUND TO HAVE CORROSION AND PITTING. SUBMITTER STATED NEED TO INSPECT BY REMOVING PINS. PI

## Other aircraft with N89068

- [Cancelled 1973-02-26](https://openairdocs.org/deregistered/N89068-1973-02-26): Cessna 140, S/N 8072. Owner: [Dickens D R& Flournoy W A](https://openairdocs.org/faa-owner/DICKENS%20D%20R%26%20FLOURNOY%20W%20A), [Houston, TX](https://openairdocs.org/faa-place/TX/Houston)

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