# N701QD: 1999 Socata TBM 700, registration cancelled 2017-08-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 3, 2017
- Status when cancelled: First renewal notice
- Airframe: [Socata TBM 700](https://openairdocs.org/model/socata-tbm-700) (registry code 8682000)
- Engine: [Pratt & Whitney PT6A series](https://openairdocs.org/engine/pratt-whitney-pt6a-series) (registry code 52032)
- Data sheets: [TCDS A60EU](https://openairdocs.org/tcds/A60EU) (OpenAirDocs)
- Serial number: 126
- Year built: 1999
- Type of aircraft: Fixed wing single engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: August 30, 1999
- Certificate issued: January 4, 2012
- Last registry action: August 13, 2014
- Mode S code: A959A7
- Owner when cancelled: [Quest Diagnstics Inc](https://openairdocs.org/faa-owner/QUEST%20DIAGNSTICS%20INC)
- Location: [Reading, PA](https://openairdocs.org/faa-place/PA/Reading)
- Owner type: Corporation
- Owner's area on the map: 40.3986° N, 75.9461° W: Placed by OpenAirDocs at the center of ZIP code 19605, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N701QD
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=701QD
- Page: https://openairdocs.org/deregistered/N701QD-2017-08-03

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 Socata TBM 700: https://openairdocs.org/model/socata-tbm-700.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 2012FA0000081](https://openairdocs.org/sdr/2012FA0000081), Jan 31, 2012: FUEL CONTROL. FAILED. DURING RUNUP, PROP FEATHER CHECK CONDUCTED NORMALLY. WHEN ADVANCING POWER LEVER TO DO A PROP OVERSPEED TEST, COULD NOT REACH 1900 RPM WITH POWER LEVER FORWARD. 
- [SDR 2006FA0000248](https://openairdocs.org/sdr/2006FA0000248), Feb 21, 2006: ATTACH BRACKET. CRACKED. DURING A 6000 HOUR INSPECTION, THE LT AND RT WING TIP ASSEMBLIES WERE REMOVED TO FACILITATE FURTHER INSPECTION OF THE AILERON SYSTEM. AFTER REMOVAL OF THE TIPS 
- [SDR 2006FA0000247](https://openairdocs.org/sdr/2006FA0000247), Feb 21, 2006: SUPPORT BRACKET. CRACKED. DURING A 6000 HOUR INSPECTION, THE LT AND RT WING TIP ASSEMBLIES WERE REMOVED TO FACILITATE FURTHER INSPECTION OF THE AILERON SYSTEM. AFTER REMOVAL OF THE TIPS 

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