# Beech/Middleton T34A

- Type: Aircraft model (FAA registry)
- Registry code: 1152001
- Manufacturer (registry): BEECH/MIDDLETON
- Model: T34A
- Aircraft type: Fixed wing single engine
- Category: Airplane
- Engines: 1 · Reciprocating
- Seats: 2
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/beech-middleton-t34a

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

None matched.

## Registered aircraft

None registered with this model now.

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (7)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2016FA0000248](https://openairdocs.org/sdr/2016FA0000248), May 17, 2016: ROD. FAILED. AFTER GEAR DROP, LT MAIN SHOWED DOWN, LOCKED, RT MAIN SHOWED UNSAFE AND NOSE WHEEL UNSAFE. ACFT LANDED AFTER TOWER REPORTED THE GEAR APPEARED DOWN. AT END OF RO
- [SDR 2015FA0000312](https://openairdocs.org/sdr/2015FA0000312), Jul 6, 2015: GLAND NUT. WRONG PART. REMOVED NR 4 CYLINDER FOR REPAIR DUE TO LOW COMPRESSION, EXHAUST VALVE, FOUND CRACKED BUSHING IN CONNECTING ROD FOR WRIST PIN. REMOVED FOR REPAIR AND FOUND INCO
- [SDR W1V2014F00002](https://openairdocs.org/sdr/W1V2014F00002), Mar 28, 2014: VALVE. CORRODED. BETA VALVE PORTION OF CSU FOUND CORRODED IN DRY AREA OF BETA VALVE. SUGGEST MFG PROVIDE BETTER CORROSION PROTECTION AND INSPECTION/LUBRICATION SCHEDULE AND INST
- [SDR W1V2014F00001](https://openairdocs.org/sdr/W1V2014F00001), Mar 28, 2014: VALVE. CORRODED. AT FIRST ANNUAL INSPECTION SINCE NEW FOUND POWER LEVER TO HAVE RESISTANCE FROM REVERSE GOING FORWARD TO THE IDLE GATE. FOUND CSU TO HAVE HEAVY RUST IN THE DRY A
- [SDR W1V2014F00000](https://openairdocs.org/sdr/W1V2014F00000), Sep 13, 2013: VALVE. CORRODED. AIRCRAFT LANDED SHORT DUE TO REPORTED "STUCK THROTTLE" CONDITION. INVESTIGATION FOUND CSU BETA VALVE TO BE CORRODED (HEAVY RUST). AFTER REPAIR OF ACFT INCLUDING
- [SDR 99ZZZX26](https://openairdocs.org/sdr/99ZZZX26), Dec 17, 1998: HUB. CORRODED. HEAVY CORROSION ON FACE AND INBOARD EDGE OF BLADE SOCKET NR 1. HUB WAS PLACED IN SERVICE IN 1992 OR 1993. TSN IS UNKNOWN.
- [SDR 97ZZZX3329](https://openairdocs.org/sdr/97ZZZX3329), Apr 21, 1997: POWER SUPPLY. CONNECTOR FAULTY. DURING INSTALLATION OF WHELEN POWER SUPPLY PN HDA-CF-14/28 WHILE ATTEMPTING TO CONNECT STROBE HARNESS SOCKET AND JUMPER SOCKET, POWER SUPPLY SOCKET DISCONNECTED

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Beech T-34A](https://openairdocs.org/model/beech-t-34a): 32 registered aircraft, registry code 1152008
- [Beech/Fuji/King T-34A](https://openairdocs.org/model/beech-fuji-king-t-34a): 1 registered aircraft, registry code 1152009

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