# Beech V35-TC

- Type: Aircraft model (FAA registry)
- Registry code: 1151540
- Manufacturer (registry): BEECH
- Model: V35-TC
- Aircraft type: Fixed wing single engine
- Category: Airplane
- Engines: 1 · Reciprocating
- Seats: 6
- Weight class: Up to 12,499 lb
- Cruise speed: 150 mph
- Certification: Type certificated
- Registered aircraft: 1
- Page: https://openairdocs.org/model/beech-v35-tc

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 (1)

- [N5062H](https://openairdocs.org/aircraft/N5062H): [Coati Aviation LLC](https://openairdocs.org/faa-owner/COATI%20AVIATION%20LLC), [San Diego, CA](https://openairdocs.org/faa-place/CA/San%20Diego), built 1967, S/N D-8379

## NTSB investigations (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB SEA83LA107](https://openairdocs.org/ntsb/SEA83LA107), May 25, 1983: Beech V35-TC (N7980M), Wendling, OR, destroyed
- [NTSB MKC69A0040](https://openairdocs.org/ntsb/MKC69A0040), Dec 21, 1968: Beech V35 (N7904M), Piedmont, MO, destroyed, 2 fatal

## 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.

- [Accident 19830525033849A](https://openairdocs.org/incident/19830525033849A), May 25, 1983: Beech D95A (N7980M), Marcola, OR, Destroyed. Lost power VFR on top. Broke out at 500 feet and landed in trees. Low boost inoperative leaky throttle shaft o ring

## Service difficulty reports (2)

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

- [SDR 97ZZZX967](https://openairdocs.org/sdr/97ZZZX967), Feb 20, 1997: CYLINDER. WEAR. DURING 100-HOUR INSPECTION, COMPRESSION CHECK REVEALED ALL SIX CYLINDERS LOW. TOTAL TIME 360.5 HOURS SINCE RAM CONVERSION TO STC SE3631SW ON ALL CYLINDERS. SUSP
- [SDR 95ZZZX486](https://openairdocs.org/sdr/95ZZZX486), Jan 11, 1995: CONTROL CABLE. FRAYED. DURING ROUTINE INSPECTION, FOUND BOTH LEFT AND RIGHT MAIN LANDING GEAR UPLOCK CABLES WITH STRANDS BROKEN. LEFT CABLE CAUSE UNKNOWN. RIGHT CABLE POSSIBLE CORROSI

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