N168M1968 Beechcraft V35A
Safety record in brief:No NTSB accidents or incidents since 19827 ADs may apply1 service difficulty report
Registration
FAA Aircraft Registry · Oct 17, 2026- Registered owner
- Individual owner
- City, state
- Anchorage, AK
- Certificate issued
- May 24, 2016
- Expires
- May 31, 2029
- Airworthiness
- Standard · Utility
- Airworthiness date
- Mar 19, 1968
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Beechcraft
- Model
- V35A
- Year
- 1968
- Serial number
- D-8762
- Aircraft type
- Fixed wing single engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 6
- Engines
- 1
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A11079
Engine
- Make and model
- Cont Motor Io 520 Series
- Type
- Reciprocating
- Power
- 285 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2016 – nowIndividual ownerAnchorage, AK · current
- 1941 – 1948Boulevard Airport INCPhiladelphia, PA · different airframe: New Standard D-29a S/N 015
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (7)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2019-23-10 | Aileron Control System | Nov 22, 2019 | Airframe (V35A)Certain serial numbers: F33A CE-290–CE-680; F33C CJ-26–CJ-128; V35B D-9069–D-9961; A36 E-185–E-925. Only with: Models E33, E33A, E33C, F33, G33, 35-C33, 35-C33A, S35, V35, V35A, and 36 apply to all serial numbers. |
| 2018-06-11 | Turbocharging | May 3, 2018 | Airframe (V35A)Only with: A36TC/B36TC equipped with turbocharged engine; S35/V35/V35A/V35B equipped with factory Continental TSIO-520-D engine with AiResearch turbocharger (excluded if one-piece v-band coupling P/N NH1000897-40 installed) or with StandardAero STC SA1035WE. |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (IO 520 SERIES)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed. |
| 94-20-04 R2 | Raytheon Aircraft Company Beech Models C35, D35, E35, F35, G35, H35, J35, K35, M35, N35… | Jun 27, 2003 | Airframe (V35A)Only with: Models S35, V35, V35A, and V35B apply only if the straight tail conversion modification per STC SA2149CE is not incorporated. |
| 2001-08-08 | Raytheon Aircraft Company Beech Models 35-C33A, E33A, E33C, F33A, F33C, S35, V35, V35A… | Jun 7, 2001 | Airframe (V35A)Only with: Incorporating a Teledyne Continental engine with a turbonormalizing system and Tornado Alley Turbo, Inc. STC SA5223NM and STC SE5222NM. |
Show all 7 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 99-05-13 | Raytheon Aircraft Company 17, 18, 19, 23, 24, 33, 35, 36/A36, A36TC/B36TC, 45, 50, 55… | Apr 19, 1999 | Airframe (V35A)Certain serial numbers: F33A CE-290–CE-1791; E33C CJ-26–CJ-179; F33C CJ-26–CJ-179; A36 E-185–E-3046; B36TC EA-242–EA-591; 58 TH-1–TH-1798 |
| 97-14-15 | Raytheon Aircraft Company (Formerly Known as Beech Aircraft Corporation) Models E33… | Sep 2, 1997 | Airframe (V35A) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (1)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Reciprocating engine · seal · leaksOct 19, 1995
SHORTLY AFTER REPLACING A REPAIRED NR 5 CYLINDER, OIL LEAKS DEVELOPED AROUND OUTBOARD ENDS OF SHROUD TUBES. COMPARISON TO ORIGINAL TCM PARTS SHOWED REPLACEMENT SEAL TO BE LARGER IN OUTSIDE DIAMETER CAUSING SEAL NOT TO PROPERLY FIT IN MACHINED RECESS CAUSING LEAKS.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026