N1566P1988 Beechcraft F33A
Safety record in brief:No NTSB accidents or incidents since 19827 ADs may apply1 service difficulty report
Registration
FAA Aircraft Registry · Oct 19, 2026- Registered owner
- Beech Powers LLC
- Owner type
- LLC
- City, state
- Henderson, NV
- Certificate issued
- Jun 4, 2018
- Expires
- Jun 30, 2028
- Airworthiness
- Standard · Utility
- Airworthiness date
- Nov 30, 1988
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
- F33A
- Year
- 1988
- Serial number
- CE-1294
- Aircraft type
- Fixed wing single engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 5
- Engines
- 1
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A0E3B1
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- 2018 – nowBeech Powers LLCHenderson, NV · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 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 (F33A)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. |
| 2009-25-01 | Hawker Beechcraft Corporation Models 58, 58A, 58P, 58PA, 58TC, 58TCA, 95-B55, 95-B55A… | Jan 8, 2010 | Airframe (F33A)Certain serial numbers: 58 TH-733–TH-1609; 58A TH-733–TH-1609; 58P TJ-3–TJ-497; 58PA TJ-3–TJ-497; 58TC TK-1–TK-151; 58TCA TK-1–TK-151; … |
| 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. |
| 2008-13-17 | Hawker Beechcraft Corporation (Type Certificates No. 3A15, No. 3A16, No. A23CE, and No.… | Aug 6, 2008 | Airframe (F33A)Certain serial numbers: F33 CD-1235–CD-1304; G33 CD-1235–CD-1304; F33A CE-290–CE-1791; F33C CJ-26–CJ-179; V35B D-9069–D-10403; A36 E-185–E-3629; …. Only with: Circuit breaker toggle switch P/N 35-380132-1 through 35-380132-53 installed. |
| 2001-08-08 | Raytheon Aircraft Company Beech Models 35-C33A, E33A, E33C, F33A, F33C, S35, V35, V35A… | Jun 7, 2001 | Airframe (F33A)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 (F33A)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 (F33A) |
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.
- Air conditioning and pressurization · shaft · failedFeb 6, 1998
UPON INSTALLING VALVE ASSY ON THE A/C HEAT VENT, THE ARM PORTION OF THE SHAFT ASSY BROKE OFF. INVESTIGATION FOUND THE WELD AT THE BOTTOM OF THE ARM POSITION MISSING WHEN COMPARED TO THE ORIGINAL ASSY. THE TOP PORTION APPEARED TO HAVE BEEN WELDED AND GROUND DOWN WITH LITTLE OR NO PENETRATION OF THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026