This N-number isn't registered right now. Below is its last known registration, canceled Jan 3, 2018.
Safety record in brief:1 NTSB accident (substantial damage, Sep 2012)10 ADs may apply2 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
In-flight loss of control for reasons that could not be determined because postaccident examination of the pilot and testing of the airplane did not reveal any anomalies that would have led to the loss of control.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN12FA617)
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 (A36)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 (A36)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-550 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 (A36)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. |
| 2003-01-01 | Raytheon Aircraft Company Beech Models 36, A36, A36TC, B36TC, 58, and 58A Airplanes | Feb 27, 2003 | Airframe (A36)Certain serial numbers: A36 E-185–E-3231; A36 E-3233; B36TC EA-242; B36TC EA-273–EA-635; 58 TH-1–TH-1811; 58 TH-1813–TH-1897; … |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2001-08-08 | Raytheon Aircraft Company Beech Models 35-C33A, E33A, E33C, F33A, F33C, S35, V35, V35A… | Jun 7, 2001 | Airframe (A36)Only with: Incorporating a Teledyne Continental engine with a turbonormalizing system and Tornado Alley Turbo, Inc. STC SA5223NM and STC SE5222NM. |
| 2000-26-16 | Raytheon Aircraft Company Beech Models A36, B36TC, and 58 Airplanes | Feb 16, 2001 | Airframe (A36)Certain serial numbers: A36 E-1–E-3231; A36 E-3233; B36TC EA-1–EA-635; 58 TH-1–TH-1811; 58 TH-1813–TH-1897 |
| 2000-20-14 | Raytheon Aircraft Company Beech Models A36 and B36TC Airplanes | Nov 28, 2000 | Airframe (A36)Certain serial numbers: A36 E-3113–E-3231; A36 E-3233–E-3263; A36 E-3265–E-3267; A36 E-3269; A36 E-3271; A36 E-3273; … |
| 99-05-13 | Raytheon Aircraft Company 17, 18, 19, 23, 24, 33, 35, 36/A36, A36TC/B36TC, 45, 50, 55… | Apr 19, 1999 | Airframe (A36)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 (A36) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
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.
TROUBLESHOT STIFF RUDDER PEDAL STEERING AND REPLACED PILOTS RT ARM ASSY. PN 002-524012-1 WITH NEW IAW MM. APPEARS ARM ASSY ROLLER BEARING WAS NEVER LUBED DURING BUILD OF AIRCRAFT. THE ROLLER BEARING WEAR CAUSED THE ARM TO SEIZE ON THE RUDDER PEDAL TORQUE TUBE AT RANDOM TRAVEL POSITIONS. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.ALTERNATOR WAS REMOVED FROM ENGINE FOR CYLINDER REMOVAL ACCESS. WHILE REMOVED A 500 HOUR INSPECTION WAS INITIATED. THE STATOR WINDINGS WERE DISCOVERED TO BE OVERHEATED AND BLACKENED. ALTERNATOR HAD ACCUMULATED ONLY 241.7 HOURS SINCE LAST 500 HOUR INSPECTION. THIS FACILITY HAS BEEN DOING 500…
From FAA Service Difficulty Reports; matched by N-number and serial number.