Safety record in brief:1 NTSB accident (substantial damage, Apr 1991)7 ADs may apply16 service difficulty reports
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THE PILOT'S FAILURE TO ENSURE THAT THE AIRPLANE'S LANDING GEAR WAS EXTENDED BY THE PASSENGER WHO HE WAS ALLOWING FLY THE AIRPLANE. A CONTRIBUTING FACTOR RELATED TO THE PILOT'S INADEQUATE SUPERVISION OF THE PASSENGER.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX91LA187)
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. |
| 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.
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.
SHORTLY AFTER TAKEOFF, HAD A REDUCTION IN FUEL FLOW, LANDED WITHOUT INCIDENT. UPON INSPECTION IT WAS NOTICED THAT THE RETAINING LOCKNUT FOR THE MIXTURE CONTROL LEVER HAD BACKED OFF THE LEVER CAUSING THE LEVER TO COME OUT OF RIG AND STRIP THE SPLINES OFF THE LEVER. THE TECH INSTALLED A O/H FUEL…
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED THAT THE NAV LIGHT WAS INOPERATIVE. THE TECHNICIAN TROUBLESHOT THE SYSTEM AND DISCOVERED THE NAV LIGHT FAILED. THE TECHNICIAN REPLACED THE NAV LIGHT CIRCUIT BREAKER SWITCH. NO CAUSE OR RECOMMENDATION AT THIS TIME.
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED THAT THE BEACON LIGHT WAS INOPERATIVE. TROUBLESHOT SYSTEM AND DISCOVERED BEACON LIGHT CIRCUIT BREAKER FAILED. REPLACED THE CIRCUIT BREAKER.
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED THE TAXI LIGHT AS BEING INOPERATIVE. ON TROUBLESHOOTING, FOUND THE CIRCUIT BREAKER TO BE AT FAULT. REPLACED THE CIRCUIT BREAKER.
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED BEACON LIGHT INOP. ON TROUBLESHOOTING, TECH FOUND CIRCUIT BREAKER/ SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 2466 FLIGHT HOURS PRIOR. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME.
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED STROBES LIGHT’S INOP. ON TROUBLESHOOTING TECHNICIAN FOUND CIRCUIT BREAKER / SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 2300 FLIGHT HOURS PRIOR, ESTIMATED CYCLES 9200. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME.
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED THE GYRO WARNING LIGHT CAME ON IN FLIGHT. UP ON TROUBLESHOOTING THE MECHANIC FOUND THE SHAFT SHEARED. INSTALLED NEW PUMP, SYS WORKED NORMAL. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME.
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED TAXI LIGHT INOP. ON TROUBLESHOOTING TECH FOUND CIRCUIT BREAKER/ SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 923 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 3692. NOTICED NEW CIRCUIT BREAKER MFG. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED TAXI LIGHT INOP. ON TROUBLESHOOTING TECHNICIAN FOUND CIRCUIT BREAKER / SWITCH TO BE AT FAULT. A.D. 2008-13-17 HAD BEEN COMPLETED 1180 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 4720. NOTICED NEW CIRCUIT BREAKER MANUFACTURER IS TYCO ELECTRONICS. NO PROBABLE CAUSE OR RECOMMENDATIONS AT…
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED AFTER PUTTING THE GEAR SELECTOR IN THE UP POSITION, THE GEAR FAILED TO RETRACT, PILOT THEN PUT THE GEAR SELECTOR IN THE DOWN POSITION AND RETURNED TO BASE. ON TROUBLESHOOTING, THE MECHANIC CYCLED GEAR SEVERAL TIMES AND WAS UNABLE TO GET THE GEAR TO FAIL. PROBABLE CAUSE AT THIS TIME…
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 16 reports.