Safety record in brief:1 NTSB accident (substantial damage, Oct 2015)7 ADs may apply20 service difficulty reports
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The student pilot's failure to maintain sufficient airspeed during the base to final turn resulting in an inadvertent aerodynamic stall and impact with terrain during recovery by the flight instructor.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for GAA16CA013)
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.
PILOT REPORTED THAT THE LANDING LIGHT WAS INOPERATIVE. THE TECHNICIAN TROUBLESHOT THE SYSTEM AND DISCOVERED THE LANDING LIGHT WAS INTERMITTENTLY FAILING. THE TECHNICIAN REPLACED THE CIRCUIT BREAKER.
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED THAT THE ANTI-COLLISION LIGHTS WERE INOPERATIVE. THE TECH TROUBLESHOT THE SYSTEM AND DISCOVERED THE ANTI-COLLISION LIGHTS FAILED. THE TECH REPLACED THE CIRCUIT BREAKER. NO CAUSE OR RECOMMENDATION AT THIS TIME.
From FAA Service Difficulty Reports; matched by N-number and serial number.GEAR REMAINED UP WHEN DOWN SELECTED IN PATTERN FOR LANDING. GEAR OPERATED NORMALLY ON SECOND ATTEMPT. REMOVED AND REPLACED DYNAMIC BRAKE RELAY, GEAR OP CHECKS GOOD ON NUMEROUS CYCLES.
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED TAXI LIGHT INOP. ON TROUBLESHOOTING, TECH FOUND CIRCUIT BREAKER TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 2593 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 10372. RECOMMEND MFG IMPROVE DESIGN FOR A MORE DURABLE CIRCUIT BREAKER OR ACFT MFG SEARCH FOR A MFG WITH A MORE DURABLE…
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED STROBE INOPERATIVE. ON TROUBLESHOOTING THE TECH FOUND THE CIRCUIT BREAKER AT FAULT. INSTALLED NEW CIRCUIT BREAKER/SWITCH. OPS CHECK OK. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME.
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED LANDING LIGHT INOP. ON TROUBLESHOOTING, TECH FOUND CIRCUIT BREAKER/SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 1900 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 7600. 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.LANDING GEAR WILL NOT RETRACK OR EXTEND. DYNAMIC RELAY FAILED.
From FAA Service Difficulty Reports; matched by N-number and serial number.WHILE ON A TRAINING MISSION, THE PILOT NOTICED THE FUEL FLOW WAS 18 GPH DURING CLIMB, PILOT REPORTED FUEL FLOW WAS NORMAL ON TAKEOFF. ON TROUBLESHOOTING, THE MX FOUND THE ARM ON THE MIXTURE SIDE WAS VERY ROUGH. FUEL METERING UNIT WAS REPLACED AND RUN-UP WAS PERFORMED, OPS CHECK GOOD. NO PROBABLE…
From FAA Service Difficulty Reports; matched by N-number and serial number.MECHANIC REMOVED NEW RELAY FROM STOCK AND INSTALLED ON AIRCRAFT AND GEAR FAILED TO EXTEND, AFTER TAPPING ON THE TOP OF RELAY GEAR WENT DOWN. MECHANIC THEN INSTALLS ANOTHER NEW RELAY FROM STOCK AND SYSTEM OPERATED NORMAL. PROBABLE CAUSE AT THIS TIME UNKNOWN. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.GEAR WOULD NOT RETRACT MADE NO NOISE AT ALL. MAINTENANCE TECH TROUBLESHOOT GEAR SYSTEM AND FOUND THAT THE DYNAMIC RELAY WAS INTERMITTENT. NO RECOMMENDATION AT THIS TIME. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 20 reports.