Ice accretion in the right main landing gear wheel brake during departure, which prevented the right main landing gear from rotating on landing and resulted in a runway excursion and subsequent impact with a snow bank.
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.
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.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (3)
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.
Exhaust · muffler · inoperativeMay 26, 2004
DURING DEPARTURE CLIMB OUT OF NONESSENTIAL ELECTRICAL ITEMS. HE INSREASED VENTILATION AS THE CO INDICATOR GOT DARKER INDICATING CO INCREASE. HE RETURNED AND LANDED WITHOUT FURTHER PROBLEMS ALTHOUGH HE DID EXPERIENCE A HEADACHE AND NAUSEA. MAINTENANCE REPLACED THE MUFFLER AND HEATER SHROUD ON THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Flight controls · control cable · out of positionMay 16, 2001
PILOT REPORTED UNCONTROLLABLE PITCH CONTROL AND LIMITED AILERON CONTROL. IN FLIGHT, AFTER TAKEOFF, WHICH RESULTED IN A CRASH LANDING. ON EXAMINATION OF THE AIRCRAFT IT WAS DISCOVERED THAT THE RIBBON CABLE ASSY FOR ELECTRICAL CONTROLS ON THE YOKE, HAD FOULED THE CONTROL WHEEL BEARING ASSEMBLY.…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Electrical power · housing · looseJun 15, 2000
PILOT REPORTED ALTERNATOR INOPERABLE AT TAKEOFF POWER. AT IDLE, ALTERNATOR APPEARED TO OPERATE NORMALLY. UPON EXAMINATION, FOUND THE COARSE THREAD INTERNAL WRENCHING BOLTS HOLDING THE ALTERNATOR CASE HALVES WERE LOOSE, WHICH AT HIGH ENGINE RPM, CAUSED THE CASE TO FLOAT ON THE ARMATURE DRIVING THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.