Reciprocating engine · exhaust valve · damagedJul 22, 2016
CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE CRACKED AND DISPLAYS EVIDENCE OF HEAT DAMAGE.
From FAA Service Difficulty Reports; matched by N-number and serial number.Landing gear · drag brace · crackedAug 15, 2013
AT SCHEDULED INSPECTION, NLG DRAG BRACE, OEM PN 5142002-5, WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMENT DRAG BRACE HAS BEEN INSTALLED IN ACFT.
From FAA Service Difficulty Reports; matched by N-number and serial number.Landing gear · drag brace · crackedNov 28, 2012
AT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMENT DRAG BRACE HAS BEEN INSTALLED…
From FAA Service Difficulty Reports; matched by N-number and serial number.Electrical power · volt regulator · failedOct 25, 2012
PILOT REPORTED THAT DURING CRUISE FLIGHT, BOTH ALTERNATORS DROPPED OFF LINE AND A SMELL OF SMOKE WAS NOTED IN THE COCKPIT. THE ACFT SUBSEQUENTLY DIVERTED AND LANDED SAFELY. UPON MX INSPECTION, INITIAL C/A OF SUSPECTED OVER VOLTAGE RELAY SHORTING AGAINST PANEL, ADJUSTED CLEARANCE FOR PANEL, AS WELL…
From FAA Service Difficulty Reports; matched by N-number and serial number.Lights · transistor · shortedJul 24, 2012
WHILE IN CRUISE FLIGHT, THE PILOT REPORTED THE OVERHEAD LIGHT ASSY ON THE F/O SIDE SHORTING OUT. THE PILOT THEN DEACTIVATED THE SYSTEM BY DEACTIVATING THE CIRCUIT BREAKER. UPON ARRIVAL THE ACFT WAS INSPECTED BY MX WHERE THE FIRST OFFICER SIDE OVERHEAD LIGHT RESISTOR AND TRANSISTOR WERE REPLACED.
From FAA Service Difficulty Reports; matched by N-number and serial number.Landing gear · drag brace · crackedFeb 8, 2011
AT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OUTLINED IN MEB941-11R1 & RETURNED TO…
From FAA Service Difficulty Reports; matched by N-number and serial number.Ice and rain protection · circuit breaker · burnedJun 3, 2008
ELECTRICAL ODOR AND SMOKE IN CABIN DURING APPROACH. SUBSEQUENT INSPECTION FOUND LOOSE SCREW SECURING WIRE TO CIRCUIT BREAKER TERMINAL AND EVIDENCE OF ARCING. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.