FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N465TM and the event date: up to this one’s cancellation.
Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CVGA20250219005Cabin Pressure · inoperativeON TAKEOFF AND CLIMB OUT AIRPLANE NOT PRESSURIZING. CYCLED PRESS SOURCE KNOBS WITH NO CHANGE- EMERGENCY DECLARED.SDR CVGA20250129006Brake · failedLEFT BREAK FAILED DURING TAXING. PERFORMED FUNCTIONAL TESTING MANUAL BRAKE SYSTEM AND POWER BRAKE SYSTEM IAW 400A AMM 32-40-00. PERFORMED POWER BRAKE BLEEDING IAW 400A AMM 32-40-00. NO DEFECTS NOTED. GAUGE ID# TL-00509, DUE 10/22/2025, GAUGE ID# TL-00503, DUE SDR CVGA20231211001Oxygen Bottle · emptyO2 NEEDS SERVICE FOR POSSIBLE LEAK. READS 0 ON GAUGE. REMOVED AND REPLACED O2 BOTTLE REF B400 AMM CH 35-11-00. OPS AND LEAK CHECK PASSED AT THIS TIME. NO DEFECTS NOTED. EMERGENCY WAS DECLARED.SDR CVGA20210601001Mixing Valve · intermittentLOSS OF BRAKE PRESSURE ON ALL BRAKE PEDALS AFTER LANDING. BRAKE PRESSURE DID COME BACK AFTER ABOUT 1O SECONDS. HYDRAULIC PRESSURE WAS IN THE GREEN.SDR T17A20200811044Brake Assy · abnormalAFTER A NORMAL LANDING W/NORMAL BRAKING ENTERED THE FBO RAMP LT TURN WHERE LT RUDDER PEDAL AND BRAKING ALONG W/DIFFERENTIAL POWER WAS REQUIRED. LT RUDDER PEDAL BLED TO THE FLOOR WHEN BRAKES WERE APPLIED THIS OCCURRED ONLY ON CAPTAINS SIDE. PERFORMED VISUAL BSDR E81RJT2309420BDuct · crackedDURING SCHEDULED INSPECTION, FOUND LT ENGINE NACELLE ANTI-ICE CROSSOVER BLEED AIR DUCT CRACKED AT BELLOWS, STAINLESS STEEL BRAIDING FRAYED AND BLOWN-OUT. MX HISTORY UNKNOWN. MAY POSSIBLY HAVE BEEN CAUSED BY PARTIAL MIS-ALIGNMENT STRESS. RECOMMEND MFG INVESTISDR E81RJT2309420ADuct · crackedDURING SCHEDULED INSP, FOUND LT ENGINE INBD SIDE ENGINE PAD TO "Y" DUCT BLEED AIR ANTI-ICING DUCT CRACKED AT BELLOWS, STAINLESS STEEL BRAIDING BLOWN-OUT AND FRAYED. MX HISTORY UNKNOWN, POSSIBLY CAUSED BY MIS-ALIGNMENT. RECOMMEND MFG INVESTIGATE WHETHER THIS ISDR 2009F00010Fuel Control · malfunctionedCREW REPORTED LT ENGINE WOULD NOT ACHIEVE CALCULATED TAKEOFF POWER N1. VERIFIED COMPLAINT, ENGINE COULD NOT ACHIEVE MORE THAN 94 PERCENT, N1 AND NOTED NO RPM DROP DURING EFC AUTHORITY CHECKS. ALSO NOTED FLUCTUATING ENGINE VIBRATION INDICATION. EFC AUTHORITY AD