NTSB investigations · 1
Matched to this aircraft by N955AA and the event date: after March 16, 1990, when the previous aircraft’s registration ended, through this one’s cancellation.
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N955AA and the event date: after March 16, 1990, when the previous aircraft’s registration ended, through 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 TIMA20090003Rib · crackedINBOARD RIB WAS CRACKED AT LEADING EDGE. CRACKS BEGIN IN BOTH UPPER AND LOWER FLANGE RADIUS AND PROGRESSED THROUGH THE FIRST RIVET HOLE IN THE WEB. CRACKS EXTENDED ABOUT .5 INCH PAST THE RIVETS WHEN DISCOVERED. THE ELEVATOR BALANCE WEIGHT SUPPORT BOLTS TO TSDR 20001109SH039Skin · crackedDURING ROUTINE INSPECTION, A CRACK WAS FOUND ON THE LEFT STABILATOR LOWER SKIN. (X)SDR 20000424SH023Scissors · crackedDURING DETAILED LANDING GEAR INSPECTION, THE SCISSORS ON THE RT MAIN GEAR WERE FOUND CRACKED. THE CRACKS ARE LOCATED NEAR THE MACHINED RADIUS WHERE THE TWO SCISSORS CONNECT. IT WAS DETERMINED THE CRACKS WERE, OR COULD HAVE BEEN CAUSED BY THE TORQUE KNEE BOLTSDR 99ZZZX4608Hinge · crackedCREW DOOR MISALIGNED WHEN PILOT ATTEMPTED TO SECURE. INSPECTION REVEALED FORWARD HINGE CRACKED AT HINGE PIN REGION. HINGE HALF WAS REPLACED WITH SERVICEABLE HINGE HALF. AN INFORMAL INSPECTION OF ALL COMPANY AIRCRAFT RESULTED IN NO OTHER DISCREPANCIES.SDR 99ZZZX4394Boot · failedLIP DEICE BOOT TRIPPED CIRCUIT BREAKER IN-FLIGHT. POST-FLIGHT INSPECTION REVEALED DEICER BURNED UP LEAVING EXPOSED WIRES AND CHARING ON COWL. DEICER WAS THEN REPLACED FOLLOWING REPAIRS TO COWL. SEVERAL THINGS COULD HAVE CONTRIBUTED TO THE PROBLEM INCLUDING SDR 99ZZZX795Fuel Cel · leakingPILOT REPORTED EVIDENCE OF FUEL ON RT OUTBOARD GEAR DOOR. INSPECTION REVEALED FUEL LEAK SOURCE AT BOX FUEL CELL JUST OUTBOARD OF NACELLE, AFT OF SPAR. REPLACED FUEL CELL; POST-WORK OPS CHECKS OK. POSSIBLE CAUSE - FUEL CELL AGE AND/OR IMPROPER INSTALLATION OSDR 98ZZZX4710Actuator · failedON POST-FLIGHT INSPECTION, PILOT REPORTED HYDRAULIC FLUID ON LOWER FUSELAGE AND TAIL. MECHANICS WERE NOTIFIED AND CLOSER INSPECTION REVEALED FLUID LEAKING FROM LOWER SHAFT SEAL. AIRCRAFT WAS JACKED AND GEAR SWUNG TO VERIFY SOURCE OF LEAKAGE. PROBLEM DUPLICASDR 98ZZZX1171Nut · corrodedRUDDER TAB ACTUATOR NUT FOUND CORRODED DURING ROUTINE INSPECTION.
Other aircraft with N955AA · 2
The FAA can assign a mark to another aircraft once a registration is cancelled. N955AA is registered now to the first aircraft listed.