Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 98ZZZX4780Bulkhead · crackedDURING A ROUTINE INSPECTION, THE FIREWALL WAS FOUND CRACKED IN 3 PLACES. THE FIREWALL THICKNESS - .016 INCH WHICH IS THINNER THAN OLDER MODELS WHICH ARE BETWEEN .020 INCH AND .024 INCH. (IT IS DIFFICULT FOR AN ACCURATE MEASUREMENT TO BE TAKEN WITHOUT DISASSESDR 98ZZZX4315Skin · crackedDURING A ROUTINE INSPECTION, NOTED BOTH LT AND RT TRAILING EDGE SKINS IN THE FLAP WELLS HAD MULTIPLE CRACKS RANGING FROM .25 INCH TO 2 INCHES EMANATING FROM RIVET HOLES. MAINTENANCE CHECKED ALL TRAVEL OF THE FLAPS, FLAP TRAVEL WAS WITH SPECS AND NOT HITTING TSDR 98ZZZX4314Skin · crackedDURING ROUTINE MAINTENANCE, BOTH FLAP LEADING EDGE SKINS WERE FOUND CRACKED. CRACKS WERE AROUND THE RIVET HOLES WERE P/N 0523923 26, ATTACHES TO FLAPS ON THE BOTTOM SIDE. CRACKS WERE .25 INCH - .50 INCH IN LENGTH, AND ALMOST EVERY RIVET HOLE WAS AFFECTED. SSDR 98ZZZX3198Fuel Servo · scoredWHILE DOING A GROUND RUN-UP PRIOR TO A 100-HOUR INSPECTION, MAINTENANCE NOTICED THE ENGINE, UPON REACHING OPERATING TEMP, BEGAN TO RUN ROUGH AT LOWER POWER SETTINGS. THE FUEL FLOWS ALSO WERE EXTREMELY ERRATIC. NO FURTHER ACTION HAS BEEN TAKEN. THIS IS AN ORSDR 98ZZZX1344O-Ring · incorrectINCORRECT O-RING INSTALLED AT FACTORY. SUBMITTER STATED THERE WAS A POSSIBILITY O-RING SWELLED CAUSING LOSS OF BRAKE PRESSURE.SDR 98ZZZX513Fuse Connector · failedFOUND COLD SOLDER AT FUSE CONNECTION FOR NR 1 BUS. WIRE PULLED OUT AFTER TROUBLESHOOTING DEFECTIVE BUS, COLD WIRE WAS NOT INSTALLED IN RETAINING HOLE, BUT LAID ON TOP AND IMPROPERLY SOLDERED AND COVERED WITH HEAT SHRINK.SDR 97ZZZX4055Hose · leakDEFECTIVE HOSE FOUND DURING ROUTINE INSPECTION. CLAMPS FOR HEAT SLEEVE WERE TIGHTENED EXCESSIVELY, LEAKING AT THAT AREA.
Other aircraft with N97100 · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N97100 now.