Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2006FA0000179Line · chafedWHILE COMPLYING WITH SB, FOUND 2 HYDRAULIC LINES PN MY20751107 AND MY20751207 CHAFED 20 PERCENT OF WALL THICHNESS LINES REPLACED. (K)SDR 2006FA0000178Line · chafedWHILE COMPLAYING WITH SB, FOUND 2 HYDRAULIC LINES PN MY20751107 AND MY20751207 CHAFED 20 PERCENT OF WALL THICKNESS LINES REPLACED. (K)SDR QY52001F00000Switch · damagedDURING SCHEDULED MAINTENANCE, A GEAR SWING WAS BEING ATTEMPTED BUT WAS UNABLE TO RETRACT GEAR. FOUND RIGHT, MAIN LANDING GEAR DOOR ACTUATOR SWITCH FAULTY, COULD NOT MAKE CONTACT ON A&B TERMINALS. REMOVED SWITCH FROM ACTUATOR AND FOUND INTERNAL DAMAGE IN ACTSDR QY52001F00001Fitting · corrodedLEFT FUEL DRAIN UNION WAS REMOVED FROM MAIN WING TANK TO SEAL LEAK. UNION WAS FOUND TO BE RUSTED AND PITTED ON INSIDE DIAMETER. PITTING ESTIMATED TO BE ONE THIRD OF WALL THICKNESS.SDR 98ZZZX4504Indicator · mismanufacturedUNIT MANUFACTURED IN 1982 AND STILL IN SEALED PACKAGE WHEN RECEIVED. STABILIZER TRIM GAVE REVERSE INDICATION WHEN INSTALLED. ACTUAL TAIL PLANE POSITION 38 DEGREES/ZERO INDICATION. UNIT EXCHANGED FOR S/N 329 NEW INDICATOR (ALSO MFG 1982) WHICH OPERATED PROPESDR 98ZZZX480Seat Frame · brokenPILOT'S INBOARD ARM REST WAS NOTICED TO FLEX EXCESSIVELY. SEAT BACK UPHOLSTERY REMOVED TO INSPECT SEAT FRAME. FRAME TUBE FOUND COMPLETELY BROKEN THROUGH APPROXIMATELY 4 INCHES BELOW ARM REST ATTACH POINT. BREAK APPEARS TO ORIGINATE FROM A POP RIVET HOLE WHE