Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR Q2S2002F00002Duct · blownAIR TURNBACK, ON TAKEOFF, AT 2500 FEET MSL, WITH TAKEOFF POWER AT 113.0 N1, NR 2 ENGINE FIRE LIGHT AND BELL CAME ON. NACELLE INDICATOR BOTH A AND B READ 6.5 SHUTDOWN ENGINE IAW QRH. DUMPED 18,700 LBS OF FUEL. NO EVIDENCE OF FIRE FOUND ON INSPECTION OF ENGINSDR Q2S2002F00001Valve · malfunctionedAIR TURN BACK: AFTER LIFT OFF, HIGH STAGE LIGHT ILLUMINATED ABOUT 200 FEET. FIRE DETECTION LIGHT ILLUMINATED AT MASTER CAUTION PANEL, NO LIGHT IN HANDLE. A AND B NEEDLE INDICATORS WERE AT 7.5. TESTED SYSTEM, NR 3 LIGHT CAME ON AND STAYED ON. SHUT DOWN ENGSDR 2003F00061Connector · looseDURING TAKEOFF, AT 60 KNOTS, FIRE DETECTION LIGHT ON FORWARD INSTRUMENT PANEL ILLUMINATED AND NR 3 ENGINE NACELLE TEMPERATURE INDICATOR 'B' LOOP WAS AT 8.5 ON INDICATOR. CHECKED FOR AIR LEAK IAW AMM 36-11-00, NO DISCREPANCIES NOTED. CHECKED FIRE LOOP NR 3 ENSDR 2001F00202Panel · crackedDURING PREFLIGHT, FOUND LEFT WING UPPER PANEL ASSEMBLY ABOVE NR 2 ENGINE PYLON AND ABOVE NR 1 SLAT CRACKED APPROXIMATELY 48 INCHES LONG FROM FORWARD TO AFT OF PANEL. REMOVED, REPAIRED AND REINSTALLED PANEL ASSEMBLY. REPAIRED IAW SRM 51-40-09 AND 51-40-12. (SDR 2001F00162Panel · crackedDURING PREFLIGHT, FOUND LEFT WING UPPER PANEL ASSEMBLY ABOVE NR 2 ENGINE PYLON AND ABOVE NR 1 SLAT CRACKED APPROXIMATELY 48 INCHES LONG FROM FORWARD TO AFT OF PANEL. REMOVED, REPAIRED AND REINSTALLED PANEL ASSEMBLY. REPAIRED IAW SRM 51-40-09 AND 51-40-12. (SDR 20010206SG002Actuator · brokenDURING CRUISE, THE RED GEAR WARNING LIGHT ILLUMINATED INTERMITTENTLY. PLACED GEAR HANDLE IN THE UP POSITION AND HEARD THUMPING NOISE APPARENTLY FROM THE NOSE LANDING GEAR (NLG) WHEEL WELL AREA WITH SUBSEQUENT LOSS OF NR 1 SYSTEM HYDRAULIC QUANTITY. PLACED GESDR 20010108AP010Structure · damagedON POSTFLIGHT, FOUND NR 15 LEADING EDGE KRUEGER FLAP DAMAGED AND APPROX HALF OF FLAP PARTIALLY SEPARATED ROM MOUNTS CAUSING IMPACT DAMAGE TO THE RIGHT HORIZONTAL STABILIZER LEADING EDGE AND UPPER SURFACE. REPLACED NR 15 LEADING EDGE KRUEGER FLAP. REPAIRED DASDR 20010108AP009Structure · damagedON POSTFLIGHT, FOUND NR 15 LEADING EDGE KRUEGER FLAP DAMAGED AND APPROXIMATELY HALF OF FLAP PARTIALLY SEPARATED FROM MOUNTS CAUSING IMPACT DAMAGE TO THE RIGHT HORIZONTAL STABILIZER LEADING EDGE AND UPPER SURFACE. REPLACED NR 15 LEADING EDGE KRUEGER FLAP. REP
Other aircraft with N744SA · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N744SA is registered now to the first aircraft listed.