NTSB investigations · 1
Matched to this aircraft by N752SA and the event date: up to this one’s cancellation.
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N752SA and the event date: up to this one’s cancellation.
Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR Q2SA752010A/C Pack · damagedUPON CLIMB, A NOISE WAS HEARD BY THE CREW ACCOMPANIED WITH A SMELL AND THEN SMOKE IN THE COCKPIT. THE FLIGHT ENGINEER IMMEDIATELY TURNED OFF THE LEFT PACK AND THE SMOKE STOPPED. AFTER REQUEST AND SUBSEQUENT APPROVAL TO HOLD TO CONSULT MANUALS, THE CREW AND OSDR Q2SA752009Actuator · brokenAIR TURN BACK: NR1 HYD SYSTEM FAILURE. MASTER WARNING INDICATION AFTER GEAR RETRACTION, UPON DEPARTING, SYSTEM INDICATED TOTAL FLUID LOSS AND FAILURE OF THE NR 1 HYD SYS. GEAR RETRACTED NORMALLY AND FLAPS WERE STILL IN POSITION 10. WHILE WORKING THROUGH THE ASDR Q2SA752008Comparator · failedAT FLIGHT LEVEL 31.0 A/C HAD INDICATOR SPLIT RUDDER. UPPER RUDDER 5 DEG RT TO LWR RUDDER 2 UNITS TO THE LEFT. A SHORT TIME LATER, UNCOMMANDED INPUT TO RUDDER, NECESSITATED EXCESSIVE AILERON USE TO CONTROL. AT APPROXIMATELY 14,000 FT AND SPEED LESS THAN 250 SDR Q2SA752007Wire · brokenNR 4 LEADING EDGE FLAP DID NOT RETRACT AFTER TAKEOFF. AMBER LEADING EDGE FLAP LIGHT ON FORWARD PANEL AND FLIGHT ENGINEER PANEL ILLUMINATED. REPAIRED WIRE NR W840-C345-20R PER WDM 20-30-12.SDR 752006Regulator Valve · leakingNR 1 ENGINE MAXIMUM TAKEOFF POWER. PILOT'S PANEL ENGINE LOOP FAULT LIGHT ILLUMINATED INTERMITTENTLY FOLLOWED BY INTERMITTENT FIRE WARNING. NACELLE TEMPERATURE FLUCTUATED 5 TO FULL SCALE. SET CLIMB POWER. NACELLE TEMPERATURE A & B SETTLED TO 2.0. TAKEOFF POSDR 752005Circuit Card · malfunctionedMAXIMUM POWER TAKEOFF OUT OF PANC, N1 SET AT 105.8 PERCENT. AFTER TAKEOFF PASSING THRU 1000 FEET, NR 1 ENGINE NACELLE FAULT LIGHT ILLUMINATED INTERMITTENTLY ACCOMPANIED BY FIRE WARNING. BELL ALSO RANG INTERMITTENTLY. NACELLE INDICATORS A & B WERE FLUCTUATINSDR Q2SA752004Wire Harness · shortedNR 3 ENGINE NACELLE A & B LOOP ON TAKEOFF HAD FLICKERING ENGINE FIRE INDICATION WITH FLICKERING FAULT LIGHT ON FLIGHT ENGINEER PANEL AT APPROXIMATELY 91 PERCENT N1. NACELLE TEMPERATURE INDICATION FLUCTUATED ABOVE 2.5 TO 7.0. A & B LOOP FLUCTUATED.SDR 752003Relief Valve · leakingNR 1 ENGINE FIRE LIGHT ILLUMINATED AT 17,000 FEET. PERFORMED QRH CHECKLIST, WITH THRUST LEVER CLOSED AND START LEVER CUTOFF, ENGINE FIRE LIGHT WENT OUT AND NACELLE TEMPERATURE DROPPED. ENGINE HYDRAULIC PUMP WAS NOT PUT INTO SUPPLY OFF. FIRE HANDLE WAS NOT PSDR 752001Duct · leakingNR 3 ENGINE FIRE LOOP FAULT LIGHT ILLUMINATED WITH ASSOCIATED AURAL FIRE WARNING HORN. ENGINE SHUTDOWN AND DISCHARGED FIRE EXTINGUISHER BOTTLE. DUMPED 150,000 LBS OF FUEL AND RETURNED TO DEPARTING AIRPORT (RKSI).SDR 752002Relief Valve · leakingNR 3 ENGINE NACELLE TEMPERATURE ROSE INTO THE YELLOW BAND AT CLIMB POWER OF 103% N1. RETARDED THRUST LEVER TO 65% N1 AND TEMPERATURE DROPPED INTO NORMAL RANGE.
Other aircraft with N752SA · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N752SA now.