Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR UIEA200400022Odor · detectedONCE AIRCRAFT LANDED, NOTICEABLE FUEL FUMES IN AIRCRAFT AND ONCE L1 DOOR WAS OPENED THE GROUND HANDLER NOTICED FUMES TOO. CHECKED ENGINES FOR ANY EVIDENCE OF BIRD STRIKE OR FOD DAMAGE IAW MM 05-51-14, NIL DAMAGE FOUND. CARRIED OTU GENERAL VISUAL INSPECTION OSDR UIEA200300054Slide · misinstalledDURING FC02 CHECK AT AMS, AN INSPECTION OF LEFT U/D TYPE 'A' DOOR THE TECHICIAN NOTICED THAT THE SLIDE DEPLOYMENT HOOK WOULD NOT ENGATE THE SLIDE DEPLOYMENT LINK. THE FIRST OBSERVATION WAS THAT THE SLIDE OUTER COVER (INBOARD SIDE) WAS NOT FLUSH WITH THE DOOR SDR UIEA200300021Controller · failedMIA/UIO - AIR TURNBACK, AFTER TAKEOFF, PRESSURIZATION INOPERATIVE. EXCESSIVE RATE OF CLIMB. WENT TO MANUAL. NO INDICATION OF FAILURE. NO RATE LIMIT LIGHT. FOUND BOTH OUTFLOW VALVES OPEN. UNABLE TO CONTROL PRESSURE MANUAL 'L' OR 'R'. NO FUEL DUMPED. REMSDR P5CA0300770Structure · dentedTHREE DENTS FOUND 5 INCHES LONG X .0312 INCH DEEP IN LEADING EDGE VARIABLE CONTOUR FLAP NR 7 LT WING - ALLOWABLE DAMAGE A/Y 62.5 THEREFORE THIS MINOR DENT ACCEPTABLE IAW SRM REF 57-50-01. 2) DENT 10 INCHES LONG X .5 INCH DEEP IN BULL NOSE LOCATION VARIABLE COSDR P5CA0300717Cable · faultyNR 4 ENGINE COMPRESSOR STALL AT TOP OF DESCENT - EGT 700 DEGREES, N1 20 PERCENT LESS THAN OTHER ENGINES. STALL CLEARED AT 33.0. REPLACED NR 4 ENGINE VSV RETURN CABLE PER MM 75-30-00. BOROSCOPED ENGINE IAW AMM 72-00-00. ENGINE RUN CARRIED OUT AS PER AMM 71-SDR P5CA0200714Windshield · failedL1 WINDOW SHATTERED ON DESCENT. REPLACED WINDOW PER 56-11-02.SDR P5CA0200704Slide · failedRIGHT UPPER DECK ESCAPE SLIDE DEPLOYED ACCIDENTLY, BUT DID NOT DEPLOY FULLY, AND DOOR BOTTLE DISCHARGED. SLIDE ASSY REMOVED & REPLACED PER 25-68-07, PG 601, DOOR AIR BOTTLE REMOVED & REPLACED PER MM 25-68-08 AND PRESSURE CARTRIDGE PER 52-23-15.SDR IUEA02016Pin · misalignedDURING WALK AROUND DAILY CHECK, INSPECTION FOUND NR 4 ENGINE PYLON MIDSPAR FUSE PIN ALIGNMENT STRIPES MISALIGNED BY 0.5 INCH. CLOSER INVESTIGATION POINTS TO POSSIBLE FUSE PIN FAILURE. THIS AS PER MM. FURTHER INSPECTION FOUND SPRING BEAMS CRACKED, REPLACEMSDR 2002F00398Hinge · wornDURING CURRENT D-CHECK AT SIAEC, FOUND L/W NR 11, 12 AND 13 L/E KRUGER FLAP HINGE FITTING ASSEMBLIES WITHWORN AND ELONGATED BORE HOLES. REAMED HOLES. PERFORMED DYE CHECK TO ENSURE CORROSION AND CRACK FREE CONDITION. NO DEFECTS FOUND. FABRICATED AND INSTALLE
Other aircraft with N24837 · 3
The FAA can assign a mark to another aircraft once a registration is cancelled. N24837 is registered now to the first aircraft listed.