N538DA, cancelled Jun 4, 2013

Service difficulty reports · 42

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N538DA' AND deregistration_id = 'N538DA-2013-06-04'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DL72S011404Pressure Switch · intermittentLOW OIL PRESSURE/FILTER BYPASS LIGHT ILLUM IN FLIGHT. OIL PRESSURE WAS NORMAL AND PRECAUTIONARY ENG SHUTDOWN WAS ACCOMPLISHED. REPLACED DIFF PRESS SWITCH AND LOP/FILTER BYPASS LIGHT MODULE ALONG WITH MASTER DIM AND TEST DIODE CARD. RAN ENGS AT HIGH POWER AND IAug 25, 2001 · N538DA · Boeing 727232 · Engine Oil PressureSDR DL72S011400Warning System · malfunctionedDURING CLIMBOUT NR 1 ENGINE LOW OIL PRESSURE OR FILTER BYPASS LIGHT ILLUMINATED. RAN POM PROCEDURE ACCOMPLISHED INFLIGHT SHUTDOWN DUE TO SUSPECTED FILTER BYPASS. ALL OTHER OIL INDICATIONS NORMAL. CA REPLACED AND INSPECTED OIL FILTER. NO TROUBLE FOUND. LEAK CKSAug 24, 2001 · N538DA · Boeing 727232 · Engine Oil PressureSDR DL72S011339Frame · wornTHE INNER CHORD OF THE RH FS 1303 FRAME WAS FOUND WITH A 1INCH AREA OF WEAR ON THE INNER FLANGE JUST ABOVE THE VENTRAL STAIRWAY TORQUE BOX DUE TO CONTACT WITH A LOOSE HYDRAULIC LINE CLAMP. THE DAMAGED AREA OF FLANGE WAS TRIMMED OUT. THE CHORD WAS REPAIRED Aug 14, 2001 · N538DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S011333Beam · crackedINSPECTION OF THE VENTRAL STAIRWAY TORQUE BOX STRUCTURE PER BAC S/B 727-53-0129 AND AD 94-07-08 REVEALED TYPICAL CRACKS IN THE RT HORIZONTAL BEAM AT FS 1263 & 1273. THE CRACKED STRUCTURE WAS REMOVED AND REPLACED WITH NEW STRUCTURE PER ER/A 381539-14AD.Aug 14, 2001 · N538DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S011203Light · inoperativePAX SEAT 19F EMERGENCY LIGHT INOP. REPLACED SEAT LIGHT ASSY.Jul 20, 2001 · N538DA · Boeing 727232 · Emergency LightingSDR DL72S010553Battery Pack · dischargedFOUND EMERGENCY EXIT LIGHT BATTERY DISCHARGED. REPLACED BATTERY PACK.Apr 3, 2001 · N538DA · Boeing 727232 · Emergency LightingSDR DL72S010523Pump · failedDURING CLIMB CHECK SWITCHED THE NR 1 B ELECTRIC PUMP OFF AND NOTICED PRESSURE FLUCTUATION ON B SYSTEM GUAGE. TURNED NR 1 ELEC PUMP BACK ON AND SEVERAL SECONDS LATER LOW NR 1 PUMP LOW PRESSURE LIGHT ILLUMINATED AND SYSTEM PRESSURE DROPPED TO 2200 PSI- UPON EXMar 30, 2001 · N538DA · Boeing 727232 · Hydraulic Pump (Electric/Engine), MainSDR DL72S010482Channel · crackedCHANNEL P/N 534201717:ATTACH POINT FOR NOSE GEAR RETRACT ACTUATOR SHEARED ON GEAR EXTENSION CAUSING A_SYSTEM COMPLETE FLUID LOSS. REPLACED SAMEMar 23, 2001 · N538DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S010016Angle · crackedA .25 INCH VISIBLE CRACK I/B OF STOP PAD NR 8 SLAT COVE SKIN ATTACH ANGLE. REPAIR PER MM 57-54-000-8.Jan 4, 2001 · N538DA · Boeing 727232 · SpoilersSDR DL72S010015Fitting · crackedFOUND ON F1 LETTER CK, NR 4 SPOILER ACTUATOR I/B MOUNT FITTING IS CRACKED. REPAIRED PER MM 57-42-000-8.Jan 4, 2001 · N538DA · Boeing 727232 · SpoilersSDR DL72S002280Window · leakingLOUD SQUUEAL FROM R2 WINDOW AT 1000 FEET AGL. REPLACED R2 WINDOW AND CHECKED TORQUE ON R3 WINDOW, PRESSURIZIED A/C CHECKS NORMALNov 21, 2000 · N538DA · Boeing 727232 · Flight Compartment WindowsSDR DL72S001776Actuator · malfunctionedSTABILIZER JAMMED IN THE 3 DEGREE NOSE UP POSITION. OCCURRED DURING FLIGHT. A/C OFF LANDED IN CVG. MTC CHANGED ACTUATOR (P/N 274001078) (S/N 104-00AA) AND ACTUATOR (P/N 2774003971) (S/N 1278-00AA. ) A/C FERRY FLIGHT TO ATL FLT 9930 ON 9/14/00. MTC REPLACINSep 13, 2000 · N538DA · Boeing 727232 · Stabilizer ActuatorSDR DL72S001219Beam · damagedWHILE ACCOMPLISHING MANDATED INSPECTIONS OF THE FS 1183, BULKHEAD VERTICAL BEAM AT LBL 17.8 PER AD 99-18-05, A HOLE COMMON TO THE BEAM AND THE WL 273.25 INTERCOSTAL WAS FOUND ELONGATED. THE HOLE WAS REAMED TO A ROUND CONDITION AND AN OVERSIZE FASTENER INSTJun 26, 2000 · N538DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S001060Door Frame · crackedONE INCH VISIBLE CRACK R-1 DOOR AFT FRAME AT LOWER STOP PAD. REPAIRED PER M/M 52-12-0.May 3, 2000 · N538DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S000802Door · unsecureLEFT AFT SERVICE DOOR NOT CLOSED PROPERLY. RETURNED TO PHX. CLOSED DOOR, PRESSURIZED AIRCRAFT. ALL CKD NORMAL.Apr 25, 2000 · N538DA · Boeing 727232 · Service DoorsSDR DL72S000216Door Frame · crackedFOUND DURING WALKAROUND CARGO STRAP STICKING OUT OF FWD LWR CORNER OF C-3 DOOR. UPON CLOSER INSPECTION A 10 INCH CRACK WAS FOUND ON INNER DOOR FRAME WHERE IT ATTACHES TO DOOR SKIN. REPLACED DOOR.Jan 28, 2000 · N538DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S992692Line · leakingDURING CLIMBOUT OF STL, A SYS QTY DROPPED TO 1.2 GAL AFTER GEAR RETRACTION. ONCE AT CRUISE ATL, A SYS QTY SLOWLY DROPPED TO .2 GAL. A SYS LOSS PROCEDURES WERE FOLLOWED. LANDING GEAR WAS LOWERED NORMALLY AND FLAPS WERE LOWERED BY ALT METHOD. LOW PRESS LIGHDec 9, 1999 · N538DA · Boeing 727232 · Hydraulic System, MainSDR DL72S992665Frame · crackTHE WEB OF THE FS 560 C1 DOOR JAMB FRAME WAS FOUND WITH 2 SMALL CRACKS AT EXISTING FASTENER HOLES BELOW THE UPPER SILL. THE CRACKS WERE ROUTED OUT OF THE WEB AND A TITANIUM DOUBLER INSTALLED TO REPAIR THE DAMAGE AND ENABLE INSTALLATION UNDER THE EXISTING UPDec 4, 1999 · N538DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S992635Web · crackedA .125 INCH CRACK LT VERTICAL TORQUE BOX WEB AT UPPER END STA 1213L (MARKED). MANUFACTURED AND INSTALLED FILLER PER MM 53-11-0 PG 832.Nov 16, 1999 · N538DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S992621Panel · wornFOUND DURING MV2 CORROSION VISIT NRC 165, A .75 INCH HOLE IN NR 4 BALANCE BOARD CLOSURE PANEL. REPAIRED PER SRM 55-20-3.Nov 16, 1999 · N538DA · Boeing 727232 · Horizontal Stabilizer, Plate/SkinSDR DL72S992568Web · crackedA .375 INCH CRACK LT VERTICAL TORQUE BOX WEB AT UPPER END STA 1223 (MARKED). REPAIRED PER MM 53-11-0 PAGE 832.Nov 16, 1999 · N538DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S991565Wire · chafedEMERGENCY EXIT CONTROL RT CIRCUIT BREAKER POPPED AND WILL NOT RESET. REPLACED WIRE W338-176-18 FROM ABOVE PACK FLOW CONTROL VLV TO ASSY L622 AND REPLACED C/B C267, OPS CK NORMAL.Jul 12, 1999 · N538DA · Boeing 727232 · Light System WiringSDR DL72S991561Light · inoperativeEMERGENCY EXIT CONTROL C/B POPPED, WILL NOT RESET. FOUND AFT STAIR LIGHT INOP. REPLACED LIGHT ASSY AND BATTERY. ALSO, FOUND LOSE TERMINAL IN 48 SEC. REPAIRED SAME, OPS CK NORMAL.Jul 11, 1999 · N538DA · Boeing 727232 · Emergency LightingSDR DL72S990688Angle · corrodedFOUND ON D2 LETTER CK, CORROSION ON ATTACH ANGLE FOR A/C DOOR 3448R. REPAIRED PER MM 53-30-1.Mar 29, 1999 · N538DA · Boeing 727232 · Air Conditioning DoorsSDR DL72S990167O Ring · leakingENGINE NR 2 LOW OIL PRESS LIGHT ON, QYT GAUGE TO ZERO AND OIL PRESS EVENTUALLY TO ZERO. SHUT DOWN NR 2 ENG PER POM. REPAIRED OIL LEAK AT BANJO FITTING.Jan 26, 1999 · N538DA · Boeing 727232 · Turbine Engine Oil SystemSDR DL72S981779Skin · dentedTHE FUSELAGE SKIN AT FS 1067 WAS FOUND DENTED JUST O/B OF STRINGER 29R. THE DAMAGE WAS ADJACENT TO AND EXISTING DOUBLER REPAIR FOR ANOTHER SKIN CUTOUT. THE DENT WAS CUT OUT OF THE SKIN, THE EXISTING DOUBLER REMOVED, AND A NEW EXTERNAL ALUMINUM DOUBLER WAS INAug 26, 1998 · N538DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S981765Bracket · crackedNR 1 L/E FLAP ACTUATOR ATTACH BRACKET CRACKED O/B LOWER END. FOUND ON D1 LETTER CK. REPAIRED PER MM 57-20-21.Aug 25, 1998 · N538DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S981236Fuel Oil Cooler · malfunctionedPRECAUTIONARY NR 3 ENG SHUTDOWN AT TOP OF CLIMB. NR 3 OIL TEMPSETTLED IN YELLOW BAND, ALL OTHER ENG IND NORM, 60 DEG HOTTER THAN 1 AND 2 ENG. COULD NOT GET TEMP OUT OF YELLOW AFTER 15 MINS. REPLACED FUEL/OIL COOLER. IN FLIGHT SHUT DOWN.Jun 10, 1998 · N538DA · Boeing 727232 · Engine Fuel/Oil CoolerSDR DL72S980923Power Pack · inoperativeON L/O, FOUND F/C OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY POWER PACK AND POWER PACK RACK. CKS NML AS PER M/M.Apr 29, 1998 · N538DA · Boeing 727232 · Emergency LightingSDR DL72S980562Batteries · dischargedEMERGENCY LIGHTS ABOVE AIRSTAIRS INOP. REPLACED BATTERIES. CKS GOOD.Mar 11, 1998 · N538DA · Boeing 727232 · Emergency LightingSDR DL72S980175Skin · crackedFOUND ON C2 LETTER CK, TWO .75 INCH CRACKS OUT OF TWO ADJACENT RIVETS LT SIDE OF LOWER RUDDER. REPAIRED PER SRM 55-20-3 REF SRM 55-40-2 FIG 1 FOR INFO.Jan 21, 1998 · N538DA · Boeing 727232 · Rudder, Plate/SkinSDR DL72S971171Floorbeam · corrosionCORROSION FOUND AT NUTPLATE HOLE ON FLOORBEAM STA 344 AND LBL 45. REPAIRED PER SRM 53-10-8, FIG. 11.Jun 16, 1997 · N538DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S962637Bulb · missingEMERGENCY PATH LIGHTS MISSING LENSES IN AFT CABIN AND ONE LIGHT HAS WIRE DAMAGED. REPLACED MISSING LENSES AND REPLACED ONE BULB AND SOCKET ASSY, OPS CKS OK.Dec 2, 1996 · N538DA · Boeing 727232 · Emergency LightingSDR DL72S961859Battery Pack · dischargedBOTH AFT DOOR SLIDE LIGHTS INOP. REPLACED BATTERY PACK, CKS GOOD.Aug 8, 1996 · N538DA · Boeing 727232 · Emergency LightingSDR DL72S961471Hinge Ftg · crackedTHE REAR SPAR OF THE LT ELEVATOR WAS FOUND CRACKED ON THE I/B SIDE OF THE THIRD FROM O/B HINGE FITTING. MODIFIED PER B727 S/B 727-55-0087, REV 1.May 18, 1996 · N538DA · Boeing 727232 · Elevator StructureSDR DL72S960995Actuator Bracket · crackedNR 8 SLAT ACTUATOR MOUNT BRACKETS CRACKED OUTBOARD AND INBOARD SIDES. REPAIRED PER M/M 57-20-21.Apr 25, 1996 · N538DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S960977Rear Spar · crackedTHE REAR SPAR OF THE LT ELEVATOR IS CRACKED ON THE INBOARD SIDE OF THE THIRD FROM OUTBOARD HINGE FITTING. THE CRACK IS APPROXIMATELY .1250 INCH LONG. THE CRACK LENGTH IS WITHIN THE .250 INCH STOP DRILL LIMITS OF THE BAC S/B 727-55-0087. THE CRACK WILL BE STOApr 19, 1996 · N538DA · Boeing 727232 · Elevator, Spar/RibSDR DL72S960838Battery Pack · dischargedEMERGENCY LIGHT OVER L1 DOOR INOP. REPLACED BATTERY PACK MFR NR 3106 DAL 334101877, BATTERY WEAK.Apr 11, 1996 · N538DA · Boeing 727232 · Emergency LightingSDR DL72S953800Angle · crackedFOUND ON A2 LETTER CHECK, NUMBER 7 SLAT COVE SKIN ANGLE CRACKED .25 INCH IN UNDER ANTI-ICE DUCT. REPAIRED PER MM 57-54-0.Sep 22, 1995 · N538DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953799Angle · crackedFOUND ON A2 LETTER CHECK, NR 1 SLAT COVE SKIN ANGLE CRACKED AT THE OUTBOARD STOP PAD. REPAIRED PER MM 57-54-0.Sep 22, 1995 · N538DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951179Stiffener · crackedFOUND DURING A-1 LETTER CHECK - .50 INCH CRACK AT NR 6 SLAT STIFFENER AT COVE PANEL BELOW ANTI-ICE T-DUCT. REPAIRED PER M/M 57-54-0 PG 807A.Mar 20, 1995 · N538DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951177Skin · crackedFOUND DURING A-1 LETTER CHECK - 48 SEC TORQUE BOX SKIN CRACKED .3750 INCH AT A LIGHTNING HOLE RT SIDE STA 1323. INSTALLED DOUBLER PER M/M 53-11-0.Mar 20, 1995 · N538DA · Boeing 727232 · Fuselage Miscellaneous Structure
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