N501DA, cancelled Apr 2, 2002

Service difficulty reports · 71

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 = 'N501DA' AND deregistration_id = 'N501DA-2002-04-02'
  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 DL72L010916Beam · crackedINSPECTION OF THE RT VENTRAL STAIRWAY TORQUE BOX PER BAC S/B 727-53-0129 AND AD 94-07-08 REVEALED A TYPICAL CRACK IN THE UPPER AFT HORIZONTAL BEAM AT FS 1273. THE CRACKED PART WAS REMOVED AND A NEW PART INSTALLED. THE REPAIR WAS ACCOMPLISHED PER THE S/B AND Jun 5, 2001 · N501DA · Boeing 727232 · Fuselage Main, StructureSDR DL72L010912Rib · crackedFOUND ON C1 LETTER CK NR 1 SLAT NOSE RIB IS CRACKED I/B SIDE OF ACTUATOR ROD END. REPAIRED PER MM 57-54-000-8.Jun 4, 2001 · N501DA · Boeing 727232 · Leading Edge DevicesSDR DL72L010911Angle · crackedFOUND ON C1 LETTER CK NR 2 SLAT LOWER COVE SKIN ANGLE IS CRACKED AT THE TAI DUCT. REPAIRED PER MM 57-54-000-8.Jun 4, 2001 · N501DA · Boeing 727232 · Leading Edge DevicesSDR DL72L010910Angle · crackedO/B ATTACH ANGLE CRACKED NR 12 SPOILER ACT SUPPORT CASTING. REPLACED ANGLE PER M/M 57-42-000-8.Jun 4, 2001 · N501DA · Boeing 727232 · SpoilersSDR DL72L010730Actuator · failedAFTER T/O AND GEAR HANDLE WAS SELECTED TO OFF AFTER 30 SEC. CREW GOT DOOR LIGHT ON FWD PANEL AND RED RT GEAR LT ON FOLLOWED BY TAIL SKID LIGHT AND RED NOSE GEAR LT. CREW CHECK OF GEAR VISUALLY LT MAIN AND NOSE UP AND LOCKED BUT RT MAIN WAS DOWN AND LOCKED. May 7, 2001 · N501DA · Boeing 727232 · Landing Gear ActuatorSDR DL72L010221Battery Pack · dischargedLT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK, ALL OPS OK.Feb 7, 2001 · N501DA · Boeing 727232 · Emergency LightingSDR DL72L010009Battery · inoperativeON LAYOVER FOUND OVERHEAD EMERGENCY EXIT IDENTIFIER LIGHT INOP. CABIN AT FWD GALLEY IN AISLE. L1021 FWD LOWERED CEILING SIGN. FOUND ALL 6 VOLT 328 LAMPS BAD. RELAMPED, NO HELP. FOUND M1085 BATTERY CHARGER MODULE BAD. REPLACED M1085 MODULE AND BATTERY PACKJan 2, 2001 · N501DA · Boeing 727232 · Emergency LightingSDR DL72L001795Battery · dischargedAFT CABIN FLASHLIGHT IS NOT BLINKING. REPLACED BATTERY, CK OK.Sep 17, 2000 · N501DA · Boeing 727232 · Emergency EquipmentSDR DL72L000634Beam · crackedTHE RT VENTRAL STAIR TORQUE BOX WAS FOUND WITH TWO TYPICAL CRACKS IN THE UPPER HORIZONTAL BEAM MEMBERS AT FS 1263 AND FS 1273. THE CRACKS ARE TYPICAL OF S/B 727-53-0129. THE CRACKED MEMBERS WERE REMOVED AND REPLACED WITH NEW PARTS PER ER/A 369707-14AD.Apr 4, 2000 · N501DA · Boeing 737232 · Fuselage Miscellaneous StructureSDR DL72L000285Noise · detectedDURING CLIMBOUT A INTERMITTENT THUMPING NOISE WAS HEARD WHICH APPEARED TO BE COMING FROM UNDER THE 1ST CLASS CABIN. THUMPING CONTINUED AT CRUISE FL330 FOR ABOUT 15 MIN AND THEN QUIT. INSPECTED E&E, FWD CARGO PIT, FWD DOORS INCLUDING E&E, L1, L2, F/CARGO DOORFeb 10, 2000 · N501DA · Boeing 727232 · Fuselage Main, StructureSDR DL72L992744Track · corrodedINBOARD FLAP / NR 5 INBOARD TRACK - TYP CORROSION AT MLG AND SPOILER BEAM ATTACH PADS, AND WEAR AT FWD ATTACH LUGS AND MLG DOOR HINGE FITTING HOLES. AUTHORIZED BLEND REPAIRS AND OVERSIZED FASTENERS.Dec 12, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L992748Track · corrodedINBOARD FLAP / INBOARD TRACK - TYP CORROSION AT MLG AND SPOILER BEAM ATTACH PADS, WEAR AT FWD LUGS, WEAR AT MLG DOOR HINGE FITTING HOLES, WEAR AT SPACER BAR HOLES, WEAR AT TOGGLE DETENT HOLE. AUTHORIZED BLEND AND BUSHING REPAIRS.Nov 16, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L992747Track · corrodedINBOARD FLAP / INBOARD TRACK - TYP CORROSION AT MLG AND SPOILER BEAM ATTACH PADS AND WEAR AT FWD LUGS. AUTHORIZED BLEND AND BUSHING REPAIR.Nov 16, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L992735Flap Track · wornINB'D FLAP / INB'D TRACK - TYP CORROSION AT MLG AND SPOILER BEAM ATTACH PADS, WEAR AT FWD LUGS, WEAR AT MLG DOOR HINGE FITTING HOLES, WEAR AT SPACER BAR HOLES AND WEAR AT TOGGLE DETENT HOLE. AUTHORIZED BUSHING AND BLEND REPAIRS.Nov 16, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L992746Track · corrodedINBOARD FLAP / INBOARD TRACK - TYP CORROSION AT MLG BEAM ATTACH PAD. AUTHORIZED BLEND AND BUSHING REPAIR.Nov 2, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L992745Track · corrodedINBOARD FLAP / INBOARD TRACK - TYP CORROSION AT MLG AND SPOILER BEAM ATTACH PADS. AUTHORIZED BUSHING REPAIR.Nov 2, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L992031Flap Track · corrodedNR 4 FLAP TRACK, REF AD 90-07-05, 90-06-09, 91-09-03, 94-05-04, TYPICAL CORROSION FOUND TO MLG BEAM AND SPOILER BEAM ATTACH PAD AND ATTACH HOLES. WEAR FOUND AT TRACK FWD ATTACH LUG FACES AND FWD MLG HINGE FITTING ATTACH HOLES. AUTHORIZED MACHINING TO OVERSIZSep 13, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L992030Flap Track · corrodedNR 5 FLAP TRACK, REF AD 90-07-05 AND AD 90-06-09, TYP CORROSION FOUND TO MLG BEAM AND SPOILER BEAM ATTACH PAD SURFACE AND ATTACH BOLT HOLES. TYPICAL WEAR FOUND AT FWD TRACK ATTACH LUG FACES. ALL CORROSION AND WEAR WAS MACHINED. AUTHORIZED REWORKED DIMENSIONSep 13, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L991998Stringer · wornSTRINGER 7L OF THE VERTICAL STABILIZER WAS FOUND TO BE WORN AT FIN STATION 228. THE DAMAGE WAS REPAIRED PER ER/A 333496.Sep 5, 1999 · N501DA · Boeing 727232 · Vertical StabilizerSDR DL72L991997Frame · corrodedTHE CARGO DOOR OPENING FRAME AT FS 1142 WAS FOUND TO HAVE CORROSION ON THE FORWARD SIDE OF THE WEB. THE DAMAGE WAS REPAIRED PER ER/A 333525-14.Sep 5, 1999 · N501DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L991996Skin · gougedTHE FUSELAGE SKIN WAS GOUGED AT FS 306 AND WL 249 ON THE LHS OF THE AIRCRAFT. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ER/A 333507-14.Sep 5, 1999 · N501DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L991995Skin · misdrilledTHE FUSELAGE SKIN WAS MISDRILLED AT FS 1096 AND STRINGER 1 DURING THE ACCOMPLISHMENT OF EO 4-60553-3AD. THIS DAMAGE WAS ADDRESSED BY ER/A 333491-14AD AT HMV.Sep 5, 1999 · N501DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L991993Stringer · gougedTOOLING DAMAGE WAS FOUND ON THE LOWER SURFACE OF STRINGER 17R AT FS 1176. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ER/A 333504-14K.Sep 5, 1999 · N501DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72L991992Stringer · crackedA CRACK WAS FOUND IN THE STRINGER TO RIB ATTACH FLANGE OF WING STRINGER 17R AT WING STATION 304. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333519-14.Sep 5, 1999 · N501DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72L991991Stringer · corrodedSTRINGER 27R WAS FOUND CORRODED AT FS 1137. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ER/A 333521-14.Sep 5, 1999 · N501DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72L991933Skin · crackedLFEC INSPECTION (PER SI 4-74176-12AD) ON THE S4R LAP JOINT REVEALED CRACK INDICATIONS BETWEEN BS 480 AND 680. INTERNAL HFEC INSPECTIONS CONFIRMED THIRTEEN (13) CRACK INDICATIONS IN THE LOWER ROW OF THE LOWER SKIN. REPAIRED PER ERA 333468-14AD, REV B.Aug 31, 1999 · N501DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L991932Skin · crackedA CRACK WAS FOUND IN THE FUSE SKIN AT APPROX BS 947 ON THE LT AT S18A AND CUTOUT. REPAIRED PER ERA 333475-14, REV C.Aug 31, 1999 · N501DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L991931Skin · crackedTHE VERT STAB LT SKIN WAS FOUND CRACKED WITH A TIME LIMITED REPAIR LOCATED AT BS 1203 WL 295. THE RESULTANT TRIM OUT IS APPROX 1.25 IN DIAMETER. REPAIRED PER ERA 333479-14, REV C.Aug 31, 1999 · N501DA · Boeing 727232 · Vertical Stabilizer, Plate/SkinSDR DL72L992316Skin · crackedDURING SHOP VISIT, THE AFT LOWER COVE SKIN WAS FOUND CRACKED 52 FROM I/B END OF THE FLAP. THE SKIN WAS REPAIRED BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER PER MM 57-52-0, FIG 809.Aug 27, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L991881Shear Tie · crackedDURING HMV, A DAMAGED SHEAR TIE ON THE FUSELAGE FRAME AT FS 1263 WAS FOUND BETWEEN STRINGERS 12L AND 14L. THIS DAMAGE WAS REPAIRED PER ERA 333487-14.Aug 23, 1999 · N501DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L991912Track · corrodedNR 4 I/B FLAP TRACK, TYPICAL CORROSION FOUND AT MLG AND SPOILER BEAM ATTACH PADS AND WEAR AT FWD ATTACH LUG. AUTHORIZED MACHINE BLENDING OF PADS AND LUG FACES.Aug 20, 1999 · N501DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72L992315Angle · crackedDURING SHOP INSP, THE LOWER AFT SPAR CAP/ANGLE WAS FOUND CRACKED 53 FROM THE I/B END. THE ANGLE WAS REPAIRED BY REPLACING A SECTION OF THE ANGLE AND INSTALLING A DOUBLER PER MM 57-52-0, FIG 802.Aug 13, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L992314Angle · crackedDURING SHOP INSP, THE LOWER AFT SPAR ANGLE/CAP WAS FOUND CRACKED 33 AND 37 FROM THE I/B END. THE ANGLE WAS REPAIRED PER MM 57-52-0, FIG 802 BY REPLACING A SECTION OF THE ANGLE AND INSTALLING A DOUBLER.Aug 13, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L992313Angle · crackedDURING SHOP INSP, THE LOWER AFT SPAR ANGLE WAS FOUND CRACKED 19 FROM I/B END. A SECTION OF THE CAP WAS REPLACED AND A DOUBLER INSTALLED PER MM 57-52-0, FIG 802.Aug 13, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L992723Fasteners · missingANGLE REPAIR AFT SPAR, LWR.ANGLE 32 TO 37 INCHES FROM I/B HAD MISSING FASTENERS. REMOVED I/B SECTION OF SPAR RAIL, FABRICATED REPLACEMENT SECTIONS AND INSTALLED PER M/M 57-52-0 FIG 802, ON SHOP ORDER 847111.Aug 12, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L992676Spar · crackedREPAIR ANGLE CRACKED I/B SPAR CAP 18 INCHES I/B TO 23 INCHES O/B. REPAIRED PER M/M 57-52-0 FIG 802, ON SHOP ORDER 847111.Aug 12, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L992675Skin · crackedCOVE SKIN CRACKED 36 INCHES FROM I/B END. REPAIRED PER M/M 57-52-0, FIG 809, ON SHOP ORDER 847111.Aug 12, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L991800Skin · crackedSEVERAL CRACKS WERE FOUND WHILE ACCOMPLISHING SI 4-74176-12 BETWEEN FS 480 AND FS 680 AT STR 4R. THIS DAMAGE WAS REPAIRED BY ER/A333468-14AD.Aug 12, 1999 · N501DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L991865Bracket · crackedNR 2 K-FLAP ACTUATOR MOUNT BRACKET IS CRACKED IN RADIUS. STOP DRILLED CRACK IN OUTBOARD BRACKET AND FABRICATED DOUBLER PER M/M 57-20-21 FIG 802. OK TO INSTALL. INSTALLED DOUBLER PER M/M 57-20-21 FIG 807.Aug 11, 1999 · N501DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72L992216Skin · wornDURING SHOP VISIT, THE LEADING EDGE OF THE UPPER SKIN WAS FOUND WORN AT THE IB END APPROX 3 LONG. THE SKIN WAS REPAIRED PER MM 57-52-0, FIG 803 BY REMOVING THE DAMAGE AND INSTALLING A SKIN FILLER AND DOUBLER.Aug 9, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L992215Skin · wornDURING SHOP VISIT, THE OB LE UPPER SKIN WAS FOUND WITH WORN AREA APPROX 3 INCH LONG AT OB END. THE SKIN WAS REPAIRED PER MM 57-52-0, FIG 803 BY REMOVING THE DAMAGED SKIN AND INSTALLING A SKIN FILLER AND DOUBLER.Aug 9, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L991929Rib · crackedAT HMV2, FOUND NR 6 L/E SLAT 10TH RIB FROM I/B END IS CRACKED IN TWO PLACES. REMOVED RIB, FABBED NEW PER SRM 51-00 AND INSTALLED.Aug 9, 1999 · N501DA · Boeing 727232 · Leading Edge DevicesSDR DL72L991852Rib · crackedAT HMV 2 FOUND VERT STAB INTERIOR-RIB CHORD HAS CRACK AT PREVIOUS STRINGER REPAIR-RT SIDE OF VERT AT STA 110.4 STR 10. STOP DRILLED CRACK PER MM 55-30-00 FIG 802. MADE REPAIR ANGLE PER SAME, INSTALLED.Aug 9, 1999 · N501DA · Boeing 727232 · Vertical Stabilizer, Spar/RibSDR DL72L991545Chord · crackedLOWER FWD CORNER OUTER T-CHORD CRACKED AT FASTENER HOLE. REPAIRED PER ERA 372131.Jul 9, 1999 · N501DA · Boeing 727232 · Cargo/Baggage DoorsSDR DL72L991255Connector · failedAT 31,000 FT CABIN ALT STILL CLIMBED AT 500 FT MIN. DESCENDED TO 18,000 FT, CABIN ALT LEVELED OFF ATL 9500 FT. BOTH PACKS APPEARED TO WORK. NO OTHER INDICATIONS TO SHOW LEAK. REPLACED LT PACK VALVE CONNECTOR. LT PACK OPS NORMAL, A/C PRESS NORMAL.Jun 4, 1999 · N501DA · Boeing 727232 · Cabin Cooling SystemSDR DL72L990871Light · inoperativeC2 DOOR EMERGENCY SLIDE LIGHT INOP.Apr 22, 1999 · N501DA · Boeing 727232 · Emergency LightingSDR DL72L990775Stiffener · cracked1.25 CRACK ON NR 7 SLAT I/B TRACK O/B SPAR STIFFENER. REPAIRED PER MM 57-20-21.Apr 9, 1999 · N501DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72L990412Beam · crackedWEB AND OUTER CHORD FOUND CRACKED JUST AFT OF THE FWD PRESSURE STOP FITTING. OUTER CHORD IS TO BE REPLACED. WEB SPLICE REPAIR IS TO BE ACCOMPLISHED PER ER/A.Feb 27, 1999 · N501DA · Boeing 727232 · Cargo/Baggage DoorsSDR DL72L981864Module · inoperativeLDG GEAR WOULD NOT RETRACT AFTER TAKEOFF. HANDLE WOULD NOT GO PAST OFF POSITION. RESET LEVER LATCH CB AND CENTERED STEERING. SAME RESULT. FOUND LANDING GEAR ELECTRICAL MODULE LEVER LATCH FUNCTION INOP. REPLACED MODULE. RAN TEST/ADJ PER MM 32-09-121 PG 50Sep 8, 1998 · N501DA · Boeing 727232 · Landing Gear SelectorSDR DL72L981837Bulkhead Fitting · crackedFOUND ON F-2 LETTER CK, RT I/B TENSION TIE FITTING CRACKED AFT OF STA 1183 BULKHEAD. REPLACED FITTING PER BOEING DWG 65-17509 REV M.Sep 4, 1998 · N501DA · Boeing 727232 · Fuselage Main, Bulkhead
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