N401DA, cancelled Aug 15, 2013

Service difficulty reports · 76

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 = 'N401DA' AND deregistration_id = 'N401DA-2013-08-15'
  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 DL72S001142Valve · inoperativeLDFT TANK 2 DUMP VALVE WON''T OPEN. LIGHT STAYS ON WHEN TRYING TO OPEN.Jun 13, 2000 · N401DA · Boeing 727232 · Fuel Dump SystemSDR DL72S000993Battery Pack · will not testBATTERY PACK FOR EMERGENCY LIGHTS AT THE C-2 CARGO DOOR (M-957) WOULD NOT TEST. REMOVED AND REPLACED BATTERY PACK AND OPS CHECK GOOD.May 20, 2000 · N401DA · Boeing 727232 · Emergency LightingSDR DL72S000806Stiffener · crackedA 1 INCH CRACK IN SPAR STIFFENER I/B SIDE OF NR 6 SLAT I/B TRACK. REPLACED STIFFENER PER M/M 57-20-21. TPA D-1 LETTER CHECK.Apr 25, 2000 · N401DA · Boeing 727232 · Leading Edge DevicesSDR DL72S000805Angle · crackedA 1.5 INCH CRACK IN BS 870 LT MLG WW I/B ATTACH ANGLE. REPAIRED PER SRM 53-10-9D.Apr 25, 2000 · N401DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S000278Acm · leakingPASSENGER CABIN FILLED WITH LIGHT SMOKE AND RIGHT AFT LAV SMOKE ALARM WENT OFF. SHORTLY THEREAFTER RIGHT PACK TRIP OFF LIGHT ILLUM. SMOKE CLEARED AFTER RUNNING SMOKE ILLIMINATION CHECK. FOUND OIL LEAKING FROM RT ACM. REPLACED SAME.Feb 9, 2000 · N401DA · Boeing 727232 · Cabin Cooling SystemSDR DL72S992444Valve · failedAFTER NR 3 ENG START AND RT PACK SELECTED ON, LOUD BANG WAS HEARD IN COCKPIT/CABIN. RT DUCT PRESS NEEDLE WENT TO ZERO AND AFT FLT ATTENDANTS REPORTED FUEL SMELL. INSPECTED DUCTS AT NR 3 ENG/PYLON/AFT AIRSTAIR FOR DAMAGE/LEAKAGE, CK GOOD. CHECKED DUCTS AT RTNov 5, 1999 · N401DA · Boeing 727232 · Cabin Cooling SystemSDR DL72S992413Actuator · failedNUMBER THREE LEADING EDGE FLAP INDICATION AND UNCOMMANDED ROLL. REPLACED NUMBER THREE LEADING EDGE FLAP ACTUATOR.Oct 31, 1999 · N401DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S991663Light · damagedONE EMERGENCY LIGHT AT 20 DEF INOP. REPLACED SEAT ASSY AT ROW 20 DEF. OPS CHECK GOOD. MCO AND PLACARD REMOVED.Jul 23, 1999 · N401DA · Boeing 727232 · Emergency LightingSDR DL72S990407Stiffener · crackedTPA - LTR CHK C-1 02/26/99, WING LE SPAR STIFFENER CRACKED AT I/B SIDE NR 2 SLAT I/B TRACK BOX. REPLACED STIFFENER PER MM 57-20-21.Feb 26, 1999 · N401DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S990406Bracket · crackedNR 8 SLAT ACT I/B MOUNT BRACKET CRACKED AT WEB. REPAIRED PER M/M 57-20-21.Feb 26, 1999 · N401DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S990405Skin · crackedNR 7 SLAT LWR COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER M/M 57-54-0.Feb 26, 1999 · N401DA · Boeing 727232 · Leading Edge DevicesSDR DL72S990367Skin · crackedLFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 460 INDICATED A SINGLE CRACK. INTERNAL HFEC INSPECTION CONFIRMED ONE CRACK ONLY AT FS 444. THE CRACK WAS ROUTED OUT OF THE SKIN LAP AND REPAIRED PER THE B727 SRM 53-30-3, FIG 5. TEN FASTEFeb 23, 1999 · N401DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990366Skin · crackedLFEC INSPECTION REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL OF THE STRINGER 4R LAP SPLICE BETWEEN FS 360 AND 481. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS ALONG THE PANEL LENGTH. THE LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PANEL LENFeb 23, 1999 · N401DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990365Skin · crackedLFEC INSPECTION REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN AT THE STRINGER 4R LAP SPLICE BETWEEN FS 681 AND 740. INTERNAL HFEC INSPECTION VERIFIED 27 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP WAS CUT OUT ALONG THE ENTIRE PANEL LENGTH AND RFeb 23, 1999 · N401DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990364Skin · crackedLFEC INSPECTION REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN OF THE STRINGER 4R LAP SPLICE BETWEEN FS 481 AND 680. INTERNAL HFEC INSPECTION CONFIRMED 31 CRACKS ALONG THE PANEL LENGTH. THE LAP SPLICE WAS CUTOUT ALONG THE PANEL LENGTH AND REPAIRFeb 23, 1999 · N401DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990362Skin · crackedLFEC INSPECTION REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN OF THE STRINGER 26L LAP SPLICE BETWEEN FS 480 AND 681. INTERNAL HFEC INSPECTION CONFIRMED A TOTAL OF 6 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIREFeb 23, 1999 · N401DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990017Power Supply · inopFUSE BLOWN, EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY.Jan 4, 1999 · N401DA · Boeing 727232 · Emergency LightingSDR DL72S982162Battery · dischargedRT FWD ENTRY DOOR OVERHEAD EMEGENCY LIGHT WILL NOT TEST. REPLACED BATTERIES AND RACK NOW CKS NORMAL.Oct 18, 1998 · N401DA · Boeing 727232 · Emergency LightingSDR DL72S982033Track · corrosionINBD FLAP INBD TRACK TYP CORROSION AT MLG BEAM ATTACH HOLES AND FWD LUG: AD 90-07-05: TYPICAL CORROSION WAS FOUND TO THE MLG BEAM ATTACH HOLES (WITHIN THE AD AREA) AND AT THE FWD ATTACH LUG. OVERSIZED CORRODED HOLES AND MACHINED LUG FACES.Oct 2, 1998 · N401DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982114Track · corrodedBUSH FWD ATTACH LUG AND REPAIR MLG BEAM ATTACH HOLES PER SB 727-57-0178, EXCEPT INCREASE HOLE DIA TO .847.Sep 28, 1998 · N401DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982113Track · corrodedTYPICAL CORROSION FOUND IN MLG BEAM ATTACH HOLES. REPAIRED SIMILAR TO SB 727-57-0178 EXCEPT TO OS HOLES, .838 MAX DIAMETER TO REMOVE ALL CORROSION.Sep 28, 1998 · N401DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S981772Switch · failedAMBER LEADING EDGE FLAP LIGHT WOULD NOT EXTINGUISH WHEN FLAPS WERE MOVED FROM 5 TO 2 DEGREES. REPLACED RETRACT SWITCH ON NR 1 SLAT ACTUATOR.Aug 27, 1998 · N401DA · Boeing 727232 · Leading Edge Slat Position Indicating SystemSDR DL72S981546Skin · crackedFOUND AT B-2 LETTER CK, .5 INCH CRACK, FUSELAGE SKIN AT L-4 WINDOW SCREW LOWER INBD CORNER. REPAIRED PER SRM 53-30-3.Jul 24, 1998 · N401DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S981478Battery Pack · dischargedLT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT ASSY AND CHANGED BATTERY PACK PER M/M. OP CHECK GOOD BATTERY PACK REMOVED 7997. BATTERY PACK INSTALLED, C6495 P/N 334102486.Jul 15, 1998 · N401DA · Boeing 727232 · Emergency LightingSDR DL72S981373Rack · inoperativeRT SIDE EMER LIGHT OVERWING EXIT LIGHTS INOP. REPLACED LIGHT RACK.Jun 30, 1998 · N401DA · Boeing 727232 · Emergency LightingSDR DL72S981202Rack · inoperativeOVERWING EXIT EMERG LIGHTS FAILED TO ILLUMINATE. REPLACED RACK.Jun 6, 1998 · N401DA · Boeing 727232 · Emergency LightingSDR DL72S980974Battery Pack · dischargedAFT GALLEY OVERHEAD EXIT SIGN INOP. REPLACED POWER PACK.May 7, 1998 · N401DA · Boeing 727232 · Emergency LightingSDR DL72S980132Battery Pack · dischargedAFT EXIT AISLE OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, SYSTEM OPERATIONAL CHECK NORMAL.Jan 17, 1998 · N401DA · Boeing 727232 · Emergency LightingSDR DL72S972661Skin · crackedSKIN, CRACKED THE FWD SECTION OF S DUCT FWD SKIN LIP AT THE 12:00 O'CLOCK POSITION. REMOVED DAMAGED SECTION OF SKIN PER SRM. FABRICATED REPAIR PARTS PER SRM 54-10-3 FIG 13. TREATED AND PAINTED PER SRM 54-10-3. OK TO INSTALL REPAIR PER SRM 54-10-3. INSTALLDec 15, 1997 · N401DA · Boeing 727232 · Nacelle/Pylon, Plate/SkinSDR DL72S972742Rib · crackedTHE I/B AFT CLOSEOUT RIB WAS FOUND CRACKED DURING SHOP VISIT. THE RIB WAS REPAIRED BY INSTALLING A DOUBLER PER 727 M/M 57-52-0.Dec 10, 1997 · N401DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S972627Beam · crackedRT WING SPOILER SUPPORT BEAM CRACKED IN O/B BOLT HOLE FOR NR 5 FLAP TRACK. REMOVED DAMAGED SECTION OF SPOILER BEAM PER M/M 57-55-0 FIG 805. REMOVED SUPPORT BETWEEN SPOILERS 7 AND 8. FABRICATED EXTRUDED CHORD IAW M/M 57-55-0 PG 810. DRILLED CHORD, DOUBLER TDec 4, 1997 · N401DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S972582Fitting · corrosionRT FT WING ATTACH FITTING HAS CORROSION AT SEVERAL LOCATIONS INSIDE BORE. REMOVED CORROSION IAW SRM 53-40-1 PG 18. TREATED AND PAINTED PER PS 900-3-6.Nov 25, 1997 · N401DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S972581Stringer · crackedSTRINGER CRACKED WS 686.5 STRINGER NR 10 IS CRACKED AT FASTENER HOLE. REPAIRED PER MM 57-13-0.Nov 25, 1997 · N401DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S972757Skin · puncturedTHE COVE SKIN WAS FOUND WITH A HOLE 26 FROM IB END DURING SHOP VISIT. THE DAMAGE WAS REMOVED AND A DOUBLER INSTALLED PER 727 MM 57-52-00.Nov 24, 1997 · N401DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S972756Angle · crackedTHE AFT LOWER CHORD ANGLE WAS FOUND CRACKED DURING SHOP VISIT. THE CHORD WAS REPAIRED PER 727 MM 57-52-00 BY REMOVING DAMAGE AND REPLACING AND INSTALLING A DOUBLER.Nov 24, 1997 · N401DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S972755Angle · crackedTHE LOWER AFT CHORD ANGLE WAS FOUND CRACKED 18 FROM IB END DURING A SHOP VISIT. THE CHORD WAS REPAIRED PER 727 MM 57-52-00 BY REMOVING DAMAGE AND INSTALLING A DOUBLER.Nov 24, 1997 · N401DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S972626Rib · crackedNR 6 SLAT RIB CRACKED LOWER SURFACE. REMOVED RIVETS FORM RIB, BEGAN FABRICATION OF REPAIR DOUBLERS PER M/M 57-40-0 FIG 814. DRILLED AFT DOUBLER, STOP DRILLED PER SRM 57-54-0. ROUTED OUT DAMAGE PER SRM. INSTALLED REPAIR PER SRM.Nov 24, 1997 · N401DA · Boeing 727232 · Leading Edge DevicesSDR DL72S972625Rib · crackedNR 7 SLAT RIB CRACKED JUST OUTBD OF ACTUATOR ROD END AREA. FABRICATED REPAIR PER MM 57-54-0 FIG 814. INSTALLED REPAIR PER MM 57-54-0 FIG 814.Nov 24, 1997 · N401DA · Boeing 727232 · Leading Edge DevicesSDR DL72S972624Rib · crackedNR 6 SLAT RIB CRACKED ON INBD END. MADE DOUBLER IAW MM. DRILLED UP AND TREATED AND PAINTED. INSTALLED DOUBLER PER M/M 57-54-0 FIG 814. INSTALLED SEAL.Nov 24, 1997 · N401DA · Boeing 727232 · Leading Edge DevicesSDR DL72S972623Stop · wornNR 4 SLAT INBD STOP WORN, 2ND WEB FROM INBD END CRACKED OUT UNDER N/P. FABRICATED REPAIR PER MM 57-54-0 FIG 814. OK TO TREAT AND PAINT. TREATED AND PAINTED PER PS 900-2 NR 5. INSTALLED REPAIR PER MM 57-54-0 FIG 814. WEAR WITHIN LIMITS PER MM 27-87-0 FIG 5Nov 24, 1997 · N401DA · Boeing 727232 · Leading Edge DevicesSDR DL72S972580Stringer · crackedLT WING STR TO RIB HFEC INSPECTION SHOWS STRINGER TO RIB ATTCH FLANGE MARKED 'C' AT WS 629.0 HAS CRACK INDICATIONS -MARKED- THAT EXTENDS FROM HOLE TO EDGE OF FLANGE. CUTOUT ACCESS HOLE ON VENT BOX PER MM 57-13-10. DRILLED REPAIR PARTS PER MM 57-13-10 FIG 804Nov 24, 1997 · N401DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S972579Fitting · corrosionCORROSION ON RT FRONT SPAR WING TO BODY FWD FITTING. REMOVED CORROSION AT PER SRM 51-10-6. TREATED AND PAINTED PER PS 900-3-6.Nov 24, 1997 · N401DA · Boeing 727232 · Wing, Fuselage Attach FittingsSDR DL72S972578Fitting · corrosionCORROSION ON LEFT AFT SPAR WING TO BODY FITTING (AFT END). REMOVED CORROSION IAW SRM 53-40-1 PG 18. TREATED AND PAINTED PER PS 900-3-6.Nov 24, 1997 · N401DA · Boeing 727232 · Wing, Fuselage Attach FittingsSDR DL72S972622Skin · crackedSKIN CRACKED AT INSPECTION PANEL 9524. ROUTED OUT CRACK AND MANUFACTURED DOUBLER PER M/M 54-30-0. INSTALLED DOUBLER PER SRM 54-30-0, FIG 803.Nov 21, 1997 · N401DA · Boeing 727232 · Nacelle/Pylon, Plate/SkinSDR DL72S972577Rib · crackedCRACK - STRINGER TO RIB WS 629, S-9 AFT HOLE, RT WING. REPAIRED PER MM 57-13-00.Nov 21, 1997 · N401DA · Boeing 727232 · Wing, Rib/BulkheadSDR DL72S972576Rib · crackedCRACK - STRINGER TO RIB WS 629, S-13 AFT HOLE, RT WING. REPAIRED PER MM 57-13-00.Nov 21, 1997 · N401DA · Boeing 727232 · Wing, Rib/BulkheadSDR DL72S972575Rib · crackedRT WING WS 629 S-AA CRACKED AT STR TO RIB CONNECTION REF OP8602 RC 882. REPAIRED PER MM 57-13-00.Nov 21, 1997 · N401DA · Boeing 727232 · Wing, Rib/BulkheadSDR DL72S972574Light Box · corrodedLIGHT BOX CORRODED AROUND EDGES STA 720B AND 720C BETWEEN STRINGERS 16R TO 14R. REMOVED LIGHT BOX. REMOVED CORROSION PER SRM 51-10-6 NOT WITHIN ALLOWABLE LIMITS PER SRM 53-30-1 FIG 7. COMPLETED DRILLING DOUBLER PER SRM 53-30-3 FIG 22. INSTALLED DOUBLER PERNov 21, 1997 · N401DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S972573Stringer · corrodedLIGHT BOX CORRODED STRINGER 152, BETWEEN STA 720B AND 720C. REMOVED LIGHT BOX FOR ACCESS, REMOVED CORROSION PER 51-10-6 NOT WITHIN ALLOWABLE LIMITS PER SRM 53-30-1 FIG 7. COMPLETED FABRICATING REPAIR DOUBLER PER SRM 53-30-3 FIG 22 T AND P PER PS 900-2 NR 5. Nov 21, 1997 · N401DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S972572Stringer · crackedHFEC INSP SHOWED CRACK INDICATION AT WS 656.5 FWD VENT HOLE. CUT ACCESS HOLE IN VENT BOX PER M/M 57-13-00. REPAIRED CRACK PER MM 57-13-0 FIG 80.Nov 21, 1997 · N401DA · Boeing 727232 · Wing, Longeron/Stringer
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