N962AS, cancelled Sep 24, 2010

Service difficulty reports · 187

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 = 'N962AS' AND deregistration_id = 'N962AS-2010-09-24'
  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 ASAA0781782Cusp Web · corrodedRIGHT CUSP WEB CORRODED. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 53-05.Jun 7, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0781781Cusp Web · corrodedRIGHT CUSP WEB CORRODED. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 53-01 AND 53-05.Jun 7, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0781780Cusp Web · corrodedRIGHT CUSP WEB CORRODED. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 53-01, 51-70-4 AND 51-70-4.Jun 7, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0781779Cusp Web · corrodedRIGHT CUSP WEB CORRODED. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER PER SRM 53-05 AND 53-01.Jun 7, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0781778Insert · corrodedCABIN FLOOR PANEL HAS NUMEROUS CORRODED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND DWG 4932106.Jun 3, 2007 · N962AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0781777Skin · dentedRIGHT INBOARD FLAP INBOARD VANE HAS SEVERAL DENTS ON LOWER SURFACE. PREPARED DAMAGED SURFACE FOR BONDING. INSTALLED REPAIR DOUBLER PER SRM 51-70-2.Jun 3, 2007 · N962AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0781776Skin · chafedLEFT OUTBOARD FLAP VANE LEADING EDGE IS CHAFED AT INBOARD SIDE. REMOVED DAMAGED EXISTING DOUBLER. INSTALLED REPLACEMENT DOUBLER PER SRM 51-70-2.Jun 3, 2007 · N962AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0781775Skin · dentedLEFT INBOARD FLAP OUTBOARD VANE LOWER INBOARD SURFACE HAS MULTIPLE DENTS. PREPARED DAMAGED AREA FOR BONDING. INSTALLED REPAIR DOUBLER PER SRM 51-70-2.Jun 3, 2007 · N962AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0781774Doubler · debondedEXISTING REPAIR DISBONDED ON LOWER SURFACE OF LEFT ELEVATOR GEARED TAB. PREPARED DAMAGED AREA FOR BONDING. INSTALLED FILLER AND DOUBLER PER SRM 51-70-2.Jun 3, 2007 · N962AS · Doug DC983 · Elevator, Tab StructureSDR ASAA0781733Web · damagedDOUBLE DRILLED HOLES ON WEB UNDER FWD CABIN FLOORBOARD SUPPORT ANGLE. CUT OUT DAMAGED AREA OF WEB, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM 51-70-4 FIG 2.May 30, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0781732Skin · dentedFUSELAGE SKIN DENTED A PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR. CUT OUT DAMAGED AREA OF SKIN. FABRICATED AND INSTALLED A SKIN FILLER INTERNAL REPAIR DOUBLERS, REPAIR STRAPS AND FINGER DOUBLERS IAW SRM 53-04 FIG 12C.May 30, 2007 · N962AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0781731Channel · damagedCABIN FLOOR PANEL HAS A DAMAGED HAT CHANNEL. LOCATED AND DRILLED A REPLACEMENT HAT CHANNEL IAW SRM 51-10-4, 51-30-2 AND DAC DWG 9957918.May 30, 2007 · N962AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0781730Floor Panel · damagedCABIN FLOOR PANEL HAS EDGE DAMAGE. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-03 PG 122B AND DCA DWG S4932106.May 30, 2007 · N962AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0781729Floor Panel · damagedCABIN FLOOR PANEL IS DELAMINATED. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.May 30, 2007 · N962AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0781728Floor Panel · damagedCABIN FLOOR PANEL HAS TEN DAMAGED INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.May 30, 2007 · N962AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0781727Floor Panel · deterioratedCABIN FLOOR PANEL HAS NUMEROUS DAMAGED INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.May 30, 2007 · N962AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0781726Floor Panel · delaminatedCABIN FLOOR PANEL IS DELAMINATED. FABRICATED A REPLACEMENT PANEL IAW SRM 53-05 PARA 44 AND DCA DWG S4932106.May 30, 2007 · N962AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0781725Floor Panel · deterioratedCABIN FLOOR PANEL IS BROKEN AT AN INSERT. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.May 30, 2007 · N962AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0781724Floor Panel · delaminatedCABIN FLOOR PANEL DELAMINATED. FABRICATED REPLACEMENT FLOOR PANEL IAW SRM 53-05 PG 122B FIGURES 50 AND 50A AND DCA DWG 9936640.May 30, 2007 · N962AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0781723Cusp Web · corrodedPASSENGER CABIN CUSP WEB IS CORRODED. REMOVED CORRODED WEB LOCATED DRILLED AND INSTALLED A REPLACEMENT WEB IAW SRM 51-30-2.May 30, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0781722Cusp Web · corrodedPASSENGER CABIN FLOOR CUSP WEB IS CORRODED. REMOVED THE CORRODED CUSP WEB LOCATED DRILLED AND INSTALLED A REPLACEMENT CUSP WEB IAW SRM 51-10-4 PG 1 AND 4 FIG 3 AND DAC DWG 9930538.May 30, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0781721Web · crackedPASSENGER CABIN FLOOR WEB IS CRACKED. CUT OUT DAMAGED AREA OF WEB, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM 51-70-4 FIG 2.May 30, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0781720Cusp Web · crackedPASSENGER CABIN FLOOR RT CUSP WEB IS CRACKED. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.May 30, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0781719Floor Support · corrodedPASSENGER CABIN FLOOR SUPPORT IS CORRODED. FABRICATED AND INSTALLED A REPLACEMENT FLOOR SUPPORT IAW SRM 51-10-4 PG 1 AND 51-30-1 PARA 1 AND PARA 11.May 30, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0781718Floor Support · corrodedPASSENGER CABIN FLOOR SUPPORT IS CORRODED. FABRICATED AND INSTALLED A REPLACEMENT FLOOR SUPPORT IAW SRM 51-10-4 PG 1 AND 51-30-1 PG 4.May 30, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0781746Frame · corrodedAFT CARGO FRAME AT STA 1307.091 CORRODED. LOCATED AND DRILLED A REPLACEMENT FRAME SECTION AND REPAIR PARTS AND INSTALLED IAW SRM 53-03 FIG 2A AND SRM 51-30-2.May 29, 2007 · N962AS · Doug DC983 · Fuselage Main, FrameSDR ASAA0781745Skin · dentedEXTERNAL FUSELAGE DENTED AT STA 579 BETWEEN LONG 20L AND 21L. MEASURED DENT AT 4.0 X .015 INCH WITHIN LIMITS PER SRM. REPAIRED IAW SRM 53-04 FIG 38 SHEETS 12 AND 21. COLD FORMED SKIN BACK TO ORIGINAL BLUEPRINT CONTOUR AND ACCOMPLISHED HFEC INSPECTION FABRICMay 29, 2007 · N962AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0781744Skin · dentedAFT CARGO DOOR EXTERIOR SKIN IS DENTED 22 INCHES FROM THE AFT EDGE 14 INCHES FROM THE TOP EDGE. CUT OUT DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER AND 2 EACH FINGER DOUBLERS IAW SRM 53-04.May 29, 2007 · N962AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0781743Insert · corrodedCABIN FLOOR PANEL HAS NUMERIOUS INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.May 29, 2007 · N962AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0781742Insert · corrodedCABIN FLOOR PANEL HAS NUMEROUS CORRODED INSERTS. FABRICATED A REPLACEMENT PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.May 29, 2007 · N962AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0781741Floor Panel · delaminatedCABIN FLOOR PANEL IS DELAMINATED. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.May 29, 2007 · N962AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0781740Floor Panel · delaminatedCABIN FLOOR PANEL IS DELAMINATED. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.May 29, 2007 · N962AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0781739Insert · corrodedCABIN FLOOR PANEL HAS NUMEROUS CORRODED INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.May 29, 2007 · N962AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0781738Insert · corrodedCABIN FLOOR PANEL HAS NUMEROUS CORRODED INSERTS. FABRICATED A REPLACEMENT PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.May 29, 2007 · N962AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0781737Floor Panel · deterioratedCABIN FLOOR PANEL HAS FIBER DAMAGE TO THE UPPER SURFACE. FABRICATED A REPLACEMENT PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.May 29, 2007 · N962AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0781736Floor Panel · damagedCABIN FLOOR PANEL HAS DAMAGED INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.May 29, 2007 · N962AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0781735Floor Panel · delaminatedCABIN FLOOR PANEL IS DELAMINATED. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.May 29, 2007 · N962AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0781734Floor Panel · corrodedCABIN FLOOR PANEL HAS CORRODED INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53 05 PARA 11 AND DAC DWG S4932106.May 29, 2007 · N962AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0781715Skin · dentedFUSELAGE SKIN IS DENTED. INSTALLED REPAIR DOUBLER AT RIGHT EXT FUSELAGE. COLD FORMED SKIN BACK TO ORIGINAL BLUEPRINT CONTOUR AND HFEC PRIOR TO DOUBLER INSTALLATION. ALL PER SRM 53-04 PG 218H.May 29, 2007 · N962AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0781714Cusp Web · corrodedPASSENGER CABIN FLOOR CUSP WEB CORRODED. REMOVED CORRODED CUSP WEB, LOCATED DRILLED AND INSTALLED A REPLACEMENT CUSP WEB IAW SRM 51-10-4 AND 51-30-2.May 29, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0781713Cusp Web · corrodedPASSENGER CABIN FLOOR CUSP WEB CORRODED. REMOVED CORROSION MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED CUSP WEB IAW SRM 51-30-2 AND 51-30-1.May 29, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0781712Skin · dentedFUSELAGE SKIN IS DENTED AFT OF THE FWD LAVATORY SERVICE PANEL WITHIN 1 INCH OF LONGERON 20L. COLD WORKED SKIN, FABRICATED DOUBLER ,TREATED, PRIMED AND INSTALLED IAW SRM 51-10-3 PARA 23 AND 30.May 29, 2007 · N962AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0680224Skin · dentedLEFT INBOARD FLAP LOWER SURFACE IS DENTED. CUT OUT DAMAGED AREA. INSTALLED FILLER AND DOUBLER PER SRM 57 01 FIG 5 SHT 2.Mar 2, 2006 · N962AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0680223Skin · damagedFOUND RUDDER LEFT SURFACE IS DINGED 23 INCHES FROM T/E 20.5 INCHES AFT OF LOWER DAMPER CUTOUT. APPLIED FILLER PER SRM 51 70 1A PARA 21.Mar 2, 2006 · N962AS · Doug DC983 · Rudder, Plate/SkinSDR ASAA0680258Repair · delaminatedRUDDER TAB EXISTING REPAIR DELAMINATED 7 TO 9 INCHES FROM T/E AND 3 TO 9 INCHES ABOVE SECOND HINGE. REPLACED EXISTING REPAIR PER SRM 51-70-1A PARA 21.Mar 1, 2006 · N962AS · Doug DC983 · Rudder, Tab StructureSDR ASAA0480627Power Supply · dischargedDURING LINE CHECK, FOUND OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. REPLACED ASSOCIATED POWER SUPPLY (BATTERY PACK). LIGHTS THEN OPERATED PROPERLY. (M)Dec 29, 2004 · N962AS · Doug DC983 · Emergency LightingSDR ASAA0480615Longeron · corrodedOKC - HV-CHECK, LONGERON 29L IS CORRODED. APPLIED SEALANT PER EA 5310-02430. (M)Dec 16, 2004 · N962AS · Doug DC983 · Fuselage Main, Longeron/StringerSDR ASAA0480614Longeron · corrodedOKC - HV-CHECK, FOUND LONGERON 30 IS CORRODED. REMOVED DAMAGED SECTION. INSTALLED U-CHANNEL AND FILLER. (M)Dec 16, 2004 · N962AS · Doug DC983 · Fuselage Main, Longeron/StringerSDR ASAA0480612Access Panel · chafedOKC - HV-CHECK, LEFT WING FUEL PANEL 1303 CHAFED AND PITTED. REPLACED PANEL. (M)Dec 16, 2004 · N962AS · Doug DC983 · Wing, Plate/SkinSDR ASAA0480616Door Frame · gougedOKC - HV-CHECK, TWO MOUNTING HOLES GOUGED AT BOTTOM FRAME OF LEFT OVERWING EXIT. INSTALLED DOUBLER PER EA 53-20-01679. (M)Dec 16, 2004 · N962AS · Doug DC983 · Fuselage Main, Structure
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