N979AS

Service difficulty reports not matched to an aircraft · 133

They name N979AS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N979AS' AND registry_match IS NULL
  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 ASAA0681178Skin · puncturedLEFT WING INBOARD FLAP VANE IS PUNCTURED. REPLACED DAMAGED SKIN SECTION AND INSTALLED REPAIR FILLER AND DOUBLER PER SRM 57 03.Nov 6, 2006 · N979AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0681177Skin · chafedVERTICAL STABILIZER LEFT SIDE SKIN IS CHAFED AT AFT END OF HORIZONTAL STABILIZER LOWER FAIRING. REPLACED DAMAGED SKIN PANEL PER SRM 51 10 4 AND 51 30 2.Nov 6, 2006 · N979AS · Doug DC983 · Vertical Stabilizer, Plate/SkinSDR ASAA0681176Skin · chafedVERTICAL STABILIZER RIGHT SIDE SKIN CHAFED AT AFT END OF HORIZONTAL STABILIZER LOWER FAIRING. REPLACED DAMAGED SKIN PANEL PER SRM 51 10 4 AND 51 30 2.Nov 6, 2006 · N979AS · Doug DC983 · Vertical Stabilizer, Plate/SkinSDR ASAA0681175Seat Track · corrodedFOUND CABIN FLOOR TRACK IS CORRODED. REPLACED TRACK PER SRM 51 10 4 51 10 3 51 30 2 AND 51 30 5.Nov 6, 2006 · N979AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0681152Longeron · corrodedFOUND LONGERON 23L IS CORRODED ON UPPER FLANGE. BLENDED FLANGE TO REMOVE CORROSION AND INSTALLED REPAIR STRAP PER SRM 53 02.Oct 30, 2006 · N979AS · Doug DC983 · Fuselage Main, Longeron/StringerSDR ASAA0681151Tab · nickedRIGHT AILERON CONTROL TAB IS NICKED ON T E. REPAIRED WITH FILLER COMPOUND AND SANDED TO ORIGINAL CONTOUR PER SRM 51 70 1A.Oct 30, 2006 · N979AS · Doug DC983 · Aileron TabsSDR ASAA0681150Floor Panel · delaminatedCABIN FLOOR PANEL DELAMINATED ALONG EDGES. REPLACED FLOOR PANEL PER SRM 53 05 DWG 9936692 AND MM 53 20 01.Oct 30, 2006 · N979AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0681149Floor Panel · delaminatedCABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL PER SRM 53 05 DWG 9951788 AND MM 53 24 01.Oct 30, 2006 · N979AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0681148Floor Panel · delaminatedCABIN FLOOR PANEL IS DELAMINATED ALONG EDGES. REPLACE FLOOR PANEL PER SRM 53 05 DWG 9951788 AND MM 53 24 01.Oct 30, 2006 · N979AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0681147Floor Panel · corrodedCABIN FLOOR PANEL IS CORRODED. REPLACED FLOOR PANEL PER SRM 53 05 DWG 9951788 AND MM 53 20 01.Oct 30, 2006 · N979AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0681146Floor Panel · corrodedCABIN FLOOR PANEL IS CORRODED AND HAS MISSING INSERTS. REPLACED DAMAGED FLOOR PANEL PER SRM 53 05 DWG 9951788 AND MM 53 20 01.Oct 30, 2006 · N979AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0681145Floor Panel · corrodedCABIN FLOOR PANEL CORRODED WITH SOME BROKEN INSERTS. REPLACED FLOOR PANEL PER SRM 53 05 DWG 9951788 AND MM 53 24 01.Oct 30, 2006 · N979AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0681144Seat Track · corrodedFOUND CABIN SEAT TRACK CORRODED. REPLACED DAMAGED TRACK SECTION AND INSTALLED REPAIR SPLICE PER SRM 53 05.Oct 30, 2006 · N979AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0681143Seat Track · corrodedFOUND CABIN SEAT TRACK IS CORRODED. REPLACED DAMAGED TRACK SECTION AND REPAIR SPLICE PER SRM 53 05.Oct 30, 2006 · N979AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0681142Skin · dentedFUSELAGE DENTED. COLD FORMED SKIN TO ORIGINAL CONTOUR. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53 04.Oct 26, 2006 · N979AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0681141Gusset · corrodedAFT CARGO BAY GUSSET CORRODED BETWEEN LONGERONS. REPLACED DAMAGED GUSSET PER SRM 51 10 4 51 10 3 51 30 5 AND DWG 5936071.Oct 26, 2006 · N979AS · Doug DC983 · Fuselage Main, StructureSDR ASAA0681125Coffeemaker · defectiveAFT GALLEY COFFEEMAKER BEGAN TO SMOKE DURING FLIGHT. PERFORMED AIR TURNBACK. REMOVED DEFECTIVE COFFEEMAKER.Oct 22, 2006 · N979AS · Doug DC983 · Buffet/GalleysSDR ASAA0680416Lanyard · misriggedTAILCONE EXIT EMERGENCY SLIDE COVER LANYARD RING ASSEMBLY WAS FOUND TO HAVE ONE LANYARD INCORRECTLY ATTACHED TO THE COMMON RING. REPLACED THE MIS ASSEMBLED LANYARD ASSEMBLY. INVESTIGATION IS BEING UNDERTAKEN TO DETERMINE HOW IT WAS THIS ANOMALY WAS NOT DISCOApr 9, 2006 · N979AS · Doug DC983 · Emergency EquipmentSDR ASAA0580559Hinge · failedCLIMB AT FL260, ENROUTE, FWD FLIGHT ATTENDANT OXYGEN MASK DID NOT DROP DURING CABIN DECOMPRESSION CAUSED BY FUSELAGE SKIN PUNCTURE. DETERMINED THE THE O2 MASK DOOR WAS JAMMED BY A DEBONDED O2 MASK DOOR HINGE. REBONDED O2 MASK DOOR HINGE AND ADJUSTED CLEARANCDec 26, 2005 · N979AS · Doug MD83 · Fuselage, Door HingeSDR ASAA0580558Skin · puncturedCLIMB, ENROUTE, CABIN DECOMPRESSED RAPIDLY AND UNCONTROLLABLE. ALL OXYGEN MASKS, SAME FOR ONE (TO BE REPORTED UNDER SEPARATE SDR), DROPPED PROPERLY. AN EMERGENCY DESCENT WAS MADE AND THE AIRCRAFT LANDED SAFELY BACK AT SEA. INVESTIGATION REVEALED THE CAUSE Dec 26, 2005 · N979AS · Doug MD83 · Fuselage Main, Plate/SkinSDR ASAA0580358Window · disengagedPREFLIGHT CHECK, FOUND COCKPIT LEFT SLIDING WINDOW COULD NOT BE OPENED. REPOSITIONED FORWARD UPPER LATCH PIN IN CHANNEL TRACK. WINDOW THEN OPERATED PROPERLY. (M)Jun 28, 2005 · N979AS · Doug DC983 · Flight Compartment WindowsSDR ASAA0580359Window · disengagedPREFLIGHT CHECK, FOUND COCKPIT LEFT SLIDING WINDOW COULD NOT BE OPENED, 2ND OCCURRENCE ON SAME DAY AND 4TH OCCURRENCE IN LAST THREE DAYS. REPOSITIONED FORWARD UPPER LATCH PIN IN CHANNEL TRACK. WINDOW THEN OPERATED PROPERLY. (M)Jun 28, 2005 · N979AS · Doug DC983 · Flight Compartment WindowsSDR ASAA0580357Window · disengagedPREFLIGHT CHECK, FOUND COCKPIT LEFT SLIDING WINDOW COULD NOT BE OPENED. REPOSITIONED FORWARD UPPER LATCH PIN IN CHANNEL TRACK. WINDOW THEN OPERATED PROPERLY. (M)Jun 27, 2005 · N979AS · Doug DC983 · Flight Compartment WindowsSDR ASAA0580356Window · disengagedPREFLIGHT CHECK, COCKPIT LEFT SLIDING WINDOW COULD NOT BE OPENED. REPOSITIONED FORWARD UPPER LATCH PIN IN CHANNEL TRACK. WINDOW THEN OPERATED PROPERLY. (M)Jun 26, 2005 · N979AS · Doug DC983 · Flight Compartment WindowsSDR ASAA0480533Lanyard · disconnectedSJC, PRE-FLIGHT CHECK, AFT SERVICE (L-2) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD.Oct 11, 2004 · N979AS · Doug MD83 · Escape SlideSDR ASAA0480448Clip · crackedOKC - DURING HV-CHECK, FOUND LOWER ATTACHMENT CLIP IS CRACKED AT FS 1463 AT RIGHT SIDE OF LONGERON 3. REPLACED CLIP PER SRM 51-10-2. (M)May 22, 2004 · N979AS · Doug MD83 · Fuselage Miscellaneous StructureSDR ASAA0480447Angle · crackedOKC - DURING HV CHECK, FOUND SUPPORT ANGLE IS CRACKED AT FS 1463 AT LONGERON 6R. REPLACED DAMAGED ANGLE PER SRM 51-10-4. (M)May 22, 2004 · N979AS · Doug MD83 · Fuselage Miscellaneous StructureSDR ASAA0480446Skin · gougedOKC - DURING HV-CHECK, FOUND LEFT NR 0 SLAT INBOARD UPPER SKIN IS GOUGED AT AFT CORNER. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 57-09. (M)May 22, 2004 · N979AS · Doug MD83 · Leading Edge DevicesSDR ASAA0480444Skin · crackedOKC - DURING HV CHECK, FOUND LEFT NR 2 SLAT LOWER SURFACE SKIN IS CRACKED. REPLACED SKIN PER SRM 51-30-8. (M)May 22, 2004 · N979AS · Doug MD83 · Leading Edge DevicesSDR ASAA0480445Rivet · shearedOKC - DURING HV CHECK, REAR SERVICE R1 DOOR HAS SHEARED RIVET IN LOWER FORWARD SECTION. INSTALLED DOUBLER AND BUSHING PER EA 5200-01017. (M)May 22, 2004 · N979AS · Doug MD83 · Passenger/Crew DoorsSDR ASAA0480451Vane · nickedOKC - DURING HV-CHECK, FOUND RIGHT OUTBOARD FLAP INBOARD VANE IS NICKED AT LEADING EDGE. INSTALLED FILLER AND DOUBLER PER SRM 51-70-2. (M)May 22, 2004 · N979AS · Doug MD83 · Trailing Edge FlapsSDR ASAA0480450Frame · corrodedOKC - DURING HV-CHECK, FOUND FRAME IS CORRODED IN AFT CARGO BAY AT FS 1079 AT LONGERON 29R. REMOVED CORROSION AND APPLIED PROTECTIVE TREATMENT PER EA 5310-02365. (M)May 22, 2004 · N979AS · Doug MD83 · Fuselage Main, FrameSDR ASAA0480449Longeron · corrodedOKC - DURING HV-CHECK, FOUND LONGERON 28R CORRODED AROUND FASTENERS IN AFT CARGO BAY AT FS 1079. REMOVED CORROSION AND APPLIED PROTECTIVE TREATMENT PER EA 5310-02364. (M)May 22, 2004 · N979AS · Doug MD83 · Fuselage Main, Longeron/StringerSDR ASAA0480432Angle · corrodedOKC - DURING HV CHECK, FOUND AFT CARGO DOOR BOTTOM EDGE 'L' ANGLE IS GOUGED. REMOVED DAMAGED ANGLE AND INSTALLED NEW ANGLE IAW 51-30-5. (M)May 17, 2004 · N979AS · Doug MD83 · Cargo/Baggage DoorsSDR ASAA0480433Panel · corrodedOKC - DURING HV CHECK, FOUND RT WING FUEL PANEL 1462 HAS LIGHT SURFACE CORROSION. REMOVED DAMAGE AND REPLACED WITH NEW FUEL PANEL IAW 51-22-2A. (M)May 17, 2004 · N979AS · Doug MD83 · Wing, Plate/SkinSDR ASAA0480429Panel · corrodedDURING HV CHECK, FOUND FUEL PANEL NR 1478C HAS SURFACE CORROSION ON INSIDE FLANGE. REMOVED DAMAGE AND REPLACED FUEL PANEL IAW 51-22-2A. (M)May 17, 2004 · N979AS · Doug MD83 · Wing, Plate/SkinSDR ASAA0480430Frame · corrodedOKC - DURING HV CHECK, FOUND FRAME IN AFT CARGO PIT AT STATION 1287, LONGERON 29L-28R IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR FRAME SEGMENT IAW 53-03. (M)May 17, 2004 · N979AS · Doug MD83 · Fuselage Main, FrameSDR ASAA0480431Panel · chafedDURING HV CHECK, FOUND RIGHT VERT STAB UNDER PANEL 3804A HAS CHAFED SURFACE. REMOVED DAMAGED SKIN PANEL AND INSTALLED NEW PANEL IAW 51-20-8. (M)May 17, 2004 · N979AS · Doug MD83 · Vertical Stabilizer, Plate/SkinSDR ASAA0480423Shear Tie · corrodedDURING HV CHECK, FOUND SHEAR TIE IN AFT PIT AT STATION 1287, LONGERON 29L TO 29R IS CORRODED. REMOVED DAMAGE AND INSTALLED FRAME REPAIR SPLICE IAW 53-03. (M)May 17, 2004 · N979AS · Doug MD83 · Fuselage Main, StructureSDR ASAA0480424Shear Tie · corrodedOKC - DURING HV CHECK, FOUND SHEAR TIE IN AFT PIT AT STATION 1148, LONGERON 29L TO 28R IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT SHEAR TIE IAW 51-10-2. (M)May 17, 2004 · N979AS · Doug MD83 · Fuselage Main, StructureSDR ASAA0480425Strap · corrodedDURING HV CHECK, FOUND AFT PIT DOOR JAMB STRAP AT STATION 1168-1207 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT STRAP IAW 51-10-2. (M)May 17, 2004 · N979AS · Doug MD83 · Fuselage Miscellaneous StructureSDR ASAA0480426Frame · corrodedOKC - DURING HV CHECK, FOUND FRAME IN AFT PIT AT STATION 1231, LONGERON 29L-29R IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR SPLICE IAW 53-03. (M)May 17, 2004 · N979AS · Doug MD83 · Fuselage Main, FrameSDR ASAA0480427Seat Track · corrodedOKC - DURING HV CHECK - FOUND SEAT TRACK AT STATION 200-237, RBL 22 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT SECTION IAW 51-10-4. (M)May 17, 2004 · N979AS · Doug MD83 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0480428Wedge · gougedDURING HV CHECK, FOUND RIG WING INBOARD FLAP, INBOARD WEDGE LOWER SURFACE IS GOUGED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW 57-03. (M)May 17, 2004 · N979AS · Doug MD83 · Trailing Edge FlapsSDR ASAA0480414Floor Panel · corrodedOKC - DURING HV CHECK, FOUND FORWARD CABIN FLOOR MEMBER AT STATION 200, RBL 8 - LBL 8 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR SPLICE IAW 51-10-4. (M)May 16, 2004 · N979AS · Doug MD83 · Fuselage Floor PanelSDR ASAA0480415Cusp Web · corrodedOKC - DURING HV CHECK, FOUND CUSP WEB BETWEEN STATION 693-712 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW 51-70-4. (M)May 16, 2004 · N979AS · Doug MD83 · Fuselage Miscellaneous StructureSDR ASAA0480416Floor Panel · puncturedOKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL BELOW FIRST OFFICERS SEAT IS PUNCTURED. REMOVED DAMAGED SKIN AND INSTALLED REPAIR DOUBLER IAW 53-01. (M)May 16, 2004 · N979AS · Doug MD83 · Fuselage Floor PanelSDR ASAA0480417Seat Track · corrodedOKC - DURING HV CHECK, FOUND CABIN SEAT TRACK AT STATION 200-237, RBL 44 IS CORRODED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR SECTION IAW 53-05. (M)May 16, 2004 · N979AS · Doug MD83 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0480418Floor Panel · corrodedOKC - DURING HV-CHECK, FOUND FLOOR WEB AT STATION 200, RBL 22 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW 51-70-4. (M)May 16, 2004 · N979AS · Doug MD83 · Fuselage Floor PanelSDR ASAA0480419Cusp Web · corrodedDURING HV-CHECK, FOUND CUSP WEB PANEL AT STATION 674, L18 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW 51-10-4. (M)May 16, 2004 · N979AS · Doug MD83 · Fuselage Miscellaneous Structure
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