N958AS, cancelled Nov 14, 2012

Service difficulty reports · 182

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 = 'N958AS' AND deregistration_id = 'N958AS-2012-11-14'
  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 ASAA0882977Doubler · corrodedFWD LAV SERVICE PANEL DOUBLER IS CORRODED AT FORWARD LOWER LATCH CUTOUT DAMAGED SECTION. FABRICATED LOCATED DRILLED AND INSTALLED REPAIR STRAP AND FILLER IAW ALASKA EA 5330 02339 AND AAR EA12687.May 21, 2008 · N958AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0782085Doubler · chafedRIGHTHAND WING OUTBOARD FLAP INBOARD FIXED VANE L/E DOUBLER IS CHAFED. REPLACED EXISTING DOUBLER PER SRM 51-70-2.Oct 5, 2007 · N958AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0782084Vane · gougedLEFTHAND WING OUTBOARD FLAP INBOARD VANE L/E DOUBLER REPAIR IS GOUGED. REPLACED EXISTING REPAIR DOUBLER PER SRM 51-70-2.Oct 5, 2007 · N958AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0782083Rib · damagedLEFTHAND WING NR 5 L/E SLAT OUTBOARD RIB HOLES OVERSIZED. REPLACED WORN RIB PER SRM 51-10-4 AND 51-30-2.Oct 5, 2007 · N958AS · Doug DC983 · Leading Edge DevicesSDR ASAA0782082Attach Angle · crackedRIGHTHAND SIDE OF VERTICAL STABILIZER EXTERNAL VERTICAL TO FUSELAGE JOIN STRAP (ATTACH ANGLE) IS CRACKED. REPLACED DAMAGED SECTION OF JOIN STRAP PER SRM 53-05.Oct 5, 2007 · N958AS · Doug DC983 · Vertical Stabilizer, Attach FittingsSDR ASAA0782081Cusp Web · crackedCUSP WEB CRACKED. STOP DRILLED CRACK. INSTALLED REPAIR PARTS PER SRM 53-05.Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0782076Track · corrodedCABIN FLOOR FALSE TRACK IS CORRODED. REPLACED FALSE TRACK PER SRM 51-10-3, 51-10-4, 53-14-1 AND 51-30-5.Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0782075Track · corrodedCABIN FALSE TRACK IS CORRODED. REPLACED TRACK PER SRM 51-10-3, 51-10-4, 53-14-1, AND 51-30-5.Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0782074Floor Panel · brokenCABIN FLOOR PANEL HAS DAMAGED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND DAC DWG S4932106.Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0782073Floor Panel · brokenCABIN FLOOR PANEL HAS DAMAGED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND DAC DWG S4932106.Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0782072Floor Panel · delaminatedCABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0782071Floor Panel · brokenCABIN FLOOR PANEL HAS DAMAGED INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0782070Floor Panel · brokenCABIN FLOOR PANEL HAS BROKEN INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0782069Floor Panel · delaminatedCABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05 AND DAC DWG S4932106.Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0782068Floor Panel · brokenCABIN FLOOR PANEL HAS BROKEN INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0782067Floor Panel · brokenCABIN FLOOR PANEL CRACKED WITH DAMAGED INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0782066Floor Panel · delaminatedCABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0782065Seat Track · corrodedCABIN SEAT TRACK EXISTING REPAIR SPLICE CORRODED. REMOVED DAMAGED SECTION OF TRACK. INSTALLED REPLACEMENT PER SRM 51-10-4 AND 53-05.Oct 5, 2007 · N958AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0782080Longeron · crackedLONGERON CRACKED. REMOVED DAMAGED SECTION OF LONGERON. INSTALLED REPLACEMENT SECTION PER SRM 53-02 (SPLICE REPAIR).Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Main, Longeron/StringerSDR ASAA0782079Frame · crackedFRAME CRACKED. REPLACED FRAME PER SRM 53-03.Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Main, FrameSDR ASAA0782078Stiffener · crackedFRAME STIFFENER CRACKED. REPLACED STIFFENER PER SRM 51-30-5, 51-30-2 AND DAC DWG 5913595.Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0782077Shear Tie · crackedSHEAR TIE IS CRACKED. REPLACED SHEAR TIE PER SRM 51-10-4, 51-30-2 AND 51-30-5.Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Internal Mounting StructureSDR ASAA0781416Frame · dentedNLG WHEELWELL LEFT FRAME JUST FORWARD OF LEFT INNER BULKHEAD WAS DENTED. REPLACE FRAME PER SRM 51 30 02.Jan 19, 2007 · N958AS · Doug DC983 · Fuselage Main, FrameSDR ASAA0681318Window · stuckCAPTAIN SIDE SLIDING WINDOW WOULD NOT OPEN. ADJUSTED WINDOW CAM FOLLOWER. OP CHECKED OK.Dec 9, 2006 · N958AS · Doug DC983 · Flight Compartment WindowsSDR ASAA0681304Engine · failedEN ROUTE SAN SEA - RIGHTHAND ENGINE R OIL STRAINER CLOGGING ANNUNCIATED. CREW SHUTDOWN ENGINE AS PRECAUTION AND DIVERTED TO SMF. SUBSEQUENTLY FOUND METAL CONTAMINATION IN THE OIL FILTER SUGGESTING IMPENDING INTERNAL FAILURE. REMOVED ENGINE. WILL BE SENT TO Dec 6, 2006 · N958AS · Doug DC983 · Engine (Turbine/Turboprop)SDR ASAA0681217Window · stuckDURING TAXI TO GATE, COCKPIT LEFT SLIDING WINDOW WOULD NOT OPEN. ADJUSTED UPPER CAM FOLLOWER.Nov 23, 2006 · N958AS · Doug DC983 · Flight Compartment WindowsSDR ASAA0681216Window · stuckON TAXI TO GATE, COCKPIT LEFT SLIDING WINDOW WOULD NOT OPEN. REALIGNED UPPER FORWARD GUIDE PIN.Nov 22, 2006 · N958AS · Doug DC983 · Flight Compartment WindowsSDR ASAA0680807Skin · gougedRIGHT OUTBOARD FLAP INBOARD VANE IS GOUGED ON EXISTING REPAIR AT INBOARD LEADING EDGE. REMOVED EXISTING REPAIR DOUBLER. INSTALLED SKIN FILLER AND EXTERNAL DOUBLER PER SRM 57 03.Jul 25, 2006 · N958AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0680806Skin · gougedLEFT OUTBOARD FLAP INBOARD VANE IS GOUGED ON EXISTING REPAIR AT INBOARD LEADING EDGE. REMOVED EXISTING REPAIR DOUBLER. INSTALLED SKIN FILLER AND EXTERNAL DOUBLER PER SRM 57 03.Jul 25, 2006 · N958AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0680805Shear Tie · corrodedFOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51 10 4 51 10 3 AND 51 30 5.Jul 25, 2006 · N958AS · Doug DC983 · Fuselage Internal Mounting StructureSDR ASAA0680790Rib · gougedTHE RT NR 4 SLAT O B FITTING (RIB ASSY) IS GOUGED OUT OF LIMITS. REMOVED DAMAGED RIB ASSY LOCATED DRILLED AND INSTALLED A REPLACEMENT RIB ASSY IAW MD 80 SRM 51 10 4 AND 51 30 8Jul 20, 2006 · N958AS · Doug DC983 · Leading Edge DevicesSDR ASAA0680789Skin · misdrilledFUSELAGE SKIN HAS MECHANICAL DAMAGE. (MISDRILLS DUE TO PREVIOUSLY ACCOMPLISHED STOP DRILLS ON THE R H ENGINE PYLON UPPER AFT FAIRING SUPPORT ANGLE) CUT OUT DAMAGED AREA OF SKIN. FABRICATED AND INSTALLED A FILLER EXTERNAL DOUBLER AND TWO TAPERED SHIMS IAW AARJul 20, 2006 · N958AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0680788Shear Tie · corrodedSHEAR TIE CORRODED OUT OF LIMITS AT FS 1211 BETWEEN LONGERONS 29R AND 30. REMOVED DAMAGED SHEAR TIE FABRICATED AND INSTALLED A REPLACEMENT SHEAR TIE IAW MD 80 SRM 51 10 4 51 40 3 AND 51 30 5.Jul 20, 2006 · N958AS · Doug DC983 · Fuselage Internal Mounting StructureSDR ASAA0580253Wire · looseANC LINE CHECK, FOUND AFT EXIT CATWALK SIDE PANEL EMERGENCY LIGHT INOPERATIVE. RESECURED LOOSE WIRE CONNECTOR. LIGHT THEN OPERATED PROPERLY. (M)May 9, 2005 · N958AS · Doug DC983 · Emergency LightingSDR ASAA0580220Skin · gougedDURING C-CHECK FOUND, LT WING OUTBOARD FLAP INBOARD FLAP VANE LEADING EDGE GOUGED. REMOVED DAMAGE. INSTALLED REPAIR FILLER AND DOUBLER. (M)Apr 25, 2005 · N958AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0580219Skin · dentedDURING C-CHECK, FOUND RT WING INBOARD FLAP OUTBOARD FLAP VANE UPPER SURFACE DENTED. INSTALLED REPAIR DOUBLER. (M)Apr 25, 2005 · N958AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0580218Skin · gougedFOUND DURING C-CHECK, FUSELAGE SKIN GOUGED. REMOVED DAMAGE. REPAINTED. (M)Apr 25, 2005 · N958AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0580217Skin · delaminatedFOUND DURING C-CHECK, LT WING INBOARD FLAP VANE OUTBOARD SEGMENT DELAMINATED. REMOVED DAMAGE. INSTALLED REPAIR FILLERS AND DOUBLERS. (M)Apr 25, 2005 · N958AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0580216Rib · crackedDURING C-CHECK, FOUND LT WING NR 4 SLAT ACCESS CUTOUT RIB CRACKED. INSTALLED REPAIR DOUBLER PER EA 5740-01447. (M)Apr 25, 2005 · N958AS · Doug DC983 · Leading Edge DevicesSDR ASAA0580213Skin · dentedFOUND DURING C-CHECK, LT ELEVATOR ANTI-FLOAT TAB UPPER SURFACE DENTED. INSTALLED REPAIR DOUBLERS. (M)Apr 20, 2005 · N958AS · Doug DC983 · Elevator, Plate/SkinSDR ASAA0580212Cusp Web · corrodedDURING C-CHECK, FOUND CABIN FLOOR PANEL CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (M)Apr 20, 2005 · N958AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0580211Skin · corrodedDURING C-CHECK, FOUND FUSELAGE SKIN CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M)Apr 20, 2005 · N958AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0480146Module · inoperativeSEA - PREFILGHT CHECK, FOUND FIRST FIVE EMERGENCY TRACK LIGHTS TESTS INOPERATIVE, TWICE. RECONNECTED MODULE CONNECTOR, TWICE. LIGHTS THEN OPERATED PROPERLY. (M)Mar 1, 2004 · N958AS · Doug DC983 · Emergency LightingSDR ASAA0480059Web · corrodedOKC - DURING 15K CHECK, FOUND WEB IS CORRODED AT LONGERON 18L NEAR L2 DOOR. REMOVED CORROSION. INSTALLED FILLER AND DOUBLER PER SRM 53-01. (M)Jan 30, 2004 · N958AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0480057Tab · dentedOKC - DURING 15K CHECK, FOUND LEFT ANTI-FLOAT TAB UPPER SURFACE IS DENTED. APPLIED FILLER PER SRM 55-04. (M)Jan 30, 2004 · N958AS · Doug DC983 · Empennage StructureSDR ASAA0480062Seat Track · corrodedOKC - DURING 15K CHECK, FOUND RIGHT INBOARD SEAT TRACK IS CORRODED AT FS 200-247. REPLACED SEAT TRACK PER SRM 53-05. (M)Jan 30, 2004 · N958AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0480060Seat Track · corrodedOKC - DURING 15K CHECK, FOUND LEFT OUTBOARD SEAT TRACK IS CORRODED AT FS 1106-1185. REPLACED DAMAGED TRACK PER SRM 51-10-4 AND 51-30-5. (M)Jan 30, 2004 · N958AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0480056Skin · dentedOKC - DURNG 15K CHECK, FOUND FUSELAGE SKIN IS DENTED AT FS 237. INSTALLED DOUBLER PER SRM 53-04. (M)Jan 30, 2004 · N958AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0480055Skin · gougedOKC - DURING 15K CHECK, FOUND FUSELAGE SKIN IS GOUGED AT STATION 235. REMOVED DAMAGED SECTION. REPAIRED WITH FILLER AND DOUBLER PER SRM 53-04. (M)Jan 30, 2004 · N958AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0480054Stringer · corrodedOKC - DURING 15K CHECK, FOUND STRINGER IS CORRODED UNDER LOWER FLANGE AT FS 1212. REMOVED DAMAGED SECTION. REPLACED WITH SPLICE PER SRM 53-02, 51-10-3, AND 51-60-0. (M)Jan 30, 2004 · N958AS · Doug DC983 · Fuselage Main, Longeron/Stringer
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