N961AS, cancelled May 4, 2010

Service difficulty reports · 154

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 = 'N961AS' AND deregistration_id = 'N961AS-2010-05-04'
  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 ASAA0883085Fitting · wornF/A REPORTS L 1 DOOR DIFFICULT TO CLOSE FOUND BAYONET FITTING WORN. REMOVED LINER, REMOVED SLIDE, REMOVED REPLACED BAYONET FITTING. FUNCTION CKD L 1 DOOR AS REQUIRED PER MM 52 11 00. REINSTALLED LINER. REINSTALLED SLIDE, OPS CKD DOOR, OPS CKD GOOD PER MM 2Jun 24, 2008 · N961AS · Doug DC983 · Passenger/Crew DoorsSDR ASAA0782386Turbine · failedEN ROUTE SEA TO DEN RIGHTHAND ENGINE STARTED TO EXPERIENCE WHAT APPEARED TO BE COMPRESSOR STALLS. ENGINE WAS PURPOSELY SHUTDOWN AND THE FLIGHT WAS DIVERTED TO SLC. INSPECTION REVEALED TURBINE FAILURE. ENGINE WAS REPLACED. CAUSE OF FAILURE TO BE DETERMINED Dec 13, 2007 · N961AS · Doug DC983 · Turbine SectionSDR ASAA0782295Frame · crackedAFT A C BAY FRAME 1418 CRACKED AT LONGERON 2 RIGHT REPAIRED AFT A C BAY FRAME 1418 IAW MD80 SRM 53 03 FIG 31A. STOP DRILLED CRACK, INSTALLED REPAIR ANGLES. LOCATED AND DRILLED 2 EACH 37 AND 1 EA 35. REPAIR ANGLES AND STRAP INSTALLED PER FIG 31A.Dec 1, 2007 · N961AS · Doug DC983 · Fuselage Main, FrameSDR ASAA0782296Skin · dentedRAMP REPORTS DENT IN AFT CARGO DOOR EXTERIOR SKIN JUST BELOW THE HANDLE CUTOUT. DAMAGED AREA OF SKIN FABRICATED REPAIR DOUBLERS AND INSTALLED IAW ASA EA 5230 01392.Dec 1, 2007 · N961AS · Doug DC983 · Cargo/Baggage DoorsSDR ASAA0782293Skin · delaminatedRT AILERON IS DELAMINATED AT THE O/B ATTACH POINT LOWER SURFACE PREPPED AREA. FABRICATED AND BONDED REPAIR PLIES IAW MD80 SRM 51 90 0 8N PG 72.Nov 29, 2007 · N961AS · Doug DC983 · AileronsSDR ASAA0782292Longeron · crackedLONGERON 2 RIGHT CRACKED AT STA 1418. REMOVED CRACKED SECTION OF LONGERON, FABRICATED AND INSTALLED REPLACEMENT SECTION OF LONGERON AND SPLICE IAW MD80 SRM 53-02 FIGURE 18.Nov 29, 2007 · N961AS · Doug DC983 · Fuselage Main, Longeron/StringerSDR ASAA0782291Longeron · crackedLONGERON 2 LEFT CRACKED AT STA 1418. REMOVED CRACKED SECTION OF LONGERON, FABRICATED AND INSTALLED REPLACEMENT SECTION ON LONGERON AND SPLICE IAW MD80 SRM 53-02 FIGURE 18.Nov 29, 2007 · N961AS · Doug DC983 · Fuselage Main, Longeron/StringerSDR ASAA0782290Frame · crackedFUSELAGE FRAME STA 1418 FROM LONGERON 5L TO 5R FAILSAFE CHORD IS CRACKED. REMOVED CRACKED CHORD RECEIVED DRILLED AND INSTALLED NEW CHORD IAW MD80 SRM 51-10-4, 51-30-5.Nov 29, 2007 · N961AS · Doug DC983 · Fuselage Main, FrameSDR ASAA0782279Skin · damagedA 9 INCH J-SHAPED CREASE ON EXTERIOR OF AFT STAIRWAY DOOR LEFT SIDE OF AIRPLANE JUST FORWARD OF EXTERNAL TAIL CONE ACCESS DOOR. CUT OUT DAMAGED SECTION OF SKIN, FABRICATED LOCATED AND INSTALLED A REPLACEMENT SKIN AND DOUBLER IAW MD80 SRM 52-05 FIG 56.Nov 25, 2007 · N961AS · Doug DC983 · Entrance StairsSDR ASAA0680959Skin · crackedRIGHT WING OUTBOARD FLAP TRAILING EDGE IS CRACKED. REMOVED DAMAGED AREA. APPLIED FOUR REPAIR PLIES PER SRM 51-70-1.Sep 12, 2006 · N961AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0680958Vane · chafedRIGHT WING INBOARD FLAP INBOARD VANE IS CHAFED ON LEADING EDGE. INSTALLED EXTERNAL REPAIR DOUBLER PER SRM 57-03.Sep 12, 2006 · N961AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0680957Stringer Clip · corrodedTEE CLIP CORRODED. REPLACED TEE CLIP PER SRM 51-10-4 AND 51-30-5.Sep 12, 2006 · N961AS · Doug DC983 · Fuselage Main, Attach FittingsSDR ASAA0680956Floor Panel · puncturedCABIN FLOOR PANEL PUNCTURED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106.Sep 12, 2006 · N961AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680955Floor Panel · crackedCABIN FLOOR PANEL IS CRACKED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106.Sep 12, 2006 · N961AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680954Floor Panel · delaminatedCABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND ASA DWG S4932106.Sep 12, 2006 · N961AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680953Shear Tie · corrodedSHEAR TIE CORRODED. REMOVED DAMAGED SECTION OF TIE. INSTALLED REPAIR SECTION AND SPLICE PER SRM 53-03.Sep 12, 2006 · N961AS · Doug DC983 · Fuselage Internal Mounting StructureSDR ASAA0680952Cusp Web · corrodedCUSP WEB CORRODED. REMOVED DAMAGED CUSP SECTION. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 51-70-4.Sep 12, 2006 · N961AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0680951Cusp Web · corrodedCUSP WEB CORRODED. REPLACED CUSP WEB PER SRM 51-10-4, 51-30-1, 51-30-2 AND 51-30-5.Sep 12, 2006 · N961AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0680921Skin · dentedFUSELAGE SKIN DENTED. REMOVED DAMAGED SECTION INCLUDING EXISTING REPAIR DOUBLER. INSTALLED EXTERNAL REPAIR DOUBLER FINGER DOUBLER LONGERON STRAP AND FILLER IAW SRM 53 04.Aug 31, 2006 · N961AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0680925Cusp Web · corrodedCUSP WEB CORRODED. REMOVED DAMAGED SECTION OF WEB. INSTALLED REPAIR DOUBLER IAW SRM 53 01.Aug 31, 2006 · N961AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0680924Floor Panel · delaminatedCABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106.Aug 31, 2006 · N961AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680923Floor Panel · delaminatedCABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106.Aug 31, 2006 · N961AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680922Floor Panel · delaminatedCABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106.Aug 31, 2006 · N961AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680915Floor Panel · delaminatedCABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL IAW SRM 52 05 AND ASA DWG S4932106.Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680914Floor Panel · delaminatedCABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106.Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680913Floor Panel · corrodedCABIN FLOOR PANEL CORRODED AT INSERTS. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106.Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680912Insert · corrodedCABIN FLOOR PANEL HAS CORRODED INSERTS. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106.Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680911Floor Panel · delaminatedCABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106.Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680910Floor Panel · crackedCABIN FLOOR PANEL CRACKED AT INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106.Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680909Floor Panel · delaminatedCABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106.Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680908Floor Panel · crackedCABIN FLOOR PANEL CRACKED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106.Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680907Floor Panel · delaminatedCABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106.Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680906Floor Panel · corrodedCABIN FLOOR PANEL HAS CORRODED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106.Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680905Floor Panel · corrodedCABIN FLOOR PANEL CORRODED AT INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106.Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680902Web · crackedL1 DOOR JAMB WEB IS CRACKED. REMOVED DAMAGED AREA OF WEB. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-70-4.Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0680903Shear Tie · corrodedAFT CARGO BAY SHEAR TIE IS CORRODED. REPLACED SHEAR TIE PER SRM 51-10-4 AND 51-30-5.Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Internal Mounting StructureSDR ASAA0680904Skin · dentedMID CARGO BAY DOOR DENTED. COLD FORMED TO ORIGINAL CONTOUR. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53-04.Aug 29, 2006 · N961AS · Doug DC983 · Cargo/Baggage DoorsSDR ASAA0680901Gusset · corrodedAFT CARGO BAY THRESHOLD WEB GUSSET IS CORRODED. REPLACED GUSSET IAW SRM 53 14 3 51 10 2 51 10 3. 51 30 2. AND 51 30 5.Aug 23, 2006 · N961AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0680759Lanyard · wornINADVERTENTLY DEPLOYED TAIL CONE WHICH SHOULD HAVE ALSO CAUSED AFT EMERGENCY SLIDE TO DEPLOY. LANYARD VELCRO AND SNAP PULLED LOOSE FROM THE SLIDE COVER BUT THE SLIDE DID NOT DEPLOY. RETRIGGER SLIDE ASSEMBLY WITH NEW LANYARD. ENGINEERING INVESTIGATION HAS BEJul 11, 2006 · N961AS · Doug DC983 · Escape SlideSDR ASAA0580300Vane · dentedOKC - FOUND HV-CHECK, RIGHT FLAP VANE DENTED ON LOWER SURFACE. REMOVED DAMAGED SECTION. INSTALLED FILLER AND DOUBLER. (M)Jun 4, 2005 · N961AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0580299Vane · gougedOKC - FOUND DURING HV-CHECK, RIGHT FLAP VANE GOUGED. REPAIRED DAMAGED SECTION PER SRM 51-70. (M)Jun 4, 2005 · N961AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0580298Skin · dentedOKC - FOUND DURING HV-CHECK, LEFT NR 2 SLAT L/E DENTED. REPAIRED DAMAGED SECTION PER SRM 57-09. (M)Jun 4, 2005 · N961AS · Doug DC983 · Leading Edge DevicesSDR ASAA0480452Wire · misinstalledSEA - FOUND DURING PREFLIGHT, COCKPIT OVERHEAD FLOOD LIGHT FOUND INOPERATIVE UPON TEST. REROUTED MIS-CONNECTED FLOOR LIGHT WIRE. LIGHT THEN OPERATED PROPERLY. (M)May 26, 2004 · N961AS · Doug DC983 · Light System WiringSDR ASAA0480188Web · corrodedOKC - DURING HV CHECK, FOUND AFT CARGO BAY DOOR CUTOUT INTERNAL WEB IS CORRODED AROUND ATTACH HARDWARE AT FS 1155-1211. REPLACED DAMAGED AREA OF WEB AND INSTALLED DOUBLER PER SRM 51-70-4. (M)Mar 14, 2004 · N961AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0480187Attach Angle · corrodedOKC - DURING HV CHECK, FOUND ATTACH ANGLE IS CORRODED AT FS 1007. REPLACED ANGLE PER SRM 51-10-4. (M)Mar 14, 2004 · N961AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0480186Seat Track · chafedOKC - DURING HV CHECK, FOUND CABIN SEAT TRACK IS CHAFED AT FS 1212-1322. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M)Mar 14, 2004 · N961AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0480153Floor Panel · delaminatedOKC - FOUND FORWARD CABIN FLOOR PANEL STATION 148 TO STATION 168 HAS DELAMINATION AROUND FASTENER HOLES. FABRICATED REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05. (M)Mar 13, 2004 · N961AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0480156Floorboard · corrodedOKC - FOUND CABIN FLOORBOARD STATION 200-256 HAS SEVERAL CORRODED INSERTS. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)Mar 13, 2004 · N961AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0480160Floor Panel · crackedOKC - FOUND INSERTS PULLING OFF, CORRODED AND PANEL CRACKED AT LOWER SURFACE, FORWARD CABIN STATION 148-200. FABRICATED REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05. (M)Mar 12, 2004 · N961AS · Doug DC983 · Fuselage Floor PanelSDR ASAAO480180Seat Track · chafedOKC - DURING HV CHECK, FOUND SEAT TRACK CHAFED AT FS 1212. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M)Mar 10, 2004 · N961AS · Doug DC983 · Fuselage, Seat/Cargo Attach Fittings
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