# Service difficulty reports: N961AS, cancelled May 4, 2010 A list on [N961AS, cancelled May 4, 2010](https://openairdocs.org/deregistered/N961AS-2010-05-04.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 4 · 154 reports - [SDR ASAA0883085](https://openairdocs.org/sdr/ASAA0883085.md): Fitting · worn · Jun 24, 2008 · N961AS · Doug DC983 · Passenger/Crew Doors > F/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 2 - [SDR ASAA0782386](https://openairdocs.org/sdr/ASAA0782386.md): Turbine · failed · Dec 13, 2007 · N961AS · Doug DC983 · Turbine Section > EN 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 - [SDR ASAA0782295](https://openairdocs.org/sdr/ASAA0782295.md): Frame · cracked · Dec 1, 2007 · N961AS · Doug DC983 · Fuselage Main, Frame > AFT 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. - [SDR ASAA0782296](https://openairdocs.org/sdr/ASAA0782296.md): Skin · dented · Dec 1, 2007 · N961AS · Doug DC983 · Cargo/Baggage Doors > RAMP 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. - [SDR ASAA0782293](https://openairdocs.org/sdr/ASAA0782293.md): Skin · delaminated · Nov 29, 2007 · N961AS · Doug DC983 · Ailerons > RT 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. - [SDR ASAA0782292](https://openairdocs.org/sdr/ASAA0782292.md): Longeron · cracked · Nov 29, 2007 · N961AS · Doug DC983 · Fuselage Main, Longeron/Stringer > LONGERON 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. - [SDR ASAA0782291](https://openairdocs.org/sdr/ASAA0782291.md): Longeron · cracked · Nov 29, 2007 · N961AS · Doug DC983 · Fuselage Main, Longeron/Stringer > LONGERON 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. - [SDR ASAA0782290](https://openairdocs.org/sdr/ASAA0782290.md): Frame · cracked · Nov 29, 2007 · N961AS · Doug DC983 · Fuselage Main, Frame > FUSELAGE 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. - [SDR ASAA0782279](https://openairdocs.org/sdr/ASAA0782279.md): Skin · damaged · Nov 25, 2007 · N961AS · Doug DC983 · Entrance Stairs > A 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. - [SDR ASAA0680959](https://openairdocs.org/sdr/ASAA0680959.md): Skin · cracked · Sep 12, 2006 · N961AS · Doug DC983 · Trailing Edge Flaps > RIGHT WING OUTBOARD FLAP TRAILING EDGE IS CRACKED. REMOVED DAMAGED AREA. APPLIED FOUR REPAIR PLIES PER SRM 51-70-1. - [SDR ASAA0680958](https://openairdocs.org/sdr/ASAA0680958.md): Vane · chafed · Sep 12, 2006 · N961AS · Doug DC983 · Trailing Edge Flaps > RIGHT WING INBOARD FLAP INBOARD VANE IS CHAFED ON LEADING EDGE. INSTALLED EXTERNAL REPAIR DOUBLER PER SRM 57-03. - [SDR ASAA0680957](https://openairdocs.org/sdr/ASAA0680957.md): Stringer Clip · corroded · Sep 12, 2006 · N961AS · Doug DC983 · Fuselage Main, Attach Fittings > TEE CLIP CORRODED. REPLACED TEE CLIP PER SRM 51-10-4 AND 51-30-5. - [SDR ASAA0680956](https://openairdocs.org/sdr/ASAA0680956.md): Floor Panel · punctured · Sep 12, 2006 · N961AS · Doug DC983 · Fuselage Floor Panel > CABIN FLOOR PANEL PUNCTURED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106. - [SDR ASAA0680955](https://openairdocs.org/sdr/ASAA0680955.md): Floor Panel · cracked · Sep 12, 2006 · N961AS · Doug DC983 · Fuselage Floor Panel > CABIN FLOOR PANEL IS CRACKED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106. - [SDR ASAA0680954](https://openairdocs.org/sdr/ASAA0680954.md): Floor Panel · delaminated · Sep 12, 2006 · N961AS · Doug DC983 · Fuselage Floor Panel > CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND ASA DWG S4932106. - [SDR ASAA0680953](https://openairdocs.org/sdr/ASAA0680953.md): Shear Tie · corroded · Sep 12, 2006 · N961AS · Doug DC983 · Fuselage Internal Mounting Structure > SHEAR TIE CORRODED. REMOVED DAMAGED SECTION OF TIE. INSTALLED REPAIR SECTION AND SPLICE PER SRM 53-03. - [SDR ASAA0680952](https://openairdocs.org/sdr/ASAA0680952.md): Cusp Web · corroded · Sep 12, 2006 · N961AS · Doug DC983 · Fuselage Miscellaneous Structure > CUSP WEB CORRODED. REMOVED DAMAGED CUSP SECTION. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 51-70-4. - [SDR ASAA0680951](https://openairdocs.org/sdr/ASAA0680951.md): Cusp Web · corroded · Sep 12, 2006 · N961AS · Doug DC983 · Fuselage Miscellaneous Structure > CUSP WEB CORRODED. REPLACED CUSP WEB PER SRM 51-10-4, 51-30-1, 51-30-2 AND 51-30-5. - [SDR ASAA0680921](https://openairdocs.org/sdr/ASAA0680921.md): Skin · dented · Aug 31, 2006 · N961AS · Doug DC983 · Fuselage Main, Plate/Skin > FUSELAGE SKIN DENTED. REMOVED DAMAGED SECTION INCLUDING EXISTING REPAIR DOUBLER. INSTALLED EXTERNAL REPAIR DOUBLER FINGER DOUBLER LONGERON STRAP AND FILLER IAW SRM 53 04. - [SDR ASAA0680925](https://openairdocs.org/sdr/ASAA0680925.md): Cusp Web · corroded · Aug 31, 2006 · N961AS · Doug DC983 · Fuselage Miscellaneous Structure > CUSP WEB CORRODED. REMOVED DAMAGED SECTION OF WEB. INSTALLED REPAIR DOUBLER IAW SRM 53 01. - [SDR ASAA0680924](https://openairdocs.org/sdr/ASAA0680924.md): Floor Panel · delaminated · Aug 31, 2006 · N961AS · Doug DC983 · Fuselage Floor Panel > CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106. - [SDR ASAA0680923](https://openairdocs.org/sdr/ASAA0680923.md): Floor Panel · delaminated · Aug 31, 2006 · N961AS · Doug DC983 · Fuselage Floor Panel > CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106. - [SDR ASAA0680922](https://openairdocs.org/sdr/ASAA0680922.md): Floor Panel · delaminated · Aug 31, 2006 · N961AS · Doug DC983 · Fuselage Floor Panel > CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106. - [SDR ASAA0680915](https://openairdocs.org/sdr/ASAA0680915.md): Floor Panel · delaminated · Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor Panel > CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL IAW SRM 52 05 AND ASA DWG S4932106. - [SDR ASAA0680914](https://openairdocs.org/sdr/ASAA0680914.md): Floor Panel · delaminated · Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor Panel > CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106. - [SDR ASAA0680913](https://openairdocs.org/sdr/ASAA0680913.md): Floor Panel · corroded · Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor Panel > CABIN FLOOR PANEL CORRODED AT INSERTS. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106. - [SDR ASAA0680912](https://openairdocs.org/sdr/ASAA0680912.md): Insert · corroded · Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor Panel > CABIN FLOOR PANEL HAS CORRODED INSERTS. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106. - [SDR ASAA0680911](https://openairdocs.org/sdr/ASAA0680911.md): Floor Panel · delaminated · Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor Panel > CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106. - [SDR ASAA0680910](https://openairdocs.org/sdr/ASAA0680910.md): Floor Panel · cracked · Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor Panel > CABIN FLOOR PANEL CRACKED AT INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106. - [SDR ASAA0680909](https://openairdocs.org/sdr/ASAA0680909.md): Floor Panel · delaminated · Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor Panel > CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106. - [SDR ASAA0680908](https://openairdocs.org/sdr/ASAA0680908.md): Floor Panel · cracked · Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor Panel > CABIN FLOOR PANEL CRACKED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106. - [SDR ASAA0680907](https://openairdocs.org/sdr/ASAA0680907.md): Floor Panel · delaminated · Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor Panel > CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106. - [SDR ASAA0680906](https://openairdocs.org/sdr/ASAA0680906.md): Floor Panel · corroded · Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor Panel > CABIN FLOOR PANEL HAS CORRODED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106. - [SDR ASAA0680905](https://openairdocs.org/sdr/ASAA0680905.md): Floor Panel · corroded · Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor Panel > CABIN FLOOR PANEL CORRODED AT INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106. - [SDR ASAA0680902](https://openairdocs.org/sdr/ASAA0680902.md): Web · cracked · Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Miscellaneous Structure > L1 DOOR JAMB WEB IS CRACKED. REMOVED DAMAGED AREA OF WEB. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-70-4. - [SDR ASAA0680903](https://openairdocs.org/sdr/ASAA0680903.md): Shear Tie · corroded · Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Internal Mounting Structure > AFT CARGO BAY SHEAR TIE IS CORRODED. REPLACED SHEAR TIE PER SRM 51-10-4 AND 51-30-5. - [SDR ASAA0680904](https://openairdocs.org/sdr/ASAA0680904.md): Skin · dented · Aug 29, 2006 · N961AS · Doug DC983 · Cargo/Baggage Doors > MID CARGO BAY DOOR DENTED. COLD FORMED TO ORIGINAL CONTOUR. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53-04. - [SDR ASAA0680901](https://openairdocs.org/sdr/ASAA0680901.md): Gusset · corroded · Aug 23, 2006 · N961AS · Doug DC983 · Fuselage Miscellaneous Structure > AFT 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. - [SDR ASAA0680759](https://openairdocs.org/sdr/ASAA0680759.md): Lanyard · worn · Jul 11, 2006 · N961AS · Doug DC983 · Escape Slide > INADVERTENTLY 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 BE - [SDR ASAA0580300](https://openairdocs.org/sdr/ASAA0580300.md): Vane · dented · Jun 4, 2005 · N961AS · Doug DC983 · Trailing Edge Flaps > OKC - FOUND HV-CHECK, RIGHT FLAP VANE DENTED ON LOWER SURFACE. REMOVED DAMAGED SECTION. INSTALLED FILLER AND DOUBLER. (M) - [SDR ASAA0580299](https://openairdocs.org/sdr/ASAA0580299.md): Vane · gouged · Jun 4, 2005 · N961AS · Doug DC983 · Trailing Edge Flaps > OKC - FOUND DURING HV-CHECK, RIGHT FLAP VANE GOUGED. REPAIRED DAMAGED SECTION PER SRM 51-70. (M) - [SDR ASAA0580298](https://openairdocs.org/sdr/ASAA0580298.md): Skin · dented · Jun 4, 2005 · N961AS · Doug DC983 · Leading Edge Devices > OKC - FOUND DURING HV-CHECK, LEFT NR 2 SLAT L/E DENTED. REPAIRED DAMAGED SECTION PER SRM 57-09. (M) - [SDR ASAA0480452](https://openairdocs.org/sdr/ASAA0480452.md): Wire · misinstalled · May 26, 2004 · N961AS · Doug DC983 · Light System Wiring > SEA - FOUND DURING PREFLIGHT, COCKPIT OVERHEAD FLOOD LIGHT FOUND INOPERATIVE UPON TEST. REROUTED MIS-CONNECTED FLOOR LIGHT WIRE. LIGHT THEN OPERATED PROPERLY. (M) - [SDR ASAA0480188](https://openairdocs.org/sdr/ASAA0480188.md): Web · corroded · Mar 14, 2004 · N961AS · Doug DC983 · Fuselage Miscellaneous Structure > OKC - 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) - [SDR ASAA0480187](https://openairdocs.org/sdr/ASAA0480187.md): Attach Angle · corroded · Mar 14, 2004 · N961AS · Doug DC983 · Fuselage Miscellaneous Structure > OKC - DURING HV CHECK, FOUND ATTACH ANGLE IS CORRODED AT FS 1007. REPLACED ANGLE PER SRM 51-10-4. (M) - [SDR ASAA0480186](https://openairdocs.org/sdr/ASAA0480186.md): Seat Track · chafed · Mar 14, 2004 · N961AS · Doug DC983 · Fuselage, Seat/Cargo Attach Fittings > OKC - DURING HV CHECK, FOUND CABIN SEAT TRACK IS CHAFED AT FS 1212-1322. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M) - [SDR ASAA0480153](https://openairdocs.org/sdr/ASAA0480153.md): Floor Panel · delaminated · Mar 13, 2004 · N961AS · Doug DC983 · Fuselage Floor Panel > OKC - 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) - [SDR ASAA0480156](https://openairdocs.org/sdr/ASAA0480156.md): Floorboard · corroded · Mar 13, 2004 · N961AS · Doug DC983 · Fuselage Floor Panel > OKC - FOUND CABIN FLOORBOARD STATION 200-256 HAS SEVERAL CORRODED INSERTS. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) - [SDR ASAA0480160](https://openairdocs.org/sdr/ASAA0480160.md): Floor Panel · cracked · Mar 12, 2004 · N961AS · Doug DC983 · Fuselage Floor Panel > OKC - 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) - [SDR ASAAO480180](https://openairdocs.org/sdr/ASAAO480180.md): Seat Track · chafed · Mar 10, 2004 · N961AS · Doug DC983 · Fuselage, Seat/Cargo Attach Fittings > OKC - DURING HV CHECK, FOUND SEAT TRACK CHAFED AT FS 1212. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M) Next page: https://openairdocs.org/deregistered/N961AS-2010-05-04/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N961AS-2010-05-04/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.