# Service difficulty reports: N960AS, cancelled May 4, 2010

A list on [N960AS, cancelled May 4, 2010](https://openairdocs.org/deregistered/N960AS-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 · 169 reports

- [SDR ASAA0782349](https://openairdocs.org/sdr/ASAA0782349.md): Skin · damaged · Dec 3, 2007 · N960AS · Doug DC983 · Fuselage Main, Plate/Skin
  > DENT IN FUSELAGE APPROX 4' FROM L1 DOOR AND 2' BELOW WINDOW BELT REMOVED DAMAGED AREA OF SKIN. FABRICATED AND INSTALLED REPAIR SECTION OF SKIN FINGER DOUBLERS SKIN SPLICE STRAP STRAPS IAW MD80 SRM 53 04 FIG 12C.
- [SDR ASAA0781923](https://openairdocs.org/sdr/ASAA0781923.md): Floor Panel · delaminated · Jul 30, 2007 · N960AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL TOP PLY IS DISBONDED. BOND REPAIR PANEL WITH GLASS CLOTH PER SRM 51-90-0.
- [SDR ASAA0781922](https://openairdocs.org/sdr/ASAA0781922.md): Floor Panel · delaminated · Jul 30, 2007 · N960AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL TOP PLY IS DISBONDED. BOND REPAIR WITH GLASS CLOTH PER SRM 51-90-0.
- [SDR ASAA0781921](https://openairdocs.org/sdr/ASAA0781921.md): Floor Panel · delaminated · Jul 30, 2007 · N960AS · Doug DC983 · Fuselage Floor Panel
  > FLOOR PANEL TOP PLY DISBONDED. BOND REPAIRED PANEL WITH GLASS CLOTH PER SRM 51-90-0.
- [SDR ASAA0781920](https://openairdocs.org/sdr/ASAA0781920.md): Floor Panel · delaminated · Jul 30, 2007 · N960AS · Doug DC983 · Fuselage Floor Panel
  > FLOOR PANEL TOP PLY DISBONDED. BOND REPAIRED WITH GLASS CLOTH PER SRM 51-90-0.
- [SDR ASAA0781919](https://openairdocs.org/sdr/ASAA0781919.md): Floor Panel · delaminated · Jul 30, 2007 · N960AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL TOP PLY PULLED LOOSE. BOND REPAIRED WITH GLASS CLOTH PER SRM 51-90-0.
- [SDR ASAA0781918](https://openairdocs.org/sdr/ASAA0781918.md): Insert · corroded · Jul 30, 2007 · N960AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAS CORRODED INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.
- [SDR ASAA0781917](https://openairdocs.org/sdr/ASAA0781917.md): Insert · corroded · Jul 30, 2007 · N960AS · Doug DC983 · Fuselage Floor Panel
  > FLOOR PANEL HAS CORRODED INSERTS. REPLACED PANEL PER SRM 53-24-0 AND 53-05.
- [SDR ASAA0781916](https://openairdocs.org/sdr/ASAA0781916.md): Insert · damaged · Jul 30, 2007 · N960AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAS CORRODED AND BROKEN INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.
- [SDR ASAA0781915](https://openairdocs.org/sdr/ASAA0781915.md): Insert · damaged · Jul 30, 2007 · N960AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAS BROKEN AND CORRODED INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.
- [SDR ASAA0781913](https://openairdocs.org/sdr/ASAA0781913.md): Vane · chafed · Jul 26, 2007 · N960AS · Doug DC983 · Leading Edge Devices
  > LEFTHAND WING OUTBOARD FLAP INBOARD VANE TRAILING EDGE IS CHAFED. REPAIRED DAMAGED AREA WITH BONDED FILLER AND DOUBLER PER SRM 51-70-2.
- [SDR ASAA0781912](https://openairdocs.org/sdr/ASAA0781912.md): Skin · dented · Jul 26, 2007 · N960AS · Doug DC983 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED. REPAIRED PER SRM 53-04.
- [SDR ASAA0781909](https://openairdocs.org/sdr/ASAA0781909.md): Skin · dented · Jul 26, 2007 · N960AS · Doug DC983 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED AT PREVIOUS REPAIR. REPLACED DAMAGED SECTION AND PREVIOUS REPAIR DOUBLER PER SRM 53-04.
- [SDR ASAA0781908](https://openairdocs.org/sdr/ASAA0781908.md): Skin · damaged · Jul 26, 2007 · N960AS · Doug DC983 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CREASED AT PRIOR REPAIR. REMOVED EXISTING REPAIR DOUBLER RECONTOURED SKIN AND INSTALLED REPLACEMENT DOUBLER PER SRM 53-04.
- [SDR ASAA0781907](https://openairdocs.org/sdr/ASAA0781907.md): Floor Panel · delaminated · Jul 26, 2007 · N960AS · Doug DC983 · Fuselage Miscellaneous Structure
  > CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND DAC DWG 9936640.
- [SDR ASAA0781906](https://openairdocs.org/sdr/ASAA0781906.md): Floor Panel · delaminated · Jul 26, 2007 · N960AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND DAC DWG 9936640.
- [SDR ASAA0781905](https://openairdocs.org/sdr/ASAA0781905.md): Floor Panel · delaminated · Jul 26, 2007 · N960AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.
- [SDR ASAA0781904](https://openairdocs.org/sdr/ASAA0781904.md): Floor Panel · delaminated · Jul 26, 2007 · N960AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-24-0 AND 53-05.
- [SDR ASAA0781903](https://openairdocs.org/sdr/ASAA0781903.md): Floor Panel · delaminated · Jul 26, 2007 · N960AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-24-0 AND 53-05.
- [SDR ASAA0781902](https://openairdocs.org/sdr/ASAA0781902.md): Floor Panel · delaminated · Jul 26, 2007 · N960AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-24-0 AND 53-05.
- [SDR ASAA0781899](https://openairdocs.org/sdr/ASAA0781899.md): Floor Panel · delaminated · Jul 26, 2007 · N960AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-24-0 AND 53-5.
- [SDR ASAA0781898](https://openairdocs.org/sdr/ASAA0781898.md): Web · corroded · Jul 26, 2007 · N960AS · Doug DC983 · Fuselage Miscellaneous Structure
  > CABIN FLOOR MEMBRANE CORRODED. CUT OUT DAMAGED AREA AND INSTALLED REPLACEMENT WEB PER SRM 51-70-4 AND 51-30-2.
- [SDR ASAA0781911](https://openairdocs.org/sdr/ASAA0781911.md): Cusp Web · cracked · Jul 26, 2007 · N960AS · Doug DC983 · Fuselage Miscellaneous Structure
  > CUSP WEB CRACKED. REPLACED WEB PER SRM 51-10-4 AMD 51-30-2.
- [SDR ASAA0781910](https://openairdocs.org/sdr/ASAA0781910.md): Skin · dented · Jul 26, 2007 · N960AS · Doug DC983 · Passenger/Crew Doors
  > FORWARD ENTRY DOOR IS DENTED. RECONTOURED DOOR SKIN AND INSTALLED INTERNAL DOUBLER PER SRM 53-04.
- [SDR ASAA0680488](https://openairdocs.org/sdr/ASAA0680488.md): Skin · dented · Apr 25, 2006 · N960AS · Doug DC983 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN DENTED. COLD WORKED DAMAGED SECTION. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53 04.
- [SDR ASAA0680487](https://openairdocs.org/sdr/ASAA0680487.md): Skin · corroded · Apr 25, 2006 · N960AS · Doug DC983 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN CORRODED. REPLACED DAMAGED SECTION BY INSTALLING REPAIR DOUBLER PER SRM 53 04.
- [SDR ASAA0680485](https://openairdocs.org/sdr/ASAA0680485.md): Cusp Web · corroded · Apr 25, 2006 · N960AS · Doug DC983 · Fuselage Miscellaneous Structure
  > FOUND CUSP WEB CORRODED. REPLACED DAMAGED SECTION BY INSTALLING REPAIR DOUBLER PER SRM 51 70 4.
- [SDR ASAA0680484](https://openairdocs.org/sdr/ASAA0680484.md): Cusp Web · corroded · Apr 25, 2006 · N960AS · Doug DC983 · Fuselage Miscellaneous Structure
  > FOUND CUSP WEB CORRODED. REPLACED DAMAGED SECTION BY INSTALLING REPAIR DOUBLER PER SRM 53 05 FIG 96 AND 51 01 PARA 3 B.
- [SDR ASAA0680476](https://openairdocs.org/sdr/ASAA0680476.md): Web · corroded · Apr 25, 2006 · N960AS · Doug DC983 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY THRESHOLD WEB CORRODED. REPLACED WEB PER SRM 51 10 4 51 30 2 AND 51 30 5.
- [SDR ASAA0680473](https://openairdocs.org/sdr/ASAA0680473.md): Beam · corroded · Apr 25, 2006 · N960AS · Doug DC983 · Fuselage Main, Structure
  > AFT CARGO DOOR CUTOUT LOWER BEAM CORRODED ON LOWER OUTBOARD FLANGE. REPLACED BEAM PER SRM 51 10 4 AND 51 30 5.
- [SDR ASAA0680486](https://openairdocs.org/sdr/ASAA0680486.md): Shear Tie · corroded · Apr 25, 2006 · N960AS · Doug DC983 · Fuselage Internal Mounting Structure
  > FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51 10 4 51 30 2 AND 51 30 5.
- [SDR ASAA0680483](https://openairdocs.org/sdr/ASAA0680483.md): Intercostal · corroded · Apr 25, 2006 · N960AS · Doug DC983 · Fuselage Miscellaneous Structure
  > FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 51 10 4 AND 51 30 5.
- [SDR ASAA0680482](https://openairdocs.org/sdr/ASAA0680482.md): Shear Tie · corroded · Apr 25, 2006 · N960AS · Doug DC983 · Fuselage Internal Mounting Structure
  > FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51 10 4 AND 51 30 5.
- [SDR ASAA0680480](https://openairdocs.org/sdr/ASAA0680480.md): Frame · corroded · Apr 25, 2006 · N960AS · Doug DC983 · Fuselage Main, Frame
  > FOUND FRAME CORRODED. REPLACED DAMAGED SECTION OF FRAME BY INSTALLING FOUR REPAIR ANGLES AND FOUR SPLICE PLATES PER SRM 53 03 FIG 2A.
- [SDR ASAA0680479](https://openairdocs.org/sdr/ASAA0680479.md): Intercostal · corroded · Apr 25, 2006 · N960AS · Doug DC983 · Fuselage Miscellaneous Structure
  > FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 51 10 4 AND 51 30 2.
- [SDR ASAA0680478](https://openairdocs.org/sdr/ASAA0680478.md): Intercostal · cracked · Apr 25, 2006 · N960AS · Doug DC983 · Fuselage Miscellaneous Structure
  > FOUND INTERCOSTAL CRACKED. REPLACED INTERCOSTAL PER SRM 51 10 4 51 30 2 AND 51 30 5.
- [SDR ASAA0680477](https://openairdocs.org/sdr/ASAA0680477.md): Longeron · corroded · Apr 25, 2006 · N960AS · Doug DC983 · Fuselage Main, Longeron/Stringer
  > FOUND LONGERON CORRODED. REPLACED DAMAGED SECTION OF LONGERON PER SRM 51 10 4 51 30 2 AND 51 30 5.
- [SDR ASAA0680475](https://openairdocs.org/sdr/ASAA0680475.md): Intercostal · corroded · Apr 25, 2006 · N960AS · Doug DC983 · Fuselage Miscellaneous Structure
  > FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 51 10 4 AND 51 30 5.
- [SDR ASAA0680474](https://openairdocs.org/sdr/ASAA0680474.md): Shear Tie · corroded · Apr 25, 2006 · N960AS · Doug DC983 · Fuselage Internal Mounting Structure
  > FOUND FRAME SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51 10 04 AND 51 30 5.
- [SDR ASAA0680481](https://openairdocs.org/sdr/ASAA0680481.md): Skin · damaged · Apr 25, 2006 · N960AS · Doug DC983 · Cargo/Baggage Doors
  > AFT CARGO DOOR DENTED ON UPPER HALF. REPLACED DAMAGED SECTION OF DOOR SKIN BY INSTALLING EXTERNAL SPLICE PLATE AND TWO FINGER DOUBLERS PER ALASKA AIR EA 5230 01312.
- [SDR ASAA0580385](https://openairdocs.org/sdr/ASAA0580385.md): Wire · loose · Jul 16, 2005 · N960AS · Doug DC983 · Light System Wiring
  > SEA LINE CHECK, AFT EXIT, CATWALK, PATH EMERGENCY LIGHT INOPERATIVE. RESECURED LOOSE WIRE CONNECTOR AND REPLACED LIGHT. LIGHT THEN OPERATED PROPERLY. (M)
- [SDR ASAA0580090](https://openairdocs.org/sdr/ASAA0580090.md): Skin · delaminated · Feb 7, 2005 · N960AS · Doug DC983 · Rudder, Plate/Skin
  > OKC - DURING C-CHECK, FOUND RUDDER T/E IS DELAMINATED. FIBERGLASS BOND REPAIRED. (M)
- [SDR ASAA0580089](https://openairdocs.org/sdr/ASAA0580089.md): Panel · chafed · Feb 7, 2005 · N960AS · Doug DC983 · Vertical Stabilizer, Plate/Skin
  > OKC - DURING C-CHECK, VERTICAL STABILIZER PANEL 6308C IS CHAFED. REPLACED PANEL. (M)
- [SDR ASAA0580088](https://openairdocs.org/sdr/ASAA0580088.md): Rib · cracked · Feb 7, 2005 · N960AS · Doug DC983 · Wing, Rib/Bulkhead
  > OKC - FOUND C-CHECK, RIGHT WING L/E HAS CRACKED RIB. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLER. (M)
- [SDR ASAA0580087](https://openairdocs.org/sdr/ASAA0580087.md): Structure · chafed · Feb 7, 2005 · N960AS · Doug DC983 · Cargo/Baggage Doors
  > OKC - DURING C-CHECK, FORWARD CARGO BAY DOOR FORWARD AND AFT LOWER EDGES CHAFED. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER. (M)
- [SDR ASAA0580086](https://openairdocs.org/sdr/ASAA0580086.md): Skin · dented · Feb 7, 2005 · N960AS · Doug DC983 · Fuselage Main, Plate/Skin
  > OKC - DURING C-CHECK, FOUND FUSELAGE DENTED NEAR RIGHT ENGINE COWL DRAIN MAST. COLD WORKED AND INSTALLED REPAIR DOUBLER. (M)
- [SDR ASAA0580084](https://openairdocs.org/sdr/ASAA0580084.md): Floor Panel · damaged · Feb 7, 2005 · N960AS · Doug DC983 · Fuselage Floor Panel
  > OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD PANEL IS FRAYING. FIBERGLASS OVERLAY REPAIRED. (M)
- [SDR ASAA0580085](https://openairdocs.org/sdr/ASAA0580085.md): Floor Panel · frayed · Feb 7, 2005 · N960AS · Doug DC983 · Fuselage Floor Panel
  > OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD PANEL IS FRAYING. FIBERGLASS OVERLAY REPAIRED. (M)
- [SDR ASAA0580083](https://openairdocs.org/sdr/ASAA0580083.md): Floor Panel · frayed · Feb 7, 2005 · N960AS · Doug DC983 · Fuselage Floor Panel
  > OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD PANEL IS FRAYING. FIBERGLASS OVERLAY REPAIRED. (M)
- [SDR ASAA0480363](https://openairdocs.org/sdr/ASAA0480363.md): Module · inoperative · Apr 30, 2004 · N960AS · Doug DC983 · Emergency Lighting
  > LAX - DURING PREFLIGHT CHECK, FOUND SEVERAL EMERGENCY TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED LOOSE MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Next page: https://openairdocs.org/deregistered/N960AS-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 = 'N960AS' AND deregistration_id = 'N960AS-2010-05-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N960AS-2010-05-04/reports

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