# Service difficulty reports: N958AS, cancelled Nov 14, 2012

A list on [N958AS, cancelled Nov 14, 2012](https://openairdocs.org/deregistered/N958AS-2012-11-14.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 · 182 reports

- [SDR ASAA0882977](https://openairdocs.org/sdr/ASAA0882977.md): Doubler · corroded · May 21, 2008 · N958AS · Doug DC983 · Fuselage Main, Plate/Skin
  > FWD 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.
- [SDR ASAA0782085](https://openairdocs.org/sdr/ASAA0782085.md): Doubler · chafed · Oct 5, 2007 · N958AS · Doug DC983 · Trailing Edge Flaps
  > RIGHTHAND WING OUTBOARD FLAP INBOARD FIXED VANE L/E DOUBLER IS CHAFED. REPLACED EXISTING DOUBLER PER SRM 51-70-2.
- [SDR ASAA0782084](https://openairdocs.org/sdr/ASAA0782084.md): Vane · gouged · Oct 5, 2007 · N958AS · Doug DC983 · Trailing Edge Flaps
  > LEFTHAND WING OUTBOARD FLAP INBOARD VANE L/E DOUBLER REPAIR IS GOUGED. REPLACED EXISTING REPAIR DOUBLER PER SRM 51-70-2.
- [SDR ASAA0782083](https://openairdocs.org/sdr/ASAA0782083.md): Rib · damaged · Oct 5, 2007 · N958AS · Doug DC983 · Leading Edge Devices
  > LEFTHAND WING NR 5 L/E SLAT OUTBOARD RIB HOLES OVERSIZED. REPLACED WORN RIB PER SRM 51-10-4 AND 51-30-2.
- [SDR ASAA0782082](https://openairdocs.org/sdr/ASAA0782082.md): Attach Angle · cracked · Oct 5, 2007 · N958AS · Doug DC983 · Vertical Stabilizer, Attach Fittings
  > RIGHTHAND SIDE OF VERTICAL STABILIZER EXTERNAL VERTICAL TO FUSELAGE JOIN STRAP (ATTACH ANGLE) IS CRACKED. REPLACED DAMAGED SECTION OF JOIN STRAP PER SRM 53-05.
- [SDR ASAA0782081](https://openairdocs.org/sdr/ASAA0782081.md): Cusp Web · cracked · Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Miscellaneous Structure
  > CUSP WEB CRACKED. STOP DRILLED CRACK. INSTALLED REPAIR PARTS PER SRM 53-05.
- [SDR ASAA0782076](https://openairdocs.org/sdr/ASAA0782076.md): Track · corroded · Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Miscellaneous Structure
  > CABIN FLOOR FALSE TRACK IS CORRODED. REPLACED FALSE TRACK PER SRM 51-10-3, 51-10-4, 53-14-1 AND 51-30-5.
- [SDR ASAA0782075](https://openairdocs.org/sdr/ASAA0782075.md): Track · corroded · Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Miscellaneous Structure
  > CABIN FALSE TRACK IS CORRODED. REPLACED TRACK PER SRM 51-10-3, 51-10-4, 53-14-1, AND 51-30-5.
- [SDR ASAA0782074](https://openairdocs.org/sdr/ASAA0782074.md): Floor Panel · broken · Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAS DAMAGED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND DAC DWG S4932106.
- [SDR ASAA0782073](https://openairdocs.org/sdr/ASAA0782073.md): Floor Panel · broken · Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAS DAMAGED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND DAC DWG S4932106.
- [SDR ASAA0782072](https://openairdocs.org/sdr/ASAA0782072.md): Floor Panel · delaminated · Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.
- [SDR ASAA0782071](https://openairdocs.org/sdr/ASAA0782071.md): Floor Panel · broken · Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAS DAMAGED INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.
- [SDR ASAA0782070](https://openairdocs.org/sdr/ASAA0782070.md): Floor Panel · broken · Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAS BROKEN INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.
- [SDR ASAA0782069](https://openairdocs.org/sdr/ASAA0782069.md): Floor Panel · delaminated · Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05 AND DAC DWG S4932106.
- [SDR ASAA0782068](https://openairdocs.org/sdr/ASAA0782068.md): Floor Panel · broken · Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAS BROKEN INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.
- [SDR ASAA0782067](https://openairdocs.org/sdr/ASAA0782067.md): Floor Panel · broken · Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL CRACKED WITH DAMAGED INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.
- [SDR ASAA0782066](https://openairdocs.org/sdr/ASAA0782066.md): Floor Panel · delaminated · Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.
- [SDR ASAA0782065](https://openairdocs.org/sdr/ASAA0782065.md): Seat Track · corroded · Oct 5, 2007 · N958AS · Doug DC983 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK EXISTING REPAIR SPLICE CORRODED. REMOVED DAMAGED SECTION OF TRACK. INSTALLED REPLACEMENT PER SRM 51-10-4 AND 53-05.
- [SDR ASAA0782080](https://openairdocs.org/sdr/ASAA0782080.md): Longeron · cracked · Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Main, Longeron/Stringer
  > LONGERON CRACKED. REMOVED DAMAGED SECTION OF LONGERON. INSTALLED REPLACEMENT SECTION PER SRM 53-02 (SPLICE REPAIR).
- [SDR ASAA0782079](https://openairdocs.org/sdr/ASAA0782079.md): Frame · cracked · Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Main, Frame
  > FRAME CRACKED. REPLACED FRAME PER SRM 53-03.
- [SDR ASAA0782078](https://openairdocs.org/sdr/ASAA0782078.md): Stiffener · cracked · Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Miscellaneous Structure
  > FRAME STIFFENER CRACKED. REPLACED STIFFENER PER SRM 51-30-5, 51-30-2 AND DAC DWG 5913595.
- [SDR ASAA0782077](https://openairdocs.org/sdr/ASAA0782077.md): Shear Tie · cracked · Oct 5, 2007 · N958AS · Doug DC983 · Fuselage Internal Mounting Structure
  > SHEAR TIE IS CRACKED. REPLACED SHEAR TIE PER SRM 51-10-4, 51-30-2 AND 51-30-5.
- [SDR ASAA0781416](https://openairdocs.org/sdr/ASAA0781416.md): Frame · dented · Jan 19, 2007 · N958AS · Doug DC983 · Fuselage Main, Frame
  > NLG WHEELWELL LEFT FRAME JUST FORWARD OF LEFT INNER BULKHEAD WAS DENTED. REPLACE FRAME PER SRM 51 30 02.
- [SDR ASAA0681318](https://openairdocs.org/sdr/ASAA0681318.md): Window · stuck · Dec 9, 2006 · N958AS · Doug DC983 · Flight Compartment Windows
  > CAPTAIN SIDE SLIDING WINDOW WOULD NOT OPEN. ADJUSTED WINDOW CAM FOLLOWER. OP CHECKED OK.
- [SDR ASAA0681304](https://openairdocs.org/sdr/ASAA0681304.md): Engine · failed · Dec 6, 2006 · N958AS · Doug DC983 · Engine (Turbine/Turboprop)
  > EN 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
- [SDR ASAA0681217](https://openairdocs.org/sdr/ASAA0681217.md): Window · stuck · Nov 23, 2006 · N958AS · Doug DC983 · Flight Compartment Windows
  > DURING TAXI TO GATE, COCKPIT LEFT SLIDING WINDOW WOULD NOT OPEN. ADJUSTED UPPER CAM FOLLOWER.
- [SDR ASAA0681216](https://openairdocs.org/sdr/ASAA0681216.md): Window · stuck · Nov 22, 2006 · N958AS · Doug DC983 · Flight Compartment Windows
  > ON TAXI TO GATE, COCKPIT LEFT SLIDING WINDOW WOULD NOT OPEN. REALIGNED UPPER FORWARD GUIDE PIN.
- [SDR ASAA0680807](https://openairdocs.org/sdr/ASAA0680807.md): Skin · gouged · Jul 25, 2006 · N958AS · Doug DC983 · Trailing Edge Flaps
  > RIGHT 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.
- [SDR ASAA0680806](https://openairdocs.org/sdr/ASAA0680806.md): Skin · gouged · Jul 25, 2006 · N958AS · Doug DC983 · Trailing Edge Flaps
  > LEFT 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.
- [SDR ASAA0680805](https://openairdocs.org/sdr/ASAA0680805.md): Shear Tie · corroded · Jul 25, 2006 · N958AS · Doug DC983 · Fuselage Internal Mounting Structure
  > FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51 10 4 51 10 3 AND 51 30 5.
- [SDR ASAA0680790](https://openairdocs.org/sdr/ASAA0680790.md): Rib · gouged · Jul 20, 2006 · N958AS · Doug DC983 · Leading Edge Devices
  > THE 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 8
- [SDR ASAA0680789](https://openairdocs.org/sdr/ASAA0680789.md): Skin · misdrilled · Jul 20, 2006 · N958AS · Doug DC983 · Fuselage Main, Plate/Skin
  > FUSELAGE 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 AAR
- [SDR ASAA0680788](https://openairdocs.org/sdr/ASAA0680788.md): Shear Tie · corroded · Jul 20, 2006 · N958AS · Doug DC983 · Fuselage Internal Mounting Structure
  > SHEAR 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.
- [SDR ASAA0580253](https://openairdocs.org/sdr/ASAA0580253.md): Wire · loose · May 9, 2005 · N958AS · Doug DC983 · Emergency Lighting
  > ANC LINE CHECK, FOUND AFT EXIT CATWALK SIDE PANEL EMERGENCY LIGHT INOPERATIVE. RESECURED LOOSE WIRE CONNECTOR. LIGHT THEN OPERATED PROPERLY. (M)
- [SDR ASAA0580220](https://openairdocs.org/sdr/ASAA0580220.md): Skin · gouged · Apr 25, 2005 · N958AS · Doug DC983 · Trailing Edge Flaps
  > DURING C-CHECK FOUND, LT WING OUTBOARD FLAP INBOARD FLAP VANE LEADING EDGE GOUGED. REMOVED DAMAGE. INSTALLED REPAIR FILLER AND DOUBLER. (M)
- [SDR ASAA0580219](https://openairdocs.org/sdr/ASAA0580219.md): Skin · dented · Apr 25, 2005 · N958AS · Doug DC983 · Trailing Edge Flaps
  > DURING C-CHECK, FOUND RT WING INBOARD FLAP OUTBOARD FLAP VANE UPPER SURFACE DENTED. INSTALLED REPAIR DOUBLER. (M)
- [SDR ASAA0580218](https://openairdocs.org/sdr/ASAA0580218.md): Skin · gouged · Apr 25, 2005 · N958AS · Doug DC983 · Fuselage Main, Plate/Skin
  > FOUND DURING C-CHECK, FUSELAGE SKIN GOUGED. REMOVED DAMAGE. REPAINTED. (M)
- [SDR ASAA0580217](https://openairdocs.org/sdr/ASAA0580217.md): Skin · delaminated · Apr 25, 2005 · N958AS · Doug DC983 · Trailing Edge Flaps
  > FOUND DURING C-CHECK, LT WING INBOARD FLAP VANE OUTBOARD SEGMENT DELAMINATED. REMOVED DAMAGE. INSTALLED REPAIR FILLERS AND DOUBLERS. (M)
- [SDR ASAA0580216](https://openairdocs.org/sdr/ASAA0580216.md): Rib · cracked · Apr 25, 2005 · N958AS · Doug DC983 · Leading Edge Devices
  > DURING C-CHECK, FOUND LT WING NR 4 SLAT ACCESS CUTOUT RIB CRACKED. INSTALLED REPAIR DOUBLER PER EA 5740-01447. (M)
- [SDR ASAA0580213](https://openairdocs.org/sdr/ASAA0580213.md): Skin · dented · Apr 20, 2005 · N958AS · Doug DC983 · Elevator, Plate/Skin
  > FOUND DURING C-CHECK, LT ELEVATOR ANTI-FLOAT TAB UPPER SURFACE DENTED. INSTALLED REPAIR DOUBLERS. (M)
- [SDR ASAA0580212](https://openairdocs.org/sdr/ASAA0580212.md): Cusp Web · corroded · Apr 20, 2005 · N958AS · Doug DC983 · Fuselage Floor Panel
  > DURING C-CHECK, FOUND CABIN FLOOR PANEL CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (M)
- [SDR ASAA0580211](https://openairdocs.org/sdr/ASAA0580211.md): Skin · corroded · Apr 20, 2005 · N958AS · Doug DC983 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FOUND FUSELAGE SKIN CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M)
- [SDR ASAA0480146](https://openairdocs.org/sdr/ASAA0480146.md): Module · inoperative · Mar 1, 2004 · N958AS · Doug DC983 · Emergency Lighting
  > SEA - PREFILGHT CHECK, FOUND FIRST FIVE EMERGENCY TRACK LIGHTS TESTS INOPERATIVE, TWICE. RECONNECTED MODULE CONNECTOR, TWICE. LIGHTS THEN OPERATED PROPERLY. (M)
- [SDR ASAA0480059](https://openairdocs.org/sdr/ASAA0480059.md): Web · corroded · Jan 30, 2004 · N958AS · Doug DC983 · Fuselage Miscellaneous Structure
  > OKC - DURING 15K CHECK, FOUND WEB IS CORRODED AT LONGERON 18L NEAR L2 DOOR. REMOVED CORROSION. INSTALLED FILLER AND DOUBLER PER SRM 53-01. (M)
- [SDR ASAA0480057](https://openairdocs.org/sdr/ASAA0480057.md): Tab · dented · Jan 30, 2004 · N958AS · Doug DC983 · Empennage Structure
  > OKC - DURING 15K CHECK, FOUND LEFT ANTI-FLOAT TAB UPPER SURFACE IS DENTED. APPLIED FILLER PER SRM 55-04. (M)
- [SDR ASAA0480062](https://openairdocs.org/sdr/ASAA0480062.md): Seat Track · corroded · Jan 30, 2004 · N958AS · Doug DC983 · Fuselage, Seat/Cargo Attach Fittings
  > OKC - DURING 15K CHECK, FOUND RIGHT INBOARD SEAT TRACK IS CORRODED AT FS 200-247. REPLACED SEAT TRACK PER SRM 53-05. (M)
- [SDR ASAA0480060](https://openairdocs.org/sdr/ASAA0480060.md): Seat Track · corroded · Jan 30, 2004 · N958AS · Doug DC983 · Fuselage, Seat/Cargo Attach Fittings
  > OKC - 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)
- [SDR ASAA0480056](https://openairdocs.org/sdr/ASAA0480056.md): Skin · dented · Jan 30, 2004 · N958AS · Doug DC983 · Fuselage Main, Plate/Skin
  > OKC - DURNG 15K CHECK, FOUND FUSELAGE SKIN IS DENTED AT FS 237. INSTALLED DOUBLER PER SRM 53-04. (M)
- [SDR ASAA0480055](https://openairdocs.org/sdr/ASAA0480055.md): Skin · gouged · Jan 30, 2004 · N958AS · Doug DC983 · Fuselage Main, Plate/Skin
  > OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN IS GOUGED AT STATION 235. REMOVED DAMAGED SECTION. REPAIRED WITH FILLER AND DOUBLER PER SRM 53-04. (M)
- [SDR ASAA0480054](https://openairdocs.org/sdr/ASAA0480054.md): Stringer · corroded · Jan 30, 2004 · N958AS · Doug DC983 · Fuselage Main, Longeron/Stringer
  > OKC - 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)

Next page: https://openairdocs.org/deregistered/N958AS-2012-11-14/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 = 'N958AS' AND deregistration_id = 'N958AS-2012-11-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N958AS-2012-11-14/reports

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