# Service difficulty reports: N968AS, cancelled May 28, 2009

A list on [N968AS, cancelled May 28, 2009](https://openairdocs.org/deregistered/N968AS-2009-05-28.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 5 · 237 reports

- [SDR ASAA0883402](https://openairdocs.org/sdr/ASAA0883402.md): Door · stiff · Aug 22, 2008 · N968AS · Doug DC983 · Passenger/Crew Doors
  > F/A REPORTS L1 DOOR DIFFICULT TO OPEN AND CLOSE. CHECK DOOR ADJUSTMENT, FOUND TO BE WITHIN LIMITS PER MM 52 11 00.
- [SDR ASAA0782144](https://openairdocs.org/sdr/ASAA0782144.md): Vane · chafed · Oct 23, 2007 · N968AS · Doug DC983 · Trailing Edge Flaps
  > RIGHT WING O/B FLAP I/B VANE REPAIR DOUBLER IS CHAFED AT I/B CORNER. REMOVED PREVIOUS REPAIR DOUBLER, PREPARED AND FABRICATED REPAIR DOUBLER, LOADED AND INSTALLED FASTENERS IAW MD80 SRM 51-70-2 PG 11 PAR 6 23 59.
- [SDR ASAA0782146](https://openairdocs.org/sdr/ASAA0782146.md): Floor Panel · broken · Oct 23, 2007 · N968AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL STA 200 TO STA 256 LBL16 TO RBL 22 PULLED OUT AND DAMAGED BROKEN INSERTS. FABRICATED AND INSTALLED A REPLACEMENT CABIN FLOOR PANEL IAW MD80 53 05 PGS 251, 257 AND DAC DRAWING S4932106.
- [SDR ASAA0782142](https://openairdocs.org/sdr/ASAA0782142.md): Floor Panel · corroded · Oct 22, 2007 · N968AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL STA 160 TO STA 195 LBL 8 TO LBL 44 BROKEN AND CORRODED INSERTS. FABRICATED AND INSTALLED A REPLACEMENT CABIN FLOOR PANEL IAW MD80 SRM 53-05 PAR 59 AND DAC DRAWING S 4932106.
- [SDR ASAA0782140](https://openairdocs.org/sdr/ASAA0782140.md): Floor Panel · corroded · Oct 22, 2007 · N968AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOORBOARD STA 160 TO STA 180 RBL 8 TO RBL 44 CORRODED. INSERTS FABRICATED AND INSTALLED A REPLACEMENT CABIN FLOOR PANEL IAW MD80 SRM 53-05 PAR 59 AND DAC DRAWING S4932106.
- [SDR ASAA0782139](https://openairdocs.org/sdr/ASAA0782139.md): Floor Panel · punctured · Oct 22, 2007 · N968AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL STA 1117 TO STA 1174 BL 0 TO LBL 22 PUNCTURED. FABRICATED AND INSTALLED A REPLACEMENT CABIN FLOOR PANEL IAW MD80 SRM 53-05 PAR 59 AND DAC DWG S4932106.
- [SDR ASAA0782138](https://openairdocs.org/sdr/ASAA0782138.md): Floor Panel · punctured · Oct 22, 2007 · N968AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL STA 1117 TO STA 1174 BL 0 TO RBL 22. PUNCTURED, FABRICATED AND INSTALLED A REPLACEMENT FLOOR PANEL IAW MD 80 SRM 53-05 PAR 59 AND DAC DRAWING S4932106.
- [SDR ASAA0782137](https://openairdocs.org/sdr/ASAA0782137.md): Floor Panel · punctured · Oct 22, 2007 · N968AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL STA 1174 TO STA 1250 LBL 22 TO RBL 22. PUNCTURED, FABRICATED AND INSTALLED A REPLACEMENT CABIN FLOOR PANEL IAW MD80 SRM 53-05 PAR 59 AND DAC DRAWING S4932106.
- [SDR ASAA0782136](https://openairdocs.org/sdr/ASAA0782136.md): Floor Panel · punctured · Oct 22, 2007 · N968AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL STA 1097 TO STA 1117 LBL 22 TO RBL 22 PUNCTURED. FABRICATED AND INSTALLED A REPLACEMENT CABIN FLOOR PANEL IAW MD80 SRM 53-05 PAR 59 AND DAC DRAWING S4932106.
- [SDR ASAA0782135](https://openairdocs.org/sdr/ASAA0782135.md): Floor Panel · corroded · Oct 22, 2007 · N968AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL CORRODED AND BROKEN INSERTS STA 196 TO STA 256 LBL 16 TO LBL 22. FABRICATED AND INSTALLED A REPLACEMENT CABIN FLOOR PANEL IAW MD 80 SRM 53-05 PAR 59 AND DAC DRAWING S4932106.
- [SDR ASAA0782133](https://openairdocs.org/sdr/ASAA0782133.md): Seat Track · corroded · Oct 22, 2007 · N968AS · Doug DC983 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK CORRODED STA 1211 TO 1130 LBL 44. REMOVED DAMAGED SEAT TRACK, LOCATED, DRILLED AND INSTALLED A REPLACEMENT SEAT TRACK AND SPLICES IAW MD 80 SRM 53-05 FIG 4B 1 AND FIG 4 F.
- [SDR ASAA0782132](https://openairdocs.org/sdr/ASAA0782132.md): Seat Track · corroded · Oct 22, 2007 · N968AS · Doug DC983 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK CORRODED TOP AND BOTTOM STA 1042 TO STA 1231 AT LBL 22. REMOVED DAMAGED SEAT TRACK, LOCATED, DRILLED AND INSTALLED A REPLACEMENT SEAT TRACK AND SPLICE DOUBLERS IAW MD80 SRM 51-10-4 PGS 1 AND 2, 53-05 FIG 4F SHTS 1 & 2.
- [SDR ASAA0782134](https://openairdocs.org/sdr/ASAA0782134.md): Intercostal · corroded · Oct 22, 2007 · N968AS · Doug DC983 · Fuselage Miscellaneous Structure
  > INTERCOSTAL UPPER FLANGS EXFOILATED STA 228 AT LBL 34. REMOVED DAMAGED INTERCOSTAL, LOCATED DRILLED AND INSTALLED A REPLACEMENT INTERCOSTAL AND REPAIR PARTS FOR WIRE FEED THRU IAW MD80 SRM 51-30-5 PG 1, 53-01 FIG 2 PG 13.
- [SDR ASAA0782131](https://openairdocs.org/sdr/ASAA0782131.md): Vane · gouged · Oct 22, 2007 · N968AS · Doug DC983 · Trailing Edge Flaps
  > LEFT WING O/B FLAP I/B VANE GOUGED ON L/E AREA MARKED. REMOVED PREVIOUS REPAIR DOUBLER, PREPARED AREA, FABRICATED REPAIR DOUBLER BONDED AND INSTALLED FASTENERS IAW MD 80 SRM 51-70-2 PG 11 23 PAR 10C PG 32 AND PAR 18B PG 91.
- [SDR ASAA0782129](https://openairdocs.org/sdr/ASAA0782129.md): Vane · dented · Oct 22, 2007 · N968AS · Doug DC983 · Trailing Edge Flaps
  > RIGHT WING I/B FLAP I/B VANE LWR SURFACE HAS GRAVEL DAMAGE (DENTED). PREPARED DAMAGED AREA, FABRICATED FILLER AND REPAIR DOUBLER BONDED AND INSTALLED FASTENERS IAW MD80 SRM 51-70-2 PGS 23, 43, 46, 59, 63 AND 64.
- [SDR ASAA0782127](https://openairdocs.org/sdr/ASAA0782127.md): Vane · delaminated · Oct 21, 2007 · N968AS · Doug DC983 · Trailing Edge Flaps
  > LEFT INBOARD FLAP OUTBOARD FLAP VANE DELAMINATED ON UPPER SURFACE 53 INCHES FROM OUTBOARD END. PREPARED DAMAGED AREA, FABRICATED FILLER AND DOUBLER REPAIR PARTS, LOADED AND INSTALLED FASTENERS IAW MD 80 SRM 51-70-2 PAT 18B PGS 91 95.
- [SDR ASAA0782106](https://openairdocs.org/sdr/ASAA0782106.md): Skin · dented · Oct 16, 2007 · N968AS · Doug DC983 · Fuselage Main, Plate/Skin
  > LEFT EXT FUSELAGE SKIN AFT OF L1 DOOR DENT OUT OF LIMITS STA 213 ABOVE LONG 166 DIA =.800 DEPTH =.034 RATIO OF 23.52 RECON TOURED DENT YAW MD80 SUM 53 04 FIG 38. HEFT INSPECTED, NO CRACKS NOTED YAW MD80 SUM 53 04 FIG 38 AND NUDISM PT 6.06 10 00 001. FABRIC
- [SDR ASAA0782102](https://openairdocs.org/sdr/ASAA0782102.md): Cusp Web · corroded · Oct 14, 2007 · N968AS · Doug DC983 · Fuselage Miscellaneous Structure
  > RIGHT CUSP WEB CORRODED STA 1212 TO STR 1231. REMOVED, CUT OUT DAMAGED AREA OF CUSP WEB, FABRICATED DOUBLER, LOCATED DRILLED AND INSTALLED DOUBLER REPAIR IAW MD80 SRM 53-05 PG 563 FIG 96.
- [SDR ASAA0782103](https://openairdocs.org/sdr/ASAA0782103.md): Floor Support · damaged · Oct 14, 2007 · N968AS · Doug DC983 · Fuselage Miscellaneous Structure
  > REMOVED DAMAGED CABIN FLOOR TRACK, LOCATED, DRILLED AND INSTALLED A REPLACEMENT TRACK IAW MD80 SRM 51-10-4 PG 1.
- [SDR ASAA0781748](https://openairdocs.org/sdr/ASAA0781748.md): Longeron · cracked · May 26, 2007 · N968AS · Doug DC983 · Fuselage Main, Longeron/Stringer
  > LONGERON CRACKED. CUT OUT DAMAGED AREA. INSTALLED REPLACEMENT SECTION WITH LONGERON SPLICES PER SRM 51-10-4 AND SRM 53-02.
- [SDR ASAA0781747](https://openairdocs.org/sdr/ASAA0781747.md): Skin · dented · May 26, 2007 · N968AS · Doug DC983 · Fuselage Main, Plate/Skin
  > FUSELAGE DENTED BEYOND SRM 53-4 LIMITS. CUT OUT DAMAGED AREA OF SKIN. INSTALLED FILLERS FINGER DOUBLERS AND REPAIR DOUBLER PER SRM 53-4 AND SRM 51-10-3.
- [SDR ASAA0781568](https://openairdocs.org/sdr/ASAA0781568.md): Skin · scratched · Mar 27, 2007 · N968AS · Doug DC983 · Fuselage Main, Plate/Skin
  > LARGE SCRATCHES ON LEFT FUSELAGE. REMOVED DAMAGED AREA. INSTALLED TWO EXTERNAL REPAIR DOUBLERS PER SRM 53-4.
- [SDR ASAA0781386](https://openairdocs.org/sdr/ASAA0781386.md): Skin · damaged · Jan 11, 2007 · N968AS · Doug DC983 · Passenger/Crew Doors
  > L1 DOOR SKIN AT UPPER CORNER PEELED BACK. REMOVED DAMAGED SECTION OF SKIN. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 52 05. PERFORMED CLASS III REPAIR PER SRM 53 04.
- [SDR ASAA0681060](https://openairdocs.org/sdr/ASAA0681060.md): Skin · corroded · Sep 28, 2006 · N968AS · Doug DC983 · Fuselage Main, Plate/Skin
  > FUSELAGE CORRODED AFT OF LAV SERVICE PANEL. REPAIRED PER EA 5330 02145.
- [SDR ASAA0680898](https://openairdocs.org/sdr/ASAA0680898.md): Skin · gouged · Aug 16, 2006 · N968AS · Doug DC983 · Trailing Edge Flaps
  > LEFT INBOARD FLAP OUTBOARD VANE L/E GOUGED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51-70-2.
- [SDR ASAA0680897](https://openairdocs.org/sdr/ASAA0680897.md): Skin · dented · Aug 16, 2006 · N968AS · Doug DC983 · Trailing Edge Flaps
  > RIGHTHAND OUTBOARD FLAP INBOARD VANE DENTED. REMOVED DAMAGED AREA. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51-70-2.
- [SDR ASAA0680896](https://openairdocs.org/sdr/ASAA0680896.md): Skin · dented · Aug 16, 2006 · N968AS · Doug DC983 · Trailing Edge Flaps
  > LEFTHAND INBOARD FLAP OUTBOARD VANE IS DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 51-70-2.
- [SDR ASAA0680895](https://openairdocs.org/sdr/ASAA0680895.md): Skin · gouged · Aug 16, 2006 · N968AS · Doug DC983 · Trailing Edge Flaps
  > LEFTHAND INBOARD FLAP OUTBOARD VANE IS GOUGED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51-70-2.
- [SDR ASAA0680894](https://openairdocs.org/sdr/ASAA0680894.md): Skin · dented · Aug 16, 2006 · N968AS · Doug DC983 · Trailing Edge Flaps
  > RIGHTHAND OUTBOARD FLAP INBOARD VANE DENTED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51-70-2.
- [SDR ASAA0680893](https://openairdocs.org/sdr/ASAA0680893.md): Skin · dented · Aug 16, 2006 · N968AS · Doug DC983 · Trailing Edge Flaps
  > RIGHTHAND OUTBOARD FLAP VANE DENTED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51-70-2.
- [SDR ASAA0680892](https://openairdocs.org/sdr/ASAA0680892.md): Skin · gouged · Aug 16, 2006 · N968AS · Doug DC983 · Trailing Edge Flaps
  > LEFTHAND OUTBOARD FLAP VANE L/E GOUGED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51-70-2.
- [SDR ASAA0680891](https://openairdocs.org/sdr/ASAA0680891.md): Skin · dented · Aug 16, 2006 · N968AS · Doug DC983 · Trailing Edge Flaps
  > LEFTHAND INBOARD FLAP OUTBOARD VANE IS DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-70-2.
- [SDR ASAA0680889](https://openairdocs.org/sdr/ASAA0680889.md): Tab · dented · Aug 15, 2006 · N968AS · Doug DC983 · Elevator, Tab Structure
  > RIGHT HAND ELEVATOR GEAR TAB UPPER SURFACE DENTED. BONDED DENTED AREA PER SRM 51-70-2.
- [SDR ASAA0680888](https://openairdocs.org/sdr/ASAA0680888.md): Tab · cracked · Aug 15, 2006 · N968AS · Doug DC983 · Elevator, Tab Structure
  > RIGHT HAND ELEVATOR CONTROL TAB EDGE CRACKED. INSTALLED REPAIR DOUBLER PER SRM 51-70-2.
- [SDR ASAA0680887](https://openairdocs.org/sdr/ASAA0680887.md): Tab · dented · Aug 15, 2006 · N968AS · Doug DC983 · Elevator, Tab Structure
  > LEFT ELEVATOR CONTROL TAB UPPER SURFACE DENTED. FILLED DENT PER SRM 55 04.
- [SDR ASAA0680885](https://openairdocs.org/sdr/ASAA0680885.md): Tab · dented · Aug 15, 2006 · N968AS · Doug DC983 · Elevator Structure
  > FOUND LEFT ELEVATOR CONTROL TAB LOWER SURFACE DENTED. FILLED DENT PER SRM 55 04.
- [SDR ASAA0680884](https://openairdocs.org/sdr/ASAA0680884.md): Skin · gouged · Aug 15, 2006 · N968AS · Doug DC983 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN REPAIR DOUBLER GOUGED. REPLACED DOUBLER PER SRM 53 04.
- [SDR ASAA0680883](https://openairdocs.org/sdr/ASAA0680883.md): Splice · corroded · Aug 15, 2006 · N968AS · Doug DC983 · Fuselage Miscellaneous Structure
  > FOUND FORWARD CARGO DOOR JAMB SPLACE CORRODED. REPLACED SPLICE PER SRM 51 10 3 AND 51 30 5.
- [SDR ASAA0680882](https://openairdocs.org/sdr/ASAA0680882.md): Shear Tie · corroded · Aug 15, 2006 · N968AS · Doug DC983 · Fuselage Internal Mounting Structure
  > FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51 30 5.
- [SDR ASAA0680881](https://openairdocs.org/sdr/ASAA0680881.md): Support · cracked · Aug 15, 2006 · N968AS · Doug DC983 · Fuselage Miscellaneous Structure
  > FOUND FRAME SUPPORT CRACKED. REPLACED SUPPORT PER SRM 51 30 5.
- [SDR ASAA0680878](https://openairdocs.org/sdr/ASAA0680878.md): Floor Panel · debonded · Aug 15, 2006 · N968AS · Doug DC983 · Fuselage Floor Panel
  > FOUND CABIN FLOORBOARD PANEL EDGE DISBONDED. REPLACED PANEL PER SRM 53 05 AND DWG 9936651.
- [SDR ASAA0680877](https://openairdocs.org/sdr/ASAA0680877.md): Gusset · corroded · Aug 15, 2006 · N968AS · Doug DC983 · Fuselage Miscellaneous Structure
  > FOUND GUSSET CORRODED. REPLACED GUSSET PER DWG 5936071 AND SRM 51 30 5.
- [SDR ASAA0680876](https://openairdocs.org/sdr/ASAA0680876.md): Skin · corroded · Aug 15, 2006 · N968AS · Doug DC983 · Fuel Storage
  > AUX FUEL TANK ACCESS PANEL MOUNTING FLANGE CORRODED. REPLACED DOUBLER PER DWG 5936434 AND SRM 51 30 5.
- [SDR ASAA0680875](https://openairdocs.org/sdr/ASAA0680875.md): Splice · corroded · Aug 15, 2006 · N968AS · Doug DC983 · Fuselage Main, Longeron/Stringer
  > FOUND LONGERON SPLICE CORRODED. REPLACED SPLICE PER SRM 53 02 AND 51 30 5.
- [SDR ASAA0680874](https://openairdocs.org/sdr/ASAA0680874.md): Intercostal · corroded · Aug 15, 2006 · N968AS · Doug DC983 · Fuselage Main, Structure
  > FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 53-01 51-30-05 AND 51-10-3.
- [SDR ASAA0680873](https://openairdocs.org/sdr/ASAA0680873.md): Skin · dented · Aug 15, 2006 · N968AS · Doug DC983 · Cargo/Baggage Doors
  > FOUND MID CARGO BAY DOOR DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 52 05.
- [SDR ASAA0580285](https://openairdocs.org/sdr/ASAA0580285.md): Floorboard · cracked · May 16, 2005 · N968AS · Doug DC983 · Fuselage Floor Panel
  > OKC - DURING HV CHECK, FOUND FLOOR PANEL E-8 IS MISSING SPACER IN SUPPORT. REMOVED DAMAGED SECTION OF HAT CHANNEL DUE CRACK. INSTALLED REPLACEMENT HAT CHANNEL SECTION AND SPLICE. (M)
- [SDR ASAA0580262](https://openairdocs.org/sdr/ASAA0580262.md): Cusp Web · corroded · May 16, 2005 · N968AS · Doug DC983 · Fuselage Miscellaneous Structure
  > OKC - FOUND HV-CHECK, FOUND RIGHT CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M)
- [SDR ASAA0580292](https://openairdocs.org/sdr/ASAA0580292.md): Skin · delaminated · May 16, 2005 · N968AS · Doug DC983 · Wing, Plate/Skin
  > OKC - DURING HV-CHECK, FOUND LEFT ANTI-FLOAT TAB HAS A COMPOSITE REPAIR ON TRAILING EDGE, LOWER SURFACE IS DELAMINATING. REMOVED DAMAGE AND INSTALLED A REPAIR DOUBLER. (M)
- [SDR ASAA0580291](https://openairdocs.org/sdr/ASAA0580291.md): Skin · gouged · May 16, 2005 · N968AS · Doug DC983 · Trailing Edge Flaps
  > OKC - DURING HV CHECK, FOUND LEFT WING OUTBOARD FLAP VANE INBOARD LEADING EDGE IS GOUGED. REMOVED DAMAGE AND REPLACED WITH FILLER AND DOUBLER. (M)

Next page: https://openairdocs.org/deregistered/N968AS-2009-05-28/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 = 'N968AS' AND deregistration_id = 'N968AS-2009-05-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N968AS-2009-05-28/reports

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