# Service difficulty reports: N962AS, cancelled Sep 24, 2010

A list on [N962AS, cancelled Sep 24, 2010](https://openairdocs.org/deregistered/N962AS-2010-09-24.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 · 187 reports

- [SDR ASAA0781782](https://openairdocs.org/sdr/ASAA0781782.md): Cusp Web · corroded · Jun 7, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous Structure
  > RIGHT CUSP WEB CORRODED. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 53-05.
- [SDR ASAA0781781](https://openairdocs.org/sdr/ASAA0781781.md): Cusp Web · corroded · Jun 7, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous Structure
  > RIGHT CUSP WEB CORRODED. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 53-01 AND 53-05.
- [SDR ASAA0781780](https://openairdocs.org/sdr/ASAA0781780.md): Cusp Web · corroded · Jun 7, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous Structure
  > RIGHT CUSP WEB CORRODED. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 53-01, 51-70-4 AND 51-70-4.
- [SDR ASAA0781779](https://openairdocs.org/sdr/ASAA0781779.md): Cusp Web · corroded · Jun 7, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous Structure
  > RIGHT CUSP WEB CORRODED. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER PER SRM 53-05 AND 53-01.
- [SDR ASAA0781778](https://openairdocs.org/sdr/ASAA0781778.md): Insert · corroded · Jun 3, 2007 · N962AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAS NUMEROUS CORRODED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND DWG 4932106.
- [SDR ASAA0781777](https://openairdocs.org/sdr/ASAA0781777.md): Skin · dented · Jun 3, 2007 · N962AS · Doug DC983 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP INBOARD VANE HAS SEVERAL DENTS ON LOWER SURFACE. PREPARED DAMAGED SURFACE FOR BONDING. INSTALLED REPAIR DOUBLER PER SRM 51-70-2.
- [SDR ASAA0781776](https://openairdocs.org/sdr/ASAA0781776.md): Skin · chafed · Jun 3, 2007 · N962AS · Doug DC983 · Trailing Edge Flaps
  > LEFT OUTBOARD FLAP VANE LEADING EDGE IS CHAFED AT INBOARD SIDE. REMOVED DAMAGED EXISTING DOUBLER. INSTALLED REPLACEMENT DOUBLER PER SRM 51-70-2.
- [SDR ASAA0781775](https://openairdocs.org/sdr/ASAA0781775.md): Skin · dented · Jun 3, 2007 · N962AS · Doug DC983 · Trailing Edge Flaps
  > LEFT INBOARD FLAP OUTBOARD VANE LOWER INBOARD SURFACE HAS MULTIPLE DENTS. PREPARED DAMAGED AREA FOR BONDING. INSTALLED REPAIR DOUBLER PER SRM 51-70-2.
- [SDR ASAA0781774](https://openairdocs.org/sdr/ASAA0781774.md): Doubler · debonded · Jun 3, 2007 · N962AS · Doug DC983 · Elevator, Tab Structure
  > EXISTING REPAIR DISBONDED ON LOWER SURFACE OF LEFT ELEVATOR GEARED TAB. PREPARED DAMAGED AREA FOR BONDING. INSTALLED FILLER AND DOUBLER PER SRM 51-70-2.
- [SDR ASAA0781733](https://openairdocs.org/sdr/ASAA0781733.md): Web · damaged · May 30, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous Structure
  > DOUBLE DRILLED HOLES ON WEB UNDER FWD CABIN FLOORBOARD SUPPORT ANGLE. CUT OUT DAMAGED AREA OF WEB, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM 51-70-4 FIG 2.
- [SDR ASAA0781732](https://openairdocs.org/sdr/ASAA0781732.md): Skin · dented · May 30, 2007 · N962AS · Doug DC983 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED A PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR. CUT OUT DAMAGED AREA OF SKIN. FABRICATED AND INSTALLED A SKIN FILLER INTERNAL REPAIR DOUBLERS, REPAIR STRAPS AND FINGER DOUBLERS IAW SRM 53-04 FIG 12C.
- [SDR ASAA0781731](https://openairdocs.org/sdr/ASAA0781731.md): Channel · damaged · May 30, 2007 · N962AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAS A DAMAGED HAT CHANNEL. LOCATED AND DRILLED A REPLACEMENT HAT CHANNEL IAW SRM 51-10-4, 51-30-2 AND DAC DWG 9957918.
- [SDR ASAA0781730](https://openairdocs.org/sdr/ASAA0781730.md): Floor Panel · damaged · May 30, 2007 · N962AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAS EDGE DAMAGE. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-03 PG 122B AND DCA DWG S4932106.
- [SDR ASAA0781729](https://openairdocs.org/sdr/ASAA0781729.md): Floor Panel · damaged · May 30, 2007 · N962AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL IS DELAMINATED. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781728](https://openairdocs.org/sdr/ASAA0781728.md): Floor Panel · damaged · May 30, 2007 · N962AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAS TEN DAMAGED INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781727](https://openairdocs.org/sdr/ASAA0781727.md): Floor Panel · deteriorated · May 30, 2007 · N962AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAS NUMEROUS DAMAGED INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781726](https://openairdocs.org/sdr/ASAA0781726.md): Floor Panel · delaminated · May 30, 2007 · N962AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL IS DELAMINATED. FABRICATED A REPLACEMENT PANEL IAW SRM 53-05 PARA 44 AND DCA DWG S4932106.
- [SDR ASAA0781725](https://openairdocs.org/sdr/ASAA0781725.md): Floor Panel · deteriorated · May 30, 2007 · N962AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL IS BROKEN AT AN INSERT. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781724](https://openairdocs.org/sdr/ASAA0781724.md): Floor Panel · delaminated · May 30, 2007 · N962AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL DELAMINATED. FABRICATED REPLACEMENT FLOOR PANEL IAW SRM 53-05 PG 122B FIGURES 50 AND 50A AND DCA DWG 9936640.
- [SDR ASAA0781723](https://openairdocs.org/sdr/ASAA0781723.md): Cusp Web · corroded · May 30, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN CUSP WEB IS CORRODED. REMOVED CORRODED WEB LOCATED DRILLED AND INSTALLED A REPLACEMENT WEB IAW SRM 51-30-2.
- [SDR ASAA0781722](https://openairdocs.org/sdr/ASAA0781722.md): Cusp Web · corroded · May 30, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOOR CUSP WEB IS CORRODED. REMOVED THE CORRODED CUSP WEB LOCATED DRILLED AND INSTALLED A REPLACEMENT CUSP WEB IAW SRM 51-10-4 PG 1 AND 4 FIG 3 AND DAC DWG 9930538.
- [SDR ASAA0781721](https://openairdocs.org/sdr/ASAA0781721.md): Web · cracked · May 30, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOOR WEB IS CRACKED. CUT OUT DAMAGED AREA OF WEB, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM 51-70-4 FIG 2.
- [SDR ASAA0781720](https://openairdocs.org/sdr/ASAA0781720.md): Cusp Web · cracked · May 30, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOOR RT CUSP WEB IS CRACKED. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781719](https://openairdocs.org/sdr/ASAA0781719.md): Floor Support · corroded · May 30, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOOR SUPPORT IS CORRODED. FABRICATED AND INSTALLED A REPLACEMENT FLOOR SUPPORT IAW SRM 51-10-4 PG 1 AND 51-30-1 PARA 1 AND PARA 11.
- [SDR ASAA0781718](https://openairdocs.org/sdr/ASAA0781718.md): Floor Support · corroded · May 30, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOOR SUPPORT IS CORRODED. FABRICATED AND INSTALLED A REPLACEMENT FLOOR SUPPORT IAW SRM 51-10-4 PG 1 AND 51-30-1 PG 4.
- [SDR ASAA0781746](https://openairdocs.org/sdr/ASAA0781746.md): Frame · corroded · May 29, 2007 · N962AS · Doug DC983 · Fuselage Main, Frame
  > AFT CARGO FRAME AT STA 1307.091 CORRODED. LOCATED AND DRILLED A REPLACEMENT FRAME SECTION AND REPAIR PARTS AND INSTALLED IAW SRM 53-03 FIG 2A AND SRM 51-30-2.
- [SDR ASAA0781745](https://openairdocs.org/sdr/ASAA0781745.md): Skin · dented · May 29, 2007 · N962AS · Doug DC983 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE DENTED AT STA 579 BETWEEN LONG 20L AND 21L. MEASURED DENT AT 4.0 X.015 INCH WITHIN LIMITS PER SRM. REPAIRED IAW SRM 53-04 FIG 38 SHEETS 12 AND 21. COLD FORMED SKIN BACK TO ORIGINAL BLUEPRINT CONTOUR AND ACCOMPLISHED HFEC INSPECTION FABRIC
- [SDR ASAA0781744](https://openairdocs.org/sdr/ASAA0781744.md): Skin · dented · May 29, 2007 · N962AS · Doug DC983 · Fuselage Main, Plate/Skin
  > AFT CARGO DOOR EXTERIOR SKIN IS DENTED 22 INCHES FROM THE AFT EDGE 14 INCHES FROM THE TOP EDGE. CUT OUT DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER AND 2 EACH FINGER DOUBLERS IAW SRM 53-04.
- [SDR ASAA0781743](https://openairdocs.org/sdr/ASAA0781743.md): Insert · corroded · May 29, 2007 · N962AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAS NUMERIOUS INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781742](https://openairdocs.org/sdr/ASAA0781742.md): Insert · corroded · May 29, 2007 · N962AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAS NUMEROUS CORRODED INSERTS. FABRICATED A REPLACEMENT PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781741](https://openairdocs.org/sdr/ASAA0781741.md): Floor Panel · delaminated · May 29, 2007 · N962AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL IS DELAMINATED. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781740](https://openairdocs.org/sdr/ASAA0781740.md): Floor Panel · delaminated · May 29, 2007 · N962AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL IS DELAMINATED. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781739](https://openairdocs.org/sdr/ASAA0781739.md): Insert · corroded · May 29, 2007 · N962AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAS NUMEROUS CORRODED INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781738](https://openairdocs.org/sdr/ASAA0781738.md): Insert · corroded · May 29, 2007 · N962AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAS NUMEROUS CORRODED INSERTS. FABRICATED A REPLACEMENT PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781737](https://openairdocs.org/sdr/ASAA0781737.md): Floor Panel · deteriorated · May 29, 2007 · N962AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAS FIBER DAMAGE TO THE UPPER SURFACE. FABRICATED A REPLACEMENT PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781736](https://openairdocs.org/sdr/ASAA0781736.md): Floor Panel · damaged · May 29, 2007 · N962AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAS DAMAGED INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781735](https://openairdocs.org/sdr/ASAA0781735.md): Floor Panel · delaminated · May 29, 2007 · N962AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL IS DELAMINATED. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781734](https://openairdocs.org/sdr/ASAA0781734.md): Floor Panel · corroded · May 29, 2007 · N962AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAS CORRODED INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53 05 PARA 11 AND DAC DWG S4932106.
- [SDR ASAA0781715](https://openairdocs.org/sdr/ASAA0781715.md): Skin · dented · May 29, 2007 · N962AS · Doug DC983 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN IS DENTED. INSTALLED REPAIR DOUBLER AT RIGHT EXT FUSELAGE. COLD FORMED SKIN BACK TO ORIGINAL BLUEPRINT CONTOUR AND HFEC PRIOR TO DOUBLER INSTALLATION. ALL PER SRM 53-04 PG 218H.
- [SDR ASAA0781714](https://openairdocs.org/sdr/ASAA0781714.md): Cusp Web · corroded · May 29, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOOR CUSP WEB CORRODED. REMOVED CORRODED CUSP WEB, LOCATED DRILLED AND INSTALLED A REPLACEMENT CUSP WEB IAW SRM 51-10-4 AND 51-30-2.
- [SDR ASAA0781713](https://openairdocs.org/sdr/ASAA0781713.md): Cusp Web · corroded · May 29, 2007 · N962AS · Doug DC983 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOOR CUSP WEB CORRODED. REMOVED CORROSION MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED CUSP WEB IAW SRM 51-30-2 AND 51-30-1.
- [SDR ASAA0781712](https://openairdocs.org/sdr/ASAA0781712.md): Skin · dented · May 29, 2007 · N962AS · Doug DC983 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN IS DENTED AFT OF THE FWD LAVATORY SERVICE PANEL WITHIN 1 INCH OF LONGERON 20L. COLD WORKED SKIN, FABRICATED DOUBLER,TREATED, PRIMED AND INSTALLED IAW SRM 51-10-3 PARA 23 AND 30.
- [SDR ASAA0680224](https://openairdocs.org/sdr/ASAA0680224.md): Skin · dented · Mar 2, 2006 · N962AS · Doug DC983 · Trailing Edge Flaps
  > LEFT INBOARD FLAP LOWER SURFACE IS DENTED. CUT OUT DAMAGED AREA. INSTALLED FILLER AND DOUBLER PER SRM 57 01 FIG 5 SHT 2.
- [SDR ASAA0680223](https://openairdocs.org/sdr/ASAA0680223.md): Skin · damaged · Mar 2, 2006 · N962AS · Doug DC983 · Rudder, Plate/Skin
  > FOUND RUDDER LEFT SURFACE IS DINGED 23 INCHES FROM T/E 20.5 INCHES AFT OF LOWER DAMPER CUTOUT. APPLIED FILLER PER SRM 51 70 1A PARA 21.
- [SDR ASAA0680258](https://openairdocs.org/sdr/ASAA0680258.md): Repair · delaminated · Mar 1, 2006 · N962AS · Doug DC983 · Rudder, Tab Structure
  > RUDDER TAB EXISTING REPAIR DELAMINATED 7 TO 9 INCHES FROM T/E AND 3 TO 9 INCHES ABOVE SECOND HINGE. REPLACED EXISTING REPAIR PER SRM 51-70-1A PARA 21.
- [SDR ASAA0480627](https://openairdocs.org/sdr/ASAA0480627.md): Power Supply · discharged · Dec 29, 2004 · N962AS · Doug DC983 · Emergency Lighting
  > DURING LINE CHECK, FOUND OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. REPLACED ASSOCIATED POWER SUPPLY (BATTERY PACK). LIGHTS THEN OPERATED PROPERLY. (M)
- [SDR ASAA0480615](https://openairdocs.org/sdr/ASAA0480615.md): Longeron · corroded · Dec 16, 2004 · N962AS · Doug DC983 · Fuselage Main, Longeron/Stringer
  > OKC - HV-CHECK, LONGERON 29L IS CORRODED. APPLIED SEALANT PER EA 5310-02430. (M)
- [SDR ASAA0480614](https://openairdocs.org/sdr/ASAA0480614.md): Longeron · corroded · Dec 16, 2004 · N962AS · Doug DC983 · Fuselage Main, Longeron/Stringer
  > OKC - HV-CHECK, FOUND LONGERON 30 IS CORRODED. REMOVED DAMAGED SECTION. INSTALLED U-CHANNEL AND FILLER. (M)
- [SDR ASAA0480612](https://openairdocs.org/sdr/ASAA0480612.md): Access Panel · chafed · Dec 16, 2004 · N962AS · Doug DC983 · Wing, Plate/Skin
  > OKC - HV-CHECK, LEFT WING FUEL PANEL 1303 CHAFED AND PITTED. REPLACED PANEL. (M)
- [SDR ASAA0480616](https://openairdocs.org/sdr/ASAA0480616.md): Door Frame · gouged · Dec 16, 2004 · N962AS · Doug DC983 · Fuselage Main, Structure
  > OKC - HV-CHECK, TWO MOUNTING HOLES GOUGED AT BOTTOM FRAME OF LEFT OVERWING EXIT. INSTALLED DOUBLER PER EA 53-20-01679. (M)

Next page: https://openairdocs.org/deregistered/N962AS-2010-09-24/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 = 'N962AS' AND deregistration_id = 'N962AS-2010-09-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N962AS-2010-09-24/reports

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