# Service difficulty reports: N973AS, cancelled Sep 30, 2013

A list on [N973AS, cancelled Sep 30, 2013](https://openairdocs.org/deregistered/N973AS-2013-09-30.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 · 200 reports

- [SDR ASAA0580542](https://openairdocs.org/sdr/ASAA0580542.md): Floor Panel · corroded · Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Floor Panel
  > C-CHECK, CABIN FLOOR PANEL HAS CORRODED INSTERTS AND IS DELAMINATED AROUND INSTERS. REPLACED FLOOR PANEL. (K)
- [SDR ASAA0580557](https://openairdocs.org/sdr/ASAA0580557.md): Vane · dented · Dec 12, 2005 · N973AS · Doug DC983 · Trailing Edge Flaps
  > C-CHECK, LT WING NR 1 FLAP VANE IS DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (K)
- [SDR ASAA0580556](https://openairdocs.org/sdr/ASAA0580556.md): Vane · punctured · Dec 12, 2005 · N973AS · Doug DC983 · Trailing Edge Flaps
  > C-CHECK, LT WING NR 1 FLAP VANE IS PUNCTURED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (K)
- [SDR ASAA0580555](https://openairdocs.org/sdr/ASAA0580555.md): Vane · gouged · Dec 12, 2005 · N973AS · Doug DC983 · Trailing Edge Flaps
  > C-CHECK, LT WING OB FLAP IB VANE IS GOUGED. BLENDED GOUGE. INSTALLED REPAIR DOUBLER. (K)
- [SDR ASAA0580554](https://openairdocs.org/sdr/ASAA0580554.md): Skin · dented · Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Main, Plate/Skin
  > C-CHECK, FUSELAGE SKIN DENTED. COLD WORKED TO ORIGINAL CONTOUR. INSTALLED REPAIR DOUBLER. (K)
- [SDR ASAA0580553](https://openairdocs.org/sdr/ASAA0580553.md): Skin · dented · Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Main, Plate/Skin
  > C-CHECK, FUSELAGE SKIN DENTED. COLD-WORKED TO ORIGINAL CONTOUR. INSTALLED REPAIR DOUBLER. (K)
- [SDR ASAA0580552](https://openairdocs.org/sdr/ASAA0580552.md): Web · cracked · Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Miscellaneous Structure
  > C-CHECK, CABIN FLOOR WEB CRACKED. REMOVED DAMAGED WEB SECTION. INSTALLED REPAIR DOUBLER. (K)
- [SDR ASAA0580551](https://openairdocs.org/sdr/ASAA0580551.md): Track · corroded · Dec 12, 2005 · N973AS · Doug DC983 · Fuselage, Seat/Cargo Attach Fittings
  > C-CHECK, CABIN FLOOR TRACK CORRODED. REPLACED FLOOR TRACK. (K)
- [SDR ASAA0580550](https://openairdocs.org/sdr/ASAA0580550.md): Track · corroded · Dec 12, 2005 · N973AS · Doug DC983 · Fuselage, Seat/Cargo Attach Fittings
  > C-CHECK, CABIN FLOOR TRACK CORRODED. REPLACED FLOOR TRACK. (K)
- [SDR ASAA0580549](https://openairdocs.org/sdr/ASAA0580549.md): Track · corroded · Dec 12, 2005 · N973AS · Doug DC983 · Fuselage, Seat/Cargo Attach Fittings
  > C-CHECK, CABIN FLOOR TRACK CORRODED. REPLACED FLOOR TRACK. (K)
- [SDR ASAA0580548](https://openairdocs.org/sdr/ASAA0580548.md): Floor Panel · delaminated · Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Floor Panel
  > C-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)
- [SDR ASAA0580547](https://openairdocs.org/sdr/ASAA0580547.md): Floor Panel · delaminated · Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Floor Panel
  > C-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)
- [SDR ASAA0580546](https://openairdocs.org/sdr/ASAA0580546.md): Floor Panel · delaminated · Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Floor Panel
  > C-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)
- [SDR ASAA0580545](https://openairdocs.org/sdr/ASAA0580545.md): Floor Panel · corroded · Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Floor Panel
  > C-CHECK, CABIN FLOOR PANEL HAS CORRODED INSERTS AND IS DELAMINATED AROUND INSERTS. REPLACED FLOOR PANEL. (K)
- [SDR ASAA0580544](https://openairdocs.org/sdr/ASAA0580544.md): Floor Panel · delaminated · Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Floor Panel
  > C-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)
- [SDR ASAA0580543](https://openairdocs.org/sdr/ASAA0580543.md): Floor Panel · delaminated · Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Floor Panel
  > C-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)
- [SDR ASAA0850542](https://openairdocs.org/sdr/ASAA0850542.md): Floor Panel · corroded · Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Floor Panel
  > C-CHECK, CABIN FLOOR PANEL HAS CORRODED INSERTS AND DELAMINATED AROUND INSERTS. REPLACED FLOOR PANEL. (K)
- [SDR ASAA0580541](https://openairdocs.org/sdr/ASAA0580541.md): Web · corroded · Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Miscellaneous Structure
  > C-CHECK, L-1 DOOR JAMB LOWER SILL WEB CORRODED. REMOVED DAMAGED SECTION OF WEB. INSTALLED REPAIR DOUBLER. (K)
- [SDR ASAA0580540](https://openairdocs.org/sdr/ASAA0580540.md): Web · corroded · Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Miscellaneous Structure
  > C-CHECK, CABIN FLOOR WEB CORRODED. REPLACED WEB. (K)
- [SDR ASAA0580539](https://openairdocs.org/sdr/ASAA0580539.md): Intercostal · cracked · Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Miscellaneous Structure
  > C-CHECK, INTERCOSTAL CRACKED AT RADIUS. REPLACED INTERCOSTAL. (K)
- [SDR ASAA0580538](https://openairdocs.org/sdr/ASAA0580538.md): Frame · punctured · Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Main, Frame
  > C-CHECK, FUSELAGE FRAME WEB PUNCTURED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)
- [SDR ASAA0580537](https://openairdocs.org/sdr/ASAA0580537.md): Fitting · corroded · Dec 12, 2005 · N973AS · Doug DC983 · Emergency Equipment
  > C-CHECK, R-1 DOOR FLOOR MOUNTED GIRT BAR FITTING CORRODED. REPLACED CORRODED FITTING. (K)
- [SDR ASAA0480597](https://openairdocs.org/sdr/ASAA0480597.md): Lanyard · disconnected · Dec 13, 2004 · N973AS · Doug DC983 · Escape Slide
  > SEA - PREFLIGHT CHECK, AFT SERVICE DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)
- [SDR ASAA0480540](https://openairdocs.org/sdr/ASAA0480540.md): Battery Pack · inoperative · Oct 24, 2004 · N973AS · Doug DC983 · Emergency Lighting
  > PDX LINE CHK - EMERGENCY OVERHEAD CABIN LIGHTS INOPERATIVE FROM ROW 2 TO 7. REPLACED ASSOCIATED BATTERY PACK (POWER SUPPLY). LIGHTS THEN OPERATED PROPERLY.
- [SDR ASAA0480531](https://openairdocs.org/sdr/ASAA0480531.md): Access Panel · leaking · Oct 2, 2004 · N973AS · Doug DC983 · Wing, Plate/Skin
  > OKC - C-CHECK, EVIDENCE OF FUEL LEAK FROM RT WING LOWER DOORS, NR 5 AND NR 7, FROM IB ENSURED HOLE CLEAN AND ROUND, TOUCH COUNTER SUNK, NDT FOR CRACKS. INSTALLED AD RIVET AND SHAVED BOTH SIDES OF REPAIR IAW EA 5710-01109 AND EA 10575.
- [SDR ASAA0480530](https://openairdocs.org/sdr/ASAA0480530.md): Access Panel · leaking · Oct 2, 2004 · N973AS · Doug DC983 · Wing, Plate/Skin
  > OKC - C-CHECK, EVIDENCE OF FUEL LEAK FROM RT WING LOWER DOORS NR 5 AND NR 7 FROM IB. REMOVED PANEL, ORDERED AND INSTALLED NEW PANEL IAW MM 28-00-00.
- [SDR ASAA0480529](https://openairdocs.org/sdr/ASAA0480529.md): Longeron · corroded · Oct 2, 2004 · N973AS · Doug DC983 · Fuselage Main, Longeron/Stringer
  > OKC- C-CHECK, AFT PIT LONGERON 28L AT STA 1098 TO CORRODED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHANNEL IAW SRM 53-02, FIG 19.
- [SDR ASAA0480528](https://openairdocs.org/sdr/ASAA0480528.md): Longeron · corroded · Oct 2, 2004 · N973AS · Doug DC983 · Fuselage Main, Longeron/Stringer
  > OKC - C-CHECK, AFT PIT STA 1087-1098, LONG 29L HOLES HAVE CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHANNEL IAW SRM 53-02, FIG 19.
- [SDR ASAA0480527](https://openairdocs.org/sdr/ASAA0480527.md): Skin · corroded · Oct 2, 2004 · N973AS · Doug DC983 · Vertical Stabilizer
  > OKC - C-CHECK, AFT BELLY SKIN CORRODED STA 1098 TO STA 1110 BETWEEN LONG 29L AND 27L. REMOVED DAMAGE, HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EA 5310-02398 AND EA 10582.
- [SDR ASAA0480526](https://openairdocs.org/sdr/ASAA0480526.md): Skin · gouged · Sep 28, 2004 · N973AS · Doug DC983 · Vertical Stabilizer
  > OKC - C-CHECK VERTICAL STAB UPPER SKIN GOUGED AROUND BANANA UPPER FAIRING PANEL 3705A ATTACHMENT AREA. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER/SKIN AND DOUBLER, IAW SRM 51-30-1 AND 51-30-2, EA 5530-01108 AND EA 10594.
- [SDR ASAA0480525](https://openairdocs.org/sdr/ASAA0480525.md): Skin · chafed · Sep 28, 2004 · N973AS · Doug DC983 · Wing, Plate/Skin
  > OKC - C-CHECK, LT WING L/E UPPER SURFACE CHAFED 25 INCHES OB OF L/E SLAT NR 0, OB TRACK REMOVED DAMAGE. HFEC, NO CRACKS NOTED, TREATED AND PRIMED IAW EA 5740-01411 AND EA 10592.
- [SDR ASAA0480524](https://openairdocs.org/sdr/ASAA0480524.md): Diverter · crazed · Sep 28, 2004 · N973AS · Doug DC983 · Air Conditioning System
  > OKC - C-CHECK, LT PRIMARY HEAT EXCHANGER RAM AIR DIVERTER WORN IN FORWARD LOWER CORNER STOP DRILLED CRACK, FPI FOR CRACK CONTAINMENT AND WELDED CRACK IAW EA 5300-01053 AND EA 10576.
- [SDR ASAA0480523](https://openairdocs.org/sdr/ASAA0480523.md): Vane · damaged · Sep 28, 2004 · N973AS · Doug DC983 · Trailing Edge Flaps
  > OKC - C-CHECK, RT IB FLAP VANE LOWER SKIN HAS DINGS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-2.
- [SDR ASAA0480522](https://openairdocs.org/sdr/ASAA0480522.md): Vane · dented · Sep 28, 2004 · N973AS · Doug DC983 · Trailing Edge Flaps
  > OKC - C-CHECK, RT OB FLAP VANE IB END LOWER SKIN HAS NUMEROUS SMALL DENTS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-2.
- [SDR ASAA0480521](https://openairdocs.org/sdr/ASAA0480521.md): Frame · corroded · Sep 28, 2004 · N973AS · Doug DC983 · Fuselage Main, Frame
  > OKC, C-CHECK, AFT CARGO COMPARTMENT FRAME STA 1098 HAS CORROSION ON FORWARD SIDE AND TOP SIDE JUST ABOVE LONGERON 30. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE, DOUBLER, SPACER AND FILLER IAW SRM.
- [SDR ASAA0480520](https://openairdocs.org/sdr/ASAA0480520.md): Skin · dented · Sep 28, 2004 · N973AS · Doug DC983 · Trailing Edge Flaps
  > OKC, C-CHECK, RT WING T/E IB FLAP DENTED AT LOWER SURFACE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-03, FIG 7.
- [SDR ASAA0480519](https://openairdocs.org/sdr/ASAA0480519.md): Longeron · corroded · Sep 28, 2004 · N973AS · Doug DC983 · Fuselage Main, Longeron/Stringer
  > OKC- C-CHECK, LONGERON 29L IS CORRODED FROM STA 1203 TO 1208 ON THE LOWER SURFACE OF THE OB FAIRING. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICES IAW SRM 53-02, FIG 18.
- [SDR ASAA0480518](https://openairdocs.org/sdr/ASAA0480518.md): Fairing · cracked · Sep 28, 2004 · N973AS · Doug DC983 · Cabin Cooling System
  > OKC- C-CHECK, LT ACM EXHAUST FAIRING IS CRACKED. STOP DRILLED CRACK, HFEC FOR CRACK CONTAINMENT, WELDED CRACK IAW EA 2120-01087 AND EA 10573.
- [SDR USAA0480517](https://openairdocs.org/sdr/USAA0480517.md): Fitting · corroded · Sep 28, 2004 · N973AS · Doug DC983 · Fuselage Main, Attach Fittings
  > OKC - C-CHECK, AFT BILLIE BATH TUB FITTING TO BULKHEAD STA 1003, LONG 30, HAS AREAS OF CORROSION ON FORWARD INSIDE OF FITTING. REMOVED DAMAGE, SPOT FACED FASTENER HOLES, TREATED AND PRIMED, SEALED AND APPLIED CORROSION INHIBITING COMPOUND IAW EA 5340-01132 AN
- [SDR ASAA0480516](https://openairdocs.org/sdr/ASAA0480516.md): Strap · broken · Sep 28, 2004 · N973AS · Doug DC983 · Fixed Inner Doors
  > OKC - C-CHECK, COMPLY WITH JOB 062, LOG NR 5784357, COCKPIT DOOR CLOSING STRAP BROKEN OFF. FABRICATED AND INSTALLED PLATE IAW EA 5250-01191 AND EA 10559.
- [SDR ASAA0480515](https://openairdocs.org/sdr/ASAA0480515.md): Skin · chafed · Sep 24, 2004 · N973AS · Doug DC983 · Vertical Stabilizer, Plate/Skin
  > OKC - C-CHECK, RT VERTICAL STAB LOWER SURFACE CHAFED IN 5 EA SPOTS INNER BANANA FAIRING PANEL 3802A, ATTACHMENT AREA. REMOVED DAMAGED SKINS, ORDERED AND INSTALLED NEW SKINS IAW SRM 51-30-2.
- [SDR ASAA0480514](https://openairdocs.org/sdr/ASAA0480514.md): Floorboard · cracked · Sep 24, 2004 · N973AS · Doug DC983 · Fuselage Floor Panel
  > OKC - C-CHECK, FLOOR PANEL AT STA 826 TO 886 AFT IB CORNER ANGLE IS CRACKED. REMOVED, ORDERED AND REPLACED (W) ANGLE IAW SRM 51-30-8.
- [SDR ASAA0480513](https://openairdocs.org/sdr/ASAA0480513.md): Vane · punctured · Sep 24, 2004 · N973AS · Doug DC983 · Trailing Edge Flaps
  > OKC - C-CHECK, RT IB FLAP OB FLAPVANE HAS A PUNCTURE ON THE IB END. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-2, PARA 18.
- [SDR ASAA0480512](https://openairdocs.org/sdr/ASAA0480512.md): Floorboard · delaminated · Sep 24, 2004 · N973AS · Doug DC983 · Fuselage Floor Panel
  > OKC - C-CHECK, FLOORBOARD IN PASSENGER CABIN AT STA 826-864, BETWEEN 22R AND 44R DELAMINATD AND CRACKED. FABRICATED REPLACEMENT FLOORBOARD IAW SRM 53-05.
- [SDR ASAA0480511](https://openairdocs.org/sdr/ASAA0480511.md): Skin · dented · Sep 24, 2004 · N973AS · Doug DC983 · Cargo/Baggage Doors
  > OKC - C-CHECK, AFT CARGO DOOR SKIN DENTED UPPER AFT AREA X=.040, D=.60, FOUND TO BE CONDITION 1B IAW SRM 53-04, FIG 38, D/X=15.
- [SDR ASAA0480510](https://openairdocs.org/sdr/ASAA0480510.md): Skin · damaged · Sep 24, 2004 · N973AS · Doug DC983 · Cargo/Baggage Doors
  > OKC - C-CHECK, FORWARD CARGO DOOR SKIN ALONG FWD EDGE DINGED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 52-05, FIG 4.
- [SDR ASAA0480509](https://openairdocs.org/sdr/ASAA0480509.md): Longeron · corroded · Sep 24, 2004 · N973AS · Doug DC983 · Fuselage Main, Longeron/Stringer
  > OKC - C-CHECK, AFT PIT LONGERON 28L AT STA 1098 TO 1110 CORRODED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHANNEL IAW SRM 53-02, FIG 19.
- [SDR ASAA0480508](https://openairdocs.org/sdr/ASAA0480508.md): Floorboard · damaged · Sep 24, 2004 · N973AS · Doug DC983 · Fuselage Floor Panel
  > OKC - C-CHECK, CABIN FLOOR PANEL, STA 826-STA 886 DAMAGED AT FWD IB CORNER. FABRICATED REPLACEMENT FLOOR PANEL IAW SRM 53-05.
- [SDR ASAA0480507](https://openairdocs.org/sdr/ASAA0480507.md): Skin · gouged · Sep 24, 2004 · N973AS · Doug DC983 · Wing, Plate/Skin
  > OKC - C-CHECK, RT WING LOWER IB T/E SKIN GOUGED. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPLACEMENT SKIN IAW SRM 51-10-4, 57-22-3.
- [SDR ASAA0480506](https://openairdocs.org/sdr/ASAA0480506.md): Floorboard · delaminated · Sep 24, 2004 · N973AS · Doug DC983 · Fuselage Floor Panel
  > OKC- C-CHECK, CABIN FLOORBOARD STA 180 TO 200 RBL 44 HAS DELAMINATION AND BROKEN EDGES. FABRICATED REPLACEMENT FLOORBOARD IAW SRM 53-05.

Next page: https://openairdocs.org/deregistered/N973AS-2013-09-30/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 = 'N973AS' AND deregistration_id = 'N973AS-2013-09-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N973AS-2013-09-30/reports

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