# Service difficulty reports: N802AT, cancelled May 9, 2003

A list on [N802AT, cancelled May 9, 2003](https://openairdocs.org/deregistered/N802AT-2003-05-09.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR AT0100105](https://openairdocs.org/sdr/AT0100105.md): Light · inoperative · Mar 8, 2001 · N802AT · Doug DC932 · Emergency Lighting
  > FOUND L-1 DOOR PORTABLE EMERGENCY LIGHT ASSEMBLY INOPERATIVE. INSTALLED PORTABLE EMERGENCY LIGHT ASSEMBLY.
- [SDR AT0100078](https://openairdocs.org/sdr/AT0100078.md): Tripler · cracked · Feb 2, 2001 · N802AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND FORWARD AIRSTAIR CUT OUT DOUBLER CRACKED IN AFT LOWER CORNER. INSTALLED TRIPLER, FILLER, INTERCOSTAL, AND CHANNEL IAW REO L00360.
- [SDR AT0100047](https://openairdocs.org/sdr/AT0100047.md): Floor Panel · corroded · Jan 14, 2001 · N802AT · Doug DC932 · Fuselage Floor Panel
  > FOUND FLOOR PANEL 97 CORRODED BEYOND LIMITS. REPAIRED FLOOR PANEL IAW DC9 SRM 53-05, 53-21, 51-10-03, AND MM 53-20-01.
- [SDR AT0100044](https://openairdocs.org/sdr/AT0100044.md): Stringer · corroded · Jan 12, 2001 · N802AT · Doug DC932 · Wing, Longeron/Stringer
  > FOUND RIGHT WING TANK XCW 58.6 CORRODED BEYOND LIMITS. INSTALLED REPAIR STRAP ON STRINGER 22 IAW DC9 SRM 57-08 FIG 2.
- [SDR AT0100046](https://openairdocs.org/sdr/AT0100046.md): Floor Support · corroded · Jan 6, 2001 · N802AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND FLOOR SUPPORT ANGLE AT BS 180 RBL 0-44 CORRODED BEYOND LIMITS. FABRICATED AND REPLACED ANGLE IAW DC9 SRM 51-10-03, 51-30-05, AND 53-01 FIG 1.
- [SDR AT0100021](https://openairdocs.org/sdr/AT0100021.md): Floor Panel · corroded · Jan 6, 2001 · N802AT · Doug DC932 · Fuselage Floor Panel
  > FOUND CORROSION ON FLOOR PANEL BS 180 RBL 0 - RBL 44 BEYOND LIMITS. FABRICATED AND INSTALLED DOUBLERS IAW DC9 SRM 51-30-08 AND 53-01 FIG 4.
- [SDR AT0100020](https://openairdocs.org/sdr/AT0100020.md): Floor Support · corroded · Jan 6, 2001 · N802AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND CABIN FLOOR PANEL SUPPORT AT BS 200 RBL 0 - RBL 51 CORRODED BEYOND LIMITS. REPLACED FLOOR SUPPORT IAW DC9 SRM 51-20-05, 51-10-04, 51-10-02, AND 53-11-01 FIG 12.
- [SDR AT01000019](https://openairdocs.org/sdr/AT01000019.md): Floor Support · corroded · Jan 6, 2001 · N802AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND FLOOR SUPPORT CORRODED BEYOND LIMITS AT BS 198 LBL 0 - LBL 51. REPLACED FLOOR SUPPORT IAW DC9 SRM 51-30-03, 51-30-05, 51-10-04, AND 53-11-01 FIG 13.
- [SDR AT0100043R1](https://openairdocs.org/sdr/AT0100043R1.md): Cargo Track · corroded · Jan 5, 2001 · N802AT · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND AFT PIT CARGO TRACK BS 937 - 966 CORRODED BEYOND LIMITS. REPAIRED CARGO TRACK IAW DC9 SRM 51-10-03, 51-10-04, AND 53-21.
- [SDR AT0100041R1](https://openairdocs.org/sdr/AT0100041R1.md): Skin Panel · corroded · Jan 2, 2001 · N802AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND SKIN UNDER C2 LOWER THRESHHOLD AT BS 917 CORRODED. INSTALLED REPAIR IAW DC9 REO-L00364.
- [SDR AT0000171](https://openairdocs.org/sdr/AT0000171.md): Skin · damaged · Mar 28, 2000 · N802AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND SKIN DAMAGE AT BS 229 AND 237 LONGERON 17 LT. CORRECTIVE ACTION: TRIMMED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC9 SRM 53-04 FIG 47 AND REO-L00124.
- [SDR AT0100042](https://openairdocs.org/sdr/AT0100042.md): Pan · corroded · Jan 19, 2000 · N802AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND C2 DOOR LOWER PAN CORRODED BEYOND LIMITS. REPLACED LOWER PAN IAW DC9 SRM 53-04 FIG 44, 51-10-03, 51-10-04, 51-30-02, AND 51-30-05.
- [SDR AT0100043](https://openairdocs.org/sdr/AT0100043.md): Cargo Track · corroded · Jan 5, 2000 · N802AT · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND AFT PIT CARGO TRACK BS 937 - 966 CORRODED BEYOND LIMITS. REPAIRED CARGO TRACK IAW DC9 SRM 51-10-03, 51-10-04, AND 53-21.
- [SDR AT0100041](https://openairdocs.org/sdr/AT0100041.md): Skin Panel · corroded · Jan 2, 2000 · N802AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND SKIN UNDER C2 LOWER THRESHHOLD AT BS 917 CORRODED. INSTALLED REPAIR IAW DC9 REO-L00364.
- [SDR AT9900889](https://openairdocs.org/sdr/AT9900889.md): Light · inoperative · Dec 10, 1999 · N802AT · Doug DC932 · Emergency Lighting
  > FWD ENTRY DOOR EMERGENCY LIGHT DID NOT ILLUMINATE DURING SERVICE CHECK. REMOVED AND REPLACED LIGHT ASSEMBLY.
- [SDR AT9900835](https://openairdocs.org/sdr/AT9900835.md): Longeron · corroded · Nov 6, 1999 · N802AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND LONGERON 20R AT BS 227 TO 285 CORRODED. CUT OUT CORRODED SECTION OF LONGERON. FABRICATED NEW LONGERON SECTION AND SPLICES. INSTALLED REPAIR IAW DC9 SRM 53-10-2, 51-30-2, 51-10-3 AND 51-10-4.
- [SDR AT9900816](https://openairdocs.org/sdr/AT9900816.md): Frame · cracked · Nov 6, 1999 · N802AT · Doug DC932 · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, FOUND FRAME AT BS 617 RIGHT TO HAVE TEMPORARY REPAIR. REMOVED AND REPLACED FRAME AT BS 617 RIGHT IAW DC9 SRM 51-30-02 AND 51-30-05.
- [SDR AT9900815](https://openairdocs.org/sdr/AT9900815.md): Skin · corroded · Nov 5, 1999 · N802AT · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, FOUND CORROSION AT BS 323-380 AND AT STATIC PORT TO BE OUT OF LIMITS. REMOVED CORROSION AND INSTALLED DOUBLER BS 323-380 IAW EO 99-1332 AND DC9 SRM 53-00.
- [SDR AT9900814](https://openairdocs.org/sdr/AT9900814.md): Skin · crack · Nov 5, 1999 · N802AT · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, A CRACK WAS FOUND ON THE FUSELAGE SKIN AT BS 120-200 RIGHT. REMOVED AND REPAIRED CRACK AT BS 120-200 RIGHT IAW EO 99-1332.
- [SDR AT9900813](https://openairdocs.org/sdr/AT9900813.md): Skin · dented · Nov 5, 1999 · N802AT · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, THE RIGHT FUSELAGE SKIN HAD NUMEROUS DENTS AT BS 227-408. REMOVED AND FABRICATED NEW SKIN IAW AT BS 227-408 EO 99-1328.
- [SDR AT9900793](https://openairdocs.org/sdr/AT9900793.md): Frame · cracked · Oct 27, 1999 · N802AT · Doug DC932 · Fuselage Main, Frame
  > FOUND FUSELAGE TAIL INTERIOR FRAME AT BS 1143 CRACKED. INSTALLED NEW FRAME SECTION REPAIR AND SPLICES IAW TIMCO EO 99-1292.
- [SDR AT9900791](https://openairdocs.org/sdr/AT9900791.md): Support · corroded · Oct 27, 1999 · N802AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND CABIN FLOOR SUPPORT AT BS 197 AND BL 0 TO LBL 44 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW DC9 SRM 51-10-2, 51-30-5 AND 53-11-1 FIG 13.
- [SDR AT9900792](https://openairdocs.org/sdr/AT9900792.md): Panel · delaminated · Oct 25, 1999 · N802AT · Doug DC932 · Wing, Plate/Skin
  > FOUND RT WING TRAILING EDGE PANEL UPPER AND LOWER SURFACES DELAMINATED AT WS 434-486. REMOVED UPPER SKIN, DOUBLER, HONEYCOMB CORE AND INNER SKIN. FABRICATED REPLACEMENT UPPER SKIN, UPPER SKIN EXTERNAL DOUBLER AND INNER SKIN. CUT AND FIT HONEYCOMB REPLACEMEN
- [SDR AT9900798](https://openairdocs.org/sdr/AT9900798.md): Panel · disbonded · Oct 22, 1999 · N802AT · Doug DC932 · Trailing Edge Flaps
  > FOUND RT WING TRAILING EDGE PANEL DISBONDED. REMOVED UPPER SKIN, DOUBLER, CORE AND INNER SKIN. FABRICATED REPLACEMENT UPPER SKIN, UPPER SKIN EXTERNAL DOUBLER AND INNER SKIN. CUT AND FIT HONEYCOMB REPLACEMENT CORE. ACCOMPLISHED COMPOSITE REPAIR ON PANEL IAW
- [SDR AT9900794](https://openairdocs.org/sdr/AT9900794.md): Support · corroded · Oct 22, 1999 · N802AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND CABIN FLOOR SUPPORT AT BS 197-256 CORRODED OUT OF LIMITS ON SUPPORT AND 2 CRACKS ON SUBFLOOR. REMOVED AND REPLACED FLOOR SUPPORT AT BS 197. FABRICATED AND INSTALLED REPAIR DOUBLER ON SUBFLOOR IAW DC9 SRM 53-20-1 AND 51-10-2.
- [SDR AT9900790](https://openairdocs.org/sdr/AT9900790.md): Support · corroded · Oct 20, 1999 · N802AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND CABIN FLOOR SUPPORT AT BS 229 AND LBL 14 CORRODED BEYOND LIMITS AND SUB-FLOOR SKIN CRACKED. REMOVED AND REPLACED FLOOR SUPPORT AT BS 229. FABRICATED AND INSTALLED REPAIR DOUBLER ON SUB-FLOOR IAW DC9 SRM 53-11-1, 53-01 FIG 2, 51-10-3, 51-30-2, AND 51-10
- [SDR AT9900787](https://openairdocs.org/sdr/AT9900787.md): Hat Channel · corroded · Oct 18, 1999 · N802AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND HAT CHANNELS ON FLOOR PANEL NR 36 CORRODED AND CRACKED. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC9 SRM 53-21 FIG 3.
- [SDR AT9900785](https://openairdocs.org/sdr/AT9900785.md): Support · corroded · Oct 18, 1999 · N802AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND FORWARD FLOOR SUPPORT AT BS 200 AND RBL 24 TO RBL 42 CORRODED. REMOVED CORRODED FLOOR SUPPORT. FABRICATED, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 53-01 FIG 1, 51-30-3, 51-10-2 AND 53-11-1 FIG 13.
- [SDR AT9900786](https://openairdocs.org/sdr/AT9900786.md): Angle · corroded · Oct 16, 1999 · N802AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND SUPPORT ANGLE AT BS 1039 CORRODED FROM RBL 4 TO RBL 15. REMOVED CORROSION, FABRICATED STACKED ANGLE REPAIR, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-2, 53-01 FIG 2, 51-30-2 AND 51-10-3.
- [SDR AT9900782](https://openairdocs.org/sdr/AT9900782.md): Panel · corroded · Oct 16, 1999 · N802AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND RT FORWARD CARGO SLANT PANEL AT BS 332-370 CORRODED OUT OF LIMITS ON UPPER SIDE AROUND FASTENER HOLES AND EDGE. REMOVED CORROSION AROUND FASTENERS AND EDGES. FABRICATED NEW SLANT PANEL. TREATED, PRIMED AND REINSTALLED IAW DC9 SRM 53-01 FIG 1, 51-10-3
- [SDR AT9900784](https://openairdocs.org/sdr/AT9900784.md): Angle · corroded · Oct 15, 1999 · N802AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND FLOOR SUPPORT ANGLE AT BS 160 CORRODED. REMOVED CORROSION FROM FLOOR SUPPORT ANGLE. FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR SUPPORT ANGLE IAW DC9 SRM 51-10-3, 51-10-2 AND 51-30-5.
- [SDR AT9900788](https://openairdocs.org/sdr/AT9900788.md): Support · corroded · Oct 14, 1999 · N802AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND FORWARD FLOOR SUPPORT AT BS 165-200 AND LBL 44 CORRODED. REMOVED CORRODED FLOOR SUPPORT, FABRICATED, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-10-2, 51-10-3 AND 51-30-5.
- [SDR AT9900749](https://openairdocs.org/sdr/AT9900749.md): Web · corroded · Oct 13, 1999 · N802AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FORWARD CARGO DOOR CUTOUT UPPER WEB AT BS 389 HAD CORROSION UNDERNEATH WEB AT FLOORBEAM. REMOVED CORROSION FROM WEB, FABRICATED REPAIR DOUBLER, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-10-3, 51-30-2 AND 53-01 FIG 2.
- [SDR AT9900748](https://openairdocs.org/sdr/AT9900748.md): Cusp Web · corroded · Oct 13, 1999 · N802AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND CUSP WEB AT BS 256 AND L18L CORRODED AT INTERSECTION OF SUBFLOOR AND SIDEWALL PANELS. REMOVED CORRODED AREA OF CUSP WEB AND REMOVED FRAME-TO-CUSP FITTING. FABRICATED REPAIR DOUBLER FOR CUSP WEB. REPLACED FRAME-TO-CUSP FITTING. INSTALLED REPAIR DOUBLE
- [SDR AT9900783](https://openairdocs.org/sdr/AT9900783.md): Support · corroded · Oct 12, 1999 · N802AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND FLOORBOARD SUPPORT CORRODED AT BS 160-197. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-10-2, 51-10-3, 51-30-1 AND 51-30-2.
- [SDR AT9900747](https://openairdocs.org/sdr/AT9900747.md): Bracket · corroded · Oct 12, 1999 · N802AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND FORWARD LAVATORY WALL ATTACH L BRACKETS CORRODED. FABRICATED ANGLE REPAIR, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-2 AND 51-10-3.
- [SDR AT9900725](https://openairdocs.org/sdr/AT9900725.md): Strap · corroded · Oct 8, 1999 · N802AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND FORWARD CARGO FLOOR PANEL TIE-DOWN STRAPS AT BS 351-465 CORRODED. REMOVED CORROSION, OBTAINED NEW TIE-DOWN EXTRUSION, DRILLED, COUNTERSUNK, DEBURRED, TREATED, PRIMED AND INSTALLED TIE-DOWN STRAPS IAW DC9 SRM 51-10-2, 51-10-3, 51-10-4 AND 53-05 FIG 4C.
- [SDR AT9900724](https://openairdocs.org/sdr/AT9900724.md): Skin · corroded · Oct 7, 1999 · N802AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN JUST FORWARD OF TAIL CONE EXTERIOR JETTISON HANDLE AT BS 1143 CORRODED. REMOVED CORROSION, FABRICATED REPAIR DOUBLER, TREATED, PRIMED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-30-3, 53-01 FIG 2, 51-10-3.
- [SDR AT9900723](https://openairdocs.org/sdr/AT9900723.md): Support · corroded · Oct 7, 1999 · N802AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND TOP SURFACE OF UPPER FLOORBOARD SUPPORT AT BS 200 - 237 CORRODED. REMOVED OLD FLOOR SUPPORT, FABRICATED REPAIR SUPPORT, DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED REPAIR SUPPORT. WORK DONE IAW DC9 SRM 51-30-2, 51-10-1 AND 51-30-2.
- [SDR AT9900750](https://openairdocs.org/sdr/AT9900750.md): Floor · corroded · Oct 2, 1999 · N802AT · Doug DC932 · Fuselage Floor Panel
  > FOUND RT INBOARD FLOOR PANEL AT BS 579-617 CORRODED. FLOOR PANEL HAT SECTION CORRODED ON SQUARE ENDS AND ANGLED ENDS. MOST OF THE FASTENER HOLES ON THE TOP OF THE FLOOR PANEL HAVE CORROSION AND CIRCULAR WEAR GROOVES. REMOVED CORROSION FROM AROUND FASTENER
- [SDR AT0000188](https://openairdocs.org/sdr/AT0000188.md): Channel · corroded · Sep 28, 1999 · N802AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FLOOR PANEL RIGHT INBOARD HAT SECTION AT BS 579 - 617 CORRODED. FOUND OUT OF LIMITS AFTER CORROSION REMOVAL. INSTALLED NEW HAT SECTIONS IAW DC9 SRM 53-01, 51-10-04, AND 53-21.
- [SDR AT9900789](https://openairdocs.org/sdr/AT9900789.md): Step · corroded · Sep 23, 1999 · N802AT · Doug DC932 · Entrance Stairs
  > FOUND SECOND STEP FROM TOP OF VENTRAL STAIRS CORRODED. REMOVED STEP, REMOVED SUPPORT ANGLES, FABRICATED AND INSTALLED NEW SUPPORT ANGLES, PREPARED AND INSTALLED NEW STEP. FABRICATED AND INSTALLED REPAIR DOUBLER IAW TIMCO EO 99-1313, DC9 SRM 52-60-0 FIG 2, 51
- [SDR AT9900551](https://openairdocs.org/sdr/AT9900551.md): Cable · disconnected · Aug 5, 1999 · N802AT · Doug DC932 · Aerodynamic Fairings
  > TAILCONE UNSAFE LIGHT CAME ON AFTER TAKEOFF. RETURNED TO ATLANTA. RE-INSERTED CABLE BALL END INTO TAILCONE RELEASE HANDLE IAW MM 52-21. RII ACCOMPLISHED.

## 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 = 'N802AT' AND deregistration_id = 'N802AT-2003-05-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N802AT-2003-05-09/reports

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