# Service difficulty reports: N824AT, cancelled Aug 22, 2013

A list on [N824AT, cancelled Aug 22, 2013](https://openairdocs.org/deregistered/N824AT-2013-08-22.md).

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

- [SDR AT0100231](https://openairdocs.org/sdr/AT0100231.md): Fire Bottle · discharged · Aug 23, 2001 · N824AT · Doug DC932 · Detection System
  > FOUND FORWARD CARGO FIRE INDICATION ILLUMINATED. CORRECTIVE ACTION: CHECKED FORWARD CARGO AREA, COULD NOT DUPLICATE PROBLEM, AICRAFT WAS FERRIED TO AVBORNE FOR REPAIRS.
- [SDR AT0100225](https://openairdocs.org/sdr/AT0100225.md): Smoke Detector · malfunctioned · Jul 15, 2001 · N824AT · Doug DC932 · Smoke Detection
  > FORWARD CARGO FIRE DETECTOR LIGHT ILLUMINATED WITH THE MASTER CAUTION LIGHT. EMERGENCY WAS DECLARED AND NR 2 FIRE BOTTLE WAS DISCHARGED AND AFT TAIL CONE SLIDE WAS DEPLOYED. INSPECTED THE FORWARD CARGO, E & E, FORWARD CABIN, AND COCKPIT AREAS FOR EVIDENCE OF
- [SDR AT0100213](https://openairdocs.org/sdr/AT0100213.md): Battery Pack · discharged · Jun 30, 2001 · N824AT · Doug DC932 · Emergency Lighting
  > FOUND EMERGENCY LIGHTS OUT ON ROWS 23, 25, AND 28. REPLACED BATTERY PACK IAW DC9 MM 33.
- [SDR AT0200004](https://openairdocs.org/sdr/AT0200004.md): Warning System · malfunctioned · May 29, 2001 · N824AT · Doug DC932 · Fire Detection
  > CARGO FIRE WARNING TONE SOUNDED WITH MASTER WARNING LIGHT ON DESCENT IN ATL. CONDITION WAS INTERMITTENT, SOUNDED TWICE WAS UNABLE TO DETERMINE WHICH LOOP. CORRECTIVE ACTION: REMOVED AND REPLACED FIRE TEST FAULT PANEL IN E/E BAY.
- [SDR AT0100098](https://openairdocs.org/sdr/AT0100098.md): Angle · cracked · Feb 22, 2001 · N824AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND FLOOR SUPPORT ANGLE CRACKED IN FORWARD PIT AT BS 218 LONGERON 28 RIGHT. FABRICATED AND INSTALLED ANGLE SUPPORT IAW DC9 SRM 51-30, 51-10-04, 51-10-03, AND 53-21 FIG 7.
- [SDR AT0100085](https://openairdocs.org/sdr/AT0100085.md): Seat Track · corroded · Feb 16, 2001 · N824AT · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND LEFT INBOARD SEAT TRACK AT BS 918 - 965 CORRODED BEYOND LIMITS. REPLACED CORRODED SECTION OF SEAT TRACK IAW DC9 SRM 53-05 FIG 4B & 4F.
- [SDR AT0100099](https://openairdocs.org/sdr/AT0100099.md): Longeron · cracked · Feb 14, 2001 · N824AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND LONGERON IN E&E COMPARTMENT CRACKED AT BS 200 LONGERON 29 RIGHT. INSTALLED LONGERON SPLICES IAW DC9 SRM 53-02 FIG 18.
- [SDR AT0100092](https://openairdocs.org/sdr/AT0100092.md): Floor Panel · corroded · Feb 14, 2001 · N824AT · Doug DC932 · Fuselage Floor Panel
  > FOUND FORWARD CABIN FLOOR PANEL BS 155 CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC9 SRM 51-10-02, 51-10-03, 51-10-04, 53-21 FIG 20 AND DC9 MM 53-20-01.
- [SDR AT0100084](https://openairdocs.org/sdr/AT0100084.md): Skin · dented · Feb 14, 2001 · N824AT · Doug DC932 · Fuselage Main, Plate/Skin
  > REPLACE TEMPORARY REPAIR WITH PERMANENT REPAIR AT BS 976. REPLACED REPAIR IAW DC SRM 53-04 FIG 12B, 51-10-03, AND 51-20.
- [SDR AT0100102](https://openairdocs.org/sdr/AT0100102.md): Skin · cracked · Feb 13, 2001 · N824AT · Doug DC932 · Cargo/Baggage Doors
  > FOUND AFT PIT CARGO DOOR INNER SKIN TORN AT AFT HINGE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 52-05, 51-30-01, 51-30-02, AND 51-30-05.
- [SDR AT0100091](https://openairdocs.org/sdr/AT0100091.md): Floor Panel · corroded · Feb 13, 2001 · N824AT · Doug DC932 · Fuselage Floor Panel
  > FOUND FLOOR PANEL 47 CORRODED BEYOND LIMITS. REPLACED FLOOR PANEL IAW DC9 SRM 53-21 AND 51-20-02.
- [SDR AT0100101](https://openairdocs.org/sdr/AT0100101.md): Longeron · cracked · Feb 9, 2001 · N824AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND LONGERON 27R CRACKED AT BS 258. FABRICATED AND INSTALLED REPAIR SPLICES IAW DC9 SRM 51-10-05, 51-10-04, AND 53-02 FIG 18.
- [SDR AT0100096](https://openairdocs.org/sdr/AT0100096.md): Web · damaged · Feb 9, 2001 · N824AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND HOLE AT NUT PLATE IN FORWARD PIT WEB BS 370 LONG 24R. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-10-03, 51-10-04, 53-01 FIG 2, 53-30-02, AND REO-L00408.
- [SDR AT0100089](https://openairdocs.org/sdr/AT0100089.md): Pan · corroded · Feb 9, 2001 · N824AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND G4 GALLEY FLOOR PAN CORRODED BEYOND LIMITS. FORMED AND INSTALLED FLOOR PAN AND HAT CHANNELS IAW DC9 SRM 51-10-03, 51-30-02, 53-01 FIG 1, AND 53-20 FIG 5C.
- [SDR AT0100088](https://openairdocs.org/sdr/AT0100088.md): Door Frame · gouged · Feb 9, 2001 · N824AT · Doug DC932 · Fuselage Main, Structure
  > FOUND FORWARD GALLEY DOOR JAMB GOUGED BEYOND LIMITS. REMOVED GOUGED SECTION AND INSTALLED REPAIR IAW DC9 SRM 53-05 FIG 55, 51-10-02, 51-10-03, 51-10-04, 51-30-01, 51-30-02, 51-30-05, AND 53-01 FIG 1.
- [SDR AT0100104](https://openairdocs.org/sdr/AT0100104.md): Panel · chafed · Feb 8, 2001 · N824AT · Doug DC932 · Vertical Stabilizer, Plate/Skin
  > FOUND VERTICAL STABILIZER UPPER FAIRING CHAFED OUT OF LIMITS. REPLACED SKIN PANEL IAW DC9 SRM 55-01 FIG 1, 55-31, 51-10-02, 51-10-03, 51-10-04, AND 51-30-02.
- [SDR AT0100103](https://openairdocs.org/sdr/AT0100103.md): Door Frame · cracked · Feb 8, 2001 · N824AT · Doug DC932 · Fuselage Main, Structure
  > FOUND AFT CARGO DOOR FRAME CRACKED. STOP DRILLED CRACK AND FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 51-10-02, 51-10-03, 51-10-04, 51-30-02, 51-30-01, AND 52-03.
- [SDR AT0100100](https://openairdocs.org/sdr/AT0100100.md): Skin · gouged · Feb 8, 2001 · N824AT · Doug DC932 · Cargo/Baggage Doors
  > FOUND AFT PIT CARGO DOOR SKIN GOUGED BEYOND LIMITS. INSTALLED REPAIR DOUBLER IAW DC9 SRM 52-05 FIG 3, 52-01 FIG 1, 51-10-04, 51-10-02, AND 51-10-03.
- [SDR AT0100097](https://openairdocs.org/sdr/AT0100097.md): Angle · corroded · Feb 8, 2001 · N824AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND RIGHT NOSE LANDING GEAR WHEEL WELL LOWER ANGLE CORRODED BEYOND LIMITS AT BS 109 RBL 27. INSTALLED REPAIR IAW REO-L00405.
- [SDR AT0100093](https://openairdocs.org/sdr/AT0100093.md): Floor Support · corroded · Feb 8, 2001 · N824AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND FORWARD CABIN FLOOR SUPPORT AT BS 200 CORRODED. REPLACED FLOOR SUPPORT IAW DC9 SRM 53-21, 53-11-01, AND 53-30-05.
- [SDR AT0100087](https://openairdocs.org/sdr/AT0100087.md): Door Frame · corroded · Feb 7, 2001 · N824AT · Doug DC932 · Fuselage Main, Structure
  > FOUND AFT CARGO DOOR JAMB CORRODED BEYOND LIMITS. INSTALLED NEW DOOR JAMB IAW DC9 SRM 53-05 FIG 44, 51-30-01, 51-30-02, 51-30-04, 51-10-03, 51-30-05, AND RES 01-220.
- [SDR AT0100086](https://openairdocs.org/sdr/AT0100086.md): Web · cracked · Feb 7, 2001 · N824AT · Doug DC932 · Fuselage Main, Structure
  > FOUND R-1 DOOR JAMB LOWER CORNER SKIN CRACKED. CUT OUT CRACK AND INSTALLED REPAIR IAW EO 09-5310-29-E1472.
- [SDR AT0100090](https://openairdocs.org/sdr/AT0100090.md): Cargo Track · corroded · Feb 6, 2001 · N824AT · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND FORWARD PIT CARGO TRACK BS 239 - 340 CORRODED BEYOND LIMITS. INSTALLED NEW SECTION OF CARGO TRACK IAW DC9 SRM 51-10-03, 51-10-04, 53-05 FIG 4C, AND 53-21.
- [SDR AT0200002](https://openairdocs.org/sdr/AT0200002.md): Controller · malfunctioned · Dec 22, 2000 · N824AT · Doug DC932 · Cabin Pressure Control System
  > CABIN CLIMBED TO 11,000 FT AND MASKS (OXYGEN) DEPLOYED. REPACKED MASK GOOD FOR SERVICE.
- [SDR AT0100004](https://openairdocs.org/sdr/AT0100004.md): Light · inoperative · Dec 20, 2000 · N824AT · Doug DC932 · Emergency Lighting
  > FOUND FORWARD EMERGENCY FLOOR LIGHT INOPERATIVE. CRIMPED BROKEN WIRE IAW 33-21.
- [SDR AT0000276](https://openairdocs.org/sdr/AT0000276.md): Battery Pack · discharged · May 18, 2000 · N824AT · Doug DC932 · Emergency Lighting
  > FOUND RIGHT ENGINE NACELLE EMERGENCY LIGHT NOT ILLUMINATING. REMOVED AND REPLACED BATTERY PACK IAW DC9 MM 33-50.
- [SDR AT0000021](https://openairdocs.org/sdr/AT0000021.md): Web · corroded · Dec 24, 1999 · N824AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND SURFACE CORROSION AND SEVERAL CRACKS IN LT CUSP WEB OUTBOARD EDGE AT BS 897 TO BS 965. REMOVED SECTION OF CUSP WEB AT BS 889-965. INSTALLED NEW CUSP WEB IAW DC9 SRM 51-30-1, 51-30-2, 51-30-5.
- [SDR AT9900914](https://openairdocs.org/sdr/AT9900914.md): Skin · lighting strike · Dec 23, 1999 · N824AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND LIGHTNING STRIKE AT FS 536 BETWEEN LONGERON 21R AND 22R ON FUSELAGE SKIN. CUTOUT STRIKE AREA. FABRICATED AND INSTALLED DOUBLER REPAIR IAW TIMCO EO 99-1445, RES 06665, SRM 51-10-1 FIG 36, 51-10-3, 51-30-5 AND 51-30-2.
- [SDR AT9900913](https://openairdocs.org/sdr/AT9900913.md): Skin Doubler · corroded · Dec 23, 1999 · N824AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND INTERNAL DOUBLER CORRODED AT BS 900 BETWEEN LONGERONS 21L AND 22L. CUTOUT CORRODED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW TIMCO EO 99-1441 AND RES 05858.
- [SDR AT0000019](https://openairdocs.org/sdr/AT0000019.md): Skin · lightning strike · Dec 21, 1999 · N824AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND LIGHTNING STRIKES AT LT CABIN WINDOW CUTOUT NR 17. FABRICATED AND INSTALLED WINDOW CUTOUT DOUBLER IAW TIMCO EO 99-1432 AND SERVICE REWORK DRAWING SR09530053.
- [SDR AT0000068](https://openairdocs.org/sdr/AT0000068.md): Tee Cap · corroded · Dec 20, 1999 · N824AT · Doug DC932 · Wing Miscellaneous Structure
  > FOUND TEE CAP IN LT WING BETWEEN STRINGER 12 AND 17 CORRODED. FABRICATED AND INSTALLED REPAIR CLIPS IAW SB 57-98R8.
- [SDR AT0000020](https://openairdocs.org/sdr/AT0000020.md): Seat Track · corroded · Dec 20, 1999 · N824AT · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > RT INBOARD SEAT TRACK CORRODED AT BS 900 TO 965. REMOVED AND REPLACED SEAT TRACK FROM BS 878 TO 965 IAW DC9 SRM 51-10-3, 53-05 FIG 4 AND 53-20-1.
- [SDR AT9900912](https://openairdocs.org/sdr/AT9900912.md): Floor Panel · corroded · Dec 13, 1999 · N824AT · Doug DC932 · Fuselage Floor Panel
  > FOUND CORROSION AROUND FASTENER HOLES ON FLOOR PANEL NR 71. FABRICATED AND INSTALLED REPAIR IAW SRM 53-3 AND 51-30-2.
- [SDR AT0000018](https://openairdocs.org/sdr/AT0000018.md): Floor Beam · chaffed · Dec 13, 1999 · N824AT · Doug DC932 · Fuselage Main, Floor Beam
  > FLOORBEAM AT BS 598 LBL 12 HAS 5 CHAFFED SPOTS. FABRICATED AND INSTALLED 1 DOUBLER, 3 SHIMS, 3 WEAR STRIPS IAW TIMCO EO 99-1415.
- [SDR AT9900911](https://openairdocs.org/sdr/AT9900911.md): Support · corroded · Dec 8, 1999 · N824AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND FLOOR SUPPORT AT BS 160 - 218 AND BL 0 CORRODED. REMOVED CORRODED FLOOR SUPPORT. FABRICATED, TRIMMED, FORMED, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED NEW FLOOR SUPPORT. WORK DONE IAW SRM 51-30-5, 51-10-4, 53-11-1 FIG 13 AND 51-30-5.
- [SDR AT0000372](https://openairdocs.org/sdr/AT0000372.md): Stringer · corroded · Dec 3, 1999 · N824AT · Doug DC932 · Wing, Longeron/Stringer
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FORWARD SIDE OF STRINGER 23 TO HAVE EXFOLIATED CORROSION. REMOVED CORRODED AREA IAW EO 99-1426 REV 1R.
- [SDR AT0000067](https://openairdocs.org/sdr/AT0000067.md): Floorbeam · corroded · Dec 3, 1999 · N824AT · Doug DC932 · Fuselage Main, Floor Beam
  > FOUND FLOOR SUPPORT AT BS 197 BL 0 TO LBL 44 HAD EXFOLIATION CORROSION. REMOVED FLOOR SUPPORT, FABRICATED, TRIMMED, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED NEW SUPPORT IAW DC9 SRM 51-10-4, 53-11-1 FIG 13, 51-10-3 AND 51-30-2.
- [SDR AT0000373](https://openairdocs.org/sdr/AT0000373.md): Web · cracked · Dec 1, 1999 · N824AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CRACK IN AFT CARGO BIN DOOR IN NR 5 WEB BEAM. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 52-01.
- [SDR AT9900639](https://openairdocs.org/sdr/AT9900639.md): O Ring · damaged · Sep 16, 1999 · N824AT · Doug DC932 · Fuel Quantity Sensor
  > ON TAKEOFF, NOTICED STRONG ODOR. FLIGHT ATTENDANT REPORTED FUMES AND SMOKE OR HAZE IN CABIN, AS ODOR DISSIPATED HAZE REMAINED. FOUND CUT O-RING ON LEFT FUEL PROBE NR 2. REMOVED AND REPLACED O-RING PER MM 2800. LEAK CHECK OK. REMOVED AND REPLACED BOTH COAL

## 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 = 'N824AT' AND deregistration_id = 'N824AT-2013-08-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N824AT-2013-08-22/reports

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