# Service difficulty reports: N818AT, cancelled Mar 8, 2002

A list on [N818AT, cancelled Mar 8, 2002](https://openairdocs.org/deregistered/N818AT-2002-03-08.md).

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

- [SDR AT0100223](https://openairdocs.org/sdr/AT0100223.md): Bulb · blown · Aug 17, 2001 · N818AT · Doug DC932 · Emergency Lighting
  > FOUND THE TAIL CONE EMERGENCY RELEASE HANDLE LIGHT INOPERATIVE. CORRECTIVE ACTION: REPLACED BULBS WITH PR4. IAW DC9 MM 33-50.
- [SDR AT0100221](https://openairdocs.org/sdr/AT0100221.md): Seal · leaking · Aug 13, 2001 · N818AT · Doug DC932 · Engine Oil Pressure
  > AT LEVEL OFF "OIL PRESSURE LOW" LIGHT FLICKERED. FOLLOWED BY LOW OIL PRESSURE INDICATION OF APPROXIMATELY 30PSI. OIL QUANTITY DROPPED TO 0 (ZERO). AT ENGINE IDLE OIL QUANTITY RETURNED TO 2 QUARTS. PRECAUTIONARY LANDING, SINGEL ENGINE OPERATION. CO
- [SDR AT0100095](https://openairdocs.org/sdr/AT0100095.md): Switch · shorted · Mar 2, 2001 · N818AT · Doug DC932 · Exterior Lighting
  > FOUND LEFT LANDING LIGHT SWITCH SHORTED INTERNALLY AND SMOKING. REPLACED LEFT LIGHT SWITCH IAW DC9 MM 33-41-01.
- [SDR AT0000316](https://openairdocs.org/sdr/AT0000316.md): Skin · corroded · Jun 16, 2000 · N818AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND SKIN CORRODED AND BULDGING AROUND RIVETS AT BS 598-664, STRINGER 29L-29R. REMOVED AND REPLACED SKIN IAW DC9 SRM 51-30-0.
- [SDR AT0000310](https://openairdocs.org/sdr/AT0000310.md): Floorbeam · corroded · May 29, 2000 · N818AT · Doug DC932 · Fuselage Main, Floor Beam
  > FOUND FLOORBEAM AT BS 160 RBL 0-55 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW TIMCO SERVICE ORDER 151057-47171.
- [SDR AT0000309](https://openairdocs.org/sdr/AT0000309.md): Longeron · cracked · May 25, 2000 · N818AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND LONGERON 6L, CRACKED AT BS 617. REMOVED CRACKED SECTION OF LONGERON, SPLICED IN NEW SECTION IAW TIMCO SERVICE ORDER 151057-49788.
- [SDR AT0000315](https://openairdocs.org/sdr/AT0000315.md): Floorboard · corroded · May 19, 2000 · N818AT · Doug DC932 · Fuselage Floor Panel
  > FOUND CABIN FLOOR CORRODED AND CRACKED. REPAIRED SKIN, FABRICATED NEW HAT CHANNELS AND INSTALLED IAW DC9 SRM 53-21-01, 51-10-4, 51-10-3, 51-10-2, 51-30-2, 51-70-1.
- [SDR AT0000314](https://openairdocs.org/sdr/AT0000314.md): Frame · corroded · May 19, 2000 · N818AT · Doug DC932 · Fuselage Main, Frame
  > FOUND CORROSION ON FRAME AT BS 889 BETWEEN 24L-23L. FABRICATED AND INSTALLED FRAME AND SPLICE ANGLE IAW DC9 SRM 51-30-1, 51-30-5, 51-10-4, 51-10-2, 51-10-2A.
- [SDR AT0000313](https://openairdocs.org/sdr/AT0000313.md): Skin · corroded · May 19, 2000 · N818AT · Doug DC932 · Nacelle/Pylon, Plate/Skin
  > FOUND LEFT PYLON, BOTTOM SIDE CORRODED. CUT OUT CORRODED AREA, FABRICATED FILLER AND DOUBLER ON TRAVELER. TREATED, PRIMED AND INSTALLED FILLER AND DOUBLER IAW DC9 SRM 54-01 FIGURE 4, 51-30-2 AND 51-10-3.
- [SDR AT0000308](https://openairdocs.org/sdr/AT0000308.md): Skin · cracked · May 19, 2000 · N818AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND A CRACK IN FUSELAGE SKIN AT RBL 18 BS 76.550. INSTALLED SKIN REPAIR IAW DWG SRO 9530239.
- [SDR AT0000312](https://openairdocs.org/sdr/AT0000312.md): Floorboard · delaminated · May 18, 2000 · N818AT · Doug DC932 · Fuselage Floor Panel
  > FOUND CABIN ENTRY FLOOR PANEL NR 4691 AT BS 160 - 200 DELAMINATED AND SPONGY. REMOVED FLOOR PANEL, FABRICATED NEW FLOOR PANEL, INSTALLED NEW FLOOR PANEL IAW TIMCO SERVICE ORDER 151057-49500.
- [SDR AT0000311](https://openairdocs.org/sdr/AT0000311.md): Door · corroded · May 18, 2000 · N818AT · Doug DC932 · Service Doors
  > FOUND RIGHT WING OUTBOARD BUTE DOOR CORRODED. REMOVED AND REPLACED BUTE DOOR IAW DC9 SRM 51-30-5.
- [SDR AT0000307](https://openairdocs.org/sdr/AT0000307.md): Floorboard · corroded · May 18, 2000 · N818AT · Doug DC932 · Fuselage Floor Panel
  > FOUND CABIN FLOOR PANEL HAS CORROSION AT PANEL 66. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC9 SRM 53-21 FIGURE 3.
- [SDR AT0000126](https://openairdocs.org/sdr/AT0000126.md): Actuator · failed · Mar 18, 2000 · N818AT · Doug DC932 · Stabilizer Actuator
  > PRIMARY HORIZONTAL TRIM ACTUATOR MOTOR INOPERATIVE. CORRECTIVE ACTION: R/R PRIMARY TRIM MOTOR IAW MM 27-40.
- [SDR AT9900833](https://openairdocs.org/sdr/AT9900833.md): Longeron · corroded · Nov 11, 1999 · N818AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND AFT CARGO COMPARTMENT LONGERON 30 AT BS 930-958 HAS CORROSION BEYOND LIMITS. REMOVED AND REPLACED LONGERON 30 AT BS 930-958 IAW DC9 SRM 53-02 FIGURE 14.
- [SDR AT9900832](https://openairdocs.org/sdr/AT9900832.md): Skin · corroded · Nov 11, 1999 · N818AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN CORRODED AT BS 954 BETWEEN L26R- S29R. REMOVED CORRODED SECTION OF SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW DC9 SRM 51-30-2, 51-10-3, 53-05, TIMCO EO 99-1369 REV IR.
- [SDR AT9900308](https://openairdocs.org/sdr/AT9900308.md): Skin · corroded · Apr 9, 1999 · N818AT · Doug DC932 · Fuselage Main, Plate/Skin
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FUSELAGE SKIN AT BS 345 L-27L CORRODED AROUND LEFT HAND ALTERNATE STATIC PORT. FABRICATED AND INSTALLED FLUSH SKIN REPAIR IAW DC9 SRM 53-04 FIG 30 AND EO NR 99-1126.
- [SDR AT9900307](https://openairdocs.org/sdr/AT9900307.md): Support · corroded · Mar 28, 1999 · N818AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOOR SUPPORT AT BS 965 CORRODED. FABRICATED FLOOR SUPPORT SECTION, FORMED DOUBLER REPAIRS AND INSTALLED IAW DC9 SRM 53-01 FIG 1, 51-10-4, 51-10-3 AND 51-30-2.
- [SDR AT9900332](https://openairdocs.org/sdr/AT9900332.md): Panel · corroded · Mar 25, 1999 · N818AT · Doug DC932 · Fuselage Main, Plate/Skin
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD PIT LEFT SLANT ACCESS PANEL COVER AT BS 340 CORRODED AND GOUGED. FABRICATED NEW ACCESS PANEL, ALODINED AND PRIMED IAW DC9 SRM 51-10-3, 51-10-2, 53-21-0 AND 51-10-4.
- [SDR AT9900298](https://openairdocs.org/sdr/AT9900298.md): Support · corroded · Mar 25, 1999 · N818AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND FLOOR SUPPORT AT BS 996 LBL-35 CORRODED. FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 53-05 FIG 20.
- [SDR AT9900262](https://openairdocs.org/sdr/AT9900262.md): Support · corroded · Mar 25, 1999 · N818AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOOR SUPPORT AT BS 996 LBL 35 CORRODED. INSTALLED FLOORBEAM REPAIR IAW DC9 SRM 53-05 FIG 20A.
- [SDR AT9900263](https://openairdocs.org/sdr/AT9900263.md): Support · corroded · Mar 24, 1999 · N818AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOOR SUPPORT AT BS 1070 CORRODED. CUT AND DRILLED REPAIR ANGLE, INSTALLED REPAIR IAW DC9 SRM 51-30-5, AND 53-05-0.
- [SDR AT9900319](https://openairdocs.org/sdr/AT9900319.md): Floor · corroded · Mar 23, 1999 · N818AT · Doug DC932 · Fuselage Floor Panel
  > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND CORROSION ON FLOOR AT BS 965 LBL-50 JUST AFT OF WALL. REMOVED CORROSION, FABRICATED NEW DOUBLER, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-3, 53-01 FIG 1, 51-10-4, 53-20-1, AND 51-30-2.
- [SDR AT9900331](https://openairdocs.org/sdr/AT9900331.md): Seat Track · corroded · Mar 22, 1999 · N818AT · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT CARGO PIT SEAT TRACK ON THE RIGHT SIDE AT BS 756-845 CORRODED. MECHANICALLY REMOVED CORROSION, DRILLED, COUNTERSINK, TREATED, AND PRIMED REPAIR TRACK IAW DC9 SRM 51-10-3, 51-10-4, AND 53-05 FIG 4C.
- [SDR AT9900330](https://openairdocs.org/sdr/AT9900330.md): Floor · corroded · Mar 22, 1999 · N818AT · Doug DC932 · Fuselage Floor Panel
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT CARGO PIT CENTER FLOOR PANEL AT BS 832-915 CORRODED, PUNCTURED AND DENTED. FABRICATED FLOOR PANEL, DRILLED, DEBURRED, ALODINED IAW DC9 SRM 51-10-2, 51-10-3 AND 53-21-0 FIG 10.
- [SDR AT9900329](https://openairdocs.org/sdr/AT9900329.md): Bracket · corroded · Mar 22, 1999 · N818AT · Doug DC932 · Rudder Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE YAW DAMPER MOUNT BRACKET CORRODED AT ALL FOUR ATTACHED LUGS. REMOVED AND REPLACED RUDDER YAW DAMPER MOUNT BRACKET, COMPLETE RUDDER SYSTEM CABLE TENSION AND RIG CHECK GOOD IAW DC9 MM 22-11-2, 20-16-0, AND 27-20
- [SDR AT9900301](https://openairdocs.org/sdr/AT9900301.md): Support · corroded · Mar 22, 1999 · N818AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FLOOR SUPPORT AT BS 965 LBL-24 CORRODED. REMOVED, FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 53-05 FIG 20, AND 53-01.
- [SDR AT9900261](https://openairdocs.org/sdr/AT9900261.md): Floorbeam · corroded · Mar 22, 1999 · N818AT · Doug DC932 · Fuselage Main, Floor Beam
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOORBEAM AT BS 965 LBL 35 CORRODED. FABRICATED NEW FLOOR SUPPORT FITTING AND INSTALLED IAW DC9 SRM 53-11-3.
- [SDR AT9900260](https://openairdocs.org/sdr/AT9900260.md): Support · corroded · Mar 22, 1999 · N818AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOOR SUPPORT AT BS 965 LBL 24 CORRODED. FABRICATED FLOOR SUPPORT REPAIR ANGLE AND INSTALLED IAW DC9 SRM 53-05 FIG 28.
- [SDR AT9900317](https://openairdocs.org/sdr/AT9900317.md): Floor · corroded · Mar 18, 1999 · N818AT · Doug DC932 · Fuselage Floor Panel
  > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE CENTER AFT FLOOR BOARD BETWEEN AFT LAVATORY AND G-4 CORRODED, CRACKED AND WORNED HAT CHANNELS. FABRICATED NEW FLOOR BOARD AND HAT CHANNELS, ALODINED, PRIMED AND INSTALLED ALL PARTS AND INSULATION IAW DC9 SRM 51
- [SDR AT9900269](https://openairdocs.org/sdr/AT9900269.md): Angle · corroded · Mar 18, 1999 · N818AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND AN L ANGLE ON THE FLOOR SUPPORT AT BS 996 RBL 29 CORRODED. REMOVED CORROSION, REMOVED AND REPLACED L ANGLE AND INSTALLED IAW DC-9 SRM 51-10-03, 51-30-02, 51-30-05, 51-10-04 AND 53-05 FIG 1.
- [SDR AT9900264](https://openairdocs.org/sdr/AT9900264.md): Floorboard · corroded · Mar 18, 1999 · N818AT · Doug DC932 · Fuselage Floor Panel
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT GALLEY FLOORBOARD AROUND THE DRAIN FITTING AT BS 996 LEFT HAND CORRODED. REPLACED SKIN AND STRINGERS IAW DC9 SRM 51-70-0, 51-10-2, AND 53-21-0.
- [SDR AT9900327](https://openairdocs.org/sdr/AT9900327.md): Bracket · corroded · Mar 17, 1999 · N818AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE NOSE LANDING GEAR PROXIMITY CABLE UPPER PULLEY BRACKET CORRODED. REMOVED AND REPLACED NOSE LANDING GEAR GROUND PROXIMITY CABLES UPPER PULLEY BRACKET IAW DC9 MM 20-16-0, 20-17-0, 32-23-1 PG 207 10A THROUGH 10D A
- [SDR AT9900318](https://openairdocs.org/sdr/AT9900318.md): Panel · corroded · Mar 17, 1999 · N818AT · Doug DC932 · Fuselage Floor Panel
  > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FLOOR BOARD PANEL NR 61D SKIN BULGING/CORRODED. FABRICATED NEW PANEL AND HAT SECTIONS, DRILLED, DEBURRED, TREATED, PRIMED ALL PARTS AND INSTALLED PANEL AND CHAFFED STRIPS IAW DC9 SRM 51-30-2, 53-21-0, 51-30-1,
- [SDR AT9900265](https://openairdocs.org/sdr/AT9900265.md): Angle · corroded · Mar 17, 1999 · N818AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOOR SUPPORT Z ANGLE ON TOP OF FLOORBEAM CRACKED AND CORRODED AT BS 965 LBL 24 TO RBL 24. REMOVED AND REPLACED TWO FLOOR SUPPORT Z ANGLES IAW DC9 SRM 51-10-4, 51-10-3, 51-10-2, 53-11-3 FIG 11 AND 51-30-2.
- [SDR AT9900328](https://openairdocs.org/sdr/AT9900328.md): Bracket · corroded · Mar 16, 1999 · N818AT · Doug DC932 · Drag Control System
  > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND PITTING CORROSION ON SPOILER MIX SUPPORT FRAME BRACKET ON LEFT WHEEL WELL. REMOVED AND REPLACED LEFT HAND WHEEL WELL SPOILER MIX SUPPORT FRAME BRACKET IAW DC9 SRM 51-10-3, MM 27-61-4, 27-10-0, 27-52-0, AND 27-61-0.
- [SDR AT9900325](https://openairdocs.org/sdr/AT9900325.md): Bracket · corroded · Mar 16, 1999 · N818AT · Doug DC932 · Aileron Control System
  > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE LEFT HAND WING AILERON RUN AROUND CABLE PULLEY BRACKET CORRODED. REMOVED AND REPLACED LEFT HAND AILERON BUS CABLE RUN AROUND PULLEY BRACKET IAW DC9 MM 27-10-0 AND 20-16-0. RIG AND OPERATIONAL CHECK GOOD IAW DC
- [SDR AT9900151](https://openairdocs.org/sdr/AT9900151.md): Wire · broken · Feb 27, 1999 · N818AT · Doug DC932 · Light System Wiring
  > FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL IN THE CABIN AFTER TAKEOFF. RETURNED TO GATE IN ATLANTA. CABIN WARNING SIGN POPS CIRCUIT BREAKER. REPAIRED BROKEN WIRE ON AFT LAVATORY RETURN TO CABIN SIGN IAW MM 33-21. ALL SYSTEMS CHECKED GOOD.

## 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 = 'N818AT' AND deregistration_id = 'N818AT-2002-03-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N818AT-2002-03-08/reports

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