# Service difficulty reports: N810AT, cancelled Dec 19, 2002

A list on [N810AT, cancelled Dec 19, 2002](https://openairdocs.org/deregistered/N810AT-2002-12-19.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 2 · 54 reports

- [SDR AT0200076](https://openairdocs.org/sdr/AT0200076.md): Battery · Sep 5, 2002 · N810AT · Doug DC932 · Emergency Lighting
  > CEILING EMERGENCY LIGHTS OUT ROWS 1-15. CORRECTIVE ACTION: REMOVED AND REPLACED BATTERIES IN B5-24 AND B5-32, OPS CHECK GOOD PER MM 33-50.
- [SDR AT0100241](https://openairdocs.org/sdr/AT0100241.md): Battery Pack · discharged · Dec 11, 2001 · N810AT · Doug DC932 · Emergency Lighting
  > FOUND AFT ACC COMPARTMENT EMERGENCY LIGHT WILL NOT SHUT OFF. CORRECTIVE ACTION: REPLACED BATTERY PACK CHARGER, B5-28. IAW DCI MM 33-53, 56
- [SDR AT0100229](https://openairdocs.org/sdr/AT0100229.md): Wire · broken · Sep 15, 2001 · N810AT · Doug DC932 · Light System Wiring
  > FOUND FORWARD RED LIGHTS OF THE PASSENGER EMERGENCY EGRESS PATH LIGHTING SYSTEM INOPERATIVE. REPAIRED BROKEN WIRE AT FORWARD LEFT PORTION OF TRACK IAW DC9 MM 33-50.
- [SDR AT0000379](https://openairdocs.org/sdr/AT0000379.md): Bulb · failed · Aug 20, 2000 · N810AT · Doug DC932 · Emergency Lighting
  > FOUND L-1 EMERGENCY POST LIGHT INOPERATIVE. RELAMPED.
- [SDR AT0000211](https://openairdocs.org/sdr/AT0000211.md): Skin · cracked · Apr 20, 2000 · N810AT · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND PASSENGER DOOR CUTOUT REPAIR NOT DONE IAW DC9 SRM 53-05 FIG 26A. INSTALLED NEW REPAIR IAW DC9 SRM 53-05 FI G 26A AND REO-L00142.
- [SDR AT0000207](https://openairdocs.org/sdr/AT0000207.md): Stringer · corroded · Apr 11, 2000 · N810AT · Doug DC932 · Wing, Longeron/Stringer
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND RIGHT WING TANK INTERNAL STRUCTURE AT XCW 58.5 STRINGER 22 TO HAVE MULTIPLE CORROSION BLEND OUTS. REMOVED AND REPLACED STRINGER 22 IAW DC9 SRM 57-08 FIG 2, 51-30-05, 51-30-01, 51-10-04, AND 51-22-0
- [SDR AT0000206](https://openairdocs.org/sdr/AT0000206.md): Floorbeam · corroded · Mar 31, 2000 · N810AT · Doug DC932 · Fuselage Main, Floor Beam
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FLOORBEAM AT BS 996 LBL 45 CORRODED BEYOND LIMITS. REPLACED UPPER ANGLE AT BS 996 LBL 45 IAW DC9 SRM 51-01, 51-30-02, 51-30-05, AND 51-30-04.
- [SDR AT0000200](https://openairdocs.org/sdr/AT0000200.md): Floorbeam · corroded · Mar 31, 2000 · N810AT · Doug DC932 · Fuselage Main, Floor Beam
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FLOORBEAM AT BS 996 LBL 25 AND LBL 45 TO BE CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW DC9 SRM 51-30-02, 51-30-05, 51-10-04, 51-10-03, AND 20-16.
- [SDR AT0000201](https://openairdocs.org/sdr/AT0000201.md): Stringer · corroded · Mar 30, 2000 · N810AT · Doug DC932 · Wing, Longeron/Stringer
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND RIGHT WING TANK STRINGER 23 XCW 58.5 TO HAVE MULTIPLE CORROSION AREAS. CORRECTIVE ACTION: INSTALLED NEW STRINGER AND SPLICE PLATES AT XCW 58
- [SDR AT0000176](https://openairdocs.org/sdr/AT0000176.md): Step · corroded · Mar 30, 2000 · N810AT · Doug DC932 · Entrance Stairs
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND NR 1AFT STEP ON AFT STAIRS TO BE CORRODED BEYOND LIMITS. REMOVED AND REPLACED NR 1 AFT STEP IAW 51-30-01.
- [SDR AT0000169](https://openairdocs.org/sdr/AT0000169.md): Stringer · corroded · Mar 30, 2000 · N810AT · Doug DC932 · Wing, Longeron/Stringer
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LEVEL 2 CORROSION ON RIGHT WING TANK XCW 58.5 STRINGER 23 BARREL NUT HOLE. INSTALLED NEW STRINGER NR 23 XCW 58.5 IAW DC9 SRM 51-30-05, 51-10-03, 51-10-02, 51-10-02, 51-10-04, AND 57-08 FIG 2.
- [SDR AT0000166](https://openairdocs.org/sdr/AT0000166.md): Floorbeam · corroded · Mar 30, 2000 · N810AT · Doug DC932 · Fuselage Main, Floor Beam
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CABIN FLOOR SUPPORT CORRODED BEYOND LIMITS AT BS 180, RBL 1 - 39. CORRECTIVE ACTION: REMOVED, FABRICATED, AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-10-02, 51-10-03, AND 51-30-05.
- [SDR AT0000175](https://openairdocs.org/sdr/AT0000175.md): Floor Support · corroded · Mar 29, 2000 · N810AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CABIN FLOOR SUPPORT AT BS 165-230 BL 0 TO HAVE LEVEL 2 CORROSION. INSTALLED NEW FLOOR SUPPORT AT BS 165 - 230 BL 0 IAW DC9 SRM 53-11-01, 51-10-02, 51-10-03, 51-10-04, AND 51-30-05.
- [SDR AT0000165](https://openairdocs.org/sdr/AT0000165.md): Web · corroded · Mar 29, 2000 · N810AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LOWER WEB AT BS 965 TO HAVE LEVEL 2 EXFOLIATION CORROSION. INSTALLED NEW WEB IAW DC9 SRM 51-10-04, 53-11-03, 51-10-03, AND 51-10-02.
- [SDR AT0000204](https://openairdocs.org/sdr/AT0000204.md): Floorbeam · corroded · Mar 28, 2000 · N810AT · Doug DC932 · Fuselage Main, Floor Beam
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CABIN FLOORBEAM AT BS 160 RBL 6 AND RBL 44 CORRODED BEYOND LIMITS. REPLACED FLOOR SUPPORT IAW DC9 SRM 51-30-02, 51-10-03, 51-30-05, 51-10-02, AND 53-11-01.
- [SDR AT0000164](https://openairdocs.org/sdr/AT0000164.md): Floor Support · corroded · Mar 28, 2000 · N810AT · Doug DC932 · Fuselage Main, Floor Beam
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CABIN FLOOR SUPPORT CORRODED BEYOND LIMITS AT BS 176 - 185, LBL 44. CORRECTIVE ACTION: REMOVED, FABRICATED, AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-30-02, 51-10-02, 51-10-03,
- [SDR AT0000162](https://openairdocs.org/sdr/AT0000162.md): Floorbeam · corroded · Mar 28, 2000 · N810AT · Doug DC932 · Fuselage Main, Floor Beam
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CABIN FLOOR SUPPORT CORRODED AT BS 200, RBL 1 - 57. CORRECTIVE ACTION: REMOVED AND FABRICATED NEW FLOOR SUPPORT IAW DC9 SRM 53-11-01, 51-30-05, 51-30-02, 51-10-04, AND 51-10-03.
- [SDR AT0000168](https://openairdocs.org/sdr/AT0000168.md): Floorbeam · corroded · Mar 26, 2000 · N810AT · Doug DC932 · Fuselage Main, Floor Beam
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CABIN FLOOR SUPPORT CORRODED BEYOND LIMITS AT BS 161 - 197, RBL 44. CORRECTIVE ACTION: REMOVED, FABRICATED, AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-30-02, 51-10-30, AND 5
- [SDR AT0000167](https://openairdocs.org/sdr/AT0000167.md): Floorbeam · corroded · Mar 25, 2000 · N810AT · Doug DC932 · Fuselage Main, Floor Beam
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CABIN FLOOR SUPPORT CORRODED BEYOND LIMITS AT BS 196, LBL 1-38. CORRECTIVE ACTION: REMOVED, FABRICATED, AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-30-02, 51-10-02, 51-10-03, AND 51-30-
- [SDR AT0000150](https://openairdocs.org/sdr/AT0000150.md): Strap · corroded · Mar 21, 2000 · N810AT · Doug DC932 · Wing Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON NUTPLATE STRAP UPPER SPAR CAP WS 445 - 430. AFTER REMOVAL OF CORROSION FOUND MATERIAL OUT OF LIMITS. CORRECTIVE ACTION: FABRICATED AND INSTALLED NEW STRAP IAW DC9 SRM 51-30-02, 51
- [SDR AT0000122](https://openairdocs.org/sdr/AT0000122.md): Light · inoperative · Mar 14, 2000 · N810AT · Doug DC932 · Emergency Lighting
  > FOUND LEFT TAILCONE EMERGENCY FLOOD LIGHT INOPERATIVE. CORRECTIVE ACTION: RELAMPED IAW MM 33-50.
- [SDR AT0000011](https://openairdocs.org/sdr/AT0000011.md): Psu · failed · Nov 19, 1999 · N810AT · Doug DC932 · Passenger Oxygen System
  > WHILE ACCOMPLISHING WORK ORDER 55311, SEVERAL PSU OXYGEN DOORS DID NOT DEPLOY WHEN SYSTEM WAS ACTIVATED. SEVERAL OXYGEN MASKS WERE FOUND UNSERVICEABLE. REPAIRED OR REPLACED THE AFFECTED PSU'S AND REPLACED ALL UNSERVICEABLE MASKS IAW EO 9-3520-29-E1461 REV A.
- [SDR AT9900633](https://openairdocs.org/sdr/AT9900633.md): Apu · failed · Sep 1, 1999 · N810AT · Doug DC932 · APU Core Engine
  > AT 5,000 FEET DURING CLIMB, SMOKE FILLED THE COCKPIT AND CABIN. AIRCRAFT RETURNED TO AIRPORT. FOUND CRACK IN TAURUS. REMOVED AND REPLACED APU. OPS CHECK AND LEAK CHECK GOOD IAW 49-10-0.
- [SDR AT9900274](https://openairdocs.org/sdr/AT9900274.md): Connector · dirty · Apr 1, 1999 · N810AT · Doug DC932 · Emergency Lighting
  > RIGHT HAND NACELLE LIGHT WILL NOT ILLUMINATE WHEN EMERGENCY LIGHT SWITCH IS TURNED ON. CLEANED CANNON PLUG PINS AT BATTERY PACK PER MM 33-35-0, OPS CHECKS GOOD.
- [SDR AT9900072](https://openairdocs.org/sdr/AT9900072.md): Brakes · malfunctioned · Jan 30, 1999 · N810AT · Doug DC932 · Landing Gear Brake System
  > UPON LANDING EVERYTHING WAS NORMAL, ON TAXI-IN IT FELT LIKE BRAKES WERE APPLIED, IT WOULD TAKE A SECOND OR TWO FOR IT TO RELEASE. AT NO TIME DID THE BRAKES DRAG TO THE EXTEND THAT THEY WERE GOING TO IGNITE. ON ARRIVAL AT THE GATE THE BRAKES WERE SMOKING. T
- [SDR AT9900020](https://openairdocs.org/sdr/AT9900020.md): Skin · dented · Jan 12, 1999 · N810AT · Doug DC932 · Fuselage Main, Plate/Skin
  > SCHEDULED INSPECTION AT AERO CORP FL, FUSELAGE SKIN HAS NUMEROUS DENTS FROM FS 229 TO FS 589 RIGHT SIDE. REMOVED AND REPLACED FUSELAGE SKIN FS 229 TO 589 RIGHT SIDE IAW RES 982130 AND RES 982249. SKIN (P/N 5920-119-5).
- [SDR AT9900015](https://openairdocs.org/sdr/AT9900015.md): Frame · corroded · Jan 9, 1999 · N810AT · Doug DC932 · Fuselage Main, Frame
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND STA 996 FRAME CORRODED UNDER LAVATORY NEXT TO FLOORBEAM ATTACHMENT RIGHT SIDE. FABRICATED AND INSTALLED FLOORBEAM SPLICE REPAIR AND WEB REPAIR AT FS 996 RIGHT HAND BL 10-55 IAW DC9 SRM 51-30, 51-10-3, 51-10-4, RES
- [SDR AT9900069](https://openairdocs.org/sdr/AT9900069.md): Skin · corroded · Jan 5, 1999 · N810AT · Doug DC932 · Elevator, Plate/Skin
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND RIGHT ELEVATOR OUTBOARD LOWER SIDE CORRODED. REPAIRED RIGHT ELEVATOR OUTBOARD LOWER SKIN BY FABRICATING SKIN AND FINGER DOUBLER. INSTALLED AND BALANCED IAW DC9 SRM 55-03 FIG 14 AND 51-30-2, 55-20-01.
- [SDR AT9900041](https://openairdocs.org/sdr/AT9900041.md): Doubler · misrepaired · Dec 30, 1998 · N810AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. EXISTING REPAIR AT LEFT HAND STA 965 L-13L AND L-14L DOES NOT FACILITATE FOR HOLE PATTERN REQUIRED IN FRAME AND FORMER MODIFICATION 53-140. REMOVED EXISTING REPAIR, FABRICATED INTERNAL AND EXTERNAL SKIN DOUBLER, DRILLED
- [SDR AT9900066](https://openairdocs.org/sdr/AT9900066.md): Skin · gouged · Dec 29, 1998 · N810AT · Doug DC932 · Landing Gear Doors
  > SCHEDULED INSPECTION AT AERO CORP, FL. NOSE LANDING GEAR DOOR RIGHT UPPER FORWARD OUTBOARD SIDE AS VIEW WITH DOOR CLOSED HAS A GOUGE IN SKIN ABOVE ACTUATOR ATTACH POINT. REMOVED, FABRICATED REPAIR AND INSTALLED IAW DC9 SRM 51-30-2, 51-10-3, 51-30-5, AND RES
- [SDR AT9900051](https://openairdocs.org/sdr/AT9900051.md): Angle · corroded · Dec 29, 1998 · N810AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND FRAME ANGLES AND CEILING SUPPORT CORRODED AT STA 943 L-30 AND STA 996 RT ABOVE CUSP WEB AND STA 965 TO 980 L-16L. REMOVED CORROSION, FABRICATED A NEW SHEAR TIE REPAIR AT STA 943. CUT OUT CORRODED SECTION ABOVE CU
- [SDR AT9900047](https://openairdocs.org/sdr/AT9900047.md): Skin · corroded · Dec 29, 1998 · N810AT · Doug DC932 · Fuselage Main, Plate/Skin
  > SCHEDULED INSPECTION AT AERO CORP, FL. CORROSION WAS FOUND BETWEEN FRAME AND SKIN AFT PIT STA 943 L-29L AND L-30L. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-01 FIG 1, 51-10-3, 53-04 FIG 12 AND RES 982285.
- [SDR AT9900007](https://openairdocs.org/sdr/AT9900007.md): Bulkhead Web · corroded · Dec 28, 1998 · N810AT · Doug DC932 · Fuselage Main, Bulkhead
  > SCHEDULED INSPECTION AT AERO CORP, FL. AFT PIT AT STA 996 SECONDARY BULKHEAD JUST UNDER FLOOR AREA AT FS 24R HAS BLOWN OUT CORROSION ON WEB. FABRICATED AND INSTALLED REPAIR IAW RES 982280, DC9 SRM 51-10-2, 51-30-2, 51-10-4 AND 51-10-3.
- [SDR AT9900068](https://openairdocs.org/sdr/AT9900068.md): Longeron · corroded · Dec 27, 1998 · N810AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND RIGHT HAND FUSELAGE EXTERIOR SKIN HAS CORROSION BULGE WITH FASTENERS HEADS POPPED AT STA 992 L-20L. FOUND LONGERON CORRODED OUT OF LIMITS, REMOVED CORRODED SECTION OF LONGERON. FABRICATED AND INSTALLED NEW SPLICE
- [SDR AT9900070](https://openairdocs.org/sdr/AT9900070.md): Angle · corroded · Dec 26, 1998 · N810AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION ON THE ATTACH ANGLE UNDER G-2 GALLEY AND OUTBOARD SIDEWALL JUST UNDER THE ELECTRICAL CONNECTOR BAY. REMOVED CORRODED ANGLE, FABRICATED AND INSTALLED NEW ATTACHED ANGLE IAW DC9 SRM 53-01 FIG 1, 51-30-2, 5
- [SDR AT9900060](https://openairdocs.org/sdr/AT9900060.md): Doubler · corroded · Dec 26, 1998 · N810AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. CORROSION WAS FOUND AROUND FASTENERS AND NUT PLATES ON FORWARD AND AFT SIDES OF FRAME STA 889 UPPER DOUBLER LONGERON 27L TO 29L. REMOVED CORRODED DOUBLER, FASTENERS, NUT PLATES, AND ANGLE. FABRICATED, PRIMED, DEBURRED,
- [SDR AT9900009](https://openairdocs.org/sdr/AT9900009.md): Skin · chafed · Dec 26, 1998 · N810AT · Doug DC932 · Vertical Stabilizer, Plate/Skin
  > SCHEDULED INSPECTION AT AERO CORP, FL. VERTICAL STABILIZER UPPER LEADING EDGE SKIN CHAFED LEFT AND RIGHT. FABRICATED REPAIR AND INSTALLED IAW RES 982239, SRM DC9 51-10-20, 55-31-0, 51-10-4, 51-10-3, 51-30-5, AND 51-20-0.
- [SDR AT9900061](https://openairdocs.org/sdr/AT9900061.md): Support · corroded · Dec 24, 1998 · N810AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT PIT FLOOR SUPPORT CORRODED AT STA 996 L-28R TO L-30R. REMOVED CORRODED AREA AND SUPPORT DUE TO MATERIAL LOSS AND OUT OF LIMITS. FABRICATED NEW SUPPORT, DRILLED, DEBURRED, PRIMED AND INSTALLED IAW DC9 SRM
- [SDR AT9900048](https://openairdocs.org/sdr/AT9900048.md): Support · corroded · Dec 22, 1998 · N810AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND NUT PLATES CORRODED ON AFT PIT FLOOR SUPPORT AT STA 813 TO STA 889 RIGHT SIDE. REMOVED AND REPLACED ALL NUT PLATES AND CLEAN ALL CORROSION. FABRICATED AFT PIT FLOOR SUPPORT CHANNEL, SPLICES, TREATED, PRIMED, REIN
- [SDR AT99000063](https://openairdocs.org/sdr/AT99000063.md): Doubler · corroded · Dec 22, 1998 · N810AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AEROCORP, FL. FOUND G-2 GALLEY TRASH BIN AREA CORRODED OUT OF LIMITS. REMOVED FASTENERS AND CORROSION IN G-2 AREA, FABRICATED DOUBLER AND INSTALLED NEW FASTENERS AND DOUBLER IAW DC9 SRM 53-01, 51-10-3 AND 51-30-2.
- [SDR AT9900054](https://openairdocs.org/sdr/AT9900054.md): Intercostal · corroded · Dec 20, 1998 · N810AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND INTERCOSTALS TO BE CORRODED AND OUT OF LIMITS AT STA 945 L-29R AND STA 976 TO 996 L-27L. REMOVED AND REPLACED, FABRICATED, INSTALLED, AND PRIMED NEW INTERCOSTALS IAW DC9 SRM 51-10-4, 51-30-2, 51-10-3, 51-30-5, AND
- [SDR AT9900064](https://openairdocs.org/sdr/AT9900064.md): Outflow Valve · corroded · Dec 18, 1998 · N810AT · Doug DC932 · Pressure Regulator/Outflow Valve
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND OUTFLOW VALVE HOUSING CORRODED AROUND NUT PLATES AND HAS SURFACE CORROSION LOWER INBOARD SIDE. REMOVED NUT PLATES AND CORROSION FOUND BEYOND LIMITS. REINSTALLED OUT FLOW VALVE IAW DC9 SRM 53-01 FIG 1, 51-10-3, AN
- [SDR AT9900062](https://openairdocs.org/sdr/AT9900062.md): Frame · corroded · Dec 18, 1998 · N810AT · Doug DC932 · Fuselage Main, Frame
  > SCHEDULED INSPECTION AT AERO CORP, FL. E/E COMPARTMENT AT FRAME STA 180 L-29L TO L-29R WAS FOUND CORRODED AT FASTENERS LOCATION. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR ANGLES AND STRAPS IAW DC9 SRM 51-10-3, 53-03 FIG 4A, 53-01 FIG 1, AND 51-30-5.
- [SDR AT9900075](https://openairdocs.org/sdr/AT9900075.md): Pan · cracked · Dec 13, 1998 · N810AT · Doug DC932 · Cargo/Baggage Doors
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CRACKS ON THE OUTER PAN FLANGE AFT CARGO DOOR AFT CENTER STOP AND ANOTHER ONE AT THE FORWARD CARGO DOOR AFT TOP (C-1 DOOR). FABRICATED, DEBURRED, PRIMED AND INSTALLED NEW DOUBLERS AND REPAIRS IAW DC9 SRM 52-03 FIG
- [SDR AT9900059](https://openairdocs.org/sdr/AT9900059.md): Jamb · corroded · Dec 12, 1998 · N810AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. THE AFT PIT DOOR THRESHOLD PAN WAS FOUND WITH CORROSION, DENTS AND PUNCTURES. REMOVED, REPLACED, INSTALLED THE DOOR PAN AND SPLICES IAW DC9 SRM 53-05 FIG 44, 51-10-4, 51-10-3, 51-30-1, AND 51-20-0.
- [SDR AT9900076](https://openairdocs.org/sdr/AT9900076.md): Longeron · cracked · Dec 11, 1998 · N810AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS CRACKS AT DIFFERENT LONGERON LOCATIONS. THE LOCATIONS ARE AS FOLLOW: STA 945 L-17R, STA 965 L-13, 16, 17R, STA 965 L-14, 17L. LONGERON (P/N 7637813-3), (P/N 2777922-4), (P/N 1A-41527-1), (P/N 2777948), S
- [SDR AT9900065](https://openairdocs.org/sdr/AT9900065.md): Bracket · corroded · Dec 11, 1998 · N810AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. THE AFT PIT DRAIN BRACKET WAS FOUND CORRODED. REMOVED AND REPLACED THE DRAIN VALVE ASSEMBLY AND BRACKET IAW DC9 SRM 51-30-2, AND 51-10-3.
- [SDR AT9900052](https://openairdocs.org/sdr/AT9900052.md): Fitting · corroded · Dec 11, 1998 · N810AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION AT END TIE AT STA 996 L-27L AND L-28L. REMOVED AND REPLACED END TIE FITTINGS, DRILLED NEW PART, DEBURRED, TREATED, PRIMED AND INSTALLED NEW PARTS IAW DC9 SRM 51-30-2, 51-30-5, 51-10-3, 51-10-4, 53-01 FIG
- [SDR AT9900074](https://openairdocs.org/sdr/AT9900074.md): Skin · dented · Dec 10, 1998 · N810AT · Doug DC932 · Fuselage Main, Plate/Skin
  > SCHEDULED INSPECTION AT AERO CORP, FL. A DENT WAS FOUND TO BE OUT OF LIMITS AT STA 338 L-28R. COLD WORKED DENT TO ORIGINAL CONTOUR, FABRICATED DOUBLER, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-3, 51-30-2, 51-10-2 AND 53-04 FIG 38.
- [SDR AT9900058](https://openairdocs.org/sdr/AT9900058.md): Floor · corroded · Dec 10, 1998 · N810AT · Doug DC932 · Fuselage Floor Panel
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT CARGO CENTER FLOOR PANEL CORRODED AND WITH ELONGATED HOLES AT STA 756 TO 794. REMOVED PANEL, FABRICATED, TREATED, PRIMED AND INSTALLED NEW FLOOR PANEL IAW DC9 SRM 51-10-2, 53-21-0 FIG 10, AND 51-10-4.

Next page: https://openairdocs.org/deregistered/N810AT-2002-12-19/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 = 'N810AT' AND deregistration_id = 'N810AT-2002-12-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N810AT-2002-12-19/reports

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