# Service difficulty reports: N836AT, cancelled Dec 16, 2005

A list on [N836AT, cancelled Dec 16, 2005](https://openairdocs.org/deregistered/N836AT-2005-12-16.md).

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

- [SDR AT0300028](https://openairdocs.org/sdr/AT0300028.md): Engine · unserviceable · Sep 27, 2003 · N836AT · Doug DC932 · Engine (Turbine/Turboprop)
  > LOW OIL PRESSURE AND LOSS OF QUANTITY DURING CLIMB OUT AT 16,000 AND 300 KNOTS. REMOVE AND REPLACED THE NR 2 ENGINE
- [SDR AT0300017](https://openairdocs.org/sdr/AT0300017.md): Door · malfunctioned · Jun 12, 2003 · N836AT · Doug DC932 · Nose/Tail Landing Gear
  > LOUD VIBRATION WHEN GEAR CAME UP. FOUND RT NLG DOOR HANGING DOWN. PERFORMED VISUAL INSPECTION OF DOORS AND HINGE AREA. NO DEFECTS NOTED. CLOSED NOSE GEAR DOORS PER STANDARD PRACTICES OUTLINED IN DC9 MM 32-00. DOORS REMAINED LOCKED NORMALLY.
- [SDR AT0200074](https://openairdocs.org/sdr/AT0200074.md): Web · corroded · Aug 18, 2002 · N836AT · Doug DC932 · Fuselage Miscellaneous Structure
  > HEAVY CORRODED SUBFLOOR PANEL AND INCLUDING AREA BELOW SEAT TRACK AT STA 230 TO 305 RBL 44. CUT OUT CORROSION ON SUBFLOOR, AND INSTALLED REPAIR IAW DC-9 SRM 53-01.
- [SDR AT0200073](https://openairdocs.org/sdr/AT0200073.md): Floor Panel · corroded · Aug 18, 2002 · N836AT · Doug DC932 · Fuselage Floor Panel
  > HEAVY CORRODED FLOOR PANEL STA 230 TO 305, RBL 44 TO RBL 56. REMOVED AND REPLACED SKIN ON FLOOR PANEL IAW DC-9 SRM 51-30-2.
- [SDR AT0100244](https://openairdocs.org/sdr/AT0100244.md): Engine · failed · Dec 22, 2001 · N836AT · Doug DC932 · Engine (Turbine/Turboprop)
  > FOUND NR 1 ENGINE LOST OIL QUANTITY. OIL TEMPERATURE WENT UP AND OIL PRESSURE WENT DOWN. ENGINE WAS SHUT DOWN, ENGINE TURNED FOR 25-30 MINUTES AT LESS THAN 10 PSI. REMOVED AND REPLACED THE NR 1 ENGINE IAW DC9 72-00.
- [SDR AT0100243](https://openairdocs.org/sdr/AT0100243.md): O-Ring · inoperative · Dec 20, 2001 · N836AT · Doug DC932 · Engine Oil Pressure
  > FOUND #1 ENGINE LOST ALL OIL, SHUT DOWN #1 ENGINE AT 38 PSI OIL PRESSURE-ALL OTHER ENGINE PARAMETERS DID NOT EXCEED ILIMITATIONS. CORRECTIVE ACTION: FOUND BAD O-RING ON GEAR BOX TO OIL COOLER. REPLACED O-RING. IAW DC9 MM 79-20-2
- [SDR AT0100220](https://openairdocs.org/sdr/AT0100220.md): Door · open · Jul 13, 2001 · N836AT · Doug DC932 · Landing Gear Doors
  > LOUD RUMBLE AFTER TAKE-OFF. CORRECTIVE ACTION: INSPECTED NOSE LANDING GEAR DOOR LINKAGE, HINGES AND NO DEFECTES NOTED. CLOSED NOSE LANDING GEAR DOOR AND CONFIRMED LATCH CHECK. IAW DC9 MM 32-00, 52-00
- [SDR AT0100180](https://openairdocs.org/sdr/AT0100180.md): Door Frame · cracked · May 29, 2001 · N836AT · Doug DC932 · Fuselage Main, Structure
  > FOUND AFT PRESSURE BULKHEAD DOOR JAMB CRACKED. REMOVED UPPER DOOR JAMB AND FRAME IAW DC9 SRM 53-05, 53-01, AND SB 53-137 REV A DRAWING JD600-88.
- [SDR AT0100181](https://openairdocs.org/sdr/AT0100181.md): Bulkhead · corroded · May 25, 2001 · N836AT · Doug DC932 · Fuselage Main, Bulkhead
  > FOUND AFT PIT BULKHEAD LEFT AND RIGHT PANELS CORRODED BEYOND LIMITS. INSTALLED DOUBLER IAW DC9 SRM 53-01 FIG 2, 53-01 FIG 1, AND 51-10-03.
- [SDR AT0000476](https://openairdocs.org/sdr/AT0000476.md): Spar · corroded · Nov 1, 2000 · N836AT · Doug DC932 · Wing Spar
  > DURING A SCHEDULED INSPECTION. FOUND RIGHT WING REAR SPAR CORRODED INBOARD OF CENTER FLAP SUPPORT FITTING. CUT AND REMOVED CORROSION. FABRICATED AND INSTALLED AFT AND FORWARD SPLICES IAW REO L-00303, REV A, PART 1A.
- [SDR AT0000464](https://openairdocs.org/sdr/AT0000464.md): Bulb · inoperative · Nov 1, 2000 · N836AT · Doug DC932 · Emergency Lighting
  > RIGHT EMERGENCY LIGHT IN VENTRAL STAIR EXIT PASSAGE IS INOPERATIVE. RELAMPED.
- [SDR AT0000444](https://openairdocs.org/sdr/AT0000444.md): Light · inoperative · Oct 6, 2000 · N836AT · Doug DC932 · Emergency Lighting
  > AFT ENTRY LEFT EMERGENCY LIGHT OUT. SECURED GROUND WIRE AT AFT ENTRY DOOR EMERGENCY LIGHT IAW DC9 MM 20-50.
- [SDR AT0000349](https://openairdocs.org/sdr/AT0000349.md): Door · open · Jul 1, 2000 · N836AT · Doug DC932 · Landing Gear Door Retract Section
  > FELT STRONG VIBRATION IN COCKPIT AFTER GEAR RETRACTION. SLOWED AIRCRAFT AND CYCLED GEAR, NO HELP. FOUND NOSE GEAR DOOR OPEN, INSPECTED NOSE GEAR FOR DAMAGE, NONE FOUND. CLOSED AND SECURED BOTH NOSE GEAR DOORS IAW DC9 MM 32-20-0.
- [SDR AT0000208](https://openairdocs.org/sdr/AT0000208.md): Psu · malfunctioned · Apr 14, 2000 · N836AT · Doug DC932 · Cabin Pressure Control System
  > DURING CRUISE LEFT PACK TURNED OFF, RIGHT PACK WOULD NOT HOLD CABIN ALTITUDE. CABIN MASKS DROPPED. RIGHT HAND PRESSURE LINE TO PRESSURE REGULATOR CAME LOOSE, INSTALLED NEW RUBBER DUCT, LEAK CHECKED GOOD. CLEANED AND REINSTALLED CABIN O2 MASK. DURING FUNCT
- [SDR AT0000060](https://openairdocs.org/sdr/AT0000060.md): Longeron · corroded · Jan 27, 2000 · N836AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LONGERON IN E&E COMPARTMENT BETWEEN BS 200-218 LONGERON 28 CORRODED BEYOND LIMITS. REMOVED DAMAGED AREA AND SPLICED IN NEW REPAIR AT BS 200-218 LONGERON 28 IAW DC9 SRM 53-02 FIG 18, 55-01 FIG 1, 51
- [SDR AT0000065](https://openairdocs.org/sdr/AT0000065.md): Frame · cracked · Jan 26, 2000 · N836AT · Doug DC932 · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND RIGHT MAIN FRAME AT BS 699 IN AFT POCKET POINT F TO D, POINT M-B-A, AND POINT G-H CRACKED. REMOVED AND REPLACED RIGHT MAINFRAME AT BS 699 IAW DC9 SRM 51-30-01, 51-30-02, AND 51-30-05.
- [SDR AT0000061](https://openairdocs.org/sdr/AT0000061.md): Door Jamb · corroded · Jan 26, 2000 · N836AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON FORWARD CARGO LOWER DOOR JAMB. REMOVED AND REPLACED LOWER CARGO DOOR JAMB IAW DC9 SRM 51-10-04, 51-10-03, AND 53-05 FIG 4A.
- [SDR AT0000052](https://openairdocs.org/sdr/AT0000052.md): Frame · corroded · Jan 24, 2000 · N836AT · Doug DC932 · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON FRAME AT BS 237 LONGERON 30. AFTER REMOVAL OF CORROSION, FOUND FRAMEOUT OF LIMITS. REMOVED AND REPLACED DAMAGED SECTION OF FRAME AT BS 237 LONGERON 30 IAW DC9 SRM 5 3-01 FIG 1, 53-03
- [SDR AT0000190](https://openairdocs.org/sdr/AT0000190.md): Cap · corroded · Jan 22, 2000 · N836AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND RIGHT MAIN TANK TEE CAP TO HAVE CORROSION BEYOND LIMITS FROM STRINGER 11 TO STRINGER 23. REMOVED AND REPLACED RIGHT TEE CAP IAW DC9 SB 57-98.
- [SDR AT0000051](https://openairdocs.org/sdr/AT0000051.md): Frame · corroded · Jan 22, 2000 · N836AT · Doug DC932 · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND AFT PIT AT BS 965 LS 23 FRAME CORRODED. REMOVED AND REPLACED CORRODED SECTION OF FRAME WITH NEW FRAME AT BS 965 LS 23 IAW DC9 SRM 51-30-02, 51-30-05, 51-10-04, 53-03 FIG 2A, AND 51-30-01.
- [SDR AT0000050](https://openairdocs.org/sdr/AT0000050.md): Skin · corroded · Jan 19, 2000 · N836AT · Doug DC932 · Vertical Stabilizer, Plate/Skin
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON PANEL NR 6402 OUT OF LIMITS. FABRICATED AND INSTALLED SKIN FOR PANEL NR 6402 IAW DC9 SRM 55-01 FIG 1, 51-70-02, AND 51-10-03.
- [SDR AT0000049](https://openairdocs.org/sdr/AT0000049.md): Longeron · corroded · Jan 19, 2000 · N836AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LONGERON NR 30 CORRODED BETWEEN STATIONS 200 AND 218 AFTER REMOVAL OF CORROSION, FOUND LONGERON OUT OF LIMITS. CUT OUT DAMAGED AREA AND INSTALLED LONGERON SPLICE IAW DC9 SRM 51-10-03, 52-01 FIG 1,
- [SDR AT0000048](https://openairdocs.org/sdr/AT0000048.md): Spar · cracked · Jan 19, 2000 · N836AT · Doug DC932 · Elevator, Spar/Rib
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CRACK ON RIGHT ELEVATOR SPAR AT ES 76-75. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLES AT ES 76-75 IAW EO 12-5520-29-B1092, DC9 SRM 51-20, 51-30-02, 51-20-03, AND 55-02.
- [SDR AT0000028](https://openairdocs.org/sdr/AT0000028.md): Floor Board · corroded · Jan 14, 2000 · N836AT · Doug DC932 · Fuselage Floor Panel
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND RIGHT SIDE CABIN FLOORBOARD CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED NEW FLOORBOARD IAW DC9 SRM 53-01 FIG 1, 51-10-03, 51-10-04, AND 51-30-02.
- [SDR AT0000027](https://openairdocs.org/sdr/AT0000027.md): Bracket · corroded · Jan 11, 2000 · N836AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND INTERCOSTAL BRACKET AT BS 433 L-28R CORRODED BEYOND LIMITS. REMOVED AND REPLACED BRACKET AT BS 433 L-28R IAW DC9 SRM 51-10-04, 51-10-03, AND 51-30-05.
- [SDR AT9900881](https://openairdocs.org/sdr/AT9900881.md): Battery · discharged · Dec 3, 1999 · N836AT · Doug DC932 · Emergency Lighting
  > FOUND BOTH SIDES FORWARD UPPER CABIN EMERGENCY EXIT DOOR, EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERIES IAW DC9 MM 33-53-0.
- [SDR AT9900838](https://openairdocs.org/sdr/AT9900838.md): Oxygen Mask · failed · Nov 28, 1999 · N836AT · Doug DC932 · Passenger Oxygen System
  > DURING OXYGEN MASK INSPECTION TO COMPLY WITH EO 9-3520-29-E1461, PASSENGER OXYGEN MASKS ABOVE SEAT POSITION 28-DEF AND AFT F/A STATION DID NOT DEPLOY. CLEANED EXCESSIVE PAINT OFF DOOR OF AFT F/A O2 MASK COMPARTMENT. RE-ATTACHED LOOSE HOSE TO MANIFOLD IN PSU
- [SDR AT9900799](https://openairdocs.org/sdr/AT9900799.md): Retract Mech · malfunctioned · Nov 1, 1999 · N836AT · Doug DC932 · Landing Gear Door Retract Section
  > AFTER TAKEOFF AND UPON GEAR RETRACTION A FLUTTER NOISE CAME FROM THE NOSE GEAR AREA. FOUND RIGHT NOSE GEAR DOOR OPEN. VISUALLY INSPECTED NOSE GEAR DOORS AND WHEEL WELL. FOUND NOTHING ABNORMAL. CLOSED GEAR DOOR. OK FOR SERVICE PER MM 52-80.
- [SDR AT9900494](https://openairdocs.org/sdr/AT9900494.md): Batteries · discharged · Jul 14, 1999 · N836AT · Doug DC932 · Emergency Lighting
  > FOUND FORWARD SERVICE DOOR AREA OVERHEAD EMERGENCY LIGHT DIM. REPLACED BATTERIES ON EMERGENCY DOOR LIGHT, OPS CHECK GOOD IAW MM 33-53-0.

## 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 = 'N836AT' AND deregistration_id = 'N836AT-2005-12-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N836AT-2005-12-16/reports

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