# Service difficulty reports: N825AT, cancelled Jan 29, 2003

A list on [N825AT, cancelled Jan 29, 2003](https://openairdocs.org/deregistered/N825AT-2003-01-29.md).

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

- [SDR AT0200007](https://openairdocs.org/sdr/AT0200007.md): Slide · out of position · Feb 7, 2002 · N825AT · Doug DC932 · Escape Slide
  > GIRT BAR WOULD NOT LATCH AT R1 DOOR. REPOSITIONED SLIDE AT R1 DOOR.
- [SDR AT0000485](https://openairdocs.org/sdr/AT0000485.md): Regulator · inoperative · Dec 6, 2000 · N825AT · Doug DC932 · Passenger Oxygen System
  > PASSING THROUGH 260FL, FIRST OFFICER HEARD SURGE FROM PAX O2 SYSTEM. ALL MASKS DEPLOYED. CABIN ALTITUDE WAS AT 7000FT. REMOVED AND REPLACED PAX O2 CYLINDER REGULATOR. IAW DC9 MM35-20
- [SDR AT0000471](https://openairdocs.org/sdr/AT0000471.md): Duct · blown · Oct 25, 2000 · N825AT · Doug DC932 · Cabin Pressure Control System
  > EXPERIENCED PRESSURIZATION PROBLEM. CABIN ALTITUDE COULD NOT BE CONTROLLED MANUALLY, O2 MASK DEPLOYED. RETURNED TO ATL. REMOVED AND REPLACED HOSE ASSEMBLY FOR LOWER WATER SEPARATOR DUCT ON RIGHT PACK. REMOVED AND REPLACED HOSE ASSEMBLY FOR UPPER AIR CONDIT
- [SDR AT0000448R1](https://openairdocs.org/sdr/AT0000448R1.md): Switch · inoperative · Oct 21, 2000 · N825AT · Doug DC932 · Exterior Lighting
  > WHEN RIGHT LANDING LIGHT SWITCH WAS ACTIVATED FOR LANDING, SMOKE CAME FROM SWITCH. REMOVED VELCRO/ADHESIVE GLUE FROM BOTTOM OF LANDING LIGHT SWITCHES, REMOVED GLUE.
- [SDR AT0000448](https://openairdocs.org/sdr/AT0000448.md): Switch · shorted · Oct 21, 2000 · N825AT · Doug DC932 · Exterior Lighting
  > WHEN RIGHT LANDING LIGHT SWITCH ACTIVATED FOR LANDING, SMOKE CAME FROM SWITCH. COULD NOT DUPLICATE, PULLED CIRCUIT BREAKER AND COLLARED.
- [SDR AT0000375](https://openairdocs.org/sdr/AT0000375.md): Light · inoperative · Aug 8, 2000 · N825AT · Doug DC932 · Emergency Lighting
  > FOUND AFT EMERGENCY LIGHTING AT AFT ENTRY DOOR WILL NOT ILLUMINATE. REPAIRED WIRE IN GROUND TO AFT EMERGENCY LIGHT IAW DC9 WDM 33-51.
- [SDR AT0000305](https://openairdocs.org/sdr/AT0000305.md): Duct · ruptured · Jun 5, 2000 · N825AT · Doug DC932 · Fuel Heater
  > ON CLIMBOUT, NR 1 ENGINE FIRE WARNING INDICATION SOUNDED, LIGHTS WENT OUT UPON POWER REDUCTION. REMOVED AND REPLACED RUPTURED FUEL HEAT DUCT IAW DC9 MM.
- [SDR AT0000246](https://openairdocs.org/sdr/AT0000246.md): Skin · lightning strike · May 9, 2000 · N825AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND LIGHTNING STRIKE BLENDED BEYOND LIMITS AT RIGHT HAND WINDOW PANEL, BS 775 - 813. FABRICATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW REO L00173.
- [SDR AT0000244](https://openairdocs.org/sdr/AT0000244.md): Structure · misrepaired · May 9, 2000 · N825AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND AFT CARGO CUT OUT LOWER SECTION HAS AN EXISTING REPAIR, NOT IAW DC9 SRM OR EO. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED PERMANENT REPAIR IAW TIMCO REO L-00161.
- [SDR AT0000243](https://openairdocs.org/sdr/AT0000243.md): Doubler · cracked · May 9, 2000 · N825AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND TEMPORARY REPAIR CRACKED AT BS 945. FABRICATED AND INSTALLED PERMANENT PEPAIR IAW TIMCO REO L-00161.
- [SDR AT0000270](https://openairdocs.org/sdr/AT0000270.md): Skin · corroded · May 8, 2000 · N825AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND FORWARD CARGO COMPARTMENT SKIN UNDER NR 2 DME ANTENNA CORRODED AT BS 427. CUT OUT CORRODED SKIN, REMOVED 2 SPLICES, SHEAR TIES AND FLAPPER VALVE. FABRICATED 2 DOUBLER REPAIRS, FABRICATED SHEAR TIE SPLICE AND INSTALLED IAW DC9 SRM 53-04 FIGURE 44, 53-08
- [SDR AT0000267](https://openairdocs.org/sdr/AT0000267.md): Skin · lightning strike · May 7, 2000 · N825AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND LIGHTNING STRIKE AT BS 317 AND BS 323. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC9 SRM 53-04 FIGURE 38 AND 12B.
- [SDR AT0000266](https://openairdocs.org/sdr/AT0000266.md): Skin · cracked · May 2, 2000 · N825AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND FORWARD CARGO COMPARTMENT LOWER AFT DOOR JAMB CORNER WAS CRACKED AT FASTENER HOLE. CUT OUT CRACKED AREA, INSTALLED FILLERS, DOUBLERS AND TRIPLER IAW TIMCO SERVICE ORDER 151015-36912.
- [SDR AT0000242](https://openairdocs.org/sdr/AT0000242.md): Angle · worn · May 2, 2000 · N825AT · Doug DC932 · Horizontal Stabilizer, Tab Structure
  > FOUND BOTTON ANGLE LEFT AFT SIDE OF VERTICAL PANEL WORN BEYOND LIMITS. REMOVED AND REPLACED ANGLE IAW TIMCO SERVICE ORDER 151015-38274.
- [SDR AT0000241](https://openairdocs.org/sdr/AT0000241.md): Skin · gouged · May 2, 2000 · N825AT · Doug DC932 · Vertical Stabilizer, Plate/Skin
  > FOUND TOP OF VERTICAL STAB PANEL DEEPLY GOUGED ALONG AFT LEFT SIDE, 2 EACH. REMOVED AND REPLACED SKIN IAW TIMCO SERVICE ORDER 151015-36905.
- [SDR AT0000303](https://openairdocs.org/sdr/AT0000303.md): Longeron · damaged · Apr 28, 2000 · N825AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND EXISTING REPAIR OUTSIDE LIMITS AT BS 180 TO 207 L-20. REPAIRED TO CORRECT TOLORANCE IAW TIMCO REO L00162.
- [SDR AT0000224](https://openairdocs.org/sdr/AT0000224.md): Skin · corroded · Apr 27, 2000 · N825AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND CORROSION OF FUSELAGE SKIN OUT OF LIMITS. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SC9 SRM 53-04 FIGURE 38.
- [SDR AT0000223](https://openairdocs.org/sdr/AT0000223.md): Stop · cracked · Apr 27, 2000 · N825AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND CRACK ON 4TH DOOR STOP AFT SIDE OF FORWARD PASSENGER DOOR. CUT OUT CRACK, FABRICATED FILLER DOUBLER AND TRIPLER AND INSTALLED REPAIR IAW EO 09-5310-29-E1475, REV A.
- [SDR AT0000222](https://openairdocs.org/sdr/AT0000222.md): Skin · cracked · Apr 21, 2000 · N825AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND 2 CRACKS IN FUSELAGE AT BS 756 L1R. INSTALLED SKIN REPAIR IAW DC9 SRO DWG 9530129.
- [SDR AT0000221](https://openairdocs.org/sdr/AT0000221.md): Skin · cracked · Apr 21, 2000 · N825AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND CRACK IN FUSELAGE SKIN AT BS 737 L1 & 2R. INSTALLED SKIN REPAIR IAW SRO DWG 9530129.
- [SDR AT0000269](https://openairdocs.org/sdr/AT0000269.md): Bulkhead · cracked · Apr 18, 2000 · N825AT · Doug DC932 · Fuselage Main, Bulkhead
  > FOUND BULKHEAD WEB AT BS 965 CRACKED. FABRICATED REPAIR WEB AND INSTALLED IAW EO 9-5310-29-E1466, REV A.
- [SDR AT0000245](https://openairdocs.org/sdr/AT0000245.md): Frame · cracked · Apr 18, 2000 · N825AT · Doug DC932 · Fuselage Main, Frame
  > FOUND FRAME AT BS 718 CRACKED. REMOVED FRAME, DRILLED NEW FRAME AND INSTALLED IAW EO 15-5311-29-B1044 OPTION 2, DC9 SRM 51-30-2, 51-30-5, 51-30-8 AND 53-05 FIGURE 4F.
- [SDR AT0000240](https://openairdocs.org/sdr/AT0000240.md): Cap · cracked · Apr 17, 2000 · N825AT · Doug DC932 · Wing Miscellaneous Structure
  > FOUND RIGHT WING AT BS 58.5 HAS CORROSION AND CRACK ON T-CAP BETWEEN STRINGER 15 AND 16. REMOVED CORROSION, DRILLED, SEALED, AND INSTALLED 6 REPAIR CLIPS IAW RES 00-0442 AND REWORK DRAWING 5932267.
- [SDR AT0000302](https://openairdocs.org/sdr/AT0000302.md): Attach Fitting · gouged · Apr 16, 2000 · N825AT · Doug DC932 · Wing, Landing Gear Attach Fittings
  > FOUND RIGHT MLG ATTACH FITTING LUG FOR SIDE BRACE GOUGED. REPAIRED GOUGED RIGHT HAND MAIN LANDING GEAR FITTING ASSEMBLY LUG IAW TIMCO REO L00163.
- [SDR AT0000220](https://openairdocs.org/sdr/AT0000220.md): Longeron · cracked · Apr 15, 2000 · N825AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND LONGERON 6R WAS CRACKED AT BS 718. REMOVED SECTION OF CRACKED LONGERON, CUT DRILLED, TREATED, PRIMED AND INSTALLED SPLICES IAW DC9 SRM 53-02 FIGURE 18, 51-10-4, 51-10-03, 51-30-2, 51-30-5.
- [SDR AT0000268](https://openairdocs.org/sdr/AT0000268.md): Skin · corroded · Apr 14, 2000 · N825AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND SKIN BELOW LEFT AFT LAVATORY SERVICE PANEL BLENDED BEYOND LIMITS. CUT OUT BLENDED AREA OF SKIN BELOW LAVATORY SERVICE PANEL, FABRICATED SKIN FILLER AND EXTERNAL DOUBLER IAW REO -L00164.
- [SDR AT0000250](https://openairdocs.org/sdr/AT0000250.md): Skin · lightning strike · Apr 13, 2000 · N825AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND LIGHTNING STRIKE AT BS 165 LONGERON 29 - 30R. FABRICATED, DRILLED, COUNTERSUNK, REPAIR DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER IAW TIMCO REO L00176 AND DC9 SRM 51-30-0.
- [SDR AT0000149](https://openairdocs.org/sdr/AT0000149.md): Light · inoperative · Mar 22, 2000 · N825AT · Doug DC932 · Emergency Lighting
  > FOUND TAILCONE EMERGENCY FLOOD LIGHT WILL NOT ILLUMINATE. CORRECTIVE ACTION: RELAMPED, IAW DC9 MM 33-50
- [SDR AT0000086](https://openairdocs.org/sdr/AT0000086.md): Lanyard · disengaged · Feb 6, 2000 · N825AT · Doug DC932 · Escape Slide
  > FOUND ON TAXI OUT, R1 DOOR SLIDE LANYARD FELL OUT. STRAIGHTENED ARM AND ATTACHED PACK, REATTACHED PIN IAW DC9 MM 25-62-00.
- [SDR AT9900378](https://openairdocs.org/sdr/AT9900378.md): Batteries · discharged · May 16, 1999 · N825AT · Doug DC932 · Emergency Lighting
  > FOUND BOTH AFT OVERHEAD EXIT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERIES IAW MM 33-53-0.
- [SDR AT9900377](https://openairdocs.org/sdr/AT9900377.md): Battery · discharged · May 16, 1999 · N825AT · Doug DC932 · Emergency Lighting
  > THREE OVERHEAD EMEGENCY LIGHTS INOPERATIVE, TWO IN ROW 20 AND ONE IN BETWEEN ROWS 19 AND 20. REMOVED AND REPLACED BATTERIES IAW MM 33-53-0.
- [SDR AT9900139](https://openairdocs.org/sdr/AT9900139.md): Floorbeam · corroded · Feb 12, 1999 · N825AT · Doug DC932 · Fuselage Main, Floor Beam
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOORBEAM AT STA 965 HAS CORROSION AND BLUE WATER STAINS ON LOWER LEG AND AROUND NUT PLATES HOLES LEFT HAND LAVATORY. MECHANICALLY REMOVED CORROSION, FABRICATED TWO DOUBLERS AND INSTALLED IAW DC9 SRM 53-05 FIG
- [SDR AT9900116](https://openairdocs.org/sdr/AT9900116.md): Skin · dented · Feb 11, 1999 · N825AT · Doug DC932 · Fuselage Main, Plate/Skin
  > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE LOWER RIGHT FUSELAGE SKIN FROM STA 389 TO STA 598 L-18R TO L-26R WITH DENTS IN DIFFERENT AREAS. REMOVED AND REPLACED FUSELAGE SKIN IAW DC9 SRM 51-30-2, 51-30-1, AND RES NR 99193.
- [SDR AT9900143](https://openairdocs.org/sdr/AT9900143.md): Floor Track · corroded · Jan 22, 1999 · N825AT · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND FLOOR TRACKS AT THE AFT PIT STA 756 TO 780 AND ON THE RIGHT LOWER SIDE AT STA 935 TO 996 WITH CORROSION. MECHANICALLY REMOVED CORROSION, FABRICATED NEW SECTION OF FLOOR TRACKS, DRILLED, DEBURRED, COUNTERSUNK, TREA
- [SDR AT9900144](https://openairdocs.org/sdr/AT9900144.md): Bracket · corroded · Jan 14, 1999 · N825AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS LOCATION WITH CORROSION. FIRST, THE CABIN FLOOR PANEL NR 89 ON THE UNDER SIDE AT FORWARD END. SECONDLY, THE CUSP WEB AND FITTING AT STA 229 LEFT SIDE AROUND RIVETS AND DOUBLER. THIRD, THE PULLEY BRACKET
- [SDR AT9900130](https://openairdocs.org/sdr/AT9900130.md): Structure · corroded · Jan 14, 1999 · N825AT · Doug DC932 · Fuselage Main, Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS LOCATIONS WITH CORROSION. FIRST, AT STA 602 LONGERON L-29L. SECONDLY, THE AFT PIT FORWARD SIDE AT STA 382 BETWEEN L-29R TO L-27L. THIRD, THE LEFT LAVATORY BULKHEAD LOWER PORTION AT STA 965. LAST, CORROS
- [SDR AT9900259](https://openairdocs.org/sdr/AT9900259.md): Fairing · delaminated · Jan 13, 1999 · N825AT · Doug DC932 · Horizontal Stabilizer Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND DELAMINATION ON INBOARD AND OUTBOARD SIDES OF LEFT HAND UPPER HORIZONTAL STABILIZER FAIRING. REMOVED INNER SKIN AND HONEYCOMB CORE FROM LEFT HAND UPPER HORIZONTAL STABILIZER FAIRING THAT WAS DELAMINATED. TRIM NEW
- [SDR AT9900146](https://openairdocs.org/sdr/AT9900146.md): Support · cracked · Jan 13, 1999 · N825AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS FLOOR FRAME AT DIFFERENT LOCATIONS CRACKED. FIRST, THE FORWARD CARGO FLOOR FRAME SCREW HOLE CRACKED/ELONGATED AT STA 237 BETWEEN L-29-30L. SECONDLY, STA 794 FRAME ON THE FORWARD SIDE BETWEEN L-29-30R. TH
- [SDR AT9900137](https://openairdocs.org/sdr/AT9900137.md): Longeron · dented · Jan 13, 1999 · N825AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND A DENT OUT OF LIMITS AT STA 361R L-28R. REMOVED FASTENERS, COLD WORKED DENT, HFCE INSPECTED DENT WITH NO CRACKS NOTED. FABRICATED DOUBLER, FINGER DOUBLERS, DRILLED, COUNTERSUNK, DEBURRED, TREATED, PRIMED, AND INS
- [SDR AT9900145](https://openairdocs.org/sdr/AT9900145.md): Support · corroded · Jan 12, 1999 · N825AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS LOCATION CORRODED AND CRACKED. FIRST, THE AFT PIT LOWER SIDE WALL TIEDOWNS COVER ON THE LOWER SIDE. SECONDLY, THE AFT PIT CEILING SUPPORT CORRODED AND CRACKED AT STA 935 TO 996. ALSO, THE GLIDE SLOPE ANT
- [SDR AT9900140](https://openairdocs.org/sdr/AT9900140.md): Fairing · cracked · Jan 12, 1999 · N825AT · Doug DC932 · Engine Thrust Reverser
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE NR 2 AFT INBOARD UPPER THRUST REVERSER ACTUATOR FAIRING IS CRACKED. REMOVED THE THRUST REVERSER FAIRING, WELDED AND REINSTALLED IAW DC9 MM 78-00 AND RES NR 99244.

## 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 = 'N825AT' AND deregistration_id = 'N825AT-2003-01-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N825AT-2003-01-29/reports

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