# Service difficulty reports: N819AT, cancelled Jan 29, 2003

A list on [N819AT, cancelled Jan 29, 2003](https://openairdocs.org/deregistered/N819AT-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.

Page 1 of 2 · 55 reports

- [SDR AT0200046](https://openairdocs.org/sdr/AT0200046.md): Duct · torn · Apr 8, 2002 · N819AT · Doug DC932 · Cabin Pressure Control System
  > AIRCRAFT WOULD NOT MAINTAIN CABIN ALTITUDE/PRESSURE IN AUTOMATIC OR MANUAL MADE AT FL290. A/C DESCENDED LOWER TO ENABLE MANUAL PRESURIZATION; THUS NORMAL/OPTIMUM CABIN ALT/PRESSURE FOR CREW AND PASSENGERS. ALL MASKS FELL. CORRECTIVE ACTION:
- [SDR AT0200036](https://openairdocs.org/sdr/AT0200036.md): Fuse · blown · Mar 18, 2002 · N819AT · Doug DC932 · Emergency Lighting
  > FORWARD EMERGENCY PATH LIGHTING WILL NOT ILLUMINATE ON THE FLOOR. INSTALLED FUSE ON FORWARD POWER SUPPLY FOR EMERGENCY PATH LIGHTING REF DC-9 MM 33-53 AND 33-00, OPS CHECK GOOD.
- [SDR AT0100240](https://openairdocs.org/sdr/AT0100240.md): Lamp · inoperative · Dec 7, 2001 · N819AT · Doug DC932 · Emergency Lighting
  > FOUND 1 EACH TAIL CONE RELEASE HANDLE EMERGENCY EXIT LIGHT WONT ILLUMINATE. CORRECTIVE ACTION: RELAMPED A REQURED. IAW DC9 MM 33-51
- [SDR AT0100239](https://openairdocs.org/sdr/AT0100239.md): Lamp · inoperative · Dec 7, 2001 · N819AT · Doug DC932 · Emergency Lighting
  > FOUND EMERGENCY LIGHT RIGHT SIDE VENTRAL STAIRS WONT ILLUMINATE. CORRECTIVE ACTION: RELAMPED AS REQUIRED. IAW DC9 MM 33-50
- [SDR AT0100212](https://openairdocs.org/sdr/AT0100212.md): Spar · cracked · Jun 13, 2001 · N819AT · Doug DC932 · Vertical Stabilizer, Plate/Skin
  > FOUND RIGHT HORIZONTAL STABILIZER SPAR CRACKED. CORRECTIVE ACTION: FABRICATED AND INSTALLED SPLICE ANGLES AND REPLACEMENT SECTION OF SPAR IAW 51-30-01, 51-30-05, AND 55-01 FIG 2.
- [SDR AT0100203](https://openairdocs.org/sdr/AT0100203.md): Skin · cracked · Jun 13, 2001 · N819AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND CRACK IN FORWARD SERVICE DOOR JAMB CORNER. CORRECTIVE ACTION: FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-30-02, 51-30-03, 51-30-04, AND 51-30-05.
- [SDR AT0100211](https://openairdocs.org/sdr/AT0100211.md): Intercostal · corroded · Jun 12, 2001 · N819AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND AFT CARGO PIT INTERCOSTAL CORRODED BEYOND LIMITS AT BS 965-980. CORRECTIVE ACTION: FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DC9 SRM 51-10-03, 51-30-02, 53-11-03, 51-10-04, AND 51-30-05.
- [SDR AT0100209](https://openairdocs.org/sdr/AT0100209.md): Skin · damaged · Jun 12, 2001 · N819AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND TEMPORARY REPAIRS AT BS 996 LONGERON 3L. INSTALLED PERMANENT REPAIRS IAW REO-L00453.
- [SDR AT0100210](https://openairdocs.org/sdr/AT0100210.md): Floor Panel · corroded · Jun 11, 2001 · N819AT · Doug DC932 · Fuselage Main, Floor Beam
  > FOUND FORWARD PIT FLOOR PANEL AT BS 218-332 CORRODED BEYOND LIMITS. CORRECTIVE ACTION: FABRICATED AND INSTALLED REPAIR PANEL IAW DC9 SRM 51-10-02, 51-10-03, AND 51-10-04.
- [SDR AT0100207](https://openairdocs.org/sdr/AT0100207.md): Floor Support · corroded · Jun 11, 2001 · N819AT · Doug DC932 · Fuselage Main, Floor Beam
  > FOUND FLOOR SUPPORT AT BS 160-218 CORRODED BEYOND LIMITS. CORRECTIVE ACTION: FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-30-05.
- [SDR AT0100206](https://openairdocs.org/sdr/AT0100206.md): Floor Support · corroded · Jun 11, 2001 · N819AT · Doug DC932 · Fuselage Main, Floor Beam
  > FOUND FLOOR SUPPORT AT BS 205 RBL 22-44 CORRODEDBEYOND LIMITS. CORRECTIVE ACTION: FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-30-05.
- [SDR AT0100205](https://openairdocs.org/sdr/AT0100205.md): Floor Support · corroded · Jun 11, 2001 · N819AT · Doug DC932 · Fuselage Main, Floor Beam
  > FOUND CABIN FLOOR SUPPORT AT LBL 15 IS CORRODED BEYOND LIMITS AT BS 205-218. CORRECTIVE ACTION: FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-30-05.
- [SDR AT0100201](https://openairdocs.org/sdr/AT0100201.md): Frame · chafed · Jun 11, 2001 · N819AT · Doug DC932 · Fuselage Main, Frame
  > FOUND FRAME CHAFED AT BS 106 LBL 15. CORRECTIVE ACTION: INSTALLED REPAIR ANGLE IAW DC9 SRM 51-10-04, 51-10-03, AND 53-01 FIG 2.
- [SDR AT0100208](https://openairdocs.org/sdr/AT0100208.md): Floor Support · corroded · Jun 10, 2001 · N819AT · Doug DC932 · Fuselage Main, Floor Beam
  > FOUND FLOOR SUPPORT AT BS 160-200 CORRODED BEYOND LIMITS. CORRECTIVE ACTION: FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-10-04, 51-10-03, 51-20, AND 51-30-02.
- [SDR AT0100202](https://openairdocs.org/sdr/AT0100202.md): Floor Panel · corroded · Jun 6, 2001 · N819AT · Doug DC932 · Fuselage Floor Panel
  > FOUND CABIN FLOOR PANEL #48 CORRODED. CORRECTIVE ACTION: FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 53-20-01, 51-10-03 AND 51-10-02.
- [SDR AT0100204](https://openairdocs.org/sdr/AT0100204.md): Retainer · cracked · Jun 4, 2001 · N819AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND SEAL DEPRESSOR CRACKED AT FORWARD C-1 DOORWAY. FABRICATED REPAIR AND DOUBLER IAW DC9 SRM 53-10 FIG 817.
- [SDR AT0100155](https://openairdocs.org/sdr/AT0100155.md): Coffeemaker · shorted · May 13, 2001 · N819AT · Doug DC932 · Buffet/Galleys
  > SMELLED SMOKE IN FLIGHT DECK. REPLACED SHORTED COFFEEMAKER.
- [SDR AT0000154](https://openairdocs.org/sdr/AT0000154.md): Bottle · discharged · Jun 9, 2000 · N819AT · Doug DC932 · Fire Bottle, Fixed
  > NR 2 AGENT LOW LIGHT ILLUMINATED DURING FLIGHT. REMOVED AND REPLACED NR 2 FIRE BOTTLE AND REPLACED Y DUCT FOR 8TH AND 13TH STAGE BLEED AIR.
- [SDR AT0000304](https://openairdocs.org/sdr/AT0000304.md): Warning Light · illuminated · Jun 5, 2000 · N819AT · Doug DC932 · Fire Bottle, Fixed
  > FIRE BOTTLE THERMAL DISCHARGED, NR 2 AGENT LOW ANNUNCIATOR ILLUMINATED, 25 MINUTES INTO FLIGHT. REMOVED AND REPLACED DUCT ASSEMBLY BEHIND FIRE BOTTLE, REMOVED AND REPLACED FIRE BOTTLE.
- [SDR AT0000231](https://openairdocs.org/sdr/AT0000231.md): Frame · cracked · Apr 8, 2000 · N819AT · Doug DC932 · Fuselage Main, Frame
  > FOUND CRACKS IN CANTNED FRAME AT BS 1143. REMOVED AND REPLACED LOWER SECTION OF FRAME AND INSTALLING SPLICES IAW TIMCO REO L00152.
- [SDR AT0000226](https://openairdocs.org/sdr/AT0000226.md): Door Frame · dented · Apr 6, 2000 · N819AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND DENTED R1 DOOR JAMB PAN BETWEEN Z17 AND Z35. REMOVED DENTED SECTION OF PAN, FABRICATED, INSTALLED NEW SECTION OF PAN AND REPAIR DOUBLER AND SPLICES IAW TIMCO REO L00112.
- [SDR AT0000197](https://openairdocs.org/sdr/AT0000197.md): Frame · damaged · Apr 5, 2000 · N819AT · Doug DC932 · Fuselage Main, Frame
  > FOUND TEMPORARY REPAIR INSTALLED AT BS 370 LONGERON 29R. REPLACED TEMPORARY REPAIR WITH PERMANENT REPAIR IAW REO L00104.
- [SDR AT0000227](https://openairdocs.org/sdr/AT0000227.md): Skin · dented · Apr 3, 2000 · N819AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN DENTED FROM BS 325 - 270. REMOVED, FABRICATED AND INSTALLED NEW SECTION OF SKIN AND SPLICES IAW TIMCO EO L00111.
- [SDR AT0000198](https://openairdocs.org/sdr/AT0000198.md): Panel · damaged · Apr 3, 2000 · N819AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND TEMPORARY REPAIR AT SLANT PANEL AT BS 588. INSTALLED PERMANENT REPAIR IAW REO L00120.
- [SDR AT0000194](https://openairdocs.org/sdr/AT0000194.md): Stringer · corroded · Apr 3, 2000 · N819AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND LEFT HAND WING STRINGER 22 CORRODED. REMOVED AND REPLACED STRINGER IAW DC9 SRM 51-30-2 AND 51-30-5, 51-10-4, 51-10-3.
- [SDR AT0000193](https://openairdocs.org/sdr/AT0000193.md): Stringer · corroded · Apr 2, 2000 · N819AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND RIGHT HAND WING STRINGER 17 CORRODED BEYOND LIMITS. CUT AND SPLICED RIGHT HAND WING STRINGER 17 IAW DC9 SRM 57-08 FIGURE 2.
- [SDR AT0000195](https://openairdocs.org/sdr/AT0000195.md): Stringer · corroded · Apr 1, 2000 · N819AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND RIGHT WING STRINGER 13 CORRODED BEYOND LIMITS. CUT OUT RIGHT HAND STRINGER 13 CORRODED SECTION, REPLACED SECTION, AND INSTALLED SPLICES IAW DC9 SRM 57-08 FIGURE 1.
- [SDR AT0000228](https://openairdocs.org/sdr/AT0000228.md): Skin · lightning strike · Mar 31, 2000 · N819AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND LIGHTENING STRIKE ON FUSELAGE SKIN AT BS 996L - L4L. CUT OUT STRIKE, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW TIMCO REO L00115.
- [SDR AT0000196](https://openairdocs.org/sdr/AT0000196.md): Doubler · dented · Mar 31, 2000 · N819AT · Doug DC932 · Leading Edge Devices
  > FOUND LEFT WING NR 4 SLAT WITH 2 DENTS OUT OF LIMITS. CUT OUT DENTS, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC9 SRM 57-09 FIGURE 10.
- [SDR AT0000192](https://openairdocs.org/sdr/AT0000192.md): Skin · lightning strike · Mar 31, 2000 · N819AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND LIGHTNING STRIKE AT BS 775 LONGERON 1 OUT OF LIMITS. CUT OUT AREA, TRIMMED EDGES, FABRICATED FILLER AND DOUBLERS, INSTALLED IAW REO L00122 AND DC9 SRM 53-04 FIGURE 37.
- [SDR AT0000191](https://openairdocs.org/sdr/AT0000191.md): Skin · dented · Mar 28, 2000 · N819AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND DENT AT BS 33, 3 INCHES BELOW LONGERON 20R. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-30-2 AND REO L00092.
- [SDR AT0000158](https://openairdocs.org/sdr/AT0000158.md): Stringer · corroded · Mar 28, 2000 · N819AT · Doug DC932 · Wing, Longeron/Stringer
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LT WING TANK STRINGER 14 CORRODED BEYOND LIMITS. CORRECTIVE ACTION: REMOVED CORRODED SECTION OF STRINGER AND REPLACED WITH NEW STRINGER AND SPLICES IAW DC9 SRM 57-08 FIG 1.
- [SDR AT0000156](https://openairdocs.org/sdr/AT0000156.md): Skin · dented · Mar 28, 2000 · N819AT · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND DENT AT BS 293, LONGERON 20 RT. CORRECTIVE ACTION: REMOVED AND REPLACED DENTED SKIN IAW REO-L00094 AND DC9 SRM 51-30-02.
- [SDR AT0000155](https://openairdocs.org/sdr/AT0000155.md): Skin · dented · Mar 28, 2000 · N819AT · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND DENTS, AT BS 1153, LONGERON 6 - 7 RT AND BS 1155, LONGERON 5 - 6 RT, BEYOND LIMITS. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW SKIN IAW REO-L00110 AND DC9 SRM 51-10-04.
- [SDR AT0000157](https://openairdocs.org/sdr/AT0000157.md): Skin · dented · Mar 27, 2000 · N819AT · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND DENT AT BS 312 LONGERON 20 RT. CORRECTIVE ACTION: REMOVED AND REPLACED DAMAGED SKIN IAW REO-L00093 AND DC9 SRM 51-30-02.
- [SDR AT0000230](https://openairdocs.org/sdr/AT0000230.md): Skin · lightning strike · Mar 23, 2000 · N819AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND LIGHTNING STRIKE AT WINDOW NR 25. BLENDED STRIKE, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW DWG SRO9530053 AND TIMCO REO L00116.
- [SDR AT0000229](https://openairdocs.org/sdr/AT0000229.md): Skin · lightning strike · Mar 23, 2000 · N819AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND LIGHTNING STRIKE IN WINDOW BELT AT WINDOW NR 21. CUT OUT LOWER AFT CORNER BY BLENDING STRIKE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DWG SRO9530053 AND TIMCO L00107.
- [SDR AT0000225](https://openairdocs.org/sdr/AT0000225.md): Longeron · damaged · Mar 21, 2000 · N819AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND AND REMOVED TEMPORARY REPAIR AT BS 227L - 17L. FABRICATED AND INSTALLED PERMANENT REPAIR IAW TIMCO REO L00099.
- [SDR AT0000148](https://openairdocs.org/sdr/AT0000148.md): Web · corroded · Mar 18, 2000 · N819AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND FUSELAGE BS 980 WEB WAS CORRODED. FORMED 1 REPAIR DOUBLER WEB AND INSTALLED IAW DC9 SRM 53-11-4 FIGURE 3, 51-10-3.
- [SDR AT0000145](https://openairdocs.org/sdr/AT0000145.md): Skin · lightning strike · Mar 18, 2000 · N819AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND LIGHTNING STRIKE AT LONGERON 3L BS 917 OUT OF LIMITS. CUTOUT LIGHTNING STRIKE, FABRICATED AND INSTALLED REPAIR. IAW DC9 SRM 53-04 FIGURE 38, 51-10-3, 51-30-2.
- [SDR AT0000144](https://openairdocs.org/sdr/AT0000144.md): Pan · corroded · Mar 17, 2000 · N819AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND G1 GALLEY OUTBOARD LOWER COMPARTMENT AT WATER DRAIN PAN CORRODED. FABRICATED PANEL AND REINSTALLED IAW DC9 SRM 51-10-4, 51-30-8, 51-10-3, 55-05.
- [SDR AT0000151](https://openairdocs.org/sdr/AT0000151.md): Panel · corroded · Mar 17, 2000 · N819AT · Doug DC932 · Buffet/Galleys
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND GALLEY LOWER COMPARTMENT PANEL CORRODED. AFTER BLENDING MATERIAL FOUND TO BE OUT OF LIMITS. CORRECTIVE ACTION: FABRICATED AND INSTALLED GALLEY PANEL IAW DC9 SRM 53-05, 51-10-03, 51-10-04, AND
- [SDR AT0000147](https://openairdocs.org/sdr/AT0000147.md): Doubler · chafed · Mar 15, 2000 · N819AT · Doug DC932 · Auxiliary Power Unit (APU) Doors
  > FOUND APU DOOR CRACK BLENDED OUT OF LIMITS. FABRICATED REPAIR DOUBLER AND INSTALLED ON APU DOOR IAW DC9 SRM 52-10 FIGURE 2.
- [SDR AT9900096](https://openairdocs.org/sdr/AT9900096.md): Slide · low pressure · Feb 9, 1999 · N819AT · Doug DC932 · Escape Slide
  > AFT TAIL CONE SLIDE PRESSURE IS LOW. REMOVED AND REPLACED TAIL CONE SLIDE IAW MM 25-62-1.
- [SDR AT9900028](https://openairdocs.org/sdr/AT9900028.md): Slant Panel · corroded · Dec 30, 1998 · N819AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULE INSPECTION AT AERO CORP, FL. UPON PRESSURIZATION FOUND LEFT AND RIGHT HAND SLANT PANELS LEAKING EXCESSIVELY. SEALS TORN AND PINCHED. REMOVED LEFT AND RIGHT SLANT PANEL CORROSION, MATERIAL LOSS FOUND OUT OF LIMITS ON LEFT HAND SIDE, FABRICATED REPAIR
- [SDR AT9900022](https://openairdocs.org/sdr/AT9900022.md): Skin · dented · Dec 30, 1998 · N819AT · Doug DC932 · Fuselage Main, Plate/Skin
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND DENTS AND CREASES AT VARIOUS FUSELAGE SKIN LOCATION OUT OF LIMITS. THE LOCATIONS ARE FS 104 TO FS 135 L-19R, FS 227 L-17L, FS 229 TO FS 598 L-18R TO 28R, FS 241 L-18L AND FS 269 L-18L. REPAIRED ALL DENTED FUSELAG
- [SDR AT9900024](https://openairdocs.org/sdr/AT9900024.md): Structure · misdrilled · Dec 23, 1998 · N819AT · Doug DC932 · Fuselage Main, Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND STRAP, FLOOR FRAME, FLOOR SUPPORT ANGLE AND FORWARD CARGO DOOR CUTOUT MISDRILLED AT STA 370 LONGERON 29R ( INBOARD FORWARD FRAME). CORRECTIVE ACTION: FABRICATE NEW WEB, FORMED NEW INTERCOASTAL AND DOUBLER,
- [SDR AT9900023](https://openairdocs.org/sdr/AT9900023.md): Doubler · cut · Dec 23, 1998 · N819AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. INTERNAL TORQUE BOX DOUBLER AT FORWARD CARGO DOOR FS 399 CUT LONGERON 18R TO 20R. FABRICATED, DRILLED, PRIMED AND INSTALLED INTERNAL DOUBLER MIL-T-9046J.025 THOUSANDS OF AN INCH 13 BY 6.125 IN IAW DC9 SRM 53-04 FIG 38
- [SDR AT9900027](https://openairdocs.org/sdr/AT9900027.md): Jamb · dented · Dec 22, 1998 · N819AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULE INSPECTION AT AERO CORP, FL. FOUND R-1 DOOR JAMMED, DENTED AND GOUGED AT STA 200 RT AT LONGERON 15R. FABRICATED DOOR PAN SECTION AND SPLICES, HEAT TREATED PARTS, PRIMED AND INSTALLED REPAIR IAW DC9 SRM 53-03 FIG 2 AND AIRTRAN RES NR 982244.
- [SDR AT9900025](https://openairdocs.org/sdr/AT9900025.md): Floorbeam · chafed · Dec 22, 1998 · N819AT · Doug DC932 · Fuselage Main, Floor Beam
  > SCHEDULED INSPECTION AT AERO CORP, FL. FORWARD CARGO COMPARTMENT FLOORBEAMS AT FS 389 TO FS 408 ARE CHAFED AND OUT OF LIMITS IAW SRM 53-01 FIG 1. REPAIRED THE CHAFED CABIN FLOORBEAMS LOWER LEGS BY FABRICATING AND INSTALLING REPAIR ANGLES IAW DC9 SRM 53-05 FI

Next page: https://openairdocs.org/deregistered/N819AT-2003-01-29/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 = 'N819AT' AND deregistration_id = 'N819AT-2003-01-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N819AT-2003-01-29/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.