# Service difficulty reports: N805AT, cancelled May 2, 2003

A list on [N805AT, cancelled May 2, 2003](https://openairdocs.org/deregistered/N805AT-2003-05-02.md).

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

- [SDR AT0100216](https://openairdocs.org/sdr/AT0100216.md): Battery Pack · inoperative · Jul 20, 2001 · N805AT · Doug DC932 · Emergency Lighting
  > FOUND EMERGENCY LIGHTS AT ROWS 18 AND 22 FAILED TEST. CORRECTIVE ACTION: REPLACED BATTERIES IN BATTERY PACK B5-26. IAW DC9 MM 33-50
- [SDR AT0000431](https://openairdocs.org/sdr/AT0000431.md): Skin · dented · Sep 6, 2000 · N805AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND DENT AT BS 484. CUT OUT DENTED AREA, FABRICATED REPAIR FILLER, INTERNAL DOUBLER, AND INSTALLED IAW DC9 SRM 53-04 FIGURE 12C.
- [SDR AT0000494](https://openairdocs.org/sdr/AT0000494.md): Skin · cracked · Aug 30, 2000 · N805AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND 2 EA CRACKS IN FUSELAGE UPPER NOSE SKIN. CUT OUT CRACKED AREA AND INSTALLED REPAIR DOUBLERS. IAW EO 12-5330-29-B1048, AD 96-11-11, SB 53-262AND DC9 SRM 53-31-0, 51-10-3, 51-30-01, 51-30-02
- [SDR AT0000434](https://openairdocs.org/sdr/AT0000434.md): Angle · corroded · Aug 30, 2000 · N805AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND CORROSION AT BS 120 ON LONGERON 28R AND BS 130 LONGERON 28 AT BAY DOOR LOCKING INDICATOR. REMOVED 1 T-ANGLE, 1 SUPPORT, FABRICATED NEW SUPPORT AND INSTALLED IAW DCI SRM 51-30-2.
- [SDR AT0000426](https://openairdocs.org/sdr/AT0000426.md): Skin · cracked · Aug 29, 2000 · N805AT · Doug DC932 · Passenger/Crew Doors
  > FOUND FORWARD ENTRY DOOR JAMB AFT SIDE AT THE DOOR STOP IS CRACKED. INSTALLED REPAIR IAW EO 09-5310-29-E1475 AND SRO 9530252.
- [SDR AT0000430](https://openairdocs.org/sdr/AT0000430.md): Floorbeam · corroded · Aug 27, 2000 · N805AT · Doug DC932 · Fuselage Main, Floor Beam
  > FOUND CORROSION ON EPC PANEL FRAME AT FLOOR SUPPORT. REMOVED FRAME AND FLOOR SUPPORT, FABRICATED NEW REPAIR AND INSTALLED IAW DC9 SRM 51-10-2, 51-30-1, 52-61-0.
- [SDR AT0000429](https://openairdocs.org/sdr/AT0000429.md): Floor Panel · corroded · Aug 25, 2000 · N805AT · Doug DC932 · Fuselage Floor Panel
  > FOUND AFT ENTRY AREA FLOOR BOARD WAS CORRODED. BLENDED OUT CORROSION, FABRICATED NEW HAT CHANNELS AND PANEL. INSTALLED REPAIRS IAW DC9 SRM 51-10-3, 51-10-4, 51-30-2.
- [SDR AT0000428](https://openairdocs.org/sdr/AT0000428.md): Skin · cracked · Aug 25, 2000 · N805AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND A CRACK IN FUSELAGE UPPER NOSE SKIN AT LBL 17 BS 69.5. REMOVED CRACKED FILLER, PERFORMED HFEC, INSTALLED DOUBLER AND FILLER IAW TIMCO SERVICE ORDER 151080-20536.
- [SDR AT0000433](https://openairdocs.org/sdr/AT0000433.md): Frame · cracked · Aug 24, 2000 · N805AT · Doug DC932 · Fuselage Main, Frame
  > FOUND FRAME AT BS 737 WAS CRACKED. REPAIRED FRAME AT BS 737 IAW SERVICE BULLETIN 53-131 DRAWING 5935650.
- [SDR AT0000436](https://openairdocs.org/sdr/AT0000436.md): Frame · lightning strike · Aug 23, 2000 · N805AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND LIGHTNING STRIKE ON WINDOW NR 50 LOWER AFT CORNER ON FRAME. BLENDED OUT LIGHTNING STRIKE, FABRICATED AND INSTALLED REPAIR IAW SRO 9530053 AND REO L-00265.
- [SDR AT0000435](https://openairdocs.org/sdr/AT0000435.md): Fitting · corroded · Aug 23, 2000 · N805AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND STRINGER 30 END CAP FITTING AT WING SPAR HAS CORROSION. REMOVED AND REPLACED STRINGER END CAP FITTING AT BS 540 - 580 IAW DC9 SRM 51-01 FIGURE 1, 51-30-0, 51-10-3.
- [SDR AT0000432](https://openairdocs.org/sdr/AT0000432.md): Skin · dented · Aug 23, 2000 · N805AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND DENT AT BS 350, LONGERON 26R, 27L. DENT OUT OF LIMITS. PERFORMED HFEC INSPECTION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-04 FIGURE 3B.
- [SDR AT0000427](https://openairdocs.org/sdr/AT0000427.md): Bracket · cracked · Aug 23, 2000 · N805AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND CRACKED SUPPORT BRACKETS FOR CABIN FLOOR PANEL AT BS 725 - 832. REMOVED AND REPLACED SUPPORT BRACKETS IAW TIMCO SERVICE ORDER 151080-20463.
- [SDR AT0000425](https://openairdocs.org/sdr/AT0000425.md): Lanyard · frayed · Aug 21, 2000 · N805AT · Doug DC932 · Emergency Equipment
  > FOUND FORWARD AND AFT ESCAPE LINE OVER RIGHT WING WERE FRAYED. REMOVED AND REPLACED FORWARD AND AFT EMERGENCY ESCAPE LINES IAW DC9 MM 25-61-0.
- [SDR AT0000263](https://openairdocs.org/sdr/AT0000263.md): Unknown · odor · May 18, 2000 · N805AT · Doug DC932 · Air Distribution System
  > DURING CLIMB, FLIGHT ATTENDANTS SMELLED SMOKE IN CABIN. INSPECTED ALL COMPARTMENTS FOR SMOKE OR ODOR, RAN ENGINES, PACKS, AND PRESSURIZED AIRCRAFT WITH NO SMOKE OR ODOR NOTED. MCO DID HAVE BRUSH FIRES IN AREA.
- [SDR AT0000035](https://openairdocs.org/sdr/AT0000035.md): Warning Light · illuminated · Jan 22, 2000 · N805AT · Doug DC932 · Landing Gear Position and Warning
  > FOUND DURING LANDING GEAR EXTENTION, GEAR DOOR OPEN AMBER LIGHT STAYED ON. RECYCLED GEAR BY EMERGENCY EXTENTION METHOD. LIGHT REMAINED ON. LANDED WITH ABNORMAL PROCEDURES. FERRIED AIRCRAFT TO ORLANDO (MCO).
- [SDR AT0000035R1](https://openairdocs.org/sdr/AT0000035R1.md): Bracket · loose · Jan 18, 2000 · N805AT · Doug DC932 · Landing Gear Retraction/Extension System
  > FOUND DURING LANDING GEAR EXTENTION, GEAR DOOR OPEN AMBER LIGHT STAYED ON. RECYCLED GEAR BY EMERGENCY EXTENTION METHOD. LIGHT REMAINED ON. LANDED WITH ABNORMAL PROCEDURES. FOUND LOOSE GEAR DOOR ROLLER BRACKET ASSEMBLY, ON LEFT HAND GEAR DOOR. TIGHTENED BR
- [SDR AT0000005](https://openairdocs.org/sdr/AT0000005.md): Wire · broken · Jan 1, 2000 · N805AT · Doug DC932 · Light System Wiring
  > EMERGENCY TRACK LIGHT INOPERATIVE. REPAIRED BROKEN WIRE ON FORWARD EMERGENCY TRACK LIGHT IAW MM 33-53.
- [SDR AT9900531](https://openairdocs.org/sdr/AT9900531.md): Panel · delaminated · Jul 4, 1999 · N805AT · Doug DC932 · Wing, Plate/Skin
  > DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND DELAMINATION AND CORROSION DAMAGE ON THE LT WING UPPER T/E PANEL P/N 5912737-1. REPAIRED PANEL IAW TIMCO EO NR 99-1184.
- [SDR AT9900525](https://openairdocs.org/sdr/AT9900525.md): Skin · cracked · Jun 30, 1999 · N805AT · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FIRST FASTENER ON RIGHT SHEAR TIE CRACKED AT BS 680 AND LONGERON 1 R. CUT OUT CRACKED AREAS. FABRICATED REPAIR DOUBLER FROM 2024 T-3.025 AND 2024-T3.063. INSTALLED IAW SERVICE REWORK DRAWING SR09
- [SDR AT9900526](https://openairdocs.org/sdr/AT9900526.md): Skin · creased · Jun 29, 1999 · N805AT · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FUSELAGE SKIN CREASE 60.0 BY 1.5 BY.030 AT BS 290 - 350 BETWEEN L-22L AND L-23L. REMOVED AND REPLACED SKIN IAW TIMCO RES NR 06046, EO NR 1180 AND SRM 53-40 FIG 15D.
- [SDR AT9900527](https://openairdocs.org/sdr/AT9900527.md): Skin · dented · Jun 22, 1999 · N805AT · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FUSELAGE SKIN DENT 16 BY.5 BY.03. AT BS 300 BETWEEN L-18R AND L-19R DENT EXCEEDS LIMITS PER DC9 SRM 53-04 FIG 38 SHEET 10 FOOT NOTE 2 AND 3. REMOVED AND REPLACED FUSELAGE SKIN FROM BS 229 TO 389 BE
- [SDR AT9900523](https://openairdocs.org/sdr/AT9900523.md): Trim Strip · corroded · Jun 20, 1999 · N805AT · Doug DC932 · Cargo Compartments
  > DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND AFT PIT CENTER CEILING PANEL ATTACH STRAPS CORRODED AT BS 965-996. DRILLED 5 EACH CEILING PANEL CLOSE OUT TRIM STRIPS IAW DC9 SRM 51-10-4, 51-10-3.
- [SDR AT9900528](https://openairdocs.org/sdr/AT9900528.md): Fitting · corroded · Jun 19, 1999 · N805AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND AFT AIRSTAIRS FWD SKIN AT BS 1090 AND L-30R MISSING INTERNAL SHIMS. AFTER OPEN UP FOUND WEB CRACKED AND FITTING CORRODED BEYOND LIMITS. FAB AND INSTALLED SHIM AND REPAIR DOUBLERS ON WEB. REMOVED AN
- [SDR AT9900463](https://openairdocs.org/sdr/AT9900463.md): Frame · corroded · Jun 16, 1999 · N805AT · Doug DC932 · Fuselage Main, Frame
  > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FRAME IN THE FORWARD PIT AT BS 541 L-29L-29R CORRODED. REMOVED CORROSION, FABRICATED REPAIR PARTS, HEAT TREATED AND INSTALLED IAW DC9 SRM 53-03 FIG 2A, 51-10-4, 51-10-3, AND 51-30-3.
- [SDR AT9900529](https://openairdocs.org/sdr/AT9900529.md): Skin · dented · Jun 10, 1999 · N805AT · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FUSELAGE SKIN CREASE 6 INCHES BELOW CUSP LINE ON LEFT SIDE AT BS 99. DRILLED.025 HOLE, INSTALLED RIVET PER RES NR 07613 AND DC9 SRM 51-10-2, 53-04 FIG 38.
- [SDR AT9900441](https://openairdocs.org/sdr/AT9900441.md): Web · corroded · May 30, 1999 · N805AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND ON THE LEFT MAIN CABIN AT BS 928 LONGERON NR 18 ATTACHED WEB CORRODED. MECHANICALLY REMOVED CORROSION, FABRICATED REPAIR DOUBLER AND FILLER, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 53-11-3, 51-10-3 AND 53-
- [SDR AT9900434](https://openairdocs.org/sdr/AT9900434.md): Web · corroded · May 30, 1999 · N805AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND CORROSION ON THE MAIN CABIN ATTACHED WEB AT BS 917 L-18L. REMOVED CORROSION, FABRICATED REPAIR DOUBLER AND INSTALLED IAW DC9 SRM 53-20-1, 51-10-3 AND 51-30-0.
- [SDR AT9900435](https://openairdocs.org/sdr/AT9900435.md): Web · corroded · May 25, 1999 · N805AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE MAIN CABIN LEFT LONGERON NR 18 AT BS 823 ATTACHED WEB CORRODED. REMOVED CORROSION, FABRICATED REPAIR DOUBLER AND INSTALLED IAW DC9 SRM 53-20-1, 51-10-3 AND 51-30-2.
- [SDR AT9900572](https://openairdocs.org/sdr/AT9900572.md): Frame · cracked · May 24, 1999 · N805AT · Doug DC932 · Fuselage Main, Frame
  > DURING SCHEDULED INSPECTION AT TIMCO, FOUND FWD CARGO COMPARTMENT HAS BENT AND CRACKED FRAME AT BS 408 L24L. REMOVED CARGO FRAME FLOOR SUPPORT, FABRICATED REPAIR ANGLE IAW EA NR 12-5321-29-C1362. PRIMED AND INSTALLED IAW DC9 SRM 51-10-3, 51-30-2.
- [SDR AT9900530](https://openairdocs.org/sdr/AT9900530.md): Jamb · gouged · May 21, 1999 · N805AT · Doug DC932 · Wing Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND MAIN RE-FUELING POINT AT LOWER WING SKIN WORN THROUGH WHERE LATCH FOR FUEL DOOR MATES TO LOWER SKIN. FABRICATED FITTINGS. DRILLED, DEBURRED AND COUNTERSUNK HOLES IN FITTINGS. INSTALLED FITTINGS IAW
- [SDR AT9900571](https://openairdocs.org/sdr/AT9900571.md): Bulkhead Panel · corroded · May 20, 1999 · N805AT · Doug DC932 · Fuselage Main, Bulkhead
  > DURING SCHEDULED INSPECTION AT TIMCO, FOUND AFT PIT FWD LT BULKHEAD PANEL HAD SEVERAL SPOTS OF SURFACE CORROSION. MECHANICALLY CLEANED AREAS, FABRICATED NEW PANEL, LOCATED, DRILLED, DEBURRED, TREATED AND PRIMED IAW DC9 SRM 51-10-4, 51-10-3.
- [SDR AT9900524](https://openairdocs.org/sdr/AT9900524.md): Strap · corroded · May 20, 1999 · N805AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FWD PIT CENTER CEILING PANEL FASTENER STRIPS CORRODED AT BS 218. MATERIAL LOSS 100 PERCENT, OUT OF LIMITS, FABRICATED, TRIMMED AND DRILLED NEW STRAPS FROM 7075-T6.032 IAW DC9 SRM 57-01, FIG 1, 51-10
- [SDR AT9900142](https://openairdocs.org/sdr/AT9900142.md): Cover · loose · Feb 24, 1999 · N805AT · Doug DC932 · Emergency Equipment
  > FOUND THE R-1 DOOR SLIDE COVER NEEDS TO BE SECURED AND INSPECTED FOR PROPER INSTALLATION. SECURED SLIDE COVER PER MM 25-60.

## 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 = 'N805AT' AND deregistration_id = 'N805AT-2003-05-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N805AT-2003-05-02/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.
