# Service difficulty reports: N830AT, cancelled Jun 8, 2005

A list on [N830AT, cancelled Jun 8, 2005](https://openairdocs.org/deregistered/N830AT-2005-06-08.md).

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

- [SDR AT0200085](https://openairdocs.org/sdr/AT0200085.md): Engine · Oct 20, 2002 · N830AT · Doug DC932 · Engine Ignition Analyzer System
  > #2 ENGINE LOST POWER ON CLIMB OUT-ROLLED BACK TO 70% N1 WITH SIGNIFICANT VIBRATION. ALL OTHER PARAMETERS WITHIN LIMITS WITH POWER AT IDLE VIBE CEASED. CORRECTIVE ACTION: REMOVED AND REPLACED #2 ENGINE IAW P.P. TASK CARDS 99-LEAK AND OP
- [SDR AT0200018](https://openairdocs.org/sdr/AT0200018.md): Longeron · cracked · Nov 7, 2001 · N830AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > LONG 5R CRACKED AT STA 617.
- [SDR AT0200017](https://openairdocs.org/sdr/AT0200017.md): Longeron · cracked · Nov 7, 2001 · N830AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > LONG 6R CRACKED AT STA 617.
- [SDR AT0200016](https://openairdocs.org/sdr/AT0200016.md): Longeron · cracked · Nov 7, 2001 · N830AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > LONG 5L CRACKED AT STA 699.
- [SDR AT0100094](https://openairdocs.org/sdr/AT0100094.md): Warn Panel · malfunctioned · Feb 15, 2001 · N830AT · Doug DC932 · Detection System
  > FOUND SMOKE DETECTOR LOOP LIGHT ON IN FLIGHT, FORWARD CARGO COMPARTMENT LOOP-B. CREW REPORTED LOWER CARGO COMPARTMENT SMOKE DETECTION SYSTEM DID NOT TEST AFTER B-LOOP LIGHT ILLUMINATED. INSPECTED FORWARD AND AFT CARGO COMPARTMENT, NO DEFECTES NOTED. CHECKED
- [SDR AT0000394](https://openairdocs.org/sdr/AT0000394.md): Frame · corroded · Aug 23, 2000 · N830AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND FRAME SEGMENT AT BS 598 CORRODED. REMOVED AND REPLACED FRAME SEGMENT IAW DC9 SRM 51-30-2, 51-30-2, 51-30-5.
- [SDR AT0000439](https://openairdocs.org/sdr/AT0000439.md): Skin · lightning strike · Aug 22, 2000 · N830AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND LIGHTNING STRIKE ON WINDOW FRAME NR 24. BLENDED STRIKE AND INSTALLED DOUBLER IAW REO-L000256 AND DC9 SRM 53-05 FIGURE 11.
- [SDR AT0000385](https://openairdocs.org/sdr/AT0000385.md): Spar Cap · mismanufactured · Aug 22, 2000 · N830AT · Doug DC932 · Horizontal Stabilizer, Spar/Rib
  > FOUND RIGHT HAND SPAR LOWER SPAR CAP REQUIRED TRIMMING PER EO 9-5510-29-1514. COMPLIED WITH EO 9-5510-29-1514.
- [SDR AT0000384](https://openairdocs.org/sdr/AT0000384.md): Spar Cap · mismanufactured · Aug 22, 2000 · N830AT · Doug DC932 · Horizontal Stabilizer, Spar/Rib
  > FOUND LEFT HAND LOWER SPAR CAP REQUIRES TRIMMING PER EO 9-5510-29-E1514 REV A. COMPLIED WITH EO 9-5510-29-E1514 REV A.
- [SDR AT0000392](https://openairdocs.org/sdr/AT0000392.md): Skin · gouged · Aug 21, 2000 · N830AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN HAS 2 GOUGES AT BS 342. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-04 FIGURE 38.
- [SDR AT0000399](https://openairdocs.org/sdr/AT0000399.md): Web · corroded · Aug 20, 2000 · N830AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND CABIN FLOOR WEB CORRODED AROUND BUTTON HEAD AT BS 170 - 180. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-10-3, 53-01 FIGURE 1, 51-10-4, 53-11-1 FIGURE 11, 51-30-2.
- [SDR AT0000389](https://openairdocs.org/sdr/AT0000389.md): Longeron · dented · Aug 20, 2000 · N830AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND DENT IN LEFT LONGERON 17 - 18 AT BS 226. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-04 FIGURE 38.
- [SDR AT0000388](https://openairdocs.org/sdr/AT0000388.md): Skin · dented · Aug 20, 2000 · N830AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND DENT AT BS 251 LEFT LONGERON. DENT OUT OF LIMITS, INSPECTED, FABRICATED AND INSTALLED INTERNAL DOUBLER IAW DC9 SRM 53-04 FIGURE 38, 51-10-3, 51-30-2.
- [SDR AT0000400](https://openairdocs.org/sdr/AT0000400.md): Trunnion · corroded · Aug 18, 2000 · N830AT · Doug DC932 · Main Landing Gear Attach Section
  > FOUND RIGHT MAIN LANDING GEAR SIDE BRACE TRUNNION LUG HAS CORROSION ON FORWARD AND AFT FACE. REMOVED BUSHING FROM RIGHT TRUNNION, REMOVED CORROSION BY SPOT FACING LUG, FABRICATED NEW BUSHING AND SHIMS AND INSTALLED IAW DC9 OHC 20-10-3, 57-40-1 AND TIMCO REO-L
- [SDR AT0000390](https://openairdocs.org/sdr/AT0000390.md): Frame · corroded · Aug 18, 2000 · N830AT · Doug DC932 · Fuselage Main, Frame
  > FOUND FRAME AT BS 148R EXFOLIATED CORROSION BEYOND LIMITS AND CUSP T-FITTING CORRODED AND CRACKED. REMOVED CUSP TO FRAME T-ATTACH FITTING, FABRICATED Z-DOUBLER, HEAT TREATED, PRIMED AND INSTALLED IAW TIMCO REO - L00250, DC9 SRM 51-10-2, 51-10-5, 51-10-4.
- [SDR AT0000386](https://openairdocs.org/sdr/AT0000386.md): Floor Panel · corroded · Aug 18, 2000 · N830AT · Doug DC932 · Fuselage Floor Panel
  > FOUND FORWARD CARGO COMPARTMENT FLOOR PANEL CORRODED. TRIMMED, DRILLED AND DEBURRED REPLACEMENT FLOOR PANEL AND INSTALLED IAW DC9 SRM 51-10-2, 51-10-4, 51-10-3.
- [SDR AT0000398](https://openairdocs.org/sdr/AT0000398.md): Floorboard · corroded · Aug 16, 2000 · N830AT · Doug DC932 · Fuselage Floor Panel
  > FOUND FLOORBOARD NR 523 HAS CORROSION AT UPPER SURFACE. REMOVED CORROSION FROM FLOORBOARD, FABRICATED AND INSTALLED NEW FLOORBOARD IAW DC9 SRM 51-10-3.
- [SDR AT0000387](https://openairdocs.org/sdr/AT0000387.md): Floor Panel · corroded · Aug 16, 2000 · N830AT · Doug DC932 · Fuselage Floor Panel
  > FOUND CORROSION ON FLOOR PANEL NR 4695A. DRILLED, DEBURRED AND REPLACED FLOOR PANEL SKIN AND HAT CHANNELS IAW DC9 SRM 51-10-2, 51-10-5, 51-40-4, 53-21-0.
- [SDR AT0000383](https://openairdocs.org/sdr/AT0000383.md): Floorboard · corroded · Aug 16, 2000 · N830AT · Doug DC932 · Fuselage Floor Panel
  > FOUND CORROSION ON FLOORBOARD NR 4694. CUT, DRILLED, DEBURRED, PRIMED AND INSTALLED HAT CHANNEL FLOORBOARD IAW DC9 SRM 51-10-03 AND 53-21-0.
- [SDR AT0000438](https://openairdocs.org/sdr/AT0000438.md): Skin · lightning strike · Aug 15, 2000 · N830AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND LIGHTNING STRIKE AT WINDOW 20, LOWER AND UPPER AFT CORNER. BLENDED STRIKE AND FABRICATED FULL SURROUND DOUBLER IAW TIMCO REO-L00254.
- [SDR AT0000397](https://openairdocs.org/sdr/AT0000397.md): Angle · gouged · Aug 15, 2000 · N830AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND L1 DOOR JAMB SEAL DEPRESSOR ANGLE WAS FOUND TO BE CHAFED, GOUGED, AND BENT AT UPPER AFT DOOR STOP. RE-CONTOURED L1 DOOR JAMB SEAL DEPRESSOR, BLENDED OUT CHAFED AND GOUGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE IAW DC9 SRM 53-01, 51-10-2, 51-10-3, 5
- [SDR AT0000396](https://openairdocs.org/sdr/AT0000396.md): Fitting · corroded · Aug 15, 2000 · N830AT · Doug DC932 · Wing Miscellaneous Structure
  > FOUND RIGHT WING AT XRS 160 BUTE DOOR HINGE FITTING CORRODED. REMOVED CORROSION AND INSTALLED REPAIR IAW DC9 SRM 53-01 FIGURE 1.
- [SDR AT0000395](https://openairdocs.org/sdr/AT0000395.md): Floor Panel · corroded · Aug 15, 2000 · N830AT · Doug DC932 · Fuselage Floor Panel
  > FOUND FLIGHT COMPARTMENT CENTER FLOOR PANEL DELAMINATED AT FORWARD RIGHT CORNER AND CORRODED AT UPPER SURFACE. CUT, DRILLED, DEBURRED AND INSTALLED NEW FLOOR PANEL IAW DCI SRM 51-10-2, 51-10-3, 51-10-4.
- [SDR AT0000393](https://openairdocs.org/sdr/AT0000393.md): Skin · corroded · Aug 15, 2000 · N830AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND CORROSION ON INTERIOR FUSELAGE SKIN BEHIND LOWER CORNER R1 DOOR CUTOUT. REMOVED CORROSION ON UPPER CUSP, FABRICATED AND INSTALLED DOUBLER, CUT SPLICED AND REPAIRED R1 DOOR JAMB IAW TIMCO REO-L00253 DC9 SRM 53-05 FIGURE 55.
- [SDR AT0000440](https://openairdocs.org/sdr/AT0000440.md): Frame · lightning strike · Aug 14, 2000 · N830AT · Doug DC932 · Fuselage Main, Structure
  > FOUND LIGHTNING STRIKE AT WINDOW FRAME NR 50 LOWER FORWARD CORNER. BLENDED AREA AND FOUND TO BE WITHIN LIMITS IAW TIMCO REO-L00252, 51-10-3 AND 53-05 FIGURE 11.
- [SDR AT0000492](https://openairdocs.org/sdr/AT0000492.md): Skin · dented · Aug 12, 2000 · N830AT · Doug DC932 · Horizontal Stabilizer, Plate/Skin
  > FOUND RIGHT HORIZONTAL STABILIZER LOWER SURFACE APPROX XHS 104 DENTED. HFEC INSPECTED RIGHT HORIZONTAL STAB LOWER SURFACE. IAW DC9 SRM PT06. NO CRACKS NOTED. REO-L00263 NOTES DENTS ACCEPTABLE FOR STRENGTH AS IS WITH NO REPAIR REQUIRED, NO SPECIAL REPETIT
- [SDR AT0000391](https://openairdocs.org/sdr/AT0000391.md): Skin · corroded · Aug 12, 2000 · N830AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND CORROSION AT PIT BOTTOM EDGE AT BS 380 - 415. REMOVED THRESHOLD, AND CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLERS IAW DC9 SRM 51-10-3, 53-01 FIGURE 1, 53-05 FIGURE 105, 25-52-1.
- [SDR AT0000365](https://openairdocs.org/sdr/AT0000365.md): Duct · disconnected · Jul 16, 2000 · N830AT · Doug DC932 · Cabin Pressure Control System
  > MASKS DEPLOYED DUE TO LACK OF PRESSURIZATION. RECONNECTED RIGHT ACM OUTLET DUCT AND CLAMP ASSEMBLY. RECONNECTED LEFT PACK DUCT AND CLAMP ASSEMBLY IAW DC9 MM 21-30.
- [SDR AT0000333](https://openairdocs.org/sdr/AT0000333.md): Battery · discharged · Jul 6, 2000 · N830AT · Doug DC932 · Emergency Lighting
  > FOUND AFT ACCESSORY EMERGENCY LIGHT NOT ILLUMINATING. REMOVED AND REPLACED NICAD BATTERIES IN BATTERY PACK IAW DC9 MM.
- [SDR AT9900496](https://openairdocs.org/sdr/AT9900496.md): Skin · cracked · Jul 22, 1999 · N830AT · Doug DC932 · Fuselage Main, Plate/Skin
  > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND FUSELAGE SKIN AT BS 169 L-22L CRACKED. REMOVED DOUBLER AND FABRICATED REPAIR AND INSTALLED IAW AIRTRAN RES NR 99-1265 AND EA NR 09-5310-29-A1487.
- [SDR AT9900497](https://openairdocs.org/sdr/AT9900497.md): Pan · cracked · Jul 1, 1999 · N830AT · Doug DC932 · Cargo/Baggage Doors
  > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE AFT LOWER CARGO DOOR INNER PAN CRACKED. BLENDED AREA SMOOTH, FABRICATED REPAIR DOUBLER, DRILLED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-3, AND EO NR 99-1181.
- [SDR AT9900503](https://openairdocs.org/sdr/AT9900503.md): Floor Support · cracked · Jun 23, 1999 · N830AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND CRACKED FLOOR SUPPORT FWD CARGO COMPARTMENT AT BS 503 AND BL 3L. STOP DRILLED CRACK IAW EA NR 12-5321-29-C1362 OPT 1 STEP 1. NDT PERFORMED, CRACK CONTAINED. WELD REPAIR 1 EACH CRACK ON FLOOR SUP
- [SDR AT9900508](https://openairdocs.org/sdr/AT9900508.md): Support · misdrilled · Jun 21, 1999 · N830AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND MISDRILLED HOLES IN FRAME AND FLOOR SUPPORT AT BS 541 AND LONGERON 24-27 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLES ON FLOOR SUPPORT AND FRAME IAW EA NR 12-5321-29-C1362 AND DC9 SRM 51-10-2, 53
- [SDR AT9900495](https://openairdocs.org/sdr/AT9900495.md): Fitting · misdrilled · Jun 19, 1999 · N830AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND MISDRILLED HOLE IN INTERCOSTAL SUPPORT FITTING AT BS 541 L-24R. REMOVED FITTING, SPOT FACE HOLE, NDT VERIFIED NO CRACKS. PLUG HOLE WITH HL-18 HI-LOK IAW DC9 SRM 51-30-5 AND TIMCO RES NR 07654.
- [SDR AT9900471](https://openairdocs.org/sdr/AT9900471.md): Angle · corroded · Jun 18, 1999 · N830AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE FORWARD CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT BS 218 CORRODED. FABRICATED SUPPORT ANGLE AND INSTALLED IAW DC9 SRM 51-10-2, 53-01 FIG 2, AND 51-10-4.
- [SDR AT9900488](https://openairdocs.org/sdr/AT9900488.md): Tie Down · corroded · Jun 12, 1999 · N830AT · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE AFT CARGO TIE DOWN CLOSE OUT RING CORRODED AT BS 889. FABRICATED NEW CLOSE OUT RING IAW DC9 SRM 53-01 FIG 1 AND 51-10-4.
- [SDR AT9900509](https://openairdocs.org/sdr/AT9900509.md): Fitting · cracked · Jun 10, 1999 · N830AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND CRACK IN FLOOR SUPPORT FWD CARGO COMPARTMENT AT BS 560 BL 16R. REMOVED CRACKED FLOOR SUPPORT FITTING, DRILLED, DEBURRED NEW FITTING AND INSTALLED IAW DC9 SRM 51-30-5, 51-10-4, AND TIMCO RES NR 076
- [SDR AT9900507](https://openairdocs.org/sdr/AT9900507.md): Support · cracked · Jun 10, 1999 · N830AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND CRACK IN FLOOR SUPPORT FWD CARGO COMPARTMENT AT BS 522 AND BL 6L. STOP DRILLED, FABRICATED DOULBER REPAIR, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-3, 53-01 FIG 2, 51-10-4 AND EA NR 12-5321
- [SDR AT9900506](https://openairdocs.org/sdr/AT9900506.md): Support · cracked · Jun 10, 1999 · N830AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND CRACK IN FLOOR SUPPORT FWD CARGO COMPARTMENT AT BS 503 AND BL13L. STOP DRILLED, CONFIRMED CRACK CONTAINED. REMOVED FLOOR SUPPORT, WELD REPAIRED 1 EA CRACK. TREATED, PRIMED AND INSTALLED IAW DC9 S
- [SDR AT9900505](https://openairdocs.org/sdr/AT9900505.md): Support · cracked · Jun 10, 1999 · N830AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND CRACK IN FLOOR SUPPORT FWD CARGO COMPARTMENT AT BS 503 AND BL 6R. STOP DRILLED, NDT VERIFED CRACK TERMINATED. WELD REPAIRED 2 EACH CRACK. TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-3, 51-3
- [SDR AT9900504](https://openairdocs.org/sdr/AT9900504.md): Support · cracked · Jun 10, 1999 · N830AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND CRACK IN FLOOR SUPPORT FWD CARGO COMPARTMENT AT BS 503 AND BL 13R. REMOVED SUPPORT, STOP DRILLED NDT VERIFIED CRACK TERMINATED. WELD REPAIRED 1 EACH CRACK IAW EA NR 12-5321-29-C1362 OPT 2 STEP 4.
- [SDR AT9900502](https://openairdocs.org/sdr/AT9900502.md): Support · cracked · Jun 10, 1999 · N830AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND THREE CRACKS IN FLOOR SUPPORT FWD CARGO COMPARTMENT AT BS 465 AND L29-30R. REMOVED FLOOR SUPPORT. STOP DRILLED 3 EACH CRACKS IAW EA NR 12-5321-29-C1362 REV IR DATED 1-5-98, OPTION 1, STEP 1. NDT
- [SDR AT9900501](https://openairdocs.org/sdr/AT9900501.md): Support · cracked · Jun 10, 1999 · N830AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND TWO CRACKS UNDERSIDE FLOOR SUPPORT FWD CARGO COMPARTMENT AT BS 446 AND L28-29L. STOP DRILLED CRACKS, NDT VERIFIED. WELD REPAIR CRACKS AND INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-30-2, AND EA NR 12-5
- [SDR AT9900511](https://openairdocs.org/sdr/AT9900511.md): Support · cracked · Jun 9, 1999 · N830AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND AFT PIT FLOOR SUPPORT FRAME STA 851 CRACKED ABOVE LONGERON 28L. REMOVED FLOOR SUPPORT. INSPECTED CRACK IDENTIFIED AND CONTAINED AFTER STOP DRILLED. FABRICATED REPAIR DOUBLER, PRIMED, AND INSTALLE
- [SDR AT9900510](https://openairdocs.org/sdr/AT9900510.md): Support · cracked · Jun 9, 1999 · N830AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND AFT PIT FLOOR SUPPORT FRAME STA 832 CRACKED ABOVE LONGERON 29L. STOP DRILL CRACK, REMOVED FLOOR SUPPORT FRAME. HFEC VERIFIED CRACK CONTAINED. WELDED REPAIR 2 CRACKS ON FLOOR SUPPORT, PRIMED AND
- [SDR AT9900500](https://openairdocs.org/sdr/AT9900500.md): Support · cracked · Jun 9, 1999 · N830AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION AT TIMCO, IN LAKE CITY, FL, FOUND CRACK BEYOND DOUBLER UNDERSIDE FLOOR SUPPORT FWD CARGO COMPARTMENT AT BS 446 AT LONGERON 30. REMOVED EXISTING SPLICE DOUBLER, STOP DRILLED CRACK, FABRICATED REPAIR AND INSTALLED REPAIR AND SPLICE
- [SDR AT9900470](https://openairdocs.org/sdr/AT9900470.md): Support · corroded · Jun 9, 1999 · N830AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE LEFT HAND FLOOR SUPPORT AT BS 828-865 CORRODED AROUND FASTENER HOLES. REMOVED AND FABRICATED REPLACEMENT IAW DC9 SRM 51-10-2, 53-01 FIG 1, 51-30-2 AND 51-10-2.
- [SDR AT9900150](https://openairdocs.org/sdr/AT9900150.md): Light · inop · Feb 17, 1999 · N830AT · Doug DC932 · Emergency Lighting
  > FOUND THE FLOOR PATH LIGHTING ASSEMBLY MISSING AT ROW 24DEF. INSTALLED SERVICEABLE LIGHT ASSEMBLY IAW MM 33-53-01, OPS CHECKED GOOD. LENS (P/N 07912), SOCKET (P/N 08169-1).

## 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 = 'N830AT' AND deregistration_id = 'N830AT-2005-06-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N830AT-2005-06-08/reports

---
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