# Service difficulty reports: N817AT, cancelled Sep 30, 2004 A list on [N817AT, cancelled Sep 30, 2004](https://openairdocs.org/deregistered/N817AT-2004-09-30.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR AT0200069](https://openairdocs.org/sdr/AT0200069.md): Wire · broken · Jul 8, 2002 · N817AT · Doug DC932 · Light System Wiring > NR 1 LEFT HAND AFT ACCESSORY EMERGENCY LIGHT WILL NOT ILLUMINATE. REPAIRED BROKEN WIRE L795W18 AT VENTRAL STAIR EMERGENCY LIGHTS PER WDM-31-51, OPS CHECK NORMAL. - [SDR AT0200012](https://openairdocs.org/sdr/AT0200012.md): Skin · cracked · Oct 11, 2001 · N817AT · Doug DC932 · Fuselage Main, Plate/Skin > FUSELAGE EXTERNAL SKIN HAS THREE (3) CRACKS AROUND RIVET HEADS AT STA 164 APPROX AND LONGERON 4 LEFT. CUT OUT DAMAGED AREA. NDT VERIFIED AFTER CUT OUT IAW NDT SRM PART 6-00-01, NO DISCREPANCIES NOTED. MADE SKIN REPAIR AND FINGER DOUBLER AND INSTALLED REPAIR - [SDR AT0200013](https://openairdocs.org/sdr/AT0200013.md): Web · cracked · Oct 10, 2001 · N817AT · Doug DC932 · Fuselage Miscellaneous Structure > FORWARD GALLEY AREA AT FS 200/LBL 31 - LBL 40, FOUND CRACKED TO FLOOR WEB ON (2) EXISTING DOUBLER REPAIRS. REMOVED EXISTING DOUBLER AS PER DC-9 SRM 51-30-2. INSTALLED NEW DOUBLER PER DC-9 SRM 53-01-09. - [SDR AT0000443](https://openairdocs.org/sdr/AT0000443.md): Coupler · missing · Sep 19, 2000 · N817AT · Doug DC932 · Emergency Lighting > E-PATH MISSING COUPLER AT ROW 21. INSTALLED COUPLER IAW BRUCE INDUSTRIES INC PEEPLES INSTALLATION MANUAL 33-21-27. - [SDR AT0000442](https://openairdocs.org/sdr/AT0000442.md): Coupler · missing · Sep 19, 2000 · N817AT · Doug DC932 · Emergency Lighting > E-PATH LIGHTING, RED WIRE HAS NO END AT ROW 17. INSTALLED E-PATH LIGHTING COUPLE IAW 33-21-27. - [SDR AT0000362](https://openairdocs.org/sdr/AT0000362.md): Battery Pack · discharged · Jul 19, 2000 · N817AT · Doug DC932 · Emergency Lighting > FOUND EXIT AND EMERGENCY LIGHTS OUT AT ROW 22 AND 19. REMOVED AND REPLACED BATTERY PACK BATTERIES IAW DC9 MM 33-53-00. - [SDR AT0000359](https://openairdocs.org/sdr/AT0000359.md): Doubler · damaged · Jul 14, 2000 · N817AT · Doug DC932 · Fuselage Main, Plate/Skin > FOUND, REMOVED DOUBLER FROM BS 775. INSTALLED NEW DOUBLER IAW REO L00225. - [SDR AT0000366](https://openairdocs.org/sdr/AT0000366.md): Fitting · gouged · Jul 7, 2000 · N817AT · Doug DC932 · Wing Miscellaneous Structure > FOUND LEFT WING LEADING EDGE GOUGED AT CENTER RIB FITTING. BLENDED OUT GOUGE AND REPAIRED IAW REO-L00228. - [SDR AT0000368](https://openairdocs.org/sdr/AT0000368.md): Skin · lightning strike · Jul 3, 2000 · N817AT · Doug DC932 · Fuselage Main, Plate/Skin > FOUND LIGHTNING STRIKE AT LEFT HAND WINDOW BELT PANEL AT BS 908 - 937. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 MM 25-21-0, 53-05 FIGURE 11 AND REO L00224. - [SDR AT0000367](https://openairdocs.org/sdr/AT0000367.md): Skin · lightning strike · Jul 3, 2000 · N817AT · Doug DC932 · Fuselage Main, Plate/Skin > FOUND LIGHTNING STRIKE AT LEFT HAND WINDOW BELT PANEL AT BS 832 - 870. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 MM 25-21-0, 53-05 FIGURE 11 AND REO L00224. - [SDR AT0000358](https://openairdocs.org/sdr/AT0000358.md): Lap Joint · corroded · Jul 2, 2000 · N817AT · Doug DC932 · Fuselage Main, Plate/Skin > FOUND SKIN LAP FUSELAGE SKIN PITTED BEYOND LIMITS AT L24 - L26. CUT OUT CORRODED SECTION AND INSTALLED REPAIR IAW REO L00229. - [SDR AT0000354](https://openairdocs.org/sdr/AT0000354.md): Attach Angle · corroded · Jun 29, 2000 · N817AT · Doug DC932 · Fuselage Main, Attach Fittings > FOUND G-2 GALLEY ANGLES CORRODED AT RIGHT SIDE OF G-2. REMOVED CORRODED ANGLES, FABRICATED AND INSTALLED NEW ANGLES IAW DC9 51-10-2, 51-10-3, 51-10-4, 51-30-2. - [SDR AT0000357](https://openairdocs.org/sdr/AT0000357.md): Skin · cracked · Jun 25, 2000 · N817AT · Doug DC932 · Fuselage Main, Plate/Skin > FOUND FORWARD CARGO DOOR JAMB, LOWER, HAS CRACKS IN EXTERNAL SKIN. REMOVED EXISTING REPAIR, DOUBLER AND FILLER. CUT OUT CRACKED AREA AND FABRICATED 4 FILLERS, FABRICATED REPAIR DOUBLER AND INSTALLED IAW REO L00223. - [SDR AT0000441](https://openairdocs.org/sdr/AT0000441.md): Spar Cap · corroded · Jun 23, 2000 · N817AT · Doug DC932 · Wing Spar > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND RIGHT OUTBOARD LOWER SPAR CAP CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED ANGLE REPAIR IAW DC9 SRM 57-09 FIG 11 AND 51-10-03. - [SDR AT0000353](https://openairdocs.org/sdr/AT0000353.md): Spar · corroded · Jun 23, 2000 · N817AT · Doug DC932 · Wing Spar > FOUND RIGHT HAND OUTBOARD LOWER SPAR CAP WAS CORRODED. REMOVED CORROSION, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR ANGLE IAW DC9 SRM 57-09 FIGURE 11, 51-10-3. - [SDR AT0000356](https://openairdocs.org/sdr/AT0000356.md): Skin · bulged · Jun 22, 2000 · N817AT · Doug DC932 · Fuselage Main, Plate/Skin > FOUND BULGING SKIN AT BS 917 - 935, L28R - L26. REMOVED AND REPLACED SKIN IAW REO L00232. - [SDR AT0000355](https://openairdocs.org/sdr/AT0000355.md): Skin · corroded · Jun 22, 2000 · N817AT · Doug DC932 · Fuselage Main, Plate/Skin > FOUND CORROSION AT BS 973, STRINGER 20 - 24 ON LEFT HAND SIDE. REMOVED CORROSION AND INSTALLED INTERNAL AND EXTERNAL DOUBLER IAW DC9 SRM 51-10-2, 51-30-2 AND REO L00230 REV B. - [SDR AT0000352](https://openairdocs.org/sdr/AT0000352.md): Attach Angle · corroded · Jun 22, 2000 · N817AT · Doug DC932 · Fuselage Main, Attach Fittings > FOUND AFT CARGO RIGHT HAND AFT BULKHEAD PANEL UPPER ATTACH ANGLE CORRODED. FORMED, FIT, TRIMMED, DRILLED, TREATED, AND PRIMED REPAIR ANGLE. INSTALLED ATTACH ANGLE IAW DCI SRM 51-10-2, 53-21-0 FIGURE 10, 51-10-4, 51-10-3. - [SDR AT9900689](https://openairdocs.org/sdr/AT9900689.md): Doubler · cracked · Sep 17, 1999 · N817AT · Doug DC932 · Fuselage Main, Plate/Skin > FOUND 3 CRACKS IN FUSELAGE NOSE SKIN AT BS 76R BELOW RIGHT INTERCOSTAL. REMOVED, FABRICATED, AND INSTALLED REPAIR INTERNAL DOUBLERS AND FILLERS AT BS 75R IAW DC9 DWG SR09530239. - [SDR AT9900437](https://openairdocs.org/sdr/AT9900437.md): Skin · dented · May 26, 1999 · N817AT · Doug DC932 · Fuselage Main, Plate/Skin > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND MULTIPLE SKIN DAMAGE (DENTS) ON THE RIGHT SIDE AT BS 229-408 L-18-26R. REMOVED AND REPLACED SKIN DAMAGE SECTION. A NEW SPLICE DOUBLER SECTION WAS INSTALLED IAW DC9 SRM 51-20-0, 51-30-1, 51-30-1, 51-30-2, 51 - [SDR AT9900403](https://openairdocs.org/sdr/AT9900403.md): Floorbeam · corroded · May 22, 1999 · N817AT · Doug DC932 · Fuselage Main, Floor Beam > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE PASSENGER CABIN FLOORBEAM IN AFT LAVATORY AREA CHAFED AND CORRODED AT BS 980 BL 0-44L. FORMED NEW FLOORBEAM, LOCATED, DRILLED AND DEBURRED. FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED REPA - [SDR AT9900389](https://openairdocs.org/sdr/AT9900389.md): Floor · corroded · May 19, 1999 · N817AT · Doug DC932 · Fuselage Floor Panel > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE FORWARD ENTRY FLOOR PANEL NR 4692 AT BS 200 BL 0-65R CORRODED. FABRICATED PARTS AND INSTALLED IAW DC9 SRM 53-01 FIG 1, 53-21-0 FIG 2D, 51-70-2, 53-05-0, AND 51-30-2. - [SDR AT9900439](https://openairdocs.org/sdr/AT9900439.md): Floor · corroded · May 15, 1999 · N817AT · Doug DC932 · Fuselage Floor Panel > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE FORWARD ENTRY FLOOR PANEL NR 4693 AT LBL 45-65 CORRODED. REMOVED FLOOR PANEL, FABRICATED, COUNTERSUNK, DEBURRED, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-3, 51-10-2, 53-21-0 FIG 2D. - [SDR AT9900391](https://openairdocs.org/sdr/AT9900391.md): Blkhd Frame · corroded · May 15, 1999 · N817AT · Doug DC932 · Nacelle/Pylon, Bulkhead/Firewall > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND ON THE CABIN LEFT FORWARD PYLON BULKHEAD AFT SIDE LOWER FRAME/FLOOR AT BS 965 CORRODED. CUT, DRILLED, AND DEBURRED NEW ANGLE (SUPPORT). LOCATED, CUT, DRILLED, TRIMMED NEW ANGLE REPAIR, ALODINED, PRIMED, AND - [SDR AT9900402](https://openairdocs.org/sdr/AT9900402.md): Floor · corroded · May 14, 1999 · N817AT · Doug DC932 · Fuselage Floor Panel > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE CABIN FLOOR PANEL NR 90 CORRODED AROUND THE EDGES. REMOVED, FIT, TRIMMED, DRILLED, TREATED, AND PRIMED REPLACEMENT SKIN PANEL AND INSTALLED IAW DC9 SRM 53-21-0, 51-10-2, 51-10-4, AND 51-30-2. - [SDR AT9900390](https://openairdocs.org/sdr/AT9900390.md): Floorbeam · corroded · May 14, 1999 · N817AT · Doug DC932 · Fuselage Main, Floor Beam > SCHEDULED INSPECTION AT TIMCO, FL, FOUND PASSENGER CABIN FLOORBEAM RIGHT SIDE AFT LAVATORY AT BS 996 RBL 17-54R CORRODED. REMOVED UPPER CAP, LOCATED, DRILLED, AND INSTALLED UPPER CAP IAW DC9 SRM 53-11-3 FIG 11, 51-30-5, 51-10-4, AND 51-10-2. - [SDR AT9900376](https://openairdocs.org/sdr/AT9900376.md): Floorbeam · corroded · May 13, 1999 · N817AT · Doug DC932 · Fuselage Main, Floor Beam > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND PASSENGER CABIN FLOORBEAM CHAFED AND CORRODED AT BS 965 BL-30L. FORMED, FIT, TRIMMED, DRILLED AND INSTALLED REPAIR ANGLE IAW DC9 SRM 53-05 FIG 20A. - [SDR AT9900375](https://openairdocs.org/sdr/AT9900375.md): Floor · corroded · May 12, 1999 · N817AT · Doug DC932 · Fuselage Floor Panel > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE FORWARD FLOOR PANEL NR 4691 AT BS 160 TO 200 BL 0-45L CORRODED. FABRICATED NEW FLOOR PANEL, FIT, DRILLED AND INSTALLED NEW SKIN ON HAT CHANNELS AND REINSTALLED FLOOR PANEL IAW DC9 SRM 53-21-0, 51-10-2, A - [SDR AT9900371](https://openairdocs.org/sdr/AT9900371.md): Floorbeam · corroded · May 10, 1999 · N817AT · Doug DC932 · Fuselage Main, Floor Beam > SCHEDULED INSPECTION AT TIMCO, FL. FOUND THE CABIN FLOORBEAM UPPER FLANGE CORRODED AT BS 196 BL 0. REMOVED FLOORBEAM, CUT, DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED NEW FLOORBEAM IAW DC9 SRM 53-01 FIG 1 SHEET 3, 51-30-2, 51-10-3, 53-13-1 AND 53-10-4. - [SDR AT9900440](https://openairdocs.org/sdr/AT9900440.md): Support · corroded · May 8, 1999 · N817AT · Doug DC932 · Fuselage Miscellaneous Structure > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE CABIN ENTRY FLOOR SUPPORT UPPER FLANGE AT BS 196 BL 0-10L CORRODED. REMOVED, FORMED, DRILLED AND INSTALLED SUPPORT IAW DC9 SRM 51-10-4, 51-30-5, 53-11-1 FIG 13, 51-10-2 AND 51-30-2. - [SDR AT9900473](https://openairdocs.org/sdr/AT9900473.md): Subfloor · corroded · May 7, 1999 · N817AT · Doug DC932 · Fuselage Miscellaneous Structure > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND CABIN ENTRY SUBFLOOR AT BS 160 TO 200 RBL 55 CORRODED. FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 53-21-0, 51-10-3, 51-10-4 AND 51-30-1. - [SDR AT9900438](https://openairdocs.org/sdr/AT9900438.md): Doubler · corroded · Apr 29, 1999 · N817AT · Doug DC932 · Fuselage Miscellaneous Structure > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE INTERNAL DOUBLER AT BS 580 STRINGER 30. REMOVED LEADING EDGE WING TO FUSELAGE FILLET PANELS, BLEED AIR DUCTS, END CAPS AND FRAMES FOR ACCESS. REMOVED CORRODED DOUBLER, FABRICATED DOUBLER, DRILLED, DEBUR - [SDR AT9900093](https://openairdocs.org/sdr/AT9900093.md): Light · out of position · Feb 8, 1999 · N817AT · Doug DC932 · Emergency Lighting > EMERGENCY FLOOR LIGHTING WILL NOT STAY ON. REPLACED FLOOR COVER AND WIRING SPLICES AT ROW NR 1. OPERATIONAL TEST NORMAL IAW MM 33-50. ## 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 = 'N817AT' AND deregistration_id = 'N817AT-2004-09-30' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N817AT-2004-09-30/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.