# Service difficulty reports: N840AT, cancelled Jan 19, 2005 A list on [N840AT, cancelled Jan 19, 2005](https://openairdocs.org/deregistered/N840AT-2005-01-19.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR AT0200050](https://openairdocs.org/sdr/AT0200050.md): Apu · leaking · Apr 23, 2002 · N840AT · Doug DC932 · Smoke Detection > AFTER TAKE OFF AFT FLIGHT ATTENDANT REPORTED BOTH AFT LAVATORY SMOKE SOUNDED AND A LIGHT SMOKE COULD BE SEEN; STRONG ODOR. CORRECTIVE ACTION: REMOVED AND REPLACED APU AND CHANGED COELESOR BAG RAN ENGINES OPS CHECK AC SYSTEM NO ODOR COMING F - [SDR AT0100187](https://openairdocs.org/sdr/AT0100187.md): Track · corroded · May 23, 2001 · N840AT · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings > FOUND CABIN SEAT TRACK AT BS 200-240 WAS FOUND TO BE CORRODED BEYOND LIMITS. CORRECTIVE ACTION: INSTALLED NEW SEAT TRACK SPLICE. IAW DC9 SRM 51-30-5,51-30-1,53-05 FIGURE 4. - [SDR AT0100193](https://openairdocs.org/sdr/AT0100193.md): Plate · corroded · May 18, 2001 · N840AT · Doug DC932 · Lavatories > FOUND RIGHT LAVATORY KICK PLATE CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-10-3, 53-01 FIGURE 1, 51-10-2, 51-10-4, 53-30-2. - [SDR AT0100192](https://openairdocs.org/sdr/AT0100192.md): Floor Support · corroded · May 18, 2001 · N840AT · Doug DC932 · Fuselage Main, Floor Beam > FOUND CABIN FLOOR SUPPORT AT BS 992 CORRODED. CORRECTIVE ACTION: REMOVED CORROSION, FABRICATED AND INSTALLED FLOOR SUPPORT REPAIR. IAW DC9 SRM 53-11-1 FIGURE 11, 51-10-3,51-30-2, 53-01 FIGURE 2 - [SDR AT0100198](https://openairdocs.org/sdr/AT0100198.md): Longeron · corroded · May 17, 2001 · N840AT · Doug DC932 · Fuselage Main, Floor Beam > FOUND LONGERON 16L CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED LONGERON SECTION AT BS 680-699. IAW DC9 SRM 51-10-1 FIGURE 36 - [SDR AT0100191](https://openairdocs.org/sdr/AT0100191.md): Floor Support · corroded · May 17, 2001 · N840AT · Doug DC932 · Fuselage Main, Floor Beam > FOUND CABIN FLOOR SUPPORT AT BS 200 CORRODED. CORRECTIVE ACTION: REMOVED CORROSION, FABRICATED AND INSTALLED FLOOR SUPPORT REPAIR. IAW DC9 SRM 53-01,51-10-4,53-11-1,51-30-5 - [SDR AT0100190](https://openairdocs.org/sdr/AT0100190.md): Floor Support · corroded · May 17, 2001 · N840AT · Doug DC932 · Fuselage Main, Floor Beam > FOUND CABIN FLOOR SUPPORT AT BS 160-218 CORRODED. CORRECTIVE ACTION: REMOVED CORROSION, FABRICATED AND INSTALLED FLOOR SUPPORT REPAIR. IAW DC9 SRM 53-11-1 FIGURE 11, 51-10-3,51-30-2 - [SDR AT0100197](https://openairdocs.org/sdr/AT0100197.md): Angle · corroded · May 16, 2001 · N840AT · Doug DC932 · Fuselage Main, Floor Beam > FOUND CORROSION IN THE AFT PIT ON THE CABIN FLOOR BEAM AT BS 996. CORRECTIVE ACTION: REMOVED, FABRICATED, DRILLED, AND INSTALLED REPLACEMENT UPPER CAP. IAW DC9 SRM 51-10-3, 53-01 FIGURE 1 51-30-2, 51-30-5, 51-10-4, 55-11-3 - [SDR AT0100194](https://openairdocs.org/sdr/AT0100194.md): Seat Track · corroded · May 16, 2001 · N840AT · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings > FOUND CAPTAINS SEAT TRACK AFT INBOARD AREA CORRODED. CORRECTIVE ACTION: REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR. IAW DC9 53-01 FIGURE 1, 51-30-2, 51-10-4, 51-10-3. - [SDR AT0100196](https://openairdocs.org/sdr/AT0100196.md): Skin · cracked · May 16, 2001 · N840AT · Doug DC932 · Fuselage Miscellaneous Structure > FOUND CRACK IN FORWARD CORNER OF L-1 DOOR CUT OUT. CORRECTIVE ACTION TRIMMED OUT CRACK, FABRICATED AND INSTALLEK FILLER, DOUBLER AND TRIPLER. IAW DC9 SRM 53-05 FIGURE 114 AND RES01-0565 - [SDR AT0100189](https://openairdocs.org/sdr/AT0100189.md): Seat Track · corroded · May 16, 2001 · N840AT · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings > FOUND CABIN SEAT TRACK CORRODED AT BS 200-965 BL22L. CORRECTIVE ACTION: REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR. IAW DC9 SRM 51-30-5, 51-30-2, 53-05 FIGURE 4, 51-10-3, 51-10-2. - [SDR AT0100186](https://openairdocs.org/sdr/AT0100186.md): Frame · corroded · May 16, 2001 · N840AT · Doug DC932 · Fuselage Main, Frame > FOUND CORROSION ON AFT SIDE OF FRAME 965. CORRECTIVE ACTION: REMOVED CORROSION AND INSTALLED NEW FRAME, LOWER AND UPPER SPLICES. FABRICATED DOUBLER AND INSTALLED. IAW DC9 SRM 53-03 FIGURE 24, 57-10-2,51-10-3,51-10-4,51-30-2,51-30-5 - [SDR AT0100185](https://openairdocs.org/sdr/AT0100185.md): Pan · corroded · May 14, 2001 · N840AT · Doug DC932 · Fuselage Main, Frame > FOUND FORWARD CARGO DOOR FRAME LOWER PAN CORRODED. CORRECTIVE ACTION: REMOVED CORROSION AND FOUND TO BE OUT OF LIMIITS. REMOVED FORWARD AND AFT LOWER PAN SPLICES. CUT, TRIMMED, DRILLED AND INSTALLED SPLICES. IAW DC9 SRM 53-04 FIGURE 44, - [SDR AT0100184](https://openairdocs.org/sdr/AT0100184.md): Longeron · corroded · May 14, 2001 · N840AT · Doug DC932 · Fuselage Main, Longeron/Stringer > FOUND CORROSION ON LONGERON AND SKIN AREA AT BS 1117-L17R IN AFT ACCESSORY COMPARTMENT. CORRECTIVE ACTION: REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPLACED LONGERON SECTION WITH REPAIR LONGERON, TRIMMED, FABRICATED AND INSTALLED REPAIR - [SDR AT0100195](https://openairdocs.org/sdr/AT0100195.md): Door Frame · damaged · May 11, 2001 · N840AT · Doug DC932 · Fuselage Main, Structure > INSTALLED PERMANENT REPAIR AT AFT CARGO DOOR JAMB UPPER CORNER. FABRICATED REPAIR DOUBLERS AND INSTALLED IAW REO-L00444. - [SDR AT0000477](https://openairdocs.org/sdr/AT0000477.md): Spar · corroded · Nov 15, 2000 · N840AT · Doug DC932 · Wing Spar > DURING A SCHEDULED INSPECTION. FOUND INTERGRANNULAR CORROSION AT RIGHT WING LOWER SPAR LOWER SIDE INBOARD OF FUELING PANEL. CUT OUT CORROSION AND INSTALLED REPAIR IAW REO L-00304. - [SDR AT0000405](https://openairdocs.org/sdr/AT0000405.md): Meter · malfunctioned · Sep 11, 2000 · N840AT · Doug DC932 · DC Power Distribution System > FOUND ELECTRICAL BURNING SMELL IN COCKPIT AND IN GALLEY AREA. REMOVED AND REPLACED LEFT AND RIGHT DC LOAD METERS. - [SDR AT0000377](https://openairdocs.org/sdr/AT0000377.md): Fuse · inoperative · Aug 4, 2000 · N840AT · Doug DC932 · Emergency Lighting > FOUND EMERGENCY PATH LIGHTS AT SECTION 6 INOPERATIVE. REPLACED FUSE AT BS 980 EMERGENCY PATH LIGHT BATTERY CHARGER POWER SUPPLY IAW MM 33-50. - [SDR AT0000235](https://openairdocs.org/sdr/AT0000235.md): Fuel Cap · missing · May 6, 2000 · N840AT · Doug DC932 · Fuel Storage > ON TAKEOFF, PASSENGER REPORTED FUEL COMING FROM RIGHT WING. FOUND FUEL CAP MISSING FROM RIGHT WING. REPLACED CAP. - [SDR AT0000215](https://openairdocs.org/sdr/AT0000215.md): Skin · dented · Mar 27, 2000 · N840AT · Doug DC932 · Fuselage Main, Plate/Skin > FOUND DENT ON VENTRAL STAIRS SKIN PANEL NR 158965, BS 1087 - 1159. REMOVED AND REPLACED VENTRAL STAIR SKIN AT BS 1087 - 1159 IAW EO 0030300 PART 1 AND DC9 SRM 51-30-02. - [SDR AT0000214](https://openairdocs.org/sdr/AT0000214.md): Skin · dented · Mar 27, 2000 · N840AT · Doug DC932 · Fuselage Main, Plate/Skin > FOUND DENTS IN SKIN AROUND RIGHT HAND SIDE OF VENTRAL STAIRS. INSTALLED SPLICE REPAIR AND SKIN PANEL AT BS 1112 THROUGH 1156 IAW EO 0030300 PART 2. - [SDR AT0000217](https://openairdocs.org/sdr/AT0000217.md): Longeron · corroded · Mar 25, 2000 · N840AT · Doug DC932 · Fuselage Main, Longeron/Stringer > FOUND BUTT SEAM AT BS 995, LONGERON 23 RIGHT TO HAVE A BULGE, D AREA. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW DC9 SRM 51-10-3, 53-04 FIGURE 12B AND EO 00.0290. - [SDR AT0000017](https://openairdocs.org/sdr/AT0000017.md): Battery Pack · discharged · Jan 17, 2000 · N840AT · Doug DC932 · Emergency Lighting > FOUND BOTH RIGHT OVERWING EMERGENCY EXIT LIGHTS DIM AND FLICKERING. REMOVED AND REPLACED BOTH RIGHT OVERWING EMERGENCY EXIT LIGHT BATTERY PACKS IAW DC9 MM 33-53. - [SDR AT9900018](https://openairdocs.org/sdr/AT9900018.md): Clamp · broken · Jan 11, 1999 · N840AT · Doug DC932 · Pneumatic Distribution System > CLIMBING THROUGH 14,000 FEET MASTER WARNING LIGHT ILLUMINATED WITH TAIL COMPARTMENT TEMPERATURE HI-LIGHT ON, NORMAL PROCEDURES FOLLOWED. REPLACED BROKEN CLAMP AT LEFT HAND HEAT EXCHANGER PRIMARY AIR DUCTING PER MM 36-10. - [SDR AT9900008](https://openairdocs.org/sdr/AT9900008.md): Skin · corroded · Jan 6, 1999 · N840AT · Doug DC932 · Fuselage Main, Plate/Skin > SCHEDULED INSPECTION AT AERO CORP, FL. REMOVED LOWER SIDE SKIN FROM FS 229 TO 598 LONGERON 18R THRU 26R FOR REPLACEMENT DUE TO NUMEROUS DENTS AND CORROSION IAW DC9 MM 28-10-7, 30-10-7, SRM 51-10-3, 53-01, 51-30-2 AND AIRTRAN RES 982246. - [SDR AT9900003](https://openairdocs.org/sdr/AT9900003.md): Skin · dented · Dec 27, 1998 · N840AT · Doug DC932 · Fuselage Miscellaneous Structure > SCHEDULED INSPECTION AT AERO CORP, FL, DENT IS CREASED OUT OF LIMITS AT FS 242 LB 19L PER DC9 SRM 53-04 FIG 38 SHEET 10 REFERENCE 099650 PAGE 1 OF 4. FABRICATED DOUBLER FROM 2024 T3.063 PO NR 675752 AND INSTALLED PER DC9 SRM 53-04 FIG 38 AND RES 982292. - [SDR AT9900043](https://openairdocs.org/sdr/AT9900043.md): Skin · dented · Dec 23, 1998 · N840AT · Doug DC932 · Fuselage Main, Plate/Skin > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND TWO DENTS TO CLOSE TO EACH OTHER AND CREASED OUT OF LIMITS AT STA 882 AND STA 884 L-24R. CUT OUT CREASED AREAS AT STRINGER, FABRICATED, TREATED, AND PRIMED DOUBLERS IAW DC9 SRM 53-04 FIG 12B, 51-10-3, AND RES NR 9 - [SDR AT9900042](https://openairdocs.org/sdr/AT9900042.md): Longeron · corroded · Dec 17, 1998 · N840AT · Doug DC932 · Fuselage Main, Longeron/Stringer > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION OUT OF LIMITS AND LEVEL 2 CORROSION AT THE FORWARD CARGO PIT COMPARTMENT AT STA 517 L-27R AND STA 218 L-29L. REMOVED CORROSION OUT OF LIMITS, FABRICATED AND INSTALLED NEW FLOOR CHANNEL AND LONGERON SECTI - [SDR AT9900099](https://openairdocs.org/sdr/AT9900099.md): Angle · corroded · Dec 15, 1998 · N840AT · Doug DC932 · Fuselage Miscellaneous Structure > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FLOOR SUPPORT ANGLE AT AFT BULKHEAD OF E/E COMPARTMENT CORRODED BEYOND LIMITS. REMOVED CORRODED FLOOR SUPPORT ANGLE, FABRICATED EXTRUSION, HEAT TREATED, DRILLED, AND INSTALLED IAW DC9 SRM 51-10-4, 51-30-1, 51-1 - [SDR AT9900101](https://openairdocs.org/sdr/AT9900101.md): Hat · corroded · Dec 11, 1998 · N840AT · Doug DC932 · Fuselage Miscellaneous Structure > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE AFT HAT SECTION CANTED FRAME AT STA 1089 L-6R CORRODED. REMOVED HAT SECTION OUTBOARD OF L-6R, ALSO TREATED AND PRIMED CANTED FRAME AT L-10L TO L-10R. FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-10-3, 53-01- - [SDR AT9900102](https://openairdocs.org/sdr/AT9900102.md): Bracket · corroded · Dec 10, 1998 · N840AT · Doug DC932 · Fuselage Miscellaneous Structure > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE AFT ACCESSORY COMPARTMENT CABLE PULLEY BRACKET HAS CORROSION AT STA 1120 LEFT SIDE LOWER AREA. REMOVED, REPLACED, AND INSTALLED NEW PULLEY BRACKET IN AFT ACCESSORY COMPARTMENT IAW DC9 MM 16-10-20. SYSTEM NOT D - [SDR AT9900097](https://openairdocs.org/sdr/AT9900097.md): Spar · misdrilled · Dec 9, 1998 · N840AT · Doug DC932 · Horizontal Stabilizer, Spar/Rib > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND LEFT HAND HORIZONTAL STABILIZER UPPER SPAR CAP HAS HOLE DRILLED ON UPPER SIDE NEXT TO FASTENER HOLE AT STA 120. REMOVED NUT PLATE CLIP, REPAIRED FASTENER HOLE BY STEPPING UP HOLE AND REINTALLING NUT PLATE CLIP IAW - [SDR AT9900100](https://openairdocs.org/sdr/AT9900100.md): Frame · chafed · Dec 8, 1998 · N840AT · Doug DC932 · Fuselage Main, Frame > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE AFT SECTION INTERIOR TAIL CONE RELEASE HANDLE METALLIC PLACARD WAS CHAFFING AGAINST THE FRAME AT STA 1143. CLEAN UP WORN FRAME, FABRICATED STRAP TO BACK SIDE OF FRAME FLANGE, PRIMED AND INSTALLED IAW DC9 SRM 53 - [SDR AT9900098](https://openairdocs.org/sdr/AT9900098.md): Panel · cracked · Dec 6, 1998 · N840AT · Doug DC932 · Cargo Compartments > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD PIT NR 2 AND NR 3 LOWER SIDE WALL PANEL HAS A 4 CRACK AND 8 HOLE. REMOVED, REPLACED, FABRICATED, TRIMMED, AND DRILLED NEW PANELS IAW DC9 SRM 51-30-0, 53-21-0, MM 25-52-1, AND RES NR 982221. ## 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 = 'N840AT' AND deregistration_id = 'N840AT-2005-01-19' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N840AT-2005-01-19/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.