N840AT, cancelled Jan 19, 2005

Service difficulty reports · 34

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

Query with SQL
duckdb -csv -c "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"

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SDR AT0200050Apu · leakingAFTER 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 FApr 23, 2002 · N840AT · Doug DC932 · Smoke DetectionSDR AT0100187Track · corrodedFOUND 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.May 23, 2001 · N840AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR AT0100193Plate · corrodedFOUND 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.May 18, 2001 · N840AT · Doug DC932 · LavatoriesSDR AT0100192Floor Support · corrodedFOUND 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 2May 18, 2001 · N840AT · Doug DC932 · Fuselage Main, Floor BeamSDR AT0100198Longeron · corrodedFOUND LONGERON 16L CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED LONGERON SECTION AT BS 680-699. IAW DC9 SRM 51-10-1 FIGURE 36May 17, 2001 · N840AT · Doug DC932 · Fuselage Main, Floor BeamSDR AT0100191Floor Support · corrodedFOUND CABIN FLOOR SUPPORT AT BS 200 CORRODED. CORRECTIVE ACTION: REMOVED CORROSION, FABRICATED AND INSTALLED FLOOR SUPPORT REPAIR. IAW DC9 SRM 53-01,51-10-4,53-11-1,51-30-5May 17, 2001 · N840AT · Doug DC932 · Fuselage Main, Floor BeamSDR AT0100190Floor Support · corrodedFOUND 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, 51-10-3,51-30-2May 17, 2001 · N840AT · Doug DC932 · Fuselage Main, Floor BeamSDR AT0100197Angle · corrodedFOUND 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, 55-11-3May 16, 2001 · N840AT · Doug DC932 · Fuselage Main, Floor BeamSDR AT0100194Seat Track · corrodedFOUND 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.May 16, 2001 · N840AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR AT0100196Skin · crackedFOUND 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 RES01-0565May 16, 2001 · N840AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0100189Seat Track · corrodedFOUND 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.May 16, 2001 · N840AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR AT0100186Frame · corrodedFOUND 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, 57-10-2,51-10-3,51-10-4,51-30-2,51-30-5May 16, 2001 · N840AT · Doug DC932 · Fuselage Main, FrameSDR AT0100185Pan · corrodedFOUND 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,May 14, 2001 · N840AT · Doug DC932 · Fuselage Main, FrameSDR AT0100184Longeron · corrodedFOUND 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 May 14, 2001 · N840AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT0100195Door Frame · damagedINSTALLED PERMANENT REPAIR AT AFT CARGO DOOR JAMB UPPER CORNER. FABRICATED REPAIR DOUBLERS AND INSTALLED IAW REO-L00444.May 11, 2001 · N840AT · Doug DC932 · Fuselage Main, StructureSDR AT0000477Spar · corrodedDURING 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.Nov 15, 2000 · N840AT · Doug DC932 · Wing SparSDR AT0000405Meter · malfunctionedFOUND ELECTRICAL BURNING SMELL IN COCKPIT AND IN GALLEY AREA. REMOVED AND REPLACED LEFT AND RIGHT DC LOAD METERS.Sep 11, 2000 · N840AT · Doug DC932 · DC Power Distribution SystemSDR AT0000377Fuse · inoperativeFOUND EMERGENCY PATH LIGHTS AT SECTION 6 INOPERATIVE. REPLACED FUSE AT BS 980 EMERGENCY PATH LIGHT BATTERY CHARGER POWER SUPPLY IAW MM 33-50.Aug 4, 2000 · N840AT · Doug DC932 · Emergency LightingSDR AT0000235Fuel Cap · missingON TAKEOFF, PASSENGER REPORTED FUEL COMING FROM RIGHT WING. FOUND FUEL CAP MISSING FROM RIGHT WING. REPLACED CAP.May 6, 2000 · N840AT · Doug DC932 · Fuel StorageSDR AT0000215Skin · dentedFOUND 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.Mar 27, 2000 · N840AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000214Skin · dentedFOUND 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.Mar 27, 2000 · N840AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000217Longeron · corrodedFOUND 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.Mar 25, 2000 · N840AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT0000017Battery Pack · dischargedFOUND 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.Jan 17, 2000 · N840AT · Doug DC932 · Emergency LightingSDR AT9900018Clamp · brokenCLIMBING 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.Jan 11, 1999 · N840AT · Doug DC932 · Pneumatic Distribution SystemSDR AT9900008Skin · corrodedSCHEDULED 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.Jan 6, 1999 · N840AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900003Skin · dentedSCHEDULED 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.Dec 27, 1998 · N840AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900043Skin · dentedSCHEDULED 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 9Dec 23, 1998 · N840AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900042Longeron · corrodedSCHEDULED 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 SECTIDec 17, 1998 · N840AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT9900099Angle · corrodedSCHEDULED 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, 51-1Dec 15, 1998 · N840AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900101Hat · corrodedSCHEDULED 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-Dec 11, 1998 · N840AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900102Bracket · corrodedSCHEDULED 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 DDec 10, 1998 · N840AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900097Spar · misdrilledSCHEDULED 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 Dec 9, 1998 · N840AT · Doug DC932 · Horizontal Stabilizer, Spar/RibSDR AT9900100Frame · chafedSCHEDULED 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 53Dec 8, 1998 · N840AT · Doug DC932 · Fuselage Main, FrameSDR AT9900098Panel · crackedSCHEDULED 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.Dec 6, 1998 · N840AT · Doug DC932 · Cargo Compartments
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