N813AT, cancelled May 16, 2006

Service difficulty reports · 37

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 = 'N813AT' AND deregistration_id = 'N813AT-2006-05-16'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR AT9900864Lamp · failedFOUND L1 DOOR OVERHEAD EMERGENCY LIGHT WILL NOT ILLUMINATE. RELAMPED, OPS CHECK NORMAL IAW DC9 MM 33-50.Dec 2, 1999 · N813AT · Doug DC932 · Emergency LightingSDR AT9900704Bulb · failedFOUND BOTH TAIL CONE SLIDE EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED LAMPS IAW DC9 MM 33-50.Oct 2, 1999 · N813AT · Doug DC932 · Emergency LightingSDR AT9900272Hardware · missingON CLIMBOUT, NR 2 ENGINE AT POWER BACK UNABLE TO REDUCE POWER BELOW MAXIMUM CLIMB. THROTTLE MOVEMENT NORMAL BUT POWER REMAINS AT MAXIMUM CLIMB AFTER BEING RETARDED, NO RESPONSE. DIVERTED TO CHICAGO O'HARE AND DECLARED EMERGENCY. OPENED NR 2 ENGINE COWLING AMar 30, 1999 · N813AT · Doug DC932 · Power LeverSDR AT9900275Jamb · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT ENTRANCE LOWER DOOR JAMB LEFT CORNER CORRODED. DISASSEMBLE AFT ENTRANCE THRESHOLD AREA, REMOVED CORRODED WEB ON LEFT AND RIGHT SIDES. FORMED NEW WEBS, DRILLED, TRIMMED, DEBURRED, ALODINED, PRIMED, AND INSTAMar 25, 1999 · N813AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900257Skin · dentedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE RIGHT HAND FUSELAGE EXTERIOR SKIN WITH NUMEROUS DENTS AND REPAIRS FROM BS 229-598 L-18-26R. REMOVED AND REPLACED SKIN FROM BS 229 TO 598 IAW DC9 SRM 51-30-2, 51-30-5, 51-10-2, 51-10-3, 51-10-4, AND RES NR 9941Mar 24, 1999 · N813AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900256Skin · dentedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT VENTRAL STAIRS FUSELAGE SKIN AT YSD 27-98 WITH NUMEROUS DENT WITH CREASES. REMOVED STEPS TO GAIN ACCESS. REMOVED SKIN, LOCATED AND DRILLED NEW SKIN, AND INSTALLED SKIN AND REINSTALLED STEP IAW DC9 SRM 51-Mar 20, 1999 · N813AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900231Skin · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND LIGHT SURFACE CORROSION ON BARE METAL 22 INCHES BELOW CUSP WEB AT BS 1142 ON THE LEFT SIDE. FOUND CORROSION ON SKIN SPLICE DOUBLER OUT OF LIMITS, FORMED SKIN SPLICE DOUBLER, ORDER NEW SKIN, LOCATED, DRILLED SKIN AMar 19, 1999 · N813AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900233Fitting · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT VENTRAL STAIRS LOWER LEFT HAND SIDE CORNER FITTING CORRODED THROUGH OUT. REMOVED AND REPLACED CORRODED AND CRACKED VENTRAL STAIRS LEFT HAND SIDE CORNER FITTING IAW DC9 SRM 51-10-4, 51-10-3, 51-10-5 AND 51-Mar 18, 1999 · N813AT · Doug DC932 · Entrance StairsSDR AT9900273Skin · dentedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE RIGHT SIDE NR 1 SLAT LOWER EXTERNAL SURFACE DENTED JUST INBOARD OF ANTI-ICE DUCT. CUT INNER SKIN FOR ACCESS, FABRICATED DOUBLER AND SKIN SPLICE DOUBLER, DRILLED, COUNTERSUNK, TREAT, PRIMED, AND INSTALLED IAW DMar 15, 1999 · N813AT · Doug DC932 · Leading Edge DevicesSDR AT9900232Skin · dentedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND A GOUGE IN DENT AT BS 235 L-18L OUT OF LIMITS. FABRICATED EXTERNAL AND INTERNAL FINGER DOUBLER AND DOUBLER, DRILLED AND TRIMMED DOUBLERS, ALODINED, PRIMED AND INSTALLED DOUBLERS WITH WET SEALANT IAW DC9 SRM 51-10-Mar 15, 1999 · N813AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900284Floorbeam · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD PIT BOTTOM OF FLOORBEAM WITH PREVIOUS REPAIR GOUGED, DENTED AND APPEARS TO HAVE A CRACK RUNNING TOWARDS CENTER OF BEAM AT BS 389. CUT OUT DAMAGE AREA, HFEC VERIFIED NO FURTHER CRACKS IN THE AREA. FABRICMar 13, 1999 · N813AT · Doug DC932 · Fuselage Main, Floor BeamSDR AT9900278Structure · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT ENTRY DOORWAY THRESHOLD WEB, JAMB SUPPORT AND SPLICE AND LOWER CHANNEL FRAME CORRODED. REMOVED CORROSION, FABRICATED DOOR SILL, FITTING, ANGLE, SPLICE PLATE AND CHANNEL. DRILLED, COUNTERSUNK, DEBURRED, PRIMMar 13, 1999 · N813AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900211Web · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE CABIN INTERIOR RIGHT AFT LAVATORY FRAME TO FLOOR BEAM ATTACHMENT EXFOLIATED AT BS 996. FABRICATED WEB AND DOUBLER REPAIRS, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 53-05 FIG 108, 51-10-4, 51-10-3, 51-30-2, 51Mar 13, 1999 · N813AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900197Skin · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE NR 1 PYLON TRAILING EDGE PANEL LOWER SIDE SKIN REPAIR DISBONDED AND CORNERS CRACKED OFF AT BS 1030 TO 1076. REMOVED SKIN, FABRICATED NEW SKIN, DRILLED, DEBURRED, COUNTERSUNK, TREATED, PRIMED, AND INSTALLED IAWMar 13, 1999 · N813AT · Doug DC932 · Nacelle/Pylon, Plate/SkinSDR AT9900258Doubler · out of positionSCHEDULED INSPECTION AT AERO CORP, FL. FOUND AN EXTERNAL DOUBLER THAT INTERFERES WITH WINDOW BELT DOUBLER AT BS 464 L-14 ON THE RIGHT SIDE. REMOVED EXISTING DOUBLER, FORMED NEW DOUBLER, DRILLED, COUNTERSUNK, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-4,Mar 9, 1999 · N813AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900210Angle · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND CORROSION AROUND FASTENER HEADS ON ATTACH ANGLE AND WEB (TOP SIDE) AT BS 130 LBL 54 ON THE E/E BAY CEILING. REMOVED CORROSION AROUND FASTENER HEADS, FABRICATED REPAIR DOUBLER, LOCATED AND DRILLED, TREATED, PRIMED, Mar 8, 1999 · N813AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900194Spar · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT HAND REAR SPAR LOWER CHORD AFT TANG HAS A CRACK INDICATION AT INBOARD BUTE DOOR THIRD HOLE FROM OUTBOARD END. STEPPED UP HOLE TO .437, FABRICATED AND INSTALLED BUSHING IAW DC9 SRM 51-10-3 AND SB 57-150 RZMar 7, 1999 · N813AT · Doug DC932 · Wing SparSDR AT9900282Cargo Track · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD PIT TRACK CORRODED ON THE BOTTOM SIDE. FABRICATED, LOCATED, DRILLED, DEBURRED, COUNTERSUNK, PRIMED, TREATED, AND INSTALLED IAW DC9 SRM 53-05 FIG 4C, 51-10-3 AND 51-10-4.Mar 3, 1999 · N813AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR AT9900277Track · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT PIT RIGHT SIDE FLOOR TRACK CORRODED ON BOTTOM FULL LENGTH. FABRICATED, DRILLED, DEBURRED, PRIMED, AND TREATED IAW DC9 SRM 53-05 FIG 4C, 51-10-4, AND 51-10-3.Mar 3, 1999 · N813AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR AT9900276Track · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD PIT RIGHT HAND TRACK BOTTOM SIDE CORRODED THROUGHOUT. REMOVED CORROSION, LOCATED NEW TRACK, DRILLED, COUNTERSUNK, DEBURRED, TREATED, AND PRIMED IAW DC9 SRM 53-05 FIG 4C, 51-10-4, AND 51-10-3.Mar 2, 1999 · N813AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR AT9900209Floorbeam · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FLOORBEAM UPPER CAP CORRODED AROUND FASTENER HOLES AT BS 980 RBL 38 TO 42. REMOVED, FIT, TRIMMED, DRILLED, AND INSTALLED UPPER CAP REPAIR ANGLE IAW DC9 SRM 51-10-3, 53-01 FIG 1, 53-05 FIG 20A, 51-10-4, 51-30-2,Mar 1, 1999 · N813AT · Doug DC932 · Fuselage Main, Floor BeamSDR AT9900280Floor · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD PIT CENTER FLOOR PANEL CORRODED ALONG THE EDGES AND ELONGATED HOLES WITH NO EDGE DISTANCE. FABRICATED REPAIR FLOOR PANEL, LOCATED, DRILLED, DEBURRED, TREATED AND PRIMED IAW DC9 SRM 51-10-3, 53-01 FIG 1, Feb 27, 1999 · N813AT · Doug DC932 · Fuselage Floor PanelSDR AT9900292Support · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CABIN FLOOR SUPPORT CORRODED ON THE UPPER SURFACE AND ON BOTTOM OF UPPER FLANGE AROUND CLIP NUTS AT BS 157 TO 218. REMOVED CORROSION, FABRICATED REPAIR ANGLE, DRILLED, DEBURRED, TREATED, PRIMED AND INSTAFeb 26, 1999 · N813AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900281Seat Track · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CABIN SEAT TRACK AT BS 200 TO 279 RBL 22 CORRODED. REMOVED FLOOR PANELS, FABRICATED NEW SEAT TRACK AND SPLICE, LOCATED, DRILLED, ALODINED, PRIMED AND INSTALLED IAW DC9 SRM 53-05 FIG 4, 51-10-3, 51-30-1, Feb 26, 1999 · N813AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR AT9900208Support · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CABIN FLOOR SUPPORT CORRODED AND PART OF UPPER FLANGE HAS BEEN PREVIOUSLY REMOVED AT BS 210 TO 237 LBL 16. REMOVED FLOOR SUPPORT, FABRICATED NEW SUPPORT, ALODINED, PRIMED, AND INSTALLED IAW DC9 SRM 53-1Feb 26, 1999 · N813AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900286Bulkhead Angle · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT HAND AFT PIT BULKHEAD LINER SUPPORT ANGLE CORRODED AND GILLINER PANEL MISSING. FORMED SUPPORT ANGLE, CUT, DRILLED, TRIMMED ANGLE AND GILLINER PANEL, TREATED, PRIMED AND INSTALLED ANGLE TO GILLINER PANEL IAWFeb 25, 1999 · N813AT · Doug DC932 · Fuselage Main, BulkheadSDR AT9900279Web · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT CUSP WEB AT BS 229 L-18 CORRODED. REMOVED CORRODED PORTION OF WEB, REMOVED SUPPORT FITTING FOR ACCESS AND FLOOR SUPPORT SECTION. FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED NEW SECTION AND REFeb 24, 1999 · N813AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900283Channel · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT COMPARTMENT LEFT HAND HAT CHANNEL ADJACENT TO THE LOWER BULKHEAD PRESSURE CAP CORRODED AT BS 996 ON THE LOWER END. REMOVED CORROSION, REMOVED AND REPLACED HAT CHANNEL, LOCATED, DRILLED AND INSTALLED IAW DC9 Feb 21, 1999 · N813AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900294Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT FORWARD LOWER FLOOR PANEL BRACKET CORRODED AT BS 218 LBL 42. REMOVED BRACKET, CUT, DRILLED, TRIM, ALODINED, PRIMED, INSTALLED NUT PLATE ON BRACKET AND INSTALLED IAW DC9 SRM 51-30-2, 53-21-0 FIG 2D, 51-10-3 Feb 20, 1999 · N813AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900290Bracket · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE GILLINER ATTACH ANGLE CRACKED AT BS 237 L-24. PERFORMED HFEC TO VERIFIED CRACK. REMOVED CRACKED ATTACH ANGLE, WELDED REPAIR CRACK ON ANGLE IAW EA 12-5321-29-C1362 USING AMS 4951 FILLER WIRE AND INSTALLED ANGLE Feb 20, 1999 · N813AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900288Floorbeam · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND UPPER CAP CRACKED AND CORRODED ON FLOORBEAM WEB AT BS 996 RBL 54. REMOVED PULLEY TOWERS, REMOVED FLOOR UPPER BEAM CAP. LOCATED AND DRILLED NEW FLOORBEAM CAP, ALODINED, PRIMED, AND INSTALLED FLOORBEAM AND REINSTALLEFeb 20, 1999 · N813AT · Doug DC932 · Fuselage Main, Floor BeamSDR AT9900287Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT CARGO COMPARTMENT FUEL SHUT OFF BRACKET AT BS 935 CORRODED. RELIEVED CABLE TENSION, REMOVED AND REPLACED BRACKET ASSEMBLY, RIGGED SYSTEM AND ALL OPS CHECKS GOOD IAW DC9 MM 20-18-0, 76-12-0 PG 206, 20-16-0, AFeb 20, 1999 · N813AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900293Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE SIDE ROLLER BEARING FITTING CORRODED ON THE INBOARD LEFT SIDE OF THE HORIZONTAL STABILIZER. REMOVED AND REPLACED LEFT HAND INBOARD BRACKET ON THE HORIZONTAL STABILIZER IAW DC9 MM 55-10-0.Feb 19, 1999 · N813AT · Doug DC932 · Horizontal Stabilizer StructureSDR AT9900285Floor · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE G-4 FLOOR PAN SKIN CORRODED. REMOVED FLOOR PAN HAT SECTION, FABRICATED NEW SKIN, TREATED, PRIMED, INSTALLED SKIN AND REINSTALLED HAT SECTION IAW DC9 SRM 51-30-2, 51-10-3 AND 51-10-2.Feb 19, 1999 · N813AT · Doug DC932 · Fuselage Floor PanelSDR AT9900295Skin · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND LIGHTNING STRIKES ON THE LEFT SIDE NOSE AT Y-69.550 AND RIGHT SIDE NOSE AT Y-69.550 AND Y-76.550. REMOVED E/E ACCESSORY DOOR, BULKHEAD VENT AND LIGHT BRACKET. CUT OUT LIGHTNING STRIKE AND FOUR FASTENER CRACKS. FOFeb 18, 1999 · N813AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900221Skin · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FUSELAGE SKIN BULGE AT BS 275 L-18L. STRIPPED AREA, REMOVED FASTENERS, FOUND CORROSION. REMOVED SECTION OF SKIN ABOVE AND BELOW LONGERON 18. FABRICATED FINGER DOUBLER, FILLERS, AND EXTERNAL DOUBLERS, ALODINEFeb 17, 1999 · N813AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900005Air Dist · odorDURING FLIGHT, THE AFT LAVATORY SMOKE DETECTOR SOUNDED FLIGHT ATTENDANT REPORTED NO SMOKE, BUT VERIFIED SMOKE ALARMS DID SOUND. AIR CONDITIONING SMOKE PROCEDURES FOLLOWED O2 MASK DON BY CREW, PILOT'S UNABLE TO DETERMINE WHICH PACK WAS CAUSING SOME SLIGHT SMELJan 6, 1999 · N813AT · Doug DC932 · Air Distribution System
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