N834AT, cancelled Aug 12, 2005

Service difficulty reports · 19

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 = 'N834AT' AND deregistration_id = 'N834AT-2005-08-12'
  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 AT0200082Contactor · looseDURING SERVICE CHECK FOUND LAST ROW EMERGENCY LIGHTS INOPERATIVE. TIGHTENED CONTACTS TO BATTERY FOR LAST ROW EMERGENCY LIGHTS, OPS CHECK GOOD IAW DC-9 MM 33-00.Oct 3, 2002 · N834AT · Doug DC932 · Emergency LightingSDR AT0200057Skin · crackedLT ELEVATOR UPPER SKIN IS CRACKED AT I/B END. STOP DRILLED ENDS OF CRACK, LT ELEVATOR UPPER SKIN AT I/B END AS PER DC9 SRM 55-03. ACCOMPLISHED HFEC ON CRACK PER NDT SPM 06-00-07; CRACK CONTAINED. INSTALLED REPAIR DOUBLER AS PER DC9 SRM 55-03, FIGURE 15.Apr 5, 2002 · N834AT · Doug DC932 · Elevator, Plate/SkinSDR AT0200059Skin · corrodedEXTERIOR FUSELAGE SKIN IS BULGED JUST FORWARD OF STA 996 AT STR 25L AND 23L. REMOVED FASTENERS AND TIE FITTING 25L AT STA 996. REMOVED CORROSION, OUT OF LIMITS. REMOVED TIE FITTING 25L. REMOVED CORROSION. REMOVED SHIM BELOW FITTING 25L. SHIM CORRODED OUTApr 4, 2002 · N834AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0200056Bulkhead · corrodedAFT CARGO COMPARTMENT, AFT PRESSURE BULKHEAD LOWER T-CHORD CORROSION BETWEEN STR 29 LEFT TO STR 29 RIGHT BS 996. REMOVED STIFFENER AT LONG 28 RIGHT AND LEFT FOR ACCESS AND REMOVED LEFT ANGLE BS 996 LONG 29R TO 29L. CUT OUT VERTICAL WEB STA 996 (INTERIOR) FORApr 4, 2002 · N834AT · Doug DC932 · Fuselage Main, BulkheadSDR AT0200058Door Frame · crackedFORWARD CARGO DOOR CUTOUT BETWEEN LOWER DOOR STOP FITTINGS HAS CRACKS ON FLANGE OF VERTICAL FRAME AND HAS BULGING (EVIDENCE OF CORROSION). REMOVED FASTENERS AND CORROSION, MATERIAL LOSS BEYOND LIMITS. REMOVED LOWER PAN AT FORWARD CARGO DOOR. REMOVED LOWER DApr 3, 2002 · N834AT · Doug DC932 · Fuselage Main, StructureSDR AT0000437Battery · dischargedBATTERIES IN B5-27 WERE WEAK DUE TO INSUFFICENT CHARGING VOLTAGE. REMOVED AND REPLACED BATTERIES IN B5-27 AND CORRECTED INPUT VOLTAGE PROBLEM TO BATTERY PACK IAW DC9 MM 33-50.Oct 1, 2000 · N834AT · Doug DC932 · Emergency LightingSDR AT0000403Light · inoperativeFOUND EMERGENCY PATH LIGHTING AT SEAT 18D WILL NOT ILLUMINATE. REPAIRED BROKEN WIRE AT SEAT 18D, EMERGENCY PATH LIGHTING IAW DC9 MM 33-00.Sep 15, 2000 · N834AT · Doug DC932 · Emergency LightingSDR AT9900918Rib · crackedFOUND LEFT WING OUTBOARD TRAILING EDGE INSIDE RIB NR 2 TOP AND BOTTOM CRACKED. INSTALLED DOUBLERS ON TOP AND BOTTOM OF NR 2 RIB.Dec 23, 1999 · N834AT · Doug DC932 · Wing, Rib/BulkheadSDR AT9900922Longeron · crackedDURING A ROUTINE INSPECTION AT AVBORNE IN MIAMI FL, FOUND DENT TO HAVE A CRACK AT LEFT FUSELAGE BS 79 LONGERON 20 LEFT. INSTALLED DOUBLER IAW DC9 SRM 53-04 FIG 38.Dec 12, 1999 · N834AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT9900921Intercostal · corrodedFOUND AFT CARGO COMPARTMENT LOWER CUT-OUT INTERCOSTAL CORRODED AT BS 917. FABRICATED AND INSTALLED NEW INTERCOSTAL.Dec 12, 1999 · N834AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900920Frame · crackedDURING A ROUTINE INSPECTION AT AVBORNE IN MIAMI FL, FOUND CRACK IN RIGHT FUSELAGE FRAME AT BS 1038. INSTALLED REPAIR AT BS 1038 IAW DC9 SRM 53-04.Dec 12, 1999 · N834AT · Doug DC932 · Fuselage Main, FrameSDR AT9900919Frame · crackedDURING A ROUTINE INSPECTION AT AVBORNE IN MIAMI FL, FOUND 2 CRACKS IN FORWARD AND 2 CRACKS IN AFT SIDE OF LEFT FUSELAGE FRAME AT BS 1038. INSTALLED REPAIR AT BS 1038 IAW DC9 SRM 51-30-02 AND 53-03.Dec 12, 1999 · N834AT · Doug DC932 · Fuselage Main, FrameSDR AT9900917Rib · crackedRIGHT ENGINE PYLON LEADING EDGE HAS CRACKED RIB ANGLE. STOP DRILLED CRACK IAW DC9 SRM 57-01.Dec 12, 1999 · N834AT · Doug DC932 · Nacelle/Pylon, Frame/Spar/RibSDR AT9900916Bracket · crackedFOUND CRACKED SUPPORT BRACKET ON RIGHT WING LEADING EDGE. FABRICATED AND REPLACED CRACKED BRACKET.Dec 12, 1999 · N834AT · Doug DC932 · Leading Edge DevicesSDR AT9900915Skin · crackedFOUND RIGHT WING, OUTBOARD SECTION OF TRAILING EDGE, TOP AND BOTTOM SKIN TO HAVE CORROSION AND FOUND RIB CRACKED ON RIGHT WING. REMOVED CORROSION AND INSTALLED DOUBLER ON RIB.Dec 8, 1999 · N834AT · Doug DC932 · Wing, Plate/SkinSDR AT0000010Intercoastal · corrodedDURING A ROUTINE INSPECTION AT AVBORNE IN MIAMI FL, FOUND INTERCOASTAL CORRODED AT BS 917 RIGHT FUSELAGE FRAME. FABRICATED AND INSTALLED NEW INTERCOASTAL AT BS 917 RIGHT FUSELAGE FRAME IAW DC9 SRM 51-00.Nov 26, 1999 · N834AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900568Duct · leakingTAIL COMPARTMENT HI LIGHT CAME ON AT 140 KNOTS ON TAKEOFF ROLL. LIGHT WENT OFF AFTER QRH PROCEDURE AND 30 SECONDS THEN ON AND OFF FOUR TIMES PRIOR TO LANDING. RESECURED SEALS ON RIGHT HEAT EXCHANGER, SECURED AUGMENTOR VALVE CLAMP. REPLACED APU EXHAUST DUCT,Aug 11, 1999 · N834AT · Doug DC932 · APU Exhaust SystemSDR AT9900484Regulator · defectiveTAIL COMPARMENT TEMPERATURE HIGH LIGHT CAME ON. REMOVED AND REPLACED TAIL COMPARTMENT TEMPERATURE HIGH SENSORS AND PNEUMATIC PILOT PRESSURE REGULATOR IAW MM 36-20-2 AND 36-10-2.Jul 5, 1999 · N834AT · Doug DC932 · Pneumatic Distribution SystemSDR AT9900432Duct · looseTAIL COMPARTMENT TEMPERATURE CAME ON IN FLIGHT FOR A FEW SECONDS ON CLIMBOUT, PERFORMED STEP IN ORH AND RETURNED TO HOUSTON. GROUND START OPS CHECKED FOR LEAKS IN AFT COMPARTMENT, DISCONNECTED LEFT PACK PER DDP. RECONNECTED LEFT PACK FOR TROUBLESHOOTING, NO Jun 3, 1999 · N834AT · Doug DC932 · Pneumatic Distribution System
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