# Service difficulty reports: N849AT, cancelled Jun 25, 2004 A list on [N849AT, cancelled Jun 25, 2004](https://openairdocs.org/deregistered/N849AT-2004-06-25.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR AT0300002](https://openairdocs.org/sdr/AT0300002.md): Ground Wire · damaged · Jan 2, 2003 · N849AT · Doug DC932 · Light System Wiring > DURING B-CHECK FOUND AFT EMERGENCY EXIT (OVERWING) IDENTIFIERS DID NOT WORK. FOUND 3 AO RIVNUT GROUND UNDER LEFT AFT OVERWING EXIT, REPAIRED OPS CHECK GOOD. - [SDR AT0200071](https://openairdocs.org/sdr/AT0200071.md): Pump · failed · Aug 23, 2002 · N849AT · Doug DC932 · Hydraulic Pump, Auxiliary > ON ROTATION NOSE WHEEL OFF GROUND AND POSITIVE RATE, THE CALLOUT FOR GEAR WAS INITIATED AND WHEN THE GEAR WAS SELECTED UP, THERE WERE CIRCUIT BREAKER'S POPPING ON AFT CIRCUIT BREAKER PANEL, RADIO FAN OFF LIGHT ILLUMINATED, CREW SMELLED SMOKE BUT THERE WAS NO V - [SDR AT0200005](https://openairdocs.org/sdr/AT0200005.md): Nut · backed out · Feb 4, 2002 · N849AT · Doug DC932 · Elevator Control System > AIRCRAFT ROTATED WITHOUT MUCH ELEVATOR INPUT. ON CLIMBOUT CREW FELT VIBRATION IN YOKE. AILERON TRIM OF 2.5 DEGREES LEFT AND 1 DEGREE LEFT, RUDDER WAS IMPUTED THROUGH LANDING. LANDING STABILIZATION TRIM WAS 2 DEGREES NOSE UP. FOUND RIGHT HAND ELEVATOR JAMME - [SDR AT0000424](https://openairdocs.org/sdr/AT0000424.md): Battery · inoperative · Sep 30, 2000 · N849AT · Doug DC932 · Emergency Lighting > AFT CEILING EMERGENCY LIGHTS DO NOT WORK. REMOVED AND REPLACED NICAD BATTERY IAW DC9 MM 33-53. - [SDR AT0000491](https://openairdocs.org/sdr/AT0000491.md): Skin · damaged · Apr 13, 2000 · N849AT · Doug DC932 · Fuselage Main, Plate/Skin > FOUND PER ENGINEERING: INSEPCT SKIN REPAIR AT BS 425-495 AND L23R- L30R, INTERNAL DOUBLERS AT STATIC PORT AND CARGO DOOR TO INSURE COMFORMANCE WITH SRM 53-04 FIGURE 30 PER WO58958. CORRECTIVE ACTION: SKIN CUT AT LOWER EDGE OF CARGO DOOR IS AT - [SDR AT9900638](https://openairdocs.org/sdr/AT9900638.md): Altimeter · defective · Aug 27, 1999 · N849AT · Doug DC932 · Altimeter, Barometric/Encoder > ON DESCENT INTO BOSTON, BOTH ALTIMETERS APPEARED TO BE INOPERATIVE. WHILE DESCENDING TO FL 240, TRIED TO LEVEL AT 240 AND CAPTAIN ALTIMETER CONTINUED TO FL 215 WHILE FIRST OFFICER CLIMBED TO FL 255 WITH BOTH VSI'S SHOWING LEVEL FLIGHT. REMOVED AND REPLACED AI - [SDR AT9900316](https://openairdocs.org/sdr/AT9900316.md): Wire · broken · Apr 9, 1999 · N849AT · Doug DC932 · Landing Gear System Wiring > WHEN LANDING GEAR WAS EXTENDED DURING APPROACH, THE NOSE GEAR UNSAFE (RED) LIGHT STAYED ON, GREEN LIGHT WAS OUT. RECYCLED GEAR, NO HELP. FOUND BROKEN WIRES TO NOSE GEAR GROUND PROXIMITY SWITCH. REPAIRED WIRES AND CYCLED NOSE GEAR FIVE TIMES, ALL OPERATIONAL - [SDR AT9900297](https://openairdocs.org/sdr/AT9900297.md): Mask · damaged · Apr 2, 1999 · N849AT · Doug DC932 · Crew Oxygen System > CAPTAIN'S PORTABLE OXYGEN FULL FACE MASK LENS SEPARATED FROM RUBBER. REMOVED AND REPLACED MASK IAW MM 25-00. - [SDR AT9900078](https://openairdocs.org/sdr/AT9900078.md): Wire · shorted · Feb 4, 1999 · N849AT · Doug DC932 · Light System Wiring > EMERGENCY PATH LIGHTING NOT WORKING FROM BUSINESS CLASS FORWARD TO AND INCLUDING THE L-1 DOOR. REPAIRED SHORTED WIRE ON FORWARD SIDE OF FLOOR TRACK LIGHTING, OPS CHECKED GOOD IAW MM 33-53. - [SDR AT9900071](https://openairdocs.org/sdr/AT9900071.md): Skin · corroded · Jan 26, 1999 · N849AT · Doug DC932 · Wing, Plate/Skin > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND ALL DOUBLERS DISBONDED AND CORROSION IN BETWEEN SKIN ON TOP OF LEFT WING TRAILING EDGE FLAP SKIN AT STA 214. REMOVED AND FABRICATED NEW SKIN AND 'T' CAP AND REINSTALLED IAW DC9 SRM 51-30-2, 51-10-4, 51-10-2, 51-10 - [SDR AT9900091](https://openairdocs.org/sdr/AT9900091.md): Skin · dented · Jan 7, 1999 · N849AT · Doug DC932 · Fuselage Main, Plate/Skin > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND DENTED AREA AT STA 968 L-26R CREASED AND OUT OF LIMITS. CUT OUT DENTED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLER, SKIN SPLICES, STRINGER SPLICES, SHEAR TIES IAW DC9 SRM 53-04 FIG 16 AND RES NR - [SDR AT9900092](https://openairdocs.org/sdr/AT9900092.md): Skin · corroded · Jan 6, 1999 · N849AT · Doug DC932 · Fuselage Main, Plate/Skin > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND PREVIOUSLY EXISTING REPAIR DOUBLER AT STA 360 BETWEEN L-24 - 26R BULGING OUT OF LIMITS. CUT OUT DAMAGE SKIN, FABRICATED NEW SKIN, SHEAR TIE, LONGERON FINGER DOUBLER, SPLICE DOUBLERS, DRILLED, DEBURRED, PRIMED AND - [SDR AT9900088](https://openairdocs.org/sdr/AT9900088.md): Angle · corroded · Jan 6, 1999 · N849AT · Doug DC932 · Wing Miscellaneous Structure > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND LEFT WING INBOARD FLAP ATTACHED ANGLE AND SPAR CAP AT STA 137.50 AND REAR SPAR ATTACHED ANGLE AT STA 149 CORRODED. REMOVED NECESSARY FASTENERS IN ORDER TO GAIN ACCESS, CLEANED CORROSION, FABRICATED RIB, DOUBLER, A - [SDR AT9900089](https://openairdocs.org/sdr/AT9900089.md): Hinge · corroded · Jan 5, 1999 · N849AT · Doug DC932 · Cargo/Baggage Doors > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CARGO DOOR FORWARD AND AFT HINGE ASSEMBLY ATTACH BOLT HOLES WITH CORROSION AND ELONGATED HOLES. REAMED ELONGATED HOLES AND CLEANED CORROSION, FABRICATED AND INSTALLED FREEZE PLUGS. REINSTALLED HINGE B - [SDR AT9900086](https://openairdocs.org/sdr/AT9900086.md): Floor · corroded · Jan 5, 1999 · N849AT · Doug DC932 · Fuselage Floor Panel > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND FORWARD CARGO CENTER FLOOR BOARD AT STA 218 THRU 446 CORRODED AROUND EDGES, TOP SIDE AND BETWEEN LAYERS. REMOVED AND REPLACED CORRODED FLOOR PANEL, FABRICATED NEW FLOOR PANELS, TREATED, PRIMED, DEBURRED AND INSTAL - [SDR AT9900085](https://openairdocs.org/sdr/AT9900085.md): Torsion Bar · corroded · Jan 5, 1999 · N849AT · Doug DC932 · Drag Control System > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE SPOILER SUPPORT ROD END AND TORSION BAR LEVER CORRODED AT STA 50 AND STA 68. REMOVED AND REPLACED THE END SUPPORT ROD END AND TORSION BAR AND OPERATIONAL ADJUSTMENT TEST ACCOMPLISHED IAW DC9 MM 27-61-2, 20-10- - [SDR AT9900084](https://openairdocs.org/sdr/AT9900084.md): Skin · corroded · Jan 5, 1999 · N849AT · Doug DC932 · Vertical Stabilizer, Plate/Skin > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT VERTICAL STABILIZER LOWER AND UPPER SKIN CHAFED, CORRODED AND HOLES MISDRILLED IN PREVIOUS REPAIRED. MECHANICALLY REMOVED CORROSION, FABRICATED DOUBLERS, HEAT TREATED PARTS AND INSTALLED ALL PARTS IAW DC9 - [SDR AT9900087](https://openairdocs.org/sdr/AT9900087.md): Frame · corroded · Jan 4, 1999 · N849AT · Doug DC932 · Fuselage Main, Frame > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND FORWARD CARGO COMPARTMENT FRAME CORRODED AT STA 180 L-29L TO L-29R AND STA 275 L29-L TO L-29R. MECHANICALLY REMOVED CORROSION, FABRICATED AND INSTALLED NEW REPAIR IAW DC9 SRM 51-10-3, 53-01 FIG 1 AND 53-04 FIG 2A - [SDR AT9900090](https://openairdocs.org/sdr/AT9900090.md): Skin · dented · Jan 3, 1999 · N849AT · Doug DC932 · Fuselage Main, Plate/Skin > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND DENTED FUSELAGE SKIN AT STA 437, 2 BELOW L-24R. CUT OUT DENTED SECTIONS, FABRICATED NEW SKIN SECTION AND REPAIR SPLICES IAW DC9 SRM 53-04 FIG 30, 51-10-2, 51-10-3, 51-10-4 AND RES NR 9920. (P/N 105846-1) ON, (P/N ## 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 = 'N849AT' AND deregistration_id = 'N849AT-2004-06-25' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N849AT-2004-06-25/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.