# Service difficulty reports: N801AT, cancelled Mar 8, 2002 A list on [N801AT, cancelled Mar 8, 2002](https://openairdocs.org/deregistered/N801AT-2002-03-08.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR AT0100228](https://openairdocs.org/sdr/AT0100228.md): Battery Pack · discharged · Sep 14, 2001 · N801AT · Doug DC932 · Emergency Lighting > FOUND STARBOARD NACELLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE STARBOARD NACELLE EMERGENCY LIGHT BATTERY PACK IAW DC9 MM 33-50. - [SDR AT0100227](https://openairdocs.org/sdr/AT0100227.md): Power Supply · discharged · Sep 13, 2001 · N801AT · Doug DC932 · Emergency Lighting > FOUND EMERGENCY LIGHTS AT FORWARD GALLEY AND FORWARD ENTRY INOPERATIVE. REMOVED AND REPLACED B5-23 EMERGENCY LIGHT POWER SUPPLY IAW DC9 MM 33-53-0. - [SDR AT0100215](https://openairdocs.org/sdr/AT0100215.md): Battery Pack · inoperative · Jul 19, 2001 · N801AT · Doug DC932 · Emergency Lighting > FOUND B5-28 FAILED TO OPERATE AFT ACCESSERY EMERGENCY LIGHTS. CORRECTIVE ACTION: REPLACED B5-28. IAW DC9 MM 33-50 - [SDR AT0100040](https://openairdocs.org/sdr/AT0100040.md): Coffeemaker · odor · Jan 29, 2001 · N801AT · Doug DC932 · Buffet/Galleys > FOUND ACRID BURNING SMELL IN COCKPIT AND FORWARD FLIGHT ATTENDANT STATION. FOUND BURNT COFFEE GROUNDS ON FORWARD COFFEE MAKER. CLEANED BURNT GROUNDS, NO SMELL NOTED. ALSO CHECKED E&E COMPARTMENT, FORWARD CARGO COMPARTMENT AND FORWARD FLIGHT ATTENDANT STATIO - [SDR AT0100006](https://openairdocs.org/sdr/AT0100006.md): Power Supply · inoperative · Jan 19, 2001 · N801AT · Doug DC932 · Emergency Lighting > FOUND OVERWING EMERGENCY EXIT LIGHTS WILL NOT EXTINGUISH. REPLACED BATTERY PACK IAW DC9 MM 33-50. - [SDR AT0000484](https://openairdocs.org/sdr/AT0000484.md): Door · disengaged · Dec 6, 2000 · N801AT · Doug DC932 · Landing Gear Doors > NOSE GEAR DOOR NOT CLOSED, DID NOT CLOSE AT GEAR RETRACTION. RESECURED DOOR ON NOSE GEAR. IAW DC9 MM32-20 - [SDR AT0000473](https://openairdocs.org/sdr/AT0000473.md): Frame · cracked · Nov 1, 2000 · N801AT · Doug DC932 · Fuselage Main, Frame > FOUND BS 110 LEFT FUSELAGE FRAME CRACKED AT 2 INCHES ABOVE CUPS, LONGERON 18. REMOVED CRACKED SECTION OF FRAME, FORMED, HEAT TREATED, SPLICED AND INSTALLED FRAME IAW REO L00305. - [SDR AT0000402](https://openairdocs.org/sdr/AT0000402.md): Battery Pack · discharged · Sep 15, 2000 · N801AT · Doug DC932 · Emergency Lighting > FOUND NR 1 ENGINE NACELLE EMERGENCY LIGHT NOT ILLUMINATED. REMOVED AND REPLACED ENGINE NACELLE LIGHT BATTERY PACK IAW DC9 MM 33-53. - [SDR AT0000370](https://openairdocs.org/sdr/AT0000370.md): Door Frame · corroded · Jul 11, 2000 · N801AT · Doug DC932 · Fuselage Miscellaneous Structure > FOUND FORWARD AIRSTAIR DOOR LOWER JAMB HAS CORROSION AT HOLD OPEN LINK SUPPORT BRACKET ATTACH POINT. INSTALLED WEB REPAIR IAW DC9 SRM 53-01 FIGURE 2 SHEET 3 AND RES NR 00-0709. - [SDR AT0000371](https://openairdocs.org/sdr/AT0000371.md): Door Frame · cracked · Jul 10, 2000 · N801AT · Doug DC932 · Fuselage Miscellaneous Structure > FOUND PER EDDY CURRENT INSPECTION, CRACK INDICATION AT L-1 DOOR JAMB DOOR STOP HOLE AT D-12. INSTALLED PERMANENT REPAIR, DOUBLER AND TRIPLER IAW SR DWG SR09530252. - [SDR AT9900632](https://openairdocs.org/sdr/AT9900632.md): Computer · malfunctioned · Sep 3, 1999 · N801AT · Doug DC932 · Autopilot System > CREW REPORTED YAW OSCILLATIONS DURING CLIMB-OUT. UNSURE IF IT WAS A YAW DAMPER PROBLEM OR AND ENGINE MALFUNCTION. AFTER LANDING DETERMINED TO BE A YAW DAMPER PROBLEM. REMOVED AND REPLACED STAB AUGMENTATOR COMPUTER. OPS CHECKED GOOD. - [SDR AT9900700](https://openairdocs.org/sdr/AT9900700.md): Fitting · cracked · Jul 14, 1999 · N801AT · Doug DC932 · Fuselage Miscellaneous Structure > FOUND ATTACH FITTING CRACKED AT BS 154 TO STRINGER 11R. TRIMMED OUT CRACK IAW EO 99-1205. REPAIRED, FABRICATED AND INSTALLED GUSSET AND L-ANGLE STRAP IAW DC9 SRM 51-10-3, TIMCO EO 99-1205 REV IR DATED 08/04/99. - [SDR AT9900481](https://openairdocs.org/sdr/AT9900481.md): Socket · loose · Jun 30, 1999 · N801AT · Doug DC932 · Emergency Lighting > STANDBY LIGHTING IN CEILING AT BS 585 WORKING INTERMITTENT. TIGHTEN LIGHT SOCKET IN CEILING AT BS 585, OPS CHECK GOOD PER 33-52-0. - [SDR AT9900446](https://openairdocs.org/sdr/AT9900446.md): Slide · detached · Jun 13, 1999 · N801AT · Doug DC932 · Emergency Equipment > ESCAPE SLIDE CAME OFF THE MAIN CABIN L-1 DOOR HOLDER. RESECURED SLIDE PACK PER MM 25-00. - [SDR AT9900370](https://openairdocs.org/sdr/AT9900370.md): Skin · dented · Apr 22, 1999 · N801AT · Doug DC932 · Fuselage Main, Plate/Skin > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FUSELAGE SKIN AT BS 163 L-3L DENTED. REPAIRED THE DENTED FUSELAGE SKIN BY COLD WORKING DENT AND REMOVING EXISTING REPAIR DOUBLER AND ENLARGING REPAIR DOUBLER TO INCORPORATE DENTED AREA IAW DC9 SRM 53-04 FIG 38 - [SDR AT9900357](https://openairdocs.org/sdr/AT9900357.md): Skin · corroded · Apr 22, 1999 · N801AT · Doug DC932 · Fuselage Main, Plate/Skin > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND AN EXISTING SKIN REPAIR DOUBLER AT THE FORWARD CARGO DOOR THRESHOLD, FORWARD AND AFT CORNERS AT BS 389-427 CORRODED. FABRICATED AND INSTALLED REPAIR TRIPLERS AT FORWARD AND AFT CORNERS IAW DC9 SRM 53-05 FIG 105 ( - - [SDR AT9900334R1](https://openairdocs.org/sdr/AT9900334R1.md): Channel · cracked · Apr 22, 1999 · N801AT · Doug DC932 · Fuselage Miscellaneous Structure > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND AN EXISTING REPAIR DOUBLER CHAFED THRU AFT VENTRAL DOOR UPPER SECTION. REMOVED, ORDERED, LOCATED, DRILLED, AND INSTALLED UPPER CHANNEL AND Z ANGLE IAW DC9 SRM 51-10-4, 51-30-2, 51-30-4 AND DOUGLAS DRAWING NR 99155 - [SDR AT9900334](https://openairdocs.org/sdr/AT9900334.md): Doubler · cracked · Apr 22, 1999 · N801AT · Doug DC932 · Tail Cone Doors > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND AN EXISTING REPAIR DOUBLER CHAFED THRU AFT VENTRAL DOOR UPPER SECTION. REMOVED, ORDERED, LOCATED, DRILLED, AND INSTALLED UPPER CHANNEL AND Z ANGLE IAW DC9 SRM 51-10-4, 51-30-2, 51-30-4, AND BOEING DRAWING NR 99155 - [SDR AT9900322](https://openairdocs.org/sdr/AT9900322.md): Skin · corroded · Apr 22, 1999 · N801AT · Doug DC932 · Fuselage Main, Plate/Skin > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FUSELAGE SKIN BULGING AT BS 636 BETWEEN L-29-30L. ACCESSED AREA FOR REPAIR ON LEFT HAND CANTED AREA, FORMED INTERNAL DOUBLER, CUT, DRILLED, TRIMMED AND REINSTALLED ALL PARTS IAW DC9 53-01 FIG 1, AND MM 30-10-7. - [SDR AT9900321](https://openairdocs.org/sdr/AT9900321.md): Threshold · corroded · Apr 22, 1999 · N801AT · Doug DC932 · Fuselage Miscellaneous Structure > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CARGO COMPARTMENT THRESHOLD PAN AT BS 370-420 CORRODED ALONG ENTIRE LENGTH OF BOTTOM. REMOVE SLANT PANELS FORWARD AND AFT OF PIT DOOR, ALSO THE THRESHOLD PAN. TRIMMED NEW SPLICE DOUBLERS AND PAN SECTIO - [SDR AT9900335](https://openairdocs.org/sdr/AT9900335.md): Skin · dented · Apr 15, 1999 · N801AT · Doug DC932 · Fuselage Main, Plate/Skin > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FUSELAGE SKIN AT BS 229-399 L-18-26R DENTED AND CREASED. REMOVED AND REPLACED FUSELAGE SKIN IAW DC9 SRM 51-30-1, 51-10-2, 51-30-5, 51-20-0 AND RES NR 99749. SKIN (P/N 1A44467-1) OFF. - [SDR AT9900323](https://openairdocs.org/sdr/AT9900323.md): Tee · corroded · Apr 8, 1999 · N801AT · Doug DC932 · Leading Edge Devices > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND A TEE CORRODED ON LEFT HAND INBOARD FLAP TRAILING EDGE ASSEMBLY. REMOVED TEE, LOCATED, FIT, TRIMMED, DRILLED, AND INSTALLED IAW DC9 SRM 51-10-2, 57-50-3, 51-10-4, AND 51-10-2. - [SDR AT9900302](https://openairdocs.org/sdr/AT9900302.md): Longeron · corroded · Apr 6, 1999 · N801AT · Doug DC932 · Fuselage Main, Longeron/Stringer > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND LONGERON 19R AT BS 229-370 CORRODED. REMOVED CORRODED LONGERON, FABRICATED REPAIR, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 53-02 FIG. 18, 51-10-3, AND 51-30-5. - [SDR AT9900359](https://openairdocs.org/sdr/AT9900359.md): Angle · corroded · Mar 29, 1999 · N801AT · Doug DC932 · Fuselage Miscellaneous Structure > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND IN THE AFT GALLEY WORK AREA UNDER THE COFFEE AND SNACK DOOR AN ANGLE CORRODED. REMOVED ANGLES FOR ACCESS, FABRICATED NEW REPAIR U CHANNEL, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED TWO EACH ANGLES AND U CHAN ## 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 = 'N801AT' AND deregistration_id = 'N801AT-2002-03-08' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N801AT-2002-03-08/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.