N812AT

Service difficulty reports not matched to an aircraft · 41

They name N812AT, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N812AT' AND registry_match IS NULL
  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 AT9900757Jamb · crackedFOUND SERVICE DOOR JAMB, LOWER AFT CORNER CRACKED .700 ALONG OUTER SKIN. FABRICATED AND INSTALLED 2 DOUBLER AND FILLERS IAW EO 09-5310-29-E1472.Oct 19, 1999 · N812AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900754Floorbeam · corrodedFOUND FLOORBEAM AT BS 996 RBL 35-RBL49 WAS CORRODED. FABRICATED FLOORBEAM AND INSTALLED IAW DC9 SRM 53-05 FIGURE 108, MM 27-20-0, 20-17-0.Oct 18, 1999 · N812AT · Doug DC932 · Fuselage Main, Floor BeamSDR AT9900744Floorbeam · corrodedFOUND FLOORBEAM UPPER ATTACH ANGLE HAD EXFOLIATION CORROSION AT BS 980 RBL 35-RBL 49. CUT OUT CORROSION, FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 53-05 FIGURE 20A.Oct 15, 1999 · N812AT · Doug DC932 · Fuselage Main, Floor BeamSDR AT9900741Skin · crackedFOUND FORWARD SERVICE DOOR JAMB LOWER AFT CORNER OF SKIN CRACKED OUT OF LIMITS. FABRICATED 2 DOUBLERS, FILLERS, TRIMMED FILLER TO FIT, BACK DRILLED AND PRIMED REPAIR AND INSTALLED IAW DC9 SRM 51-10-3, 51-10-4, AND EO 09-5310-29-E1472.Oct 15, 1999 · N812AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900745Panel · gougedFOUND LEFT WING PANEL GOUGED BEYOND LIMITS. FABRICATED PANEL REPAIR IAW EO 99-1288.Oct 10, 1999 · N812AT · Doug DC932 · Wing, Plate/SkinSDR AT9900713Angle · crackedFOUND RIGHT PYLON WEB LOWER SUPORT ANGLE FOUND 3 CRACK, PYLON STATION 105 3 BELOW PYLON REFERANCE PLANE, 5 OUTBOARD FUSELAGE SKIN. REMOVED SUPPORT ANGLE, FABRICATED AND INSTALLED NEW SUPPORT ANGLE IAW DC9 SRM 51-10-2, 51-10-3, 51-30-2, 51-30-4.Oct 6, 1999 · N812AT · Doug DC932 · Nacelle/Pylon StructureSDR AT9900753Balance Wt · corrodedFOUND RIGHT ELEVATOR BALANCE WEIGHT WAS CORRODED. REMOVED AND REPLACED RIGHT ELEVATOR BALANCE WEIGHT IAW DC9 SRM 55-01 PG 3, 51-30-1.Oct 4, 1999 · N812AT · Doug DC932 · Elevator StructureSDR AT9900694Support · corrodedFOUND IN CABIN FORWARD SECTION AT RIGHT FLOOR SUPPORT 10 FROM SERVICE DOOR WAS CORRODED, BS 160-200. REMOVED CORRODED FLOOR SUPPORT, FABRICATED AND INSTALLED REPAIR SUPPORT IAW DC9 SRM 51-10-2, 51-10-4, 51-10-3, 53-01 FIGURE 1, 51-30-5.Oct 3, 1999 · N812AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900714Window Frame · corrodedFOUND UPPER CORNER OF WINDOW FRAME WAS CRACKED AT BS 699R. REMOVED WINDOW FRAME, INSTALLED NEW WINDOW FRAME IAW DC9 SRM 51-30-5, 53-04 FIGURE 34.Oct 1, 1999 · N812AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900746Angel · corrodedFOUND CAP L ANGEL CORRODED AND CRACKED 4AT BS 965-BL24R. REMOVED CAP ANGEL AND REPLACED, FABRICATED AND INSTALLED 8 TRACKED ANGLE REPAIR IAW TIMCO RES 07186 AND DC9 SRM 53-30-5.Sep 29, 1999 · N812AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900706Angle · corrodedFOUND AFT AIRSTAIR, FIFTH STEP FROM THE BOTTOM AT SUPPORT ANGLE, WAS CORRODED. REMOVED CORRODED ANGLE, FABRICATED, TREADED, PRIMED, AND INSTALLED NEW ATTACH ANGLE IAW DC9 SRM 51-10-1, 52-60-0, 51-10-3, 51-10-5, 51-30-2, 51-30-5.Sep 29, 1999 · N812AT · Doug DC932 · Entrance StairsSDR AT9900688Angle · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND SUPPORT ANGLE FOR AFT VENTRAL STAIRS AND 3RD STEP CORRODED. REMOVED, FABRICATED, AND INSTALLED SUPPORT ANGLE ON AFT STAIRS AND NR 3 STEP IAW DC9 SRM 51-10-3, 51-30-2, 51-30-5.Sep 29, 1999 · N812AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900708Support · corrodedFOUND FLOOR SUPPORT AT BS 200-218 WAS CORRODED, ABOUT 14 FROM CENTER LINE. REMOVED FLOOR SUPPORT, FABRICATED, TREATED, PRIMED AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-10-2, 51-10-4, 51-30-1.Sep 28, 1999 · N812AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900707Step · corrodedFOUND AFT AIRSTAIR NR 3 WAS CORRODED. REMOVED AND REPLACED STEP IAW DC9 SRM 51-10-3, 53-01, 53-30-1.Sep 28, 1999 · N812AT · Doug DC932 · Entrance StairsSDR AT9900692Support · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND FLOOR SUPPORT AT LBL 50 BS 160-200 WAS CORRODED. REMOVED, FABRICATED, AND INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-10-3, 51-30-2, 53-11-1.Sep 28, 1999 · N812AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900690Suport · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND FLOOR SUPPORT CORRODED AT BS 205, RBL 0-40. REMOVED, FABRICATED, AND INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-10-3, 51-10-4, 51-30-5.Sep 28, 1999 · N812AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900752Support · corrodedFOUND CABIN FLOOR SUPPORT BS 200 BL 0-BL 42L WAS CORRODED BEYOND LIMITS. REMOVED CORRODED SECTION OF FLOOR SUPPORT, FABRICATED AND INSTALLED REPAIR FLOOR SUPPORT IAW DC9 SRM 53-11-1, 51-10-3, 51-10-4, 51-30-5.Sep 27, 1999 · N812AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900711Step · corrodedFOUND AFT AIRSTAIR, FOURTH STEP FROM THE BOTTOM, WEB ON INBOARD AND OUTBOARD SIDE OF STEP WAS CORRODED. CUT OUT CORROSION, FABRICATED AND INSTALLED REPAIR FILLERS, DOUBLERS AND ATTACH ANGLE IAW DC9 SRM 52-01 FIGURE 1, 51-30-2, 51-20-4, 51-10-2.Sep 24, 1999 · N812AT · Doug DC932 · Entrance StairsSDR AT9900765Longeron · crackedFOUND LONGERONS 3 AND 4 AT BS 148-178 CRACKED. REMOVED CRACKED SECTIONS, TRIMMED TO FIT AND INSTALLED NEW SECTIONS OF LONGERONS 3 AND 4 WITH SPLICES IAW DC9 SRM 53-02 FIGURE 18.Sep 23, 1999 · N812AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT9900680Support · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND CORRODED FLOOR SUPPORT AND ATTACHMENT HARDWARE AT BS 157-218. REMOVED AND REPLACED FLOOR SUPPORT AND HARDWARE AT BS 157-218IAW DC9 SRM 51-10-3, 51-10-4, 51-30-1, 53-01 FIGURE NR 1.Sep 23, 1999 · N812AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900751Rod Assy · corrodedFOUND FORWARD AIRSTAIRS AND LOWER ROD ASSEMBLY WERE CORRODED. REMOVED AND REPLACED THE LOWER ROD ASSEMBLY OF FORWARD AIRSTAIRS, AND RIGGED IAW DC9 MM 20-10-0, 52-62.Sep 22, 1999 · N812AT · Doug DC932 · Entrance StairsSDR AT9900764Longeron · crackedLONGERON AT BS 680-699 L6R WAS FOUND CRACKED. CUT OUT CRACKED SECTION, FABRICATED LONGERON REPAIR AND SPLICE IAW DC9 SRM 53-02 FIGURE18, 51-10-3, 51-10-4, 51-30-5.Sep 14, 1999 · N812AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT9900767Support · corrodedFOUND RIGHT OUTBOARD FLOOR SUPPORT ABOUT 10 FROM SERVICE DOOR AT BS 160-200 WAS CORRODED. REMOVED FLOOR SUPPORT, FABRICATED, AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-30-4, 53-01 FIGURE 1, 51-10-2, 51-10-4, 51-30-5.Sep 13, 1999 · N812AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900719Seat Track · gougedFOUND LEFT OUTBOARD SEAT TRACK WAS GOUGED AT BS 908. REMOVED AND REPLACED TRACK IAW DC9 SRM 53-05 FIGURE 4F 53-20-1, 51-10-3, 51-10-4.Sep 13, 1999 · N812AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR AT9900717Beam · crackedFOUND L-1 DOOR NR 4 BEAM WAS CRACKED AT THE AFT END. INSTALLED NEW FITTING, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-10-3, 52-01 FIGURE 1, 51-30-2, 51-10-3, 51-10-4.Sep 13, 1999 · N812AT · Doug DC932 · Passenger/Crew DoorsSDR AT9900693Stop · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND RIGHT INBOARD ELEVATOR TRAVEL STOP WAS CORRODED. REMOVED AND REPLACED ELEVATOR TRAVEL STOP AND CADMIUM PLATE IAW DC9 OHM 27-10-1, DC9 DPS 9.89.Sep 13, 1999 · N812AT · Doug DC932 · Elevator Control SystemSDR AT9900691Support · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND PASSENGER ENTRY WAY FLOOR SUPPORT WAS CORRODED AT BS 200. REMOVED, FABRICATED, AND INSTALLED FLOOR SUPPORT IAW DC9 SRM 53-10 FIGURE NR 1.Sep 13, 1999 · N812AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900795Control Column · corrodedFOUND FIRST OFFICERS CONTROL COLUMN ON THE AFT LOWER SIDE BELOW THE MACH TRIM INDICATOR WAS CORRODED. TRIMMED OUT CRACK, MECHANICALLY REMOVED CORROSION. FABRICATED AND INSTALLED DOUBLER REPAIR IAW TIMCO EO 99-1301 REV DATE 10/13/99.Sep 12, 1999 · N812AT · Doug DC932 · Control Column SectionSDR AT9900768Rib · gougedFOUND RIGHT WING 5TH SLAT TRACK WAS CHAFING INTO XRS 241 LEADING EDGE RIB. BLENDED GOUGED AREA, TREATED AND PRIMED. REMOVED AND REPLACED ROLLER BEARING IAW TIMCO EO 99-1294 REV DATED 10/05/99.Sep 12, 1999 · N812AT · Doug DC932 · Wing, Rib/BulkheadSDR AT9900762Rib · crackedFOUND RIGHT WING LEADING EDGE HAD TWO CRACKED REPAIR FRAMES/RIBS AT BS 383. FABRICATED AND INSTALLED REPAIR ANGLES/FRAMES/RIBS IAW DC9 SRM 51-30-1, 51-30-2, 51-10-4, 57-22-1, 57-01 FIGURE 3.Sep 12, 1999 · N812AT · Doug DC932 · Wing, Rib/BulkheadSDR AT9900718Skin · crackedFOUND RIGHT ELEVATOR CRACKED IN THE SECONDARY SKIN AT THE RIVET OF THE OUTBOARD TRIM ATTACH POINT. STOP DRILLED HOLE NDT REVEALED CRACK CONTINUED. FABRICATED AND INSTALLED REPAIR STRIP IAW DC9 SRM 51-30-8, 53-10-2, 51-10-2, 51-10-4, 51-10-3.Sep 12, 1999 · N812AT · Doug DC932 · Elevator, Plate/SkinSDR AT9900710Skin · corrodedFOUND RIGHT OUTBOARD ELEVATOR UPPER TRAILING EDGE AT THE TIP WAS CORRODED. CUT OUT CORROSION. FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR IAW DC9 SRM 51-10-2, 51-10-3, 51-30-2 AND 55-03 FIGURE 5.Sep 12, 1999 · N812AT · Doug DC932 · Elevator, Plate/SkinSDR AT9900766Panel · delaminatedFOUND LEFT WING UPPER TRAILING EDGE PANEL INBOARD OF THE AILERON AT XRS 383 WAS DELAMINATED. CUT OUT DELAMINATED HONEYCOMB CORE, BONDED NEW CORE, DOUBLERS AND SKIN. REINSTALLED TRAILING EDGE PANEL IAW DC9 SRM 51-30-1, 51-30-2, TIMCO EO 99-1309 REV DATED 10/1Sep 11, 1999 · N812AT · Doug DC932 · Wing, Plate/SkinSDR AT9900742Longeron · corrodedFOUND A BULGE AT BS 598, LB 0, GAINED ACCESS AND FOUND CORROSION AT LONGERON 30. REMOVED LONGERON 30 LEFT AND RIGHT HAND WEB ASSEMBLY, INSTALLED NEW LONGERON, FABRICATED AND INSTALLED WEB REPAIRS IAW DC9 SRM 53-04 FIGURE 43, 51-30-2, AND DC9 MM 30-10-7.Sep 11, 1999 · N812AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT9900709Skin · dentedFOUND A DENT OUT OF LIMITS AT BS 445.3 BELOW L 19R. CUT OUT DENT, FABRICATED AND INSTALLED REPAIR IAW TIMCO EO 99-1281 REV DATED 10/01/99.Sep 11, 1999 · N812AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900763Stringer · crackedFOUND LEFT SIDE CABIN AT BS 756 STRINGER 2L WAS CRACKED AT ATTACH POINT. CUT OUT CRACKED SECTION, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICES IAW DC9 SRM 53-02 FIGURE 18, 51-30-2, 51-20-4, 51-10-3, AND 51-10-4.Sep 6, 1999 · N812AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT9900761Rib · crackedFOUND RIGHT WING LEADING EDGE HAD THREE CRACKED REPAIR FRAMES/RIBS AT BS 445. REMOVED, FABRICATED AND INSTALLED REPAIR ANGLES IAW DC9 SRM 51-30-5, 57-01 FIGURE 3.Aug 12, 1999 · N812AT · Doug DC932 · Wing, Rib/BulkheadSDR AT9900461R1Switch · defectiveDURING APPROACH, NOTED SMOKE AFTER TURNING ON LEFT AND RIGHT WING LANDING LIGHTS, SMOKE STOP AFTER TURNING LIGHTS OFF. REMOVED AND REPLACED RIGHT WING LANDING LIGHT SWITCH AND OPS CHECKED GOOD PER MM 33-40.Jun 22, 1999 · N812AT · Doug DC932 · Exterior LightingSDR AT9900461Switch · failedDURING APPROACH, NOTED SMOKE AFTER TURNING ON LEFT AND RIGHT WING LANDING LIGHTS, SMOKE STOPPED AFTER TURNING LIGHTS OFF. RIGHT WING LANDING LIGHT SWITCH WAS FOUND TO BE AT FAULT AND PLACED ON MEL (DM24543). LEFT WING LANDING LIGHT WAS OK FOR SERVICE.Jun 22, 1999 · N812AT · Doug DC932 · Exterior LightingSDR AT9900131Slide · looseGALLEY DOOR SLIDE CAME OUT OF BIN. RESECURED GALLEY DOOR EVACUATION SLIDE IAW MM 25-62-0.Feb 18, 1999 · N812AT · Doug DC932 · Emergency EquipmentSDR AT9900114Bulb · failedDURING A B CHECK, FOUND THE TAIL CONE EMERGENCY EXIT INOPERATIVE. RELAMPED TAIL CONE EMERGENCY EXIT LIGHT IAW MM 33-53-0, OPS CHECKED NORMAL.Feb 12, 1999 · N812AT · Doug DC932 · Emergency Lighting
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