N126AA

Service difficulty reports not matched to an aircraft · 34

They name N126AA, 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 = 'N126AA' 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 HALA0100250Adc · failedATO - DURING TAKEOFF NO AIRSPEED INDICATION ON F/O'S AIRSPEED INDICATOR. REPLACED NR 2 ADC. OPS CHECK OF NR 2 ADC CHECKED GOOD PER 34-16-01. INSPECTED F/O'S PITOT TUBE, PRESSURE CHECK GOOD. (M)Oct 18, 2001 · N126AA · Doug DC1010 · Air Data ComputerSDR AALA20010534Bulkhead · corrodedTUL - FOUND FORWARD SIDE OF BULKHEAD AND STIFFENER HAS CORROSION 10 INCHES UP FROM FLOOR. INSTALLED REPAIR DOUBLERS PER ESO 7349 DATED 03-09-2001. (M)Mar 14, 2001 · N126AA · Doug DC1010 · Fuselage Main, BulkheadSDR AALA20010376Skin · damagedTUL - FOUND SKIN AT FORWARD CARGO ABOUT 48R TO 43R, FS 1059 TO 1150 OUT OF LIMITS. INSTALLED CLASS I REPAIR DOUBLER PER SRM 53-30-00 VOL I. (M)Mar 2, 2001 · N126AA · Doug DC1010 · Fuselage Main, Plate/SkinSDR AALA20010360Angle · corrodedTUL - FOUND CORROSION ON J-ANGLE AT STATION 879 AND STRINGER 52 AND CORROSION AT STATION 52 AND STRINGER 868-824. REPLACES SECTION OF J-ANGLE AND SECTION OF STRINGER PER SRM 53-00-01 VOL I AND SRM 53-10-00. (M)Feb 27, 2001 · N126AA · Doug DC1010 · Fuselage Main, StructureSDR AALA20010424Skin · corrodedTUL - FOUND PITTING AND CORROSION ON SKIN UNDER SHEAR TIE BETWEEN STRINGER 51L AND 52L UNDER STATION 824. ALODINED, PAINTED, AND REPLACED CORRODED AREA IAW SRM 53-20-00 VI CLASS II REPAIR, PER ESO 7349 DATE 3-5-01. (M)Feb 19, 2001 · N126AA · Doug DC1010 · Fuselage Main, Plate/SkinSDR AALA20010425Splice · corrodedTUL - FOUND CORROSION ON STRINGER SPLICE LN 50L STATION 755 TO 775 E-58 0193619, 0193621, 0193622, 0193632. REPAIRED PER ESO 7349 DATED 3-7-01. (M)Feb 12, 2001 · N126AA · Doug DC1010 · Fuselage Miscellaneous StructureSDR AALA20001555Engine · failedHNL - FLT 0162 - AFTER TAKEOFF DURING CLIMB-OUT PASSING 17,000 FEET, A LOUD BANG WAS HEARD WITH VIBRATION BEING NOTED AS WELL AS SMOKE AND FUMES IN CABIN. NR 1 ENGINE FAILED. ACCOMPLISHED FIRE/SEVERE DAMAGE CHECKLIST, DUMPED FUEL, AIR INTERRUPTED, AND LANDEDSep 13, 2000 · N126AA · Doug DC1010 · Engine (Turbine/Turboprop)SDR AALA20001264Fitting · crackedTUL - FOUND CRACK INDICATION IN BOTTOM OF C HOLE MOST INBOARD FORWARD FLANGE OF AFT BULKHEAD FITTING. ACCOMPLISHED BY WORKCARDS ECO ESO DR 549404-DR549402 P-4233, 4234, 4439, 4450, 4483, 4932. ECO-45594B, ESO 8783 UPPER SPAR REWORKED, DC10-5485 ESO 7349 D-1-Jul 27, 2000 · N126AA · Doug DC1010 · Fuselage Main, Attach FittingsSDR AALA982135Trunnion · corrodedTUL - FOUND CORROSION PITTING IN TOP AFT MOUNT HOLE IN THE MAIN GEAR TRUNNION FITTING FOR RETRACT CYLINDER UPPER SUPPORT FRAME RIGHT WING. REPAIRED PER ESO 7349, DATED 11-17-98. (M)Nov 18, 1998 · N126AA · Doug DC1010 · Wing, Landing Gear Attach FittingsSDR AALA982133Trunnion · corrodedTUL - FOUND CORROSION PITTING IN TOP FORWARD MOUNT HOLE IN THE MAIN GEAR TRUNNION FITTING FOR RETRACT CYLINDER UPPER SUPPORT FRAME. REPAIRED PER ESO 7349, DATED 11-18-98. (M)Nov 18, 1998 · N126AA · Doug DC1010 · Wing, Landing Gear Attach FittingsSDR AALA982070Stringer · crackedTUL - FOUND CRACK INDICATION IN HOLE 'D' RIGHT WING NR 8 STRINGER COMPENSATOR FLANGE. REMOVED AND REPLACED RT INBOARD STRINGER NR 8 PER ESO 7349, DATED 11-5-98. (M)Nov 6, 1998 · N126AA · Doug DC1010 · Wing, Longeron/StringerSDR AALA982134Trunnion · corrodedTUL - FOUND CORROSION IN TRUNNION BORE OF HOLES FOR FITTING ARB 7170-1 FOR UPLOCK CYLINDERS. CORROSION REMOVAL AND REWORKED PER ESO 7349 DATED 11-5-98 AND ESO 7349 DATED 11-17-98. (M)Nov 1, 1998 · N126AA · Doug DC1010 · Fuselage, Landing Gear Attach FittingsSDR AALA982023Tee · crackedTUL - FOUND BULKHEAD TEE CAP STATION 1156 IS CRACKED OUTBOARD END, TEMP REPAIR INSTALLED. REPAIRED LEFT SIDE TEE CAP PER MOD DRAWING SR10530073. (M)Oct 30, 1998 · N126AA · Doug DC1010 · Fuselage Miscellaneous StructureSDR AALA982022Seat Track · corrodedTUL - FOUND CORROSION IN SEAT TRACK NR 6 FROM STATION 715-755. OK FOR CONTINUED SERVICE PER ESO 7349, DATED 10-29-98. (M)Oct 30, 1998 · N126AA · Doug DC1010 · Fuselage, Seat/Cargo Attach FittingsSDR AALA982020Floorbeam · crackedTUL - FLOORBEAMS AT STATION 800 AND 810 CRACKED AT THE END LEFT SIDE. SPLICED IN NEW SECTION OF FRAME PER AARD 51-01-00-05 AND SRM 53-60-01 PAGE 7 VOL 1. (M)Oct 30, 1998 · N126AA · Doug DC1010 · Fuselage Main, Floor BeamSDR AALA982019Support · corrodedTUL - FOUND CORROSION GALLEY SUPPORT BETWEEN TRACKS 4 AND 5 AT STATION 775. INSTALLED DOUBLER PER ECO 7349, 10-30-98. (M)Oct 30, 1998 · N126AA · Doug DC1010 · Fuselage Miscellaneous StructureSDR AALA982018Support · corrodedTUL - FOUND CORROSION ON GALLEY SUPPORT BETWEEN SEAT TRACKS 3 AND 4 STATION 775. INSTALLED DOUBLER PER ECO 7349, 10-30-98. (M)Oct 30, 1998 · N126AA · Doug DC1010 · Fuselage Miscellaneous StructureSDR AALA982021Seat Track · corrodedTUL - FOUND CORROSION IN SEAT TRACK NR 6 AT STATION 765-770. REMOVED AND REPLACED SEAT TRACK FROM 765-832 PER SRM 53-70-00 FIG 1. (M)Oct 29, 1998 · N126AA · Doug DC1010 · Fuselage, Seat/Cargo Attach FittingsSDR AALA981275Tire · failedSFO - FLT 0020 - AFTER TAKEOFF SFO, 5 KNOTS PRIOR TO V1, AIRPLANE VIBRATED EXCESSIVELY. AFTER GEAR RETRACTION, ALL THREE RED LIGHTS STAYED ILLUMINATED. GEAR HANDLE POPPED OUT AND THEN BACK INTO THE UP DEFAULT. VISUAL INSPECTION SHOWED RIGHT MAIN GEAR DOORS Jun 26, 1998 · N126AA · Doug DC1010 · TireSDR AALA970288Bell Frame · corrodedTUL - BELL FRAME HAS HEAVY PITTING AND FLAKING CORROSION 50L TO 51R, STRINGERS STATION 1099. REPLACED BELL FRAME FROM LONG 46T TO 48L, STATION 1099, PER SRM 53-40-00 FIG 1. (M)Feb 4, 1997 · N126AA · Doug DC1010 · Fuselage Main, FrameSDR AALA970283Shear Tie · corrodedTUL - AFT SECTION OF SHEAR TIE CORRODED 50L TO 51R, STRINGER STATION 1099. INSTALLED NEW SECTION OF SHEAR TIE FROM STRINGER 47L TO 49R PER SRM 53-40-00. (M)Feb 4, 1997 · N126AA · Doug DC1010 · Fuselage Miscellaneous StructureSDR AALA970175Roller Tray · corrodedTUL - RIGHT INBOARD GALLEY ROLLER TRAY HAS AREAS OF CORROSION. INSTALLED NEW SECTION OF ROLLER TRAY PER SRM 53-70-00 FIG 8. (M)Jan 23, 1997 · N126AA · Doug DC1010 · Buffet/GalleysSDR AALA970199Skin · corrodedTUL - MID LAV SERVICE PANEL HAS CORROSION AROUND HINGE FASTENER HOLES. REMOVED CORRODED AREA, INSTALLED FILLER AND DOUBLERS PER ESO 7349 DATED 1-17-97. (M)Jan 22, 1997 · N126AA · Doug DC1010 · Fuselage Main, Plate/SkinSDR AALA970160Skin · corrodedTUL - SKIN HAS CORROSION AND IS BULGED. INSTALLED CLASS I STRUCTURAL REPAIR PER SRM 53-20-00-0 VOL I FIG. (M)Jan 21, 1997 · N126AA · Doug DC1010 · Fuselage Main, Plate/SkinSDR AALA970151Bulkhead Support · corrodedTUL - FOUND CORROSION ON VERTICAL BULKHEAD SUPPORT AFT FRAME 1784 CENTER CARGO LONG 51L TO 51R. INSTALLED DOUBLER ANGLE PER SRM 53-00-01. (M)Jan 20, 1997 · N126AA · Doug DC1010 · Fuselage Main, BulkheadSDR AALA970150Track · corrodedTUL - CORROSION INSIDE 10 HOLES ON LEFT INBOARD FLAP TRACK MOUNTS. REMOVED CORROSION BY MECHANCIAL METHOD PER SRM VOL 11 51-21-00 PAGE 27 PAR 34 4 HOLES IN LIMITS) 6 HOLES OUT, CLEANED AND ALODINED ALL HOLES. MADE NEW BUSHING OUT OF 17-4PHH900. INSTALLED WEJan 15, 1997 · N126AA · Doug DC1010 · Trailing Edge FlapsSDR AALA970116Skin · crackedTUL - FOUND 1 INCH CRACK ON OUTBOARD FLAP, 10 FEET OUTBOARD OF INBOARD END. INSTALLED EXTERNAL DOUBLER PER SRM 57-20-00 PAGE 41. (M)Jan 14, 1997 · N126AA · Doug DC1010 · Trailing Edge FlapsSDR AALA970110Angle · corrodedTUL - CORROSION ON 2 ANGLE, RIGHT SIDE. MANUFACTURED AND INSTALLED TWO REPAIR DOULERS AND FILLERS PER SRM 53-00-01. (M)Jan 14, 1997 · N126AA · Doug DC1010 · Fuselage Miscellaneous StructureSDR AALA970152Angle · corrodedTUL - FOUND CORROSION AT THE LOWER OUTBOARD CORNER, AT STATION 1381 SLANT PANEL. REMOVED CORRODED ANGLE, INSTALLED NEW ANGLE PER SRM 53-40-00 PAGE 55. (M)Jan 10, 1997 · N126AA · Doug DC1010 · Fuselage Miscellaneous StructureSDR AALA970145Trunnion · corrodedTUL - FORWARD TRUNNION HAS CORROSION ON FORWARD AND AFT LUGS, ON FORWARD AND AFT SURFACES AND CENTER BORE. REFACED ALL SURFACES PER SRM 57-20-00 PAGE 72 AND COMPLETED CORROSION REPAIR AS PER 51-21-00 VOL 11. (M)Jan 10, 1997 · N126AA · Doug DC1010 · Fuselage, Landing Gear Attach FittingsSDR AALA970143Trunnion · corrodedTUL - AFT TRUNNION HAS CORROSION ON FORWARD AND AFT LUGS, ON FORWARD AND AFT AND CENTER BORE. REPLACED ALL SURFACES PER SRM 57-20-00 PAGE 72 AND COMPLETED CORROSION REPAIR PER SRM 51-21-00 VOL II. (M)Jan 10, 1997 · N126AA · Doug DC1010 · Fuselage, Landing Gear Attach FittingsSDR AALA970107Drain Pan · corrodedTUL - FOUND CORROSION IN BOTTOM OF GALLEY DRAIN PAN, LEFT SIDE. INSTALLED NEW GALLEY DRAIN PAN, LEFT STATION 771. (M)Jan 10, 1997 · N126AA · Doug DC1010 · Fuselage Miscellaneous StructureSDR AALA970113Bulkhead Skin · corrodedTUL - INTERIOR SKIN IN CAC AT FORWARD SIDE OF BULKHEAD, CORRODED. REMOVED AND INSTALLED NEW CLIP, TREATED, PRIMED AND PAINTED. (M)Jan 8, 1997 · N126AA · Doug DC1010 · Fuselage Main, BulkheadSDR AALA950038Control Cable · defectiveLAX-BOS - FLT 94 - DURING CRUISE, NR 2 ENGINE THROTTLE LEVER FROZE. ACFT PROCEEDED TO BOS. NR 2 ENGINE SHUTDOWN DURING APPROACH TO BOS AND ACFT LANDED WITHOUT INCIDENT. REPLACED NR 2 ENGINE THROTTLE CABLE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. Jan 10, 1995 · N126AA · Doug DC1010 · Power Lever
Back to N126AA