N467AT
Service difficulty reports not matched to an aircraft · 55
They name N467AT, 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 = 'N467AT' 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.
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 = 'N467AT' AND registry_match IS NULL ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR AT9900521Wire · brokenEMERGENCY PATH LIGHTING MODULE HAD BROKEN WIRE. REPLACED EMERGENCY PATH LIGHTING MODULE IAW B737 20-0, OPS CHECK GOOD.SDR AT9900491Controller · failedAT FLIGHT LEVEL 250, REDUCED POWER FOR DESCENT, CABIN ALTITUDE STARTED TO CLIMB AT 1500 FEET PER MINUTE. STANDBY MODE WAS SELECTED AND TOTALLY LOST PRESSURIZATION, OXYGEN MASK DROP. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. PERFORMED PRESSURE DECAY CHSDR AT9900472Solenoid · defectiveGEAR HANDLE WILL NOT RETRACT PAST OFF POSITION. LEVER LATCH CIRCUIT BREAKER REPEATED POPPED WHEN GEAR LEVER WAS CYCLED. DUMPED FUEL, RETURNED TO ATLANTA. REPLACED LEVER LATCH SOLENOID, OPS CHECKED NORMAL IAW MM 32-31-31.SDR AT9900349Light · defectiveOVER DOOR ( L-1 ) EMERGENCY EXIT LIGHT INOPERATIVE IN ARM POSITION. REMOVED AND REPLACED EMERGENCY EXIT LIGHT.SDR AT9900181Skin · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND FORWARD FUSELAGE AT BS 350 AFT LOWER CORNER CRACKED AT AIRSTAIR CUTOUT. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER, TREATED, PRIMED, PAINTED, AND INSTALLED IAW B737 SRM 51-10-2, MM 51-20-11, AND AERO CORP EO 99SDR AT9900094Wire · looseAFT PORTION OF AISLE WAY EMERGENCY EXIT LIGHTING WAS SNAGGED BY PASSENGER, WIRING IS LOOSE. REPAIRED LOOSE WIRING AS PER MM 2050, OPERATIONAL CHECKED GOOD PER 33-53.SDR AT9900033Wire · brokenTWO EMERGENCY PATH LIGHTS INOPERATIVE. FOUND BROKEN WIRE. SPLICED WIRE AND REINSTALLED IAW DC-9 MM 33-21-27 AND OPS CHECKED GOOD.SDR AT9900021Battery Pack · dischargedAFT EMERGENCY LIGHTS SECTION INOPERABLE FROM ROW 24 BACK. RE-SEATED CANNON PLUG ON BATTERY CHARGER RIGHT HAND AT AFT UPPER PACK. OPS CHECKED GOOD PER MM 33-50. (X)SDR AT9900006Battery Pack · dischargedFOUND BAD CONNECTION ON BATTERY PACK WHILE TROUBLESHOOTING EMERGENCY LIGHTING AT RIGHT EMERGENCY EXIT OVERHEAD. REMOVED AND REPLACED BATTERY PACK IAW B737 SRM 33-51-31. (X)SDR VJ9800593Fuel Control · failedON CLIMBOUT, LOST POWER ON NR 2 ENGINE. FLIGHT CREW SHUTDOWN ENGINE AND DIVERTED TO SAV. REPLACED DEFECTIVE FUEL CONTROL.SDR VJ9800315Battery · dischargedR1 AND R2 PORTABLE EXIT LIGHTS INOP. REPLACED BATTERIES; OPS CHECKED GOOD IAW MM 33-10.SDR VJ9800221Bulb · failedLT WING OVERWING EMERGENCY LIGHT INOP. RELAMPED; OPS CHECKS NORMAL IAW MM 33-50-00.SDR VJ9800034Light · inoperativeRIGHT OVERWING EMERGENCY EXIT LIGHT BROKEN. REPLACED LIGHT ASSEMBLY IAW MM 33-50-01, OPS CHECKED OK.SDR ZZDA3228797Gear Handle · malfunctionedSWF - FLT 533 - DURING FLIGHT, THE LANDING GEAR HANDLE WOULD NOT GO UP. HORN SOUNDED AFTER FLAPS RETRACTED. RETURNED TO SWF. VERIFIED OPERATION OF AIR/GROUND SENSOR LOGIC SYSTEM, LANDING GEAR SAFETY SENSOR, LOCKS AND CABLE. ALL WORK PERFORMED IAW B MM 32-3SDR ZZDA3318097Light · brokenFLT 553 - DURING FLIGHT, FOUND ROW 1D EMERGENCY FLOOR PATH LIGHT BROKEN. REPLACED EMERGENCY FLOOR PATH LENS AND LAMP AT ROW 1D. (X)SDR ZZDA5316897Skin · crackedCRACK IN THE FUSELAGE SKIN AT RIGHT SIDE FUSELAGE STA 727 A-1 BETWEEN STR 14 AND STR 15. CRACK REPAIRED BY REMOVING DAMAGED AREA. FABRICATED REPAIR DOUBLER AND INSTALLED WITH RIVETS WET WITH SEALANT IAW SRM 51-30-3, FIG 1 AND SRM 51-30-1. (X)SDR 97ZZZM925Lens · brokenDURING LAY OVER CHECK, THE EMERGENCY LIGHTS WERE TESTED, L2 DOOR EXIT LENS COVER WAS BROKEN. REPLACED THE LENS.SDR ZZDA3310297Light · brokenDURING TRANSIT CHECK, FOUND R1 EMERGENCY LIGHT INOPERATIVE. FOUND CONTACT BROKEN AT R1 LIGHT ASSY. REMOVED UNSERVICEABLE EMERGENCY LIGHT ASSEMBLY AND INSTALLED SERVICEABLE ASSEMBLY PER B737 MM 33-51-81. OPERATIONALLY CHECK NORMAL. (X)SDR 97ZZZM622Fitting · corrodedRIGHT MLG STABILIZER BEAM MOUNTING ATTACH FITTINGS CORRODED. REMOVED FITTINGS FROM FWD AND AF TRT MLG STABILIZER BEAM MOUNT ATTACH FITTING. CORROSION WENT BEYOND LIMITS IAW SRM 51-10-6 AND 53-10-1. DRILLED AND DEBURRED TWO FORWARD AND AFT ATTACH FITTINGS IASDR 97ZZZM621Beam · corrodedRIGHT MLG STABILIZER BEAM FORWARD AND AFT ATTACH POINT CORRODED ON BEAM. REMOVED STABILIZER BEAM LINK. REPLACED WITH NEW STAB BEAM LINK IN RIGHT MLG IAW B737 MM 57-40-00.SDR 97ZZZM614Chord · corrodedRIGHT WING T/E LOWER CHORD CORRODED AT INBOARD FLAP OUTBOARD TRACK ATTACH POINT ON LOWER SURFACE AND INSIDE OUTBOARD ATTACH HOLE. REMOVED LIGHT SURFACE CORROISON (.001) IN LIMITS IAW SRM 51-10-6 AND MM 51-21-51. FABRICATED BUSHINGS ON OUTBOARD HOLE PER EO 97SDR 97ZZZM613Flap Track · corrodedRIGHT WING REAR SPAR OUTBOARD FLAP INBOARD TRACK MOUNT RIGHT HOLE HAS PITTING IN INSIDE DIAMETER. REMOVED CORROSION. FABRICATED BUSHINGS AND INSTALLED BUSHINGS IAW EO NR 97-457.SDR 97ZZZM612Fitting · corrodedLEFT WING OUTBOARD FLAP OUTBOARDTRACK AFT MOUNT IS CORRODED. REMOVED TWO BUSHINGS FROM LEFT OUTBOARD FLAP INBOARD TRACK FITTING OUTBOARD HOLE AND OUTBOARD TRACK FITTING OUTBOARD HOLE. REMOVED CORROSION BY REAMING HOLES TWO EACH. NDT INSPECTED, NO CRACKS, NOSDR 97ZZZM611Flap Track · corrodedRIGHT WING REAR SPAR OUTBOARD FLAP INBOARD TRACK MOUNT RIGHT HOLE HAS PITTING IN INSIDE DIAMETER. REMOVED CORROSION. FABRICATED BUSHINGS AND INSTALLED IAW EO NR 97-457.SDR 97ZZZM610Flap Track · corrodedLEFT WING OUTBOARD FLAP INBOARD TRACK AFT MOUNT IS CORRODED. REMOVED CORROSION AND REFINISHED FLAP TRACK IAW EO NR 97-457 PAGE 2-5. CORROSION BEFORE REMOVAL .345 AND .317 CORROSION AFTER REMOVAL .319 AND .290.SDR 97ZZZM609Fitting · pittedRIGHT WING SPAR OUTBOARD FLAP INBOARD TRACK MOUNTING RIGHT HOLE I/D HAS PITTING. REMOVED CORROSION BY REMOVING BUSHINGS FROM RIGHT REAR SPAR OUTBOARD FLAP INBOARD TRACK MOUNT AND OUTBOARD TRACK MOUNT. REAMED HOLES TO REMOVE CORROSION. NDT INSPECTED, NO CORRSDR 97ZZZM608Fitting · pittedRIGHT WING SPAR OUTBOARD FLAP INBOARD TRACK MOUNTING RIGHT HOLW I/D HAS PITTING. REMOVED CORROSION BY REMOVING BUSHINGS FROM RIGHT REAR SPAR OUTBOARD FLAP INBOARD TRACK MOUNT AND OUTBOARD TRACK MOUNT. REAMED HOLES TO REMOVE CORROSION. NDT INSPECTED, NO CORRSDR 97ZZZM607Chord · corrodedRIGHT WING T/E LOWER CHORD CORRODED AT INBOARD FLAP OUTBOARD TRACK ATTACH POINT ON LOWER SURFACE AND INSIDE ATTACH HOLE. REMOVED LIGHT SURFACE CORROSION (.001) IN LIMITS IAW SRM 51-10-6 AND MM 51-21-51. FABRICATED BUSHINGS ON OUTBOARD HOLE PER EO 97-457 AND SDR 97ZZZM618Floorbeam · corrodedFORWARD CARGO STATION 328 CABIN FLOORBEAM HAS CORROSION RBL 24-56. FABRICATED 'L' ANGLES, TWO 1 INCH BY 2 INCH BY 100 INCH, ONE 1INCH BY 2 INCH BY 30 INCH FROM BAC 1505 100246 T-ANGLE, TWO 1 FOOT 1.5 INCHES BY .063 INCH AND TWO 1 INCH BY 1 INCH BY 8 INCH BY .SDR 97ZZZM617Floorbeam · corrodedCORROSION ON FLOORBEAM BS 294 BL 24 LEFT. FABRICATED 4 'L' ANGLES FROM 7075 .063 12 INCH BY 1.25 INCH BY 1 INCH AND 2.10 INCH BY 1.25 INCH BY 1. INSTALLED IAW SRM 53-10-9 FIG 5.SDR 97ZZZM615Floorbeam · corrodedFLOORBEAM T-CAP CORRODED AT FS 294.5 FROM LBL 12 TO RBL 12. CORROSION WAS .030 BEYOND LIMITS IAW SRM 53-10-1. FABRICATED FLOORBEAM SECTION OUT OF 7075 T611 98.5 INCH BY 2 INCH BY 1 INCH. INSTALLED REPAIR IAW SRM 51-30-2, 51-10-1, 51-10-2 AND MM 51-21-21.SDR 97ZZZM606Floorbeam · corrodedFLOORBEAM FS 344 (UPPER T-CAP) CORRODED FROM LBL 45-58. CORROSION WAS .030 BEYOND LIMITS IAW SRM 53-10-1 FIG 1. FABRICATED ONE FLOORBEAM REPAIR. FABRICATED 6 ATTACH ANGLES. ONE OUT OF 7075 T6 11 11.75 INCH BY 1 INCH BY 1 INCH BY .063. THREE OUT OF 7075 T61SDR 97ZZZM605Frame · crackedFS 639 LEFT 639 FRAME IS CRACKED 3 INCH SPANWISE AT WL 218. FABRICATED WEB STATION FROM 2024 T3 .063 20 INCH BY 5.75 INCH IAW DWG 69-76459. INSTALLED WEB REPAIR IAW DWG 65C31 658 AND SB B737-53-106.SDR 97ZZZM604Splice · corrodedSTRINGER SPLICE CORRODED AT FS 907 STRINGER 24L. SPLICE WAS CORRODED BEYOND LIMITS. FABRICATED NEW SPLICE AND INSTALLED IAW SRM 53-10-3, 53-10-1, 51-10-2 AND MM 51-21-21.SDR 97ZZZM603Stringer · corrodedSTRINGER 19 RIGHT HAS HEAVY CORROSION BETWEEN FS 747 AND 767. STRINGER WAS FOUND TO BE BEYOND LIMITS. FABRICATED NEW SPLICE FROM 7075.0 .063 16 INCH BY 1.25 INCH, 14.25 INCH BY 1 INCH. INSTALLED ALL REPAIRS IAW SRM 53-10-3, 51-10-2, AND MM 51-21-21.SDR 97ZZZM602Stringer · crackedSTRINGER 26R HAS CRACK 27 INCHES LONG AT BS 927 AT SHEAR CLIP ATTACH. REMOVED CRACKED STRINGER. CUT AND TRIM TO FIT SRINGER PART NR BAC-1498-157 (27 INCH LONG). FABRICATED SPLICE DOUBLER FROM 7075 T6 .040 914.75 INCH BY 1 INCH BY 1 INCH BY 1 INCH). FABRICASDR 97ZZZM601Skin · lightning strikeLOWER FUSELAGE ANTENNA BETWEEN STATION 380-400 HAS LIGHTNING STRIKE. REMOVED FORWARD PIT AND FORWARD DECK PANEL FOR ACCESS. REMOVED ANTENNA AND BASE. CAPPED AND SLOWED CO-AXIAL CABLES. FABRICATED 2 DOUBLERS OUT OF 2024 T3 .080 5.25 INCH BY 2.25 INCH. FABRSDR 97ZZZM593Seat Track · corrodedSEAT TRACKS HAVE EXFOLIATED CORROSIN FORWARD GALLEY AREA BS 294 RBL 12 AND RBL 24 FORWARD GALLEY TIE DOWN. CUT AND TRIMMED 2 SEAT TRACKS TO FIT PART NR BAC 1520-792 24.5 INCH AND INSTALLED SEAT TRACKS ALL IAW B737 SRM 53-10-5. (M)SDR 97ZZZM591Floorbeam · corrodedSTATION 967 CENTER ABOVE LAVATORY TANK HAS CORROSION. CUT OUT CORRODED AREA. FABRICATED 'L' ANGLE FROM 7075 T6 .080 15.2 INCH BY 2.7 INCH. FABRICATED 'L' ANGLE FROM 7075 T6 .071 12 INCH BY 2.7 INCH. FABRICATED FILLER 7075 T6 .125 2.5 INCH BY 2.0 INCH. FABSDR 97ZZZM595Angle · corrodedFORWARD SIDE OF FRAME HAS CORROSION AT STATION 727A BETWEEN STRINGER 21L AND 22L. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG 1 PAGE 4. REMOVED STRINGER TIE ANGLE. FABRICATED REPAIR 8 INCH BY 1.3 INCH BY 1.7 INCH .070 7075 T6 IAW BAC SRMSDR 97ZZZM594Angle · corrodedDURING HEAVY SERVICE VISIT TO AERO CORP, FORWARD SIDE OF FRAME HAS CORROSION AT STATION 727A BETWEEN STRINGER 21L AND 22L. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG 1 PAGE 4. REMOVED STRINGER TIE ANGLE FABRICATED REPAIR 8 INCH BY 1.3 INSDR 97ZZZM624Skin · corrodedRIGHT OUTBOARD FLAP BADLY CORRODED INBOARD END OF FLAP. CUT OUT CORRODED AREA 4.375 INCH BY 2.625 INCH. FABRICATED FILLER FROM 7075-T8 .083 4.375 INCH BY 2.625. FABRICATED ANGLE FROM 7075 T6 2.75 INCH BY .375 INCH. FABRICATED NEW ATTACH ANGLE FROM 2024 T-3SDR 97ZZZM623Skin · crackedEXTERNAL FUSELAGE SKIN CRACKED .25 INCH BS 294 AT R-1 DOOR UPPER HINGE CUT OUT CONFIRMED BY HFEC. FABRICATED DOUBLER FROM MIL 5-5059 .50 HARD .063 AND FILLER FROM 2024 T3 .063 7.375 INCH BY 5.25 INCH. DOUBLER DIM 15.375 INCHY BY 5.5 INCH. INSTALLED REPAIRS SDR 97ZZZM600Web · corrodedCORROSION BLOW OUT ON WEB UNDER SCUFF PLATE AT STATION 500B LONGERON 27 LEFT. MECHANICALLY REMOVED CORROSION METAL LOSS OVER 20 PERCENT OUT OF LIMITS IAW B737 FABRICATED REPAIR DOUBLER FROM 2024 T3 .050 INCH BY 16 INCH BY 1 INCH PER SRM 51-40-2 AND INSTALLED SDR 97ZZZM596Stringer · corrodedSTRINGER 21 RIGHT BULGED AT FS 770 AT DOME NUT. CUT OUT CORRODED STRINGER AND FABRICATED U-CHANNEL FROM 7075 T6 .032 11.5 INCH BY 1 INCH BY 1 INCH BY .750 INCH. FABRICATED NEW CHIP FROM 7075 T6 .032 BY .600 INCH BY 1.40 INCH BY 1.40 BY 3.4O INCH. INSTALLED SDR 97ZZZM620Angle · crackedFORWARD PIT HAS CRACK IN CORNER UNDER SCUFF PLATE ON WEB AND NUT PLATE AT STATION 380 LONGERON 27R. REMOVED CRACKED ATTACH HANDLE. FABRICATED NEW ANGLE OUT OF 2024 T 3.5 INCH BY 1.5 INCH BY 1.875 INCH BY .032. INSTALLED IAW SRM 51-10-1, 51-06-1, AND MM 51-2SDR 97ZZZM371Web · crackedDURING HEAVY SERVICE VISIT AT AERO CORP IN LAKE CITY, FL, FOUND CRACK UNDER SCUFF PLATE, ON THE WEB AT FS 380, LONGERON 27R. REPAIRED CRACK IAW B737 SRM 51-10-01, 51-10-6 AND MM 51-21-71. (M)SDR 97ZZZM599Floorbeam · corrodedFLOORBEAM FS 312 UPPER T-CAP CORRODED LBL 12 - RBL 12. FABRICATED T-ANGLE FLOORBEAM AND SPLICE 'L' ANGLE. 'T' ANGLE 82.5 INCH BY 1 INCH FROM 7075 T6 .090. 'L' ANGLES 14 INCH BY 1 INCH BY 1 INCH 2 FROM 7075 T6 .063 INSTALLED IAW SRM 53-10-9.SDR 97ZZZM598Intercostal · corrodedFLOORBEAM SUPPORT INTERCOSTAL HAS CORROSION BETWEEN FS 294.5-312 LBL 12. REMOVED INTERCOSTAL AND FABRICATED NEW INTERCOSTAL AND 2 INCH T-ANGLES 17 INCH BY 2 INCH BY 1 INCH FROM 7075 T6 .090. FABRICATED STRAP 15.5 INCH BY 2 INCH. INSTALLED IAW SRM 53-10-2.SDR 97ZZZM597Angle · corrodedINTERIOR LOWER LOBE HAS CORROSION AT E/E CUTOUT FRAME BS 344 BETWEEN STRINGER 29-28L. CORROSION WAS FOUND TO BE BEYOND LIMITS IAW SRM 53-10-1. FABRICATED ANGLE REPAIR OUT OF 7075 T6 .40 9.25 INCH BY 1 INCH BY 1 INCH AND 3 INCH BY 1 INCH BY 1 INCH IAW SRM 37-
Back to N467AT