N75429
Service difficulty reports not matched to an aircraft · 71
They name N75429, 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 = 'N75429' 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 = 'N75429' 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 MZZA99054Actuator · failedFLT 921 - GUM - AIR RETURN DUE TO SYSTEM 'A' HYDRAULIC LEAK. MAINTENANCE FOUND FLAP HYDRAULIC MOTOR FAILED. REMOVED AND REPLACED FLAP ACTUATOR HYDRAULIC MOTOR IAW MM 27-51-62. INSPECTED CASE DRAIN FILTERS ALL CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE. (M)SDR MZZA99023Skin · corrodedTNN - DURING S-CHECK INSPECTION AT AIR ASIA, CORROSION WAS FOUND ON FUSELAGE SKIN INNER SURFACE AT LEFT SIDE WING SCANNING LIGHT CUTOUT. THE CORRODED SKIN WAS CLEANUP AND REPAIRED PER B727 SRM 53-30-3 FIGURE 22. (M)SDR MZZA99018Battery · dischargedTNN - DURING S-CHECK INSPECTION AT AIR ASIA, PASSENGER CABIN EMERGENCY EXIT LIGHT BATTERIES WERE FOUND INOPERATIVE. THE BATTERIES, P/N S104 AND 106 WERE REMOVED AND REPLACED PER B727 MM 33-50-0 AND OPERATIONAL CHECK FOUND SATISFACTORY. (M)SDR 99ZZZM182Battery · dischargedTNN - DURING S-CHECK INSPECTION AT AIR ASIA, PASSENGER CABIN EMERGENCY EXIT LIGHT BATTERIES WERE FOUND INOPERATIVE. THE BATTERIES, P/N S104 AND 106 WERE REMOVED AND REPLACED PER B727 MM 33-50-0 AND OPERATIONAL CHECK FOUND SATISFACTORY. (M)SDR MZZA99012Spar Web · crackedTNN - DURING S-CHECK INSPECTION AT AIR ASIA, CRACK WAS FOUND ON WING CENTER SECTION REAR SPAR WEB AT WL 185 FROM RBBL 2 TO RBBL 4. THE WING CENTER SECTION REAR SPAR WEB CRACK END WAS STOP DRILLED AND REPAIRED PER EA 5750-01843 OP 3. (M)SDR MZZA99020Stiffener · crackedTNN - DURING S-CHECK INSPECTION AT AIR ASIA, CRACK 2 INCH LONG WAS FOUND ON VERTICAL FIN LEFT SIDE STIFFENER S-7 AT FS 112. THE DAMAGED STIFFENER 2 INCHES LONG WAS TRIMMED OUT AND REPAIRED PER B727 SRM 55-30-04 FIG 1. (M)SDR MZZA99011Control Cable · brokenTNN - DURING S-CHECK INSPECTION AT AIR ASIA, EXCESSIVE BROKEN WIRES WAS FOUND ON NR 3 ENGINE THRUST CONTROL CABLE (T3A) AT BS 1190. THE DAMAGED CABLE ASSEMBLY, P/N 61-32155D3KJ2069 WAS REMOVED AND REPLACED PER B727 MM 76-11-11 AND OPERATION CHECK FOUND SATISFSDR MZZA99010Control Cable · brokenTNN - DURING S-CHECK INSPECTION AT AIR ASIA, EXCESSIVE BROKEN WIRES WAS FOUND ON NR 3 ENGINE START CONTROL CABLE AT BS 1186. THE DAMAGED CABLE ASSY, P/N 61-32155D3KJ2496 WAS REMOVED AND REPLACED PER B727 MM 76-11-11 AND OPERATION CHECK FOUND SATISFACTORY. (MSDR MZZA99009Control Cable · brokenTNN - DURING S-CHECK INSPECTION AT AIR ASIA, EXCESSIVE BROKEN WIRES WAS FOUND ON NR 2 ENGINE THRUST CONTROL CABLE (T2A) AT BS 1188. THE DAMAGED CABLE ASSEMBLY, P/N BCREF13259 WAS REMOVED AND REPLACED PER B727 MM 76-11-11 AND OPERATION CHECK FUOND SATISFACTORYSDR MZZA99008Control Cable · brokenTNN - DURING S-CHECK, INSPECTION AT AIR ASIA, EXCESSIVE BROKEN WIRES WAS FOUND ON NR 1 ENGINE START CONTROL CABLE AT BS 1186. THE DAMAGED CABLE ASSY, P/N 61-32155D3KJ2496 WAS REMOVED AND REPLACED PER B727 MM 76-11-11 AND OPERATION CHECK FOUND SATISFACTORY. (SDR MZZA99007Keel Beam · crackedTNN - DURING S-CHECK INSPECTION AT AIR ASIA, CRACK 1.5 INCH LONG WAS FOUND ON STRINGER S29R OUTBOARD FLANGE BETWEEN BS 950 AND 951.5. THE CRACKED STRINGER S29 KEEL BEAM OUTBOARD FLANGE ALONG OUTBOARD FACE OF VERTICAL CHORD FROM FORWARD END TO ONE AND A HALF FSDR MZZA99006Stiffener · corrodedTNN - DURING S-CHECK INSPECTION AT AIR ASIA, CORROSION WAS FOUND ON BS 950 BULKHEAD LOWER TEE CHORD HORIZONTAL AND VERTICAL FLANGES ADJACENT TO KEEL BEAM S29R. THE CORRODED LOWER TEE CHORD 5 INCHES LONG WAS TRIMMED OUT AND REPAIRED PER EC/RA NR 5310-03810 DATSDR MZZA99019Skin · corrodedTNN - DURING S-CHECK INSPECTION AT AIR ASIA, CORROSION WAS FOUND ON FUSELAGE SKIN AT BS 1360 AT ONE O'CLOCK POSITION. THE CORRODED SKIN 6 INCH BY 6 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-30-3. (M)SDR MZZA99005Skin · corrodedTNN - DURING S-CHECK INSPECTION AT AIR ASIA, SEVERE CORROSION WAS FOUND ON FUSELAGE BELLY SKIN AT S29R BETWEEN BS 950 PLUS 11.09 AND BS 950A. THE CORRODED SKIN 5 INCH BY 5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER EC/RA NR 5310-03809 DATED 15 JAN 1999. (SDR MZZA99004Spring · rustedTNN - DURING S-CHECK INSPECTION AT AIR ASIA, RUSTED AND DAMAGED SPRING WAS FOUND ON LEFT MLG MANUAL EXTENSION MECHANISM. THE DAMAGED SPRING P/N 66-16789-1 WAS REMOVED AND REPLACED PER B727 MM 32-34-1 AND OPERATIONAL CHECK FOUND SATISFACTORY. (M)SDR MZZA99003Stringer · corrodedTNN - DURING S-CHECK INSPECTION AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FUSELAGE STRINGER AT S28R BS 1042. THE CORRODED STRINGER 19 INCHES LONG WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-03 FIGURE 1. (M)SDR MZZA99002Skin · corrodedTNN - DURING S-CHECK INSPECTION AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FUSELAGE BELLY SKIN AT STRINGER S28R BETWEEN BS 1042 AND BS 1065. THE CORRODED SKIN 4 INCH BY 2 INCH AND 2 INCH BY 2 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PERSDR MZZA99001Shear Tie · corrodedTNN - DURING S-CHECK INSPECTION AT AIR ASIA, IG CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FRAME SHEAR TIE AT BS 1130, STRINGER S26L. THE CORRODED FRAME SHEAR TIE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-04 FIGURE 13. (M)SDR MZZA99015Sign · malfunctionedTNN - DURING SELF ILLUMINATION BRIGHTNESS TEST ON AIRCRAFT AT AIR ASIA, LEFT FORWARD EMERGENCY EXIT DOOR 'EMERGENCY' AND 'PULL' SIGN BRIGHTNESS MEASUREMENT WERE FOUND BELOW THE SPECIFIED LIMIT. THE 'EMERGENCY' SIGN P/N 10-61789-1007 AND 'PULL' SIGN P/N 10-617SDR MZZA99014Sign · malfunctionedTNN - DURING SELF ILLUMINATION SIGN BRIGHTNESS TEST ON AIRCRAFT AT AIR ASIA, RIGHT AFT EMERGENCY EXIT DOOR 'PULL' SIGN BRIGHTNESS MEASUREMENT WAS FOUND BELOW THE SPECIFIED LIMIT. THE 'PULL' SIGN P/N 10-61789-1008 WAS REMOVED AND REPLACED PER B727 MM 33-50-31.SDR MZZA99013Sign · malfunctionedTNN - DURING SELF ILLUMINATION SIGN BRIGHTNESS TEST ON AIRCRAFT AT AIR ASIA, RIGHT FORWARD EMERGENCY EXIT DOOR 'PULL' SIGN BRIGHTNESS MEASUREMENT WAS FOUND BELOW THE SPECIFIED LIMIT. THE 'PULL' SIGN P/N 10-61789-1008 WAS REMOVED AND REPLACED PER B727 MM 33-50SDR 99ZZZM181Sign · malfunctionedTNN - DURING SELF ILLUMINATION BRIGHTNESS TEST ON AIRCRAFT AT AIR ASIA, LEFT FORWARD EMERGENCY EXIT DOOR 'EMERGENCY' AND 'PULL' SIGN BRIGHTNESS MEASUREMENT WERE FOUND BELOW THE SPECIFIED LIMIT. THE 'EMERGENCY' SIGN P/N 10-61789-1007 AND 'PULL' SIGN P/N 10-617SDR MZZA98261Indicator · malfunctionedCTS - FLT 938 - ON TAKEOFF ROLL, NR 3 OIL QTY INDICATOR WENT TO .5 GALLON, ON TAXI BACK TO GATE, INDICATOR RETURNED TO NORMAL. REJECTED TAKEOFF AT 90 KNOTS APPLIED MEL 79-01. TANK VISUAL CHECK WAS FULL ON ARRIVAL OF FLT 937 AND AGAIN ON RETURN TO GATE. REMOSDR MZZA98081Controller · failedGUM - FLT 0975 - L/P 7963825 - AT APPROXIMATELY 25 MINUTES OUT AFTER TAKEOFF, CREW ADVISED CABIN CLIMBING AT 400 FEET PER MINUTE WITH AIRCRAFT AT FL 29.0. UNABLE TO CONTROL PRESSURIZATION AT ALL MODES AUTO/STANDBY/MANUAL. MAINTENANCE TROUBLESHOT SYSTEM AND SDR MZZA98035Fairing · crackedKUL - NR 7 FLAP TRACK MID FAIRING FOUND CRACKED AND DELAMINATED AT FWD EDGE OF O/BOARD SKIN. TYPICAL SRM DOUBLER REPAIR IAW ECRA 5720-01628. (M)SDR MZZA98014Floorbeam · corrosionKUL - FLOORBEAM AT STATION 328 AT LBL 30 HAS SURFACE CORROSION. REMOVED CORROSION IAW SRM 51-10-6. FOUND BEYOND LIMIT IAW ECRA 5310-03651. CARRY OUT REPAIR IAW SRM 53-10-8. (M)SDR MZZA98023Skin · corrodedKUL - SEVERAL PREVIOUS CORROSION BELNDOUTS ON FUSELAGE SKIN FORWARD OF BS 1166 AND BETWEEN STRINGER 23L AND 25L FOUND BEYOND SRM ALLOWABLE LIMITS. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 3. (M)SDR MZZA98034Skin · misdrilledKUL - LOWER FORWARD SKIN OF LEFT INBOARD MIDFLAP FOUND WITH MISDRILLED HOLES AT THE FOURTH AND EIGHT HOLES COUNTED FROM OUTBOARD EDGE. DAMAGE AREAS REMOVED AND FILLETS MANUFACTURED AND DOUBLER INSTALLED IAW ECRA 5750-02873. (M)SDR MZZA98032Frame · corrodedKUL - FRAME 1110 UPPER CHORD IS PUNCTURED ABOVE STRINGER 27R DUE LONGER SCREW INSTALLED AT TIED DOWN FITTING AFT OUTBOARD POSITION. DOUBLER MANUFACTURED AND INSTALLED IAW SRM 51-40-3 FIG 1. (M)SDR MZZA98022Frame · hole elongatedFRAME 1110, RT EDGE SUPPORT PANEL INNER ATTACHMENT HOLE FOUND ELONGATED AT FRAME UPPER CHORD. A DOUBLER REPAIR CARRIEID OUT AS PER SRM 51-40-3. (M)SDR MZZA98027Frame · corrodedKUL - FRAME 1166 LOWER CHORD AND WEB IS CORRODED BETWEEN STRINGER 281 AND 28R. BLENDED OUT OF LIMIT IAW SRM 53-10-1, AREA 3 INCH BY 2 INCH BY .018 INCH. REPAIR C/OUT IAW SRM 53-10-4, FIG 12. (M)SDR MZZA98016Seat Track · corrosionKUL - CORROSION ALONG SEAT TRACK FROM STATION 344-480, RBL 24. REMOVED CORROSION IAW SRM 51-10-6. FOUND BEYOND LIMIT IAW SRM 53-10-1. CARRY OUT REPAIR IAW SRM 53-10-5. (M)SDR MZZA98006Seat Track · corrosionKUL - CORROSION ALONG SEAT TRACK, RBL 24 AND 45, STATION 1050--1130. CORROSION FOUND OUT OF LIMIT. FABRICATE SEAT TRACK IAW B727 SRM 53-10-5. INSTALLED TRACK. (M)SDR MZZA98030Seat Track · corrodedKUL - BS 415- BS 420 RBL 60 WINDSCREEN TRACK BADLY CORRODED. BLENDED BEYOND LIMIT IAW 53-10-2. TRACK REPLACED IAW SRM 51-30-2. (M)SDR MZZA98024Skin · crackedKUL - NR 2 SLAT ASSY HAS TWO CRACKS AT THERMAL ANTI-ICE DUCT CUTOUT IN AFT LOWER SKIN ATTACH ANGLE AT SLAT STATION 271. CRACKS STOP DRILLED AND DOUBLER INSTALLED IAW ECRA 5750-02875. (M)SDR MZZA98013Seat Track · corrosionKUL - BS 720D - BS 720C RBL 45.5 SEAT TRACK CENTER AREA FOUND BROKEN. FABRICATED SEAT TRACK IAW B727 SRM 53-10-5 AND INSTALLED IAW B727 SRM 53-10-5. (M)SDR MZZA98010Seat Track · corrosionKUL - BS 380 - BS 440 RBL 45.5 SEAT TRACK FLANGE CORROSION. REMOVED CORROSION IAW SRM 51-10-6. FOUND BEYOND LIMIT IAW SRM 53-10-1. REPLACED SEAT TRACK IAW SRM 53-10-2. (M)SDR MZZA98021Floorbeam · corrodedKUL - FLOORBEAM AT STATION 344 FROM LBL10 TO LBL150 HAS SURFACE CORROSION ON THE HORIZONTAL FLANGE, UPPER AND LOWER SURFACE AT SEVERAL LOCATIONS. CORROSION REMOVED IAW RM 51-10-6, CLEANUP DIMENSION OF .020 INCH BY 3 INCH BY 2 INCH IS FOUND TO BE OUT OF LIMIT SDR MZZA98020Bushing · misinstalledKUL - LEFT INBOARD MIDFLAP. INBOARD AFT FLAP DRIVE SYSTEM DRIVE WHEEL HAS SERRATED RUB MARKS ON LOWER SURFACE INDICATING RUBBING ON STRUCTURE. DRIVEWHEEL REMOVED AND FOUND SHIM WASHER LOCATED BETWEEN BEARING AND HOSING MISSING. ALSO, FOUND FWD END OF AFT FLSDR MZZA98019Control Rod · corrodedKUL - LEFT WHEEL WELL AREA SPPED BRAKE CONTROL VALVE ROD CONNECTING TO QUADRANT FOUND CORRODED. CORROSION BLENDED OUT IAW ECRA 2760-01157. PENETRANT INSPECT IAW OHM 20-20-02. ALODINE REWORKED AREA IAW OHM 20-43-03. PRIME WITH BMS 10-11 TYPE PRIMER, FINISH SDR MZZA98009Support · crackedKUL - FIXED L/E SUPPORT STRUT SITUATED AT WS 175 (AT OUTBOARD END OF NR 3 L/E FLAP ACTUATOR MOUNTING TORQUE BOX) IS CRACKED AT AFT END, THROUGH HI-LOCK HOLES. LEFT WING FIXED L/E SUPPORT STRUT AT NR 3 KRUEGER FLAP ACTUATOR MOUNTING TORQUE BOX, REPLACED IAW SRSDR MZZA98003Seat Track · corrosionSEAT TRACK BETWEEN STATION 950F TO 990 LBL 24.75 HAS NUMEROUS SURFACE CORROSION AT UPPER FLANGE. FOUND CORROSION OUT OF LIMIT. FABRICATE SEAT TRACK AS PER SRM 53-10-05. INSTALLED AS PER SRM 53-10-5. (M)SDR MZZA98002Seat Track · corrosionKUL - FOUND CORROSION AT SEAT TRACK STATION 1050 LBL 24.75. CORROSION FOUND OUT OF LIMITS. FABRICATE SEAT TRACK IAW SRM 53-10-5. INSTALLED IAW SRM 53-10-5. (M)SDR MZZA98001Seat Track · corrosionKUL - SURFACE CORROSION AT SEAT TRACK LBL 24.75, STATION 1070-1110. CORROSION FOUND OUT OF LIMIT. FABRICATE SEAT TRACK IAW SRM 53-10-2. INSTALLED IAW SRM 53-10-02. (M)SDR MZZA98026Frame · corrodedKUL - AFT CARGO FRAME 950C WEB AND CHORD IS CORRODED BETWEEN STRINGER 27R AND 28R. DOUBLER MANUFACTURED AND INSTALLED IAW SRM 53-10-4 FIG 13. (M)SDR MZZA98025Fittings · corrodedKUL - LEFT OUTBOARD FOREFLAP, OUTBOARD STABILIZING TRACK FITTING INBOARD LUG AND MIDDLE STABILIZING TRACK FITTING INBOARD LUB CORRODED BEYOND LIMIT IAW SRM 57-40-00. FITTINGS REPLACED IAW SRM 51-30-2, TRACKS REFITTED AND FOREFLAP REFITTED. FUNCTIONAL CHECK SSDR MZZA98018Splice · misinstalledKUL - SIGN OF OVERHEAT ON APU FEEDER CABLE SPLICES (GENERATOR) LOCATED AT LEFT AIRCOND BAY. SPLICES CHANGED AS PER MM 24-00-09. FOUND SPLICES CRIMPED BY INCORRECT CRIMPING TOOL. (M)SDR MZZA98017Sill · corrosionKUL - SURFACE AND EXFOLIATION CORROSION ON LEFT CREASE BEAM BETWEEN BS 1070 TO 1090. FOUND CORROSION OUT OF LIMITS. REPLACED SILL BEAM AS PER SRM 51-30-2. (M)SDR MZZA98015Sill · corrosionKUL - LEFT CREASE BEAM BETWEEN STATION 990 TO 1030 HAS NUMEROUS SURFACE CORROSION. FOUND CORROSION OUT OF LIMITS. REPLACED CREASE BEAM AS PER SRM 51-30-2. (M)SDR 98ZZZM289Fittings · corrodedKUL - LEFT OUTBOARD FOREFLAP, OUTBOARD STABILIZING TRACK FITTING INBOARD LUG AND MIDDLE STABILIZING TRACK FITTING INBOARD LUB CORRODED BEYOND LIMIT IAW SRM 57-40-00. FITTINGS REPLACED IAW SRM 51-30-2, TRACKS REFITTED AND FOREFLAP REFITTED. FUNCTIONAL CHECK S
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