N964AX, cancelled Jan 4, 2010
Service difficulty reports · 63
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N964AX' AND deregistration_id = 'N964AX-2010-01-04' 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 = 'N964AX' AND deregistration_id = 'N964AX-2010-01-04' 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 ABXA070283Pan · crackedWHILE COMPLYING WITH NEA 52300001-001, FOUND INNER DOOR PAN CRACKED. REPAIRED PAN IAW DC9 SRM 52-05, FIGURE 26A.SDR ABXA070282Pan · crackedDURING INSPECTION OF DOOR NEA 52300001-001, FOUND INNER DOOR PAN CRACKED. REPAIRED PAN IAW DC9 SRM 52-05, FIGURE 26A.SDR ABXA070281Angle · crackedDURING ROUTINE SERVICE BULLETIN INSPECTION OF LEFT DORSAL FIN ATTACH ANGLE, FOUND ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-2 AND 51-30-5.SDR ABXA060294Door Frame · crackedLEFT AND RIGHT UPPER DOOR JAMBS ON AFT P-DOME WERE CRACKED. REPAIRED AREA IAW REA D953-54944.SDR ABXA060243Battery · dischargedFOUND EMERGENCY LIGHTS VERY DIM. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8-0001.SDR ABXA060058Battery · dischargedEMERGENCY LIGHTS DO NOT TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53. OPS CHECK GOOD.SDR ABXA050357Coalescer Bag · unknownEN ROUTE RIGHT AC PACK MAINTAINED 13 PSI, AC PRESSURIZATION CONTROLLER WENT TO STBY/LOCKOUT AT TOP OF DESCENT, CABIN PRESSURE CONTROLLER FAILED, PERFORMED EMERGENCY DESCENT. PERFORMED BITE CHECK ON BOTH CABIN PRESSURE CONTROLLERS. NO FAULTS FOUND. SWAPPED NSDR ABXA050285Controller · defectiveCABIN PRESSURIZATION LOSS AT TOP OF DESCENT. CABIN PRESSURE EMERGENCY LIGHT ILLUMINATED, EMERGENCY PROCEDURE COMPLETED. NO FURTHER INCIDENT. PERFORMED BITE TEST PROCEDURES AND THE FOWARD CABIN PRESSURE CONTROLLER FAILED TEST. REPLACED FORWARD CABIN PRESSUSDR ABXA050243Fitting · leakingAT FLIGHT LEVEL 350, NOTICED CREW 02 BOTTLE WAS LOSING PRESSURE. DESCENDED TO LOWER ALTITUDE (170). REMAINDER OF FLIGHT, PRESSURE REMAINED AT 1000 PSI. SERVICED CREW 02 BOTTLE TO 1800 (WAS 1000) PSI. FOUND LINE FROM BOTTLE TO VALVE FITTING ON BULKHEAD LEAKSDR ABXA050208Duct · looseAT FL 350 LOST CABIN PRESSURE. LT PACK WAS NOT PROVIDING PRESSURIZATION BUT WAS IN AUTO AND INDICATED 160 PSI. ONLY ABLE TO MAINTAIN FL 210 WITH RIGHT PAC AT 260 PSI. BOTH PAC TEMPS NORMAL. FOUND RIGHT ACM DISCHARGE DUCT LOOSE AND RESECURED. REMOVED AND REPLACSDR ABXA040391Shear Tie · crackedUPPER END OF SHEAR TIE CRACKED AT LONGERON 14 RIGHT, AFT OF FRAME 1056. REMOVED AND REPLACED SHEAR TIE IAW DC-9 SRM 51-30-5.SDR ABXA030326Radome · out of toleranceRADAR PAINTS STREAK OF GROUND RETURNS AT 60 DEGREES RIGHT OF NOSE ON COUNTER CLOCKWISE SWEEP. SOUNDS LIKE RADAR HITS DOME ON CLOCKWISE SWEEP. FOUND RADAR DRIVE PLATE BINDING AGAINST RADOME STATIC DISCHARGE STRIP PLASTIC NUT PLATES. REPLACED THE RADOME ASSEMBLYSDR ABXA030183Attach Angle · crackedVERTICAL STAB TO FUSELAGE ATTACH ANGLE CRACKED, LEFT SIDE OF VERTICAL AFT END. REPAIRED ANGLE IAW DC-9 SRM 53-05.SDR ABXA030083Sensor · failedAFTER LANDING GEAR RETRACTION, THE NOSE GEAR UNSAFE LIGHT REMAINED ON. AFTER CYCLING GEAR, THE LIGHT REMAINED ON FOR ONE MINUTE, THEN WENT OUT. REMOVED AND REPLACED THE NOSE LANDING GEAR LOCK SENSOR IAW DC-9 MM 32-60-01-2.SDR ABXA020059Fuel Control · malfunctionedNR 1 ENGINE WOULD NOT DECELERATE FROM FULL POWER TO IDLE, WOULD NOT RESPOND AFTER THE THROTTLE WAS RETARDED. IN-FLIGHT SHUTDOWN AND DID AN AIR TURN BACK. REPLACED THE FUEL CONTROL AND MAIN FUEL PUMP IAW DC-9 MM 73-20-01-2.SDR ABXA010567Packing · defectiveRIGHT ENGINE LOST OIL PRESSURE ON CLIMBOUT, FOR DURATION OF 9 MINUTES ENGINE WINDMILLED. OIL PRESSURE DECREASED AS OIL QUANTITY DECREASED. IN FLIGHT SHUT-DOWN. REPLACED THE MAIN OIL FILTER HOUSING CAP O-RING AND INSPECTED THE MAIN OIL FILTER, NO METAL FOUND, ISDR ABXA010521Doubler · corrodedCORROSION SPOTS WERE NOTED BELOW FRAME AT FUSELAGE STATION 617L AND LONGERON 29L. MAINTENANCE REPLACED THE INTERNAL DOUBLER IAW DC-9 SRM 51-30-5 AND 51-30-1.SDR ABXA000490Light · inoperativeOVERHEAD EVACUATION LIGHTS INOPERATIVE. MAINTENANCE INSPECTED AND CLEANED THE EVACUATION LIGHT BATTERY CONTACTS, IAW DC-9 MAINTENANCE MANUAL. OPERATIONAL CHECKED GOOD.SDR ABXA000091Frame · corrodedFUSELAGE FRAME AT STA 1041 CORRODED BETWEN LONGERON 28 LEFT SIDE TO 28 RIGHT SIDE IN AFT BAG BIN. REPAIRED FRAME IAW DC9 SRM 53-03 FIGURE 2A.SDR ABXA000087Pan · crackedLEFT MAIN ENTRY DOOR PAN CRACKED AT TOP HINGE CUT OUT. FABRICATED DOOR REPAIR ANGLE IAW DC9 SRM 52-05 FIGURE 47. INSTALLED DOOR REPAIR ANGLE IAW DC9 SRM 51-30-5 AND 51-30-1 AND 52-05 FIGURE 4.SDR ABXA000086Support · crackedRIGHT WING INBOARD SPOILER OUTBOARD SPOILER SUPPORT CRACKED. REPLACED SUPPORT FITTING IAW DC9 SRM 51-30-1.SDR ABXA000085Bracket · crackedRIGHT WING OUTBOARD SPOILER OUTBOARD SUPPORT CRACKED. REPLACED OUTBOARD SPOILER SUPPORT BRACKET IAW 51-30-2 AND 51-30-5.SDR ABXA000080Pan · crackedFORWARD LOWER CARGO DOOR INNER PAN CRACKED IN TWO AREAS JUST ABOVE BEAM NR 1 FORWARD SIDE OF DOOR. REPAIRED EXTERNAL CRACK IAW DC9 SRM 52-05 PAGE 110A. MATERIAL 2024-T3-.063. EDDY CURRENT INTERNAL MARKED AREA. NO CRACK FOUND.SDR ABXA9801183Battery Pack · dischargedDURING SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPS CHECKED GOOD.SDR ABXA9800639Prox Control · malfunctionAFTER LANDING GEAR RETRACTION, RIGH GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLED GEAR, LIGHT REMAINED ON. REPLACED PROX CONTROL BOX, OPS CHECKED GOOD IAW DC9 MM 32-60-00.SDR ABXA9800568Floorbeam · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND A FLOORBEAM AT FS 718 CRACKED AT RBL 48. REPLACED FLOORBEAM IAW DC9 SRM CHAPTERS 51-30-1, 51-30-2 AND 51-30-5.SDR ABXA9800569Shear Tie · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT ENGINE PYLON SHEAR-TIE CRACKED AT LONGERON 14 LEFT AND FS 1041. REPLACED SHEAR-TIE IAW DOUGLAS DC9 SRM CHAPTERS 53-12-3, 51-30-1, 51-30-2 AND 51-30-5.SDR ABXA9800567Longeron · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND LONGERON 17 LEFT CRACKED AT PYLON ATTACH BOLT AT FS 1041. REPAIRED LONGERON IAW DC9 SRM CHAPTER 53-02.SDR ABXA9800566Longeron · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND LONGERON 17 RIGHT CRACKED AT UPPER FASTENER HOLE ATTACHING IT TO BULKHEAD AT FS 1052. REPLACED LONGERON SECTION IAW DC9 SRM CHAPTER 53-02.SDR ABXA9800565Longeron · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND LONGERON 16 LEFT CRACKED AT PYLON UPPER ATTACH BOLT AT FS 1041. REPAIRED LONGERON IAW DC9 SRM CHAPTER 53-02.SDR ABXA9800570Spar Cap · corrodedWHILE COMPLYING WITH C-INSPECTION, FOUND LEVEL 2 CORROSION ON THE LEFT WING REAR SPAR UPPER T-CAP AT STATION XRS 160. REPAIRED LEFT WING REAR SPAR UPPER CAP IAW ABX REA D957-23974 MR.SDR ABXA9701326Uplatch Assy · out of adjustRIGHT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTED. RECYCLED GEAR, LIGHT REMAINED ON. ADJUSTED DOOR UPLATCH ASSY AND ROLLER. OPS CHECKED GOOD IAW DC9 MM 32-31-4.SDR ABXA9701157Uplimit Switch · worn hardwareRIGHT GEAR UNSAFE LIGHT ILLUMINATED AFTER TAKE OFF AND DURING FLIGHT. GEAR UPLATCH CHECKED GOOD. REPLACED WORN HARDWARE ON RIGHT MAIN LANDING GEAR UP-LIMIT SWITCH. PERFORMED ADJUSTMENT AND TEST IAW DC9 MM 32-60-00. OPS CHECKED GOOD.SDR ABXA9701021Skin · corrodedFOUND LEFT FLAP UPPER AND LOWER SKINS CORRODED. REPLACED SKINS (P/N 9957578-15, 995757-503) IAW DC9 SRM 51-30-1.SDR ABXA9701022Rib · crackedFOUND RIGHT FLAP OUTBOARD HINGE INBOARD AND OUTBOARD RIBS CRACKED. REPLACED FITTINGS (P/N 9957600-7, 9957600-15) IAW DC9 SRM 51-30-2.SDR ABXA9700701Angle · crackedDURING ACCEPTANCE INSPECTION FOUND THE LEFT ENGINE PYLON TO FUSELAGE ATTACH ANGLE CRACKED IN TWO PLACES. REPAIRED LEFT PYLON ATTACH ANGLE IAW ABX REA D954-16868-MR.SDR ABXA9700696Bulkhead Clip · crackedDURING ACCEPTANCE INSPECTION FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER CRACKED AT LONGERON 16L. REMOVED AND REPLACED END CLIPS AT LONGERON 16L IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.SDR ABXA9700711Spar Cap · corrodedDURING ACCEPTANCE INSPECTION, FOUND THE VERTICAL STABILIZER REAR SPAR CAPS CORRODED AT STATIONS ZRS 4, 8 AND 10. REPAIRED VERTICAL STAB REAR SPAR CAPS IAW ABX REA D957-16873-MR.SDR ABXA9700699Angle · crackedDURING ACCEPTANCE INSPECTION, FOUND THE RIGHT ENGINE PYLON UPPER FUSELAGE ATTACH ANGLE CRACKED. REPLACED THE RT UPPER PYLON TO FUSELAGE ATTACH ANGLE IAW DC-9 SRM CHAPTER 51-30-2 AND 51-30-5 AND REPAIRED ONE CRACK IAW ABX REA D954-16695-MR.SDR ABXA9700712Skin · erodedDURING ACCEPTANCE INSPECTION, FOUND THE LEFT HORIZONTAL STABILIZER LEADING EDGE SKINS ERODED. REPAIRED LEFT HORIZONTAL STAB LEADING EDGE SKINS IAW ABX REA D955-16859-MR.SDR ABXA9700700Angle · crackedDURING ACCEPTANCE INSPECTION, FOUND THE RIGHT ENGINE PYLON UPPER FUSELAGE ATTACH ANGLE CRACKED AT FS 1095. REPAIRED THE RIGHT PYLON UPPER ATTACH ANGLE IAW ABX REA NR D954-16695-MR.SDR ABXA9700695Bulkhead Clip · crackedDURING ACCEPTANCE INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER CRACKED AT LONGERON 15L. REPLACED END CLIP AT LONGERON 15L IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.SDR ABXA9700710Keel Beam · corrodedDURING ACCEPTANCE INSPECTION, FOUND THE BUTT LINE O KEEL BEAM UPPER CAP SEVERELY CORRODED AT FS 660. REPAIRED KEEL BEAM UPPER CAP IAW ABX REA D953-16673-MR.SDR ABXA9700713Rib · crackedDURING ACCEPTANCE INSPECTION, FOUND THE OUTBOARD LEFT WING LEADING EDGE RIB AT SLAT TRACK NR 10 CRACKED. REMOVED AND REPLACED LEADING EDGE RIB IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.SDR ABXA9700702Panel · corrodedDURING ACCEPTANCE INSPECTION, FOUND THE RIGHT WING LOWER TRAILING EDGE BONDED PANEL JUST INBOARD OF MLG CORRODED. REPLACED RIGHT WING LOWER INBOARD TRAILING EDGE PANEL IAW DC9 SRM 51-30-1.SDR ABXA9700705Jamb · crackedDURING ACCEPTANCE INSPECTION, FOUND THE RIGHT MLG WHEEL WELL DOOR JAMB CRACKED INBOARD OF HYDRAULIC SUMP JAR. REPAIRED RIGHT MLG DOOR JAMB IAW ABX REA D953-16723.SDR ABXA9700704Panel · delaminatedDURING ACCEPTANCE INSPECTION, FOUND THE RIGHT WING OUTBOARD TRAILING EDGE PANEL FORWARD OF AILERON DELAMINATED AND CORRODED. REPLACED RIGHT WING OUTBOARD TRAILING EDGE PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.SDR ABXA9700703Panel · delaminatedWHILE COMPLYING WITH ACCEPTANCE INSPECTION, FOUND THE RIGHT WING UPPER TRAILING EDGE BONDED PANEL FORWARD OF AILERON DELAMINATED AND CORRODED. REMOVED AND REPLACED RIGHT WING TRAILING EDGE PANEL IAW DC-9 CHAPTERS 51-30-1 AND 51-30-2.SDR ABXA9700884Spoiler · corrodedTHE RIGHT WING OUTBOARD SPOILER HAD SEVERAL AREAS OF CORROSION. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.SDR ABXA9700709Spar Car · corrodedDURING ACCEPTANCE INSPECTION, FOUND THE LEFT WING REAR TEE CAP DOUBLER CORRODED. REPAIRED LEFT WING REAR SPAR CAP IAW ABX REA D957-16504-MR.
Back to N964AX, cancelled Jan 4, 2010