N714AX, cancelled Mar 12, 2025
Service difficulty reports · 61
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 = 'N714AX' AND deregistration_id = 'N714AX-2025-03-12' 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 = 'N714AX' AND deregistration_id = 'N714AX-2025-03-12' 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 IXXA20230313022Unknown · unknownPRE-FLIGHT CREW REPORTED L1 ENTRY DOOR CAME OFF TRACKS. ADJUSTED L1 ENTRY DOOR INTO CORRECT POSITION OF TRACK IAW B767 AMM 52-11-00.SDR IXXA20230221017None · noneCENTER HYDRAULIC PRESSURE EICAS ON APPROACH. QUANTITY IN CENTER REACHED 0.08. ALTERNATE FLAP AND GEAR EXTENSION ENGAGED. HYDRAULIC QTY WAS FULL AT TOP OF DESCENT AND EMPTY WHEN FLAPS 5 SELECTED. DUE TO IRREGULAR OPERATIONS CREW ELECTED AN EMERGENCY DESCENT. LSDR IXXA20230211016Flashlight · inoperativeFOUND COCKPIT EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW B767 AMM 25-05-03. OPERATIONAL CHECK GOOD.SDR IXXA20221101143Pump · damagedDESCENT THRU FL190, OIL PSI RT ENGINE DECREASING. ENG NEAR IDLE & SHUTDOWN BEFORE OIL WENT TO 0. SINGLE ENG APPR & LDG PROCEDURES COMPLIED WITH. DECLARED EMERGENCY. OIL PSI AT 6 PSI AT SHUTDOWN & #2 ENG WINDMILLED APROX 7 MIN. LANDING UNEVENTFUL. ACFT RFSDR IXXA2022050501Vent · crackedCORE COWL VENT CRACKEDSDR IXXA2022050408Thrust Reverser · chafed#2 ENGINE OUTBD THRUST REVERSER HAS A GOUGE AT THE 12 O'CLOCK POSITIONSDR IXXA202205040008Support Angle · cracked#6 SLAT LOWER EDGE HAS A CRACKED SUPPORT ANGLE. LOCATED BETWEEN THE CENTER AND THE OUTBD AUX TRACKSDR IXXA2022050407Thrust Reverser · gougedTHRUST REVERSER HAS GOUGE ON INTERNAL FAIRINGSDR IXXA2022050406Cowl Latch · wornCORE COWL AFT LATCH HAS WEARSDR IXXA2022050405Thrust Reverser · bentTHRUST REVERSER TRAILING EDGE BENTSDR IXXA2022050403Bracket · crackedBRACKET CRACKED ON SKIRT FAIRINGSDR IXXA2022050402Thrust Reverser · crackedTHRUST REVERSER TRAILING EDGE CRACKEDSDR IXXA2022050304Sleeve · deteriorated#1 ENGINE EXHAUST SLEEVE LEADING EDGE WEAR COATING CHIPPED AND DETERIORATED.SDR IXXA2022050303Sleeve · worn#1 ENGINE EXHAUST SLEEVE HAS A HOLE WORN ON THE LEADING EDGE AT 7 O'CLOCK POSITIONSDR IXXA2022050302Cowling · chafedLOWER CLOSE OUT CHANNEL CHAFED IN MULTI AREAS WHERE STOP PADS MATE UP ON #1 ENGINE O/B CORE COWL LOWER ENDSDR IXXA2022050301None · cracked#1 ENGINE I/B CORE COWL UPPER LOUVER EXHAUST ON AFT FLANGE CRACKEDSDR IXXA2022043001Torque Tube · corrodedRH FLAP IB TORQUE TUBE PITTEDSDR IXXA20220427002Panel · corrodedALC PANEL SUPPORT ON BILGE PANEL RBL16 AT STATION 1281 CORRODEDSDR IXXA2022042201Floor Panel · crackedFLOOR PANEL 122C CRACKEDSDR IXXA2022041502Seal Bracket · crackedFAN COWL SEAL RETAINER BRACKET CRACKEDSDR IXXA202204290002Beam · corrodedR/W TRAILING EDGE FLAP #8 SUPPORT 1-2-3 BEAM HAS TWO FASTENERS COMMON TO THE SIDE BRACE ATTACH FITTING WITH DEFECT INDICATION WITH HFEC HOLE SCANSDR IXXA2022050502Support Bracket · corrodedL/H BILGE PANEL SUPPORT BRACKET (L-2) AT STA 1270 CORRODEDSDR IXXA2022050305Torque Tube · wornL/H I/B FLAP #4 TORQUE TUBE FOUND PITTED AND WORN BEYOND LIMITSSDR IXXA2022042801Torque Tube · wornRH I/B FLAP TORQUE TUBE REQUIRES REMOVAL FOR INSPECTION IAW J/C ATI-57-793-12-02 #5 TORQUE TUBE FOUND TO BE PITTED AND WORNSDR IXXA2022050201Retainer Seal · crackedI/B FLAP FAIRING 671FB INSIDE O/B SEAL RETAINER CRACKEDSDR IXXA20210522038Battery Pack · inoperativeMULTIPLE EMERGANCY EXIT SIGN LIGHTS INOPERATIVE. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. REMOVED AND REPLACED BATTERY PACK IAW BOEING 767 AMM 33-51-07. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RELEASED TO SERVICE.SDR IXXA20210405014Connector · damagedDURING SERVICE CHECK, FOUND LEFT ENTRY DOOR EXIT SIGN LIGHT NOT ON WITH FLIGHT DECK EMERGENCY LIGHT SWITCH IN THE ON POSITION. TROUBLESHOT IAW B767 IAI WDM 33-51-11 & 33-51-13, IDENTIFIED CRACKED PIN IN FEMALE END CONNECTOR D1084 PIN 2 CAUSING INTERMITTENT FUNSDR IXXA20201202444Warning Message · illuminatedPRE-DEPARTURE: CREW REPORTS L1 DOOR INDICATION AFTER ENGINE START. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE, WORK IN PROGRESS.SDR IXXA20200519010Mount Bracket · gougedAIRCRAFT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-54-408-00-02 " GVI - EXTERNAL - NO. 2 NACELLE STRUT" LEFT AFT PRECOOLER MOUNT BRACKET CRACKED VIEWED BENEATH #2 LEFT CORE COWL. REMOVED AND REPLACED LEFT AFT PRECOOLER MOUNT BRACKET IAW B767 SRM SDR ABXR2020050600026Bracket · crackedL/H AFT PRECOOLER MOUNT BRACKET CRACKED VIEWED BENEATH #2 L/H CORE COWL. REMOVED AND REPLACED L/H AFT PRECOOLER MOUNT BRACKET IAW B767 SRM 51-40-02 PARA 9 AND IAW 47404FAB04.SDR ABXR2020050600027Tee Fitting · corrodedCORROSION ON INTERIOR "T" SECTION OF ALC DOOR 10" FROM AFT EDGE, 24" FROM TOP EDGE.REMOVED AND REPLACED INTERIOR "T" SECTION OF ALC 3RD FROM TOP USING 140T2604-3 IAW BOEING DWG# 140T2604.SDR IXXA20200519015Floor Support · corrodedAIRCRAFT GROUNDED FOR CHECK-C24. IN COMPLIANCE OF TASK CARD ATI-53-572-00-01 "GVI - INTERNAL - BULK CARGO COMPARTMENT BULK FLOOR SUPPORT" F.S. 1417 HAS CORROSION ALONG LENGTH OF THE SUPPORT TOP SIDE. REMOVED AND INSTALLED "Z" BEAM IAW BOEING DWG 452T3260 REV ESDR IXXA20200519012Skin · corrodedAIRCRAFT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-20-073-00-01, ALC DOOR HAS LIGHT CORROSION AT INTERIOR PANEL MOUNTING SCREW LOCATIONS. REPLACED SKIN ON ALC DOOR IAW B767 51-40-02 PAR 4 BOEING DWG 140T2640 AND
DOC 47404FAB02.SDR ABXR2020050600028Web · corrodedALC DOOR HAS LIGHT CORROSION AT INTERIOR PANEL MOUNTING SCREW LOCATIONS.REPLACED SKIN ON ALC DOOR IAW B767 51-40-02 PAR 4 BOEING DWG 140T2640 AND DOC 47404FAB02SDR IXXA20200519014Skin · crackedAIRCRAGT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-53-730-00-02 "GVI - EXTERNAL - EXTERIOR SECTION 48 - RIGHT SIDE", THE FOLLOWING FINDINGS WERE NOTED: AFT RIGHT EXTERIOR FUSELAGE SKIN IS CRACKED STA 1654.5 BETWEEN STRINGERS 4R-5R. REPAIRED EXTESDR IXXA20200519013Web · brokenAIRCRAFT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-20-105-00-01 "DET - FORWARD NACELLE STRUT FAIRING - NACELLE 2 (EZAP)" THE FOLLOWING FINDINGS WERE NOTED:
NUMBER 2 PYLON - WEB AND BRACKET WHICH THE NOSE COWL ANTI-ICE DUCT ATTACHES TO AT FORWARDSDR ABXR2020050600030Stringer Splice · corrodedSTRINGER SPLICE AT STA. 434 S31R CORRODED.REMOVED AND REPLACED CORRODED SPLICE AT STA 434 S31R IAW B767 SRM 51-40-02.SDR ABXR2020050600029Web · crackedNUMBER 2 PYLON - WEB AND BRACKET THAT NOSE COWL ANTI-ICE DUCT ATTACHES TO AT FORWARD END OF PYLON AT PASS THRU ARE WORN/BROKEN.REPLACE WORE BRACKET IAW B767 SRM 51-40-02, NEW WEB REPLACEMENT DONE ON AMES REA 47404FAB01 ON #2 PYLON FWD END.SDR ABXR2020050600031Skin · crackedAFT R/H EXTERIOR FUSELAGE SKIN IS CRACKED STA 1654.5 BETWEEN STRINGERS 4R-5R. (VERIFIED WITH HFEC SURFACE SCAN).REPAIRED EXTERIOR FUSELAGE SKIN STA 1654.5 S3R-S8R IAW B767 SRM 53-80-01 REPAIR 4.SDR IXXA20200519017Stringer · corrodedAIRCRAFT GROUNDED FOR CHECK-C24. IN COMPLIANCE OF TASK CARD ATI-53-454-00-01, "GVI - INTERNAL - BULK CARGO COMPARTMENT" THE FOLLOWING FINDINGS WERE NOTED: FLC - CORROSION ON STRINGER 32R JUST FORWARD OF STA.434. REPAIRED STRINGER 32R STA. 412-434 IAW B767 SRM SDR IXXA20200519016Stringer · corrodedAIRCRAFT GROUNDED FOR CHECK-C-24.IN COMPLIANCE OF TASK CARD ATI-53-454-00-01,"GVI - INTERNAL - BULK CARGO COMPARTMENT" FLC - CORROSION ON STRINGER 31R AT STA.412. REPAIRED STRINGER 31R STA 412-434 IAW B767 SRM 53-00-03 REPAIR 2.SDR IXXA20200519009Slat · bulgedAIRCRAFT GROUNDED FOR C-CHECK 24. IN COMPLIANCE OF TASK CARD ATI-57-806-00-02, "GVI - ZONAL - INBOARD SLAT NO. 7" THE FOLLOWING FINDINGS WERE NOTED:
7 SLAT - LOWER LEADING EDGE HAS BULGE 93 INCHES FROM OUTBOARD END AND 7 INCHES FROM TRAILING EDGE.SDR ABXR2020050600025Slat · corrodedNUMBER 7 SLAT - LOWER LEADING EDGE HAS BULGE 93 INCHES FROM OUTBOARD END AND 7 INCHES FROM TRAILING EDGE.REPAIRED #7 SLAT LOWER LEADING EDGE IAW REA# 47404REA02SDR IXXA20180515023Failsafe · crackedRIGHT WING FAILSAFE STRAP AT WS 955, REAMED HOLES IAW SRM 51-40-02. LOWER HOLE DAMAGE EXTENDED BEYOND ALLOWABLE LIMITS AND WAS REPAIRED IAW 47317REA01.SDR IXXA20180515022Bulkhead · dentedAFT PRESSURE BULKHEAD WAS FOUND DENTED. REPAIRED THE BULKHEAD IAW REA 47317, REA 05, REV IR.SDR IXXA20180515021Skin · bulgedBULGING FUSELAGE SKIN BS 462, STRINGER 23R. REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-01, REPAIR 1.SDR IXXA20180515020Seat Track · crackedFIRST OFFICER'S RIGHT FORWARD SEAT TRACK WAS CRACKED. REMOVED AND REPLACED THE SEAT TRACK IAW IAW AMM 25-11-01-822-095-001SDR IXXA20180515019Failsafe · crackedLT FAILSAFE STRAP LOWER HOLE COMMON TO THE TEE FITTING CRACKED. THE FAILSAFE WAS REPAIRED.SDR IXXA20170726253Escape Reel · failedEMERGENCY DESCENT DEVICE NUMBER 5 PARTIALLY EXTENDED. REMOVED AND REPLACED THE EMERGENCY DESCENT DEVICE IAW MMS 25-61-03. AIRCRAFT RELEASED TO SERVICE.SDR IXXA20170726252Escape Reel · inoperativeEMERGENCY DESCENT DEVICE NUMBER 7 IN THE SUPERNUMERARY AREA WILL NOT EXTEND. REMOVED AND REPLACED THE EMERGENCY DESCENT DEVICE IAW 25-61-03. ACFT RELEASED TO SERVICE.
Back to N714AX, cancelled Mar 12, 2025