N795AX, cancelled Apr 9, 2024
Service difficulty reports · 120
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 = 'N795AX' AND deregistration_id = 'N795AX-2024-04-09' 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 = 'N795AX' AND deregistration_id = 'N795AX-2024-04-09' 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 ABXA202210132110Fmc · malfunctionedAFTER LEFT ENG START, LEFT FMC WENT FULL BRIGHT WHICH CAUSED AND OVERLAY OF LINES. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED THE LEFT CDU IAW MEL 34-61-1-1A. MAINTENANCE PROCEDURES COMPLIED WITH. PLACARD INSTALLED. AIRCRAFT RETUSDR ABXA2022082283Outflow Valve · faultedLOSS OF ALL CABIN PRESSURIZATION CONTROL @ FL 360 MX PAGE SHOWED AUTO 1/AUTO2 INOP. HI FLOW /EICAS SHOWED CABIN ALT MASTER WARNING CABIN AUTO INOP MASTER CAUTION. CREW ELECTED TO AIR TURNBACK TO DEN, MAINTENANCE GROUNDED AIRCRAFT. MAINYENANCE T/S PER 767FIM 21SDR ABXA2022080591Warning Message · false activationAFTER START R HD DEMAND PUMP EICAS MSG. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OPS CK OF RH ACMP & RH ENG DRIVEN HYD PUMPS WITH & WITH-OUT ENG RUNNING IAW B767 AMM 29-11-00. ALL OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR 2022FA0000302None · noneL GEN DRIVE , L GEN "OFF" EICAS MESSAGE. AIRCRAFT BTB AND GROUNDED BY MAINTENANCE. PERFORMED BPCU BITE IAW B767 FIM 24-20 FAULT TREE 01 AND TASK 24-20 804. RECONNECTED IDG AND RAN ENG. COULD NOT DUPLICATE NO FAULTS FOUND. PLACARD REMOVED. MX PROC C/W. AIRCRAFTSDR ABXA2022022528Duct · crackedLEFT PACK WILL NOT HOLD CABIN ALTITUDE BELOW 10000'. AT FL 340, CABIN ALTITUDE ALARM SOUNDED. CABIN RETURNED TO AN ALTITUDE BELOW 10000' AT FLT 280. CREW ELECTED TO DO AN AIR TURNBACK. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS GROUNDED BY MAINTENASDR ABXA2022012818Not Reported · not reportedR PACK TEMP" ICAS MESSAGE AFTER BLOCK OUT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. BITE R PACK CONTROL PANEL CONTROL PANEL, NO FAULT SHOW ON CURRENT OR PREVIOUS FAULTS, RUN R PACK ONE HOUR ALL TEMP ARE NORMAL. OPS CHECKED GOOD IAW B767 MM 21-51-00.SDR ABXA2022012700615Pump · intermittentL HYD PRIM PUMP EICAS MSG" EICAS MESSAGE AND LEFT ENGINE DRIVEN PRIMARY PUMP "PRESS LIGHT ILLUMINATED. AICRAFT RETURNED TO BLOCK AND GROUNDED BY MAINTENANCE.REMOVED AND REPLACED #1 ENGINE EDP IAW AMM CHP 29 -11-05. LEAK CHECK GOOD. PERF - PWR CHK AT L ENG HYD SDR ABXA2022010602Relay · stickingL AOA PROB EICAS MESSAGE ON ENGINE START. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE R/R RELAYS AT POS. K400 AND K644 I/A/W B767 WDM, CH.30-32-11. PERFORMED TEST OF AOA PROBE HEAT I/A/W B767 AMM, CH. 30-32-00. OPS CHECK GOOD.AIRCRAFT RETURNSDR ABXA20211119121Cable · bindingLT ENG COMPRESSOR STALL (MODERATE) ALL ENG INDICATIONS NORMAL IN CLIMB THROUGH 35000'. FLIGHT CREW ELECTED TO DIVERT TO CVG. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE FOUND VSV CABLE BINDING.REMOVED OLD, THEN INSTALLED NEW L/H ENGINE VSV CABLE PER AMM SDR ABXA20211011099Transmitter · faultyAFTER TAKEOFF DURING CLIMB THE FOLLOWING LIGHTS ILLUMINATED; AMBER TE FLAP DISAGREE EICAS AMBER TRAILING EDGE DISCREET LIGHT PERFORMED NON-NORMAL PROCEDURE FOR TE FLAP DISAGREE AND LANDED BACK IN KILN WITH FLAPS 20 THE LIGHTS BEGAN ILLUMINATING WHILE FLAPS RSDR ABXA202193087Transmitter · faultedDURING CONTROL CHECK, RIGHT ELEVATOR FAILED TO MOVE FROM NEUTRAL POSITION. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE VERIFIED MOVEMENT OF RH ELEVATOR AND POSITION TRANSMITTER WAS AT FAULT.R/H POSITION INDICATOR DEFERRED IAW MEL 27-08-1. ASDR ABXA202108053070Control Valve · intermittentCABIN ALT & CABIN ALTITUDE LIGHTS ILLUMINATED. EICAS MESSAGE CABIN ALTITUDE WAS DISPLAYED. UNABLE TO RESTORE CABIN PRESS. USING MANUAL MODE. DESCENDED TO FL 280 LIGHT WENT OUT. OXYGEN WAS USED. AICRAFT CONTINUED TO SCHEDULED ARRIVAL AIPORT. AIRCRAFT WAS GROUNSDR ABXA2021710065Start Valve · faultedDURING L ENG START, L ENG STARTER EICAS MSG. NO N2 ROTATION. AIRCRAFT RETURNED TO BLOCK AND GROUNDED BY MAINTENANCE. REMOVED AND REPLACED #1 ENG. START VALVE IAW B767 AMM 80-11-02. AIRCRAFT RELEASED FOR FLIGHTSDR ABXA2021619058Unknown · unknownUPON ENTERING RUNWAY MAKING LEFT TURN NWS MAKING GRINDING SOUNDS AND BURNING RUBBER SMELLED. AIRCRAFT BTB. MAINTENANCE GROUNDED AIRCRAFT.INSPECTED NOSE WHEEL STEERING SYSTEM. NO FAULTS NOTED. GREASED STEERING ACTUATORS AND TORQUE LINKS IAW AMM 32-51-00. AIRCRASDR ABXA2021528054Shutoff Valve · leakingTHE CENTER HYDRAULIC QUANTITY EICAS MESSAGE DISPLAYED INDICATION. AN IN FLIGHT EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY WITH NO OTHER PROBLEMS. AIRCRAFT WAS THEN GROUNDED BY MAINTENANCE. A HYDRAULIC LEAK WAS FOUND ON THE CENTER FLAP/SLAT SHUT OFF VALSDR ABXA2021425028Warning Light · illuminatedL PACK TEMP EICAS MESSAGE ON TAXI OUT. ACCOMPLISHED QRH PROCEDURE. AFTER 5 MINUTES IN STBY N PACK INOP LIGHT REMAINED ILLUMINATED. AIRCRAFT BACK TO BLOCK. AIRCRAFT GROUNDED BY MAINTENANCE. LEFT PACK DEFERRED. AIRCRAFT RELEASED FOR FLIGHT.SDR ABXA2021331020Door · unlatchedAFTER TAKE OFF, MX CARGO DOOR LIGHT ILLUMINATED.AIRCRAFT DECLARED AN EMERGENCY AND RETURNED TO ORIGIN. AIRCRAFT WAS GROUNDED BY MAINTENANCE. FOUND THE MCD DOOR DOOR NOT LATCHED LIGHT ON. OPERATED THE UNLOCK SWITCH UP, UNLOCKED DOOR AND POSITIONED THE CLOSED SWSDR ABXA2021228017Pca · leakingL HYD QTY LOW EICAS MSG,FLIGHT CREW DECLARED AN EMERGENCY AND EXECUTED AN AIR TURN BACK AND LANDED UNEVENTFULLY. MAINTENANCE DETERMINED #1 SPOILER WAS LEAKING HYDRAULIC FLUID AND AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED #1 SPOILER PCA OPS CHECK/RIG CHECK GOSDR ABXA2021223016Fseu · faultedTE FLAPS DISAGREE CAUTION MESSAGE RAN THE QRH IN-FLIGHT. TRAILING EDGE DISCREET LIGHT. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED BY MAINTENANCE. BITE TESTED FSEU AS PER FIM 27-51 FT 809. EXTRACTED FAULT MSG NO. 27-51102 " L FLAP.STAB POS" PERFOSDR ABXA20200803215Autothrottle Sys · malfunctionedON PUSH, AUTOTHROTTLES WENT INOPERABLE FOLLOWED BY LOSS OF THRUST SETTINGS BEING DELETED. WILL NOT TAKE ANY THRUST SETTINGS. AIRCRAFT BACK TO BLOCK. AIRCRAFT GROUNDED. ACCOMPLISHED OPERATIONS CHECK OF TMS DISPLAY AND TMC, REF AMM 22-31-01, C/W MCDP TESTS 0SDR ABXA20200803210Line · leakingON TAXI OUT, LT HYDRAULIC SYSTEM LOW QTY EICAS MESSAGE IN VIEW STATUS PAGE SHOWS ZERO QTY. AICRAFT BACK TO BLOCK AND GROUNDED. UPON INSPECTION FOUND LEAKING RETURN LINE FROM EDP IN THE LT PYLON. REMOVED LINE, REPAIRED HYD LINE WITH RYNGLOK, REF B767 MM 20-1SDR ABXA202009038169Seat Track · corrodedCORROSION WAS FOUND ON THE INBOARD FLANGE OF AFT LOWER CARGO COMPARTMENT SEAT TRACK (P/N: 96FS667842-107) AT STA 1307, RBL 15.01. THE DAMAGE WAS REMOVED BY BLENDING. ORIGINAL FLANGE THICKNESS IS .080 AND MINIMUM REMAINING THICKNESS IN THE BLENDED AREA IS .03SDR ABXA20200903 172Panel · gougedGOUGE DAMAGE WAS FOUND ON THE STRUT SKIN PANEL (P/N 311T1400-21) OF THE LT PYLON. THE GOUGE WAS REMOVED BY BLENDING, PER 767-200 SRM 51-10-02 EXCEEDING SRM LIMITS. ALL FASTENERS COMMON TO REWORKED AREAS, AS REQUIRED, WERE REMOVED AND HFEC OPEN-HOLE AND SURFASDR ABXA202009038173Support Fitting · corrodedDURING AIRCRAFT C-CHECK AT TAMPA, AIRBORNE MAINTENANCE WAS REQUIRED TO INSPECT THE NR 8 FLAP SUPPORT 1-3 BEAM ASSEMBLY PER ABX WORK CARD ABX-57-796-28-02. INSPECTION REVEALED CORROSION WITHIN A HOLE LOCATION. THE SUBJECT HOLE WAS REWORKED TO A CLEAN AND ROUNSDR ABXA20200803171Door Sill · corrodedDURING AIRCRAFT CURRENT CHECK AT AIRBORNE (TPA), CORROSION WAS FOUND ON THE AFT LOWER CARGO DOOR CUTOUT LOWER SILL FAIL SAFE STRAP (P/N 146T8048-3), BETWEEN STA 1241 AND STA 1263 AT STRINGER S-33R. THE CORROSION WAS REMOVED AND EVALUATED PER 767-200 53-00-15 SDR ABXA202009038170Skin · corrodedWHILE PERFORMING THE SCRIBE LINE INSPECTION, PER ABX TASK CARD ABX-SCL-5330-0016-23145 REFERENCE AD 2010-06-16 AND BOEING SB 767-53A0193, CORROSION WAS FOUND ON THE FUSELAGE SKIN (P/N 146T3330-41 ASSY) IN ZONE A AT STRINGER S-17L BETWEEN STA 1395 AND STA 1417.SDR ABXA2020062419070Warning Message · illuminatedL ENG STARTER EICAS MESSAGE ILLUMINATED DURING ENGINE START. AIRCRAFT WAS GROUNDED.SDR ABXA20200603065Valve · malfunctionedLEFT BLEED AIR ISOLATION VALVE LIGHT STAYS ON. AIRCRAFT WAS GROUNDED.SDR ABXA202004051051Escape Reel · deployedINERTIAL ESCAPE REELS DEPLOYED. AIRCRAFT GROUNDED.SDR ABXA20180828096Engine · making metalON CLIMB OUT AT APPROXIMATELY FLIGHT LEVEL 190, THE CREW HEARD A BOOM AND SMELLED A STRONG SMOKE ODOR. AT THE SAME TIME, THE AIRPLANE YAWED AND SHUTTERED. THE RIGHT ENGINE HAD HIGH EGT (1100 DEG) AND N2 INDICATION (113.1). THE RIGHT ENGINE WAS SHUT DOWN AND THSDR ABXA20180705075Stringer · corrodedCORROSION ON THE UPPER NR 8 STRINGER COMMON TO THE UPPER SURFACE OF THE LOWER HORIZONTAL FLANGE JUST OUTBOARD OF RIB 2 (LBL 41.5 - RSS 0.00) OF THE LEFT HORIZONTAL STABILIZER. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA20180705074Keelbeam · corrodedCORROSION ON KEEL BEAM LOWER INBOARD FLANGE AT BODY STATION 955 TO 1009. THE KEEL BEAM FLANGE WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA20180705073Structure · corrodedCORROSION ON OUTBOARD LONGERON CHORD AT BODY STATION 1047 TO 1051 IN THE LEFT WHEEL WELL. THE CHORD WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA20170830096Carabiner · missingTHREE EMERGENCY DESCENT SAFETY HARNESS CARABINERS WERE MISSING FROM THEIR STOWAGE POUCH. WHILE THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED), THREE NEW SAFETY HARNESS CARABINERS WERE INSTALLED INTO THE STOWAGE POUCH. THE CAUSE OF THE MISSING CARABINERS IS USDR ABXA20170603070Container · unsecureON CLOSING THE L1 DOOR, TWO DESCENT DEVICES FELL OUT OF THE DESCENT DEVICE CONTAINER AND THEY UNWOUND TO THE FLOOR. WHILE THE AIRPLANE WAS GROUNDED, THE DESCENT DEVICES WERE REPLACED WITH SERVICEABLE DESCENT DEVICES. THE CAUSE FOR THE DESCENT DEVICES DROPPING SDR ABXA20170225012Escape Rope · defectiveWHILE THE AIRPLANE WAS REMOVED FROM SERVICE, TWO DESCENT DEVICES WERE FOUND PARTIALLY UNWOUND. THE DESCENT DEVICES WERE REPLACED. THE CAUSE FOR THE DESCENT DEVICES BECOMING UNWOUND IS UNKNOWN.SDR ABXA20160830139Socket · inoperativeEXTERIOR EMERGENCY LIGHTING SYSTEM INOPERATIVE. THE LAMP WAS REPLACED IN THE EMERGENCY LIGHT LAMPHOLDER ASSEMBLY. THE CAUSE OF THE INOPERATIVE LIGHT WAS A FAILED LAMP.SDR ABXA20160830138Battery Pack · dischargedINTERIOR EMERGENCY LIGHTING SYSTEM INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK WAS REPLACED. THE CAUSE OF THE INOPERATIVE LIGHTS WAS A DISCHARGED BATTERY.SDR ABXA20160613098Beam · corrodedLEFT WING, T/E, STA WS 370, OTBD OF AFT CORNER OF PANEL 551XBX, FWD OF FLAP TRANSMISSION, MAJOR CORROSION. R & R BEAM, CHORD LT WING T/E STA WS 370 IAW SRM 51-40-02. CORRODED LEVEL 2, PN 113T1407-5, SPOILERS BEAM CHORD, EXACT FS/BS LOCATION ON ACFT FROM STR,SDR ABXA20160609100Stringer · crackedAFT SIDE STA 676, STR 8L CRACKED IN RADIUS IN UPPER HAT FLANGE APPROXIMATELY 2" FROM FORWARD END. STR 8L AT STA 676 IAW ENGINEERING SKETCH ES 02821. CRACKED 2.0", PN 143T3001-6, STR 8L, LOCATION AT STA TO 709, STR LOCATION S8L. ACFT WAS GROUNDED.SDR ABXA20160608099Attach Angle · corrodedCORRODED LOWER T/E PANEL ATTACH ANGLE AT WS 364 AFT OF PANEL 651XBX. BLENDED AREA WITH THICKNESS OF .110" REMAINS .076" OUT OF LIMITS IAW SRM 57-51-02. R & R LOWER T/E PANEL ATTACH ANGLE AT WS 364 IAW SRM 51-40-02, SEC 9. CORRODED, PN 113T1407-6, SPOILER BESDR ABXA20160607096Stringer · corrodedHORIZONTAL STABILIZER BOX STR S-1U AFT HORIZONTAL LEG AT ATTACH POINT TO OTBD SIDE OF RIB 2R IS CORRODED, BLOWN OUT. REPAIRED STR 1 UPPER IN THE RT HORIZONTAL STABILIZER IAW REA B655-62090-MR. CORRODED LEVEL 2, PN: 182T3101-6, STRINGER, EXACT FS/BS LOCATION SDR ABXA20160606097Stringer · corrodedHORIZONTAL STABILIZER BOX STR S-5L FORWARD VERTICAL LEG AT ATTACH POINT TO INBD SIDE OF RIB 2L IS CORRODED, BLOWN OUT. REPAIRED STRINGER 5 LOWER IN THE HORIZONTAL STABILIZER CENTER BOX IAW REA B655-62086-MR. 181T4100-5, STR, CORRODED: LEVEL 2, EXACT FS/BS LOSDR ABXA20160603101Stringer · crackedAFT SIDE STA 676, STR 11L CRACKED APPROXIMATELY 1.5" AROUND FORWARD HI-LOCK IN LOWER HAT FLANGE. REPAIRED STR 11L IAW SRM 53-0-03 AND ES 02821. CRACKED 1.5", PN 143T3001-7, STR 11L, EXACT FS/BS LOCATION ON AC FROM S11L, STA 676. ACFT WAS GROUNDED.SDR ABXA20160602095Splice Plate · corrodedLEFT WING L/E LOWER SPLICE PLATE IS CORRODED AT STA 627. REMOVED CORROSION IAW SRM 57-41-01 ON LOWER SPLICE PLATE AT STA 627 AND FOUND TO BE OUT OF LIMITS. REPAIRED ON REA NR B657-62081. CORRODED, LEVEL 2, PN 114T0222-9, PART NAME: SPLICE PLATE, EXACT STR/WSDR ABXA20160601102Structure · crackedINNER CHORD AT STA 883.5, RBL89 HAS CRACK INDICATION. REPAIR COMPLETED ON EA 53000050-101. CRACKED, PN 145T1004-2, INNER CHORD, EXACT FS/BS LOCATION ON ACFT AT STA 883.5, EXACT STR, WS LOCATION ON ACFT AT RBL 89. ACFT WAS GROUNDED.SDR ABXA20140925311Channel · damagedWING TE PANEL ATTACH CHANNEL LOWER CHORD SPLIT ON EDGE AT WS 424.22 INCHES FROM REAR SPAR. INSTALLED NEW CHORD IAW REA B657-61210-MR & SRM 51-40-02. PANEL 552JB INSTALLED IAW SRM 51-40-02. SDR INFO PN 113T1407-1, PART NAME SPOILER BEAM CHORD, L2 CORROSION, SDR ABXA20140924315Bushing · wornLEFT WING NR 2 FLAP HINGE 9 - 10 BEAM HAS LOOSE BUSHINGS IN CTR OF THE BEAM. REPLACED BUSHINGS IAW REA C027-61235-MR. PN 113T1347-7, PART NAME BUSHING, WORN & LOOSE BUSHING, EXACT FS & BS LOCATION ON ACFT LT WING, EXACT WS LOCATION ON ACFT WS 616. ACFT WAS SDR ABXA20140924314Bearing · wornRIGHT FLAP HINGE POINT 9 - 10 BEAM HAS A LOOSE BEARING & A LOOSE BUSHING. R & R BEARING ON 9 - 10 BEAM AT FLAP SUPPORT NR 7 IAW CMM 27-51-97. THE 9 - 10 BEAM WILL BE INSTALLED ON NR 0037, SEE REACO27-61234-MR. PN 60B00180-236, PART NAME BEARING, WORN & LOOSSDR ABXA201409243008Keelbeam · corrodedCORROSION FOUND BETWEEN STATION 999 & 1021 IN LT WW CTR BEAM. REMOVED CORROSION IAW SRM 53-50-12 & COMPLIED WITH REA NR B653-61251-MR. CORRODED L2, PN 145T8612-1, PART NAME KEEL WEB, SN N/A, LOCATION STATION 999 LBL TO 1021 LBL. ACFT WAS GNDED.
Back to N795AX, cancelled Apr 9, 2024