N794AJ
Service difficulty reports · 62
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 = 'N794AJ' AND registry_match = 'registration' 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 = 'N794AJ' AND registry_match = 'registration' 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 FXGA07312024001Hose · leakingON DESCENT "A" SYSTEM HYDRAULIC QUANTITY FLUID STARTED DECREASING. FOUND LEAK FROM HOSE FITTING ON #2 SPOILER ACTUATOR. REPLACED ORING ON FITTINGSDR FXGA202307122336Unknown · unknownDAMAGE TO FLOOR STRUCTURE F/S 1148 BL RIGHT 45 WL 208. REPAIR OF DAMAGE FLOOR STRUCTURE AT F/S1148 BL RIGHT 45 WL 208. FABRICATE REPLACEMENT PARTS AND INSTALL PER SRM.SDR FXGA2022121400512Battery · dischargedCREW RECEIVED A LOWER AFT CARGO FIRE WARNING AT FL360 ON ARRIVAL INTO EFD. CREW IMMEDIATELY INITIATED THE EMERGENCY PROCEDURE AND BEGAN AN EMERGENCY DECENT AND DIVERTED TO CWF, WHICH WAS JUST SOUTH OF POSITION. THE FIRE CREW SWEPT AIRCRAFT UPON LANDING AND NO SDR FXGA20211129001Duct · crackedON CLIMB APPROXIMATELY 1500' #3 ENGINE HAD FIRE WARNING. ACCOMPLISHED CHECKLIST. LIGHT EXTINGUISHED DID NOT FIRE BOTTLE. RETURNED TO KFLL. ON VISUAL INSPECTION OF ENGINE IT WAS FOUND THAT THE BLEED AIR DUCT HAD RUPTURED/CRACKED.SDR FXGA202103182103Stiffener · crackedL/H WING FRONT SPAR VERTICAL STIFFENER CRACKED AT W/STA 255L. TO REPLACE A CRACKED VERTICAL STIFFENER ON THE LEFT WING FRONT SPAR WEB AT W/STA 254. REPLACE VERTICAL STIFFENER PER EA 20-2021-008. OBTAIN DTA WITHIN 12 MONTHS.SDR FXGA202103182110Skin · corrodedCORROSION ON L/H ELEVATOR OUTBOARD TRAILING EDGE. TO REPAIR CORRODED ELEVATOR SKIN AT THE TRAILING EDGE IN THE STATIC WICKS AREA. PERFORM REPAIR OF ELEVATOR TRAILING EDGE PER STS ENGINEERING AUTHORIZATION 80-2021-016 AND 80-2021-015. OBTAIN DTA WITHIN 12 MONTSDR FXGA202103042114Web · damagedDAMAGE WEB AT L/H AILERON TAB HINGE ASSEMBLY. TO PREFORM SPLICE ON A DAMAGED WEB SUPPORTING THE L/H OUTBOARD AILERON TRIM ROD HINGE ASSEMBLY.REMOVE AILERON TRIM ROD HINGE ASSEMBLY. REPAIRE DAMAGE WEB PER B727 SRM 51-40-02 TYPICAL WEB REPAIR. INSTALL AILERON TRSDR FXGA202102022111Skin · delaminatedDELAM ON LH AILERON COMPOSITE TRAILING EDGE. TO REPAIR DELAMINATION ON AILERON TRAILING EDGE. REPAIR AILERON TRAILING EDGE PER B727 SRM 51-40-20 GENERAL REPAIR - ALUMINUM HONEYCOMB REPAIRS - 250 DEGREE FAHRENHEIT (121 DEGREE CELSIUS) CURE.SDR FXGA202102012109Stringer · corrodedCORRODED FUSELAGE STRINGER AT F/STA 443, STRINGER 11R. TO REPAIR A CORRODED FUSELAGE STRINGER AT F/STA 443, 11 RIGHT. CUT OUT DAMAGED AREA AND PERFORM REPAIR PER DC-6A&B OVERHAUL MANUAL FIGURE 12-2.SDR FXGA202101062102Hinge Fitting · corrodedOUTBOARD HINGE FITTING CORRODED FOR L/H WING #2 LEADING EDGE FLAP AT W/STA 269L. TO REMOVE AND REPLACE A CORRODED FITTING ON #2 LEADING EDGE FLAP (W/STA 269L). REMOVED CORRODED FITTING. MANUFACTURE NEW FITTING PER DRAWINGS NUMBER 65-16271 AND BAC1508-128. INSTSDR FXGA202101062101Hinge Fitting · corrodedCORRODED HINGE FITTING FOR L/H WING #1 LEADING EDGE FLAP AT W/STA 283L. TO REMOVE AND REPLACE A CORRODED FITTING ON #1 LEADING EDGE FLAP (W/STA 283L). REMOVE CORRODED FITTING. MANUFACTURE NEW FITTING PER DRAWINGS NUMBER 65-16273 AND BAC 1508-128. INSTALL NEW FSDR FXGA202101062106Stringer Clip · corrodedCORRODED CLIP AT STRINGER 19L, F/STA 1186 BULKHEAD. TO REPLACE A CORRODED CLIP AT FUSELAGE STRINGER 19L, F/STA 1186. REMOVE AND REPLACE CORRODED STRINGER CLIP.SDR FXGA202101062104Stringer Clip · corrodedCORRODED CLIP AT STRINGER 17L, F/STA 1186 BULKHEAD. TO REPLACE A CORRODED CLIP AT FUESLAGE STRINGER 17L, F/STA 1186. REMOVE AND REPLACE CORRODED STRINGER CLIP.SDR FXGA202101062105Stringer Clip · corrodedCORRODED CLIP AT STRINGER 18L, F/STA 1186 BULKHEAD. TO REPLACE A CORRODED CLIP AT FUSELAGE STRINGER 18L, F/STA 1186. REMOVE AND REPLACE CORRODED STRINGER CLIP.SDR FXGA2020011392002Support Bracket · crackedLEFT WING #3 FLIGHT SPOILER ACTUATOR SUPPORT BRACKETS CRACKED, INBRD AND OUTBRD. REPALACED LEFT WING #3 SPOILER ACTUATOR BRACKETS (BOTH). REMOVED AND REPLACE LEFT WING #3 SPOILER ACTUATOR BRACKETS P/N 65-24608-17 OUTBOARD BRACKET, AND P/N 65-24608-19 INBOARDSDR FXGA201906261920Spar · corrodedCORROSION ON AFT WING SPAR LOWER CHORD BETWEEN LBBL 19.2 AND WS 210L. CORROSION WAS FOUND ON THE AFT WING SPAR LOWER CHORD CENTER SECTION AND LT SECTION. SPLICES WILL BE PERFORMED AT LBBL 19.2 ON THE CENTER WING SECTION AND AT WS 210 ON THE LT WING SECTION. SDR FXGA201906181949Mount · corrodedREPLACEMENT OF CORODED #2 ENGINE MOUNT FITTING. TO REPLACE CORRODED AFT ENGINE MOUNT FITTING AND TEE CHORDS AT #2 ENGINE POSITION. REMOVE AND REPLACE #2 ENGINE SUPPORT FITTING P/N 65-18670-1, CHORDS P/N 65-31281-3, 65-31281-4, 65-22913-5, 65-22913-6, AND WEBSDR FXGA201906111946Door Frame · corrodedMAIN CARGO DOOR JAMB INNER SKIN REPLACEMENT. TO REPLACE THE MAIN CARGO DOOR JAMB INNER SKIN (FORWARD LOWER SECTION AT F/STA 520) FOR CORROSION DAMAGE. REMOVE AND REPLACE CORRODED SECTIO OF DOOR JAMB PER B727 SRM 51-30-2.SDR FXGA201905241945Spar · damagedCENTER WING SPAR TEMPORARY REPAIR FOR FERRY FLIGHT. TEMPORARY REPAIR FOR DAMAGE TO CENTER WING AFT SPAR LOWER CAP FOR FERRY FLIGHT TO INSTALL PERMANENT REPAIR. 727-227 LEFT HAND WING REPAIR TEMPORARY. S/N 21243.SDR FXGA201905231944Skin · corrodedFUESLEAGE SKIN REPLACEMENT BETWEEN F/STA 259.5 AND 360 STRINGER 19L AND 26L. TO REPLACE A CORRODED SKIN BETWEEN F/STA 259.5 AND 360, FROM STRINGER 20L AND 25L. REMOVE AND REPLACE CORRODED SKIN PER SRM.SDR FXGA2019040941932Stringer · corrodedCORRODED FUSELAGE LONGERON #27R F/STA 950. TO REPAIR A CORRODED STRINGER. REMOVE CORROSION AND INSTALL REPAIR PER B727 SRM 51-40-4.SDR FXGA201903081922Beam · corrodedCORROSION ON LT HORIZONTAL STABILIZER LOWER TRAILING EDGE BEAM. TO REPAIR A CORRODED HORIZONTAL STABILIZER TRAILING EDGE BEAM. CUT DAMAGED BEAM AT STA 78.29 AND SPLICE IN NEW OUTBOARD SECTION PER SRM 55-10-6 FIGURE 1 HORIZONTAL STABILIZER T.E. BEAM REPAIR.SDR FXGA201903081923Beam · corrodedCORROSION ON LT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM. TO REPAIR A CORRODED HORIZONTAL STABILIZER TRAILING EDGE BEAM. CUT DAMAGED BEAM AT STA 82.5 AND SPLICE IN NEW OUTBOARD SECTION PER SRM 55-10-6 FIGURE 1 HORIZONTAL STABILIZER T.E. BEAM REPAIR.SDR FXGA201903081924Beam · corrodedCORROSION ON RT HORIZONTAL STABILIZER LOWER TRAILING EDGE BEAM. TO REPAIR A CORRODED HORIZONTAL STABILIZER TRAILING EDGE BEAM. CUT DAMAGED BEAM AT STA 88.29 AND SPLICE IN NEW OUTBOARD SECTION PER SRM 55-10-6 FIGURE 1 HORIZONTAL STABILIZER T.E. BEAM REPAIR.SDR FXGA201903081925Beam · corrodedCORROSION ON RT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM. TO REPAIR A CORRODED HORIZONTAL STABILIZER TRAILING EDGE BEAM. REMOVE AND REPLACE CORRODED BEAM WITH NEW PER SRM 51-30-2 FASTENER REMOVAL AND INSTALLATION.SDR FXGA201902081912Crossbeam · crackedCRACK ON CROSS BEAM STA 856-850 @ LBL 45.50. TO REPAIR A CRACKED WEB ON A FLOOR CROSS BEAM. THE CRACK IS LOCATED BETWEEN F/SAT 850 AND 856 AT LBL 45.50. PERFORM REPAIR OF CRACKED WEB PER REPAIR DRAWING #E2499-001. DTA MUST BE OBTAINED WITHIN 12 MONTHS.SDR FXGA201902041918Skin · corrodedCORROSION AT RT WING ILLUMINATION LIGHT. TO REPAIR A CORRODED SKIN BETWEEN F/STA 720B AND 720C AND LONGERON S-14R AND S-16R. REPAIR CORRODED SKIN PER SRM 53-30-3 FIGURE 22. SEE PAGE 2 FOR RE-INSPECTION REQUIREMENTS.SDR FXGA201901081901Floorbeam · corrodedCORROSION ON O/B END STA 880 FLOORBEAM LOWER CHORD @ RBL 68. CORROSION ON OUTBOARD END OF STA 880 FLOORBEAM LOWER CHORD AT RBL 68. CUT OUT AND REMOVE DAMAGE, REPAIR PER SRM 53-10-08 FIGURE 8. RE-INSPECTION REQUIREMENTS: HFEC REQUIRED. INITIAL: 55,000 CYCLESSDR FXGA20160226001Controller · failedAIRCRAFT DEPRESSURIZED IN THE MIDDLE OF A PARABOLA. DESCENT WAS INITIATED AT FIRST INDICATION OF DEPRESSURIZATION. MAXIMUM ALTITUDE REACHED WAS FLIGHT LEVEL 310. FOUND THAT THE CABIN PRESS CONTROLLER HAD FAILED.SDR FXGA20151026001Wire Harness · brokenDURING CRUISE FLIGHT NR 3 ENG FIRE INDICATION. PROCEDURE & CHECKLIST INITIATED. BOTH ENG FIRE BOTTLE DEPLOYED. FIRE INDICATION REMAINED ON. ALL ENG PARAMETERS NORMAL EXCEPT ENG OIL TEMP AT RED LINE. ENG FIRE INDICATION REMAINED ON UP TO SECURING AIRPLANE SDR PCSA2013120501Warning Light · illuminatedDURING CLIMB OUT, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED CHECKLIST & RETURNED TO KTIX.SDR PCSA2012060501Engine · power lossDURING CLIMBOUT THE NR 2 ENGINE LOSS POWER.SDR PCSA2011072201Hydraulic Line · rupturedCLIMBING THROUGH 12000FT B-SYSTEM 2 PUMP LOW PRESS LIGHT FLICKERED FOLLOWED BY A-SYSTEM FLUID DECREASING TO 2.5 GALLONS AND B-SYSTEM FLUID DECREASING TO 0. APPROPRIATE CHECKLIST INITIATED AND RETURNED TO BASE WITHOUT INCIDENT. AN EMERGENCY WAS NOT DECLARED. SDR PCSA2011060901Regulator Valve · leakingDURING PARABOLA NUMBER 2 STRONG SMELL IN FLIGHT DECK AND CABIN AFTER NUMBER 5. COULD NOT IDENTIFY AND RETURNED TO BASE. MAINTENANCE FOUND THE SMELL TO BE SKYDROL FROM THE HYDRAULIC RESERVOIR PRESSURE REGULATOR LEAKING INTO THE PRESSURIZING LINE. THE LINES WSDR PCS2008F00000Compressor · failedDURING CLIMB BETWEEN 180 TO 210 FLIGHT LEVEL NR 1 ENG COMPRESSOR STALL FOLLOWED BY OIL TEMP RISE. AFTER SECOND COMPRESSOR STALL NR 1 ENG OIL PRESS LIGHT ILLUMINATED. ENG WAS SHUT DOWN PER AOM. NR 1 ENG OPERATED APPROX 9 MINUTES OIL PRESS ABOUT 20 PSI. POSTSDR PCSA9210601Detection Sys · false indicationFLIGHT 819 DEPARTED FROM MIA, WHILE IN CRUISE AT THE ASSIGNED ALTITUDE (ONE HOUR OUT ) THE CREW REPORTED THE NUMBER 3 STRUT OVERHEAT LIGHT ILLUMINATED, THE CREW PERFORMED THE ABNORMAL PROCEDURES, THE NUMBER 3 STRUT OVERHEAT LIGHT WENT OUT. THE AIRCRAFT RETURNSDR PCSA8180601Actuator · bypassingFLIGHT 8413 DEPARTED MIA WHILE IN THE CLIMB THE CREW REPORTED THE LEFT HAND MAIN LANDING GEAR DOOR WARNING LIGHT CAME ON AFTER THE LANDING GEAR SELECTOR HANDLE WAS MOVED FROM THE GEAR UP POSITION TO THE OFF POSITION. THE AIRCRAFT RETURNED BACK TO MIA AND LANDSDR PCSA0526051Pcu · malfunctionedON TAXI OUT CONTROL YOKE JAMMED WILL NOT MOVE FWD. AC RETURNED TO RAMP. AIRCRAFT WAS FERRIED BACK TO MIAMI. NO DEFECTS REPORTED ON FLIGHT. REMOVED FLOOR PANEL, INSPECTED CONTROL CABLES EBL, EAL, EBR, EAR & PULLEYS BS 540, 740, 870, 950 & 1050 NO DEFECTS. SDR 2004F00304Chip Detector · missingEN ROUTE TO MEXICO, THE NR 2 OIL QUANTITY DECREASED TO ZERO FOLLOWED BY A DROP IN OIL PRESSURE. PRECAUTIONARY SHUT DOWN NR 2 ENGINE. AIRCRAFT DIVERTED BACK TO MMMD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED NR 2 ENGINE AND FOUND NR 4 BEARINGSDR 2004F00243Engine · malfunctionedFLT 813 - KMIA-TBPB - AFTER DEPARTURE FORM KMIA, NR 3 OIL PRESSURE INDICATED ABOVE ARC LINE, AND THEN OIL TEMP BEGAN CLIMBING AND WENT ABOVE ARC LINE. SHUT OFF NR 3 ENGINE AS PER PROCEDURES. AIRCRAFT DIVERTED BACK TO KMIA AND LANDED WITHOUT FURTHER INCIDENT.SDR 2003F00555Fuel Control · contaminatedAFTER DEPARTURE FROM KMIA, NR 1 ENGINE RPM BEGAN TO INCREASE AND DECREASE DURING CLIMB OUT. AIRCRAFT DIVERTED BACK TO KMIA AND LANDED WITHOUT FURTHER INCIDENT. MAITNENANCE INSPECTED NR 1 ENGINE INLET AND EXHAUST IAW CHAPTER 71-00. NO DAMAGE FOUND, INSPECTEDSDR 2003F00298Blade · damagedIN FLIGHT NR 3 ENGINE COMPRESSOR STALLED TWICE AND HAD HIGH EGT INDICATION. ENGINE NR 3 WAS SHUTDOWN IN FLIGHT AND FLIGHT CONTINUED TO KMIA WITHOUT FURTHER INCIDENT. MIA MAINTENANCE INSPECTED ENGINE NR 3 AND FOUND THE C-9 THROUGH C-13 BLADES DAMAGED. ENGNE SDR 2003F00316Oil Cap · looseFLT 835 - KMIA/UVF - CAPTAIN REPORTED, NR 2 ENGINE OIL QUANTITY INDICATED 1.5 WHILE INFLIGHT. LOW OIL QUANTITY LIGHT DID NOT ILLUMINATE. AIRCRAFT DIVERTED TO SJU AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR 2 ENGINE OIL CAP NOT SECURED. ENGINESDR COOSDR02201Door Frame · crackedLEFT MAIN LANDING GEAR, WING DOOR AFT FRAME CRACKED.SDR COOSDR020198Floorbeam · corrodedMAIN CARGO CABIN BS 1130 LOWER CHORD CORRODED.SDR COOSDR020192Structure · delaminatedRIGHT WING OUTBOARD FORE FLAP (PN 65-21631-274) (SN BN386) UPPER SKIN AND HONEYCOMB CORE DELAMINATED SECTION.SDR COOSDR020191Structure · delaminatedLEFT WING INBOARD FORE FLAP (PN 652130-188) (SN BN720) UPPER, LOWER SKIN AND HONEYCOMB CORE DELAMINATED SECTION.SDR COOSDR020190Access Panel · delaminatedAIR CONDITION BAY ACCESS PANEL (PN 65-58513-12) INNER SKIN DELAMINATED.SDR COOSDR020189Structure · corrodedRIGHT WING INBOARD AFT FLAP (PN 65-21634-80) (SN BN375) UPPER, LOWER SKIN AND HONEYCOMB CORE CORRODED.SDR COOSDR0220188Skin · delaminatedLEFT WING OUTBOARD AFT FLAP (PN 65-21635-85) (SN BN486) UPPER AND LOWER SKIN DELAMINATED.
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