N794AX, cancelled Apr 8, 2024
Service difficulty reports · 93
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 = 'N794AX' AND deregistration_id = 'N794AX-2024-04-08' 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 = 'N794AX' AND deregistration_id = 'N794AX-2024-04-08' 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 ABXA20171127141Sensor · malfunctionedPASSING THROUGH FLIGHT LEVEL 230, THE RIGHT ENGINE EXPERIENCED COMPRESSOR STALLS. THE CREW COULD NOT RESTORE NORMAL ENGINE OPERATION VIA THE QUICK REFERENCE HANDBOOK PROCEDURES. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE RIGHT ENGINE'S MAIN ENGINE CONTROL SDR ABXA20171124140Stator Vane · out of adjustDURING CLIMB THROUGH FLIGHT LEVEL 200, THREE LOUD BANGS OCCURRED THAT JOLTED THE AIRCRAFT. THE AIRPLANE SEEMED TO YAW EACH TIME. NO ABNORMAL ENGINE INDICATIONS WERE OBSERVED. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE LEFT ENGINE'S VARIABLE STATOR VANE SYSTSDR ABXA20171122139Compressor · stalledRIGHT ENGINE HAD A COMPRESSOR STALL. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE FAULT ISOLATION MANUAL DIAGRAM 71-05, FAULT TREE 808 WAS ACCOMPLISHED. ALL FINDINGS WERE WITHIN LIMITS. THE CAUSE OF THE COMPRESSOR STALL IS UNKNOWN.SDR ABXA20171121138Tee Fitting · corrodedCORROSION ON THE ATTACH TEE AT THE REAR SPAR/UPPER RIB INTERSECTION OF THE LEFT HORIZONTAL STABILIZER AT HORIZONTAL STABILIZER BUTT LINE 357.442 LEFT. THE TEE WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20171121137Rib · corrodedCORROSION ON UPPER RIB CHORD OF THE LEFT HORIZONTAL STABILIZER AT HORIZONTAL STABILIZER BUTT LINE 357.442 LEFT. THE CHORD WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20171121135Floorbeam · corrodedCORROSION ON THE FORWARD SIDE OF THE FLOOR BEAM CHORD AT FUSELAGE STATION 1109, LBL 46, IN THE AFT LOWER CARGO COMPARTMENT. THE CHORD WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20171121134Tee Fitting · corrodedCORROSION ON THE LOWER SURFACE OF UPPER CABIN FLOOR SUPPORT TEE FROM FUSELAGE STATION 1541 TO STATION 1562, RBL 80. THE SUPPORT TEE WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20171121133Tee Fitting · corrodedCORROSION ON THE LOWER SURFACE OF UPPER CABIN FLOOR SUPPORT TEE FROM FUSELAGE STATION 1541 TO STATION 1562, LBL 80. THE SUPPORT TEE WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20171121132Stringer · corrodedCORROSION ON STRINGER 32L AT FUSELAGE STATION 434. THE STRINGER WAS REPAIRED. AIRPLANE WAS GROUNDED.SDR ABXA20171121131Rib · corrodedCORROSION IN RIGHT LOWER AIR LOAD RIB. THE RIB WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20171121130Rib · crackedCRACK IN RIGHT WING NOSE RIB. THE RIB WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20171121129Rib · corrodedCORRODED NUT PLATES ON THE RIGHT WING LOWER AIR LOAD RIB. THE RIB WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20171121128Stringer · crackedCRACK IN STRINGER 5L AT SPLICE. THE STRINGER WAS REPAIRED. AIRPLANE WAS GROUNDED.SDR ABXA20171121127Fitting · crackedCRACK IN FRAME TO STRINGER ATTACH CLIP AT STA 1702. THE ATTACH CLIP WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20170830095Carabiner · missingTWO EMERGENCY DESCENT SAFETY HARNESS CARABINERS WERE MISSING FROM THEIR STOWAGE POUCH. WHILE THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED), TWO NEW SAFETY HARNESS CARABINERS WERE INSTALLED INTO THE STOWAGE POUCH. THE CAUSE OF THE MISSING CARABINERS IS UNKNOSDR ABXA20170513063Wire · shortedDURING TAXI, EICAS MESSAGE FOR THE LT REVERSER ISOLATION VALVE DISPLAYED AND THE THRUST REVERSER INDICATION CIRCUIT BREAKER TRIPPED OPEN. THE AIRPLANE WAS REMOVED FROM SERVICE. THE CAUSE OF THE EICAS MESSAGE AND TRIPPED CIRCUIT BREAKER WAS WIRE W756-503-24 WASDR ABXA20160506088Failsafe · crackedLOWER FASTENER HOLE IN RT FAILSAFE COMMON TO T FITTING IS CRACKED, VERIFIED BY HFEC HOLE SCAN. TRIMMED OUT CRACK ON FAILSAFE STRAP COMMON TO T FITTING IAW DOCUMENT 47008ORD04, THAT IS ATTACHED TO JC EA 53500014-003 FOR WORK STEPS TAKEN. CRACKED LENGTH .125",SDR ABXA20160505089Failsafe · crackedLEFT FAILSAFE LOWER HOLE COMMON TO T FITTING HAS CRACK INDICATION, VERIFIED BY HFEC ROTARY HOLE SCAN. TRIMMED OUT CRACK ON FAILSAFE STRAP COMMON TO T FITTING IAW DOCUMENT 47008ORD03, THAT IS ATTACHED TO JC EA 53500013-003 FOR WORK STEPS TAKEN. CRACKED LENGTHSDR ABXA20151209201Fitting · corrodedNUMBER 9, COUNTED FROM FRONT, MAIN DECK CARGO DOOR LATCH CAM PIN FITTING HAS CORROSION IN THE BORE. REMOVED, REPAIRED & RE-INSTALLED NR 9 LATCH PIN & LATCH PIN FITTING IAW REA B652-61882-MR & AMM SUPP 52-32-00. SDR INFO, CORRODED LEVEL 2, PN 368-53-00-95347-SDR ABXA20151208199Skin · corrodedSUSPECTED CORROSION ON RT WING AT REAR SPAR & WS 912. REMOVED PANELS, REMOVED CORROSION & NDT INSPECTED. PERFORMED REPAIR ON REA B657-61824-MR. REINSTALLED PANELS IAW SRM 51-40-02 & REA B657-61824-MR. TOUCH UP PAINT TO BE DONE ON NR 1241. DANGER TAG REMOVSDR ABXA20151208198Skin · corrodedSUSPECTED CORROSION ON RT WING AT REAR SPAR & WS 1025. REPAIRED CORRODED AREA ON RT WING AT REAR SPAR & WS 1030 IAW REA B657-61825-MR. REINSTALLED FIXED PANELS IAW SRM 51-40-02 & REA 657-61825. REPAIR AREA TO BE PAINTED ON NR 1241. FUEL PANEL 652BB TO BE LSDR ABXA20151208196Skin · corrodedLEFT WING SURFACE CORRODED AFT OF OVERWING EXIT AT WING TO BODY FAIRING AT APPROX STATION 938. REMOVED CORROSION & REPAIRED AREA IAW REA B657-61841-MR. SDR INFORMATION, CORRODED LEVEL 2, PN 112T3229-11, SN N/A, PART NAME RIB CHORD, EXACT FS & BS LOCATION ON SDR ABXA20151205204Bulkhead · crackedMID FREQUENCY EDDY CURRENT DEFECT INDICATION 1 EACH FASTENER TS4 & TS5, RS23, INBD OF APU SHROUD. REPAIRED ON REA B653-61835-MR. CRACKED LENGTH .100, PN 148T2610, PART NAME AFT PRESS BULKHEAD, FS & BS LOCATION TS4 - 5, RS23. ACFT WAS GNDED.SDR ABXA20151205203Bulkhead · crackedMID FREQUENT EDDY CURRENT DEFECT INDICATION 1 EACH FASTENER MIDWAY, BETWEEN TS4 & TS5, RS17 INBD ROW. REPAIRED ON REA B653-61835-MR. CRACKED LENGTH .100, PN 148T2610, PART NAME AFT PRESS BULKHEAD, FS & BS LOCATION TS4 - 5, RS17. ACFT WAS GNDED.SDR ABXA20151205202Bulkhead · crackedMID FREQUENCY EDDY CURRENT DEFECT INDICATION 1 EACH FASTENER MIDWAY, BETWEEN TS4 & TS5, RS17 INBD ROW. REPAIRED ON REA B653-61835-MR. CRACKED LENGTH .100, PN 148T2610, PART NAME AFT PRESS BULKHEAD, FS & BS LOCATION TS4 - 5, RS17. ACFT WAS GNDED.SDR ABXA20151203213Structure · crackedLEFT 1809 FWD OUTER CHORD INBD FLANGE AT OTBD FASTENER BELOW SPLICE FITTING CRACKED APPROX 1.5". HFEC VERIFIED IAW NDTM PART 6 51-00-19. REMOVED & REINSTALLED ANGLES & ATTACH BRACKETS TO FACILITATE REPLACEMENT OF LT 1809 OUTER CHORD IAW SRM 51-40-02 PARA 7D SDR ABXA20151203197Skin · corrodedCORROSION SUSPECTED AT LT WING REAR SPAR WS 854. BLEND OUT FOR CORROSION REMOVAL WAS ACCOMPLISHED ON REA 657-61837-MR, WS 810-815. BLEND OUT & TRIM OUT FOR CORROSION REMOVAL WAS ACCOMPLISHED ON REA B657-61838-MR, WS 850 - 859. SDR INFORMATION CORRODED LEVELSDR ABXA20151202215Support Beam · corrodedRIGHT WING TE UPPER PANEL SUPPORT AT WS 1052 IS CORRODED. REMOVED CORRODED PANEL SUPPORT BEAM & INSTALLED NEW FABRICATED BEAM REV NO 61536-0000-0005 & REA NO B657-61840 IAW SRM 51-40-02 GENERAL PG 7 PARA 70. CORRODED LEVEL 2, PN 113T1913024, PART NAME PANEL SDR ABXA20151130214Skin Panel · corrodedRIGHT WING SKIN UPPER TE IS CORRODED UNDER PANEL 113T1651 AT WS 512 - 521. CORROSION UNDER UPPER WING TRAILING EDGE PANEL WAS REPAIRED ON REA B657-61823-M. PANEL WAS REPAIRED ON NR-0468 & REINSTALLED ON NR-0682. CORRODED LEVEL 2, PN 112T3101-6, PART NAME SKSDR ABXA20151127216Support · corrodedRIGHT WING TE OTBD AILERON, HINGE SUPPORT RIB AT WS 1079.95 HAS CORROSION ON THE UPPER CHORD OF THE SUPPORT ASSEMBLY. REMOVED CORRODED CHORD & REPLACED WITH NEW FABRICATED UPPER CHORD REF REA B657-51827, IAW SRM 51-40-02 PG 2 PARA 4B & 51-40-02 PG 7 PARA 7D. SDR ABXA20151125211Stringer · crackedUPPER CARGO STRINGER 19L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE. REPAIRED STRINGER 19L, STATION 698 - 720 IAW ENGINEERING SKETCH NO ESO2821 REV A & 767 - 200 SRM 53-00-03 REPAIR 1 DETAIL II. CRACKED 0.5", SN N/A, PART NAME STRINGER, EXACT FS & BSSDR ABXA20151125194Bracket · crackedNUMBER 6 SLAT LOWER TE ATTACH ANGLE, OUTBOARD OF CTR AUX TRACK, IS CRACKED. R & R ATTACH ANGLE, INSTALLED FASTENERS IAW SRM 51-40-02 PARAGRAPH 7D & 9B. SDR INFORMATION, CRACKED, LENGTH .250, PN 14T3166Y111, SN N/A, PART NAME BRACKET, EXACT FS & BS LOCATION ASDR ABXA20151125193Attach Angle · crackedNUMBER 6 SLAT LOWER TE ATTACH ANGLE, LOCATED OUTBOARD OF OUTBOARD AUX TRACK IS CRACKED. R & R ATTACH ANGLE, INSTALLED FASTENERS IAW SRM 51-40-02 PARAGRAPH 7D & 9B. SDR INFORMATION CRACKED LENGTH .250, PN 114T3166-71, SN N/A, PART NAME ANGLE, EXACT FS & BS LOSDR ABXA20151118210Stringer · crackedUPPER CARGO STRINGER 17L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE. CONTACT ENGINEERING FOR REPAIR. REPAIRED CRACKED LONGERON STRINGER 17L, FS 676 - 708 IAW ENGINEERING SKETCH NR ES02821 REV A & SRM 53-00-03 REPAIR 1. CRACKED 0.5", PN 143T3001, SN SDR ABXA20151118209Stringer · crackedUPPER CARGO STRINGER 7L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE. REPAIRED CRACKED LONGERON STRINGER 7L, FS 676 - 708 IAW ENGINEERING SKETCH NR ES 02821 REV A & SRM 53-00-03 REPAIR 1. CRACKED 0.5", PN 143T3001, PART NAME STRINGER, SN N/A, EXACT FS SDR ABXA20151117205Channel · corrodedWING TE PANEL ATTACH LOWER CHANNEL SPLIT ON EDGE AT TE WS 936. REMOVED DAMAGED CHANNEL, NEW CHANNEL FABRICATED REA B657-61805 & INSTALLED NEW CHANNEL IAW SRM 51-40-02 & REA B657-61805. CORRODED LEVEL 2, PN 113T1912-3, PART NAME CHORD CHANNEL, SN NSN, FS & BSSDR ABXA20151113212Stringer · crackedFORWARD LOWER CARGO STRINGER 21L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE. REPAIRED STRINGER 21L AT FS. 676 - 707 IAW SRM 53-00-03 FIG 201 REPAIR 2 & NEA 53100137-201. PN 143T3001, PART NAME STRINGER, SN NSN, CRACKED 4.75", EXACT FS & BS LOC ON ACFSDR ABXA20151111208Stringer · crackedFORWARD LOWER CARGO STRINGER 21L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE, CONTACT ENGINEERING FOR REPAIR. REPAIRED STRINGER 21L AT FS 676 - 707 IAW SRM 53-00-03 FIG 201 REPAIR 2 & NEA 53100137-201. PN 143T3001, PART NAME STRINGER, SN NSN, CRACKED SDR ABXA20151111206Support · corrodedAT OPENING ABOVE LT LG, AFT WING PANEL ATTACH BEAM CORRODED AROUND NUTPLATE. REMOVED CORRODED PANEL ATTACH BEAM, DRILLED FOR LOCATION & INSTALLED IAW SRM 51-40-05 TABLE 3 & 51-40-02-7. CORRODED LEVEL 2, PN 113T1632-197, SN N/A, PART NAME RIB TE PANEL SUPPORTSDR ABXA20151111195Structure · corrodedHORIZONTAL STABILIZER S10 UPPER AFT FLANGE AT RIB 2R OUTBOARD CORROSION. BLENDED AREA WITHIN LIMITS TO REMOVE CORROSION IAW SRM 51-10-02. SDR INFO, CORRODED LEVEL 2, STRINGER & WS LOCATION, FROM STRINGER 10 TO RIB 2R. ACFT WAS GNDED.SDR ABXA20151110207Beam · crackedNUMBER TWO STRUT INTERIOR STRUCTURE IS CRACKED WHERE PANEL 447ERX ATTACHES AT LOWER EDGE. R & R NR 2 PYLON HYD BAY OTBD BEAM WHERE PANEL 447ERX ATTACHES IAW SRM 51-40-02. CRACKED 1.0", PN 313T1380-242, PART NAME BEAM, AFT FAIRING OTBD, SN NSN, STRINGER & WS SDR ABXA20151103200Keelbeam · corrodedCORROSION FOUND ON LT LOWER KEEL CHORD STATION 952. CLEANED UP CORROSION ON LT LOWER KEEL CORD AT FS 952 IAW SRM 53-50-12 ALLOWABLE DAMAGE 1 FIG 101. CORROSION IS WITHIN ALLOWABLE LIMITS. SDR INFO, CORRODED LEVEL 2, PN 145T8610-5005, PART NAME KEEL CORD, SNSDR ABXA20150201002Switch · out of toleranceMAIN CARGO DOOR LIGHT & SIREN ILLUMINATED DURING CLIMB OUT AT APPROXIMATELY 2.0 TO 2.1 PSID. INDICATION SWITCHES GAP ADJUSTED TO TOLERANCE & E1-1 BURNDY BLOCK CLEANED. WORN DOOR MECHANISM CAUSING SWITCH GAP TO FALL OUT OF TOLERANCE.SDR ABXA2014021423Support · corrodedHINGED PANEL 651TB OTBD LOWER PANEL ATTACH CHANNEL SPLIT ON EDGE. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REMOVED BEAM, REPAIRED IAW REA B657-60865, PN 113T1623-40, SN N/A, PART NAME UPPER SUPPORT, LOCATION RTW WS 358 AFT OF REAR SPAR. ACFT WAS GROUNDEDSDR ABXA2014021422Structure · corrodedTRAILING EDGE PANEL 652HB AFT ATTACH BEAM LOWER CHORD SPLIT ON EDGE. REPLACED LOWER CORD AT PANEL 652HB AFT ATTACH IAW SRM 51-40-02 PER 4 & 7. SDR INFO CORRODED, PN 113T1407-2, SN N/A, PART NAME CHORD LOWER, FUSELAGE & BODY STATION, LOCATION FROM WS 412 TO WSDR ABXA2014021421Beam · corrodedREAR SPAR TO TE PANEL ATTACH BEAM SPLIT ON INBD SIDE LOWER CHORD AT STATION 257, 20 INCHES FROM REAR SPAR. REPLACED REAR SPAR TO TE PANEL ATTACH BEAM IAW SRM 51-40-02. SDR INFO CORRODED, PN 113T1622-9, SN N/A, PART NAME CHORD, BEAM LOWER, STRINGER & WING STASDR ABXA2014021324Skin · corrodedRIGHT WING TRAILING UPPER WING SKIN IS CORRODED 40 INCHES OTBD OF FUSE AT FWD EDGE OF PANEL 651 FT. BLENDED CORROSION AS DESCRIBED IAW SRM 51-20-01, AREA BLENDED IS WITHIN LIMITS IAW ENGINEERING DISPOSITION ON ENTRY NR 8. UPSIZED TWO FASTENER HOLES COMMON TOSDR ABXA2014021225Support Beam · corrodedLEFT WING UPPER SURFACE, BULGE IN PANEL JUST FWD OF NR 5 SPOILER CTR OTBD FITTING. FOUND SPOILER SUPPORT BEAM TO BE CORRODED BEYOND LIMITS. FABRICATED NEW BEAN PN 654T0391-3 IAW REA B657-60857-MR & REPAIRED NEW BEAM IAW REA B657-60862-MR. INSTALLED BEAM IASDR ABXA2014021220Former · crackedRIGHT WING LE NOSE BEAM FORMER IS CRACKED AT THE NR 8 SLAT INBD AUXILIARY TRACK INBD SIDE. REMOVED DAMAGED NOSE FORMER & INSTALLED NON-NOSE FORMER IAW SRM 51-40-02. SDR INFO CRACKED .750 INCHES, PN 114T2200-6, SN NSN, PART NAME FORMER, NOSE BEAM, LOCATION OSSDR ABXA2014021216Angle · corrodedCORROSION FOUND BETWEEN STATION 999 & STATION 1021 IN LT WW BEHIND MAIN GEAR DOOR ACTUATOR ON CTR BEAM. CLEANED LT WW BEHIND MLG DOOR ACTUATOR FS 999 - 1021, FOUND ANGLE PN 145T8601Y37 CORRODED. REPLACED IT WITH A NEW PART IAW SRM 51-40-02 PARA 7. SDR INFO
Back to N794AX, cancelled Apr 8, 2024