N519AS
Service difficulty reports · 485
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 = 'N519AS' 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 = 'N519AS' 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 ASAA2015081012826Warning Message · false activationDISCOVERED FMC DISAGREE ON GROUND AFTER 2ND ENGINE START, ACFT GROUNDED. ACCOMP QRH CHECKLIST NORMAL, OPS RESTORED.SDR ASAA2015080912810Converter · malfunctionedAPU CSS ATTEMPT TEMP EXCEEDED 980F, SHUTDOWN AND FAULT LIGHT ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED APU BITE CHECK, FOUND FAULT CODE 49-31016 OVERTEMP SHUT DOWN ON CURRENT STATUS. CHECKED OTHER OCCURENCES AND FOUND CODE 49-31016 LOGGED ON 1, 10, AND 11. SDR ASAA2015080712783Warning Light · illuminatedCSS APU INCOMPLETE. ATTEMPTED FL380/FL310, FAULT LIGHT ILLUMINATED-AUTO SHUTDOWN. START AFTER LANDING SUCCESSFUL. ACFT GROUNDED. BITE CHECKED APU-NO FAULTS. ACCOMPLISHED NORMAL APU START. CONTINUE MEL 49-99A.SDR ASAA2015080412732Fuel Divider · faultedDURING FIRST ATTEMPTED APU START FOR A CSS, APU EGT APPROACHED 1000". WE WERE LEVEL AT FL 380 AND HAD BEEN AT CRUISE ALTITUDE FOR APPROXIMATELY 3.5 HRS. FAULT LIGHT ILLUMINATED AND APU SHUTDOWN, FAILED TO START, NO SUBSEQUENT STARTS WERE ATTEMPTED. ACFT GROSDR ASAA2015080212684Seal · failedAPU CSS START FAULT LIGHT CAME ON. COOLED DOWN WITHIN 5 MINUTES. SECOND ATTEMPT SUCCESSFUL AT 35000. ACFT GROUNDED. REMOVED APU, REPLACED AIR INLET SIGMA SEAL IAW MM 49-15-11-400-801, 41581, INSTALLED, LEAK/OPS CHECKED APU.SDR ASAA2015073112665Oil System · lowAPU FAILED TO START DURING CSS TEST ON FIRST ATTEMPT AT FL 380 AMBER "FAULT" LIGHT ILLUMINATED QRH FOLLOWED. ACFT GROUNDED. BITE CHECK FOUND APU OIL LOW, SERVICED OIL. OPS CK NORMAL, NO CURRENT FAULTS FOUND.SDR ASAA2015072812619Satcom · malfunctionedWHEN USING SATCOM 1, TRANSMISSION FROM AIRPLANE TO GROUND WORKS AS ADVERTISED BY PRESSING ACP SATCOM 1 PUSH BUTTON, BUT NEITHER PILOT CAN HEAR ON SATCOM 1 UNLESS SATCOM 2 VOLUME IS SELECTED AND TURNED UP. WHEN USING SATCOM 2 GROUND RECEIVER OVER TRANSMISSION SDR ASAA2015072612596Fuel Control · unknownAPU FAULT LIGHT ILLUMINATED ON 1ST APU START ATTEMPT OF CSS AT FLIGHT LEVEL 360. SECOND ATTEMPT DESCENDING THROUGH 35,000' WAS SUCCESSFUL. ACFT GROUNDED. TECH SERVICES REQUESTS FUEL CONTROL CHANGE ON APU. REPLACED APU FUEL CONTROL IAW AMM 49-31-11. PERFORMESDR ASAA2015072212551Sensor · malfunctionedFAULT LIGHT ILLUMINATED DURING 1ST APU START ATTEMPT AT FL 380. REATTEMPTED START AT FL 330 WAS SUCCESSFUL WITH NO FAULT LIGHT. ACFT GROUNDED. REPLACED APU INLET PRESSURE SENSOR IAW AMM 49-52-31 AND REPLACED APU INLET TEMPERATURE SENSOR IAW AMM 49-61-31. BOSDR ASAA2015071312418Apu · faultedAPU "FAULT LIGHT" ILLUMINATED DURING 1ST CSS START ATTEMPT AT FL 360. ACFT GROUNDED. ACCOMPLISHED APU BITE TEST REF 49-60, TASK 801 FOUND FAULT CODE 49-31016 LOGGED. ACCOMPLISHED FIM TASK 49-30, TASK 803, FOUND CURRENT STATUS CLEAR OF FAULT. INTERMITTENT FAULSDR ASAA2015071012392Fault Light · false activationDURING TAXI IN, TRIED TO START APU AND RECEIVED A FAULT LIGHT. ACFT GROUNDED. PERFORMED FIM TASK 49-60, TASK 802. FOUND CURRENT STATUS CLEARED, INTERMITTENT FAULT CORRECTED.SDR ASAA2015062312200Warning Message · false activationFMC DISAGREE LIGHT ILLUMINATED ON GROUND. ACFT GROUNDED. QRH PROCEDURE APPLIED. NORMAL OPERATIONS RESTORED.SDR ASAA2015061112080Pressure Switch · failedAFTER LANDING, NR 2 FUEL FILTER BYPASS LIGHT ILLUMINATED. LIGHT WENT OUT AFTER ENGINE SHUTDOWN. ACFT GROUNDED. PERFORMED FIM 73-05 TASK 801. FOUND FAULT 73-31072. REPLACED NR 2 ENGINE FUEL FILTER IAW AMM 73-11-02. NO CONTAMINATION FOUND DURING REPLACEMESDR ASAA2015060812030Fuel Feed · faultedDURING ACCOMPLISHMENT OF T/C 78273000, LONG TIME FAULT MSG 73-31072, FUEL FLOW SIGNALS DISAGREE. NR 2 ENGINE LEG 2. ACFT GROUNDED. ON DEFERRAL.SDR ASAA2015050911810Floor Support · corrodedAFT CARGO COMPARTMENT, RT FLOOR SUPPORT INTERCOSTAL FS 747-767 IS CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2, 10 PERCENT THICKNESS MAX ORIGINAL MATERIAL THICKNESS IS 0.032 IN REMOVED 0.005 IN REMAINING TSDR ASAA2015050911797Channel · crackedAFT CARGO COMPARTMENT, RT SIDEPLATE CHANNEL IS CRACKED AT APPROXIMATELY FS 727C+10. ACFT GROUNDED. ACCOMPLISHED SPLICE REPAIR TO RT SIDEPLATE CHANNEL, APPROXIMATELY FS 727B+10 TO FS 727D+10 IAW SRM 53-00-53-2R-5.SDR ASAA2015050811855Floor Panel · corrodedAFT CARGO FLOOR PANEL CORRODED LT SIDE FROM FS 727D TO FS 727. ACFT GROUNDED. R & R FLOOR PANEL STA 727-727D 140AF /IAW AMM 25-52-10 AND SRM 51-10-02, PARA 9. REMOVED DOT O0170. NO CORROSION FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-1 MAX ALLOWABLESDR ASAA2015050811854Floor Panel · corrodedAFT CARGO FLOOR PANEL CORRODED LT SIDE FROM FS 727I TO FS 727D. ACFT GROUNDED. R & R FLOOR PANEL FS 727D-727I, 140EF IAW AMM 25-52-10 AND SRM 51-10-02, PARA 9. REMOVED DOT O170. CORROSION FOUND BEYOND ALLOWABLE LIMITS IAW ASA 737-800 SRM 53-00-53-1A-1 , MAXSDR ASAA2015050811853Floor Panel · corrodedAFT CARGO FLOOR PANEL CORRODED LT SIDE FROM FS 767 TO FS 847. ACFT GROUNDED. R & R FLOOR PANEL STA 767-847, 140CF IAW AMM 25-52-10 AND SRM 51-10-02, PARA 9, REMOVED DOT O169. CORROSION FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-1, MAX ALLOWABLE DAMAGSDR ASAA2015050811809Channel · corrodedAFT CARGO LT TRANSITION PANEL HAS NUMERUS AREAS OF CORROSION FROM FS 727 TO FS 847. ACFT GROUNDED. REMOVED CORROSION AND FOUND WITHIN ALLOWABLE LIMITS OF 10 PERCENT MAX IAW SRM 53-00-1AZ FS 727 TO FS 727B+8, 727E+10 TO 755 AND 779 TO 847, ORIGINAL MATERIAL TSDR ASAA2015050811808Floorbeam · corrodedAFT CARGO FLOOR STRAP CORRODED AT BS 767. ACFT GROUNDED. R & R AFT CARGO FLOOR STRAP AT BS 772 IAW AMM 25-52-10. REMOVED DOT. CORROSION FOUND BEYOND ALLOWABLE LIMITS OF 10 PERCENT THICKNESS MAX IAW SRM 53-00-53-1A-1. ORIGINAL THICKNESS IS 0.010 IN, REMOVEDSDR ASAA2015050811807Frame · corrodedAFT CARGO RT FRAME CORRODED AT TRANSITION PANEL AT FS 727D. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS DUE TO BLENDOUT COMMON TO FASTENER HOLES IAW SRM 53-00-07-1A-1, FIG 102, DETAIL C. ORIGINAL MATERIAL THICKNESS IS 0.063 IN, REMOVEDSDR ASAA2015050711795Skin · crackedCRACK FOUND ON RT HORIZONTAL STABILIZER LWR SKIN JUST INBD OF STABILIZER STA 101.9 APPROX 20" FWD OF REAR SPAR. CRACK IS APPROX 1" LONG, ENDS ARE MARKED AND CRACK IS CIRCLED. ACFT GROUNDED. REMOVED DAMAGE AND INSTALLED FILLER & DOUBLER REPAIR ON RT HORIZONTALSDR ASAA2015050711702Floor Support · scratchedFLOOR SUPPORT BS 887, LBL 49, SCRATCHED ON UPPER SURFACE. ACFT GROUNDED. BLENDED OUT SCRATCH ON UPPER FLOOR SUPPORT AT BS 887, LBL49 FOUND TO BE IN LIMITS IAW SRM 51-10-02 & DWG 147A5690, ALODINED & PRIMED IAW SRM 51-20-01, BLEND OUT IAW AMM 51-02-01.SDR ASAA2015050711698Intercostal · crackedMAIN CABIN BS 344-360, LBL 11 INTERCOSTAL IS CRACKED AT FASTENER HOLE. ACFT GROUNDED. R & R THE INTERCOSTAL IAW SRM 51-40-02 AND DWG 141A5400.SDR ASAA2015050611643Floorbeam · crackedMAIN CABIN UNDER FLOOR AT BS 540 FLOOR SUPPORT INTERCOSTAL CRACKED, RBL 1.5, DOT ATTACHED. ACFT GROUNDED. REMOVED FLOORBOARD IAW AMM 53-21-00. REMOVED DAMAGED SUPPORT IAW SRM 51-40-02. LOCATED, DRILLED AND DEBURRED NEW SUPPORT IAW SRM 51-40-05 AND BAC DWG 1SDR ASAA2015050611642Intercostal · crackedMAIN CABIN UNDER FLOOR AT BS 540 FLOOR SUPPORT INTERCOSTAL CRACKED, LBL 1.5. ACFT GROUNDED. REMOVED FLOORBOARD IAW AMM 53-21-00. REMOVED DAMAGED SUPPORT IAW SRM 51-40-02. LOCATED, DRILLED AND DEBURRED NEW SUPPORT IAW SRM 51-40-05 AND BAC DWG 143A5240. INSTSDR ASAA2015050411857Attach Bracket · gougedE & E BAY DOOR CUTOUT AFT SIDE DOOR STOP ATTACH BRACKET IS GOUGED. ACFT GROUNDED. R & R E & E COMPARTMENT CUTOUT AFT FRAME LATCH FITTING IAW SRM 51-10-02, PARA 9, SRM 51-40-02, AND EA 800-53EA-15120, REV NEW, REF CARD G502608, FRAME OVERSIZED HOLES. REMOVED SDR ASAA2015050311597Idg · lowTECH SERVICE REQUEST. REPLACE NR 2 ENGINE IDG DUE TO FREQUENT OIL SERVICING. ACFT GROUNDED. REPLACED NR 2 IDG IAW AMM 24-11-11-000-801, FIG 401 AND AMM 24-11-11-400-801. OP CK & LK CK GOOD IAW AMM 24-11-00-700-803 SERVICING CK GOOD.SDR ASAA2015042711539Satcom · lockedSATCOM LOCKUP. ACFT GROUNDED. RESET IAW QRH PROCEDURE.SDR ASAA2015042611483Idg · unknownNR 2 IDG REQUIRES FREQUENT SERVICING. ACFT GROUNDED. NR 2 IDG OIL LEVEL AT ADD LINE. PERFORMED LEAK CHECK IAW MM 24-11-00-700-801. NO LEAKS NOTED. PRESSURE REMAINED AT 25 PSI FOR 10+ MINUTES. R & R NR 2 IDG SCAVENGE AND CHARGE FILTERS AND O-RINGS IAW MM 24-SDR ASAA2015042011435Warning Light · false activationNR 2 PACK LIGHT ILLUMINATED ON RECALL. RESETS WITH MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED BITE CHECK OF PACK/TEMP CONTROLLER NR 2. FOUND TCV FAULT ON FIRST CHECK. NO FAULTS SECOND CHECK.SDR ASAA2015040711245Vent · unknownFOLLOW-UP TO NR 2 IDG CONTINUED FREQUENT OIL SERVICING. ACFT GROUNDED. RAN NR 2 END AT IDLE FOR 10 MIN THEN CHECKED FOR OIL ACCUMULATION FROM DRAIN, NO OIL LEAKS OR ACCUMULATION NOTED. R & R THE VENT VALVE IAW AMM 24-11-00-700-804, AS REQUESTED.SDR ASAA2015040311226Wire Harness · failedNR 2 ENGINE "B" LOOP INOPERATIVE. ACFT GROUNDED. FOUND NR 2 ENGINE "B" LOOP DETECTOR, RT SIDE CORE, OPEN. REPLACED RT SIDE CORE LOOP FIRE DETECTOR IAW AMM 26-11-01-401. ENGINE FIRE OPS TEST GOOD IAW AMM 26-11-00-710-801.SDR ASAA2015032411102Warning Light · false activationLEFT PACK LIGHT COMES ON AT RECALL, GOES OUT ON MASTER CAUTION RESET. ACFT GROUNDED. NR 1 CONT. BITE SHOWED RAM AIR ACTUATOR FAULT, RESET FAULT. SECOND BITE, NO FAULTS, REF FIM 21-62-00-810-801. GROUND VERIFICATION SUCCESSFUL REF MM 21-61-00. NO HISTORY 30SDR ASAA2015031510966Valve · malfunctionedRIGHT PACK LIGHT ILLUMINATED DURING RECALL AND RESETS. ACFT GROUNDED. FOUND TEMPERATURE CONTROL VALVE FAILED BITE CHECK. REPLACED TEMPERATURE CONTROL VALVE ON RT PACK IAW MM 21-51-10.SDR ASAA2015031110922Idg · failedNR 2 ENG IDG DPI FOUND EXTENDED. ACFT GROUNDED. ACCOMP FIM 24-11, TASK 803. ACCOMPLISHED IDG SCAVENGE FILTER & IDG OIL INSP CK IAW IDG SCAVENGE & CHG FILTERS INSP/CK TASK 204-11-41-200-801. FOUND NON-METALLIC PARTICLES WITHIN SCAVENGE & CHG FILTERS REF TASK SDR ASAA2015022410762Sign · dislodgedF/A REPORTS - MID-CABIN, "EXIT" SIGN IS DISLODGED FROM MOUNTING BRACKET. ACFT GROUNDED. RESECURED THE EMERGENCY SIGN AS REQUIRED. OK TO CONTINUE. NON ASA 3436144.SDR ASAA2015021010612Idg · failedAFTER STARTING THE NR 2 ENGINE, THE NR 2 ELECTRIC GENERATOR WOULD NOT COME ON. ZERO FREQS, ZERO VOLTS. ACFT GROUNDED. R & R NR 2 ENGINE IDG ASSY IAW MM 24-11-11-400-801. OPS AND LEAK CHECKED NORMAL.SDR ASAA2015012010324Satcom · malfunctionedDURING POWER TRANSFER FROM GATE/GROUND POWER TO APU SATCOM LOCKOUT. ACFT GROUNDED. PERFORMED QRH PROCEDURE. SATCOM REGAINED.SDR ASAA2015011010205Seal · damagedNR 1 ENG FAN OUTLET GUIDE VANES INNER SEALS TORN, MATERIAL MISSING 2 EA AT 10 O'CLOCK POSITION, MARKED. ACFT GROUNDED. R & R SEALS FOR 31 ENG FAN OUTLET GUIDE VANES 72-23-01-400-801-100.SDR ASAA2015011010204Panel · crackedNR 1 ENGINE FAN DUCT PANEL CRACKED AT FASTENER HOLE NR 6 PANEL. ACFT GROUNDED. R & R 1 ENG FAN DUCT PANEL 72-2302-400-801-100.SDR ASAA2015010910184Valve · failedAFT CABIN ZONE TEMP LIGHT ILLUMINATED. ACFT GROUNDED. PERFORMED BITE TEST OF PACK ZONE TEMP CONTROLLERS IAW AMM. NR 1 CONTROLLER FAULTS ZONE TEMP CONTROL VALVE FOR AFT CABIN. R & R AFT CABIN ZONE TRIM AIR MODULATING VALVE IAW AMM 21-61-21. OPS CHECKED NOSDR ASAA2015010710174Power Supply · failedDURING ACCOMPLISHEMENT OF TC 78233001 EMERGENCY LIGHT BATTERY PACK FAILED TIME CHECK. ACFT GROUNDED. REMOVED BATTERY PACK POWER SUPPLY AT POSITION M1673 IAW 33-51-06-960-806. INSTALLED BATTERY PACK POWER SUPPLY IAW SAME MM. OPS CHECKED IAW T/C 78233001. OPSDR ASAA2014122410051Indicator · failedREFUELING CTR QTY GAUGE INOPERATIVE. ACFT GROUNDED. VERIFIED, TAPPING ON FACE OF GAUGE GOES ON & OFF. R & R CTR REFUEL GAUGE REF MM 28-41-61 4, C/B OPEN & CLOSED, OPS NORMAL.SDR ASAA2014121609948Shutoff Valve · failedDURING TAKEOFF, DUCT SPLIT NOTED PALT N1, N2 LT DUCT, RT DUCT SAT 2000 88.9 95.1 43-26 +5 302 KTS, 10000 91.4 96.1 45-27-0 M.79, 25000 96.4 97.3 45 30 -31 M.77, 37000 88.8 90.8 45-33-62. ACFT GROUNDED. PERFORMED NR 2 ENGINE BLEED AIR SYS HEALTH CHECK IAW T/C SDR ASAA2014120509867Warning Light · false activationRIGHT PACK LIGHT ON. LIGHT GOES OUT ON PUSH TO RESET MASTER CAUTION. ACFT GROUNDED. ACCOMPLISHED FIM TASK 21-53 TASK 810. NO FAULTS NOTED.SDR ASAA2014112009721Warning Message · false activationAFTER ENGINE START AND SUBSEQUENT POWER CHANGE, FMC DISAGREE. ACFT GROUNDED. PERFORMED FMC DISAGREE PROCEDURE QRH 11.2. DUAL FMC OPERATION FULLY RESTORED.SDR ASAA2014111209647Warning Light · false activationPACK LIGHT ILLUMINATES ON RECALL, GOES OUT WITH MASTER CAUTION RESET. ACFT GROUNDED PERFORMED PACK/ZONE TEMP FIM 21-62 TASK 848, NR 2 PACK LIGHT RESET, NO HISTORY 30 DAYS.SDR ASAA2014111009630Satcom · malfunctionedSATCOM INOPERATIVE. SATCOM PROMPT DOES NOT APPEAR ON FMC. ACFT GROUNDED. REBOOTED SATCOM - BITE OK.
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