N585AS
Service difficulty reports · 564
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 = 'N585AS' 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 = 'N585AS' 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 ASAA2026070167113Latch · damagedR1 DOOR WILL NOT CLOSE AND LATCH PROPERLY THERE IS A GAP IN THE UPPER RIGHT CORNER WHEN DOOR IS LATCHED. GROUNDED - YES. REPLACED THE AFT LATCH RECEIVERS (UPPER AND LOWER), CENTERING GUIDE, CENTERING GUIDE RECEIVER, AND ADJUSTED THE R1 DOOR REF AMM 52-41-00-82SDR ASAA2026012864095Power Supply · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPY M1695 ARE INOPERATIVE. GROUNDED - YES. R & R POWER SUPPLY M1695 IAW AMM 33-51-06-960-806. OPS TESTED GOOD.SDR ASAA2026012864094Power Supply · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY M1694 ARE INOPERATIVE. GROUNDED - YES. R & R THE POWER SUPPLY M1694 IAW AMM 33-51-06-960-806. OPS TESTED GOOD.SDR ASAA2025110962207Cover · detachedOUTBOUND FA'S REPORT EXIT ROW SIGN COVER FOUND. GROUNDED - YES. FOUND OVERHEAD EXIT ROW SIGN LOCATED AT THE OVERWING EXITS AFT LENS REMOVED. REINSTALLED THE OVERHEAD EXIT SIGN AFT LENS IN REF TO AMM 33-51-01. EXIT LIGHTS OPS-CHECK GOOD.SDR ASAA2025072259577Skin · crackedLEFT HORIZONTAL STAB LOWER SKIN IS CRACKED AT STAB STA147.90 MARKED. GROUNDED - YES. PERFORMED SKIN REPAIR ON LEFT HORIZONTAL STAB LOWER SKIN IAW B737-800 SRM 55-10-01-2R-11 REPAIR 11.SDR ASAA2025042857630Sign · detachedCENTER ISLE AFT- "EXIT/SALIDA" SIGN BECAME DETACHED. GROUNDED - YES. SNAPPED LENS BACK INTO POSITION. LENS REMAINS SECURE. REF AMM 33-51-01.SDR ASAA2025041257256Lens · detachedFA REPORTS EMERGENCY EXIT COVER OVER L1 DOOR FELL OFF. GROUNDED - YES. (RESOLVED ON W/O: 2046587 TASKCARD: N/R-00002 ) REMOVED AND REPLACED EXIT SIGN LIGHT ASSEMBLY PER AMM 33-51-01 MX PROC REVERSED SEAMC JOEY NOTIFIED.SDR ASAA2025040657138Lens · missingFA REPORTS 17A EXIT LENS MISSING. GROUNDED - YES. INSTALLED LENS AS REQ.SDR ASAA2024082552040Battery Pack · inoperativeRT FUSELAGE EXTERIOR EMERGENCY LIGHT AFT OF R-1 DOOR INOPS. GROUNDED - YES. REMOVED AND REPLACE DR1 DOOR EMERGENCY LIGHT BATTERY PACK S/N 195197. OP CK GOOD IAW B737-NG AMM 33-51-06-960-805.SDR ASAA2024052149776Lamp · inoperativeR1 EMERGENCY SLIDE LIGHT INOP. GROUNDED - YES. REMOVED AND REPLACED LAMP AT R1 EMERGENCY SLIDE REF AMM 33-51-04. OPS CHECK GOOD.SDR ASAA2024010347139Lens · detachedFLEET SERVICES REPORTED MID CABIN CIELING EXIT LIGHT LENS CAME OFF. GROUNDED - YES. REINSTALLED LENS REF AMM 33-51-01-960-802.LIGHT OPS CHECK GOOD.SDR ASAA2023110646063Generator · damagedDURING TAXI IN, APU AUTO SHUTDOWN AND LOW OIL PRESSURE ANNUNCIATOR LIGHT AND MASTER CAUTION ILLUMINATED. GROUNDED - YES. (RESOLVED ON W/O: 1976115 TASKCARD: N/R-00003 ) ACCOMPLISHING FIM 49-90 TASK 803, OIL PRESSURE SHUTDOWN, FOUND LOW OIL QUANTITY AND SGU CASSDR ASAA2023102445829Unknown · unknown#1 AUTO THROTTLE DID NOT COME UP ON TOGA #2 OPERATES NORMALLY. GROUNDED - YES. (RESOLVED ON W/O: 1975213 TASKCARD: N/R-00001 ) PERFORMED AUTOTHROTTLE BITE NO FAULTS FOUND.PERFORMED SERVOMOTOR TEST.TEST PASSED.NO HISTORY WITHIN LAST 30 DAYS.PERFORMED LAND VERIFSDR ASAA2023081644629Modulating Valve · faultyLEFT PACK LIGHT ON AFTER MASTER CAUTION RECALL ON DESCENT. QRH COMPLETED. GROUNDED - YES. (RESOLVED ON W/O: 1965708 TASKCARD: N/R-00001 ) INIITIAL EVALUATION, LH PACK LT ILLUMINATED AT OVERHEAD ON MASTER RECALL. PERFOMRED PZTC BITE IAW FIM 21-62 TASK 801, BOTHSDR ASAA2023081544627Unknown · unknownLEFT PACK LIGHT ON WHEN MASTER CAUTION PUSHED, OFF WHEN RESET. GROUNDED - YES. ACCOMLIHSED FIM TASK 21-53 TASK 821. PERFORMED PACK/ZONE TEMP CONTROLLER #1 BITE PER MM 21-30-00-700-806. NO FAULTS NOTED RAN PACKS FOR 10 MINUTES AND REACCOMPLISHED PACK/ZONE TEMP SDR ASAA2023080744456Actuator · malfunctionedRIGHT PACK LIGHT ILLUMINATES ON RECALL. PACK LIGHT EXTINGUISHES ON RESET. GROUNDED - YES. REF LOG PAGE 60443445 AFTER FURTHER TROUBLESHOOTING REPLACED MEL 21-32B WITH MEL 21-5C. PLACARDS REMOVED. SEAMC CARL NOTIFIED.LP 60443445: REMOVED AND REPLACED R/H RAM SDR ASAA2023073144322Unknown · unknownDURING TAKEOFF ROLL AUTOTHROTTLE DISENGAGED. GROUNDED - YES. (RESOLVED ON W/O: 1963823 TASKCARD: N/R-00002 ) FFR LOGGED 22-31687.ASM 1 RATE MONITOR.RESET ASM'S.OP CK NORMAL.REF FIM 22-32 TASK 819.CLEARS MEL 22-4B & 22-99B,SDR ASAA2023072544298Unknown · unknown#1 ENG FIRE DETECT LOOP A FAILED TEST DURING PREFLIGHT. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023071344009Unknown · unknownAT CRUISE BOTH LNAV / VNAV DISCONNECTED AND WAS FOLLOWED BY AN AMBER VTK FLAG ON THE CAPTAINS DISPLAY AS WELL AS BOTH CDU'S WENT TO MENU MODE AFTER APPROXIMATELY 20 SECONDS EVERYTHING SELF CORRECTED AND ALL WAS NORMAL. GROUNDED - YES. ACC FIM TASK 34-61-TASK 8SDR ASAA2023071244008Lens · missingTHE FLIGHT ATTENDANT REPORTS THE CENTER CEILING EXIT SIGN IS MISSING OVER ROW 16. GROUNDED - YES. INSTALLED NEW CENTER CEILING EXIT LENS COVER AFT SIDE OF CENTER EXIT SIGN. OPS NORMAL.SDR ASAA2023070743936Unknown · unknownEMERGENCY EXIT LIGH NEAR L1 DOOR IS INOP. GROUNDED - YES. PERFORMED GOOD EMERGENCY LIGHTS OPS CHECK IAW B737 AMM 33-51-00-720-801. NO DEFECT NOTED.SDR ASAA2023070243891Power Supply · inoperativeEMERGENCY LIGHT SYSTEM POWER SUPPLY (M2335) OPERATIONAL TEST FAILED. GROUNDED - YES. REMOVED, REPLACED AND OPERATIONAL TESTED EMERGENCY LIGHT SYSTEM POWER SUPPLY M2335 B737-800 AMM 33-51-06-960-806, OPS TEST GOOD.SDR ASAA2023070243890Power Supply · inoperativeEMERGENCY LIGHT SYSTEM POWER SUPPLY (M1676) OPERATIONAL TEST FAILED. GROUNDED - YES. REMOVED, REPLACED AND OPERATIONAL TESTED EMERGENCY LIGHT SYSTEM POWER SUPPLY M1676 B737-800 AMM 33-51-06-960-806, OPS TEST GOOD.SDR ASAA2023070243889Power Supply · inoperativeEMERGENCY LIGHT SYSTEM POWER SUPPLY (M1670) OPERATIONAL TEST FAILED. GROUNDED - YES. REMOVED, REPLACED AND OPERATIONAL TESTED EMERGENCY LIGHT SYSTEM POWER SUPPLY M1670 B737-800 AMM 33-51-06-960-806, OPS TEST GOOD.SDR ASAA2023062043751Skin · corrodedCRACK FOUND ON THE LOWER SKIN OF THE LEFT-HAND HORIZONTAL STABILIZER AFT OF THE FWD SPAR, INBOARD OF STAB STA 138.70. APPROX 1 INCH LONG, BOTH ENDS MARKED. GROUNDED - YES. REPAIRED THE CRACK FOUND ON THE LOWER SKIN OF THE L/H HORIZ STAB I/B OF STAB STA 138.70 SDR ASAA2023062043732Skin · crackedCRACK FOUND LEFT HAND HORIZONTAL STABILIZER LOWER SKIN FWD OF REAR SPAR INBOARD OF STAB STA 129.50. APPROX 1 INCH, BOTH ENDS MARKED. GROUNDED - YES. REPAIRED THE CRACK FOUND ON THE LOWER SKIN OF THE L/H HORIZ STAB I/B OF STAB STA 129.50 USING MAT .071 2024-T3 SDR ASAA2023061543652Skin · debondedFOUND DISBOND ON BOTTOM SKIN OF LEFT HAND INBOARD MAIN FLAP. AREA MARKED. GROUNDED - YES. PERFORMED PERMANENT REPAIR ON BOTTOM SKIN OF LEFT HAND INBOARD MAIN FLAP IAW ASA B737-800 SRM 57-53-01-2R-7 & ASA B737-800 SRM 51-70-10-2R-0. NO FURTHER ACTION REQUIRED.SDR ASAA2023060943753Web · corrodedBS 987 L/H PRESSURE WEB CORRODED. GROUNDED - YES. REMOVED CORROSION.ORIGINAL WEB THICKNESS AT CORROSION AREA 0.020 IAW BAC DWG 147A5712 REV B REMAINING THICKNESS 0.004,REMOVED 0.016.OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1REMOVED WEB IAW B737-800 SRM 51-40SDR ASAA2023060943752Floor Support · corrodedMAIN CABIN FLOOR SUPPORT BEAM UPPER CHORD CORRODED AT STA.986.5. GROUNDED - YES. BLENDED CORROSION,ORIGINAL THICKNESS 0.015 IAW B737-800 SRM 53-70-51-0I-1REMAINING THICKNESS 0.110,REMOVED 0.040.OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1REMOVED UPPER "T" CHORSDR ASAA2023060943733Web · corrodedFWD CARGO DOOR CUTOUT SURROUND WEB HAS CORRSION IN MANY SPOTS. GROUNDED - YES. EVALUATED WEB ORIG THICK .045"REMOVED .018"REMAINING .027"FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-30-15-1A-1.REMOVED DAMAGED WEBLOCATED & DRILLED NEW WEB P/N:654A0003-58 PO 10SDR ASAA2023060943731Shield · corrodedFWD CARGO, AT STA 490R TO STA 500AR AFT SHIELD HAS SPOT'S OF CORROSION. STREAMER IS ATTACHED.DOT#A768. GROUNDED - YES. EVALUATED FWD CARGO, AFT SHIELD ORIG THICK =.032" REMOVED = .005" REMAINING = .027" FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-30-15-1A-1.SDR ASAA2023060843730Web · corrodedAFT CARGO DOOR SURROUND WEB HAS MULTIPLE SPOTS OF CORROSION. GROUNDED - YES. EVALUATED WEB, ORIG THICK= .045" REMOVED =.012" REMAINING = .033" FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-60-15-1A-1. REMOVED DAMAGED WEB, LOCATED AND DRILLED NEW WEB P/N:146A81SDR ASAA2023061583569Floor Panel · delaminatedFLOOR PANEL DELAME PN 141A5810-183. GROUNDED - YES. REPAIRED DELAM ON FLOOR PNL PN 141A5810-183 WITH 150* FIBER GLASS DOUBLER REPAIR IAW B737-800 SRM 53-00-50-2R-1.SDR ASAA2023041742915Unknown · unknownON TAKEOFF FROM SFO LEFT AUTOTHROTTLE WOULD NOT MOVE FORWARD TO TAKEOFF POSITION AND RED AUTOTHROTTLE ANNUNCIATOR ILLUMINATED. TRIED TO RESET SEVERAL TIMES BUT WAS UNSUCCESSFUL. GROUNDED - YES. AUTO THROTTLE BITE TEST HAS MSG 22-31263. ACCOMPLISHED B737-800 FISDR ASAA2023041442876Control Panel · intermittentCAPT COURSE INDICATOR DIGITS FROZEN/ INTERMITTENT KNOB IS TURNED. GROUNDED - YES. REMOVED AND REPLACED DFGC MODE CONTROL PANEL PWER B737-800 AMM 22-11-34.SDR ASAA2023040842769Unknown · unknownMID CABIN CEILING EXIT SIGN, AFT SIDE, IS UPSIDE DOWN. GROUNDED - YES. RE POSITIONED MID CABIN OVERHEAD LENS COVER FOR EMERGENCY EXIT SIGN REF B737-800 AMM 33-51-02.SDR ASAA2023040342694Control Panel · inoperativeF/O RADAR WX+T SWITCH INOP. GROUNDED - YES. WEATHER RADAR CONTROL PANEL REPLACED, OPS NORMAL.REF B737-800 AMM 34-43-91-400-801.SDR ASAA2023030842264Unknown · unknownR2 DOOR WOULD NOT CLOSE PROPERLY- LARGE GAP. GROUNDED - YES. CYCLED R2 DOOR TO ENSURE PROPER OPERATION. PFMD CABIN PRESS LEAK TEST REF B737-800 AMM 05-51-94. NO LEAKS FND.SDR ASAA2023020441826Window · not reportedCAPTAINS L-2 WINDOW OUTER PANE SHATTERED, AKSI K SIDE OVERHEAT LIGHT ILLUMINATED SHORTLY AFTER SHATTER AND L-2 WINDOW IS EXCESSIVELY HOT COMPARED TO OTHER HEATED WINDOWS. GROUNDED - YES. DURING TROUBLE SHOOTING FOUND L/H WHCU FAIL B737-800 FIM 30-41 TASK 801. SDR ASAA2023013051701Motor · inoperativeON PREFLIGHT THE RIGHT CENTER FUEL BOOST PUMP LIGHT ILLUMINATED. GROUNDED - YES. REMOVED RIGHT CENTER BOOST PUMP REF B737-800 AMM 28-22-41. COMPLETED STEPS A-1 THROUGH H-47 FOR RIGHT CENTER BOOST PUMP INSTALLATION REF AMM 28-22-41. REVERSED MEL 28-2E, PULLED CSDR ASAA2023011861547Motor · faultedIN CRUISE FLIGHT NO. 2 MAIN TANK FWD FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED. APPROXIMATELY 5500 LBS FUEL IN TANK. GROUNDED - YES. FOUND #2 FWD FUEL PUMP BAD. REMOVED AND REPLACED #2 MAIN TANK FWD FUEL PUMP (MOTOR IMPELLER). OPS CHECK NORMAL REF B737-800 AMM SDR ASAA2023011311504Sliding Window · crackedR2 OUTSIDE LAYER WINDOW CRACKED ASSOCIATED WINDOW HEAT LIGHT OVERHEAT ILLUMINATED. GROUNDED - YES. PERFORMED B737-800 AMM 56-12-11-400-801 STESP 3.F.7-8, CONFIRMED H16 WINDOW CODE, CONFIRMED TRANSFORMER TOP IS ON POSITION #1 REF B737-800 WDM 30-41-11. REMOVED SDR ASAA2023010621428Idg · inoperative#2 DRIVE LIGHT DID NOT TURN ON AFTER ENG SHUTDOWN. GROUNDED - YES. REMOVED AND REPLACED #2 IDG IAW AMM 24-11-11. ORIG SUBMISSION DATE: 1/6/2023SDR ASAA2022122441259Overheat Loop · false activationAPU DET INOP LIGHT ILLUMINATED. GROUNDED - YES. R/R APU OVERHEAT DETECTOR REF B737-800 AMM 26-15-01.SDR ASAA2022122241213Warning Message · false indicationHF 2 FAIL. GROUNDED - YES. PERFORMED OPERATIONAL TEST REF B737-800 AMM 23-11-00-710-801, TEST OK. MESSAGE CLEARED.SDR ASAA2022121241142Guide Vane · crackedWHILE ACCOMPLISHING ASA T/C 78472022, FOUND 4 CRACKED LPT 1ST STAGE NOZZLE GUIDE VANES CRACKED AT 12, 1 AND 3 O'CLOCK. #1 ENG. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE. DEFECT TRANSFERRED TO SHOP W/O # 1951228.SDR ASAA2022111040742Wire Harness · failed#2 ENGINE FIRE TEST DID NOT ILLLUMINATE. GROUNDED - YES. REFERENCE TSR 713386 REMOVED & REPLACED MW0326 AND ETOPS GROUND VERIFICATION PASSED REF B737-800 AMM 26-11-02/401.SDR ASAA2022110340653Knob · brokenFMS DIMMER KNOB STOP BROKEN. GROUNDED - YES. REMOVED AND REPLACED FMCS CDU KEYBOARD ON LEFT CDU IAW B737-800 AMM 34-61-01.SDR ASAA2022110340642Autothrottle Sys · faultedA/T ONLY ADVANCED TO 78 PERCENT ON T/O WHEN PERF DATA REQUIRED 101 PERCENT. GROUNDED - YES. NO LOGGED FAULTS A/T OR DFGS. SYS TEST GOOD TASKS B737-800 AMM 22-31-00-710-801 & 802.SDR ASAA2022102540522Overheat Loop · faultedENGINE #2 'B' LOOP ENGINE OVERHEAT INDICATES A FAULT LIGHT AND UNSATISFACTORY TEST WHEN OVERHEAT SWITCH IN THE NORMAL POSITION. ENGINE FIRE TEST SATISFACTORY WHEN OVERHEAT SWITCH IS PLACED IN THE A LOOP POSITION. GROUNDED - YES. PERFORMED ENGINE/APU FIRE DETEC
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