N581AS
Service difficulty reports · 484
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 = 'N581AS' 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 = 'N581AS' 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 ASAA2023022142332Unknown · corrodedINTERNAL PASSENGER FLOOR STRUCTURE WET AREA HAS CORROSION BELOW FASTENER HOLE AT FRAME STA 967, RBL 18. GROUNDED - YES. REMOVED CORROSION ORIG .125, REMAIN .098 LOSS OF .027.FOUND OUT OF LIMITS IAW B737-800 SRM 53-70-51 CUTOUT DAMAGE, FABBED REPAIR PARTS, ALODSDR ASAA2023022142331Shear Tie · crackedFWD CARGO FLOOR STRUCTURE @ STA. 500G UNDER R/H TRANSITION PANEL, FWD SIDE OF FRAME TO INTERCOSTAL ATTACH SHEAR TIE CRACKED AS MARKED. GROUNDED - YES. REMOVED DAMAGED CLIP @ STA 500G .LOCATED AND DRILLED NEW CLIP @ STA 500G IAW B737-800 SRM 51-40-02 AND DWG #1SDR ASAA2023022142329Shear Tie · crackedFWD CARGO DLOOR STRUCTURE @ SAT.500H UNDER R/H TRANSITION PANEL, FWD SIDE OF FRAME TO INTERCOSTAL ATTACH SHEAR TIE CRACKED AS MARKED. GROUNDED - YES. REMOVED DAMAGED CLIP @ STA 500H LOCATED AND DRILLED NEW CLIP @ STA 500H IAW B737-800 SRM 51-40-02 AND DWG# 143SDR ASAA2023022142328Shear Tie · crackedFWD CARGO DLOOR STRUCTURE @ STA .500H UNDER R/H TRANSITION PANEL, AFT SIDE OF FREME TO INTERCOSTAL ATTACH SHEAR TIE CRACKED AS MARKED. GROUNDED - YES. REMOVED DAMAGED CLIP @ STA 500H,LOCATED AND DRILLED NEW CLIP @ STA 500H IAW B737-800 SRM 51-40-02 AND DWG # 1SDR ASAA2023022142159Transition Panel · corrodedAFT PIT RH TRANSITION PANEL UPPER AND LOWER SURFACES HAVE CORROSION FROM STA 727E+10 - 767 (MARKED). GROUNDED - YES. REMOVED CORROSION ON AFT PIT RH TRANSITION PANEL UPPER AND LOWER SURFACES FROM STA 727E+10 - 767. ORG MAT .040. MAT REMOVED .016. MAT REMAININGSDR ASAA2023022142158Transition Panel · corrodedAFT PIT RH TRANSITION PANEL UPPER AND LOWER SURFACES HAVE CORROSION FROM STA 727B+10 - 727E+10 (MARKED). GROUNDED - YES. REMOVED CORROSION ON AFT PIT RH TRANSITION PANEL UPPER AND LOWER SURFACES FROM STA 727B+10 - 727E+10. ORG MAT. .040. MAT REMOVED .013. MAT SDR ASAA2023022142156Transition Panel · corrodedAFT PIT LH TRANSITION PANEL UPPER AND LOWER SURFACES HAVE CORROSION FROM STA 727G+10 - 787 (MARKED). GROUNDED - YES. REMOVED CORROSION AT AFT PIT LH TRANSITION PANEL STA 727G+10. ORIGINAL THICKNESS .040". REMOVED .010", REMAINING MATERIAL THICKNESS IS .030". FSDR ASAA2023022142155Transition Panel · corrodedAFT PIT LH TRANSITION PANEL UPPER AND LOWER SURFACES HAVE CORROSION FROM STA 727C+10 - 727G+10 (MARKED). GROUNDED - YES. REMOVED CORROSION AT AFT PIT LH TRANSITION PANEL FROM STA 727C+10 - 727G+10. ORIGINAL THICKNESS .040". REMOVED .013". REMAINING .027". FOUNSDR ASAA2023022142148Transition Panel · corrodedAFT PIT LH TRANSITION PANEL UPPER AND LOWER SURFACES HAVE CORROSION FROM STA 727A+10 - 727C+10 (MARKED). GROUNDED - YES. REMOVED CORROSION AT AFT PIT LH TRANSITION PANEL FROM STA 727A+10 - 727C+10. ORIGINAL THICKNESS .040". REMOVED .006". REMAINING .034". FOUNSDR ASAA2023022142132Transition Panel · corrodedAFT PIT LH TRANSITION PANEL IS CRACKED AT APPROX STA 780, LBL 22 (MARKED). GROUNDED - YES. EVALUATED DAMAGE AT AFT PIT LH TRANSITION PNL AT STA 780, LBL 22. FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2. PANEL TO BE REPLACED ON TASK CARD G1774079 OPSDR ASAA2023022142131Shield · corrodedFWD CARGO FLOOR STRUCTURE BETWEEN STA. 500 AND 500A, RBL24 HAS TRANSITION PANEL CORRODED AS MARKED. GROUNDED - YES. EVALUATED SHIELD & FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVENREMOVED OLD SHIELD, LOCATED & DRILLED NEW SHIELD P/N 143A8126-29 PO 1054152.1SDR ASAA2023022042129Floorboard · delaminatedFLOOR PANEL #147A5810-28 HAS 1EA INSERT PULLED THROUGH. AREA MARKED. GROUNDED - YES. REPAIRED FLOOR PANEL #147A5810-28 IAW B737-800 SRM 53-00-50-2R-0 AND 53-00-50-2R-1.SDR ASAA2023012531642Fmc · faultedVTK ON RT NAV DISPLAY FOLLOWED BY LOSS OF LNAV/VNAV ASSOCIATED WITH A RIGHT FMC FAILURE 2 HOURS INTO FLIGHT. FMC SUBSEQUENTLY RECOVERED ON ITS OWN BEFORE QRH CHECKLIST WAS INITIATED. GROUNDED - YES. ACCOMPLISHED B737-800 FIM TASK 34-61 TASK 804, NO FAULTS, CONSDR ASAA2022123041354Oil Filter · cloggedDURING ASA T/C 78349004 FOUND BUTTON ON THE OIL FILTER INDICATION POPPED. GROUNDED - YES. REMOVED AND REPLACED LUBE FILTER ELEMENT REF B737-800 AMM 49-91-12 OPS CHECK GOOD.SDR ASAA2022122761240Pressure Switch · inoperative#2 TANK AFT BOOST PUMP LOW PRESSURE LIGHT NOT ILLUMINATED WHEN SWITCH IN OFF POSITION. GROUNDED - YES. REMOVED AND REPLACED #2 TANK AFT BOOST PUMP PRESSURE SWITCH REF B737-800 AMM 28-42-11. OPERATIONAL TEST PASS REF AMM 28-42-11-700-801, AND LIGHT NOW ILLUMINASDR ASAA2022121641176Pressure Sensor · faultyREF T/C 78273000 CDU CHECK FOR FAULTS FOUND ENG 2 SHORT TIME FAULT 79-11092. THE ENG OIL PRESSURE SIGNAL (PEO) IS OUT OF RANGE. GROUNDED - YES. REMOVED AND REPLACED OIL PRESSURE SENSOR REF B737-800 AMM 79-32-01-400-801-F00. OPS CHECK NORMAL AND NO LEAK NOTED. SDR ASAA2022121641166Bleed Valve · failedDURING CLIMBOUT RT PACK DUCT PRESSURE @ 8 PSI. GROUNDED - YES. AIR TURNBACK -- ACCOMPLISHED PNEUMATIC- TROUBLESHOOTING PER B737-800 AMM 36-11-00-700-804, FOUND BAD BAR AND PRSOV. REMOVED & REPLACED THE #2 ENG. BLEED AIR REGULATOR AND PRSOV, REF AMM 36-11-03 ANSDR ASAA2022120941114Bulb · dirtyCONT CAB ZONE TEMP LIGHT ILLUMINATES ON RECALL AND EXTINGUISHES ON MASTER CAUTION RESET. GROUNDED - YES. CONT CAB ZONE TEMP LT ON WITH MASTER RECALL AT OVERHEAD. PERFORMED PZTC BITE IAW B737-800 FIM 21-62 TASK 801. NR 1 LT PZTC NO FAULTS. NR 2 RT PZTC, FLT DECSDR ASAA2022120941099Hook · wornWHILE ACCOMPLISHING ASA T/C SBCFM 56-7B-72-1074-1 NOTED THAT THE AFT SIDE OF THE 3RD STAGE J-HOOK IS COMPLETELY WORN THROUGH AT BOTH THE 6 O'CLOCK AND 12 O'CLOCK POSITIONS, SEE INSP SERVER FOR PICTURES AND REPORT. PER T/C STEP 8 ENG MUST BE REMOVED WITHIN 10 CSDR ASAA2022120543241Unknown · unknownPER ASA T/C 78472000 #2 ENG. INLET INSPECTION #10 DUCT PANEL IS LOOSE. GROUNDED - YES. RE-SECURED #10 DUCT PANEL IAW B737-800 AMM 72-23-07-400-861-F00.SDR ASAA2022120541028Spacer · debondedPER ASA T/C 78472010 #2 ENG FAN BLADE LUBE SPACERS #7, 12, AND 24 ARE DISBONDED. GROUNDED - YES. REMOVED AND REPLACED #2 ENG FAN BLADE LUBE SPACERS #7, 12, & 24. REF AMM 72-21-02 AND ASA T/C 78472010.SDR ASAA2022110840673Engine · vibrationAT TOP OF DESCENT AS THRUST LEVERS WENT TO IDLE THE #1 ENGINE "VIB" INDICATION INCREASED RAPIDLY TO 4.3. GROUNDED - YES. ENG 1 S/N 894613 EXPERIENCED CORE VIBRATION OF 3.0 AS SEEN BY FORWARD AND REAR VIBRATION SENSOR (ASA TSR 713396). PERFORMED VISUAL INSPECTISDR ASAA2022110240596Circuit Breaker · openAFTER START LEFT ELEVATOR PITOT LIGHT ILLUMINATED ON OVERHEAD. GROUNDED - YES. FOUND C/B OPEN - RESET - SYS OPS OK.SDR ASAA2022102840540Modulating Valve · faultedAFTER ENG START, UPON RECALL CONT CAB ZONE TEMP LT ILL. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 21-62 TASK 801, BITE TEST OF L PZTC FAULTING ZONE TRIM VALVE ON VERIFY TEST. ACCOMPLISHED FIM 21-62 TASK 835, VERIFY STILL FAULTING ZONE TRIM VALVE. REMOVED AND RSDR ASAA2022102440493Actuator · leaking#1 ENGINE R/H VSV ACTUATOR FOUND TO HAVE FUEL LEAK AFTER SHUT DOWN APPROX 5 DPM. GROUNDED - YES. REMOVED AND REPLACED REF B737-800 75-31-01/401. PERFORMED ACTUATOR LEAK TEST AMM TASK 75-31-01-790-801. OPERATIONAL TEST IS GOOD. NO LEAKS NOTED. TEST 12 AND TESTSDR ASAA2022102440492Valve · leaking#1 ENG HPTACC VALVE FOUND TO HAVE FUEL LEAK AFTER SHUT DOWN OF APPROX. 7 DPM. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE HPTACC VALVE REF B737-800 AMM 75-21-01. OPS CHECK GOOD AT THIS TIME WITH NO LEAKS DETECTED.SDR ASAA2022102240449Actuator · leakingEVIDENCE OF FUEL LEAKING ON #1 ENGINE FROM LEFT VSV DRAIN PIPE. GROUNDED - YES. ENGINE #1 RAN TO CHECK FOR EVIDENC OF LEAKING VSV DRAIN PIPE. LEAKING AT A RATE OF 5 DROPS PER MINUTE. REMOVED AND REPLACED LEFT #1 ENGINE VSV ACTUATOR PER B737-800 AMM 75-31-01-84SDR ASAA2022101740429Warning Light · inoperativeAFTER TAKEOFF, WE ATTEMPTED TO COMPLY WITH MEL 28-2E, PER THE PROCEDURE . HOWEVER THE CROSSFEED VALVE AND LIGHT WERE INOPERATIVE ALL CIRCUIT BREAKER WERE IN AND NORMAL ADDITIONALLY, THE FOLLOWING LIGHTS WERE INOPERATIVE : NO. 1 TANK AFT LOW PRESSURE LIGHT, NO.SDR ASAA2022101440317Pump · faultyLEFT FWD FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED. GROUNDED - YES. REPLACED LEFT FWD FUEL PUMP OPS CHECK GOOD LEAK CHECK GOOD. REF B737-800 AMM 28-22-41.SDR ASAA2022101340318Pump · reads lowLEFT MAIN FWD LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT ACCOMPLISHED QRH. LIGHT REMAIN ILLUMINATED. GROUNDED - YES. NO HISTORY 60 DAYS PERFORMED GOOD OPERATIONAL TEST FOR LEFT MAIN FWD FUEL PUMP. REF B737-800 AMM 28-22-41-400-802. OK TO SERVICE.SDR ASAA2022101140331Pump · inoperativeCENTER RIGHT FUEL PUMP INOP. GROUNDED - YES. REMOVED AND REPLACED RIGHT CENTER BOOST PUMP REF B737-800 AMM 28-22-41, OPS CHECKS GOOD.SDR ASAA2022100940229Fuel · reads lowCENTER FUEL TANK RIGHT FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED WITH APPROX 6,000 LBS REMAINING IN TANK. BOOST PUMP SWITCH TURNED OFF AND LIGHT EXTINGUISHED. GROUNDED - YES. PERFORMED OPERATIONAL TEST OF RH CENTER BOOST PUMP PRESSURE SWITCH PER B737-800 AMM TASDR ASAA2022092240025Circuit Breaker · poppedPWS FAIL. WXR FAIL. GROUNDED - YES. WXR CB AND FMC CB RESETTED PER B737-800 AMM 20-60-01-860-801. OPS TEST GOOD WXR OPS GOOD.SDR ASAA2022090439771Control Valve · faultedRIGHT PACK LIGHT ILLUMINATED. GROUNDED - YES. PERFORMED PACK TEMP CONTROL BITE TEST PER B737-800 FIM 21-62 TASK 801. FOUND TCV FAULTING. RESET TCV SUCCESSFUL PER FIM 21-62 TASK 831. FAULT CLEARED. NO OTHER DEFECTS NOTED.SDR ASAA2022082639672Unknown · unknownAIR COND TEMP INDICATOR FOR RIGHT PACK POSITION IS INOP (FULL SCALE ZERO). GROUNDED - YES. REMOVED & REPLACED RH PACK TEMPERATURE BULB REF B737-800 AMM 21-51-60-000/400-801.SDR ASAA2022082639669Unknown · faultyAT THE GATE THE RIGHT PACK LIGHT ILLUMINATED. TEMPERATURE INDICATOR FOR R PACK WAS PEGGED HIGH. GROUNDED - YES. RIGHT PACK HAD TRIPPED OFF, ZONE TEMP CONT LOGGED TCV. RESET PACK, RAN FOR SEVERAL MINUTES - OPS CKS GOOD. ZONE TEMP BITE CKS GOOD REF B737-800 AMSDR ASAA2022081139465Circuit Breaker · trippedRIGHT PACK LIGHT ILLUMINATED. GROUNDED - YES. ACCOMPLISHED RIGHT PACK CONTROLLER BITE CHECK B737-800 FIM 21-62 TASK 801 AND GOT RIGHT TCV LIGHT ON, ACCOMPLISHED RIGHT TCV CIRCUIT BREAKER FIM 21-82 TAKS 831 RESET AND POWER DOWN A/C . PACK BITE CHECK PASSED AND SDR ASAA2022071339091Shroud · debondedWHILE PERFORMING ASA TASK CARD 78472000 FOUND DISBONDING AT THE 6 O'CLOCK POSITION AFT ON THE ABRADABLE SHROUD. GROUNDED - YES. PERFORMED RECONDITION OF ABRADABLE SHROUD AS REQUIRED ON #1 ENG. AT 6 O'CLOCK INLET POSITION REF B737-800 AMM 72-24-02.SDR ASAA2022070839011Apu · failedAT PUSHBACK AND CLEARED TO START THE START SEQUENCE WAS INITIATED, THE APU SHUTDOWN ON IT'S OWN WITH A FAULT LIGHT QRH 7.2 WAS RAN. APU PUT OUT A LARGE AMOUNT OF SMOKE. RAMP CREW ADVISED A LARGE AMOUNT OF SMOKE WAS COMING OUT OF THE APU COMPARTMENT. GROUNDED -SDR ASAA2022070338904Pressure Switch · faultyRIGHT CENTER TANK FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED WITH 8,000 LBS FUEL REMAINING IN CENTER TANK. GROUNDED - YES. TRANSFERED 5000 LBS TO CNTR TANK. RAN RT CNTR TANK PUMP FOR 20 MIN WITH NO FAULT. WITH PWR RMVD CK'D RT CNTR LOW PRESS SWITCH CONNECTOR-NO SDR ASAA2022062738831Connector · looseRIGHT CENTER FUEL PUMP LOW PRESSURE ILLUMINATED STAYED IN FLIGHT. GROUNDED - YES. DIVERSION - INSPECTED R/H CENTER BOOST PUMP FOUND CANNON PLUG LITTLE LOOSE. RESECURED CANNON PLUG NO FURTHER DEFECT NOTED REF B737-800 FIM 28-22 TASK 802. TRANSFERRED THE FUEL USSDR ASAA2022060538571Sensor · failedAFTER PUSH BACK RIGHT FWD WINDOW HEAT LIGHT COME ON. RESET PER QRH, NO FIX. GROUNDED - YES. RT FRONT WHCU BITE SHOWS WINDOW SENSOR FAULT AND FAULT HIST LOG MULTIPLE SENSOR FAULTS. REF B737-800 FIM 30-41 TASK 812 AND B737-800 AMM TASK 30-41-21-760-801, VERIFIEDSDR ASAA2022050638229Boot · crackedWHILE PERFORMING T/C N8420001 FOUND IGNITOR BOOT CRACKED AT 6 O'CLOCK POSITION. GROUNDED - YES. REMOVED MATING PAD, SHROUD, AND HOSE CLAMPS REF B737-800 AMM 74-21-01. REPLACED IGNITOR LEAD COOLING BOOT. REINSTALLED MATING PAD, SHROUD, AND HOSE CLAMPS REF AMM 7SDR ASAA2022050638227Harness · damagedWHILE PERFORMING T/C N8420001 FOUND DAMAGE ON J9 HARNESS. GROUNDED - YES. REPLACED J9 HARNESS REF B737-800 AMM 73-21-06/401 ALL REQUIRED TEST PASSED.SDR ASAA2022042438098Window · overheatedR SIDE WINDOW HEAT OVERHEAT LIGHT ILLUMINATED. RAN QR, LIGHT REMAINED ILLUMINATED. GROUNDED - YES. PERFORMED GVI OF R/H SIDE SLIDING WINDOW AND FOUND EVIDENCE OF WIRE ARCING IN UPPER AFT CORNER OF R/H SIDE SLIDING WINDOW. REMOVED AND REPLACED RH SLIDER WINDOW SDR ASAA2022041938075Module · faultyRH SIDE WINDOW OVERHEAT ILLUMINATED DURING TAXI TO GATE. TURNED WINDOW HEAT OFF, WAITED 5 MINS PER QRH, TURNED WINDOW HEAT BACK ON, OVERHEAT ILLUMINATED AGAIN. GROUNDED - YES. ON DEFERRAL.
REMOVED AND REPLACED WINDOW/PITOT HEAT MODULE IAW B737-800 AMM 30-41SDR ASAA2022041638031None · degradedTECH SERVICES REQUEST FOLLOW-UP TO CONTINUED NGS REPORTS BLUE DEGRADED LIGHT GROUNDED - YES. REMOVED AND REPLACED LH FLOW CONTROL AND SHUTOFF VALVE IN REFERENCE TO B737-800 AMM 21-51-01. OPS CHECK GOOD.SDR ASAA2022032437762Battery Pack · failedDURING ACCOMPLISHMENT OF T/C 78233001 BATTERY PACK M1673 FAILED CAPACITY TEST. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK REF B737-800 AMM 33-51-06-960-805. OPC GOOD NO FURTHER DEFECTS FOUND.SDR ASAA2022031037676Harness · faultyREF PREVIOUS LOG 60309274 AFTER MEL APPLIED, ON SECOND PREFLIGHT CK, AIR CONDITIONING BLEED AIR VALVE RIGHT POPPED AGAIN. GROUNDED - YES. ON THE #2 ENGINE, REMOVED CONNECTOR DP1102 FROM BLEED AIR REGULATOR AND C/B STILL POPS. REMOVED CONNECTOR DP1104 AT PYLON SDR ASAA2022031037668Unknown · unknownDURING PREFLIGHT FOUND AIRCONDITIONING BLEED AIR VALVE RIGHT C/B OUT. GROUNDED - YES. REF LOG PG# 60309276 & 60309288 FOR WIRING HARNESS CHANGE AND OPS TESTS. OPS TESTS GOOD. C/B DID NOT POP.
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