N508AS
Service difficulty reports · 429
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 = 'N508AS' 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 = 'N508AS' 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 ASAA2026020364312Seat Track · crackedWHILE WORKING T.C. 800-25EO-26332-3-9, FOUND SEAT TRACK AT AFT MAIN CABIN STA 887 LBL24.8 TO BE CRACKED. SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A REPAIR AT MAIN CABIN STA 887 LBL 24.8 IAW B737-800 SRM 53-00-52-2R-5 (MAJOR REPAIR) SRXR430X.SDR ASAA2026011063671Door · no discrepancyL2 DOOR DOES NOT OPEN. GROUNDED - YES. REINSPECTED OPENING AND CLOSE MECHANISM AND FOUND NO FAULTS . OPS CLOSING AND OPENING WORKS NORMAL IAW AMM 52-13-00. OK FOR SERVICE.SDR ASAA2025081360079Lens · missingEXIT SIGN MISSING 17F. GROUNDED - YES. INSTALLED NEW EMERGENCY EXIT SIGN LENS AT ROW 17DEF OPS GOOD. REF AMM 33-51-01.SDR ASAA2025052258225Tire · blownBLOWN #1 MAIN TIRE FOUND AFTER BLOCKING IN. GROUNDED - YES. REMOVED & REPLACED BOTH #1 AND #2 MLG TIRES PER MM 32-45-11. COMPLIED WITH CONDITIONAL INSPECTION TIRE TREAD LOSS OR TIRE BURST CONDITIONAL INSPECTION IAW AMM 05-51-54-210-801 UP TO STEP 2 (E). ACCOMPSDR ASAA2024081052791Skin · corrodedEXTERIOR SKIN HAS 3 AREAS OF CORROSION BS. 727 TO BS.887 STR. 4R LOWER SKIN. GROUNDED - YES. REMOVED CORROSION AT 3EA LOCATIONS BETWEEN BS 727 TO BS 887 STR 4R LOWER SKIN AND REPAIRED ALL DAMAGE LOCATIONS IAW ASA EA 800-53EA-27601. REPAIR DOUBLER LOCATION BETWSDR ASAA2024042349843Attach Angle · corrodedUPON REMOVAL OF AFT PIT DOOR SURROUND FWD SHIELD, FOUND ATTACHING ANGLE UNDERNEATH TO HAVE MULTIPLE AREAS OF CORROSION. GROUNDED - YES. REMOVED CORR. FROM AFT PIT DOOR SURROUND FWD SHIELD ATTATCHED ANGLE ORIG THICKNESS .050. I.A.W. B737-800 SRM 53-60-15 MAT. LSDR ASAA2024042249819Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR PANEL 147A5810-30 HAS CORRODED INSERTS. GROUNDED - YES. EVALUATED AND REPAIRED IAW B737-800 SRM 53-00-50-2R-0, SRM 53-00-50-2R-1.SDR ASAA2024042249818Floor Panel · corrodedMAIN CABIN WET AREA FLOOR PANEL 147A5810-28 HAS CORRODED INSERTS. GROUNDED - YES. REMOVED AND REPLACED 62 EA INSERTS, REPAIRED PANEL 147A5810-28 WITH FIBERGLASS DOUBLERS IAW B737-800 SRM 53-70-50-2R-0, 53-00-50-2R-0 & 53-00-50-2R-1.SDR ASAA2024042249817Floor Panel · corrodedMAIN CABIN AFT WET AREA FLOOR PANEL 147A5810-27 HAS CORRODED INSERTS. GROUNDED - YES. REMOVED AND REPLACED 62 EA INSERTS, REPAIRED PANEL 147A5810-27 WITH FIBERGLASS DOUBLERS IAW B737-800 SRM 53-70-50-2R-0, 53-00-50-2R-0 & 53-00-50-2R-1.SDR ASAA2024042249816Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR PANEL 147A5810-137 HAS CORRODED INSERTS. GROUNDED - YES. REPAIRED FLOOR BOARD 147A5810-137 BY REPAIRING TOP SKIN AND REPLACING INSERTS IAW B737 SRM 53-00-50-2R-0; 53-00-50-2R-1.SDR ASAA2024042249815Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR PANEL 147A5810-123 HAS CORRODED INSERTS. GROUNDED - YES. REPLACED CORRODED INSERTS ON FLOOR PANEL 147A5810-123 IAW ASA B737-800 SRM 53-00-50-0I-1, SRM 53-00-50-1A-1, SRM 53-00-50-2R-0, SRM 53-00-50-2R-4, AIPC 53-21-51-56C.SDR ASAA2024042249814Floor Panel · delaminatedMAIN CABIN FWD WET FLOOR PANEL 141A5810-454 HAS CORRODED INSERTS. GROUNDED - YES. REPAIRED FLOOR PANEL 141A5810-454 BY REPAIRING TOP SKIN AND REPLACING INSERTS IAW B737 SRM 53-00-50-2R-0; 53-00-50-2R-1.SDR ASAA2024042249813Floor Panel · delaminatedMAIN CABIN FWD WET AREA FLOOR PANEL 141A5810-755 HAS DELAM & CORRODED INSERTS. GROUNDED - YES. REPAIRED IAW B737-800 SRM 53-00-50-2R-0, SRM 53-00-50-2R-1.SDR ASAA2024042249812Floor Panel · delaminatedMAIN CABIN FWD WET AREA FLOOR PANEL 141A5810-769 HAS PEELING FIBERS & CORRODED INSERTS. GROUNDED - YES. REPAIRED DAMAGED FIBERS AND REPLACED CORRODED INSERTS ON FLOOR PANEL 141A5810-769 IAW ASA B737-800 SRM 53-00-50-0I-1, SRM 53-00-50-1A-1, SRM 53-00-50-2R-0, SDR ASAA2024042249811Floorboard · delaminatedMAIN CABIN FWD WET AREA FLOOR PANEL 141A5810-763 HAS DELAM & CORRODED INSERTS. GROUNDED - YES. REPAIRED MAIN CABIN FWD WET AREA FLOOR PANEL 141A5810-763 HAS DELAM & CORRODED INSERTS IAW ASA B737-800 SRM 53-00-50.SDR ASAA2024041949891Skin · crackedRIGHT HORIZONTAL STABILIZER LOWER SKIN IS CRACKED AT STAB. STA. 101.90 RIB LOCATED 9" FROM THE REAR SPAR. APPROX. 1.250" IN LENGTH. (MARKED AND IDENTIFIED END OF CRACK). GROUNDED - YES. REPAIRED RIGHT HORIZONTAL STAB LOWER SKIN CRACKS 2EA. IAW B737-800 SRM 55-SDR ASAA2024041849918Web · corrodedAFT PIT WEB HAS CORROSION. GROUNDED - YES. REMOVED CORR.FROM AFT PIT WEB ORIG. THICKNESS .045 I.A.W B737-800 SRM53-60-15. MAT LOSSED .040 REMAINING THICKNESS .005 FOUND TO BE OUT OFLIMITS I.A.W B737-800 SRM 53-60-15.TOOL#T8224K DUE 25/OCT/24.REMOVED AND REPLASDR ASAA2024041849917Transition Panel · corrodedAFT PIT TRANSITION PANEL @ STA727E+16 TO STA767 IS CORRODED. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT R/H TRANSITION PNL AT STA727E+16 TO ST767 ORIG THICK .040 I.A.W B737-800 SRM 53-60-53. AREA FOUND TO BE OUT OF LIMITS AND PUNCTURED I.A.W B737-800 SRM 53-0SDR ASAA2024041849842Shield · corrodedAFT PIT DOOR SURROUND FWD SHIELD HAS CORROSION. GROUNDED - YES. EVALUATED AFT PIT FWD SHIELD ORIG THICKNESS IS .050" IAW B737-800 SRM 53-60-15-0I-1 REMOVED .007" REMAINING .043" AND IS FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-60-15-1A-1 4.G.2 TOOL# T8224KSDR ASAA2024041849841Transition Panel · corrodedAFT PIT RH TRANSITION PANEL @ STA727 TO STA727E+15 IS CORRODED. GROUNDED - YES. REMOVED CORR. FROM AFT PIT R/H TRANSITON PNL AT STA.727 TO STA.727E+15 ORIG. THICKNESS .040 I.A.W B737-800 SRM 53-60-53 MAT. LOSSED .010 REMAIING THICKNESS .030 FOUND TO BE OUT OFSDR ASAA2024041849840Transition Panel · corrodedAFT PIT LH TRANSITION PANEL IS CORRODED @ STA727I+14 TO STA827. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT L/H TRANSITION PANEL @ STA 727I +14 TO STA 827 IAW B737-800 SRM 53-00-53-1A-2.2.D. ORIG. THICKNESS: .040 IAW B737-800 SRM 53-60-53-IO-2. 100% MAT LOSS ASDR ASAA2024041849839Transition Panel · corrodedAFT PIT LH TRANSITION PANEL IS CORRODED @ STA727C+7 TO STA727I+13. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT L/H TRANSITION @ STA727C+7 TO 727I+13 IAW B737-800 SRM 53-00-53-1A-2.R.D. ORIG. THICKNESS: .040 IAW B737-800 SRM 53-60-53-OI-1 REMOVED: .007, REMAINISDR ASAA2024041849838Transition Panel · corrodedAFT PIT LH TRANSITION PANEL IS CORRODED @ STA727 TO STA727C+6. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT L/H TRANSITION PANEL @ STA727 TO STA727C+6 IAW B737-800 SRM 53-00-55-1A-2. ORIG THICKNESS: .040 IAW B737-800 SRM 53-60-53-IO-2. 100% MAT LOSS AND IS FOUNSDR ASAA2024041849836Floorbeam · corrodedMAIN CABIN AFT WET AREA, FLOOR BEAM CORRODED ON UPPER SURFACE AT BS 947.5 BETWEEN LBL-30 AMD RBL-10. MARKED. GROUNDED - YES. CORROSION IS LOCATED ON A PREVIOUS T-CAP REPAIR. CORROSION FOUND TO BE OUT OF LIMITS DUE TO BEING LOCATED AT A HARD MOUNT ATTACHMENT LOSDR ASAA2024041449835Stop Fitting · gougedMAIN CABIN, L/H AFT ENTRY DOOR I/B TOP 'DOOR STOP FITTING' HAS BARE (METAL.GOUGE). DOT#Z211 STREAMER IIS ATTACHED. GROUNDED - YES. EVALUATED STOP FITTING AND FOUND DAMAGE TO THE BUSHING, DAMAGE TO BUSHING IS NOT PERMITTED AND FOUND TO BE OUT OF LIMITS IAW B737SDR ASAA2024032748691Gust Lock · lack of lubeL2 ENTRY DOOR WONT STAY OPEN. GROUNDED - YES. (RESOLVED ON W/O: 1995171 TASKCARD: N/R-00001 ) CLEANED AND LUBE L2 DOOR GUST LOCK MECHANISM, OPENED AND CLOSED L2 DOOR SEVERAL TIMES REF AMM 52-13-00, OPS CHECK GOOD NO DEFCETS NOTED AT THIS TIME. NO HISTORY IN LASDR ASAA2024030648295Light · damagedAIRCRAFT LEFT LAST FLOOR TRACK LIGHTING ABEAM LAVS COMING UP. GROUNDED - YES. AFTMOST L/H FLOOR PHOTOLUMINESCENT STRIP IS DAMAGED BEYOND LIMITS. REPLAED FLOOR STRIP, REF AMM 33-51-15 OK FOR SVC.SDR ASAA2024011947425Light · missing16F EMERGENCY EXIT PLACARD MISSING. GROUNDED - YES. REMOVED AND REPLACE EMERGENCY EXIT SIDE/OVERWING LIGHT ASSY IAW AMM 33-51-04, OPS CHK GOOD.SDR ASAA2023121546794Lens · looseFWD GALLEY EMER EXIT SIGN LOOSE (ABOVE COCKPIT DOOR). GROUNDED - YES. SECURED EMERGENCY EXIT SIGN LENS WITH TAPE AND DEFERRED REPLACEMENT OF ASSY REF ASA EA# 800-33EA-26359 FOR 150 FH.SDR ASAA2023102145781Lens · missingR2 DOOR EXIT SIGN LIGHT COVER MISSING. GROUNDED - YES. REPLACED R2 EM. LIGHT EXIT LIGHT LENS, OK FOR SERVICE.SDR ASAA2023101645676Unknown · unknownRIGHT PACK LIGHT ILLUMINATED ON MASTER CAUTION RECALL LIGHT DOES EXTINGUISH ON RESET. GROUNDED - YES. ACCOMPLISHED PACK TEMP CONTROL BITE PER B737-800 FIM 21-61 TASK 801. #2 CONTROLLER LOGGED TCV FAULT - FAULT RESET. RAN BITE CHECK AGAIN - NO FAULTS NOTED.SDR ASAA2023091145051Unknown · unknownAUTO FAIL ILLUMINATED BRIEFLY. GROUNDED - YES. PERFORMED SYSTEM BITE CHECK, REF FIM 21-31 TASK 801. OPS CHECKS GOOD.SDR ASAA2023090444928Unknown · unknownFO SIDE NUMBER 2 WINDOW HEAT OVRHT. GROUNDED - YES. RELEASED PER MEL 30-11E FO NO 2 WINDOW HEAT INOP. AUTH BY SEAMC JEREMY AT 1342Z. FOUND R SIDE WINDOW HEAT PWR C/B C393 ON P6-11 PANEL OUT. RESET C/B REF MM 20-60-01 & WDM 30-41-11 & WINDOW HEAT OPS NORMAL GNDSDR ASAA2023082844835Unknown · unknownFMC VNAV INFORMATION BLANKED ON FMC SCREEN DID NOT RETURN. GROUNDED - YES. COULD NOT DUPLICATE ANY FAULT. EXPANDED BITE LOGGED NO FAULTS. RESET BOTH FMC'S. OP CK NORMAL. REF B737-800 FIM 34-61 TASKS 837 & 801.SDR ASAA2023080344435Unknown · unknownAPU WOULDN'T START ELEC LIGHT ILLUMINATED. GROUNDED - YES. ACCOMPLISHED ELEC LIGHT MESSAGE BITE PROCEDURE PER FIM 24-31 TASK 801. FOUND SPCU FAULT, SPCU FAULT WOULD NOT RESET. FOUND SW HOT BAT BUS C/B OPENDED. RESET C/B PER MM 20-60-01. REACCOMPLISHED ELEC LIGSDR ASAA2023080344419Unknown · unknownHF 2 FAIL MESSAGE. GROUNDED - YES. ACCOMPLISHED FIM 23-11 TASK 801. HF2 OPS CHECK NORMAL.SDR ASAA2023080244381Power Supply · malfunctionedWORKING TC 78233001, FOUND EMERGENCY LIGHTING BATTERY PACKS M1673 AND M1671 TO FAIL CAPACITY CHECKS. GROUNDED - YES. EMERGENCY LIGHTING BATTERY PACKS M1673 & M1671 REMOVED AND REPLACED PER AMM 33-51-06-960-805. TWO MIG-51A TAGS INSTALLED AND REMOVED. OPS CHECKSDR ASAA2023071944123Indicator · brokenEMERGENCY LT COVER O/W EXIT COVER IS MISSING. ROW 16 DEF. GROUNDED - YES. REPLACED DEFECTIVE (BROKEN) EMERGENCY EXIT LIGHT ASSY PER MM 33-51-00-710-801, OPS CKS NORMAL. DEACT. REACT. CH 5 TABLE #3 ITEMS I AND 2. A/C GOOD FOR SVC.SDR ASAA2023061043517Lens · missingLOWER EMERGENCY EXIT LOWER PLACARD MISSING AT 17F. GROUNDED - YES. INSTALLED NEW LIGHT LENS COVER @ LOWER EMERGENCY LIGHT 17F.SDR ASAA2023052443386Oil System · leakingWHILE ACCOMPLISHING ASA TSR714364 FOUND FWD SUMP DRAIN LEAKING AT 1 DROP EVERY 3 SECOND AT IDLE. DURING PART POWER LEAK CHECK ON TSR, FWD SUMP DRAIN FILLED BAG AND BURST. PER 71-71-00-010-004-F00. SERVICEABLE LIMITS 20 DROP PER SECOND. ESN # 896-629 #1 ENGINE.SDR ASAA2023042142987Fuel Control · faultyFAULT LIGHT ILLUMINATED DURING APU START ATTEMPT AT FL 360 SUCESSFUL CSS ACCOMPLISHED AFTER FAULT LIGHT EXTINGUISHED. GROUNDED - YES. DURING APU BITE TEST FOUND MAINT MSG 49-31016 OVERTEMPERATURE SHUTDOWN IN FAULT HISTORY. NO FAULTS IN CURRENT STATUS. CONTINUESDR ASAA2023041442893Fmc · faultedRIGHT FMC FAIL IN FLIGHT AT FL360. VTK ON FO'S NAV DISPLAY, SINGLE FMC OPERATION MESSAGE IN SCRATCH PAD. STAYED FAILED FOR ABOUT A MINUTE AND THEN RETURNED TO NORMAL OPERATION. FMC SWITCH REMAINED IN NORMAL POSITION. GROUNDED - YES. REMOVED AND REPLACED FMCSSDR ASAA2023040742762Unknown · unknownF/A REPORTS R2 DOOR EXIT SIGN NEAR TRASH CAN FALLING OFF. GROUNDED - YES. RESECURED EXIT SIGN NEAR R2 DOOR AS REQUIRED, NO DEFECTS NOTED.SDR ASAA2023032642588Regulator · leakingPER TC NG-36WC-00002-2 STEP L (REVERSE FLOW DIAPHRAGM LEAK CHECK), HIGH STAGE REGULATOR REQUIRES REPLACEMENT. GROUNDED - YES. REMOVED AND REPLACED HSR REF B737-800 AMM 36-11-07 OPS CHECK GOOD.SDR ASAA2023032542578Valve · leakingFOLLOW-UP TO REPORT OF #2 (RH) BLEED TRIP ISSUE DURING NO-BLEEDS TAKEOFFS, ACCOMPLISH RIGHT ENG PNEUMATIC SYSTEM HEALTH CHECK PER TASK CARD NG-36WC-00002-2 GROUNDED - YES. PERFORMED #2 ENGINE BLEED AIR SYSTEM HEALTH CHECK UP TO AND INCLUDING STEP 04.P ON PAGE SDR ASAA2023032442552Unknown · unknownSATCOM LOCK-UP. GROUNDED - YES. SATCOM LOCK-UP PROCEDURE ACCOMPLISHED.SDR ASAA2023032042433Unknown · unknown17F LOWER EXIT LIGHT / SIGN BROKEN. GROUNDED - YES. RE-SECURED 17F LOWER EXT LIGHT SIGN PER B737-800 AMM 33-51-00 OPS TEST NORMAL.SDR ASAA2023031542394Actuator · faultedRIGHT PACK LIGHT STAYS ILLUMINATED ON RECALL. GROUNDED - YES. FOUND R/H RAM AIR DOOR FAULT AND HISTORY OF THE SAME FAULT. REMOVED AND REPLACED RH RAM AIR INLET ACTUATOR IN REF TO B737-800 AMM 21-51-21. OPS CHECK GOOD IN REF TO AMM 21-61-00. NO FAULTS DETECTED.SDR ASAA2023031242343Unknown · unknownRH PACK LIGHT ILLUMINATES, ON M/C RESET IT EXTINGUISHES. GROUNDED - YES. PERFORMED B737-800 FIM 21-62 TASK 801. PREVIOUS FLY INDICATED R/H RAM AIR ACTUATOR FAULT. RAN VERIFICATION TEST. TEST PASSED RAN PACKS, OPS CHECK GOOD.SDR ASAA2023031042312Bolt · unknownFO SIDE FLIGHT DECK EMERGENCY ESCAPE WINDOW IS VERY DIFFICULT TO OPEN. GROUNDED - YES. STARTED FO WINDOW ADJUSTMENT PER B737-800 AMM 56-12-11-820-801(12) REPLACED FWD BOTTOM SPECIAL BOLT THREADS RUINED. NEEDS TO BE RETHREADED. REPLACED FWD LOWER ROLLER AND BOL
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