N538AS
Service difficulty reports · 345
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 = 'N538AS' 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 = 'N538AS' 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 ASAA2026090368923Web · corrodedAFT PIT CARGO SILL WEB HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT LIMITS, REMOVED AND REPLACED AFT PIT CARGO SILL WEB IAW B737-800 SRM 51-40-02-0G-0 STEP 5.B(1,2).SDR ASAA2026090368922Cargo Track · corrodedAFT CARGO TRACK INBD OF SILL WEB HAD CORROSION. GROUNDED - YES. REMOVED DAMAGE, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2, REPAIRED AFT CARGO TRACK INBD OF SILL WEB IAW SRM 53-00-53-2R.SDR ASAA2026090368753Door Sill · corrodedFWD CARGO SILL WEB HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED FWD CARGO SILL WEB P/N 654A0003-58 T/N AS62881 IAW SRM 51-40-02-0G-0.SDR ASAA2026050765947Power Supply · inoperativeFORWARD RT GALLEY EMERGENCY LIGHTS INOP. GROUNDED - YES. REMOVED AND REPLACED POWER SUPPLY M02816 REF AMM 33-51-06. FORWARD R/H GALLEY EMERGENCY LIGHTS OPS CHECK GOOD REF AMM 33-51-06.SDR ASAA2026050765946Power Supply · inoperativeLEFT HAND OVERWING EMERGENCY EXIT SIGNS ABOVE DOORS, FORWARD LEFT-HAND LOWER EXIT LIGHT AND FORWARD RIGHT-HAND LOWER EXIT LIGHT INOP. GROUNDED - YES. REMOVED AND REPLACED EMERGENCY POWER SUPPLY M1694 AND OPS CHECK GOOD IAW B737 AMM 33-51-06-960-806.SDR ASAA2025110462085Cover · missingDURING DEPLANING, FOUND EMERGENCY EXIT LIGHT COVER MISSING ON ROW 16A. GROUNDED - YES. REPLACED EMERGENCY EXIT LIGHT REF AMM 33-51-01. OK FOR SVC.SDR ASAA2025101761713Light · no discrepancyEMERGENCY LIGHTS ON WHEN EMERGENCY LIGHT SWITCH IN ARMED POSITION. GROUNDED - YES. C/W EMERGENCY LIGHT OPS CK+ NO DEFECTS NOTED REF AMM 33-51-00. SEAMC WILL NOTIFIED.SDR ASAA2025082960921Angle · corrodedWHILE GAINING ACCESS FOR REPAIR IN AFT CARGO FOUND AREAS OF CORROSION ON LH TRANSITION FROM FS727 TO FS 849. GROUNDED - YES. REMOVED CORROISON FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2 FIG 103 FABBED , LOCATED & DRILLED NEW LH TRANSITION IAW B73SDR ASAA2025082860922Transition Panel · corrodedWHILE GAINING ACCESS FOR REPAIR IN AFT CARGO FOUND AREAS OF CORROSION ON RH TRANSITION FROM FS 727 TO FS 767. GROUNDED - YES. REPAIRED TRANSITION FROM F.S 727 TO FS 767 IAW BOEING 737-800 SRM 53-00-53-2R-5W= 1' O= .040" R= .000 L= 3" D= .040.SDR ASAA2025070559190Cover · missingMID CABIN EXIT SIGN BACKSIDE OF SIGN IS MISSING. GROUNDED - YES. FOUND EXIT SIGN COVER. RE-INSTALLED EXIT SIGN COVER AND OP CHECK GOOD PER AMM 25-21-20.SDR ASAA2025060358436Handle · bindingL1 DOOR HANDLE OPENING FORCE TOO HIGH- 480 LBS. GROUNDED - YES. REMOVED L1 DOOR SLIDE ASSY AND LINER. ADJUSTED HORIZ CONTROL ROD. REF AMM 52-11-00-820-801 STEP 2K. REINSTALLED L1 DOOR LINER PER AMM 52-11-31. REINSTALLED L1 DOOR SLIDE PER AMM 25-66-01. L1 DOOR SDR ASAA2025052158106Cover · detachedEXIT COVER IS OFF FROM EMRG ROW. GROUNDED - YES. REINSTALLED SIGN AS REQ'D NO DEFECTS NOTED.SDR ASAA2025010555110Rod · disconnectedL1 DOOR WILL NOT OPEN. GROUNDED - YES. FOUND L1 DOOR ROD ASSY DISCONNECTED FROM LATCH TORQUE TUBE. RE-INSTALLED L1 DOOR LOWER ROD ASSY PER IPC 52-11-11-03A, AND TORQUE ROD ASSY BOLT PER AMM 20-50-11-910-801 TABLE 209. REMOVED AND RE-INSTALLED PER AMM 52-11-31-SDR ASAA202401247452Sign · detachedR1 EXIT SIGN FELL OFF. GROUNDED - YES. FOUND R-1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY BROKEN, REMOVED AND REPLACED ASSEMBLY REF AMM 33-51-01, OPS CKECK GOOD. REFM AMM 33-51-00.SDR ASAA2023112146334Unknown · unknownAFT GALLEY A/C LEFT LIGHT COVER BROKEN. GROUNDED - YES. REPLACED LAV D AFT BULKHEAD FWD FACING WORK/EMERGENCY LIGHT ASSY AS REQ. OPS CHECKED GOOD REF AMM 33-51-00.SDR ASAA2023110746068Relay · faultyWHILE ACCOMPLISHING T/C 78273000, FOUND ENG. 2 LONG TIME FAULT MSG.# 76-31362, THE START LEVER SIGNALS DISAGREE. GROUNDED - YES. (RESOLVED ON W/O: 1976254 TASKCARD: N/R-00002 ) PERFORMED EEC TEST PER FIM 76-11 TASK 801 NO FAULTS FOUND DUE TO HISTORY REPLACED ESDR ASAA2023110546008Unknown · unknownZONE TEMP CAUTION ILLUMINATED ON MASTER RECALL CHECK. EXTINGUISHED UPON MASTER CAUTION RESET. GROUNDED - YES. (RESOLVED ON W/O: 1976284 TASKCARD: N/R-00001 ) PERFORMED BITE PROCEDURE NO DEFECTS NOTED AT THIS TIME PER AMM 21-62 TASK 801 THIS REMOVES MEL 21-21G SDR ASAA2023102345793Unknown · unknownREF TC 78273000. #1 ENG FAULT DISPLAYS SHORT TERM 75-30451, THE VBV POSTITION SIGNALS DISAGREE. GROUNDED - YES. (RESOLVED ON W/O: 1975071 TASKCARD: N/R-00001 ) PERFORMED FIM 75-32 TASK 803. ENG #1 EEC BITE TEST SHOWS NO FAULTS IN THE LAST 10 LEGS HISTORY. THISSDR ASAA2023100945547Unknown · unknownENGINE #2 LONG TIME FAULT MSG #76-31362 THE START LEVER SIGNALS DISAGREE. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023100745480Control Module · faultyUNABLE TO SELECT LANDING ALTITUDE. LANDING ALTITUDE FROZEN WITH KNOB SELECTOR MOVING. GROUNDED - YES. REMOVED AND REPLACED PRESSURE SELECTOR UNIT REF B737-800 AMM 21-31-02/401. PERFORMED PRESSURIZATION SYS GROUND TEST OF AMM TASK 21-31-00-700-802. BOTH TEST SUSDR ASAA2023100445442Unknown · unknownON ENG #2; LONG TIME FAULT 76-31362 THE START LEVER SIGNALS DISAGREE. GROUNDED - YES. (RESOLVED ON W/O: 1971953 TASKCARD: N/R-00005 ) REF L/P 60165285, ACCOMPLISHED FIM 76-11 TASK 801 FAULT ISOLATION, OPS CK NML. AIRCRAFT RELEASED FROM PLT DEFERRAL, C/N 040165SDR ASAA2023100445441Unknown · unknownON ENG #1; SHORT TIME FAULT 75-20451 THE VBV POSITION SIGNALS DISAGREE. GROUNDED - YES. (RESOLVED ON W/O: 1972527 TASKCARD: N/R-00001 ) PERFORMED FIM 75-32 TASK 803 AND NO ACTIVE FAULTS FOUND. FAULT DETERMINED TO BE INTERMITTENT. THIS CLEARS PLT ENG 1 SHORT TISDR ASAA2023100245431Unknown · unknownAT CRUISE FL320 CA "LDG ALT" FLAG AND CA "NO VTK" FLAG ILLUMINATED. CLEARED W/IN 15 SECONDS W/O INTERVENTION. GROUNDED - YES. FOUND TO BE AN INTERMITTENT FAULT. NO HISTORY. ACCOMPLISHED FMC TEST. CYCLED POWER ON A/C REF FIM 34-61 TASK 801 & 837. SEAMC CHRIS.SDR ASAA2023092545295Unknown · unknownENG LOOP "B" (FIRE LOOP) SHOWS FAULT DURING TEST. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023092445300Unknown · unknownF/O'S DME IS INOP. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023090745047Floor Panel · puncturedMAIN CABIN FLOOR BOARD P/N 143A5810-517 R/H SIDE JUST AFT OF FWD WET AREA HAS PUNCTURE. GROUNDED - YES. EVALUATED MAIN CABIN FLOOR BOARD P/N 143A5810-517 AND FOUND 1 EA PUNCTURE AND EDGE DAMAGE TO AFT EDGE OF PANEL ON RH SIDE. ALSO FOUND HAIL STRIKE DAMAGE THRSDR ASAA2023082544983Intercostal · corrodedMAIN CABIN FWD WEB AREA STA 300 LBL 11 INTERCOSTAL HAS CORROSION ON UPPER SURFACE. GROUNDED - YES. REMOVED CORROSION ON INTERCOSTAL. ORIG THICKNESS IS .071",REMOVED .016"WITH 0.055' REMAININGFOUND OUT OF LIMITS IAW B737-800 SRM 53-10-51-1A-1.REMOVED AND REPLACSDR ASAA2023082444881Floorboard · delaminatedFWD WET AREA BOARD DELAM P/N 141A5810Y183. GROUNDED - YES. EVALUATED & ACCOMPLISH PERMANENT REPAIR TO FWD WET AREA FLOOR BOARD P/N 141A5801Y183 IAW B737-800 SRM 53-00-50-1A-1, 53-00-50-2R-01, 53-00-50-2R-6.SDR ASAA2023082244982Frame · gougedAFTER REMOVAL OF LOWER SEAL RETAINER/LOCATOR AND SEALANT ON L1 DOR FOUND GOUGED FRAME. GROUNDED - YES. REMOVED DAMAGED FRAME, REFERENCE B737-800 SRM 51-40-02, LOCATED & DRILLED NEW FRAME, REFERENCE B737-800 SRM 51-40-02 & BAC DWG 141A6185 REV D & 141A6101 REV SDR ASAA2023082244869Floorbeam · corrodedMAIN CABIN AFT WET AREA STA986.5 FLOOR BEAM AT LBL 43 HAS CORROSION AT FASTENER HOLE. GROUNDED - YES. REMOVED CORROSION.ORIGINAL THICKNESS 0.150 IAW B737-800 SRM 53-70-51-0I-1.REMAINING THICKNESS 0.085,REMOVED 0.065.OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1SDR ASAA2023082244868Floorbeam · corrodedMAIN CABIN AFT WET AREA STA 986.5 FLOOR BEAM AT RBL43 HAS CORROSION AT FASTENER HOLE. GROUNDED - YES. REMOVED CORROSION.ORIGINAL THICKNESS 0.150 IAW B737-800 SRM 53-70-51-0I-1.REMAINING THICKNESS 0.90.REMOVED 0.060.OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1.SDR ASAA2023081945127Floor Support · corrodedAFT PIT FLOOR SUPPORT STA 787 TO 832 RBL 13.84 IS CORRODED. GROUNDED - YES. REMOVED THE CORROSION FROM THE AFT PIT FLOOR SUPPORT STA 787 TO 832, RBL 13.84 IAW B737-800 SRM 53-00-53-1A-2.D. ORIG THICKNESS IS .070 IAW B737-800 SRM 53-60-53-01-2 TABLE 2. REMOVED SDR ASAA2023081944981Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL STA 727I+10 TO 835 IS CORRODED GROUNDED - YES. EVALUATED AFT PIT L/H TRANSITION PANEL STA 727I+10 TO 835 ORIGINAL MAT'L THKS .040 PER BOEING PROFILE DWG BAC 1496-377 RENIVED .007 MAT'L REMAINING .033 FOUND TO BE OUT OF LIMITS IAW ASDR ASAA2023081944980Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL STA 727E+18 TO 727I+10 IS CORRODED. GROUNDED - YES. EVALUATED AFT PIT L/H TRANSITION PNL FROM ST 727E+18 TO 727I+10 ORIGINAL MATERIAL THICKNESS .040 PER BOEING PROFILE DWG BAC 1496-377 REMOVED .018 MATERIAL REMAINING .022 FOUND TO SDR ASAA2023081944884Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL STA 727B+10 TO 727E+18 IS CORRODED GROUNDED - YES. EVALUATED AFT CARGO L/H TRANSITION PANEL FROM STA 727B+10 TO 727E+18. ORIG THICKNESS IS .040 PER BOEING PROFILE DWN BAC1496-377. REMOVED .008. REMAINING .032, FOUND TO BE OUT OF LISDR ASAA2023081944883Transition Panel · corrodedAFT PIT R/H TRANSITION PANEL STA 727E+14 TO 727H+12 IS CORRODEDDOT T222. GROUNDED - YES. EVALUATED AFT CARGO R/H TRANSITION PANEL FROM STA 727E+14 TO 727H+12 ORIG. MAT THKS .040" PER BOEING PROFILE DWG BAC 1496-377, REMOVED .008" MAT'L, REMAINING .032" FOUND TSDR ASAA2023081944882Transition Panel · corrodedAFT PIT R/H TRANSITION PANEL STA 737 TO 767 IS CORRODEDDOT J164. GROUNDED - YES. EVALUATED AFT CARGO R/H TRANSITION PANEL FROM STA 737 TO 767. ORIG THICKNESS .040 PER BOEING PROFILE DWG BAC 149-377, REMOVED .006. REMAINING .034, AND IS FOUND TO BE OUT OF LIMITSDR ASAA2023081844867Transition Panel · corrodedFWD PIT R/H TRANSITION PANEL STA 500+12 TO 500F+10 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM FWD PIT R/H TRANSITION PANEL IAW B737-800 SRM 53-00-53-1A-2.2.D. ORIG. THICKNESS: .040 IAW B737-800 SRM 53-30-53-IO-2. REMOVED: .006, REMAINING: .034 & IS FOUSDR ASAA2023081844866Transition Panel · corrodedFWD PIT R/H TRANSITION PANEL STA 500H+10 TO 500H+18 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM FWD PIT R/H TRANSITION PANEL IAW B737-800 SRM 53-00-531A-2.2.D. ORIG. THICKNESS: .040 IAW B737-800 SRM 53-30-53-0I-2. REMOVED: .007, REMAINING: .033 & IS FOUSDR ASAA2023081844864Transition Panel · corrodedFWD PIT R/H TRANSITION PANEL STA 500B+10 TO 500C+14 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE ON FWD PIT TRANSITION PANEL @ STA 500B+10 TO 500C+14 IAW B737-800 SRM 53-00-53-1A-2.2.D. ORIG. THICKNESS: .040 IAW B737-800 SRM 53-30-53-0I-2. REMOVD: .006, REMAISDR ASAA2023081844761Transition Panel · corrodedFWD PIT L/H TRANSITION PANEL STA 500B+18 TO 500D+10 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM FWD PIT L/H TRANSITION PANEL @ STA 500B+18 - 500D+10 IAW B737-800 SRM 53-00-53-1A-2.2.D. ORIG. THICKNESS: .040 IAW B737-800 SRM 52-30-53-0I-2. REMOVED: .006 SDR ASAA2023081144553Unknown · unknownENGINE 1 FAULT CODE 75-20451 VBV POSITION SIGNALS DISAGREE SHORT TIME FAULT DISCOVERED WHILE ACCOMPLISHING T/C 78273000. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023081144552Unknown · unknownENGINE FAULT CODE 75-10451 VBV POSITION SIGNALS DISAGREE SHORT TIME FAULT DISCOVERED WHILE ACCOMPLISHING T/C 78273000. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023072044144Unknown · unknown#2 ENG LONG TIME FAULT. FAULT CODE 76-31362. THE START LEVER SIGNALS DISAGREE. GROUNDED - YES. ACCOMPLISHED TC 78273000, FAULT IS GONE, AND NO HISTORY THIS CLEARS PLT, SEAMC ANDY NOTIFIED.SDR ASAA2023071444048Indicator · inoperativeFUELER REPORTS REFUEL PANEL INDICATOR FOR CENTER TANK READS "FAIL". GROUNDED - YES. VERIFIED CNTR TANK REFUEL INDICATOR SHOWS "FAIL" ACCOMPLISHED WIRE CHECKS PER B737-800 FIM 28-21-805 NO DEFECTS NOTED REPLACED CNTR TANK REFUEL INDICATOR REF B737-800 AMM 28-41SDR ASAA2023071143994Unknown · unknownDURING TC 78273000 FOUND TWO SHORT TIME FAULTS CODES FOR # 1 ENGINE. CODE 75-20451 " VBV POSITION SIGNALS DISAGREE." AND CODE 75-10451 " VBV POSITION SIGNALS DISAGREE.". GROUNDED - YES. (RESOLVED ON W/O: 1961364 TASKCARD: N/R-00002 ) FOLLOWED FIM 75-32-805 NO.SDR ASAA2023062643773Unknown · unknownDURING TASK CARD 78273000 FOUND #1 ENG SHORT TIME FAULT MSG #75-30451THE VBV POSITION SIGNALS DISAGREE. GROUNDED - YES. PERFORMED T/C 78273000, VERIFIED FAULT MSG 75-30451 IS NOT LOGGED FOR THE LAT 8 FLT LEGS ON #1 ENG. REF FIM TASK 75-32 TASK 803, #1 EEC BITESDR ASAA2023060943518Indicator · failedCENTER FUEL TANK QUANTITY BLANK. GROUNDED - YES. PERFORMED B737-800 FIM 28-41 TASK 810 REMOVED AND REPLACED CENTER REFUEL QUANTITY INDICATOR ASSY REF B737-800 AMM TASK 28-41-61-000/400-801 AND FUEL QUANTITY PROCESSOR UNIT REF AMM 28-41-81-000/400-801 OPS TEST SDR ASAA2023051343227Unknown · unknownL/H AFT BODY VORTEX GENERATOR ABOVE H/STAB BROKEN OFF AT BASE. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023050443143Fmc · faultyREF LP 60591300-FMC SINGLE OPERATION ON SCRATCH PAD, FO MAP FIGURE FLAG AND VTR ON NAV DISPLAY. GROUNDED - YES. REMOVED AND REPLACED R/H FMC COMPUTER PER B737-800 AMM 34-61-02 ALL SOFTWARE AND OPERATONIAL CHECKS OK.
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