N564AS
Service difficulty reports · 539
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 = 'N564AS' 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 = 'N564AS' 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 ASAA2019071630125Tube · clogged<SEA>G.E. DIAGNOSTIC REPORTS #1 ENGINE ESN804748 HAS HAD A SUDDEN INCREASE IN OIL PRESSURE. CNR ISSUED. GROUNDED - YES. PERFORMED EEC BITE CK FIM 73-00 TASK 801, NO FAULT MESSAGE. EXAMINED ELECTRICAL CONNECTOR @ OIL PS SENSOR, NORMAL. NO DEFECT NOTED. INSPECTSDR ASAA2019071430027Wire Harness · failedFOLLOW UP TO HISTORY OF #2 ENGINE FIRE LOOP A FAULTS GROUNDED - YES. PERFORMED FIM 26-10 TASK 805 AND COULD RESISTANCE TO FLUCTUATE ON D998 PINS 24-25 FRIN 2.5 OHMS TO 7 OHMS BY MANIPULATING MW0315 HARNESS. REPLACED HARNESS IN REF TO AMM 26-11-02.SDR ASAA2019070729971Module · intermittentREF LP 12160592 - #2 ENG FIRE WARNING LIGHT DOES NOT TEST. GROUNDED - YES. REF TSR 703262 FOR TROUBLESHOOTING C/W BITE TEST REF FIM 26-10 TASK 801. NO FAULTS FOUND. RERACKED M279 MODULE IN E&E BAY, REF AMM 26-10-00 NO HELP. WHILE CHECKING CKPT FIRE PANEL FASTESDR ASAA2019062929865Connector · dirtyDURING PREFLIGHT #2 FIRE HANDLE LIGHT DOES NOT ILLUMINATE DURING FIRE/OVERHEAT TEST. GROUNDED - YES. REFERENCE FIM 26-10 TASK 810, INSPECTED AND CLEANED # 2 ENGINE FIRE LOOP DETECTOR CONNECTIONS. RE-ACCOMPLISHED FIRE WARNING TESTS, TEST PASSED.SDR ASAA2019062929861Control Unit · malfunctionedELEC LIGHT ILLUMINATED ON OVERHEAD PANEL DURING PREFLIGHT. GROUNDED - YES. REFERENCE FIM 24-31 TASK 801. PERFORMED ELECTRIC LIGHT BITE TEST. FOUND SPCU INOP FAULT, CYCLED SPCU C/B'S RE-PERFORMED BITE TEST, FAULT CLEARED AND ELECTRIC LIGHT WENT OUT.SDR ASAA201906129674Switch · malfunctionedDURING ENG FIRE TEST THE #2 ENG FIRE SWITCH DOES NOT ILLUMINATE. GROUNDED - YES. PERFORMED ENGINE/APU FIRE DETECTION CONTROL MODULE BITE REFERENCE B737-800 FIM 26-10 TASK 801. TEST PASS. OPERATED ENG 2 AT IDLE FOR FIVE MINUTES REFERENCE AMM 71-00-00 AND ACCOMPSDR ASAA2019052029385Fuel Nozzle · defectiveAPU CT5ATP EGT TREND DATA SHOWS EGT HAS SHIFTED ABOVE THE MAINTENANCE THRESHOLD OF 593 BUT LESS THAN 605 DEGREES. ACCOMPLISHMENT OF LISTED MAINT. TASK WILL EFFECT APU ON DEMAND IN FLIGHT START CAPABILITY. CONTACT MAINTENANCE CONTROL. GROUNDED - YES. ACCOMPLISHSDR ASAA2019051429337Spacer · debondedNR 1 ENGINE, SPACERS 19, 21, 24 ELASTOMER DISBONDED AT 2 LOCATIONS REF T/C 78472010. GROUNDED - YES. REPLACED NR 1 ENG SPACERS 19, 21 AND 24 PER T/C 78472010.SDR ASAA2019031728661Outflow Valve · inoperativeFLIGHT ATTENDANTS REPORTING CONTINUOUS LOUD SQUEAL FROM R2 DOOR. IT BEGAN 10 MINUTES AFTER DEPARTURE AND HAS PROGRESSIVELY BECOME LOUDER DURING FLIGHT, PRESSURIZATION IS NORMAL. FLIGHT ATTENDANTS STATE IT DOES AFFECT COMMUNICATION. GROUNDED - YES. REMOVED AND SDR ASAA2019030628518Unknown · malfunctionedCANNOT TRANSMIT ON HF 1 RADIO FROM EITHER AUDIO CONTROL PANEL. ALL OTHER FUNCTIONS APPEAR NORMAL, INCLUDING TRANSMIT ABILITY FROM HF 2. GROUNDED - YES. CYCLE POWER TO THE NR 1 HF TRANSCEIVER IAW AMM 20-60-99. ACCOMPLISHED OPS CHECK OF NR 1 HF IAW FIM 23-11-TASSDR ASAA2019020628078Transceiver · intermittentWHILE TAXING OUT. CHECK OF HF RADIOS. NR 2 HF WOULD NOT TUNE OR TRANSMIT. GROUNDED - YES. NR 2 HF TRANSCEIVER FAULTS BITE INTERMITTENTLY. REPLACED NR 2 TRANSCEIVER REF AMM 23-11-21-000-801. GROUND VERIFICATION TEST NORMAL.SDR ASAA20181227550Control Valve · faultedRT PACK LIGHT COMES ON W/ RECALL EXTINGUISHES WITH RESET. GROUNDED - YES. PERFORMED BITE CHECK OF #2 PACK/ZONE TEMP CTRL SHOWS "TCV-THIS PACK" LAST FLIGHT, REF B737-800 FIM 21-62 TASK 801. FAULT CLEARS. RE-PERFORMED RH PACK TEMP CONTROL BITE PROCEDURE, CONFIRMSDR ASAA2018122437508Warning Light · false activationAUTO FAIL AND ALTN LIGHTS ARE ILLUMINATED ON PRESSURIZATION PANEL WITH AUTO POSITION SELECTED. GROUNDED - YES. MOVED PRESSURIZATION MODE SELECTOR TO "MAN" AND BACK TO "AUTO", LIGHT REMAINS EXTINGUISHED. THIS CORRECTS FAULT.SDR ASAA2018122437506Valve · faultedDURING AFTER START CHECKLIST WHEN RECALL PUSHED THE AIR COND AND CABIN ZONE TEMP LIGHTS ILLUMINATED. LIGHTS EXTINGUISHED WHEN MASTER CAUTION RESET. CHECKLIST COMPLETED. GROUNDED - YES. BITE CKD BOTH PTC #2 ON BIT & PREV FLT FLT DECK TRIM VALVE FAULTED WITH A GSDR ASAA201812267516Coupler · failedUNABLE TO TRANSMIT HF 2. GROUNDED - YES. REPLACED HF COUPLER #2 REF B737-800 AMM 23-11-61 TESTED NORMAL CLEARS MEL 23-11A.SDR ASAA2018112637056Backlight · malfunctionedMCP HAS NO LIGHTING. THIS OCCURED AFTER EXTERNAL POWER WAS INTERUPTED SEVERAL TIMES. GROUNDED - YES. VERIFIED DEFECT, CYCLED A/C PWR REF B737-800 AMM 20-60-99, MCP LIGHTING WAS RE-ESTABLISHED. ACCOMPLISHED DFCS AUTO TEST AND BITE B737-800 FIM 22-11 TASK 801 NOSDR ASAA2018102226588Idg · leakingFOUND NR 1 ENG LEAKING OIL AFTER SHUTDOWN AT GATE. GROUNDED - YES. REMOVED AND REPLACED NR 1 IDG IAW AMM 24-11-11-000/400-801.SDR ASAA2018101826546Warning System · false activationZONE TEMP CONTROL CAB ILLUMINATED. QRH PROCEDURE COMPLETED LIGHT EXTINGUISHED. GROUNDED - YES. PERFORMED AMM TASK 21-61-00-700-808-001. BITE TEST. CHECKED GOOD. NO FAULT NOTED. ALSO RESET BOX. OPS NORMAL.SDR ASAA2018101626494Not Reported · meltedNR 1 ENGINE WAS OBSERVED TO HAVE MELTED MATERIAL ON THE FRONT COMPRESSOR CASE BETWEEN THE 2ND AND 3RD STAGE VSV ACTUATION RINGS FROM APPROX THE 4 O’CLOCK TO 2 O’CLOCK POSITION. GROUNDED - YES. REMOVED AND REPLACED NR 1 ENGINE.SDR ASAA2018101626492Bonding Wire · frayedNR 1 ENGINE COWL THERMAL ANTI-ICE VALVE BONDING WIRE IS FRAYED. GROUNDED - YES. REPLACED NR 1 ENG COWL THERMAL ANTI-ICE VALVE BONDING WIRE PER CFM56-7 POWER PLANT BUILDUP MANUAL 71-00-02 FIG 27-1 PGS 2 & 3. AND ALSO AMM 30-21-11.SDR ASAA2018101526477Control Valve · intermittentON RECALL PRIOR TO DESCENT THE LEFT PACK LIGHT ILLUMINATED, WHEN MASTER CAUTION IS RESET LIGHT EXTINGUISHES. GROUNDED - YES. PERFORMED PZTC BITE PROCEDURE REF FIM 21-62 TASK 801 ON LT PZTC. PREV FLIGHT LOGGED TCV VALVE FAULT. REMOVED AND REPLACED LT PACK TCV VSDR ASAA2018101526437Actuator · leakingNR 1 ENGINE HAS HISTORY AND REPORTS OF FUEL LEAKS FROM THE LEFT VSV ACTUATOR DRAIN. GROUNDED - YES. REMOVED AND REPLACED NR 1 ENGINE LT VSV ACTUATOR. OPS/LEAK CHECKS NORMAL REF AMM 75-31-01.SDR ASAA2018100826401Indicator · abnormalREFUEL PANEL CENTER FUEL QTY GAUGE TEST PATTERN NOT CORRECT. GROUNDED - YES. BOTTOM ROW OF 8'S MISSING DURING TEST. REPLACED CTR TANK REFUEL QTY IND. DID NOT HAVE TO REMOVE PNL. OPS CHECK SAME GOOD. REF AMM 28-41-61. CLEARED MEL 28-12B.SDR ASAA2018092526310Module · faultySAT PHONE INOP. UNABLE TO SELECT ANY NUMBER FROM DIRECTORY TO SAT-1 OR SAT-2. "-NO NUMBER-" ON BOTTOM OF SAT-PHONE 1/2. "BITE OK" ON SAT PHONE 2/2. GROUNDED - YES. VERIFIED DISCREPANCY. AFTER SELECTING A DISPATCH FROM GEN DIRECTORY, SAT-1 AND SAT-2 SHOW "NOT RSDR ASAA2018092426214Power Supply · inoperativeEXTERNAL EMERGENCY EXIT LIGHT INOP AT FWD LEFT OVERWING EMERGENCY EXIT. GROUNDED - YES. EXTERNAL EMERGENCY LIGHT POWER PACK REPLACED & OPS CHECK GOOD IAW AMM 33-51-06-960-806.SDR ASAA2018092426202Power Supply · inoperative'CUSTOMER WALK' EMERGENCY CABIN LIGHT AT FOLLOWING LOCATION INOP ROW 6 ABC, 9 ABC AND 11 ABC. GROUNDED - YES. EMERGENCY CABIN LIGHT POWER PACK ASSY M2335 REPLACED (SN: 33706) IAW AMM 33-51-06-960-806 OPS CHECK GOOD.SDR ASAA2018092426200Power Supply · inoperativeR1 DOOR EMERGENCY LIGHTS INOP. GROUNDED - YES. REMOVED AND REPLACED M1674 POWER SUPPLY S/N 13913 IAW AMM 33-51-06-960-806. OPS CHECK GOOD.SDR ASAA2018091726127Intercostal · crackedMAIN CABIN FLOOR INTERCOSTAL AT BS 344 TO BS 360, LBL 11 CRACKED AT UPPER FLANGE HOLES. GROUNDED - YES. RECIEVED NEW INTERCOSTAL P/N 141A5410U148 PO: 904730.2, LOCATED, DRILLED AND DEBURRED IAW BAC DWG 141A5400 REV A.SDR ASAA2018091926164Floorbeam · corrodedMAIN CABIN FLOORBEAM AT BODY STATION 947.5 CORRODED AT LBL 16. GROUNDED - YES. REMOVED CORROSION IAW SRM 53-70-15-1A-1 FIG 104 DET D. ORIGINAL THICKNESS .180" REMOVED, .059" REMOVING .121" FOUND TO BE OUT OF LIMITS. FABRICATED, MODIFIED, ALODINED, PRIMED, AND SDR ASAA2018082426182Strap · corrodedMAIN CABIN RIGHT HAND SIDE STRAP IS CORRODED STA 1021 RBL4. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN STRAP AT FS 1021 RB24 P/N 147A571484 IAW SRM 51-40-02 AND BAC DWG 147A5700, FOUND TO BE BEYOND ALLOWABLE LIMITS REF SRM 53-70-51.SDR ASAA2018091926171Intercostal · corrodedMAIN CABIN L2 DOOR DRAIN PAN FWD DRAIN LINE SUPPORT IS CORRODED. GROUNDED - YES. RECIEVED NEW P/N 147A5660Y21, LOCATED, DRILLED, AND DEBURRED PER BAC DWG 147A5650 REV A TO BE INSTALLED ON N/R, CUST CARD. FOUND TO BE BEYOND ALLOWABLE LIMITS REF SRM 53-70-51.SDR ASAA2018091926170Strap · corrodedMAIN CABIN RIGHT HAND SIDE STRAP IS CORRODED STA 1018 - 1024 AT RBL 24. GROUNDED - YES. REMOVED AND REPLACE MAIN CABIN STRAP AT FS 1018-1024 RBL 24 P/N 147A571483 IAW SRM 51-40-02 AND DWG 147A5700 FOUND TO BE BEYOND ALLOWABLE LIMITS REF SRM 53-70-51.SDR ASAA2018091926169Strap · corrodedMAIN CABIN LEFT HAND SIDE STRAP IS CORRODED STA 1028 AT LBL18. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN STRAP AT FS 1028 LBL18 P/N 147A5714U5 IAW SRM 51-40-02 AND DWG 147A5700, FOUND TO BE BEYOND ALLOWABLE LIMITS REF SRM 53-70-51.SDR ASAA2018091926166Web · corrodedMAIN CABIN LEFT HANDLE SIDE WEB AS SMALL AREA OF CORROSION STA 986.5 LBL 31. GROUNDED - YES. REMOVED CORR NO AVAILABLE LIMITS IN THIS AREA. ORIG .040 REMAIN .030 LOSS OF .010. REMOVED AND REPLACED WEB IAW 51-40-02. LOCATED AND DRILLED NEW WEB IAW BAC DWG 147A5SDR ASAA2018091926165Web · corrodedMAIN CABIN RIGHT HAND SIDE WEB IS CORRODED STA 1016 AT RBL 32. GROUNDED - YES. REMOVED CORR NO LIMITS AVAILABLE IN THIS AREA ORIG .040 REMAIN .028 LOSS OF .012. REMOVED AND REPLACED WEB IAW SRM 51-40-02. LOCATED AND DRILLED NEW WEB IAW BAC DWG 147A5700.SDR ASAA2018091726133Support · corrodedMAIN CABIN LEFT HANDLE SIDE GALLEY SUPPORT HAS SMALL AREA OF CORROSION STA 993 LBL 33. GROUNDED - YES. REMOVED ANGLE OUT OF LIMITS IAW SRM 51-40-02. LOCATED AND DRILLED NEW SUPPORT ANGLE. IAW BAC DWG 147A5700 REV A. INSTALLED NEW ANGLE IAW BAC DWG 147A5700 REVSDR ASAA2018091726132Support · corrodedMAIN CABIN RIGHT SIDE GALLEY SUPPORT HAS SMALL AREA OF CORROSION STA 995 RBL 33. GROUNDED - YES. LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-40-05. INSTALLED SUPPORT IAW SRM 51-40-02.SDR ASAA2018091726131Stiffener · corrodedMAIN CABIN STIFFENER RBL 16 BETWEEN FLOORBEAM 947.5 & 967.5 IS CORRODED AT FASTENER HOLE. GROUNDED - YES. REMOVED CORROSION ORIG. .075 REMAIN .066 LOSS OF .009. FOUND OUT OF LIMITS IAW SRM 53-705. REMOVED AND REPLACED STIFFENER IAW BAC DWG 147A5650.SDR ASAA2018091726130Floorbeam · corrodedMAIN CABIN FLOORBEAM STA 986.5 UPPER CAP IS CORRODED AT FASTENER HOLES NUMEROUS LOCATIONS. GROUNDED - YES. REMOVED CORROSION. ORIG. 150, REMAIN 125, LOSS OF .025. FOUND OUT OF LIMITS IAW SRM 53-70-57. ACCOMPLISHED T CAP REPAIR IAW SRM 53-70-51.SDR ASAA2018090526011Panel · crackedCABIN STA 540 LBL 24 TO BL 0 PANEL BREAK CRACKED. GROUNDED - YES. REMOVED AND REPLACED PNL BREAK AT STA 540 LBL 24 P/N 143A5240 U33 AND 143A5240 Y11 IAW SRM 51-40-02.SDR ASAA2018090425970Floor Support · crackedMAIN CABIN STA 538 RBL 2 FLOOR BOARD SUPPORT IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED FLOOR BOARD SUPPORT MAIN CABIN ON STA 538 RBL 2 IAW SRM 51-40-02 AND DWG 143A0060 REV A.SDR ASAA201808305951Floorbeam · corrodedMAIN CABIN FLOOR BEAM STA 328 UPPER CAP LOWER SURFACE IS CORRODED AT FASTENER HOLE RBL 50. GROUNDED - YES. REMOVED CORROSION ON FLOOR BEAM STA328 RB2-50. REMOVED .029 REMAINING .096 ORIGINAL THICKNESS .125 OUT OF LIMITS IAW B737-800 SRM 53-10-51. ACCOMPLISHED SDR ASAA2018082426201Floorbeam · corrodedCABIN FWD WET AREA SECT 41 STA 344 LBL 24 TO RBL 11 FLOORBEAM CORR ON UPPER FLANGE. GROUNDED - YES. REMOVED CORROSION ON FLOORBEAM UPPER FLANGE, FOUND TO BE BEYOND ALLOWABLE LIMITS (ORIG .125 REMOVED .060", REMAINING .065") REFERENCE SRM 53-10-51 AP1. REMOVED SDR ASAA2018091926168Intercostal · corrodedCABIN FWD WET AREA SECT 41 STA 328-344 LBL 11 INTERCOSTAL CORR UPPER FLANGE. GROUNDED - YES. RECEIVED NEW P/N 141A54104149. LOCATED, DRILLED, AND DEBURRED IAW DWG 141A5400. TO BE INSTALLED ON N/R, CUST CARD. NO LIMITS ALLOWABLE IN THIS AREA.SDR ASAA2018091726128Attach Angle · crackedLOWER ATTACH ANGLE, ATTACHED TO THE VERTICAL PRESSURE DECK WEB AT BS 663, LBL 25-LBL 45, CRACKED FROM WEB SLOT TO THE FIRST/LOWER INBOARD DOME NUT ATTACH FASTENER HOLE. GROUNDED - YES. REMOVED DAMAGE ON THE LOWER ATTACH ANGLE IAW SRM 51-10-02. ACCOMPLISHED HFESDR ASAA2018090526001Intercostal · crackedCABIN FWD WET AREA SECT 41 STA 312-328 RBL 34 INTERCOSTAL CRACKED UPPER FLANGE. GROUNDED - YES. REMOVED AND REPLACED CABIN FWD WET AREA SECTION 41 STA 312-328 RBL 34 INTERCOSTAL P/N 141A5410-12 PO:921708.1 IAW SRM 51-40-02 AND BAC DWG 141A5400.SDR ASAA2018090526000Intercostal · crackedCABIN FWD WET AREA SECT 41 STA 277-294 BL 0 INTERCOSTAL CRACKED UPPER FLANGE. GROUNDED - YES. REMOVED AND REPLACED CABIN FWD WET AREA SECT 41 STA 277-294 BL"0" INTERCOSTAL P/N 141A5410-139 P/O 923932.1 IAW SRM 51-40-02 AND BAC DWG 141A5400.SDR ASAA2018090425972Intercostal · crackedCABIN FWD WET AREA SECT 41STA 312-328 LBL 11 INTERCOSTAL CRACKED UPPER FLANGE. GROUNDED - YES. REMOVED INTERCOSTAL IAW SRM 51-40-02. LOCATED AND DRILLED INTERCOSTAL IAW 51-40-05. INSTALLED INTERCOSTAL IAW SRM 51-40-02.SDR ASAA2018083025950Bulkhead Web · crackedMAIN WHEEL WELL, STA 663 RBL 35, UPPER VERTICAL PRESSURE WEB HAS POSSIBLE CRACK. GROUNDED - YES. ACCOMPLISHED HFEC INSPECTION OF THE VERTICAL PRESSURE DECK WEB AT BS 663, RBL 25 - RBL 45 IAW B737 NDTM PART 6 51-00-00 PROCEDURE 23, FOUND A CRACK 1.500" IN THE CSDR ASAA2018070525284Regulator · failedNR 2 ENGINE FAILS TO MAINTAIN 32-42 PSIG DUCT PRESSURE WITH TLA GREATER THAN 60% N1. GROUNDED - YES. REMOVED & REPLACED NR 2 ENGINE BAR PER AMM 36-11-03-000/400-801. COMPLETED EA PWRPL-71EA-11276, NR 2 ENGINE SATISFIES N1/DUCT PRESSURE CRITERIA PER AMM 36-11-0
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