N560AS
Service difficulty reports · 562
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 = 'N560AS' 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 = 'N560AS' 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 ASAA11510051Filter · dirtyNR 1 ENG IDG PRESSURE DIFFERENTIAL PIN POPPED. DRAINED IDG & RMVD SCAVENGE CHG FILTERS REF AMM 24 11 41. INSP FILTERS REF AMM 24 11 41 200 801. INSTALLED FILTERS & LEAK CHECKED REF AMM 24 11 41 400 801.SDR ASAA11510035Flex Line · leakingBLEED AIR DUCT PRESSURE DIFFERENTAL LEFT 37 RIGHT 17 SINCE TAKEOFF CLIMB CRUISE AT FL 380. ACCOMPLISHED BLEED AIR SYSTEM HEALTH CHECK REF MM 36 11 00 700 801, FOUND BRAIDED FLEX LINE TO 450 THERMOSTAT LEAKING. REPLACED LINE. LEAK & OPS CHECK ACCOMPLISHED CHSDR ASAA1159816Unknown · malfunctionedON TAXI OUT FMC DISAGREE MESSAGE DISPLAYED ON CDU. ACCOMPLISHED QRH 11.0 MESSAGE WENT AWAY WITH QRH COMPLETE. FMC OPS NORMAL.SDR ASAA1159818Turbine Blades · damagedAPU CT5 ATP EGT TREND DATA SHOWS EGT HAS SHIFTED ABOVE THE ESTABLISHED THRESHOLD. ACCOMPLISHED APU ENG INSP REF AMM TASK 49 21 00 200 801 FOUND DAMAGE TO 2ND STAGE TURB BLADES TRAILING EDGES. APPEARS TO BE ALL BLADES. REPLACED APU PER T/C 78349010. LEAK ANSDR ASAA1159729Bulb · defectiveAPU TREND DATA CONTINUES TO REPORT CT5ATP EGT TEMPS THAT ARE HIGHER THAN EXPECTED. REPLACED T2 APU INLET TEMPERATURE REF AMM TASK 49 61 31.SDR ASAA1159674Control Panel · failedAUTOPILOT DISCONNECTED FOR NO REASON AT CRUISE BOTH IN CMD A & CDM B SEVERAL TIMES AT CRUISE. A&B LOGGED MCP FAILURES MSG 22 11627 AND 22 11607. REMOVED AND REPLACED MCP REF MM 22 11 34 OPS CHECK NORMAL. ACCOMPLISHED ALL MCP LWMP CHECKS REF LWMP CHECKLIST MSDR ASAA1159653Idg · failedNR 2 GEN SOURCE OFF LIGHT ILLUMINATED WOULD NOT RESET. REPLACED NR 2 IDG REF MM 24 11 11 & MM 24 11 11 090 801C3. PERFORMED OPERATIONAL CHECK REF MM 24 11 00. OPS AND NO LEAKS OKAY.SDR ASAA1159467Detector · failedAPU FIRE DETECT SYSTEM INOP. MASTER CAUTION ANNUNCIATOR PANEL ILLUMINATED WITH MASTER CAUTION LIGHT. APU DETECT INOP LIGHT ILLUMINATED STEADY ON FIRE DETECTION PANEL ON CENTER CONSOLE. REMOVED AND REPLACED APU TAILPIPE DETECTOR IAW AMM 26 15 01 000 802 AND SDR ASAA1159466Warning System · malfunctionedAPU DET INOP LIGHT ILLUMINATED ON DESCENT APU WAS OFF. RESET APU FIRE DETECTION CB C403. RE-RACKED APU FIRE DETECTION MODULE. UNABLE TO DUPLICATE MALFUNCTION IAW MM 26 15 00 710 801.SDR ASAA1159350Unknown · malfunctionedFL 350 CRUISE (3 MINUTES AFTER L/O) M.787/AS 266 KTS.AIRCRAFT ON TRIM: A/P B UNCOMMANDED DISCONNECT RE-ENGAGED A/P B AIRCRAFT FLOWN NORMALLY REMAINDER OF FLIGHT TILL 1500 WITH NO OTHER PROBLEMS. AFCS BITE PROCEDURE REF FIM 22 11 00 810 801 CURRENT STATUS QUICSDR ASAA1159349Control Panel · faultyUNCOMMANDED AUTO PILOT DISENGAGE. WHEN LEVELING OUT AT FL 300 .76 MACH ALSO AT 2000FT 160 KTS GEAR DOWN FLAPS 15 COUPLED TO ILS AIRCRAFT IN TRIM ON BOTH OCCASIONS. ALSO ON 3/29/11 FLT 889 FL 350 CRUISE (3 MINUTES AFTER L/O) M.787/AS 266 KTS. AIRCRAFT ON TRISDR ASAA1159191Sense Line · leakingNR 1 ENGINE PRECOOLER CONTROL VALVE FAILED INSTALLATION TEST PER AMM 36 12 02 400 801 STEP G. DETERMINED PRECOOLER CONTROL VALVE IS EFFECTIVE FOR AIRCRAFT. REMOVED AND REPLACED NR 1 ENG PRECOOLER CONTROL VALVE IAW ASA AMM 36 12 02 000 801 AND AMM 36 12 02 40SDR ASAA1159152Battery Pack · dischargedBATTERY PACK M1671 FAILED CAPACITY TEST. REPLACED BATTERY PACK IAW B737 800 AMM 33 51 06.SDR ASAA1159151Battery Pack · dischargedBATTERY PACK M1694 FAILED CAPACITY TEST. REPLACED BATTERY PACK IAW B737 800 AMM 33 51 06.SDR ASAA1159146Bracket · crackedLEFT WING TRAILING EDGE VERTICAL WEB CRACKED ON FORWARD SIDE AT FASTENER HOLES. REMOVED AND REPLACED CRACKED BRACKET IAW B737 700 SRM 51 40 02. NO DAMAGE TO WEB.SDR ASAA1159150Battery Pack · dischargedBATTERY PACK M1673 FAILED CAPACITY TEST. REPLACED BATTERY PACK IAW B737 800 AMM 33 51 06.SDR ASAA1159135Pump · inoperativeNR 1 ENGINE DRIVEN HYD PUMP DOES NOT DEPRESSURIZE WHEN SWITCH IS TURNED OFF. REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP PER MM 29-11-11-000-802-002-2 AND MM 29-11-11-400-802-002-2. PERFORMED NR 1 ENGINE DRIVEN HYDRAULIC PUMP INSTALLATION TEST REF MM 29-11-1SDR ASAA1159134Keyboard · wornLEFT AND RIGHT MCDU LINE SELECT BUTTONS HAVE BLACK WORN OFF. REPLACED LEFT AND RIGHT MCDU KEYBOARDS AND PERFORMED GOOD INSTALLATION TEST IAW AMM 34-61-01-000-801 AND AMM 34-61-01-400-801.SDR ASAA1159133Control Panel · malfunctionedMCP HEADING DISPLAY FLICKERS. REMOVED AND REPLACED MODE CONTROL PANEL PER MM'S 22 11 34 000 801 AND 22 11 34 400 801. PERFORMED GOOD TEST PER MM 22 11 34 740 801.SDR ASAA1158729Igniter · faultyNO LIGHT OFF ON RIGHT ENGINE START. FUEL FLOW INITALLY CAME UP TO 1.1 THEN ROLLED BACK TO 0 AFTER 2 SECONDS. REPLACED NR 2 RT IGNITER REF AMM 74 21 02. REPLACED NR 2 RT IGNITER LEAD REF AMM 74 21 01. NR 2 RT IGNITER SYSTEM, OPS CHECKS GOOD.SDR ASAA1158717Exciter · failedNR 2 ENG WON'T START NO LIGHT OFF. REPLACED NR 2 ENGINE IGNITION EXCITER RT SIDE PER TASK 74 11 01 400 801 F00 PAGES 1 3. OPS CHECK GOOD PER TASK 74 00 00 750 801 F00 PAGES 1 8.SDR ASAA1058573Pcu · malfunctionedDURING PREFLIGHT NOTED RCCB C/B POPPED. REPLACED THE STANDBY POWER CONTROL UNIT PER MM 24 34 11 00 801 AND 24 34 11 000 801, OPS CHECKS NORMAL. MAIN BATTERY CHARGER OPS CHECKS NORMAL PER 24 31 25 710 801. AUX BATTERY CHARGER OPS CHECKS NORMAL PER 24 31 31 7SDR ASAA1058547Unknown · malfunctionedWHILE ACCOMPLISHING T/C 78273000 FOUND FAULT LONG TIME MSG NR 74-30971 (THE APL INPUT VOLTAGE FOR THE L EXCITER " IGN 1 " IS OUT OF RANGE) AT NR1 ENG. DEFER FOR 450 FLIGHT HOURS PER T/C 78273000. PERFORMED FMV ENGINE NR 1 "RECENT FAULTS" AND "FAULT HISTORY".SDR ASAA1058546Unknown · malfunctionedWHILE ACCOMPLISHING T/C 78273000 FOUND FAULT LONG TIME MESSAGE NR 73-31351 (THE APL VOLTAGE INPUT TO THE EEC IS OUT OF RANGE) AT NR 1 ENG. DEFER FOR 450 FLT HRS PER T/C 78273000. PERFORMED FIM TASK 73-22-00-810-808. PER STEP E (D) NO MAINTENANCE MESSAGES APSDR ASAA1058482Filter · dirtyNR 2 ENG IDG DPI DELTA P INDICATOR FOUND EXTENDED. REMOVE AND REPLACE NR 2 ENG IDG SCAVENGE FILTER AND OIL AMM REF 24 11 41. LEAK CHECK GOOD. DPI RESET AND DECAL NR 2 RUBBED OUT.SDR ASAA1058405Warning System · false activation"FAIL" IS DISPLAYED ON ACTIVE AND STANDBY WINDOWS OF HF1 RADIO. CONFIRMED FAULT HF1 "FAIL" MESSAGE IN ACTIVE AND STANDBY ON BOTH CAPT'S AND F/O'S RADIO FREQ WINDOWS. PERFORMED BITE TEST ON HF1 TRANCEIVER. NO FAULTS FOUND. NO HISTORY LAST 30 DAYS. "FAIL" MSDR ASAA1058339Filter · faultyWHILE PROVIDING PNEUMATICS ONLY THE APU SHUTDOWN. AMBER FAULT LIGHT IS ILLUMINATED. INTERAGATED CDU FOUND FAULT 49 94299 "STARTER GEN OIL FILTER SHOWS CLOGGED". PERFORMED FIM 49 90 00 810 809 REPLACED LUBE FILTER AND STARTER GEN FILTER AND INSPECTED MAGNETISDR ASAA1058309Wire Harness · corrodedGE DIAGNOSTICS REPORTS NR 1 ENGINE TREND DATA SHOWS A SUDDEN SHIFT IN EGT HOT DAY MARGIN ALL OTHER PARAMETERS NORMAL. EGT INDICATION ERRORS ARE SUSPECT. PERFORMED FMC CDU FAULT TC 78273000 NO RECENT FAULTS FOUND. FOUND CJ10 HARNESS S3-S4 CONNECTORS HAD CORRSDR ASAA1058105Pcu · failedCPT OUTBOARD DU INBOARD DU AND UPPER DU INOP. CPT AUDIO CONTROL PANEL INOP VHF 1 & VOR 1 INOP. STBY BUS SECT 1 OF STANDBY POWER CONTROL UNIT POPPED. REPLACED SPCU PER MM 24 34 11 OPS TEST NORMAL PER MM 24 34 00. GROUND VERIFICATION SYSTEM OPERATION NORMAL.SDR ASAA1058059Window · delaminatedLEFT SIDE WINDOW HEAT OVHT LIGHT CAME ON. FOUND LEFT SIDE WINDOW DELAMINATED ALONG PRIMARY SENSOR WIRE FROM BOTTOM TO 2/3 WAY UP TO THE PRIMARY SENSOR. REPLACED L2 OPENABLE WINDOW REF MM 56 12 11 400 801 STEPS E5 F8 AND F12. OPS NORMAL.SDR ASAA1057998Unknown · malfunctionedFMC FUEL QTY SHOWED 300 LBS UNDER BURN. THEN 300 LBS OVER BURN THEN ON BURN THEN 400 LBS OVER BURN. THIS OCCURRED DURING A TIME SPAN OF 1.5 HRS. PERFORMED FQIS BITE PROCEDURE REF FIM 28 41 00 810 801 W/ NO DEFECTS NOTED. FMC BITE PROCEDURE GOOD REF FIM 34 61SDR ASAA1057830Unknown · malfunctionedON TAXI OUT AFTER ENGINE START ON MASTER CAUTION RECALL. "AIR COND" AND CONTROL CABIN "ZONE TEMP" ILLUMINATED AND EXTINGUISHED ON MASTER CAUTION RESET. CREW REPORTED NO FAULT ON RECALL AFTER LANDING. PERFORMED BITE TEST ON BOTH PACK/ZONE CONTROLLER. REF FISDR ASAA1057479Sensor · faultyAUTOPILOT ELEVATOR POSITION SENSOR AND NEUTRAL SHIFT SENSORS REQUIRE ADJUSTMENT. ADJUSTED ELEVATOR POSITION SENSOR REF MM 22 11 30 AND NSS REF MM 22 11 14. GROUND FUNCTIONAL TEST GOOD REF MM 22 11 00. BITE TEST GROUP 47 GOOD. PITCH SENS LRU REPLACEMENT TESSDR ASAA1057480Connector · damagedDURING LAND VERIFY TEST NR 35 DUAL STAB FAILS. REPLACE D2257 AND RE-TERMINATE PINS 4 5 6 7 OF D381. ACCOMPLISHED LAND VERIFY TEST REF MM 22 11 00.SDR ASAA1057316Sensor · failedSPEED AND ALT FLAGS ILLUMINATED ON PFD F/O SIDE. DIVERTED 0116Z 46 MIN. VERIFIED FAULT RERACKED ADIRU'S, NO HELP. RERACED DEU'S OPS CHECK GOOD IAW MM 31-62-21-400-801 AND BITE TEST GROUP 30 AND LRU TEST FOR CDS CHECKS GOOD DEU TESTS ALL PASS UNDER FMCS DEU SDR ASAA1057312Packing · tornOIL CAP PACKING ON NR 2 ENGINE IS TORN. REPLACED TORN OIL CAP PACKING ON NR 2 ENGINE. OPS NORMAL.SDR ASAA1057255O-Ring · wornWHILE SERVING RT ENG OIL FOUND ENG OIL SERVICE CAP O-RING SEAL WORN. REMOVED AND REPLACED RT ENG OIL FILLER CAP O-RING SEAL. OPS CHECKED RT RNG AT IDLE, NO LEAKS NOTED. REFERENCE AMM 79 11 01.SDR ASAA0957145Wire Harness · shortedGE DIAGNOSTICS REPORTS NR 2 ENGINE TREND DATA SHOWS A SUDDEN SHIFT IN EGT HOT DAY MARGIN ALL OTHER PARAMETERS NORMAL. EGT INDICATION ERRORS ARE SUSPECT. ACCOMPLISHED EGT CONNECTOR CLEANING REF MM 77 21 00, NO HELP. S4 VALUE OVER 200 DEG LOWER WHILE RUNNING SDR ASAA0956999Filter · dirtyAC TEMP CONTROLLERS FWD AND AFT RUNNING IN AUTO FLUCTUATED WITH TEMPS 12 DEG TO 55 DEG CONT CAB SEEMED OK IN AUTO POS PUT ALL IN OFF AND HAD BETTER CONTROL OF TEMP. LEFT PACK 30 DEG RIGHT PACK 25 DEG GROUNDED YES. FOUND FWD AND AFT CABIN TEMPERATURE CONTROL SDR ASAA0956873Autothrottle Sys · malfunctionedAUTOTHROTTLES WILL NOT REMAIN ENGAGED. WILL ENGAGE BRIEFLY THEN DISENGAGE. THIS OCCURS WITH FCC MASTER SWITCH ON EITHER SIDE CAPT OR F/O. C/B P18 E1 REMAINS IN. FAULT CODE 223 130 00. PERFORMED A/T CURRENT STATUS NO FAULTS. A/T INTERACTIVE TESTS NO FAULTSDR ASAA0956788Autopilot Sys · malfunctionedAUTOLAND EVAL ATTEMPTED ON SEA 34L. A/P SEEMED TO PITCH DOWN A LITTLE TOO MUCH AT ABOUT 100' AGL SHOWING NO SIGNS OF CORRECTING. HGS GAVE "APP WARN" COUPLE OF SECONDS LATER. DISCONNECTED A/P AND LANDED MANUALLY. ATC SAID ILS 34L WAS OPERATING NORMALLY AND ILS SDR ASAA0956738Eec · malfunctionedWHEN CLIMB POWER SELECTED NR 1 THRUST LEVER ADVANCES BEYOND CLIMB POWER & AUTO THROTTLES DISCONNECTED. A/T LIMIT IS ANNUNCIATED. EEC 1 CHANNEL A IS INOP. REMOVED AND REPLACED NR 1 ENG EEC PER AMM 73 21 60 000 801. GROUND VERIFICATION FOR EEC GOOD. NO DEFESDR ASAA0956701Unknown · malfunctionedTHE "WXR STAB" YELLOW FAULT LIGHT ON WHEN OPERATING RADAR. PERFORMED FIM TASK 34 43 00 SYSTEM OPS NORMAL. A/C OK FOR SERVICE. NO HISTORY PAST 30 DAYS SEAMC NOTIFIED.SDR ASAA0956697Transceiver · faultyHF1 DIFFICULT TO TRANSMIT ON, IT TAKES MULTIPLE ATTEMPTS TO ESTABLISH A TRANSMISSION. RECEPTION IS NORMAL. HF2 WORKS NORMALLY. NR 1 HF FAULT PER FIM 23 11 00 810 806 "FAIL" SHOWED ON RADIO TUNING PANEL INTERMITTENTLY DURING TRANSMIT. REPLACED AND TESTED NR SDR ASAA0956694Control Head · malfunctionedIN FLIGHT NR 1 HF RADIO DISPLAYED "FAIL" BOTH CONTROL HEAD WINDOWS DURING ATTEMPTED TX NO SIDE TONE AND A NON COUPLER "BEEP" ON EACH SUBSEQUENT ATTEMPTS. SWITCHED NR 1 HF TO DATA INTERMITTENT DATA RX/TX FOR ENTIRE FLT. HFDR MAINT PAGES SHOWED NORMAL/NORMAL HSDR ASAA0956692Transceiver · malfunctionedUNABLE TO TRANSMIT OR TUNE HF1 OR HF2. ABLE TO MONITOR SELECTED FREQ. REMOVED AND REPLACED HF COUPLER NR 1 REF MM 23-11-61 AND HF RT NR 2 REF 23-11-21 MM. BOTH SYSTEMS OPERATIONAL TEST REF MM 23-11-00. SYSTEMS OPERATIONAL TEST GOOD.SDR ASAA0956643Eec · malfunctionedGE DIAGNOSTICS REPORTS NR 1 ENGINE EGT SHIFT. NR 1 ENG EEC VERIFIED BY SEAMC. REMOVED AND REPLACED PER AMM 73 21 60 000 801 AND 73 21 60 400 801 THRU STEP E (F)4 38682. COMPLETED EEC INSTALLATION TEST REF AMM 73 21 60 400 801 STEP F(1 3) 38682. VERIFIED LASDR ASAA0956617Probe · faultyGE DIAGNOSTICS REPORTS NR 1 ENGINE TREND DATA SHOWS A LARGE FLUCTUATION IN EGT HOT DAY MARGIN AND DELTA EGT ALL OTHER PARAMETERS NORMAL. EGT INDICATION ERRORS ARE SUSPECT. PRE CONNECTOR CLEANING VALUES S1 83 S2 43 S3 49 & S4 101. ACCOMPLISHED CONNECTOR CLEASDR ASAA0956538Starter Gen · faultyAPU FAILED WITH FAULT LIGHT. STARTED APU UNABLE TO CONFIRM DISCREPANCY. PERFORMED BITE CHECK OF APU. FOUND FAULT CODE 49 41012 FOR FLT LEGS 0 1 & 2 & 49 41248 FOR FLT LEGS 3 & 4 PERFORMED FIM 49 40 00 810 803 A F.1 4(A E). REPLACED STARTER/GEN REF MM 49 41SDR ASAA0956469Warning System · activatedFAULT LIGHT ILLUMINATED DURING APU START AFTER LANDING. ACCOMPLISHED APU STARTING AND OPERATION PER AMM TASK 49 11 00 860 801. ACCOMPLISHED APU BITE TEST. NO FAILURES FOUND PER FIM TASK 49 60 00 810 801. STARTED APU TWICE AND STARTED NORMAL AFTER POWER DOW
Back to N560AS