N559AS
Service difficulty reports · 540
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 = 'N559AS' 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 = 'N559AS' 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 ASAA2018122407514Satcom · malfunctionedSATCOM INOP. GROUNDED - YES. VERIFIED PROPER SATCOM SYSTEM LED STATUS/NO FAULTS NOTED REF B737-800 AMM 23-15-00. PERFORMED SATCOM SYSTEM TEST REF AMM 23-15-00. OPS CKS GOOD. ALL TESTS PASS.SDR ASAA2018122197495Indicator · inoperativeFUELER REPORT #2 TANK REFUEL QTY INDICATOR INOP. GROUNDED - YES. REMOVED AND REPLACED #2 TANK REFUEL INDICATOR REF B737-800 AMM 28-41-61. ALL TESTS PASS. OPS CKS GOOD. ETOPS SIGNIFICANT SYSTEM GROUND VERIFICATION SUCCESSFUL.SDR ASAA2018121527435Pressure Switch · failedAFTER ENGINE START AT FIRST APPLICATION OF TAXI THRUST THE NR 2 ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED FOR APPROX 30 SECONDS THEN EXTINGUISHED. THE LIGHT DID NOT COME ON AGAIN WHILE TAXING TO ANOTHER GATE. GROUNDED - YES. EEC BITE SHOWS FAULT CODE 73-3107SDR ASAA2018121027389Warning Message · false activationENG #1, MSG # 76-31361. THE START LEVER SIGNALS DISAGREE. OCCURRED FLIGHT LEG 1. LONG TIME FAULT. GROUNDED - YES. ACCOMPLISHED EEC BITE PER B737-800 FIM 76-11 TASK 801. FOUND NO FAULTS ON ANY FLIGHT LEGS RECENTLY OR IN HISTORY. NO HISTORY IN LAST 30 DAYS.SDR ASAA2018112527072Coupler · malfunctionedPERFORMED NR 1 HF CHECK AND UNABLE TO RECEIVE OR TRANSMIT. GROUNDED - YES. REMOVED AND REPLACED THE #1 HF ANTENNA COUPLER PER B737-800 AMM 23-11-61/401. OP-CHECKS GOOD PER SAME.SDR ASAA2018112637057Coupler · failedAFTER MX REPLACED HF1 IN KOA, OPS CHECK NORMAL BY HEARING TRANSMISSIONS ON HF2. PRIOR TO REACHING GATEWAY FIX, ATTEMPTED NUMEROUS CONTRACT ATTEMPTS W/ AIRINC. COULD HEAR OTHER A/C ON HF1. COULD HEAR OUR TRANSMISSIONS USING HF2. USED HF2 TO ESTABLISH CONTACT W/SDR ASAA2018112227058Transceiver · failedNR 1 HF TRANSMITTER IS INTERMITTENT INITIALLY IT WAS WORKING OK AND THEN COULD NOT BE HEARD BY SFO RADIO OR OTHER AIRCRAFT. IT RECEIVED TRANSMISSIONS AND SELCAL NORMALLY. DURING THE TIME NR 1 HF COULD NOT BE HEARD NR 2 HF OPERATED NORMALLY. GROUNDED - YES. REMSDR ASAA2018111946869Hf Comm · malfunctionedTRANSMIT FUNCTION ON HF RADIO #1 COULD NOT BE HEARD BY SFO RADIO EXCEPT MAYBE 1-2 TIMES OUT OF APPROX 20 ATTEMPTS FROM BOTH PILOT STATIONS AND HAND HELD MICROPHONE, THE ONE OR TWO TIMES THEY COULD HEAR US ONLY POORLY AT 1 X 1, HF 2 XMIT OPS OK AND HF 1 RECEIVESDR ASAA2018102926643Warning System · false activationLONG TIME FAULT CODE 76-21361 ON NR 1 ENG START LEVER SIGNALS DISAGREE. GROUNDED - YES. ACCOMPLISHED AN EEC BITE PER FIM 76-11/801 AND FOUND NO ACTIVE FAULTS ON ANY FLIGHT LEG IN HISTORY/RECENT FAULTS PAGES. THIS CLEARS PLT.SDR ASAA2018101526462Pump · inoperativeNR 1 MAIN TANK FWD FUEL PUMP LOW PRESS LT ON. GROUNDED - YES. REMOVED AND REPLACED THE NUMBER ONE TANK FORWARD POSITION BOOST PUMP ASSY REF AMM 28-22-41, OPS GOOD, NO LEAKS FOUND.SDR ASAA2018072325539Warning System · false activationFMC CDU FAULT CODE NR 1 ENG, FLT LG 3. MSG 76-31361"THE START LEVER SIGNALS DISAGREE" LONG TIME FAULT DEFERRED PER T/C 78273000. GROUNDED - YES. PERFORMED TASK CARD 78273000 (INTERROGATE THE FMC CDU FOR ENGINE FAULTS) NO FAULTS FOUND THIS CLEARS DEFERRAL.SDR ASAA2018071825471Trim Motor · failedSTAB TRIM INOPERATIVE. SET TRIM FOR T/O AFTER ROTATION TRIM WAS INOP. RAN QRH AUTOPILOT TRIM INOP ALSO. GROUNDED - YES. AIR TURNBACK, DIVERSION TIME 30 MINUTES. ACCOMPLISHED FIM 27-41 TASK 804, RESET CIRCUIT BREAKER OPS CHECK GOOD. REMOVED AND REPLACED STABILISDR ASAA2018070925321Warning System · false activationZONE TEMP (CONT CAB) ILLUMINATED UPON RECALL, EXTINGUISHES WHEN MASTER CAUTION SYSTEM IS RESET. GROUNDED - YES. NR 2 CONTROLLER LOGGED FLT DECK TRIM VALVE FAULT. RESET FAULT. COMPLETED FIM 21-62 TASK 801, PACK TEMP CONTROL BITE. NO FAULTS, OK FOR SERVICE.SDR ASAA2018063025282Control Panel · defectiveMCP ALT SELECTOR BLEMISH IN MIDDLE OF DISPLAY-DISPLAY STILL READABLE. GROUNDED - YES. REMOVED & REPLACED MCP REF AMM 22-11-34. ACCOMPLISHED MCP INSTALLATION TEST REF AMM 22-11-34-740-801, LRU REPLACEMENT (GP 32) TEST (MCP) REF AMM 22-11-34/501, DFCS LAND VERIFSDR ASAA2018061975110Battery · no testEMERGENCY BATTERY AT THE R2 DOOR FAILED A CHECK. ACFT GROUNDED. REMOVED AND REPLACED BATTERY AND POWER SUPPLY IAW AMM 33-51-06-960-805, AND 33-51-06-960-806, OPS CHECKED GOOD IAW AMM 33-51-06-960-805, STEP 5E.4 A-C.SDR ASAA2018060532910Pump · malfunctionedDURING CRUISE FLIGHT, WITH APPROX 1300 LBS OF FUEL IN THE CENTER TANK, THE LEFT CENTER LOW PRESSURE LIGHT STAYED ILLUMINATED WITH CENTER PUMP SWITCHED ON. QRH 12.8 COMPLETED. ACFT GROUNDED. ACCOMPLISHED FIM 28-22, TASK 801. PRIMED THE PUMP BY FILLING CENTSDR ASAA2018052924856Anti-Ice Valve · intermittentAFTER SELECTING THE NR 1 ENGINE ANTI-ICE, COWL VALVE OPEN LIGHT REMAINED ILLUMINATED BRIGHT BLUE, AMBER TAI ILLUMINATED ON ENGINE INSTRUMENTS. APPROXIMATELY 5 MINUTES LATER, THE LIGHTS EXTINGUISHED AND EAI OPERATED NORMALLY. ACFT GROUNDED. REMOVED THE NR 1SDR ASAA2018052184700Actuator · inoperativeAFTER THE GEAR WAS RAISED AFTER TAKEOFF, A RED RIGHT GEAR LIGHT REMAINED ILLUMINATED. ON RETURN TO LANDING, ALL GEAR LIGHTS INDICATED GREEN WITH HANDLE LOWERED. ACFT GROUNDED. AIR TURNBACK. REMOVED AND REPLACED THE RT MLG UPLOCK ACUATOR IAW AMM 32-32-41.SDR ASAA2018041724269Web · wornE&E BAY DOOR CUTOUT ABOVE THE RT LATCH RECEIVER, FRAME SKIN WORN. ACFT GROUNDED. REMOVED THE E&E DOOR LATCH RECEIVER IAW SRM 5-1-40-02, REMOVED AND REPLACED THE WEB IAW DWG 141A8511, REV-. REINSTALLED LATCH RECEIVER IAW DWG 141A3501, REV-. PERFORMED AN ESDR ASAA2018041624394Floorbeam · crackedFWD CARGO BAY, FLOORBEAM ANGLE CRACKED AT RBL 25, BS 500G WAS FOUND CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02, AND BAC DWG 143A7502, REV A.SDR ASAA2018041124407Intercostal · crackedFWD CARGO BAY INTERCOSTAL FOUND CRACKED BETWEEN BS 500F - 500G, STRINGER 25R. ACFT GROUNDED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02, SRM 51-40-05, SRM 51-40-02, AND EA 800-53EA-20157.SDR ASAA2018040724408Floor Support · corrodedMAIN CABIN FLOOR SUPPORT BS 308, LBL 12, UPPER SURFACE CORRODED. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG 141A5600 REV N.SDR ASAA2018043024405Cusp Web · corrodedMAIN CABIN, AT THE R1 DOOR CREASE BEAM THE CUSP WEB HAD CORROSION ON THE FWD AND AFT SIDES. BS 294 - 338. ACFT GROUNDED. REMOVED AND REPLACED IAW DWG 141A8310, REV B, AND SRM 51-40-02.SDR ASAA2018043024400Strap · corrodedMAIN CABIN AT BS 1016, RBL 27 STRAP HAS CORROSION. ACFT GROUNDED. REMOVED AND REPLACED THE STRAP IAW DWG 147A5700, REV B.SDR ASAA2018040624225Floor Support · crackedFLOOR SUPPORT CRACKED BS 540, RBL 1R. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG 143A0060, REV A, AND SRM 51-40-02.SDR ASAA2018040624224Floor Support · crackedFLOOR SUPPORT CRACKED BS 540, LBL 1. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG 143A0060, REV A, AND SRM 51-40-02.SDR ASAA2018043024406Channel · corrodedAFT CARGO BAY, RT TRANSITION PANEL CHANNEL IS CORRODED BETWEEN BS 887 & 947. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS IAW SRM 53-00-53 FIG103. FOUND TO BE OUT OF LIMITS. FABRICATEED A NEW CHANNEL IAW BAC DWG 147A-7500, REV B. REV-SDR ASAA2018040524404Channel · corrodedAFT CARGO BAY, RT TRANSITION PANEL CHANNEL IS CORRODED AT BS 727 TO 727F. ACFT GROUNDED. BLENDED THE CORROSION, FOUND TO BE OUT OF LIMITS, FABRICATED A NEW REPAIR SECTION IAW SRM 53-00-53, REPAIR 5. REMOVED THE DAMAGED SECTION AND INSTALLED THE REPAIR SECTIOSDR ASAA2018040524235Intercostal · crackedFWD CARGO BAY, BS 500H, STRINGER 25R INTERCOSTAL AND ANGLE CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE INTERCOSTAL AND ANGLE IAW DWD 143A7505, REV B.SDR ASAA2018040524223Floorbeam · corrodedMAIN CABIN BS 947.5 UPPER FLOORBEAM CORRODED AT RBL 5. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1, FIGURE 104, DETAIL C. ACCOMPLISHED A CATEGORY A REPAIR ON THE UPPER FLOORBEAM TEE LBL 10 - RBL 60 IAW 53-70-51-2R-5, REPAIR 5, ALTERNATISDR ASAA2018040524220Shear Tie · crackedFWD CARGO PIT STA 500H LT STR 25 FWD INTERCOSTAL CLIP CRACKED. GROUNDED - YES. REMOVED AND REPLACED CLIP P/N 143A85020159, PO 913549.2 AT FWD CARGO ST5004 LT STR 25 IAW BAC DWG 143A7505 REV B AND SRM 51-40-02.SDR ASAA2018040524219Shear Tie · crackedFWD CARGO PIT STA 500H LT STR 25 AFT INTERCOSTAL CLIP CRACKED. GROUNDED - YES. REMOVED AND REPLACED CLIP P/N 143A75020155 PO 909512.1 AT FWD CARGO STA 500H LT STA 25 IAW BAC DWG 143A7505 REV B AND SRM 51-40-02.SDR ASAA2018040524190Web · corrodedAFT CARGO BAY WEB AT THE DOOR CUTOUT CORRODED AT MULTIPLE PLACES. ACFT GROUNDED. REMOVED DAMAGE IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 50-60-15, DETAIL 6. REMOVED AND REPLACED THE WEB IAW SRM 51-40-02, SRM 51-40-05, AND DWG 146A8340, REV A.SDR ASAA2018040524178Transition Panel · corrodedAFT CARGO COMPARTMENT RT TRANSITION PANEL IS CORRODED STA 727F TO 727J. GROUNDED - YES. BLENDED CORROSION FROM THE RT ZEE CHANNEL IN THE AFT PIT FROM BS-727F - 727J. (ORIGINAL MATERIAL WAS .040; .006 MAT REMOVED; .034 REMAINS) FOUND TO BE OUT OF LIMITS PER SRMSDR ASAA2018040424271Bracket · wornE&E BAY DOOR CUTOUT AFT LATCH RECEIVER ATTACH BRACKET WORN. ACFT GROUNDED. REMOVED AND REPLACED THE LATCH RECEIVER BRACKET IAW DWG 141A8505, REV B, LATCH RECEIVER OPS CHECK PERFORMED AND OPS CHECKED GOOD.SDR ASAA2018031023816Unknown · malfunctionedNR 1 ENGINE LAGS BEHIND NR 2 ENGINE DURING INCREASE AND DECREASE IN POWER SETTING. WITH 10% N1 CHANGE NR 1 ENGINE WOULD TAKE 4-5 SECONDS TO REACH SAME POWER SETTING AS NR 2 N1. THIS OCCURRED DURING DESCENT FROM FL 360 INCLUDING LEVEL OFF AND CONTINUED DURING TSDR ASAA2018010823137Valve · failedDUCT PRESSURE SPLIT, RIGHT 22, LEFT 45, DURING CLIMB. ACFT GROUNDED. TROUBLESHOT THE NR 2 ENGINE IAW AMM 36-11-00, THE PRSOV FAILED THE TEST. REMOVED AND REPLACED THE NR 2 ENG PRSOV IAW AMM 36-11-04-000-801. LEAK CHECKED GOOD.SDR ASAA2017123023056Exciter · failedNR 1 ENG NO LIGHT OF WITH IGN L SELECTED. NORMAL START WITH IGN R SELECTED. GROUNDED - YES. R&R NR 1 ENG LT IGNITER PLUG REF AMM 74-21-02. NO HELP. FOUND LT IGNITION LEAD WELDED INSIDE EXCITER BOX PLUG. R&R NR 1 ENG LT IGNITION LEAD REF AMM 74-21-01, R&R NR 1 SDR ASAA2017120122772Warning Message · illuminatedDURING ACCOMPLISHMENT OF T/C 78273000 #1 ENG HAS ECONOMIC FAULT MSSG 73-11371 UPPER EGT SECTORS READING HIGH. GROUNDED - YES. PERFORMED TASK CARD 78279000 FOR #1 ENG FOR FAULT MSG 73-11371 FOR 50 HR RECHECK, NO RECENT FAULTS NOTED. #1 ENG ECONOMIC FAULT 73-11SDR ASAA2017112822744Connector · damagedFWD CARGO DET LOOP A WON'T TEST. GROUNDED - YES. VERIFIED PIN 10 ON CONNECTOR D13846 NOT LOCKING. REMOVED AND REPLACED CONNECTOR P/N BACC45FN12-12PH REF B737-800 WDM 26-16-21-7. OPS CHECK GOOD REF B737-800 AMM TASK 26-16-00-710-801. THIS CLEARS MEL 26-19H.SDR ASAA2017112722702Indicator · failedNR 2 TANK REFUEL PANEL INDICATION INOP. GROUNDED - YES. REMOVED AND REPLACED REFUEL PANEL #2 TANK INDICATOR PER B 737-800 AMM 28-412-61-400-801. GROUND BITE TEST OK.SDR ASAA2017112522677Fire Detector · malfunctionedFWD CARGO FIRE DETECTOR LOOP B WILL NOT TEST. ACFT GROUNDED. AFTER PERFORMING CARGO BAY SMOKE DETECTOR OPS TEST IAW AMM 26-16-00-710-801 AND CEU INSTALLATION TEST IAW AMM 26-16-02-710-801, BEING UNSUCCESSFUL IN DUPLICATING THE FAULT, AND HAVING NO HISTORY OFSDR ASAA2017112422678Smoke Detector · failedFWD CARGO FIRE LOOP A INOPERATIVE. ACFT GROUNDED. PERFORMED FIM 26-16, TASK 806, FOUND FAULTY SMOKE DETECTOR A29 AND FWD CARGO CEU M2236. REMOVED AND REPLACED CEU AND SMOKE DETECTOR IAW AMM 26-16-02-000/400-801 AND 26-16-01-000/400-801. OPS CHECKED GOOD IAWSDR ASAA2017112122691Not Reported · dirtyNR 1 ENGINE HAS FAULT MESSAGE 73-21371 UPPER EGT SECTORS READING HIGH, FLIGHT LEGS 8 AND 10. ECONOMIC FAULT, DEFERRED PER T/C 78273000. GROUNDED - YES. REF FIM 73-11 TASK 801 UPPER EGT SECTORS READING HIGH. ENGINE 1 EEC BITE SHOWS NO CURRENT FAULTS OR IN HISTOSDR ASAA2017112122689Not Reported · dirtyNR 1 ENGINE HAS A FAULT MESSAGE 73-11371, UPPER EGT SECTORS READING HIGH, FLIGHT LEGS 7 AND 9, ECONOMIC FAULT. DEFERRED PER TC 78273000. GROUNDED - YES. REF FIM 73-11 TASK 801 UPPER EGT SECTORS READING HIGH. ENGINE 1 EEC BITE SHOWS NO CURRENT FAULTS OR IN HISTSDR ASAA2017112122692Connector · looseNR 1 ENGINE HAD A RECENT FAULT MESSAGE NR 73-21271, THE ALTERNATOR VOLTAGE INPUT TO THE EEC IS OUT OF RANGE, FLIGHT LEGS 8 AND 10, SHORT TIME FAULT. ACFT GROUNDED. TROUBLESHOT IAW FIM 73-27, 804. FOUND CONNECTOR DP0808 LOOSE. SECURED THE CONNECTOR. REPAIR COSDR ASAA2017112122690Heater · leakingFUEL HEATER SERVO LEAKING FUEL ON THE NR 1 ENGINE. ACFT GROUNDED. REMOVED AND REPLACED THE SERVO FUEL HEATER IAW AMM 73-11-07-000-801-F00, AND AMM 73-11-07-400-801-F00. LEAK CHECKED GOOD ON GROUND RUN. NO DEFECTS NOTED.SDR ASAA2020050832709Pressure Deck · crackedG0938004 LEFT-HAND VERTICAL PRESSURE DECK WEB AT BS 663, LBL 34-LBL 36 HAS A CRACK IN THE CENTER MACHINED POCKET. GROUNDED - YES. REPAIRED PRESSURE WEB REF SRM 57-10-10-2R-3 REPAIR 3 ALTERNATIVE 1. THIS IS A CATEGORY "B" REPAIR WITH AN INSPECTION THRESHOLD OF SDR ASAA2017110422427Idg · failedAFTER ENGINE START, SOURCE OFF LIGHT ILLUMINATED ON GENERATOR 1 AND WOULD NOT EXTINGUISH WITH GEN 1 SELECTED ON. ACFT GROUNDED. REMOVED THE NR 1 IDG IAW AMM 24-11-11. DUE TO UNSCHEDULED REMOVAL OF THE NR 1 IDG, BOTH FILTERS REMOVED AND CHECKED FOR CONTAMINASDR ASAA2017102222278Blade · damagedWHILE ACCOMPLISHING TC 78472002 ON THE NR 2 ENGINE FOUND PLATFORM SEAL DAMAGE IS MORE THAN 39.37 INCHES IAW AMM 72-21-02. ACFT GROUNDED. REPLACED THE PLATFORMS REMOVED DURING ACCOMPLISHMENT OF TC 78472002. ALL PLATFORMS INSTALLED IAW TC 78472002.
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