N514AS

Service difficulty reports · 370

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 = 'N514AS' 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.

SDR ASAA2014071908699Switch · failedDURING PREFLIGHT, ON THE OVERHEAD FUEL PANEL, THE NR 2 ENGINE VALVE CLOSED, ANNUNCIATOR LIGHT IS ON BRIGHT. ACFT GROUNDED. REPLACED HPSOV SWITCH ON NR 2 ENGINE REF AMM 73-21-09-000/400-801-F00. OPS NORMAL. ENGINE RUN NORMAL.Jul 19, 2014 · N514AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2014061308188Warning Light · false activationDURING PRE-FLT, NOTICED NR 2 ENGINE CLOSED LIGHT ON. ACFT GROUNDED. PERFORMED EEC BITE CHECK IAW FIM 73-00, TASK 801. NO FAULTS, NO HISTORY 90 DAYS. PERFORMED FIM TASK 73-06-801, ENGINE CONTROL LIGHT ON FAULT ISOL. NO FAULTS. OK FOR SERVICE.Jun 13, 2014 · N514AS · Boeing 737890 · Central WarningSDR ASAA2014052307920Warning Message · false activationON TAXI OUT FMC DISAGREE. ACFT GROUNDED. FMC PROCEDURE COMPLETED, ALL OK.May 23, 2014 · N514AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014042707592Ignition Sys · unknownNR 2 LT ENGINE IGNITION SYS INOPERATIVE. ACFT GROUNDED. PERFORMED FIM 74-21, TASK 806. EEC BITE SHOWS NO FAULTS. AUDIBLE IGNITOR TEST PASSED. STARTED NR 2 ENGINE USING LT IGNITOR. ENGINE STARTS AS SHOULD WITH NO ISSUES. FAULT INTERMITTENT.Apr 27, 2014 · N514AS · Boeing 737890 · Ignition SystemSDR ASAA2014042507569Valve · malfunctionedCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED ON MASTER CAUTION RECALL. LIGHT EXTINGUISHES ON RESET. ACFT GROUNDED. R & R TRIM AIR MODULE VALVE REPLACED IAW IAW 21-61-021-00MM. OPS CHECKED GOOD.Apr 25, 2014 · N514AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2014042207558Satcom · malfunctionedSATCOM LOCKED UP, ACFT GROUNDED. SAT PROMPT RESTORED AFTER QRH PROCEDURE.Apr 22, 2014 · N514AS · Boeing 737890 · Communications SystemSDR ASAA2014032307283Warning Message · false activationFMC DISAGREE LIGHT ON GROUND. ACFT GROUNDED. QRH PROCEDURE PERFORMED. OPS NORMAL.Mar 23, 2014 · N514AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014031207174Quick Disconnect · leakingHYDRAULIC LEAK NR 1 ENGINE. ACFT GROUNDED. FOUND A SYS HYD PRESSURE LINE QUICK DISCONNECT LEAKING AT PUMP CONNECTION. R & R PRESSURE LINE. RAN ENG AT GROUND IDLE FOR 15 MINUTES, NO LEAKS NOTED AT THIS TIME.Mar 12, 2014 · N514AS · Boeing 737890 · Hydraulic System, MainSDR ASAA2014030707107Control Unit · inoperativeLIGHT ILLUMINATED ON ELECTRICAL PANEL. ACFT GROUNDED. PERFORMED FIM 24-34, TASK 802. FOUND FAULT SPCU INOP 1. CLEARED FAULT AND DOES NOT RETURN. IAW FIM INTERMITTENT FAULT. NO HISTORY 90 DAYS. GROUND VERIFICATION SUCCESSFUL.Mar 7, 2014 · N514AS · Boeing 737890 · DC Generating SystemSDR ASAA2014022406977Warning Message · false activationON RECALL CONTROL CABIN ZONE TEMP LIGHT ILLUMINATED. EXTINGUISHES WITH MC RESET. ACFT GROUNDED. ACCOMPLISHED FIM TASK 21-62 TASK 842, NO ZONE TEMP LIGHT. INTERMITTENT FAULT. ACCOMPLISHED PACK ZONE TEMP CONTROLLER BITE PROCEDURE 21-62 TASK 801, NO FAULT.Feb 24, 2014 · N514AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2014020206753Warning Message · false activationFMC DISAGREE AFTER PUSHBACK. ACFT GROUNDED. QRH 11.2, STEPS 2-9 FOLLOWED. OPS NORMAL.Feb 2, 2014 · N514AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014012612493Warning Message · false activationDURING RECALL, CABIN ZONE TEMP LIGHT ILLUMINATED. DURING RESET, MASTER CAUTION LIGHT EXTINGUISHED. ACFT GROUNDED. PERFORMED A BITE TEST OF TEMPERATURE CONTROLLER IAW AMM 21-61-00-700-806-002. NO FAULTS NOTED.Jan 26, 2014 · N514AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2014011612416Warning Message · false activationFMC DIAGREE ON GROUND. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE. OPS NORMAL.Jan 16, 2014 · N514AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013120496634Spinner · damagedWHILE ACCOMPLISHING ENG INLET INSPECTION ON NR 2 ENGINE, FOUND FRONT SPINNER 50 LOSS OF ANODIZED COATING. ACFT GROUNDED.Dec 4, 2013 · N514AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2013101196164Actuator · malfunctionedRIGHT PACK LIGHT ILLUMINATED ON DESCENT. LIGHT EXTINGUISHED ON RECALL. ACFT GROUNDED. REPLACED RT RAM DOOR ACTUATOR IAW AMM 21-51-21. OPS CHECK GOOD IAW AMM 21-61-00-700-806-002.Oct 11, 2013 · N514AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013100696129Warning Light · illuminatedRIGHT PACK LIGHT ILLUMINATED DURING APPROACH WHEN MASTER CAUTION WAS CHECKED, IT RESET, WENT OUT, WHEN MASTER CAUTION WAS PUSHED. ACFT GROUNDED.Oct 6, 2013 · N514AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013100596111Warning Message · false activationFMC DISAGREE LT ON TAXI OUT. ACFT GROUNDED. ACCOMPLISHED FMC DISAGREE CHECKLIST FMC DISAGREE MESSAGE NO LONGER DISPLAYED.Oct 5, 2013 · N514AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013092496050Circuit Breaker · trippedHF NR 2 CIRCUIT BREAKER TRIPPED. ACFT GROUNDED. RESET CIRCUIT BREAKER IAW AMM 20-60-01-860-801. SYS OPS CHECKED GOOD IAW AMM 23-11-00-710-801.Sep 24, 2013 · N514AS · Boeing 737890 · HF Communications SystemSDR ASAA2013091696005Skin · damagedFUSELAGE SKIN CREASED BS 360 THRU 400 BETWEEN STRINGER 19L & 20L. REPAIRED CREASED SKIN WITH REPAIR DOUBLER AND TRIPLER IAW EA 800-53EA-11126, REV NEW DATED 22SEP13 AND REO-G16660, REV C, DATED 09/21/13.Sep 16, 2013 · N514AS · Boeing 737890 · Fuselage Main, Plate/SkinSDR ASAA2013090795980Skin · bentEXTERNAL POWER RECEPTICAL DOOR CUTOUT BENT AND SEALANT SEPARATED FROM SKIN. ACFT GROUNDED. REPAIRED EGPR DOUBLER IAW SRM 53-10-15-2R-4, REPAIR 4.Sep 7, 2013 · N514AS · Boeing 737890 · Fuselage Main, Plate/SkinSDR ASAA2013090795978Sill · gougedFWD CARGO DOOR SILL HAS SEVERAL GOUGES ON INNER FWD LOWER CORNER. ACFT GROUNDED. BLENDED GOUGES IAW SRM 51-10-2 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15-1A-1. REMOVED WEB IAW SRM 51-40-02. LOCATED & DRILLED NEW WEB IAW SRM 51-40-05. INSTALLED NEW Sep 7, 2013 · N514AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2013090795946Attach Angle · corrodedFWD CARGO COMPT AFT BULKHEAD LOWER ATTACH ANGLE CORRODED. REMOVED LOWER RAIL IN FWD PIT AFT AREA AT STA 500I IAW SRM 51-40-02. REMOVED CORROSION IAW SRM 53-00-53-1A-2. ORIG MAT 0.071 IAW BAC DWG 143A9485, REV F. REMOVED DAMAGE 0.025 AND REMAINING MAT 0.046 Sep 7, 2013 · N514AS · Boeing 737890 · Fuselage Main, Attach FittingsSDR ASAA2013090696004Seat Track · crackedCABIN SEAT TRACK AT BS 727B, RBL 45.50 CRACKED. ACFT GROUNDED. REPAIRED SEAT TRACK IAW REO G16605, REV C, AND EA 800-53, EA-11101.Sep 6, 2013 · N514AS · Boeing 737890 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2013090695987Transition Panel · puncturedAFT CARGO COMPARTMENT TRANSITION PANEL HAS DRILL SHANK AND LIGHT SURFACE CORROSION AT STA 727D, RBL 24. ACFT GROUNDED. REMOVED CORROSION, FOUND ADDITIONAL DAMAGE, PUNCTURE. ADDITIONAL DAMAGE FOUND TO BE OUT OF LIMITS. R & R CORROSION AND ADDITIONAL DAMAGE Sep 6, 2013 · N514AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2013090695986Web · corrodedAFT CARGO DOOR CUTOUT FROM BS 787-849 HAS CORROSION OF LOWER DOOR SILL WEB. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-60-15-1A-1, REMOVED WEB IAW SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-40-05. INSTALLED IAW SRMSep 6, 2013 · N514AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2013090495979Floor Panel · puncturedAFT CARGO COMPARTMENT FLOOR PANEL 140BF IS PUNCTURED. ACFT GROUNDED. FABRICATED NEW FLOOR PANEL IAW DWG 453A2610, REV E.Sep 4, 2013 · N514AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2013082095853Fmc · false indicationFMC DISAGREE ON TAXI OUT. ACFT GROUNDED. PERFORMED QRH PROCEDURE. FMC DISAGREE NOT ANNUNCIATED AFTER RESET OF C/BS.Aug 20, 2013 · N514AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013071495600Control Valve · failedON CLIMBOUT AND AT FL 360 LT AND RT DUCT PRESSURE SPLIT BY 20 PSI. LT READS 45 PSI RT 25 PSI. ACFT GROUNDED. WHILE ACCOMPLISHING TASK CARD NG-36WC-00001 NR 2 ENGINE BLEED AIR SYS HEALTH CHECK, FOUND PRECOOLER CONTROL VALVE FAILED STEP F. (5), FAILED TO MOVJul 14, 2013 · N514AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2013062995353Keyboard · inoperativeLEFT FMC MCDU 1L KEY NO TACTILE FEEL. ACFT GROUNDED. REPLACED THE LT FMCS CDU KEYBOARD IAW M 34-61-01, OPS CKS NORMAL.Jun 29, 2013 · N514AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013050594709Fmc · unknownFMC DISAGREE LIGHT ON TAXI OUT. ACFT GROUNDED. QRH PERFORMED, OPS NORMAL.May 5, 2013 · N514AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013050394681Handle · gougedAFT CARGO DOOR HANDLE MISSING BUMPER AND HANDLE HOUSING GOUGED. ACFT GROUNDED. GOUGE IN HANDLE HOUSING IS BEYOND ALLOWABLE DAMAGE LIMITS REF 52-31-15-801. REMOVED CARGO DOOR HANDLE MECHANISM 52-31-14-400-801. REMOVED CARGO DOOR HANDLE HOUSING SRM 51-40-02 PMay 3, 2013 · N514AS · Boeing 737890 · Cargo/Baggage DoorsSDR ASAA2013041794527Shutoff Valve · defectiveBLEED AIR DUCT PRESSURE SPLIT AT CRUISE FL380. RIGHT PRESSURE READS 41, LEFT PRESSURE READS 18. PERFORMED PNEUMATIC SYS TROUBLESHOOTING IAW AMM 36-11-00-700-804. FOUND NR 1 ENGINE PRSOV VALVE DEFECTIVE. R & R PRSOV IAW AMM 36-11-04-400-801. ACCOMPLISHED EApr 17, 2013 · N514AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2013041494464Fmc · warning lightFMC DISAGREE. QRH CHECKLIST ACCOMPLISHED. OPS NORMAL.Apr 14, 2013 · N514AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013031794211Valve · malfunctionedCONT CAB ZONE TEMP LIGHT ILLUMINATES ON RECALL, RESETS WITH MASTER CAUTION. ACFT GROUNDED. ZONE TEMP CONTROLLER NR 2 BITE FAULTS FLT DECK TRIM VALVE ON BITE AND PREVIOUS FLIGHT. REPLACED FLIGHT DECK TRIM VALVE (V143). BITE CHECK PASSES AND LEAK CK OK. REF Mar 17, 2013 · N514AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2013031494172Unknown · odorVERY STRONG UNPLEASENT ODOR ON DESCENT PASSING THRU 11000 FT UNTIL 3000 FT. F/A REPORT A CHEMICAL ODOR IN THE BACK. CABIN ODOR TROUBLESHOOTING ACCOMPLISHED AND APU REPLACED. AIR CONDITIONING SYS REPAIRED.Mar 14, 2013 · N514AS · Boeing 737890 · Air Distribution SystemSDR ASAA2013031394163Warning Light · false activationSTART VALVE OPEN LIGHT ILLUMINATED ON NR 2 ENGINE. CHECKLIST FOLLOWED TO NORMAL SHUTDOWN. STARTED NR 2 ENGINE WITH ALL NORMAL INDICATION. NO FURTHER ACTION. NO HISTORY 30 DAYS. ACFT RELEASED FOR SERVICE.Mar 13, 2013 · N514AS · Boeing 737890 · Central WarningSDR ASAA2013031194145Unknown · unknownOVERHEAD AIR TEMP, SUPPLY DUCT, PACK INDICATOR GAUGE READS ZERO IN ALL POSITIONS. COMPLETE CONTROL OF PASSENGER CABIN TEMP, SUPPLY DUCT, AND PACK TEMP. NO OTHER ABNORMAL INDICATIONS. PERFORMED OPS CHECK IAW AMM 21-61-32-400-801. OPS CHECKED NORMAL, NO HISTORMar 11, 2013 · N514AS · Boeing 737890 · Air Conditioning SystemSDR ASAA2013021893939Idg · leakingDURING NR 2 ENGINE IDLE RUN, FOUND IDG PAD DRAIN TUBE DRIPPING 60 DROPS. REPLACED NR 2 ENGINE IDG AMM 24-11-11. LEAK AND OPS CHECKED GOOD.Feb 18, 2013 · N514AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2013020693838Terminal · miswiredLEFT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED. COMPLETE QRH LIGHT EXTINGUISHED. ON DESCENT WINDOW OVERHEAT LIGHT ILLUMINATED AGAIN. C/W QRH. LT SLIDING WINDOW SENSOR FAILED FIM TASK 30-41-00-810-811, PG 4, PAR 6. RESISTANCE HIGH. SWAPPED WIRE TO SPARE TEMP SEFeb 6, 2013 · N514AS · Boeing 737890 · Ice/Rain Protection System WiringSDR ASAA2013013193799Warning Light · illuminatedLEFT OVERHEAT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED. FOUND LT SIDE WINDOW HEAT C/B P18-3 D3 OUT. RESET CIRCUIT BREAKER IAW AMM 20-60-01. OPS CHECKED LT SIDE WHCU IAW AMM 30-41-11. ALL OPS CHECKED NORMAL. RANG OUT SENSOR IAW AMM 30-41-21 RANG OUT GOOD. ALJan 31, 2013 · N514AS · Boeing 737890 · Overheat DetectionSDR ASAA2013012993764Valve · malfunctionedFOLLOW-UP TO NR 2 IDG FREQUENT SERVICING. ACCOMPLISHED STATIC LEAK CHECK REF MM 24-11-00-700-801, NO LEAKS NOTED. REPLACED IDG VENT VALVE REF MM 24-11-00-700-804, AND SERVICING FITTING REF CMM 24-11-85, MOTORED ENGINE AND LEAK CHECKED GOOD. IDG SERVICED TO Jan 29, 2013 · N514AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2013010293594Valve · malfunctionedCONT CAB ZONE TEMP LIGHT ILLUMINATED ON TAXI OUT. ACFT GROUNDED. ZONE TEMP CONTROLLER NR 2 SHOWS FLT DECK TRIM VALVE FAULT ON BITE AND PREVIOUS FLT. REPLACED CONT CAB ZONE TEMP VALVE AS REQUIRED. OPS CHECKED GOOD, REF AMM 21-61-21-400-801.Jan 2, 2013 · N514AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2012121193441Idg · failedSOURCE LIGHT NR 1 GENERATOR ILLUMINATED ALONG WITH NR 1 DRIVE LIGHT - QRH 6.9 AND 6.3 COMPLETE. PERFORMED TASK 24-11-11-090-801C3, REMOVED AND REPLACED NR 1 IDG AND NR 1 IDG AIR/OIL COOLER IAW 27-11-21-400-801. PERFORMED TASK 24-11-00-77-802 OPS CHECKS, NO Dec 11, 2012 · N514AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2012120293395Valve · failedDURING DESCENT, RT COWL VALVE OPEN LIGHT CYCLED TO BRIGHT BLUE NO CHANGE IN DUCT PRESSURE NOTED EXCEPT WHEN THE SWITCH WAS CYCLED. R & R NR 2 ENGINE COWL TAI VALVE IAW AMM 30-21-11, PB 401 OPS CHECKED GOOD.Dec 2, 2012 · N514AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA2012112393358Warning Light · false activationON TAXI OUT RECEIVED FMC DISAGREE MESSAGE. PERFORMED THE APPROPRIATE CHECK LIST IN THE QRH AND RESOLVED THE PROBLEM.Nov 23, 2012 · N514AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012112093348Warning Light · false activationFWD WINDOW OVERHEAT LIGHT ON. PERFORM FIM TASK 30-41 / 801 NO FAULTS FOUND. SUSPECT INTERMITTENT FAULT. NO HISTORY PAST 60 DAYS GROUND VERIFICATION CHECKS OK. ACFT OK FOR SERVICE.Nov 20, 2012 · N514AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2012112093333Unknown · unknownNR 2 ENGINE PERFORMED T/C 78273000 AND FOUND ECONOMIC FAULT 77-20872, THE TOP LEFT EGT SIGNAL (T495S4) IS OUT OF RANGE. ACCOMPLISH EEC BITE TEST. RECENT FAULTS 73-21-00-740-803-F00, NO FAULTS FOUND ON NR 1 & 2 ENGINES, REF L/P 7048197 FOR NO FAULTS FOUND.Nov 20, 2012 · N514AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2012111693308Warning Light · false activationON RECALL THE CONT CAB ZONE TEMP LIGHT CAME ON. QRH WAS CONDUCTED LIGHT GOES OUT ON MASTER CAUTION RESET. FAULT CODE 216.211.00 ACFT GROUNDED. PERFORMED BITE PROCEDURE ON NR 1 & NR 2 PACK/ZONE TEMP CONTROLLER IAW FIM TASK 21-62, TASK 801, NO FAULT NOTED NR Nov 16, 2012 · N514AS · Boeing 737890 · Central WarningSDR ASAA2012100393014Lamp · inoperativeEMERGENCY LIGHT EXIT LOCATOR SIGN AT R2 DOOR HAS MULTIPLE LAMPS INOPERATIVE. LAMPED AND TESTED IAW MM 33-51-01-960-801. OPS NORMAL.Oct 3, 2012 · N514AS · Boeing 737890 · Emergency LightingSDR ASAA2012090592836Autopilot Sys · malfunctionedAUTOPILOT WOULD NOT ENGAGE. REMOVED RT ADIRU IAW 34-21-01-000-807 AND REMOVED FCC IAW 22-11-33-00-801 FOR T/S IAW FIM TASK 22-11-00-810-807. PERFORMED CONTINUITY CHECK BETWEEN PINS C10 AND C11 OF D3693B AND B1 AND B2 OF D45257P NO FAULTS NOTED. PERFORMED COSep 5, 2012 · N514AS · Boeing 737890 · Autopilot System
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