N516AS

Service difficulty reports · 400

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 = 'N516AS' 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 ASAA2016062217125Sign · brokenEMERGENCY LIGHT EXIT LOCATOR SIGN AT R-1 DOOR IS BROKEN AND LENS IS MISSING. ACFT GROUNDED. REF WDM 33-51-21 REMOVED, REPLACED, AND TESTED L1186 EXIT LOCATOR SIGN AND LENS IAW AMM 33-51-01-960-802. OPS NORMAL.Jun 22, 2016 · N516AS · Boeing 737890 · Emergency LightingSDR ASAA2016061116995Control Valve · malfunctionedRIGHT PACK LIGHT ILLUMINATES WITH RECALL. PACK LIGHT EXTINGUISHES ON MASTER CAUTION RESET. ACFT GROUNDED. ACCOMPLISHED FIM 21-62, TASK 801. FOUND CURRENT STATUS AND PREVIOUS FLIGHT FAULTS TCV ON THE NR 2 PACK/ZONE TEMP CONTROLLER. BOTH PACK/ZONE TEMP CONTRJun 11, 2016 · N516AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016052216819Bulb · failedLEFT FORWARD EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. ACFT GROUNDED. RELAMPED LT FWD OVERWING EXIT LIGHT, REF AMM 33-51-04. OPS CHECK GOOD.May 22, 2016 · N516AS · Boeing 737890 · Emergency LightingSDR ASAA2016051016688Probe · failedWHILE ACCOMPLISHING TASK CARD 800-28EA-16443-1, FOUND THE NR 2 TANK COMP PROBE, NR 1 TU, NR 2 TU, AND NR 9 TU OUT OF LIMITS IAW AMM 28-41-21-710-801. ACFT GROUNDED. REPLACED THE NR 1 TANK COMPENSATOR PROBE IAW AMM 28-41-21/401. THE NEW NR 1 TANK COMPARTMENT May 10, 2016 · N516AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2016051016687Probe · failedWHILE ACCOMPLISHING TASK CARD 800-28EA-16443-1, FOUND NR 1 TANK COMPENSATOR OUT OF LIMITS IAW AMM 28-41-21-710-801. READ 61 PICOFARADS, LIMIT 58.7. ACFT GROUNDED. REPLACED THE NR 1 TANK COMPENSATOR PROBE IAW AMM 28-41-21/401. THE NEW NR 1 TANK COMP PROBE OPMay 10, 2016 · N516AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2016040616259Control Unit · failedFORWARD CABIN ZONE TEMP ILLUMINATED ON PUSH BACK RESETS WITH MASTER CAUTION RESET. ACFT GROUNDED. ACFT CHECKED. PERFORMED ZONE TEMP CONTROLLER BITE TEST IAW AMM 21-61-00. NR 2 CONTROLLER SHOWS FAULT ON ZONE TRIM VALVE. FAULT CLEARS AFTER VERIFY AND FLT DECKApr 6, 2016 · N516AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016040116189Filter · dirtyHAD ZONE TEMP LIGHT FOR CONTROL CABIN AND FWD CABIN ON RECALL. RESETS WITH MASTER CAUTION. ACFT GROUNDED. PERFORMED CABIN TEMP CONTROLLER BITE TEST ON BOTH RT AND LT BITE BOXES, REF FIM 21-61, TASK 801. FOUND ALL CABIN TEMP SENSOR FILTERS DIRTY. R & R FLIGHApr 1, 2016 · N516AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016031215860Warning Light · false activationFWD CABIN ZONE TEMP LIGHT CAME ON DURING PUSHBACK. MASTER CAUTION RECALL RAN QRH, LIGHT WENT OUT. ACFT GROUNDED.Mar 12, 2016 · N516AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016022715673Fan · damagedAFTER T/O, NR 2 ENGINE HAD A MOMENTARY EGT EXCEEDENCE. ACFT GROUNDED. EGT PEAKED AT 960 FOR 6-05 SECONDS. PERFORMED A GVI OF NR 2 ENGINE. NO FAULTS NOTED. ACCOMPLISHED FIM 71-06, TASK 805, EGT PEAK TEMP FALLS WITHIN TABLE A. CREATED A PLT DEFERRAL FOR NRFeb 27, 2016 · N516AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2016022515712Probe · failedTREND DATA SHOWS A INCREASE IN DELTA EGT AND DECREASE IN EGT HOT DAY MARGIN ON NR 2 ENGINE. ACFT GROUNDED. R & R NR 2 ENGINE T495S2 PROBE IAW AMM 77-21-01/401. NR 2 ENGINE ELECTRONIC ENGINE CONTROL BITE TESTED NORMAL WITHOUT FAULTS. T49.5 PROBE'S INPUT READFeb 25, 2016 · N516AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2016021315439Engine · faultedWHILE ACCOMPLISHING T/C 78273000 NR 2 ENGINE MAINT FAULT 77-10852, BOTTOM RT EGT SIGNAL T495S2 IS OUT OF RANGE, ECONOMIC FAULT. ACFT GROUNDED, ON DEFERRAL.Feb 13, 2016 · N516AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2016020315282Shim · wornDURING ACCOMPLISHMENT T/C 78472002 FAN BLADE LUBRICATION FOUND FAN BLADE SHIMS WORN TO LIMITS AT ENGINE NR 1. ACFT GROUNDED. R & R FAN BLADE SHIMS AT ENG NR 1, 24 EA IAW T/C 78472002.Feb 3, 2016 · N516AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2016012715067Satcom · malfunctionedFOLLOWING POWER TRANSFER, SAT NOT AVAILABLE ON ACARS MENU. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. SATCOM RESTORED NORMAL. ACCOMPLISHED VOICE TEST, TEST PASS REF AMM 23-15-00-730-801.Jan 27, 2016 · N516AS · Boeing 737890 · Communications SystemSDR ASAA2016012615027Satcom · malfunctionedMISSING SAT SELECTION ON THE MCDU MENU PAGE AND NO SATCOM PAGES AVAILABLE. ACFT GROUNDED. ACCOMPLISHED QRH SATCOM LOCKUP PROCEDURE ALL NORMAL SAT SELECTION AND SATCOM PAGES AVAILABLE, NORMAL OPS.Jan 26, 2016 · N516AS · Boeing 737890 · Communications SystemSDR ASAA2016011114731Satcom · lockedSATCOM LOCKUP, ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. SATCOM RESTORED NORMAL.Jan 11, 2016 · N516AS · Boeing 737890 · Communications SystemSDR ASAA2015121614296Valve · malfunctionedFOWARD CABIN ZONE TEMP LIGHT COMES ON WHEN RECALL IS PUSHED. IT GOES OUT WITH RESET. ACFT GROUNDED. R & R FWD CABIN ZONE TRIM MODULATING VALVE IAW AMM 21-61-21-000-801 AND AMM 21-61-21-400-801. GROUND FUNCTIONAL CHECK GOOD IAW AMM 21-61-00.Dec 16, 2015 · N516AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2015121114196Warning Light · false activationFWD CABIN-ZONE TEMP AMBER LIGHT ILLUMINATED ON RECALL. ACFT GROUNDED. NR 2 ZONE TEMP CONTROLLER LOGGED TRIM VALVE ZONE TEMP. RESET FAULT, PERFORMED BITE CHECK, OPS TEST NORMAL AMM 21-61-00.Dec 11, 2015 · N516AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2015120214245Lens · missingEMERGENCY LIGHT EXIT LOCATOR SIGN LENS MISSING AT R-1 DOOR. ACFT GROUNDED. REPLACED LENS AND TESTED LIGHT ASSY IAW AMM 33-51-01-960-801. OPS NORMAL.Dec 2, 2015 · N516AS · Boeing 737890 · Emergency LightingSDR ASAA2015111313756Warning Message · false activationAFTER ENGINE START, WE GOT A FMC DISAGREE MESSAGE. ACFT GROUNDED. ACCOMPLISHED QRH RESET PROCEDURE. NORMAL OPS RESTORED.Nov 13, 2015 · N516AS · Boeing 737890 · Central WarningSDR ASAA2015110213600Control Valve · failedLEFT PACK LIGHT ILLUMINATED ON RECALL. EXTINGUISHES WITH MASTER CAUTION. ACFT GROUNDED. PERFORMED BITE TASK 21-62-801. NR 1 TEMP CONTROLLER FAULTED TCV. R & R TCV REF MM 21-51-10. OPS CK/ LEAK CK GOOD. PACK LIGHT DOES NOT ILLUMINATE ON RECALL.Nov 2, 2015 · N516AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2015102913557Control Valve · malfunctionedAFTER LANDING, LT PACK LIGHT CAME ON, WENT OUT PRESSING MASTER RECALL. ACFT GROUNDED. BITE CHECKS LT PACK TEMP CONTROLLER IAW FIM 21-62, TASK 801. THIS PACK TCV FAULT DISPLAYED, RESET FAULT. RAN LT PACK, OPS CHECK GOOD ON GROUND. RECALL CK CLEAR.Oct 29, 2015 · N516AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2015101613513Warning Light · false activationON RECALL FWD CABIN ZONE TEMP LIGHT ON EXTINGUISHES WITH MASTER CAUTION RESET. ACFT GROUNDED. RIGHT PACK ZONE CONTROLLER LOG FAULT. RESET FAULT, PERFORMED BITE CHECK. BITE CHECK NORMAL, REF AMM 21-61-00.Oct 16, 2015 · N516AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2015101513509Controller · malfunctionedAUTO-FAIL LIGHT AND ALTN LIGHT ILLUMINATED ON PRESSURIZATION PANEL. ACFT GROUNDED. RESET SYS-SELECTING MANUAL MODE THEN BACK TO AUTO. PRESSURE CONTROLLERS SHOW NO CURRENT FAULTS AND GROUND TEST NORMAL IAW FIM 21-31, TASK 801. GROUND VERIFICATION SUCCESSFUL.Oct 15, 2015 · N516AS · Boeing 737890 · Cabin Pressure ControllerSDR ASAA2015092513199Control Unit · failedMAIN BATTERY SHOWS 1 AMP TO 2 AMP CHARGE THROUGHOUT FLIGHT -27 VOLTS. ACFT GROUNDED. R & R MAIN BATTERY AND AUX BATTERY, REF MM 24-31-11. OPS CHECK FAIL- ONCE CHARGED MAIN BATTERY VOLTS DROPPED TO 26V AND NEG 2 AMP DISCHARGE, THEN RETURNED TO 31V AND 2A CHASep 25, 2015 · N516AS · Boeing 737890 · Battery/Charger SystemSDR ASAA2015092013140Handle · faultedDURING PREFLIGHT TEST OF ENGINE FIRE DETECTION SYS, ENGINE NR 2 FIRE HANDLE DOES NOT ILLUMINATE. ACFT GROUNDED.Sep 20, 2015 · N516AS · Boeing 737890 · Detection SystemSDR ASAA2015091913098Light · malfunctionedDURING FIRE TEST, NR 2 ENGINE FIRE SWITCH DOES NOT LIGHT. ENGINE 2 OVERHEAT DOES NOT LIGHT. ACFT GROUNDED. PERFORMED T/S IAW FIM 26-10, TASK 803. PERFORMED ENGINE/APU FIRE DETECTION CONTROL MODULE BITE IAW FIM 26-10, TASK 801, NO FAULTS. CURRENTLY NR 2 ENSep 19, 2015 · N516AS · Boeing 737890 · Detection SystemSDR ASAA2015082512904Warning Light · false activationFWD CAB ZONE TEMP LIGHT ILLUMINATES ON RECALL AND EXTINGUISHES WITH RESET. ACFT GROUNDED. NR 2 PACK TEMP CONTROLLER LOGGED FWD CAB TRIM AIR FAULT, PERFORMED FIM 21-62, TASK 834 & FAULT CLEARED. PERFORMED PACK TEMP CONTROLLER BITE CK, FIM 21-62, TASK 801 & BIAug 25, 2015 · N516AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2015082012969Warning Light · illuminatedAFTER APU START THE MAINT LIGHT ILLUMINATED. ACFT GROUNDED. ON DEFERRAL.Aug 20, 2015 · N516AS · Boeing 737890 · Airborne Auxiliary Power Unit (APU) SystemSDR ASAA2015081312890Warning Message · false activationFMC DISAGREE, ACFT GROUNDED. FOLLOWED QRH, DUAL OPS RESTORED.Aug 13, 2015 · N516AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015080412726Autothrottle Sys · malfunctionedAUTOTHROTTLE CHECK ON TAXI WAS GOOD. RAN ENGINE TO 40 PERCENT, HIT TOGA AND AUTOTHROTTLE DISCONNECTED. REPEATED WITH SAME RESULT. ACFT GROUNDED. NO FAULTS LOGGED IN FAULT HISTORY. A/T CURRENT STATUS TEST PASSED REF MM 22-31-00. NO HISTORY PAST 30 DAYS.Aug 4, 2015 · N516AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2015072912630Modulating Valve · malfunctionedFWD CABIN ZONE TEMP LIGHT ILLUMINATED WITH RECALL, EXTINGUISHES WITH MASTER CAUTION RESET. ACFT GROUNDED. REPLACED THE FWD CABIN ZONE TRIM AIR MODULATING VALVE IAW AMM 21-61-21-00-801 AND AMM 21-61-21-400-801. BITE CHECK OF THE PACK/ZONE TEMPERATURE CONTROJul 29, 2015 · N516AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2015070612346Fmc · malfunctionedNO TEMP INPUT FOR FMC FROM PITOT PROBE SYS. NO T/O DATA AVAILABLE. ACFT GROUNDED. OPENED BOTH FMC C/B'S AND RESET. SIMULTANEOUS MAINTENANCE CDS BITE TEST, NO FAULTS FOUND. REFAMM FIM TASK 31-62 TASK 801. TAT PROBE OPS CHECKED, NO FAULTS FOUND, REF TASK 34Jul 6, 2015 · N516AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015062912268Warning Message · false activationON APPROXIMATELY AT APPROXIMATELY 5000' AGL AND AFTER SELECTING FLAPS TO 5 DEGREES, BOTH ND'S SHOWED "FMC DISAGREE" WITH A CDU MESSAGE INDICATING THE SAME. AFTER APPROXIMATELY 30 SECS BOTH MESSAGES WENT AWAY. NO QRH PROCEDURE WAS FOLLOWED. ACFT GROUNDED. ACJun 29, 2015 · N516AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015062512234Warning Light · no testDURING PREFLIGHT "ENG 2 OVERHEAT" & NR 2 FIRE HANDLE FAILED TO ILLUMINATE DURING OVHT, FIRE TEST. CHECKED LIGHTS & WORKED. ACFT GROUNDED.Jun 25, 2015 · N516AS · Boeing 737890 · Detection SystemSDR ASAA2015061012066Fault Code · activatedFOUND NR 1 ENGINE WITH A LONG TERM FAULT MESSAGE, 79-31121, OIL FILTER SIGNAL DISAGREE. ACFT GROUNDED. ACCOMPLISHED T/C. NO FAULTS DETECTED. PLT CLEARED.Jun 10, 2015 · N516AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2015060912044Warning Light · illuminatedAFTER LANDING, OIL FILTER BYPASS LIGHT ILLUMINATED ON NR 1 ENGINE ALL OTHER INDICATIONS NORMAL. ACFT GROUNDED. PARTIALLY REMOVED NR 1 OIL SCAVENGE FILTER BOWL, DURING REMOVAL BOWL THREADS SEIZED ON HOUSING, REF MM 79-21-06. COMPLETED REMOVAL OF NR 1 ENG OIL SJun 9, 2015 · N516AS · Boeing 737890 · Engine Oil Distribution (Airframe Furnished)SDR ASAA2015060611978Control Valve · malfunctionedFWD CABIN ZONE TEMP LIGHT ILLUMINATED ON RECALL, EXT ON MAST CAUTION RESET. ACFT GROUNDED. VERIFIED ZONE TRIM FAULT ON THE NR 2 ZONE TEMP CONTROLLER. REPLACED THE FORWARD CABIN ZONE TRIM MODULATING VALVE IAW AMM'S 21-61-21-000-801 AND 21-61-21-400-801. VALVEJun 6, 2015 · N516AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2015060511999Regulator · failedAFTER NR 2 ENGINE START, TURNED ON RT PACK & AIR CONDITIONER BLEED AIR VALVE RT CIRCUIT BREAKER OPENED. ACFT GROUNDED. REPLACED NR 2 ENGINE BLEED AIR REGULATOR REF AMM 36-11-03-400-801. OPS AND LEAK CHECKED GOOD.Jun 5, 2015 · N516AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2015060411998Valve · failedRIGHT DUCT PRESSURE READS 5 PSI IN FLIGHT GROUNDED. RETURNED TO DEPARTURE. DIVERSION TIME - 38 MINUTES. PERFORMED ENGINE BLEED HEALTH CHECK REF. T/C NG-36WC-00001 IAW STEP .04, HIGH STAGE VALVE FAILED WRENCH CHECK. REPLACED NR 2 ENGINE HIGH STAGE VALVE IAWJun 4, 2015 · N516AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2015053011905Fire Loop · no testDURING PREFLIGHT, NR 2 ENGINE LOOP "A" TESTS BAD. "B" TESTS NORMAL. ACFT GROUNDED. COULD NOT DUPLICATE PROBLEM. NR 2 ENGINE FIRE DET TEST, OPS NORMAL W/ SELECTOR SWITCH IN A, B, AND BOTH POSITION, SEVERAL SUCCESSFUL TESTS IN EACH POSITION. NO HISTORY LAST 90May 30, 2015 · N516AS · Boeing 737890 · Smoke DetectionSDR ASAA2015052911916Paint · missingNR 2 ENGINE SPINNER MISSING PAINT. ACFT GROUNDED.May 29, 2015 · N516AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2015052711877Controller · malfunctionedZONE TEMP FWD CABIN ILLUMINATED ON MASTER CAUTION RECALL. ACFT GROUNDED. BITE OF NR 2 CONTROLLER SHOWS ZONE FAULT LAST LEG. RESET FAULT & RAN BITE REF TASK 21-61-20. OPS CHECK NORMAL.May 27, 2015 · N516AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2015052711876Warning Message · false activationFMC DISAGREE ON THE GROUND. ACFT GROUNDED. QRH CHECKLIST COMPLETED. OPS NORMAL.May 27, 2015 · N516AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015051911782Valve · malfunctionedON RECALL, GOT FWD CAB ZONE TEMP LIGHT. EXTINGUISHES WITH MASTER CAUTION RESET. TEMPS NORMAL. ACFT GROUNDED. PERFORMED ZONE TEMP CONTROLLER BITE ON BOTH CONTROLLERS IAW FIM 21-62, TASK 801, FOUND NR 2 CONTROLLER ZONE TRIM VALVE FAULT. REPLACED FWD CAB ZONE May 19, 2015 · N516AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2015051311717Relay · malfunctionedRIGHT FWD FUEL PUMP "LOW PRESSURE" LIGHT ILLUMINATED IN CRUISE FLIGHT. RIGHT WING TANK WAS FULL. COMPLIED WITH QRH AND TURNED PUMP OFF. ACFT GROUNDED. FOUND GFI RELAY, R21, TRIPPED. RESET RELAY. PERFORMED GROUND FAULT INTERRUPTER OPS TEST REF MM 28-22-41-May 13, 2015 · N516AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA2015042711584Intercostal · crackedMAIN CABIN FLOOR, INTERCOSTAL CRACKED AT AFT HOLES, BS 344-360, LBL 11. ACFT GROUNDED. R & R INTERCOSTAL IAW DWG 141A5410, REV C, BS 344-360, LBL11 AND REMOVED INTERCOSTAL, TO FOM AND REINSTALLED BS 344-360, BL-0 IAW BAC DWG 141A5410.Apr 27, 2015 · N516AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015042411556Intercostal · crackedMAIN CABIN INTERCOSTAL FS 344-360 BL0 IS CRACKED AT FASTENER HOLE. ACFT GROUNDED. REMOVED CRACKED INTERCOSTAL IAW SRM 51-40-02. LOCATED AND DRILLED NEW INTERCOSTAL IAW DWG 141A5410, REV. B. INSTALLED NEW INTERCOSTAL IAW DWG 141A5410, REV B.Apr 24, 2015 · N516AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015042411555Floorbeam · crackedMAIN CABIN PANEL BREAK IS CRACKED, FS 540, BL 0 TO RBL 24. ACFT GROUNDED. R & R PANEL BREAK IAW SRM 51-40-02. REMOVED IAW DOT K449.Apr 24, 2015 · N516AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2015042411554Floorbeam · crackedMAIN CABIN PANEL BREAK IS CRACKED, FS 540, BL 0 TO LBL 24. ACFT GROUNDED. R & R PANEL BREAK IAW SRM 51-40-02. REMOVED DOT K448.Apr 24, 2015 · N516AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2015042211621Skin · gougedRIGHT ELEVATOR OTBD LOWER SKIN SCRAPED AND DENTED. ACFT GROUNDED. REPAIR RT ELEVATOR LOWER SKIN AT STA 218.5 TO 219.5 BY SEPARATING ELEVATOR SKINS TO STA 178-16, REMOVING DAMAGED SKIN SECTION AND APPLYING CARBON REPAIR IAW SRM 55-20-01 AND 51-70-05, REASSEMBApr 22, 2015 · N516AS · Boeing 737890 · Elevator, Plate/Skin
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