N402AS
Service difficulty reports · 333
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 = 'N402AS' 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 = 'N402AS' 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 ASAA2018081095730Warning Light · false activationRIGHT PACK FAILED. ACFT GROUNDED. FOUND THE RIGHT PACK LIGHT ILLUMINATES ON RECALL, BUT CLEARS. RIGHT CONTROLLER SHOWS TCV FAULT LAST LEG. ACCOMPLISHED IAW FIM 21-62, TASK 831. FAULT CLEARS AND BITE TESTED GOOD . NO PREVIOUS HISTORY.SDR ASAA2018070525303Fmc · malfunctionedDURING CRUISE FLIGHT AT FL340 LT FMC FAILED FOR APPROXIMATELY 1 MINUTE WITH VTK DISPLAYED ON CAPTAIN INBOARD DU AND LNAV DISENGAGED, SELECTED B AUTOPILOT AND LNAV AND SYSTEM RESTORED. GROUNDED - YES. LEFT FMC LOGGED PRES POS LAT- RATE FAULT. ACCOMPLISHED BOTH SDR ASAA2018070225239Controller · malfunctionedON DESCENT CHECKLIST AND RECALL RIGHT PACK LIGHT STAY ILLUMINATED. RAN QRH AND LIGHT EXT. WHEN RESET MASTER CAUTION. GROUNDED - YES. PERFORMED PACK ZONE/TEMP CONTROLLER BITE TEST ON NR 1 & NR 2 CONTROLLER PER AMM 21-61-00-700-806-002. NR 2 CONTROLLER SHOWS RT SDR ASAA20180625177Panel · damagedWHILE ACCOMPLISHING TC 78472000 ON THE NR 2 ENGINE, FOUND FAN DUCT PANEL NR 12, AFT OTBD FASTENER PULLED THRU THE PANEL. ACFT GROUNDED. REMOVED AND REPLACED KEY-LOCKED INSERT FOR THE NR 12 FAN DUCT PANEL IAW SPM 70-42-13. INSTALLED THE FAN DUCT PANEL IAW SDR ASAA2018062125153Panel · damagedWHILE ACCOMPLISHING TC 78472000 NR 2 ENGINE S/N 963292 FOUND FAN DUCT PANEL NR 12 AFT O/B FASTENER PULLED THRU PANEL. GROUNDED - YES. REMOVED NR 2 ENGINE REF T/C 78471000 FOR ACCESS TO FAN DUCT PANEL NR 12 INSERT REPLACEMENT. REMOVED AND REPLACED KEY-LOCKED INSDR ASAA2018061865071Autoland Sys · malfunctionedAUTOLAND, AUTOPILOT STEERED LEFT THEN RIGHT IN FLARE. LEFT MAIN WHEEL TOUCHED DOWN ON CENTERLINE. ACFT GROUNDED. ACCOMPLISHED LAND VERIFICATION TESTS IAW AMM 22-11-00-700-801, AND ALL LLM TESTS LISTED IN AMM 22-00-01-730-803. ALL TESTS PASSED. NO HISTORY LASDR ASAA2018061425220Idg · unknownFOLLOW-UP TO NR 1 IDG CONTINUED FREQUENT SERVICING. GROUNDED - YES. NR 1 IDG OIL LEVEL WAS JUST BELOW ADD MARK. CLEANED/INSP IDG AND ASSOCIATED PLUMBING. NO LEAKS. PERFORMED STATIC LEAK TEST PER AMM 4-11-00-700-801. PRESSURE STABLE AT 25 PSI FOR OVER 1 HOUR. RSDR ASAA2018031123878Floorbeam · crackedFWD CARGO, FLOORBEAM ANGLE AT BS 500K CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-40-02 AND DWG 143A7505, REV -.SDR ASAA2018030823953Floorbeam · crackedFWD CARGO RT FLOORBEAM ANGLE AT BS 500J AFT SIDE IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE FLOORBEAM ANGLE 6.1 IAW SRM 51-40-02 & DWG 143A7505, REV-.SDR ASAA2018030823877Floorbeam · crackedFWD CARGO, RT FLOORBEAM ANGLE AT BS 500K FWD SIDE IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-40-02, AND DWG 143A7505, REV-.SDR ASAA2018030823876Floorbeam · crackedFWD CARGO RIGHT FLOORBEAM ANGLE, BS 500J FWD SIDE IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-40-02, AND DWG 143A7505, REV-.SDR ASAA2018030723875Floor Support · crackedFWD CARGO BAY FLOOR SUPPORT, BS 500J - 500K, RBL 25 IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 143A7505, REV-.SDR ASAA2018030723874Floor Support · crackedFWD CARGO BAY FLOOR SUPPORT, BS 500H - 500I, RBL 25 IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE FWD FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 143A1505, REV -.SDR ASAA2018030623972Gusset · corrodedAFT CARGO BAY FLOOR SUPPORT GUSSET HAS CORROSION, BS 767, STRINGERS 25R AND 26R. ACFT GROUNDED. REMOVED & REPLACED THE GUSSET IAW SRM 51-40-02, & DWG 146A0081, REV-.SDR ASAA2018030623840Transition Panel · crackedAFT PIT RT SIDE TRANSITION PANEL HAS CRACK AT BS 727K ABOVE STR 26R. GROUNDED - YES. REPAIR ACCOMPLISHED ON CARD G0973086.SDR ASAA2018030623839Transition Panel · crackedAFT PIT RT SIDE TRANSITION PANEL HAS CRACK AT BS 727J ABOVE STR 26R. GROUNDED - YES. REPAIR ACCOMPLISHED ON CARD G0973086.SDR ASAA2018030623838Transition Panel · corrodedAFT PIT RT SIDE TRANSITION PANEL HAS CORROSION NUMEROUS PLACE BETWEEN BS727I+6 AND BS767 AS MARKS. GROUNDED - YES. REMOVED CORROSION ON AFT PIT RT TRANSITION PANEL FROM STA 727I+6 TO STA 767 IAW SRM 51-10-02. ORIGINAL THICKNESS IS .040, REMAINING THICKNESS IS SDR ASAA2018030623837Transition Panel · corrodedAFT PIT RT SIDE TRANSITION PANEL HAS CORROSION NUMEROUS PLACE BETWEEN BS 727E AND BS727G AS MARKS. GROUNDED - YES. REMOVED CORROSION ON AFT PIT RT TRANSITION PANEL BETWEEN STA 727E AND 727G IAW SRM 51-10-02. ORIGINAL THICKNESS IS .040. FROM STA 727E TO STA 727SDR ASAA2018030623827Shield · corrodedAFT CARGO COMPARTMENT FLOOR SUPPORT SHIELD HAS CORROSION BETWEEN BS 767 AND BS 787, STR 25R AND STR 26R. GROUNDED - YES. REMOVED CORROSION ON SHIELD IAW SRM 51-10-02 ORIGINAL THICKNESS IS .050 REMAINING THICKNESS IS .040 LOSS OF .010 OUT OF LIMITS IAW SRM 53-6SDR ASAA2018030623795Transition Panel · corrodedAFT CARGO BAY, RT SIDE TRANSITION PANEL HAS CORROSION NUMEROUS PLACES BETWEEN BS 727G AND 727I+6. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. REMOVED AND REPLACED THE SECTION IAW SRM 51-40-02 & DWG 146A750SDR ASAA2018030523955Floor Support · crackedMAIN CABIN INTERNAL FLOOR SUPPORT CRACKED BS 312 - 328, RBL 30. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02. DWG 141A5410, REV A, AND SRM 51-40-10-2R-0.SDR ASAA2018030523954Floor Support · crackedMAIN CABIN FLOOR SUPPORT CRACKED, BS 312 - 328, LBL 46. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 141A5400, REV-.SDR ASAA2018030523826Transition Panel · corrodedFORWARD CARGO COMPARTMENT RIGHT SIDE TRANSITION PANEL CORRODED BS 500A - BS 500L, RBL 23. GROUNDED - YES. REMOVED CORROSION ON RT TRANSITION PANEL IN FWD CARGO STA 500A-500L IAW SRM 51-10-02 LOWEST READING STA 500A-500E+7 IS .037 ORIG THICKNESS .040 REMOVED .0SDR ASAA2018030423825Floor Support · crackedCBN UNDER FLOOR CROSS FLOOR SUPPORT CHANNEL CRACKED BS 540, LBL 1. GROUNDED - YES. LOCATED AND DRILLED NEW SUPPORT CHANNEL AND COVER PLATE IAW SRM 51-40-05 AND DWG 143A5240 REV- . INSTALLED NEW SUPPORT AND COVER PLATE IAW SRM 51-40-02 AND BAC DWG 143A5240 REV-SDR ASAA2018022223670Filter · dirtyAT INITIAL LEVEL OFF , FLIGHT ATTENDANT REPORTED EXCESSIVELY WARM OR HOT. PERFORMED QRH AND TEMPERATURES RETURNED TO NORMAL WITH TRIM AIR OFF. ACFT GROUNDED. CLEANED COCKPIT AND FWD CABIN AND AFT CABIN TEMPERATURE SENSOR ASSEMBLY FILTERS IAW AMM 21-61-06-10SDR ASAA2018022023635Actuator · faultedWHILE PERFORMING BITE IAW AMM 21-51-00, THE NR 2 CONTROLLER RAM AIR ACTUATOR FAULT LIGHT. ACFT GROUNDED. REMOVED & REPLACED THE RT RAM AIR INLET ACTUATOR IAW AMM 21-51-21, OPS CHECKED NORMAL. NR 2 PACK/ZONE TEMP CONTROLLER BITE TESTED IAW AMM 21-61-00-700-80SDR ASAA2018022023637Warning Light · false activationCONTROL CABIN TEMP ZONE LIGHT ILLUMINATED ON RECALL. ACFT GROUNDED. PERFORMED A BITE CHECK IAW AMM 21-51-00, FLT DECK TRIM VALVE NR 2 CONTROLLER RESET.SDR ASAA2018021323526Lens · missingAFT EMERGENCY EXIT LIGHT COVER MISSING. ACFT GROUNDED . INSTALLED THE LENS.SDR ASAA2018012223264Idg · failedON DEPARTURE PASSING 24K FEET NR 1 DRIVE ILLUMINATED, FOLLOWED QRH NR 1 DRIVE DISCONNECT ACTIVATED. ACFT GROUNDED. PERFORMED FIM 24-11 TASK 801, GCU BITE INDICATES NR 1 IDG FAILURE, DRAINED OIL AND INSPECTED FILTERS, NO CONTAMINATION NOTED. REMOVED IDG IAW SDR ASAA2018010923113Light · damagedA FLIGHT ATTENDANT REPORTED THAT THE FORWARD SIX INCHES OF THE FLOOR EMERGENCY LIGHT STRIP WAS MISSING. ACFT GROUNDED. INSTALLED A NEW SECTION OF EMERGENCY LIGHT IAW AMM 33-51-15-960-801.SDR ASAA2017122823020Warning Light · false activationCONTROL CAB ZONE TEMP LIGHT ILLUMINATED WITH MASTER CAUTION RECALL. LIGHT EXTINGUISHED WITH MASTER CALL RESET. TEMP CONTROL FOR CONTROL CABIN IS OPERATIVE. ACFT GROUNDED. ACCOMPLISHED PACK ZONE TEMP CONTROL BITE CHECK. NR 1 CONTROLLER PASSED, NO FAULTS NOTSDR ASAA2017121722946Sensor · malfunctionedWINDOW OVERHEAT LIGHT ON, REMAINED ON AFTER QRH PROCEDURE, RIGHT FWD WINDOW. ACFT GROUNDED. PERFORMED A BITE CHECK OF WHC. FOUND SENSOR FAULT ON THE R1 WINDSCREEN. SWAPPED SENSORS AT TOGGLE SWITCH. PERFORMED SECOND BITE CHECK OF WHC NO FAULTS FOUND AT THISDR ASAA2017112722701Warning Light · malfunctionedSTAB OUT OF TRIM LIGHT ILLUMINATED AT SOME POINT ON FINAL APPROACH, WHILE HAND FLYING. LEFT LIGHT REMAINED ILLUMINATED DURING TAXI IN AND SHUT DOWN. ACFT GROUNDED. VERIFIED DEFECT, STAB TRIM OUT OF TRIM ILLUMINATED LEFT AND WAS INTERMITTENT. ACCOMPLISHED SDR ASAA2017111922644Warning Light · false activationAT ROTATION, THE STAB OUT OF TRIM LIGHT ILLUMINATED AND STAYED ON THRU 12200 FT WHILE HAND FLYING. PASSING FL 212 STILL HAND FLYING, THE STAB OUT OF TRIM LIGHT ILLUMINATED AGAIN AND STAYED ON THE REMAINDER OF THE FLIGHT. AUTO PILOT WAS ENGAGED. OPS NORMAL. FIRSDR ASAA2017102922346Autoland Sys · malfunctionedAUTOLAND UNSATISFACTORY. LANDED MORE THAN 35 FT LEFT OF CENTER LINE. ACFT GROUNDED. PERFORMED FIM 22-11, TASK 825. ACCOMPLISHED FIM 22-11, TASK 801 DIGITAL FLIGHT CONTROL SYSTEM BITE PROCEDURE. NO ACTIVE FAULTS FOUND. ACCOMPLISHED MMR NR 1 AND 2 BITE. NO FASDR ASAA2017102322292Autothrottle Sys · malfunctionedAUTOTHROTTLE CIRCUIT BREAKER TRIPPED. ACFT GROUNDED. CLOSED THE CIRCUIT BREAKER IAW AMM 20-60-01. ACCOMPLISHED AN AUTOTHROTTLE BITE CHECK. NO FAULTS IAW AMM 22-31-00. ACCOMPLISHED SERVO MOTOR TEST, NO FAULTS NOTED.SDR ASAA2017100122085Sign · brokenEMERGENCY LIGHT EXIT SIGN AT THE NR 1 GALLEY ADJACENT TO THE R1 DOOR IS BROKEN. ACFT GROUNDED. REMOVED, REPLACED, AND TESTED EXIT SIGN ASSY IAW MM 33-51-01-960-802. OPS NORMAL.SDR ASAA2017092822071Spacer · detachedWHILE ACCOMPLISHING T/C 78472002 FOR NR 1 ENGINE FAN LUBRICATION. FOUND THE NR 1 BLADE SPACER RUBBER COMING OFF. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE BLADE NR 1 SPACER IAW T/C 78472002 AND T/C 78472002.SDR ASAA2017092322012Warning Message · false activationDURING CLIMB, ABOVE 10,000 FEET, THE RIGHT SIDE WINDOW HEAT OVERHEAT LIGHT ILLUMINATED AND RESET AFTER QRH PERFORMED. ACFT GROUNDED. PERFORMED BITE ON RIGHT WHCU IAW FIM 30-41, OPS CHECKED GOOD, NO DEFECTS NOTED.SDR ASAA2017092322011Window · overheatedRIGHT WINDOW OVERHEAT IN FLIGHT. WOULD NOT RESET IAW QRH. ACFT GROUNDED. REMOVED AND REPLACED THE WINDOW IAW AMM 56-12-11-401. FUNCTION AND OPS CHECKED GOOD.SDR ASAA2017092222013Sensor · malfunctionedRT SIDE WINDOW OVERHEAT AT GATE. ACFT GROUNDED. REPOSITIONED RT SIDE WINDOW PRIMARY SENSOR TO SPARE SENSOR IAW FIM 30-41 TASK 811, AND WDM 30-41-11, SHEET 2. OPS CHECKED NORMAL NO FAULTS IAW AMM 30-41-00.SDR ASAA2017053120923Warning Message · false activationRIGHT PACK LIGHT ON RECALL, EXTINGUISHED WITH MASTER CAUTION RESET. ACFT GROUNDED. FOUND RIGHT PACK TCV FAULT LIGHT ON. RESET RIGHT PACK TEMP CONTROLLER. RIGHT PACK OPS CHECKED GOOD IAW FIM 21-62 TASK 831.SDR ASAA2017052120845Fire Detector · failedMASTER CAUTION FOR APU DETECTION LOOP INOPERATIVE. ACFT GROUNDED. FOUND APU TAILPIPE FIRE DETECTOR FAULT LIGHT ON MODULE. REMOVED AND REPLACED THE APU TAIL PIPE FIRE DETECTOR IAW AMM 26-15-01. OPS CHECKED NORMAL.SDR ASAA2017050520649Grommet · wornNR 2 ENGINE FIRE LOOP MW0326 GROMMET WORN. ACFT GROUNDED. REMOVED AND REPLACED THE GROMMET IAW AMM 26-11-02.SDR ASAA2017040920406Warning System · false activationRIGHT PACK LIGHT ILLUMINATES ON RECALL. GOES OUT WITH PUSH OF MASTER CAUTION BUTTON. GROUNDED - YES. ACCOMPLISHED PZTC BITE, REF FIM 21-62 TASK 801. NR 2 CONTROLLER FAULTED TCV ON BIT AND PREVIOUS FLIGHT WITH A GO ON VERIFY. ACCOMPLISHED FIM 21-62 TASK 831 RIGSDR ASAA2017040420362Satcom · lockedSATCOM LOCK-UP OCCURRED. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE PER QRH. SATCOM OPS RESTORED NORMAL.SDR ASAA2017032720282Satcom · lockedSATCOM LOCKUP AFTER POWER TRANSFER. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. SATCOM OPS RESTORED NORMAL.SDR ASAA2017032420253Satcom · lockedSATCOM LOCK-UP. RAN CHECKLIST, SYSTEM DID RESET. GROUNDED. VERIFIED SATCOM PROMPT IS AVAILABLE AND SATCOM NOT LOCKED UP. IAW FIM 23-15 TASK 801.SDR ASAA2017032320255Anti-Ice Valve · failedNR 2 ENGINE DISPLAYED AMBER TAI INDICATION WHEN ENGINE ANT-ICE TURNED ON. ACFT GROUNDED. REPLACED THE NR 2 ENGINE INLET COWL THERMAL ANTI-ICE VALVE ASSY IAW AMM 30-21-11. THIS CLEARS MEL 30-4C.SDR ASAA2017031720228Stringer · dentedSTRINGER 25L IS DENTED AT BS 802. ACFT GROUNDED. REPAIRED THE STRINGER IAW ER 17-01746 AND EA 900ER-53EA-18647.
Back to N402AS