JASC 7830
Service difficulty reports · 5,918
Reports filed under 7830 · Engine Thrust Reverser, 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 jasc_code = '7830' 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 jasc_code = '7830' 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 COMA0260485Thrust ReverserFLIGHT 5770 T/O ABORTED DUR TO REVERSE UNLOCK WARNING.SECURED THE R/H ENGINE T/R AND DEFERRED MAINTENANCE PER MEL.SDR AUS20020901Module · leaking(AUS) RH ENGINE THRUST REVERSER HYDRAULIC ISOLATION LEVER ASSEMBLYFAILED ALLOWING HYDRAULIC FLUID TO LEAK.SDR USA2002F00078Warning Light · false indicationTHE NR 1 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. CAPTAIN FELT THE AIRCRAFT YAW, SO HE SHUT DOWN THE NR 1 ENGINE. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. TOTAL SINGLE ENGINE TIME WAS 20 MINUTESDR USAA020343Support · brokenCLT - FOUND APPROX 8 INCH SECTION BROKEN/MISSING, NR 1 ENGINE T/R 11 O'CLOCK POSITION. REMOVED AND REPLACED T/R REAR CASCADE SUPPORT RING PER SRM 51-10-02. (M)SDR GTIA020909Thrust Reverser · dentedFTW - FOUND THREE DENTS ON FORWARD PART OF LOWER T/R 1 ENGINE. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)SDR AWXA200200662Beam · wornMCN - MAJOR REPAIR - DURING C-12 CHECK ELONGATED HOLES WERE FOUND ON THE # 1 ENGINE INBOARD THRUST REVERSER UPPER SUPPORT BEAM. MAINTENANCE DRILLED DAMAGED HOLES ON # 1 ENGINE INBOARD THRUST REVERSER UPPER SUPPORT BEAM TO A LARGER DIAMETER, FABRICATED 2 EACH DSDR AWXA200200548Warning Light · illuminatedABORTED TAKEOFF - FLT 0130 - TAKING OFF FROM SNA TO LAS. NR 1 ENGINE THRUST REVERSER LIGHT ILLUMINATED ON TAKEOFF AT 100KTS. NR 1 THRUST REVERSER DEACTIVATED AND PLACED ON "MEL 78-7 CONDITION NR 1. SUPPLIMENTAL OPENSDR GTIA020948Acoustic Panel · crackedFTW - FOUND NR 1 ENGINE T/R HAS DENT AND CRACK AT ACOUSTIC PANEL. T/R REPLACED ON BOO03611-R-2. (M)SDR C2XA02IA122Warning System · activatedIAH- DURING FLIGHT 3921, THE CREW NOTED THAT THE NUMBER 1 ENGINE THRUST REVERSER DISAGREE MESSAGE ILLUMINATED ON THE EICAS. THE CREW RETURNED THE AIRCRAFT TO IAH WITHOUT INCIDENT.SDR AALA20020822B-Nut · looseLAS - FLT 1236 - WHILE TAXIING AT LAS, CABIN AND COCKPIT FILLED WITH SMOKE, PERFORMED EMERGENCY EVACUATION. TURNED OFF APU SMOKE STOPPED. SECURED LOOST B-NUT AT LEFT THRUST REVERSER. CLEANED ACCUMULATOR AREA. ACCOMPLISHED PACK BURN OUT. SYSTEM GROUND CHECSDR 02FDEA00372Thrust Reverser · unlockedPDIS- AFTER TAKEOFF FROM TULSA HAD IND OF NR 1 REVERSER UNLOCKED, UPON SLAT RETRACTION HAD YAW COMMENSURATE WITH UNLOCKED REVERSER. R/R LT THRUST REVERSER CDU SWITCH.SDR 02FDEA00375Fitting · crackedNR 2 ENG LT T/R COWL UPPER TRANSLATING SLEEVE CHANNEL END FOUND CRACK. HFEC CARRIED OUT CRACK LENGTH APPROX .625 INCH LONG. R&R COWL & INSTALLED FITTING AT UPPER TRACK BEAM.SDR AALA20020755Switch · malfunctionedPHL - FLT 1479 - EN ROUTE PHL-DFW - AFTER TAKEOFF, LEFT ENGINE REVERSER UNLOCK LIGHT ILLUMINATED AND REMAINED ON. RETURNED AND LANDED PHL WITHOUT INCIDENT. REPLACED BOTH UPPER AND LOWER LATCH SWITCHES. PERFORMED OPERATION CHECK. SYSTEM GROUND CHECKED NORMASDR UPS02438358Skin · crackedINSPECTION TYPE:N/A NR 4 ENG HONEYCOMB SKIN CRACKED 3 O'CLOCK POS INSIDE ON INSIDE OF T/R A/C FERRIED TO HKG FOR C CHECK REPAIR TO BE COMPLETED. NR 4 ENG T/R SLEEVE INNER SKIN CRACKED AND DELAM AREA REPAIRED REF SRM 54-34-03 FIG 26.SDR SIMA200215119Switch · failedAMA - FLT 3861 - FLIGHT CREW REPORTED ENGINE NR 2 THRUST REVERSER HAD FAILED INDICATION ON EICAS DURING APPROACH. REPLACED LOWER OUTBOARD STOW SWITCHES AND BOTH UPPER STOW SWITCHES S/N'S 2374, 2370. (M)SDR C1HA200281005Switch · lack of lubeNR 3 REVERSER OPERATING LIGHT ILLUMINATED AT FL 330 AND NORMAL THRUST SETTING. PERFORMED COM PROCEDURE, LIGHT REMAINED ILLUMINATED. PERFORMED VISUAL INSPECTION OF TR ACTUATOR SWITCH AND CONNECTIONS. INSPECTED ACTUATOR AND TR BUCKETS FOR LOOSENESS. OPERATEDSDR 02FDEA00348Connector · contaminatedON TAKEOFF ECAM WARN NR 1 REVERSER PRESS FOLLOWED ECAM INSTRUCTIONS TO BRING NR 1 THROTTLE TO IDLE. FOUND CANNON PLUG GOING TO DIRECTIONAL PILOT VALVE WITH MOISTURE. CLEANED PLUG AND RAN NR 1 ENG. OK FOR SERVICE.SDR UPS02238288Bracket · crackedINSPECTION TYPE:C #1 ENG. TR PRIMARY ACTUATOR FAIRING MID. ATTACH BRACKET CRACKED REPLACED BRACKET IAW SRM 51-30-02 & MM 20-80-01SDR UPS02238287Bracket · crackedINSPECTION TYPE:C #3 ENG. TR PRIMARY ACTUATOR FAIRING MID ATTACH BRACKET CRACKED REPLACED BRACKET IAW SRM 51-30-02 & MM 20-80-01SDR GTIA020428Door · crackedDTW - FOUND CRACK IN THE NR 2 UPPER T/R DOOR. STOP DRILLED CRACK AND INSTALLED DOUBLER. (M)SDR GTIA020446Support Bracket · crackedFTW - FOUND ENGINE NR 1 T/R INTERLOCK MECH SUPPORT BRACKET CRACKED. REMOVED BRACKET NR 1 ENGINE T/R INTERLOCK MECH. INSTALLED BRACKET ON NR 1 ENGINE T/R INTERLOCK MECH. (M)SDR A6WA200240016Fairing · crackedNR 2 ENGINE UPPER STANG FAIRING CRACKED MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE UPPER STANG FAIRING.SDR A6WA200240013Thrust Reverser · crackedNR 1 ENGINE THRUST REVERSER UPPER CASCADE IS CRACKED. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE THRUST REVERSER UPPER CASCADE.SDR A6WA200240015Fairing · crackedNR 1 ENGINE UPPER STANG FAIRING CRACKED MAINTENANCE REMOVED AND REPLACED UPPER STANG FAIRING.SDR A6WA200240014Thrust Reverser · crackedNR 2 ENGINE THRUST REVERSER UPPER CASCADE IS CRACKED. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE THRUST REVERSER UPPER CASCADE.SDR CA020502022Switch · failed(CAN) DURING FLIGHT AT FL290, THE RT REVERSER UNLOCK MESSAGE APPEARED. AIRCRAFT DIVERTED TO ATLANTA AND LANDED WITHOUT FURTHER INCIDENT. RT THRUST REVERSER DEFERRED PER MEL. LATER R&R RT ENGINE TR STOW SWITCH IAW AMM 78-37-01-400-801. RT THRUST REERSER OPS CHESDR SWIA200210799Switch · out of adjustDURING CLIMBOUT RECEIVED LEFT THRUST REVERSER UNLOCKED MESSAGE. FOLLOWED QRH AND RETURNED TO GSO. ADJUSTED THROTTLE LOCKOUT MICROSWITCH IAW CRJ MM 78-30-00. OPS CHECK GOOD.SDR AUS20020362Segment · separated(AUS) DURING INSPECTION, THE LT ENGINE INBOARD THRUST REVERSER NR 1 CASCADE (PN LJ76662) AND THE SUPPORT RING SECTION (PN LJ7599) WERE FOUND MISSING.SDR 200200245Vane · crackedLEFT HAND NR 4 CASCADE VANE WAS CRACKED AT AFT ATTACH AREA. REPLACED CASCADE VANE IN ACCORDANCE WITH B747 M/M 78-31-07.SDR AUS20020319Nut · worn(AUS) NO1 ENGINE THRUST REVERSER FAULTY. FEEDBACK LEVER AND CABLE COULD BE MOVED FROM THE STOWED POSITION TO THE DEPLOYED POSITION WITH THE THRUST REVERSER LOCKED OUT. INVESTIGATION FOUND THE PROBLEM WAS CAUSED BY WEAR ON THE FEEDBACK NUT PNO 315A1814-1.SDR COMA0260236Power Unit · malfunctionedFLIGHT 5931 R/H THRUST REVERSER UNLOCKED MESSAGE DURING T/O.REPLACED THE PDU.SDR CA020408012Vane · misinstalled(CAN) DURING CUSTOMER ACCEPTANCE FLT, UPON TOUCH DOWN & AFTER APPLICAITON OF FULL THRUST REVERSER POWER, A/C VEERED TO RT APPROX. 30 TO 40 DEGS FROM RWY HEADING. CORRECTIVE ACTION TO STOW THRUST REVERSERS & CONTROL DIRECTIONAL CONTROL USING RUDDER. INVESTIGSDR CA020502013Thrust Reverser · contaminated(CAN) BOTH REVERSERS ONLY DEPLOYED AT MID TRAVEL ON LANDING.FOUND MOISTURE TRAP IN THE THRUST REVERSERS CDU (CONTROL AND DRIVE UNIT). REMOVED ALL MOISTURE, FUNCTIONAL TEST CARRIED OUT, AIRCRAFT FOUND SERVICEABLE.SDR AUS20020271Blocker Door · separated(AUS) NR 4 ENGINE THRUST REVERSER NR 5 BLOCKER DOOR SEPARATED IN FLIGHT. DAMAGE CAUSED TO RT OUTBOARD AILERON.SDR 02FDEA00202Thrust Reverser · malfunctionedDURING T/O N1 GOT NR 1 THRUST REVERSER PRESSURIZED ON LEFT ECAM REJECT AT LOW SPEED. PERFORMED FUNCTION CHECK CND.SDR 0200826745Warning System · activatedDURING TAKEOFF ROLL, THE NR 4 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AT 100 KNOTS. MAINTENANCE INSPECTED THE THRUST REVERSER. OPERATIONAL CHECK SATISFACTORY.SDR AUS20020187Segment · missing(AUS) ENGINE THRUST REVERSER NR 12 CASCADE SEGMENT MISSING. FORWARD ANDAFT FLANGES CRACKED.SDR UPS02537808Actuator · leakingINSPECTION TYPE:N/A UPON LANDING AT OMA CABIN SMOKE WHEN REVERSE INITIATED (NOTE: ONLY RT PACK ON DURING LANDING). INSPECTED A/C FOR LEAKS. FOUND UPPER I/B TR ACT LEAKING REPLACED RT UPPER I/B ACTUATOR. RAN PACK, OPS CHECKS NORMAL.SDR 02FDEA00187Pilot Valve · faultyON CLIMB AFTER GEAR RETRACTION NR 1 ENG REVERSE UNLOCK LIGHT CAME ON. REMOVED AND REPLACED NR 1 ENG DIRECTIONAL PILOT VALVE AND PDU POS SWITCH MODULE PER MM 78-31-06-02-B, 78-32-09-04-B.SDR AALA20020258Switch · failedJFK - FLT 133 - EN ROUTE JFK-LAX - JUST AFTER TAKEOFF, LEFT ENGNE REVERSER UNLOCK LIGHT ILLUMINATED. NO ADVERSE YAW NOTED. RETURNED JFK AND LANDED WITHOUT INCIDENT. REPLACED MICRO SWITCH PACK TO LEFT ENGINE REVERSER PER MM. ALL OPERATIONAL CHECKS NORMAL. SDR COMA0260160Power Unit · malfunctionedFLIGHT 5786 R/H ENGINE REVERSE UNLOCKED DURING FLIGHT.REPLACED THE R/H ENGINE PDUSDR 2002FA0000439Thrust Reverser · misinstalledDOOR POSITION INDICATOR WIRING HARNESS WAS CUT AT RECEPTACLE. DOOR POSITION INDICATOR RECEPTACLE INSTALLED UPSIDE DOWN, CAUSING DAMAGE TO MALE PINS IN RECEPTACLE. DOOR POSITION INDICATOR WIRING HARNESS RETAINING CLAMP RIVET REPLACED WITH SCREW AND NUT. DISCSDR 2002FA0000604Housing · crackedHAIR LINE CRACK ON SEAM OF BODY ON PORT NR 1 NEAR MOUNTING LUG. OCCURED DURING NORMAL OPERATION.SDR P2EA2002M009Thrust Reverser · crackedON WALK-AROUND FOUND THE NR 2 ENGINE THRUST REVERSER WITH CRACK ON THE RIGHT HAND SIDE. REPLACED THE NR 2 ENGINE THRUST REVERSER IAW MM 78-32-10, LEAK CHECK AND OPS CHECK NORMAL.SDR 0200471235Thrust Reverser · malfunctionedDURING CLIMB, THE NR 1 THRUST REVERSER INTRANSIT LIGHT ILLUMINATED FOLLOWED BY A SEVERE AIRCRAFT YAW. THE CREW FOLLOWED COM PROCEDURE AND SHUT DOWN THE NR 1 ENGINE. FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO IAD LANDING WITHOUT INCIDENT. MAINTENANCE PLACESDR CA020222001Access Panel · missing(CAN) WHEN AIRCRAFT LANDED CREW SELECTED REVERSERS, THE NR 2 ENGINE, RT THRUST REVERSER WOULD NOT STOW. DURING THE WALK AROUND, THE CREW FOUND THE NR 2 ENGINE THRUST REVERSER DUCT ACCESS PANEL (P/N LJ76673) RIPPED OFF AND DAMAGE TO THE THE RT TRANSLATING SDR 02FDEA00098Pdu · faultyUPON TAKEOFF PWR THE GREEN REVERSER LIGHT FLICKERED THEN ILLUMINATED STEADY, IT W/N EXTINGUISHED UNTIL PWR REDUCED TO IDLE. SYS TO BAD DRIVE UNIT. REMOVED AND REPLACED PDU PER DC10-10 MM 78-31-01-2, OPS CHECK GOOD.SDR 2002F00393Clutch · malfunctionedDURING CRUISE, LEFT AND RIGHT THRUST LEVERS DIFFICULT TO MOVE. MAINTENANCE REMOVED AND REPLACED THE AUTOTHROTTLE CLUTCH PACK. REMOVED AND REPLACED LEFT ENGINE OUTBOARD FEEDBACK ACTUATOR IAW MM 78-34-06. (M)SDR MEX2002027Actuator · failedFLT 402 - MEX-NYC - DURING TRANSIT CHECKED ENGINE NR 1 AND THE REVERSER WAS FOUND DEACTIVATED. THE WIRE BUNDLE OF THE REVERSER CONTROL VALVE WAS CHAFED AGAINST THE WIRE BUNDLE OF THE FIRE DETECTOR. WIRE BUNDLES WERE ISOLATED, REVERSERS WORKED OK AND NO SCREESDR F3LA200200025Attach Fitting · crackedDURING C-3 CHECK, INSPECTION REPORTED NR 1 ENGINE BOTTOM OUTBOARD THRUST REVERSER ATTACH POINT DAMAGED AND CRACKED IN 2 PLACES. REPAIRED CRACKS AND DAMAGED AREA PER SRM 51-30-6.
Back to JASC 7830