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 SWAA960200Tr Sleeve · came looseON DESCENT AT 24,000 FL, NUMBER 1 ENGINE O/B THRUST REVERSER SLEEVE PARTIALLY SEPARATED FROM AIRCRAFT. AIRCRAFT MADE AN UNEVENTFUL LANDING AT AUS. REINSTALLED NEW SLEEVE PER BOEING M/M.SDR P5CA9600205Tr Drive Unit · inopNR 2 REVERSER DRIVE MOTOR FAILED AD 95-16-02 INSPECTION. PLACARDED AS INOP, REMOVED AND REPLACED NR 2 DRIVE UNIT AT LAX IAW MM 78-31-02.SDR CA960415013Air Motor · seized(CAN)DURING LANDING AFTER THRUST REVERSER OPERATION, #1 THRUST REVERSER JAMMED IN THE DEPLOY POSITION. UPPER RH COWL TRANSLATING ROD BENT AND CRACKED. #1 SCREW JACK BENT. BOTH DRIVE CABLES SHEARED AT AIR MOTOR AND MOTOR SEIZED. PARTS REPLACED.SDR ASAA9680080Tr Return Line · leakingLAS - FLT NR 624 - CREW REPORTED AN ELECTRICAL OR HOT PLASTIC ODOR IN THE CABIN DURING DESCENT AND LANDING. INSPECTION OF ALL LAVATORY WASTE CONTAINERS, OVENS, BUN WARMERS AND COFFEE MAKERS REVEALED NO PLASTIC RESIDUE OR OVERHEAT CONDITION, ODOR HAS DISSIPATESDR P5CA9600161Tr Unit · malfunctionedNR 3 ENGINE OVERTEMPED IN REVERSE, EGT REACHED 920 DEGREES. VISUALLY INSPECTED ENGINE INTAKE AND TAILPIPE, NO DAMAGE FOUND. REVERSER DEACTIVATED, PENDING RABS SYSTEM CHECK AT JFK.SDR 96ZZZX1369Screw Shaft · corrodedBALLSCREW ACTUATORS SCREW SHAFTS WERE FOUND CORRODED. NO CORROSION ALLOWED IAW COMPONENT MAINTENANCE. MANUAL CHAPTER 78-30-29, PAGE 505, PARAGRAPH 5B, ITEM NR 5. (BRAZIL)SDR CA960321515Motor · inoperative(CAN) #3 ENGINE THRUST REVERSER INOPERATIVE ON LANDING. REPLACED #3 THRUST REVERSER MOTOR. OPERATIONAL CHECK CARRIED OUT, OK.SDR CA960311011Torque Box · cracked(CAN)FORWARD FRAME INBOARD FLANGE OF TORQUE BOX FOUND CRACKED AT RADIUS AND A PIECE IS MISSING. CAUSE UNKNOWN.SDR 9605973213Tr Unit · malfunctionedDURING LANDING, THE NR 1 ENGINE FLAMED OUT AFTER COMING OUT OF SECOND THRUST REVERSER ENGAGEMENT AND ENGINE RESTARTED DURING TAXI INTO GATE. GROUND MAINTENANCE INSPECTED, RAN AND OPERATED NR 1 ENGINE THRUST REVERSER SEVERAL TIMES, NO PROBLEMS FOUND.SDR 96ZZZX1954Bucket · corrodedDURING A C-CHECK/4,800 HOUR-INSPECTION, FOUND LEFT ENGINE'S LOWER T/R BUCKET, OUTER SKIN HAD CORRSION HOLES FROM INSIDE OUT IN TWO SEPARATE LOCATIONS.SDR 9603601150Tr Unlock Light · illuminatedDURING TAKEOFF, THE NR 1 REVERSER UNLOCK LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE NR 1 REVERSER AND FOUND NORMAL. PLACARD NR 1 REVERSER INDICATION PER MEL 78-2A.SDR CA960304009Pneumatic Drive · failure(CAN) FAILURE OF INTERNAL LOCK MECHANISM OF THE FLEX SHAFT LOCK ON PNEUMATIC DRIVE UNIT. FAILURE OCCURRED DURING THRUST REVERSER STOW CYCLE. THRUST REVERSER ANNUNCIATOR REMAINED ON. FURTHER INVESTIGATION REVEALED THE PDU FLEX SHAFT LOCK FAULTY WITHIN THE UNIT.SDR 96UAL900094Blocker Door · failedUPON DEPLOYING REVERSERS AT LAX ON 1/9/96, LOST NR 2 RT REV. TRANSLATING COWL. FOUND BROKEN IN SEVERAL PIECES. UPPER BLOCKER DOOR FAILED CAUSING DOOR TO JAM BETWEEN COWL AND CORE STRUCTURE. THIS CAUSED ACTUATOR ATTACH FITTINGS TO SHEAR, LIBERATING THE COWL.SDR CA960214019Flexshaft Lock · not engaging(CAN)FLEXSHAFT LOCK NOT ENGAGING CAM. FOUND UNSECURED AND FAILED ON SHAFT.SDR 96ZZZX964Reverser · malfunctionUPON LANDING, THRUST REVERSER FAILED TO STOW ALL THE WAY, PILOT TRIED TO CYCLE T/R SEVERAL TIMES WITH NO SUCCESS, CAUSING MORE DAMAGE. APPEARS BLOCKER DOORS DID NOT GET CLOSED ALL THE WAY BEFORE STOWING AND CAUGHT ON LIP OF THE T/R STRUCTURE.SDR 96ZZZX1232Actuator · failedJFK - FLT 12 - DURING TAKEOFF ROLL, NR 3 ENGINE THROTTLE WOULD NOT ADVANCE. REMOVED AND REPLACED THRUST REVERSER SEQUENCE ACTUATOR, MFG PN R1409M13-1. OPERATIONAL CHECK NORMAL. CHECK C-2 - 10-23-95 - JFK.SDR P2RA960003Thrust Reverser · delaminatedDAMAGE ON CORE SECTION OF NR 1 ENGINE LEFT THRUST REVERSER. REMOVED AND REPLACED NR 1 ENGINE LEFT THRUST REVERSER PER A300MM, OPERATIONAL CHECK OK. (M)SDR P5CA9600169Cascade Vane · crackedFOUND NR 3 ENGINE LEFT HAND UPPERMOST CASCADE VANE CRACKED. BLENDING CARRIED OUT AND VANE REINSTALLED AS PER MM 78-32-04.SDR 96FDEA00059Tr Switch · failedAFTER ROTATION NR 3 REVERSER OPERATING LIGHT ILLUMINATED, PERFORMED APPROPRIATE CHECKLIST AND SHUTDOWN NR 3 ENG. REPLACED NR 3 ENG REVERSER SWITCH PER MM 78-30-00. OPS CHECKED NORMAL, PANELS SECURED.SDR USAASB96008Control Valve · failedTPA - FLT 202 - NR 2 ENGINE REVERSER LIGHT ON OVERHEAD PANEL ILLUMINATED DURING FLIGHT, THROTTLE OPERATED NORMALLY AND REVERSER OPERATED NORMALLY ON GROUND. MAINTENANCE REPLACED THRUST REVERSER CONTROL VALVE. NO LEAKS NOTED. OK FOR SERVICE. (X)SDR 9600175529Tr Unit · malfunctionedDURING CLIMB, REVERSER ISOLATION VALVE STATUS MESSAGE AND REVERSER ISOLATION WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DEPARTURE AIRPORT, NO FUEL WAS DUMPED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE DEACTIVATED AND STOWED THRUST REVERSER. THRUSSDR 9600326304Tr Sensor · out of adjustDTW - AFTER TAKEOFF, THE NR 2 ENGINE REVERSER AMBER LIGHT ILLUMINATED. NO STATUS, NO EICAS AND NO PRESENT LEG FAULT MESSAGES DISPLAYED. CREW FOLLOWED COCKPIT OPERATING MANUAL, DUMPED 135,000 LBS OF FUEL AND DIVERTED FLIGHT TO MSP. MAINTENANCE VISUALLY INSPESDR DL757960199Thrust Reverser · damaged757 NR 2 ENGINE HIGH PRESSURE AIR LINE NOT CONNECTED AT FIREWALL, BLEW HOLE IN THRUST REVERSER INNER CORE (315N3101 ASSY) AT NAC STA 110, APPOX 3 INCH BY 8 INCH AT 1 O'CLOCK POSITION. REQUIRES REPAIR AT NORDAM PER LIASON ENGINEERING. ERA PENDING, SENT TO OUTSDR CA960116003Valve · seized(CAN)AFTER TOUCHDOWN WHEN REVERSE THRUST WAS SELECTED THE #1 THROTTLE STUCK ON THE IDLE GATE AND THE REVERSER WOULD NOT ENGAGE. MAINTENANCE FOUND THE THRUST CONTROL SYSTEM DIRECTIONAL VALVE VERY STIFF. AFTER VALVE REPLACEMENT THE SYSTEM FUNCTIONED NORMALLY.SDR P5CA9600106Vane · crackedNR 3 ENGINE CASCADE VANE ASSY 2ND FROM TOP, LT SIDE FOUND CRACKED. REPAIRED AND REINSTALLED AS PER MM 78-31-07.SDR P5CA9600105Vane · crackedFOUND NR 2 ENGINE CASCADE VANE CRACKED AT 8 O'CLOCK POSITION BELOW JACKSCREW. REPAIRED IAW OHM 78-31-51.SDR CA960116011Actuator · failed(CAN)#2 ENGINE THRUST REVERSER LIGHT ILLUMINATED DURING TAKEOFF ROLL. ABLE TO SELECT THRUST REVERSER REGARDLESS OF THRUST LEVER POSITION. REJECTED TAKEOFF BELOW 80 KNOTS. REVERSER LOCKED IN FORWARD THRUST AND DEACTIVATED AS PER MM 78-30-00. LOCKED THRUST REVESDR AALA960285Tr Drive · defectiveHNL - FLT NR 14 - DURING CLIMB-OUT, FLT CREW NOTED IMPAIRED CLIMB PERFORMANCE AND SOME AILERON AND RUDDER TRIM REQUIRED TO MAINTAIN WINGS LEVEL. A/C RETURNED TO HNL AND LANDED W/O INCIDENT. AFTER ARRIVAL, NR 2 ENG RT TRANSLATOR COWL NOTED PARTIALLY DEPLOYED.SDR ASAA9580289Hyd Line · brokenPDX - AIR TURN BACK OF FLIGHT 524, CREW REPORTED, THE LEFT ENGINE THRUST REVERSER ACCUMULATOR LOW PRESSURE WARNING LIGHT ILLUMINATED AND LEFT HYDRAULIC QUANTITY DECREASED, SHUT OFF LEFT ENGINE DRIVEN HYDRAULIC PUMP AND HYDRAULIC QUANTITY STABILIZED. LANDED WISDR 96ZZZX24Thrust Reverser · deployedLEFT THRUST REVERSER DEPLOYED ON TAKEOFF. DEACTIVATED BOTH T/R SYSTEMS AND FERRIED TO OMA. COMPLETED COMPLETE RIGGING AND OPERATIONAL TEST OF T/R SYSTEM. NO SYSTEM MALFUNCTIONS WERE NOTED. REPLACED BOTH T/R STOW SWITCHES AT THE RECOMMENDATION OF RAYTHEON ASDR ABXA9600047Skin · crackedDURING 826AX MOD-DISCOVERED NR 3 ENGINE THRUST REVERSER INBOARD SKIN CRACKED AT YN 232. REPAIRED NR 3 THRUST REVERSER INNER SKIN AND FRAME THAT WAS CRACKED AT YN 232 IAW ABX REA D878-12841MR.SDR 96ZZZX757Thrust Reverser · crackedWHILE PERFORMING A BLOCKER DOOR REPAIR, NOTICED THE INNER BARREL AT THE 6 O'CLOCK POSITION HAD A 6-INCH LONG CRACK IN THE SHAPE OF THE LETTER 'L'. CONSIDERING THE PRELOADING PROBLEM ON THE BLOCKER DOOR AND APPARENT MISALIGNMENT OF THE BLOCKER DOOR MOUNTS AT PSDR CA951122026Switch · broken wire(CAN)WHILE CONDUCTING GROUND TEST, L/H THRUST REVERSER DID NOT DEPLOY. TECHNICIAN FOUND WIRE #K106C20 BROKEN AT THE MICROSWITCH P/N V3 15.SDR 9518271149Tr Unit · malfunctionedTHE NR 3 ENGINE REVERSER LIGHT ILLUMINATED AT 80 KNOTS AND THE TAKEOFF WAS ABORTED. THE REVERSER WAS LOCKED OUT AND PLACED ON MEL.SDR CA951122028Switch · intermittent(CAN)#2 ENGINE REVERSER LIGHT ILLUMINATED ON TAKEOFF ROLL. REJECTED. REVERSER LOCKED IN FORWARD AND LOCKED POSITION AND DEFERRED TO MEL 78.02. REVERSER POSITION SWITCH REPLACED.SDR 9517786622Tr Light · illuminatedDURING CLIMB, THE NR 1 ENGINE REVERSER UNLOCK LIGHT ILLUMINATED. ACFT DUMPED 90,000 LBS OF FUEL AND FLIGHT DIVERTED TO MSP WHERE THE REVERSER WAS LOCKED OUT AND PLACED ON MEL.SDR CA951120008Switch · broken wiring(CAN)AFTER LANDING,THRUST REV LIGHTS SHOWED NORMAL DEPLOYMENT,BUT AFTER SELECTING STOW,THEY REMAINED DEPLOYED & THE UNLOCK LIGHTS REMAINED ON.SELECTING THE EMERGENCY STOW SWITCH STOWED THE THRUST REV. TROUBLESHOOTING, FOUND THAT SWITCHES S153 & S161, IN THE PSDR W8PA9502Actuator · bypassingCOS - RIGHT ENGINE THRUST REVERSER OVERHEAD LIGHT ILLUMINATED JUST AFTER TAKEOFF. AIRCRAFT RETURNED TO COS. FOUND NR 2 THRUST REVERSER OUTBOARD CENTER ACTUATOR BYPASSING. REPLACED ACTUATOR. ALSO, ADJUSTED THRUST REVERSER TARGETS ON SWITCHES S-831 AND S-832SDR WRLA95044Tr · failedDURING INITIAL TAKEOFF ROLL, FLIGHT CREW NOTED NR 1 ENGINE NOT REACHING TARGETED EPR. TAKEOFF TERMINATED. ACFT RETURNED TO GATE. DURING MAINTENANCE T/S, MAINTENANCE CONFIRMED NR 1 ENGINE WOULD NOT ACCELERATE PAST GROUND IDLE POWER. CFDS FAULT REVIEW INDICASDR 9516909853Tr Unlock Sw · failedNR 1 THRUST REVERSER UNLOCK WARNING ILLUMINATED SHORTLY AFTER TAKEOFF. STAYED ON APPROXIMATELY 15 MINUTES THEN EXTINGUISHED. THE FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE REVERSER UNLOCK SWITCH. SUBSEQUENT FUNCTIONAL TESTSDR 95FDEA01581Clamp · failedDURING T/O ROLL, THE FIRE DETECTION LIGHT AND FIRE WARNING LIGHT ILLUMINATED ON NR 1 ENG. THE NR 1 ENG NACELLE OVERHEAT TEMP REACHED 9, THEN QUICKLY DROPPED TO ZERO. ABORTED T/O AT 60 KNOTS AND RETURNED TO RAMP. FOUND REVERSER DUCT CLAMP BLOWN. REMOVED ANDSDR P5CA9500825Tr Rail · crackedNR 2 ENGINE R-RAIL CRACKED AT THE FOUR-THIRTY POSITION. WELDED CRACK IAW P AND W MM 72-53-01.SDR P5CA9500824Tr Rail · crackedNR 3 ENGINE R-RAIL CRACKED IN TWO PLACES, APPROXIMATELY 5 O'CLOCK POSITION. WELDED CRACK IAW P AND W MANUAL 72-53-01.SDR USAA951100Switch · out of adjustPIT - FLT NR 591 - AFTER TAKEOFF AT APPROXIMATELY 2000, NR 1 THRUST REVERSER LIGHT FLICKERED ON AND OFF. AT 3000, THE PROCEDURE LIGHT CAME ON STEADY. CREW ELECTED TO RETURN TO FIELD. NO EMERGENCY DECLARED. MEL WAS ADDED AND FLIGHT DEPARTED TO SDF WITH DELAYSDR 96ZZZX918Control Cable · misroutedDUE TO CABLE MISRIGGING, LEFT THRUST REVERSER CABLE CHAFED THROUGH THE FORWARD PULLEY MOUNTING BRACKET UNDER THE COCKPIT PEDESTAL.SDR 95ZZZX6797Tr Isolation Vlv · dirtySAL/LAX - FLT 510 - DURING CLIMB, THE ADVISORY MESSAGE R REV ISOLATION VALVE WAS SHOWN ON THE EICAS. DUE TO THIS SITUATION, THE AIRCRAFT RETURNED TO SAL. AFTER CHECKING RT ENGINE THRUST REVERSER VALVE AND CLEANING THE ISOLATION VALVE PRESSURE, AND CHECKING TSDR ABXA9500824Tr Unit · defectiveJOLT FELT IN FLIGHT AT 13,000 FEET, ENGINE INSTRUMENTS NORMAL, NO COCKPIT INDICATION OF MALFUNCTION. CARGO INSPECTED IN FLIGHT BY FIRST OFFICER. EMERGENCY DECLARED FOR LANDING. LANDING NORMAL, EXCEPT LEFT ENGINE THRUST REVERSER DID NOT GET BLUE LIGHT. INSPSDR P5CA9500814R Rail · crackedNR 4 ENGINE R-RAIL IS CRACKED AT FIVE THIRTY POSITION. REPAIRED RAIL IAW MM 72-53-01.SDR 95ZZZX5865Actuator · leakingREMOVED THRUST REVERSER ACTUATOR DUE TO LEAKING AT SHAFT. PARKER HANNIFIN CALLS OUT MINOR LEAKING AFTER SO MANY CYCLES. ACTUATOR REMOVED HAS 12.8 HOURS TSO AND IS LEAKING SMALL 'PUDDLES' UNDER COWL.SDR 95ZZZX5864Actuator · leakingREMOVED THRUST REVERSER ACTUATOR DUE TO LEAKING AT SHAFT. PARKER HANNIFIN CALLS OUT MINOR LEAKING AFTER SO MANY CYCLES. ACTUATOR REMOVED, HAS 18 HOURS TSO AND IS LEAKING SMALL 'PUDDLES' UNDER COWL.
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