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 RRXA98131Spacer · corrdedDURING MAINTENANCE VISIT, FOUND NR 1 PYLON, T/R SPACER (P/N 305-519-803), WORN AND CORRODED AROUND SHAFT AT ATTACH PONITS. FABRICATED AND INSTALLED NEW T/R SPACER, IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04727.SDR ABXA9800446Drive Link · crackedDURING COMPLIANCE WITH AD 96-10-11 AND AD 75-14-06, FOUND NR 2 ENGINE THRUST REVERSER, UPPER, LEFT, DRIVE LINK CRACKED. REPLACED DRIVE LINK IAW DC9 MM 78-31-5.SDR 9808911150Tr Rigging · out of adjustUPON APPLICATION OF TAKEOFF POWER, THE NR 3 ENGINE REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE ADJUSTED THE REVERSER VENT VALVE RIGGING AND FOUND ALL INDICATIONS NORMAL. AIRCRAFT DEPARTED WITSDR 98ZZZX1900Switch · damagedGULFSTREAM ISSUED CUSTOMER BULLETIN 92 WHICH ADJUSTED THE THRUST REVERSER UNLOCK SWITCHES. NO DEFECTS WERE NOTED ON S/N 1034. LATER, GAC RE-ISSUED CB 92 AMI WHICH CANCELLED CB 92. NEXT, CB 92A WAS ISSUED WHICH DID NOT FUNCTION ON S/N 1034. IT DESTROYED THSDR 98ZZZX1892Actuator · failedTHE FAILURE OCCURRED DURING A FLIGHT CREW TRAINING FLIGHT CONSISTING OF 3 FULL STOP LANDINGS, AND TAKEOFFS. ON THE 3RD LANDING, THE AIRCRAFT WAS CLEAR OF THE RUNWAY AND WAS TAXIING TO THE DEPARTURE END OF THE RUNWAY. IDLE REVERSE THRUST WAS BEING USED, AS NESDR AALA980878Line · looseDEN - FLT 1320 - IMMEDIATELY AFTER TAKEOFF DEN SMOKE AND FUMES ENTERED THE CABIN, AIR INTERRUPTED BACK TO DEN AND LANDED WITHOUT INCIDENT. TIGHTENED NR 2 ENGINE THRUST REVERSER BYPASS VALVE B-NUT. CLEANED OUT RESIDUAL HYDRAULIC FLUID IN APU. CHANGED COALESCSDR 98ZZZX1872Latch Actuator · crackedINSPECTION FOUND LT THRUST REV INBD LATCH ACTUATOR CRACKED.SDR P5CA9800856Support · crackedCRACKED CASCADE SUPPORT RING UPPER END. BLENDED OUT CRACK PER BOEING SRM 51-10-01 AND REPROTECTED PER 51-10-02.SDR P5CA9800928Housing · brokenBROKEN NR 1 ENGINE DIAPHRAGM SEGMENT AT 9 O'CLOCK POSITION. REPLACED HOUSING ASSY PER M/M 78-31-15.SDR DLL19980844Tr Light · illuminatedREVERSER PRESSURE LIGHT ON IN FLT POM. FOUND REVERSER STOWED AND REPLACED PRSOV WITH NO HELP. SUSPECT WIRING.SDR CKSA98263Tr Actuator · failedDURING DESCENT, NR 2 ENGINE FIRE WARNING CAME ON. PROCEDURES FOLLOWED IAW AIA FOM. ENGINE SHUTDOWN AND NR 2 BOTTLE FIRED. NR 2 BOTTLE PRESS LOW LIGHT DID NOT COME ON NR 1 BOTTLE FIRED AND PRESS LOW LIGHT CAME ON. FOUND T/R ACTUATOR LEAKING BADLY WHICH CAUSSDR 9806911148Tr Unit · malfunctionedDURING TAKEOFF ROLL, THE NR 2 ENGINE REVERSER UNLOCKED LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PLACED THE REVERSER ON MEL 78-1A.SDR SCNA98035Tr Valve · failedNUMBER THREE THRUST REVERSER OPERATION LIGHT ILLUMINATED AT APPROXIMATELY 1.95 EPR ON TAKEOFF ROLL. TAKEOFF ABORTED AT 60 KNOTS. REMOVED AND REPLACED THRUST REVERSER DIRECTIONAL VALVE PER MAINTENANCE MANUAL CHAPTER 783015, OPERATIONAL CHECK GOOD.SDR ABXA9800343Hose · leakingLOSS OF HYDRAULIC FLUID DOWN TO STANDPIPE LEVEL. AILERON CONTROL MANUAL LIGHT ILLUMINATED, HYDRAULIC PRESSURE VERY LOW AND NR 2 THRUST REVERSER LIGHT WAS FLASHING. REPLACED LEAKING HYDRAULIC HOSE TO THE THRUST REVERSER PUMP. RESERVICED HYDRAULIC SYSTEM, OPSDR 9806411148Tr Unit · malfunctionedWHEN ENGINE POWER WAS ADVANCED TO THE TAKEOFF SETTING, THE NR 2 ENGINE THRUST REVERESER UNLOCK INDICATION ILLUMINATED. THE TAKEOFF WAS ABORTED AT APPROXIMATELY 30 KTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PLACED THE REVERSER ON MEL 78-1A.SDR SCNA98034Tr Light · illuminatedON TAKEOFF ROLL, NUMBER THREE REVERSER LIGHT ILLUMINATED, ABORTED TAKEOFF. MEGGED WIRES BACK TO THRUST REVERSER SWITCH AND FUNCTIONALLY TESTED GOOD. SYSTEM OPERATIONAL CHECKS NORMAL.SDR SCNA98033Tr Light · illuminatedON TAKEOFF ROLL, NUMBER THREE REVERSER LIGHT ILLUMINATED. ABORTED TAKEOFF. MEGGED WIRES BACK TO THRUST REVERSER SWITCH AND FUNCTIONALLY TESTED GOOD. SYSTEM OPERATIONAL CHECKS NORMAL.SDR SCNA98030Switch · inoperativeAT TAKEOFF, ENGINE NUMBER THREE REVERSE OPERATING LIGHT ILLUMINATED. TAKEOFF ABORTED AT 60 KNOTS. REMOVED AND REPLACED NUMBER THREE ENGINE THRUST REVERSER UNLOCK SWITCH, FUNCTIONALLY CHECK GOOD.SDR 98ZZZX1850Link · crackedTHREE LINKS FOUND CRACKED USING DOUGLAS NDT 8-1 INSPECTION. THESE LINKS ARE NEW. LINKS ARE AFFECTED BY AD 96-10-11, DOUGLAS SB 78-66. THIS HAS BEEN REPORTED TO DOUGLAS ON 5-5-98.SDR 98UAL900133Eau Fork · fracturedBOTH THRUST REVERSER UNLOCK LIGHTS ILLUMINATED AFTER TAKEOFF. *S/D* FOUND ENGINE ACCESS UNIT RETAINING FORK ON RADIO RACK FRACTURED AND MISSING PIN. EAU WAS LOOSE IN RACK. REPLACED FORK AND PERFORMED EAU OPS CHECK, OPS CHECK GOOD.SDR ORJA9864Tr Fault Light · activatedRETURN TO GATE LEFT ENGINE SYSTEM FAIL AND LEFT REVERSER FAULT. INSPECTION OF NR 1 ENGINE INLET AND EXHAUST, NO DISCREPANCIES NOTED TEMP MOMENTARY RISE ACCEPTABLE PER TRANSIENT GRAPH MM CH 71-01-02 REV FAULT GONE. (M)SDR 98UAL900124Reverser Light · illuminatedON TAKEOFF AT 138 KTS, AMBER NR 2 REVERSER CAME ON. ABORTED TAKEOFF.SDR CA980318043Ballscrew · broken(CAN) THE RIGHT THRUST REVERSER 4 O''CLOCK BALL SCREW ACTUATOR ANTI-ROTATION TANG FOUND BROKEN.SDR 98FDEA00198Tr Unit · malfunctionWHEN ACTIVATING AUTO THROTTLES FOR T/O, LEFT ECAM ANNUNCIATED ENG 1 REV PRESSURIZER AND MASTER CAUTION LIGHT REJECTED TAKEOFF.LOCKED OUT NR 1 T/R PER MEL 78-1 AND MX PROCEDURES 78-1 COMPLIED WITH. IN ADDITION, DISCONNECTED & PLUGGED BOTH DU SUPPLY LINES PER MSDR ABXA9800195Tr Link · crackedDURING C-CHECK, FOUND THE LOWER RIGHT THRUST REVERSER LINK CRACKED. REPLACED LINK IAW DC9 MM 78-31-5.SDR ABXA9800194Tr Link · crackedDURING C-CHECK, FOUND THE UPPER RIGHT THRUST REVERSER LINK CRACKED. REPLACED LINK IAW DC9 MM 78-31-5.SDR CA980325044Stop · damaged(CAN) DAMAGED BLOCKER DOOR FOUND ON RAMP INSPECTION, REPLACED.SDR ASAA9840051Door · damagedSEA - DURING C-CHECK, THE NR 2 ENGINE INBOARD T/R MID ACTUATOR ACCESS DOOR CUTOUT WAS FOUND TO BE DAMAGED. REPAIRED PER EA 7110-01064 AND BOEING TELEX ASA-SEA-98-0061RR. (M)SDR ABXA9800135Link · crackedDURING COMPLIANCE WITH AD 96-10-11, FOUND NR 2 ENGINE UPPER LEFT THRUST REVERSER DRIVER LINK CRACKED. REPLACED THRUST REVERSER DRIVER LINK IAW DC9 MM 78-31-5.SDR ABXA9800134Link · crackedDURING COMPLIANCE WITH AD 96-10-11, FOUND NR 2 ENGINE LOWER RIGHT THRUST REVERSER DRIVER LINK CRACKED. REPLACED THRUST REVERSER DRIVER LINK IAW DC9 MM 78-31-5.SDR AU980457Gearbox · jammed(AUS) AFTER LANDING, THE NR 2 ENGINE THRUST REVERSER FAILED TO STOW. GROUND INVESTIGATION FOUND THE THRUST REVERSER'S NR 3 GEARBOX JAMMED AND DAMAGED.SDR 9803171157Tr Unit · malfunctionedDURING LANDING ROLLOUT, THE NR 3 ENGINE THRUST REVERSER DID NOT STOW AND THE ENGINE COMPRESSOR STALLED. THE EGT REACHED 1000C AND THE ENGNE WAS SHUT DOWN. MAINTENANCE INSPECTED THE ENGINE AND DEFERRED THE REVERSER PER MEL 78-1A. THE REVERSER WAS STOWED AND SDR CALA9800263Tr Panel · delaminatedINSPECTION FOUND A 10 INCH AREA OF DELAMINATION AT NR 2 ENGINE LEFT THRUST REVERSER LOWER SIDEWALL PANEL (FAN AIR BYPASS AREA). THE C-DUCT ASSEMBLY WAS REPLACED IAW MM 78-32-11.SDR 9802281160Tr Unit · malfunctionedDURING LANDING ROLL AND WHILE COMING OUT OF REVERSE THRUST, THE NR 2 ENGINE THRUST REVERSER REMAINED DEPLOYED. THE CREW ATTEMPTED TO RECYCLE THE REVERSER AND A COMPRESSOR STALL OCCURRED. THE ENGINE WAS SHUT DOWN WITH A MAXIMUM EGT OF 800C. MAINTENANCE INSPESDR ASAA9840023Tr Unit · gougedSEA - DURING C-CHECK, THE NR 2 ENGINE INBOARD T/R BULLNOSE SECTION WAS FOUND GOUGED AT THE 10 AND 11 O'CLOCK POSITIONS. REPAIRED PER EA 5430-01027 AND BOEING TELEX ASA-SEA-98-0028RR. (M)SDR ASAA9840022Tr Unit · gougedSEA - DURING C-CHECK, THE NR 1 ENGINE INBOARD T/R BLOCKER DOORS WERE FOUND RIDING THE BULLNOSE IN SEVERAL PLACES. REPAIRED PER EA 5430-01027 AND BOEING TELEX ASA-SEA-98-0028RR. (M)SDR 9801791156Actuator · out of adjustON TAKEOFF ROLL AT APPROXIMATELY 60 KNOTS, THE NR 3 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE THRUST REVERSER AND ADJUSTED A LOCK ACTUATOR. THE OPERATIONAL CHECKSDR P5CA9800045Sleeve · damagedNR 1 ENGINE FAN REVERSER SLEEVE DAMAGED AT THE 5 O'CLOCK POSITION. REPAIRED AS PER SRM 54-30-03.SDR SWAA980083Isolation Valve · failedRETURNED TO DAL DUE TO THRUST REVERSER ISOLATION VALVE LIGHT ILLUMINATING. MADE AN UNEVENTFUL LANDING. REPLACED ISOLATION VALVE PER BOEING M/M.SDR CALA9800720Stiffener · gougedINSPECTION FOUND THE NR 1 ENGINE THRUST REVERSER PANEL NR 7519DS GOUGED ON FORWARD UPPER CORNER. THE STIFFENER WAS REMOVED AND THE GOUGE WAS BLENDED OUT IAW SRM 53-01. A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW DOUGLAS DRAWING NR 5958762, SRM 51-10-3, SDR W8PA980013Tr Light · illuminatedNR 1 ENGINE THRUST REVERSER LIGHT ON AFT OVERHEAD PANEL ILLUMINATED IN FLIGHT. RETURNED TO MDW. DEFERED PER MEL 78-1 CAT C.SDR 98ZZZX239Rod End · separatedAIRCRAFT CAME IN WITH REPORT STATING LEFT T/R FAILS TO STOW AFTER DEPLOY CYCLE. REMOVED ACCESS PANELS TO TROUBLESHOOT. FOUND LOWER REVERSER DOOR LINK SEPARATED FROM ROD END. AFTER A VISUAL INSPECTION OF LINK AND ROD END, ROD END ENGAGEMENT INTO LINK WAS APPSDR UPS97825348Tr Unit · inopINSPECTION TYPE-N/A, ON LANDING THRUST REVERSERS WOULD NOT DEPLOY. THRUST REVERSER HYDRAULIC VALVE C/B POPPED. REMOVED AND REPLACED T/R HYD S/O VALVE ASSY PER DC8 MM 78-37-03, SYS OPS CKS NORMALLY. INSPECTED TIRES AND BRAKES AND FOUND ALL TO BE OK FOR CONTISDR 98ZZZX11Cowl · damagedINSPECTION FOUND NR 2 ENGINE T/R COWL RT DAMAGED. ALSO FOUND TRANSLATING COWL RT LOWER SIDE DAMAGE ABOUT 10 CM BY 8 CM WHEN TRANSIT IN ANC. REPLACED RT HALF OF BOTH FAN COWL AND TRANSLATING COWL.SDR ABXA9701904Tr Link · crackedDURING COMPLIANCE WITH AD 96-10-11 AND 75-14-06, FOUND FORWARD, UPPER RIGHT THRUST REVERSER LINK CRACKED. REPLACED THRUST REVERSER DRIVE LINK IAW DC9 MM 78-31-5.SDR 9722511146Tr Unit · malfunctionedON TAKEOFF ROLL AS POWER WAS APPLIED, THE NR 1 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AT APPROXIMATELY 30 KTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PLACED THE REVERSER ON MEL 78-1A.SDR WRLA97144Switch · out of adjustDURING INITIAL TAKEOFF ROLL (MAX SPEED 60 KNOTS) FLIGHT CREW OBSERVED NR 1 ENGINE THRUST REVERSER UNLOCK LIGHT. FLIGHT CREW ELECTED TO DISCONTINUE TAKEOFF. AIRCRAFT RETURNED TO GATE. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL ADJUSTED SDR 9722521144Tr Unit · malfunctionedDURING TAKEOFF ROLL, THE NR 3 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AT 70 KTS WITH THE INDICATION EXTINGUISHING WITH POWER REDUCTION. MAINTENANCE PLACED THE REVERSER ON MEL 78-1A AND THE AIRCRAFT RETURNED TO SERVICE.SDR CA971208011Link · cracked(CAN) ON ROUTINE "C" CHECK, NR1 ENGINE THRUST REVERSER UPPER INBOARD DRIVE LINK FOUND CRACKED. NEW MODIFIED LINK INSTALLED.SDR 9722201146Thrust Reverser · malfunctionedDURING LANDING ROLLOUT, THE NR 1 ENGINE THRUST REVERSER FAILED TO STOW. THE CREW RECYCLED THE REVERSER AND A COMPRESSOR STALL OCCURRED. MAX EGT WAS 650C. THE ENGINE WAS SHUT DOWN. THE OUTBOARD REVERSER SLEEVE DEPARTED THE AIRCRAFT. MAINTENANCE LOCKED OUT
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