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 ASMF20120321004Sleeve · puncturedDURING TRANSIT CHECK, THE RT ENGINE THRUST REVERSER WAS HIT, CAUSING A PERFORATION OF 10.0" LONG, 8.5 WIDE ON INTERIOR TRANSLATING SLEEVE THRUST REVERSER. THE RT ENGINE TRANSLATING SLEEVE WAS REPLACED IAW MM 78-31-02, ALL CORRECT.SDR UALA2012032001796Thrust Reverser · damagedNR 2 ENGINE RIGHT THRUST REVERSER HALF C-DUCT (ALF) HAS A PREVIOUS REPAIR THAT IS COMING LOOSE UP INTO THE SECONDARY GAS PATH. REPLACED NR 2 ENGINE RIGHT REVERSER OUTBOARD SLEEVE PER MM. NEW SLEEVE OFF OF A-C 6444, OPS CHECK GOOD.SDR Z6WR20120319005Ring · wornREF: CMM 78-31-37, 01MAR2012, REV 023. INSPECTION FINDING OF (2) MISSING BACB30LE6K29 BOLTS (FIGURE 12, ITEM 100) NOTES THE FOLLOWING RELATED DISCREPANCIES. A) FIGURE 12, ITEM 115 AREA OF MATERIAL WEAR MEASURING .32 X .08 X .018 DEEP ON THE 315A2222-5 CASCADSDR USAA2012031900031Proximity Sensor · faultyNR 1 ENGINE THRUST REVERSER FAULT ON LANDING ROLLOUT. ACCOMPLISHED OPERATIONAL TEST WITH NO FAULTS FOUND. ON THE NEXT DAY, 3/18/12, AIRCRAFT EXPERIENCED THE SAME FAULT - THRUST REVERSER WAS DEACTIVATED AND PLACED ON MEL. MAINTENANCE TROUBLESHOT - REMOVED ANSDR CA120319004Link · corroded(CAN) DISCOLOR ON BOLT AND BUSHING FOUND ON ROUTINE INSPECTION. FURTHER INSPECTION OUTSIDE THE SCOPE OF ORIGINAL INSPECTION REVEALED CORROSION ON PRESSED FIT BUSHING. THE CORROSION HAD GONE THROUGH THE BUSHING AND MADE A VISABLE HOLE. CORROSION WAS ALSO IDENTSDR WX0A071129Pipe · leakingFLIGHT CREW REPORTED CABIN FILLS UP WITH SMOKE WITH THE RIGHT PACK ON. SMOKE DUE TO APU OIL INJESTION. REPLACED BOTH COALESCER BAGS PER TASK CARD R0592101 AND REPLACED LEFT THRUST REVERSER ACCUMULATOR LOW PRESSURE SWITCH PIPE ASSY. OPERATED BOTH PACKS AT WASDR YENA20120314455Line · brokenFLT 755 JFK-AUA, ON TOUCH DOWN ENGINE UNLOCK REV HYD G RSVR LO LVL, LOST NOSE WHEEL STEERING. REQUIRED TOWING OFF RUNWAY. ENGINE 1 REV WOULD NOT STOW, LOST ALL GREEN HYD FLUID. FOUND NR 1 ENGINE OUTBD T/R PRESSURE LINE BROKEN. REMOVED AND REPLACED LINE IAWSDR USAA2012031600015Relay · faultyON LANDING ROLLOUT, 'ENG 1 REVERS UNLOCK' ECAM MESSAGE. MAINTENANCE REMOVED AND REPLACED RELAYS 3EG1 AND 2EG1 IAW TROUBLESHOOTING MANUAL 78-00-810-807 AND ELECTRICAL STANDARD PRACTICES MANUAL 20-46-50. OPERATIONAL CHECK OF NR 1 ENGINE T/R WAS GOOD.SDR Z6WR20120316004Skin · misrepairedA REPAIR LOCATED ON THE AFT END MOVES FORWARD APPROX 18" AND APPROX 25" FROM THE UPPER EDGE MOVING DOWNWARD ON THE 315A2502-102 INNER WALL BONDED PANEL, HAS AN AREA OF BLOCKAGE (PERF SKIN TO CORE) THAT MEASURES APPROX 15" X 15" C/T THE 315A2501-16 ACOUSTIC SDR UIEA2012031600094Sensor · out of rigNR 2 ENGINE ONLY DEVELOPS 75 PERCENT, N1 POSITION SENSOR ON LT THRUST REVERSER OUT OF RIG. ADJUSTED IAW AMM 78-34-10-404--009-300. ENGINE POWER RUN. OPS CHECKED NORMAL AND COMPLETED SUCCESSFUL.SDR USAA2012031500009Control Unit · failedNR 1 THRUST REVERSER FAILED ON LANDING ROLLOUT. MAINTENANCE REMOVED AND REPLACED NR 1 HYDRAULIC CONTROL UNIT IAW AIRBUS MAINTENANCE MANUAL 78-31-51.SDR REXA2012030600345Warning System · activatedUNSCHEDULED LANDING AND EMERGENCY DECLARED FOR RT TR UNLOCK MESSAGE AFTER TAKEOFF. PLACED ON MEL.SDR EE4Y20120306092Pad · wornNR 1 ENGINE LT AND RT THRUST REVERSER COWLS, INSIDE UPPER SECTION, PAD PLATES WITH WEAR. REPAIRED NR 1 ENGINE THRUS REVERSE LT AND RT BUMPER PAN DOW DUE TO WEAR IAW SRM 51-30-00, REPAIR 38.SDR EE4Y20120306093Pad · wornNR 2 ENGINE INBD AND OTBD COWLS CHOCKING PAD WEAR. REPAIRED NR 2 ENGINE THRUS REVERSE INBD AND OTBD BUMPER PAN DOW DUE TO WEAR, SRM 51-30-00, REPAIR 38.SDR Z6WR20120302003Panel · delaminatedCMM 78-31-37 REV 23 FIG 35 ITEM 40B. THE 315A2101-41 INNER WALL BONDED PANEL HAS AN AREA OF DISBOND (PERF SKIN TO CORE) THAT MEASURES 1.5 X 24.5". AFTER REMOVING THE DISBONDED PORTION OF THE SKIN IT WAS DISCOVERED THAT THE PERF SKIN WAS PERPARED INCORRECTLY SDR Z6WR20120301002Ring · wornTHE 315A2222-5 CASCADE RING HAS EXTENSIVE WEAR/DAMAGE CT THE AFT LWR ATTACHING BOLT LOCATION. HOLE SHOULD BE .3750 -.3754. ACTUAL IS ELONGATED TO APPROX .6210 WITH HEAVY WEAR/MISSING MATERIAL CT THE NUT SIDE. THE 315A2402-5 LATCH BEAM HAS A CORRESPONDING ELOSDR UIEA2012022300057Structure · damagedDURING MX WALKAROUND, FOUND DAMAGE TO THE NR 2 ENGINE THRUST REVERSER CORE COWL AFT EXTRUSION.SDR UALA2012022101053Thrust Reverser · damagedNR 2 ENGINE INBD THRUST REVERSER DAMAGED. DAMAGE IS LOCATED NEAR THE CORE COWL VENT PANEL UPPER-FWD CORNER AREA. DAMAGE IS APPROXIMATELY 3 INCHES BY 3 INCHES. DETERMINED BOTH INNER AND OUTER FACE SHEETS ARE DAMAGED AT EDGE OF GRILL CUTOUT.SDR UIEA2012021600052Acoustic Liner · damagedDURING MX WALKAROUND, FOUND DAMAGE TO NR 2 ENGINE THRUST REVERSER ACOUSTIC MESH AND HONEYCOMB. DAMAGE IS LOCATED AT THE 5 O'CLOCK POSITION AND HAS DIMENSIONS 3' LENGTH, .3750" WIDTH AND .2500" DEPTH. REF TO FIG 1 FOR DAMAGE DETAILS. PERFORMED A TIME LIMITEDSDR RU3A1203Thrust Reverser · malfunctionedAT FL150, GOT RIGHT T/R UNLOCK LIGHT. CREW PRESSED T/R EMERGENCY STOW AND COMPLIED WITH CHECKLISTS. DECLARED EMERGENCY AND DIVERTED TO NEAREST AIRPORT WITH ADEQUATE RUNWAY LENGTH.SDR SWIA201229638Pdu · failedRIGHT REVERSER UNLOCKED CAUTION MESSAGE SHORTLY AFTER TAKEOFF. ACCOMPLISHED EMERGENCY ENGINE SHUTDOWN. (FLT 3275) REPLACED RIGHT THRUST REVERSER PDU.SDR 2012F00052Panel · delaminatedAFTER AN NDT INSPECTION OF THE INNER SKIN BONDED PANEL IAW NDT MANUAL, REVEALED AN AREA OF DISBONDMENT APPROX 35.0 X 54.0 ON THE BAG SIDE. SEVERAL AREAS OF CORE ARE DISBONDED FROM THE PLY'S FACE. THERE ARE ALSO NUMEROUS AREAS OF CRACKING TO THE BAG SIDE FACSDR CA120214004Structure · detached(CAN) LOWER LT ENGINE TRANSLATING COWL COME LOOSE IN FLIGHT AND DEPART THE ACFT SHORTLY AFTER DEPARTURE. THE DEPARTING COWL CAUSED DAMAGE TO THE LT LOWER FUSELAGE AREA, AFT OF THE PRESSURE BULKHEAD IN THE APU BAY. DAMAGE INCLUDED DENTED/GOUGED SKIN AND DEFLESDR A6WA201240344Structure · damagedELONGATED HOLE UNDER MOLDED SEAL. REPAIRED IAW REO 601R-78-30-4091.SDR SWIA201229617Pdu · failedRIGHT THRUST REVERSER UNLOCK MESSAGE. (FLT 5343) REPLACED THE RIGHT ENGINE POWER DRIVE UNIT. P/N OFF 126758-7, S/N OFF 1659SDR UALA2012021300852Acoustic Liner · tornNR 1 ENG FOUND 5 INCH TEAR IN THE INBD SIDE OF THRUST REV AT THE 5 O'CLOCK POSITION. RPR'D TEAR IN ACOUSTICAL LINER SKIN PER SRM, REPAIR 2 DETAIL 1SDR SWIA201229620Switch · failedRIGHT THRUST REVERSER UNLOCK CAUTION MESSAGE. (FLT 5254) REPLACED RIGHT THRUST REVERSER STOW SWITCH.SDR UALA2012020800754Thrust Reverser · damagedNR 2 ENG LT REVERSER DAMAGED. THREE DAMAGED AREAS, TWO IN SLEEVE ACCOUSTICAL SKIN AND ONE ON INNER BARREL ACCOUSTICAL SKIN, MOST LIKELY DAMAGED FROM PREVIOUS BLOCKER DOOR OR FAIRING DEPARTURE. DENT IN SLEEVE 1.375" X 1.875" X .125" A-Y=11, CREASE IN SLEEVE 1SDR UALA2012021000805Actuator · faultyREF LM2901 REMOVED NR 2 THRUST REVERSER UPPER NON LOCKING ACTUATOR PER MM. NEED TO CONTINUE INSTALLATION OF NEW ACTUATOR. REPLACED ACT PER MM CHECKS GOOD.SDR CA120211001Blocker Door · damaged(CAN) AFTER LANDING, CREW OBSERVED THE NR 3 REVERSER, UNLOCK AND PRESSURE, LIGHTS REMAINED ILLUMINATED. MAINTENANCE DISCOVERED THAT THE BLOCKER DOORS AND THE BRACKETS THAT ATTACH THE JACKSCREWS TO THE SLIDING PANEL HAD BECOME DAMAGED/BROKEN POSSIBLY DUE TO OSDR UALA2012020900788Actuator · leakingRT ENG HAS OIL LIKE FLUID LEAKING FROM ENG HAS A 3 FT DIAMETER PUDDLE BL0. DEPLOYED RT ENG THRUST REVERSER AND STOWED. THRUST REVERSER LOCKING ACTUATOR NO LEAKS WHEN PRESSURIZED, OPERATION NORMAL.SDR USAA2012020700022Reservoir · leakingFLT 1250, THE CREW REPORTED AN ODOR IN THE CABIN DURING DESCENT. MAINTENANCE FOUND THE RIGHT ENGINE THRUST REVERSER RESERVOIR ASSEMBLY TOP LEAKING OIL ONTO THE RT ENGINE. REPLACED THE RT ENGINE THRUST REVERSER AUX RESERVOIR ASSEMBLY.SDR CA120130013Warning Message · false activation(CAN) DURING TAKEOFF ROLL AT APPROXIMATELY 60 KNOTS THE MASTER CAUTION AND ENGINE ANNUNCIATOR LIGHTS, ON THE GLARESHIELD ILLUMINATED. FLIGHT CREW ELECTED TO ABORT THE TAKEOFF AND RETURNED TO THE GATE UNEVENTFULLY. MAINTENANCE CARRIED OUT AN ELECTRONIC ENGINE SDR UALA2012013000601Valve · failedNR 1 ENG T-R SYC LOCK VALVE IS NOT IN COMMANDED POSITION. ITEM HAS MULTIPLE HIT IN FAULT HISTORY. REF J-C2-2020 ITEM 7. RPLC'D SYNC LOCK VALVE PER MM ON NR 1 ENG SYNC LOCK VALVE FAILED OPERATIONAL TEST. FOUND C-B P23 ON PANEL P110 POPPED. RESET C-B. SYNCSDR A6WA201240142Thrust Reverser · malfunctionedDURING CLIMB OUT, RECEIVED RT THRUST REVERSER UNLOCK CAUTION WITH EMERGENCY TOW LIGHT. PUSHED EMERGENCY STOW AND LIGHT PERSISTED, ACFT FLEW NORMALLY. COMPLIED WITH THRUST REVERSER OPS CHECK, OPERATED NORMALLY 3 TIMES IAW 71-00-00-710-806.SDR REXA201200146Switch · out of adjustAIR RETURN RT T/R REV UNLOCK MSG IN FLT. T/S RT T/R REV UNLOCK MSG IAW FIM 78-30-00. COULD NOT DUPLICATE ON GROUND. FOUND STOW SWITCH OUT OF RIG (0.100"). RIGGED STOW, DEPLOY & THROTTLE LOCKOUT MICROSWITCHES IAW AMM 78-37-01. REMOVED AND REPLACED RELAY 1KSDR REXA201200138Warning System · activatedDIVERTED TO TYS FOR L REV UNLOCKED CAUTION IN FLIGHT HAPPEND AT 15,000 FT INDICATION ONLY. NO ADVERSE FLIGHT CHARACTERISTICS. OPC LT TR IAW AMM 78-30-00. OPC GOOD.SDR FDEA201201180245Shutoff Valve · malfunctionedNR 1 ENGINE REVERSER UNLOCKED ON TAKEOFF. ECAM MESSAGE FOR NR1 THRUST REVERSER PRESSURIZED NO THROTTLE RESPONSE ON NR 1 ENGINE, THROTTLE LEVER MOVED FREELY. PERFORMED A GENERAL VISUAL INSPECTION OF THE NR 1 ENG THRUST REVERSER, CDU SWITCH CONNECTORS AND SWITCSDR FDEA201201180241Thrust Reverser · corrodedCORROSION FOUND ON TRANSLATING SLEEVE OUT SKIN. THRUST REVERSER ASSEMBLY REPLACED.SDR UALA2012011600324Sleeve · delaminatedNR 1 THRUST REVERSER SYSTEM INOPERATIVE. SAMC COMMENTS: REVERSER INOPED DUE TO SLEEVE OUTER W ALL ACCOUSTIC MESH DELAMINATED. OPBLM-EMC SAMC TEXT: REVERSER CAN BE REACTIVATED AFTER SLEEVE REPAIR IS ACCOMPLISHED. OPBLM-EMC :LCL MAINT DEACTIVATED ENG 1 THRUSSDR REXA201200118Switch · dirtyAIR RETURN L REV UNLOCKED CAUTION DURING CLIMBOUT RAN IAI CARD & QRH RETURNED TO DTW NO BUFFETING/YAW ISSUES NORMAL AIRPLANE CONTROL. CLEANED L/H T/R STOW SWITCH. MSG CLEARED. OPC GOOD IAW CRJ AMM 78-30-00.SDR G1IAJAN12N35CYSwitch · out of adjustFAR 135.415(C) 1/13/12 ON CLIMBOUT OF FAI THE RIGHT THRUST REVERSER UNLOCK LIGHT CAME ON. THE FLIGHT CREW REDUCED THE AIRCRAFT SPEED AND THE LIGHT WENT OUT. RETURNED TO FAI AND LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND UPPER DOOR POSITION INDICATORSDR UIEA2012011300009Structure · damagedDURING MX WALKAROUND, FOUND DAMAGE TO THE NR 2 ENGINE THRUST REVERSER ACOUSTIC MESH AND HONEYCOMB. PERFORMED A TIME LIMITED REPAIR.SDR ZKFR2012011103243Actuator · leakingRT ENGINE, INBD THRUST REVERSER ACTUATOR LEAKING. MM SPECIFICALLY STATES THERE ARE NO ALLOWABLE LEAKAGE FOR COMPONENTS, FILTERS, PRESSURE SWITCHES, TRANSDUCERS, VALVES OR TUBING UNLESS SPECIFICALLY MENTIONED AND TO CONTACT MFG CUSTOMER SUPPORT WHEN ANY MX ON SDR ZKFR201201113243Actuator · leakingLT ENGINE, INBD THRUST REVERSER ACTUATOR LEAKING. MM SPECIFICALLY STATES THERE ARE NO ALLOWABLE LEAKAGE FOR COMPONENTS, FILTERS, PRESSURE SWITCHES, TRANSDUCERS, VALVES OR TUBING UNLESS SPECIFICALLY MENTIONED AND TO CONTACT MFG CUSTOMER SUPPORT WHEN ANY MX ON SDR UALA2012010900205Actuator · stuckLEFT REVERSER LEVER STUCK IN IDLE REV. REV LEVER INTERLOCK ACTUATOR IN RETRACTED POSITION. RMV'D POWER FROM ACFT, REPOWER ACFT TRIED REVERSER - REVERSE LEVER INTERLOCK NOW INOP (EXTENDED). REPLACED INTERLOCK RELAY - NO HELP. REVERSE LEVER INTERLOCK INOP EXSDR A6WA201240172Link Assy · chafedRT THRUST REVERSER NR 1 LINK ARM CHAFED. BLENDED CHAFE IAW REO 601R-78-30-2940, FOUND TO BE WITHIN LIMITS.SDR ASOA201200065Pdu · failedLEFT THRUST REVERSER UNLOCKED MESSAGE DURING CLIMB, EMERGENCY DECLARED. PERFORMED CHECKLIST AND COMPLIED WITH QRH PROCEDURE. AIR RETURN TO DEPARTURE. R & R LT ENGINE PDU IAW AMM 78-32-03 AND 78-32-03, ITEM 5A. OPS CHECKED GOOD.SDR UALA2012010600142Helicoil · failedLEFT THRUST REVERSER DEACTIVATION PIN HELICOIL PULLED OUT. REPLACED RIGHT ENGINE INBOARD DEACTVATION PIN HELICOIL.SDR CA120106003Thrust Reverser · malfunctioned(CAN) AFTER TAKEOFF THE MASTER CAUTION LIGHT ILLUMINATED FOLLOWED BY THE OVERHEAD NR 2 ENGINE REVERSER LIGHT AND THE NR 2 ENGINE CONTROL LIGHT. CREW ELECTED TO RETURN TO DEPARTURE AIRPORT FOR MAINTENANCE AND LANDED UNEVENTFULLY. FOLLOWING THE PROCEDURE IAW MEL
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