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 DHL9780258CTr Sleeve · wornAT C-CHECK, ENG NR 1 ON RT REV SLEEVE INTERIOR SKIN 30 AFT OF FWD TOP HOLE WORN THROUGH. CUT OUT DAMAGED AREA AND FABRICATED REPAIR PER CFM 56 MM 78-31-10. INSTALLED REPAIR PER SRM 51-1-21A, 3 X 3.SDR AU971659Sleeve · worn(AUS) NO2 ENGINE THRUST REVERSER INBOARD `SLEEVE NOT STOWED' PROXIMITY SWITCH SLEEVE WORN AND OUT OF ADJUSTMENT.SDR AU971657Thrust Reverser · corroded(AUS) NO2 ENGINE OUTBOARD THRUST REVERSER HALF CORRODED AND DAMAGED.METAL STRUT LEADING EDGE DAMAGED AND BROKEN OFF LODGING INCASCADE FORWARD RECESS CAUSING A BLOCKER DOOR TO BREAK AND SEVERE BLOCKER DOOR CARRIAGE DAMAGE.SDR AU971510Thrust Reverser · corroded(AUS) RH OUTBOARD THRUST REVERSER CORRODED AND DAMAGED. METAL STRUT LEADING EDGE DAMAGED AREA BROKEN OFF AND LODGED IN CASCADE FORWARD RECESS CAUSING A BLOCKER DOOR TO BREAK AND SEVERE BLOCKER DOOR CARRIAGE DAMAGE.SDR CALA9701595Thrust Reverser · crackedINSPECTION FOUND A CRACK ON INNER SKIN ADJACENT TO OPEN CLOSE ACTUATOR OF #2 ENGINE C DUCT RH. THE #2 ENGINE R/H THRUST REVERSER WAS REPLACED IAW MM 78-32-11.SDR CALA9701594Thrust Reverser · delaminatedINSPECTION FOUND #2 ENGINE L/H THRUST REVERSER UPPER AFT SIDEWALL DELAMINATED. THE #2 ENGINE L/H THRUST REVERSER WAS REPLACED IAW MM 78-32-11.SDR CA971104011Thrust Reverser · malfunction(CAN) THRUST REVERSER LIGHT ON DURING CRUISE. AIRCRAFT DIVERTED. THRUST REVERSER HAS BEEN LOCKED AND AIRCRAFT HAS BEEN DISPATCHED AS PER MEL 78-31-33.SDR AU971604Lock · faulty(AUS) LH INBOARD THRUST REVERSER SYNCH LOCK FAULTY. WORKSHOP TESTING COULD FIND NO MALFUNCTION.SDR P5CA9701800Tr Sleeve · damagedUPGRADE PREVIOUS REPAIR, NR 1 ENGINE L/THRUST REVERSER SLEEVE 7 O'CLOCK POSITION. REPAIRED PER SRM 51-40-06.SDR ABXA9701832Stinger · delaminatedDURING INSPECTION, FOUND THRUST REVERSER STINGER ASSY HAD SEVERE DELAMINATION AND WIDE SPREAD CORROSION. REPAIRED UNIT COMPLETE.SDR ABXA9701831Stinger · delaminatedDURING INSPECTION, FOUND SEVERE DELAMINATION AND WIDESPREAD CORROSION ON LOWER THRUST REVERSER STINGER. REPAIRED UNIT COMPLETE.SDR 97ZZZX4571Clip · missingTHRUST REVERSER BLOCKER DOOR CONTROL ARM PIN RETAINER CLIPS FOUND MISSING WITH ABNORMAL REGULARITY. SUBMITTER RECOMMENDATION: RE-DESIGN WITH DRILLED PIN AND INSTALL COTTER PIN VERSUS RETAINER CHIP.SDR ABXA9701673Angle · crackedDURING C-CHECK, FOUND THE NR 1 THRUST REVERSER LOWER DOOR ANGLE AT THE INBOARD IDLER LINK ATTACH POINT CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-1, 51-30-2, AND 51-30-8.SDR CA971015032Selector Valve · leaking(CAN) DURING A "C" CHECK INSPECTION THE THRUST REVERSER SELECTOR VALVE OF NR1 ENGINE WAS FOUND TO HAVE A LEAKING SHAFT SEAL, THE SELECTOR WAS REMOVED AND A SERVICEABLE UNIT INSTALLED AND THE SYSTEM RETURNED TO SERVICE.SDR 97ZZZM1081Actuator · leakingGREEN SYSTEM HYDRAULIC FLUID DROP, MESSAGE DISPLAYED ON ECAM. FLUID LOSS AND CHECKLIST FOLLOWED. (M)SDR ABXA9701542Tr Track · wornNR 4 PYLON THRUST REVERSER UPPER CENTER TRACK WORN AT AFT FLANGES. WELDED TRACK IAW ABX DWG C89R01, COUNTER BORED TRACK IAW DWG 9753006 AND INSTALLED TRACK IAW DC8 SRM 51-3-0.SDR 97ZZZX4570Track Beam · excess wearFOUND BOEING 747, PW4000 SERIES ENGINE THRUST REVERSER WITH LOWER TRACK BEAM EXCESS WEAR. THE WEAR WAS FOUND ALONG AUXILIARY TRACK.SDR 97ZZZX4568Track Beam · excess wearFOUND BOEING 747, PW4000 SERIES ENGINE THRUST REVERSER HAD LOWER TRACK BEAM EXCESS WEAR. THE WEAR WAS FOUND ALONG AUXILIARY TRACK.SDR 97ZZZX4567Track Beam · excess wearINSPECTION FOUND PW4000 SERIES ENGINE THRUST REVERSER HAD LOWER TRACK BEAM EXCESS WEAR. THE WEAR WAS FOUND ALONG AUXILIARY TRACK.SDR 97ZZZX4569Track Beam · excess wearSUBMITTER REPORTS AN INCREASE OF BOEING 747 PW4000 SERIES ENGINE THRUST REVERSER WITH LOWER TRACK BEAM EXCESS WEAR. THE WEAR WAS FOUND ALONG THE AUXILIARY TRACK.SDR 97ZZZX4566Track Beam · excess wearSUBMITTER REPORTS AN INCREASE OF BOEING 747 PW4000 SERIES ENGINE THRUST REVERSER, LOWER TRACK BEAM EXCESS WEAR. THE WEAR WAS FOUND ALONG THE AUXILIARY TRACK.SDR DLM88971919Line · looseON CLIMBOUT, HOT BURNED AIR SMELL CAME IN COCKPIT AND CABIN W/ ENG ANTI-ICE IN USE. F/A REPORTED THIN MIST/SMOKE INAFT CABIN AND SMOKE ALARM ACTIVATION IN AFT LAV. SMELL DISIPATED, SMOKE CLEARED AND SMOKE ALARM STOPPED WHEN ENG ANTI-ICE SECURED. FOUND LEFT SDR P5CA9701553Tr Sleeve · damagedDAMAGE ON TRAILING EDGE INBOARD LOWER SIDE OF NR 4 ENGINE FAN THRUST REVERSER SLEEVE. REPAIRED DAMAGE ON NR 4 ENGINE FAN SLEEVE PER BAC SRM 54-30-03.SDR AWXA9700541Shuttle Valve · malfunctionedAIR TURNBACK TOTAL 'A' SYSTEM HYDRAULIC FAILURE AFTER GEAR UP. REMOVED AND REPLACED NR 1 ENGINE THRUST REVERSER SHUTTLE VALVE PER BMM 78-34-22. REMOVED AND REPLACED HYDRAULIC STANDBY PUMP, LEAK AND OPS CHECK GOOD. REMOVED, INSPECTED AND REPLACED STANDBY PRESDR 9716251144Tr Light · illuminatedON TAKEOFF ROLL, THE NR 3 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AT 100 KNOTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE DEFERRED THE REVERSER INDICATION SYSTEM UNDER MEL 78-2A WITH THE REVERSER STOWED AND LOCKED. ESDR 9716051148Tr Cable · out of adjustWHILE ADVANCING THROTTLES TO TAKEOFF POWER, THE NR 2 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE LOCKED OUT THE NR 2 THRUST REVERSER AND PLACED IT ON MEL 78-1A. AIRCRAFT THEN DESDR HALA9700164Skin · crackedSBA - IN C-CHECK, NR 2 ENGINE THRUST REVERSER LOWER CLAM SHELL EXT SKIN AFT EDGE FOUR CRACKS AFT OF RIVETS HOLE THREE .375 INCH LONG, AND ONE 1.75 INCH LONG. REMOVED RIVETS, STOP DRILLED PER M 19N-010 PAGE 1. FABRICATED REPAIR DOUBLER, AND INSTALLED PER M 19SDR 9715581149Tr Unit · malfunctionedDURING LANDING ROLLOUT, THE NR 3 ENGINE THRUST REVERSER DID NOT STOW. THE NR 3 ENGINE EGT CLIMBED TO 920C AND THE ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED THE ENGINE PER MM 70-00-00. EGT WAS WITHIN LIMITS AND NO DEFECTS WERE NOTED. GROUND RUN OF ENGINE SDR 9714566719Tr Unit · malfunctionedAFTER LANDING, THE NR 3 ENGINE THRUST REVERSER DID NOT INDICATE GREEN (FULLY DEPLOYED). THE ENGINE DID APPEAR TO GO INTO REVERSE. EGT INDICATION ROSE RAPIDLY AND THE ENGINE WAS SHUT DOWN. MAINTENANCE FOUND THE NR 3 REVERSER PART WAY DEPLOYED. REVERSER WAS SDR CA970731003Switch · intermittent(CAN) HISTORY OF THRUST REVERSER ISOLATION LIGHT ON BRIEFLY AFTER TAKEOFF. ON NEXT FLIGHT ISOLATION LIGHT REMAINED ON.AIRCRAFT RETURNED. SWITCH S529 REPLACED.SDR ABXA9701268Tr Link · crackedDURING C-CHECK, FOUND THE NR 1 ENGINE THRUST REVERSER LOWER INBOARD DRIVE LINK CRACKED AT THE FORWARD GREASE FITTING. *S/D* REPLACED DRIVE LINK IAW DC9 MM 78-31-5.SDR 97ZZZX3437Body · crackedTHE 1U1225'S ISOLATION BODY, PN 1225-10, IS SUSCEPTIBLE TO PINHOLES AND CRACKS ALONG THE BODY'S SEAMS AND WITHIN THE FITTING PORTS. RONSON MIGHT CONSIDER MANUFACTURING A STRONGER BODY, PERHAPS A CHANGE OF MATERIAL.SDR CA970722037Duct · adrift(CAN) AIRCRAFT RETURNED FROM FLIGHT BECAUSE THE LEFT HAND THRUST REVERSER UNLOCK LIGHT WAS ON. INSPECTION FOUND THE PNEUMATIC INTERMEDIATE PRESSURE DUCT ADRIFT. DUCT REINSTALLED. ALSO THE LEFT ENGINE THROTTLE LOCKOUT AND STOW SWITCHES WERE REPLACED AND THE DAMSDR COMA9760127Tr Unit · inoperativeLEFT ENGINE THRUST REVERSE UNLOCK AND REV ICON ON DURING FLIGHT. SECURED AND DEFERRED LT THRUST REVERSE SYSTEM PER MEL.SDR REXA97179Tr Linkage · out of adjustRIGHT ENGINE FLAMED OUT ON LANDING AFTER COMING OUT OF DEEP REVERSE. PULLED T-HANDLES AND FOLLOWED CHECKLIST. FLAME WAS OBSERVED IN ENGINE INLET. ENGINE WAS FOUND TO BE OUT OR RIG IN REVERSE. RIGGED REVERSE LINKAGE. (M)SDR UPS97223779Ramp Skin · wornINSPECTION TYPE:C, NR 3 ENG THRUST REV LOWER DOOR RAMP SKIN WORN DUE TO CHAFFING OF SEAL REPAIRED I.A.W. EFIS AND RE ENGINE SUPP SRM 54-10-03 FIG 203.SDR UPS97223776Ramp Skin · wornINSPECTION TYPE:C, NR 1 ENG T.REV LOWER DOOR INNER RAMP SKIN WORN DUE TO CHAFFING OF SEAL. REPAIR CARRIED OUT I.A.W. EFIS AND RE ENGINE SUPPLEMENT SRM 54-10-0 3 FIG 203.SDR 9712551224Tr Unit · malfunctionedAFTER LANDING, THE NR 3 ENGINE WOULD NOT COME OUT OF REVERSE THRUST. THE ENGINE WAS SHUT DOWN. MAINTENANCE OPERATED NR 3 REVERSER AND FOUND NO PROBLEMS. AIRCRAFT RETURNED TO SERVICE.SDR 97UAL900484Reverser · delaminatedON WALK AROUND INSPECTION, FOUND DELAMINATION OF RIGHT HAND SIDE UPPER SIDEWALL ON THE FLOW SIDE OF THE RIGHT REVERSER AT 12:00 O'CLOCK POSITION MEASURING 12 BY 8 INCHES. *S/D* THE DELAMINATION WAS DUE TO MOISTURE INTRUSION THROUGH SEAM. AIRFLOW CAUSED A LASDR 9711421146Tr Unit · locked outDURING TAKEOFF ROLL, NR 2 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AT 90 KNOTS. MAINTENANCE VERIFIED THAT THE THRUST REVERSER WAS LOCKED OUT AND CHANGED THE MEL TO 78-2A.SDR 9711431224Tr Unit · malfunctionedAFTER LANDING, THE NR 3 ENGINE THRUST REVERSER DID NOT COME OUT OF REVERSE THRUST. THE ENGINE WAS SHUT DOWN AFTER CLEARING THE RUNWAY. MAINTENANCE LOCKED OUT NR 3 THRUST REVERSER PER MEL 78-1A. EXACT PART CAUSING PROBLEM TO BE DETERMINED.SDR SWAA970550Connector · shortedEN ROUTE, NR 1 ENGINE REVERSER UNLOCKED LIGHT ILLUMINATED, ACCOMPANIED BY MID CABIN VIBRATION AND NOISE. AIRCRAFT DIVERTED TO HOU AND MADE AN UNEVENTFUL LANDING. TROUBLESHOT AND FOUND A SHORT AT ISOLATION VALVE CONNECTOR PLUG. REPLACED CONNECTOR PER BOEING SDR 97UAL900447Relay · failedIMMEDIATELY AFTER LIFTOFF, RECEIVED NR 4 ENGINE THRUST REVERSER EICAS MESSAGE. AIRCRAFT RETURNED TO FIELD. *S/D* EICAS MESSAGE WAS FIXED BY REPLACING 4 RELAYS IN THE INDICATION CIRCUIT. THE RELAY NUMBERS FROM THE WIRING SCHEMATIC 78-36-04 PAGE 101 SHEET 1 SDR SWAA970548Sensors · out of adjustEN ROUTE, NR 1 ENGINE REVERSER LIGHT ILLUMINATED INTERMITTENTLY FOR ABOUT 40 SECONDS, ALONG WITH SLIGHT VIBRATION AT MID CABIN AREA. ALSO, OVERHEAD REVERSER LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO ABQ AND MADE AN UNEVENTFUL LANDING. LOCKED OUT REVERSER PER SDR 9711136624Tr Unit · malfunctionedNR 1 ENGINE THRUST REVERSER WOULD NOT STOW AFTER LANDING. CREW RECYCLED THE NR 1 REVERSER LEVER AND THE ENGINE COMPRESSOR STALLED. EGT PEAKED AT 550C FOR 2 TO 3 SECONDS AND THE ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED ENGINE INLET, EXHAUST, AND BLEED SYSSDR 97ZZZM864Link · chafedNR 1 ENGINE REAR LINK UPPER HALF CHAFED BEYOND MAX ALLOWABLE DEPTH. REPLACED NR 1 ENGINE REAR LINK UPPER HALF, REF ENG CHANGE CHECKLIST FOR DETAILS.SDR CALA9700771Hyd Line · brokenTHE LT HYDRAULIC QUANTITY GAUGE DROPPED TO ZERO WITH THE LEFT HYDRAULIC PRESSURE AND LEFT BRAKE PRESSURE ALSO AT ZERO AFTER TOUCHDOWN AT EWR. MAINTENANCE FOUND THE LT THRUST REVERSER HYDRAULIC PRESSURE SWITCH LINE BROKEN. THE LINE WAS REMOVED AND REPLACED. SDR 9710206729Tr Unit · malfunctionedDURING LANDING, THE NR 3 ENGINE DID NOT COME OUT OF REVERSE THRUST. OIL PRESSURE DECREASED AND EGT ROSE TO 860 CELSIUS. ENGINE WAS SHUTDOWN. MAINTENANCE RAN ENGINE AND OPERATED THE THRUST REVERSER WITH ALL INDICATIONS NORMAL.SDR P5CA9700863Cascade Web · crackedNR 4 ENG 6R CASCADE WEB IS CRACKED. BLENDED OUT IAW MM 78-31-07, REF CWS NR 854171.SDR IXKA9700032Switch · out of positionEWR - FLT 309 - EWR/ATL - ON TAKEOFF ROLL, NR 2 ENG REVERSER LIGHT FLICKERING, ABORTED TAKEOFF. ENGINE PARAMETER NORMAL AND NO OTHER INDICATIONS OF LOSS OF THRUST. BRAKE COOLING TIME OBSERVED. CHECKED SECURITY OF WIRING AND SWITCH PLUG CONNECTOR, ALL CHECK
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