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 95ZZZX5863Actuator · leakingREMOVED TRUST 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.SDR ABXA9600354Tr Drive Link · crackedDURING COMPLIANCE OF AD 75-14-06, AD 90-18-03; SB'S 78-36, 78-38, 78-40 AND 78-66, FOUND A CRACK INDICATION ON THE NR 2 ENGINE UPPER OUTBOARD THRUST REVERSER DRIVER LINK. REMOVED LINK IAW DC-9 MM 78-31-5. LINK CRACKED, SCRAPPED LINK.SDR 95UAL900159Connector · looseABORTED TAKEOFF AT 80 KNOTS DUE TO A REVERSER LIGHT. FOUND LOOSE CONNECTOR, RESET THE ENGINE ACCESSORY UNIT, AND REPLACED THE CONTROL VALVE MODULE.SDR 95ZZZX5837Former · crackedLEFT ENGINE, OUTBOARD. THE FORWARD ATTACH FORMER CRACKED AT THE 2 MOUNT ATTACH HOLES. THIS ALLOWED THE LEADING EDGE OF THE STANG FAIRING TO FOLD BACK AND BREAK OFF. THE AIRCRAFT LANDED SAFELY. SUBMITTER STATED AFTER INSPECTING A SECOND BEECH JET, 2 MORE FOSDR 95ZZZX5547Stang · departedLEFT OUTBOARD STANG DEPARTED THE AIRCRAFT IN-FLIGHT. NO DAMAGE TO THE AIRCRAFT WAS FOUND, FLIGHT CREW FELT NOTHING IN-FLIGHT. ROHR SB BS 400 78-4 ADDRESSES THIS PROBLEM AND HAS KITS OUT TO FIX THE PROBLEM. SUBMITTER SUGGESTS THIS SHOULD BE AN AD.SDR ABXA9500915Translating Ring · crackedDURING 825AX MOD, FOUND NR 4 ENGINE THRUST REVERSER TRANSLATING RING CRACKED. REPAIRED NR 4 ENGINE THRUST REVERSER TRANSLATING RING IAW ABX REA D878-11909.SDR ABXA9500914Translating Ring · crackedDURING 825AX MOD, FOUND NR 2 ENGINE THRUST REVERSER TRANSLATING RING CRACKED. REPAIRED NR 2 ENGINE THRUST REVERSER TRANSLATING RING IAW ABX REA D878-11887.SDR 95ZZZX5878Flex Shaft · strands brokenDURING AN INTERMEDIATE THRUST REVERSER INSPECTION ON AIRCRAFT, FOUND BOTH FLEX SHAFTS HAD BROKEN STRANDS IN THE OUTER STAINLESS STEEL BRAIDING. THE CAUSE OF THE BROKEN STRANDS WAS DUE TO THE SEPARATION IN THE TEFLON HOUSING THAT HOLDS THE ROTATING SHAFT. WHESDR 9513591156Tr Drive Cable · brokenDURING TAKEOFF, THE NR 2 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED. REMOVED BROKEN DRIVE CABLE, INSTALLED LOCKOUT PLATES AND DEFERRED PER MEL 78-1A.SDR UIEA9503Tr Duct · chafedDURING CLIMB-OUT, NR 4 PYLON VALVE CLOSE LIGHT CAME ON FOLLOWED BY HI-STAGE OPEN LIGHT, FOLLOWED BY FIRE WARNING ALMOST FULL SCALE. FIRE WARNING AND HI-STAGE OPEN LIGHT WENT OUT WHEN THROTTLE PULLED BACK. DUMP FUEL, AIR TURN BACK. FOUND REVERSER BLEED AIR DSDR DL757953458Reverser Panel · damagedDURING THRU/SERVICING CHECK, FOUND A 6 INCH BY 8 INCH HOLE BURNED THROUGH RT INBOARD REVERSER COLDSTREAM ACOUSTIC PANEL JUST AFT OF INTAKE FOR PNEUMATICS HEAT EXCHANGER COLD AIR AT THE 11 O'CLOCK POSITION. FOUND IMMERSION THERMOCOUPLE BACKED OUT OF MOUNTING HSDR W8PA9501Tr Prox Switch · out of adjustFLT 115 - COS-LAS - NR 2 THRUST REVERSER LIGHT ILLUMINATED JUST AFTER TAKEOFF. AIRCRAFT RETURNED TO COS. FOUND S832 STOW PROXIMITY SWITCH OUT OF ADJUSTMENT. ADJUSTED PROXIMITY SWITCH PER MM 78-34-03. (M)SDR 9501W8PAStow Prox Switch · out of adjustFLT NR 115 - COS-LAS - NR 2 THRUST REVERSER LIGHT ILLUMINATED JUST AFTER TAKEOFF. AIRCRAFT RETURNED TO COS. FOUND S832 STOW PROXIMITY SWITCH OUT OF ADJUSTMENT. ADJUSTED PROXIMITY SWITCH PER MM 78-34-03. (M)SDR ASAA9580185Hyd Line · brokenPDX - JUST PRIOR TO PARKING AT GATE OF FLIGHT NR 475, CREW REPORTED SMOKE/FUMES IN CABIN AND LEFT HYDRAULIC QUANTITY DECREASED TO ZERO. SHUTDOWN ENGINES, APU, ELECTRICAL POWER AND OPENED ALL DOORS. PASSENGERS DEPLANED WITHOUT INCIDENT. FOUND HYDRAULIC LINE SDR 9512221150Tr Unit · malfunctionedDURING TAKEOFF ROLL, THE NR 1 ENGINE REVERSER UNLOCK LIGHT ILLUMINATED AND THE TAKEOFF WAS ABORTED. THE REVERSER WAS DEACTIVATED AND PLACED ON MEL.SDR COM60534Tr Unit · malfunctionedAFTER TAKEOFF, WHEN RIGHT THRUST REVERSER ARM SWITCH SET TO OFF, THE RIGHT T/R UNSAFE MESSAGE CAME ON. ACFT RETURNED TO FIELD. THRUST REVERSER WAS STOWED AND SECURED AND SYSTEM PLACED ON DEFERRED MAINT LIST.SDR HEEA955547Ejector · crackedLT EJECTOR RING ASSEMBLY CRACKED AND PARTS OF RING MISSING.SDR AWXA9500506Tr Door · out of adjustPHX - DURING SCHEDULED C-15 INSPECTION, FOUND NR 2 ENGINE UPPER T/R BUCKET DOOR BUMPERS DO NOT HAVE FULL CONTACT. WELDED PER ER 2-78-32-02. (M)SDR ASAA9580170Hyd Line · brokenSFO - FLT NR 232 - AFTER LANDING, FLIGHT ATTENDANTS REPORTED FUMES/VAPOR IN CABIN. CREW NOTED LEFT HYDRAULIC QUANTITY AT 'O' ENTERING TAXI WAY. ACCOMPLISHED EMERGENCY EVACUATION OF PASSENGERS ON TAXI WAY WITHOUT INCIDENT. FOUND HYDRAULIC LINE TO LEFT ENGINESDR 95ZZZX4260Tr Unit · malfunctionedSTL - FLT 720 - DURING TAKEOFF, SHUT DOWN NR 1 ENGINE, SN 4173, DUE TO UNCOMMANDED THRUST LEVER MOVEMENT TO IDLE AND REVERSER OPERATING LIGHT ILLUMINATION FOR FIVE SECONDS. CHECKED ENGINE CONTROL SYSTEM AND OPERATION WAS NORMAL. DEACTIVATED THRUST REVERSER PSDR ABXA9500652Link · corrodedDURING COMPLIANCE OF A.D. 75-14-06; A.D. 90-18-03; S.B.'S 78-36, 78-38, 78-40 AND 78-66, FOUND NR 2 LOWER LEFT DRIVER LINK HAD A CRACK INDICATION. REPLACED LINK IAW DC-9 OVERHAUL MANUAL 78-30-1. SHOP FINDINGS: LINK CORRODED AND PITTED BEYOND LIMITS. LINK WASDR 95ZZZX3947Switch · arm failedLEFT THRUST REVERSER WOULD DEPLOY ON GROUND ANY TIME SYSTEM WAS ARMED WITHOUT SELECTING DEPLOY. INSPECTED AND FOUND STOW/DEPLOY SWITCH MECHANICAL ARM AND ROLLER BROKEN OFF FROM SWITCH DUE TO FAILURE OF MECHANICAL ARM TO PIVOT POINT THROUGH PIN WELD.SDR ABXA9500604Bracket · chafedDURING C-CHECK INSPECTION, FOUND NR 1 ENGINE THRUST REVERSER CABLE RUN NR 47 CHAFING THROUGH PULLEY BRACKET BELOW COCKPIT PEDESTAL, APPROXIMATELY STA. 110. REPAIRED IAW ABX REA D953-11824-MR.SDR 95ZZZX3376Tr Valve · leakingMROC/KATL - FLT EB814 - DURING CLIMB, LOST HYDRAULIC FLUID AFTER UPLATCH CHECK DEPARTING MROC. ACCOMPLISHED EMERGENCY CHECK LIST AND PROCEDED TO KATL. EMERGENCY DECLARED AT KATL AND LANDED SUCCESSFULLY. MAINTENANCE ISOLATED FLUID LOSS TO THRUST REVERSER SOLSDR COM60494Tr Unit · malfunctionedLEFT ENGINE AMBER REVERSE MESSAGE AND LEFT REVERSE UNLOCKED MESSAGE ON EICAS. MANUALLY DEPLOYED AND STOWED THRUST REVERSER. GROUND RUNS AND SYSTEM OEPRATED NORMALLY.SDR ABXA9500592Tr Fairing · crackedDURING COMPLIANCE OF A.D. 92-22-08, FOUND CRACKED FAIRING ON LOWER THRUST REVERSER BUCKET, INBOARD SIDE, LEFT ENGINE. REPAIRED IAW DC-9 OVERHAUL MANUAL 78-30-1.SDR P5CA9500019Tr Sleeve · gougedFORWARD EDGE OF FAN THRUST REVERSER SLEEVE WORN TO KNIFE EDGE 4 O'CLOCK POSITION. SMOOTH BLENDED GOUGE AS PER BOEING SRM 54-36-01 AND RESTORED TO NORMAL FINISH.SDR P5CA9500014Tr Sleeve · scratchedSCRATCHES RIGHT SIDE NR 4 ENGINE THRUST REVERSER SLEEVE FROM 3:30 TO 4:00 POSITION. REMOVED SCRATCHES AS PER BOEING SRM 51-10-01 PAGE 11 TREATED AND PAINTED AREA.SDR P5CA9500010Skin · working rivetsSMALL AREA OF NR 1 ENGINE THRUST REVERSER SLEEVE SKIN AFT EDGE DELAMINATED. REMOVED AND REPLACED WORKING RIVETS IN DAMAGED AREA AS PER BOEING SRM 51-30-02.SDR 95ZZZM157Tr Sleeve · gougedFORWARD EDGE OF NR 1 ENGINE FAN THRUST REVERSER SLEEVE WORN TO KNIFE EDGE 4 O'CLOCK POSITION. SMOOTH BLENDED GOUGE AS PER BOEING SRM 54-36-01 AND RESTORED TO NORMAL FINISH.SDR 95ZZZM154Tr Sleeve · delaminatedSMALL AREA OF NR 1 ENGINE THRUST REVERSER SLEEVE SKIN AFT EDGE DELAMINATED. REMOVED AND REPLACED WORKING RIVETS IN DAMAGED AREA AS PER BOEING SRM 51-30-02.SDR ABXA9500628Tr Link · crackedDURING COMPLIANCE OF A.D. 75-14-06, A.D. 90-18-03; S.B.'S 78-36, 78-40 AND 78-66, FOUND CRACK INDICATION ON RIGHT ENGINE LOWER INBOARD THRUST REVERSER DRIVER LINK. REPLACED DRIVER LINK IAW DC-9 M.M. 78-31-5. SHOP FINDING: LINK CRACKED. SCRAPPED LINK.SDR DL76E954321Thrust Reverser · delaminationNUMBER ONE ENGINE LEFT THRUST REVERSER ASSEMBLY INNER WALL HAD EXISTING SRM REPAIRS AND ADDITIONAL DELAMINATION. ALSO, UPPER BEAM HAD EXISTING SRM REPAIR AND ADDITIONAL DELAMINATION. COMPONENT WAS REPAIRED PER ER/A 276777-14. REPAIR CONSISTED OF REPLACING FSDR USAA950527Fitting · crackedJFK - FLT 968 - ON INITIAL CLIMB-OUT OF LGA, 'A' SYSTEM HYDRAULICS FAILED. FLIGHT DIVERTED INTO JFK WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED TEE FITTING AT RIGHT THRUST REVERSER PRESSURE SWITCH, 'A' SYSTEM HYDRAULICS RETURN, PRESSURE SDR ABXA9500454Line · rupturedDURING ROLLOUT, THE THRUST REVERSER SYSTEM HYDRAULIC RETURN LINE RUPTURED. DEFERRED AND DEACTIVATED THE T/R SYSTEM. INSPECTED AND PREPARED AIRCRAFT FOR FERRY FLIGHT TO ILN, AT ILN, THE HYDRAULIC LINE WAS REPLACED. SYSTEM OPERATIONALLY AND LEAKED CHECKED GOOSDR AWXA9500264Accessory Unit · malfunctionPHX-SFO - FLT 605 - AFTER TAKEOFF, THE TAKEOFF WARNING HORN WOULD NOT SHUT OFF. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE PERFORMED TAKEOFF WARNING TEST PER AWA TASK CARD A1B31007, NO DEFECTS WERE NOTED. MAINTENANCE ALSO REPLACED ENGINE ACCESSDR ABXA9500553Drive Link · crackedDURING COMPLIANCE OF AD 75-14-06, AD 90-18-03, SB'S 78-36, 78-38, 78-40 AND 78-66, FOUND OUTBOARD LOWER THRUST REVERSER DRIVE LINK HAD A CRACK INDICATION. REPLACED OUTBOARD LOWER THRUST REVERSER DRIVE LINK IAW DC-9 MM 78-32, LINK WAS SCRAPPED.SDR DLL13951652Tr Angle · crackedT/R REPAIR NR 2 ENG TRANSLATING SLEEVE REPAIRED PER SRM 54-37-00 FIG 802. UNDERLYING BULKHEAD REPAIR SPLICE ANGLE DAMAGE PER RB-211-22B ENGINE MANUAL 78-32-07 FIG 78-32-07-990-012.SDR DLL13951766Sleeve · damageT/R REPAIR NR 2 ENG TRANSLATING SLEEVE REPAIRED PER SRM 54-37-00 FIG 802 PG 803 AND UNDER LYING BULKHEAD. REPAIRED SPLICE ANGLE DAMAGE PER 222B ENG MANUAL 78-32-07 FIG 990-012.SDR ABXA9500355Link · crackedDURING COMPLIANCE OF AD 75-14-06, AD 90-18-03, SB 78-38, 78-66, 78-40, 78-36, FOUND THE NR 2 THRUST REVERSER LOWER RIGHT DRIVER LINK HAD A CRACK INDICATION. REPLACED LINK IAW DC-9 MM 78-32. LINK WAS SCRAPPED.SDR SWAA95287Tr Module · malfunctionedAFTER DEPARTURE, THRUST REVERSER ISOLATION VALVE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. REPLACED BOTH ISOLATION PRESSURE SWITCHES AND T/R ISOLATION MODULE. LEAK AND OPS CHECKED NORMAL PER BOEING MM.SDR 95ZZZX2249Bypass Duct · crackedWHILE PERFORMING OTHER MAINTENANCE ON THE AIRCRAFT, A TECHNICIAN NOTED LIGHT SHOWING THROUGH THE TAILPIPE FROM THE BYPASS DUCT TO THRUST REVERSER ATTACH FLANGE. THE COWLING RING WAS REMOVED AND THE OUTBOARD T/R ATTACH FLANGE WAS FOUND CRACKED AND DEFORMED. OSDR 95ZZZX1990Switch · out of adjustT/R LIGHT CAME ON IN-FLIGHT. SWITCHES OUT OF ADJUSTMENT GIVING AN INDICATION LIGHT TO COCKPIT. T/R WAS STOWED. SWITCHES 36K AND 37K WERE ADJUSTED PER MM AND SYSTEM F/T OKAY. SUSPECT CAUSE: SWITCHES IN A HIGH HEAT AREA AND OVER TIME CAN GO OUT OF ADJUSTMENSDR 95ZZZX1989Switch · out of adjustT/R LIGHT CAME ON IN-FLIGHT. SWITCHES OUT OF ADJUSTMENT GIVING AN INDICATION LIGHT TO COCKPIT. T/R WAS STOWED. SWITCHES 36K AND 37K WERE ADJUSTED PER MM AND SYSTEM F/T OKAY. SUSPECT CAUSE: SWITCHES IN A HIGH HEAT AREA AND OVER TIME CAN GO OUT OF ADJUSTMENSDR 95ZZZX1934Door · openWINDSOR LOCKS, CN - DURING CLIMB, HEARD BANG AND AIRCRAFT YAWED LEFT. DUMPED FUEL TO LANDING WEIGHT. RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. INSPECTION OF AIRCRAFT REVEALED NO DAMAGE. AFTER SHUT DOWN, NOTED LT CASCADE DOORS ON NR 1 ENGINE OPEN. RSDR 95UAL737038Tr Light · illuminatedRIGHT ENGINE REVERSER LIGHT ON OVERHEAD PANEL CAME ON AT 95 KNOTS ON TAKEOFF.SDR 95ZZZX1746Hinge · crackedDURING A SCHEDULED INSPECTION OF NR 2 T/R, THE RT AFT HINGE OF THE UPPER DOOR WAS FOUND CRACKED. CAUSE UNKNOWN.SDR 95ZZZW345Switch · failedENGINE NR 2 REVERSER OPERATING LIGHT WILL NOT EXTINGUISH. REMOVED AND REPLACED NR 2 ENGINE REVERSER LIGHT SWITCH. OPS CHECKS NORMAL, MM 78-00.SDR CAL950187T/R Cntl Valve · rupturedSFO - FLT 0165 - THE MAIN CABIN BEGAN TO FILL WITH SMOKE DURING TAXI TO TERMINAL AFTER LANDING AT SFO. THE AIRCRAFT WAS STOPPED ON THE TAXIWAY, THE L-1 DOOR AND TAIL CONE EMERGENCY SLIDES WERE DEPLOYED, AND THE PASSENGERS EVACUATED AS A PRECAUTIONARY MEASURE.SDR 95ZZZX1646Inner Arm · mismanufacturedARMS ARE MANUFACTURED BY LEARJET UNDER PMA. BIZJET RECEIVED AND PUT IN STOCK, 1 EACH DASH 511 ARM AND 6 EACH DASH 512 ARMS. ONE EACH DASH 511 ARM AND 2 EACH DASH 512 ARMS WERE INSTALLED ON A CUSTOMER'S AIRCRAFT. BIZJETS PURCHASING AGENT NOTICIED BY LEAR SAL
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