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 P5CA9600715Fairing Plate · tornBLOCKER DOOR FAIRING PLATE TEARING UPWARD THROUGH SCREWS OF NR 2 ENGINE FAN REVERSE SLEEVE IN AFT AREA AT 6:30 POSITION. REMOVED AND REPLACED FAIRING PLATE PER BAC SRM 51-10-01 AND 51-30-02.SDR 9619153203Connector · damagedDURING TAKEOFF ROLL, NR 1 ENGINE REVERSE UNLOCK MESSAGE ILLUMINATED. TAKEOFF WAS ABORTED AT 40 KNOTS AND AIRCRAFT RETURNED TO THE GATE. GROUND MAINTENANCE FOUND DAMAGED PINS ON CANNON PLUG 402VC. CANNON PLUG PINS WERE REPAIRED.SDR TC8A96057Tr Line · looseNR 2 ENGINE FIRE WARNING, SECURED ENGINE. FOUNDED PNEUMATIC LINES LOOSE AT AFT REVERSER AREA. TIGHTENED LINES, RAN UP TO T/O POWER 1.83 EPR, COULD NOT DUPLICATE THE ITEM MM 78-7-0 AND 71-00.SDR 96ZZZX4886Support Former · crackedIN PROCESS OF ROUTINE INSPECTION, NOTICED THE STANG FAIRING SUPPORT FORMERS, OUTBOARD SIDE OF EACH ENGINE, WERE CRACKED WHERE THEY ATTACH TO STANG. BEECH SB NR 2674 APPLIES TO THIS SUBJECT, HOWEVER, NOT TO THIS SPECIFIC REVERSER PART NUMBER. RECOMMEND REVISSDR CA960827010Pdu · failed(CAN) PDU WOULD NOT MAINTAIN INITIAL RIGGING AS PER MM 1 1/3 TURNS ON DIRECTIONAL CONTROL VALVE GAP (0.315 +/- 0.015). FAILED RESET OF DIRECTIONAL CONTROL VALVE (SHOP AIR).SDR ARWA9608016Tr Unit · cracked1.50 INCH CRACK UPPER STRINGER AND T/R RT SIDE NR 2 ENGINE. REPAIRED PARTS PER ARROW DRAWING NR ARW 016675-0831. FORMED DOUBLER PER DC-8 SRM'S 51-1-7, 78-3-3. INSTALLED PER DC-8 SRM 51-1-21.SDR 96ZZZX4387Longeron · crackedFOUND CRACK ON LEFT ENGINE THRUST REVERSER UPPER DOOR INBOARD LONGERON ASSEMBLY ABOUT TWO INCHES FROM BUMPER. LONGERON ASSY IS WEAK IN MACHINED AREA WHICH IS WHERE THE CRACK IS LOCATED. SUBMITTER STATED IF THE BUMPER IS MODIFIED TO EXTEND PAST THE WEAK AREA,SDR DL76L961883Tr Unit · damagedON ARRIVAL, FOUND NR 1 ENG FAN DUCT COWL ASSY DAMAGED. REPLACED NR 1 ENGINE INBD THRUST REVERSER HALF.SDR HALA96109Tr Unit · inoperativeHNL - FLT 108 - RIGHT ENGINE REVERSE UN-LOCK LIGHT CAME ON AFTER GEAR RETRACTION. RETURNED TO HNL FOR LANDING. LIGHT WENT OUT AFTER LANDING. PLACARD NR 2 REVERSE INOP. LOCKED OUT REVERSER AND DMI NR 98226 ISSUED. ITEM ENTERED ON 1414. (M)SDR ABXA9700108Link · crackedDURING C-CHECK AND COMPLIANCE WITH AD 75-14-06, 90-18-03, FOUND NR 2 ENGINE UPPER OUTBOARD THRUST REVERSER DRIVER LINK CRACKED. REPLACED IAW DC-9 M/M 78-31-5.SDR 96ZZZX4339Bumper Pad · defectivePILOTS REPORTED LT REVERSER WOULD INTERMITTENTLY 'HANG UP' WHILE OPENING, BUT CLOSE AND LOCKING WERE NORMAL. 319.7 HRS, 490 CYCLES PRIOR TO THIS OCCURRENCE, ROHR SB CIT 78-8R1 WAS C/W WHICH INSTALLS NEW DOOR BUMPERS OVER OLD BUMPERS. THIS DECREASES CLEARANCESDR 96ZZZX4338Bumper Pad · defectivePILOTS REPORTED LT REVERSER WOULD INTERMITTENTLY 'HANG UP' WHILE OPENING, BUT CLOSE AND LOCKING WERE NORMAL. 319.7 HRS, 490 CYCLES PRIOR TO THIS OCCURRENCE, ROHR SB CIT 78-8R1 WAS C/W WHICH INSTALLS NEW DOOR BUMPERS OVER OLD BUMPERS. THIS DECREASES CLEARANCESDR 96UAL900579Tr Switch · shortedNR 2 ENGINE REVERSER LIGHT CAME ON DURING TAKEOFF ROLL. TAKEOFF WAS ABORTED. *S/D* THRUST REVERSER STOW POSITION INDICATOR SWITCH HAD INTERMITTENT SHORT. REPLACED SWITCH.SDR DHL9680614CTr Forging · crackedAT C-CHECK, NR 3 ENGINE OUTBOARD THRUST REVERSER UPPER HALF AFT END FORGING FOR SLIDE TUBE BRACKET CRACKED AT AFT END. REPAIRED CRACK PER HSLH REF 19-80059 AND G.E. FAX.SDR 96ZZZX4178Switch · failedTHRUST REVERSER CONTROL CIRCUIT BREAKER ON LEFT SIDE 'POPPED' WHEN REVERSERS WERE ACTUATED. TROUBLESHOOTING DETERMINED THRUST REVERSER CONTROL BOX, P/N 45A5888656-5, HAD BURNT RESISTOR AND TRANSISTOR IN THE THROTTLE T/R LOCK HOLDING SOLENOID CIRCUITS. T/R THSDR IXXA96133Tr Cowl · crackedDURING ROUTINE C-CHECK INSPECTION, THE NR 3 THRUST REVERSER OUTBOARD COWLING WAS FOUND CRACKED AT THE FOUR O'CLOCK POSITION. REPAIR WAS ACCOMPLISHED IAW CFMI SHOP MANUAL 78-32-11, REPAIR 30. (M)SDR COMA9660124Tr Switch · malfunctionRT THRUST REVERSER ICON CAME ON IN FLIGHT. THRUST REVERSER DID NOT DEPLOY. REPLACED THE RT ENGINE THRUST REVERSER STOW SWITCH.SDR P5CA9600377Tr Sleeve · corrodedNR 4 ENGINE HAS SURFACE CORROSION ON THRUST REVERSER SLEEVE AT RT UPPER JACKSCREW BARREL NUT HOLES. REMOVED LEVEL ONE CORROSION AND TREATED IAW SRM 51-10-01.SDR 96ZZZX3724Longeron Assy · crackedFOUND CRACK ON LEFT ENGINE THRUST REVERSER UPPER DOOR INBOARD LONGERON ASSEMBLY, ABOUT 2 INCHES FROM BUMPER. LONGERON ASSEMBLY IS WEAK IN MACHINED AREA WHICH IS WHERE THE CRACK IS LOCATED.SDR SWAA960605Tr Unit · inoperativeAFTER TAKEOFF, CREW EXPERIENCED T/R ISOLATION VALVE LIGHT ILLUMINATING. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. REPLACED ENGINE ACCESSORY UNIT AND BOTH PRESSURE SWITCHES PER BOEING M/M.SDR ABXA9700215Fairing · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-07, FOUND NR 1 REVERSER UPPER DOOR INBOARD FAIRING CRACKED. REPLACED IAW DC-9 SRM 51-30-2, 51-30-8.SDR 9614181150Unlock Light · illuminatedEN ROUTE DTW-MSP, THE NR 3 ENGINE REVERSER UNLOCK LIGHT ILLUMINATED. CREW FOLLOWED COM PROCEDURE, SHUT DOWN THE ENGINE, AND CONTINUED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED VIBRATION AND WINDMILLING CHECKS. REVERSER WAS ALSO CHECKED FOR STOW SDR ABXA9700212Fairing · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND NR 2 REVERSER UPPER DOOR OUTBOARD FAIRING CRACKED. REPLACED IAW DC-9 SRM 51-30-2, 51-30-8.SDR CALA9600824Press Line · crackedTHE RT HYDRAULIC SYSTEM PRESSURE TEMPORARILY WENT TO ZERO UPON GEAR EXTENSION FOR LANDING AT IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC QUANTITY AT ZERO. THE RT THRUST REVERSER CONTROL VALVE HYDRAULIC PRESSURE LINE WAS FOUND SDR ARWA9606063Translating Ring · crackedNR 3 ENGINE TRANSLATING RING HAS 2 INCH CRACK IN RT FORWARD UPPER STRINGER. REPAIRED UPPER STRINGER IAW DC-8 SRM 78-3-3.SDR ARWA9606062Translating Ring · crackedNR 3 ENGINE TRANSLATING RING, AFT UPPER CORNER IS CRACKED. REPAIRED IAW ARROW AIR DRAWING NR ARW 015713-1182, FAA 8110-APPROVED.SDR ARWA9606043Angle · crackedNR 3 ENGINE TRANSLATING RING UPPER ANGLE CRACKED. REPAIRED IAW DRAWING ARW 015713-1184 FAA FORM 8110 APPROVED.SDR 96UAL900440Prox Sensor · out of adjustLEFT ENGINE THRUST REVERSER UNLOCKED LIGHT ILLUMINATED DURING TAKEOFF ROLL. TAKEOFF ABORTED AT APPROXIMATELY 100 KNOTS. *S/D* THE LOCK PROXIMITY SENSOR WAS OUT OF ADJUSTMENT. THE SENSOR WAS REPLACED, OPERATIONS CHECK NORMAL.SDR DL31J961391Switch Module · intermittentREVERSE UNLOCK ECAM WARNING ACCOMPANIED BY REV (GREEN) AT FL 350, NR 2 ENGINE. FLIGHT DIVERTED TO MIA. NO BUFFET OR BANK EXPERIENCED. ECAM WARN DISAPPEARS AND RECURS A FEW TIMES DURING DIVERSION. LOCKED OUT NR 2 T/R PER MEL 78-30-01. REPLACED RVDT/STOW SWSDR CA960614008Cable · broken(CAN) AIRCRAFT HAD TO REJECT TAKEOFF DUE TO ENGINE NOT REACHING TO POWER BECAUSED OF THROTTLE JAM. THRUST REVERSER CABLE BROKEN RESULTING A FEEDBACK CABLE CAM IN UNLOCK POSITION. CAM REPOSITIONED AND THRUST REVERSER DEACTIVATED AS PER MM AND RELEASED AS PER MESDR USAAF96057T/R Cables · brokenPIT - FLT 1672 - CREW COULD NOT ADVANCE THROTTLES PAST 34 UNITS DURING CLIMB. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MX FOUND THE NR 1 THRUST REVERSER FEEDBACK CABLES FROZEN AND BROKEN. CABLES WERE REPLACED. (M)SDR 96ZZZM1051T/R Cables · brokenPIT - FLT 1672 - CREW COULD NOT ADVANCE THROTTLES PAST 34 UNITS DURING CLIMB. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MX FOUND THE NR 1 THRUST REVERSER FEEDBACK CABLES FROZEN AND BROKEN. CABLES WERE REPLACED. (M)SDR 96ZZZM1017Tr Cables · brokenPIT - FLT 1672 - CREW COULD NOT ADVANCE THROTTLES PAST 34 UNITS DURING CLIMB. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE NR 1 THROTTLE FEEDBACK CABLES FROZEN AND BROKEN. CABLES WERE REPLACED. REFERENCE USAAF96057.SDR 96ZZZX3628Intercostal · crackedTHRUST REVERSER SECONDARY BRACKET LATCH SUPPORT INTERCOSTAL FOUND CRACKED NUMEROUS PLACES. MATERIAL IS .032 INCH 2024T6 ALUMINUM.SDR 96ZZZX3625Intercostal · crackedINSPECTION FOUND RT T/R SECONDARY BRACKET LATCH INTERCOSTAL CRACKED.SDR CA960620006Junction Box · mis wired(CAN) WHILE PERFORMING A ROUTINE PHASE 5 INSPECTION, THE TECHNICIAN FOUND THAT IMPROPER WIRING PROCEDURES WERE FOLLOWED DURING MANUFACTURE OF THE THRUST REVERSER JUNCTION BOX P/N 5538328-16 REF. IPC 78-30-03. IT WAS NOTED THAT SEVERAL WIRES WERE INCORRECTLY ROSDR CA960620011Quadrant Switch · broken wiring(CAN) ON THIS AIRCRAFT AND 4 OTHERS, THROTTLE QUADRANT SWITCHES S153, S161, S154 AND S162 WHICH CAUSE THRUST REVERSER TO STOW OR DEPLOY, HAVE FAILED. CAUSE WAS FOUND TO BE BECAUSE THE SWITCHES ARE MOUNTED ON THE MOVING THROTTLE WHERE THE WIRING IS CONTINUOUSLYSDR 9611291155Tr Unit · malfunctionedDURING TAKEOFF ROLLOUT, THE NR 3 ENGINE REVERSER UNLOCK LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE NR 3 REVERSER AND FOUND IT TO BE NORMAL. DURING REVERSER OPERATION WITH GROUND AIR, REVERSER DEPLSDR AU960696Slider · separated(AUS) ENGINE THRUST REVERSER NO2 OUTBOARD REVERSER HALF LOWER SLIDER SEPARATED FROM THE SLIDER TRACK - TRANSLATING COWL HAD BEEN RECENTLY REMOVED TO CARRY OUT A LOWER BLOCKER DOOR HINGE REPLACEMENT - PERSONEL/MAINTENANCE ERRORSDR ZIAA96014Tr Seq Valve · leakingHUF - DURING CRUISE, SHUT DOWN NR 4 ENGINE DUE TO FIRE WARNING INDICATION. FOUND THRUST REVERSER SEQUENCE VALVE LEAKING AND BLOWING HOT AIR ON THE FIRE DETECTION LOOP. REMOVED AND REPLACED SEQUENCE VALVE. OPERATIONAL CHECK GOOD. (M)SDR CA960514001Rod Assembly · disconnected(CAN) PILOTS REPORTED RT THRUST REVERSER TRANSIT LIGHT SLOW TO EXTINGUISH DURING STOW CYCLE. HAD TO CYCLE A FEW TIMES BEFORE LIGHT WOULD EXTINGUISH. INSPECTION PANELS REMOVED AND FOUND INBOARD LOWER END OF SCREWJACK TRANSMISSION ROD ASSY WAS NOT IN SAFETY ANSDR AU961076Fairing · separated(AUS) NO3 ENGINE THRUST REVERSER TRANSFER DRIVE FAIRING ADRIFT IN FAN EXIT - DAMAGE TO BLOCKER DOORS, OIL FEED LINE AND ONE FUEL VENTDRAINSDR CAL960588Drive Link · brokenMTY - FLT 0705 - THE LEFT ENGINE REVERSE UNLOCK LIGHT ILLUMINATED ON LANDING AT MTY. MAINTENANCE FOUND A LEFT ENGINE THRUST REVERSER DRIVE LINK BROKEN. THE DRIVE LINK REMOVED AND REPLACED. OPERATION CHECKED GOOD PER MM 78-31-5, PAGES 201-207, FIGURE 201. (SDR 96UAL900287Reverser Cowl · delaminatedLARGE AREA OF HEAT AND DELAMINATION DAMAGE ON THE NR 2 ENGINE RIGHT REVERSER COWL. THERE IS ALSO INSULATION DAMAGE. THERE WAS NO FIRE WARNING INDICATION ON THE FLIGHT DECK. UNDER INVESTIGATION. SUPPLEMENTAL DATA UPDATE: DAMAGE CAUSED BY NR 2 PNEUMATIC DUCSDR 96FDEA00848Reverser Half · missingNR 2 THRUST REVERSER UNLOCK LIGHT ILLUMINATED AFTER LANDING AT ISD. FOUND NR 2 LT TRANSLATING SLEEVE MISSING FROM A/C. TRANSLATING SLEEVE WAS FOUND ON RUNWAY AFTER A/C LANDED. REPLACED NR 2 LT ENGINE THRUST REVERSER ASSY, AS PER WORK CARD NR 78T3101 AND 78TSDR CA960604007Thrust Reverser · sheared hyd line(CAN)THRUST REVERSER LH LOWER LATCH RETURN LINE #1 ENGINE SHEARED AT MIDPOINT CAUSING LOSS OF HYDRAULIC FLUID GREEN SYSTEM. AIRCRAFT USED ALTERNATE GEAR EXTENSION AND LANDED SAFELY. LINE SENT TO NRC FOR AN ALYSIS.SDR 96FDEA00791Tr Switch · failedAFTER T/O, ENG NR 1 REVERSER OPERATING LIGHT CAME ON NR 1 ENGINE, SHUTDOWN AS PER PROCEDURE. A/C RELEASED FOR SERV PER MEL 78-2A. CHECKED WIRING HARNESS AT SWITCH FOR CONDITION, FOUND GOOD. CHECKED SW ADJ, WITHIN LIMITS. DURING T/S HAD NR 1 T/R OPS LIGHT GSDR 96ZZZM897Tr Light · broken wireSTL - DURING CLIMB, RIGHT THRUST REVERSER LIGHT ILLUMINATED. REPAIRED WIRING TO RIGHT THRUST REVERSER. OPERATIONAL CHECK NORMAL. (M)SDR COMA9660065Tr Unit · malfunctionedTHE RT ENGINE THRUST REVERSER WILL NOT STOW. THE NOSE COWL ASSY (P/N 22850020-113), THE TORQUE BOX ASSY (P/N 22850200-140) AND THE SLIDER BLOCK ASSY (P/N 22850281-113) HAD EXTENSIVE DAMAGE. THE 10 O'CLOCK POSITION DRIVE ACTUATOR ASSY (P/N 3272570-6) FAILED ASDR ABXA9600523Tr Link · crackedDURING COMPLIANCE OF AD'S 75-14-06, 90-18-03 SB'S 78-36, 78-38, 78-40 AND 78-66, FOUND RIGHT THRUST REVERSER OUTBOARD UPPER DRIVER LINK HAD A CRACK INDICATION. REPLACED RIGHT THRUST REVERSER OUTBOARD UPPER DRIVER LINK IAW DC-9 MM 78-31-5. LINK FOUND TO BE CR
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