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.

SDR RAIA2009010200001Warning System · activatedNR 1 T/R DISAGREE ON T/O. MAINT DEFERRED T/R IAW MEL MX PROCEDURE.Jan 5, 2009 · N809HK · Emb EMB145EPSDR RAIA2009010800004Thrust Reverser · unwanted deployNR 1 THRUST REVERSER DEPLOYED ON TAKEOFF. NR 1 THRUST REVERSER PLACED ON DEFERRAL IAW MEL MX PROCEDURE.Jan 5, 2009 · N809HK · Emb EMB145EPSDR UPS09554376Fitting · gougedINSPECTION TYPE:C2 NR 1 ENGINE O/B T/R INNER SURFACE AFT LWR CORNER FITTING IS GOUGED. REMOVED AND REPLACED FITTING PER RR EM 70-42-28-300-05.Dec 30, 2008 · N461UP · Boeing 75724APFSDR UPS09154312Support Angle · crackedINSPECTION TYPE:1C NR 2 ENG INBOARD T/R SLEEVE LOWER WEDGE SUPPORT ANGLE IS CRACKED JUST NEXT TO SLIDER TRACK. REPAIRED NR 2 INBOARD T/R SLEEVE LOWER WEDGE SUPPORT ANGLE REF EA300-5430- 01-A1591 AND EO C-7830-31801-A.Dec 29, 2008 · N141UP · Airbus A300F4622RSDR UPS09154314Thrust Reverser · crackedINSPECTION TYPE:1C NR 2 ENGINE OUTBOARD T/R DOOR UPPER EDGE JUST OUTBOARD OF FWD SPRING SEAL HAS A CRACK ON UPPER LONGERON OUTER SKIN. REPAIRED NR 2 OUTBOARD T/R DOOR UPPER EDGE REF EA 300-7830-01-A1592 AND EO C-7830-31824-A.Dec 28, 2008 · N141UP · Airbus A300F4622RSDR UPS09154311Support Angle · crackedINSPECTION TYPE:1C NR 2 OUTBOARD T/R SLEEVE LOWER WEDGE SUPPORT ANGLE T-CHORD CRACKED AT BEND RADIUS (LOCATED JUST BELOW SLIDER TRACK). REPAIRED NR 2 OUTBOARD T/R SLEEVE LOWER WEDGE SUPPORT ANGLE REF EA 300-5430-01-A1589 AND EO C-7830-31810.Dec 28, 2008 · N141UP · Airbus A300F4622RSDR COMA2008122450046Thrust Reverser · malfunctionedDURING CLIMB RECEIVED A RIGHT THRUST REVERSER UNLOCK MESSAGE, FLIGHT DIVERTED TO IND. DEFERRED THE RIGHT THRUST REVERSER PER MEL 78-30-01.Dec 24, 2008 · N451CA · Cndair CL6002B19SDR Q2SA758004Thrust Reverser · deployedON CLIMB-OUT FROM ADDIS ABABA, ETHIOPIA (HAAB), AIRCRAFT PERFORMED AN AIR TURN BACK DUE TO INDICATION OF NR 4 ENGINE THRUST REVERSER TRYING TO DEPLOY IN FLIGHT. CREW WAS ALERTED BY THRUST REVERSER VALVE LIGHT AND TRANSIT LIGHT ILLUMINATING. CREW RETURNED TO Dec 21, 2008 · N758SA · Boeing 747281FSDR FDEA200812175190Clamp · failedAFTER TAKEOFF AT 500 FT, FELT A LOUD "THUMP" LIKE A BIRDSTRIKE. THIS WAS FOLLOWED BY AN INDICATION OF NR 3 BLEED CLOSED (VALVE WAS SELECTED OPEN). THIS WAS FOLLOWED BY A "REV 3 PRESS FAULT". T/R WAS 'NOT' UNLOCKED. ALL OTHER ENGINE INDICATIONS WERE NORMAL. Dec 17, 2008 · N550FE · Doug MD1010FSDR FDEA200812165174Frame · chafedNR 1 OTBD T/R AFT FRAME INNER SURFACE HAS CHAFED AREAS FROM CONTACT WITH CORE COWLS. REMOVED AFT CLOSE OUT FRAME IAW SRM 51-40-21, PARA 5 AND 6. FABRICATED AND PART MARKED NEW CLOSE OUT FRAME IAW EA 6-7830-123697. ALODINED 7 PRIMED FRAME IAW SRM 51-21-10 ANDec 16, 2008 · N428FE · Airbus A310203SDR AALA200803112Thrust Reverser · damagedNRT INFLIGHT - CREW REPORTED JOLT AND EICAS NR 1 ENGINE SURGING AND STATUS MESSAGES FOR EEC, PRESSURE REGULATING SHUTOFF VALVES, FIRE LOOP 1 AND 2, AND OVERHEAT ONE AND TWO FAULTS. RETURNED TO NRT AND LANDED WITHOUT INCIDENT. FOUND LT WING LOWER SURFACE IMPADec 14, 2008 · N760AN · Boeing 777223SDR F3LA2008121600726Isolation Valve · crackedENROUTE AT FL330, PILOT REPORTED INDICATION OF HYDRAULIC RESERVOIR LOW LEVEL FOLLOWED BY ENGINE NR 2 PUMP LOW LEVEL AND NOTED THE YELLOW SYSTEM FLUID QUANTITY DEPLETED. MAINTENANCE INSPECTED THE NR 2 ENGINE AND FOUND THE THRUST REVERSER ISOLATION VALVE HYDRAUDec 13, 2008 · N807FR · Airbus A318111SDR FDEA200812095113Warning System · illuminatedNR 2 ENGINE REVERSER UNLOCK ECAM AT ABOUT 60 KTS ON TAKEOFF. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 14 DEC 08. FOUND NR 2 ENGINE LT REVERSER STOW SWITCH FALLING OFF CAM WHILE SHAKING WIRES FOR T/S. DUPLICATED UNLOCK LIGHT. Dec 9, 2008 · N449FE · Airbus A310222SDR FDEA200812085106Sleeve · dentedNR 2 ENGINE LEFT TRANSLATING COWL OUTER SKIN IS DENTED. REPAIRED NR 2 LEFT TRANSLATING SLEEVE/COWL OUTER SKIN BY DRILLING INJECTED HOLES AND INJECTING EA 934 ADHESIVE AND FILLING THE DENT WITH POTTING COMPOUND AND CURING IAW CF6-6 ENGINE MANUAL 78-00-32; REPADec 8, 2008 · N397FE · Doug MD1010FSDR CA081208010Thrust Reverser · malfunctioned(CAN) BOTH THRUST REVERSERS FAILED TO STOW AFTER LANDING. RT T/R FOUND DEPLOYED APPROX 1/2 WAY. LT T/R FOUND DEPLOYED JUST A CRACK FROM STOWED POSITION. ONCE NOSE OLEO SERVICED, RESET T/R STOW USING OPERATIONAL CHECK OF T/R REF:AMM 78-30-00 P 201 TASK 78-30Dec 6, 2008 · Cndair CL600*SDR CA081208011Cowling · delaminated(CAN) ON DESCENT INTO YYC, WITH POWER LEVERS AT IDLE, THE ACFT SHUDDERED MOMENTARILY. THE NR 2 THRUST REVERSER UNLOCK LIGHT ILLUMINATED AND IN-FLIGHT SHUT DOWN OF NR 2 ENGINE WAS CARRIED OUT. THE ACFT LANDED WITHOUT INCIDENT AND AN INSPECTION WAS CARRIED OUTNov 26, 2008SDR MASA2008112000788Switch · out of rigASH FLT 7229 CAE-LEX. EN ROUTE TO ORD CAPTAIN DIVERTED TO LEX DUE TO A RT REV UNLOCK CAUTION MESSAGE. CAPTAIN DECLARED EMERGENCY. MX RE-RIGGED STOW MICRO SWITCHES.Nov 24, 2008 · N593ML · Cndair CL6002B19SDR DXTA200811173362Pivot · lack of lubeON LANDING ROLL RT THRUST REVERSER UNLOCKED BUT WOULD NOT DEPLOY, TRIED AGAIN ON TAXI & NO DEPLOY. ON THE THRUST REVERSER CHECK PRE-FLT, DEPLOYED. ACTUATED THRUST REVERSERS SEVERAL TIMES. THRUST REVERSER DEPLOYED & LIGHT ILLUMINATED. INSPECTED THRUST REVERSERNov 17, 2008 · N367QS · Cessna 560CESSNASDR REX2008F00059Warning Message · false activationDURING CLIMB FROM KDTW THE R REV UNLOCKED MSG ILLUMINATED. THE FLIGHT CREW PERFORMED THE QRH AND DECLARED AN EMERGENCY. THE ACFT WAS ROUTED BACK TO KDTW WHERE AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WAS MADE. MX INSPECTED THE ACFT AND DEFERRED THE RT TNov 15, 2008 · N8432A · Cndair CL6002B19SDR ASAA0893947Bracket · crackedNR 2 ENG OUTBOARD TR HEAT SHIELD BRACKET BROKEN. REMOVED AND REPLACED BRACKET.Nov 15, 2008 · N302AS · Boeing 737990SDR SWIA200820657Channel · crackedDURING C-CHECK, LEFT LOWER TRANSCOWL 'U' CHANNEL CRACKED. REPAIRED PER REO.Nov 14, 2008 · N728SK · Cndair CL6002C10SDR UPS08M53931Web · crackedINSPECTION TYPE:1C NR 2 ENGINE RT T/R LOWER FWD WEB FOUND CRACKED AND 2 EA FASTENERS BROKEN AT 5 O'CLOCK POSITION. STOP DRILLED CRACK, FABRICATED, AND INSTALLED DOUBLER IAW CF6-80C2 CMM 78-32-02, REPAIR 24.Nov 14, 2008 · N254UP · Doug MD11FSDR UPS08153922Panel · crackedINSPECTION TYPE:C DURING MAINTENANCE CHECK INSP FOUND NR 1 ENGINE RT T/R INNER BARREL PANEL HAD A 0.4 INCH CRACK AT UPPER FORWARD AREA. CUT OUT AND REPAIRED DAMAGED AREA PER UPS EO A300-7830-31176-A AND SAA EA 300-7830-01-A1556.Nov 7, 2008 · N142UP · Airbus A300F4622RSDR 08FDEA04615Structure · crackedNR 2 ENGINE INBD T/R, CORE COWL SECTION HAS A CRACK AT THE AFT UPPER SECTION ABOVE THE LOCK HANDLE. MATERIAL ID PER P/W CMM 78-32-34, 0.050, PO 607468.1. HEAT TREAT IAW TPS 1003; REV "A" (HT102408.2). STOP DRILL THE CRACK TO 0.0625 PER P/W CMM 78-32-34. Oct 29, 2008 · N722FD · Airbus A300B4622RSDR UPS08M53983Web · gougedINSPECTION TYPE:1C NR 2 ENGINE RT T/R CENTER FWD WEB FOUND WITH GOUGE AT 3 O`CLOCK POSITION. GOUGE FOUND OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS EO MD11-7830-31193-A AND CF6-80C2 CMM 78-32-02 REPAIR 24.Oct 26, 2008 · N254UP · Doug MD11FSDR ASOA200801403Actuator · malfunctionedIN FLIGHT RETURN, RT THRUST REV UNLOCK MSG AT 22000FT, UNCOMMANDED YAW. RT ENGINE SHUTDOWN IN FLIGHT. EMERGENCY DECLARED. A/C RETURNED TO ATL AFTER T/O. REMOVED AND REPLACED BALL SCREW ACTUATOR IAW AMM 78-3201, OPS CHECK GOOD. CLEARED, PLACARD REMOVED.Oct 26, 2008 · N835AS · Cndair CL6002B19SDR UPS08153756Shutoff Valve · malfunctionedINSPECTION TYPE:N/A ATB - NR 1 ENG REVERSER UNLOCK LIGHT ILLUMINATED. REMOVED & REPLACED THRUST REVERSER PRSOV FOR TSM 78-31-40 BLOCK 22 PER AMM 78-31-05-04. PERFORMED OPS CHECK PER AMM 78-32-11-05. NR 1 ENG REVERSER SYSTEM HAS NO DEFECTS NOTED.Oct 25, 2008 · N137UP · Airbus A300F4622RSDR 08FDEA04543Frame · crackedNR 1 ENG INBD T/R FWD FLANGE FOR MOUNTING RING LATCH ASSY HAS 2 INCH CRACK AT 12 O'CLOCK POS REMOVED CRACK AND REPAIRED NR 1 ENG INBD T/R FWD FLANGE IAW FEDEX EA 6-7830-124133, RELEASE DATE 8 OCTOBER, 2008.Oct 25, 2008 · N668FE · Airbus A300F4605RSDR 08FDEA04541Frame · crackedNR 1 ENG OTBD T/R FWD FLANGE FOR MOUNTING RING LATCH ASSY HAS 2.25 IN CRACK AT 12 O'CLOCK POS REMOVED CRACK AND REPAIRED NR 1 OTBD T/R FWD FLANGE IAW FEDEX EA 6-7830-124134, RELEASE DATE 8 OCTOBER, 2008.Oct 25, 2008 · N668FE · Airbus A300F4605RSDR 08FDEA04484Frame · crackedNR 2 ENG OTBD T/R FWD FLANGE FOR MOUNTING RING LATCH ASSY HAS 2.750 INCH CRACK AT 12 O'CLOCK POSITION. REPAIRED CRACK ON NR 2 OTBD T/R FLANGE IAW FEDEX EA 6-7830-124135, RELEASE DATE 8 OCTOBER, 2008.Oct 22, 2008 · N668FE · Airbus A300F4605RSDR 08FDEA04442Bracket · brokenNR 1 ENGINE INBD T/R UPPER FWD STOP BRACKET IS BROKEN. REMOVED BUMPER & BRACKET IAW CF-6 ENGINE MANUAL 78-32-03; PG 409; 405. LOCATED & DRILLED UP BUMPER P/N 3111M84P001A & P/N 3110M30P001A IAW ENGINE MANUAL 78- 32-03; FIG 405; PG 409. INSTALLED BUMPEOct 20, 2008 · N390FE · Doug MD1010FSDR 08FDEA04418Panel · crackedNR 3 ENGINE RIGHT T/R UPPER HINGE CLOSE OUT PANEL IS CRACKED AT THE HINGE RELIEF. REPLACED DAMAGED HINGE ACCESS PANEL WITH A NEW PANEL IAW SRM 51-31-01.Oct 17, 2008 · N390FE · Doug MD1010FSDR 08FDEA04349Frame · crackedNR 2 ENG INBD THRUST REVERSER HAS A CRACK .225 INCH LONG ON UPPER FWD END FRAME ROUTED CRACK ON NR 2 ENG INBD T/R TORQUE BOX FWD FRAME AND REPAIRED IAW FEDEX EA 6-7830-124136, RELEASE DATE 8 OCTOBER, 2008.Oct 15, 2008 · N668FE · Airbus A300F4605RSDR U2R2008F00012Fitting · corrodedDURING C-CHECK FOUND NR 1, 2, 3, 4 ENGINE THRUST REVERSER TRANSLATING COWL RAIL FITTINGS CORRODED. (K)Oct 13, 2008 · N872SJ · Doug DC871FSDR CA081016008Switch · inoperative(CAN) ON CLIMB OUT, NR 3 ENGINE THRUST REVERSER OPERATING LIGHT ILLUMINATED THROUGH 5000 FT. THE ACFT RETURNED TO THE AIRPORT. THE NR3 ENG THRUST REVERSER WAS DEACTIVATED AND MEL APPLIED. UPON REACHING THE DESTINATION, THE NR3 ENGINE THRUST REVERSER SWITCH WASOct 3, 2008 · Boeing 7272Q6SDR UPS08553515Flange · crackedINSPECTION TYPE:C2 DURING INSPECTION, FOUND NR 2 ENGINE OUTBOARD T/R, NR 11 CASCADE VANE SEGMENT, AND NR 2 ENGINE INBOARD T/R, NR 2 CASCADE VANE SEGMENT TO BE CRACKED ON THE FWD MOUNTING FLANGE, UPPER EDGE. REMOVED & REPLACED NR 2 ENGINE OUTBOARD T/R, NR 11 CSep 28, 2008 · N425UP · Boeing 75724APFSDR 08FDEA04074Actuator · brokenFOUND NR 1 LT T/R DAMAGED. FOUND LT LWR SCREWJACK BROKE OFF AND DAMAGED THE TRANSLATING COWL, DAMAGED PARTS FOUND AT RUNWAY TOUCH DOWN AREA. VISUALLY INSPECTED LT WING, FLAP, AFT FUSELAGE, STAB SURFACE AND NO DAMAGE FOUND. MANUAL DEPLOY AND STOW NR 1 RT REVSep 27, 2008 · N603FE · Doug MD11FSDR 2008UALA05878Skin · delaminatedNR 2 ENGINE LT INBOARD REVERSER UPPER BIFURCATION PANEL IS DELAMINATED INNER SKIN ABOUT 60 PERCENT OF PANEL LENGTH FROM EDGE TO EDGE. REPLACED REVERSER HALF.Sep 24, 2008 · N540UA · Boeing 757222SDR 2008UALA05877Skin · delaminatedNR 2 ENGINE RT OUTBOARD REVERSER UPPER BIFURCATION PANEL INNER SKIN DELAMINATED FROM FWD END TO AFT END EDGE TO EDGE. REPLACED REVERSER HALF.Sep 24, 2008 · N540UA · Boeing 757222SDR CHQA200800185Control Panel · faultedFLIGHT 5601 IAH TO JAX. DURING FLIGHT THE CREW RECEIVED AN E2 REV ICON INTERMITTENTLY. THE REVERSER DID NOT DEPLOY. THE FLIGHT LANDED WITHOUT INCIDENT. THE REVERSER WAS PLACED ON MEL AND THE ACFT WAS RELEASED BACK TO SERVICE. THE MEL WAS CLEARED ON THE 22Sep 21, 2008 · N701BR · Cndair CL6002B19SDR FDEA200809163906Relay · malfunctionedL REV AMBER LIGHT ON RAN QRH NO YAW OR ADVERSE CONDITIONS. ACFT RELEASED FOR SERVICE PER MEL/CDL: 78-36-01 CATEGORY: C EXPIRATION: 26SEP08 MEL 78-36-01: LEFT ENGINE REVERSER UNLOCK INDICATION INOP. REVERSER DEACTIVATED IN FORWARD THRUST POSITION. "A/C CAT Sep 16, 2008 · N903FD · Boeing 7572B7SDR 08FDEA03906Thrust Reverser · malfunctionedL REV AMBER LIGHT ON RAN QRH NO YAW OR ADVERSE CONDITIONS. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-36-01 CATEGORY: C EXPIRATION: 26SEP08 MEL 78-36-01: LEFT ENGINE REVERSER UNLOCK INDICATION INOP. REVERSER DEACTIVATED IN FORWARD THRUST POSITION." "A/C CAT ASep 16, 2008 · N903FD · Boeing 7572B7SDR 08FDEA03640Skin · gougedNR 3 ENGINE INBD THRUST REVERSER OUTER SKIN IS GOUGED. 2 SPOTS CHECKED LIMITS & FOUND 1 DENT WITHIN LIMITS AND 1 OUT OF LIMITS IAW MM 78-32-01. REMOVED THE DAMAGED AREA. FABRICATED FILLER, BONDED FILLER. CURED & SANDED FLUSH IAW MM 78-32-01. CLEANED PRIMEAug 29, 2008 · N550FE · Doug MD1010FSDR RAIA00808027Thrust Reverser · malfunctionedFLT NR 5558 BNA DURING CRUISE CREW RECEIVED A NR 2 T/R MESSAGE ON THE EICAS. MX DEFERRED THE NR 2 T/R SYSTEM AS PER THE MEL PROCEDURES.Aug 26, 2008 · N816HK · Emb EMB145LRSDR 08FDEA03556Web · crackedNR 1 ENGINE OUTBD T/R FWD UPPER WEB IS CRACKED. FABBED DOUBLER IAW A300-600 MRA CMM 78-32-02. MATERIAL ID 2024-T3, 0.063. LOCATED HOLES IAW A300-600 MRA CMM 78-32-02. ALODINED, PRIMED AND INSTALLED DOUBLER IAW A30-600 MRA CMM 78-32-02. MATERIAL PO NR 614Aug 22, 2008 · N650FE · Airbus A300F4605RSDR 08FDEA03555Web · crackedNR 1 ENGINE INBD T/R FWD UPPER WEB IS CRACKED. STOP DRILLED CRACK; NDT'D AREA FOR CRACK PROPAGATION AT THE CRACK END IAW A300 NTM 51-90-00 PT 9. FABBED A NEW DOUBLER IAW MRA CMM 78-32-01. TREATED DOUBLER AND AREA IAW A30-600 SRM 51-1-23 AND MRA CMM 78-32-01Aug 22, 2008 · N650FE · Airbus A300F4605RSDR MAS2008F00062Thrust Reverser · damagedDURING TRANSIT CHECK WAS DETECTED THE OUTBOARD REVERSER OF THE RT ENGINE WITH EXTENDED DAMAGE ON FAN DUCT INNER WALL WITH MATERIAL MISSING OF 70 X 60 INCH BY IMPACT OF THE BOROSCOPE L PLUG, THE ACFT WAS SENT TO HANGAR FOR REVERSER REPLACEMENT WHICH WILL BE SENAug 21, 2008 · N745AM · Boeing 7772Q8SDR REX2008F00030Unknown · unknownAT LEVEL CRUISE FROM KTYS TO KMSP, THE RT THRUST REVERSER DEPLOYED MASTER CAUTION ILLUMINATED. THERE WERE NO UNUSUAL ACFT FLIGHT CHARACTERISTICS NOTED. FLIGHT CREW PERFORMED THE QRH WHICH REQUIRED LANDING AT NEAREST SUITABLE AIRPORT. THE FLIGHT CREW DECLAREAug 11, 2008 · N841AY · Cndair CL6002B19SDR AALA200801995Rvdt · separatedJFK INFLIGHT T1892/29JUL. ON ROLL OUT LARGE SECTION OF NR 2 THRUST REVERSER DEPARTED ACFT. REPLACED NR 2 OUTBOARD REVERSER. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)Jul 29, 2008 · N77080 · Airbus A300B4605RSDR 08FDEA03040Door · damagedNR 2 ENGINE INBD REVERSER LOWER DOOR FLANGE IS DAMAGED. EVALUATED 6 WORN AREAS. 2 HAD MATERIAL LOSS OF .005 AND 2 EA HAD MATERIAL LOSS OF 0.010. THESE 4 AREAS ARE WITHIN LIMITS REF MRA CMM 78-32-02. 1 AREA HAD A MATERIAL LOSS OF 0.045 & 1 AREA HAD 100% MATJul 24, 2008 · N664FE · Airbus A300F4605R
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