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 QXEA2010022200105Structure · damagedC-CHECK - CHAFE DAMAGE FOUND ON RT ENG LOWER TRANSCOWL SLIDER INBD. BLENDED DAMAGED AREA IAW AND WITHIN TOLERANCE OF REO 670-78-34-384. TREATED AND PRIMED IAW SRM 51-21-11-001-001, 51-25-06-001-001. ALL WORK WAS PERFORMED IAW REO 670-78-34-384.Feb 18, 2010 · N612QX · Cndair CL6002C10SDR A6WA201040165Lug · chafedLT TR MAIN TRACK LOWER OTBD LUG CHAFED REO 601R-78-34-2435 CARRIED OUT.Feb 17, 2010 · N430AW · Cndair CL6002B19SDR A6WA201040167Track · chafedLT TR MAIN LOWER INBD TRACK CHAFED, REO 601R-78-34-2435.Feb 17, 2010 · N430AW · Cndair CL6002B19SDR A6WA201040166Lug · chafedLT TR MAIN TRACK INBD LOWER LUG CHAFED REO 601R-78-34-2435 CARRIED OUT.Feb 17, 2010 · N430AW · Cndair CL6002B19SDR Z6WR 001 2010Blade · wornTHE 315A2233-18 V-BLADE ASSEMBLY HAS WORN / GOUGED AREAS MEASURING BETWEEN .000 TO .030 IN DEPTH. THE WORN / GOUGED AREA IS LOCATED ALONG THE 54.0 LENGTH OF THE V-BLADE AND IS COMMON TO THE INNER SURFACE OF THE V-BLADE.Feb 17, 2010 · N27734 · Boeing 737724SDR UALA2010021600600Clamp · brokenNR 2 ENG HOOPTIE BAND CLAMP UPPER PIVOT PIN RETAINER IS BROKEN. REPLACED CLAMP.Feb 15, 2010 · N775UA · Boeing 777222SDR A6WA201040244Lug · chafedRT ENGINE LWR INBD T/R TRACK LUG IS CHAFED. CHAFE BLENDED IAW REO 601R-78-34-2435.Feb 14, 2010 · N430AW · Cndair CL6002B19SDR A6WA201040124Support · chafedRT ENG LOWER OTBD TR TRACK LUG SUPPORT IS CHAFED. CHAFE BLENDED IAW REO 601R-78-34-2435.Feb 14, 2010 · N430AW · Cndair CL6002B19SDR A6WA201040126Support · chafedRT ENG LOWER OTBD TRACK LUG IS CHAFED. CHAFE BLENDED IAW REO 601R-78-34-2435.Feb 14, 2010 · N430AW · Cndair CL6002B19SDR A6WA201040125Support · chafedRT ENG INBD TRACK LUG SUPPORT IS CHAFED. CHAFE BLENDED IAW REO 601R-78-34-2435.Feb 14, 2010 · N430AW · Cndair CL6002B19SDR UALA2010021600601Heat Shield · damagedRIGHT ENGINE COWL HEAT SHIELD MISSING. RT ENG THRUST REVERSER THERMAL INSULATION BLANKET LEFT SIDE DAMAGE SIZE IS 25 INCH BY 25 INCH. REPLACED THRUST REVERSER THERMAL INSULATION BLANKET ASSY.Feb 12, 2010 · N788UA · Boeing 777222SDR SWIA201023679Casting · crackedRIGHT UPPER TRANS COWL CASTING CRACKED. (C CHECK) REPLACED CASTING PER AMM.Feb 8, 2010 · N820SK · Cndair CL6002D24SDR SWIA201023663Casting · crackedRIGHT ENGINE UPPER TRANS COWL INBOARD 'A' CASTING CRACKED. (C CHECK) REPLACED CASTING PER AMM.Feb 8, 2010 · N820SK · Cndair CL6002D24SDR SIMA201004007Structure · crackedDURING THE MAINTENANCE BASE VISIT INSPECTION FOUND THE LATCH DOOR COMING CRACKED ON THE RIGHT TRANS COWLS. PERFORMED AN OPERATIONAL CHECK OF THE RIGHT TRANS COWL. NO DEFECTS NOTED IAW AMM 78-30-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED Feb 8, 2010 · N520DC · Cndair CL6002C10SDR SIMA201004006Fitting · crackedDURING THE MAINTENANCE BASE VISIT INSPECTION FOUND THE OUTBOARD EXTRUSION CRACKED ON THE RIGHT UPPER TRANS COWL. ACCOMPLISHED OPERATIONAL CHECK OF THE RIGHT TRANS COWL IAW AMM 78-30-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.Feb 8, 2010 · N520DC · Cndair CL6002C10SDR SIMA201004005Fitting · crackedDURING THE MAINTENANCE BASE VISIT INSPECTION FOUND THE INBOARD STANDOFF CRACKED ON THE RIGHT UPPER TRANS COWL. ACCOMPLISHED OPERATIONAL CHECK OF THE RIGHT TRANS COWL IAW AMM 78-30-00. THE OPERATIONAL CHECK WAS GOOD.Feb 8, 2010 · N520DC · Cndair CL6002C10SDR SIMA201004004Fitting · crackedDURING THE MAINTENANCE BASE VISIT INSPECTION FOUND THE INBOARD STANDOFF CRACKED ON THE LEFT LOWER TRANS COWL. PERFORMED LEFT TRANS COWL OPERATIONAL CHECKS, NO DEFECTS NOTED IAW AMM 78-30-00. THE AIRCRAFT WAS RETURNED TO SERVICE.Feb 8, 2010 · N520DC · Cndair CL6002C10SDR A6WA201040218Vane · crackedRT ENGINE THRUST REVERSER TOP CASCADE HAS 1 (EA) VANE GOUGED AND 1 (EA) VANE CRACKED. REPAIRED 1 INCH CRACK & 1 GOUGE ON RT ENGINE T/R TOP CASCADE IAW DWG AW 78-30-0711-04.Feb 5, 2010 · N429AW · Cndair CL6002B19SDR ASOA201000158Switch · malfunctionedCLIMBING THROUGH FL220, REV CAUTION ICON ON LT N1 AND L REV UNLOCKED CAUTION CAME ON INTERMEDIATLEY THEN WENT AWAY. ABOUT 10 SEC LATER MSG RETURNED AND STAYED ON. AIRPLANE YAWED TO THE LT AND WE RAN THE QRH PROCEDURE- WHICH LED TO ENG SHUTDOWN. F/A NOTICED YFeb 4, 2010 · N861AS · Cndair CL6002B19SDR REXA201000017Switch · misriggedON CLIMBOUT FROM KCKB, THE LT THRUST REVERSER UNLOCK MESSAGE ILLUMINATED. THE FLIGHT CREW COMPLETED THE QRH AND REQUESTED TO RETURN TO KCKB. AN OTHERWISE NORMAL APPROACH AND LANDING WAS PERFORMED. BOMBARDIER MAINTENANCE FOUND THE THRUST REVERSER STOW SWITCHFeb 4, 2010 · N8733G · Cndair CL6002B19SDR SIMA201003602Thrust Reverser · obstructedON FLIGHT 3353 UPON LANDING AT AMA THE CREW REPORTED, RECEIVED AN ENGINE 1 REVERSE DISAGREE FAIL MESSAGE FOLLOWED BY AN ENGINE 1 UNCOMMANDED SHUTDOWN. DURING AFTER LANDING CHECKLIST, FLAPS RETRACTED TO 0 FOLLOWED BY FLAP FAIL MESSAGE ON EICAS. ON PARKING, FOFeb 3, 2010 · N918AE · Emb EMB145LRSDR HALA2010020200047Bleed Valve · malfunctionedLT HYD TEMP HI EAD DISPLAY. PERFORMED FIM 29-30 TASK 803 FOUND LT T/R ACCUMULATOR BLEED VALVE KNURLED KNOB NOT FULLY CLOSED. CLOSED VALVE PERFORMED REPAIR CONFIRMATION BY OPERATING BOTH HYD SYS 15 MIN ALERT DID NOT SHOW.Feb 2, 2010 · N490HA · Boeing 717200SDR ABXA2010032615Thrust Reverser · crackedRT ENGINE OUTBOARD T/R 2ND CASCADE SECTION FROM BOTTOM CRACKED TOWARD FORWARD SECTION. REMOVED AND REPLACED RT OUTBOARD T/R.Jan 30, 2010 · N783AX · Boeing 767281SDR A6WA201040083Pdu · malfunctionedRT REVERSER UNLOCK MESSAGE CAME ON OUT OF 13000 FT. FOLLOWED QRH. RETURNED TO DEPARTURE. MESSAGE EXTINGUISHED AT SHUTDOWN. "MEL. COMPLIED WITH MX ACTION H OF DEACTIVATION OF RT THRUST REVERSER REF AMM 78-30-00-040-802, REF BLK 2 FOR MEL. R & R RT ENGINE Jan 30, 2010 · N402AW · Cndair CL6002B19SDR UALA2010012800359Structure · delaminatedNR 2 ENG REVERSER UPPER BI-FURCATION IS DELAMINATED. APPROX 300 SQUARE INCHES FWD END GOING AFT (MARKED) ACCOMPLISHED TIME LIMITED BACK SHEET REPAIR IAW MM-78-31-93. REPAIR INSTALLED MEASURES APPROX 280 SQ INCHES. IAW MM PG 803: REPAIR TO BE RE-CHECKED ATJan 28, 2010 · N586UA · Boeing 757222SDR IPXA10558285Duct · chafedINSPECTION TYPE:C3 NR 2 ENGINE OTBD C-DUCT, BIRUCATION DUET INNER LOWER SURFACE IS CHAFED. REPAIRED CRACKED HONEYCOMB PANEL PERFORATED SKIN IAW AMM 78-31-20-8.Jan 27, 2010 · N459UP · Boeing 75724APFSDR MASA2010012500060Pdu · dirtyAIRSHUTTLE 7131 FROM ORD TO ROC ABORTED TAKEOFF AT 20 KTS AND RETURNED TO GATE DUE TO A NR 2 ENG TR UNLOCKED. MX IS AT THE PLANE AND LOOKING TO COMPLY WITH THE MEL. CLEANED AND LUBED PDU.Jan 25, 2010 · N27185 · Cndair CL6002B19SDR DXTA2010012503955Hinge · lack of lubePASSING THROUGH 18,000' AND AN AIRSPEED OF APPOX 260KTS, FELT A SUDDEN JOLT FOLLOWED BY MEDIUM TO HIGH FREQUENCY VIBRATIONS IN THE FUSELAGE AND FLIGHT CONTROLS. AIRPLANE ALSO SEEMED TO WANT TO PITCH NOSE DOWN. LEVELED OFF AND DISENGAGED THE AUTOPILOT AND THEJan 24, 2010 · N695QS · Cessna 560CESSNASDR IPXA10558242Sleeve · chafedINSPECTION TYPE:C2 NR 2 ENGINE OTBD C-DUCT, TRANSLATING SLEEVE INNER AFT LOWER EDGE IS CHAFED, WITH FIBER DAMAGE, FROM AFT EDGE TO 8" FWD REPAIRED TRANSLATING SLEEVE IAW SRM 54-31-01-1A FIG 101, SRM 54-31-01-2R FIG 201, SRM 51-70-17-0G PAR 4.6(1-3)Jan 23, 2010 · N426UP · Boeing 75724APFSDR AALA20100123JFK01Control Valve · defectiveJFK - INFLIGHT ORD-LGA. CREW REPORTED ON APPROACH LEFT ENGINE THROTTLE WAS NOT ABLE TO MOVE OR ADJUST ENGINE POWER SETTING. EMERGENCY DECLARED DIVERTED JFK LANDED WITHOUT INCIDENT. UPON LANDING CREW SHUT DOWN ENGINE. AIRCRAFT REMOVED FROM SERVICE. REPLACEJan 22, 2010 · N9622A · Doug DC983SDR IPXA10558243Sleeve · chafedINSPECTION TYPE:C2 NR 2 ENGINE INBD C-DUCT, TRANSLATING SLEEVE INNER AFT LOWER EDGE IS CHAFED, WITH FIBER DAMAGE, FROM AFT EDGE TO 8" FWD REPAIRED TRANSLATING SLEEVE IAW SRM 54-31-01-1A FIG 101 SRM 54-31-01-2R FIG 201, SRM 51-70-17-0G PAR 4.6 (1-3)Jan 17, 2010 · N426UP · Boeing 75724APFSDR ASOA20100050Pdu · failedR & R LT THRUST REVERSER PDU IAW AMM 78-32-03. OPS CK GOOD, DEFER CLEARED PLACARD REMOVED. (CLOSED)Jan 15, 2010 · N860AS · Cndair CL6002B19SDR ASOA201000050Thrust Reverser · malfunctionedAMBER L REV UNLOCKED MESSAGE AT FL230 DURING CRUISE. PRESSED LT EMERGENCY STOW AND SHUTDOWN ENGINE IAW QRH, DIVERTED. DIVERTED TO DUE TO MX-- EMERGENCY DECLARED -- OPEN (THRUST REVERSER SYSTEMS )Jan 15, 2010 · N860AS · Cndair CL6002B19SDR ZESA2010001Thrust Reverser · bindingAT FL 220, CREW NOTED A BUFFET/VIBRATION IN THE AIRFRAME. IN CHECKING THE CONFIGURATION OF THE ACFT, THE CREW DEPRESSED THE THRUST REVERSER EMERGENCY STOW FOR THE RT SIDE WITH NO CHANGE, THEN WHEN THE LT EMER STOW WAS DEPRESSED, THE VIBRATION EXTINGUISHED. CJan 8, 2010 · N58LQ · Cessna 560XLSDR FDEA201001030004Valve · failedREV 3 PRESS FAULT ON T/O REJECTED T/O AT 60KT. PERFORMED HI-POWER RUN IAW JRH, REV 3 PRESS FAULT APPEARED BEFORE 80 PERCENT. SUSPECT NR 3 PRESS REG SHUTOFF VALVE AT FAULT. SWAPPED NR1 AND NR3 PRESS REG SHUTOFF VALVE FOR T/S PURPOSE AND PERFORMED HI-POWER RUJan 3, 2010 · N606FE · Doug MD11FSDR UALA2009123004065Panel · delaminatedNR 1 ENG OTBD REVERSER UPPER BIFURCATION PANEL HAS DELAMINATION APPROX 265 SQUARE INCHES. REPAIRED NR 1 ENG OTBD REVERSER BIFURCATION PANEL.Dec 29, 2009 · N546UA · Boeing 757222SDR MASA2009121900354Pdu · malfunctionedASH 2727 SBA-PHX - CREW DECLARED AND EMERGENCY LT REVERSER UNLOCK CAUTION. MX REPLACED PDU.Dec 19, 2009 · N17358 · Cndair CL6002B19SDR 2009FA0001063Bushing · crackedPROBLEM FOUND ON THRUST REVERSER REMOVED FROM ACFT. UPON PRELIMINARY INSP AT APPLIED COMPOSITES ENGINEERING (ACE) IT WAS DISCOVERED THAT ONE FWD HINGE BUSHING PN 14G0311-203 WAS CRACKED ACROSS THE SHOULDER AND AROUND THE TRANSITION FROM THE RADIAL TO THE FLANDec 18, 2009 · N827MD · Emb ERJ170100SUSDR A6WA201040168Track · chafedLT TR MAIN LOWER OTBD TRACK CHAFED REO 601R-78-2435 CARRIED OUT.Dec 15, 2009 · N430AW · Cndair CL6002B19SDR C2XA09CL158Thrust Reverser · malfunctionedPVD FLT 2575 THE CREW REPORTED A NR 2 ENGINE THRUST REVERSER DISAGREE MESSAGE ON TAKEOFF. THE TAKEOFF WAS ABORTED. MAINTENANCE INSPECTED AND PLACED THE THRUST REVERSER SYSTEM ON MEL. THE NR 2 THRUST REVERSER WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD.Dec 12, 2009 · N16976 · Emb EMB145LRSDR MASA2009121000123Pdu · malfunctioned*DIVERT* L REV UNLOCK CAUTION IN FLIGHT. PLACED ON MEL. REPLACED THE PDU. OPS CHECK GOOD.Dec 10, 2009 · N17358 · Cndair CL6002B19SDR IXXA090069OActuator · out of adjustDURING CRUISE, THE LT ENG REVERSE AMBER LIGHT REMAINED ON AFTER FWD THRUST SELECTED, THRUST LEVER COULD BE ADVANCED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX ACCOMPLISHED FIM 78-36-00 AND FOUND THE CTR ACTUATOR OUT OF ADJUSTMENT. MX ADJUSTDec 10, 2009 · N748AX · Boeing 767232SDR DXTA2009113003871Switch · malfunctionedON TAKEOFF ROLL, PWR APPROX 80-90 PERCENT, LT THRUST REVERSER ARM AND UNLOCK LIGHT CAME ON. AS WE TAXIED IN, FULL T/R DEPLOYMENT ON LT SIDE; EMER SWITCH STOWED T/R. REENABLED T/R SYS. CYCLED T/R'S AND DUPLICATED MALFUNCTION. GAINED ACCESS TO THROTTLE GUARD. Nov 28, 2009 · N366QS · Cessna 560CESSNASDR 2009FA0000987Bushing · crackedPROBLEM FOUND ON THRUST REVERSERS REMOVED FROM ACFT. UPON PRELIMINARY INSP AT APPLIED COMPOSITES ENGINEERING (ACE) IT WAS DISCOVERED THAT 3 OF THE 4 FWD HINGE BUSHINGS PN 14G0311-203 WERE CRACKED ACROSS THE SHOULDER AND AROUND THE TRANSITION FROM THE RADIAL Nov 24, 2009 · N646RW · Emb ERJ170100SESDR UALA2009111803598Skin · crackedNR 2 ENG OUTBOARD REVERSER SLEEVE UPPER AFT SECTION HAS A CRACK IN SKIN. REMOVED OUTBOARD SLEEVE BLISTER FAIRING, CUTOUT DAMAGE, LAID OUT RIVET PATTERN FOR REPAIR DOUBLERS. NEED TO MANUFACTURE REPAIR DOUBLERS AND FILLERS FOR TWO AREAS OF DAMAGE AND REINSTALNov 16, 2009 · N808UA · Airbus A319131SDR FDEA200911143956Actuator · leakingODOR OF ENG OIL SMOKE IN COCKPIT. RAN CHECKLISTS AND WAS UNABLE TO DETERMINE SOURCE. DIVERTED. FOUND LT ENG THRUST REVERSER ACTUATOR LEAKING ON DUCTS. REPLACED ACTUATOR IAW MM 78-33-14-4 1. RE-ACTIVATED REG AIR VALVE AND RAN ENG AT HIGH PWR FOR APPROX 15Nov 14, 2009 · N572FE · Doug MD11SDR FDEA200911133955Actuator · leakingODOR OF ENG OIL SMOKE IN COCKPIT. RAN CHECKLISTS AND UNABLE TO DETERMINE SOURCE. DIVERTED. RELEASED FOR SERVICE IAW MEL: 36-12-01. CHECKED NR 1, 2 & 3 PACK COALESCER FILTERS. NR 1 FILTER WATER SEPARATOR HAD CONTAMINATION. OPENED NR 1 SYS DUCTS IN CAC & NNov 13, 2009 · N572FE · Doug MD11SDR UIEA201000173Skin · delaminatedNR 4 RH T/R COWL WITH DELAMINATION DAMAGE TO THE OUTER SKIN FROM A PREVIOUS REPAIR, LOCATED AT APPROX 2:00 POSITION. DISPOSITION WAS MADE TO PERFORM A REPAIR BY FILLING THE DAMAGED AREA WITH BMS5-28 POTTING COMPOUND OR EQUIVALENT TO CONTOUR AND APPLY (2) LAYERNov 9, 2009 · N429MC · Boeing 747481SDR HALA2009110900515Duct · damagedSUP - ETOPS SIGNIFICANT SYS - FOUND DAMAGE TO OTBD REV HALF DUCT WALL OF NR2 ENG, TRIANGULAR DENT APPROX 24" AFT OF FWD. DENT MEASURES 2 INCHES X 2 INCHES X2 INCHES X 0.0625 INCHES DEEP. ALSO NUMEROUS SCRATCHES. REPL NR2 ENG OUTER REVERSER HALF IAW AMM 78-31Nov 9, 2009 · N597HA · Boeing 767332SDR HALA2009110900516Duct · dentedOPEN - ETOPS SIGNIFICANT SYS - FOUND DAMAGE TO OTBD REV HALF DUCT WALL OF NR 2 ENG, TRIANGULAR DENT APPROX 24" AFT OF FWD DENT MEASURES 2 INCHES X 2 INCHES X 2 INCHES X 0.0625 INCHES DEEP. ALSO NUMEROUS SCRATCHES. OK TO CONTINUE IAW HALM105 FILE NR R0033.Nov 9, 2009 · N597HA · Boeing 767332
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