JASC 7830

Service difficulty reports · 5,917

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 CA151223003Tube · broken(CAN) ENGINE NR 2 THROTTLE JAMMED DUE TO A RUPTURE THRUST REVERSER AIR TUBE. THE SAME TUBE WAS INSTALLED ON SEPT 02, 2015 IN THE EXACT LOCATION FOR THE SAME REASON.Dec 21, 2015 · Airbus A310SDR ASOA20151221208Warning Message · activatedREVERSER ICON AND REVERSER UNLOCKED IN FLIGHT.Dec 21, 2015 · N877AS · Cndair CL6002B19SDR AALA201512249001Acoustic Liner · damagedAIRCRAFT WAS GNDED. SHORTLY FOLLOWING TAKEOFF, CREW HEARD A NON-SPECIFIC THUD. POSSIBLE BIRD STRIKE, FLIGHT CONTINUED TO DESTINATION. CFR WAS REQUESTED AS A PRECAUTIONS. AN EMER WAS NOT DECLARED. FOUND THE RT OTBD ENG THRUST REVERSER C DUCT ACOUSTIC LINERDec 20, 2015 · N838AW · Airbus A319132SDR CA151217007Rod End · sheared(CAN) CREW TAXIED OUT FROM THE RAMP AND PERFORMED PREFLIGHT CHECKLIST, CHECKING THE THRUST REVERSER SYS. THE THRUST REVERSER WAS DEPLOYED AND THE RT UPPER PIVOT DOOR ACTUATOR FAILED, FRACTURED. THE DOOR OVERTRAVELED AND AS A RESULT CAUSED DAMAGE TO THE REVERDec 16, 2015 · Bombdr BD1001A10SDR REXA2015121601235Torque Box · crackedNUMBER 1 ENG THRUST REVERSER TORQUE BOX TE IS CRACKED AT THE 5:30 POSITION. REPAIRED CRACK TO NR 1 ENG THRUST REVERSER TORQUE BOX AT THE 5:30 POSITION IAW REO 601R-78-30-2616.Dec 16, 2015 · N8940E · Cndair CL6002B19SDR REXA2015121601234Torque Box · crackedNUMBER 1 ENG THRUST REVERSER TORQUE BOX TE IS CRACKED AT 6:30 POSITION. REPAIRED CRACK TO NR 1 ENG THRUST REVERSER TORQUE BOX AT THE 6:30 POSITION IAW REO 601R-78-30-2616.Dec 16, 2015 · N8940E · Cndair CL6002B19SDR Z6WR20151216009Panel · burnedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2102-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 45B, REVEALS 8 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION CT -174 BONDED PANEL ASSEMBLDec 16, 2015 · Boeing 737800*SDR Z6WR20151216008Panel · burnedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2101-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 40B, REVEALS 9 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION CT -174 BONDED PANEL ASSEMBLDec 16, 2015 · Boeing 737800*SDR Z6WR20151216007Panel · burnedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2102-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 45B, REVEALS 9 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION CT -174 BONDED PANEL ASSEMBLDec 16, 2015 · Boeing 737800*SDR Z6WR20151216006Panel · burnedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2101-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 40B, REVEALS 11 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION CT -174 BONDED PANEL ASSEMBDec 16, 2015 · Boeing 737800*SDR CA151208008Pdu · malfunctioned(CAN) AS REPORTED BY PILOT IN COMMAND IN INCIDENT REPORT DURING TAKEOFF ROLL, AT APPROXIMATELY 100 KTS, THE ATS DISENGAGED IMMEDIATELY FOLLOWED BY RT THRUST REVERSER UNLOCKED AMBER MESSAGE AND UNLOCK PBA AMBER. NO EVIDENCE OF YAW OR ACTUAL THRUST REVERSER DEPDec 6, 2015SDR SIMA20151203003Slider · damagedPROXIMITY SYS FAULT 1 STATUS MSG DISPLAYED SHORTLY AFTER TAKEOFF. PERFORMED PERMANENT REPAIR TO UPPER RT THRUST REVERSER LATCH BEAM SLIDER IAW ERS-CR-78DF-108R1 PART B. ALL MDC INDICATIONS NORMAL FUNCTIONAL CHECK GOOD.Dec 3, 2015 · N528EG · Cndair CL6002C10SDR CALA2015111894843Actuator · leakingAFTER TAKEOFF, BURNING ELEC PLASTIC SMELL. DISSIPATED AFTER 25 MIN. CREW COMMENTED, LIKE OIL SMELL. FOUND NR 2 ENG AFT LINEAR HYD ACTUATOR LEAKING ON ENG DUCTING. REPLACED ORIFICE VLV O RING IAW AMM MT78-01. LEAKS CHECKED GOOD. ALSO REPLACED BOTH RECIRCUNov 18, 2015 · N435UA · Airbus A320232SDR CA151111003Beam · chafed(CAN) L/H LOWER TRANS COWL AFT END OF HINGE BEAM IS CHAFED. THIS CHAFE WAS CAUSED BY THE NYLON BLOCK THAT IS RIVETED ON THE AFT END OF THE HINGE LINE FAIRING. THIS WAS CAUSED BY THE FAILURE OF THE TRANS COWL`S AFT HINGE ATTACH BOLT AND BEARING ASSY AND ALONG WNov 10, 2015 · Cndair CL6002D24SDR DALA2015111107004Line · leakingON DESCENT, FUMES, LIGHT SMOKE AND MIST REPORTED BY F/A IN AFT CABIN AREA. MAINTENANCE FOUND LT THRUST REVERSER STOW LINE LEAKING. REPAIRED LINE IAW AMM. OPERATION AND LEAK CHECKS OK.Nov 10, 2015 · N926DH · Doug MD9030SDR UIEA2015110900619Doubler · crackedINBOARD THRUST REVERSER ON NR 2 ENG HAD CRACKED DOUBLER. REPLACED DOUBLER IAW 47177REA02.Nov 6, 2015 · N657GT · Boeing 767281SDR V0XD20151117331Bracket · crackedRIGHT UPPER THRUST REVERSER, INBD, STANDOFF, WEDGE BRACKET IS CRACKED. R & R RT UPPER THRUST REVERSER INBD WEDGE BRACKET, PN CN624-2082-201, IAW SRM 51-42-13, 51-42-24 & 51-40-11.Oct 28, 2015 · N162GJ · Cndair CL6002C10SDR V0XD20151028229Bracket · crackedLEFT LOWER THRUST REVERSER INBD STANDOFF WEDGE BRACKET CRACKED. R & R DAMAGED WEDGE BRACKET. REPLACED WITH NEW BRACKET IAW SRM 51-42-24, 51-42-13 & 51-40-11.Oct 26, 2015 · N162GJ · Cndair CL6002C10SDR DALA1615293703Skin · puncturedNR 2 ENGINE, EXHAUST SECTION, LT TRANSLATING SLEEVE, OUTER SKIN, NAC STA 200, PUNCTURE 540527-14, LOG 7299788.Oct 21, 2015 · N373DA · Boeing 737832SDR V0XD20151020223Stand Off · crackedLEFT UPPER THRUST REVERSER HAS TWO CRACKED WEDGE BRACKETS, STANDOFFS. R & R TWO LT UPPER THRUST REVERSER WEDGE BRACKETS, STANDOFFS, PN:CN624-2082-201, IAW SRM 51-42-24, 51-42-13 & 51-40-11.Oct 20, 2015 · N162GJ · Cndair CL6002C10SDR V0XD20151020222Stand Off · crackedRIGHT UPPER THRUST REVERSER WEDGE BRACKET IS CRACKED. R & R RT UPPER THRUST REVERSER WEDGE BRACKET STANDOFF, PN CN624-2082-201, IAW SRM 51-42-24, 51-42-13 & 51-40-11.Oct 20, 2015 · N162GJ · Cndair CL6002C10SDR IPXA2015101894896Louver · detachedFOUND NR 2 ENGINE LEFT T/R LOUVER HAS DEPARTED ACFT AND CAUSED COMPOSITE AND S/M DAMAGE TO LT T/R. REPAIRED NR 2 ENGINE LT T/R INNER BARREL IAW EO 7830-59016A, PARA 6A. STEPS 1-3. C/W STEPS 4 AND 5 REF EO 7830-59016B. PERMANENT REPAIR COMPLETED IAW EO 7830-Oct 17, 2015 · N270UP · Doug MD11FSDR FDEA201510153230Door · missingDURING POST FLIGHT WALK AROUND, FOUND THE NR 1 OTBD THRUST REVERSER BLOCKER DOOR MISSING & ATTACH STRUCTURE BROKEN. ALSO TRANS COWL DAMAGED FROM DOOR. INSTALLED NR 1 ENG LT OTBD TRANSLATING COWL IAW M 78 3116 41. THE 3 LOWER BLOCKER DOORS ARE INSTALLED UP Oct 15, 2015 · N616FE · Doug MD11FSDR SIMA20151012004Stand Off · crackedLEFT ENG, UPPER TRANS COWL, INBD STANDOFF ANGLE IS CRACKED, APPROX .500 INCHES. R & R STANDOFF ANGLE IAW SRM CHAPTERS 51-42-20, 51-42-28 & ETN-CR-54-015R1.Oct 12, 2015 · N502AE · Cndair CL6002C10SDR SIMA20151012005Stand Off · crackedLEFT ENG, LOWER TRANS COWL, INBD STANDOFF ANGLE IS CRACKED, APPROX .500 INCHES. R & R LT LOWER TRANS COWL STANDOFF IAW SRM 51-42-06 & ETN CR-54-015R1.Oct 12, 2015 · N502AE · Cndair CL6002C10SDR SIMA20151012003Stand Off · crackedRIGHT ENG, LOWER TRANS COWL, INBD STANDOFF ANGLE IS CRACKED, APPROX .500 INCHES. REPLACED RT ENG, UPPER TRANS COWL, INBD STANDOFF IAW ETN-CR-54-015R1.Oct 12, 2015 · N502AE · Cndair CL6002C10SDR A6WA201543121Torque Box · crackedRIGHT ENG TORQUE BOX CRACKED AT 8 O CLOCK AM PANEL MOUNT. REPAIRED RT ENG TORQUE BOX IAW REO 601R-78-30-2553 REV A DATED 26 MAY 2004.Oct 9, 2015 · N425AW · Cndair CL6002B19SDR V0XD20150929200Baffle · crackedLEFT UPPER THRUST REVERSER, CTR BAFFLE IS CRACKED. R & R LT UPPER THRUST REVERSER CTR BAFFLE PN:CN624-2057-201 IAW SRM 51-42-06.Sep 29, 2015 · N161GJ · Cndair CL6002C10SDR CA150930003Cdu · cracked(CAN) CDU HOUSING CRACKED DURING TESTING OF THRUST REVERSER. OPERATED OK FOR 1 CYCLE AND THEN CRACKED AND SEPARATED ON CYCLE 2.Sep 25, 2015 · Airbus A310300SDR FDEA201509172894Switch · failedDURING TAKEOFF ROLL, RECEIVED A MOMENTARY NR 2 THRUST REVERSER UNLOCKED ALERT & INSTRUMENT CLUSTER TOP LIGHT. LIGHT EXTINGUISHED & TAKEOFF WAS CONTINUED. AFTER TAKEOFF & WHEELS UP, THE ALERT CAME BACK ON. NO ADVERSE CONTROL WAS NOTICED. COMPLIED WITH ECAM.Sep 17, 2015 · N810FD · Airbus A310324SDR IPXA2015091893677Ring · chafedINSPECTION TYPE:C, DURING MAJOR MAINTENANCE VISIT 6779 FOUND CHAFING - POS 1 ENGINE RT T/R CASCADE AFT SUPPORT RING UPPER, NEAR AGB ACTUATOR CHAFING MARK TRANSFERRED TO EGAT NRC DCU05038 AND ACCOMPLISHED EO B767-7830-14712-N AND B767-7830-52256-B. REPLACED DASep 17, 2015 · N325UP · Boeing 76734AFSDR IPXA2015091893676Frame · crackedINSPECTION TYPE:C, DURING MAJOR MAINTENANCE VISIT NR 6779, FOUND CRACK POS 1 ENGINE LT T/R INNER FAN AIR DUCT SUPPORT FRAME CRACK TRANSFERRED TO EGAT NRC DCU05021 AND REPLACED DAMAGED PARTS WITH NEW PARTS IAW EO B767-7830-14712-N AND B767-7830-52256-B.Sep 17, 2015 · N325UP · Boeing 76734AFSDR IPXA2015092493884Barrel · gougedNR 1 ENGINE OTBD THRUST REVERSER INNER BARREL APPROXIMATELY LOCATION AROUND NR 1 THRU NR 3 BLOCKER DOOR FROM THE TOP HAS A GOUGE WORN INTO IT REPAIRED AND EVALUATED AREA IAW REO G19190, REV A AND SREO M-7830-25334-G.Sep 7, 2015 · N139UP · Airbus A300F4622RSDR FDEA201509012732Hinge Fitting · chafedNUMBER 1 NAC, RT AFT T/R HINGE FITTING CHAFFED. COMPLIED WITH EA F-5400-T0319272. FITTING NR 1 PYLON T/R COWL HINGE NAC, STATION 144.00 INBD SIDE, REPAIR. MAJOR REPAIR.Sep 1, 2015 · N787FD · Boeing 757222SDR AALA20150901005Sensor · intermittentDURING CRUISE, THE LT ENG THRUST REVERSER DEPLOY LIGHT ILLUMINATED INTERMITTENTLY. EMERGENCY DECLARED, DIVERTED, AND LANDING UNEVENTFUL. R & R LT ENGINE SENSOR S436. OPS CHECKED NORMAL IAW AMM 78-30-00.Aug 31, 2015 · N687AA · Boeing 757223SDR AALA201509049010Thrust Reverser · defectiveFLIGHT 647 DEPARTED & AT 15000 FT THEY GOT AN ENG ONE OVER SPEED FAULT & THE ENG BEGAN OSCILLATING ON ITS OWN. THE ENG WAS BROUGHT BACK TO IDLE & THE ACFT RETURNED FOR MX. AN EMER WAS DECLARED & THE ACFT LANDED WITHOUT INCIDENT. REPLACED THE NR 1 ENG RT TRAug 29, 2015 · N673AW · Airbus A320232SDR IPXA2015091793648Pan · gougedINSPECTION TYPE:C 1, ENGINE OTBD T/R INTERIOR SIDE METAL PAN AFT SIDE GOUGED. R & R NR 1 ENGINE OTBD T/R INTERIOR SIDE METAL PAN, PN: LJ75051-43, BATCH 0002845422 IAW SRM 51-40-05-0G, AND SRM 51-40-02-0G.Aug 28, 2015 · N449UP · Boeing 75724APFSDR Z6WR20150828005Panel · burnedRECEIVED POST AIRWORTHINESS DIRECTIVE 2012-05-02 SERVICE BULLETIN 737-78-1079, REVISION 3 THRUST REVERSER PN 315A2295-699 78-31-40, FIGURE 1, ITEM 3G. UPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2101-165 BONDEDAug 27, 2015 · Boeing 737800*SDR Z6WR20150828004Panel · burnedRECEIVED POST AIRWORTHINESS DIRECTIVE 2012-05-02 SERVICE BULLETIN 737-78-1079, REVISION 3 THRUST REVERSER PN 315A2295-700 78-31-40 FIGURE 1 ITEM 7E. UPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2102-165 BONDED PAug 25, 2015 · Boeing 737800*SDR Z6WR20150828003Panel · burnedRECEIVED POST AIRWORTHINESS DIRECTIVE 2012-05-02 SERVICE BULLETIN 737-78-1079 REVISION 3 THRUST REVERSER PN 315A2295-702 78-31-40 FIGURE 1 ITEM 17F. UPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2102-165 BONDED PAug 25, 2015 · Boeing 737800*SDR CALA2015082700701Isolation Valve · failedLEFT ISOLATION VLV STATUS MSG CAME ON AFTER TAKEOFF. ACCOMPLISHED QRH & AIR RETURN. PLACED NR 1 THRUST REVERSER ON MEL, COMPLIED WITH DDP. AC OK TO CONTINUE.Aug 25, 2015 · N14115 · Boeing 757224SDR AALA201508249008Relay · faultyFLIGHT 633 EN-ROUTE, DURING CLIMB, CREW RECEIVED AN R REV ISLN VAL STATUS MSG. THE FLIGHT DECLARED AN EMER & RETURNED TO FIELD. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. METERED THROUGH THRUST REVERSER PRESS SWITCH S331, NO CONTINUITY & SWITCH CHECKED NORAug 22, 2015 · N902AW · Boeing 7572S7SDR UIEA2015081900436Liner · missingLEFT ENG OTBD THRUST REVERSER, INTERIOR LINER MISSING AT 10 O CLOCK POSITION. IAW EO 6778A019 COMPLIED WITH PART 1 INTERIM REPAIR. PART 2 DVI REQUIRED EVERY 5 FC. PART 3 PERMANENT REPAIR DUE AT NEXT A CHECK. PLACED ON NON-MEL 59424.Aug 19, 2015 · N641GT · Boeing 76738ESDR SWIA201541395Switch · out of adjustWHILE CLIMBING THRU FL 280, RECEIVED A LT THRUST REVERSER UNLOCK CAUTION MESSAGE ASSOCIATED WITH LIGHT BUFFETING. DIVERTED. ADJUSTED THE STOW AND THROTTLE LOCK OUT SWITCHES ON THE LT ENGINE THRUST REVERSER IAW AMM.Aug 18, 2015 · N495CA · Cndair CL6002B19SDR CALA2015081400665Cowling · damagedFOUND NR 2 ENG OTBD THRUST REVERSER COWL DAMAGED. RT OTBD THRUST REVERSER C DUCT HAD BURN THROUGH HOLE DUE TO BORESCOPE PLUG DISLODGED. REPLACED NR 2 ENG OTBD THRUST REVERSER ASSEMBLY WITH BORROWED SERVICEABLE UNIT IAW AMM TASK 78-31-01-400-801-G-00. BORESAug 14, 2015 · N77006 · Boeing 777224SDR AALA201508119011Hinge Fitting · wornNUMBER 1 ENG INBD THRUST REVERSER AFT HINGE BEARING LOOSE & ROTATES IN THE HINGE FITTING. REPLACED HINGE FITTING IAW AMM 54-57-17-400-003-A.Aug 10, 2015 · N122US · Airbus A320214SDR AALA201508119010Hinge Fitting · wornNUMBER 1 ENG INBD THRUST REVERSER MIDDLE HINGE BEARING LOOSE & ROTATES IN THE HINGE FITTING. REPLACED HINGE FITTING IAW AMM 54-57-17-400-003-A.Aug 10, 2015 · N122US · Airbus A320214SDR CA150923011Transcowl · out of position(CAN) LT INBD T/R NR 1 ENGINE, TRANSLATING COWL FOUND ASKEW ON WALKAROUND AND DIFFICULTY CLOSING THRUST REVERSER. THE UPPER ACTUATOR ROD END WAS FOUND DISLOGED FROM THE CLEVIS FITTING. LT ENGINE R/N POSITION T/R REPLACED IAW AMM 78-31-04, P 401.Aug 9, 2015 · Boeing 767333SDR AALA20150808002Switch · faultyEMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE, LT ENG REVERSER UNLOCK LIGHT ILLUMINATED. QRH PROCEDURES FOLLOWED, LIGHT DID NOT EXTINGUISHED. ENG OPERATED AT IDLE TILL LANDING. R & R & TESTED THE UPPER THRUST REVERSER LATCH INAug 8, 2015 · N473AA · Doug DC982SDR SIMA20150802004Structure · crackedRIGHT LOWER TRANS COWL OTBD JOINT EXTRUSION IS CRACKED. R & R RT LOWER TRANS COWL OTBD JOINT EXTRUSION IAW ETN-CR-54-015R1.Aug 2, 2015 · N518AE · Cndair CL6002C10
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