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 Z6WR0012011Panel · delaminatedTHE 315A2102-161 BONDED PANEL ASSY HAS 2 VISUAL CRACKS TO THE BAG SIDE. ONE CRACK IS CENTERED 24.0 FROM THE FWD EDGE AND 21.0 FROM THE LOWER EDGE. CRACK IS 14.0 LONG WITH A HOLE MEASURING 1.00 X .250. THE OTHER CRACK IS CENTERED 36.5 FROM THE FWD EDGE AND 18.SDR A6WA201141085Fitting · looseRT THRUST REVERSER HAS 2 LOOSE INTERLOCK FITTINGS. REMOVED UNSERVICEABLE FASTENERS AND INSTALLED SERVICEABLE FASTENERS IN RT T/R INTERLOCK FITTINGS (2 EA).SDR FDEA201110134459Torque Box · crackedNR1 ENGINE INBD THRUST REVERSER FWD UPPER TOP CORNER CRACK 4 INCHES. REPAIRED NR1 ENGINE INBD THRUST REVERSER TORQUE BOX UPPER CORNER IAW SRM 51-40-21 AND DWG SRZ 78-002. PERFORMED NTD IAW SRM 70-32-03 TO VERIFY CRACK DOES NOT EXTEND AFTER STOP DRILL. LOCATSDR 2011FA0000682Selector Valve · failedCREW WAS PERFORMING NIGHT PROFICIENCY FLIGHT. UPON 1ST LANDING, AIRCRAFT TAXIED AROUND FOR SECOND TAKEOFF. ON POWER UP FOR TAKEOFF ROLL, THE RIGHT ENGINE THRUST REVERSER HAD AN UNCOMMANDED DEPLOYMENT. CREW ABORTED TAKEOFF. RIGHT REVERSER WOULD NOT STOW. ASDR EE4Y201110559Skin · corrodedENGINE NR 2, LEFT C-DUCT LOWER BIFURCATION OUTER SKIN WITH CORROSION, LOCATED JUST ABOVE THE 740-0420 FAIRING AT 6 O'CLOCK POSITION. NOTE: THE C-DUCT OUTER SKIN REQUIRES A MAJOR REPAIR IAW ENGINEERING GUIDELINES.SDR A6WA201141034Transcowl · chafedRT LOWER TRANSCOWL HAS CHAFE DAMAGE AT AFT POINT. REPAIRED DAMAGE TO RT LOWER TRANSCOWL AFT OF HINGE POINT IAW REO 601R-78-33-3969.SDR FDEA201110074377Frame · crackedNR1 ENGINE OTBD THRUST REVERSER UPPER UPPER TOP CORNER CRACKED 4". REPAIRED NR1 ENGINE OTBD THRUST REVERSER TORQUE BOX UPPER CORNER IAW SRM 51-40-21 AND DWG SRZ 78-002. PERFORMED NTD IAW SPM 70-32-03 TO VERIFY CRACK DOES NOT EXTEND AFTER STOP DRILL. LOCATEDSDR P5CA2011100700480Blowout Door · wornBLOW OUT DOOR AT 6 O`CLOCK POSITION ON NR 2 ENGINE, RIGHT THRUST REVERSER IS WORN ON THE LEADING & NBSP; AND THE TRAILING EDGES. REPAIR ACCOMPLISHED TO BOTH EDGES AS PER EO 4478A191.SDR FDEA201110064345Shutoff Valve · malfunctionedON INITIAL T/O ROLL, LEVEL 1 ALERT " REV PRESS FAULT", ABORTED TO BLOCKS. FAULT EXTINGUISHED AFTER CLEAR OF RUNWAY. PERFORMED FIM 78-30-01, FIG 103, CONTINUITY CHECK BETWEEN J4 PIN 19 (ECU) TO PIN B PRESS, SW DPV AND PIN C (PRESS SW) TO GROUND - OK. HOWEVESDR COMA2011100550075Thrust Reverser · faultyRECEIVED A RIGHT THRUST REVERSER UNLOCK MESSAGE DURING TAKEOFF AT MEM, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. DEFERRED THE RIGHT THRUST REVERSER PER MEL 78-30-01.SDR UALA2011100305323Panel · delaminatedNR 1 ENG THRUST REVERSER OUTBOARD COWL UPPER BIFURCATION PANEL INNER (NON PERFORATED) AND OUTER (PERFORATED) SKINS BOTH DELAMINATED FROM L/E TO T/E AND FROM SIDE TO SIDE TOTAL AREA OF DELAM IS BETWEEN 680 AND 700 SQ INCHES, EXCEEDS LIMITS OF MM. INSTALLED REPSDR CVGA201110012761Warning Light · illuminatedTHE RT THRUST REVERSER AMBER UNLOCK LIGHT ILLUMINATED AFTER TAKEOFF.SDR UIEA2011092900529Thrust Reverser · damagedDURING WALKAROUND, MX FOUND THE NR 2 RT THRUST REVERSER INSULATION DAMAGED. DAMAGE IS SUSPECTED TO BE DUE TO DAMAGE FROM THE IDG AIR/OIL COOLER PARTIAL VANE LIBERATION.SDR UALA2011091604994Sleeve · delaminatedAREA OF DELAM ON THE NR 2 ENG LT REVERSER SLEEVE AT THE BOTTOM SEAM LINE JUST FWD OF THE TWO AFT MOST LATCHES. ACP'D HFEC ON NR 2 ENG INBD UPR REV TRACK PER NTM 51-10-08 PART 6 AND UA-EVA81307. NO CRKS DETECTED. BLENDED GOUGES PER UA EVA 8137. ALODINED AND PRSDR A6WA201140843Thrust Reverser · malfunctionedRT T/R UNLOCKED CAUTION MSG 1000 FT AGL. PRESSED EMERGENCY STOW AND SHUTOFF RT T/R MSG REMAINED. RETURNED TO DEPARTURE. LANDING WEIGHT 47000 LBS. C/A IN PROGRESS: PLACED ON MEL.SDR EE4Y20110533Pad · wornNR 2 ENGINE OTBD THRUST REVERSER C DUCT INNER SIDE AFT SECTION, PAD DOWN PLATE WITH WEAR. NOTE: PAD DOWN WILL BE REPAIRED IAW SRM 54-30-00 REPAIR 038.SDR EE4Y20110532Pad · wornNR 2 ENGINE INBD THRUST REVERSER C DUCT INNER SIDE AFT SECTION PAD DOWN PLATE WITH WEAR. NOTE: THE PAD DOWN WILL BE REPAIRED IAW SRM 54-30-00, REPAIR 038.SDR EE4Y20110531Pad · wornNR 1 THRUST REVERSER OTBD C-DUCT, PAD DOWN WITH WEAR. NOTE: PAD DOWN WILL BE REPAIRED IAW SRM 54-30-00, REPAIR 038.SDR EE4Y20110530Plate · wornNR 1 THRUST REVERSER INBD C DUCT, PAD DOWN WITH WEAR. NOTE: PAD DOWN PLATE WILL BE REPAIRED IAW SRM 54-30-00, REPAIR 038.SDR A6WA201140876Lug · chafedLEFT THRUST REVERSER OTBD LOWER TRACK LUG CHAFED, BLENDED DISCREPANT AREA IAW SRM 51-21-06 AND COMPLIED WITH REO 601R-78-34-2435.SDR A6WA201140792Pdu · out of rigRT REVERSER UNLOCK CAUTION MESSAGE INFLIGHT IN CRUISE FLIGHT 26.0. REMAINED ILLUMINATED UNTIL ENGINE SHUTDOWN. FOUND PDU OUT OF RIG ADJUSTED DIRECTIONAL CONTROL VLV IAW AMM 78-32-03. OPS CK GOOD CLEARS PLACARD & MEL.SDR UIEA2011090200479Fairing · brokenENGINE EXHAUST -NR 2 ENGINE RT UPPER INNER FAIRING REPLACEMENT - DURING THE CURRENT C-CHECK, THE UPPER INNER FAIRING WAS FOUND BROKEN (PARTIAL MISSING) AT FWD SECTION. A REPLACEMENT UPPER INNER FAIRING (PN: 9059M49P002C) HAS BEEN ORDER FOR REPLACEMENT IAW EMSDR UIEA2011082700474Skin · puncturedDURING WALKAROUND, MX FOUND THE NR 4 RT THRUST REVERSER CORE COWL HAS 2 PUNCTURES IN THE SKIN LOCATED ABOVE THE ACCESS PANEL AND BLOWOUT DOOR. DAMAGE TO THE ACCESS PANEL AND BLOWOUT DOOR HINGES, LATCHES AND LANYARDS. REPAIRED.SDR A6WA201140785Torque Box · damagedRT THRUST REVERSER TORQUE BOX HAS NUMEROUS DAMAGED AREAS, REO 78-30-4072.SDR FDEA201108243451Thrust Reverser · inoperativeNR 2 ENGINE THRUST REVERSER "UNLOCKED" ECAM ILLUMINATED ON TAKEOFF AT 90 KTS, REJECTED TAKEOFF. PERFORMED CDU POSITION SWITCH MODULE FUNCTIONAL CHECK, NO DEFECTS NOTED. CHECKED LT AND RT TRANS GAPS, ALL IN LIMITS PER MM 78-31-00-05. CW CDU INSPECTION PER MMSDR UFHR20110825001Control Valve · crackedTHE BODY WAS SUBJECTED TO NDT WHICH REVEALED AN INDICATION AND WAS REJECTED FOR RETURN TO SERVICE.SDR UALA2011082204446Actuator · leakingHYDRAULIC LEAK NR 1 ENGINE. LOWER RIGHT REVERSER ACT LEAKS 10 DROPS PER CYCLE. NR 1 ENGINE ACT NEED REPLACEMENT PCN 152-9609 OK TO CONT 75 FLT. 18AUG ORD CQT- SHOULD READ 10 DROPS PER MIN. CLEANED ALL THREE RT ACTUATORS. CYCLED NR 1 ENG REVERSER 10 TIMESDR JR2R2011082100346Thrust Reverser · cracked1 UPPER TR COAMING IS CRACKED. REMOVED AND REPLACED 1 ENG UPPER TRANCOWL COAMING IAW CRJ 900 SRM 51-42-06, 51-42-13.SDR P5CA2011081800455Thrust Reverser · damagedFOUND DAMAGE TO THE NR 3 ENG RT THRUST REV 4 INCHES WIDE BY 2 INCHES LONG & NBSP; FROM A LIGHTNING STRIKE AT 5 O'CLOCK POS. (COMPLIED WITH LIGHTNING STRIKE INSP PER AMM 05-51-13. ACCOMPLISHED EO 4478A184 (FAA FORM 8110-3 DATED 17AUG2011): TIME LIMITEDSDR UALA2011081504326Thrust Reverser · crackedNR 2 ENG OTBD T-R HAS 2 LARGE CRACKS AND ONE SMALL CRACK IN SHEETMETAL WITH SEVERAL RIVETS PULLING THRU LEADING EDGE OF PANEL BETWEEN 2 LARGE CRACKS AT 1 O'CLOCK POSITION. INSTALLED ROBBED UNIT FROM AC 4278 SFOOV NR 2 ENG RT SIDE PER MM, OPS CHECKS OKAY.SDR A6WA201140836Structure · crackedRT UPPER THRUST REVERSER CASCADE CRACKED IN 4 PLACES. REPAIRED CRACKS IN RT UPPER THRUST REVERSER CASCADE IAW AWAC PROCESS SPEC 1.SDR UIEA2011080700432Skin · damagedDURING MX WALKAROUND, MX FOUND DAMAGE TO THE NR 2 ENG RT THRUST REVERSER TRANSLATING COWL EXTERNAL SKIN OUTER FINISH DAMAGE. THE DAMAGE IS LOCATED IN NEAR THE REVERSER COWL SKIN T/E (REF FIG 1-3): PERFORMED A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK ISDR UALA2011080804156Thrust Reverser · malfunctionedCREW REPORTS NR 1 REVERSER DID NOT DEPLOY ON LANDING. SAMC TEXT: NEED TO ACP OPERATIONAL CHECK OF LEFT REVERSER PER MM. WHILE ACCOMPLISHING REVERSER FIM PROCEDURES, DISCOVERED C-B'S D14 & D18 OUT AND COLLARED. THESE ARE FOR THE L ENG REV CONTROL. RESET BREASDR UIEA2011080600429Skin · damagedDURING INSP, MX FOUND THE NR1 ENGINE LT THRUST REVERSER CORE COWL INNER SKIN DAMAGED/DELAMINATED. REF FIG 1. DISPOSITION IS TO REPAIR THE SIDEWALL DAMAGE ON THE THRUST REVERSER IAW AMM 78-31-01, AND REPLACEMENT OF THE THRUST REVERSER AT THE NEXT "A" CHECK. SDR FDEA201108053112Support Bracket · crackedNR1 ENGINE THRUST REVERSER TRANSLATING COWL UPPER GUIDE SUPPORT SLIDER BRACKET CRACKED. REMOVED NR 1 ENG O/B TRANSLATING SLEEVE IAW A310-200 AMM 78-32-11-04. REMOVED CRACKED UPPER COWL GUIDE SUPPORT BRACKET IAW SRM 54-40-21 AND SRM 54-04-01 PG.11. FABRICATESDR ASOA201101458Pdu · unserviceableLT REVERSE UNLOCK MESSAGE APPEARED IN FLIGHT. C/W QRH. ACFT HANDLED WELL. LANDING AT NEAREST SUITABLE AIRPORT. ENROUTE, DIVERTED DUE TO MX -- EMERGENCY DECLARED AS A PRECAUTION. R & R LT THRUST REVERSER PDU IAW AMM 78-32-03.SDR UALA2011080203996Rivet · looseNR 1 ENG INBOARD T-R SLEEVE HAS SEVERAL LOOSE RIVETS AFT UPPER T-R ASSY (OUTER SHEETMETAL). REPLACED LOOSE RIVETS PER SRM, REPAIR NR 48, FIG 202.SDR UALA2011080103982Actuator · leakingRAMP REPORTED FLUID LEAK NR 2 ENGINE. FOUND NR 2 ENGINE INBOARD UPPER REVERSER ACTUATOR LEAKING 5 DROPS PER MINUTE.SDR FDEA201107283007Bracket · chafed1 ENG INBD THRUST REVERSER LOWER HARD MOUNTED PANEL ON L/E HAS PANEL LAND FOR T/R. LATCH PANEL CHAFED ON AFT END. R & R PART IAW SRM 51-40-21.SDR FDEA201107283006Fitting · gougedNR 2 ENG OTBD THRUST REVERSER FWD LWR BUMPER FITTING GOUGED IN 2 EA AREAS. MEASUREMENTS ARE APROX .4 X .3 X .10D AND .35 X .15 X .050D. R & R BUMPER FITTING AT NR2 ENG OTBD THRUST REVERSER FWD LWR IAW MRA CMM 78-32-11 AND 78-32-00.SDR FDEA201107232913Skin · chafedNR 2 ENGINE OTBD THRUST REVERSER UPPER SIDE T/E AREA FOUND SKIN CHAFED. ACCOMPLISHED THE EA 6-7830-149011. REPAIR EVALUATED IAW GMM 6-2-100 AND CLASSIFIED AS MINOR.SDR UALA2011072203748Control Valve · failedL ENG REV WILL NOT GO INTO REVERSE. REPLACED ISOLATION VALVE, NO HELP. NO VOLTAGE TO ISOLATION VALVE. REPLACED LT REVERSER DIRECTIONAL CONTROL VALVE PER MM.REPLACED PSEU. REVERSER DEPLOYS AND NO FAULT MESSAGES. OPS CHECKED PER MM, PASSED.SDR UALA2011072203747Rod End · brokenNR 2 ENG AFT COMPRESSION ROD END BROKEN. REPLACED ROD ASSY.SDR REXA201100471Indication Sys · activatedON APPROACH INTO DTW CREW DECLARED CLASS II EMERGENCY DUE TO LEFT ENGINE THRUST REVERSER UNLOCKED INDICATION, A/C LANDED WITHOUT INCIDENT.SDR JR2R2011071800305Stand Off · crackedRT UPPER TRANSCOWL INBOARD STANDOFF IS CRACKED. REMOVED AND REPLACED INBOARD STANDOFF IAW CRJ 900 SRM 51-42-21 AND 51-42-14.SDR UALA2011071703617Panel · missingNR 1 ENGINE INBOARD THRUST REVERSER MISSING ISLAND ASSY APPROXIMATELY 1 O'CLOCK. INSTALLED MISSING PANEL. THRUST REVERSER OPS CHECKED GOOD.SDR UALA2011071503595Structure · damagedFOUND TWO AREAS ON NR 1 ENG OTBD REVERSER HALF WHERE LIGHTNING EXITED AIRCRAFT. MARKED BY BURN MARKS AND SHREDDED GRAPHITE CLOTH. ALSO NOTED SEVERAL BURNED RIVETS ON REVERSER HALF. SUPPLEMENTAL DATA UPDATE REMOVED TRANSCOWL. FOUND 6 BAD HINGES. REMOVED BLOCKESDR JR2R2011071200291Stand Off · crackedLEFT LWR TRANSCOWL STAND OFF CRACKED. REMOVED AND REPLACED LEFT LWR TRANSCOWL STAND OFF IAW CRJ 900 SRM 51-42-21, 51-42-13.SDR UALA2011071103410Panel · missingNR 2 ENGINE ISLAND PANEL MISSING FROM TRANSLATING COWL. PART ON AOG 5186. ISLAND ASSY 222-1349. REPLACED THE ISLAND ASSY (222-1349) IAW AMM.SDR UALA2011070603352Sleeve · damagedENG 2 OUTBOARD THRUST REV OUTER PANEL HAS DAMAGE. SPEED TAPE APPLIED AS AN INTERIM REPAIR. VISUAL INSPECTION OF AIRCRAFT AND FOUND IN SAFE CONDITION FOR TYPE II FERRY FLT FORM ORD TO SFO FOR REPAIR OF NR 2 ENG OTBD REV T/E. SUGGEST A 2 SHIFT SLOT FOR LAY-UP
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