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 P5CA2011052000057Thrust Reverser · damagedDURING WALK AROUND INSPECTION FOUND DAMAGE & NBSP; TO NR 4 ENGINE LT AND R /H THRUST REVERSER TRAILING EDGE AT 6 O`CLOCK POSITION. (PER EO 4478A174 PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS WITH A DVI EVERY 1000 FLIGHT HOURS AND ASDR IPXA11166693Sleeve · damagedUPON ARRIVAL, MX INSP DISCOVERED RT ENG OTBD T/R SLEEVE PARTIAL SEPARATION FROM ACFT. APPX 1 FT X 7 FT SECTION OF T/R SLEEVE MISSING. DEBRIEF FROM FLT CREW NOTED LANDING RW 35L. TOWER AND CFR WAS NOTIFIED AND RWY INSP RECOVERED SEVERAL SMALL SECTIONS OF SAMESDR IPXA1166693Sleeve · separatedUPON ARRIVAL, MX INSP DISCOVERED RT ENG OTBD THRUST REVERSER SLEEVE PARTIAL SEPARATION FROM ACFT. APPX 1 FT X 7 FT SECTION OF T/R SLEEVE MISSING. DEBRIEF FROM FLT CREW NOTED LANDING SDF RW 35L. TOWER AND CFR WAS NOTIFIED AND RWY INSP RECOVERED SEVERAL SMALLSDR UIEA2011051700269Nozzle · crackedDURING A "C" CHECK OF AIRCRAFT, MX FOUND CRACKS ON THE NR 1 AND NR 2 ENGINE FIXED COWL EXHAUST NOZZLE FWD FLANGE CORE COWL SUPPORT ASSY (REF FIG 1 AND 2 ). (THE CRACKS CAN BE REPAIRED IAW THE ENGINE SHOP MANUAL (ESM) TASK 78-33-05, REPAIR 78-33-05, REPAIR 002SDR JR2R2911051400209Baffle · crackedNR 2 LOWER TRANSCOWL BAFFLE CRACKED. REMOVED AND REPLACED LOWER TRANSCOWL BAFFLE IAW CRJ 900 SRM 51-42-06.SDR JR2R2011051400208Panel · crackedLT ENGINE UPPER TRANSCOWL LATCH DOOR COAMING CRACKED. REMOVED AND REPLACED LT ENG UPPER TRANSCOWL LATCH COAMING IAW CRJ900 SRM 51-42-13.SDR JR2R2011051400210Stand Off · crackedNR 2 LWR TRANSCOWL STANDOFF ANGLE CRACKED. REMOVED AND REPLACED STANDOFF ON NR 2 LWR TRANSCOWL IAW CRJ900 SRM 51-42-14 AND 51-42-21.SDR P5CA2011051200049Ring · crackedNUMBER 3 ENGINE, RIGHT THRUST REVERSER, FORWARD TORQUE BOX J-RING UPPER SIDE HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A78B-911.SDR REXA201100286Warning System · activatedRIGHT T/R UNLOCK MSG IN FLIGHT DEFERRED RIGHT T/R PER MEL 78-30-01 AUTH 43603 PER MOC.SDR EE4Y20110277Bumper · wornENGINE NR 2, OTBD/RT THRUST REVERSER C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE: THE BUMPER WEAR REQUIRES A MAJOR REPAIR.SDR EE4Y20110276Bumper · wornENGINE NR 2, INBD/LT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE: THE BUMPER WEAR REQUIRES A MAJOR REPAIR.SDR EE4Y20110275Bumper · wornENG NR1, INBD/RT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE: THE WEAR REQUIRES A MAJOR REPAIR.SDR EE4Y20110274Bumper · wornENGINE NR 1, OTBD/ LT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE: THE WEAR REQUIRES A MAJOR REPAIR.SDR P5CA2011051000020Blowout Door · wornNR 3 ENGINE, RIGHT THRUST REVERSER FORWARD AND AFT EDGES OF BLOW OUT DOOR SHOWS WEAR. PERMANENT REPAIR ACCOMPLISHED IAW T2011A78B-1028.SDR P5CA2011051000018Blowout Door · wornNR 1 ENGINE, RIGHT THRUST REVERSER FORWARD AND AFT EDGES OF BLOW OUT DOOR SHOWS SIGNS OF WEAR. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A78B-1026.SDR P5CA2011051000019Blowout Door · wornNR 2 ENGINE RIGHT THRUST REVERSER FORWARD AND AFT EDGES OF BLOW OUT DOOR SHOWS WEAR. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A78B-1028.SDR CALA2011051100360Transducer · out of adjustRIGHT ENGINE DID NOT RESPOND ON ENGINE RUN FOR TAKEOFF N1 READ 50 PERCENT EGT 400 WITH THROTTLE FULL POWER. PERFORMED RE-ADJUSTMENT OF POSITION FEEDBACK TRANSDUCER IAW AMM 78-36-03/401. PERFORMED MAXIMUM POWER ASSURANCE GROUND TEST 5 IAW AMM 71-00-00 P538. SDR UALA2011050902276Thrust Reverser · dentedCREW REPORT: SMALL DENT ON RT ENGINE OTBD SIDE. AMC TEXT: FBO TO EVALUATE AND REPORT FINDINGS TO SAMC-EMC. FBO FOUND DENT .5 X .5 AND .010D. NO DELAMINATION, CREASES OR CRACKS. MUST BE REPAIRED PER MT WITHIN 50T. SAMC REMARKS: THIS DENT ON NR 2 ENG TRUSTSDR UALA2011050502209Sleeve · damagedNR 2 ENGINE THRUST REVERSER IS DAMAGED ON THE OUTBOARD TRAILING EDGE AND IS ALSO DAMAGED INBOARD AT THE 5 O'CLOCK POSITION. ACCOMPLISHED INTERIM REPAIR. INSTALLED SERVICEABLE THRUST REVERSER SLEEVE PER MM.SDR JR2R2011050500196Baffle · crackedTWO UPPER TRANS COWL BAFFLE CRACKED. REMOVED AND REPLACED UPPER TRANS COWL BAFFLE IAW CRJ 7 SRM 51-42-06.SDR HALA2011042500168Warning Light · illuminatedETOPS SIGNIFICANT SYS - BTB LT REV ISO VALVE STATUS DISPLAYED. RESET AND ERASED LT REVERSER ISO MSG IAW AMM 78-31-00 LIGHT STAYED OUT. OK FOR SERVICE.SDR A6WA201140325Panel · missingLT ENGINE LOWER STANG PANEL MISSING. PERFORMED EDDY CURRENT INSP ON LT LOWER STANG PANEL BRACKETS IAW NDTM PART 6-53-00-096, FOUND NO DEFECTS. INSTALLED LOWER ENGINE STANG PANEL.SDR JR2R2011042000154Structure · damagedONE UPPER TRANS COWL COAMING HOLE ELONGATED. REMOVED AND REPLACED COAMING IAW CRJ 9 SRM 51-42-06, 51-42-13.SDR AALA20110419DFW02Unlock Switch · inoperativeDFW - CAPTAIN REPORTED ON CLIMBOUT LEFT THRUST REVERSER BLUE UNSAFE LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. FOUND UPPER UNLOCK SWITCH INOPERATIVE. REPLACED SWITCH. SYSTEM GROUND CHECK NORMAL OPERATION.SDR A6WA201140297Track · damagedRT THRUST REVERSER INBD LOWER TRACK AND LUG DAMAGED. BLENDED LUG WITHIN LIMITS IAW REO 601R-78-34-2435. R & R WITH INBD TRACK.SDR DALA1127039856Fairing · crackedENGINE NR 2 LOWER T/R BUCKET OTBD FAIRING CRACKED. STOP DRILLED CRACK, FABRICATED DOUBLER FROM 2024T3 .050 PO NR 1130701, INSTALLED DOUBLER IAW SRM 54-01, F2, P106 17APR11. REQUIRED INSP COMPLETED.SDR ASOA201100779Switch · out of adjustRT REVERSER UNLOCK MESSAGE IN FLIGHT FOLLOWED QRH. (ENROUTE TO CHS A/C DIVERTED TO RIC DUE TO MX -- EMERGENCY DECLARED) ADJUSTED RT T/R STOW SWITCH IAW AMM 78-37-01. OPS CHECK GOOD AT THIS TIME.SDR ZZDA2011391Angle · crackedNR 2 ENGINE, I/B LEADING EDGE END TR DEFLECTOR DOOR ANGLE, CRACKED. ACCOMPLISHED TR DEFLECTOR DOOR ANGLE DOUBLER REPAIR PER EA 17-54-03118IR AND B717 SRM 54-30-05.SDR CLCA040620111Pressure Switch · faultedREJECTED TAKEOFF, BELOW 89 KTS (MIA) DUE TO REV NR 3 PRESS FAULT. TRANSFERRED TO DMI 5705 IAW MEL 78-30-1. DE-ACTIVATED NR 3 TR. CAT "C" PLACARD INSTALLED. ON TROUBLESHOOTING OF DISCREPACY, FOUND DEFECTED PRESSURE SWITCH. ( 04-17-2011) R & R PRESSURE SWITCHSDR IPXA11566082Angle · crackedINSPECTION TYPE:C1, WHILE WORKING CARD NR 930340, FOUND NR 2 ENG OTBD THRUST REVERSER TO HAVE CRACKED ANGLE ADJACENT TO L/E RUBSTRIP,27" ABOVE LWR INBD END OF COWL. REPLACED FRAME IAW SRM 51-40-02-0G, SRM 51-40-05-0G, AMM 51-21-10-7, SRM 51-10-02-0G, STEP 9.SDR UALA2011040701683Actuator · leakingRIGHT ENGINE HAS OIL DRIPPING FROM COWL. DURING RETRACT OPERATION INBOARD, MIDDLE RETRACT ACTUATOR LEAKS BEYOND DISPATCH LIMITS, APPROX 40 DROPS PER CYCLE. NO LEAKAGE STATIC. LOCKED OUT REVERSER PER MEL7831A. REPLACED THRUST REVERSER ACTUATOR REF MM. LEAKSDR UALA2011040501642Skin · damagedNR 1 ENGINE FAN EXIT ACOUSTIC LINER HAS A FOUR INCH CUT. DAMAGE IS LOCATED AT THE 5 O'CLOCK POSITION ON THE INNER C DUCT INNER SKIN. THIS DAMAGE IS ON THE REVERSER COWL INNER AIRSTREAM HALF. SEE SRM 54-33-01 PG2 ITEM 9 FOR SKIN DAMAGE LOCATION. DAMAGE IS 3.25 SDR UALA2011040601653Seal · damagedON WALK AROUND SECTION OF DAMAGED SEAL, LESS THAN 10 PERCENT. REMAINING SEAL SECURE AND RESEALED ENDS WERE DAMAGED REMOVED. PART INF (PCN 120-2870). NIL STOCK IN SYSTEM. LOOKED FOR SEAL MATCH AT SMB NOTHING FOUND NEED 120-2870. MF7133 CREATED TO MONITOR. UPONSDR A6WA201140371Structure · crackedRT ENGINE THRUST REVERSER UPPER CENTER CASCADE CRACKED. REPAIRED RT ENGINE THRUST REVERSER UPPER CENTER CASCADE IAW AWAC PROCESS SPECIFICATION 1.SDR A6WA201140340Structure · crackedLT T/R UPPER INBD CASCADE CRACKED. REPAIRED LT T/R UPPER INBD CASCADE IAW PROCESS SPECIFICATION 1, DWG AW78-30-0711-04.SDR UALA2011040401630Sleeve · damagedREPAIR HAS DEPARTED AIRCRAFT FROM NR 4 ENGINE ACOUSTIC LINER ON RT REVERSER SLEEVE BETWEEN 3 AND 4 O'CLOCK. DAMAGED AREA IS 5.0" LONG X 1.25" WIDE X 0.5" DEEP. INSTALLED NEW SLEEVE PER MM, OPS CHECKED GOOD.SDR V0XR20110404021Frame · crackedLEFT BOTTOM THRUST REVERSER FRAME CRACKED. REMOVED AND REPLACED LT LOWER THRUST REVERSER FWD FRAME WET WITH SEALANT IAW SRM 51-40-02. W/C 4034SDR DALA1124080909Line · leakingDURING TAKEOFF AND CLIMB THE CREW REPORTED AN ACRID/OIL SMELL IN CABIN AND COCKPIT AND SMOKE IN THE COCKPIT. NO OVERHEAT INDICATIONS INDICATED FOR ENGINES OR PACKS. SMOKE CLEARED PRIOR TO LANDING. MAINTENANCE FOUND LEAKING LINE ON LEFT T/R CONTROL VALVE. MSDR IPXA1565914Bracket · brokenINSPECTION TYPE:C1, NR 1 INBD T/R BRACKET IS BROKEN ON HYD LINE 36 INCHES FROM BOTTOM AT FWD END. R & R BRACKET IAW SB RB.211-78-9613.SDR CA110330001Control Quadrant · failed(CAN) DURING THE LANDING AND TAXI THE CREW DISCOVERED ENGINE NR 2 THRUST LEVER WILL GO INTO REVERSE POSITION WHEN THRUST LEVER BROUGHT TO IDLE, WITHOUT SELECTING REVERSE. THE THRUST CONTROL QUADRANT, TCQ, WAS REPLACED. T/S A MECHANICAL FAULT WITHIN THE BOX,SDR DHLA201100044Frame · wornNR 2 ENG HALF THRUST REVERSER STRUCTURAL FWD FRAME SHOWS EXISTING WEAR DAMAGE STA YN 202.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-22-11, EVA D878-00401 REV IR DATED 04-06-11. REMOVED FASTENERS SRM 51-1-20D. CUT OUT DAMAGED AREA & FABRICATED NESDR MASA2011033002281Pdu · damagedNR 2 ENGINE PDU THRUST REVERSER HAS DAMAGED THREADS. MX R2 NR 2 ENG PDU TRUST REV, OPS CHECK GOOD.SDR ASAA1149453Panel · corrodedNR 2 ENGINE RIGHT THRUST REVERSER UPPER AFT BIFURCATION PANEL CORRODED. REPAIRED PANEL IAW ASA EA 400 78EA 04303.SDR DXTA2011032804525Warning Light · illuminatedCLIMBING THROUGH FL280, THE RIGHT ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THE EMERGENCY STOW SWITCH WAS SELECTED AND THE UNLOCK LIGHT EXTINGUISHED. A MINUTE LATER THE UNLOCK LIGHT REILLUMINATED AND REMAINED ON THROUGHOUT DESCENT AND LANDING. IT WAS STSDR UIEA2011031800158Frame · crackedTHE LT NR 4 FAN REVERSER EXHIBITED A CRACK ON THE TORQUE BOX FWD FRAME. (IN THIS INSTANCE THE CRACK HAD BEEN STOP DRILLED AND REGULARLY INSPECTED BY THE PRIOR OPERATOR JAL. AS THE ACFT WAS IN HEAVY CHECK, SIAEC WAS ADVISED TO PERFORM A PERMANENT REPAIR IAW SSDR UALA2011031501231Actuator · faultyNR 1 ENG REV FAULT, FLIGHT DIVERTED. REPLACED NR 1 ENGINE THRUST REVERSER NON LOCKING ACTUATOR ON INBOARD UPPER SIDE (FADAC NR 1B CHANNEL) WAS AT FAULT. REPLACED PER MM. OPS CHECKED NORMAL BOTH STATICALLY AND ENGINE OPERATIONAL, ALL SAFETIES APPLIED AND REMSDR UALA2011031401225Panel · peelingNR 2 ENG RT REVERSER LOWER BIFURCATION PANEL ALBLANTIVE COATING COMING OF FWD 2-3RDS. REPAIRED COATING LARGE AREA REPAIR PER MM.SDR UALA2011031401212Panel · damagedACCOUSTICAL PANEL DAMAGE AT NR 2 ENG. REPLACED RT TRANSLATING COWL ON NR 2 ENGINE. OPS CHECKED REF MM. NO FAULTS NOTED.SDR MYWA110035Transducer · out of adjustETOPS SIGNIFICANT SYSTEM: ENGINE CONTROL LIGHT ILLUMINATED WITH NR 1 ENGINE RUNNING. FOUND NR 1 ENGINE OUTBOARD T/R SLEEVE LVDT OUT OF ADJUSTMENT. ADJUSTED PER AMM FAULT CLEARED, LIGHT EXTINGUISHED.SDR UALA2011031001165Pin · damagedNR 1 ENG AFT RT CORE COWL RT AFT HOP TIE BAND PIN DAMAGED. INSTALLED NEW PIN. UNIT NOW SERVICEABLE
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