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 DHLA201100018Frame · wornNR 4 ENG RT THRUST REVERSER STRUCTURAL FWD FRAME HAS WEAR DAMAGE AT STA YN 202.000 BETWEEN 5 AND 6 O'CLOCK POS PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-11-11, EVA D878-00389 REV IR DATED 01-31-11, SMN DWG ED-5311 DATED 01-25-11. REMOVED FASTENERS IASDR DHLA201100017Frame · wornNR 4 ENG LT THRUST REVERSER STRUCTURAL FWD FRAME HAS WEAR DAMAGE STA YN 202.000 BETWEEN 7 AND 9 O'CLOCK POS PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-15-11 EVAD878-00388 REV IR DATED 01-28-11, SMN DWG ED-5310 DATED 01-24-00. REMOVED FASTENERS IAW SRMSDR A6WA201140043Actuator · malfunctionedLT THRUST REVERSER UNLOCK MSG IN FLIGHT, C/W`D QRH DIVERTED TO PIT. RESET ALL 4 BALLSCREW ACTUATORS TO PROPER POSITIONS AND REZEROED ON DOG STOPS. RECONNECTED TO TRACKS AND INSTALLED FLEX DRIVES IAW AMM 78-32-01. OPS CHECKED GOOD.SDR A6WA201140054Lug · crackedRT THRUST REVERSER BLOCKER DOORS 1 THRU 9 HAVE WORN ATTACH HARDWARE UPON REMOVAL OF HARDWARE ON BLOCKER DOOR NR 9 FWD INBD LUG TO BE DAMAGED. R & R BLOCKER DOOR HINGE SUPPORT FITTING P/N 228-50758-809 IAW CMM 78-30-00, REPAIR NR SRS097.SDR FDEA201101100184Cable · gougedNR1 PYLON LOWER SIDE OF NACELLE LT & RT THRUST REVERSER INTERLOCK CABLES GOUGED THRU CABLE INSULATION. MARKED, R & R NR1 PYLON LT INTERLOCK CABLE IAW AMM 76-11-41-04, REMOVED NR1 PYLON RT INTERLOCK CABLE IAW AMM, REPAIRED RT INTERLOCK CABLE IAW EA 6-7611-SDR DALA1102429202Acoustic Liner · departedFLIGHT CREW DIVERTED, DUE TO REPORTS OF DEBRIS ON DEPARTURE RUNWAY OUT OF MSP WHICH "MAY HAVE COME OFF OF OUR JET". DEBRIS IDENTIFIED AS ACOUSTICAL LINER AND ACFT WAS THE LAST TO DEPART. MX FOUND ACOUSTIC MATERIAL MISSING ON THE NR1 ENGINE THRUST REVERSER. USDR F3LA2011010600575Skin · gougedC-CHECK: NON ROUTINE N0633; NR 2 ENGINE OTBD THRUST REVERSER LOWER BLOCKER INTERNAL SIDE THE PERFORATED SKIN HAS A GOUGE MEASURING .7500 INCH LONG, .2500 INCH WIDE AND .115 INCH DEEP. REPAIRED IAW CMM 78-32-36, REPAIR NR8.SDR F3LA2011010600574Cowl Door · dentedC-CHECK: NON ROUTINE NR N0636; NR 2 ENGINE OTBD THRUST REVERSERS INNER PERFORATED COWL BELOW THE UPPER BLOCKER DOOR THERE IS A DENT MEASURING .1250 INCH CIRCUMFERENCE AND .030 INCHES DEEP. REPAIRED 1 INCH DENT IAW CMM 78-32-36, REPAIR NR8.SDR CTASRD2011001Sleeve · deformedRIGHT ENGINE NR 2 INBOARD THRUST REVERSER SLEEVE HALF IS DEFORMED DUE TO RUBBING WITH THE THRUST REVERSER BLOCKER DOORS IN FOUR PLACES. DEFORMATION RANGES FROM ONE INCH, TO .375 OF AN INCH.SDR 2011FA0000009Isolation Valve · sluggishCREW NOTED THAT AFTER LANDING THE LT THRUST REVERSER SEEMED SLOW TO DEPLOY: REMOVED ISOLATION VALVE DUE TO LT T/R SLOW TO DEPLOY. REMOVED THRUST REVERSER LOCKOUT PINS AND ENABLED THE THRUST REVERSER SYS. THRUST REVERSER SYS OPS CHECK AND LEAK CHECK GOOD IAWSDR IPXA11564413Ramp · chafedINSPECTION TYPE:C1, NR2 OTBD T/R, LWR AFT INNER FITTING IS CHAFED, 5" FROM AFT END. REPLACED INNER FITTING (RAMP) IAW SRM 51-10-02-0G STEP 9.C., SRM 51-40-02-0G, SRM 51-40-05-0G, AND SRM 51-40-08-0G, ON NR2 OTBD T/R, AFT LWR LOCATION.SDR AALA20110101JFK01Sensor · faultedCREW REPORTED RIGHT THRUST REVERSER "DEPLOYED" INDICATION APPEARED ON EICAS. NO UNUSUAL BUFFET, VIBRATION OR YAW WAS NOTED BY THE COCKPIT CREW. EMERGENCY DECLARED, FLIGHT DIVERTED, LANDED WITHOUT INCIDENT. THRUST REVERSER DEPLOYED INDICATION RETURNED TO NORSDR UIEA2010122900248Latch · brokenDURING MX WALKAROUND OF ACFT, REVEALED NR 1 ENGINE THRUST REVERSER LOWER AFT ACCESS DOOR AND BLOWOUT DOOR WERE FOUND OPENED. UPON FURTHER INSP, MX FOUND THE AFT TENSION LATCH BROKEN. (DISPOSITION IS TO ACCOMPLISH A TIME LIMITED REPAIR BY INSPECTING THE 2 OTHSDR UALA2010122904761Relay · inoperative"AIR-GND DISAGREE" STATUS MESSAGE APPEARED AT/OR AFTER TAKEOFF. ACARS DISPLAYS AN "ON". BITE TEST OF PSEU FAULTING 015 CARD. CARD REPLACED ON 12-18. REPLACED LT REVERSER AIR GROUND SYS 1 RELAY K178 REF WDM 78-34-11. PSEU BIT AND VERIFY TESTS OK.SDR UALA2010122704709Pressure Switch · faultyLEFT REVERSER ISOLATION VALVE LIGHT, UPPER EICAS DISPLAYED MOMENTARILY DURING LT REVERSER STOW FOLLOWED BY LATCHED STATUS MESSAGE. SUSPECT PRESSURE SWITCH S858 PCN 481-1961 OR M1987 MODULE PCN 563-3874 NIS DENVER. REPLACED S858, NO HELP. REPLACED RELAYS K26 SDR SIMA201036202Relay · inoperativeON FLIGHT 4532 ON DESCENT AT APPROX 11,000 FT, RECEIVED A " ENG 1 REV FAIL" MESSAGE ON EICAS. PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN AS DIRECTED BY OPS MANUAL. CAPTAIN DECLARED AN EMERGENCY & LANDED SINGLE ENGINE. POST FLT INSPECTION REVEALED NO DAMAGE OR SDR UALA2010122704707Isolation Valve · faultyEICAS & STATUS MSG R REVERSER ISOLATION VALVE. REV LOCKED OUT. TR RELAY MODULE HAD LIGHT ON FOR HIV PRESSURE (HYD ISOLATION VALVE PRESS). REPLACED REVERSER ISOLATION VALVE ON NR 2 ENGINE, FAILED OPS CK, FAULT STILL SHOWING. CORRECTION TO LAST UPDATE, STOW SDR FDEA201012224739Frame · crackedENG 1 RT THRUST REVERSER COWL FWD RING FLANGE GOT CRACK AT UPPER EDGE, ABOUT 1.5 INCH. REPAIR THE DAMAGE AREA WITH DOUBLER AND FASTENERS IAW DWG NR: SRZ-78-002. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR GTIA1000184Bumper Block · wornENGINE NR 2, OTBD/RT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE AFT BUMPER WITH WEAR. THE BUMPER WEAR REQUIRES A MAJOR REPAIR.SDR GTIA1000183Bumper Block · wornENGINE NR 2, INBD/LT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE AFT BUMPER WITH WEAR. THE BUMPER WEAR REQUIRES A MAJOR REPAIR.SDR GTIA1000182Bumper Block · wornENGINE NR 1, INBD/RT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE AFT BUMPER WITH WEAR. THE BUMPER WEAR REQUIRES A MAJOR REPAIR.SDR GTIA1000181Bumper Block · wornENGINE NR1, OTBD/LT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. THE WEAR REQUIRES A MAJOR REPAIR.SDR EE4Y100561Bumper Block · worn(EE4Y) ENGINE NR2, OTBD/RT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE AFT BUMPER WITH WEAR. NOTE: THE BUMPER WEAR REQUIRES A MAJOR REPAIR.SDR EE4Y100560Bumper Block · wornENG NR 2, INBD/LT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE AFT BUMPER WITH WEAR. NOTE: THE BUMPER WEAR REQUIRES A MAJOR REPAIR.SDR EE4Y100559Bumper Block · wornENGINE NR1, INBD/RT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE AFT BUMPER WITH WEAR. NOTE: THE BUMPER WEAR REQUIRES A MAJOR REPAIR.SDR EE4Y100558Bumper Block · wornENGINE NR1, OTBD/LT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE: THE WEAR REQUIRES A MAJOR REPAIR.SDR UIEA2010121300190Structure · damagedDURING ROUTINE A-CHECK OF ACFT , THE NR 2 AND NR 4 LT THRUST REVERSER CORE COWL L/E WERE FOUND WITH LOOSE FASTENERS AND BROKEN BONDING MATERIAL. THE NR2 AND NR4 RT T/R CORE COWL L/E'S WERE FOUND WITH BROKEN BONDING MATERIAL. (DISPOSITION IS TO REPAIR ALL THESDR UALA2010121304530Bracket · bentRIGHT ENG INBD FORWARD REVERSER LOAD SHARE TOP MOUNT BRACKET BENT AND BRACKET SUPPORT HOLE TORN OPEN. REMOVED RIGHT ENGINE REVERSER CROSS TIE ROD ASSY, LEGS, AND BRACKETS. ALL PARTS IN IADMM FOREMAN OFFICE. REPLACED BRACKETS, LEGS, SUPPORT ASSY. REPLACED BRACSDR UALA2010121004512Connector · dirtyEICAS MESSAGE REVERSER ISOLATION VALVE DISPLAYED AND REVERSER ISOLATION LIGHT ILLUMINATED DURING REVERSE THRUST. REACTIVATED REVERSER. CLEANED CONNECTOR AT REVERSER ISOLATION VALVE. CHECKED OPERATION SEVERAL TIMES. REVERSER OPERATION NORMAL, NO FURTHER MESSAGSDR DXTA2010121104360Warning Light · illuminatedDURING TAKEOFF AND CLIMBOUT, THE LT ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED PASSING THROUGH 6000' AND 235 KIAS. EMERGENCY STOW SWITCH WAS PLACED IN EMERGENCY POSITION. EMERGENCY CHECKLIST WAS COMPLETED AND AIRSPEED REDUCED BELOW 200 KIAS. TR "UNLOCK" LSDR CA101214005Latch · failed(CAN) AFTER DEPARTURE, THE FLIGHT CREW RECEIVED AN ENGINE VIBRATION FOLLOWED BY AN ECAM MESSAGE "THRUST REVERSER UNLOCK". THE NUMBER TWO (2) ENGINE WAS SHUTDOWN AS A PRECAUTION. THE AIRCRAFT RETURNED DEPARTING STATION. THE HCU (HYD CONTROL UNIT) AND THE DOORSDR A6WA201040936Pdu · malfunctionedWHILE CLIMBING THRU FLIGHT LEVEL 255. RECEIVED R-REV UNLOCK CAUTION MESSAGE. BOTH REVERSER DISARM AT THE TIME MESSAGE RECEIVED. MESSAGE PERSISTED UNTIL ENGINE SHUTDOWN AT GATE C/W QRH. DIVERTED. R & R RT T/R PDU IAW AMM 78-32-03. OPS CHECKED GOOD, REMOVESDR ZZDA2010617Angle · crackedNR 1 ENGINE, O/B AFT LIGHTENING HOLE, TR DEFLECTOR DOOR ANGLE, CRACKED. ACCOMPLISHED TR DEFLECTOR DOOR ANGLE REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 51-41-05.SDR GTIA1000163Bumper Block · wornENG NR 2, OTBD/RT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. BUMPER WEAR REQUIRES A MAJOR REPAIR.SDR GTIA1000162Bumper Block · wornENGINE NR 2, INBD/LT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. BUMPER WEAR REQUIRES A MAJOR REPAIR.SDR GTIA1000161Bumper Block · wornENGINE NR 1, INBD/RT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. BUMPER WEAR REQUIRES A MAJOR REPAIR.SDR GTIA1000160Bumper Block · wornENG NR 1, OTBD/ LT THRUST REVERSER C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. WEAR REQUIRES A MAJOR REPAIR.SDR EE4Y100528Bumper Block · worn(EE4Y) ENGINE NR 2, OTBD/RT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE: THE BUMPER WEAR REQUIRES A MAJOR REPAIR.SDR EE4Y100527Bumper Block · wornENGINE NR.2, INBD/LT THRUST REVERESE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE THE BUMPER WEAR REQUIRES A MAJOR REPAIR.SDR EE4Y100526Bumper Block · wornENGINE NR 1, INBD/RT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE: THE BUMPER WEAR REQUIRES A MAJOR REPAIR.SDR EE4Y100525Bumper Block · wornENGINE NR 1, OTBD/LT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE: THE WEAR REQUIRES A MAJOR REPAIR.SDR EE4Y100520Bumper Block · worn(EE4Y)ENGINE NR2, OTBD/RT THRUST REVERSE C-DUCT, PAN DOWN ENGINE BUMPER WITH WEAR. THE BUMPER WEAR REQUIRES A MAJOR REPAIR.SDR EE4Y100516Bumper Block · worn(EE4Y) ENG NR2, INBD/ LT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. THE WEAR REQUIRES A MAJOR REPAIR.SDR EE4Y100515Bumper Block · worn(EE4Y) ENGINE NR1, INBD/RT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. THE WEAR REQUIRES A MAJOR REPAIR.SDR EE4Y100514Bumper Block · worn(EE4Y) ENGINE NR1, OTBD/LT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. THE WEAR REQUIRES A MAJOR REPAIR.SDR REXA201000286Transcowl · dentedTHE RT ENGINE LOWER TRANSCOWL AND TORQUE BOX HAS SUSTAINED DENT/GOUGE DAMAGE ON THE FWD LEADING EDGE AT THE 6 O'CLOCK POSITION. DAMAGE TO TRANCOWL IS 13 X 2.5 X .150 INCH DEEP. DAMAGE TO TORQUE BOX IS 3 X 1.25 X .085 DEEP. TEMPORARY REPAIR IAW BOMBARDIER RSDR UALA2010113004404Liner · missingPIECE MISSING FROM RT ENG BETWEEN STATOR AND BLOCKER DOORS 6:30 POSITION. FOUND NR 2 ENGINE FAN EXIT LINER SEGMENT INTERMEDIATE CASE COMPRESSOR MISSING. DRILLED AND INSTALLED NEW BRACKETS AND INSTALLED NEW PNL. WILL REQUIRE SEALANT INSTALLATION.SDR A6WA201040863Torque Box · crackedLT LOWER CORE COWL CHAFED FROM BLOCKER DOOR NEXT TO FWD LATCHES. BLENDED DAMAGE IAW REO 601R-71-12-232, REV D AND WAS FOUND TO BE WITHIN ALLOWABLE LIMITS DAMAGE MEASURES 4.00 LONG, 0.25 WIDE AND .007 DEEP TREATED AREA IAW CMM 200 AND SRM 51-25-06.SDR CA101123006Actuator · damagedON NR 1 ENGINE, 7 O`CLOCK POSITION THRUST REVERSER ACTUATOR FORK END BROKEN. ACTUATOR REPLACED IAW 78-32-01 AMM. FUNCTIONAL CHECKS COMPLETED.SDR NOCA06910Transcowl · damagedAIRCRAFT IS IN LGA AND IS ON AOG STATUS DUE TO NR 2 ENGINE T/R TRANSLATING COWL DAMAGE IN LGA IS MX REP AND CURRENTLY AT REST UPON ARRIVAL IN LGA FOUND DAMAGE TO NR 2 OUTBOARD T/R TRANSLATING SLEEVE AT THE 5 O'CLOCK POSITION DAMAGE DIMENSIONS ARE 11 INCHES IN
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