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 REXA2012052900793Unknown · unknownRIGHT THRUST REVERSER WILL NOT DEPLOY. PERFORMED OP`S CHECK OF RIGHT THRUST REVERSER IAW AMM 78-30-00. NO DEFECTS NOTED. OK FOR SERVICE.SDR A6WA201240575Warning Message · illuminatedON CLIMB OUT, RECEIVED RT THRUST REVERSER UNLOCK MESSAGE. COMPLIED WITH QRH, SELECTED EMERGENCY STOW, RT THRUST REVERSER UNLOCK MESSAGE PERSISTS, WITH THRUST LEVER AT IDLE, FELT SLIGHT VIBRATION IN AIRFRAME, NO ABNORMAL N1 OR N2 VIBRATION INDICATIONS. VIBRATSDR IU6R20120525Control Valve · crackedCONTROL VALVE HAS A BROKEN CRACKED AND PIN HOLE FOUND ON HOUSING.SDR DALA1701450665Thrust Reverser · damagedTHRUST REV DAMAGED NR 1 ENGINE ON TRAILING EDGE APP 9 OCLO POS, REPAIRED IAW SRM 54-31-01.SDR DALA1233450665Structure · damagedMAINTENANCE DISCOVERED DAMAGE TO THE NR 1 THRUST REVERSER ON THE TRAILING EDGE APPROXIMATELY 9 O'CLOCK POSITION. PERFORMED REPAIR AND INSPECTED PER SRM 54-31-01.SDR UIEA2012052100248Access Panel · damagedDURING MX WALKAROUND OF ACFT AT PVG REVEALED NR 3 ENGINE THRUST REVERSER ACCESS DOOR WAS FOUND OPEN AND DAMAGED. ACCOMPLISHED A TIME LIMITED REPAIR.SDR A6WA201240557Attach Fitting · gougedPANEL 444AB GOUGED ON INBD ATTACH FITTING. REPAIR GOUGE ON PANEL 444AB ATTACH FITTING IAW REO 601R-78-33-3992, REV NC.SDR A6WA201240558Attach Fitting · gougedPANEL 444AT GOUGED IN INBD SIDE ATTACH FITTING. REPAIR GOUGE ON INBD SIDE ATTACH FITTING IAW REO 601R-78-33-3992 REV, NC.SDR REXA2012051700743Unknown · malfunctionedLEFT THRUST REVERSER DOES NOT DEPLOY. PERFORMED OPS CHECK ON LEFT THRUST REVERSER IAW AMM 78-30-00. OPC GOOD.SDR REXA2012051600739Thrust Reverser · inoperativeRIGHT THRUST REVERSER INOP. DEFERRED PER MEL 78-30-01.SDR REXA2012051400731Switch · failedRIGHT THRUST REVERSER NOT DEPLOYING, DEFER OUTBOARD IAW MEL 78-30-01 AUT NR 63568. REMOVED AND REPLACED DEPLOY SWITCH IAW AMM 78-37-01. OPS CHECK GOOD, CLEAR DM X63568 PLACARD REMOVED.SDR REXA2012051400728Switch · dirtyLT ENGINE THRUST REVERSER WOULD NOT ENGAGE OR DEPLOY. CLEANED DEPLOY SWITCH, PERFORMED OPS CHECK IAW AMM 78-30-00. OK FOR SERVICE.SDR REXA2012051300727Lever · dirtyLEFT THRUST REVERSER LEVER STICKY, FEELS TIGHT MAKES IT MORE DIFFICULT TO DEPLOY. INSPECTED AND CLEANED LEFT THRUST REVERSER LEVER. LEVER IS NOW EASIER TO MOVE. NO FURTHER DEFECTS NOTED.SDR REXA2012051000721Pdu · failedLEFT THRUST REVERSER WOULD NOT DEPLOY ON LANDING. LEFT REVERSER ARM STATUS MESSAGE POSTED AS NORMAL YELLOW REVERSER INDICATION APPEARED IN N1 BUT REV WOULD NOT DEPLOY, REMOVED AND REPLACED PDU IAW AMM 78-32-03. OPS CHECKED GOOD.SDR REXA2012051000718Thrust Reverser · malfunctionedLEFT THRUST REVERSER WILL NOT DEPLOY. PERFORMED OPERATIONAL CHECK OF LT TRUST REV IAW AMM 71-00-00. ALL CHECKED GOOD. AIRCRAFT OK FOR SERVICE.SDR REXA2012051000717Thrust Reverser · malfunctionedLEFT THRUST REVERSER WOULD NOT DEPLOY ON LANDING. PERFORMED MUTIPLE OPERATIONAL CHECKS, COULD NOT DUPLICATE. OPS CHECKED GOOD IAW AMM 78-30-00. OK FOR SERVICE.SDR Z6WR20120510008Panel · debondedULTRASONIC INSPECTION IAW NDT MANUAL REVEALS THE THRUST REVERSER 315A2101-141 INNER WALL HAS AN AREA OF DISBOND 1.8 X 2.0" LOCATED 18.5" FROM AFT EOP AND 6.0" FROM UPR EOP IN THE FOOT PRINT OF THE NR 3 UPPER COMPRESSION PAD. VISUAL AREA OF DISCOLORATION C/T 3SDR Z6WR0072012Ring Assembly · wornREF: CMM 78-31-37, 01MAR2012, REV 023 INSPECTION FINDING OF (2) MISSING BACB30LE6K29 BOLTS (FIGURE 12, ITEM 100) NOTES THE FOLLOWING RELATED DISCREPANCIES. A) FIGURE 12, ITEM 115 AREA OF MATERIAL WEAR MEASURING .9240 LONG X .2125 WIDE X .0465 DEEP ON THE 315SDR DALA1230873209Ring · gougedDURING INSPECTION, FOUND LT ENGINE OTBD THRUST REVERSER 9 O'CLOCK TO 12 O'CLOCK JAY RING GOUGED AND HAS FRETTING DAMAGE. REPLACED LT ENGINE OTBD THRUST REVERSER JAY RING IAW CMM 78-32-35. ADJUSTED LT ENGINE RING IAW AMM 78-36-42-820-001.SDR REXA2012050800614Unknown · malfunctionedLEFT THRUST REVERSER WOULD NOT DEPLOY AFTER LANDING. T/S PER FIM 78-30-00. PERFORMED OPS CHECK OF LEFT THRUST REVERSER IAW GROUND RUN MANUAL 71-00-00. OPS CHECK GOOD.SDR EE4Y201205060182Frame · corrodedENGINE NR 1 INBD THRUST REVERSER LOWER ACTUATOR, FWD FRAME BORE WAS FOUND WITH CORROSION.SDR EE4Y201205060183Frame · corrodedENGINE NR 2 OTBD THRUST REVERSER UPPER ACTUATOR, FWD FRAME BORE WAS FOUND WITH CORROSION.SDR EE4Y201205060184Frame · corrodedENGINE NR 2 INBD THRUST REVERSER LOWER AND UPPER ACTUATORS, FWD FRAME BORES WERE FOUND CORRODED.SDR EE4Y201205060185Frame · corrodedNR 1 ENGINE OTBD THRUST REVERSER UPPER ACTUATOR FWD FRAME BORE WAS FOUND CORRODED.SDR UALA2012050302619Actuator · leakingNR 2 OTBD THRUST REVERSER COWL OPEN ACTUATOR LEAKING. REPLACED ACTUATOR.SDR 2012F00098Skin · damagedINSPECTION OF THE LT AND RT THRUST REVERSER ASSEMBLIES, FOUND THE RT TORQUE BOX SKIN TO HAVE NUMEROUS CRACKS AND 1 LARGE TRIANGULAR PIECE BROKEN OUT, AND THE LT TORQUE BOX TO HAVE CRACKS IN THE SKIN ALONG THE EDGE OF THE INBD BLOCKER DOOR HOUSING. FURTHER INSSDR REXA2012050300608Thrust Reverser · malfunctionedAFTER LANDING COULD NOT STOW LEFT THRUST REVERSER. UNLOCK LIGHT ILLUMINATED. OPS CHECKED GOOD AT THIS TIME REF AMM 78-30-00.SDR REXA2012050200605Switch · failedNR 2 ENGINE THRUST REVERSER WILL NOT ENGAGE OR DEPLOY ON LANDING. REMOVED AND REPLACED RT ENGINE THRUST REVERSER DEPLOY SWITCH IAW 78-37-01. FOUND OLD DEPLOY SWITCH TO BE INTERMITTENT. OPS TESTED GOOD.SDR REXA2012050100604Switch · dirtyRIGHT THRUST REVERSER WILL NOT STOW. CLEANED STOW SWITCH. OPS CHECKED GOOD.SDR CA120504010Valve · malfunctioned(CAN) IN CRUISE, ENGINE NR 2 REVERSER PRESSURE LIGHT ILLUMINATED IAW AOM PROCEDURE, CREW PERFORMED A PRECAUTIONARY SHUTDOWN AND RETURNED TO DEPARTING STATION. MAINTENANCE REPLACED THE OVER PRESSURE INLET SHUTOFF VALVE AND THE ACFT WAS RETURNED TO SERVICE.SDR REXA2012042900577Unknown · malfunctionedLEFT TR WOULD NOT DEPLOY ON LANDING. LEFT TR CHECKS GOOD IAW AMM 78-30-00.SDR SIMA20120426009Thrust Reverser · crackedDURING 2C CHECK FOUND LEFT ENGINE LOWER I/B CASCADE CRACKED AND MISSING A FIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW CASCADE IAW CRJ AMM TASK 78-34-01-400-801. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR REXA2012042500569Switch · miswiredRIGHT THRUST REVERSER WOULD NOT DEPLOY. FOUND DEPLOY SWITCH INCORRECTLY WIRED. REWIRED IAW WDM 78-30-00 AND PERFORMED OPS CHECK IAW AMM 78-30-00, OPS CHECKED GOOD.SDR 2012FA0000237Pressure Switch · shortedNR 1 THRUST REVERSER "ARM" LIGHT ILLUMINATED CONTINUOUSLY, WITH ENGINES SHUTDOWN. THE FAULT LIES IN THE ARM LIGHT PRESSURE SWITCH. INSTALLING A NEW SWITCH FIXED THE PROBLEM.SDR USAA2012042000014Hinge Fitting · damagedRIGHT OUTBOARD AFT THRUST REVERSER HINGE FITTING HAS PYLON LOWER BOLT HOLES AT PPS 174, PPWL 145. HOLES REAMED AND NEW FITTINGS INSTALLED IAW US AIRWAYS EA 103807B AND US AIRWAYS EO 5408R114 REV C.SDR UALA2012041302244Sleeve · damagedDURING NR 1 ENGINE INBOARD BLISTER FAIRING REPAIR PER MAINT TIP 78-014A ACCIDENTALLY DRILLED THE BEAM FITTING LOCATED BELOW THE FAIRING. NR 1 ENGINE THRUST REVERSER SLEEVE REPLACED PER MM. SYS OPS AND INSTALL OK NORMAL.SDR R61A201204100239Actuator · corrodedWHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE NR 2 ENG (RT) OUTBOARD T/R FEEDBACK ACTUATOR MOUNTING GIMBAL BUSHING AND HARDWARE. MAINTENANCE REMOVED AND REPLACED THE FEEDBACK ACTUATOR ON THE NR 2 ENG (RT) OUTBOARD T/R IAW EMB 170-ESDR REXA2012041000493Switch · failedRIGHT THRUST REVERSER WOULD NOT DEPLOY ON LANDING. REMOVED AND REPLACED RT THRUST REVERSER DEPLOY SWITCH IAW AMM 78-37-01. OPS CHECKED GOOD, OK FOR SERVICE.SDR ZESA20120420001Switch · out of adjustRT ENGINE THRUST REVERSER ARM AND HYD PRESS ANNUNCIATOR CAME ON IN FLIGHT DURING CLIMB. INSPECTION FOUND SWITCH TO BE ON THE EDGE OF ADJUSTMENT FOR ACTIVATION.SDR USAA2012041300006Proximity Sensor · faultyCREW REPORTED ENGINE 2 REVERSER FAULT ON LANDING WHEN THRUST REVERSERS WERE SELECTED ON. DEACTIVATED NR 2 THRUST REVERSER AND PLACED ON MEL. REPEATED FAULTS2. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE EEC (ELECTRONIC ENGINE CONTROL) AND NR 2 T/R LOCK PROXSDR USAA2012041300005Eec · faultyCREW REPORTED ENGINE 2 REVERSER FAULT ON LANDING WHEN THRUST REVERSERS WERE SELECTED ON. DEACTIVATED NR 2 THRUST REVERSER. REPEATED FAULTS. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE EEC AND NR 2 THRUST REVERSER LOCK PROXIMITY SENSOR IAW MM 78-31-15-400.SDR WX0A071151Control Valve · leakingFLIGHT CREW PERSONNEL REPORTS ALL FLIGHT ATTENDANTS REPORT SMOKEY SMELL IN CABIN. MAINTENANCE PERSONNEL FOUND APU SUCKING SKYDROL IN DUE TO A LEAK ON LEFT THRUST REVERSER CONTROL VALVE. REPLACED CONTROL VALVE IAW MM 78-31-02, OPS AND LEAKS CHECK GOOD. AIRCRSDR U2RA2012041045301Stiffener · crackedLEFT THRUST REVERSER TORQUE RING STIFFENER HAS A .5 INCH CRACK. REPLACED STIFFENER ON LT THRUST REVERSER TORQUE BOX IAW ACFT MM 20-11-00/201.SDR DHLA201200005Warning Light · false activationON CLIMB OUT, NR 4 THRUST REVERSER LIGHT ILLUMINATED. RAN THRUST REVERSER EMERGENCY STOW CHECKLIST. LIGHT REMAINED ILLUMINATED. RAN ABNORMAL IN FLIGHT ENGINE SHUTDOWN AND SHUTDOWN ENGINE. WINDMILLED OIL PRESSURE JUST ABOVE 0 PSI AND SHUTDOWN FOR APROX 10 MSDR UALA2012040402095Sleeve · out of positionGAP BETWEEN ENGINE THRUST REVERSER SLEEVE AND FAN COWLING. NR 1 ENGINE APPROX 7 O'CLOCK POSITION. REPAIRED RUB STRIP. STILL MISMATCHED BY 070. OK PER MT 71-031 AND AMM 71-10-00-607 FOUND THAT .070 INCH UNDERFAIR (OUT OF WIND) TO BE ACCEPTABLE. THE REVERSSDR 2012FA0000172Paddle · missingPILOT REPORTED THAT THAT THE NR 1 (LT) THRUST ATTENUATOR PADDLE WAS NOT PRESENT WHEN HE PERFORMED HIS POST FLIGHT INSPECTION. INSPECTION BY MX REVEALED THAT THE THRUST ATTENUATOR PADDLE HAD BROKEN OFF IN A CIRCUMFERENCE SURROUNDING THE ATTACHMENT FASTENERS. SDR UALA2012032901964Ring · gougedNR 2 ENGINE OUTBD CASCADE SUPPORT RING GOUGED AT VARIOUS LOCATIONS ON INNER SURFACE. REMOVED DAMAGED RING ASSY. REPLACED RING ASSY.SDR 2012FA0000278Bracket · crackedTHRUST REVERSER WOULD NOT INDICATE EXTENDED. FOUND BRACKET THAT HOLDS THE RETRACT AND EXTEND SWITCHES TO BE CRACKED AROUND THE EXTEND SWITCH WHICH ALLOWED THE SWITCH TO MOVE WHEN THE THRUST REVERSER CONTACTED IT DURING EXTENSION. CAUSE APPEARS TO BE CRACKINGSDR USAA2012032800006Shutoff Valve · faultyENGINE 1 REVERSER FAULT AFTER LANDING. REMOVED AND REPLACED NR 1 ENGINE HCU SHUTOFF VALVE IAW AIRBUS MAINTENANCE MANUAL 78-37-51.SDR USAA2012032600028Bracket · defectiveENGINE 1 REVERSER FAULT ON LANDING. REFERENCE SDR USAA2012031900031 FOR PREVIOUS T/R FAULTS ON NR 1 ENGINE. SUBSEQUENT T/R FAULTS HAVE ALSO BEEN REPORTED ON 3/24 & 3/25. AIRCRAFT CONTINUED TO EXPERIENCE SAME FAULTS. REMOVED AND REPLACED NR 1 ENGINE TERMINA
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