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 IXXA20120830019OProximity Sensor · out of adjustDURING TAKEOFF ROLL, RT ENGINE THRUST REVERSE AMBER LIGHT REMAINED ON AFTER FORWARD THRUST WAS SELECTED. THRUST LEVERS WERE ADVANCED AND CREW REJECTED TAKEOFF AT 30 KTS. PERFORMED HIGH ENERGY STOP INSPECTION IAW AMM 05-51-14. ADJUSTED LT CENTER THRUST REVERSDR UALA2012073004102Duct · crackedNR 1 ENGINE INBD THRUST REVERSER C DUCT IS CRACKED AND CHIPS MISSING JUST AFT OF BLEED 7A. CAN BE REPAIRED PER MT 78-10 EPOXY REPAIR. COMPLETED PER MT 78-010.SDR Z6WR201207240014Panel · delaminatedREF CMM 78-31-24, REV 24, 01JUL2012, FIGURE 3, ITEM 675. THE 315A2502-102 BOND PANEL HAS VISUAL DELAMINATION ALONG THE AFT EDGE 6.00 FROM THE LOWER EDGE TO 23.00 FROM THE LOWER EDGE. ULTRASONIC INSPECTION PER NDT MANUAL REVEALS SEVERAL AREAS OF DISBOND THROUSDR Z6WR201207240013Panel · delaminatedREF CMM 78-31-24, REV 24, 01JUL2012, FIGURE 3, ITEM 670. ULTRASONIC INSPECTION PER NDT MANUAL REVEALS SEVERAL AREAS OF DISBOND THROUGHOUT THE ENTIRE NOZZLE END OF THE 315A2502-101 BOND PANEL ASSEMBLY. AREA MEASURES 19.0 X 71.0". AN APPROX 6X6 REPRESENTATIVESDR DALA1243640609Structure · puncturedDURING WALK AROUND MAINTENANCE DISCOVERED TWO PUNCTURES ON LT ENGINE REVERSER COWL INBD AT 4 O'CLOCK POSITION. COMPLIED WITH REPAIR PER SRM 54-31-01. TOUCHED UP PAINT PER AMM 51-21.SDR UALA2012072303958Heat Shield · delaminatedNR 3 ENGINE OTBD THRUST REVERSER HEAT BLANKET DELAMINATED AND HAS HONEYCOMB EXPOSED. OTBD REVERSER REPLACED.SDR Z6WR201207200012Fitting · gougedREF CMM 78-31-37 REV 024 01JUL2012 FIG 19. THE OUTBOARD SURFACE OF THE 315A2311-1 HINGE BEAM (DETAIL PART OF THE 315A2310-1 FITTING ASSY) HAS AN AREA OF MATERIAL WEAR LOCATED 13.0" FWD FROM AFT END OF PART MEASURING 1.20" LONG .21" WIDE. EDDY CURRENT INSPECTSDR UALA2012072003949Rub Strip · wornNR 2 ENGINE INBOARD THRUST REVERSER HALF LOWER FWD COWL FLANGE WHERE RUB STRIP ATTACHES HAS AN AREA WORN 18 INCHES LONG AND A DEPTH HALF THE THICKNESS OF THE FLANGE AND .250 WIDE. REMOVED DAMAGED FLANGE APPROX 27.125 LONG AND 10 INCHES UP FROM BOTTOM. REMOVEDSDR UALA2012071903919Rub Strip · wornNR 2 ENG OUTBOARD HALF REV RUBSTRIP AT 10 O' CLOCK POSITION WORN. FWD OF ENG OIL ACCESS DOOR ON REV AND 12 INCHES UP. REPLACED DAMAGED SECTION OF RUBSTRIP.SDR REXA2012071901171Relay · failedRIGHT THRUST REVERSER WILL NOT RELEASE FROM IDLE AFTER DEPLOYMENT. REMOVED AND REPLACED RELAY IN JB3 DESIGNATOR 2K6KE IAW AMM/CMM 24-01-03 AND WDM 91-32-03. OPS CHECKS AT LEAST 20 TIMES AND NO DEFECTS WERE NOTED.SDR REXA2012071901174Switch · dirtyLEFT THRUST REVERSER WOULD NOT STOW. CLEANED STOW AND DEPLOY SWITCH IAW AMM 20-10-00. PERFORMED OPS CHECK IAW AMM 78-30-00. OPS CHECK GOOD NO DEFECT NOTED.SDR UALA2012071903917Structure · damagedNR 1 OTBD THRUST REVERSER HALF HAS DAMAGE. REMOVED THRUST REVERSER HALF. INSTALLED REVERSER HALF.SDR UALA2012071803884Rub Strip · wornNR 4 ENGINE OTBD THRUST REVERSER HALF AND CORE COWL AT 2 O' CLOCK POSITION RUBSTRIPS WORN. REPLACED RUBSTRIP REF GPM 1-0-8-61 AND 1-0-8-67.SDR FDEA201207182602Actuator · inoperativeSHORTLY AFTER SETTING TAKEOFF PWR, NR 3 THRUST REVERSER CAME ON. ABORTED TAKEOFF & RETURNED TO RAMP. REMOVED AND REPLACED #3 ENGINE O/B UPPER FEEDBACK ACTUATOR AIW ATA/WRI 78-30/2865 AND ATA/WRI 78-30/2869. A/C OK FOR SERVICE. REMOVED AND REPLACED #3 ESDR UALA2012071803882Sleeve · damagedINBD BLOCKER DOOR AT 7 O'CLOCK POS ON NR 2 ENGINE HAS TWO BROKEN SUPPORT FITTINGS AND ONE BENT CONTROL ROD. FOUND ON LANDING. REPLACED NR 2 TRANSLATING SLEEVE PER MM.SDR UALA2012071803892Structure · damagedNR 2 ENGINE INBOARD THRUST REVERSER HALF LOWER FWD COWL FLANGE, WHERE RUB STRIP ATTACHES HAS AN AREA WORN 18 INCHES LONG AND A DEPTH HALF THE THICKNESS OF THE FLANGE AND .250 WIDE. REMOVED DAMAGED FLANGE APPROX 27.125 LONG AND 10 INCHES UP FROM BOTTOM.SDR U2RA201207180012Access Panel · crackedNR 4 ENGINE RT THRUST REVERSER COWL CENTER DRIVE UNIT ACTUATOR ROD END ACCESS PANEL FOUND CRACKED.SDR U2RA201207180013Access Panel · crackedNR 4 ENG LT THRUST REVERSER UPPER AND LOWER BALLSCREW ACTUATOR ROD END ACCESS PANELS FOUND CRACKED.SDR U2RA201207180011Access Panel · crackedNR 1 ENGINE LT TRUST REVERSER BALLSCREW ACCESS PANELS HAS THREE CRACKS.SDR REXA2012071601160Warning Light · false activationON LANDING, USED THRUST REVERSER, STOWED IT, THE LEFT UNLOCK MESSAGE CAME ON. LEFT ENGINE THEN SHUTDOWN WITH THRUST REVERSER LEVER AT IDLE. LEFT INDICATIONS NORMAL EXCEPT REVERSER AND UNLOCK LIGHTS ON. PERFORMED ENGINE RUN IAW AMM 71-00-00 AND OPS CHECKED BSDR REXA2012071401158Thrust Reverser · unknownLEFT THRUST REVERSER INOPERATIVE. INSPECTED LEFT THRUST REVERSER. PERFORMED OPS CHECK, IAW AMM 78-30-00. OPS CHECKED GOOD.SDR REXA2012071400116Unknown · unknownLEFT THRUST REVERSER WOULDN'T DEPLOY. OPS CHECKED LEFT THRUST REVERSER SEVERAL TIMES IAW AMM 78-30-00. NO DEFECTS NOTED, OK FOR SERVICE.SDR REXA2012071101071Thrust Reverser · malfunctionedLEFT THRUST REVERSER INOPERATIVE. PERFORMED OPS CHECK OF LEFT HAND THRUST REVERSER IAW AMM 78-30-00. AIRCRAFT OK FOR SERVICE.SDR UALA2012071203749Actuator · failedLT REVERSER ISOLATION EICAS ON LANDING. LT THROTTLE WILL NOT MOVE. FOUND LT REVERSER HALF NOT STOWED, LOWER ACTUATOR AFT ATTACH HARDWARE MISSING, CHECKED THROTTLES FOUND NO BINDING AND FREE MOVEMENT. LOWER ACTUATOR REPLACED. OPS AND LEAK CHECKS GOOD. AIRCSDR UALA2012070503585Rub Strip · damagedNR 3 ENGINE LEFT REVERSER REAR RUBSTRIP WORN AND CRACKED. SUPPLEMENTAL DATA UPDATE, REMOVED DAMAGED RUB STRIP ON NR 3 ENG LT REV HALF. COMPLETED REMOVAL OF NR 3 ENG REV UP TO STEP F.(5) PER MM. NEED TO CONTINUE FROM STEP F.(6) PER MM. CONTINUED FROM STEP 2SDR U2RA201207120001Bracket · crackedNR 3 ENGINE THRUST REVERSER FWD TORQUE BOX BULKHEAD AFT SURFACE AT 2 O`CLOCK POSITION ONE BRACKET CRACKED, CRACK LENGTH .7".SDR J7SA20120628001Control Unit · failedAMBER REVERSER LIGHT CAME ON INFLIGHT. RETURNED TO DEPARTURE. REPLACED RT THRUST REVERSER HYD CONTROL UNIT.SDR REXA2012062701024Pdu · malfunctionedRIGHT THRUST REVERSER DID NOT FULLY DEPLOY AND WILL NOT STOW. CHECKED RIGGING OF STOW, DEPLOY AND THROTTLE LOCKOUT SWITCHES IAW AMM 78-37-01. ALL GOOD. INSPECTED THRUST REVERSER PDU, PDU WILL NOT MANUALLY OPERATE. REMOVED AND REPLACED PDU IAW 78-32-03. VESDR REXA2012062701025Pdu · failedLEFT THRUST REVERSER INOPERATIVE. REMOVED AND REPLACED LEFT THRUST REVERSER PDU IAW AMM 78-32-03. OPS CHECKED GOOD. OK FOR SERVICE.SDR UALA2012062903462Seal · brokenUPPER AFT SECTION OF STAINLESS STEEL REV TO PYLON SEAL BROKEN AND MISSING, 2.5 IN LONG BY 3 IN SECTION OF SEAL AFT END. NUMBER 2 ENGINE INBOARD SIDE. REPLACED SEAL SECTION.SDR SWIA201231073Switch · failedLEFT REVERSE UNLOCK MESSAGE. (FLT 5557) REPLACED LEFT THRUST REVERSER STOW MICROSWITCH IN REFERENCE TO AMM.SDR DXTA2012061805001Warning Light · illuminatedRIGHT THRUST REVERSER UNLOCK LIGHT ILLUMINATED IN FLIGHT. PERFORMED THRUST REVERSER RT OPS TEST. OPS TEST GOOD. NO DEFECTS NOTED. SERVICED FLIGHT HYD SYS TO FULL, REMOVED HYD PWR FROM ACFT. SYS, OPS CHECKS GOOD. REF G-IV CMP 783010 AND MM 78-00-0, WDSDR AALA20120615012Hinge · crackedNUMBER 1 ENGINE INBOARD THRUST REVERSER HINGE HAS A CRACK IN THE AFT UPPER MOUNT HOLE. OVER SIZED HOLE AND INSTALLED FREEZE PLUG PER EA B757-54-024386.SDR Z6WR201206130010Blade · crackedREF CMM 78-31-37 REV 23 01MAR2012 FIG 25 ITEM 290. THE 315A2233-14 OUTER V-BLADE HAS A VISUAL CRACK MEASURING 7.25 LONG.SDR REXA2012061100834Control Lever · malfunctionedON LANDING, LEFT THRUST REVERSER LEVER DIFFICULT TO UNLOCK TO SPOOL REVERSE THRUST. MUST RELEASE BUTTON AFTER THRUST REVERSER UNLOCKS THEN PULL LEAVER UP WHICH IS ABNORMAL. OPS CHECKED GOOD OF LT THRUST REVERSER IAW AMM 78-30-00. OK FOR SERVICE.SDR UALA2012061103192Actuator · failedREVERSER FAULT DISPLAYED ON UPPER ECAM SCREEN. NO PROBLEMS FOUND. REPLACED UPPER NO LOCKING ACTUATOR. REMOVED AND REPLACED AND RIG. REPLACED ACTUATOR.SDR REXA2012060700820Warning Message · false activationRT THRUST REVERSER UNLOCK MESSAGE IN FLIGHT AND DID NOT DEPLOY ON LANDING. OPS CHECK RT THRUST REVERSER IAW AMM 78-30-00. OPS CHECK GOOD.SDR REXA2012060500821Switch · inoperativeLT THRUST REVERSER WILL NOT STOW. REMOVED AND REPLACED LT THRUST REVERSER STOW SWITCH IAW AMM 78-37-01. OPS CHECKS GOOD.SDR Z6WR0092012Ring Assembly · wornONE BACB30LE6K29 BOLT COMMON TO THE AFT HOLE OF THE ,315A2222-5 CASCADE SUPPORT RING, AND THE ,315A2310-1 LATCH BEAM, WAS VISUALLY FOUND TO BE LOOSE. AFTER BOLT REMOVAL, 2EA HOLES FOR 2EA, BACB30LE6K29 BOLTS, MEASURE; FWD HOLE C/T, 315A2310-1 BEAM = .3762 WITSDR IXXA20120604013Warning Light · false activationREJECTED TAKEOFF, ENGINE THRUST REVERSE AMBER LIGHT DISPLAYED DURING FWD THRUST. FAULT CODE 78-36-04-02. TROUBLESHOT IAW FIM PROCEDURE 78-36 FAULT TREE 806 AND PSEU BITE CHECK 32-09-03. SYS CHECKED OK.SDR A6WA201240582Diode · failedRECEIVED RT THRUST REVERSER UNLOCK CAUTION MESSAGE, TESTED AFTER ROTATION INDICATION ONLY. NO PERFORMANCE CHANGE. COMPLIED WITH QRH MESSAGE PERSISTED. R & R DIODE MODULE TB207-7-2CR7KE IAW WIRE MANUAL 78-30-00. THRUST REVERSERS OPS CHECKED GOOD IAW 78-30-0SDR UALA2012060303067Blocker Door · crackedNR 2 ENGINE INBOARD, TR PANEL ASSY BETWEEN L5 AND L6 BLOCKER DOORS CRACKED. REPLACED NR 2 ENGINE INBOARD, TR PANEL ASSY BETWEEN L5 AND L6 BLOCKER DOORS.SDR UALA2012060303057Door · damagedNR 4 ENG THRUST REVERSER DEACTIVATION DOOR HAS CRACK COMING FROM UPPER SCREW HOLE. NO CRACK FOUND, UPPER FASTENER HOLE WORN AND OVERSIZED. INSTALLED FLUSH WASHER IN DAMAGED HOLE. REINSTALLED PANEL.SDR 2012FA0000386Thrust Reverser · bindingDURING TAXI OUT, SUBSEQUENT TO THRUST REVERSER AND ANTI-ICE OPS CHECKS, THRUST REVERSER ON RT ENGINE FAILED TO DEPLOY WHEN COMMANDED. RETURNED TO HANGAR AND FOUND KNOB LOCK JAMMED. MANUALLY CRANKED T/R TOWARDS OPEN/DEPLOYED DIRECTION AND LOCK FREED UP. OPS CHSDR UALA2012053103029Warning Message · false activationNR 2 ENGINE THRUST REVERSER FAULT DISPLAYED ON UPPER ECAM SCREEN. CHECKED ROOT FAULT PER AMM 70-00-00 P301 ON MCDU WITH FADEC SWITCH ON. ACCOMPLISHED TEST OF THE NR 2 ENGINE THRUST REVERSER SYSTEM THRU THE MCDU, FOR BOTH CHANNEL A AND B. TEST PASSED. FAULTSDR CVGA20120530002Switch · failedAFTER LANDING, THE LEFT THRUST REVERSER DEPLOYED AND STOWED SEVERAL TIMES BEFORE FINALLY STAYING DEPLOYED.SDR UALA2012052903009Bushing · missingNR 1 ENGINE, LT THRUST REVERSER, NR 1 (TOP) BLOCKER DOOR MISSING 2 BUSHINGS THROUGH BLOCKER DOOR SPRING. REPLACED BUSHINGS AND HARDWARES PER MT 78-011 ON WU P4439G. OPS CHECKED GOOD.SDR UALA2012052903008Spacer · missingNR 1 ENG, LT THRUST REVERSER, NR 2 (FROM TOP) BLOCKER DOOR MISSING 2 BUSHINGS THROUGH BLOCKER DOOR SPRING. REPLACED SPACERS AND BUSHINGS PER MT 78-011 ON WU P4440G.SDR UALA2012052903007Bolt · faultyNR 1 ENGINE, THRUST REVERSER, NR 3 (FROM TOP) BLOCKER DOOR MISSING 2 BUSHINGS THROUGH BLOCKER DOOR SPRING. REPLACED BOLT AND SPACERS AND BUSHINGS PER MT 78-011 ON WU P4441G.SDR UALA2012053103033Actuator · malfunctionedNR 1 ENGINE THRUST REVERSER FAULT ECAM AFTER TAKEOFF. STARTED ACTUATOR DISCONNECT NR 1 ENGINE LEFT UPPER NON LOCKING ACTUATOR. GOT AS FAR AS STEP NR 4E3. CONNECTOR ON NR 1 ENGINE HAS PUSHED BACK PIN CONN IS 4005VC-A AND IT'S PIN 4. REPLACED CONNECTOR REF
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