JASC 7830
Service difficulty reports · 5,915
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 SWIA202054260Cascade · crackedLT LOWER TR CASCADE ASSEMBLY HAS EVIDENCE OF CRACK IN ONE VANE AT INBOARD SIDE OF ASSEMBLY. C-CHECK RO 11/21/2020. REMOVED LT LOWER TR CASCADE ASSEMBLY, AS PER CRJ 200 AMM & INSTALLED NEW LT LOWER TR CASCADE ASSEMBLY, AS PER CRJ 200 AMM.SDR AALA202010019001Switch · inoperativeAIRCRAFT WAS NOT GROUNDED: SHORTLY AFTER SETTING FLEX POWER, INDICATION THAT THE #1 ENGINE THRUST REVERSER WAS UNLOCKED WITH REVERSE THRUST ENGINE NOISE. REJECTED TAKEOFF IMMEDIATELY BELOW 60 KNOTS. REPLACED BLOCKER DOOR STOW SWITCH IN LOWER RIGHT 4104KS2 POSISDR IPXA2020101061145Angle · crackedINSPECTION TYPE: 2C NR 2 ENGINE LT T/R FWD CASCADE FRAME SUPPORT ANGLE CRACKED AT 9 O`CLOCK POSITION. REPLACED CRACKED ANGLE AT NR 2 ENGINE LT T/R FWD FRAME SUPPORT, IAW SRM 51-31-01 (MINOR).SDR IPXA2020100661023Stiffener · crackedINSPECTION TYPE: 2C NR 3 ENGINE OUTBOARD T/R FAS A SUPPORT BRACKET/STIFFENER CRACKED AT THE 4 O'CLOCK POSITION. REMOVED AND REPLACED STIFFENER, IAW SRM 54-01-42. (MINOR)SDR ASAA2020092433217Switchpack · inoperativeNR 1 ENGINE T/R LIGHT ON. GROUNDED-YES. REMOVED AND REPLACED LT AUTOTHROTTLE SWITCHPACK ASSEMBLY, IAW B737-800 AMM 76-11-07-020-802-F00 AND 76-11-07-400-802-F00. OPS CHECK GOOD, IAW B737-800 AMM 76-11-07-400-802-F00 PARAGRAPH I.SDR ABXA20200803181Warning Light · illuminatedLEFT REVERSER ISOLATION VALVE LIGHT AND EICAS MESSAGE. AIRCRAFT BACK TO BLOCK AND GROUNDED. REVERSER WAS DEFERRED AND A/C RELEASED FOR FLIGHT.SDR T17A20200811041Angle · crackedRIGHT TR FAN DUCT ANGLE CRACKED. REMOVED AND REPLACED TR FAN DUCT ANGLE, IAW HAWKER 400XP CMM 78-30-07.SDR AALA202009239011Switch · inoperativeAIRCRAFT WAS NOT GROUNDED. ENGINE 1 REVERSER UNLOCK DURING TAKEOFF ROLL AT 40 KNOTS, NORMAL DECELERATION WITH MANUAL BREAKING. REPLACED BLOCKER DOOR DEPLOY SWITCH, REF AMM 78-31-17-000-001-A AND 78-31-17-400-001-A.SDR UIEA2020092512027Sealant · deterioratedNR 2 ENGINE INBOARD AND OUTBOARD T/R COWLING INNER SIDE PROTECTOR HEAT SEALANT IS DETERIORATED, MISSING IN SEVERAL AREAS. PREPARED, CLEANED, AND REPAIRED PROTECTOR HEAT SEALANT NR 2 ENG INBOARD AND OUTBOARD T/R COWLING INNER SIDE, PER B767-300 AMM 78-31-00-30SDR AWKA2020100201Switch · failedWHILE ENROUTE TO VNY, FLIGHT CREW RECEIVED A CYAN LEFT REVERSER UNLOCK FAULT CAS MESSAGE. CREW CONSULTED WITH MX CONTROL AND BOMBARDIER TECH SUPPORT VIA SAT PHONE, AND WAS ADVISED THAT IT’S LIKELY A MALFUNCTIONING MICROSWITCH, AND THAT THERE ARE NO OTHER INDISDR T17A202008141038Fairing · crackedLT LOWER TR DOOR INBOARD FAIRING ANGLE CRACKED. REPAIRED ANGLE BY INSTALLATION OF DOUBLER IAW BEECHJET 400XP CMM CH 78-30-07 REPAIR NR 16.SDR IPXA2020091196038Support Angle · damagedINSPECTION TYPE: A 300 NR 2 OUTBOARD TR LOWER FWD ANGLE SUPPORT FOR RUB STRIP HAS CHOFING MARKS. REMOVED & REPLACED REPAIR FILLER, IAW SRM 51-40-21.SDR IPXA2020091196037Support Angle · damagedINSPECTION TYPE: A 300 NR 2 ENG INBOARD TR LOWER FWD ANGLE SUPPORT FOR RUB STRIP HAS CHOTING MARKS. REMOVED & REPLACED REPAIR FILLER, IAW SRM 51-40-21.SDR 2020F00413Duct · gougedAIRBORNE/PEMCO NON-ROUTINE 2911N98 (3022.0098) DISCREPANCY: NR 2 ENGINE INBOARD T/R BIF-DUCT HAS 2 GOUGES ON AFT OUTER SLEEVE. CORRECTIVE ACTION: EVALUATED NR 2 ENGINE INBOARD TR BIF-DUCT AFT OUTER SLEEVE MATERIAL REMAINING AT LOWEST POINT .044", MAX ALLOWABLSDR ABXA2020091183175Warning Message · false activationREV ISOLATION VALVE CAUTION LEFT ENGINE AFTER ENGINE START. AIRCRAFT BACK TO BLOCKS. AIRCRAFT WAS GROUNDED WHILE TROUBLESHOOTING. RECYCLED C/B, OPS CHECKED GOOD IAW B767 MM 78-31-00 REMAINS CAT 111B.SDR P5CA2020083170290Relay · malfunctionedREJECTED TAKEOFF AT 35 KNOTS FOR ENGINE 2 REV STATUS MESSAGE REMAINED.DMI 133482 RAISED, MEL 78-31-01A APPLIED, CAT 'C'. MAINT PROCEDURES CARRIED OUT. R/R RELAY IAW AMM 78-36-07. OPS CHECK GOOD.SDR SWAA2020083111315Warning Light · false activationL THRUST REVERSER UNLOCK ILLUMINATED IN FLT. PERFORMED QRH PROCEDURE AND ENGINE SHUTDOWN CHECKLIST / NO FAULTS FOUND ON THE E.A.U. OK TO CONTINUE PER M.E.L. 78-1-01 SP1, SP1A AND SP78, AIRCRAFT IS DOWNGRADED TO CAT I STATUS TRK#50076SDR SWIA202008252074Structure · chafedENG 2 INBD UPPER BEAVER TAIL, FRAME AND COMPOSITE ARE CHAFED. REPAIRED THE NR 2 UPPER I/B BEAVER TAIL IAW CMM.SDR SWIA202008252073Structure · chafedENG 2 OTBD UPPER BEAVER TAIL, FRAME AND COMPOSITE ARE CHAFED. REPAIRED THE NR 2 UPPER O/B BEAVER TAIL IAW CMM.SDR SWIA202008252072Frame · chafedENGINE 1 UPPER INBD BEAVER TAIL, COMPOSITE AND FRAME ARE CHAFED. REPAIRED THE NR 1 UPPER I/B BEAVER TAIL IAW CMM.SDR IPXA2020081859189Actuator · damagedFOUND DAMAGE ON THE NR 1 ENGINE THRUST REVERSER UPPER ACTUATOR CLEVIS FITTING REF DEFERRAL M 716678. EO B767-7830-77544A C/W. PLACED ON DEFERRAL PER EO B767-7830-77544-A. REMOVED TRANS NR 1 ENG OUTBOARD TRANSCOWL, IAW AMM 78-1-10-401. INSTALLED TRANSCOWL UPSDR U2RA202009200012Skin · delaminatedWHILE ACCOMPLISHING TASK CARD 71-830-01-02 FOUND NR 2 ENGINE INBOARD T/R EXTERNAL AND LOWER SURFACE HAVE DELAMINATION ABOUT 3". REPAIRED PER VT-SAA EA 747-5430-56-A8486 REV A.SDR UIEA2020081329648Angle · crackedNO.4 ENG R/H T/R FWD WEB ANGLE FOR PLASTIC RUB STRIP UPPER CORNER CRACKED.(<P>REPAIRED AS PER MRAS CMM 78-32-02 REPAIR 040 REV.59</P>)SDR UIEA202008120737Quick Disconnect · leakingDURING PRE-FLIGHT INSPECTION, FOUND OIL POOLING UNDER NR 2 ENGINE. SECURED THE NR 2 ENGINE QUICK DISCONNECT T/R FITTING IAW MM 71-11-04. OPS CHECK OK.SDR SWAA2020081107734Thrust Reverser · leakingCREW REPORTED ON REVERSE THRUST, LIGHT SMOKE WAS OBSERVED IN THE CABIN, WITH A ACCOCIATED ODOR. FIRE CREW REPORTED SMOKE OUT OF THE NR 2 ENGINE TAIL PIPE ON SHUTDOWN. PERFORMED CONDITIONAL INSPECTION IAW AMM 05-51-56.SDR U2RA202009190006Stop Fitting · gougedWHILE ACCOMPLISHING A VISUAL INSPECTION FOUND NR 3 ENGINE OUTBOARD T/R INTERIOR SIDE UPPER, FWD STOP FITTING IS GOUGED AND HAS DAMAGED HI-LOCK FASTENER. REPAIRED PER VT-SAA EA 747-5400-56-A8511 REV A.SDR U2RA202009190005Stop Fitting · gougedWHILE ACCOMPLISHING A VISUAL INSPECTION, FOUND NR 1 ENGINE OUTBOARD T/R INTERIOR SIDE UPPER STOP FITTING HAS GOUGES. REPAIRED PER VT-SAA EA 747-5400-56-A8502 REV A.SDR IPXA2020081218942Bracket · crackedINSPECTION TYPE: SEG, NR 2 ENGINE INBD THRUST REVERSER DOOR HYD ACTUATION CONNECTION FITTING BRACKET CRACKED. REMOVED AND REPLACED IAW AMM 78-36-02-0401.SDR IPXA2020081218941Bracket · brokenINSPECTION TYPE:SEG#2 ENG O/B T/R HYD ACTUATION CONNECTION BRACKET BROKENREMOVE AND REPLACE BRACKET IAW AMM 78-36-02-0401.SDR IPXA2020081158937Bracket · crackedINSPECTION TYPE: SEG, NR 1 ENGINE OTBD THRUST REVERSER DOOR HYDRAULIC ACTUATION CONNECTOR FITTING BRACKET WAS CRACKED. REMOVED AND REPLACED IAW AMM 78-36-02-0401.SDR IPXA2020080548631Angle · damagedNR 1 ENGINE INBD THRUST REVERSER COWL AFT UPPER FWD CUTOUT CORNER METAL SUPPORT DAMAGED. INSTALLED A NEW WEAR ANGLE IAW SRM 51-40-20.SDR IPXA2020080548630Doubler · gougedNR 1 ENGINE INBD THRUST REVERSER COWL AFT UPPER FWD CUTOUT DOUBLER. REPAIRED HAS DEEP GOUGE. INSTALL NEW DOUBLER IAW SRM 51-40-21.SDR ABXA20200803155Vane · departed#2 ENG THRUST REVERSER CASCADE VANE DEPARTED AIRCRAFT ON LANDING. AIRCRAFT WAS GROUNDED.SDR HALA2020073100161Pcu · malfunctionedETOPS SIGNIFICANT SYSTEM - DURING 14 DAY CHECK, FOUND ENG 2 REV FAULT ON THRUST REVERSER CYCLE. DURING TROUBLE SHOOTING, FOUND FAULT CODE 783751, T LOCK (E2-
4005EG1 1/2/3/4) PCU (EG4007EG) BLOCKER DOORS 1 & 2 UPPER RIGHT AND LOWER RIGHT. REMOVED AND SDR IPXA2020073058413Thrust Reverser · gougedNR 2 ENGINE I/B THRUST REVERSER FWD EDGE LOWER SIDE GOUGED. FABRICATED A FILLER IAW SRM 51-4-21.SDR IPXA2020072978316Plate · wornINSPECTION TYPE:A300ENG #2 O/B TR INNER BARREL UPPER BIFURCATION UPPER EDGE AFT SIDE METAL PLATE WORN & TORNREMOVED & REPLACED RUB STRIP & WEAR ANGLE IAW SRM 51-70-21, 54-30-00SDR IPXA2020072438130Rub Strip · wornNR 2 ENGINE INBD INNER 6011EL UPPER BIFUNCTION UPPER OFF METAL EDGE WORN & TORN. REMOVED & REPLACED THE RUB STRIP & WEAR ANGLE IAW SRM 51-42-21SDR T17A2020072219029Stiffener · crackedMX REPORTED THE RH UPPER TR OUTBOARD STIFFENER CRACKED. MX REMOVED AND REPLACED THE UPPER THRUST REVERSER OUTBOARD STIFFENER WITH A NEW UNIT. IAW NORDAM CMM 78-30-07 REPAIR NO 1SDR T17A202007219029Stiffener · crackedMX REPORTED THE RT UPPER THRUST REVERSER OUTBOARD STIFFENER CRACKEDSDR 120B2020071500088Thrust Reverser · damagedNR 1 ENGINE OTBD T/R HALF ABLATIVE MATERIAL IS DAMAGED ON THE AFT SECTION 6" FROM THE EDGE (REPAIRED).SDR IPXA2020071557800Strip · wornINSPECTION TYPE:A300 NR 1 ENGINE I/B TR COWL UPPER LANDING AFT METAL STRIP WORN OUT. REMOVED & REPLACED IAW SRM 51-40-21.SDR 120B2020071400083Hinge · wornNR 1 ENGINE, INBD T/R NR 12 BLOCKER DOOR UPPER HINGE IS LOOSE / WORN.SDR 120B2020071400082Hinge · wornNR 1 ENGINE, INBD TR NR 11 BLOCKER DOOR, LOWER HINGE WORN/LOOSE.SDR 120B2020071400080Hinge · wornNR 1 ENGINE INBD T/R NR 7 BLOCKER DOOR LOWER HINGE IS LOOSE/WORN.SDR IPXA2020081435005Skin · crackedINSPECTION TYPE:3C#1 ENG.O/B T/R AFT FIXED INNER BARREL UPPER SKIN IS CRACKED AT STA. NAC= 194.5.REPAIRED #1 ENG. O/B T/R SKIN IAW VT-SAA EA 011-7830-01-A8446 REV, I/R AND UPS EO MD11-7830-77337-A. (MINOR)SDR U2RA202007100003Skin · chafedDURING ACCOMPLISHMENT OF TASK CARD 71-810-01-01, CHAFING NOTED ON THE SKIN OF THE NUMBER 1 ENGINE LEFT THRUST REVERSER COWL INNER FACE LOWER BIFURCATION. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20319-2.SDR U2RA202007100002Structure · chafedDURING ACCOMPLISHMENT OF TASK CARD 71-810-01-01, CHAFING WAS NOTED ON THE SKIN OF NUMBER 1 ENGINE RIGHT THRUST REVERSER COWL INNER SURFACE FORWARD SIDE, NAC STA 131.78. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUSDR UIEA2020071001516Transducer · malfunctionedDURING TAKEOFF RIGHT ENGINE DID NOT SPOOL UP. RIGHT THRUST LEVER WAS SUBSTANTIALLY FRAIL TO BE UNRESPONSIVE TO INPUTS. REMOVED AND REPLACED; RH ENG. T/R POSITION FEED BACK TRANSDUCER IAW AMM 78-36-03. RIG CONFIRMED. REQUIRES HIGH POWER RUN TO COMPLETE OPERATIOSDR 120B2020070900050Fire Seal · damagedNR 2 ENGINE OUTBOARD THRUST REVERSER UPPER FIRE SEAL IS DAMAGED.SDR U2RA202007070005Torque Box · wornDURING ACCOMPLISHMENT OF TASK CARD 71-812-01-02, NR 2 ENGINE RIGHT THRUST REVERSER TORQUE BOX UPPER CABLE BOLT HOLE WORN WAS NOTED AS WORN. ACCOMPLISHED REPAIR IAW FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20316-7.
Back to JASC 7830