JASC 7830
Service difficulty reports · 5,911
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 SWI202404290325Stand Off · crackedR/H UPPER TRANSCOWL INBD "A" BRACKET IS CRACKED (C-CHECK RO 4/26/2024) REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H UPPER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51-900-1002-SKY.SDR SWI20240429000324Bracket · crackedL/H LWR TRANSCOWL OTBD "A" BRACKET IS CRACKED (C-CHECK RO 4/26/2024) INSTALLED A NEW O/B "A" BRACKET (PN CN624-2082-201) INTO L/H LWR TRANSCOWL REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY. SEE CONTINUATION SHEET SDR SWI2024042900323Skin · crackedL/H LWR TRANSCOWL OUTER SKIN IS CRACKED @ LATCH SCREW HOLE. (C-CHECK RO 4/26/2024) L/H LWR TRANSCOWL OUTER SKIN HAS BEEN REPAIRED REF REO# 670-54-21-1623, REV --, DATED 3/18/24. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY. REFER TO CONTINUATION SHEET FOR DETASDR SWIA20240229Stand Off · crackedL/H UPPER TRANSCOWL INBD "A" BRACKET IS CRACKED (C-CHECK RO 4/26/2024) REMOVED AND REPLACED L/H UPPER TRANSCOWL I/B "A" BRACKET W/A NEW "A" BRACKET (PN CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SKSDR HNAA2024030100167Warning Message · illuminatedIRREGULARITY, DURING T/O ROLL E1 REV DISAGREE MESSAGE, ABORTED T/O AT ABOUT 70 KTS. CREW PERFORMED TR ACUATION CHECK WITH NO DEFECTS NOTED. IRREGULARITY CLEARED USING NORMAL CREW PROCEDURES.SDR SWIA202404250315Stand Off · crackedL/H LWR TRANSCOWL INBD "A" BRACKET IS CRACKED (C-CHECK RO 4/24/2024) REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H LOWER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. M-337 AND SKYWEST TASK CARD 51-900-1002-SKY COMPLIED WITH.SDR SWIA202404250312Transcowl · crackedR/H LWR TRANSCOWL PERFORATED SKIN UNDER Z STIFFENER IS CRACKED (C-CHECK RO 4/24/2024) R/H LWR TRANSCOWL SKIN CRACK UNDER "Z" STIFFENER HAS BEEN REPAIRED REF REO# 670-54-21-1619, REV --, DATED 3/12/24 ALL STEPS COMPLIED WITH. SEE CONTINUATION SHEET FOR DETSDR SWIA20240425227Transcowl · pulledL/H UPPER TRANSCOWL 3 EA FASTENERS ARE PULLED IN Z STIFFENER (C-CHECK RO 4/24/2024) REPAIRED CRACK DAMAGE TO THE L/H UPPER TRANS COWL INNER SKIN COMMON TO ZED STIFFENER, REF REO 670-54-21-1616, REV. --, 2024-03-05. COMPLIED WITH MAJOR REPAIR M-337 AND SKYSDR 2024FA0000186Thrust Reverser · gougedDURING ROUTINE MAINTENANCE CHECK, FOUND ENG # 1 RH THRUST REVERSER SECONDARY SLIDER 6H WITH GOUGING DAMAGE. (INSPECTION WAS PERFORMED PER AD 2021-24-14).SDR UIEA2024021000084Actuator · leakingENG 2, LH T/REVERSER HYD ACTUATOR WITH LEAK EVIDENCE.(<P>ENG 2, LH T/REVERSER HYD ACTUATOR WAS REPLACED PER AMM 78-31-06-404-006-H00 REV 140, AUG 22-2023</P>)SDR AALA202402296046Latch · defectiveAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PDX DUE TO RECIEVING ENGINE 1 THRUST REVERSER UNLOCK JUST AFTER TAKEOFF. THE FLIGHT CREW ACCOMPLISHED THE ECAM PROCEDURES WHICH INSTRUCTED THEM TO SHUT DOWN THE ENGINE. THE AIRCRAFT SDR AALA202402290320Control Unit · trippedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PDX DUE TO RECIEVING ENGINE 1 THRUST REVERSER UNLOCK JUST AFTER TAKEOFF. THE FLIGHT CREW ACCOMPLISHED THE ECAM PROCEDURES WHICH INSTRUCTED THEM TO SHUT DOWN THE ENGINE. THE AIRCRAFT SDR GTIA2024022037925Sleeve · damagedDAMAGE FOUND DURING ACCOMPLISHMENT OF T/C 712213-02-1-L NKS ENGINE #1 THRUST REVERSER TX SLEEVE L/H DAMAGE RAF - 01 GENERATED DAMAGE AREA LENGTH 1.932IN AND WIDTH 0.732IN-PERFORMED PERMANENT REPAIR OF THE ENG #1 THRUST REVERSER OUTBOARD TRANSLATING SLEEVE IAW SDR AALA202402196046Actuator · defectiveAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PDX DUE TO RECIEVING ENGINE 1 THRUST REVERSER UNLOCK JUST AFTER TAKEOFF. THE FLIGHT CREW ACCOMPLISHED THE ECAM PROCEDURES WHICH INSTRUCTED THEM TO SHUT DOWN THE ENGINE. THE AIRCRAFT SDR AALA202402031000Fitting · crackedAIRCRAFT WAS NOT GROUNDED: # 2 ENGINE THRUST REVERSER PIVOT FITTING CRACKED AT FASTENER HOLE. REPLACED PIVOT FITTING PER CMM 78-32-36 REPAIR 71SDR SWIA20240304131Skin · dentedL/H UPPER TRANSCOWL HAS 2 EA DENTS ON EXTERIOR SKIN (C-CHECK RO 3/2/2024) EVALUATED 2EA DENTS ON THE L/H UPR TRANSCOWL AND FOUND OUT OF LIMITS PER CRJ900SRM 54-21-00-101-001-A01. RECEIVED AND COMPLIED WITH REO 690-54-21-477 REV -- 2024-02-22 BY REMOVING SDR 2024FA0000081Carriage · wornWE HAVE SEEN NUMEROUS INSTANCES OF LOOSE BOLTS THAT CONNECT THE LINKS TO THE CARRIAGE ON THE NORDAM THRUST REVERSERS. THERE IS CURRENTLY NO INSPECTIONS THAT REQUIRE THESE BOLT TO BE INSPECTED OR LUBRICATED. THE CMM STATES A TORQUE VALUE OF 300 IN LBS. FOR THESSDR SWIA2024032600129Transcowl · chafedL/H LWR TRANSCOWL INNER COAMING IS CHAFED @ FWD LATCH. (C-CHECK RO 3/23/2024) REMOVED DAMAGED COAMING ON LH LOWER TRANSCOWL AND PERFORMED REPAIR IAW ALL STEPS OF REO 670-54-21-1615 REV--, DATED 2024-02-05. COMPLIED WITH TASK CARD 51-900-1002-SKY.SDR CALA2024012400209Cover · damagedL/H ENGINE OUTBOARD C-DUCT PART OF PANEL BROKEN OFF, INVESTIGATION IN PROGRESS. HINGECOVER ASSY P/N 721Z3562-89 PART 7 INCH X 4 INCH MISSING. AREA INSPECTED, NO ADD DAMAGE, ALL TIGHT INSTALLED. TOMC APPROVED : QC REVIEWED. RECORDS UPDATE...UK PART 1 INTERIM RESDR HALA20240123027Control Unit · leakingOTHER - FOUND #1 ENG TR ISOLATION CONTROL UNIT LEAKING FROM REDUCER FITTING. FOUND REDUCER FITTING SEALS BROKEN. REPLACED #1 ENG TR ISOLATION CONTROL UNIT PER AMM 78-31-41.SDR 2024FA0000056Thrust Reverser · chafedTHRUST REVERSER NOZZLE CHAFFE FROM DOOR. REFERENCE NORDAM FIELD ENGINEERING DISPOSITION NTRD-24TP-006.SDR 2024F00012Thrust Reverser · chafedTHRUST REVERSER NOZZLE CHAFFE FROM DOOR. REFERENCE NORDAM FIELD ENGINEERING DISPOSITION NTRSD-24TP-006SDR WX0A2024011631944Unknown · unknown(EMERGENCY DECLARED) FELT A THUMP AND GOT AN ENG 1 REVERSE UNLOCKED ECAM. FOLLOWED ECAM ACTION SHUT DOWN ENG 1. / PERFORMED OPERATIONAL TEST OF THE THRUST REVERSER SYSTEM (ENGINE #1) REF AMM 78-31-00-710-042-A. NO FAULTS FOUND. THIS CLEARS DMI #114487 MEL #78SDR HALA20240112014Unknown · unknownETOPS - ENG 2 REV FAULT CAUTION AFTER STARTING ENG 1. T/S IN REF WITH TSM 78-30-00-810-863-A. FIN 39CE2 REMOVED AND REPLACED RELAY NO FAULTS DETECTED IN WIRING OPS CHECKS GOOD OK FOR SERVICE.SDR IPXA2024020875857Sleeve · debondedENG#2 T/R O/B SLEEVE FWD, EDGE DISBONDING. DOT 641/11 INSTALLED 02 TRANSLATING SLEEVE EDGE PROTECTOR ON ENGINE #2 T/R, O/B, IAW SRM 51-40-21.SDR IPXA2024013175620Angle · dentedFAULT, ENG#2 T/R I/B FWD BOTTOM IN THE CORNER, DENT DOT 641/07 INSTALLED ANGLE AT #2 ENG. T/R I/B FWD FRAME. IAW A300-600 PW4000 SRM 54-04-01.SDR CALA2024010900069Actuator · leakingON T/O ROLL THE RIGHT YELLOW REV LIGHT CAME ON A GAIN EVEN AFTER MEL 7831 F HAD BEEN APPLIED. REVERSED MEL #2 ENG T/R. PERFORMED ACTUATOR LOCK, CROSSOVER SHAFT INTEGRITY TEST IN REF AMM 78-31-00. CHECK OK. PERFORMED #2 ENG T/R OPS TEST IN REF AMM 78-31-00-715SDR CALA2024010900070Thrust Reverser · warning messageNO 2 ENGINE YELLOW REV LIGHT CAME ON DURING ROLL ON TAKE OFF RTO LOW SPD CYCLE REV TRIED 2ND. PLACARD #2 ENGINE T/R INOP PER MEL COWLING CLOSED AND SECURED. PLACARD #2 T/R INOP PER MEL .OK TO CONTINUE. DISPATCH DESK: 52 NAME: B.A. DATE: 07-JAN-24- NOC DESK: 75SDR SWAA2024010937934Web · cracked#1 ENGINE I/B THRUST REVERSER IS CRACKED ON THE AFT WEB TORQUE BOX JUST FORWARD OF THE SECOND FROM UPPER CASCADE LOCATED JUST UNDER T/R STOW SENSOR .<[01] REMOVED AND REPLACED #1 ENGINE I/B THRUST REVERSER IAW AMM 78-31-01. OPS AND LEAK CHECKED GOOD.SDR CALA2024010500034Thrust Reverser · damagedFOUND CRACK ON NO. 1 ENG COWLING O/B T/R REF LOG PAGE 6708820. UPON OPENING TRANSLATING SLEEVE, FOUND O/B CASCADE VANE MISSING FROM T/R. SEE LOG PAGE 6708820 FOR PHOTOS. HIGHLIGHTED SDR MARKER.UPPER ACOUSTIC PANEL SIZE ESTIMATE, BASED OFF MEASURING FROM THE MOSDR CALA2024010400018Thrust Reverser · crackedFOUND CRACK ON NO. 1 ENG COWLING O/B T/R REF LOG PAGE 6708820. UPON OPENI NG TRANSLATING SLEEVE, FOUND O/B CASCADE VANE MISSING FROM T/R. SEE LOG PAGE 6708820 FOR PHOTOS. MISSING UPPER ACOUSTIC PANEL SIZE ESTIMATE, BASED OFF MEASURING FROM THE MOUNTING POINTS SDR UIEA2023122701022Unknown · unknownENG 2, OUTBOARD THRUST REVERSER, MISSING ANTI-FIRE COVER AT INTERNAL PROTECTION(<P> ENG 2, OUTBOARD THRUST REVERSER, ANTI-FIRE COVER AT INTERNAL PROTECTION WAS REPAIRED AMM 78-31-00-308-072-H00 REV 140 22 AUG 23. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023122701021Unknown · unknownENG 2, OUTBOARD THRUST REVERSER, DISBONDED ANTI-FIRE SEAL PROTECTION AT UPPER FWD CORNER(<P> </P> / <P>ENG 2, OUTBOARD THRUST REVERSER, ANTI-FIRE SEAL PROTECTION AT UPPER FWD CORNER WAS REPAIRED PER AMM 78-31-00-308-072-H00 REV 140 22 AUG 23</P>)SDR UIEA2023122701020Unknown · unknownENG 2, OUTBOARD THRUST REVERSER, MISSING ANTI-FIRE PROTECTION (RED SEALANT) ON INTERNAL FACE(<P>ENG 2, OUTBOARD THRUST REVERSER, ANTI-FIRE PROTECTION (RED SEALANT) ON INTERNAL FACE. WAS REPAIRED AMM 78-31-00-308-072-H00 REV 140 22 AUG 23. NO FURTHER DEFECTS NOSDR M17F202401170001Duct · damagedWHEN READY FOR PUSHBACK DURING BEFORE START CHECKLIST A VEHICLE CRASH THE AIRCRAFT FROM THE RIGHT SIDE OF THE AIRPLANE GOING THRU THE LEFT SIDE STOPPING THE MOVEMENT ON THE LEFT ENGINE, CAUSING SEVERE DAMAGE TO THE ENGINE AND FUSELAGE.SDR HALA20231220280Unknown · unknownETOPS - AFTER LANDING ECAM "ENG 1 REV FAULT". REMOVED & REPLACED #1 ENG LEFT LOWER STOW SWITCH & CLEANED/LUBRICATED DOOR RIGGING MECHANISIMS. T/R OPS TEST GOOD. IAW AMM 78-31-13-400-802-A/TSM 78-30-00-810-864-A.SDR ABXA2023122019225Unknown · unknownBOTH THRUST LEVERS ARE DIFFICULT TO PUSH FORWARD TOGETHER AC RETURNED TO GATE AND GROUNDED BY MAINTENANCE. TROUBLESHOT .C/W FIM 76-11 FT 806 BLOCK 23. SYS CKS OK. VERIFIED A/C REMAINS ETOPS 180 AC RETURNED TO SERVICE .SDR QXEA2023121800184Control Quadrant · malfunctionedENG 1 TLA REV FAIL. ( THRUST REVERSER SYSTEMS – SYSTEM FAULTS – REV TLA FAIL EICAS CAUTION MESSAGE ). REMOVED FROM SERVICE. INTEROGATED CMC. FOUND FAULT CODE 76100151. PER E175 FIM 76-11-00-810-803-A, R+R THRUST CONTROL QUADRANT IAW E175 AMM 76-11-01-000/400-8SDR SWAA2024020632403Thrust Reverser · corrodedCORROSION ** NO-1 ENG OUB T/R ASSY LOWER AFT TRAILING EDGE<[01] # 1 ENGINE OUTBOARD T/R ASSY WAS REPLACED ON FAULT TTG8Q00QPXB7;[02] VERIFIED STATEMENT AND TTG8Q00QPXB7SDR SWI2024F00140Structure · crackedL/H LWR TRANSCOWL HAS SUSPECT CRACK @ OUTER SKIN @ FWD LATCH. (C-CHECK RO 2/18/2024) L/H LWR TRANSCOWL CRACK LOCATED ON OUTER SKIN @ FWD LATCH HAS BEEN REPAIRED REF REO# 670-54-21-1609, REV --, DATED 1/23/24. SEE CONTINUATION SHEET FOR DETAILS. COMPLIED WISDR SWI2024F00139Skin · crackedL/H LWR TRANSCOWL INNER PERFORATED SKIN IS CRACKED UNDER Z STIFFENER. (C-CHECK RO 2/18/2024) L/H LWR TRANSCOWL INNER SKIN CRACKED UNDER "Z" STIFFENER HAS BEEN REPAIRED REF REO# 670-54-21-1609, REV --, DATED 1/23/24. REFER TO CONTINUATION SHEET FOR DETAILS.SDR SWIA2024021931214Stand Off · crackedL/H UPPER TRANSCOWL INBD "A" BRACKET IS CRACKED. (C-CHECK RO 2/18/2024) REMOVED DAMAGED A-BRACKET STANDOFF, AND INSTALLED 1 EA. NEW INBD A-BRACKET STANDOFF P/N CN624-2082-201 ON L/H UPPER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITSDR CVGA20231216001Unknown · unknownDURING CLIMB L AND R TR ARM LIGHTS BECAME ILLUMINATED WITHOUT THE MASTER CAUTION WARNING LIGHT. AN EMERGENCY WAS DECLARED. THE LEFT AND RIGHT THRUST REVERSERS WERE PLACED ON MEL.SDR JJBA20231213004Adapter · inoperativeEICAS IN FLIGHT ENG 2 REV DISAGREE, SPOILER FAIL. PULLED CBS F13, F14, AND F20. PERFORMED CONTINUITY CHECK OF WIRING HARNESS ON WHEEL SPEED TRANSDUCER NUMBER 3 AND 4 (PINS 1 TO 2 AND 3 TO 4). NO DEFECTS NOTED. CONTINUITY CHECK DID NOT PASS ON PINS A43 TO GROUNSDR I5PA2023121178801Actuator · faultyFLT. NO: MGE300. ESI - LH ENG REV CONT STATUS MSG ON MEL. REPLACED LHIB TR LVDT PER APPLICABLE AMM. CLEARED DMI.SDR CALA2023120803595Access Door · missingPDA, #1 ENG I/B AFT FAIRING THRUST REVERSER HINGE BEAM ACCESS DOOR MISSING. REMOVED AND REPLACED ACCESS DOOR REF SRM 51-40-02.SDR HNAA2023120500455Unknown · unknownE2 REV DISAGREE ON EICAS ON TAKE OFF ROLL. #2 TR ICU AND HARNESS ASSY REPLACED AND COMPLIED WITH THRUST REVERSER RIGGING PROCEDURE. EVALUATION FLIGHT REQUIRED DUE TO "E2 REVERSE DISAGREE ON EICAS T/O ROLL. SBY EVALUATION FLIGHT SATISFACTORY.SDR IPXA2023112891721Door · cracked#1 ENG I/B REVERSER, UPPER BLOCKER DOOR CRACKED * OII 3 * (LINKED FAULT T3F18E003DYD0) INSTALLED THRUST REVERSER BLOCKER DOOR IAW AMM 78-31-14 AND CORRESPONDING DRAG LINK INSTALLED IAW AMM 78-31-15 OPERATIONAL CHECK SATIS DMP 78-31-1 REVERSED. CDL 78-31-3 CLEASDR MK1Y20231127006Unknown · unknownEVALUATION - ENGINE #2 - OUTBD SIDE, THRUST REVERSE UPPER AND LOWER TRACK FAIRINGS - FOUND EXISTING DOUBLER REPAIRSDR MK1Y20231127001Unknown · unknownEVALUATION - ENGINE #1 - INBD SIDE, THRUST REVERSER UPPER AND LOWER TRACK FAIRINGS - FOUND EXISTING DOUBLER REPAIR.
Back to JASC 7830