JASC 7810
Service difficulty reports · 1,900
Reports filed under 7810 · Engine Collector/Tailpipe/Nozzle, 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 = '7810' 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 = '7810' 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 UIEA2020042800905Sleeve · dentedNO. 2 ENG TURBINE EXHAUST SLEEVE FOUND 4EA DENT AT 8 O/C, 10 O/C, 2 O/C, 4 O/C POSITION.(<P>NO. 2 ENG TURBINE EXHAUST SLEEVE 2 O/C DENT AREA REPAIRED IAW RI-78-11-14012 REV. A. #4 O/C, 8 O/C, 10 O/C DENT AREA REPAIRED IAW SRM 54-41-30-1A-1.</P>)SDR UIEA2020042800907Sleeve · dentedNO. 4 ENG TURBINE EXHAUST SLEEVE SKIN FOUND DENT AT 11 O/C POSITION.(<P>NO. 4 ENG TURBINE EXHAUST SLEEVE 11 O/C DENT AREA REPAIRED IAW RI-78-11-14013 REV. A.</P>)SDR UIEA2020042800908Sleeve · dentedNO. 4 ENG TURBINE EXHAUST SLEEVE SKIN FOUND DENT AT 9 O/C POSITION.(<P>NO. 4 ENG TURBINE EXHAUST SLEEVE 9 O/C DENT AREA REPAIRED IAW RI-78-11-14013 REV. A. </P>)SDR SWAA2021042942208Skin · crackedWHILE PERFORMING WORK INSTRUCTION NO. INSP 78 EA07742. FOUND A CRACK ON #1 ENGINE PRIMARY EXHAUST NOZZLE PREFORATED SKIN AT THE 12 O'CLOCK POSITION. DID A DETAILED VISUAL INSPECTION IAW SRM 5440021A3 LENGTH OF CRACK IS APPROXIMATELY 6 INCHES. DYE PENETRANT INSSDR SWAA2020051276688Acoustic Liner · crackedACCOMPLISH A DYE PENETRANT INSPECTION OF THE CRACK LOCATED ON THE #1 ENGINE EXHAUST ACOUSTIC LINER AT THE 6 O'CLOCK POSITION PER SOPM 20-20-02 WITHIN 10 CYCLES ( MX NOTE ) / CLEARING DMA:0157323ACCOMPLISHED DYE RENETRANT NO FURTHER DEFECTS AT THIS TIME PER AMMSDR 7C7A2020032400014Shroud · chafedLEFT NACELLE, CENTER EXHAUST SHROUD, LOWER HALF HAS 2 CHAFED HOLES.SDR P5CA2020031900111Plug · crackedFOUND #1 ENG EXHAUST PLUG CRACK(<P>IAW AMM 78-11-02-004-001 REV. 129 REMOVED THE #1 ENG EXHAUST PLUG. REFER TO J/C ATTACHING SHEET CONTROL NO. 0243072.0198389. IAW AMM 78-11-02-404-006 REV. 129 INSTALLED THE #1 ENG EXHAUST PLUG. CONDITION CHECK NORMAL.</P>)SDR YV3R2020003070244Collector · bulgedCUSTOMER REPORTED EXHAUST COLLECTOR P/N: C169-6 WAS BULGING (HOT SPOT).SDR SWAA2021082324327Nozzle · cracked# 1 ENG HAS MULTIPLE CRACKS ON PRIMARY EXHAUST NOZZLE AT 6 O'CLOCK POSITION ON THE PERFORATED SKIN AREA. / R & R PRIMARY EXHAUST NOZZLE PER AMM 78-11-01. POS # 1; TAG/GRB NO. 1047362; P/N OFF 314A2630-103; S/N OFF B63389; P/N ON 314A2630-103; S/N ON B362542SDR SWAA2021082385257Nozzle · debonded# 2 ENG EXHAUST NOZZLE PERFORATED SKIN HAS DISBOND IN AREA ZONE 1 @ 2.1 BY 3.6 INCHES AT 6 OCLOCK POSITION / R & R ENGINE EXHAUSE NOZZLE PER AMM 78-11-01 SEE NON-ROUTINE 0020349E; 0020350E. POS #2 TAG 93366 P/N OFF: 314A2630 S/N OFF: B63382 PN ON: 314A2630-103SDR AALA202001139001Arrestor · malfunctionedAIRCRAFT WAS GROUNDED: FLAME REPORTED 1 FOOT IN LENGHT WHILE TAXING ALL ENG PARAMATERS NORMAL RIGHT ENGINE. ACCOMPLISHED INSPECTION ON RIGHT ENGINE FLAME ARRESTOR IAW AMM 71-00-00. FLAME ARRESTOR HONEYCOMB IS PRESENT AND NOT DETERIORATED. OK FOR CONTINUED SERVSDR VNAA2022012011101Fairing · bentUPPER FWD CORE COWL HINGE NOT PINNED CORRECTLY. NO. 2 ENGINE EXHAUST NOZZLE FAIRINGÏ¿½S ACCESS PANEL WAS FOUND TO BE BENT AND TWISTED. PLACED ON TEMP REPAIR REFERENCE EA25-2019-321 FOR DETAILS. C/W PERMANENT REPAIR. R+R RH ENGINE EXHAUST NOZZLE ASSY IAW CRJ200SDR 9PMA2020042700008Bracket · failedPIC REPORTS SLIGHT VIBRATION FELT ON LANDING IN COLLEGE STATION. ONCE AIRCRAFT WAS SHUT DOWN PILOT REPORTS EXHAUST DUCT BRACKET HAD CRACKED. NO FURTHER DAMAGE CAUSED TO AIRCRAFT OR CREW.SDR A6WA2019121047048Doubler · cracked436AL HAS CRACKED DOUBLER AT MOUNTING HOLE PANEL AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED DOUBLER AT MOUNTING HOLE ON PANEL 436AL IAW BOMB. CMM 20-42-06SDR EVCA201911260001Collector · crackedENGINE EXHAUST COLLECTOR HAS A 1.10 INCH CRACK LH AFT SIDE.SDR AALA201911259026Unknown · fireAIRCRAFT NOT GROUNDED: WHILE ON TAXI. FLT CREW FROM A FOLLOWING AIRCRAFT REPORTED FIRE EMANATING FROM NO. 2 ENGINE BREATHER TUBE. MAINTENANCE INSPECTED #2 ENGINE IAW-AMM 71-00-00-800-803 F00 AND FOUND OKAY FOR SERVICE.SDR HALA2019111800487Rivet · looseETOPS SIGNIFICANT SYSTEM - MULTIPLE RIVETS LOOSE ON A/C AND ENGINE. // FLIGHT CREW POINTED OUT RIVETS ON INNER 12' O'CLOCK SECTION OF CAN #2 ENGINE. REMOVED AND REPLACED DEFECTIVE RIVETS PER RB211 CMM 54-40-01(REPAIR NO.11) ALL RIVETS SECURE OK FOR SERVICE.SDR SWIA2019122747405Cover · cracked*RH ENGINE EXHAUST FAIRING FIRE LOOP COVER CRACKED (MARKED) (C-CHECK) RO:12/24/2019 REMOVED AND INSTALLED A NEW R/H ENGINE EXHAUST FAIRING FIRE LOOP COVER REF CRJ200 SRM NEW HARDWARE USED P/N 4 EA. WASHER NAS1149C0332R, SCREW 4 EA. NAS623-3-2 AND NUT SDR SWIA2019122747397Exhaust Cone · cracked*LH ENGINE EXHAUST FAIRING 2ND INNER RIB CRACKED ON INBRD SIDE (MARKED) (C-CHECK) RO:12/24/2019 ORDERED/RECEIVED LH ENG EXHAUST NOZZLE FAIRING ASSY. SEE CAMP 19772916 FOR MAINTENANCE PERFORMEDSDR A6WA2019101546920Rib · crackedPANEL 436AL EXHAUST FAIRING #2 RIB CRACKED AT TOOLING HOLE. REPAIRED CRACKED STIFFENER IAW 78-11-11 SRS042SDR YV3R2019091100181Collector · distortedCUSTOMER REPORTED EXHAUST COLLECTOR P/N: C169-6 IS DISTORTED.SDR I5PA2019090475702Cone · dentedDURING HEAVY MAINTENANCE PHASE "C" CHECK, FOUND DENT ON #1 ENGINE EXHAUST CONE REQUIRING REPAIR.SDR AALA201908289018Exhaust Cone · contaminatedAIRCRAFT WAS GROUNDED: PILOT REPORTS AIRCRAFT BEHIND US REPORTED TAILPIPE FIRE ON LEFT ENGINE, NO FIRE INDICTIONS ON FLIGHT DECK. RAN QRC/QRH AND SHUT ENGINE DOWN. GROUND CREW REPORTED FIRE OUT. FIRE CHIEF REPORTED FIRE OUT. MAINTENANCE INSPECTED NO 1 ENGINE FSDR FDEA2019082181930Nozzle · crackedNR 1 ENGINE CNA HAS CRACKS AT THE 3 O'CLOCK AND 9 O'CLOCK POSITIONS. CRACKS REMOVED IAW EM 78-11-04 AND CRACKS REPAIR IAW E.A. F-7810-T0348465.SDR HALA2019082000348Structure · puncturedETOPS SIGNIFICANT SYSTEM - UPON INSP #1 CAN FOUND 4 PUNCTURES @ 6 O CLOCK POSITION APPROX. 37" FWD OF EDGE. REPAIRED PER SRM 78-11-14-300-003, OK FOR SERVICE. PRIMED AND PAINTED PER SRM 54-02-04.SDR ASAA2019081530420Bolt · missingBOLT MISSING FROM #1 ENG AFT EXHAUST FLANGE AND IS LAYING INSIDE THE EXHAUST CONE. GROUNDED - YES. INSPECTED AREA AND NO OTHER DEFECTS NOTED REMOVED BOLT. INSTALLED NEW BOLT IN #1 AFT EXHAUST FLANGE AND RE-TORQUED ALONG WITH ALL REMAINING BOLTS. REF AMM 72-56-SDR UIEA2019081635136Seal · brokenBROKEN - SPRING SEAL #1 ENG EXHAUST SLEEVE NEAR 1 O'CLOCK POSITION QTY 2EA(<P>REPLACED NO 1 ENG EXHAUST SLEEVE SPRING SEAL WITH NEW</P>)SDR UIEA2019081305090Skin · dentedDENT-OUTER SKIN NO.1 ENG EXHAUST SLEEVE NAC STA 346 NEAR 1 OCLOCK POSITION(<P>MEASURED THE EXHAUST SLEEVE DENT AREA LENGTH 0.2" WIDTH=0.2", DEPTH AND .0094", A/Y=0.2/.0094=21.28. WITHIN ALLOWABLE DAMAGE IAW SRM 54-42-30-1A-1 REV.110. JOB COMPLETED AND COND CHKSDR UIEA2019081635092Nut Plate · damagedDAMAGE NO.1 ENG EXHAUST SLEEVE NUTPLATE DAMAGE AT 9 O'CLOCK(<P>REMOVE DAMAGED NUTPLATE IAW SRM 51-40-02-0G-0 REV.110. INSTALLED NEW NUTPLATE IAW SRM 51-40-02-0G-0 REV 110 AND BOEING DWG 314U2100 5H6 REV.N. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2019080264855Plate · worn#4 ENG LH C-DUCT COLD STEAM INNER FACE AFT EDGE WEAR PLATE FOUND WORN.(<P>THE SUBJECT FRAME AND WEAR PLATES REPLACED AS PER HX RI-78-31-13643 REV A.</P>)SDR IPXA2019071144315Receptacle · gougedINSPECTION TYPE:4C#1 ENGINE EXHAUST NOZZLE O/B CORE COWL AFT LATCH PIN RECEPTACLE IS GOUGED. REPAIRED GOUGED #1 ENGINE EXHAUST NOZZLE O/B CORE COWL AFT LATCH PIN RECEPTACLE IAW EA 011-7810-01-A7834 REV. IR AND EO MD11-7810-73170-A. (MINOR)SDR AALA2019062099008Tailpipe · fireAIRCRAFT WAS GROUNDED: PILOT REPORTS TAILPIPE FIRE REPORTED FROM TOWER AND AIRCRAFT ON TAXIWAY. NO COCKPIT INDICATIONS. QRC/QRH COMPLIED WITH. MAINTENANCE PERFORMED INSPECTION OF NR 2 FLAME ARRESTOR IAW AMM 71-00-00, SUBTASK 2, OPS CHECK NORMAL, OK FOR SERVICSDR REXA2019062070927Stiffener · crackedLH ENG EXHAUST FAIRING STIFFNER ANGLE RING CRACKED. REMOVED AND REPLACED STIFFNER DUE TO CRACK.SDR CA190606002Pipe · broken(CAN) DURING SCHEDULED BASE MAINTENANCE VISIT (REMOVAL FOR THE ACCESS) FOUND THE FOLLOWING PARTS BROKEN: - JET PIPE FWD (P/N PER IPC 87804002-015, S/N UNKNOWN) RH ENGINE - JET PIPE AFT (P/N PER IPC 87804005-009, S/N UNKNOWN) RH ENGINE ALL 4 ATTACHMENTS OF SDR YN82020F00000Exhaust Stack · crackedDURING OIL CHANGE, WITH THE RIGHT HAND LOWER COWL PANEL REMOVED, NOTICED THE AERODUCT HAVING EXHAUST RESIDUE ON IT. INSPECTED THE EXHAUST STACK AND FOUND THE LOWER FORWARD SEAM OF THE STACK TO BE SPLIT ABOUT 5 INCHES ABOVE THE MUFFLER ASSEMBLY. THE AREA OF TSDR CA190604026Clamp · damaged(CAN) #1 ENGINE ZONE 1 FIRE INDICATION SHORTLY AFTER TAKEOFF. FIRE INDICATION CEASED FOLLOWING REDUCTION IN POWER. LOAD ABORTED AND #1 ENGINE EMERGENCY HANDLE ACTIVATED. #1 ENGINE TAILPIPE CLAMP P/N 4215AF18.92 FOUND BROKEN, CAUSING TAILPIPE SEPARATION. #1 ENGSDR REXA2019051300717Skin · chafedLT ENG EXHAUST NOZZLE EXT SKIN HAS FRETTING FROM CONTACT WITH PYLON SEAL. PERFORMED EXHAUST SKIN AND DOUBLER REPAIR IAW EA #CRJ254-08921 REV A.SDR REXA2019050200709Angle · chafedRT ENG EXHAUST NOZZLE FWD T ANGLE EDGE MEMBER CHAFED IN SEVERAL AREAS. REPAIRED RT ENG EXHAUST NOZZLE FWD T ANGLE EDGE (LEADING EDGE) IAW CMM 78-11-00.SDR JJBA201904263014Exhaust Cone · missing#1 ENGINE EXHAUST CONE MISSING. R&R #1 ENGINE. OPS AND LEAK CHECK SAT. DOWNLOADED FDR.SDR CALA2019042200635Fence · crackedPDA 3 LEFT ENG EXHAUST NOZZLE OUTBD FWD FENCE MISSING SEGMENT AND CRACKED AT AFT FASTENER HOLE. REMOVED DAMAGED FENCE AND INSTALLED A NEW FENCE REF ECRA 7811-01314.SDR 2019FA0000107Tailpipe · crackedOWNER STATED TAIL PIPE CLAMP WAS REPLACED AT ANNUAL INSPECTION 5-25-18 AS WELL AS 3 OTHER CLAMPS ON THE WASTE GATE AND EXHAUST. OWNER FOUND ON PREFLIGHT THAT THE TAIL PIPE WAS LOOSE. UPON FURTHER INSPECTION AT THE MAINTENANCE SHOP FOUND TAIL PIPE CLAMP TO BE ISDR 2019FA0000102Exhaust Riser · crackedWITHIN THE LAST FEW WEEKS THIS FLIGHT SCHOOL DISCOVERED SEVERAL INSTANCES OF CRACKED EXHAUST RISERS AND FLANGES AFFECTING THE NR 2 AND NR 3 CYLINDERS. SEVERAL ADDITIONAL M&D REPORTS HAVE BEEN FILED FOR THIS TIME PERIOD.SDR REXA201904109440Intercostal · crackedR/H ENGINE EXHAUST NOZZLE HAS BENT INTERCOSTAL BY O/B ACCESS PANEL INNER SECTION. REMOVED AND REPLACED WITH NEW INTERCOASTAL ON R/H ENGINE EXHAUST NOZZLE O/B INNER SECTION I.A.W. CRJ-200 BOMB CMM 20-42-06 AND CMM 20-42-20.SDR CALA2019031800429Fence · crackedPDA 2 RIGHT ENG EXHAUST NOZZLE INBD AFT MOST FENCE CRACKED AND MISSING SEGMENT - DEPARTED AIRCRAFT. NOZZLE P/N 314A2610-1 INSTALLED. ONLY 1 FENCE MISSING ALL OTHERS ARE PRESENT. REQUEST CDL 78V DISPATCH DESK: 33 NAME: A.L.M. DATE: 17-MAR-19- TOMC APPROVES CDL SDR 2019FA0000071Exhaust Riser · crackedWITHIN THE LAST FEW WEEKS, THIS FLIGHT SCHOOL DISCOVERED SEVERAL INSTANCES OF CRACKED CYLINDER NR 2 OR NR 3 EXHAUST RISER FLANGE AND FLANGES.SDR CALA2019030800370Rivet · missingNR 2 ENG COMMON NOZZLE HAS SEVERAL MISSING RIVETS AND SEVERAL LOOSE RIVETS (RIVETS MARKED) REPLACED THE NUMBER TWO ENGINE CNA AS PER 78-11-11-400-010-A WORK PERFORMED, ROTABLE PARTS CHANGE WAS INDICATED - TT # 1445047 SN OFF 5716 NOZZLE, NON-VEC OFF 31-7811-9SDR REXA2019022200267Seal · chafedLT TAIL PIPE FAIRING LE METAL SEAL HAS CHAFING DAMAGE. REMOVED AND REPLACED WITH NEW METAL SEAL ON LT TAIL PIPE FAIRING L/E IAW CMM 20-42-06 AND CMM 78-11-00.SDR A6WA2019022746420Stiffener · cracked436AL EXHAUST FAIRING SECOND STIFFENER AFT CRACKED NEAR PREVIOUS REPAIR. REPLACEDSDR REXA2019021700247Stiffener · crackedRT EXHAUST FAIRING NR 2 STIFFENER FROM FWD END IS CRACKED AT TOOLING HOLE. REPAIRED STIFFENER ON RT EXHAUST FAIRING IAW CMM 78-11-00.SDR YV3R2019012200023Exhaust Duct · crackedCUSTOMER REPORTED ENGINE EXHAUST P/N: F169-1 WAS CRACKED.
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