JASC 7810
Service difficulty reports · 1,904
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 UALA2012012400497Acoustic Liner · tornTEMP REPAIR OF NR 1 ENG ACOUSTIC LINER IS PEELING BACK AND COMING OFF. RE-SECURED TAPE REF MT 78- 010, SEE CF405 FOR INTERIM REPAIR. NR 1 ENGINE ACOUSTIC LINER INBOARD AFT OF REVERSER HAS TORN PROTECTIVE LINER. FOUND APPROX 900 SQ OF SCREEN MISSING. PER MTSDR FDEA201201230306Strut · corrodedLEFT ENGINE, CNA SIDE STRUT AT 9 O'CLOCK AFT LOOKING FORWARD UPPER SURFACE CORRODED. SIDE STRUT REPLACED.SDR UALA2012011100237Seal · crackedNR 1 ENG HEAT SHIELD SEAL CRACKED. ABOUT TWO AND HALF INCH LONG CRACK. REMOVED HEAT SHIELDS FROM POSITIONS 2 THRU 6. CONT OF AMIS ITEM 5462013 REMOVED NR 1 HEAT SHIELD PAN CASTING PER MM. INSTALLED HEAT SHIELD SEAL AND SHIELD. LEAK CHECKED PER MM. TESTED PESDR UIEA2012010400002Nozzle · crackedDURING MX WALKAROUND, MX FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, BETWEEN APPROX THE 10 TO 12 O'CLOCK POSITION (LT SIDE) ON THE NR3 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 11" LONG AND IS 13" FROM AFT SIDE OF EXHAUST SLEEVE JUST IN FRONT OF NAC STSDR P5CA2011122900513Nozzle · crackedTHERE IS A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, BETWEEN THE 10 AND 12 O'CLOCK POSITION (LT SIDE) OF THE NR 3 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROXIMATELY 15 INCHES LONG AND IS 13 INCHES FROM AFT SIDE OF EXHAUST SLEEVE JUST IN FRONT OF NAC STA 349.2SDR HALA2011122400617Sleeve · crackedETOPS SIGNIFICANT SYS - NR 1 ENGINE EXHAUST NOZZLE (SLEEVE) HAS NUMEROUS CRACKS A LONG LENGTH OF EXHAUST ABOUT 8 O'CLOCK POS. R & R NR1 ENG EXHAUST NOZZLE SLEEVE IAW AMM 78-11-01. SECURITY CHECK OK.SDR UIEA2011121200715Nozzle · dentedDURING MX WALKAROUND OF MX FOUND A DENT ON THE EXHAUST NOZZLE AT THE 8 O'CLOCK POSITION ON THE NR 2 ENGINE. THE DENT IS APPROX 1.0" INCH X 1.250" INCH X 0.168" DEPTH. THE DENT IS APPROX 29.5" FROM THE NOZZLE EDGE. IAW SRM 54-41-30 THE DENT IS OUT OF LIMITS. PSDR A6WA201240113Fairing · looseLEFT JET PIPE FAIRING ALL 2 NUT PLATE ASSY LOOSE. R & R WITH NEW FABBED 3 EA NUTPLATE ASSY`S ON LT JET PIPE FAIRING IAW CMM 20-42-06.SDR UALA2011112206415Rivet · failedFAILED RIVET ON LEFT ENGINE EXHAUST NOZZLE 12 O'CLOCK POSITION REF MT 78-001 MISSING RIVETS ALLOWED, MUST BE REPAIRED. REPLACED WITHIN 50 HRS. OK TO CF PER THIS MAINT TRIP. REPLACED MISSING RIVET.SDR CA111109004Exhaust Duct · unserviceable(CAN) DURING 100 HR INSP, FOUND CYLINDER NR 4 EXHAUST RISER BULGED AT COLLECTOR, BULGE IS CONSISTENT WITH DIRECTION OF CYLINDER NR 4 EXHAUST FLOW. UPON REMOVAL, NOTICED THE EXHAUST TO BE QUITE THIN AND APPEARED TO HAVE LOST MATERIAL. A GENTLE TAP WITH A SOFTSDR A6WA201141123Skin · crackedSKIN AROUND THE UPPER OTBD PANEL ON LT JET PIPE IS CRACKED. REMOVED UNSERVICEABLE DOUBLER AND INSTALLED SERVICEABLE DOUBLER IAW CMM 78-11-00 AND SRM 51-42-06.SDR UALA2011110906096Bolt · backed outNR 1 ENGINE EXHAUST CONE BOLT BACKED OUT AT 6 O'CLOCK POSITION. CHASED THREADS AND INSTALLED NEW BOLT AND TORQUED PER MM.SDR CA111109011Blanket · separated(CAN) NR 2 ENGINE EXHAUST EJECTOR INSULATING BLANKET SEPARATED AND WAS PULLED INTO THE TAIL ROTOR DRIVETRAIN. DAMAGED COMPONENTS INCLUDE: FANSHAFT ASSY, FWD OIL COOLER BLOWER, AFT OIL COOLER BLOWER, OIL COOLER ASSY, AND AFT SEGMENTED TAIL ROTOR DRIVESHAFT. NSDR A6WA201141070Stiffener · crackedCRACKED FWD STIFFENER ON PANEL 446L, REPAIRED CRACKED STIFFENER IAW CMM 78-11-00-997-022-A07.SDR UALA2011103105871Tail Cone · crackedRAMP FOUND A 6 INCH CRACK AT 6 O`CLOCK ON TAIL CONE, OF LEFT ENGINE. REMOVED OLD AND INSTALLED NEW ENGINE EXHAUST TAIL CONE PER MM.SDR UALA2011103105872Tail Cone · damagedCREW REPORT: ENG 1 EXHAUST TAIL CONE CRACKED AT 9 O'CLOCK POSITION APPROX 1 INCH FROM END. ACP INSP OF TAIL CONE, DAMAGE 2.25 IN. FORWARD OF TRAILING EDGE. CRACK IS TWO INCHES LONG. CRACK IS WITHIN OPERATIONAL LIMITS. NO REMEDIAL ACTION REQUIRED, REVIEWESDR CA111025009Exhaust Duct · warped(CAN) ALL EXHAUST FLANGE JOINTS WARPED.SDR UALA2011101805644Cone · crackedNR 1 ENGINE EXHAUST CONE CRACKED. REPLACED NR 1 ENGINE EXHAUST CONE PER AMM, CHECKED OKAY.SDR UALA2011101705627Exhaust Pipe · crackedNR 1 ENGINE EXHAUST CONE HAS A 13 INCH CRACK. REPLACED NR 1 ENGINE EXHAUST CONE PER AMM.SDR P5CA2011100700482Sleeve · dentedOUTER SURFACE OF NR 4 ENGINE EXHAUST SLEEVE HAS 5 DENTS THAT ARE OVER SRM LIMITS. ACCOMPLISHED REPAIR AS PER EI T2011A54B-1994 REV 1.SDR P5CA2011100700481Sleeve · damagedNR 1 ENGINE EXHAUST SLEEVE OUTER SKIN HAS SEVERAL DENTS AND NICKS BETWEEN NSTA 318 & NSTA 349. BAC APPROVED LEAVING ALL DENTS AS IS SINCE THEY ARE WITHIN ALLOWABLE LIMITS IAW SRM 54-51-30-1A-1 DETAIL VI. NICKS WERE REPAIRED AS PER EI T2011A54B-1997.SDR EE4Y20111001548Pan · crackedENGINE NR 1, COMMON NOZZLE ASSY, PAN WITH CRACK. PAN CRACKED REQUIRES A MAJOR REPAIR IAW SRM GUIDELINES.SDR EE4Y20111001547Pan · crackedENGINE NR 2, COMMON NOZZLE ASSY, PAN WITH CRACK. NOTE: THE PAN CRACKED REQUIRE A MAJOR REPAIR IAW SRM GUIDELINES.SDR UIEA2011092900530Sleeve · crackedDURING MX WALKAROUND, FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, BETWEEN APPROX THE 9 TO 10 O'CLOCK POSITION ON THE NR 2 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 12" LONG . IAW SRM 54-41-30 THE LENGTH OF THE CRACK IS OUT OF LIMITS. STOP DRILLED ENDSDR A6WA201140919Doubler · crackedRIGHT JET PIPE LOWER NUTPLATE DOUBLER IS CRACKED. REMOVED DAMAGED DOUBLER AND REPLACED WITH NEW.SDR A6WA201140875Skin · bentRIGHT ENGINE TAIL PIPE FAIRING CUT OUT FOR ACCESS PANEL 446BB IS BENT AND GOUGED. REPAIRED RT ENGINE TAIL PIPE IAW CMM 78-11-00, REPAIR SRS 062.SDR CA110908002Collector · cracked(CAN) EXHAUST COLLECTOR FOUND CRACKED DURING PREFLIGHT INSPECTION.SDR 2011FA0000670Exhaust Duct · brokenDURING SCHEDULED INSP, THE LT INBD EXHAUST DUCT THAT CONNECTS THE LT ENG COWLING`S INTAKE HEATED LIP TO THE EXHAUST PORT OF THE LT ENGINE`S INBD EXHAUST STACK WAS FOUND TO BE BROKEN AND DETACHED FROM ITS MATING FLANGE. THIS, IN TURN, WAS ALLOWING EXHAUST GASESDR 3S8R201109020009Heat Shield · gougedNR 2 ENGINE FINGERNAIL UPPER SURFACE PATCH (HEAT SHIELD) DAMAGED. R & R FINGERNAIL PATCH IAW RD 8-54-177.SDR GLBA20110830GExhaust Stack · cracked"SUP" - SIG EVENT - PILOT REPORTED THAT THE NR2 T-HANDLE ILLUMINATED IN FLIGHT, NO INDICATION OF A FIRE WAS VISIBLE, WITH NO ABNORMAL ENGINE INDICATIONS NOTED. MX FOUND EVIDENCE OF AN EXHAUST LEAK ON THE FIRE LOOP NEAR THE EXHAUST MOUNTING FLANGE, RR EXHAUST SDR UIEA2011081800456Sleeve · crackedDURING WALK AROUND CHECK, FOUND SEVERAL CRACKS COMING FROM THE SKIN, ON THE OUTER SLEEVE OF THE LONG FIXED CORE EXHAUST NOZZLE (LFCEN) ON THE NR 4 ENGINE. THE CRACKS ARE APPROX AT THE 7 O'CLOCK POSITION. REF FIG 1. REMOVED ANY BURRS AND STOP DRILLED CRACK ENSDR UIEA2011081700455Sleeve · crackedDURING MX WALKAROUND, FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, BETWEEN APPROX THE 9 TO 12 O'CLOCK POSITION ON THE NR 3 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 11" LONG AND IS JUST IN FRONT OF NAC STA 349.236. IAW SRM 54-41-30 THE LENGTH OF THE CSDR JIKA11051001Exhaust Pipe · damagedIN CRUISE FLIGHT, RT ENGINE STARTED SPUTTERING BECAUSE THE RT OUTBOARD FUEL TANK WAS GOING EMPTY. THE PILOT SWITCHED BOTH FUEL TANKS TO THE INBOARDS AND AT THAT POINT THE RT ENGINE FAILED. THE PILOT FOLLOWED THE FAILED ENGINE PROCEDURE AND TRIED TO RESTART TSDR CA120306002Exhaust Duct · buckled(CAN) EXHAUST NOZZLE SUSTANED EXTENSIVE BUCKLING DAMAGE ON THE BODY OF UNKNOWN CAUSE. RULED OUT GROUND MISHANDLING.SDR 2011FA0000527Exhaust Pipe · rupturedNR2 ENGINE FIRE WARNING ON TAKEOFF (ZONE 2 & 3). REPLACED NR 2 ENGINE IAW MM. INSPECTION OF REMOVED ENGINE REVEALED NO FIRE DAMAGE BUT OVERHEAT DAMAGE CAUSED BY A RUPTURED EXHAUST JOINT ON THE NR 9 CYLINDER.SDR UALA2011080804160Cone · crackedNR 1 ENG TAIL CONE HAS A CRACK ABOUT 24 INCHES LONG. REQUIRES NEW TAIL CONE. REPLACED THE NR 1 ENG EXHAUST CONE PER MM.SDR A6WA201140812Stiffener · crackedRT JET PIPE FAIRING HAS CRACKED STIFFENER. REMOVED UNSERVICEABLE STIFFENER ON RT JET PIPE FAIRING IAW CMM 20-421-06. LOCATED AND DRILLED SERVICEABLE STIFFENER IAW CMM 20-40-11 INSTALLED SERVICEABLE STIFFENER ON RT JET PIPE IAW CMM 20-42-06.SDR EPDA20110804001Seal · leakingRT ENGINE FIRE WARNING LIGHT CAME ON DURING CLIMB AT HIGH POWER SETTING. REDUCED POWER AND LIGHT WENT OUT. RETURNED TO DEPARTURE AIRPORT, LANDING UNEVENTFUL. INSPECTION REVEALED POSSIBLE EXHAUST SEAL LEAK.SDR UIEA2011080400416Nozzle · crackedDURING AN ENGINE CHANGE AT AN A-CHECK, MX FOUND 3 EA CRACKS ON THE NR 4 ENGINE FIXED COWL EXHAUST NOZZLE FOWARD FLANGE CORE COWL SUPPORT ASSY (REF FIGURE 1). REPAIRED IAW EO 4778A148.SDR NOCA07011Plug · crackedEXHAUST PLUG CRACKED AT 5 OCLOCK POSITION AT END OF PLUG ON NR 2 ENGINE. WELDED, VISUAL INSPECTED AND DYE CHECKED REPAIR AREA PER CMM 314T43201, ATA 78-11-15 REPAIR 2-1, ALL WORK COMPLIED WITH ON DELTA SHOP ORDER EA 5673.SDR UALA2011072203729Fastener · missingNR 1 ENGINE HAS 1 RIVET MISSING AFT INSIDE TAIL CONE AT LOWER SUPPORT. MISSING RIVET IS LOCATED AT THE 11 :00 POSITION AFT LOOKING FORWARD.SDR UIEA2011071300359Nozzle · crackedDURING A 'C4/A4' CHECK OF ACFT, MX FOUND 2 CRACKS ON THE NR 1 ENGINE EXHAUST NOZZLE OUTER SKIN AT 12 O'CLOCK POSITION (REFER TO FIG 1 AND 2 ). (THE CRACKS CAN BE REPAIRED IAW THE ENGINE MANUAL (ESM) TASK 78-11-01-300-011. REPAIR 78-11-01 REPAIR 011. THIS RESDR UALA2011062003029Cone · crackedNR 2 ENGINE EXHAUST CONE HAS SEVERAL CRACKS AT FWD END BY MOUNT BOLTS. REPLACED EXHAUST CONE PER AMM.SDR UALA2011062002996Nozzle · damagedCREW REPORTED THREE FAILED RIVETS ON LEFT ENG EXHAUST NOZZLE 12 O'CLOCK POSITION. OK TO CONTINUE IN SERVICE FOR UP TO 50T WITH MISSING RIVETS TILL REPAIR. CF'D PER MAINTENANCE TIP. REPLACED RIVETS AS REQ'D.SDR CA110613007Exhaust Duct · separatedNR 2 ENGINE AFT EXHAUST SECTION SEPARATED FROM FWD SECTION.SDR UALA2011060602739Cone · crackedNR 2 ENGINE EXHAUST CONE HAS MULTIPLE CRACKS ON THE FWD END BETWEEN APROX 8 O'CLOCK AND 10 O'CLOCK POSITION AND HAS A 2 1-8" CRACK AT THE AFT END AT 9 O'CLOCK POSITION. REPLACED EXHAUST CONE PER MM. ROBBED EXHAUST CONE FROM ENG 2 ACFT 4238.SDR CA110606017Exhaust Duct · crackedAFT FLANGE WELD AREA CRACKED 1.5 INCH. DUCT REPLACED AND ACFT RETURNED TO SERVICE.SDR A6WA201140441Panel · missingSMALL PANEL MISSING ON LWR PORTION OF LT ENG JETPIPE. INSTALLED NEW EXHAUST NOZZLE BOLT COVER IAW AMM 78-11-01.SDR 2011FA0000463Exhaust Riser · damagedEXHAUST SYS WAS INSTALLED IN CONJUNCTION WITH 180 HP CONVERSION. THE NR1 EXHAUST RISER WAS FOUND TO BE COMPLETELY SEVERED APPROX .3750 -.5 INCH BELOW THE WELD LINE AT THE CYLINDER FLANGE.SDR JR2R2011060200229Exhaust Duct · crackedRIGHT ENGINE EXHAUST OUTLET SHROUD ASSY INNER LINER CRACKED.
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