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 I5HA0524001Augmentor Tube · fireRT ENG FIRE WARNING BELL SOUNDED AND ASSOC FIRE WARNING LIGHT ILLUMINATED DURING TAXI. RT FIRE BOTTLE WAS DISCHARGED AND ENG SHUTDOWN. FIRE WAS EXTINGUISHED WITH NO FURTHER ACTION. EXAMINATION OF RT ENG REVEALED INSIDE OF AUGMENTOR TUBE HAD CAUGHT FIRE. FIRSDR 2005FA0000520Clamp · brokenIN FLIGHT, TAILPIPE CLAMP FAILED ALLOWING HOT GASSES TO ENTER NACELLE REGION. PAINT ON HOT AIR SHIELD/DUCTING WAS BLISTERED. N-1 TACHOMETER BEGAN TO WORK INTERMITTENTLY, ITT IND WENT OUT, FIRE LIGHT CAME ON, HIGH-PRESSURE BLEED AIR DUCT OVERHEAT WARNING CAMESDR 2007FA0000408Exhaust Duct · crackedWHILE PREFORMING SCHEDULED MAINTENANCE,REMOVED EXHAUST STACKS TO FACILTATE INSPECTING THE EXHAUST DUCT.A CRACK WAS FOUND IN THE SKI SLOPE.POWER SECTION WAS REMOVED FOR REPAIR.SDR 2005FA0000458Exhaust Stack · crackedCRACK IN FLANGE DUE TO ENGINE VIBRATION. (K)SDR 03132005Exhaust Duct · damagedPILOTS REPORT THAT WHILE EN ROUTE FROM MERRILL FIELD TO ANCHORAGE INTL, HEARD AN UNUSUAL NOISE AND FEEL A LOW FREQUENCY VIBRATION. ALL SYSTEM AND ENGINE INDICATIONS WERE NORMAL. POST FLIGHT INSPECTION REVEILED DAMAGE ON THE NR 1 ENGINE TURBINE WHEEL AND REARSDR 2005FA0000405Exhaust Stack · crackedEXHAUST STACK CRACKED IN BASE METAL DUE TO VIBRATION. (K)SDR 2005FA0000404Exhaust Stack · crackedCRACK IN BARE METAL DUE TO ENGINE VIBRATION. (K)SDR CA050309012Duct · cracked(CAN) AT EXHAUST PORT, THE FLANGE THAT PROTRUDES OUT OF THE CASE TO PREVENT EXHAUST GASES FROM EXITING THROUGH THE FLANGE WHERE THE EXHAUST STACK BOLTS ON, WAS CRACKED ABOUT 320 DEGREES AROUND THE CIRCUMFERENCE. THE OPPOSITE PORT WAS DETERMINED TO BE CRACKED TSDR 2005FA0000634Clamp · crackedLT ENGINE IB EXHAUST TAILPIPE CRACKED, EXPELLING HEAT INTO ENGINE COMPARTMENT, BURNING PAINT ON COWLING. PART FAILURE OCCURRED BECAUSE OF BROKEN SUPPORT CLAMP, NO PN AVAILABLE DUE TO THE LIMITED PRODUCTION OF THIS AIRCRAFT ON EITHER EXHAUST TAILPIPE OR SUPPORSDR QXEA200500369Shroud · crackedYYC - LEFTHAND NACELLE AFT EXHAUST SHROUD IS CRACKED AT MID SPRING CLIPS AND AT AFT BRACKET. REPAIRED IAW RD 8/4-54-227 AND 8/4-54-009 AND HORIZON AIR EA 6-54-332.SDR 2005FA0000364Clamp · oversizedBOTH TAILPIPE/MUFFLER CONNECTIONS WERE FOUND TO BE OVERSIZED. THE EXHAUST PIPE CLAMPS WERE NOT OF SUFFICIENT STRENGTH TO SQUEEZE THE OVERSIZED PIPE DOWN ON THE MUFFLER EXHAUST TUBE. THE RESULTING LOOSE FIT WAS ALLOWING EXHAUST FUMES TO SHOOT INTO THE CABIN HSDR 05FDEA00021Thrust Reverser · crackedNR 3 ENGINE, LT THRUST REVERSER, TRANSLATING COWL, UPPER TRACK, MOST AFT END FOUND WITH CRACKED. THRUST REVERSER P/N 683L220G04, S/N R591-090 NR 3 ENGINE, LT THRUST REVERSER REMOVED AND REPLACED PER AMM 78-33-01-4. THRUST REVERSER DOOR ADJUSTMENT AND CHESDR CA050105005Exhaust Duct · cracked(CAN) PILOT REPORTED, NO N2 INDICATION FOR NR 2 ENGINE. UPON INSPECTION, WHEN N2 PICKUP WAS REMOVED FROM THE ACCY GEARBOX, IT WAS OBSERVED THAT THE NR 5 BEARING NUT HAD BACKED OFF ON THE PT OUTER SHAFT TRAVELING AWAY FROM THE N2 PICKUP, HENCE 'NO N2 INDICATIONSDR 2005FA0000332Exhaust Pipe · crackedAIRCRAFT OWNER SQUAWKED MANIFOLD PRESSURE AT 11 PERCENT. FOUND EXHAUST CRACKED AT NR 5 CYLINDER EXHAUST PORT. CRACK EMINATES FROM REAR OF MOUNTING FLANGE AND SPIRALS DOWN COUNTER CLOCKWISE SEVERAL INCHES FROM THERE.SDR CA041216012Tank · cracked(CAN) RIGHT FUEL COLLECTOR TANK WAS LEAKING INSIDE THE WHEEL WELL.FOUND TANK WAS CRACKED ON THE UPPER INBOARD WELD FLANGE.SDR CA041215001Exhaust Duct · cracked(CAN) DURING ROUTINE MAINTENANCE 2 CRACKS WERE FOUND ON THE STARBOARD ENGINE EXHAUSTDUCT. THE CRACKS WERE LOCATED APPROXIMATELY 1.250 INCHES AFT OF THE REDUCTION GEARBOX MOUNTING FLANGE BETWEEN THE 10 AND 11:30 CLOCK POSITIONS. THE ORIGIN APPEARED TO BE FROM TSDR IJA2005F00002Exhaust Pipe · vibrationSTARTER GEN VIBRATION WAS CHECKED AFTER A NR 1 ENGINE EXHAUST PIPE WAS FOUND CRACKED. VIBRATION WAS ABOVE LIMITS AND THE STARTER WAS REMOVED AND REPLACED WITH O/H STARTER GEN. SERVICEABLE EXHAUST PIPE WAS INSTALLED. (CE07200506287) (K)SDR UIEA200400201Structure · missingPOST FLIGHT INSPECTION, FLT EK4979, 07/DEC/2004. DURING INSPECTION, FOUND NR 4 ENGINE AFT CENTER BODY CRACKED OFF. MISSING, LAST 20 INCHES FROM T/E. REMOVED AND REPLACED NR 4 ENGINE AFT CTR BODY IAW MM 78-11-02. INSPECTED AREA AFT OF NR 4 ENGINE FLAPS, WINSDR 2005FA0000010Clamp · crackedTHE DEFECT IS A FATIGUE CRACK, CAUSED BY BEING OVERSTRESSED DUE TO LOAD LIMITS, POSSIBLE OVERTORQUED. MAYBE THIS PART SHOULD BE MADE STRONGER, TO HANDLE THE STRESS. THIS DEFECT WAS FOUND BY A PENETRANT INSPECTION. THE LOCKING NUT NEEDS TO BE REMOVED, IN THSDR 2005FA0000235Exhaust Riser · crackedFOUND LT ENGINE OB EXHAUST RISER CRACKED WHILE PERFORMING A 50 HOUR EXHAUST INSPECTION IAW AD 00-01-16. (GL21200500869) (K)SDR CA041119002Segment · burnedDURING THE INSPECTION OF THE LT ENGINE AFTER IN-FLIGHT STOPPAGE, A HOLE WAS FOUND N AN EXHAUST SEGMENT. DUE TO RESTRICTED SPACE A HEAT SHROUD THAT CONCEALED THE HOLE COULD NOT BE REMOVED WITHOUT REMOVING THE ENTIRE EXHAUST SYSTEM. THE HOT GASES ESCAPING FROMSDR CA051003016Exhaust Header · cracked(CAN) NR5 EXHAUST HEADER FOUND CRACKED 75 PERCENT OF THE WAY AROUND JUST BELOW FLANGE WELD.SDR MALA040664Tail Cone · detachedGROUND CREW FOUND TAILCONE ON GROUND AFTER PUSHBACK. BY THE TIME GROUND CREW FOUND CONE AND NOTIFIED DISPATCH AND MAINTENANCE CONTROL, A/C HAD DEPARTED DSM. MAINTENANCE CONTROL AND DISPATCH NOTIFIED CREW TO RETURN TO DSM. WHEN A/C RETURNEDTO DSM, FOUND TAILSDR 2005FA0000239Exhaust Pipe · broken(ACCIDENT NR DFW05CA024) ON TAKEOFF CLIMB, EXHAUST PIPE BROKE AND WENT THROUGH 4 BLADED PROPELLER, SHEARING OFF ONE PROPELLER BLADE. EXHAUST PIPE STRUCK RT TAILBOOM, DOING STRUCTURAL DAMAGE TO TAILBOOM. (SW11200502888) (K)SDR IJA2005F00001Exhaust Pipe · failed(3) OUT OF (4) STRUTS THAT HOLD THE OUTSIDE PART OF THE EXHAUST ON FAILED. TT OF THE PART IS UNKNOWN. MFG THINKS THE PROBLEM IS RELATED TO A HIGH VIBRATION IN THE STARTER GEN. THE VIBRATION LEVEL WAS .04 WHICH IS WELL BELOW THE LIMIT. (CE07200502200) (K)SDR CHQA000559Diffuser · separatedON WALK AROUND AFTER FLIGHT 6357, THE FLIGHT CREW NOTICED .3333 TO .5000 OF THE NR 2 ENGINE EXHAUST MIXER ASSEMBLY WAS MISSING. MAINTENANCE DISCOVERED .3333 OF THE DIFFUSER IS MISSING ALONG WITH INTERNAL DAMAGE TO THE THRUST REVERSER AND EXHAUST CONE. MAINTENSDR 2004FA0000702Exhaust Header · brokenON INSTALLATION OF NEW NR 4 EXHAUST PIPE, THE FLANGE WELD BEGAN TO CRACK. THIS WAS WITH LITTLE TORQUE APPLIED THE FLANGE. SUBMITTED REPORT TO MFG AND DISCUSSED WHAT MAY POSSIBLY BE CAUSING THIS PROBLEM. THEY SEEMED TO THINK IT WAS THE USE OF MFG EXHAUST GASSDR 2004FA0000701Exhaust Header · brokenON 100 HR INSPECTION FOUND EXHAUST RISER CRACKED AND NEARLY BROKEN AT NR 4 EXHAUST OB MOUNTING BOLT EXTENDING INTO THE WELD AROUND THE PIPE.SDR 2689200410001Crossover Tube · crackedDURING ANNUAL INSPECTION, DISCOVERED CRACK APPROXIMATELY 1.5 INCHES IN LENGTH AROUND THE LT CROSSOVER ASSEMBLY. UPON REMOVAL, ALSO FOUND DETERIORATION IN THE SLIP JOINT CONNECTING THE RT CROSSOVER ASSEMBLY (PN 2254013). REPLACED BOTH PARTS WITH FACTORY NEW.SDR 2004FA0000703Exhaust Header · brokenON 100 HOUR INSPECTION FOUND EXHAUST RISER BROKEN AT NR 2 EXHAUST IB MOUNTING BOLT. SUBMITTED REPORT TO MFG.SDR 16970704Exhaust Header · crackedTHIS AIRCRAFT HAD THE NR 1,NR 3,NR 5 HEADERS REPLACED WITH NEW PARTS AT 154.0 HRS. THE AIRCRAFT THEN EXPERIENCED A CRACK IN THE NR 5 HEADER AT 180.0 HRS. THERE DOES NOT SEEM TO BE ANY ABNORMAL STRESS ON THE PART/INSTALLATION. AIRCRAFT EXHAUST SYSTEM WILL BE MSDR CA040719006Turnbuckle · shearedDURING INSPECTION MAINTENANCE CREW NOTED THAT THE RIGHT HAND ENGINE OUTBOARD EXHAUST SUPPORT TURNBUCKLE HAD SHEARED CAUSING THE TAILPIPE TO REST ON THE BOTTOM OF THE EXHAUST SHROUD INSTEAD OF BEING SUPPORTED IN THE CENTER. THE TURNBUCKLE WAS REPLACED WITH A SSDR CA040713009Exhaust Stack · cracked(CAN) LT EXHAUST STACK CRACKED FROM ONE MOUNTING HOLE OUTWARDS. STACK REPLACED WITH SERVICEABLE UNIT. CRACK DISCOVERED DURING ENGINE INSPECTION.SDR CA040713002Exhaust Stack · cracked(CAN) UNDISTINGUISHABLE ODOR OF SOMETHING BURNING, FOLLOWED BY STIFF CARB HEAT CABLE AND ENGINE RUNNING ROUGH WITH CARB HEAT APPLICATION. THE RT EXHAUST STACK HAD CRACKED, HIDDEN BY THE CARBURETOR HEAT SHROUD. DURING FLIGHT, THE HEAT FROM THE EXHAUST BEING ESDR QXEA200400486Panel · damagedPDX - NR 2 ENGINE AFT RIGHT EXHAUST PANEL 424AR HAS DAMAGE ON AFT EDGE FROM INTERFERENCE WITH AFT EXHAUST COLLECTOR SHROUD. REPAIRED IAW RD 8/4-54-012.SDR QXEA200400485Shroud · crackedPDX - NR 2 EXHAUST SHROUD DECK CRACKED ABOVE CHANNEL AT AFT EXHAUST EJECTOR SHROUD AFT ATTACH BOLTS. REPAIRED IAW RD 8/4-54-044.SDR QXEA200400484Shroud · crackedPDX - NR 2 EXHAUST SHROUD DECK CHANNEL AT AFT EXHAUST EJECTOR SHROUD ATTACH BOLTS CRACKED. REPAIRED IAW RD 8/4-54-033.SDR CA040630004Tube · cracked(CAN) CRACK WAS DISCOVERED AT INSPECTION NEXT TO EXHAUST TUBE USED TO SUPPLY ENGINE EXHAUST TO COWLING LIP DEICE. ABOUT ONE INCH FROM ENGINE MOUNTING FLANGE , CRACK WAS ABOUT ONE AND A QUARTER INCH LONG. REPAIR PERFORMED IAW MM CHAPTER 78 10-01.SDR 2004FA0000631Clamp · crackedWHILE DOING THE EXHAUST AD2000-01-16, THE ONE PIECE V CLAMP THAT HOLDS THE EXHAUST TO THE TURBO WAS FOUND CRACKED APPROX 50 PERCENT AROUND, REPLACED CLAMP AND LEAK CHECKED OK. THE CRACKED CLAMP DID NOT APPEAR TO BE OVER TORQUED.SDR CA040609014Tailpipe · cracked(CAN) DURING ROUTINE MAINTENANCE A 5-6 IN CRACK AT THE 6 O’CLOCK POSITION AND A 4 IN CRACK AT THE 12 O’CLOCK POSITION, OF THE NR 2 ENGINE TAILPIPE WAS FOUND. BOTH CRACKS REPAIRED IAW MFG MM 78-38-43.SDR 421C052404MTExhaust Stack · crackedON THE DAILY INSPECTION, EXHAUST STAINS WERE NOTED ON THE IB SIDE OF THE NR 2 ENGINE COWL. ON FURTHER INSPECTION A CRACK WAS DISCOVERED ON THE EXHAUST STACK AT THE NR 6 RISER. THE 9 INCH CRACK APPEARS TO HAVE STARTED ON THE WELD BETWEEN THE RISER AND STACK OSDR QXEA200400351Attach Bracket · crackedPDX - NR 1 EXHAUST OUTLET (FINGERNAIL) HAS SIX CRACKED BRACKETS BETWEEN INNER AND OUTER LAYERS AND THE LOWER AFT ATTACH BRACKET IS CRACKED. REPAIRED IAW -8 TASK 78-10-26-400-801.SDR CED2004F00001Case · crackedWHILE ENROUTE, AT FLIGHT LEVEL 390 FLIGHT CREW OBSERVED A FIRE INDICATION ON THE NR 2 ENGINE. THE FLIGHT CREW WAS ABLE TO EXTINGUISH THE FIRE INDICATION LIGHT USING STANDARD EMERGENCY PROCEDURES. THE FLIGHT CREW THEN DECLARED AN EMERGENCY AND RETURNED WITH NSDR AUS20040396Shield · separated(AUS) EXHAUST SHIELD MISSING. ATTACHMENT TABS REMAINED ON EXHAUST ASSEMBLY.SDR CA040428003Exhaust Stack · cracked(CAN) DURING ROUTINE INSPECTION A CRACK WAS NOTED AT THE LIP HEAT WELD TO THE FORWARD SECTION OF THE EXHAUST STACK. EXHAUST UNIT WAS ORDERED AND INSTALLED WITHOUT ANY INCIDENT.SDR 2004FA0000389Exhaust Duct · brokenIB EXHAUST ON LT ENGINE BROKE AT THE WELD BELOW NR 3 CYLINDER. BURNED HOLE IN LOWER ENGINE COWLING. BURNED WIRE BUNDLE ON THE FIREWALL AFT OF NR 1 CYLINDER. SCORCHED FIRE SLEEVE ON THREE FUEL HOSES.SDR P5CA0401099Nozzle · dentedNR 1 ENGINE EXHAUST NOZZLE HAS A DENT AT 7 O`CLOCK 5.125 LONG .5 INCH WIDE AND .001 INCH DEEP, BEYOND .80 LIMIT. REMOVED AND REPLACED EXHAUST NOZZLE.SDR 2004FA0000386Exhaust Stack · fracturedDURING CRUISE FLT AT 7,500 FT. VFR, AIRCRAFT WOULD NOT MAINTAIN 25 INCHES MP. MP DROPPED TO 23 INCHES AFTER APPROX. 15 MIN. MP DROPPED ABRUPTLY TO 18.5 INCHES MP MADE EMERGENCY DESCENT & UNSCHEDULING LANDING AT VNX WITHIN 3 MINUTES OF POWER LOSS. UPON EXAMINATSDR KBM2004F00140Strap · wornENGINE EXHAUST STACK HEAT SHIELD STRAP BRACKET IS WORN. REMOVED AND REPLACED.SDR KBM2004F00115Strap · wornEXHAUST HEAT SHRINK STRAP WORN. REMOVED AND REPLACED.
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