JASC 7160
Service difficulty reports · 1,162
Reports filed under 7160 · Engine Air Intake System, 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 = '7160' 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 = '7160' 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 A6WA200000068Scoop · crackedNR 1 ENGINE OUT BOARD DOOR NACA SCOOP AND ATTACHMENTS CRACKED. MAINTENANCE REPAIRED FAN DOOR NACA SCOOP AS REQUIRED ALSO REPAIRED APLITTER ANGLE IAW SRM AND FAX BARA/AVR/5228/00.SDR L1GA200000390Nose Cowl · crackedA .3 INCH LONG CRACK NR 1 ENG NOSE COWL 11 O CLOCK POS 10 INCHES AFT OF L/E. INSTALLED REPAIR DOUBLER.SDR L1GA200000389Nose Cowl · dentedFOUR LOCALIZED DENTS NR 2 ENGINE NOSE COWL. INSTALLED DOUBLERS.SDR SWAA002309Bullet · looseIN FLIGHT SHUT-DOWN, AIR TURNBACK, DECLARED EMERGENCY. NR 1 ENGINE DEVELOPED HIGH VIBRATION AND LOSS OF POWER ON TAKEOFF, ENGINE SECURED PER QRH. FOUND NOSE DOME SEPARATED FROM ENGINE. REMOVED AND REPLACED NR 1 ENGINE PER MM.SDR 20001204SH001Alt Air Door · brokenIMMEDIATELY AFTER THROTTLE UP FOR TAKEOFF, ENGINE LOST SIGNIFICANT POWER. PILOT TRIED TO RETARD THROTTLE TO ABORT, BUT LEVER WOULD ONLY GO ABOUT HALF WAY BACK. HE THEN SLIGHTLY ADVANCED THROTTLE AND THEN WAS ABLE TO PULL THROTTLE ALL THE WAY BACK TO IDLE POSSDR 20001101SH008Alt Air Door · failedPILOT REPORTED LOSS OF POWER ON TAKEOFF CLIMB. AFTER RETURNING TO THE AIRPORT, INVESTIGATION REVEALED A FAILED ALTERNATE AIR DOOR. (X)SDR 20001013SH028Bolt · missingFOUND FORWARD SECURING BOLT MISSING FROM INTAKE PLENUM. SUBMITTER STATED THERE WAS NO SIGN OF EVER BEING INSTALLED. (X)SDR 20001109SH032Valve · brokenON ENGINE TBO CHANGE BEFORE INSTALLING THE INDUCTION AIR BOX, DISCOVERED THAT ONE HALF OF THE FLASHBACK VALVE HAD BROKEN AND WAS BACK IN THE AIR BOX. BOTH HALVES AND SPRING WERE REPLACED. (X)SDR DHL200072002CSkin · brokenDURING C CHECK, FOUND NR 3 ENGINE NOSE COWL, 3 O'' CLOCK POSITION, T/E SKIN PIECE BROKEN OFF. INSTALLED DOUBLER REPAIR PER B727 SRM 54-30-3, SIZE OF REPAIR 2 X 6 INCH.SDR UPS00233768Duct · crackedINSPECTION TYPE:N/A, S-DUCT HAS 14 INCH CRACK REF D198327. REPAIRED DAMAGED DUCT AS PER B727-SRM-54-30-4.SDR 20001120SH050Nose Cowl · crackedNR 1 ENGINE NOSE COWL FLANGE CRACKED. REPAIRED PER ECRA 621-71-007. (X)SDR 20000913SH028Alt Air Door · brokenDURING A FLIGHT LESSON, ENGINE LOST POWER AND AN EMERGENCY LANDING WAS MADE, NO INJURIES OR DAMAGE. DURING INSPECTION AFTER LANDING, ENGINE DEVELOPED POWER WHEN COLD. REMOVED AIR FILTER ELEMENT, DISCOVERED HEAT DAMAGE TO FILTER ELEMENT AND FOUND ALT AIR DOORSDR DHL200072011CSkin · crackedNR 3 ENGINE NOSE COWL, 4 O'' CLOCK SIDE POSITION T/E SKIN CRACKED AT FASTENER. INSTALLED DOUBLER REPAIR.SDR AU000786Hose · missing(AUS) CARBURETOR HEAT HOSE LOCATED BETWEEN FORWARD RIGHT ENGINE BAFFLE AND THE RIGHT MUFFLER MISSING. (X)SDR DHL200072004CDuct · crackedDURING C CHECK, FOUND NR 2 ENGINE INLET S DUCT WITH APPROX 4 INCH VERTICAL CRACK BETWEEN FASTENERS 80 INCHES FROM AFT END OF DUCT AT 8 O CLOCK. INSTALLED DOUBLER PER B727 SRM 54-10-3 FIG 65, SIZE OF REPAIR 10 X 5.5 INCHES.SDR 20000913SH027Plenum · crackedINLET PORTION OF PLENUM ASSEMBLY CRACKED AT WELD AREA. (X)SDR 20000814SH003Gasket · inadequateTHIS AIRCRAFT HAS THE SAME AIR FILTER AND LANDING LIGHT ASSY AS THE PA28140 150-150 WITH BAD GASKETS. SUBMITTER FEELS AD96-10-01-R1 SHOULD APPLY. (X)SDR 20000811SH022Duct · crackedINLET DUCT, CRACKED OUT AT NUTPLATE AT FORWARD MIDDLE SCREW OF DOOR PN 58-910028-17 THAT IS ATTACHED TO THE INLET DUCT. NOTE: BOTH LEFT AND RIGHT ENGINES INLET DUCTS BROKEN AT THE SAME TIME. THE CAUSE COULD BE VIBRATION INDUCED BY THE AIR STREAM. SUBMITTERSDR 20000808SH018Rivet · frettedDURING ROUTINE INSPECTION, LOOSE RIVETS WERE FOUND IN THE TOP PLATE CURBED AREA AFT OF THE ENGINE IN BOTH MOUNT BEAMS OF LEFT ENGINE. SOME RIVET HEADS HAD FRETTED INTO THE SURFACE OF THE PLATE. THE SUSPECTED CAUSE WOULD BE A VIBRATION IN THIS AREA. AN ENGINSDR 20010425CW016Clamp · unsecureNR 1 ENGINE POWER FAILED TO REDUCE BELOW 2200 LBS. TORQUE FOR LANDING. THE ENGINE WAS SHUT DOWN IN FLIGHT JUST PRIOR TO LANDING. A NON EVENTFUL LANDING WAS ACCOMPLISHED AND THE ENGINE WAS RESTARTED FOR TAXI TO HANGAR. MAINTENANCE WAS UNABLE TO VERIFY THE CASDR 20000724SH026Air Box · detachedDURING T/S OF ROUGH ENG OPERATION FOLLOWED BY NOTED REDUCTION IN AVAILABLE POWER, THE ALTERNATE-AIR DOOR PN 1652013-25 WAS FOUND LOOSE IN THE INDUCTION BOX. THE HINGE PIN HAD SLID OUT OF THE HINGE ALLOWING THE DOOR TO PARTIALLY OBSTRUCT THE AIR FLOW TO HE ENSDR 20000821SH005Air Filter · deterioratedAIR FILTER IS LISTED AS A 500-HOUR REPLACEMENT ITEM. AT 100-HOUR INSPECTION, MADE AT 300 HOURS, NOTED THE INSPECTION AT 200 HOURS AND THE INSPECTION AT 300 HOURS THE PAPER ELEMENT OF THE FILTER ASSY HAD BADLY ERODED ON APPROXIMATELY 40 PERCENT OF THE FORWARD SDR 20000713SH006Paint · looseDURING THE FIRST PHASE 1 INSPECTION, AN AREA APPROXIMATELY 3 INCHES SQUARE ON THE INSIDE BOTTOM OF THE INERTIAL SEPARATOR HAD LOOSE EPOXY PAINT PEELING LOOSE. 15 GRAMS OF CHIPS REMOVED WITH FINGERNAIL. AN UNKNOWN MOUNT WAS MISSING AND PRESUMABLY WENT THROUGHSDR 20000627SH013Air Box · missingENGINE DEVELOPED VIBRATION IN-FLIGHT AND LOSS OF POWER. MAINTENANCE REMOVED CARBURETOR AIR BOX AND CARBURETOR. FOUND PIECE OF SEAL FROM AIR BOX FLAPPER VALVE BROKEN OFF AND LODGED IN THE VENTURI. (X)SDR CA000714037Screw · worn(CAN) THE RETAINING BOLT FOR THE AIR FILTER HOUSING BACKED OFF FROM THE TORQUED POSITION AND ALLOWED THE HOUSING TO MOVE FORWARD AND STRIKE THE PROPELLER DURING FLIGHT. A VIBRATION WAS FELT BY THE PILOT AND HE RETURNED THE AIRCRAFT TO BASE AND LANDED SAFELY. SDR AU000456Hose · loose(AUS) ENGINE CARBURETOR HEAT SCAT HOSE CLAMP MISSING.SDR 20000626SH010Gasket · looseTHE DIAMETER OF HEAT BOX THROAT IS LARGER THAN SEALING SURFACE OF CARBURETOR GASKET ALLOWING CARBURETOR BASKET TO REMAIN LOOSE. COULD BE SUCKED INTO CARBURETOR. NOTED DURING ENGINE CHANGE. (X)SDR PCAA0004028Door · failedFLT 3800: UPON CLIMBOUT, THE NR 1 ENGINE BYPASS INTAKE DOOR WOULD NOT OPEN. AIRCRAFT RETURNED TO FIELD DUE TO EXPECTED ICING CONDITIONS. MAINTENANCE INSPECTED, CLEANED AND LUBED THE BYPASS DOOR ACTUATOR SHAFT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WSDR AU000326Retainer · missing(AUS) FOAM AIR FILTER ELEMENT INGESTED INTO THE CARBURETTOR.INVESTIGATION FOUND ONLY ONE FILTER RETAINER WAS FITTED INSTEAD OF TWO. FURTHER CHECKING FOUND THAT THE IPC MAY BE MISLEADING INTHE NUMBER OF RETAINERS TO BE FITTED.SDR AU000136Intake Duct · contaminated(AUS) AIR INTAKE HOUSING BLOCKED BY WATER FOLLOWING LANDING IN FLOOD WATER. ENGINE FAILURE CAUSED A HARD LANDING WHICH RESULTED IN DAMAGE TO THE LANDING GEAR, ENGINE FRAMES AND BELLY SKIN.SDR CA000301004Retainer · damaged(CAN) DURING CRUISE OPERATIONS, THE THUMB SCREW (PIPER P/N 63674-00) BECAME LOOSE OWING TO WORN PLASTI-LOK ON THE ANCHOR PLATE WHICH IS MOUNTED ON THE AIR FILTER RETAINING ASSEMBLY; WHICH IS THE ONLY ATTACHING POINT FOR THE AIR FILTER RETAINING ASSEMBLY. THE SDR AC2A0000014Screen · damagedBROKEN WIRES IN SCREEN. REPLACED SCREEN WITH LIKE ITEM. (X)SDR PLGA000103ADuct · damagedBOS - FLT 3055 - ON CLIMB-OUT, THE RIGHT ENGINE INTAKE HEAT FAILED. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT INLET PARTICLE DUCT, P/N NH24668-083 S/N L219855, AND LOWER DUCT AND PERFORMED ALL OPERATIONAL CHECKS GOOSDR AU000128043Arm · broken(AU) CARBURETOR HEAT BOX ACTUATOR ARM HAD BROKEN OFF AT RIVETS THAT SECURE SPRING STEEL STRIP TO ARM.SDR CA991028057Air Filter · clogged(CAN) AIRCRAFT FLEW IN RAIN APPROXIMATELY 45 MINUTES, AND THEN CAME OUT IN THE CLEAR AT 7,000 FEET, AND -5 DEGREES CELSIUS. ENGINES FUEL FLOW DECREASED, ENGINES SLOWED DOWN. PILOT SELECTED ALTERNATE AIR ON AND RECOVERED POWER. RE-SELECTED ALTERNATE AIR OSDR 2000ZZZX702Rivet · shearedNR 1 ENGINE RIVET HEAD SHEARED IN INTAKE FOR PNEUMATIC HEAT EXCHANGER. IT IS ACCEPTABLE TO USE AS IS, IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-3 DATED 9-9-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR ERAA064508Air Filter · crackedTHERE ARE SEVERAL CRACKS ON FILTER HOUSING ADJACENT TO O-RING BORE.SDR 99ZZZX3815Screen · brokenDURING POST-FLIGHT CHECK OF NR 1 ENGINE, THE INLET COMPRESSOR WAS FOUND WITH FOD DAMAGE. THE FOD DAMAGE WAS BEYOND ENGINE MANUFACTURER LIMITS. MAINTENANCE AND FLIGHT CREWS INSPECTED THE AIRCRAFT'S NR 1 ENGINE INLET PLENUM TO DETERMINE WHERE THE SOURCE OF FODSDR 99ZZZX3814Screen · brokenDURING POST-FLIGHT CHECK OF NR 1 ENGINE, THE INLET COMPRESSOR WAS FOUND WITH FOD DAMAGE. THE FOD DAMAGE WAS BEYOND ENGINE MANUFACTURER LIMITS. MAINTENANCE AND FLIGHT CREWS INSPECTED THE AIRCRAFT'S NR 1 ENGINE INLET PLENUM TO DETERMINE WHERE THE SOURCE OF FODSDR AU991006Connector · failed(AUS) NR 1 STRUT BULKHEAD CONNECTORS ARCING. FURTHER INVESTIGATION FOUND THE WIRING LOOM CONDUIT D8451P DRAIN HOLE INCORRECTLY POSITIONED ALLOWING A BUILD UP OF HYDRAULIC FLUID AT THE REAR OF THE CONNECTOR WHICH CAUSED DETERIORATION OF THE RUBBER INSERT WHICHSDR 2000ZZZX701Rivet · shearedNR 1 ENGINE RIVET HEAD SHEARED IN INTAKE FOR OIL COOLER. IT IS ACCEPTABLE TO USE AS IS. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-3 DATED 9-9-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR CA990927010Actuator · failed(CAN) FLIGHT CREW REPORTED THAT THE NR 2 ENGINE INTAKE DOOR WOULD NOT OPEN. PROBLEM TRACED TO THE AIR INTAKE DOOR LINEAR ACTUATOR.SDR 99ZZZX3602Air Door · brokenAIRCRAFT LOST POWER ON TAKEOFF AND HAD TO MAKE AN EMERGENCY LANDING. AIRCRAFT WAS ABLE TO RETURN TO AIRPORT. TOWER REPORTED A LARGE AMOUNT OF BLACK SMOKE COMING FROM AIRCRAFT. DUPLICATED PROBLEM ON GROUND RUN. REMOVED AIRBOX AND FOUND ALTERNATE AIR DOOR LASDR CA990907089Sealer · dislodged(CAN) SEALER USED IN ASSEMBLY OF CARBURETOR. HEAT BOX DISLODGED AND CAUGHT AROUND CARBURETOR VENTURI.SDR 99ZZZX2941Gasket · deterioratedREMOVED FILTER ASSY, P/N BA 8110, TO CHECK GASKET, 8 INCHES OF GASKET WAS MISSING. SCREEN MESH COMING LOOSE FROM FILTER FRAME.SDR RRXA991490Skin · dentedDURING A MAINTENANCE VISIT FOUND DENT, NR 1 ENGINE RING COWL AT 5 O'CLOCK POSITION. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. CUT ACCESS HOLE, STRAIGHTENED DENT WITHIN LIMITS DC8 SRM 71-5-2. FABRICATED AND INSTSDR 99ZZZX2735Airbox · brokenDURING FIRST PHASE 1 INSPECTION, FOUND AIRBOX ASSY HAD PIECE MISSING AROUND ALTERNATE AIR DOOR AND THE DOOR HAD A GAP WHERE THE PIECE WAS MISSING. A FILLER MATERIAL WAS USED TO FILL IN ONE EDGE AS THE AIR DOOR HINGE WAS MISALIGNED. THE FILLER MATERIAL BROKE OFSDR 99ZZZX2573Air Filter · alteredDURING ANNUAL INSPECTION, THE ORIGINAL AIR FILTER ASSEMBLY WAS FOUND TO HAVE HAD THE GUTS REMOVED AND ALTERED TO ACCEPT A BRACKET AIR FILTER ELEMENT BA-4106 WHICH WAS CUT TO SIZE. THIS IS NOT APPROVED AND NOT SAFE. AIRCRAFT TT: 2,385.0 HOURS.SDR 99ZZZX2546Air Box · crackedPILOT REPORTED THAT WiTH FULL THROTTLE AND THE WASTEGATE CLOSED, ENGINE HAD EXCESSIVELY LOW BOOST. (TURBO CHARGER INSTALLATION WAS AN AFTERMARKET INSTALLATION. ALSO, RECORDS WERE UNAVAILABLE AS OF THIS DATE TO DETERMINE AIRCRAFT TIMES, TURBO CHARGER STC, ETCSDR HEEA062155Support · crackedCRACK AROUND BOTTOM SUPPORT BOLT AREA.
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