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 HALA0600823Skin · damagedNR 1 ENGINE IB FAN COWL HAS FIBER DAMAGE ON AFT EDGE 12" DOWN FROM UPPER EDGE. NR 1 ENGINE INBD FAN COWL REPAIRED ON AFT EDGE 12" DOWN FROM UPPER EDGE, IAW SRM 54-23-01-2R-0, SRM 51-70-17-0G-0, SRM 51-70-04-0G-0, SRM 51-40-02-0G-0 AND AMM 51-21-10-377-003.SDR QXEA200602573Door · damagedSEA FLIGHT NR 2528: NR 1 ENGINE INTAKE BYPASS DOOR SWITCHLIGHT WAS DARK WITH SWITCH ACTIVATED. LAMPS CHECKED GOOD. SWITCH ACTIVATION/DEACTIVATION HAD NO EFFECT. CIRCUIT BREAKER (P6-'INTK DEC ACT 1') WAS TRIPPED. MAINTENANCE REMOVED AND REPLACED INTAKE BYPASDR MWEA060210Skin · delaminatedNR 2 ENGINE INLET COWL AFT CENTER EXHAUST HAS SKIN DELAMINATED AT 6 O'CLOCK POSITION AREA.SDR 06FDEA03258Inlet · unknownEXISTING EXTERNAL DOUBLER REPAIR APPROX 6 1/2" BY 6" ON NR 2 ENGINE NOSE INLET LT SIDE. (DOT 32) REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED NR 2 ENGINE LT AND RT NSDR CA060822004Intake · damaged(CAN) OUR AC WAS ABOUT TO DEPART WHEN DEFECT WAS SPOTTED. DURING A NORMAL PRE-FLIGHT PILOT WALK AROUND OUR PILOT NOTICED A GAP/ ABNORMAL SPACE BETWEEN THE LOWER ENGINE INLET AND THE UPPER MATING COWL. WE GROUNDED THE A/C TO AOG STATUS AND SENT AME`S TO RESCUSDR QXEA200602196Duct · gougedPDX: LEFT ENGINE LOWER INTAKE COWLING FORWARD INNER DUCT GOUGED ON LOWER SURFACE. MAINTENANCE REPAIRED IAW HORIZON EA 6-71-251. LT ENGINE LOWER INTAKE COWLING FORWARD INNER DUT MEETS THE PARAMETERS STATED IN EA 6-71-251 AND MAY BE LEFT AS IS.SDR Z6WR200600001Fitting · crackedTHE REFERENCED TR WAS SENT IN FOR SPECIFIC REPAIR AND DURING THE INSPECTION DISCOVERED A .8 INCH LONG CRACK IN THE VEE GROOVE FTG. THE CRACK IS AT THE UPPER END RUNNING THROUGH THE FIRST FASTENER LOCATION.SDR 2006UALA01004Cowling · dentedNR 2 ENG INLET COWL IS DENTED AT 11 O'CLOCK.SDR CA060530004Air Box · separatedSTUDENT REMOVED CARB HEAT AFTER EXERCISE AND A/C RPM RESPONDED BY DROPPING, SO CARB HEAT WAS REAPPLIED. ENG CONTINUED TO GET ROUGHER AND POWER WAS ADDED. ENDED UP WITH FULL POWER/CARB HOT AND ENGINE RESPONSE WAS 1900 RPM/75 KTS DESCENDING. ANY CHANGE TO PUTSDR CA060512006Flap · cracked(CAN) THE CARB HEAT FLAP ASSEMBLY HAD CRACKED UNDER THE DOUBLER PLATE, ALONG THE RIVET ATTCH LINE THAT CONNECTED THE FLAP/DOOR TO THE ACTUATING SHAFT BRACKET. (TC NR 20060512006)SDR PG9A109045Intake Duct · crackedCRACK FOUND AT THE WELD JUST IN FRONT OF THE BOTTOM SUPPORT BRACKET. REPLACED DUCT.SDR MALA060292Structure · chafedDURING 2 YEAR CHECK IN BNA, FOUND LT NACELLE, INTAKE COMPARTMENT DECK IS CHAFED OUT OF LIMITS AND HAS BEEN REPAIRED IAW MESABA EO#S54095, REF: EAMS WORK ORDER 213786 TASK 4502.SDR 2006FA0000494Air Box · maint errorAC HAD 180 HP ENGINE INSTALLED ON 7/10/96. AC HAS 1443.5 HOURS SINCE INSTALLATION. OPERATOR NOTED 2300 RPM AT CRUISE, FULL THROTTLE. INSPECTED AND FOUND AIRBOX STILL HAD THE HOLE SIZE FOR 160 HP ENGINE. AIRBOX HAD NOT BEEN MODIFIED IAW STC. IT HAD BEEN REPSDR 4437811Air Filter · debondedPN P560007-3, GASKET HAD SEPERATED FROM FILTER ON ONE SIDE AND WAS PULLED INTO THE AIR STREAM ON THE ENGINE SIDE OF THE FILTER. INSTALLED NEW FILTER.SDR CA060501006Vane · cracked(CAN) VANE FOUND SEVERELY CRACKED ON VISUAL INSPECTION. CRACK APPEARS TO HAVE STARTED AT LEADING EDGE OF VANE FROM THE HINGE AREA. HINGE WAS FOUND CRACKED ALSO. DAMAGE POSSIBLY ACCELERATED DUE TO FLUTTER OF THE DAMAGED VANE. (TC NR 20060501006)SDR PG9A108522Intake · crackedDURING AN INSPECTION ENGINE AIR INTAKE FOUND CRACKED, JUST AFT OF THE SUPPORT ASSEMBLY.SDR USAA060489Plate · damagedENGINE INLET, PPS 68.15 AT 6:00 O'CLOCK DAMAGED. CUT OUT DAMAGE, INSTALLED REPAIR, PER SRM 51-20-01 & EM71-11-03-300-019, DEFECT SIZE: 1" X 6".SDR CA060316001Clamp · failedDURING INSPECTION, RT ENGINE COWLING WAS OPENED AND TECHNICIAN FOUND PARTS OF RUBBER HOSE INSIDE COWLING. FURTHER INVESTIGATION LEAD TO OPENING OF THE RT LOWER ACCESS PANEL WHERE THE CLAMP FOR THE RT LOW PRESSURE BLEED AIR TO THE MIXING VALVE DUCT WAS FOUND BSDR UPS06146449Skin · crackedNR 1 ENGINE LIP SKIN CRACKED AT THE 4:00 POSITION APPROX 1 INCH IN LENGTH. REPAIRED NR 1 ENGINE LIP SKIN PER E.O. A300-7110-19750-E AND SRM 51-25-00 AND 54-10-00.SDR MALA060084Intake Duct · chafedDURING 4K INSPECTION IN YQB FOUND THE RT INTAKE DUCT WAS CHAFING ON THE NACELLE FRAME AT STATION 197. THE REPAIR WILL BE CARRIED OUT IAW MESABA EOS54147 ON MM409263256.SDR CA060124005Arm · cracked(CAN) ENGINE RECIEVED FOR OVERHAUL WITH AIRBOX INSTALLED. THE CARB DRIP TRAYS ARE CONNECTED TO THE AIRBOX BY A SUPPORT ARM WITH TWO SCREWS HOLDING THE TRAYS ONTO THE SUPPORT ARM. THE DRIP TRAY SUPPORT ARM WAS FOUND CRACKED AT THE HOLES FOR THE SCREWS. (TC 200SDR 2005FA0001636Filter · failedTHIS IS AN INDUCTION AIR FILTER BEARING. REMOVED 5 OF THESE FILTERS FROM SERVICE IN ADDITION TO THE ONE IN THIS REPORT WITH THE SAME DAMAGE SIMILAR TIME IN SERVICE. THE WIRE MESH THAT ENCLOSES THE COTTON FIBER FILTER MATERIAL IS TEARING AND EXPOSING THE FILTSDR 05FDEA04017Cowling · scratchedNR 2 ENG INLET COWL L/E HAS A 4.8" LONG SCRATCH AT 5:00 POS. REMOVED DAMAGED AREA IAW P&W SRM 54-10-00. PERFORMED HFEC IAW NTM 51-10-08. NO CRACKS NOTED. INSTALLED REPAIR DOUBLER AND FILLER IAW P&W SRM 54-10-00 REPAIR NR 10.SDR 05FDEA03928Frame · crackedNR 1 ENG NOSE INLET COWL INTERIOR AFT BULKHEAD CHORD ANGLE IS CRACK AT 7 O`CLOCK POSITION CAN BE VIEWED FROM OUTBOARD SIDE. REMOVED AND REPAIRED CRACKED CHORD ANGLE IAW DC10 SRM 54-11-00 FIG 1C VOL 1. N/R N00405, W/O N/R 00030375.SDR CA051108002Bolt · wornINDUCTION AIR BOX SUPPORT MOUNTING BOLT (AN3-34 BOLT) IS WORN PREMATURELY BY SUPPORT BRACKET 15671-002. THE SAME BOLT ALSO IS WEARING AT CONTACT AREA FROM ALTERNATE AIR DOOR SUPPORT BEARING P/N 50200-101. THIS BOLT SUPPORTS THE INDUCTION AIR BOX ONTO THE CRASDR AALA20050709Guide Vane · leakingDFW INFLIGHT T450/28OCT - AFTER TAKEOFF, RIGHT ENGINE OIL TEMPERATURE INDICATED 184 DEGREES FOLLOWED BY HEAVY SMOKE IN COCKPIT AND CABIN. SOURCE CLEARED WHILE ON APPROACH AND OIL TEMPERATURE RETURNED TO NORMAL. FOUND OIL LEAKING FROM VARIABLE GUIDE VANES ON SDR 2005FA0001454Intake · crackedCRACK IN BASE METAL FROM ENGINE VIBRATION. (K)SDR AU510001704Elbow · wornRT ENGINE AIR INDUCTION HOSE FLEXIBLE ELBOW TORN ON INSIDE RADIUS.SDR 05FDEA02942Nose Cowl · bird strikeAT ROTATION NOTICED BIRD FLOCK LEFT OF NOSE LEVEL AT 2000 FT NOTICED VIBRATION, CONTINUED TO CLIMB VIBRATION WAS NOTICED IN NR 1 START LEVER AND THROTTLE. AT 17000 NR 1 RED REV U/L APPEARS. RAN RED TABS, SHUT DOWN NR 1 ENGINE, RETURNED TO AFW. INSPECTED NR SDR CA050922002Structure · cracked(CAN) TRACES OF EXHAUST EMISSIONS WERE NOTICED COMING OUT OF EDGE OF INTAKE LIP. PART WAS REMOVED FROM COWL AND WITH THE TAPE AND INSULATION REMOVED, AN 8 INCH CRACK WAS REVEALED ON THE AFT SIDE OF THE EXHAUST CHAMBER PASSAGE. NEW INTAKE LIP KIT WAS FITTED, SDR CA050912005Air Filter · damaged(CAN) DURING AN 100 HR INSPECTION, THE AIR FILTER WAS BEING REPLACED. THE FILTER WAS FOUND DAMAGED AND REPLACED. INVESTIGATION REVEALED NO APPARENT REASON. THE PILOT WAS ASKED IF A BACKFIRE CONDITION OCCURRED AND NONE WAS EXPERIENCED AT THE TIME. THIS IS TSDR UPS05245508Intake Duct · crackedNR 2 ENG S-DUCT HAS A CRACKED ON INNER SKIN AT 3 O`CLOCK POS. ON RIB NR 5 REPAIR CARRIED OUT IAW AAAE EO 2005-087-002. UPS ENGINEERING FILE NR 727-54-20024.SDR 05FDEA02589Nose Cowl · vibrationON TAKEOFF RWY 25L VHHH, AFTER POWER REDUCTION TO CLIMB AT 1500 AFL, GOT A YAW "BUMP" AND NOISE AND VIBRATION "BUZZ" IN AIRFRAME. NO ABNORMAL INDICATIONS INITIALLY, THEN NR 1 COMPRESSOR VIBRATION CLIMBED TO 5.0 AMBER, REDUCED NR 1 THROTTLE AND BUZZ DIMINISHEDSDR DLM88050468Packing · leakingAFTER TAKEOFF, FLIGHT ATTENDANTS NOTIFIED FLIGHT CREW THAT BOTH AFT LAV SMOKE DETECTORS WERE GOING OFF. REPLACED PACKING IN LEFT ENGINE NOSE BULLET DUE TO OIL LEAK.SDR CA050920006Control Cable · separated(CAN) PILOT ACTUATED CARB HEAT AND HANDLE CAME UNSWAGED FROM CABLE. AIRCRAFT HAD TO COME BACK TO BASE PREMATURELY.SDR MWEA050072Support Angle · crackedRIGHT ENGINE NOSE COWL SUPPORT ANGLE CRACKED, FORWARD OF CIRCULAR WEB. -- FABRICATED AND INSTALLED CUP AND INSTALLED NEW CLIP.SDR 05FDEA02004Nose Cowl · damagedNR 1 ENGINE, NOSE INLET COWL INNER BARREL FROM 3, 9 AND 12 O' CLOCK POSITION FOUND DOUBLER WITH SHEARED RIVETS. NR 1 ENGINE, NOSE INLET COWL REMOVED AND REPLACED AS PER AMM 71- 11-01-4.SDR 05FDEA02003Nose Cowl · damagedNR 3 ENGINE, NOSE INLET COWL INNER BARREL FROM 6 TO 9 O' CLOCK POSITION FOUND WITH CORROSION. NR 3 ENGINE, NOSE INLET COWL REMOVED AND REPLACED PER AMM 71-11- 01-4.SDR B3OR20050718Intake Pipe · crackedWHILE REMOVING LT MAGNETO FOR TBO, THE NR 4 CYLINDER INTAKE PIPE HAD TO BE REMOVED FOR ACCESS TO THE MAGNETO. REMOVAL OF THE INTAKE PIPE REVEALED THAT THE INTAKE PIPE HAD A CRACK IN THE FLARE END THAT IS SECURED TO THE CYLINDER INTAKE PORT. FURTHER INVESTIGATISDR UPS05145259Cowling · damagedNR 2 ENG OTBD FAN COWL HAS HEAT DAMAGE. REMOVED AND REPLACED NR 2 ENG OTBD FAN COWL REF MM 71-13-02-4.SDR CLC2005F00007Ring · damagedDURING PREFLIGHT CHECK, DAMAGE WAS FOUND TO NR 2 ENGINE INTAKE AND FAN BLADES. ENGINE INTAKE HAS DAMAGE TO UPPER AND LOWER BELL MOUTH ADAPTOR RINGS, INTAKE INLET LIP HAD SKIN BLOWN OUT, NUMEROUS CRACKS FOUND ALONG CIRCUMFERENCE AT ATTACH FASTENERS. INLET SEASDR CLC2005F00006Inlet · damagedDURING PREFLIGHT CHECK, DAMAGE WAS FOUND NR 2 ENGINE INTAKE AND FAN BLADES. ENG INTAKE HAS DAMAGE TO UPPER AND LWR BELL MOUTH ADAPTOR RINGS, INTAKE INLET LIP HAD SECTION OF SKIN BLOWN OUT, NUMEROUS CRACKS FOUND ALONG CIRCUMFERENCE AT ATTACH FASTENERS. INLET SDR CLC2005F00005Seal · damagedDURING PREFLIGHT CHECK, DAMAGE WAS FOUND TO NR 2 ENGINE INTAKE AND FAN BLADES. ENGINE INTAKE HAS DAMAGE TO UPPER AND LWR BELLMOUTH ADAPTOR RINGS, INTAKE INLET LIP HAD SECTION OF SKIN BLOWN OUT, NUMEROUS CRACKS FOUND ALONG CIRCUMFERENCE AT ATTACH FASTENERS. ISDR CLC2005F00004Adapter Ring · damagedDURING PREFLIGHT CHECK, DAMAGE WAS FOUND TO NR 2 ENGINE INTAKE AND FAN BLADES. ENGINE INTAKE HAS DAMAGE TO UPPER AND LOWER BELL MOUTH ADAPTOR RINGS, INTAKE INLET LIP HAD SKIN BLOWN OUT, NUMEROUS CRACKS FOUND ALONG CIRCUMFERENCE AT ATTACH FASTENERS. INLET SEASDR CA050708001Nose Cowl · crackedDURING ROUTINE C-CHECK INSPECTION OF AIRCRAFT, SEVERAL CRACKS WERE FOUND ON THE NR 1 ENGINE INTAKE COWL. THE FORWARD DIAPHRAGM HAD MULTIPLE CRACKS ALL AROUND THE CIRCUMFERENCE, INCLUDING A 27 INCH CRACK AT THE LOWER SIDE. THE REAR DIAPHRAGM HAD 2 CRACKS. THSDR 2005FA0000978Nose Cowl · debondedSKIN PANELS HAVE DELAMINATED AT FWD EDGE, COMMON TO LIP SKIN. EVIDENCE OF HIGH TEMPERATURE AS FIBERGLASS APPEARS DARKENED AND IS BRITTLE. OUTER SKINS OF BARREL ARE DEBONDED AND DISCOLORED BY HIGH TEMPERATURE. PROBABLE CAUSE: ANTI-ICE LEFT OPERATING FOR LONSDR GTIA050198Packing · deterioratedAT CLIMB, EPR LEFT THROTTLE 1 AND ONE-HALF KNOB WIDTHS FORWARD OF RIGHT THROTTLE AT 210 CL, AIRCRAFT TAIL SWAP WITH 802. FOUND NOSE INLET BULLET PACKING AND GROMMET DETERIORATED. REMOVED AND REPLACED PACKINGS. THROTTLES STAGGER WITHIN LIMIT, LEAK CHECKED PTSDR 05FDEA01678Skin · crackedNR 2 ENGINE, NOSE INLET LIP FOUND CRACKED AT 8 O'CLOCK POSITION AND EXISTING REPAIR DOUBLER HAS LOOSE FASTENERS. REMOVED AND REPLACED AS PER AMM 54-22-01-4 AND APPLIED SEALANT AS PER AMM 54-22-01-4.SDR 2005FA0001070Door · failedINVESTIGATION OF LOW MANIFOLD PRESSURE BY TECH RVEALED THE STEEL TAB RIVETED TO ALTERNATE AIR DOOR FOR MAGNETIC CLOSURE HAD FALLEN OFF AND ENTERED TURBOCHARGER. THE RIVETS USED TO FASTEN TAB TO DOOR WERE MISSING ALONG WITH THE TAB. THE RIVET HOLES LOOKED ELOSDR 2005FA0001252Air Filter · failedACCIDENT INVESTIGATION FOUND RIGHT TURBO CHARGER COMPRESSOR INGESTED PAPER AND JAMMED. IT WAS DETERMINED THAT THE PAPER WAS THE INSTRUCTIONS AND APPLICATION CHART FOR THE FILTER. A CHECK OF A NEW REPLACEMENT DONALDSON (FAA/PMA FOR CESSNA FILTERS) FILTER REVE
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