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 6PMR202009150409Flange · corrodedAIRBORNE/PEMCO NON-ROUTINE 3024.0021 DISCREPANCY: NR 2 ENGINE INLET DUCT ATTACHMENT FLANGE HAS CORROSION AROUND MATING HOLES. CORRECTIVE ACTION: EVALUATED AND REPAIRED REF EO 54-757-7284.SDR IPXA2020083199606Web · crackedINSPECTION TYPE:A 300 #2 ENGINE NOSE INLET AFT SIDE AT 9 O'CLOCK HAS CRACK NET TO ELBOW FITTING. FABRICATED & INSTALLED NEW WEB IAW SRM 54-10-00.SDR IPXA2020083199605Web · crackedINSPECTION TYPE:A 300 #1 ENGINE NOSE COLUMN AFT BULKHEAD CRACKED AT AMBIENT PRESSURE SENSOR LINE OUTLET ON RT SIDE 3' OCLOCK POSITION. FABRICATED & INSTALLED WEB IAW SRM 54-10-00.SDR UIEA2020090101907Intake · corrodedON WALKAROUND FOUND LEFT ENGINE INLET COWL INSIDE AFT 12 O'CLOCK POSITION HAS CORROSION(<P>ACCOMPLISHED PERMANENT HOT BOND COMPOSITE REPAIR ON LEFT ENGINE IAW SRM 51-21-01, 54-12-01-1A-1 AND 54-12-01 REPAIR 6, BY AVENIR FAA CRS #8AVR479B W.O # W14997 FEAM R.O SDR IPXA2020072258093Inlet · crackedINSPECTION TYPE:4C, NR 2 ENGINE INLET LIP SKIN CRACKED AROUND ONE FASTENER AT 6 O'CLOCK POSITION. REPAIRED THE NR 2 ENGINE INLET LIP SKIN IAW SRM 54-10-01, REPAIR 4.SDR T17A2020072710025Intake · crackedMX FOUND A CRACK ON THE #2 ENGINE INTAKE COWL AT THE 8 OCLOCK POSITION AND AT THE 5 OCLOCK POSTION AT THE BULKHEAD.MX FABRICATED A DOUBLER AND INSTALLED WE. IAW BEECHJET 400A SRM 54-00-01 AND 54-10-01SDR T17A202007100025Intake · crackedMX FOUND A CRACK ON THE #2 ENGINE INTAKE COWL AT THE 8 OCLOCK POSITION AND AT THE 5 OCLOCK POSTION AT THE BULKHEADSDR IPXA2020072438141Inlet · crackedINSPECTION TYPE:2C, NR 2 ENGINE INLET COWL CRACKS BETWEEN FASTENERS REQUIRES PERMANENT REPAIR.REPAIRED CRACKED #2 ENGINE INLET COWL BETWEEN FASTENERS IAW MD-11 SRM 54-10-01 REPAIR 4. (MINOR)SDR 8HBR20200629023Flapper Valve · failedCARBURETOR HEAT FLAPPER VALVE MATERIAL FAILURE. A PIECE OF THE CARB HEAT FLAPPER VALVE MATERIAL SEPARATED FROM THE VALVE ASSEMBLY AND GOT STUCK IN THE THROTTLE BODY OF THE CARBURETOR, CAUSING SIGNIFICANT DEGRADATION OF THE ENGINE'S PERFORMANCE.SDR T17A20200624022Intake Duct · crackedMX FOUND THE RH INTAKE FORWARD BULKHEAD CRACKED WHEN LOOKING THRU THE STARTED GENERATOR DUCT HOLE. MX STOP DRILLED THE CRACK AND INSTALLED A DOUBLER IAW BEECHJET 400A SRM 51-43-01,51-50-01 AND 51-50-15SDR T17A20200624021Intake · crackedMX DISCOVERED MULTIPLE CRACKS ON THE LH INTAKE OUTER SKIN LOOKING THRU THE STARTER GENERATOR DUCT HOLESDR IPXA2020061766666Bulkhead · crackedNR 2 ENGINE INLET AFT BULKHEAD HAS CRACK ON RH SIDE. REPAIRED IAW PW SRM 54-10-00. REPAIR #14 PAG 201SDR IPXA2020056255744Skin · delaminatedINSPECTION TYPE:ETOPDELAMINATION ON #2 ENG R/H FAN COWL AT 2 O'CLOCK POSITION. DELAM APPROX 3" LONG BY 2" WIDE RUNNING PARALLEL TO THE ENGINE AXIS. PEELED UP AND THICKNESS 1/64". C/W WITH E.O. B767-7110-76630-A AND ITEM PLACED ON DEFERRAL WITH INSPECTION DUE ISDR 2020FA0000217Inlet · damagedLH ENGINE INLET DUCT DEEP COUNTERSINK. REFERENCE TEXTRON AVIATION ENGINEERING MEMO: DQ25329M1 RRL DATED: 3/31/2020.SDR 2020FA0000172Arm · wornAMERICAN CHAMPION AICRAFT 7ECA CARBURETOR HEAT CONTROL CABLE ATTACHMENT BOLT IS WEARING ON THE CARBURETOR HEAT DOOR ARM TO THE POINT THE BOLT IS ALMOST CUT IN HALF. THERE ARE MULTIPLE INSTANCE OF THIS THAT HAVE BEEN SEEN IN THE HANGAR.SDR AC2A2020050113918Filter · crackedIBF MAINTENANCE AID FOUND CRACKED.SDR AC2A2020050113917Filter · crackedIBF MAINTENANCE AID FOUND CRACKED.SDR IPXA2020012215184Web · crackedINSPECTION TYPE:SEG, NR 2 ENG INLET - AFT WEB CRACKED AT THE OUTBD SENSE LWE . REMOVED CRACKED WEB & FABRICATED NEW WEB & INSTALLED IAW PRATT & WHITNEY SRM 54-10-00 FIG201SDR SWIA202047986Panel · crackedRH ENGINE INLET ANTI EXHAUST PANEL 421DR HAS 4 CRACKED WELDS ON THE FINS. (C-CHECK) RO:1/22/2020TIG WELDED 4 CRACKED FINS USING ER 6AL-4V PO# 134200 REF CF34-8E MHD REPAIR SCHEME.SDR SWIA2019122747418Rivet · crackedLEFT ENGINE NOSE COWL HAD ON CRACKED RIVET INSIDE THE INLET ON INBD SIDE. REPLACED THE RIVET ON THE LT ENG NOSE COWL IAW SRM.SDR P5CA2019120280221Inlet · crackedFOUND ENG 1 INNER INLET COWL RIVET AREA CRACK (0.5" X 0.5") AT SIX O'CLOCK POSITION;REMOVED AND REPLACED L ENG INLET COWL IAW AMM 71-11-01. TAI DUCT LEAK CHECK SATISFACTORY.SDR DALA2019112006791Skin · corrodedCORROSION LIP SKIN BTW 3 AND 9 O CLOCK ON ENGINE 1. REPLACED THE AIR INTAKE COWL ON ENG #1 ASPER A320 FAM AMM.SDR 2019FA0000370Plate · crackedUPON VISUAL INSPECTION, FOUND THE RIGHT ENGINE CARBURETOR HEAT AIRBOX BACKPLATE (WELD) CRACKED AT TOP LEFT ATTACH POINT. CRACK WAS FOUND NEAR TOP SUPPORT BRACKET. AIRCRAFT USED DAILY FOR FLIGHT TRAINING WITH AN AVERAGE OF 100 HOURS OF FLIGHT TIME EVERY 90 DAYSSDR SWIA2019122747377Skin · delaminatedLH ENGINE NOSE COWL LEADING EDGE HAS NUMEROUS AREA OF DELAMINATION AND SEALANT GAPS ON THE INNER AND OUT TRAILING EDGE. REPAIRED LH ENGINE NOSE COWL LEADING EDGE SURROUND AND SEALANT GAPS ON INNER AND OUT TRAILING EDGE APPLIED REPAIR RESIN AND FILLET SEAL SDR SWIA2019122747249Skin · erodedLEFT ENGINE INLET LIP SKIN HAD EROSION DAMAGE. REPAIRED THE LT ENGINE INLET LIP SKIN IAW CMM.SDR 2019FA0000369Plate · crackedUPON VISUAL INSPECTION, FOUND THE RIGHT ENGINE CARBURETOR HEAT AIRBOX BACKPLATE (WELD) CRACKED AT TOP LEFT ATTACH POINT. CRACK WAS FOUND NEAR TOP SUPPORT BRACKET. AIRCRAFT USED DAILY FOR FLIGHT TRAINING WITH AN AVERAGE OF 100 HOURS OF FLIGHT TIME EVERY 90 DAYSSDR SWIA2019121847017Inlet · erodedRIGHT ENGINE NOSE INLET IS HAS EROSION DAMAGE AROUND LIPSKIN (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED RH INLET IAW CRJ200 AMM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.SDR 2019FA0000371Plate · wornUPON VISUAL INSPECTION, FOUND THE LEFT ENGINE CARBURETOR HEAT AIRBOX BACKPLATE (WELD) STEEL STAPLES WEARING THROUGH ALUMINUM WALL DUE TO AIR VIBRATION WHEN CARB HEAT DOOR IS FULLY DEFLECTED. SHOULD THE STAPLES WEAR THROUGH THE WALL ENTIRELY, FELT DOOR-STOP COUSDR 2019FA0000368Plate · crackedUPON VISUAL INSPECTION, FOUND THE RIGHT ENGINE CARBURETOR HEAT AIRBOX BACKPLATE (WELD) CRACKED AT TOP LEFT ATTACH POINT. CRACK WAS FOUND NEAR TOP SUPPORT BRACKET. AIRCRAFT USED DAILY FOR FLIGHT TRAINING WITH AN AVERAGE OF 100 HOURS OF FLIGHT TIME EVERY 90 DAYSSDR AC2A2020050113916Filter · crackedIBF MAINTENANCE AID FOUND TO BE CRACKED.SDR 2019FA0000367Plate · crackedUPON VISUAL INSPECTION, FOUND THE RIGHT ENGINE CARBURETOR HEAT AIRBOX BACKPLATE (WELD) CRACKED AT TOP LEFT ATTACH POINT. CRACK WAS FOUND NEAR TOP SUPPORT BRACKET. AIRCRAFT USED DAILY FOR FLIGHT TRAINING WITH AN AVERAGE OF 100 HOURS OF FLIGHT TIME EVERY 90 DAYSSDR QMLA2019092619076Filter · abnormalDURING CLIMB OUT, PILOT TURNED ON AIR CONDITIONING SYSTEM AND CABIN FILLED WITH SMOKE. PILOT IMMEDIATELY RETURNED BACK TO BASE AND MAINTENANCE WAS ON SITE TO INSPECT. UPON INVESTIGATION, IT WAS NOTICED THAT THE INLET BARRIER FILTERS HAS JUST BEEN REPLACED WITHSDR AC2A2020050113915Filter · crackedIBF MAINTENANCE AID FOUND TO BE CRACKED.SDR AC2A2020050113914Filter · crackedIBF MAINTENANCE AID FOUND TO BE CRACKED.SDR R61A2019080790817Inlet · corrodedCORROSION FOUND BETWEEN NOSE LIP SKIN AND OUTER BARREL SKIN LOWER SECTION ON ENG,#1. REPLACED ENG.#1 INLET COWL IAW AMM 71-61-00.SDR CA190611012Hose · failed(CAN) DURING SCHEDULED MAINTENANCE ON R44 II IT WAS NOTED THAT THE MANUFACTURER SERVICE BULLETIN R44 SB-97 PART A (REQUIRED WITHIN ONE FLIGHT HOUR) HAD NOT YET BEEN ACCOMPLISHED. VISUAL INSPECTION OF THE INSTALLED HOSE A785-31 FOUND EVIDENCE OF SEPARATION BETWSDR UIEA2019050304120Paint · deterioratedNR 2 ENGINE INLET CASE PAINT IS DAMAGED /DETERIORATED IN SEVERAL AREAS.(<P>PREPARED CLEANED MASKED PRIMED AND PAINTED NR 2 ENGINE INLET CASE WHITE PER SRM 51-20-01-0G-0</P>)SDR AC2A2020050113920Filter · crackedIBF MAINTENANCE AID FOUND TO BE CRACKED.SDR AC2A2020050113913Filter · crackedIBF MAINTENANCE AID FOUND TO BE CRACKED.SDR AC2A2020050113912Filter · crackedIBF MAINTENANCE AID FOUND TO BE CRACKED.SDR 6KYR2020012900092Air Filter · failedDURING AN ANNUAL INSPECTION, WHILE CHANGING THE INDUCTION AIR FILTER IT WAS DISCOVERED THE FILTER BASKET HAS STARTED TO COME APART. THERE ARE SEVERAL PIECES OF THE BASKET MISSING. THE BASKET APPEARS TO BE MADE OF STAINLESS STEEL. THE BASKET SETS IN THE INDUSDR AC2A2020050113911Filter · crackedIBF MAINTENANCE AID FOUND TO BE CRACKED.SDR AC2A2020050113910Filter · crackedIBF MAINTENANCE AID FOUND TO BE CRACKED.SDR CWQA202021252019Breather · obstructedRE-SUBMISSION OF SDR BASED ON ENGINE FINAL REPORT.
DURING CLIMB JUST AFTER TAKE OFF CREW NOTICED A WHITE SMOKE FILLING THE COCKPIT AND CABIN.
CHECK LIST FOLLOWED, EMERGENCY DECLARED, AND UNSCHEDULED LANDING PERFORMED WITHOUT INCIDENT.
MAINTENANCE EVALUATIONSDR IPXA2019022039263Inlet · crackedINSPECTION TYPE:1C#1 ENGINE NOSE INLET COWL AFT SIDE AT THE 9 O'CLOCK POSITION, AIR INLET LINE IS LOOSE AND INLET SURFACE IS CRACKEDREPAIRED PER P&W SRM 54-10-00 FIG 201SDR QMLA2019011519007Intake · crackedWHILE CLEANING THE ENGINE AREA (COWLING OFF DUE TO OTHER MAINT) I FOUND A CRACK ALONG A WELD ON THE LT SIDE OF THE ENGINE INTAKE.SDR QMLA2019010119001Filter · contaminatedTWO MINUTES INTO AN INTER-FACILTY FLIGHT, AND AS THE PILOT AND CREW WERE APPROACHING AIRPORT WHEN THE LOW INLET PRESSURE LIGHT ILLUMINATED. THE PILOT OPENED THE BYPASS DOORS AND DIVERTED TO THE AIRPORT. UPON LANDING, THE PILOT INSPECTED THE INLET FILTER AND SASDR GTIA2018121903030Actuator · malfunctionedAT ABOUT 2,000 MSL WE RECEIVED AN ENG 2 STALL ECAM. THE MESSAGE WENT AWAY FOR A SECOND BUT WAS FOLLOWED BY ENG 2 FAIL. WE PERFORMED ECAM ACTIONS UNTIL THE RELIGHT AND PROCEEDED TO LAND. THE ENGINE AUTO SHUTDOWN ON APPROACH.-REF LOG PG 2424007-1, 2424007-2 FOR SDR CA190424021Hose · leaking(CAN) HOSE SPLIT AND LEAKING.SDR AC2A2020050113909Filter · crackedIBF MAINTENANCE AID FOUND TO BE CRACKED.
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