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 EPUA20111201005Vane · crackedBYPASS DOOR LOOSE (WILL NOT CLOSE ALL THE WAY). UPON INVESTIGATION FOUND FWD INERTIAL VANE ASSY SHAFT CRACKED. WHILE REPAIRING THE PREVIOUS DISCREPENCY, THE MECHANIC NOTICED THAT THE INLET SPLITTER PN 200803-513-01 WAS CRACKED AT THE CORNER.SDR EPUA20111201004Lever · brokenWHEN IN BYPASS, DOOR IS HALF WAY BETWEEN NORMAL AND BYPASS. ON INVESTIGATION IT WAS FOUND THAT FWD INERTIAL SEPERATOR LEVER WAS BROKEN.SDR JR2R2011102800536Structure · crackedNR 2 LOWER FAN COWL OTBD EDGE MEMBER NEAR ALLIGNMENT PIN DENTED IN AND CRACKED. - REPLACED OTBD EDGE MEMBER IAW SRM.SDR UALA2011102505776Structure · damagedNR 2 ENGINE RT FAN COWL DAMAGED. DAMAGE OUT OF LIMITS PER AMM. FBO FOUND DAMAGE .125" D X 4" L X .375" W. NO CRACKS. GOUGE INTO CORE. OUT OF LIMITS PER AMM FOR ZONE 'C'. REPLACED FAN COWL.SDR CA111012010Air Box · separated(CAN) DURING A ROUTINE INSPECTION IT WAS DISCOVERED THAT THE SCOOP FOR THE HEATED AIR INLET WAS SEPARATED FROM THE AIRBOX STRUCTURE. THE SCOOP IS NORMALLY SWAGED OR WELDED IN PLACE AND THE SCAT DUCT IS CLAMPED TO THIS SCOOP TO DIRECT INCOMING WARM AIR FROM THSDR UALA2011100305340Nose Cowl · puncturedNR 1 ENG NOSE COWL HAS PUNCTURE DAMAGE TO INNER ACCOUSTICAL PANELS. 4 EACH FROM 12:00 TO 4:00, 3 EACH FROM 4 :00 TO 8:00 AND 6 EACH FROM 8:00 TO 12:00. REPAIRED ALL DAMAGE TO INNER ACCOUSTICAL PANELS ON NR 1 NOSE COWL REF EVA-72053. REPLACED NR 1 ENG NOSE CSDR VNAA2011100600006Cowling · dentedAT CLT, CREW REPORTED BIRD STRIKE ON LEFT ENGINE COWL. MAINTENANCE INSPECTED AIRCRAFT, REPAIRED DENT ON LEFT HAND ENGINE INLET COWL AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.SDR CA110921003Piccolo Tube · cracked(CAN) DURING A HMV THE NR 2 ENG INTAKE COWL WAS REMOVED, UPON FURTHER INSPECTION OF THE COWL LOOSE RIVETS WERE NOTICED BEHIND THE INTAKE LIP. THE TECH PROCEDED TO REMOVE THE INTAKE LIP TO FURTHER ACCESS THE PULLED RIVETS. IT WAS DISCOVERED THE ATTACH BRACKETSSDR CA111124003Scoop · failed(CAN) BOTTOM OF AIR SCOOP BEHIND AIR CLEANER BROKE OUT IN SMALL PIECES WHICH WERE INGESTED INTO THE ENGINE HOLDING VALVES WHICH CAUSED ENGINE TO QUIT. HEAVY MATERIAL WAS INSTALLED IN DEFECTED AREA. WILL MONITOR. ORIGINAL MATERIAL WAS SOFT AND WAS FLEXING CAUSDR CA110811006Control Cable · separated(CAN) THE ACFT WAS ON APPROACH AFTER A ROUTINE PIPELINE PATROL WHEN THE PILOT PULLED THE CARBURETOR HEAT CONTROL TOWARDS THE "ON" POSITION. THE PILOT REALIZED THAT THE CONTROL FELT LOOSE AS HE CONTINUED TO PULL IT OUT OF THE PANEL. THE INNER CONTROL CABLE HADSDR FDEA201107293017Panel · crackedEMPENNAGE - NR 2 ENGINE RT AIR INTAKE REAR INTERIOR SUPPORT STRUCTURE (364RR) FOUND SUSPECTED CRACKED. REPAIRE CARRIED OUT AS PER EA 1-5530-143624. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 112.SDR FDEA201107272990Inlet · dentedENGINE NR 2 - INLET COWL LIP FOUND WITH FOUR DENTS. DENTS MEASURED AND FOUND EXCEEDED LIMITS PER SRM 54-42-02 REV 46, TABLE 102. DENT DIMENSION: DEPTH = 0.065 INCH; DIAMETER = 0.380 INCH DEPTH OF DENT IS MORE THAN 10% OF THE DENT DIAMETER AND THE DISTANSDR E81RJT2307930Skin · damagedDURING SCHEDULED PHASE INSP OF ACFT PREVIOUSLY MODIFIED, STC ST09559AC, ENGINE INSTALLATION NOTED (2) MISSING RIVET HEADS IN LT ENGINE INLET DUCT SKIN. SUBSEQUENT INVESTIGATION REVEALED MINOR CRACK FROM RIVET HOLE. NO FOD DAMAGE NOTED TO ENGINE. INLET DUCT SKSDR FK8R201107190004Support Bracket · crackedAIRBOX FRONT SUPPORT BRACKET WAS FOUND CRACKED AT THE STARTER. THIS PART WAS REPLACED AT THE ANNUAL INSPECTION IN 2010.SDR DJFA2011035Skin · crackedDURING INSPECTION OF ENGINE INLETS, CRACKS AND MISSING/DAMAGED FASTENERS WERE FOUND ON THE RH ENGINE INLET. THE FASTENERS WERE REPLACED. ADDITIONAL CORRECTIVE ACTIONS REQUIRE THE REPLACEMENT OF THE INLET WITH A -405 UNIT; IN THE MEAN TIME, THE AIRCRAFT MANUSDR DJFA2011034Skin · crackedDURING INSPECTION OF ENGINE INLETS, CRACKS AND MISSING/DAMAGED FASTENERS WERE FOUND ON THE LT ENGINE INLET. THE FASTENERS WERE REPLACED. ADDITIONAL C/A REQUIRE THE REPLACEMENT OF THE INLET WITH A -405 UNIT; IN THE MEAN TIME, THE ACFT MFG HAS DETERMINED THATSDR DJFA2011033Skin · crackedDURING RECURRING INSP OF ENGINE INLETS, ADDITIONAL CRACKS AND MISSING/DAMAGED FASTENERS WERE FOUND ON THE RT ENGINE INLET. THE FASTENERS WERE REPLACED. ADDITIONAL C/A REQUIRE THE REPLACEMENT OF THE INLET WITH A -405 UNIT; IN THE MEAN TIME, THE ACFT MFG HAS SDR DJFA2011032Skin · crackedDURING INSPECTION OF ENGINE INLETS, CRACKS AND MISSING/DAMAGED FASTENERS WERE FOUND ON THE LT ENGINE INLET. THE FASTENERS WERE REPLACED. ADDITIONAL C/A REQUIRE THE REPLACEMENT OF THE INLET WITH A -405 UNIT; IN THE MEAN TIME, THE ACFT MFG HAS DETERMINED THATSDR DJFA2011031Skin · crackedDURING INSP OF ENGINE INLETS, CRACKS WERE FOUND ON THE RT ENGINE INLET.SDR EE4Y20110382Strap · wornENGINE NR 2, FAN COWL, AIR INTAKE COWL, CAPPING STRAP UPPER AREA LT AND RT CORNERS WITH WEAR. NOTE: THE CAPPING STRAP WEAR REQUIRES A MAJOR REPAIR IAW SRM GUIDELINES.SDR QMLA2011061711067Air Filter · overservicedENGINE INLET FILTER OVER SERVICED, EXCESS OIL ACCUMUATED IN INLET TO ENGINE AND SMOKED WHEN OPERATING TEMPS IN ENGINE BECAME HOT.SDR 2011FA0000364Air Filter · debondedDURING ANNUAL INSP, INPECTOR NOTED ONE BRACKET AIR FILTER ELEMENT, PN BA3 TO HAVE SEPARATED AT SEAM. INSPECTOR NOTES HAVING FOUND SEVERAL OTHER FILTERS FAILED IN THE SAME WAY.SDR DJFA2011028Inlet · crackedDURING INSPECTION OF ENGINE INLETS, CRACKS AND MISSING/DAMAGED FASTENERS WERE FOUND ON THE RT ENGINE INLET. AIRCRAFT MANUFACTURER HAS DETERMINED THAT THE DAMAGE IS ACCEPTABLE AND HAS ALLOWED THE INLET TO CONTINUE IN SERVICE WITH ADDITIONAL PERIODIC INSPECTIONSDR 2011FA0000373Filter Element · splitDURING ROUTINE INSPECTION, AIR FILTER WAS FOUND SPLIT OPEN AT THE SEAM. IT IS A CYLINDRICAL SHAPE AND IT WRAPS AROUND A METAL SCREEN. THE SPLIT AREA COMPRISED SEVERAL SQ INCHES OF UNFILTERED AIRPATH.SDR DJFA2011026Inlet · crackedDURING INSP OF RT ENGINE INLET, CRACKS, SCRATCHES, AND MISSING RIVETS WERE FOUND ON BOTH ENGINE INLETS. THE AIRCRAFT MANUFACTURER HAS DETERMINED THAT THE DAMAGE IS ACCEPTABLE AND HAS ALLOWED THE INLET TO CONTINUE IN SERVICE WITH ADDITIONAL PERIODIC INSPECTIONSDR ASMF201105017Nose Cowl · crackedDURING OVERNIGHT CHECK, DETECTED A CRACK OF 3.5 INCH LENGTH NEAR FORWARD L/E AT 6 HOURS POSITION IN LT ENGINE NOSE COWLING. MX REPLACED THE LT ENGINE NOSE COWLING IAW MM 71-11-02, ALL CORRECT.SDR FOTR2104614721Dome · dentedNR 3 ENGINE NOSE COWL DOME HAS 1 EACH DENT AT THE 10 OCLOCK POSITION. REPAIRED ON FASI WO 21046 NR AT 14721.SDR DJFA2011020Inlet · crackedDURING INSP OF LT ENGINE INLET, MULTIPLE CRACKS WERE FOUND ALONG WITH SHEARED RIVET HEADS ON THE FWD ROW OF RIVETS AFT OF THE HEATED L/E. RIVETS WERE REPLACED AND CRACKS WERE TEMPORARILY REPAIRED PER EMBRAER ENGINEERING REPAIR DATA. PERMANENT REPAIR REQUIREDSDR DJFA2011019Inlet · crackedDURING INSP OF RT ENGINE INLET, A 1 INCH CRACK WAS FOUND AT THE 3 O'CLOCK POSITION. THE INLET WAS REPLACED.SDR WRLA20110505476Nose Cowl · crackedNR 2 ENGINE NOSE COWL INLET LOWER LIP FOUND CRACKS EMANATING FROM SEVERAL FASTENERS FROM THE 4 TO 8 O'CLOCK POSITION. PERFORMED HFEC INSPECTION AND FOUND EXISTENCE OF CRACKS MENTIONED ABOVE IAW NDT MANUAL PART 6. REF: CARD WM-445 AND NON-ROUTINE 046. REMOVEDSDR FDEA201104291672Skin · dentedENGINE NR 2 INLET NOSE COWL LEADING EDGE AREA AT APPROXIMATELY 1 O'CLOCK POSITION FOUND DENTED. ENGINE NR 2 INLET NOSE COWL LEADING EDGE DENT AREA REPAIRED AS PER SRM 54-10-01 FIG 202 REVISION 46. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 112. SDR HALA2011041500156Guide Vane · damagedETOPS SIGNIFICANT SYS - NR 1 ENGINE HAS 1 FAN EXIT GUIDE VANE AREA B DAMAGED MORE THAN 1" RADIAL LENGTH 3 O'CLOCK POSITION. REPAIRED FEGV AT 3 O'CLOCK POS IAW AMM 72-33-02-308-001-N00. OK FOR SERVICE.SDR 2011FA0000274Mount · chafedSCAT HOSE FOR AIRBOX CHAFING THROUGH ENG MOUNT INBD LOWER SIDE. COULD LEAD TO CATASTROPHIC MOUNT FAILURE.SDR DJFA2011014Inlet · crackedDURING INSP OF LT ENGINE INLET, CRACKS WERE FOUND AT THE 9 AND 3 OCLOCK POSITIONS. DURING INSPECTION OF LH ENGINE INLET, CRACKS WERE FOUND AT THE 9 AND 3 OCLOCK POSITIONS. REPAIRED CRACKS ON INLET IN ACCORDANCE WITH ISR 8000027867R1.SDR CA110314004Adapter · damaged(CAN) DURING THE CRUISE, CREW HEARD A MODERATE BANG SOUND BEHIND US. THE INTAKE LIP HTR 1, LEFT WDO HT, FUEL AUX PUMP 1+2 CB`S ALL POPPED." INTAKE ADAPTER FOUND BLOWN, ALSO THE INTAKE ADAPTER PLUG BACKSHELL ON LOOM 8245410-003 FOUND LOOSE. ON CLOSER INSPECTIONSDR UIEA2011030100135Rub Strip · damagedACFT AT SIN D CHECK. THE NR 1 LT FAN COWL WAS ROUTED TO THE COMPOSITE SHOP FOR REPAIRS. DURING INSTALLATION ON THE ACFT THE L/E RUB STRIP MISMATCH (6 O'CLOCK) WITH THE NOSE INLET COWL NOT ALLOWING THE FAN COWL TO LATCH PROPERLY. (DISPOSITION WAS MADE TO PERFSDR DJFA2011010Inlet · crackedDURING ACCOMPLISHMENT OF REPETATIVE INLET INSP, REQUIRED BY SB SB505-71-0001, MX FOUND MULTIPLE CRACKS ON THE LT ENG INLET. DURING ACCOMPLISHMENT OF REPETATIVE INLET INSPECTION REQUIRED BY EMBRAER SERVICE BULLETIN SB505-71-0001, MAINTENANCE TECHNICIANS FOUNDSDR E07A392ASInlet · crackedON PREFLIGHT INSP, 2 CRACKS WERE FOUND IN THE RT ENGINE INLET. THE INLET WAS INSPECTED WITH EDDY CURRENT AND ANOTHER 8 CRACKS WERE FOUND. INLET WAS REPLACED AND ACFT WAS RETURNED TO SERVICE. A VIBRATION AND SONIC SURVEY WERE COMPLIED WITH, NO DEFECTS WERE SDR A6WA201140083Bracket · crackedAFT FACE OF RT NOSE INLET HAS CRACKED BRACKET AT 4 O`CLOCK POSITION. R & R BRACKET IAW SRM 51-42-06, 51-21-11, 51-25-16.SDR CWQR201107Flange · crackedBULKHEAD FLANGE THAT ATTACHES TO THE ENGINE INLET HAS A 1.7 AND 1.1 INCH LONG CRACKS THAT WENT THROUGH FASTNER BOLT HOLES. BUT THESE CRACKS DID NOT CONNECT. THESE CRACKS WERE FOUND DURING A SCHEDULED INSPECTION. ALSO SUBMITTED TO CESSNA AIRCRAFT COMPANY, ON SSDR CWQR201106Flange · crackedBULKHEAD FLANGE THAT ATTACHES TO THE ENGINE INLET HAS A 1.15 INCH LONG CRACK THAT WENT THROUGH A FASTNER BOLT HOLE. THIS CRACK WAS FOUND DURING DIASSEMBLY OF ENGINE INLET ASSY FOR OTHER CRACKS FOUND DURING A SCHEDULED INSP. ALSO SUBMITTED TO MFG, ON (SCR 55SDR CWQR201104Attach Bracket · crackedMANIFOLD ATTACH BRACKETS (3 OF 5) WERE FOUND CRACKED DURING THE DISASSEMBLY OF ENGINE INLET ASSY FOR OTHER CRACKS THAT WERE FOUND DURING A SCHEDULED INSP.SDR CWQR201103Doubler · crackedDOUBLER WAS FOUND CRACKED DURING THE DISASSEMBLY OF ENGINE INLET ASSY FOR OTHER CRACKS FOUND DURING A SCHEDULED INSP.SDR FDEA201101200331Skin · cracked# 3 ENGINE INLET COWL AFT EDGE HAS TORN SKIN AT 4 O'CLOCK POSITION. CUT OUT DAMAGED SKIN, IAW SRM 54-30-3, FIG 5. FABRICATED REPAIR DOUBLER , AND FILLER IAW SRM 54-30-3, FIG 5. INSTALLED REPAIR DOUBLER IAW SRM 54-30-3, FIG 5 AND 51-30-2, REV 103.SDR A6WA201140116Seal · chafedRT ENG UPPER NOSE COWL EDGE SEAL CHAFED. R & R EXISTING SPLICE IAW CMM 71-14-01.SDR DJFA2011005Inlet · crackedDURING ACCOMPLISHMENT OF REPETATIVE INLET INSP, REQUIRED BY SB 505-71-0001, MX FOUND MULTIPLE CRACKS ON THE RT ENGINE INLET. MX REPLACED THE INLET.SDR QXEA2011011800035Skin · dentedC6 CHECK - LT ENGINE INLET COWL LOWER SKIN DENT. COMPLETED INSP IAW SRM 54-11-01-001-A01. DENT MEASURES .60"L X .40"W X .050" DEEP. FOUND TO BE OUT OF LIMITS. SENT ENGINEERING REQUEST TO MFG. REPAIRED IAW REO 670-71-12-094 AND REO 670-54-11-1027.SDR DJFA2011006Inlet · crackedDURING ACCOMPLISHMENT OF REPETATIVE INLET INSP REQUIRED BY SB 505-71-0001, MX FOUND MULTIPLE CRACKS ON THE RT ENGINE INLET. CRACKS WERE REPAIRED IAW THE ACFT MM.SDR DJFA2011007Inlet · crackedDURING ACCOMPLISHMENT OF REPETATIVE INLET INSP REQUIRED BY SB 505-71-0001, MX FOUND MULTIPLE CRACKS ON THE LT ENGINE INLET. CRACKS WERE REPAIRED IAW THE ACFT MFG INSTRUCTIONS.SDR HALA2011011300063Skin · gougedENG NR 2 NOSE COWL OUTER L/E SKIN DAMAGED AT 5 O'CLOCK & 4" FROM FRONT. GOUGE REMOVED IAW SRM 51-10-02, REV 84. REMOVAL CONFIRMED BY 10X MAGNIFICATON.
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