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 2007FA0001090Control Arm · brokenCARBURETOR HEAT CONTROL ARM BROKEN OFF OF CARB AIR BOX CAUSING UNCONTROLLED SELECTION OF CARB HEAT VS RAM (COLD) AIR INTAKE. RECOMMEND INSTALLED THICKER MATERIAL ON CARB HEAT CONTROL ARM LEVER. DIFFERENT WELDING PROCESS, OR DIFFERENT ATTACHMENT PROVISION ALTSDR UIEA200700477Nose Cowl · crackedNR 2 ENGINE NOSE COWL HAS 3 EACH CRACKS. ONE CRACK AT 7 O'CLOCK POSITION IS 15" LONG. NEXT CRACK AT 6 O'CLOCK POSITION IN 6 INCH LONG AND THE NEXT CRACK AT 6.45 O'CLOCK POSITION IS 11 INCH LONG. REPAIRED NR 2 ENGINE NOSE COWL IAW SRM 51-43-01 AND XEO 71-11SDR QXEA200701718Actuator · malfunctionedPDX FLIGHT NR 2119, NR 2 ENGINE BYPASS DOOR DOES NOT INDICATE OPEN (LIGHT TEST OK) FROM CRUISE (FL230/-20'C) TO PARKING (+10"C). REPAIRED CHAFFED WIRES AND REPLACED NR 2 ENGINE INTAKE BYPASS DOOR LINEAR ACTUATOR. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SSDR HALA0700487Cowling · dentedETOPS SIGNIFICANT SYSTEM - NR 2 ENG INLET COWL DENTED AT APPROX 5:30 POSITION AS VIEWED LOOKING FWD DENT MEASURE APPROX: 28"L, 2.5"W, 0.042" DEPTH. REPAIRED PER M105 FILE NR 585114 AND TRANSFERED TO DPM P98977. OK FOR SERVICE.SDR 2007UALA04537Nose Cowl · damagedBIRDSTRIKE ON NR 2 ENG INLET DEPTH OF DENT BEYOND SRM LIMITS BY FACTOR OF TWO. NR 2 ENG NOSE COWL LE LIP HAS A DENT APPROX 3 INCHES IN DIA AND 1-4TH INCH DEEP AT 9 O'CLOCK POS.SDR SWAA075352Rib · crackedDURING SCHEDULED 14Y CHECK, FOUND NR 2 ENGINE INLET FWD BULKHEAD RIB CRACKED AT 2 O'CLOCK POSITION. REMOVED AND REPLACED BULKHEAD RIB PER SRM.SDR SWAA075353Rib · crackedDURING SCHEDULED 14Y CHECK, FOUND NR 2 ENGINE INLET FWD BULKHEAD RIB CRACKED AT 10 O'CLOCK POSITION. REMOVED AND REPLACED BULKHEAD RIB PER SRM.SDR 2007UALA04354Skin · puncturedTAKEOFF RUNWAY DEBRIS CAUSED NR 2 ENG NOSE COWL OUTER SKIN PUNCTURE AND FAN COWL SKIN DAMAGE. A/C STRIKING FOD TO NR 2 ENG AREA OR FUESLAGE FROM BLOWING CONSTRUCTION DEBRIS ON TAKE OFF. A/C FERRIED TO ORD WHERE NOSE NR 2 NOSE COWLING WAS REPLACED.SDR UIEA200700438Bearing · wornNR 2 ENG RT VSV ACTUATOR ROD END BEARING CONNECTION TO VSV LEVER ARM WORN AND ALSO SLIDE (GUIDE) BLOCK WORN. NR 2 ENG RT VSV ACTUATOR. REMOVED AND REPLACED IAW AMM SLIDER BLOCK. REPLACED IAW GE MM 72-32-10.SDR UIEA200700437Slide Block · wornNR 2ENG LT VSV ACTUATOR SLIDE BLOCK WORN. SLIDE BLOCK REMOVED AND REPLACED IAW BOEING 747 REV 60 SUBTASK 72-36-00-408-015-500.SDR UIEA200700436Bearing · wornNR 2 ENG RT VSV ACTUATOR ROD END BEARING CONNECTION TO VSV LEVER ARM WORN AND ALSO SLIDE (GUIDE) BLOCK WORN. NR 2 ENG RT VSV ACTUATOR REMOVED AND REPLACED IAW AMM SLIDER BLOCK. REPLACED IAW GE MM 72-32-10.SDR UIEA200700435Inlet Guide Vane · bentNR 2 ENG 3 IGV BENT<4DEG AT 1230 O/C POSITION. NR 2 ENG 3 LEVER ARMS REPLACED AT 1230 O/C POSITION IAW 72-36-00-408-005-REV 60.SDR 2007UALA03982Liner · damagedFOUND HOLE INSIDE NR 1 ENGINE COWL ON WALK AROUND, UNDER ENG BLADE, APPROX 2 INCHES LONG AND 1 INCH WIDE. HOLE IS AT 6 O'CLOCK POS. MEASURES APPROX .75 INCH DIA. *S/D* REPAIRED NR 1 ENG FAN CASE ATTRITION LINER, CURED FOR 3 HOURS WITH HEAT LAMP.SDR 2007UALA03895Valve · misriggedENGINE NR 1 COMPRESSOR STALL IN CRUISE. MISRIGGED VSV SYSTEM. ACP CHECKS PER MM 71-00-00 FOUND VSV UNISON RING MISRIGGED AT VGV AND STAGE 5. ADJ 1 TURN EA, OPS CHECK NORMAL.SDR CA070921004Seal · loose(CAN) REFERENCED TO SDR NR 20070917013 AFTER FINDING COWLING SEAL LODGED IN THE CARB VENTURI. THE PILOT/OWNER OF THIS AIRCRAFT WAS REQUESTED TO CHECK THE CONDITION OF THE COWLING SEAL, IT WAS FOUND TO BE LOOSE AND DETERIORATED AS WELL. ALL OF THE SEAL WAS REMOSDR VNAA0709010Intake · damagedCREW REPORTED A BIRD STRIKE ON APPROACH TO THE RIGHT HAND ENGINE INTAKE COWLING LEADING EDGE. MAINTENANCE INSPECTED AND FOUND THE DAMAGE TO BE 2 INCH LENGTH BY 1 INCH WIDTH BY .15 DEEP. DAMAGE WITHIN LIMITS IN ACCORDANCE WITH THE SHORTS CMA CMM 71-61-01. TSDR 2007FA0000919Control Arm · brokenCARBURETOR HEAT CONTROL ARM BROKE OFF OF CARB AIR BOX CAUSING UNCONTROLLED SELECTION OF CARB HEAT VS RAM (COLD) AIR INTAKE. (K)SDR DJFA2007107Inlet · crackedDURING A SCHEDULED INSPECTION, MAINTENANCE DISCOVERED A CRACK ON THE RT ENGINE INLET AT THE 12 O'CLOCK POSITION THAT EXTENDED FWD AND AFT OF THE SCREW TRANSECTING THE SCREW HOLE. MAINTENANCE REPLACED THE INLET.SDR DJFA2007105Inlet · crackedDURING A SCHEDULED MAINTENANCE EVENT MAINTENANCE FOUND A CRACK ON THE RT ENGINE INLET RING AT THE 7 O’CLOCK POSITION. THE CRACK TRANSECTED THE SCREW HOLE FROM THE AFT EDGE OF THE RING. 10-9-07 MAINTENANCE REPLACE THE INLET ASSEMBLY.SDR CA070829004Intake Duct · corroded(CAN) LEVEL 3 CORROSION WAS FOUND BETWEEN THE LOWER INTAKE FORWARD LIP AND THE NACELLE STRUCTURE. (TC NR 20070829004)SDR CWQR200712Intake Duct · crackedDURING A PHASE INSPECTION FOUND RT ENGINE INLET DUCT ASSY CRACKED. CRACKS WERE FOUND ON THE AFT PORTION OF THE INLET DUCT ASSY THROAT. THIS UNIT HAD TO BE RETURNED TO THE MFG FOR REPAIR. AN SCR WAS SUBMITTED TO MFG UNDER NR 308873.SDR CWQR200711Intake Duct · crackedDURING A PHASE INSPECTION FOUND LT ENGINE INLET DUCT ASSY CRACKED. CRACKS WERE FOUND ON THE AFT PORTION OF THE INLET DUCT ASSY THROAT. THIS UNIT HAD TO BE RETURNED TO THE MFG FOR REPAIR. AN SCR WAS SUBMITTED TO MFG UNDER NR 308858.SDR DHL2007783516Nose Cowl · out of toleranceNR 1 ENGINE NOSE COWL AT 11 O`CLOCK POSITION, 2 BLIND FASTENERS IMPROPERLY INSTALLED, NAC STA 81.5. REMOVED 2 BLIND FASTENERS ON NR 1 NOSE COWL AT 11 O`CLOCK POSITION IAW B727 SRM 51-30-2. FASTENERS HOLES OUT OF LIMITS AND OVER SIZE IAW B727 SRM 51-30-2. RESDR DHL2007783523Nose Cowl · gougedNR 1 ENG NOSE COWL 4 O`CLOCK POS EXISTING REPAIR DOUBLER AN ADJACENT SKIN GOUGED AT NAC STA 82.5. REMOVED DAMAGED DOUBLER ON NR 1 ENGINE NOSE COWL 9 O`CLOCK POSITION IAW B7627 SRM 51-30-2. REMOVED DAMAGED SKIN ADJACENT TO DOUBLER AREA ON NR 1 ENG NOSE COWL ISDR 2007FA0000787Air Box · brokenCARBURETOR HEAT CONTROL ARM BROKE OFF OF CARB AIR BOX CAUSING UNCONTROLLED SELECTION OF CARB HEAT VS RAM (COLD) AIR INTAKE WHILE IN FLIGHT. (K)SDR 2007FA0000634Support · crackedMECH DISCOVERED ON A 50 HR INSP, THE SUPPORT COLLAR ON THE AIRBOX MOUNTED TO THE CARBURETOR WAS CRACKED. THIS COULD LEAD TO THE SEPARATION OF THE AIRBOX FROM THE CARBURETOR AND LOSS OF POWER. PN 0750288 WAS REPLACED WITH NEW SUPPORT COLLAR PN 0750288-1 IAW SSDR 2007FA0000786Air Box · brokenCARBURETOR HEAT CONTROL ARM BROKE OFF OF CARB AIR BOX CAUSING UNCONTROLLED SELECTION OF CARB HEAT VS RAM (COLD) AIR INTAKE. (K)SDR FDKA200705236Acoustic Panel · dentedNR 2 INLET, INNER SKIN, IS DAMAGED IN TWO AREAS. THE DAMAGE HAS BEEN REPAIRED.SDR 2007FA0000476Air Filter · debondedAPPEARS THAT THE FOAM AIR FILTER ELEMENT, THAT IS CYLINDER SHAPED AND BONDED TOGETHER, DID NOT HAVE SUFFICIENT GLUEUU OR CAME UNBONDED AND WAS ALLOWING UNFILTERED AIR TO ENTER THE ENGINE INTAKE.SDR CA071031002Intake Pipe · deteriorated(CAN) INTAKE PIPE FLANGE DETERIORATED AND AIR LEAK OCCURRED. ENGINE IDLE INCREASED AND ENGINE RUNS SLIGHTLY ROUGH. INSTALLED NEW INTAKE PIPE P/N 655224-1 AND GASKET 554227 (NR 3 CYLINDER) (TC NR 20071031002)SDR DHL2007806587Nose Cowl · wornNR 2 ENG RT NOSE COWL UPPER PORTION WORN (STA YN 147.534 - 163.000, AT 12 O'CLOCK POS) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED SKIN (AL2024T3 0.080")SDR DHL2007806585Nose Cowl · wornNR 1 ENGINE NOSE COWLING RT UPPER PART WORN AT 12 O'CLOCK POS STA YN 163.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED SKIN (AL2024T3 0.080") AND SPLSDR 2007FA041101Air Box · failedCARBURATOR AIR BOX AIR FILTER RETAINING SHAFT SHEARED ADJACENT TO FISH MOUNTH WELD AT FORWARD EDGE OF HORIZONTAL PLATE (APPROXIMATELY 1/3 SHAFT LENGTH FROM BASE). AIR FILTER DOME, SHAFT AND RETAINING NUT APPEARANTLY DEPARTED AIRPLANE IN FLIGHT. AIR FILTER WASSDR AC2A2007032871967Screen · brokenNR 1 ENGINE INLET SCREEN HAS BROKEN WIRES.SDR 2007UALA00676Duct · looseRTFL DUE TO SIGNIFICANT VIBRATION IN LEFT ENGINE AFTER TAKEOFF. COULD NOT ADVANCE POWER W/O VIBRATION INCREASING. 3RD STAGE LPT BLADE FRACTURED. THE 3RD STAGE LPT BLADES AND VANES WERE SULFIDED. DURING DISASSEMBLY A BOLT FOR THE OUTER DUCT WAS FOUND FRACTSDR DJFA2007026Inlet · crackedDURING A SCHEDULED MAINTENANCE EVENT MAINTENANCE FOUND A CRACK ON THE RT ENGINE INLET RING AT THE 12 O'CLOCK POSITION. THE CRACK IS ABOUT .25 INCH LONG. MAINTENANCE REPLACED THE INLET.SDR 2007FA0000247Clamp · failedLT ENGINE REPORTED TO BE ROUGH RUNNING. INDUCTION HOSE CLAMP(P/N-RAM 1170-2)FAILED; ALLOWING INDUCTION COUPLER(P/N-632323) TO SEPARATE FROM INDUCTION TUBE. THIS INDUCTION LEAK OCCURRED BETWEEN THE Y AND INTAKE TUBES TO CYLINDERS NR 2, NR 4 AND NR 6.SDR DHL2007781015Nose Cowl · dentedNR 3 ENG NOSE COWL LOWER SIDE DENTED BETWEEN NAC STA 70 AND 85. CUT OUT DAMAGED AREA OF COWL, 17.5" BY 9.5" APPROX, PER B727 SRM 54-30-3 FIG 3.FABRICATED; FILLER FROM 2024-T3, .040" BY 9" BY 18", PO NR 9004042; AND DOUBLER FROM 2024-T3, .050" BY 20.5" BY 6.5"SDR SWIA200718052Nose Cowl · crackedRT ENGINE NOSE COWL HAS A CRACKED BRACKET AT 4 O'CLOCK POSITION AND XN122.72, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW BRACKET RT ENGINE NOSE COWL AT 4 O'CLOCK POSITION PER ENGINEERING ORDER 601R-71-11031.SDR Y2PA200700022Inlet · damagedWEATHER CLEAR - VFR - CLIMBING THROUGH 8000' CREW HEARD A LOUD NOISE FROM REAR AND FELT AN IMPACT. CREW NOTICED LEFT ENGINE EPR CLIMB AND OIL PRESSURE DECREASING. AFTER CREW CONFIRMED SECONDARY INDICATIONS AN ENGINE SHUTDOWN WAS INITIATED USING APPROVED USA SDR DJFA2007021Intake · crackedDURING A SCHEDULED MAINTENANCE EVENT MAINTENANCE FOUND A CRACK ON THE ENGINE INLET RING AT THE 12 OCLOCK POSITION. THE CRACK WAS APPROX .67 INCH LONG AND TRANSECTED THE SCREW HOLE FROM THE AFT EDGE OF THE RING. MAINTENANCE IS REPLACING THE INLET RING. THE SSDR DLM88081371Inlet · damagedDURING SHOP VISIT EROSION AND DAMAGE FOUND TO INLET COWL OUTER COMPOSITE SKIN. REPAIRED PER ERA 095803-14.SDR 2007FA0000083Seal · missingINTAKE SEALS FOUND MISSING. AD 77-04-05 PERTAINING TO THIS DEFECT HAD BEEN PREVIOUSLY ACCOMPLISHED IN 1977. DUE TO THE AGE OF THE FLEET I BELIEVE THAT THE ONE TIME INSPECTION IAW THIS AD IS INSUFFICIENT. AS THIS IS NOT THE FIRST TIME I HAVE FOUND THE SAME CONDSDR 2007FA0000112Air Filter · twistedDURING REMOVAL OF THE AIR FILTER THE CENTER WIRE MESH SCREEN WAS FOUND TWISTED AND BENT. SOME OF THE WELDS WERE BROKEN. SCREEN DEFORMATION CAN LEAD TO UNFILTERED AIR AND FOD ENTERING THE ENGINE. APPARENT CAUSE IS EITHER OVERTORQUEING WING NUT AND/OR INSUFFISDR DL76G070542Inlet · dentedNR 2 ENGINE INLET ACCOUSTIC LINER DENTED AT 6 O:CLOCK POSITION. REPAIRED PER SRM ROHR 54-12-01 REPAIR NR 3.SDR QXEA200603325Skin · damagedC3 YYC - RIGHT ENGINE INTAKE LEADING EDGE HAS ONE LOOSE RIVET INSIDE LIP OF REPAIR 11:00. REPAIRED IAW SRM 51-42-13, 54-11-05.SDR QXEA200603099Intake Duct · chafedC3 YYC - RIGHT ENGINE COWL INSIDE LEADING EDGE IS CHAFED BY STAGE 6 BLEED AIR TUBE. REPAIRED IAW SRM 54-23-00 AND 51-12-00.SDR C2XA06SH121Intake · corrodedSHV - DURING C-CHECK THE NR 2 ENGINE INTAKE FLANGE WAS FOUND TO BE CORRODED AROUND THE BOLT HOLES. MAINTENANCE REMOVED AND REPLACED THE INTAKE IAW EMB 145 AMM 71-60-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 2006FA0001033Air Filter · deterioratedMETAL PIECES COMING OFF AIRFILTER (AIR FILTER P/N: CPE1173, PREVIOUSLY INSTALLED IAW STC NR SA01669CH. THE METAL PIECES THAT ARE COMING A PART ARE LOCATED ON THE TOP, FRONT AND REAR OF THE FILTER ASSEMBLY. AN FAA-PMA STAMP COVERS THE PN ON THE FILTER. THE ONLSDR 2006UALA01928Duct · puncturedNR 1 ENGINE INLET DUCT HAS PUNCTURE AT 12 CLK POS FWD OF MOUNTING FLANGE. MAJOR REPAIR: FABRICATED AND INSTALLED A STAINLESS BONDED DOUBLER.
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