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"

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SDR WRLA20101230461Inlet · crackedU05059- CRACK: NR 2 ENG INLET LIP CRACK AT 4 TO 6 O'CLOCK. NRC U05059 ISSUED.Dec 30, 2010 · N276WA · Doug MD11FSDR UALA2010122804740Cowling · damagedENG NR 2 RT SIDE FAN COWL DAMAGED. REPLACED ENG NR 2 RT FAN COWLING IAW AMM. NO DEFECTS FOUND.Dec 27, 2010 · N838UA · Airbus A319131SDR UALA2010122804739Nose Cowl · damagedENG 2 NOSE COWL DAMAGED. REPLACED ENG NR2 NOSE COWLING IAW AMM. ALL OK, NO DEFECTS FOUND.Dec 27, 2010 · N838UA · Airbus A319131SDR UALA2010122204686Inlet · damagedCREW REPORT: NR 2 ENG COWL INLET HAS CHUNK MISSING. SAMC TEXT: PLEASE IDENTIFY LOCATION, SIZE OF "CHUNK" (INCLUDING LENGTH WIDTH AND DEPTH) AND WHAT TYPE OF MATERIAL IS MISSING. DIMENSIONS OF AREA ARE IN QUESTION ARE 1.25 WIDE BY 0.75 LONG, BY .325 DEEP. OK TDec 22, 2010 · N851UA · Airbus A319131SDR A6WA201040959Skin · corrodedRT ENG INLET LIP SKIN PITTED. REMOVED LIGHT PITTING ON RT ENG INLET LIP SKIN BY SANDING. REMOVING .004 MATERIAL WITH .059 MATERIAL REMAINING, THE LIPSKIN IS WITHIN LIMITS IAW CMM 71-61-01, FIG 5003 LIGHT.Dec 14, 2010 · N454AW · Cndair CL6002B19SDR A6WA201040958Skin · erodedLT ENGINE INLET LIP SKIN HAS EROSION DAMAGE. LT ENGINE INLET LIPSKIN HAS CORROSION AT 315 AREA, SANDED LIPSKIN REMAINING .003 MATERIAL WITH .060 MATERIAL. REMAINING AREA IS WITHIN LIMITS IAW CMM 71-61-01, FIG 5003N.Dec 14, 2010 · N454AW · Cndair CL6002B19SDR CA101210003Air Filter · unserviceable(CAN) THE RUBBER SECTION OF THE INDUCTION AIR FILTER NEAR WHERE THE WORM CLAMP HOLDS THE FILTER TO THE INDUCTION HOUSING SHEARED NEAR THE OUTER RIM.Dec 9, 2010 · Diamon DA40SDR FDEA201011234467Duct · dented#2 ENGINE INLET "S" DUCT INTERIOR HAS DENT AT BS 1320, 9 O'CLOCK POSITION. CUTOUT DAMAGED AREA OF SKIN, CUTOUT CHANNEL SECTION, FABRICATED DOUBLER PLATE, FILLER PLATED, SHIMS, FABRICATED RIB REPAIR CHANNEL AND TWO ANGLES, LOCATED & DRILLED PARTS, TREATED ANov 23, 2010 · N233FE · Boeing 727247SDR QXEA2010112900812Adapter · failedENGINE ADAPTER HEAT 1 CAUTION MSG, DUE TO WEATHER CONDITIONS, RETURNED TO THE FIELD. LANDING UNEVENTFUL. R & R NR1 ENG INTAKE ADAPTER HEATER IAW AMM TASKS 30-21-15-000/400-801. OPS TEST GOOD. RETURNED TO SERVICE.Nov 22, 2010 · N435QX · Bombdr DHC8402SDR FDEA201011194444Duct · crackedNR 2 ENGINE INLET "S" DUCT INTERIOR HAS A CRACK AT RIVET HOLE, BS 1342 11 0'CLOCK POSITION CUTOUT DAMAGED AREA IAW SRM 54-10-3 FIG 8, FABRICATED REPAIR PARTS ANGLE, PLATE, AND FILLER PLATE IAW SRM 54-10-3 FIG 8 AND SRM 54-10-2 FIG 5, LOCATED AND DRILLED PARTNov 19, 2010 · N233FE · Boeing 727247SDR CA101122016Bellows · detached(CAN) DURING CRUISE FLIGHT, RT ENGINE LOST POWER. PILOT ELECTED TO RETURN TO AIRPORT OF DEPARTURE (WINDSOR AIRPORT). PILOT CONDUCTED A POST FLIGHT RUN UP AND ONLY ACHIEVED 33 IN MAP. THE INTAKE, TURBO CHARGER AND TURBO CONTROL SYSTEM WAS INSPECTED FOR OBVIONov 18, 2010 · Piper PA60601PSDR CA101118008Dome · stripped(CAN) DURING TAKEOFF ROLL AT APPROX 80 KNOTS, ENGINE NR 2 NOSE DOME FELL OFF IN THE ENGINE INLET. THIS CAUSED THE ENGINE TO STALL (LOUD BANGS). THE TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE 4 STUDS THANov 12, 2010 · Boeing 737201SDR UALA2010110904163Actuator · leakingNR 1 ENGINE VARIABLE STATOR VANE ACTUATOR FUEL IS LEAKING FROM DRAIN MAST. INSTALLED SVA UP TO 3H(1)G (ATTACH THE GROUND CABLE TO STATOR VANE ACTUATOR). REPLACED SVA PER MM.Nov 8, 2010 · N796UA · Boeing 777222SDR UALA2010110504102Guide Vane · damagedNR 2 ENGINE FAILED BORO INSP. FOUND MULTIPLE (MORE THAN 3) T1 NGV WITH T/E BURNBACK MORE THAN 0.15". ALSO FOUND ONE VANE WITH COMPLETE BURN THROUGH THRU BAFFLE FROM CONVEX SIDE TO CONCAVE SIDE WITH CONCAVE SIDE COOLING HOLES VISIBLE.Nov 5, 2010 · N778UA · Boeing 777222SDR UIEA201000237Nose Cowl · dentedMX FOUND NR 3 ENGINE INLET NOSE COWL L/E DENTED AT APPROX 2 O' CLOCK POSITION MEASURING 12.0 INCHES IN LENGTH X 5.0 INCHES WIDTH AND 0.5 INCH DEPTH. AFTER DETAIL VISUAL INSP (10X MAGNIFYING GLASS) IT WAS VERIFIED THAT NO SHARP CREASES AND/OR CRACK CONDITION EXOct 24, 2010 · N408MC · Boeing 74747UFSDR ASOA201001640Bracket · crackedRT ENGINE INLET COWL HAS A CRACKED BRACKET ON AFT SIDE OF BULKHEAD AT 5 O'CLOCK POSITION. C/W REO 601R-71-61-3415 REV NC.Oct 22, 2010 · N868AS · Cndair CL6002B19SDR UALA2010102103895Actuator · leakingAFTER ARRIVAL FOUND LT ENGINE FUEL LEAK FROM DRAIN TUBE NR5, VARIABLE STATOR VANE ACTUATOR. PERFORMED ENG RUN UP IAW AMM. LEAK WITHIN LIMIT IAW AMM. REPLACE THE VSV ACTUATOR NOT MORE THEN 50 F HOURS. INSPECT THE LEAK BEFORE EACH DEPARTURE. TO PREVENT IRREG Oct 20, 2010 · N651UA · Boeing 767322SDR USAA2010101992324Actuator · failedFLT 149 - IFSD/EMERGENCY LANDING - AT CRUISE, COMPRESSOR VANE FAULT EGT AND N2 ABOVE LIMITS, SHUT DOWN NR 1 ENG. FOUND VARIABLE STATOR VANE (VSV) ACTUATOR BAD. REMOVED AND REPLACED VARIABLE STATOR VANE ACTUATOR (VSV) PER JOBCARD 26T40075005. REMOVED AND REPOct 15, 2010 · N832AW · Airbus A319132SDR CA101124002Seal · damagedDETERIORATION OF THE INLET FILTER SEAL CAUSED PARTS OF THE SEAL TO SEPARATE AND DAMAGED COMPRESSOR PARTS.Oct 13, 2010SDR FDEA201010083978Shield · crackedNUMBER 1 ENGINE LT FAN COWL TOP HINGE SHIELD NR 4 COVER CRACKED. REPAIRED AS PER E.A. F-7110-139358. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Oct 8, 2010 · N935FD · Boeing 7572T7SDR C2XA10TY161Inlet · corrodedNR 1 ENGINE AIR INLET HAS 36 BOLT HOLES THAT ARE CORRODED. REPAIRED FLANGE HOLES BY REMOVING PREVIOUS BUSHING REPAIRS, REAMED HOLES AND INSTALLED COUNTERSUNK BUSHINGS IAW EC5420-01158 REV C.Oct 7, 2010 · N36915 · Emb EMB145LRSDR FDEA201009203564Duct · corrodedNR2 ENGINE INLET DUCT INTERIOR SKIN IS CORRODED; FASTENERS SHEARED AND IS CORRODED INSIDE PANEL 362 DOOR (RT), STA 222. REMOVED AND REPLACED INLET SKIN IAW MD/DC10 SRM 51-31-01, VOL II AND DWG AJC7288, REV "D".Sep 20, 2010 · N370FE · Doug MD1010FSDR C2XA10TY145Intake · corrodedTYS - ENG 2 AIR INTAKE PLACED ON DMI FOR 5000 FC OR UNTIL NEXT C-CHECK FOR CORROSION ON MOUNTING HOLES PER EC 5420-01142. REPAIRED CORRODED HOLES IAW EC 5420-01158.Sep 20, 2010 · N15912 · Emb EMB145LRSDR CA100913011Air Box · crackedINDUCTION AIR BOX SENT IN FOR REPAIR. AD 85-10-02 APPLIES TO THIS UNIT. UNIT HAS .040" THICK SKIN AS OUTLINED IN AD AND IS STILL CRACKED WITH LARGE PIECES MISSING. UNIT WILL BE REPAIRED IAW AC 43.13-1A AND AC43.13-2A USING MATERIAL .050" THICK. AD 85-10-02 INSep 13, 2010 · Cessna U206FSDR 2010FA0000950Air Filter · debondedFOUND AIRFILTER ELEMENT TO HAVE SEPARATED AT GLUED SEAM, LEADING TO INJESTION OF UNFILTERED AIR FOR AN UNKNOWN LENGTH OF TIME.Sep 7, 2010 · N55460 · Piper PA28R200SDR UALA2010090703311Cowling · delaminatedFOUND DELAMINATED ON NR1 ENGINE LT SIDE FAN COWL RT OF OIL ACCESS DOOR. REMOVED FAN COWL AND ROUTED TO SHOP 273. R & R REPLACED WITH FAN COWL FROM ANOTHER ACFT.Sep 3, 2010 · N417UA · Airbus A320232SDR UIEA2010083100150Nose Cowl · damagedDURING WALK AROUND INSP, IN MX, FOUND THE NR 3 ENGINE INLET NOSE COWL L/E DENTED (SUSPECTED BIRD-STRIKE) AT APPROX 4 O' CLOCK POSITION MEASURING 5.5 INCHES IN LENGTH, 3.0 INCHES WIDTH AND 0.5 INCH DEPTH. AFTER DETAIL VISUAL INSP (10X MAGNIFYING GLASS) IT WAS VAug 31, 2010 · N408MC · Boeing 74747UFSDR C8GA2010000020Duct · corrodedWHILE IN HEAVY MX INSP, IT WAS NOTED THAT CORROSION WAS NOTED ON THE CTR ENGINE AIR DUCT AT THE LOWER PRODUCTION BREAK. FABRICATED NEW SPLICE STRAP FROM 301.2500 HD .063" NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Aug 24, 2010 · N755DH · Boeing 727225SDR 2010FA0000961Gasket · looseGASKET CAME OFF THE AIR FILTER. THE ADHESIVE HAD FAILED LETTING THE GASKET GET LOOSE AND IT CAN BE SUCKED INTO THE ENGINE, SHUTTING IT DOWN. CALLED MFG AND TALKED TO REP ABOUT THIS.Aug 20, 2010 · N35UP · Beech V35SDR UALA2010081302968Drain Mast · brokenNR 1 ENG HAD CONTACT WITH BELT LOADER. NEED TO OPEN FAN COWLS AND INSPECT FOR DAMAGE UNDER COWLING. LCL FBO OPENED FAN COWLS IAW AMM AND CHECKED FOR DAMAGE. FOUND DRAIN MAST BROKEN AND LOWER EDGE OF LT FAN COWL DAMAGED. FAN COWLS ARE SECURED CLOSED.Aug 13, 2010 · N491UA · Airbus A320232SDR Z6WR 004 2010Panel · debondedTHE 314W1510-2 COWL BOND PNL. (CMM 71-11-30, FIG 2 ITEM 585), HAS EXPOSED GRAPHITE PLIES DUE TO MISSING FIBERGLASS AND WIRE MESH. ON THE UPPER SIDE THERE ARE (3) AREAS WITH MATERIAL STILL ATTACHED AS WELL AS THE LWR END, BUT THE EDGES ARE LOOSE AND LIFTING UPAug 6, 2010 · Boeing 777367ERSDR UIEA2010080500132Skin · damagedDURING WALKAROUND INSP, MX FOUND DAMAGE TO THE NR 2 ENG INLET COWL OUTER BARREL SKIN CRACK/DAMAGE (REF FIG 1). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS; SCHEDULE REPEAT INSPECTIONS AT EVERY 25 FC AND PERMAug 5, 2010 · N523MC · Boeing 7472D7BSDR 2010FA0000848Strip · migratedACFT REPORTED AS LT ENGINE WOULDN’T SLOW TO IDLE. DISCONNECTED THROTTLE CONTROL AND DETERMINED PROBLEM WITHIN THE CARB. THE CARB WAS REMOVED AND A VISUAL INSPECTED NOTED A FELT STRIP WEDGED IN BETWEEN THROTTLE PLATE AND CARB HSG. THE STRIP WAS REMOVED AND TAug 4, 2010 · N520MS · Piper PA44180SDR U43R2010FA0000195Housing · damagedTHE THREADS ON THE ALTERNATE AIR VALVE BODY WERE STRIPPED OUT COMPLETELY. THE CONTROL CABLE WAS NO LONGER ATTACHED TO THE VALVE BODY, AS A RESULT THE VALVE BODY WAS FREE TO ROTATE WITHOUT RESTRICTIONS. SO THE ENGINE COULD BE GETTING UNFILTERED AIR.Jul 24, 2010 · N317AF · Diamon DA40SDR CA100831014Screen · crackedFOD SCREEN, PN 101-910049-125 FOUND CRACKED.Jul 12, 2010 · Beech B200SDR CA100831013Angle · crackedANGLES PN 101-910049-137, 101-910049-139, 101-910049-140, FOUND CRACKED. THESE INDIVIDUAL ANGLE FORM THE STRUCTURE SUPPORTING THE INTAKE FOD SCREEN.Jul 12, 2010 · Beech B200SDR 2010FA0000722Air Box · defectiveA MODIFIED BRACKET AIR FILTER ELEMENT DELAMINATED AND WAS SUCKED INTO THE CARBURATOR, BLOCKING THE AIR FLOW. THE AIR BOX HOLDING THE MODIFIED AIR FILTER ELEMENT DID NOT HAVE A SCREEN GUARDING THE ENTRANCE TO THE CARBURATOR AIR INTAKE DUCT AS IS COMMON ON CERTJul 12, 2010 · N11WC · Amtr HATZVANSDR UIEA2010071000098Nose Cowl · dentedDURING WALK AROUND INSP, MX FOUND THE NR 4 ENGINE INLET NOSE COWL L/E DENTED AT APPROX 10 O' CLOCK POSITION MEASURING 10.0 INCHES IN LENGTH AND 0.9 INCH DEEP. AFTER DETAIL VISUAL INSP (10X MAGNIFYING GLASS) IT WAS VERIFIED THAT NO CRACK CONDITION EXISTS. (DISJul 10, 2010 · N429MC · Boeing 747481SDR U43R2010AF0000190Valve · stripped(U43R) DURING SCHEDULED INSP, A&P MECHANIC FOUND THAT THE ALTERNATE AIR VALVE CONTROL LINE WAS LOOSE. FURTHER INSP FOUND THAT THE "EYE" BOLT HAD STRIPPED THE THREADS IN THE VALVE BODY HSG. THE BODY HSG IS MADE FROM ALUMINUM, THE "EYE" BOLT FROM STEEL. THE "Jun 11, 2010 · N306AF · Diamon DA40SDR A6WA201040605Strip · chafedLT UPPER NOSE COWL T/E CHAFED. REPLACED AFT EDGE STRIP PN 228-50080-107 IAW CMM 71-14-01-300-814-A01 REPAIR NR SRS091.Jun 10, 2010 · N406AW · Cndair CL6002B19SDR 2010FA0000902Air Filter · looseTHE GASKET ON THE BACK SIDE OF THIS K & N INDUCTION AIR FILTER CAME LOOSE AND WAS SUCKED INTO THE ENGINE, CAUSING IT TO STOP RUNNING. THIS AIR FILTER IS NOT AN OEM PRODUCT. IT IS INSTALLED WITH AN STC AND LOG BOOK ENTRY. OTHER COMPANY HAD THE SAME PROBLEM AMay 27, 2010 · N4427W · Beech V35BSDR A6WA201040493Skin · erodedLT ENGINE INLET L/E OUTER SKIN HAS EROSION DAMAGE. REPAIRED THE LT ENGINE INLET L/E OUTER SKIN EROSION DAMAGE.May 21, 2010 · N442AW · Cndair CL6002B19SDR A6WA201040494Skin · erodedRT ENGINE NOSE INLET COWL L/E OUTER SKIN HAS EROSION DAMAGE. REPAIRED THE RT ENGINE NOSE INLET COWL L/E OUTER SKIN EROSION DAMAGE.May 21, 2010 · N442AW · Cndair CL6002B19SDR UALA2010042901441Nose Cowl · dentedRAMP REPORTED DENT IN NR 2 ENG NOSE COWL 6 O'CLOCK POSITION. EVALUATED DENT APPROX DIMENSIONS ARE 3.5 IN L X 2 IN W .090 DEPTH BEYOND ALLOWABLE LIMITS. APPEARS TO BE PREVIOUS REPAIR. IAW UA-EVA-73731 PERFORMED EDDY CURRENT (HFEC) INSP. NO DEFECTS NOTED. NOApr 29, 2010 · N544UA · Boeing 757222SDR A6WA201040327Bracket · deterioratedREPAIR SENSE LINE BRACKETS (C-CHECK) 601R-71-61-3941 - (BRACKETS ON LT ENGINE NOSE INLET COWL ATTACH FLANGE). REPLACED 4 STAND OFF BRACKETS IAW REO 601R-71-61-3941, PN 228-50020-145, -161, -162, -165.Apr 27, 2010 · N441ZW · Cndair CL6002B19SDR IPXA10B59442Inlet · dentedON ASN FOUND DENT ON NR4 ENGINE INLET COWL AT 7 O'CLOCK POSITION. ITEM DEFERRED IAW EO B747-7110-37490A PARAGRAPH 6A. DEF NR 423771, DENT IS BEYOND SRM LIMITS. R & R NR 4 ENG INLET COWL IAW MM 71-11-01-4.Apr 22, 2010 · N575UP · Boeing 74744AFSDR C2XA10TY057Inlet · corrodedTYS - NR 1 ENGINE INLET HAS CORROSION INSIDE FASTENER HOLES. REAMED AND INSTALLED BUSHING ON NR 1 ENG INLET FASTENER HOLES TO REMOVE CORROSION.Apr 20, 2010 · N12167 · Emb EMB145XRSDR 2010FA0000384Gasket · out of positionGASKET IS OUT OF PLACE AND IS BEING NGESTED INTO INTAKE. Apr 3, 2010 · N5289M · Beech C23SDR 2010FA0000383Gasket · out of positionGASKET IS OUT OF PLACE AND IS BEING INGESTED INTO INTAKE.Apr 3, 2010 · N5289M · Beech C23SDR UALA2010032601025Nose Cowl · delaminatedNR 2 ENG NOSE COWL HAS AN AREA OF DELAMINATION AT 2 O'CLOCK POSITION, 24 INCHES BY 18 INCHES. REPLACED NOSE COWL.Mar 26, 2010 · N667UA · Boeing 767322
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