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.

SDR KBM2005F00202Actuator · failedENGINE ALT AIR DOOR WILL NOT OPEN. INSTALLED NEW MOTOR. (K)May 22, 2005 · N345SH · Snias AS350B2SDR 05FDEA01344Acoustic Panel · dentedCOMPLY WITH EA 6-7110-55485 POWER PLANT-INLET COWL NR 1 ENGINE ACOUSTIC PANEL DENT REPAIR. REPAIRED AREA PER EA 6-7110-55485.May 17, 2005 · N653FE · Airbus A300F4605RSDR KBM2005F00230Intake · crackedARRIEL ENGINE INTAKE HAS MULTIPLE CRACKS, REMOVED AND REPLACED. (K)May 5, 2005 · N53SH · Snias AS350B1SDR 2005FA0001453Intake · crackedCRACKS IN BASE METAL AND PITTING. ENGINE VIBRATION EXPOSURE TO ENVIRONMENT. (K)May 2, 2005 · Snias AS350*SDR KBM2005F00055Seal · damagedAIR INTAKE SEAL REQUIRED REPLACEMENT. REMOVED AND REPLACED. (M)Apr 21, 2005 · N751H · Snias AS350B2SDR 2005FA0000745Intake · crackedAIR INTAKE, CRACKED BASE METAL DUE TO VIBRATION. (K)Apr 11, 2005 · Snias AS350*SDR MALA050323Duct · burnedA SMELL OF ELECTRICAL BURNING IN CABIN. CREW THINKS IT WAS COMING FROM HOT JUG. FA PULLED C/B FOR HOT JUG AND SMELL LESSENED. ON POST FLIGHT, CREW FOUND RT INTAKE DUCT WITH 3 BURNED SPOTS IN IT. REPLACED RT ENGINE LOWER DUCT.Apr 10, 2005 · N422XJ · Saab 340BSDR CA050406004Duct · cracked(CAN) DURING OTHER MAINTENANCE ON AIRCRAFT, NOTICED RAM AIR DUCT IN REAR EQUIPMENT BAY CRACKED. UPON CLOSER INSPECTION OF RAM AIR DUCT, NOTICED SEVERE CHAFFING BETWEEN RAM AIR DUCT AND RT ENGINE BLEED AIR LINE JUST PRIOR TO BLEED AIR CHECK VALVE. RAM AIR DUCApr 4, 2005 · Cessna 550SDR ASMF200503020Inlet Guide Vane · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF CAPTAIN REPORTED APU PNEUMATIC PRESSURE DOWN TO 8 PSI WHEN LEFT ENGINE STARTED INSULATION VALVE WAS OPENED. ENGINES WERE STARTED WITH A GPU AND REPORT WAS DEFERRED IAW MEL 49-11-01. DURING OVERNIGHT SERVICE, Mar 27, 2005 · N806AM · Boeing 7572Q8SDR EIA2004148Fairing · damagedFOLDING FAIRING (BULL NOSE) NR 20, 2ND INBOARD OF NR 4 ENGINE DAMAGED. REMOVED NR 20 BULLNOSE IAW CDL 27-81-0 DMI 339 ENTERED.Dec 14, 2004 · N479EV · Boeing 747132SDR 04FDEA03324Angle · crackedDURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND ON NR 2 ENGINE INLET DUCT, INBOARD PANEL 361 HL, ANGLE BROKEN. REMOVE NOSE COWL PER MM 20-50-02, REPLACE CRACKED SHIELDS PER DWG AJC7151, P/N AJC 7151-27, AJC 7151-29, INSTALL NOSE COWL PER MM 20-50-02.Dec 2, 2004 · N559FE · Doug DC1010SDR 2005FA0000001Duct · wrong partDURING TEARDOWN OF F/T ASSEMBLY, A BROKEN EPR PROBE WAS FOUND AND THE INLET DUCT WAS SITTING LOW WHICH WOULD ALLOW MORE AXIAL TRAVEL OF INLET DUCT DURING OPERATION. AFTER REMOVING INLET DUCT, FOUND THE OVERALL HEIGHT OF INLET DUCT TO BE SHORT. THIS CAUSED WENov 30, 2004 · N158AC · Skrsky CH54BSDR 04FDEA03188Nose Cowl · damagedDURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND ENG NR 3 NOSE COWL BORDER ENTRY, WITH NR 6 HOLE APPROX .125 INCH PLUS NICK. REPLACE ENG NR 3 NOSE COWL IAW MM 71-11-00-2: P/N NSL 6051-511.Nov 23, 2004 · N559FE · Doug DC1010SDR 2004UALA01012Skin · puncturedNR 1 ENG INLET COWL OUTER SURFACE PUNCTURED-DELAMINATED AT THE 2 O`CLOCK POSITION APPROXIMATELY 30 INCHES FROM FWD END. DAMAGE WAS FOUND ON INLET COWL WAS PERMANENTLY REPAIRED.Nov 2, 2004 · N301UA · Boeing 737322SDR 24041004Bracket · chafedTHE INDUCTION DUCT SUPPORT BRACKET P/N 15671-002 HAS BEEN FOUND TO BE CHAFING INTO THE ALTERNATE AIR DOOR PIVOT BOLT P/N AN3-34. REPORTED THIS CONDITION BEFORE. A CHECK OF MULTIPLE AIRCRAFT HAVE SHOWED SIGNS OF CHAFFING AT THIS LOCATION. SUGGEST CLOSE LOOK Oct 28, 2004 · N787CD · Cirrus SR22SDR 041403Air Filter · wrong partDURING TROUBLESHOOTING FOR EXCESSIVE MAGNETO DROP, FOUND FACE OF AIR FILTER ELEMENT DETERIORATED. THE INSTALLATION IS FOR A BRACKETT FILTER. REMOVED ELEMENT AND FOUND THAT ELEMENT WAS AN UNAPPROVED PART. THE (FILTER) WAS HAND CUT FROM A PIECE OF GREEN FOAM .62Oct 5, 2004 · N117MM · Cessna 177SDR 04FDEA02867Segment · corrodedENGINE NR 2 INLET BELLMOUTH TRANSITION RING LOWER SURFACE FOUND WITH CORROSION. ENGINE NR 2 INLET BELLMOUTH TRANSITION RING LOWER SURFACE CORROSION REPAIR CARRIED OUT.Oct 4, 2004 · N585FE · Doug MD11SDR 22010904Bolt · chafedDURING REMOVAL AND REPLACEMENT OF THE P/N 15708-001 INDUCTION DUCT ASSY. IT WAS NOTED THAT THE INDUCTION DUCT WAS CRACKED IN AREA OF AN3-34 BOLT WHICH SERVES AS HINGE POINT FOR ALTERNATE AIR DOOR. AFTER REMOVING BOLT IT WAS FOUND TO HAVE A GROOVE WORN INTO BOct 4, 2004 · N968BG · Cirrus SR22SDR MALA040757Duct · chafedDURING C1 INSPECTION IN YYC, NR 3 ENGINE LT AFT FAN DUCT COWLING CHAFED. MAINTENANCE MANUFACTURED AND INSTALLED PART IAW SRM 51-26-11, 51-42-00, 51-43-00. AIRCRAFT RETURNED TO SERVICE 10/7/04.Sep 26, 2004 · N519XJ · Bac AVRO146RJ85ASDR MALA040755Duct · chafedDURING C1 INSPECTION IN YYC, NR 4 ENGINE RT AFT FAN DUCT COWLING CHAFED. MAINTENANCE MANUFACTURED PART AND INSTALLED IAW SRM 51-24-11, 51-42-00, 51-43-00. AIRCRAFT RETURNED TO SERVICE 10/7/04.Sep 26, 2004 · N519XJ · Bac AVRO146RJ85ASDR MALA040756Duct · chafedDURING C1 INSPECTION IN YYC, NR 4 ENGINE LT AFT FAN DUCT COWLING CHAFED. MAINTENANCE REPAIRED IAW SRM 51-71-12. AIRCRAFT RETURNED TO SERVICE 10/7/04.Sep 26, 2004 · N519XJ · Bac AVRO146RJ85ASDR GTIA040781Nose Cowl · delaminatedNR 1 ENGINE INLET COWL INNER BARREL 'DYNA RONR' WOVEN WIRE MESH DELAMINATING 3 O'CLOCK TO 9 O'CLOCK. INSTALLED CONDITION 2 REPAIR ON LEFT NR 1 ENGINE LOWER NOSE COWL, C/O NR 254595-2. (M)Sep 15, 2004 · N808NK · Doug DC983SDR GAIA04142Skin · crackedDURING C-CHECK INSPECTION FOUND NR 2 ENGINE INLET INTERIOR RT SIDE STA 1183 CRACKED. REF FASI NR 86722 CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR IAW SRM 54-10-3, FIG 9.Sep 10, 2004 · N180AX · Boeing 727222SDR ASAA0410371Cowling · wornFOUND NR 2 ENGINE NOSE COWL AFT LIP REPAIR WORN/DENTED. REMOVED AND REPLACED LOWER AFT CAP. (M)Aug 13, 2004 · N746AS · Boeing 737200SDR 2004FA0000754Door · brokenPILOT COMPLAINED OF STUCK THROTTLE ON GROUND. FOUND ALTERNATE AIR DOOR BROKEN OFF AND WEDGED IN THROTTLE BODY. HINGE APPEARED TO HAVE WORN COMPLETELY THROUGH.Aug 6, 2004 · N49J · Propjt 200DSDR GTIA040700Guide Vane · crackedNR 2 ENGINE IGV HAS CRACK AT 1:00 POSITION, UPON INSPECTION FOUND CRACK HAS PROGRESSED BEYOND LIMITS AND ALSO HAS CRACK AT BOTTOM OF SAME VANE. REMOVED AND INSTALLED NR 2 ENGINE IGV. (M)Jul 31, 2004 · N835NK · Doug DC983SDR B3OR20040719Hinge · looseANNUAL INSP, ALTERNATE AIR SOURCE DOOR WAS LOOSE. MECHANIC FOUND DOOR SPRING P/N 1250728-1, HINGE PIN P/N MS20253P2-364 IN INDUCTION AIR BOX DUCTING. PIN AND SPRING WERE RE-ASSEMBLED WITH DOOR. WHEN PARTS WERE RE-ASSEMBLED, BOTH UPPER AND LOWER ENDS OF HINGEJul 19, 2004 · N5515Y · Cessna T210NSDR 2004FA0000577Sealant · separatedACFT HAD LOW POWER DURING TAKE OFF, DURING THE FOLLOW-UP INSPECTION THE MECH. FOUND PIECES OF SILICON MISSING AROUND THE CARB INTAKE SUSPECTED THAT IT WAS INGESTED THROUGH THE CARB DURING TAKE OFF. THIS ACFT HAD STC NR SA4428SW INSTALLED ON 9-16-98 PART OF THJul 14, 2004 · N738GV · Cessna 172MSDR 2004F00318Inlet · departedAFTER TAKEOFF, NR 1 ENGINE INBOARD AND OUTBOARD FAN COWL DEPARTED AIRCRAFT. A SHUTTER WAS FELT BY THE AIRCREW AND THE NR 1 ENGINE INSTRUMENT LIGHTS FLASHED AMBER AND THEN WENT TO NORMAL. THE NR 1 ENGINE OIL QUANTITY LIGHT REMAINED AMBER. AN EMERGENCY WAS DECJul 13, 2004 · N951LF · Airbus A320233SDR 04FDEA02057Shroud · gougedAT C-CHECK AT BFM N/R N00504 WAS WRITTEN FOR THE NR 2 ENGINE LT SHROUD FAN COWL LAND BEING GOUGED. REMOVE AND REPLACE THE SHROUD IAW SRM 51-31-01. THE SHROUD PANEL WAS FABBED ON MAE TRAVELER T/4-442977.Jul 12, 2004 · N398FE · Doug MD1010FSDR GTIA040680Nose Cowl · crackedFTW - FOUND RIGHT INLET COWL HAS TWO CRACKS APPROX 8 INCHES IN LENGTH IN MOUNT RING FLANGE, INTERNALLY AT 4 AND 6 O'CLOCK POSITION. REMOVED NR 2 ENGINE INLET. INSTALLED SERVICEABLE NR 2 ENGINE INLET. (M)Jul 10, 2004 · N803NK · Doug DC982SDR UPS04M42730Skin · crackedINSPECTION TYPE: C2, NR 2 ENGINE INLET EXTERIOR UPPER LT SEGMENT HAS 4 CRACKS AROUND FASTENER HOLES. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUT OUT, FABRICATED AND INSTALLED 2 FILLERS AND REPAIR DOUBLER IAW SRM 51-31-04 AND DWG AJC7558.Jun 16, 2004 · N252UP · Doug MD11FSDR UPS04M42729Skin · crackedINSPECTION TYPE:C2, NR 2 ENGINE INLET EXTERIOR UPPER RIGHT SEGMENT HAS 3 CRACKS AT FASTENER HOLES. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER IAW SRM 54-10-00 AND DWG PLAJC8311.Jun 16, 2004 · N252UP · Doug MD11FSDR UPS04M42728Skin · separatedINSPECTION TYPE:C2 NR 1 ENGINE NOSE COWL INTERNAL RIB IS SEPARATED FROM SKIN APPROX 4 TO 8 O'CLOCK POSITION. REMOVED AND REPLACED INLET COWL IAW M/M 71-11-01.Jun 16, 2004 · N252UP · Doug MD11FSDR UPS04M42731Skin · crackedINSPECTION TYPE:C2, NR 2 ENGINE INLET EXTERIOR SIDE LOWER FROM 4 TO 8 O'CLOCK HAS NUMEROUS CRACKS. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUTS. FABRICATED AND INSTALLED FILLERS AND REPAIR DOUBLER IAW SRM 54-10-00 FIG 1B AND DWG ATC8311 IT-5.Jun 14, 2004 · N252UP · Doug MD11FSDR COMA0460351Inlet · erodedRT HAND ENGINE HEATED IN-LIT LIP ERRODED OUT OF LIMITS. REPAIRED RIGHT HAND ENGINE LIP-SKIN USING SERVICEABLE SKIN, 12.5 SECTION IAW SHORTS CMM 71-61-01.Jun 4, 2004 · N975CA · Cndair CL6002B19SDR 2004FA0000800Latch · failedDURING THE ANNUAL INSPECTION, FOUND THE PN 1250938-8, MAGNET LATCH ON THE ALTERNATE AIR DOOR WITH ONE OF ITS STEEL BONDED PLATES LOOSE AND READY TO FALL INTO THE TURBO, COULD CAUSE INFLIGHT FAILURE. INSTALLED THE NEW IMPROVED CATCH PN C100200. RECOMMEND MANDJun 3, 2004 · N7568M · Cessna T210MSDR 2004FA0000770Plate · separatedENGINE ALTERNATE AIR DOOR IS HELD CLOSED WITH A MAGNETIC LATCH ORIGINAL PN 1250938-8. THE MAGNETIC LATCH HAS 2 STEEL SMALL PLATES BONDED TO THE MAGNET THAT MAKE CONTACT WITH THE ALTERNATE AIR DOOR. ONE STEEL PLATE CAME DEBONDED FROM AGE VIBRATION. PLATE WASJun 3, 2004 · N732WP · Cessna T210MSDR CA040604001Inlet Guide Vane · out of limits(CAN) CRACK FOUND ON ONE ENGINE INLET GUIDE VANE APROX 3.5 IN LONG (OUT OF LIMITS IAW MM 72-00-00). AIRCRAFT WAS FERRIED, IAW FLIGHT PERMIT AUTHORIZATION AND THE MANUFACTURER APPROVAL, ENGINE NR 2 HAS BEEN REPLACED.Jun 1, 2004 · Doug DC983SDR C2XA04SH322Intake · gougedDURING C-CHECK THE NR 2 INTAKE WAS FOUND TO BE GOUGED AT 12 O'CLOCK. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 26, 2004 · N11565 · Emb EMB145LRSDR C2XA04SH321Intake · gougedSHV - DURING C-CHECK THE NR 1 ENGINE INTAKE COWLING MOUNTING FLANGE WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 26, 2004 · N11565 · Emb EMB145LRSDR QU22004F00000Inlet · cracked(REGISTRATION NR CHANGE FROM 888MF). DURING INSPECTION, A FLUSH PATCH APPROXIMATELY .5 INCH BY 2 INCHES WAS NOTED IN THE ENGINE INLET. THIS IS NOT AN APPROVED REPAIR. MFG REQUIREMENTS ARE TO RESKIN THE INNER INLET.May 20, 2004 · N888ME · Amd FALCON50MYSTSDR 2004FA0000660Door · ingestedPARTIAL LOSS OF ENG PWR OCCURRED JUST AFTER T/O. MANIFOLD PRESS DROPPED TO 15 INCHES HG AND RPM DROPPED TO 1900. PRE T/O ENG RUN UP, ALTERN AIR CHECK WAS REPORTED AS (NORMAL). POST FLT INSP REVEALED THAT ALTERN AIR (HEAT BOX) DOOR HAD SEPARATED FROM ALTERNAMay 19, 2004 · N2495M · Piper PA28R201SDR 2004FA0000513Door · failedPARTIAL LOSS OF ENGINE POWER OCCURRED JUST AFTER TAKEOFF. THE MANIFOLD PRESSURE DROPPED TO 15 INCHES HG, RPM DROPPED TO 1900. PRE TAKEOFF ENGINE RUN UP, ALTERNATE AIR CHECK WAS REPORTED AS NORMAL. A POST FLIGHT INSPECTION REVEALED THAT ALTERNATE AIR (HEAT May 19, 2004 · N2495M · Piper PA28R201SDR C2XA04SH294Skin · dentedDURING C CHECK THE NR 2 ENGINE INTAKE PERFORATED SKIN WAS FOUND TO BE DENTED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 54-20-01, SECTION 7, (FIGURE 207). THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 18, 2004 · N15973 · Emb EMB145SDR GTIA040452Nose Cowl · dentedNR 1 INLET COWL HAS A DENT AT 5 O`CLOCK POSITION. REMOVED AND REPLACED NOSE COWL.May 12, 2004 · N809NK · Doug DC983SDR UPS04M42586Inlet · crackedINSPECTION TYPE: C2, NR 2 ENGINE INLET EXTERIOR SKIN IS CRACKED AROUND FASTENER HOLES. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUTS, FABRICATED FILLERS AND DOUBLERS IAW SRM 54-10-00 FIG 1 AND SERVICE BULLETIN MD11-54-065.May 11, 2004 · N251UP · Doug MD11FSDR DHL2004754016Nose Cowl · dentedDURING A C-CHECK, NR 3 ENGINE NOSE COWL INLET RING OUT EXTERIOR SURFACE AFT SKIN EDGE AREA AT 3 O'CLOCK POSITION HAS A DENT. DAMAGE OUT OF LIMITS IAW B727 SRM 54-30-1 FIG 1, CUT OUT DAMAGED AREA DIM 2.25 X 1.75 INCH AND FABRICATED NEW FILLER DIM 2.25 X 1.75 IMay 9, 2004 · N754DH · Boeing 727223SDR ASAA0410240Nose Cowl · crackedDURING C-CHECK, FOUND NR 2 ENGINE NOSE COWL CRACK EMINATING FROM FASTENER HOLE. REMOVED DAMAGE AND INSTALLED RPR ANGLE IAW EA7110-01233. (M)May 1, 2004 · N730AS · Boeing 737290CSDR 2004FA0000745Air Box · damagedDURING RUN-UP, BEFORE DEPARTURE, THE CARBURETOR HEAT WAS CHECKED AT 1000 AND 1700 RPM WITH ABOUT 75 RPM DROP. DURING THE FLIGHT BACK, IN CRUISE FLIGHT, THE CARB HEAT WAS CHECKED AGAIN AT VARIOUS POWER SETTINGS, WORKING NORMALLY WITH ABOUT A 100 RPM DROP. AFTApr 24, 2004 · N5048E · Cessna 172N
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