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 GTIA040334Accoustic Liner · damagedDTW - FOUND ACCOUSTIC LINE DAMAGE AT 12 O'CLOCK POSITION ON NR 1 ENGINE REAR FAN CASE SECTION. REMOVED AND REPLACED NR 1 ENGINE. (M)SDR C2XA04SH233Intake · gougedSHV- DURING C-CHECK THE RIGHT HAND ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE UPPER COWLING ALIGNMENT HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMBRAER IC 2004-145/1466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH222Cowling · gougedDURING C-CHECK THE LT LOWER ENGINE COWLING WAS FOUND TO BE GOUGED ON THE INNER SKIN AT STATION XN1485.0. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A PATCH REPAIR IAW EMB 145 SRM 54-10-01 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH208Intake · gougedSHV- DURING C-CHECK THE LEFT 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.SDR C2XA04SH207Intake · gougedDURING C-CHECK THE RIGHT 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.SDR 04FDEA00823Bellmouth · delaminatedCOMPLY WITH EA 8-7110-75131 ENGINE BELL-MOUTH RING ASSY INTERIM REPAIR A/C N389FE. COMPLIED WITH EA 8-7110-75131.SDR C2XA04SH187Intake · gougedSHV- DURING C-CHECK THE NR 2 ENGINE INTAKE UPPER COWLING GUIDE PIN HOLE WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 2004F00187Skin · damagedDURNG WALK AROUND INSPECTION FOUND, SKIN DAMAGE WITH SKIN PEELED AND MISSING ON LOWER FORWARD RIGHT SIDE CENTER ENGINE AIR INLET DUCT HOUSING, BETWEEN FUSELAGE STATION 1183 AND 1233. REMOVED SKIN DAMAGE AS NECESSARY. INSTALLED EXTERNAL DOUBLER REPAIR AT LOWESDR GTIA040221Liner · looseACY - NR 2 ENGINE INTAKE LINER LOOSE FOUND ON WALKAROUND. REMOVED DAMAGED ACOUSTIC PANEL LINER. INLET COWL INSPECTION AND REPAIR OF THE DYNA ROHR ACOUSTIC PANELS ACOUSTIC LINING MISSING BETWEEN 4 O'CLOCK AND 8 O'CLOCK POSITION NOSE COWL TO BE REPLACED ON C/OSDR C2XA04SH152Intake · gougedSHV - DURING C-CHECK, THE NR 2 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH151Intake · gougedSHV - DURING C-CHECK, THE NR 1 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR P5CA0401055Intake · delaminatedNR 2 ENG INBOARD OUTSIDE FAN COWL REQ UPGRAGE, INTERNAL 84 X 20 INCH AREA DELAMINATED BEYOND LOCAL REPAIR. REPLACED COWLING.SDR BAQA093683Actuator · failedEXCHANGE - CORE RETURN FOR EXCHANGE PO 2-023236-05, ACTUATOR IS CAUSING COMPRESSOR STALLS. PLEASE NOTE THAT THIS ACTUATOR (S/N 2939) WAS INSTALLED ON ENGINE LE45512 FOR ONLY 7.2 HOURS, (DO NOT REPAIR AND RETURN S/N 2939). REPLACED WITH SERVICABLE UNIT. 03/18/SDR C2XA04SH131Intake · gougedSHV- DURING C-CHECK THE NR 2 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH130Intake · gougedSHV- DURING C-CHECK THE NR 1 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH123Intake · gougedSHV- DURING C-CHECK THE NR 1 ENGINE AIR INTAKE WAS FOUND TO BE GOUGED AROUND THE UPPER COWLING ALIGNMENT HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH122Intake · gougedSHV- DURING C-CHECK THE NR 2 ENGINE INTAKE AFT FLANGE WAS FOUND TO BE GOUGED AROUND THE UPPER COWLING ALIGNMENT HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH101Intake · gougedSHV- DURING C-CHECK THE NR 2 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH100Intake · gougedSHV- DURING C-CHECK THE NR 1 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR BAQA093508Actuator · failedMECHANIC WAS UNABLE TO ADJUST FLOW OF ACTUATOR. REPLACED WITH SERVICABLE UNIT FROM ITS 03/05/2004SDR 04FDEA00411Pipe · damagedCOMPLY WITH EA 8-7160-73881. POWERPLANT - ENGINE DRAINS MINOR DEVIATION TO FEDEX EO 8-7160-7-5000. POWERPLANT - ENGINE DRAINS - MINOR DEVIATION TO FEDEX EO 8-7160-7-5000 COMPLIED WITH AT BFM/MAE.SDR GTIA040198Nose Cowl · corrodedFTW - FOUND NR 1 ENGINE NOSE COWL LIPPING CORRODED AT 1:00 AND 5:00 O'CLOCK POSITION. FOUND CORROSION OUT OF LIMITS. REMOVED NOSE COWL. INSTALLED THE NR 1 ENGINE NOSE COWL. (M)SDR NACA20040011Intake Pipe · rupturedNR 4 ENGINE BACKFIRING ON FINAL AND UPON LANDING. ENGINE SHUT DOWN AFTER LANDING. REPLACED NR 4 ENGINE, NR 15 & 16 Y-PIPE DUE TO BEING RUPTURED. CHECKED GOOD ON RUN.SDR PG9R118895Intake · crackedAIR INTAKE CRACKED WITH ONLY 531.8 HOUR. (RMA NR R046964)SDR VNAA0402002Intake · defectiveDURING FLIGHT, THE CREW RECEIVED A LEFT HAND ENGINE INTAKE DE-ICE FAIL INDICATION AND RETURNED TO CLT. MAINTENANCE INSPECTED AND REPLACED THE AIR INTAKE ASSEMBLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THSDR C2XA04SH055Structure · gougedSHV - DURING C-CHECK THE RIGHT ENGINE INTAKE UPPER COWLING GUIDE PIN HOLE SURROUNDING AREA WAS FOUND TO GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EXPRESS JET EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH054Structure · gougedSHV - DURING C-CHECK THE LEFT ENGINE INTAKE UPPER COWLING GUIDE PIN HOLE SURROUNDING AREA WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EXPRESS JET EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR KMB2004F00000Actuator · inoperativeENGINE ALTERNATE AIR INTAKE DOORS WILL NOT ACTUATE, OPEN. REMOVED AND REPLACED.SDR PG9R118894Intake · crackedAIR INTAKE HAS A CRACK. (RMA NR R046894)SDR GTIA040106Nose Cowl · wornFTW - NR 1 ENGINE NOSE COWL HAS EXPOSED FIBERGLASS AFT OF INLET RING ENTIRE CIRCUMFERENCE. ON FURTHER INVESTIGATION FOUND NOSE COWL SKIN DELAMINATED. REPAIRED COWL. (M)SDR CA040126002Hinge · worn(CAN) MAINTENANCE INSPECTION DISCOVERED LT ENGINE INLET VANE HINGE PIN WAS WORKING OUT OF THE HINGE AND CONTACTING THE INNER COWL STRUCTURE. MFG ADVISES THE HINGE ENDS ARE CRIMPED TO PREVENT PIN MOVEMENT, HOWEVER ON THIS ASSY THE PIN APPEARS TO HAVE WORN THRSDR QXEA200400058Switch · damagedRDM FLIGHT 2128, DIVERTED TO PDX DUE TO WEATHER NR 2 BYPASS DOOR SWITCH WILL NOT LATCH IN THE OPEN POSITION. REPLACED BYPASS CONTROL SWITCH IAW HORIZON AIR EO 2-30-04B. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR CX7A194J0409Ring · missingRIGHT ENGINE IGV ACTUATOR RING MISSING PIN FOR 6 O'CLOCK POSITION IGV ACTUATING ARM.SDR GTIA040158Nose Cowl · missingRT ENGINE NOSE COWL SN 49123 ACOUSTIC LINING MISSING ON LOWER HALF OF PERFORATED INTERIOR. REMOVED NOSE COWL. INSTALLED RT NOSE COWL.SDR CM2RSeparator · obstructedOLD ENGINE SEPARATOR WAS CRACKED. ORDERED NEW PART. INSPECTED NEW PART AND COULD NOT BLOW THROUGH IT. THE AIR OUTLET TUBE WAS BLOCKED INTERNALLY. NEW OUT OF BOX FAILURE. IF THIS UNIT WAS INSTALLED ON THE ENGINE IT WOULD HAVE PRESSURIZED THE CASE AND LEAD SDR 2004FA0000222Cage · failedWELDS FAILED ON AIR FILTER CAGE END THAT ATTACHES END RING.SDR C2XA04SH011Structure · gougedSHV- DURING C-CHECK THE NR 2 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH010Structure · gougedSHV- DURING C-CHECK THE NR 1 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 2004FA0000068Air Filter · mismanufacturedFACTORY NEW PART- SCREEN ATTACH TABS ARE BENT 90, AND SPOT WELDED ON TO SCREEN FRAME. WELDS DO NOT PENETRATE BASE MATERIAL. ATTACH TABS WORK LOOSE. HAVE FOUND THIS CONDITION 3 TIMES. SOME HAVE BEEN REPAIRED WITH SHEET METAL SCREWS. TABS SHOULD BE RIVETED SDR PG92004F00006Structure · crackedAIR INTAKE ASSEMBLY CRACKED. (RMA NR R045785) (K)SDR YENA200338Actuator · failedENGINE ONE COMPRESSOR VANE ECAM ON TAKEOFF AT ABOUT 50 KTS. DID LOW SPEED RTO. REMOVED AND REPLACED NR 1 ENG VARIABLE STATOR ACTUATOR IAW AMM 75-32-41, AS PART OF TSM 75-30-00. PERFORMED TEST NR 11 (HIGH POWER ASSURANCE TEST) ON NR 1 ENGINE IAW 71-00-00-710SDR BAQA089617Actuator · failedMLG ACTUATOR FAILED AFTER 13.6 HOURS.SDR 2003FA0001072Filter Element · separatedENGINE LOST POWER SHORTLY AFTER TAKEOFF. FORCED LANDING RESULTED IN SUBSTANTIAL DAMAGE TO THE AIRCRAFT. INVESTIGATION FOUND PIECES OF THE AIR FILTER ELEMENT IN THE VENTURI OF THE CARBURETOR. THE FILTER ELEMENT HAD BEEN IMPROPERLY INSTALLED ALLOWING THE ENTIRE SDR BAQA089758Actuator · failedACTUATOR ONLY LASTED 67.1 HOURS SINCE OVERHAUL. TORQUE AND N1 FLUCTUATING. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 10/22/03SDR GTIA030744Acoustic Liner · damagedON WALK AROUND FOUND NR 2 ENGINE INLET ACOUSTIC LINING DAMAGED 15 BY 39 SECTION MISSING NO DAMAGE TO HONEYCOMB STRUCTURE. REMOVED AND REPLACED NR 2 ENGINE NOSE COWL AS REQUIRED. NO FURTHER DEFECTS NOTED. (M)SDR UPS03541237Acoustic Liner · dentedRT ENGINE HAS DENT & DELAMINATION ON INLET SOUND ABSORBENT LINER. REPAIRED DENT IN RT NOSE COWL ACOUSTICAL LINER PER MM 72-33-05-8 PG 1.SDR GTIA030657Inlet Guide Vane · crackedENGINE 2-217A ESN 708450 INLET GUIDE VANE HAS ROOT AND INNER SHROUD WELD TO SHROUD CRACKED. REMOVED AND REPLACED IGV CASE. (M)SDR C2XA03SH290Intake · gougedSHV DURING C CHECK THE NUMBER ONE ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR AWXA200300971Actuator · malfunctionedON TAKEOFF ROLL AT SMF EN ROUTE FOR PHX RECEIVED NR 2 ENGINE COMPRESSOR VANE FAULT, REJECTED TAKEOFF AT 60 KTS. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75306, OPERATIONAL AND LEAK CHECK WERE GOOD PER T/C F5MSDR 2003FA0000865Air Box · crackedENGINE AIRBOX CRACKED IN THE FLANGE AREA WHERE THE CARB HEAT CABLE ATTACH BRACKET IS ATTACHED TO THE AIRBOX ASSEMBLY WITH TWO RIVETS. THIS IS A CONSTANTLY CRACKING AREA ON THE AIRBOX. MFG IS WELL AWARE OF THE PROBLEM AND HAS BROUGHT OUT AN (IMPROVED) ASSEMBL
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