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 RMXA32210613NAInlet · burnedUPON DEPARTING, PILOT NOTICED A BURNING SMELL FOLLOWING GEAR RETRACTION. PILOT CONFIRMED THE ODOR IN THE CABIN WITH THE CLINICAL CREW MEMBERS AND THEN ELECTED TO RETURN FOR A PRECAUTIONARY LANDING. MECHANIC RESPONSE TO DUPLICATE THE ODORS, HAD PILOT RUN THE SDR 2010FA0000183Inlet · damagedON POST FLIGHT INSP, DISCOVERED 2 RIVET HEADS MISSING FROM THE LT ENGINE INLET COWL. THE ENGINE WAS VISUALLY INSPECTED AND DAMAGE TO THE FAN BLADES WAS NOTED. A BOROSCOPE INSP WAS ACCOMPLISHED ON THE 1ST STAGE COMPRESSOR BLADES AND DAMAGE WAS NOTED. THE ENGINESDR A6WA201040123Nose Cowl · gougedLT LOWER NOSE COWL CHAFED AND GOUGED ON T/E. REMOVED DAMAGED T/E AND INSTALLED SERVICEABLE PN 228-50091-107 T/E IAW CMM 20-26-00, 20-42-061, 20-40-11, 71-14-01.SDR 2010FA0000184Housing · damagedAFTER 150 HOURS ON ACFT DURING SCHEDULED MAINTENANCE THE FIRST ONE OF THE TYPE OF PROBLEM WAS FOUND. MECHANICS ARE FINDING THE ALTERNATE AIR VALVE BODY CONTROL CABLE (PN NR DAI-9076-00-04) LOOSE OR COMPLETELY DISCONNECTED AND HANGING NEXT TO THE PRIMARY/ALTERSDR FOTR20006NR4879Nose Cowl · chafedNR 3 ENGINE AFT T/E FROM 2-3 O`CLOCK POSITION CHAFED AND HOLE WORN THRU AS MARKED A NOSE COWL. REPAIRED ON FASI WO 20006, N/R 04879. REPAIRED NR 3 ENGINE NOSE COWL T/E FROM 2 TO 3 O’CLOCK POSITION IAW B727 SRM 54-10-3 FIG 3, REV 102. MATERIAL USED: ANGLE- 2SDR FOTR20006NR4888Nose Cowl · gougedNR 3 ENGINE NOSE COWL AT 4 O`CLOCK POSITION T/E GOUGED. REPAIRED ON FASI WO 20006, N/R 04888. REPAIRED NR 3 ENGINE NOSE COWL T/E AT 4 O’CLOCK POSITION IAW B727 SRM 54-10-3 FIG 3, REV 102. MATERIAL USED: ANGLE; 2024-T3, 0.063, DIM: 10.0 BY 2.0, FILLER; 2024-SDR C2XA10TY007Intake · corrodedNR 2 ENGINE AIR INTAKE FLANGE HOLES HAVE CORROSION. REMOVED CORROSION IAW EC5420-01158.SDR ALGA0111105694Mount · crackedFWD FLANGE ON COMPRESSOR REAR MOUNT CRACKED.SDR 2010FA0000023Duct · collapsedDURING ANNUAL INSP, FOUND DUCT JUST AFT OF INDUCTION FILTER TO BE PARTIALLY COLLAPSED. AFTER REMOVING DUCT, FOUND THE INTERNAL WIRE FORMERS TO BE DISCONNECTED AND UNRAVELED CAUSING THE DUCT TO COLLAPSE.SDR UALA2009122303986Inlet · gougedNR 2 ENG INLET WAS GOUGED AND SCRATCHED AT THE 4:30 POSITION WHEN THE FLIGHT CREW TAXIED INTO A BREAKAWAY STOP SIGN.SDR QXEA2009121101028Cowling · chafedC5 CHECK - LT LWR FAN COWL HAS CHAFE ON THE INSIDE. BLENDED CHAFE DAMAGE IAW SRM 51-12-00-001-001-A01. BLEND IS WITHIN LIMITS IAW SRM 54-14-00-101-001-A01 AND SRM 54-14-05-001-001-A01. TREATED AND PRIMED WORKED AREAS IAW SRM 51-21-11-001-001-A01 AND 51-25-SDR UALA2009111603564Inlet · damagedRAMP CREW REPORTS FINDING DAMAGE TO THE INLET COWL ABOUT 2:00 POSITION (ALF) SIX INCHES AFT OF THE LE. REPAIRED IN SHOP ON RR R13 469 AND REINSTALLED.SDR F3LA2009111800232Inlet · damagedTHE FLIGHT CREW MADE AN AIR RETURN DUE TO MULTIPLE BIRD STRIKES DURING CLIMB OUT CAUSING THE NR 2 ENG COMPRESSOR TO STALL. MX REMOVED AND REPLACED THE NR 2 ENG ASSY AND INLET COWL ASSY, REFERENCE MP71042-01 AND MP71042-02. MX PERFORMED AN OPS CHECK, LEAK CHECSDR GUUA93721111409AIntake · contaminatedPILOT REPORTED CHEMICAL ODOR COMING FROM RT BLEED. FOUND RESIDUAL OIL AT RT ENG INTAKE CLEANED AREA OF OIL. PREVIOUSLY SUBMITTED CORRECTED DATE.SDR GUUA93721110409AIntake · contaminatedPILOT REPORTED CHEMICAL ODOR COMING FROM RT BLEED. FOUND RESIDUAL OIL AT RT ENG INTAKE. CLEANED AREA OF OIL.SDR CA100601008Inlet · cracked(CAN) CRACKS HAVE BEEN FOUND AT THE INTERMEDIATE CASE INNER STRUT RADII. MANUFACTURER WILL INVESTIGATE TO ESTABLISH CAUSE AND DEFINE MITIGATING MAINTENANCE ACTION.SDR DXTA2009111003857Nose Cone · damagedPOSSIBLE BIRD STRIKE ON RT ENGINE AT 7 O`CLOCK POSITION. DENT FOUND ON ENGINE LIP AND BLOOD WITH FEATHERS AROUND INTAKE. PERFORMED A BIRD STRIKE INSP ON RT ENG AND BOROSCOPRED AND FOUND NO RESIDUE OF BIRD FID INGESTION. REMOVED AND REPLACED NOSE CONE LIP WITSDR A6WA200940790Strip · erodedRT ENGINE LOWER FAN COWL AFT EDGE STRIP IS CHAFED/ERRODED. REMOVED AND REPLACED IAW CMM SHORTS TASK 71-14-01-300-814-A01.SDR A6WA200940714Cowling · erodedRT UPPER FAN COWL T/E IS CHAFED/ERODED. REPLACED IAW SHORTS CMM 71-14-01-300-814-A01.SDR C2XA09TY258Inlet · corrodedNR 1 AND NR 2 ENGINE INLETS HAVE CORROSION IN THE BOLT HOLES. REMOVED CORROSION IAW EC5420-01158.SDR 2009FA0000921Screen · crackedREPAIR STATION IS HOLDER OF STC SA03674AT FOR THE INSTALATION OF R-134 COOLANT AIR CONDITIONER SYS IN THIS ACFT. IAW THIS STC INSTALLATION, A CONDENSER HOUSING IS MOUNTED ON THE BOTTOM OF THE ACFT FUSELAGE. IT HAS BEEN DISCOVERED THAT THE SCREEN WHICH COVERSSDR CA090812001Air Box · crackedFOUND CRACKED IN TWO PLACES.SDR N6WA20090802Intake · dentedDENT FOUND ON NR 2 ENG INTAKE LIP AT THE 4 O'CLOCK POSITION. REPAIRED DAMAGED LIPSKIN ON NR 2 LIPSKIN IAW SRM 54-11-05-201-001-A01. CLOSE CARRYOVER NR 951 (MAJOR REPAIR).SDR CA090805003Control Cable · frayedUPON COMPLETION OF A ROUTINE TRAINING FLIGHT, THE PILOT REPORTED THAT THE LT CARBURETOR HEAT CONTROL FELT LOOSE. UPON CLOSER INSP BY MX, IT WAS DISCOVERED THAT THE CABLE ASSY HAD FAILED WHERE THE FLEXIBLE CABLE IS SWAGED TO THE LEVER END ROD. INNER CABLE WASSDR C8GA20090245Web · crackedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE NR 3 ENGINE NOSE COWL INTERIOR WEB IS CRACKED AT THE 7 O'CLOCK POSITION. REMOVED WEB AND FABRICATED NEW FROM 2024 T3 .032" DIM 13" X 36". INSTALLED WEB, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TSDR C2XA09TY152Flange · corrodedNR 2 ENG INLET MOUNTING FLANGE HAS CORROSION AT MOUNTING HOLES. CLEANED AREA AND FOUND 3 HOLES TO HAVE CORROSION. REPAIRED THE MOUNTING FLANGE HOLES IAW EC5420-01158.SDR 2009FA0000828Air Filter · splitTHE FILTER IS SEPARATING AT MFG SEAM. THIS IS THE 3RD FILTER FOUND IN THIS CONDITION.SDR C2XA09TY071AInlet · corrodedTYS - DURING A CURRENT 6C INSPECTION THE NR 2 ENGINE INTAKE MOUNTING FLANGE WAS FOUND WITH SEVERAL BOLT HOLES PITTED AND CORRODED. MAINTENANCE REPAIRED 6 HOLES ON THE NR 2 ENGINE INLET IAW EC 5420-01158. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE SDR 2009F00030Inlet · damagedDURING SCHEDULED INSP, IT WAS DISCOVERED THAT 1 INLET RIVET HEAD WAS MISSING FROM THE NR 2 ENGINE INLET INNER SKIN (BARREL). THE INLET WAS INSTALLED 288.1 HOURS 206 CYCLES AFTER REPAIR DUE TO SAME CONDITION OF SEVERAL MISSING AND CRACKED RIVETS ON THE INNER SKSDR N9990001274Attach Fitting · crackedTHE UPPER ATTACH RING PN 314W1442-4 OF THE SN 000428 ENGINE INLET HAS 4 CRACKS, (1 EA) 2.55 INCH LONG, (1 EA) 1.85 INCH LONG, (1 EA) 4.07 INCH LONG, AND
(1 EA) 2.04 INCH LONG. THE MATING STRUCTURE WAS NDI`D (NO DEFECT NOTED) AND THE UPPER ATTACH RING WAS REMSDR C8GA20090069Skin · puncturedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE NR 1 ENGINE NOSE COWL LEADING EDGE EXTERIOR SKIN HAS A DEEP DENT PUNCTURE. DAMAGED AREA WAS REMOVED DIM 3 INCH BY 2 INCH. FABRICATED NEW REPAIR FROM 2024 T3 .063 INCH DIM 7 INCH BY 5 1/8 INCH, INSTALLED REPAISDR HALA2009032300094Nose Cowl · damagedETOPS SIGNIFICANT SYSTEM, NR 1 ENGINE NOSE COWL HAS DAMAGE ON OUTBOARD SIDE APPROX 1 FT AFT OF L/E , HALFWAY UP SIDE OF COWL. INSPECTED NR 1 ENGINE NOSE COWL OUTBOARD SIDE DAMAGE. CLEANED AND PERFORMED INTERIM REPAIR PER SRM 54-11-01-1A ALLOWABLE DAMAGE 1 INSDR IPXA09B55213Inlet · damagedINSPECTION TYPE:N/A NR 3 ENGINE NACELLE DAMAGED BY DE-ICE TRUCK DURING DE-ICE. INLET COWL NR 3 ENG NACELLE REMOVED AND INSTALLED PER MM 71-11-01-4.SDR CA090319009Intake · damaged(CAN) DURING B CHECK INSP NR 1, ENGINE INTAKE SCOOP MISSING ONE ROW OF RIVETS HOLDING RUBBER BOOT, DAMAGE TO BLOWER OCCURED DUE TO INGESTION OF RIVETS.SDR C2XA09TY046Flange · corrodedTYS - DURING C-CHECK INSPECTION FOUND THE NR 2 ENG AIR INTAKE MOUNTING FLANGE BOLT HOLES CORRODED. COMPLETED REPAIRS FOR 4 HOLES AT .300 INCH AND 11 HOLES FOR BUSHING INSTALLATION IAW EC 5420-01158. A/C STILL IN C-CHECK.SDR USAA2009031090552Inlet · erodedBFM - C1 - MAJOR REPAIR - NR 2 ENGINE INLET COWL ERODED AT ALUMINUM LIP COMPOSITE SECTION. CLEANED & PREPPED AREA, BONDED SEALER & REPAIR MATERIALS.SDR C2XA09SH063Inlet · corrodedSHV - DURING C-CHECK LT ENG INLET HAS CORRODED BOLT HOLE. MAINTENANCE REPAIRED LT ENGINE INLET MOUNTING ATTACHMENT FLANGE BOLT HOLE IAW EC5420-01158. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR FDEA200902270764Nose Cowl · dentedDURING TAXI IN, ACFT SLID OF TAXITRACK ON TURN. ACFT HIT SNOWBANK WITH NOSE GEAR AND ENGINE NR 2. ENGINE NR 2 NOSE COWL HEAVILY DAMAGED. REQUIRES PYLON, NOSE LANDING GEAR AND ENGINE INSPECTION PERFORMED INSPECTION PER AMM 72-22-00-6 FOR RUBSTRIP DAMAGE. DASDR C2XA09TY034Inlet · corrodedDURING A C-CHECK INSPECTION EIGHT BOLT HOLES WERE FOUND SHOWING CORROSION ON THE NR 1 ENGINE INTAKE MOUNT FLANGE. THE HOLES WERE CLEANED AND REAMED TO REMOVE ALL TRACES OF CORROSION IAW EC 5420-01158. A/C IS STILL IN C-CHECK.SDR C2XA09SH055Inlet · corrodedSHV - DURING C-CHECK RT ENG INLET FLANGE HAS CORRODED BOLT HOLES (MARKED). MAINTENANCE COMPLETED INSTALLATION OF NEW RT ENG INLET FLANGE IAW EC7160-01015. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH051Inlet · corrodedSHV DURING C-CHECK LT ENGINE INLET ATTACHING FLANGE HAS MULTIPLE SCREW HOLES WITH CORROSION. MX REPAIRED LT ENGINE INLET ATTACHING FLANGE IAW EC5420-01158. THE ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C8GA20090056Intake Duct · corrodedWHILE IN HEAVY MAINTENANCE IS WAS NOTED THAT THE NR 2 ENGINE S DUCT HAS CORROSION ON THE LOWER INNER SKIN BY THE DUCT ACCESS DOOR BS 1342.40. CUT OUT DAMAGE DIM 19.68 INCH BY 8 INCH. FABRICATED DOUBLER FROM 7075-O .080 INCH DIM 26 INCH BY 14 INCH. HEAT TSDR C8GA20090055Intake Duct · corrodedWHILE IN HEAVY MAINTENANCE IS WAS NOTED THAT THE NR 2 ENGINE S DUCT HAS CORROSION ON THE LOWER INNER SKIN AT UPPER AFT CORNER OF DUCT ACCESS DOOR. CUT OUT DAMAGE DIM 9.25 INCH BY 5 INCH. FABRICATED DOUBLER FROM 7075-O .080 INCH DIM 16 INCH BY 11.5 INCH HEATSDR C8GA2009Intake Duct · corrodedWHILE IN HEAVY MAINTENANCE IS WAS NOTED THAT THE NR 2 ENGINE S DUCT HAS CORROSION ON THE LOWER INNER SKIN AT UPPER AFT CORNER OF DUCT ACCESS DOOR. CUT OUT DAMAGE DIM 9.25 INCH BY 5 INCH. FABRICATED DOUBLER FROM 7075-O .080 INCH DIM 16 INCH BY 11.5 INCH HEATSDR HNAA2009061900186Web · damagedLT ENGINE BOTTOM COWLING INBD INTAKE WEB DAMAGE. REPAIR INTAKE WEB IAW RD8-71-74.SDR 2009FA0000055Duct · dislodgedTHE BYPASS DOOR ON THE ENGINE AIR INDUCTION FILTER DUCT TO THE THROTTLE BODY WAS FOUND LAYING IN THE BOTTOM OF THE DUCT, THE DOOR PIN HAD FALLEN OUT AND THE DOOR, THE SPRING, AND THE HINGE PIN WERE FOUND IN THE BOTTOM OF THE DUCT , NO PARTS HAD GONE ANY FURTHESDR CA090129014Nose Cowl · separatedTHE OPERATOR HAS REPORTED THE FOLLOWING, DURING TAKEOFF ON A FLIGHT THE NR 2 ENGINE UPPER ENGINE COWL DETACHED. THE CREW NOTED A SLIGHT BUFFET DURING THE EVENT AND CONTINUED TO THE DESTINATION AIRPORT WHERE IT WAS DISCOVERED THAT THE COWL WAS MISSING. THIS WSDR DALA1134579221Skin · crackedCRACKS ON THE NR 1 ENGINE INLET COWL LIP SKIN (S/N 0216001).SDR C2XA09SH013Intake · corrodedRT ENGINE AIR INTAKE HAS VARIOUS MOUNTING BOLT HOLES THAT ARE CORRODED. REPAIRED RT ENGINE AIR INTAKE MOUNT HOLES IAW EC5420-01158. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR CA090119013Sleeve · looseON GROUND RUN IT WAS DISCOVERED THAT CYLINDER NR 5 ON THE RIGHT ENGINE, EGT WAS NOTICABLY HIGHER THAN OTHER CYLINDERS. INDUCTION TUBE WAS REMOVED FROM THE CYLINDER, THE INDUCTION TUBE SLEEVE IN THE OIL SUMP WAS FOUND TO BE LOOSE.
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