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 IPXA2024062546410Inlet · crackedNR 2 ENGINE INLET COWL ANTI-ICE DUCT FLANGE IS CRACKED AT INLET COWL AFT BULKHEAD. INSTALLED INLET COWL ANTI-ICE DUCT IAW AMM 30-21-00-401.- PERFORMED LEAK TEST IAW AMM 71-00-00/501 NO LEAKS FOUND. DYE PENETRANT INSPECTION FOR THE NR 2 ENGINE INLET COWL WAS PSDR SWI2024062100519Inlet · dentedADM# N742SK-7436(CRJ700) RH ENG INLET @ 9:00 FORWARD OF FADEC PANEL. DENT DEPTH = 0.025 INCH DEEP X 1.0 INCH WIDE X 1.0 INCH LONG. (C-CHECK RO 6/19/2024) REPAIRED DENT ON THE RH ENGINE INLET @9:00 FORWARD OF FADEC PANEL AS PER REO# 670-54-11-1385 REV --SDR SWAA2024052881039Inlet · cracked# 1 ENGINE INLET COWL OUTER BARREL LOWER SKIN ANTI-ICE AIR GRILL OUTLET CRACKED AT 6 O'CLOCK. MARKED DOT 251-006<[01] ENG 1 INLET COWL WILL BE REPLACE USING TASK CARD 7111-E-17062-NG (REP - INLET COWL AND CRUSHABLE WEAR SPACERS) [TTG8Q00S71ZL];[02] VERIFIED STSDR JJBA20240304014Doubler · damagedLH ENGINE AIR INTAKE REAR BULKHEAD TOP DOUBLER FROM COWL ALIGNMENT PIN DAMAGED. LH ENGINE AIR INTAKE REAR BULKHEAD TOP DOUBLER FOR COWL ALIGNMENT PAN REPAIR CARRIED OUTSDR TAMF20240220042Inlet · dentedDURING TRANSIT CHECK A BIRD STRIKE WAS FOUND ON RH ENGINE AIR INTAKE INLET COWL. THE AIR INTAKE INLET COWL(PN: SJ30361, SN SB/RR/T700/1614) NEEDS TO BE REPLACED.SDR SWAA2024022750377Fastener · cracked#1 ENGINE INLET HAS 3EA FASTENERS WITH CRACKED HEADS AT THE 10:00 SPLICE IN THE OUTER LIP SKIN: REQUIRES REPLACMENT OF INLET ASSY.<[01] UPDATED PARTS;[02] REMOVED AND REPLACED #1 ENG INLET COWL IAW AMM 71-11-01-400-802-F00<BR><BR>CAL TOOL<BR>T/W ID:ATS2321 DUESDR SWAA2024011842355Fastener · missing#2 ENGINE INLET COWL; LIP SKIN HAS MISSING FASTENER AT APPROX 1 OCLOCK POSITION; AS VIEWED FROM AFT. REMOVED AND REPLACED #2 ENGINE INLET COWL PER AMM 71-11-01 C/W. REMOVED AND REPLACED #2 ENGINE INLET COWL PER AMM 71-11-01SDR COEA2023112902708Unknown · unknownWO 252637/NR 6 DISCREPANCY: DURING A SCHEDULED MAINTENANCE INSPECTION, IT WAS DISCOVERED THAT THE R/H INTAKE INTERIOR LOWER SURFACE PANEL IS CRACKED. REPLACED THE R/H ENGINE LOWER COWL SKIN IAW 408 SRM CH 51-00-00 AND IPC 71-10-10.SDR JGVR2023112201Deflector · corrodedAPU STARTER INLET DEFLECTOR HAS NUMEROUS AREAS OF CORROSION. REMOVED CORRODED APU GENERATOR INLET DEFLECTOR AND INSTALLED NEW P/N: 6950610-7SDR UIEA2023112080961Blade · damagedBIRDSTRIKE ON RH ENG. FOUND FANBLADES #32 & 34 DAMAGED(<P>R/R FAN BLADES #32, 34, 13 AND 15 IAW AMM 72-31-02. C/W ENG TEST #8. ALL VIBE INDICATIONS WITHIN LIMITS.</P>)SDR IPXA2023092094211Bulkhead · crackedINSPECTION TYPE:1C2 ENG I/B SIDE OF INLET AREA PT2 LINE ANCHOR POINT IS CRACKED IN SHEET METAL (BULKHEAD)FABRICATED REPAIR DOUBLER IAW SRM 54-10-00.SDR 2023FA0000317Grommet · excess playTHE SILICONE GROMMET P/N 463-544 USED ON AIR BOX P/N 28P71A007-001 IS WEARING ON THE METAL STRUCTURE OF THE AIR BOX CAUSING EXCESSIVE PLAY. THIS ALLOWS THE ALTERNATE AIR VALVE TO MOVE INSIDE OF THE AIR BOX CAUSING DAMAGE TO THE AIR BOX AND VALVE. THIS ALSO IS SDR 2023FA0000768Lock Nut · missingWE WERE INFORMED THAT THE LAST COUPLE OF TREND NUMBERS WERE LOOKING A BIT HIGH FOR NG & ITT. BEFORE THE NEXT FLIGHT, WE LOOKED AT THE INERTIAL SEPARATOR AND FOUND THAT THE VANE HAD PLAY. A WASHER WAS ALSO FOUND IN THE BOTTOM OF THE ENGINE COWL. A PIVOT POINT OSDR 2023FA0000299Grommet · excess playTHE SILICONE GROMMET P/N 463-544 USED ON AIR BOX P/N 28P71A007-001 IS WEARING ON THE METAL STRUCTURE OF THE AIR BOX CAUSING EXCESSIVE PLAY. THIS ALLOWS THE ALTERNATE AIR VALVE TO MOVE INSIDE OF THE AIR BOX CAUSING DAMAGE TO THE AIR BOX AND VALVE. THIS ALSO IS SDR IPXA2023030791646Web · crackedINSPECTION TYPE:CK1C#2 ENG O/B NOSE COWL AFT BULKHEAD PITO TUBE CONNECTION PLATE HAS A CRACKREMOVED, FABRICATED, AND INSTALLED WEB IAW SRM 51-40-21SDR IPXA2023030791645Splice · crackedINSPECTION TYPE:CK1C#2 ENG O/B NOSE COWL AFT BULKHEAD PITO TUBE CONNECTION PLATE HAS A CRACKREMOVED, FABRICATED, AND INSTALLED SPLICE IAW SRM 51-40-21SDR IPXA2023030491518Web · crackedINSPECTION TYPE:CK1C#2 ENG I/B NOSE COWL AFT BULKHEAD PITO TUBE CONNECTION PLATE HAS A CRACKREMOVED, FABRICATED, AND INSTALLED WEB IAW SRM 51-40-21SDR IPXA2023030491517Splice · crackedINSPECTION TYPE:CK1C#2 ENG O/B NOSE COWL AFT BULKHEAD PITO TUBE CONNECTION PLATE HAS A CRACKREMOVED, FABRICATED, AND INSTALLED SPLICE IAW SRM 51-40-21SDR IPXA2023030491516Web · crackedINSPECTION TYPE:CK1C#2 ENG O/B NOSE COWL AFT BULKHEAD PITO TUBE CONNECTION PLATE HAS A CRACKREMOVED, FABRICATED, AND INSTALLED WEB IAW SRM 51-40-21SDR 7C7A2022121900039Warning Message · illuminated#1 ENGINE INTAKE BYPASS DOOR OPEN LIGHT INTERMITTENT IN FLIGHT. OPEN LIGHT ILLUMINATES WHEN ADVISORY LIGHT TEST SWITCH MOVED TO ADVISORYSDR A6WA202210258417Skin · dentedRIGHT ENGINE LOWER TRANSLATING COWL HAD A DENT ON THE OUTER SKIN. AIRCRAFT REMOVED FROM SERVICE. FOUND OUT OF LIMITS IAW CMM 78-30-00, REV 24. CLEANED AND DRIED REPAIR AREA COMMON TO DENT IAW EA AWAC-CRJ254-01933, REV IR. INJECTED STRUCTURAL ADHESIVE INTO OPSDR 2022FA0000553Gasket · detachedDURING CRUISE FLIGHT AT 1500FT AGL PILOT OF L-5 REPORTED ENGINE POWER LOSS THROTTLE AT FULL POWER ENGINE AT IDLE. SUBSEQUENT OFF AIRPORT LANDING ACCOMPLISHED WITH NO DAMAGE TO AIRCRAFT . MAINTENANCE INVESTIGATION REVEALED THAT A PORTION OF THE AIR MAZE AIR FISDR UIEA2022061900619Fastener · missing# 2 ENGINE INLET CASE CHAFING STRIP MISSING PLASTIC FASTENERS AT 5 AND 9 O'CLOCK POSITIONS. INSTALLED MISSING PLASTIC FASTENERS AT ENGINE INLET CASE CHAFING STRIP AS PER 767-300 SRM 51-40-02-0G-0SDR A6WA202205268214Bracket · crackedL/H #1 ENGINE BRACKET P/N:228-50020-805 CRACKED AT 7 O'CLOCK POSITION AND BRACKET P/N: 228-50020-161 CRACKED AT 11-12 O'CLOCK POSITON ON NOSE INLET ATTACH RING. L/H #1 ENGINE NOSE COWL ATTACH RING FLANGE HAS 2 EA ELONGATED HOLES AT 7 O'CLOCK POSITION AND BETWSDR QXEA2022051200191Actuator · inoperativeWHEN ENGINE INTAKE SELECTED ON #1 SIDE, BYPASS DOOR REMAINS CLOSED, HEATER STILL COMES ON. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. REMOVED FROM SERVICE. CONFIRMED WHEN ENGINE INTAKE SELECTED ON #1 SIDE THE DOOR DOES NOT OPEN + ACTUATOR CONTINUOUSLY RUNS,SDR BIER2022011301Manifold · chafedINDUCTION MANIFOLD P/N 655607 WAS REMOVED FROM CURRENT ENGINE MODEL TSIO-550C(11) DUE TO CHAFE DAMAGE. WHEN NEW REPLACEMENT MANIFOLD P/N 646440 WAS RECEIVED AND COMPARED TO DAMAGED MANIFOLD. NEW INDUCTION COULD NOT BE MOUNTED BECAUSE OF ALIGNMENT ISSUES. RESEASDR HNAA2022021000074Not Reported · not reportedE896607 - R/H ENGINE CONTAINMENT RING GOUGED AT LOWER SURFACE .... BLENDED OUT GOUGE ON RH ENGINE CONTAINMENT
RING LOWER SURFACE IAW EMB 145 SRM 51-- 10-03. NO DAMAGE LIMITS FOR THIS AREA. MAPPED DAMAGE AND SENT OUT FOR FURTHER EVALUATION IAW PIEDMONT MPPM 13SDR DALA2021091005351Skin · corrodedSHIP 3327 CORROSION SKIN AIR INTAKE LIP ON ENGINE 1. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON SKIN AIR INTAKE LIP AT ENGINE 1 AS PER ER/A #593806-14. (1942606)SDR CALA2021090801534Rivet · missingPDA 3 #2 ENG AIR INTAKE COWL OUTER LIP SKIN HAS ONE RIVET HEAD BROKEN OFF/MISSING AT 7 O-CLOCK POS AFT LOOKING FORWARD-- SEE PHOTO PHOTO ADDED REPLACED DAMAGED FASTNER WITH NEW FASTNER WITH NEW FASTNER REF. EC/RA 7111-01387.SDR UIEA2021083101925Skin · dented2 ENG. INLET CASE HAS A DENT OUT OF LIMITS @ 11 O'CLOCK POSITION, MEASURED DENT AT NR 2 ENG INLET AT THE 11 O'CLOCK POSITION, FOUND MAX DEPTH TO BE .070". FOUND TO BE OUT OF LIMITS IAW SRM 54-12-01-1A, ALLOWABLE DAMAGE 1, FIG 101. REMOVED AND REPLACSDR IPXA2021090473547Fastener · looseINSPECTION TYPE:1C#2 ENGINE INLET NOSE SKIN HAS 23 LOOSE FASTENERS.REPAIRED #2 ENGINE INLET NOSE SKIN LOOSE FASTENERS IAW VT-SAA EA 011-7110-01-A9334 REV. IR AND UPS EO MD11-7110-81459-A. (MINOR)SDR CALA2021072801205Rivet · damagedPDA 3 TOTAL OF 6EA RIVET HEADS BROKEN/MISSING AT OUTER LIP SKIN OF #1 ENG AIR INLET COWL -- SEE PHOTO CORRECTION - #2 ENG AIR INTAKE COWL REPLACED 6 EA RIVETS REF ECRA 7111-01387SDR YV3R2021081000475Gauge · faultedCUSTOMER REPORTED CARBURETOR AIR TEMPERATURE GAUGE P/N: C604-8 WAS FAULTY.SDR UIEA2021050101042Fastener · worn#1 ENG INLET CASE O/B ANTI - ICE PANELS HAS (2 EA) HOLES THAT FASTENERS HAS WORN THRU. REQUIRES DIMPLE WASHER ON FASTENERS.(<P>REMOVED AND REPLACED WORN FASTENERS AT #1 ENG BY INLET CASE O/B ANTI-ICE ACCESS PANEL PER B767-300 AMM 20-11-00-910-802.<BR /></P>)SDR 2021FA0000153Seal · unsecureAIRCRAFT WAS IN CRUISE FLIGHT AND SUDDENLY LOST ENGINE POWER WITH NO PRIOR WARNING. AIRCRAFT PERFORMED EMERGENCY LANDING TO AIRSTRIP WITH NO DAMAGE. UPON INSPECTION IT WAS DETERMINED THAT THE SEAL THAT SURROUNDS THE CONNECTION BETWEEN THE AIR INTAKE AND THE CASDR DALA2021042802451Acoustic Liner · corrodedSHIP 3125 - CORROSION ON ACOUSTIC INNER BARREL AIR INTAKE COWL LOWER AREA ENGINE 2. CORRECTIVE ACTION: REMOVED AIR INTAKE COWL. INSTALLED AIR INTAKE COWL AS PER A320 FAM, AMM 71-11. (1790418)SDR SWIA202157734Skin · dentedTRANSFER FROM EAML 621831 : DENT ON #1 COWL INLET LIP SKIN MEASURING 4.25IN HIGH X 3.25IN WIDE X 0.37IN DEEP LOCATED APPROXIMATELY AT THE 2 O'CLOCK POSITION LOOKING AFT. DAMAGE IS OUT OF SERVICEABLE LIMITS PER SRM 71-61-01. (FLIGHT 3848 - FILED CLOSED) SDR HALA202103041026Skin · crackedETOPS - #2 ENGINE INLET COWL EXTERNAL SKIN IS CRACKED/PUNCTURED @ APPROX. 5:30 POSITION 1" FROM AFT EDGE EXTENDING 9 1/4" FWD. // REMOVED #2 AIR INTAKE COWL PER AMM 71-61-41-000-802-A. 1724236 3/3/21 REPLACED AND INSTALLED #2 AIR INTAKE COWL PER AMM 71-61-41-4SDR QXEA2021022700080Door Actuator · malfunctioned#1 ENGINE INTAKE BYPASS DOOR REMAINS CLOSED WHEN SWITCH IS PRESSED TO OPEN. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. REMOVED FROM SERVICE. VERIFIED INTK DEF ACT 1 CB (P6) WAS IN. DEPRESSED #1 ENG. INTAKE BYPASS DOOR SWITCH. CLOSED LIGHT REMAINED ILLUMINATSDR AC2A20210221002Indicator · crackedINLET BARRIER FILTER MAINTENANCE INDICATOR AID FOUND CRACKED DURING INSPECTION.SDR AC2A20210221001Indicator · crackedINLET BARRIER FILTER MAINTENANCE INDICATOR AID FOUND CRACKED DURING INSPECTION.SDR IPXA2021022366029Angle · crackedINSPECTION TYPE:S/V#2 ENGINE INLET LOWER VERTICAL STABILIZER REAR SPAR FIRE SEAL ZEE EXTRUSION IS CRACKED.REPAIRED CRACKED #2 ENGINE INLET LOWER VERTICAL STABILIZER REAR SPAR FIRE SEAL ZEE EXTRUSION IAW VT-SAA EA 011-5530-01-A8878 REV. I/R AND UPS EO MD11-5530SDR R61A2021021900163Inlet · crackedRIGHT ENGINE AIR INLET PANEL 421DR MIDDLE FIN IS CRACKED ON EXHAUST OUTLET GRATE. RT ENGINE AIR INLET PANEL 421DR MIDDLE FIN ON EXHAUST OUTLET GRATE REPAIRED IAW ETD2021-170-003531.SDR MK1Y01132021010Inlet · dentedDURING MAINTENENCE INSPECTION FOUND A DENT WITH CREASE AT ENGINE NR 2 INLET COWL INNER BARREL.SDR IPXA2021012464823Angle · crackedINSPECTION TYPE: S/V NR 2 ENGINE INLET LOWER VERTICAL STABILIZER REAR SPAR FIRE SEAL ZEE EXTRUSION IS CRACKED. REMOVED, FABRICATED AND REPLACED CRACKED NR 2 ENGINE INLET LOWER VERTICAL STABILIZER REAR SPAR FIRE SEAL ZEE EXTRUSION, IAW VT-SAA EA 011-5530-01-A8SDR UIEA2021011200038Inlet · damagedNR 1 INLET COWL HAS A SMALL DAMAGE AT 5:00 POS TAIL. ACCOMPLISHED PERMANENT HOT BOND COMPOSITE REPAIR OF NR 1 INLET COWL AT 5 O'CLOCK POSITION, PER AVENIR AVIATION FAA CAS 8AVR479B WO W15287 FEAM RO 5002395 FAA FORM 8130-3 ATTACHED.SDR DALA2021010400017Skin · dentedDENT SKIN AIR INTAKE LIP ON ENGINE 1. CORRECTIVE ACTION: EVALUATED DENT AND FOUND WITHIN LIMITS, AS PER A320 SRM 64-10-00 PAGE 107, FIGURE 102 AND ITEM 5, PAGE 118 AND MONITOR CONDITION DENT ZONE CL2 AT 750 FLIGHT HOURS/750 FLIGHT CYCLES/4 CALENDAR MONTHS.SDR UIEA2020121502569Liner · delaminatedNR 1 ENGINE INLET AT POSITION 4 O'CLOCK ACOUSTIC PANEL FOUND DELAMINATED. REMOVED AND REPLACED DAMAGED ACOUSTIC PANEL LINER AT NR 1 ENGINE INLET AT POSITION 4 O'CLOCK, PER B767-300 AMM 72-33-01-004-001-H00 AMM 72-33-01-004-011-H00.SDR IPXA2020112162625Rivet · looseINSPECTION TYPE: 4C NR 2 ENGINE INLET NOSE COWL LIP HAS NUMEROUS LOOSE AND WORKING RIVETS. REPAIRED NR 2 ENGINE INLET NOSE COWL LIP LOOSE AND WORKING RIVETS, IAW VT-SAA EA 011-7110-01-A8735 REV IR AND UPS EO MD11-7110-78559-A. (MINOR)SDR 2022FA0000577Screen · damagedTOTAL HOURS ON PART IS 193.0. DURING 100 HR. / ANNUAL INSPECTION FOUND AFT SCREEN FOR INDUCTION FILTER MISSING. SMALL PARTS FOUND STUCK TO ELEMENT. FOUND LARGE SECTION IN #4 INDUCTION TUDE. FOUND SMALL PARTS STUCK TO EXHAUST TAIL PIPE. THIS ACCOUNTED FOR APPRO
Back to JASC 7160