JASC 7220
Service difficulty reports · 1,721
Reports filed under 7220 · Turbine Engine Air Inlet Section, 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 = '7220' 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 = '7220' 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 ASAA2017022119899Flange · looseWHILE ACCOMPLISHING NR 1 ENGINE INLET & FAN BLADE INSPECTION, FOUND TEST PORT FLANGE TO FAN CASE LOOSE BETWEEN FLANGE B6 AND B7, AT 11 O'CLOCK. ACFT GROUNDED. REMOVED, CLEANED, AND REINSTALLED TEST PORT BOSS IAW ENGINE SUPPLEMENTAL MANUAL 72-23-31.SDR IPXA2017030514720Fastener · missingINSPECTION TYPE: 2C, NR 2 ENGINE INLET COWL HAS A MISSING FASTENER. INSTALLED THE FASTENER IAW EA 011-7110-01-A6677, REV. I/R AND UPS EO MD11-7110-63395-A.SDR ASAA2017021319801Panel · crackedFOUND TWO CRACKS ON FWD FASTENER HOLES AT AFT ENDS (L/H & R/H) OF 12 O'CLOCK POS STRUT FAIRINGS BLACK PLASTIC OTBD END FILLER. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENG POST STRUT FAIRING PROFILE PANEL. SECURED IAW AMM 72-23-02.SDR ASAA2017020919770Fastener · pulledWHILE ACCOMPLISHING A NR 2 ENGINE INLET AND FAN BLADE INSPECTION IAW T/C 78472000, FOUND THE NR 1 FAN DUCT PANEL WITH A FASTENER PULLED THRU. ACFT GROUNDED. REMOVED AND REPLACED THE DAMAGED KEY LOCK INSERT AT THE NR 2 ENGINE INLET, NR 1 FAN DUCT PANEL FASTSDR ASAA2017020819747Shim · wornNR 1 ENGINE ALL FAN BLADE SHIMS WORN IAW T/C 78472002. ACFT GROUNDED. REMOVED AND REPLACED THE SHIMS IAW T/C 78472002.SDR UIEA2017020200143Spinner · crackedON WALKAROUND, FOUND NR 1 ENGINE SPINNER CAP CRACKED ON SEVERAL OF THE FLANGE SURFACES (<P>REMOVED AND REPLACED FORWARD SPINNER CAP IAW B767 AMM 72-51-01 TORQUE CHECKS GOOD </P>)SDR ASAA2017020119638Case · crackedNR 1 ENGINE FAN INLET CASE HAS CRACK AT B1 FLANGE 11:30 O'CLOCK AFT LOOKING FWD AT FIRE DETECTOR BRACKET. ACFT GROUNDED. COMPLETED REWORK OF FAN CASE REF TASK CARD SBCFM56-7B ASA 36205.SDR ASAA2017012919588Shim · wornALL NR 2 ENGINE FAN BLADE SHIMS WORN. GROUNDED - YES. REMOVED AND REPLACED ALL 32 ENGINE FAN BLADE SHIMS, REF T/C 78472002.SDR ASAA2017012819574Bolt · missingBOLT MISSING FROM NR 1 ENGINE FORWARD SPINNER CONE. ACFT GROUNDED. PERFORMED CONDITIONAL INSPECTION OF NR 1 ENGINE, FOUND NO EVIDENCE OF PARTS ENTERING ENGINE IAW AMM 71-00-00-800-802-F00 AND 05-51-59-200-801. REPLACED THE BOLT IAW AMM 72-21-01.SDR HALA2017012600017Blade · bentRIGHT ENGINE FAN BLADE DAMAGED, THE TIP IS BENT AND APPEARS TO BE HITTING RUB STRIP. THE RUB STRIP FOUND DAMAGED AND A BIG PIECE AT 6:00 MISSING. RT ENG FAN BLADE REMOVED AND BLENDED AS REQUIRED. READY FOR INSTALL. THE ACOUSTIC LINEAR WAS REPAIRED.SDR ASAA2017012519552Shim · wornNR 2 ENGINE ALL 24 FAN BLADE SHIMS WORN. ACFT GROUNDED. REMOVED AND REPLACED THE FAN BLADE SHIMS IAW T/C 78472002.SDR ASAA2017012319526Shim · wornNR 1 ENGINE FAN BLADE SHIMS WORN. ACFT GROUNDED. REMOVED AND REPLACED NR 1 ENGINE FAN BLADE SHIMS IAW TASK CARD 78472002 .SDR ASAA2017012019494Spinner · erodedENG NR 2 FRONT CONE. SPINNER BLACK ANODIZED COATING AND WHITE ANTI-EROSION PAINT IS MISSING. GROUNDED - YES. REMOVED AND REPLACED NR 2 FRONT CONE SPINNER REF AMM 72-21-01.SDR ASAA2017012019493Spinner · erodedENG NR 1 SPINNER FRONT CONE BLACK ANODIZED COATING AND WHITE ANTI-EROSION PAINT IS MISSING. GROUNDED - YES. REMOVED AND REPLACED ENG NR 1 SPINNER FRONT CONE REF AMM 72-21-01.SDR ASAA2017011919492Blade · chippedON PERFORMING T/C 78472002 FOUND NR 2 ENG BLADES POSITION 2,3,12,17,23,24 CU-NI COATING IN AREA Y CHIPPED. GROUNDED - YES. ON DEFERRAL.SDR ASAA2017011919491Seal · missingNR 2 ENGINE 24 PLATFORMS MISSING SEALS. GROUNDED - YES. REPLACED PLATFORMS (24EA) ON NR 2 ENG PER T/C 78472002.SDR ASAA2017011719490Balance Weight · out of adjustNR 1 ENGINE TREND DATA SHOWS LOW PRESSURE ROTOR VIBRATION LEVELS TO BE TRENDING HIGHER THAN EXPECTED AFTER LAST FAN MAINTENANCE. GROUNDED - YES. ACCOMPLISHED AMM TASK 71-00-00-750-808-F00 TEST 14B. BALANCE WEIGHTS 24 P12 CHANGED TO P14, 28 P12 CHANGED TO P14, SDR ASAA2017011419384Shim · wornPER TASK CARD 78472002, REPLACEMENT OF FAN BLADE SHIMS (24) TWENTY-FOUR REQUIRED. GROUNDED - YES. REMOVED AND REPLACED (24)TWENTY FOUR SHIMS PER MAINTENANCE TASK CARD 78472002 STEP 23, WITH P/N 340-252-307-0.SDR IPXA2017020313658Inlet · gougedINSPECTION TYPE: 3C, NR 2 ENGINE INLET INNER SKIN HAS GOUGES AT THE 10:30 POSITION. REPAIRED IAW EA 011-5430-01-A6610 REV. I/R AND EO MD11-7110-63154-A.SDR ASAA2017010919290Shim · wornFOUND 24 FAN BLADE SHIMS WORN ON NR 1 ENGINE. ACFT GROUNDED. REMOVED AND REPLACED THE SHIMS IAW T/C 78472002.SDR ASAA2016123119224Shim · wornNR 2 ENGINE FAN BLADE SHIMS WORN (24 EA) GROUNDED - YES. REMOVED AND REPLACED NR 2 ENGINE FAN BLADE SHIMS (24 EA) REF T/C 78472002.SDR ASAA2016122919227Elastomer · wornNR 2 ENGINE, S/N-895170, PLATFORM ELASTOMERS WORN OUT OF LIMITS. GROUNDED - YES. REMOVED AND REPLACED 24 PLATFORMS ON THE NR 2 ENGINE PER T/C 78472002.SDR ASAA2016122919226Shim · wornNR 2 ENGINE FAN BLADE SHIMS WORN. GROUNDED - YES. REMOVED AND REPLACED ALL 24 FAN BLADE SHIMS ON NR 2 ENGINE PER T/C 78472002.SDR ASAA2016122919225Acoustic Panel · delaminatedNR 2 ENGINE, S/N 895170, NR 5 ACOUSTIC PANEL FWD EDGE IS DELAMINATED. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENGINE AFT ACOUSTIC PANEL AT NR 5 STRUT.SDR ASAA2016122619166Shim · lack of lubeRIGHT ENGINE HAD A CONSISTENT VIBRATION READING OF BETWEEN 2.0-2.4 UNITS DURING CRUISE FLIGHT. ACFT GROUNDED. COMPLETED FAN BLADE LUBE IAW T/C 78472002. ALL PLATFORMS AND SHIMS WERE REPLACED. VIBRATION LEVELS WITHIN LIMITS.SDR KO0R201612160128Inlet · corrodedNR 2 ENGINE INLET DUCT PLATING IS CORRODED AT YID 279.443, ZID -44.00, XID 0.00 TO 9.5, POSITION 6 O'CLOCK.SDR ASAA2016121519068Spinner · gougedDURING ACCOMPLISHMENT OF TC 78472002 FOUND NR 2 ENG FWD SPINNER GOUGED. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENG FWD SPINNER. REF TASK CARD 78472002.SDR ASAA2016121219024Panel · damagedNR 1 ENGINE INLET AND FAN BLADE DETAILED INSPECTION FOUND STRUT PANEL NR 5 AT 5 O'CLOCK POSITION HAS ONE AFT INBD INSERT DELAMINATED FROM PANEL. ACFT GROUNDED. REMOVED AND INSTALLED A NEW STRUT PANEL NR 5 AT 5 O'CLOCK POSITION IAW AMM 72-23-07.SDR ASAA2016121119012Shim · wornREMOVED NR 1 ENGINE SHIMS WORN, REF T/C 78472002. GROUNDED - YES. REPLACED NR 1 ENGINE NEW SHIMS, REF T/C 78472002.SDR DALA2016121209817Liner · dentedLT ENG FAN CASE INTERIOR LINING BETWEEN FAN BLADES AND FAN EXHAUST GUIDE VANES FOUND 03EA DENTS AS MARKED. ERA 553433-14.SDR ASAA2016120818990Spacer · debondedFOUND THE ELASTOMER STRIP FOR NR 11 AND 23 SPACER UNBONDED, ACFT GROUNDED. REMOVED AND REPLACED THE SPACERS . ACCOMPLISHED TEST 7 VIBRATION SURVEY IAW AMM 71-00-00 PB501, NO FURTHER DEFECTS NOTED.SDR ASOA20161201006Carbon Seal · wornA/C WAS DESCENDING AT 12,000 FEET WHEN A STRONG SMELL OF ENGINE OIL FROM PACKS APPEARED FROM ENGINE NR 1 SMELL CAME FROM NR 1 ENGINE BLEED ONLY. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE CARBON SEAL IAW RRMM 72-25-25. OPS CHECK WAS GOOD AND VIBE CHECKS SDR ASAA2016112118788Fairing · crackedWHILE PERFORMING A BORESCOPE INSPECTION, FOUND 3 O'CLOCK STRUT FAIRING ON NR 1 ENGINE TO BE CRACKED ON LOWER SECTION. ACFT GROUNDED. REMOVED & REPLACED THE STRUT FAIRING.SDR ASMF201612008Fan · distortedDURING TRANSIT CHECK, IT WAS DETECTED IN THE RIGHT ENGINE DISTORTION AT FAN BLADE LEADING EDGE POSITION 2. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING DISTORTION AT FAN BLADE LEADING EDGE POSITION 2 IN THE RIGHT ENGINE WITH 2.0” OF RADIAL DISPLACEMENT, SDR ASAA2016110618583Shim · wornWHILE ACCOPLISHING T/C 78472002 FOR FAN BLADE LUBRICATION, FOUND THE FAN BLADE SHIM'S COATING TO WORN ON THE NR 1 ENGINE. ACFT GROUNDED. INSTALLED NEW FAN BLADE SHIMS IAW T/C 78472002. REPLACED ALL 24 FAN BLADE SHIMS ON THE NR 1 ENGINE.SDR ASAA2016092518127Seal · exposedNR 2 ENGINE NR 1 FAN BLADE RUBBER DAMPNER COMING OUT OF SPINNER. ACFT GROUNDED. TRIMMED THE FAN BLADE PLATFORM SEAL, REMOVED .5 OF SEAL FROM FWD EDGE OF PLATFORM. WITHIN LIMITS, IAW AMM 72-21-02.SDR ASMF201611012Fairing · crackedDURING RIGHT ENGINE 2 DAY CHECK, A BIRD STRIKE EVIDENCE WAS DETECTED AT RIGHT ENGINE AIR COOLER / OIL COOLER (ACOL). MAINTENANCE PERSONNEL PERFORMED THE BIRD STRIKE CONDITIONAL INSPECTION IAW AMM DMC B787-A-05-51-18-00A-280A-A, DETECTING BENT AND MISSING OF FISDR ASAA2016082917950Spacer · debondedNR 2 ENGINE TREND DATA SHOWS A SUDDEN INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS. DATA SCATTER INDICATES FAN LUBE AND HARDWARE INSPECTION REQUIRED. ACFT GROUNDED. PERFORMED FAN BLADE LUBE ON NR 2 ENGINE. FOUND FOUR SPACERS DEBONDED AT 6, 12, 14 & 15. RESDR ASAA2016082617823Cone · wornNR 2 ENGINE FRONT SPINNER CONE ANTI-EROSION COATING, ROTATION INDICATOR WORN. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE FRONT SPINNER CONE, IAW AMM 72-21-01-00-801-F00 STEPS 2E AND 2F(1) AND 72-21-01-400-801-F00 STEPS 3F(5) AND 3G.SDR ASAA2016082117773Shim · wornDURING NR 2 ENGINE FAN LUBE, FOUND ALL SHIMS WITH WORN COATING. ACFT GROUNDED. REPLACED THE SHIMS IAW T/C 78472002.SDR ASAA2016081417703Spinner · damagedNR 1 ENGINE FAN BLADE LUBRICATION. FOUND ONE INSERT FOR SPINNER CONE BAD. ACFT GROUNDED. REMOVED & REPLACED THE SPINNER CONE IAW TASK CARD 78472002.SDR ASAA2016080617630Elastomer · tornREF T/C 78472002, NR 2 ENGINE FAN BLADE PLATFORMS HAVE TORN, REMOVED ELASTOMER SEALS THAT TOTAL 44.1". ACFT GROUNDED. R & R 24 PLATFORMS ON NR 2 ENGINE IAW T/C 78472002.SDR ASAA2016080617629Elastomer · tornREF T/C 78472002,NR 2 ENGINE FAN RETAINING FLANGE AXIAL STOP PINS TORN, DAMAGED. ACFT GROUNDED. R & R NR 2 ENGINE FAN RETAINING FLANGE AXIAL STOP PINS IAW T/C 78472002 AND AMM 72-21-01-900-801-F00.SDR ASAA2016080617628Shim · wornREF T/C 78472002, NR 2 ENGINE FAN BLADE SHIMS WORN, QTY 24. ACFT GROUNDED. R & R FAN BLADE SHIMS IAW TASK CARD 78472002, NR 2 ENGINE.SDR ASAA2016080417632Shim · wornNR 2 ENGINE 24 FAN BLADE SHIMS AND ELASTOMERS REQUIRE REPLACEMENT. ACFT GROUNDED. REMOVED AND REPLACED THE FAN BLADE DOVETAIL SHIMS AND ELASTOMERS IAW T/C 78472002.SDR ASAA2016080417631Spinner · erodedNR 2 ENGINE FRONT SPINNER CONE HAS APPROXIMATELY 50 PERCENT OF BLACK EROSION PAINT MISSING, REQUIRES REPLACEMENT. ACFT GROUNDED. R & R NR 2 ENGINE FRONT SPINNER CONE ASSY, REF T/C 78472002.SDR ASAA2016072517508Shim · wornDURING FAN BLADE LUBRICATION ON NR 1 ENGINE, FOUND BLADE SHIMS WORN. ACFT GROUNDED. REMOVED AND REPLACED THE FAN BLADE SHIMS IAW T/C 78472002.SDR ASAA2016071717411Shim · worn24 BLADE SHIMS WORN. ACFT GROUNDED. REMOVED AND REPLACED THE BLADE SHIMS IAW TC 78472002.SDR ASAA2016071617394Shim · wornNR 2 ENGINE FAN BLADE SHIMS WORN, QUANTITY 24. ACFT GROUNDED. REMOVED AND REPLACED NR 2 ENGINE FAN BLADE SHIMS, QUANTITY 24, IAW T/C 78472002.SDR ASAA2016071317369Blade · damagedWHILE ACCOMPLISHING NR 2 ENGINE FAN BLADE LUBE T/C 78472002, FOUND MISSING THE COATING IN THE CONTACT AREA ON BLADES 3, 4, 8, 9, 10, 11, 12, 15, 16, 17, 19, AND 20. THE MISSING COATING WAS BEYOND LIMITS OF AREA X, BUT WITHIN LIMITS OF AREA Y. ACFT GROUNDED.
Back to JASC 7220