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 ASAA2016071317370Shim · wornWHILE ACCOMPLISHING NR 2 ENGINE FAN LUBE T/C 78472002, FOUND FAN BLADE SHIMS WITH WEAR TO BASE MATERIAL. ACFT GROUNDED. REPLACED ALL SHIMS FOR NR 2 ENGINE FAN BLADES IAW T/C 78472002.SDR ASAA2016071317368Shim · wornFAN BLADE SHIMS REQUIRE REPLACEMENT. 24 EACH REQUIRED. ACFT GROUNDED. REPLACED FAN BLADE SHIMS IAW T/C 78472002.SDR ASAA2016071217353Spinner · abnormalWHILE ACCOMPLISHING NR 2 ENGINE FAN BLADE LUBE IAW T/C 78472002, FOUND SPINNER FRONT CONE MISSING WHITE ANTI-EROSION PAINT. ACFT GROUNDED. REPLACED FRONT SPINNER PER T/C 78472002, FAN LUBE.SDR ASAA2016070917316Seal · tornNR 1 ENGINE OUTLET GUIDE VANES INNER SEALS AT 2:30 AND 11:30 O'CLOCK POSITIONS BOTH HAVE MISSING MATERIAL. ACFT GROUNDED. REMOVED AND REPLACED THE SEALS IAW AMM 72-23-01.SDR ASAA2016070717315Shim · wornNR 1 ENGINE 24EA. FAN BLADE SHIMS REQUIRE REPLACEMENT. ACFT GROUNDED. REMOVED AND REPLACED 24 EACH FAN BLADE SHIMS NR 1 ENGINE IAW TASK CARD 78472002.SDR ASAA2016070617286Spacer · damagedACCOMPLISHED TASK CARD 78472002, FOUND NR 2 ENGINE SPACERS NUMBERS 22, 21, 20, AND 19 DAMAGED. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE SPACERS IAW TASK CARD 78472002. ACCOMPLISHED ENGINE RUN IAW AMM 71-00-00-800-806 AND VIBRATION SURVEY IAW AMM 7SDR ASAA2016070317278Shroud · wornNR 2 ENGINE, F/O NOTED SOME SCRAPING OF FAN BLADES AGAINST INNER SHROUD DURING WALKAROUND. ACFT GROUNDED. ACCOMPLISHED VISUAL INSPECTION OF GROOVES & CIRCUMFERENTIAL DAMAGE, DETERMINED TO BE FAN BLADE RUB & FOUND TO BE WITHIN LIMITS IAW AMM 72-24-02-200-801-SDR ASAA2016070117239Case · crackedWHILE ACCOMPLISHING NR 2 ENGINE INLET INSPECTION T/C 7847100, FOUND FAN CASE FLANGE B-1 CRACKED AT 11 O'CLOCK LOOKING FWD AT BRACKET FOR FIRE DETECTOR TRANSPONDER. ACFT GROUNDED. REPAIRED FAN CASE B-1 FLANGE IAW T/C SBCFM56-7B-72-0580-1, OPS AND LEAK CHECKEDSDR ASAA2016063017206Shim · wornNR 2 ENGINE TREND DATA SHOWS VIBRATION LEVELS FROM THE LOW PRESSURE ROTOR TO GREATER THAN EXPECTED. DATA SCATTER INDICATES FAN LUBE REQUIRED. PER T/C 7847200 NR 2 ENGINE FAN BLADE SHIMS EXHIBIT MORE THAN 25% MOLYDAG COATING LOSS PER AMM 72-21-02-801 STEP L (1)SDR DALA2016062704947Attach Fitting · crackedCRACK AT INNER ATTACH FITTING ON RT ENGINE BULLET. STOP DRILL ACCOMPLISHED, CRACK WAS WELDED, WELDED AREA WAS BLENDED OUT AND STRESS RELIEVE WAS ACCOMPLISHED IAW ER/A 547807, REV ORIGINAL, FITTING WAS REMOVED AND REINTALLED IAW SRM 51-30-2.SDR ASAA2016061117009Shim · wornNR 1 ENGINE REQUIRES NEW FAN BLADE SHIM 24 EA. ACFT GROUNDED. R & R NR 1 ENGINE FAN BLADE SHIMS IAW T/C 78472002.SDR ASAA2016061117007Shim · wornREF TASK CARD 78472002, FAN BLADE SHIMS WORN ON NR 2 ENGINE. ACFT GROUNDED. R & R NR 2 ENGINE FAN BLADE SHIMS IAW TASK CARD 78472002.SDR ASAA2016060917008Panel · looseREF T/C 78472000, NR 1 ENGINE, 4-5 O`CLOCK AFT LOOKING FWD, LPTACC SCOOP FAN DUCT PANEL. AFT 2 FASTENERS ARE PULLED THROUGH PANEL. ACFT GROUNDED. R & R NR 1 ENGINE FAN DUCT PANEL, REF AMM 72-23-07.SDR ASAA2016052916885Inlet · looseREF T/C 78472000, NR 2 ENGINE INLET AND FAN BLADES, DETAILED INSPECTION. FOUND NR 3, NR 8, NR 9 STRUT PANEL, 3 AT 2 O`CLOCK POSITION, NR 8 AT 7 O'CLOCK POSITION, NR 9 AT 8 POSITION LOOSE. ACFT GROUNDED. RETORQUED NR 3, NR 8 ND NR 9 SRUT PANELS ON NR 2 ENGISDR ASAA2016052916884Blade · damagedREF T/C NR 2 ENGINE INLET AND FAN BLADES, DETAILED INSPECTION. FOUND NR 1 STRUT PANEL, RT SIDE OF 12 O'CLOCK POSITION HAS AFT INBD FASTENER HOLE DAMAGED. ACFT GROUNDED. R & R NR 1 STRUT PANEL AT NR 2 ENGINE REF AMM 72-23-02.SDR ASAA2016050916662Shim · worn2 ENGINE TREND DATA SHOWS A SUDDEN INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS. DATA SCATTER INDICATES FAN LUBE AND HARDWARE INSPECTION REQUIRED. ACFT GROUNDED. ACCOMPLISHED FAN LUBE AND REPLACED ALL SHIMS AND SPACERS REF T/C 78472002 NR 2 ENGINE. ACCOMPLSDR WX0A2016042973141Acoustic Panel · crackedDURING DAILY CHECK WALK AROUND, DISCOVERED CRACKED ACOUSTIC PANEL AT 12 - 2 O'CLOCK POSITION ON NR 2 ENG. R & R ACOUSTIC PANEL AT 12 - 2 O'CLOCK POSITION IAW AMM 72-23-00. ALL IS GOOD.SDR HALA2016042700143Fan · contaminatedFOUND OIL IN NR 2 ENGINE AFT OF FAN AT 6 OCLOCK. CLEANED OIL RESIDUE FROM ENGINE. RAN NR 2 ENGINE AT IDLE. LEAK CHECKS OK. OK FOR CONTINUED SERVICE.SDR ASAA2016042216504Shim · damagedNR 2 ENGINE FAN BLADE SHIMS MISSING MOLYDAG COATING. ACFT GROUNDED. REPLACED ALL 24 SHIMS, PN 340-252-307-0 ON NR 2 ENG REF T/C 78472002.SDR AALA20160418008Bullet · leakingAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER WAS DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB, OBSERVED AN EPR SPLIT BETWEEN NR 1 & 2 ENGS. FOUND PT2 LINE DISLODGED INSIDE OF BULLET ON NR 1 ENG. R & R BULLET IAW AMM 77-11-03. ACCOMPLISHED SDR ASAA2016041016341Case · crackedNR 2 ENGINE FAN CASE B1 FLANGE LUG CRACKED AT FIRE DETECTOR MOUNT. 11 O'CLOCK POSITION. ACFT GROUNDED. ACCOMPLISHED EA POWER PL-72EA-16945.SDR ASAA2016041016340Panel · delaminatedREF T/C 78472000, NR 1 ENGINE INLET AND FAN BLADES. DETAILED INSPECTION FOUND NR 5 FAN STRUT PANEL 5 O'CLOCK POSITION HAS 1 FASTENER INSERT DELAMINATED FROM PANEL, AFT OTBD FASTENER. ACFT GROUNDED. REPLACED NR 5 FAN STRUT PANEL AT 5 O'CLOCK POSITION, REF AMSDR ASAA2016040616265Bolt · looseNR 2 ENGINE FAN DUCT PANELS AT 5:00, 7:00 AND 8:00 POSITIONS HAVE LOOSE BOLTS, 3 EA PANELS, 1 EA BOLT AT LOCATION. ACFT GROUNDED. TIGHTENED BOLTS ON NR 2 ENGINE FAN DUCT PANELS 5, 7, AND 8 O'CLOCK POSITIONS, REF AMM 72-23-07.SDR ASAA2016040616264Blade · damagedWHILE ACCOMPLISHING NR 2 ENGINE FAN LUBE TC 78472002, ESN-894361 FOR TSR907910, FOUND RUBBER MISSING ON NR 4, NR 10, AND NR 7 PLATFORMS BOTH SIDES AND ALL SHIM COATINGS WORN. ACFT GROUNDED. R & R NR 2 ENGINE FAN BLADE PLATFORMS NR 4, NR 10, AND NR 7 AND ALL 2SDR ASAA2016040516252Shim · wornWHILE ACCOMPLISHING TASK CARD 78472002, FOUND MOLYDAG WORN ON ALL 24 FAN BLADE SHIMS. ACFT GROUNDED. REPLACED IAW TASK CARD 78472002 ALL 24 WORN SHIMS.SDR ASAA2016040416241Blades · lack of lubeNR 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. TASK CARD 78472002, FAN BLADE LUBRICATION ON NR 2 ENGINE ACCOMPLISHED. 24 SHIMS REPLACEDSDR ASAA2016030915812Fan · lack of lubeNR 2 ENGINE TREND DATA SHOWS A SUDDEN INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS. DATA SCATTER INDICATES FAN LUBE REQUIRED. ACFT GROUNDED. PERFORMED FAN LUBRICATION TC NR 78472002 AND REPLACED ALL FAN BLADE SPACERS ON NR 2 ENGINE IAW T/C 78472002. SPASDR ASAA2016022715673Fan · damagedAFTER T/O, NR 2 ENGINE HAD A MOMENTARY EGT EXCEEDENCE. ACFT GROUNDED. EGT PEAKED AT 960 FOR 6-05 SECONDS. PERFORMED A GVI OF NR 2 ENGINE. NO FAULTS NOTED. ACCOMPLISHED FIM 71-06, TASK 805, EGT PEAK TEMP FALLS WITHIN TABLE A. CREATED A PLT DEFERRAL FOR NRSDR ASAA2016021115430Spinner · wornREF T/C 78472002, NR 2 ENGINE FRONT SPINNER BLACK ANODIZED COATING WORN TO LIMITS. ACFT GROUNDED. R & R NR 2 ENGINE FRONT SPINNER REF T/C 78472002.SDR ASAA2016020315282Shim · wornDURING ACCOMPLISHMENT T/C 78472002 FAN BLADE LUBRICATION FOUND FAN BLADE SHIMS WORN TO LIMITS AT ENGINE NR 1. ACFT GROUNDED. R & R FAN BLADE SHIMS AT ENG NR 1, 24 EA IAW T/C 78472002.SDR ASOA2016020214510Inlet · erodedLEFT ENGINE INLET ERODED. COMPLIED WITH PERMANENT REPAIR OF LT ENGINE INLET IAW CMM 71-61-01. REPAIRED LT ING INLET EROSION IAW CMM TASK 71-61-01-300-822-A01.SDR ASAA2016012515005Blade · damagedDURING ACCOMPLISHMENT OF T/C 78472000 FOUND NICK ON NR 2 ENGINE 6 FAN BLADE. 14" FROM THE TIP. ACFT GROUNDED. BLEND REPAIRED IAW AMM 72-21-02 NR 2 ENGINE, NR 6 FAN BLADE, AREA B. PERFORMED FL OPEN INSPECTION REF AMM 70-40-01, NO DEFECTS.SDR ASAA2016011814871Blade · nickedNR 2 ENGINE, NR 8 FAN BLADE HAS A SHARP NICK ON L/E. ACFT GROUNDED. DAMAGE FOUND WITHIN AREA C, DEPTH .093 6" FROM TIP. ACCOMPLISHED FAN BLADE REPAIR REF AMM 72-21-02-300-801-F00 2.A THRU H. 4. PERFORMED FPI OF BLENDED AREA, NO RELEVENT INDICATIONS NOTED. RSDR ASAA2016011314770Shim · wornWHILE ACCOMPLISHING FAN BLADE LUBE ON NR 1 ENGINE FOUND SHIMS WORN AND SEVERAL RUBBER AXIAL BUMPERS WORN ON AFT SPINNER REF T/C 78472002. ACFT GROUNDED. R & R SHIMS AND RUBBER AXIAL BUMPERS FOR NR 1 ENGINE IAW FAN BLADE LUBE T/C 78472002.SDR ASAA2016010214619Shim · wornFOUND SHIMS WORN ON FAN LUBE, NR 1 ENGINE. ACFT GROUNDED. REPLACED ALL SHIMS ON NR 1 ENGINE. REF TASK CARD NR 78472002.SDR ASAA2016010214615Elastomer · missingFOUND 1 AXIAL STOP PIN MISSING ON FAN RETAINING FLANGE DURING FAN LUBE, NR 1 ENGINE. ACFT GROUNDED. REPLACED ALL AXIAL STOP PINS ON NR 1 ENGINE. REF TASK CARD NR 78472002.SDR ASAA2016010214614Seal · missingFOUND 2 PLATFORMS WITH 1 MISSING SEAL, EACH ON FAN LUBE, NR 1 ENGINE. ACFT GROUNDED. REPLACED PLATFORMS ON NR 1 ENGINE, REF TASK CARD NR 78472002.SDR ASAA2016010114618Shim · wornWHILE PERFORMING T/C 78472002 FAN BLADE LUBE ON NR 2 ENGINE FOUND FAN BLADE SHIMS WORN. ACFT GROUNDED. REPLACED, 24EA, FAN BLADE SHIMS, PN 340-252-307-0 ON NR 2 ENGINE IAW T/C 78472002, STEP 42.SDR ASAA2016010114613Insert · missingNR 2 ENGINE FRONT SPINNER CONE HAS ONE JACKSCREW THREADED INSERT MISSING. ACFT GROUNDED. REPLACED NR 2 ENGINE FRONT SPINNER CONE IAW AMM 72-21-01.SDR DALA2015123007757Hub · damagedNR 1 AND NR 2 ENGINE N1'S WENT TO 103 PERCENT FOR 7 SECS. DURING LOW ALTITUDE GO AROUND. REPLACED NR 2 ENGINE HUB IAW SPC 03-7201-9-0016. REPLACED NR 1 ENGINE HUB IAW SPC 03-7201-9-0016.SDR ASAA2015122414468Shim · wornIAW T/C 78472002 NR 1 ENGINE FAN BLADE LUBRICATION FOUND NR 18 BLADE SHIMS WORN. ACFT GROUNDED. R & R NR 18 BLADE SHIMS. SHIMS WERE REPLACED WITH THE SAME PN 340-252-307-0.SDR ASAA2015122414467Shim · wornREF T/C 78472002, FOUND SHIMS WORN ON NR 2 ENGINE, SN 962761. ACFT GROUNDED. SHIMS REPLACED AND INSTALLATION ACCOMPLISHED ON T/C 78472002. FAN BLADE LUBRICATION.SDR CA151214004Case · corroded(CAN) DURING PRELIMINARY INSPECTION OF THE FAN CASE (LEVEL 3 OVERHAUL) MINOR BULGING OF THE FAN TRACK LINING WAS NOTICED AT BOTTOM DEAD CENTER POSITION. IN ORDER TO DETERMINE THE ROOT CAUSE OF THIS BULGING, THE INSPECTOR HAS REQUESTED FOR REMOVAL OF THE AFFECTSDR ASAA2015112813997Panel · looseNR 2 ENGINE FAN DUCT PANEL AT 5:30 POSITION HAS 2 EA LOOSE BOLTS. ACFT GROUNDED. TIGHTEN NR 2 ENGINE FAN DUCT PANEL AT 5:30 POSITION BOLTS 2 EA REF T/C 7847200.SDR ASAA2015112513999Seal · missingNR 1 ENGINE FAN LUBE PLATFORMS MISSING 57" OF ELASTOMER SEAL. ACFT GROUNDED. R & R NR 1 ENGINE ALL PLATFORMS REF T/C 78972002.SDR ASAA2015112513996Acoustic Panel · damagedNR 1 ENGINE INLET AND FAN BLADES DETAILED INSPECTION. FOUND NR 5 FAN FRAME PANEL AT 5 O`CLOCK POSITION HAS 3 FASTENERS AND FASTENER INSERTS DAMAGED AND WORN. ACFT GROUNDED. R & R AFT FAN FRAME ACOUSTICAL PANEL AT 5 O`CLOCK POS REF AMM 72-23-02.SDR ASAA2015112413998Liner · crackedNR 1 ENGINE HAS CRACK IN THE LINER THAT SURROUNDS THE FAN BLADES. ACFT GROUNDED.SDR ASAA2015111913909Blade · wornWHILE ACCOMPLISHING FAN BLADE LUBE ON NR 1 ENGINE IAW TC 78472002, FOUND ALL SHIMS WORN. ACFT GROUNDED. R & R 24 EA SHIMS ON NR 1 ENGINE IAW TC 78472002, STEP 42.SDR ASAA2015111013718Shroud · crackedNR 1 ENGINE HAS 6" SECTION OF ABRAIDABLE SHROUD COMING LOOSE AT 5 O'CLOCK POSITION, LOOKING AFT; ABOVE NOTED SECTION HAS 1 CRACK STARTING AT AFT EDGE FORWARD 2" AND TURNING TOWARDS 6 O'CLOCK POSITION WITH L/E LIFTING UP. THE OTHER CRACK AT 6 O'CLOCK POSITIONSDR SIMA20151110001Pin · lack of lubeRIGHT AFTER TAKEOFF, RT ENG VIBRATION, N1 WENT TO 1.9. WE READ THE CHECKLIST AOM VOL 1 & INITIALLY WE WERE ABLE TO CONTROL THE VIBRATION TO 1.7, GREEN, BUT AS WE CLIMBED TO FL270 VIBRATION GOT WORSE UP TO 2.1, AMBER, & WE WERE NOT ABLE TO CONTROL IT WITH POWE
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