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 ASAA2018062725224Fastener · missingNR 2 ENGINE INBD STRUT FAIRING HAS MISSING HARDWARE ON LOWER SIDE 9OCLOCK POSS. GROUNDED - YES. INSTALLED MISSING SCREW FOR STRUT FAIRING AT 9 O'CLOCK POSITION, REF AMM 72-23-02.SDR ASAA2018062525195Seal · damagedWHILE ACCOMPLISHING TASKCARD 78472000, FOUND OUTLET GUIDE VANE AT AROUND THE 4 O CLOCK POSITION ( FORWARD LOOKING AFT) WITH A DAMAGED BASE SEAL. GROUNDED - YES. REMOVED AND REPLACED OUTLET GUIDE VANE SEAL AT AROUND THE 4 O CLOCK POSITION REF AMM 72-23-01.SDR ASAA2018062505173Blade · damagedNR 2 ENGINE FAN BLADES 2 AND 24 ROOT DOVE TAIL CU-NI-IN COATING OUT OF LIMITS . NO DAMAGE ON BASE METAL . ACFT GROUNDED. REMOVED AND REPLACED THE FAN BLADES 2 AND 24 IAW TASK CARD 78472002.SDR ASAA201806255174Panel · looseFOUND FAN DUCT PANELS AT THE 6 AND 3 O`CLOCK POSITIONS TO BE LOOSE. ACFT GROUNDED. TIGHTENED FASTENERS ON FAN DUCT PANELS IAW AMM 72-23-07. PANELS ARE SECURE.SDR ASAA201806255175Spacer · debondedNR 1 ENGINE HAD EIGHT DEBONDED FAN BLADE SPACERS. ACFT GROUNDED. REPLACED THE FAN BLADE SPACERS IAW TC 78472002.SDR ASAA2018062125153Panel · damagedWHILE ACCOMPLISHING TC 78472000 NR 2 ENGINE S/N 963292 FOUND FAN DUCT PANEL NR 12 AFT O/B FASTENER PULLED THRU PANEL. GROUNDED - YES. REMOVED NR 2 ENGINE REF T/C 78471000 FOR ACCESS TO FAN DUCT PANEL NR 12 INSERT REPLACEMENT. REMOVED AND REPLACED KEY-LOCKED INSDR ASAA2018062105143Shim · damagedNR 1 ENGINE SHIMS 13 & 14 MISSING BASE MATERIAL. ACFT GROUNDED. REPLACED THE SHIMS IAW T/C 78472002.SDR ASAA2018061825144Seal · wornDURING NR 1 ENG FAN BLADE LUBRICATION, PLATFORMS ELASTOMER SEALS WERE WORN BEYOND LIMITS, MORE THAN 39.39 INCHES. ACFT GROUNDED. ALL BLADE PLATFORMS WERE REPLACED IAW T/C 78472002.SDR ASAA2018061985118Blade · wornDURING NR 2 ENGINE FAN BLADE LUBRICATION. FOUND NR 1 FAN BLADE MISSING CU NI IN COATING ON CONCAVE SIDE, AFT END IS BEYOND LIMITS. BLADE NR 13 TO BE CHANGED AS A PAIR WITH BLADE NR 1. ACFT GROUNDED. REPLACED THE 1 & 13 FAN BLADES IAW T/C 78472002.SDR ASAA2018061875088Bolt · wornDURING T/C 78472002 OF THE NR 2 ENGINE FRONT SPINNER CONE HAD SIX BOLT THREADS WORN. GROUNDED. REMOVED AND REPLACED THE BOLTS IAW AMM 72-21-01-400-801-F00.SDR ASAA2018061625087Blade · damagedDURING ACCOMPLISHMENT OF T/C 78472002 ON THE NR 2 ENGINE, FOUND BLADES 1, 13, 16, 17, 19, 23, AND 24 CU-NI-IN COATING DAMAGED BEYOND LIMITS. ACFT GROUNDED. INSTALLED NEW FAN BLADES IAW T/C 78472002.SDR ASAA2018061525092Spacer · debondedDURING ACCOMPLISHMENT OF T/C 78472002, FOUND 15 FAN BLADE SPACERS DEBONDED ON THE NR 1 ENGINE. ACFT GROUNDED. REMOVED AND REPLACED THE SPACERS IAW T/C 78472002.SDR ASAA2018061525091Blade · wornWHILE ACCOMP T/C 78472002, FOUND CU-NI - IN COATING ON BLADE 20 ON THE NR 1 ENGINE FAN, WORN OUT OF LIMITS. ACFT GROUNDED. REMOVED AND REPLACED THE BLADE PAIR IAW T/C 78472002 AND AMM 72-21-02.SDR ASAA2018061855090Blade · wornWHILE ACCOMPLISHMENT OF T/C 78472002, FOUND CU-NI-IN COATING ON BLADE 21 OF THE NR 1 ENGINE WORN, OUT OF LIMITS. ACFT GROUNDED. REMOVED AND REPLACED THE BLADE PAIR 9 AND 21 IAW T/C 78472002, AND AMM 72-21-02.SDR ASAA2018061855089Shim · distortedDURING T/C 7842002, FOUND SHIMS 1 THROUGH 24 HAD SIGNS OF AXIAL RETENTION DISTORTION MORE THAN 0.04 X 0.04 INCH ON THE NR 1 ENGINE. ACFT GROUNDED. REPLACED THE SHIMS IAW T/C 7872002.SDR ASAA2018061855086Blade · nickedDURING T/C 78472002 ON THE NR 1 ENGINE, FOUND PLATFORMS NR 5, 16, 18, 19, & 20 WITH NICKS ON AREA B. ACFT GROUNDED. REPLACED THE NR 1 ENGINE PLATFORMS IAW T/C 78472002.SDR ASAA2018061225065Paint · missingWHILE ACCOMPLISHING FAN BLADE LUBE ON NR 1 ENG T/C 78472002, FOUND FRONT SPINNER WITH MISSING PAINT. GROUNDED - YES. ON DEFERRAL.SDR ASAA2018061225044Shim · wornWHILE ACCOMPLISHING FAN BLADE LUBE T/C 78472002, ON NR 1 ENGINE FOUND ALL SHIMS WORN INTO PARENT MATERIAL. GROUNDED - YES. REMOVED AND REPLACED ALL FAN BLADE SHIMS ON NR 1 ENGINE, REF AMM 72-21-02/401.SDR ASAA2018061125033Spinner · damagedNR 2 ENGINE FRONT SPINNER CONE HAS DAMAGED THREADED INSERT AND TOOLING MARKS. GROUNDED - YES. REMOVED AND REPLACED FRONT SPINNER CONE REF TASK CARD 78472002.SDR ASAA2018061195007Blade · damagedIAW T/C 78412002, NR 2 ENGINE FAN BLADE LUBRICATION, NUMBERS 17, AND 18 BLADES CU-NI COATING WAS MISSING BEYOND LIMITS. ACFT GROUNDED. REMOVED AND REPLACED THE FAN BLADES.SDR ASAA2018061195006Blade · damagedIAW T/C 78472002, THE NR 2 ENGINE FAN BLADE LUBRICATION, NUMBERS 3, 7, AND 15 BLADES CU-NI COATING MISSING BEYOND LIMITS. ACFT GROUNDED. REMOVED AND REPLACED THE FAN BLADES IAW TC 78472002.SDR ASAA2018060724970Shroud · damagedWHILE ACCOMPLISHING TC 78472000 NR 2 ENGINE FOUND ABRAIDABLE SHROUD CRATER AND SHOWING PARENT METAL AT 12 O’CLOCK POSITION. PARENT METAL HAS NO DEFECTS. GROUNDED - YES. ACCOMPLISHED RECONDITION OF THE ABRAIDABLE SHROUD PER AMM 72-24-02-200-802-F00. THIS CLEARSSDR ASAA2018060624947Shroud · damagedDURING ACCOMPLISHMENT OF T/C 78472002, FOUND A PORTION OF ABRADABLE SHROUD DAMAGED AT THE 11:00 POSITION. ACFT GROUNDED. ACCOMPLISHED ABRADABLE SHROUD RECONDITION IAW AMM 72-24-02-802-F00.SDR ASAA2018060624946Seal · debondedDURING ACCOMPLISHMENT OF T/C 78472002, FOUND 21 PLATFORMS WITH DISBONDED ELASTORMER SEALS ON THE NR 2 ENGINE. ACFT GROUNDED. REPLACED THE PLATFORMS IAW T/C 78472002.SDR ASAA2018060764945Stop Pin · damagedDURING ACCOMPLISHMENT OF T/C 78472002, ON THE NR 2 ENGINE, FOUND THE ELASTOMER STOP PINS ON THE RETAINING FLANGE DAMAGED. ACFT GROUNDED. REPLACED THE ELASTORMER STOP PINS.SDR ASAA2018060764944Blade · damagedDURING THE ACCOMPLISHMENT OF T/C 78472002, ON THE NR 2 ENGINE, FOUND THEN NR 7 FAN BLADE AFT SHANK CU-NI COATING DAMAGE BEYOND LIMITS ON CONCAVE SIDE. ACFT GROUNDED. REPLACED THE NR 7 AND 19 BLADES.SDR ASAA2018060534913Blade · debondedDURING NR 2 ENGINE FAN BLADE LUBRICATION, FOUND THE NR 18 PLATFORM RUBBER SEAL ON THE CONVEX SIDE, MORE THAN 3/4 OF IT`S LENGTH WAS DISBONDED. ACFT GROUNDED. REMOVED AND REPLACED THE NR 18 PLATFORM IAW TC 78472002.SDR ASAA2018060324901Blade · damagedNR 1 ENG FAN BLADES NR 24, 19, 10, 9, 5, AND 4 HAS CU-NI-IN DAMAGE OUT OF LIMITS. AND THE NR 1 BLADE ROOT DAMAGED FROM SHIM CONTACT OUT OF LIMITS. ACFT GROUNDED. REPLACED THE BLADE PAIRS IAW TC 78472002 ON THE NR 1 ENGINE.SDR ASAA2018060434900Seal · missingNR 1 ENGINE FAN BLADE PLATFORMS NR 18,16, 15, 10, 8, 6,5 SEALS MISSING. ACFT GROUNDED. REPLACED THE FAN BLADE PLATFORMS SEALS IAW T/C 78472002.SDR ASAA2018060324899Spinner · damaged#1 ENG FRONT SPINNER PAINT COATING WORN. GROUNDED - YES. REPLACED THE #1 ENG FRONT SPINNER PER T/C 78472002.SDR ASAA2018060224898Blade · damagedWHILE ACCOMPLISHING T/C 78472002 ON THE NR 2 ENGINE STEP 34. FOUND FAN BLADE 14 MISSING CU-NI-IN COATING OUT OF LIMITS. ACFT GROUNDED. REMOVED AND REPLACED THE NR 14 AND 2 FAN BLADES IAW TC 78472002.SDR IPXA2018061330626Inlet · crackedINSPECTION TYPE:2C, NR 2 ENG INLET L/E SKIN IS CRACKED AT THE 6 O'CLOCK POSITION. STOP DRILLED CRACK AND WELD REPAIRED PER SRM 54-10-01 REPAIR 4 /DPS10.301. (MINOR)SDR ASAA2018060424897Seal · damagedDURING FAN LUBE OF THE NR 1 ENGINE, FOUND PLATFORMS ELASTOMER SEALS DAMAGED, MORE THAN 39.37 INCH. ACFT GROUNDED.SDR ASAA2018060424895Case · crackedWHILE ACCOMPLISHING T/C 78472000, FOUND THE NR 1 ENGINE FAN CASE FLANGE CRACKED FWD ATTACH POINT OF FIRE OVERHEAT DETECTOR BRACKET AT 11;30 O`CLOCK. ACFT GROUNDED. THE NR 1 ENGINE FAN CASE FLANGE WORKED ON TC SBCFM56-7B-72-0580-1. INSTALLED. OPS CHECKED GOSDR ASAA2018060124875Cone · wornWHILE ACCOMPLISH T/C 78472000 FRONT CONE SPINNER BLACK ANODIZED COATING IS MISSING MORE THAN 50 PERCENT #1 ENGINE. ACFT GROUNDED. REPLACED THE CONE IAW. AMM 72-21-01.SDR ASAA2018060424896Shim · damagedWHILE ACCOMPLISHING FAN BLADE LUBE ON THE NR 2 ENGINE. FOUND THE COATING MISSING ON ALL SHIMS. NO WEAR TO BASE MATERIAL. ACFT GROUNDED.SDR SIMA20180529005Retainer · damagedNR 1 ENGINE LP VIBRATION INDICATED AMBER AND 4.0. ABNORMAL INDICATION REMAINED AFTER COMPLYING WITH APPROPIATE CHECKLISTS, INCLUDING A REDUCED THRUST SETTING. REPLACED NR 1 ENGINE FAN BLADES IAW EA72-00-00-011, OPS CHECKED GOOD. REPLACED THE NR 1 ENGINE FANSDR ASAA2018052824828Panel · damagedNR 1 ENGINE INLET AND FAN BLADES, DETAILED INSPECTION FOUND ONE LOOSE FASTENER ON THE LOWER OTBD SIDE, AT THE 3 O'CLOCK POSITION. STRUT FAIRING PANEL APPEARS TO BE DAMAGED FROM LOOSE FASTENER. ACFT GROUNDED. REMOVED DAMAGED STRUT FAIRING PANEL. INSTALLED NEWSDR ASAA2018052954827Panel · looseDURING T/C 78472000 ACCOMPLISHMENT, FOUND THE NR 7 FAN DUCT PANEL WAS LOOSE. ACFT GROUNDED. TIGHTENED THE FASTENERS IAW AMM 72-23-07. THE FAN DUCT PANEL WAS SECURE.SDR ASAA2018052324772Spacer · debondedWHILE ACCOMP T/C 78472002 FAN LUBE/INSPECTION NR 1 ENG S/N 894549 FOUND 2 EACH BLADE SPACERS WITH DISBONDED ELASTOMER. GROUNDED - YES. INSTALLED SERVICEABLE REPLACEMENT FAN BLADE SPACERS IN CONJUNCTION WITH IN PROGRESS NR 1 ENGINE FAN LUBE TASK CARD 78472002 USDR ASAA2018052324771Seal · tornWHILE ACCOMP T/C 78472002 FAN LUBE/INSP ON NR 1 ENG S/N 894549 FOUND ALL PLATFORMS HAD TORN/DAMAGED ELASTOMER SEALS OVER 38 INCHES. GROUNDED - YES. INSTALLED SERVICEABLE REPLACEMENT FAN BLADE PLATFORMS IN CONJUNCTION WITH IN PROGRESS NR 1 ENGINE FAN LUBE TASK SDR ASAA2018052224748Spacer · debondedWHILE ACCOMPLISHING TC 78472002, FOUND NR 2 ENG FAN BLADE SPACERS NR 3 AND NR 11 DISBONDED. GROUNDED - YES. REMOVED AND REPLACED NR 3 AND NR 11 FAN BLADE SPACERS ON NR 2 ENGINE IAW MTX TASK CARD 78472002 (CFM56-7 FAN BLADE LUBRICATION).SDR ASAA201805214708Elastomer · damagedIAW T/C 78472002, NR 2 ENG STEP 32, PLATFORM LOCATION 2, 8, 12, 13, 14, & 17 HAD MISSING, TORN OR UNBONDED ELASTOMERS. ACFT GROUNDED. REMOVED & REPLACED THE PLATFORMS IAW AMM 72-21-00 AND T/C 78472002.SDR ASAA201805214706Blades · damagedIAW T/C 78472002, NR 2 ENGINE STEP 29 BLADES NR 1, 8, 13, 14, 15, 17, 18, 19, AND 20, HAVE MISSING CU-NI-IN COATING BEYOND LIMITS ON THE CONVEX SIDE. BLADES 6, 15, & 16 HAVE MISSING CU-NI-IN COATING BEYOND LIMITS ON THE CONCAVE SIDE. NR 2 BLADE CU-NI-IN COATINSDR ASAA201805184685Blade · damagedWHILE ACCOMP T/C 78472002, FOUND ELASTOMER DAMAGE TO ALL PLATFORMS BEYOND MM LIMITS. ACFT GROUNDED. NEW PLATFORMS INSTALLED IAW CARD 78472002, SUB TASK 839-045.SDR ASAA201805184684Blade · damagedWHILE ACCOMP T/C 78472002, FOUND 10 PAIRS OF BLADES WITH CU-N1 COATING DAMAGED BEYOND Y DIMENSION LIMITS. ACFT GROUNDED. REPLACED THE FAN BLADE SETS IAW AMM 72-21-02-900-801-F00.SDR ASAA2018051184683Shim · wornWHILE ACCOMPLISHING FAN BLADE LUBE ON THE NR 2 ENGINE IAW T/C 78472002, FOUND ALL SHIMS WORN INTO PARENT MATERIAL. ACFT GROUNDED. REPLACED THE SHIMS.SDR ASAA201805184682Spinner · damagedWHILE ACCOMPLISHING FAN BLADE LUBE ON THE NR 2 ENGINE IAW T/C 78472002, FOUND THE SPINNER DAMAGED ON THREADS FOR TACK BOLT, AND MISSING PAINT. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENG SPINNER CONE IAW AMM 72-21-01-000-801-F00 STEP 2F(1), AND 72-21-0SDR ASAA201805164647Blade · damagedDURING A FAN BLADE LUBRICATION ON THE NR 2 ENGINE. FOUND THE NR 3 BLADE CU-NI-IN COATING MISSING BEYOND LIMITS. ACFT GROUNDED. REMOVED AND REPLACED THE NR 3 AND 15 FAN BLADES IAW T/C 78472002.SDR ASAA201805164646Seal · missingDURING FAN BLADE LUBRICATION ON THE NR 2 ENGINE. ALL 24 PLATFORMS WERE MISSING RUBBER SEALS BEYOND TOTAL LIMITS. ACFT GROUNDED. REMOVED AND REPLACED THE PLATFORMS IAW T/C 78472002.
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