JASC 7220
Service difficulty reports · 1,719
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 ASAA2022041037944Engine · nonePER T/C # 7847200 #2 ENG NLET INSP PS13 BOSS AT FAN CASE IS LOOSE. GROUNDED - YES. REMOVED AFT ACOUSTICAL PANEL AT 10 O'CLOCK POSITION REF B737-800 AMM 72-23-02-000-801-F01. REMOVED LOOSE FASTENER. REF B737-800 SRM 51-40-02. FOUND DAMAGE UNDER BOSS, MAPPED DASDR ASAA2022040437914None · nonePER T/C 78472010 #2 ENG FAN BLADE LUBE #16 FAN BLADE CU-NI-IN COATING MISSING BEYOND LIMITS ON CV SIDE. GROUNDED - YES. INSTALLED NEW FAN BLADE #16, REF T/C 78472010 FAN BLADE LUBE.SDR ASAA2022040437913None · nonePER T/C 78472010 #2 ENG FAN BLADE LUBE #13 FAN BLADE CU-NI-IN COATING MISSING BEYOND LIMITS ON CV SIDE. GROUNDED - YES. INSTALLED NEW FAN BLADE #13 REF T/C 78472010 FAN BLADE LUBE.SDR ASAA2022040437912Blade · nonePER TC 78472010#2 ENG FAN BLADE LUBE #23 FAN BLADE CU-NI-IN COATING MISSING BEYOND LIMITS ON CV SIDE. GROUNDED - YES. INSTALLED NEW FAN BLADE #23 REF TC 78472010 FAN BLADE LUBE.SDR ASAA2022040437911Blade · nonePER T/C 78472010 #2 ENG FAN BLADE LUBE, FAN BLADES #1 AND #14 CU-NI-IN COATING MISSING BEYOND LIMITS ON LV AND CC SIDES. GROUNDED - YES. INSTALLED NEW BLADES #1 AND #14, REF T/C78472010 FAN BLADE LUBE.SDR ASAA2022040437910None · nonePER T/C 78472010 #2 ENG. FAN BLADE LUBE SPACERS # 1,2,3,5,10,12,18,22,23, AND 24 ARE DISBONDED. GROUNDED - YES. REMOVED AND REPLACED SPACERS 1,2,3,5,10,12,18,22,23,24 REF T/C 78472010.SDR ASAA2022040437909None · nonePER T/C 78472010 #2 ENG. FAN BLADE LUBE FAN BLADE #2 CU-NI. IN COATING MISSING BEYOND LIMITS ON CV AND CC SIDES. GROUNDED - YES. INSTALLED NEW FAN BLADE #2, REF 78472010 FAN BLADE LUBE.SDR ASAA2022040437908None · nonePER T/C 78472010 #2 ENG FAN BLADE LUBE #11 FAN BLADE CU-NI-IN COATING MISSING BEYOND LIMITS ON CV AND CC SIDE. GROUNDED - YES. INSTALLED NEW FAN BLADE #11 REF TC 78472010 FAN BLADE LUBE.SDR ASAA2022040437907None · nonePER T/C 78472010 #2 ENG FAN BLADE LUBE #4 FAN BLADE CU-NI-IN COATING MISSING BEYOND LIMITS ON CV SIDE. GROUNDED - YES. INSTALLED NEW FAN BLADE #4, REF TC 78472010 FAN BLADE LUBE.SDR ASAA2022033137858None · nonePER T/C 78472010 #1 ENGINE FAN BLADE LUBE, SPACERS #2,4,6,10,16, AND 24 ARE DISBONDED. GROUNDED - YES. REPLACED AFOREMENTIONED SPACERS REF TC 78472010.SDR ASAA2022033037850Spacer · abnormalWHILE ACCOMPLISHING FAN LUBE ON #2 ENG T/C #78472010, FOUND SPACERS #14 AND #19 UNUSUALLY DIFFICULT TO INSTALL. GROUNDED - YES. REMOVED AND REPLACED SPACERS #14 AND #19 ON #2 ENG PER T/C #78472010.SDR ASAA2022032837812Spacer · debondedPER T/C 78472012 #1 ENGINE FAN BLADE LUBE SPACERS #4 AND #8 ARE DISBONDED. GROUNDED - YES. R&R SPACER #4 AND #8 PER T/C 78472010.SDR ASAA2022032637795Spinner · abnormalWHILE ACCOMPLISHING T/C 78472010, #2 ENGINE INLET SPINNER FRONT CONE FOUND WITH MORE THAN 50% OF WHITE ANTI-EROSION PAINT MISSING. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE INLET SPINNER FRONT CONE PER T/C 78472010.SDR ASAA2022032337900Rotor · vibrates#1 ENGINE TREND DATA SHOWS INDICATION ERRORS HAVE BEEN RESOLVED. LOW PRESSURE ROTOR VIBRATION LEVELS CONTINUE TO BE HIGHER THAN DESIRED. GROUNDED - YES. ACCOMPLISHED B737-900 AMM TASK 71-00-00-750-808-F00 TEST 14B- FAN TRIM BALANCE. ACCOMPLISHED ENG #1 BALANCESDR ASAA2022032237757Spacer · worn#2 ENGINE TREND DATA SHOWS A RISE IN LOW PRESSURE ROTOR VIBRATION LEVELS. GROUNDED - YES. REPLACED 4 SPACERS AND COMPLIED WITH TASKCARD 78472010.SDR ASAA2022031037664Spacer · debondedPER T/C 78472010 #2 ENGINE FAN BLADE LUBE SPACERS #1/2/6/9/12/13 AND 19-23 ARE DISBONDED. GROUNDED - YES. REMOVED AND REPLACED #1,2,6,9,12,13,19 AND 19-23 SPACERS PER TASKCARD 78472010.SDR ASAA2022031037663Blade · damagedPER T/C 78472010 #2 ENGINE FAN BLADE LUBE #14 FAN BLADE CU-NI-IN COATING MISSING BEYOND LIMITS ON CV SIDE. GROUNDED - YES. REMOVED AND REPLACED #14 AND #2 FAN BLADES ON #2 ENG PER TASKCARD 78472010.SDR ASAA2022022037516Platform · delaminatedFOUND PLATFORMS DELAM1NATED/DETERIORATED #2 ENG. GROUNDED - YES. REMOVED AND REPLACED PLATFORMS AS REQUIRED #2 ENG REF T/C 78472010.SDR ASAA2022012637303Spinner · damaged#1 ENG FRONT SPINNER CONE IS MISSING MOST ALL OF ITS PAINT, OVER 50%. GROUNDED - YES. REMOVED AND REPLACED #1 ENG FRONT SPINNER CONE. REF B737-800 AMM 72-21-01.SDR ASAA2022012537259Blade · damagedPER T/C 78472010 #2 ENGINE FAN BLADE LUBE #23 FAN BLADE CU NI IN COATING MISSING BEYOND LIMITS CONCAVE SIDE. GROUNDED - YES. REPLACED #2 ENGINE FAN BLADE #23 PER T/C 78472010 (OPPOSITE BLADE #11 ALSO REPLACED FOR PAIRING).SDR ASAA2022012537258Platform · tornPER T/C 78472010 #2 FAN BLADE LUBE PLATFORMS #1,2,3,5,6,7,,9,10,10,20,23 AND 24 SEALS ARE TORN. GROUNDED - YES. REPLACED FAN BLADE PLATFORMS AT POSITIONS 1,2,3,5,6,7,9,10,19,20,23 AND 24, REF ASA T/C 78472010.SDR ASAA2022012537257Blade · damagedPER T/C 78472010 #2 ENGINE FAN BLADE LUBE #6 FAN BLADE CU NI IN COATING MISSING BEYOND LIMITS CONCAVE SIDE. GROUNDED - YES. REPLACED #2 ENGINE FAN BLADE #6, REF T/C 78472010 (OPPOSITE BLADE #18 ALSO REPLACED FOR WEIGHT PAIRING).SDR ASAA2022012537256Blade · damagedPER T/C 78472010 #2 ENGINE FAN BLADE LUBE #10 FAN BLADE CU NI IN COATING MISSING BEYOND LIMITS CONCAVE SIDE. GROUNDED - YES. REPLACED #2 ENGINE FAN BLADE #10 REF T/C 78472010 (OPPOSITE BLADE #22 REPLACE FOR WEIGHT PAIRING).SDR ASAA2022012537255Blade · damagedPER T/C 78472010 #2 ENGINE FAN BLADE LUBE #13 FAN BLADE CU NI IN COATING MISSING BEYOND LIMITS CONCAVE SIDE. GROUNDED - YES. REPLACED #2 ENGINE FAN BLADE #13 REF T/C 78472010 (OPPOSITE BLADE #1 REPLACED, ALSO FOR WEIGHT PAIRING).SDR ASAA2022012537254Blade · damagedPER T/C 78472010 #2 ENGINE FAN BLADE LUBE #19 FAN BLADE CU NI IN COATING MISSING BEYOND LIMITS CONCAVE SIDE. GROUNDED - YES. REPLACED #2 ENGINE FAN BLADE #19, REF T/C 78472010 (OPPOSITE BLADE # 7 ALSO REPLACED FOR WEIGHT PAIRING).SDR ASAA2022012037233Spinner · damagedPER T/C 78472010 # 1 ENG FAN BLADE LUBE FRONT SPINNER CONE WHITE ANTI-EROSION PAINT MISSING BEYOND LIMITS. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE FRONT SPINNER CONE REF AMM 72-21-01. SEAMC RAY NOTIFIED TERMINATING DEFECT NO, 60299724.SDR ASAA2022012037210Spacer · debondedPER T/C 78472010 #1 ENGINE FAN BLADE LUBE SPACERS # 3,8,9,10,11,16,19,21,AND 23 ARE DISBONDED. GROUNDED - YES. REPLACED #1 ENGINE FAN BLADE SPACERS #3,8,9,10,11,16,19,21, AND 23 REF. T/C 78472010.SDR ASAA2022012037209Blade · damagedPER TC 78472010 #1 ENGINE FAN BLADE LUBE #20 FAN BLADE CU-NI-IN COATING MISSING BEYOND LIMITS ON CC SIDE. GROUNDED - YES. REPLACED #1 ENGINE FAN BLADE #20 AND #8 REF T/C 78472010.SDR ASAA2022012037208Blade · damagedPER TC 78472010 #1 ENGINE FAN BLADE LUBE #17 FAN BLADE CU-NI-IN COATING MISSING BEYOND LIMITS ON CV SIDE. GROUNDED - YES. REPLACED #1 ENGINE FAN BLADE #17 AND #5 REF T/C 78472010.SDR ASAA2022011637178Blade · nickedPER T/C 78472010 #1 ENGINE FAN BLADE LUBE, FAN BLADE #16 HAS A NICK AT AREA T ON CONCAVE SIDE. GROUNDED - YES. MEASURED ADAMAGE AREA USING STARLITE SMARTSCOPE WITH REPO RUBBER METHOD...DEPTH MEASURE AT .005" IN BEYOND THE LIMITS .004" IN. REF B737-800 AMM 72-2SDR ASAA2022011637177Spacer · debondedPER T/C 78472010 #1 ENGINE FAN BLADE LUBE SPACERS #1 AND #3 ARE DISBONDED. GROUNDED - YES. INSTALLED SERVICEABLE SPACERS ON #1 ENGINE POSITIONS #1 AND #3 REF T/C 78472010.SDR ASAA2022011637176Platform · tornPER T/C 78472010 #1 ENGINE FAN LUBE PLATFORMS #7, #10, AND #12 ELASTOMER SEALS ARE TORN. GROUNDED - YES. INSTALLED SERVICEABLE PLATFORMS ON #1 ENGINE AT POSITIONS #7, #10 AND # 12 REF/ T/C 78472010.SDR NACA2022011500001Not Reported · not reportedRIGHT ENGINE FAN BLADE #23 HAS SMALL NICK APROX 2 MM AND 14" FROM TIP. RIGHT ENGINE FAN BLADE 23 BLENDED AND FOUND WITHIN LIMITS IAW B767 AMM 72-00-00. FLUORESCENT PENETRANT INSPECTION COMPLETED, NO DEFECTS NOTED.SDR ASAA2022010337065Spacer · debondedPER T/C 78472010 # 2 ENG FAN BLADE LUBE # 22 SPACER IS DISBONDED. GROUNDED - YES. REMOVED AND REPLACED #2 ENG, #22 SPACER REF TC 78472010.SDR ASAA2022010237059Platform · noneWHILE PERFORMING T/C 78472010 ON #2 ENGINE FOUND ON THE ALL PLATFORMS THE WEIGHTS ALL DISLODGED. GROUNDED - YES. REPLACED ALL 24 PLATFORMS ON THE #2 ENG WHILE PERFORMING T/C 78472010.SDR ASAA2021122536996Unknown · nonePER TC 78472010 #1 ENG FAN BLADE LUBE SPACER #1 ELASTORMER IS DISBONDED. GROUNDED - YES. REMOVED AND REPLACED #1 SPACER REF T/C 78472010.SDR ASAA2021122536995Unknown · nonePERT/C 78472010 #1 ENG. FAN BLADE LUBE #2 FAN BLADE CU-NE-IN COATING IS MISSING BEYOND LIMITS ON CONCAVE SIDE. GROUNDED - YES. REMOVED & REPLACED #2 & #14 FAN BLADES REF T/C 78472010.SDR NACA2021122400003None · noneRIGHT ENGINE FAN BLADE #19 HAS A SMALL DENT 2 INCH APPROX FROM TIP. BLENDED RIGHT ENGINE FAN BLADE 19 @ 2" APPROX FROM TIP AND FOUND WITHIN LIMITS IAW B767 AMM 72-31-02. DENT WAS 2 MM X .25 MM. NDT ACCOMPLISHED WITH NO FAULTS FOUND.SDR NACA2021122400002None · noneRIGHT ENGINE FAN BLADE #18 HAS A SMALL DENT 6 IN APPROX FROM TIP. BLENDED RIGHT ENGINE FAN BLADE 18 AND FOUND WITHIN LIMITS IAW B767 AMM 72-31-02. DENT WAS 2 MM X 0.5 MM. NDT INSPECTION ACCOMPLISHED, NO FAULTS NOTED.SDR NACA2021122300001None · noneLEFT ENGINE # 28 BLADE HAS BLEND. INSPECTED AND FOUND # 28 BLADE WITHIN LIMITS IAW B767 AMM 72-00-000SDR SIMA20211216001None · noneFLT EXPERIENCED ON CLIMBOUT AMBER LP ENGINE 2 VIBRATION EMERGENCY DECLARED VIB LP NO 2 ENG AMBER 4.0- 16000 FT-C/A-DEFERRED PER FMR REF ETN EJ 72-009 TDMI AUTHORIZATION NUMBER 001T7229.SDR ASAA2021121536917Shim · worn#2 ENGINE FAN BLADE SHIMS MOLYDAG COATING WORN. GROUNDED - YES. REPLACED #2 ENGINE FAN BLADE SHIMS, REF T/C 7872010.SDR ASAA2021121336896Spinner · damaged#1 ENG FRONT SPINNER CONE MISSING COATING IN EXCESS OF 50%. GROUNDED - YES. REMOVED AND REPLACED THE #1 ENGINE FRONT SPINNER PER TASK CARD 78472010 "CFM56-7 FAN BLADE LUBRICATION".SDR ASAA2021121036876Shim · damaged#1 ENG FAN BLADE SHIMS MISSING MOLYDAG COATING. GROUNDED - YES. REPLACED #1 ENG FAN BLADE SHIMS PER T/C 78472010 " CFM56-7 FAN BLADE LUBRICATION.".SDR ASAA2021120936878Shim · damagedENGINE #1 ALL FAN BLADE SHIMS MISSING MOLYDAG COATING. GROUNDED - YES. REMOVED AND REPLACED ALL THE FAN BLADE SHIMS IN THE #1 ENGINE. REF T/C 78472010 " CFM56-7 FAN BLADE LUBRICATION".SDR ASAA2021120936877Platform · damagedENGINE #1 FAN BLADE PLATFORMS HAVE DAMAGE AT LOCATIONS 2, 9, 10 , 15, 16, AND 18. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE FAN BLADE PLATFORMS AT LOCATIONS 2, 9, 10, 15, 16, AND 18. REFERENCE TAK CARD 78472010 " CFM56-7 FAN BLADE LUBRICATION".SDR ASAA2021120436811Blade · nickedREF L/P 60242308 AND L/P 6024309. #2 ENG FAN BLADE # 2, # 5, # 14 AND # 20 AND # 21 NEED REPLACED. GROUNDED - YES. REMOVED AND REPLACED END FAN BLADE # 8, # 9 AND # 17 AS PAIRS TO # 5, #20 AND # 21. REF T/C 78472010.SDR ASAA2021120436810Spacer · debondedWHILE ACCOMPLISHING T/C 78472010 FOUND ON ENG #2 THE SPACERS FOR THE BLADES #2, #3, #17, #18 ELASTOMER IS DISBONDED. GROUNDED - YES. REMOVED AND REPLACED ENG #2 SPACERS #2, 3, 17, 18 PER T/C 78472010.SDR ASAA2021120436809Blade · damagedREF L/P 60242308 #2 ENG FAN BLADE #20 REPLACEMENT. GROUNDED - YES. REMOVED AND REPLACED #20 FAN BLADE ON #2 ENG REF T/C 78472010.SDR ASAA2021120436808Blade · nickedWHILE ACCOMPLISHING T/C 78472010 FOUND ON ENG #2 BLADE 21 NICK IS OUT OF LIMITS. REF L/P 60026683 FOR PREVIOUS WRITE UP. GROUNDED - YES. REMOVED AND REPLACED FAN BLADE #21 ON #2 ENG REF T/C 78472010.
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