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 ASAA2019011127767Paint · wornNR 2 ENG FWD SPINNER CONE WHITE MARKING PAINT WORN PAST 50%. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENG FWD SPINNER CONE REF AMM 72-21-01.SDR K8FF2018123100112Blade · shearedMIAMI AIR INTL LOGPAGE 254162-3: "DURING FLIGHT AT 33000 FT IDG DRIVE AMBER LIGHT FOLLOWED BY HIGH VIBRATION #1 ENGINE. UPON LANDING, VISUAL INSPECTION REVEALED DAMAGED FAN BLADES." THE CREW DECLARED AN EMERGENCY AND DIVERTED TO MKE. VISUAL INSPECTION REVEALEDSDR UIEA2018122602941Spinner · worn#1 ENG SPINNER NEEDS REPAINT AS PER CUSTOMER.(<P>REMOVED,PAINTED & REINSTALLED #1 ENG SPINNER IAW B767 AMM 72-31-01 & ENGINE MANUAL (GEK 92451) TASK 72-21-10-300-802-0.</P>)SDR ASAA2018122627580Spacer · debondedFOUND 12 FAN BLADE SPACERS ON #2 ENGINE DISBONDED WHILE ACCOMPLISHING ASA T/C 78472010. GROUNDED - YES. REMOVED AND REPLACED 12 FAN BLADE SPACERS ON #2 ENGINE. REF ASA T/C 78472010.SDR ASAA2018122127497Panel · damaged#2 ENGINE LPTACC SCOOP FAN DUCT PANEL HAS AFT TWO FASTENERS PULLED THROUGH PANEL. GROUNDED - YES. REPLACED LPTACC FAN DUCT PANEL REF B737-800 AMM 72-23-07-400-801-F00.SDR ASAA20181227579Fitting · separatedFOUND TEST PIN FITTING TO HAVE SEPARATED FROM BOSS # 2 ENGINE 1 O'CLOCK POSITION LOOKING FWD. GROUNDED - YES. ON DEFERRALSDR ASAA2018121327388Fastener · looseENGINE #2 STRUT PANEL AT 3'CLOCK POSITION ALF HAS LOOSE FASTENERS. GROUNDED - YES. REMOVED & REPLACED FAN DUCT PANEL @ 3'CLOCK POSITION REF B737-900 AMM 72-23-07.SDR B90A20181213001Liner · crackedDURING SCHEDULED FJ44 CHECKS 1 AND 2, RT ENGINE INLET LINER FOUND DAMAGED/CRACKED. PERFORMED IP AND HP COMPRESSOR (BORESCOPE) INSPECTION IAW FJ44-1A LMM TASK 71-00-30 FOR POSSIBLE FOD DAMAGE. NO EVIDENCE OF FOD DAMAGE FOUND. RT ENGINE INLET ASSEMBLY WAS REPLACSDR FDEA201811283384Inlet · failed82081 APROX 1200 FT AGL EXPERIENCED WHAT WE THOUGHT WAS A LEFT ENG COMPRESSOR STALL. HEARD A LOUD BANG SURGE IN EGT. INSTRUMENTS RETURED TO NORMAL IN A SECOND. DECLARED AN EMERGENCY AND RETURNED TO MEM REMOVED AND REPLACED LEFT ENGINE PER 7180260-01-0SDR ASAA2018111927076Shroud · damagedDURING EXTERIOR WALK AROUND, DISCOVERED SHROUD DAMAGE ON NR 2 ENGINE AT 4 O'CLOCK POSITION. DAMAGE IS 1/8'' IN DIAMETER. GROUNDED - YES. REPAIRED THE DAMAGE TO THE NR 2 ENG ABRAIDABLE SHROUD AT 4 O'CLOCK POSITION REF AMM 72-24-02-200-802-F00.SDR ASAA2018111966890Case · damagedWHILE ACCOMPLISHING T/C 78472000 #2 ENGINE FOUND FAN INLET CASE DAMAGE APPROX. 8 INCHES FWD OF O/B ENGINE CRADLE MOUNT AREA. 700X .150. GROUNDED - YES. REMOVED HIGH METAL AND SWAP ETCHED AREA PER B737-800 AMM 72-23-05-700 2.F.(1) & (2). FOUND GOUGE TO BE .004 SDR ASAA2018111526873Seal · damagedWHILE ACCOMP. FAN LUBE #2 ENG S/N 894151 FOUND PLATFORM SEAL DAMAGE TO ALL PLATFORMS TOTAL DAMAGE GREATER THAN 40". GROUNDED - YES. REPLACED ALL PLATFORM.SDR ASAA2018111526872Shim · damagedWHILE ACCOMP FAN BLADE LUBE #2 ENG S/N 894151 FOUND ALL BLADE SHIMS WORN MISSING MOLY DAG COATING >25%. GROUNDED - YES. REPLACED ALL #2 ENG BLADE SHIMS.SDR ASAA2018111526871Blade · damagedWHLE ACCOMP. T.C. SBCFM56-7B--72-1033-1 FAN BLADE ULTRASONIC INSP. FOUND BLADE #3 S/N DC980532-L ' 34% INDICATION .8" FROM T.E CONVEX SIDEBLADE #13 S/N DD281020-O ' 35% INDICATION 1.5" FROM L.E CONVEX SIDEBLADE #17 S/N DD281033-U ' 35% INDICATION 1.0" FROM L.ESDR ASAA2018111656870Blade · damagedWHILE ACC. FAN LUBE T.C. ESN - 894151 FOUND CU-NI DAMAGE TO BLADE POSN. #8 S/N DD280468-G #16 DD280056-8 #20 S/N DC975822-G. GROUNDED - YES. REPLACED BLADES ON #2 ENGINE, #8 & #20 AND #16 AND ITS PAIR #4 PER T/C 78472010. MAPPED BLADES PER BLAMAP V. 3.0, ENTERSDR ASAA2018111646864Guide Vane · damagedFOUND #2 ENG 4 O'CLOCK POSITION, 1 OUTLET GUIDE VANE HAS DAMAGE OUT OF LIMIT. GROUNDED - YES. REMOVED AND REPLACED #2 ENG 4 O'CLOCK POSITION, 1 OUTLET GUIDE VANE REF B737-800 AMM 72-23-01.SDR ASAA2018111426863Spacer · damagedWHILE ACCOMP T/C #78472010 ( FAN LUBE ) ON #1 ENGINE FOUND DAMAGE TO FAN BLADE SPACERS BEYOND MAX LIMIT OF 8. GROUNDED - YES. REMOVED AND REPLACED ALL 24 FAN BLADE SPACERS ON #1 ENG REF B737-800 AMM 72-21-02.SDR UIEA2018111602633Doubler · corrodedCORROSION AROUND DOUBLER AT 7 O' CLOCK POSITION IN FAN CASE ENGINE #1(<P>ACCOMPLISHED REPAIR IN ENG #1 FAN CASE AT 7 O'CLOCK POSITION IAW GE CF6-80C2 ENGINE MANUAL 72-22-01.</P><P><BR DATA-MCE-BOGUS="1" /></P>)SDR UIEA2018111602632Doubler · corrodedCORROSION AROUND DOUBLER AT 5 O'CLOCK POSITION IN FAN CASE ENG #1(<P>ACCOMPLISHED REPAIR ON ENG #1 FAN CASE AT 5 O'CLOCK POSITION IAW GE CF6-80C2 ENGINE MANUAL 72-22-01</P>)SDR UIEA2018111602631Doubler · corrodedCORROSION AROUND DOUBLER AT 6 O' CLOCK PSOTION IN FAN CASE #1 ENGINE(<P>ACCOMPLISHED REPEAIR ON ENGINE #1 FAN CASE AT 6 O' CLOCK POSITION IAW GE CF6-80C2 ENGINE MANUAL 72-22-01.</P>)SDR UIEA2018111642613Case · corrodedCORROSION AROUND 3EA FASTENERS HOLES ON #1 ENG FAN CASE EXTERNAL SURFACE, LOCATED APPROX BETWEEN 7 AND 8 O CLOCK POSITION AND JUST BELOW THE ECU(<P>REMOVED CORROSION, EVALUATED AREA AND FOUND WITHIN LIMITS IAW GE CF6-80C2 ENGINE MANUAL 72-22-01. TREATED AND PRSDR ASAA2018111226826Spinner · erodedPER T/C 78472010 NR 2 ENGINE INLET SPINNER FRONT CONE MORE THAN 50 PER CENT PAINT MISSING. GROUNDED - YES. INSTALLED NEW INLET SPINNER FRONT CONE ON ENGINE NR 2 PER T/C 78472010.SDR ASAA2018102926642Spacer · debondedWHILE ACCOMPLISHING T/C 78472002 NR 1 ENGINE FOUND 9 SPACERS DEBONDING. GROUNDED - YES. REMOVED AND REPLACED 24 SPACERS ON NR 1 ENG REF.SDR ASAA2018102926641Spacer · debondedWHILE ACCOMPLISHING TC 78472002 NO 2 ENGINE SN 658290 FOUND NR 8 SPACER DISBONDED. GROUNDED - YES. REPLACED NR 8 SPACER ON NR 2 ENGINE SN 658290. REF TC 78472002 FOR WORK PERFORMED AND VIB SURVEY.SDR ASAA2018102226583Bolt · wornNR 2 ENGINE FAN FRAME OUTBOARD STRUT COVER HAS A FASTENER HEAD WORN BOTTOM SIDE. GROUNDED - YES. REPLACED DAMAGE FASTENER SEE MIG 2C 40-0026341 FOR DETAILS.SDR ASAA2018102326572Shroud · wornNR 1 ENG ABRADABLE SHROUD HAS GROOVES COMPLETELY AROUND THE SHROUD. MAX WIDTH WAS 2.9 IN. OUT OF LIMITS PER AMM 72-24-02 F.(1)(E). GROUNDED - YES. INSTALLED NEW COMPOUND TO THE ABRADABLE SHROUD IAW AMM 72-24-02-200-802. 2.A.-F.(1)-(10). COMPLETED NR 1 ENG ABRASDR ASAA2018101526500Case · corrodedNR 2 ENG OUTER FAN CASE NUTPLATES BETWEEN B6-B7 FAN FRAME SHROUD FLANGES SHOWS CORROSION (APPROX) 11 EA. AT 1-8 O'CLOCK ALF. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENGINE.SDR ASAA2018101526496Nut Plate · corrodedWHILE ACCOMPLISHING T/C 78472000 NR 1 ENGINE FOUND 3 NUTPLATE CORRODED BEHIND OIL TANK. GROUNDED - YES. REMOVED AND REPLACED ENGINE NR 1 REF W/O 428952.SDR 3FPY201810078003Stator Vane · damagedDURING ROUTINE ENGINE INSPECTIONS, THE LT ENGINE FAN STATOR VANES - LEADING EDGE SCREENS WERE FOUND DAMAGED - QTY 13 NEW VANE FAN STATORS INSTALLED.SDR IPXA2018093034543Blade · missingINSPECTION TYPE:N/A**SUPPLEMENTAL SDR** PERFORMED BORESCOPE INSPECTION #2 ENG PER PMC 6. FOUND 1ST STAGE HPT BLADE MISSING MATERIAL ON LEADING EDGE MEASURING DIMENSION GREATER THAN 5 EDGE HOLES. REFER TO AMM 72-00-00-206-363-H00 TABLE 680 FOR MAX SVCABLE LIMISDR UIEA2018102902405Acoustic Panel · damagedLOOSE FIBERGLASS MESH ON ACOUSTICAL PANEL NR 2 ENGINE FAN CASE AT 5 OCLOCK POSITION IAW SRM 54-12-01 REPAIR 6. REPAIRED MESH ON ACOUSTICAL PANEL NR 2 ENGINE FAN CASE AT 5 OCLOCK POSITION IAW SRM 54-12-01 REPAIR 6. (SUP DD 10/27)SDR ASAA2018092626277Acoustic Liner · delaminatedDURING ACCOMPLISHMENT OF MTC 7847200 FOUND AFT NR 2 ENGINE ACOUSTIC PANEL AT 7'OCLOCK POSITION LOOKING AFT DELAMINATED. GROUNDED - YES. REPLACED NR 2 ENGINE ACOUSTIC PANEL PER AMM 72-23-02-400-801-F00, REMOVED MCT.SDR ASAA2018092626279Spinner · wornWHILE ACCOMPLISH T/C 78472000 FOUND FRONT SPINNER CONE 50% MISSING WHITE SPIRAL - SHAPE MARK WHITE ANTI EROSION PAINT. GROUNDED - YES. REMOVED & REPLACED FRONT SPINNER CONE REF AMM 72-21-01.SDR ASAA2018092626278Nut Plate · looseWHILE ACCOMPLISHING NR 1 ENG INLET INSP T/C 78472000, FOUND AFT O/B LWR FASTENER LOOSE ON 3 O'CLOCK STRUT FAIRING. GROUNDED - YES. REMOVED STRUT FAIRING TO ALLOW ACCESS TO NUTPLATES. REMOVED & REPLACED NUTPLATE REF B737-800 SRM 51-40-02. REINSTALLED STRUT FAIRSDR ASAA2018091926194Panel · damagedDURING NR 1 ENG INLET AND FAN BLADES DETAILED INSP. FOUND NR 5 STRUT PANEL DAMAGED AT FWD LWR FASTENER BEING LOOSE. AFT LOOKING FWD (M) APPROX 5 O'CLOCK POS. GROUNDED - YES. REMOVED AND REPLACED FAN DUCT PANEL PER AMM 72-23-07/401. NO OTHER DEFECTS NOTED AT THSDR IPXA2018100394641Inlet · crackedNR 2 ENGINE INLET LIP HAD A CRACK AT THE 1:00 O`CLOCK POSITION, AT A FASTENER. REPAIRED THE NR 2 ENGINE INLET LIP IAW SRM 54-10-01, REPAIR 4. MINOR.SDR ASAA2018091726149Acoustic Panel · damagedNR 1 ENG AT NR 3 ROTATION ACOUSTIC PANEL DAMAGED. GROUNDED - YES. REPLACED ACOUSTIC PANEL PER AMM 72-23-02-400-801-F00.SDR ASAA2018090526010Blade · damagedWHILE ACCOMP T/C 78472002 ON NR 1 ENG. FOUND ONE PLATFORM DAMAGED. GROUNDED - YES. REMOVED AND REPLACED 1 PLATFORM ON NR 1 ENG.SDR ASAA2018090526009Elastomer · debondedWHILE ACCOMPLISHING T/C 78472002 FOUND ALL FAN BLADE SPACERS ON NR 1 ENG TO HAVE DISBONDED ELASTOMERS ON BOTH SIDES. GROUNDED - YES. REMOVED AND REPLACED ALL 24 FAN BLADE SPACERS ON NR 1 ENG.SDR ASAA2018090425997Spacer · debondedWHILE ACCOMPLISHING TC 7872002 NR 2 ENGINE FOUND 9 EA SPACERS DISBONDED. GROUNDED - YES. REMOVED AND REPLACED ALL 24 SPACERS ON NR 2 ENG.SDR P5CA2018082217195Spinner · erodedPANT PEELED ON THE NR 2 ENGINE SPINNER CONE. REPAINTED THE SPINNER CONE IAW ESM 72-21-10, REPAIR 6 REV 87.SDR UIEA2018081801739Acoustic Liner · missingPOST FLIGHT, LEFT ENGINE AFT INBOARD CASE FAN ACUSTIC LINER SEGMENT PANEL AT 5 O'CLOCK POSITION MISSING. (FAN STATOR LINER) REPLACED LEFT ENGINE AFT INBOARD FAN STATOR LINER AT 5 O'CLOCK POSITION IAW AMM 72-33-01. PERFORMED REPAIR TO LEFT ENGINE INBOARD THRUSTSDR ASAA201808135749Blade · damagedNR 2 ENGINE FAN BLADE ROOT HAS CU-NI-IN COATING MISSING, AND WAS OUT OF LIMITS. ALL BLADES EXCEPT NR 4 & 16 IAW T/C 78472002. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE FAN BLADES EXCEPT NR 4 AND 16 IAW T/C 78472002.SDR ASAA2018080325647Blade · damagedFOUND SEVEN BLADES WAS MISSING CU-NI-IN COATING, OUT OF LIMITS. BLADES NR 1, 2, 3, 4, 16, 17, AND 21. ACFT GROUNDED. REMOVED AND REPLACED THE BLADES.SDR ASAA2018072625538Spinner · damagedWHILE ACCOMPLISHING T/C 78472000 NR 1 ENGINE FOUND FRONT SPINNER CONE MISSING 50% OF BLACK SULFURIC ANODIZING COATING. GROUNDED - YES. REMOVED AND REPLACED NR 1 ENGINE FRONT SPINNER PER AMM 72-21-01. NO DEFECTS NOTED AT THIS TIME.SDR P5CA2018072600166Spinner · damagedPEEL OFF-PAINTING NR 2 ENGINE SPINNER CORE EXTERNAL SURFACE. CLEAN UP SURFACE AND APPLY THE COATING IAW ESM 72-21-10 REPAIR006 REV 87. COND CHK RESULT SATISFY.SDR SWAA2018071623512Guide Vane · crackedNR 1 ENG STAGE 1 NOSE GUIDE VANE CRACKS. R&R NR 1 ENG PER MT.SDR SWAA2018071123334Guide Vane · crackedNR 1 ENGINE FOUND 2 EACH SEGMENT OF INLET GUIDE VANE WITH LEADING EDGE TO TRAILING EDGE AXIAL AT 2 DIFFERENT LOCATION 8 O'CLOCK & 3 O'CLOCK AXIAL CRACKED. R&R NR 1 ENGINE PER MT.SDR ASAA2018070225236Shim · damagedWHILE ACCOMPLISHING FAN BLADE LUBE ON NR 2 ENGINE PER T/C 78472002, FOUND ALL SHIMS TO HAVE 25% TO 100% MOLYDAG COATING MISSING. GROUNDED - YES. ON DEFERRAL.SDR ASMF20180821009Shroud · damagedDURING TRANSIT CHECK, IT WAS DETECTED IN THE RIGHT ENGINE A MISSING MATERIAL AT FAN BLADE ABRADABLE SHROUD. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING A CRATER OF 3.5" LENGTH AND 0.968" WIDTH IN ABRADABLE SHROUD OF ENGINE. THEREFORE CREATER ON ABRADABL
Back to JASC 7220