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.

SDR ASAA0956402Paint · peelingNR 1 ENG SPINNER CONE PAINT PEELING. REMOVED & REPLACED NR 1 ENG FRONT SPINNER CONE REF MM 72 21 01.Aug 12, 2009 · N587AS · Boeing 737890SDR C2XA09TY201Case · corrodedNR 2 ENG FAN CASE FWD FLANGE HAS CORROSION IN BOLT HOLES. REMOVED CORROSION FROM 12 HOLES BY REAMING IAW EC 7220-01066.Jul 29, 2009 · N14933 · Emb EMB145EPSDR ASAA0956210Shroud · damagedNR1 ENG FAN FRAME JUST FWD OF ABRADABLE SHROUD IS MISSING .25 WIDE 360 DEG OF COATING GROUNDED, YES. REPAIRED IAW 70 62 14 USING ALT METHOD STEP 4.DJul 17, 2009 · N564AS · Boeing 737890SDR ASAA0956209Shim · wornWHILE ACCOMPLISHING FAN BLADE LUBE ON NR 1 ENG T/C NR 78472002 FOUND ALL SHIMS WORN. GROUNDED YES. INSTALLED 24 EA. FAN BLADE SHIMS MFG. PN 340 252 307 0 ON NR1 ENGINE. REF T/C 78472002.Jul 16, 2009 · N563AS · Boeing 737890SDR ASAA0956208Shroud · damagedWHILE ACCOMPLISHING FAN BLADE LUBE T/C NR 78472002 ON NR 1 ENG, FOUND 2 AREAS OF ABRADABLE SHROUD DAMAGE AT 9:30 AND 10 O'CLOCK LOOKING AFT DAMAGE TO PARENT MATERIAL. GROUNDED YES. ACCOMPLISHED LOCAL RECONDITIONING OF MISSING SHROUD MATERIAL IAW MM 72 24 02. NJul 16, 2009 · N563AS · Boeing 737890SDR ASAA0956041Inlet Bullet · wornNR 2 ENG FRONT CONE WORN. REMOVED AND REPLACED NR 2 ENG FRONT CONE REF MM 72 21 01 400 801.Jun 27, 2009 · N583AS · Boeing 737890SDR ASAA0956040Inlet Bullet · wornNR 1 ENG FRONT CONE WORN. REMOVED AND REPLACED NR 1 ENG FRONT CONE REF MM 72 21 01 400 801.Jun 27, 2009 · N583AS · Boeing 737890SDR CA090622011Dome · damaged(CAN) UPON LEVELING AT FL380 AND REDUCING THRUST TO CRUISE POWER SETTINGS, FLIGHT CREW NOTICED THAT NR 2 ENG EXPERIENCED AN ENG STALL. THERE WERE NO FURTHER PROBLEMS DURING REMAINDER OF FLIGHT. UPON ARRIVAL AT DESTINATION, MX CARRIED OUT TROUBLESHOOTING OF NJun 18, 2009 · Boeing 727225SDR REXA200900071Blades · damagedON TAKEOFF, AIRCRAFT SUFFERED A BIRDSTRIKE TO THE LT ENGINE WHICH PRODUCED INCREASED N1 VIBRATION. THE FLIGHT CREW ELECTED TO RETURN AND NOTIFIED ATC. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE. MAINTENANCE INSPECTED THE ENGINE AND FOUND TWO DAMAGED Jun 14, 2009 · N8969A · Cndair CL6002B19SDR UALA2009061501679Acoustic Liner · crackedNR 1 ENGINE ACOUSTIC LINER HAS A 1.25 INCH CRACK LOCATED 0.25 INCH FWD OF THE FAN RUBSTRIP AT THE 10 O'CLOCK POSITION. THE DAMAGED CRACKED AREA IS ALSO DENTED FROM CRACK AFT TO RUBSTRIP JOINT. CRACK MUST BE CHECKED PRIOR TO EACH DEPARTURE AND INLET COWL MUSTJun 12, 2009 · N653UA · Boeing 767322SDR ASAA0955842Spinner · damagedWHILE ACCOMPLISHING ASA T/C 78472002 ON NR 2 ENGINE FOUND FRONT SPINNER CONE MISSING ANODIZED COATING (BLACK SULFURIC ANODIZING) GREATER THAN 20 PERCENT. PARTS NOT AVAILABLE. NR SPINNER CONE REPLACEMENT TO BE ACCOMPLISHED AT NEXT "C" CHECK PER TC 78472002. Jun 3, 2009 · N560AS · Boeing 737890SDR ASAA0955820Structure · nickedWHILE C/W T/C 78472002 FOUND 9 PLATFORMS P/N 340 001 816 0 WITH NICKS EXCEEDING .008 IN AREA C NR 1 ENGINE. RE-INSTALLED NEW PLATFORMS 9 EACH P/N 340 001 816 0 PER T/C 78472002 STEP 48.Jun 2, 2009 · N565AS · Boeing 737890SDR UALA2009042801230Acoustic Liner · damagedNR 2 ENGINE ACOUSTIC LINER HAS A DENT WHICH IS PUNCTURED BETWEEN 2 PERFORATIONS, LOCATED AT THE 9 O'CLOCK POSITION AND IS 8 INCHES FWD OF THE BLADES. IT IS 3-8TH INCH WIDE. ACCOMPLISHED REPAIR. APPLIED HEAT TO EXPEDITE CURE TIME.Apr 28, 2009 · N646UA · Boeing 767322SDR ASAA0955327Paint · erodedFAN BLADE LUBE T/C 78472002 FOUND NR 2 ENGINE FRONT SPINNER CONE PAINT ERODED PAST 20 PERCENT. INSTALLED NEW FRONT SPINNER CONE IN REF WITH T/C 78472002.Apr 25, 2009 · N558AS · Boeing 737890SDR ASAA0954998Paint · missingNR 1 ENG SPINNER CONE PAINT GONE. REMOVED & REPLACED FRONT SPINNER CONE REF MM 72 21 01.Mar 30, 2009 · N570AS · Boeing 737890SDR ASAA0954895Shim · damagedNR 1 ENG REF T/C 78472002 FOUND BLADE SHIMS MISSING MORE THAN 25 PERCENT OF MOLYDAG COATING REF MM 72-21-02-200-801-F00. SHIMS NIS SEA DEFERRED FOR 250 CYCLES IAW MM 72-21-02-200-801 SEAMC NOTIFIED.Mar 23, 2009 · N558AS · Boeing 737890SDR ASAA0954894Paint · missingREF T/C 78472002 STEP 6 NR 1 ENGINE FRONT SPINNER CONE IS MISSING MORE THAN 20 PERCENT OF WHITE ANTI EROSION PAINT. REPLACED FRONT SPINNER CONE IAW T/C 78472002.Mar 23, 2009 · N558AS · Boeing 737890SDR ASAA0954826Paint · missingNR 2 ENGINE FRONT SPINNER MISSING BLACK ANTI EROSION PAINT. REPLACEMENT OF NR 2 ENGINE FRONT SPINNER DEFERRED UNTIL NEXT C-CHECK PER MM 72 21 01 200 801, SEAMC NOTIFIED.Mar 15, 2009 · N519AS · Boeing 737890SDR C2XA09TY038Inlet · corrodedAIRCRAFT CURRENTLY IN A C-CHECK STATUS. INSPECTION FOUND EIGHT BOLT HOLES ON THE NUMBER ONE ENGINE INTAKE INLET THAT WERE CORRODED. MAINTENANCE REPAIRED THE CORRODED BOLT HOLES IAW EC5420-01158 BY USING REAMERS AND NEW BUSHINGS. ALL WORK WAS COMPLIED WITH AMar 1, 2009 · N15932 · Emb EMB145EPSDR ASAA0954247Shim · missingWHILE ACCOMPLISHING ASA T/C 78472002 ON NR 1 ENGINE FOUND SHIMS 24EA MOLYDAG COATING MISSING GREATER THAN 25% ON PRESSURE FACE REF AMM 72 21 02 PARA L.(1)(A) FIG 609. ON PLT DEFERRAL REF. DEFECT 6558758. REMOVED AND REPLACED 24 EA SHIMS ON THE NR 1 ENG FAN BJan 15, 2009 · N585AS · Boeing 737890SDR C2XA09TY003Inlet · corrodedNR 1 ENG INTAKE ATTACHMENT FLANGE HAS IN MULTIPLE BOLT HOLES. REAMED HOLES TO REMOVE CORROSION, PERFORMED DYE PEN INSPECTION ALODINED AND INSTALLED BUSHINGS IAW EC5420-01187. ACFT IS CURRENTLY IN C-CHECK.Jan 5, 2009 · N16954 · Emb EMB145LRSDR C2XA09TY002Inlet · corrodedNR 1 ENG INTAKE ATTACH NUT PLATE HOLES HAVE CORROSION. REAMED HOLES TO REMOVE CORROSION ON INTAKE FLANGE, PERFORMED DYE PEN INSP, ALODINED AND INSTALLED BUSHINGS IAW EC5420-01186. ACFT CURRENTLY IN C-CHECK.Jan 4, 2009 · N12957 · Emb EMB145LRSDR C2XA09TY001Inlet · corrodedNR 2 ENG AIR INTAKE ATTACH NUTPLATE HOLES HAVE CORROSION. REAMED HOLES TO REMOVE CORROSION, PERFORMED DYE PEN INSP, ALODINED ALL HOLES AND INSTALLED BUSHINGS IAW EC5420-01186. ACFT STILL IN C-CHECK.Jan 4, 2009 · N12957 · Emb EMB145LRSDR COMA2008120290001Fan Blade · damagedEN ROUTE FROM ORD TO JFK NR 2 ENGINE N1 VIBE. ACFT IN ICING CONDITIONS. FOLLOWED QRH FOR ICING BUT VIBE CONTINUED TO CLIMB, PERFORMED IFSD OF NR 2 ENGINE. EMERGENCY DECLARED, ACFT DIVERTED TO FWA LANDED SAFELY. REMOVED AND REPLACED 3 SETS OF DAMAGED FAN BLDec 1, 2008 · N679CA · Cndair CL6002D24SDR MU12008F00004Acoustic Panel · damagedENGINE FOREING OBJECT DAMAGE. MX REPORT DURING TRANSIT CHECK IN BOG ENG N1 WAS FOUND FOD EVIDENCE. BOROSCOPIC INSPECTION ON HP AND HI COMPRESSOR IAW TASK 72-00-00-200-812 AND PENETRANT LIQUID INSPECTION ON LEADING EDGE OGV IAW TASK 70-20-02-230-804. NO DAMAOct 22, 2008 · N948AC · Airbus A330243SDR 2008UALA05754Inlet Bullet · damagedCRACK AND DELAMINATION FOUND ON INLET CONE (SPINNER) ON RT ENGINE. SPINNER FOUND CRACKED/DELAMINATED. ASSY SENT TO SHOP. REPLACED INLET CONE. NO FAN BLADE DAMAGE FOUND. AFTER VERIFICATION FLIGHT, A/C DETERMINED OK FOR SERVICE.Sep 17, 2008 · N651UA · Boeing 767322SDR CA080917019Inlet Guide Vane · malfunctioned(CAN) IT IS REPORTED THAT 10 MINUTES BEFORE LANDING, ENGINE NR 1 SHUTDOWN BY ITSELF FOLLOWED BY A "NO DISPATCH" MSG ON THE COCKPIT DISPLAY. TROUBLESHOOTING SHOWED THAT THE IGV POSITION DID NOT MATCH THE REQUESTED VALUE. THE VIGV WAS REPLACED AND THE FAULT CLSep 13, 2008 · Amd FALCON2000SDR DHLA200800094Nose Bullet · contaminatedWHEN TAKE OFF THRUST WAS APPLIED ENG NR 1 AND NR 3 AT 2.19 EPR SHOWED 88% N1 520* EGT. 90% N2. FAILED TO MAKE TAKE OFF OFF THRUST. REMOVED DEBRIS WITH DRY NITROGEN OUTWARD THROUGH NOSE DOME ON NR 1 & NR 3 ENG. NOSE DOME NOT REMOVED. PT 2 LINES RESECURED. Aug 29, 2008 · N741DH · Boeing 7272Q9SDR C2X2008F00019Inlet · corrodedTYS - DURING A 2C INSPECTION CORROSION WAS FOUND IN THE NR 2 ENG AIR INLET ATTACH POINT HOLES. MAINTENANCE REWORKED THE ATTACH POINT HOLES IAW EC 5420-01136 AND WILL BE RELEASED AT THE END OF THE C-CHECK. (S)Aug 7, 2008 · N16178 · Emb EMB145XRSDR ASAA0853169Inlet Bullet · erodedNR 1 ENGINE FWD SPINNER (CONE) HAS EXCESSIVE ERROSION OF BLACK AND WHITE COATING. REMOVED AND REPLACED SPINNER (CONE) PER TC 78472002.Jul 1, 2008 · N570AS · Boeing 737890SDR CA080730001Nut · missing(CAN) DURING SHOP VISIT, ONE VARIABLE VANE SPINDLE NUT WAS FOUND MISSING ON STAGE 5 VANE. THE LEVER ARM REMAINED ENGAGED. A NUT WAS INSTALLED IAW THE ENGINE MANUAL 72-32-00 AS RECOMMENDED IAW SB 72-0184.Jun 23, 2008SDR DL76G080109Vane · wornNR 1 ENGINE REPLACED DUE TO VSV WEAR.Jan 17, 2008 · N1604R · Boeing 767332SDR DJFA2007140Inlet · crackedDURING POSTFLIGHT, CREW REPORTED CRACKS ON THE NR2 INLET RING. MAINTENANCE CONFIRMED THE DISCREPANCY AND REPLACED THE INLET RING.Dec 7, 2007 · N449LX · Beech 400ASDR 2007FA0000759Fairing · crackedDURING INSPECTION OF THE AIR INTAKE ROTATING FAIRING, WE FOUND A CRACK BETWEEN THE MOUNT BOLT HOLE AND THE ADJACENT ALIGNMENT PIN HOLE.Aug 31, 2007 · N73M · Gulstm GULFSTREAMGVSDR WRLA2007085Bellmouth · crackedTHREE EA CRACKS AT NUMBER 2 ENGINE BELLMOUTH BETWEEN 6-7 O'CLOCK POSITION. REPLACED NR 2 ENGINE BELLMOUTH ASSYWITH NEW PARTS AS PER AMM 71-11-04-000-868/71-11-04-400-868 REV.59Aug 16, 2007 · N275WA · Doug MD11FSDR SROM200700005Casting · brokenDURING TAKEOFF, AT APPROXIMATELY 300 FEET, CREW EXPERIENCED NR 2 ENGINE COMPRESSOR STALL WITH RAPIDLY RISING EGT. SHUTDOWN NR 2 ENGINE AND MADE UNEVENTFUL LANDING AT DEPARTURE AIRPORT. INSPECTION REVEALED THE NOSE DOME HAD SEPARATED FROM ITS MOUNT DAMAGING THEJul 31, 2007 · N245US · Boeing 737201SDR 2007UALA02268Acoustic Liner · out of positionFLIGHT DIVERTED DUE TO NR 2 ENGINE COMPRESSOR STALL DURING GO-AROUND AT ORD. FAN BYPASS AIR STALL DUE TO AIR BLOCKAGE FROM ACOUSTIC LINING. ENGINE REMOVAL: SB ENG-72-0392 ISSUED TO ADDRESS PROBLEM OFF WING.Jun 26, 2007 · N457UA · Airbus A320232SDR DJFA2007067Inlet · crackedTRIP NR 1174419 ON POST FLIGHT CREW DISCOVERED A CRACK AT THE 1 O'CLOCK POSITION ON THE NR 2 INLET. MAINTENANCE REPLACED THE NR 2 INLET.Jun 19, 2007 · N445LX · Beech 400ASDR UPS07649926Case · corrodedINSPECTION TYPE:C2 NR 1 ENGINE CORROSION ON AFT FAN CASE AT 5-6:30 POS AT NUT PLATES 8 INCHES FROM AFT END OF CASE. REPAIRED PER UPS ENGINEERING FILE NUMBER 80C2-72-20000.May 7, 2007 · N306UP · Boeing 76734AFSDR F3LA200700026Guide Vane · crackedDURING C-2 CHECK, INSPECTION REPORTED NR 1 ENG OUTLET GUIDE VANE AT 8 O'CLOCK POSITION HAD CRACK AT T/E. REPLACED OUTLET GUIDE VANE IAW AMM 72-23-00-400-008 AND 72-23-00-400-026.Feb 18, 2007 · N929FR · Airbus A319111SDR ASMF200701007Blade · nickedDURING TRANSIT CHECK, A BLADE WAS DETECTED DAMAGED DUE TO A FOD IN RT ENGINE. A NICK WAS DETECTED AT 2.5 INCHES BETWEEN PLATFORM AND MIDSPAN SHROUD OF 1 INCH LONG WITH .1250 INCH DEPTH. THE BLADE WAS REWORKED IAW MM 72-33-21 AND BOROSCOPIC INSPECTION WAS PERFOJan 29, 2007 · N216AM · Doug DC987SDR CA070126013Fan · dislodged(CAN) THE NR 1 ENGINE FAN DISLODGED ITSELF FROM THE ENGINE AND TORE OFF THE INLET AND FAN CASING. IT ALSO DID EXTENSIVE DAMAGE TO THE PYLON AND THE FUSELAGE. NTSB IS ON SITE FOR THE INVESTIGATION. MORE INFORMATIOON TO FOLLOW ONCE AVAILABLE. (TC NR 20070126013Jan 26, 2007 · Cndair CL6002B19SDR DJFA2007001Inlet · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, MAINTENANCE FOUND THE INLET CRACKED. THE CRACK WAS LOCATED AT THE INNER SECTION WHERE THE INLET MOUNTS TO THE ENGINE AND WAS ABOUT .25 INCH LONG FROM THE FASTENER HOLE TO THE INLET EDGE. THE INLET WAS REPAIRED IAW Jan 3, 2007 · N478LX · Beech 400ASDR 2006FA0001082Tube · crackedTHE TUBES ARE CRACKING ALONG THE WELDS, WHICH CONNECT THEM TO THE INLET LIP ASSEMBLY. REQUIRES REMOVAL OF INLET LIP ASSY AND REPAIR OF THE CRACKED WELDS. (K)Nov 8, 2006 · N200HV · Beech C90ASDR UIEA200600222Fan Blade · lack of lubeN415MC AT PIK FOR MSG-3, C-4&A-4 CHECK. AS PER N/ROUTINE 154, NR 1 ENGINE S/N 704-916 FAN BLADES REMOVED FOR LUBRICATION. IT WAS FOUND, FAN DISKS HAVE NO EVIDENCE OF LUBRICANT. INSPECTION PERFORMED IAW MM 72-31-00, 206 TABLE 601 NR 1 DOVETAILS ON FAN DISK HAug 31, 2006 · N415MC · Boeing 74747UFSDR MALA060521Engine · malfunctionedLT ENGINE WARNING MESSAGE WAS DISPLAYED. COMPLETED QRH AND NOTED ENGINE OIL TEMP WAS NORMAL. DIVERTED TO DFW. REMOVED AND REPLACED LT ENGINE, P/N CF34-3B1, S/N OFF GE-E950371, S/N ON GE-E872556.Aug 17, 2006 · N602XJ · Cndair CL6002B19SDR F3LA200600090Guide Vane · crackedENGINE NR 1, 14 OUTLET GUIDE VANES DOUBLERS WERE CRACKED AND WERE OUT OF LIMITS. REPAIRED AND REPLACED PER AMM 72-23-00-400-008.Aug 6, 2006 · N903FR · Airbus A319112SDR UPS06547173Nose Bullet · contaminatedINSPECTION TYPE:N/A STRONG BAD ODOR FROM PACKS SUSPECT LT PACK. INSPECTED AND CLEANED BUGS OFF LT AND RT ENGINE SPINNERS. RAN ENGINES AND PACKS. ALL CHECKS NORMAL OK FOR CONTINUED SERVICE PER 21-00-01-2.Jun 22, 2006 · N409UP · Boeing 75724APFSDR F3LA200600071Guide Vane · crackedDURING C-4 CHECK, INSPECTION REPORTED NR 1 ENGINE OUTLET GUIDE VANES CRACKED FROM EDGE TO GUIDE VANE THROUGH BOLT HOLE (OVER 1 INCH LONG). RT SIDE OF ENGINE FROM 12 O'CLOCK TO 4 O'CLOCK. INSPECTED CRACKS PER MM 72-23-00-991-310-06 AND 72-23-00-991-310-06, SHJun 12, 2006 · N902FR · Airbus A319111SDR CA060601002Duct · cracked(CAN) CRACK DEVELOPED IN THE DOMED PORTION OF THE SMALL EXIT DUCT BESIDE THE WELD. FOUND DURING THE BOROSCOPE INSPECTION. (TC NR 20060601002)May 31, 2006 · Beech A100
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