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 R61A201404190582Rub Strip · corrodedDURING HEAVY CHECK, LT ENGINE OTBD FAN COWL UPPER METALLIC STRIP WORN AND CORRODED. MX R & R LT ENGINE OTBD FAN COWL UPPER METALLIC STRIP IAW SRM 51-41-02, PN 341-2311-505, RUB STRIP.SDR ASAA2014041707513Panel · looseNR 2 ENGINE FAN DUCT PANELS AT 12:30 AND 2:00 POSITIONS HAVE SEVERAL LOOSE BOLTS EACH. ACFT GROUNDED. TIGHTENED FASTENERS AS REQUIRED, REF: AMM 72-23-07.SDR MASA2014041731036Blade · vibrationDURING ENGINE FAN BLADE INSPECTION, BLADE SHAKE, AND VIBRATION CHECK ENGINE RUNS COMPLIED WITH AS REQUIRED IAW AMM 72-21-02. FAN BLADE LUBRICATION COMPLIED WITH & ENGINE VIBRATION CHECK WITHIN LIMITS.SDR ASAA2014041307534Shim · damagedDURING 2 ENGINE FAN BLADE LUBE FOUND ALL FAN BLADE SHIMS MISSING MOLYDAG COATING. REF T/C 78472002, STEPS 32-33. ACFT GROUNDED. ON DEFERRAL.SDR CA140414005Blade · lack of lube(CAN) AFTER DEPARTURE, THE CREW NOTICED EXCESSIVE ENGINE VIBRATION. AFTER CONSULTATION WITH MAINTENANCE, IT WAS DECIDED THAT THE FLIGHT SHOULD RETURN. CARRIED OUT NR 1 ENGINE BLADE LUBE IAW EMM 72-00-00-030-806, 72-00-00-030-808 & 72-00-00-030-805, PERFORMED SDR ASAA2014041107524Spacer · damagedFOUND NR 6 AND NR 7 FAN BLADE SPACER DIFFICULT TO REMOVE ON NR 2 ENGINE. FOUND NR 6 AND NR 7 FAN BLADE SHIMS CONTACTING SPACER. ACFT GROUNDED. REPLACED SPACER AT NR 6 & NR 7 BLADE POSITION IAW T/C 78472002 STEP 47. REPLACED SHIM AT NR 6 & NR 7 BLADE POSITISDR ASAA2014040907501Panel · looseWHILE ACCOMPLISHING NR 1 ENGINE INLET INSPECTION, FOUND NR 5 DUCT PANEL WITH LOOSE FASTENERS. ACFT GROUNDED. R & R NR 5 DUCT PANEL, REF AMM 72-23-07.SDR ASAA2014040807482Rotor · out of balanceNR 2 ENGINE TREND DATA SHOWS LOW PRESSURE ROTOR VIBRATION LEVELS TO BE TRENDING HIGHER THAN EXPECTED. CURRENT LEVELS NEAR 1.5 UNITS. ACFT GROUNDED. ACCOMPLISHED ON BOARD FAN TRIM IAW AMM TASK 71-00-00-750-830- F00, TEST 14B. BALANCE WEIGHT SCREWS NR 3, P1SDR CA140408003Case · delaminated(CAN) QTY-35 FAN CONTAINMENT CASES FROM CF34-3B1 ENGINES HAVE BEEN FOUND WITH DELAMINATION ON THE ABRADABLE RUB STRIP AREA. THE CYCLES SINCE SHOP REPAIR ON THESE INCIDENTS RANGE FROM 183 CYCLES TO 11171 CYCLES. THESE WERE REPAIRED BETWEEN 2009 AND 2012. FOR SDR ASAA2014032807348Duct · damagedNR 1 ENGINE, NR 1 FAN DUCT (VBV) PANEL HAS A SCREW PULLED THROUGH AT THE AFT INBD ATTACH POINT. ACFT GROUNDED. REPLACED NR 1 ENGINE, NR 1 STRUT FAN DUCT PANEL IAW MM 72-23-07-000/400-801-F00.SDR ASAA2014031207176Panel · damagedNR 1 ENGINE, FAN DUCT PANEL AT 9:00 POSITION HAS 1 EA FASTNER (BOLT) PULLED THROUGH. ACFT GROUNDED. R & R NR 1 ENGINE FAN DUCT PANEL AT 9:00 POSITION SECURED IAW AMM 72-23-07.SDR ASAA2014030807115Panel · damagedNR 2 ENGINE INLET AND FAN BLADES, DETAIL INSPECTION FOUND NR 5 STRUT PANEL LT MIDDLE FASTENER ATTACHMENT DAMAGED. ACFT GROUNDED. R & R STRUT PANEL ON NR 2 ENGINE IAW AMM 72-23-07.SDR ASAA2014021206842Spinner · damagedWHILE ACCOMPLISHING ENGINE INLET INSPECTION ON NR 2 ENGINE, FOUND SPINNER FRONT CONE WITH MORE THAN 50 PERCENT MISSING ANODIZED COATING. ACFT GROUNDED. ON DEFERRAL.SDR ASAA2014021106833Shim · wornALL FAN BLADE SHIMS HAVE WORN COATING. ACFT GROUNDED. REPLACED FAN BLADE SHIMS IAW T/C 78472002, STEP 44.SDR ASAA2014020106745Shim · damagedNR 2 ENGINE FAN BLADE SHIMS HAVE DAMAGED COATING. ACFT GROUNDED. R & R NR 2 ENGINE FAN BLADE SHIMS IAW TASK CARD 78472002.SDR ASAA2014013006746Bolt · looseNR 1 ENGINE FAN DUCT PANEL AT 10:00 POSITION HAS LOOSE BOLTS. ACFT GROUNDED. TIGHTENED LOOSE BOLTS.SDR USAA2014011000006Seal · out of positionCLT FLT 706 EN-ROUTE MCO TO CLT. DURING CLIMB OUT, THE LT ENG N1 EICAS VIBRATION WAS HIGH, READING 2.8. ENG INDICATIONS WERE NORMAL. VIBRATION RETURNED BELOW 2.5 WITH THRUST LEVER RETARDED TO IDLE, ENG WAS NOT SHUT DOWN. THERE WAS NO VIBRATION FELT AT CRUSDR CALA2014010990114Liner · damagedNR 2 ENG ATTRITION LINER AT 5:30 POSITION IS MISSING A SECT 1 1-4 BY 5-8 & AT 6:00 1-4 BY 1-2.SDR CALA2013123194061Inlet Bullet · damagedNR 2 ENG RUBBER SPINNER CAP MISSING. R & R INLET CONE ON NR 2 ENG.SDR CALA2013122693942Acoustic Liner · damagedACOUSTIC LINER ON ENG 1 AT 8 O'CLOCK REPAIR CAME UNDONE LEAVING HOLE IN LINER. GRAPHITE MATERIAL MISSING & HONEYCOMB EXPOSED APPROXIMATELY 1.250 X.500 JUST AFT OF PREVIOUS REPAIR AT 8 O'CLOCK POSITION. MUST FIX IAW MT 71-006 ITEM 8. REPAIRED NR 1 ENG INLET SDR CALA2013121993805Acoustic Liner · damagedNR 2 ENG 6 O`CLOCK POSITION 2 INCH BY 1 DAMAGE IS IN ACOUSTICAL MATERIAL APPROXIMATELY 4 INCHES FROM AFT FLANGE. IAW MT71-006G FOR ALLOWABLE LIMITS. IAW ECRA 7111-01489 FOR ALLOWABLE FLY ON CRITERIA. INSPECTED IAW ECRA 7111-0 1489 & FOUND TO BE OK FOR CONTISDR ASAA2013121696901Shim · wornNR 1 ENGINE FAN BLADE SHIMS REQUIRE REPLACEMENT. ACFT GROUNDED. R & R FAN BLADE SHIMS IAW T/C 78472002.SDR ASAA2013120596635Shim · wornNR 1 ENGINE FAN BLADE SHIMS HAVE COATING WORN. ACFT GROUNDED. REPLACED SHIMS FROM NR 1 ENGINE FAN BLADES REF T/C 78472002.SDR ASAA2013120496634Spinner · damagedWHILE ACCOMPLISHING ENG INLET INSPECTION ON NR 2 ENGINE, FOUND FRONT SPINNER 50 LOSS OF ANODIZED COATING. ACFT GROUNDED.SDR ASAA2013120396592Shim · worn24 EA SHIMS ON NR 1 FAN BLADES HAVE COATING WORN. ACFT GROUNDED. R & R 24 EA SHIMS ON NR 1 ENGINE FAN BLADES, REF T/C 78472002.SDR ASAA2013112596482Seal · debondedNR 2 ENGINE TREND DATA SHOWS A SUDDEN INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS. DATA SCATTER INDICATES HARDWARE INSPECTION AND FAN LUBE REQUIRED. ACFT GROUNDED. PERFORMED FAN BLADE LUBE IAW T/C 78472002. REPLACED ALL 24 PLATFORM RUBBER SEALS, DISBONSDR ASAA2013111696429Shim · wornACCOMPLISHING FAN BLADE LUBE, NR 1 ENGINE IAW T/C 784725002. FOUND ALL FAN BLADE SHIMS MISSING MORE THAN 25 MOLYDAG COATING ON PRESSURE FACE IAW MM 72-21-02-200-801 STEP 2(L), (1), (B), (1) GROUNDED. ALL 24 SHIMS R & R ON T/C 78472002, ON NR 1 ENG.SDR CALA2013111492939Acoustic Liner · damagedNR 2 ENG ACOUSTICAL PANEL CHUNK MISSING 6 O'CLOCK WITH ANOTHER SMALLER PIECE LOOSE. INSPECTED FAN CASE ATTRITION LINER IAW MT72-017 REV E. REMOVED LOOSE PIECE OF LINER APPROXIMATELY 0.250 INCH DIAMETER. DAMAGE IS LESS THAN 20% OF PANEL & TO BE REPAIRED WITHSDR CALA2013111492937Liner · damagedENG 1 INLET LINER HAS APPROXIMATELY 1-2 IN HANGING DOWN LOOSE AT 12 O'CLOCK POSITION.SDR ASAA2013111296393Blades · damagedFAN BLADE PLATFORMS FOUND WITH SEAL DAMAGE DURING ABRADABLE SHROUD REPAIR. ACFT GROUNDED. REPLACED ALL FAN BLADE PLATFORMS IAW T/C 78472002. PERFORMED VIBRATION SURVEY TEST 7 IAW MM 71-00-00-700-814-F00. NO DEFECTS NOTED.SDR ASAA2013111296386Frame · damagedDURING NR 1 ENGINE INLET AND FAN BLADES DETAILED INSPECTION. FOUND DAMAGE AROUND FASTENER HOLE ON NR 5 GLASS FAN FRAME PANEL. ACFT GROUNDED. R & R NR 1 ENGINE LPTACC SCOOP NR 5 FAN DUCT PANEL IAW AMM 72-23-07.SDR ASAA2013110796337Seal · looseNR 2 ENGINE FAN BLADE PLATFORM RUBBER SEAL CAME LOOSE. ACFT GROUNDED. CUT AND REMOVED ABOUT .5" OF LOOSE RUBBER SEAL MATERIAL ON NR 2 ENG, NR 1 FAN BLADE PLATFORM REF AMM 72-21-02, PG 7, STEP I (5) B. OK FOR SERVICE.SDR ASAA2013110696310Shim · wornWHILE ACCOMPLISHING NR 2 FAN BLADE LUBE FOUND SHIMS TO BE WORN. ACFT GROUNDED. R & R SHIMS REF TC 78472002.SDR ASAA2013110696296Blade · wornNR 2 ENGINE TREND DATA SHOWS A GRADUAL INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS. DATA SCATTER INDICATES HARWARE INSPECTION AND FAN LUBE REQUIRED. ACFT GROUNDED. ACCOMPLISHED FAN BLADE LUBRICATION REF TASK CARD 78472002. BLADE PLATFORMS SHOW EVIDENCESDR CALA2013110792720Acoustic Liner · damagedACOUSTIC LINER NEEDS TO BE REEXAMINED FOR INTEGRITY. MORE DAMAGE NOTED AT 1 O'CLOCK POSITION. PREVIOUS REPAIRS AT 2:00 POSITION & 7:00 POSITION. NR 2 ENG INLET ATTRITION GRC LAYER REQUIRE PERM REPAIR IAW A320 MT 72-017. DAMAGE LESS THAN 20 PERCENT, PLACED SDR CALA2013110692691Acoustic Liner · deterioratedACOUSTIC PANEL REPAIR ENG 2 HAS DETERIORATION. PLACED NR 2 ENG ATTRITION LINER AT 8 O'CLOCK POSITION ON CF873, NO LOOSE MATERIAL & GRC LAYER NOT PUNCTURED, IAW MT 72-017.SDR ASAA2013103196272Shim · wornWHILE CONDUCTING FAN LUBE, ON NR 2 ENGINE, IT WAS NOTED THAT THE MOLY DAG COATING ON ALL BLADE SHIMS IS WORN OFF. ACFT GROUNDED. REPLACED ALL FAN BLADE SHIMS IAW T/C 78472002 ON NR 2 ENG.SDR CALA2013103092513Acoustic Liner · damagedENG 2 ACOUSTIC LINER 11 O’CLOCK POSITION HAS 1 IN CHUNK MISSING. ACCOMPLISHED REPAIR IAW MT-72-017.SDR ASAA2013102896246Shim · damagedWHILE CONDUCTING FAN LUBRICATION, NOTED THAT ALL FAN BLADE SHIMS MISSING MOLYDAG COATING. ACFT GROUNDED. R & R ALL FAN BLADE SHIMS IAW T/C 78472002.SDR CA131105003Fan · seized(CAN) BASED ON PRELIMINARY INFORMATION, THE ENGINE SUFFERED IFSD UNDER UNKNOWN CIRCUMSTANCES. POST FLIGHT INSPECTION REVEALED THE FAN ROTOR SEIZED. NO FURTHER INFORMATION AVAILABLE AT THIS TIME.SDR ASAA2013102496229Shim · wornNR 1 ENGINE FAN BLADE SHIMS MOLYDAG COATING WORN. ACFT GROUNDED. R & R SHIMS WITH NEW IAW T/C 78472002 ON NR 1 ENGINESDR CALA2013102492371Inlet Bullet · damagedNR 2 ENG REAR SEGMENT OF INLET CONE FAILED INSPECTION. HAS NUMEROUS CRACKS & PEELING OF FIBERS. FAILED INSPECTION IAW MM 72-31-01 STEP 2E 2CB NOTE AREA & STEP 2 A, PEELING OF FIBERS. R & R REAR CONE.SDR ASAA2013101896196Shim · wornNR 2 ENGINE FAN BLADE SHIMS WORN ON BLADES 1, 2, 13, & 14. ACFT GROUNDED. REPLACED FAN BLADE SHIMS IAW 72-21-02-00-802-F00.SDR ASMF201311080007Blades · nickedDURING TRANSIT CHECK, DETECTED NICKS IN FOUR FAN BLADES OF THE LT ENGINE. MAINTENANCE PERFORMED REVISION DETECTING TWO NICKS WITHIN OPERATIONAL LIMITS IAW MM 72-21-02. LT ENGINE FAN BLADES REPAIRED IAW AMM 72-21-02 PAGE 804, FIG 802.SDR MASA2013101516788Blade · lack of lubeENGINE 1 HIGH VIBRATION. ENGINE FAN BLADE INSPECTED, BLADE SHAKE, & VIBRATION CHECK ENGINE RUNS COMPLIED WITH. FAN BLADE LUBRICATION COMPLIED WITH ENGINE VIBRATION CHECK WITHIN LIMITS.SDR ASAA2013101196167Panel · gougedNR 2 ENGINE, NR 5 FAN DUCT PANEL FOUND TWO FORWARD FASTENERS HAVE GOUGED & ELONGATED HOLES INTO FAN CASE. ACFT GROUNDED. REMOVED NR 5 FAN DUCT PANEL 72-23-07 MM. SUBJECT DEFECT AREA CHECKED/INSPECTED & DETERMINED TO BE WITHIN CONTINUE IN SERVICE LIMITS IAW SDR CALA2013101592063Inlet · damagedNR 2 ENG INLET BETWEEN 8 & 9 O'CLOCK POSITION. HAS SMALL DAMAGED TO COMPOSITE AREA.SDR CALA2013101191977Inlet · damagedNR 2 ENG INLET BETWEEN 8 & 9 O'CLOCK POSITION, HAS SMALL DAMAGED TO COMPOSITE AREA.SDR CALA2013101191962Inlet · damagedNR 2 ENG INLET BETWEEN 8 & 9 O'CLOCK POSITION HAS SMALL DAMAGED TO COMPOSITE AREA.SDR ASAA2013100896138Panel · wornNR 2 ENG INLET AND FAN BLADES, DETAILED INSPECTION. FOUND NR 1, 12 O`CLOCK POS RT, FAN STRUT PANEL HAS ONE FASTENER WORN THRU PANEL, AFT LT SIDE. ACFT GROUNDED. R & R NR 1, 12 O`CLOCK POS RT FAN DUCT PANEL REF AMM 72-23-07-400-801-F00.
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