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 CALA2013100791793Liner · missingNR 2 ENG INTAKE INSULATION AT 2 O'CLOCK POSITION HAS COME OFF. ACTUAL IS ATTRITION LINER MISSING 1X1 SECTION AT THE 11 O'CLOCK POSITION. MUST BE REPAIRED IAW MT 72-017 WITHIN 20 CYCLES. REPAIRED ATTRITION LINER IAW MT 72-017.SDR ASAA2013100596112Shim · wornNR 2 ENGINE FAN BLADE SHIMS WORN. ACFT GROUNDED. R & R .SDR CALA2013100791776Guide Vane · crackedNR 2 ENG FOUND CRACKED GUIDE VANE ON WALK AROUND INSPECTION. ONE EACH ALUMINUM EXIT GUIDE VANE REMOVED FROM THE ONE O'CLOCK POSITION, ENG SN 727114. INSTALL REPLACEMENT VANE DURING NEXT ENGINE SHOP VISIT SINCE ENGINE HAS LESS THAN 500 CYCLES REMAINING TO SHOSDR ASMF201311080002Blades · damagedACFT RETURNED DUE TO THE LT ENGINE VIBRATION REACHING 6.0 UNITS. FLIGHT CREW ACCOMPLISHED QRH 7.24 PROCEDURE AND VIBRATION WAS STABILIZED IN 4.0 UNITS. MAINTENANCE DETECTED A CRACK ON FOUR FAN BLADES 1 INCH LONG AND 0.750 INCHES IN DEPTH, CRACKS OUT OF LIMITSDR UA2R20131001007Inlet · crackedDURING INSPECTION FOUND NR 1 ENGINE INLET CRACKED AT THE RIVET ATTACHING THE BRACKET FOR THE INLET HEAT DUCT. CRACKED WHERE THE INLET IS STARTING TO CURVE.SDR CA131001011Housing · damaged(CAN) DURING INITIAL INSTALLATION THE UPPER AND LOWER HALVES ARE MATED TOGETHER WHILE BEING INDIVIDUALLY FITTED TO EACH ACFT. THE UPPER HOUSING HAS A SHORT EXTENDED LIP AT HE AFT OF THE HOUSING TO ALLOW FOR THE ADJUSTMENT FOR THE CUSTOM FIT. THE EXCESS APPROSDR CNMA20131004001Frame · corrodedCORROSION ON LOWER FAN CASE FRAME FROM 5 TO 7 O`CLOCK POSITION BLENDED AND FOUND TO BE OUT OF LIMITS. R & R FAN CASE.SDR XCGA60ES92013Actuator · inoperativeON DESCENT, THE RIGHT ENGINE SHUTDOWN AND THE FADEC FAIL RT CAS MESSAGE ILLUMINATED. PILOTS ATTEMPTED TO RESET THE FADEC WITHOUT SUCCESS AND THEN COMPLIED WITH THE EMERGENCY CHECKLIST. THE AIRPLANE LANDED WITHOUT INCIDENT AND WAS TURNED OVER TO MX AT THE SERSDR ASAA2013091795997Shim · wornWHILE ACCOMPLISHING FAN BLADE LUBE ON NR 1 ENGINE, . FOUND 24 SHIMS COATING WORN REF T/C 78472001. ACFT GROUNDED. REPLACED SHIMS IAW TASK CARD 78472002.SDR CA130919002Fan · failed(CAN) CREW REPORTED ENGINE VIBRATION, DURING VISUAL INSPECTION FOUND FAN CASE ABRADABLE MATERIAL WORN OUT. (TC# 20130919002)SDR QMLA2013091113132Actuator · wornDURING AN AIRWORTHINESS CHECK, THE ENGINE AIR INLET BYPASS DOORS, OBSERVED NR 2 BYPASS DOOR WOULD NOT FULLY CLOSE. AFTER INSPECTION, FOUND ACTUATOR MOUNTING BOLT TO THE TRANSMISSION COWLING SIDE HAD WORN THROUGH ACTUATOR MOUNTING HOLE CAUSING THE DOOR NOT TOSDR ASAA2013090895938Duct · wornWHILE PERFORMING FOD INSPECTION NR 2 ENGINE, FOUND NR 3 FAN DUCT PANEL FASTENER HOLES WORN THROUGH. ACFT GROUNDED. REPLACED NR 3 FAN DUCT PANEL REF MM 72-23-07-000-801-F00.SDR CALA2013090991116Repair · debondedNR 2 ENGINE INTAKE RUB STRIP-5 O'CLOCK POSITION. PREVIOUS REPAIR DISBONDED LESS THAN 3 INCHES. CARRIED FWD IAW THE AMM & TOMC FOR 500 HOURS OF 200 CYCLES. IF UNABLE TO REPAIR PLEASE UPDATE WITH TIME & PARTS REQUIRED.SDR CA130905003Vane · torn(CAN) WHILE PERFOMING AN INSPECTION AN AME NOTED THAT THE ICE VANE INLET ROTATING PANEL HAD A LARGE TEAR IN IT. THE HINGE PIN WAS FOUND TO HAVE MIGRATED OUT OF THE PIANO HINGE HALVES. THIS CAUSED STRESS ON THE ICE VANE PANEL CAUSING IT TO FAIL. THE PIANO STYSDR CA130910008Fan · lack of lube(CAN) STRANGE NOISE FROM ENGINE NR 1 AND VIBRATION. FAN LUBRICATION CARRIED OUT AFTER BOROSCOPE INSPECTION. ACFT RETURNED TO SERVICE.SDR CALA2013090591002Repair · missingNR 2 ENGINE ATTRITION LINER PREVIOUS REPAIR IAW MT72-017 HAS 1" X 1" MISSING AT 6:00 POSITION REPAIRED MISSING AREA IAW MT 72-017.SDR UA2R20130910004Duct · crackedDURING INSPECTION, FOUND NR 2 ENGINE FWD AIR INLET DUCT CRACKED AT THE OTBD RIVET THAT ATTACHES THE BRACKET FOR THE INLET HEAT DUCT. CRACKED WHERE THE INLET IS STARTING TO CURVE.SDR UA2R20130910003Duct · crackedDURING INSPECTION, FOUND NR 1 ENGINE FWD AIR INLET DUCT CRACKED AT THE INBD RIVET THAT ATTACHES THE BRACKET FOR THE INLET HEAT DUCT. CRACKED WHERE THE INLET IS STARTING TO CURVE.SDR CALA2013081990526Nose Cowl · crackedNR 1 ENGINE NOSE COWL INNER SKIN AT 4 O'CLOCK POSITION HAS A CRACK INDICATION. LENGTH OF CRACK 0.300" AND TERMINATES INTO FASTENER HOLE.SDR CALA2013082090593Fastener · missingFOUND TWO NOSE CONE INNER BARREL RIVETS MISSING AT THE SIX O'CLOCK POSITION. REPLACED MISSING RIVETS ON NUMBER ONE ENGINE REFERENCE MT 71-002.SDR ASAA2013081595806Panel · damagedNR 1 ENGINE FAN DUCT PANEL NR 1 HAS SCREW PULLED THRU. ACFT GROUNDED. R & R NR 1 ENG NR 1 FAN DUCT PANEL REF AMM 72-23-07.SDR ASAA2013080795751Shim · wornCOATING WORN ON FAN BLADE SHIMS NR 1 ENGINE. NR 1 ENGINE FAN BLADE PLATFORM SEALS ARE TORN. ACFT GROUNDED. R & R SHIMS. R & R FAN BLADE PLATFORMS IAW MM 71-00-00.SDR AALA20130804005Bullet · obstructedDFW CREW REPORTED AFTER TAKEOFF DURING CLIMB OUT RPM VARIED ON LT ENGINE. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT ENGINE INLET BULLET THAT HAD DEBRIS. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.SDR ASAA2013073195708Shim · wornNR 2 ENGINE FAN BLADE SHIMS COATING WORN. ACFT GROUNDED. REPLACED NR 2 ENGINE FAN BLADE SHIMS IAW T/C 78472002.SDR ASAA2013072895693Shim · wornFAN BLADE SHIMS REQUIRE REPLACEMENT DUE MISSING MOLYDAG. FAN RETAINING FLANGE AXIAL STOP PINS DETERIORATED. FAN DISK / RETAINING RING ELASTOMER SPACERS DETERIORATED. ACFT GROUNDED. REPLACED FAN BLADE SHIMS REF TASK CARD 78472002 FOR INSTALLATION. REPLACEDSDR ASAA2013071695616Panel · wornFOUND FAN DUCT PANEL NR 1 WITH FASTENERS WORN THRU PANEL ON NR 1 ENGINE INBD SIDE OF 1200 STRUT. ACFT GROUNDED. REPLACED FAN DUCT PANEL REF MM 72-23-07.SDR ASAA2013062495293Panel · looseNR 1 ENGINE FAN DUCT PANELS LOOSE, 1130 -1200 O`CLOCK POSITION AND 230- 300 POSITION AFT LOOKING FORWARD. ACFT GROUNDED. REMOVED PANELS AS REQUIRED, INSTALLED SERVICEABLE PANELS IAW AMM 72-23-07-400-801-F00.SDR UALA2013061704188Acoustic Liner · damagedHOLE IN ACCOUSTIC LINING ON NR 2 ENGINE.SDR ASAA2013061595114Spinner · damagedNR 1 ENGINE INLET SPINNER FRONT CONE MISSING PAINT AND ANODIZED COATING. ACFT GROUNDED. NR 1 ENGINE R & R INLET SPINNER FRONT CONE IAW TC 78472002.SDR ASAA2013061595113Shim · wornNR 1 ENGINE, TWENTY FOUR FAN BLADE SHIMS WORN. ACFT GROUNDED. R & R SHIMS IAW T/C 78472002.SDR UALA2013061804210Liner · damagedNR 2 ENG FAN CASE ATTRITION LINER HAS MISSING MATERIAL AT THE 6 O'CLOCK POSITION. ACCOMPLISHED ATTRITION LINER REPAIR, REF MT 72-017.SDR ASAA2013053194950Shim · worn24 NR 1 ENGINE FAN BLADE SHIMS WORN. ACFT GROUNDED. R & R NR1 ENGINE FAN BLADE SHIMS, 24EA IAW T/C 78472002.SDR ASAA2013052495437Skin · dentedNR 2 ENGINE INLET COWL INNER SKIN DENTED AT 6:30 O`CLOCK POSITION 5 FROM AFT EDGE. ACFT GROUNDED. REPAIRED NR 2 ENGINE INLET COWL INNER SKIN IAW EA 400-71EA-10607, REV NEW ISSUED 6/28/13.SDR ASAA2013051594833Spinner · wornWHILE ACCOMPLISHING NR 2 ENG INLET INSPECTION T/C NR 78472000, FOUND SPINNER FRONT CONE WITH MORE THAN 50 MISSING ANODIZED COATING MISSING. ACFT GROUNDED. R & R NR 2 ENG FRONT SPINNER REF AMM 72-21-01.SDR ASAA2013051094780Shim · wornNR 1 ENGINE FAN BLADE SHIMS WORN. ACFT GROUNDED. NR 1 ENGINE R & R FAN BLADE SHIMS IAW T/C 78472002.SDR ASAA2013042494612Panel · damagedNR 2 ENGINE FAN DUCT PANELS AT 1130 AND 1230 POSITIONS HAVE ONE PULLED THRU BOLTS. ACFT GROUNDED. R & R FAN DUCT PANELS IAW AMM 72-23-07.SDR UALA2013042402846Inlet · dentedNR 1 ENGINE INLET COWL DENTED. REPAIRED.SDR IXXA20130415009OBlades · damagedCOMPLIED WITH ATI BIRD STRIKE INSPECTION JOB CARD 13.01-4. DAMAGE WAS FOUND TO NR 13 AND 14 FAN BLADES. R & R 44C1 FAN BLADES IAW AMM 72-21-00. OPS CHECKS GOOD IAW ENGINE RUN HANDBOOK 70.01.SDR IXXA20130415009Blades · damagedON POST FLIGHT INSPECTION, FOUND EVIDENCE OF BIRD STRIKE TO THE NR 3 ENGINE. DAMAGE WAS FOUND TO THE NR 12 AND NR 13 FAN BLADES. C/A TO FOLLOW.SDR UALA2013041502540Acoustic Panel · delaminatedCREW REPORT: A PREVIOUS PATCH OF THE ACOUSTIC PANEL ON THE NR 2 ENGINE APPEARS TO BE DELAMINATED. SAMC TEXT: FBO REPORTS 2 AREAS OF PREVIOUS ATTRITION LINER REPAIR IS SEPARATING. ONE AREA IS APPROX 2 INCH IN DIAMETER AND THE OTHER IS 1 INCH IN DIAMETER. OKSDR UALA2013041002414Acoustic Panel · damagedACOUSTICAL PNL ON INLETOF ENG 2 MISSING A CHUNK AT THE 6 O'CLOCK POSITION. FAN CASE ATTRITION LINER HAS MISSING MATERIAL AT 6 O'CLOCK POSITION TOP LAYER MEASURING 2"X 1.750" NEEDS TO BE REPAIRED WITHIN 20 CYCLES. RPR- :REPAIRED ATTRITION LINER AT 6 O'CLOCK PSDR ASAA2013040994436Disk · damagedNR 2 ENG, FAN DISK SLOTS 2, 7, 9, 13 & 20 ARE WORN FROM BUCKLED SHIMS. GREATEST FOUND TO BE .0095. COATING WORN ON ALL SHIMS. REAR SPINNER IS NICKED AT SURFACE AREA D. PLATFORMS NR 4,10 & 24 ARE NICKED ON FWD LUG. FAN BLADES NR 1,4 & 21 ARE FROM SHIM CONTACSDR UALA2013040502279Acoustic Panel · damaged1 ENG ACOUSTIC MATERIAL AT 6 O'CLOCK POS IS MISSING BY AN AMOUNT OF HALF A BASEBALL. INSPECTED PER MX TIP LESS THAN 20 PERCENT MUST BE REPAIRED WITHIN 20 CYCLES (PARTS: 841-0591 ADH3002-48 ADHESIVE)SDR ASAA2013040394340Shim · wornWHILE ACCOMPLISHING T/C 78472002 FOUND TWENTY FOUR FAN BLADE SHIMS WORN ON NR 1 ENGINE. REPLACED ALL FAN BLADE SHIMS REF T/C 78472002.SDR ASAA2013040194318Shim · wornNR 1 ENGINE FAN BLADE SHIMS WORN. ACFT GROUNDED. R & R TWENTY FOUR FAN BLADE SHIMS REF T/C 78472002.SDR UALA2013032801990Nose Cone · crackedON NR 1 ENGINE NOSE CONE ON CIRCULAR RETAINER WITH 6 BOLTS. METAL AROUND A BOLT HAS CRACK. PLACED ON CF PER AMM 72-38-11-200-010-B13. MUST BE INSPECTED PRIOR TO EACH DEPARTURE. MUST BE REPAIRED BY "C" CHECK. INF- : REPLACE SPINNER FAIRING 1ST AVAILABLE PCNSDR EE4Y2013032000031Acoustic Liner · delaminatedENGINE NR 1 NOSE COWL ACOUSTIC INNER BARREL INNER SKIN WITH DELAMINATION. THE MENTION DAMAGE WAS REPAIRED UNDER NRI A1B089 4-3 AND EO# COO-CMP9-54-035-13.SDR ASAA2013031994207Panel · wornNR 2 ENGINE INLET AND FAN BLADES DETAILED INSPECTION. FOUND FAN DUCT PANEL NR 5 AT APPROX 430 O`CLOCK POS (ALF) HAS DAMAGED FASTENER HEADS FROM BEING LOOSE. REPLACED NR 5 FAN DUCT PANEL FASTENERS REF MM 72-23-07.SDR CA130318016Vane · damaged(CAN) THE FWD RIVET LINE AT THE PIVOT ROD/SKIN ATTACH POINT RIVETS WERE FOUND LOOSE. THERE WAS NO INDICATION OF THESE RIVETS BEING LOOSE, THERE WAS NO SMOKE TRAILS OR BLACK RESIDUE NOTED ANOUND THESE RIVETS. THIS RIVET LINE IS NOT VISIBLE TO INSPECT WITH THE SDR UALA2013031201470Inlet · dentedRAMP REPORT DENT ON NR 1 ENGINE INLET COWL SKIN. PERFORMED INTERIM REPAIR PER ECRA 5411-01066 PART 1 INTERIM STEPS 1-4. INITIATED CF TO INSPECT PER PART 2 AT INTERVALS NOT TO EXCEED 3 DAYS AND PERFORM PERMANENT REPAIR PER PART 3 WITHIN 15 DAYS. CW PART 2 O
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