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 ASAA12510951Paint · missingNR 1 ENGINE INLET SPINNER FRONT CONE MISSING MORE THAN 50 PERCENT OF WHITE ANTI EROSION PAINT. REMOVED AND REPLACED NR 1 ENGINE INLET SPINNER FRONT CONE REF T/C 78472002.SDR ASAA12510939Cone · damagedNR 2 ENG SPINNER FRONT CONE MISSING BLACK COATING. GROUNDED YES. REPLACED NR 2 ENGINE FRONT SPINNER CONE ASSY REF T/C 78472002.SDR ASAA12510882Panel · looseWHILE ACCOMPLISHING ENGINE INLET AND FAN BLADE INSP FOUND FAN DUCT PANELS LOOSE. PANELS NR 6, 7, 8, 9 AND 12. TIGHTEN SCREW ON FAN DUCT PANEL NR 1 ENG REF MM 72 23 07.SDR ASAA11510832Shim · damagedNR 1 ENGINE BLADE SHIMS PROTECTIVE COATING WORN. NR 1 ENGINE REPLACED SHIP SET OF BLADE SHIMS IAW TASKCARD NR 78472002. 24 FAN BLADE SHIMS REPLACED.SDR ASAA11510831Seal · tornNR 1 & NR 5 PLATFORM SEALS TORN ON NR 1 ENGINE. REPLACED NR 1 & NR 5 PLATFORMS IAW TASKCARD 78472002.SDR ASAA11510829Spinner · damagedHELICOIL CAME OUT FROM SPINNER ON REMOVAL. REPLACED FRONT SPINNER CONE IAW TASKCARD # 78472002.SDR ASAA11510799Panel · damagedREF T/C #78472000 NR 2 ENG FAN AND INLET INSP FOUND NR 12 FAN FRAME STRUT DUCT PANEL A HAS FWD AFT SCREW (LT SIDE) LOOSE AND HAS DAMAGED PNL. REPLACED NR 2 ENG NR 12 FAN DUCT PANEL REF MM 72 23 07.SDR ASAA11510711Screw · looseREF T/C 78472000 NR 2 ENG INLET & FAN BLADES DETAILED INSP FOUND STRUT PNL BETWEEN STRUTS 8 & 9 POS HAS LWR FWD FAST LOOSE. TORQUED BOLT TO 61 IN LBS PER AMM 72 23 07 400 801. OK FOR SERVICE.SDR ASAA11510599Liner · delaminatedNR 1 ENGINE INLET ABRADABLE SHROUD AT 5 O'CLOCK LOOKING INTO FAN IS DELAMINATED APPX 12" LENGTH REF T/C 78472000. COMPLETED ABRADABLE SHROUD REPAIR THRU F 6 C REF 72 24 02 200 802 F00. COMPLETED ABRADABLE SHROUD REPAIR 6(D) 10(A) PER MM REF 72 24 02 200 802 SDR ASAA11510511Screw · out of balanceNR 1 ENGINE VIRBRATION 1.0 TO 1.1 GREATER THAN 1 MINUTE WHEN OPERATING AT MAX CONT THRUST. PERFORMED FAN TRIM BALANCE ON NR 1 ENGINE IAW ALASKA B737NG AMM 71 00 00 750 803 FOO. CHANGED NR 8 TO PO7 NR 18 TO PO7 NR 21 TO PO8 AND 28 TO PO8 USING NR T8484F. PESDR ASAA11510492Panel · damagedREF T/C #78472000 NR 1 ENG INLET AND FAN BLADE INSP FOUND NR 1 STRUT PNL BETWEEN NR 1 AND NR 2 ENG STRUTS HAS ONE FASTENER PULLED THRU PANEL. REPLACED NR 1 STRUT PANEL BETWEEN NR 1 AND NR 2 ENG STRUTS PER AMM 72 23 07.SDR MASA2011091463680Actuator · leakingFUEL LEAK RT ENG DRAIN MAST DURING PUSH. R2 SLAVE VG ACTUATOR.SDR ASAA11510346Inlet Bullet · damagedFOUND FWD SPINNER FOR FAN BLADES ON NR 1 ENGINE BLACK ANODIZED COATING MISSING GREATER THAN 50 PERCENT. REMOVED AND REPLACED FWD SPINNER FOR FAN BLADES ON NUMBER 1 ENGINE PER MM 72 21 01 400 801 F00.SDR CA110826001Inlet · cracked(CAN) REAR INLET CASE HAD A THROUGH GOING CRACK AT THE STRUT LOCATION ADJACENT TO THE FUEL PUMP/OIL PUMP DRIVE. THE CASE WAS NOT A MFG CASTING. 1 VANE OF THE LP IMPELLER HAD A DENT/BEND BEYOND REPAIR LIMITS. THE IMPELLER WAS SCRAPPED. THERE WAS NO EVIDENCESDR C2XA11TY125Case · fodTYS - A/C WAS FERRIED FRON BNA TO TYS FOR FOD DAMAGE WHERE MAINTENANCE REMOVED AND REPLACED THE FAN CASE (PN-145-75001-409-SN-NC1476); MULTIBLE BYPASS VANES (PN-23067033) BOROSCOPE NR 1 ENGINE IAW RR MM 05--50-200-804 AND RR MM 72-50-00-801, NO DAMAGE OR DEFECSDR SROM2011010Case · crackedREPLACED NR 1 ENGINE FAN INLET CASE DUE TO CRACKED FLANGE B WELD WITH OVERHAULED ASSEMBLY; FAN CASE P/N 786269, S/N DX6417, NR 1 BEARING HOUSING P/N 765471, S/N JU7622 AND REAR SUPPORT P/N 5003534-01, S/N LX9712 IN ACCORDANCE WITH PRATT AND WHITNEY MAINTENANCESDR UALA2011070703373Acoustic Panel · damagedCREW REPORT: 6X12 INCH SECTION OF ACCOUSTIC MATL LOOSE AT 6 O`CLOCK JUST AFT FAN BLDS NR 1 ENG. DAMAGED ACOUSTICAL PNL HAS BEEN REMOVED. OK TO CONTINUE IN SERVICE FOR 10T OR 5C. REVIEWED WITH SAMC-EMC. PER ENG SHOP THIS IS THE ANTI-ICE IMPACT PANEL RPR MMSDR EIAA2011080Spinner · malfunctionedNR 2 ENGINE EXPERIENCED SURGE STALL WITH INSTANTANEOUS EGT EVENT AND SHUTDOWN, WITH VIOLENT VIBRATION PRIOR TO EVENT. CREW REPORTED VISIBLE DEBRIS IN AREA OF NR 2 INLET, DUMPED FUEL AND RETURNED TO HIK, NO FIRE REPORTED. FOUND NR 2 ENGINE SPINNER & FAN WITH SDR UALA2011070503297Acoustic Liner · tornCREW REPORT: NR 1 ENGINE HAS A 1 1-2 TEAR IN ACOUSTIC LINING AT THE APPROX 4 O'CLOCK POSITION. SAMC TEXT: LCL CO MAINT REPORTS: ENG1 INLET COWL (NOSE COWL) WIRE MESH HAS A TEAR APPROX.1.250 INCHES AT 7 O'CLOCK. DAMAGE IS WITHIN CARRY FORWARD LIMIT OF MT71-0SDR SWAA114640Inlet Guide Vane · activatedDIVERSION - NR 1 ENGINE HAD 4-5 COMPRESSOR STALLS AFTER STARTING CLIMB FROM 370-390 (37800FT). INSPECTED NR 1 ENGINE FOUND DEBRIS FROM NR 1 ENGINE IGV IN CORE COWL. REMOVED AND REPLACED NR 1 ENGINE IAW MT.SDR ASAA1159922Shim · wornNR 2 ENG FAN BLADES SHIMS WORN. REPLACED 24 FAN BLADE SHIMS MFG P/N 340 252 307 0. REF TC 78472002.SDR ASAA1159921Shim · wornCOATING ON NR 2 ENGINE INLET SPINNER CONE MISSING COATING 24 FAN BLADE PLATFORM SEALS TORN 24 FAN BLADE SHIMS MISSING COATING. REPLACED ENGINE INLET SPINNER CONE PER T/C 78472002 STEP 7, 24 FAN BLADE PLATFORMS P/N 340 001 816 0 INSTALLED PER T/C 78472002 STEPSDR UALA2011060902844Liner · tornNR 2 ENG 10:OCLOCK POSITION SEGMENT FAN EXIT LINER IS TORN APPROX 4-5 INCHES.SDR ASAA1159621Spinner · damagedWHILE ACCOMPLISHING T/C 78472002 FOUND NR 2 ENGINE REAR SPINNER CONE HAS BAD NUT PLATE THREADS. REMOVED/REPLACED NR 2 ENGINE REAR SPINNER CONE REF MM 72 21 01 400 801 F00 & TASK CARD 78472002 UNDER W/O 117757.SDR MASA2011040702358Spinner · vibrationHIGH CONT NR 1 ENG VIB 2.8 MILS CRUISE - RTF. MX REMOVED AND REPLACED SPINNER CORRECTLY AND PERFORMED ENGINE RUNS. VIBE W/IN LIMITS.SDR CA110228014Inlet · vibration(CAN) CREW REPORTED NR 2 ENGINE WAS AT 4.0 UNITS OF FAN VIBRATIONS DURING CLIMB AND AT CRUISE, FLT LEVEL 33, IT WAS 3.4. ACFT TURNED BACK TO BASE. MAINTENANCE CARRIED OUT A FAN BLADE LUBE IAW AMM 72-21-00 AND FOUND 12 PLATFORMS WITH SEALS DAMAGED ALL WITHIN SDR ASAA1158877Seal · unbondedWHILE PERFORMING T/C 78472002 (NR 2 ENGINE FAN BLADE LUBRICATION) FOUND NR 22 PLATFORM'S SEAL UNBONDED (4 INCHES IN LENGTH). REMOVED LOOSE SEAL SECTION. RE-INSTALLED THE NR 22 PLATFORM REF T/C 78472002. REPLACED NR 2 ENGINE NR 22 FAN BLADE PLATFORM REF AMM SDR 2011FA0000108Inlet Screen · wornON RECEPTION FOR MX THE LT ENGINE INLET ACOUSTIC MESH WAS FOUND DEPARTED FROM INLET AREA AT 3PM POSITION TO 6PM POSITION. ENGINE DIGESTED THE MESH CAUSING DAMAGE TO THE INLET CASE & STATOR GUIDE VANES.SDR ASAA1058703Blade · wornNR 2 ENGINE REQUIRES 20 EACH PLATFORMS (FAN BLADE) DUE TO P/N & WEAR. REPLACED 16 EACH FAN BLADE PLATFORMS P/N 340 001 814 0 FOR P/N UPDATE AND 4 EACH P/N 340 001 816 0 PLATFORMS FOR WEAR. ALL FAN BLADE PLATFORMS ARE NOW P/N 340 001 816 0. WORK PERFORMED PESDR CA110105008Phase Relay · failed(CAN) BEFORE TAXIING, THE INLET ANTI ICE WAS TURNED ON, BUT SHOWED THE DEICE LIGHT ON THE 32 ALPHA PANEL AND COULD NOT BE RESET WITH MULTIPLE TRIES AND ENGINE STARTS.SDR C2XA10TY185Inlet · dentedTYS - A/C WAS DESENDING INTO TYS WHEN A BIRD STRUCK THE NR 1 ENGINE INLET. THE CREW CHANGED A/C TO A/C 909 AND CONTINUED ON. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE INLET AFTER BOROSCOPING THE ENGINE. BOROSCOPE REVEAL NO DAMAGE TO THE ENGINE CORE. SDR HALA2010102700492Blade · nickedETOPS SIGNIFICANT SYS - DURING 11K CK RT ENGINE EXTERNAL INSP, FOUND NR 2 ENGINE BLADE NR26 L/E NICKED AREA C. BLENDED OUT DAMAGE TO A DEPTH OF .160 BLADE NR26, NR 2 ENGINE AREA C L/E, NEEDS EDDY CURRENT PRIOR TO 121 HOURS OF OPERATION. REF AMM 72-31-02-308-00SDR DHLA201000132Blades · damagedREF LOG A022635, ITEM 2M: DURING POST MX RUN, WALK AROUND, FOUND HEAVY FOD DAMAGE TO NR4 ENGINE INLET FAN BLADES AND INLET COWLING. NR4 ENGINE WAS REPLACED AS A RESULT OF THE DAMAGE.SDR UALA2010100103642Linkage · brokenNR 1 ENGINE NOT SPOOLING UP PAST 50 PERCENT N1. ACCOMPLISHED ENGINE OVERSPEED INSPECTION CHECK. FOUND INLET GUIDE VANE LINKAGE BROKEN. REPLACED ENGINE.SDR SIMA201026309Frame · corrodedDURING MAINTENANCE BASE VISIT FOUND THE RIGHT ENGINE FRONT FRAME BOLT HOLES HAVE CORROSION. REMOVED CORROSION DEFERRED AND PERMANENT REPAIR REQUIRED AT OR BEFORE 200 FLIGHT HOURS IAW PART B OF EO EM-72MR-115. REMOVED AND REPLACED THE NR 2 ENGINE. THE OPERATSDR ASAA1058270Spinner · unserviceableREF T/C 78472000 NR 1 ENGINE INLET SPINNER CONE MISSING GREATER THAN 20 PERCENT OF BLACK SULFURIC ANODIZING COATING. R & R NR 1 ENG FRONT SPINNER CONE IAW MM 72-21-01.SDR UALA2010081903046Liner · damagedNR 2 ENG ATTRITION LINER IS DAMAGE AT THE 6 O'CLOCK POSITION. FOUND A PIECE MISSING AT THE 6 O`CLOCK POSITION FROM A PREVIOUS REPAIR- APPROX 1.5 INCHES BY .5 INCHES. THE DAMAGE DOES 'NOT' GO INTO THE GRC LAYER AND THERE IS NO LOOSE MATERIAL. ACP REPAIR OF DASDR ASAA1058078Nose Bullet · damagedREF T/C 78472000 NR 2 ENG INET & FAN BLADES DETAILED INSPECTION FOUND FWD NOSE CONE MISSING MORE THAN 20 PERCENT OF ANTI EROSION PAINT & COATING. REMOVED AND REPLACED NR 2 ENG SPINNER CONE REF 72 21 01.SDR ASAA1058052Inlet Bullet · out of limitsWHILE PERFORMING TC 78472000 ENG INLET & FAN BLADES DETAILED INSPECTION FOUND FORWARD SPINNER CONE OUT OF LIMITS. REMOVED AND REPLACED NR 2 FORWARD SPINNER CONE REF MM 72 21 01.SDR ASAA1058021Paint · missingNR 1 ENG FWD NOSE CONE MISSING PAINT OVER 50 PERCENT. PULLED AND TAGGED START VALVE BREAKER. REMOVED AND REPLACED NR 1 ENG FWD NOSE CONE REF AMM 72 21 01 000 801. RESET START VALVE BREAKER. SEAMC NOTIFIED.SDR AALA20100620DFW14Nose Cone · defectiveDFW - CREW REPORTED AUTOPILOT AND AUTO THROTTLE KICKED OFF AND BOTH ENGINES EXPERIENCED LOW EPR INDICATIONS. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE NOSE CONE ASSEMBLY AND TWO PT7 LINES OSDR ASAA1057883Nose Bullet · wornPER T/C 78472000 PG 3 PAR D FRONT SPINNER EXHIBITS MORE THAN 20 PERCENT BLACK ANODIZED COATING LOSS NR 2 ENGINE. REMOVED AND REPLACED NR 2 SPINNER CONE FRONT REF MM 72 21 01.SDR ASAA1057652Spinner · damagedWHILE ACCOMPLISHING FAN LUBE ON NR 1 ENG FOUND NOSE SPINNER FRONT CONE MISSING ANODIZED COATING. REMOVED AND INSTALLED SERVICEABLE NOSE CONE IAW TASK CARD 78472002 FAN BLADE LUBRICATION.SDR MASA2010032500235Probe · contaminatedNR 1 ENGINE N2 ZERO ON TAKEOFF. FOUND OIL CONTAMINATION IN PROBE, CONNECTOR CLEANED AND OPS GOOD.SDR AALA20100226MIA01Acoustic Panel · defectiveMIA - CAPTAIN REPORTED LOUD NOISE FROM LEFT ENGINE AND VIBRATIONS AT LEFT NUMBER 2 DOOR ON TAKEOFF NO ANOMALIES WITH GAUGES OR AIRCRAFT. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE ACOUSTIC PANEL AND ADJUSDR ASAA1057417Shroud · damagedTWO (2) EA CRATERS FOUND IN ABRADABLE SHROUD NR 2 ENGINE AT 10 O’CLOCK AND 11 O’CLOCK POSITION. CRATER AT 10 O’CLOCK MEASURES 1.75 X 1.5 CRATER AT 11 O’CLOCK MEASURES 1.0 X .75 REPAIR OF BOTH CRATERS MUST BE ACCOMPLISHED IN 50 CYCLES OR 75 HOURS WHICHEVER COMSDR ASAA1057376Paint · missingNR 2 ENG FRONT SPINNER CONE FOUND MISSING PAINT, MORE THAN 20 PERCENT. REPLACED NR 2 ENG SPINNER CONE FRONT, REF MM 72 21 01 000 801 F00 72 21 01 400 800 F00.SDR SIMA200935504Engine · odorAFTER LANDING THE CREW OF FLIGHT 3762 REPORTED A STRONG ELECTRICAL SMELL IN THE COCKPIT. AFTER ENGINE RUNS A STRONG OIL SMELL WAS PRESENT IN THE COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED ENGINE RUN PER THE GROUND HANDLING CHECKLIST AND FOUNDSDR ASAA0957003Paint · missingWHILE PERFORMING TASK CARD NR 78472000, NR 1 ENG INLET AND FAN BLADES INSPECTION. FOUND MORE THAN 20 PERCENT OF BLACK SULFURIC ANODIZING PAINT MISSING ON SPINNER FRONT CONE. ACFT GROUNDED. NO CORROSION NOTED AT THIS TIME. REPLACED NR 1 ENGINE SPINNER.SDR ASAA0956808Spinner · damagedWHILE PERFORMING T/C 78472000 ENGINE INLET INSP FOUND NR 2 ENG FRONT SPINNER CONE MISSING APPROX MORE THAN 20 PERCENT OF BLACK ANODIZING COATING. REPLACED NR 2 ENGINE FOR PERFORMANCE POSITIONING.
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