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 ASAA2015110113585Case · crackedNR 1 ENGINE, B1 FLANGE 11.00 O'CLOCK POSITION CRACK AT FIRE DETECTOR BRACKET. ACFT GROUNDED. ACCOMPLISHED TASK CARD SBCFM 56-7B-72-0580-1 "REWORK FAN CASE, FLANGE IF CRACKED AT FIRE DETECTOR".SDR ASAA2015102913566Elastomer · separatedNR 1 ENGINE FAN BLADE SPACERS AT LOC'S 2, 4, 7, 13-21, 11EA HAVE ELASTOMER SEPARATION, MAX IAW MM ALLOWED 8 EA. ACFT GROUNDED. ALL 24 FAN BLADE SPACERS ON NR 1 ENGINE WERE REPLACED.SDR CALA2015102894728Acoustic Liner · damagedBIRD STRIKE ON TAKEOFF ROLL IN NR 2 ENG, STALL ECAM ALONG WITH AUDIBLE STALL. ABORTED TAKEOFF AT 90 KNOTS. ENG 2 REPLACED FOR ACOUSTIC LINER DAMAGE, CF247. ESN V10017 INSTALLED & NR 4 BEARING SCAVENGE LINE REPLACED.SDR ASMF201510031Blade · faultyDURING CLIMB, THE RT ENG VIBRATION REACHED 4.6 UNITS. ACCOMPLISHED THE QRH 7.24 PROCEDURE & THE VIBRATION WAS STABILIZED IN 4.0 UNITS. ACFT WAS SENT TO THE HANGAR & MX PERFORMED A BORESCOPE INSPECTION TO BOOSTER BLADES STAGES 2 - 4 & LPT STAGES 1 - 3 IAW AMMSDR ASAA2015101213481Panel · damagedNR 2 ENGINE INLET AND FAN BLADES, DETAILED INSPECTION FOUND 3 O'CLOCK POSITION FAN FRAME STRUT PANEL IS CRACKED ON LOWER SIDE. M, ALF. ACFT GROUNDED. REMOVED DAMAGED PANEL, REF AMM 72-23-07. INSTALLED REPLACEMENT PANEL REF 72-23-07-400-801-F00.SDR P5CA2015101300163Blade · damagedBIRD STRIKE DURING CLIMBOUT, FOUND NR 2 ENGINE FAN BLADE NR 33 DISTORTION. LENGTH 2.5 CORD WIDTH 1.125 DISTORTION .5, 4" FROM TIP OF BLADE. PERFORMED BLEND OUT IAW AMM 72-31-02-226-012-400. AFTER BLEND OUT DIMENSION LENGTH 3.5, CHORD .55, WIDTH .25 DISTORTISDR ASAA2015101113467Acoustic Panel · delaminatedDURING A NR 1 ENGINE INLET AND FAN BLADES DETAILED INSPECTION. FOUND NR 8 AFT ACOUSTICAL PANEL AT 8 O"CLOCK POSITION HAS L/E OF PANEL DELIMITATION AND FWD RT FASTENER AND INSERT ARE DAMAGED, WORN. ACFT GROUNDED. R & R ACUSTIC PANEL AT 8 O'CLOCK POSITION ALFSDR ASAA2015100213306Shim · wornNR 1 ENGINE FAN BLADE SHIMS COATING WORN. ACFT GROUNDED. CHANGED THE FAN BLADE SHIMS IAW T/C 78472002.SDR ASAA2015100213291Blade · distortedNR 1 ENGINE TREND DATA SHOWS A SUDDEN INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS. DATA SCATTER INDICATES FAN LUBE REQUIRED. ACFT GROUNDED. PERFORMED FAN BLADE LUBE ON NR 1 ENGINE IAW W/O NR 311983, T/C NR 78472002. NR 4 BLADE HAS TIP CURL, NR 5 BLADE HADSDR ASAA2015092213173Blade · wornNR 1 ENGINE FAN BLADE PLATFORM SEALS MISSING OVER 42", EXCEEDS MM 72-21-02 ALLOWABLE LIMITS OF 39.37. ACFT GROUNDED. REPLACED ALL 24 PLATFORMS ON NR 1 ENGINE REF TASK CARD NR 78472002.SDR ASAA2015092213172Spinner · wornNR 1 ENGINE SPINNER CONE WHITE PAINT WORN IN SEVERAL SPOTS. ACFT GROUNDED. R & R NR 1 ENGINE SPINNER CONE REF MM 72-21-01.SDR IPXA2015092393866Blades · damagedINSPECTION TYPE:ETOP, ON T/O, APPROXIMATELY 400 FT AGL WE FLEW INTO SEVERAL BIRDS ON RT SIDE OF ACFT AND RT ENG VIBRATION WAS 5.0 ON INSTRUMENT AND NOTICEABLE IN THE COCKPIT. RT ENGINE FAN BLADE SET REPLACED IAW AMM 72-31-02-404-084-H00, REV AUG 15. FAN ROTSDR ASAA2015091813111Shim · wornMORE THAN HALF OF THE NR 2 ENGINE FAN BLADE PLATFORMS HAVE SEAL DAMAGE. 1 PLATFORM HAS DISBONDED RIGHT AND ALL 24 FAN BLADE SHIMS HAVE WORN MOLLY DAG COATING. ACFT GROUNDED. REPLACED ALL NR 2 ENGINE FAN BLADE PLATFORMS & SHIMS. PERFORMED AMM TASK 71-00-00-SDR CA150914005Case · leaking(CAN) ENGINE WAS RECEIVED FOR INVESTIGATION AND REPAIR AFTER THE OPERATOR REPORTED EXTERNAL OIL LEAKAGE FROM THE REAR INLET CASE AREA.SDR ASAA2015090812976Fastener · looseREF T/C 78472000, NR 2 ENGINE INLET AND FAN BLADES-DETAILED INSPECTION. FOUND NR 5 STRUT PANEL AT 5 O'CLOCK POS, ALF, HAS 2 LOOSE FASTENERS AND BOTH INSERTS APPEAR TO BE DAMAGED. ACFT GROUNDED. INSERTS CK GOOD, SECURED FASTENERS NR 5 STRUT PANEL NR 2 ENGINE,SDR P5CA2015082700103Sealant · misinstalledNR 1 ENGINE INLET LIP SEALANT VOID IAW CMM 71-11-16. REPAIR 5, REV 42 APPLY A1 ENG INLET LIP SEALANT. CONDITION CHECK NORMAL.SDR ASAA2015080812787Spinner · damagedNR 1 ENGINE SPINNER FRONT CONE MISSING MORE THAN 50 PERCENT OF ITS IODIZED BLACK PAINT. ACFT GROUNDED.SDR ASAA2015072212553Shim · wornNR 2 ENGINE ALL FAN BLADE SHIMS WORN 24 EA. ACFT GROUNDED. REPLACED 24 EA FAN BLADE SHIMS ON NR 2 ENGINE REF T/C 78472002.SDR ASAA2015072212552Panel · looseNR 2 ENGINE FAN DUCT PANEL AT 01:00 POSITION HAS LOOSE BOLTS. ACFT GROUNDED. SECURE LOOSE FASTNERS NR 2 ENGINE FAN DUCT PANEL AT 01:00 POSITION, REF AMM 72-23-07-400-801-F00.SDR DALA2015062103894Nose Cowl · damagedRIGHT ENGINE NOSE COWL DAMAGED BY FOD EVENT. R & R NOSE COWL IAW AMM. PERFORMED ANTI-ICE CHECK.SDR WX0A2015061572652Acoustic Panel · damagedLEFT ENG HAS DAMAGE IN 1 PLACE TP FWD ACOUSTIC PANEL AT 12 O'CLOCK POSITION ON INTAKE. REPAIRED PANEL IAW EB-SR NO 001318971001 NR 11636. REINSTALLED PANELS IAW AMM 72-23-00. IAW EB-SR-NO, 00131897001 REQUIRES REINSPECTION WITHIN 50 FLIGHT HOURS & REPLACEMENSDR ASAA2015052911916Paint · missingNR 2 ENGINE SPINNER MISSING PAINT. ACFT GROUNDED.SDR ASAA2015052311850Counterbalance · out of adjustNR 2 ENGINE TREND DATA SHOWS LOW PRESSURE ROTOR VIBRATION LEVELS TO BE TRENDING HIGHER THAN EXPECTED. CURRENT LEVELS NEAR 1.5 UNITS. ACFT GROUNDED. NR 2 ENGINE ON BOARD FAN TRIM BALANCE COMPLETE IAW MM 71-00-00.SDR ASAA2015052011803Blade · vibrationENGINE NR 2 VIB VARIES BETWEEN .7 AND 2.7 IN DIFFERENT PHASES OF OPERATION. ACFT GROUNDED. ACCOMPLISHED FAN LUBE IAW T/C 78472002, ACCOMPLISHED. VIBRATION SURVEY IAW AMM 71-00-00. ALL PARAMETERS PASSED.SDR ASAA2015052011802Blade · wornNR 2 ENGINE TREND DATA SHOWS A SUDDEN INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS. DATA SCATTER INDICATES FAN LUBE REQUIRED. ACFT GROUNDED. PERFORMED NR 2 ENGINE FAN LUBE REF TASKCARD 78472002 AND ALSO TAST 7 VIB SURVEY REF AMM 71-00-00. OPS CHECK GOOD OSDR AALA20150511001Seal · debondedAIR INTERRUPT, EMER DECLARED. LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CRUISE, LT ENG VIBRATION INCREASED TO 4.1 AFTER 30 MINUTES OF FLIGHT. BRINGING THROTTLE TO NEAR IDLE BROUGHT INDICATIONS IN LIMITS. RECEIVED EICAS MSG, L ENG VIB, L ENG BB. FOUND SSDR WX0A2015051172581Inlet Bullet · dentedLEFT ENG INLET BULLET HAS TWO SMALL DENTS. R & R LT ENG INLET BULLET. NO DEFECTS NOTED IAW MM 71-10-02.SDR SWIA201541217Vane · crackedLT ENGINE LOWER INBD CASCADE HAS CRACKED VANE. REPAIRED IAW EA.SDR ASAA2015050511631Panel · damagedNR 2 ENG INLET AND FAN BLADES-DETAILED INSPECTION FOUND NR 3 FAN DUCT PANEL APPROXIMATELY 2 O'CLOCK POSITION HAS FASTENER HOLE DAMAGED. ACFT GROUNDED. R & R FAN DUCT PANEL AT NR 3 POSITION REF AMM 72-23-07.SDR ASAA2015050511630Panel · damagedWHILE ACCOMPLISH ENGINE 2 INLET INSPECTION TC 78472000 FOUND FAN DUCT 1 PANEL WITH AFT INBD FASTENER PULLED THROUGH. ACFT GROUNDED. REPLACED NR 2 ENG FAN DUCT PANEL AT NR 1 POSITION REF MM 72-23-07.SDR ASAA2015050311619Panel · debondedREF T/C 78472000, NR 2 ENGINE INLET AND FAN BLADES, DETAILED INSPECTION FOUND NR 5 FAN DUCT PANEL AT THE 5 O'CLOCK POSITION HAS ONE FASTENER INSERT THAT HAS BECOME DISBONDED FROM PANEL. ACFT GROUNDED. R & R FAN DUCT PANEL AT 5 O`CLOCK POSITION, REF M/M 72-23SDR ASAA2015050311618Panel · damagedREF T/C 78472000, NR 2 ENGINE INLET AND FAN BLADES, DETAILED INSPECTION. FOUND NR 12 FAN DUCT PANEL AT LT 12 O'CLOCK POSITION HAS DAMAGED FASTENER HOLE DUE TO LOOSE FASTENER. ACFT GROUNDED. R & R FAN DUCT PANEL AT LT 12' CLOCK POSITION REF MM 72-23-07. OK SDR ASAA2015041911387Spinner · damagedNR 1 ENGINE FRONT SPINNER CONE MISSING 50 PERCENT OR GREATER OF BLACK ANODIZED COATING. ACFT GROUNDED. R & R NR 1 ENGINE SPINNER IAW MM 72-21-01-000-801, AMM 72-21-01-400-801.SDR CA150410014Probe · leaking(CAN) STRONG CHEMICAL ODOR IN COCKPIT ON DESCENT, LASTED TILL LANDING. ON GND RUN FOUND NR 2 ENGINE N1 PROBE GUIDE TUBE LEAKING. SEALS REPLACED IAW EMM 72-23-00. GND RUN COMPLIED WITHIN LIMITS, AT 12 DROPS A MIN. BLACK LIGHT CHECK COMPLIED WITH ON BOTH ENGSDR ASAA2015040511248Shim · worn24 EA SHIMS WORN & MISSING COATING, NR 2 ENGINE. ACFT GROUNDED. R & R 24 EA SHIMS IN REF TASK CARD 78472002, NR 2 ENGINE.SDR WX0A2015040872514Guide Vane · damagedOGV AT 5:30 POSITION ENG 1. DAMAGE BEYOND LIMITS. R & R OGV AT THE 5:30 O CLOCK POSITION ON ENG NR 1 IAW AMM 72-23-00. NO DEFECTS NOTED.SDR ASAA2015040311232Fastener · looseREF T/C 78472000, NR 2 ENGINE FAN DUCT PANEL, WITH LPTACC SCOOP, AT 4-5 OCLOCK, ALF, LOWER MIDDLE FASTENER LOOSE, DAMAGED. FAN DUCT PANEL AT 5-6 OCLOCK, ALF, UPPER AND LOWER MIDDLE FASTENERS PULLED THROUGH PANEL. ACFT GROUNDED. R & R THE NR 2 ENGINE FAN DUCSDR ASAA2015040311231Spinner · unknownWHILE WORKING TC 78472002, FOLLOWING ITEMS REQUIRE REPLACEMENT ON NR 2 ENGINE. FRONT SPINNER CONE, ALL SHIMS, PLATFORMS AND SPACERS FROM BLADES 19 AND 22. ACFT GROUNDED. INSTALLED NEW FRONT SPINNER CONE, ALL SHIMS AND PLATFORMS AND SPACERS FROM BLADES 19 ANSDR ASAA2015040111207Spinner · dislodgedACCOMPLISHING T/C 78472002, FAN BLADE LUBE FOUND FWD SPINNER WITH INSERT DISLODGED. ACFT GROUNDED. INSTALLED NR 1 ENGINE FWD SPINNER IAW TC 78472002.SDR ASAA2015033111194Shim · wornENGINE FAN BLADE LUBE, NR 1 ENGINE, SN 802109, FAN BLADE SHIMS EXHIBIT MOLYDAG LOSS MORE THAN 25 PERCENT IAW MM 72-21-02-200-801, STEP 2L, 1, B, 1. ACFT GROUNDED. INSTALLED NR 1 ENG FAN BLADE SHIMS IAW TC 78472002.SDR ASAA2015032611157Shim · wornALL FAN BLADE SHIMS COATING WORN, NR 2 ENGINE. ACFT GROUNDED. REPLACED ALL 24 FAN BLADE SHIMS, REF TASK CARD 78472002.SDR ASAA2015032211069Cone · wornREF T/C 78472000, NR 1 ENGINE FRONT SPINNER CONE BLACK ANODIZED COATING WORN 50 PERCENT OR GREATER. ACFT GROUNDED. R & R NR 1 ENGINE FRONT SPINNER CONE REF MM 72-21-01-400-801-F00.SDR VNAA2015031700023Blades · damagedCREW REPORTED LOUD VIBRATION ON TAKEOFF AND LT FAN VIBRATION OF 1.6. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE COMPLIED WITH BIRD STRIKE INSPECTION AND FOUND DAMAGE TO LT ENGINE FAN BLADES FROM BIRD STRIKE. NO OTHER DEFECTS NOTED. MAINSDR ASAA2015031710998Shim · wornREF FAN LUBE T/C 78472002, FOUND NR 2 ENGINE FAN SHIMS WORN 24 EA. GROUNDED - YES. REPLACED 24 EA FAN BLADE SHIMS IAW T/C 78472002.SDR ASAA2015031010911Shim · wornREF T/C 78472002, NR 2 ENG FAN BLADE LUBRICATION . FOUND ALL 24 EA FAN BLADE SHIMS HAVE THE MOLYDAG COATING MISSING AND WORN TO BASE METAL. ACFT GROUNDED. INSTALLED 24 NEW FAN BLADE SHIMS, PN: 340-252-307-0 IAW TASK CARD NR 78472002 ON NR 2 ENGINE FAN BLADESSDR ASAA2015030310844Fan · out of balanceON CLIMB OUT, NR 2 ENG VIB WAS 2.2 UNITS AT APPROX 98 PERCENT N1, WITH POWER REDUCTIONS IT WOULD REDUCE TO 1.8 UNITS. AT CRUISE IT WAS .8 AT FL 290 AND APPROX 87 PERCENT N1. VIBRATION COULD BE FELT IN RUDDER PEDDALS WHEN IT WAS ABOVE 2.0 VIB UNITS. ACFT GROUSDR ASAA2015022210743Screw · looseREF. T/C 78472000, NR 1 ENGINE INLET AND FAN BLADES-DETAILED INSPECTION, FOUND 2 EA STRUT PANELS HAVE LOOSE SCREWS. AT 7 O'CLOCK & 8 O'CLOCK POS, NR 7 & 8 PANEL. ACFT GROUNDED. TIGHTEN 2 EA STRUT PANELS AT 7 O'CLOCK & 8 O'CLOCK POSITION, NR 7 & 8 PANELS ONSDR ASAA2015021910725Seal · wornWHILE ACCOMP FAN BLADE LUBE TC 78472002 - SEVEN PLATFORMS ARE MISSING OR HAVE LOOSE ELASTOMER SEAL. ACFT GROUNDED. REPLACED NR 2 ENGINE FAN BLADE PLATFORMS ACCOMPLISHED ON TASK CARD 78472002.SDR ASAA2015021910724Shim · wornWHILE ACCOMP FAN BLADE LUBE TC 78472002 ALL FAN BLADE SHIMS FOUND TO BE WORN. ACFT GROUNDED.. REPLACED NR 2 ENGINE FAN BLADE SHIMS ACCOMPLISHED ON TASK CARD 78472002.SDR ASAA2015021310641Shim · wornNR 1 ENG FAN BLADE SHIM AND ELESTOMER STOPS ARE WORN. ACFT GROUNDED. R & R IAW TC 78472002.
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