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 GTIA020557Inlet Screen · delaminatedDTW - FOUND NR 2 ENGINE INLET WIRE MESH DELAMINATED AT 9 O'CLOCK POSITION. REPAIRED DELAMINATED IAW MD80 SRM 54-04. (M)SDR HEEA079285Inlet Screen · brokenENGINE INLET SCREEN HAS BROKEN STRANDS.SDR CA020515012Duct · cracked(CAN) DURING INSPECTION BOTH INERTIA SEPARATORS WERE FOUND CRACKED IN SEVERAL PLACES WITH CRACKS EXTENDING BEYOND 3 INCHES IN EITHER DIRECTIONS. REPLACED.SDR S2YA02006Inlet Screen · delaminatedJUST AFTER TAKEOFF OF FLIGHT 2432, MKE-BDL, THE CREW NOTED LOUD POP AND SUCKING SOUND FROM THE RIGHT ENGINE. THE CREW DID AN AIR-TURN-BACK AND A PRECAUTIONARY LANDING. MAINTENANCE INSPECTED THE A/C AND FOUND THE INLET SCREEN DELAMINATED AND PART OF IT MISSINSDR P2EA2002M008Inlet Guide Vane · crackedON INSPECTION OF THE NR 2 ENGINE INLET FOUND THE IGV AT 4 O'CLOCK WITH CRACK. UPON FURTHER INSPECTION FOUND THE NR 2 ENGINE BEARING HUB CRACKED. REPLACED THE NR 2 ENGINE INLET GUIDE VANE ASSY AND REPLACED THE NR 2 ENGINE BEARING HUB IAW 72-23-01 AND 72-23-02SDR CA020321001Engine · fod(CAN) UNUSUAL SOUND HEARD FROM THE A/C ON COOL DOWN COMING FROM THE ENGINE INLET AREA. UPON FURTHER INVESTIGATION THE COMPRESSOR HAD FOD. A NUTPLATE ON THE FORWARD SIDE OF THE PARTICLE SEPERATOR, THAT FASTEN THE FOWARD INLET COWLS ON, HAD SPLIT AND HALF OF THESDR EISA20010149Nose Bullet · detachedAT 300' AFTER TAKEOFF, #2 ENGINE STOPPED PRODUCING POWER, STARTED COMPRESSOR STALLING. PERFORMED CHECKLIST, AIR TURN BACK TO AIRPORT.SUSPECTED CAUSE: DETACHMENT OF NOSE BULLET DURING FLIGHT.CORRECTIVE ACTION:REMOVED AND REPLACED #2 ENGINE IAW EXPRESS ONE ENGSDR C2XA01TY199Inlet · damagedTYS DURING A SCHEDULED INSPECTION THE RIGHT HAND ENGINE AIR INLET WAS FOUND TO HAVE TWO NICKS ON THE ACOUSTIC PERFORATED INNER SKIN. MAINTENANCE REWORKED THE NICKS (BLEND-OUT) IAW EMB-135 SRM 54-20-01 AND EMBRAER GST 3879/01, THE REPAIR WAS FOUND TO BE SATISDR UPS01237043Bullet · crackedINSPECTION TYPE:S-10 ENGINE 3 SPINNER CRACK FOUND DURING SEG-10 CHECK. HAS 1 INCH CRACK AT BOLT HOLE. REMOVED AND REPLACED NR 3 ENG SPINNER FAIRING IAW MM 72-30-10. OPS NORMAL AT THIS TIME.SDR 0103452289Inlet Bullet · dislodgedDURING CLIMBOUT FROM LAN, THE LEFT ENGINE FAILURE LIGHT ILLUMINATED WITH ASSOCIATED LOSS OF THRUST AND VIBRATION FROM THE LEFT ENGINE. CREW SHUT DOWN THE LEFT ENGINE AND AIRCRAFT RETURNED TO LAN. MAINTENANCE FOUND NOSE DOME DISLODGED IN NOSE COWL. REPLACED SDR CA011018016Rivet · loose(CAN) AIRCRAFT DOWN FOR PHASE 5 INSPECTION. L/H ENGINE - 2 RIVET IN THE 5 O'CLOCK POSITION AND 3 RIVETS AT 7 O'CLOCK POSITION HAD THE HEADS PULLED 1/3 TO 2/3 AROUND THE SHANK DIAMETER.R/H ENGINE 5 TO 6 RIVETS IN THE 3 TO 6 O'CLOCK POSITION HAD THE HEADS PULLEDSDR GTIA010902Nose Bullet · damagedAUTOTHROTTLES OFF AND EQUAL ERP, THE LEFT EPR VALUE DECREASES .11 AND THE RIGHT EPR INITIALLY INCREASES .02 THEN DECREASES .03 LEAVING AN EPR SPLIT OF .08 N1 AND N2 BOTH CHANGE BY APPROXIMATELY EQUAL AMOUNT. WITH AUTOTHROTTLES ON AND SYNC ON THE EPR SPLIT IS SDR MALA010594EngineDURING FLIGHT #2906, FROM DTW LH CHIP DETECT LIGHT ILLUMINATED AFTER DEPARTURE FROM DTW. AT UNDER 1000' AGL. ALL ENGINE PARAMETERS NORMAL. QRH WAS COMPLETED MX NOTIFIED. AIR RETURN TO DTW. MAINTENANCCE REPLACED LH ENGINE S/N ON GE-E-367252. IAW JC #7100-301SDR MALA010577Connector · shortedOn Flight #3243, in route to MSP from CWA Right Tailpipe light came on about 30-40 miles out from MSP, crew was in the clear with no precipitation. Shutdown Engine. About 5-10 minutes after Shutdown Right Engine, Left Engine Low Engine Oil pressure light cameSDR MALA010570EngineDuring Flight # 3407, enroute to Fargo, #3 Engine Oil Pressure low light illuminated. Crew checked Oil Press gauge, indicated no oil pressure in #3 Engine. N1 was about 19%, N2 was about 12%, Airspeed 230 Kts. Windmill time 15 min. Temp at Shutdown normal. MSDR EVA002Engine · fod1. AIRCRAFT B-16107 DURING T/O RUN IN BRU, A/C NO.3 ENGINE BIRD STRIKE. VIBRATION JUMP UP TO 4.2 & FELT BY THE CREW. CAPTAIN S/D THE ENGINE, DUMP FUEL AND AIR RETURN TO BRU.2. ON GND, VISUAL CHK FND 3 FAN BLADES DAMAGED.3. PFM BSI ON #3 ENGINE, ALL COND NML.4.SDR ABXA010357Case · crackedNR 4 ENGINE INLET GUIDE VANE CASE HAD NUMEROUS CRACKS AT WELDS. WELDED CRACKS ON INLET CASE IAW P&W OVERHAUL MANUAL 72-21-1.SDR RRXA010006Engine · fodON WALK-AROUND FOUND FOD ON NR 3 ENGINE.SDR DL757010126Fan Blade · fodFOUND DURING L/O CHECK FOD ON RT ENG FAN BLADE AND ACOUSTICAL LINER. REPAIRED ACOUSTICAL LINER. REMOVED AND REPLACED FAN BLADES NR 15 AND 35, BLENDED BLADES 16,30 AND 31. ACCOMPLISHED ENGINE RUN PER PFHB, ALL CKS NORMAL.SDR MALA010108Intake Duct · contaminatedEN ROUTE CLIMBING THROUGH 15,000, -10 DEGREE CELSUIS AND ANTI-ICE OFF, GOT 900+ DEGREE ON RT ENGINE, PRECAUTIONARY LANDING BACK IN DTW. AVOIDED 80 - 84 PERCENT NG RANGE. MAINTENANCE REMOVED DEBRIS FOUND IN RT ENGINE INLET, PERFORMED ENGINE INLET BLOCKAGE INSSDR 2000UALA00806Bullet · separatedENGINE COMPRESSOR STALL ON TAKEOFF. *S/D* THE STALL WAS CAUSED BY THE NR 2 ENGINE NOSE DOME BEING LIBERATED FROM THE FRONT ACCESSORY SUPPORT. THE ACCESSORY SUPPORT AND NOSE DOME WERE REPLACED.SDR DL72L002083Flange · bentAT HMV, THE AFT FLANGE OF THE NR 2 INLET WAS TORN/BENT. REMOVED DAMAGE PER SRM 54-10-3D FIG 801D. DYE CKED, NO FURTHER DAMAGE NOTED. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 54-10-3D FIG 801D.SDR CA001003016Engine · damaged(CAN) DURING MORNING CREW PRE-FLIGHT WALK AROUND, RT ENGINE INTAKE, FAN & GUIDE VANES FOUND DAMAGED.ENGINE CHANGED, A/C BACK IN SERVICE.TC: SUSPECT FOD NO - FURTHER ACTIONSDR MWEA00789Nose Cowl · dentedMCO - FLT 90 - ON APPROACH, HAD BIRD STRIKE ON LEFT ENGINE INLET. INSPECTED AND FOUND LEFT ENGINE INLET COWL RING DENTED. REMOVED AND REPLACED LEFT ENGINE COWL. (X)SDR 20000911SH020Rivet · missingRIVET MISSING IN LEFT ENGINE INLET AND ONE FAN BLADE HAD SMALL CURL AT LEADING EDGE TIP. REPLACED MISSING RIVET, INSPECTED AND REPAIRED FAN ASSEMBLY. (X)SDR F3LA00223Structure · wornDEN - DURING C-3 CHECK, FOUND NR 2 ENGINE INLET TRAILING EDGE MATING SURFACE FOR ENGINE COWL AT 6:00 POSITION WORN VERY THIN. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED TWO REPAIR ANGLES AND FILLERS PER SRM 54-10-03 AND TREATED AND PRIMED PER SRM 51-10-02. SDR 00FDEA00421Case · crackedDURING ROUTINE INSPECTION, THE NR 3 ENGINE INLET GUIDE VANE CASE WAS FOUND CRACKED. R&R NR 3 ENGINE IAW FEDEX WORK CARD 70T0001-03.SDR 20000601SH026Intake Duct · crackedDURING NR 2 ENGINE CHANGE, FOUND 7.5 INCH LONG CRACK IN THE TOP OF THE ''S'' DUCT ALONG THE LONGITUDINAL AXIS APPROXIMATELY 3 FEET IN FRONT OF THE ENGINE INLET. THERE IS ALSO A CRACK IN THE AFT ATTACHMENT FLANGE OF THE ANTI-ICE MANIFOLD ON THE TOP SIDE OF THESDR 2000UALA00267Blade · bird strikeRETURNED TO TUS DUE TO A NR 1 ENGINE BIRD STRIKE. *S/D* INSPECTION REVEALED 3 DAMAGED FAN BLADES AND MIDSPAN SHROUD OVERLAP ON THE FAN BLADES. BORESCOPE INSPECTION OF HIGH PRESSURE COMPRESSOR WITH NO LIMITING DEFECTS. THREE FAN BLADE PAIRS WERE REPLACED ANDSDR CA000329008Intake Duct · gouged(CAN) DURING PRE-START INSPECTION DAMAGE WAS DISCOVERED TO THE ABRADABLE STRIP SURROUNDING THE FAN ON BOTH ENGINES. ON THE FLIGHT PRIOR TO THIS THE A/C ENCOUNTERED ICING DURING ITS LANDING APPROACH TO CALGARY. DAMAGE CONSISTED OF NUMEROUS CUTS AND GOUGES JUSSDR CA000317013Engine · vibrates(CAN) FAN BALANCED AND VIBRATIONS AT TAKEOFF. RETUNED WITHIN PARAMETERS.SDR DHL2000717102Case · crackedNR 3 ENGINE B-FLANGE INLET CASE, 7 INCH CRACK AT 10 O'CLOCK. STOP DRILLED PER PW-MM-72-00 PAGE 664B. WELDED PER PRATT & WHITNEY ENGINE MANUAL 72-23-01 REPAIR 14 SECTION G.SDR GAIA99267Case · damaged'NO FLIGHT' - FOUND DURING HEAVY C-MAINTENANCE CHECK AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND FIBERGLASS PATCH DETERIORATED AND PEELING AT THE 12 O'CLOCK POSITION BETWEEN IGV HEAT VALVES AND SIX INCHES AFT ON OUTER CASE OF NR 3 ENGINE. SDR DL76L992784Blade · damagedUPON ARRIVAL FOUND NUMBER 1 ENGINE WITH FAN BLADE DAMAGE AND FAN CASE DAMAGE. MTC FERRY TO ATL FOR REPAIR. REPLACED DAMAGED FAN BLADES AND 3 FAN EXIT GUIDE VANES BECAUSE OF DAMAGE.SDR HEED064622Screen · brokenINTAKE SCREEN HAD BROKEN WIRE. REPLACED PART.SDR CA991116014Nr 1 Bearing · leaking(CAN) ENGINE EXPERIENCED HIGH VIBRATIONS ON TAKEOFF. OIL FOUND IN SPINNER. OPERATOR SPECIFIED THAT THIS IS A KNOWN PROBLEM BUT HAPPENS VERY INFREQUENTLY. OIL IS PROPAGATING FROM NR 1 BEARING UNDER CERTAIN CONDITIONS.SDR 2000ZZZX700Spinner · crackedNOSE COWL CRACKED AT 6:00 O'CLOCK POSITION NR 4 ENGINE. CUT OUT PREVIOUS WELD, NDT TO ASSURE ALL CRACKS STOPPED. FABRICATED PLUG AND WELDED IN PLACE. NDT WELD NO FLAWS FOUND PER EO 99-136 WITH APPROVED 8110-3 DATED 8-31-99. REF: ZANTOP INTERNATIONAL AIRLSDR DHL9970204CInlet · crackedC CHECK, NR 1 ENG INLET, AFT FLANGE CRACKED, OUTBD AFT SIDE WHILE COWLING MATES TO INLET. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR 8 BY 1 BY 1 FT PER SRM 51-40-2, N/R 6019.SDR CA990505004Duct · failed(CAN) IN CLIMB, NR 2 ENG REQD 5 PERCENT HIGHER RPM TO MAINTAIN SAME THRUST AS NR 1 ENG. ON LEVELING OFF, CREW DECIDED TO TREND BOTH ENGS TO ASSIST MAINT IN T/S OF LOWER POWER PROBLEM. 100 MILES OUT, A THUD FOLLOWED BY A CONTINUOUS SHUDDER FELT ACCOMPANIED BYSDR CA990423013Duct · chafed(CAN) INSPECTION FOUND THE COOLING INLET DUCT (PN 215T50191010) WILL MAKE CONTACT AND CHAFE THE OIL PRESSURE FUEL HEATER LINE IF A BAD WELD LED TO SEPARATION. THE DUCT WAS REPLACED. (X)SDR HEEA0015987Screen · damagedINTAKE SCREEN HAS SEVERAL BROKEN WIRES AND CHAFING.SDR 98ZZZX3742Screen · wornAIR INLET SCREEN WORN BEYOND SERVICEABLE LIMITS. WIRE MESH IS LOOSE AND FRETTI NG. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 98ZZZX3738Screen · wornAIR INLET SCREEN WORN BEYOND SERVICEABLE LIMITS. WIRE MESH IS LOOSE AND FRETTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 98ZZZX3724Screen · wornSCREEN WORN BEYOND SERVICEABLE LIMITS. WIRE MESH IS LOOSE AND FRETTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 9800899928Nose Bullet · obstructedAS TAKEOFF POWER WAS APPLIED, THE LEFT ENGINE WOULD NOT REACH TARGET EPR. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REMOVED OBSTRUCTION FROM THE LEFT ENGINE NOSE BULLET, OPERATIONAL CHECK OK.SDR CA971113070Spacer Casing · failed(CAN) THE AIRCRAFT SUFFERED A COMPLETE LOSS OF POWER ON NR NR3 ENGINE DURING CLIMB-OUT. INVESTIGATION FOUND COMPRESSOR DAMAGE CAUSED BY THE INGESTION OF FAILED SECTIONS OF A SPACER CASING BETWEEN THE INLET GUIDE VANE CASE AND THE FIRST STAGE COMPRESSOR.SDR DL72K972082Skin · crackedFOUND DURING B-2 LETTER CHECK, 3 EA .75 INCH CRACKS IN OUTER SKIN OF NR 2 ENG INLET AT 3 O'CLOCK POSITION. REPAIRED PER M/M 54-30-0.SDR IH971355014Dome · crackedNR 2 ENGINE FRONT BULLET IS CRACKED AROUND RIVETS, 2 CRACKS WERE FOUND IN THE 5930646-25 DOME SKIN. CRACKS WERE COMMON TO THIS SKIN ONLY. THE INNER DETAILS OF THE 5930646 DOME ASSEMBLY WERE REMOVED, CRACKS STOP DRILLED AND THEN WELDED PER DPS 10.301. SKIN ASDR CA970624013Stator Vane · missing bolt(CAN) TAKEOFF REJECTED AT APPROXIMATELY 100 KTS DUE TO INABILITY TO ACHIEVE TAKEOFF POWER ON #3 ENGINE. REPLACED MISSING BOLT ON VARIABLE STATOR VANE BELLCRANK ASSEMBLY ON #3 ENGINE. POWER ASSURANCE CHECK CARRIED OUT. #3 ENGINE CHECKED SERVICEABLE.SDR 97ZZZX2681Inlet · bolts looseAFTER ENGINE FAILURE, MORE THAN HALF THE BOLTS SECURING THE ENGINE INLET HA D UNSCREWED THEMSELVES. THE REMAINING WERE LOOSE. SUBMITTER SUSPECTS UNUSUAL ENGINE VIBRATION CAUSED THE BOLTS TO BACK OUT. THE INLET COULD POSSIBLY FALL OFF THE AIRCRAFT IN-FLIGHT.
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