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.

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)May 29, 2002 · N603CA · Doug DC982SDR HEEA079285Inlet Screen · brokenENGINE INLET SCREEN HAS BROKEN STRANDS.May 21, 2002 · N40466 · Snias AS350B2SDR CA020515012Duct · cracked(CAN) DURING INSPECTION BOTH INERTIA SEPARATORS WERE FOUND CRACKED IN SEVERAL PLACES WITH CRACKS EXTENDING BEYOND 3 INCHES IN EITHER DIRECTIONS. REPLACED.May 10, 2002 · Piper PA46500TPSDR 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 MISSINFeb 21, 2002 · N356SK · Dorner DO328300SDR 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 72-23-02Feb 17, 2002 · N131NJ · Doug DC983SDR 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 THEFeb 12, 2002 · Hughes 369DSDR 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 ENGDec 19, 2001 · N725RW · Boeing 7272M7SDR 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 SATIDec 14, 2001 · N27512 · Emb EMB135ERSDR 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.Oct 14, 2001 · N902UP · Boeing 72751CSDR 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 Sep 26, 2001 · N289US · Boeing 727251SDR 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 PULLEDSep 20, 2001 · Cessna 550SDR 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 Sep 15, 2001 · N957AS · Doug DC982SDR 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 #7100-301Jul 22, 2001 · N79XJ · Saab SF340ASDR 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 cameJul 19, 2001 · N76XJ · Saab SF340ASDR 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. MJul 4, 2001 · N509XJ · Bac AVRO146RJ85ASDR 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.Jun 24, 2001 · Doug MD11FSDR 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.Apr 18, 2001 · N828AX · Doug DC863SDR RRXA010006Engine · fodON WALK-AROUND FOUND FOD ON NR 3 ENGINE.Feb 1, 2001 · N795FT · Doug DC873FSDR 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.Jan 23, 2001 · N649DL · Boeing 757232SDR 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 INSJan 11, 2001 · N456XJ · Saab 340BSDR 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.Dec 23, 2000 · N995UA · Boeing 737291SDR 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.Oct 5, 2000 · N508DA · Boeing 727232SDR 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 ACTIONSep 20, 2000 · Cndair CL6002B19SDR 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)Sep 11, 2000 · N804ME · Doug DC982SDR 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)Aug 21, 2000 · N225J · Cessna 550SDR 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. Aug 4, 2000 · N118RW · Boeing 7372Y5SDR 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.Jul 3, 2000 · N262FE · Boeing 727233SDR 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 THEMay 23, 2000 · N150TX · Amd FALCON50MYSTSDR 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 ANDMay 17, 2000 · N389UA · Boeing 737322SDR 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 JUSMar 13, 2000 · Lear 45LEARSDR CA000317013Engine · vibrates(CAN) FAN BALANCED AND VIBRATIONS AT TAKEOFF. RETUNED WITHIN PARAMETERS.Mar 10, 2000 · Lkheed 10113853SDR 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.Jan 6, 2000 · N717DH · Boeing 72723SDR 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. Dec 20, 1999 · N180AX · Boeing 727222SDR 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.Dec 17, 1999 · N179DN · Boeing 767332SDR HEED064622Screen · brokenINTAKE SCREEN HAD BROKEN WIRE. REPLACED PART.Nov 8, 1999 · N478X · Skrsky S76CSDR 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.Nov 4, 1999 · Lkheed 1011385114SDR 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 AIRLSep 15, 1999 · N812TC · Doug DC8F55SDR 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.Jun 21, 1999 · N702DH · Boeing 72730CSDR 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 BYApr 27, 1999 · Fokker F28MK1000SDR 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)Apr 15, 1999 · Cndair CL2156B11415SDR HEEA0015987Screen · damagedINTAKE SCREEN HAS SEVERAL BROKEN WIRES AND CHAFING.Sep 4, 1998 · N6100R · Snias AS350B2SDR 98ZZZX3742Screen · wornAIR INLET SCREEN WORN BEYOND SERVICEABLE LIMITS. WIRE MESH IS LOOSE AND FRETTI NG. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.Jul 29, 1998 · N901CF · Doug MD900SDR 98ZZZX3738Screen · wornAIR INLET SCREEN WORN BEYOND SERVICEABLE LIMITS. WIRE MESH IS LOOSE AND FRETTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.Jul 29, 1998 · N901CF · Doug MD900SDR 98ZZZX3724Screen · wornSCREEN WORN BEYOND SERVICEABLE LIMITS. WIRE MESH IS LOOSE AND FRETTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.Jul 29, 1998 · N901CF · Doug MD900SDR 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.Jan 12, 1998 · N8921E · Doug DC931SDR 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.Oct 30, 1997 · Boeing 727233SDR 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.Oct 17, 1997 · N415DA · Boeing 727232SDR 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 AAug 12, 1997 · N583MDSDR 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.May 26, 1997SDR 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.May 20, 1997 · N790M · Amd FALCON2000
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