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 AMTA200600298Actuator · unserviceableNR 2 ENGINE LEAKING FUEL FROM LT VSV DRAIN. REMOVED AND REPLACED NR 2 ENGINE VARIABLE STATOR VANE ACTUATOR REF AMM. OPS AND LEAK CHECK GOOD. (K)Apr 30, 2006 · N323TZ · Boeing 73783NSDR DHL2006802001Stator Vane · out of adjustENCOUNTERED MAJOR UPDRAFT AT FL 410 ENGNE NR 3 FLAMED OUT PERFORMED INFLIGHT ENGINE START ABNORMAL PROCEDURE NORMAL SYSTEM OPERATION NR 3 RESTARTED. C/W ROUGH AIR INSPECTION PER DC-8 M/M 05-51-0. A/C FOUND SERV. NO DEFECTS. PERFORMED FAULT CODE 50 PER DC-Mar 21, 2006 · N802DH · Doug DC873SDR KBM2006F00118Pressure Switch · inoperativeDIFF PRESSURE SWITCH, LOW AIR PRESSURE LIGHT FOR FDC FILTER CAME ON DURING HOVER, REMOVED AND REPLACED. (K)Mar 13, 2006 · N53SH · Snias AS350B1SDR KBM2006F00120Intake · crackedARRID AIR INTAKE, UNIT HAS CRACKED AT MOUNTING POINT, REMOVED AND REPLACED. (K)Mar 11, 2006 · N751H · Snias AS350B2SDR MASA200600690Actuator · leakingASH 7273 AUS - CAPTAIN REPORTED EXCESSIVE FUEL LEAKING FROM NR 1 ENG DRAIN. MX R2 THE NR 1 SLAVE ACTUATOR. OP'S CHECK GOOD.Mar 7, 2006 · N511MJ · Cndair CL6002C10SDR UIEA200600012Fan Blade · bird strikeON WALKAROUND FOUND NR 3 ENGINE SUSTAINED BIRD STRIKE, FOUND FAN BLADE BENT. PERFORMED CHAPTER FIVE BIRD STRIKE INSPECTION, NO FINDINGS. REMOVED AND REPLACED FAN BLADE. BORESCOPED CORE ENGINE, NO FINDINGS. PERFORMED OPS RUNUPS WITH NO FINDINGS. RELEASED AFeb 22, 2006 · N527MC · Boeing 7472D7BSDR MALA060205Case · chafedDURING 2Y CHECK IN BNA, FOUND COLD SECTION 3 PARTICLE SEPARATOR CASE CHAFFED ON BOTTOM AS MARKED, C/W EO#S71081.Feb 21, 2006 · N415XJ · Saab 340BSDR 06FDEA0581Skin · crackedNR 2 ENGINE INLET INNER SKIN AT 12 O'CLOCK POSITION WHERE IT MEETS THE 'S' DUCT IS BENT AND CRACKED. REPAIRED NR 2 ENGINE INLET INNER SKIN AT 12 O'CLOCK POSITION IAW FED EX EA 7-7160- 96621.Feb 7, 2006 · N485FE · Boeing 727200SDR AU510001654Bearing · wornLT ENGINE INLET GUIDE VANE BEARINGS PNO UP60336 (1OFF) AND PNO EU61711 (2OFF) WORN. FOUND DURING INSPECTION IAW SB TAY-75-1655.Dec 12, 2005 · Fokker F28MK0100SDR CA051110002Engine · surges(CAN) AIRCRAFT EXPERIENCED NR 2 ENGINE SURGE DURING TAKEOFF ROLL. SEVERE CROSSWINDS WERE EXPERIENCED WHICH WILL CAUSE THIS ENGINE SURGE. DUE TO THE CROSSWINDS AND THEN INTERRUPTION OR DISTURBANCE OF AIRFLOW THRU THE AIR INTAKE.Nov 10, 2005 · Boeing 727247SDR DL73S050574Engine · bird ingestionON T/O AT 1000 FT, HEARD LOUD BANG AND AIRCRAFT YAWED MOMENTARLLY LT AND RT. PASSENGER REPORTED BLUE FLAME FROM FWD OF LT ENGINE. FOWL SMELL IN CABIN. ENGINE PARAMETERS NORMAL. RETURNED TO CVG. FOUND EVIDENCE OF BIRD INGESTION IN NR 1 ENGINE. INSPECTED SSep 29, 2005 · N311DL · Boeing 737232SDR 2005FA0001431Duct · looseENGINE WAS TORN DOWN, BY AN APPROVED ENGINE SERVICE CENTER, FOR AN AUDIT OF ITS SB AND TBO CONFIGURATION, DUE TO CROSSOVER DUCT/DIFFUSER FAILURE OF ITS SISTER ENGINE ON THE SAME AIRCRAFT. IT WAS FOUND THE MAINTENANCE RECORDS CONCERNING SB STATUS AND TBO STATUSep 15, 2005 · N361MA · Mtsbsi MU2B40SDR MALA050378Panel · wornDURING A8 INSPECTION, FOUND FASTENER HOLES IN THE NR 1 & NR 2 ENGINE ATTENUATOR PANELS TO BE WORN THROUGH. ONE ON EACH ENGINE PANEL.Apr 21, 2005 · N503XJ · Bac AVRO146RJ85ASDR ASOA05270SHydromech Unit · malfunctionedDURING CRUISE, THE CREW NOTICED THE LT ENGINE ITT RISE IN EXCESS OF 800 DEGREES ITT AND REDUCED THE POWER ON THE ENGINE TO BRING IT WITHIN ITT LIMITS AT WHICH TIME THE ENGINE BEGAN TO SURGE. AN EMERGENCY WAS DECLARED AND JUST PRIOR TO THE CREW SHUTTING DOWN TMar 29, 2005 · N641AS · Aerosp ATR72SDR AWXA200500368Actuator · malfunctionedON TAKEOFF ROLL RECEIVED ECAM MESSAGE FOR NR 2 ENGINE COMPRESSOR VANE, REJECTED TAKEOFF BELOW 70 KTS AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75303, OPERATIONAL CHECK WAS GOOD. VENDORS TEAR DOWN REMar 25, 2005 · N670AW · Airbus A320232SDR HYTA2005003Seal · looseFELT SEALING STRIP APPROXIMATELY .5 INCH X 7 INCHES WAS COMING LOOSE FROM INSIDE THE ENGINE INDUCTION AIR PLENUM. OFFENDING FELT STRIP WAS REMOVED AS IT SERVES NO PURPOSE. THIS STRIP WAS LOCATED AT ABOUT 4 O’CLOCK ON THE INSIDE SURFACE ACROSS THE RT END OF TNov 19, 2004 · N976E · Cessna 208BSDR MALA040613Engine · seizedRT CHIP DETECT LIGHT ILLUMINATED ENROUTE ON DESCENT ITT OVERTEMP LIGHT ILLUMINATED SO WE SHUT DOWN THE ENGINE. MAINTENANCE INSPECTED, CORE SEIZED UP. REMOVED AND REPLACED RT ENGINE SN/0N 785770, SN/OFF 785738 IAW TASK CARD 7100-310R, SEE WORK PACKAGE 10-13-0Oct 13, 2004 · N438XJ · Saab 340BSDR GTIA040784Guide Vane · crackedFOUND LT ENGINE INLET GUIDE VANES CRACK FOUND ON 3 VANES AT 3 O'CLOCK POSITION. REMOVED AND REPLACED INLET CASE. (M)Sep 16, 2004 · N831NK · Doug DC983SDR R2J2004F00004Duct · failedENGINE EGT SUDDENLY ROSE IN FLIGHT AND POWER HAD TO BE REDUCED. SAFE LANDING ACCOMPLISHED AT HOME BASE TROUBLESHOOTING REVEALED THE COMPRESSOR CROSSOVER DUCT (DIFFUSER) HAD FAILED, CAUSING LOW COMPRESSOR PERFORMANCE. A VANE HAD BROKEN OFF AND LODGED, PREVENTSep 15, 2004 · N361MA · Mtsbsi MU2B40SDR R2J2004F00003Duct · looseENGINE WAS TORN DOWN FOR AN AUDIT OF ITS SB AND TBO CONFIGURATION, DUE TO CROSSOVER DUCT (DIFFUSER) FAILURE OF ITS (SISTER ENGINE) ON THE SAME AIRCRAFT. IT WAS FOUND, THE MAINTENANCE RECORDS CONCERNING SB STATUS AND TBO STATUS WERE IN ERROR ON THIS ENGINE ALSSep 15, 2004 · N361MA · Mtsbsi MU2B40SDR GTIA040734Guide Vane · crackedDTW - NR 1 ENGINE IGV HAS A HAIRLINE CRACK ON THE VANE ATTACHMENT WELD AT THE 3:30 POSITION APPROX 2.750 INCH LONG. REMOVED AND REPLACED IGV. (M)Aug 18, 2004 · N803NK · Doug DC982SDR CA040805001Fairing · failed(CAN) ENGINE EXPERIENCED A SPINNER FAIRING FAILURE ON THE T/O ROLL. PILOT ADVISED BY TOWER OF SPARKS AND FLAMES FROM JET PIPE AS REPORTED BY ANOTHER A/C & THE TAKE OFF WAS ABORTED. SPINNER FAIRING IS OF THE OLD FABRICATED SHORT FAIRING STANDARD & FAIRING UNZIPJul 21, 2004 · Boeing 757*SDR CA040518003Hose · kinked(CAN) AFTER TAKE OFF, CABIN BEGAN TO FILL WITH FUMES AND OIL VAPOR. CREW TURNED OFF ENGINE BLEED AIR AND RETURNED TO AIRPORT. MAINTENANCE FOUND NR 1 ENGINE BREATHER HOSE HAD BEEN KINKED AND PINCHED CAUSING THE ACCESSORY CASE TO PRESSURIZE AND FORCE OIL TO PASSMay 15, 2004 · Beech 1900CSDR AUS20040284Case · corroded(AUS) RT ENGINE AIR INLET CASE CORRODED.Mar 19, 2004 · Beech 300BEECHSDR AUS20040229Case · corroded(AUS) LT AND RT ENGINE AIR INLET CASES CORRODED IN AREA WHERE THE INLET CASE MATES WITH THE COMPRESSOR SHROUD. AIR INLET CASE IS MANUFACTURED FROM MAGNESIUM ALLOY.Mar 18, 2004 · Beech 300BEECHSDR CA040216007Retainer · missing(CAN) ENGINE TSN 13318, TSO291, CSN 13305,AFTER TAKEOFF CONTROL TOWER NOTED FLUID LOSS/SMOKE FROM ENGINE AND INFORMED PILOT. PILOT REDUCED POWER AND RETURNED TO DEPARTURE AIRPORT WHERE UNEVENTFUL LANDING WAS MADE. EXAMINATION OF THE ENGINE SHOWED BREATHER SHAFFeb 5, 2004SDR CA040220009Duct · cracked(CAN) LOWER FORWARD COWL AIR INLET DUCT CRACKED. REPAIR TO BE ACCOMPLISHED IAW MFG FIELD REPAIR PROCEDURE.Feb 2, 2004 · Beech C90ASDR MALA040124Engine · shutdownDURING FLIGHT 3627, ON CLIMBOUT WHILE PASSING THRU FL250, NR 2 ENGINE AUTOMATICALLY SHUTDOWN WITH NO INDICATION OF OVERSPEED OR FIRE. QRH PROCEDURES COMPLIED. ALL OTHER ENGINE PARAMETERS LOOKED NORMAL AT THE TIME OF SHUTDOWN. MAINTENANCE REMOVED & REPLACED Jan 21, 2004 · N532XJ · Bac AVRO146RJ85ASDR ARWA20040103Liner · damagedENGINE NR 3 EXPERIENCED A SLOW INCREASE IN VIBRATION FROM 105 TO 218 UNITS IN 3 MINUTES WITH A OR B SELECTED. ALL OTHER PARAMETERS NORMAL. INSPECT MASTER AND INTERNAL GEARBOX CHIP DETECTORS AND OIL FILTERS, NO EVIDENCE OF ENGINE FAILURE NOTED. ACOMPLISHED BORJan 19, 2004 · N307GB · Lkheed 1011385115SDR CA031118005Duct · cracked(CAN) CRACK DETECTED IN UPPER FORWARD AREA OF THE INLET DUCT EXTENDING FORWARD AND 1 AFT OF THE OUTBOARD RIVET ROW OF THE INLET LIP. THIS EXCEEDED THE SR-KA-00011 LIMITS, REQUIRING DUCT REPLACEMENT. WHEN DISASSEMBLING THE COWL FOR DUCT REPLACEMENT IT WAS NOTNov 3, 2003 · Beech C90ASDR MALA030478Engine · surgesDURING FLT, SHORTLY AFTER T/O, LT ENGINE SURGED TO OVER 100 PERCENT TORQUE, THEN BACK TO 80 PERCENT. ITT FOLLOWED SAME TREND. PERFORMED ERRATIC. ENGINE QRH INFLIGHT AND LOCKED OUT TORQUE MOTOR, ENGINE AND INDICATIONS STABILIZED EXCEPT FOR TORQUE. TORQUE GOct 25, 2003 · N366PX · Saab 340BSDR MALA030447Engine · malfunctionedDURING FLIGHT, LT ENGINE SHUTDOWN DUE TO CHIP LIGHT ON AND OIL PRESSURE LOSS. LT ENGINE CHIP LIGHT LITE UP AT 16000 FT. FOLLOWED QRH & REDUCED POWER. ENGINE PARAMETERS NORMAL FOR 10 MINS THEN A SUDDEN POP AND A/C SHOOK TO THE LT. ITT SUDDENLY RISED FOLLOWED Oct 6, 2003 · N457XJ · Saab 340BSDR QXEA200301209Fan · vibrationON FLIGHT 2528 AIRCRAFT RETURNED TO FIELD DUE TO, LEFT ENGINE FAN VIBRATION 1.6 AFTER TAKEOFF, INCREASED TO 2.2 DURING CLIMB AT 25K, REDUCED TO AS LOW AS 1.6 WHEN POWER WAS AT IDLE. DEFINITE AIRFRAME VIBRATION FELT AND INCREASE CABIN NOISE. AIRCRAFT LANDED WITSep 30, 2003 · N604QX · Cndair CL6002C10SDR CA030930001Breather Tube · kinked(CAN) THE AIRCRAFT WAS WORKED ON FOR HOT ENVIRONMENTAL ODOR. THE ENVIRONMENTAL SYSTEM WAS CHECKED OVER AND THE DUCT WORK WAS CHECKED WITH A BORESCOPE. PILOTS REPORTED THE ODOR WAS BACK WITH SMOKE WHEN THE POWERED UPTHE ENGINES.THE ENGINE COWLS WERE REMOVED ANSep 25, 2003 · Piagio P180SDR QXEA200301142Fan Blade · vibrationON FLIGHT 2469 SEA TO FAT AIRCRAFT DIVERTED TO PDX DUE TO RIGHT ENGINE VIBRATION INDICATION OF 1.9 VIBRATION FELT IN AIRFRAME. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED ALL FAN BALDES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETUREND TO SERVICE.Sep 17, 2003 · N603QX · Cndair CL6002C10SDR MALA030369Engine · flamed outON TAKEOFF OF FLIGHT NR 2932, AT APPROXIMATELY 80 KNOTS LT ENGINE FLAMED OUT. CREW HEARD A LOUG BANG, FA WITNESSED A LARGE FLAME FROM LT ENGINE EXHAUST PIPE. FLIGHT WAS ABORTED AND RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED ENGINE ASSEMAug 4, 2003 · N410XJ · Saab 340BSDR MALA030319Engine · making metalDURING FLIGHT 3254, LT CHIP DETECTOR LIGHT ILLUMINATED INFLIGHT. AIR RETURN TO MSP. MAINTENANCE REPLACED LT ENGINE IAW JC 7100-301 PN ON/OFF CT7-5A2 SN/OFF GE-E367320 SN/ON GE-E367273 SEE 409 NR 167742 AND OWRK PACKAGE DATED 6/22/03 FOR ALL INFO.Jun 21, 2003 · N98XJ · Saab SF340ASDR SWAA031183Pin · looseDURING SCHEDULED A1 CHECK, SWA SI 11165-72, NR 2 ENGINE RETAINING RING PINS AND MID FLANGE FAN DISK PINS FAILED TORQUE PIN CHECK. REMOVED AND REPLACED NR 2 ENGINE PER MM.May 27, 2003 · N428WN · Boeing 7377H4SDR 2003F00491Liner · erodedAT C-CHECK FOUND NR 2 ENGINE AIR INTAKE ATTRITION LINING WITH EROSION. REPAIRED ATTRITION LINING IAW EM 72-32-85 PAGE 6, FIGURE 72-32-85-990-016. (M)May 15, 2003 · N951LF · Airbus A320233SDR MEX2003212Inlet · damagedFLT 6444 - MEX-HMO - DURING TRANSIT CHECK, DETECTED FAN INLET GUIDE DAMAGED BY AND FOD. IN THE HANGAR THE FAN INLET GUIDE WAS REWORKED, TEST PERFORMED IAW 72-00-00, ALL CORRECT. (M)May 6, 2003 · N802AM · Boeing 7572Q8SDR CA030103012Fitting · cracked(CAN) APPROXIMATELY 8 INCH CRACK WHERE FLANGE IS WELDED TO PICCOLO TUBE AND 2 INCH CRACK IN PICCOLO TUBE ON OTHER SIDE OF INLET FITTING RESULTING IN BLEED AIR LEAK.Dec 23, 2002 · Cessna 550SDR MALA020683EngineAFTER DEPARTING MSP ON FLIGHT #3625, CAPT FROM 502XJ CALLED MAINTENANCE CONTROL, WITH THE FOLLOWING INFORMATION. #2 ENGINE N1 85.5, N2 93.2, EFT 608. MAINTENANCE CONTROL HAD CREW MOVE POWER LEVER UP LOOKING FOR INCREASE IN THE TEMP WITH VERY LITTLE CHANGE INDec 15, 2002 · N502XJ · Bac AVRO146RJ85ASDR MALA020678EngineAFTER TAKEOFF ON FLIGHT #3142, AT APPROXIMATELY 400' DURING THE AFTER TAKEOFF FLOW THE LH ENGINE TORQUE WENT TO 20%, AND A MASTER WARNING LIGHT ILLUMINATED. ALMOST SIMULTANIOUSLY THE LH ENGINE OVERTEMP LIGHT WENT ON TEMP WAS AT 1000-1007 DEGREES C. CLEAR, NODec 6, 2002 · N411XJ · Saab 340BSDR BJNA021102Cover · brokenHARD COMPRESSOR STALL ON NR 1 ENGINE AT 2.20 EPR - 96 PERCENT N1 - 20 KNOTS SPEED, POWER WAS PULLED TO IDLE WITHIN 300 FT OF TAKE OFF ROLL, TAKE OFF ABORTED. ENGINE INSPECTION: NOSE CONE OFF AND DAMAGED BASEBALL SIZE DAMAGE TO INNER LINER AND HONEYCOMB STRUCNov 10, 2002 · N344TM · Boeing 737200SDR MALA020598EngineDURING FLIGHT #3183, RH ENGINE STARTED TO OPERATE VERY IRRATICALLY ABOUT 15 MINUTES AFTER TO. TORQUE PEGGED TO 120, AND ITT OVERTEMPED. WITNESSED AS HIGH 977 DEGREES AND RED LIGHT. DID PRECAUTIONARY SHUTDOWN AND AIR RETURN TO MSP. MAINTENANCE FOUND FDR PAROct 6, 2002 · N79XJ · Saab SF340ASDR MALA020534Engine#2 ENGINE FAILED INFLIGHT. MAINTENANCE REPLACED #2 ENGINE SN/OFF P07686, SN/ON P07672 IAW TASK CARD 7100-502 ALSO COMPLETED WORK PACKAGE DATED 08282000. ALL OPS AND LEAK CHECKS ARE GOOD. REF WORK PACKAGE FOR DETAILS.Aug 29, 2002 · N532XJ · Bac AVRO146RJ85ASDR AUS20020953Bolt · missing(AUS) LT ENGINE NOSE CONE SUPPORT RING BOLTS MISSING.Aug 26, 2002 · Boeing 767338SDR AUS20020743Controller · faulty(AUS) NO1 ENGINE VIGV CONTROLLER FAULTY. CONTROLLER COULD NOT BE ADJUSTED TO BRING ENGINE PARAMETERS WITHIN LIMITS.Jul 22, 2002 · Boeing 747238BSDR MALA020407EngineDURING FLIGHT #3505 CREW REPORTED AT 1,000 FT. THE #4 ENGINE HAD TWO LOUD BANGS AND THE EGT WENT HIGH. INFLIGHT SHUTDOWN. AIR RETURN TO MSP. MAINTENANCE REPLACED #4 ENGINE PN lF507-1F SN/OFF P07877 SN/ON P07854 REF TASK CARD 7100-502 FOR DETAILS.Jul 16, 2002 · N501XJ · Bac AVRO146RJ85ASDR GTIA020719Inlet Screen · delaminatedFLL - NR 1 ENGINE INLET SCREEN DELAMINATING INSIDE NOSE COWL. AREA OF LINER DELAMINATED REMOVED. ENTERED ON C/O PER FAA BULLETIN FSAW 00-05 REPLACE IN 90 DAYS. REMOVED AND REPLACED LEFT ENGINE NOSE COWL PER MD80 MM 71-10-01. (M)Jun 25, 2002 · N815NK · Doug DC983
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