JASC 7297

Service difficulty reports · 275

Reports filed under 7297 · Turbine Engine System Wiring, 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 = '7297'
  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 CA100910002Wire Harness · damagedAPPROX 3 MINS AFTER REACHING CRUISE ALTITUDE ON FLIGHT 8724, CREW NOTICED TORQUE AND NH FLUCTUATIONS ON NR1 ENG OF APPROX 10 PERCENT. THEY THEN STARTED TO PULL POWER BACK ON THAT ENGINE TO NO AVAIL. THEY EVENTUALLY HAD POWER BACK TO FLIGHT IDLE, YET ENG WAS Sep 9, 2010 · Dhav DHC8102SDR CA100622008Wire Harness · damagedINABILITY TO MODULATE POWER ON BOTH CLIMBING, BOTH ENGINES DECREASED ENGINES DURING REVENUE FLIGHT, WHILE BY 5 PERCENT N1 UNCOMMANDED. THERE WAS NO RESPONSE TO THROTTLE ADVANCEMENT. THROTTLES WERE RETARDED TO CRUISE SETTING AND AGAIN THERE WAS NO RESPONSE TO May 11, 2010SDR N93A04032010Connector · looseDURING CLIMB, LT ENGINE TGT EXCEEDANCE WAS NOTED. MX FOUND CONNECTORS 900A1P16 AND 900A1P17 LOOSE. BOTH CONNECTORS ARE LOCATED AT THE ENGINE PYLON JUST AFT OF THE FIXED COWL AND CONNECT TO THE THRUST REVERSER. RATCHETING TYPE CONNECTORS WERE SECURED AND OPSApr 3, 2010 · N428QS · Gulstm GIVSDR CA100117004Wire Harness · open(CAN) IT WAS REPORTED THAT DURING CRUISE AT FL410 , THE ENGINE POWER (N1) FLUCTUATED BETWEEN THE TARGET OF N1 90 PERCENT AND 85 PERCENT DOWN TO 78 PERCENT WITHOUT ANY PILOT INPUTS. N1 FINALLY DROPPED TO 40 PERCENT AND SLOWLY RECOVERED ON ITS OWN WHILE THE PILJan 1, 2010SDR IPXA99M57904Wire Harness · damagedINSPECTION TYPE:N/A ATB - NR 2 ENGINE HIGH VIBRATION DURING CLIMB. RETURNED TO ANC. LANDED SAFELY. REMOVED AND REPLACED NR 2 ENG VIBRATION HARNESS IAW MM 71-50-01-4/2 AND REMOVED AND REPLACED NR 2 ENG FAN CASE ACCELEROMETER PER MM 77-32-03-4/2. HIGH POWER Nov 7, 2009 · N275UP · Doug MD11FSDR COEA2009102104919Connector · looseENGINE SHUTDOWN: WHEN CLIMBING TO CRUISE PWR NR 2 ENG TORQUE BECAME ERRATIC WITH PWR CHANGES. CREW NOTICED THE RT ENGINE APPEARED TO BE SURGING OUT OF CONTROL. PILOT ELECTED SHUTDOWN NR 2 ENG. NO EMERGENCY WAS DECLARED. T/S FOUND CONNECTOR FOR TSC, ECU, Oct 21, 2009 · N919FX · Aerosp ATR42300SDR UHLA2009082800089Wire Harness · corrodedRIGHT WING AFT SPAR, FORWARD OF OUTBOARD GROUND SPOILER ACTUATOR, OVERBRAID ON WIRE BUNDLE SHOWS EVIDENCE OF CORROSION. REMOVED AND REPLACED RT ENG W604 HARNESS IAW EMB 170 WM 73-21-50, AMM 20-10-01, IPC 24-02-73.Aug 28, 2009 · N858RW · Emb ERJ170100SESDR UHLA2009082800088Wire Harness · corrodedEVIDENCE OF CORROSION ON OVERBRAID LOCATED AT REAR OF RIGHT ENGINE PYLON AND EVIDENCE OF CHAFING. REMOVED AND REPLACED RT ENGINE W604 HARNESS IAW EMB 170 WM 73-21-50, AMM 20-10-01 AND IPC 24-02-73.Aug 28, 2009 · N858RW · Emb ERJ170100SESDR UHLA2009082800087Wire Harness · corrodedEVIDENCE OF CORROSION ON OVERBRAID LOCATED AT REAR OF LEFT ENGINE PYLON AND EVIDENCE OF CHAFING. CLEANED CORROSION FROM BRAIDED LINE, INSPECTED IAW EMB SRM 51-12. FOUND CHAFING TO BE WITHIN LIMITS.Aug 28, 2009 · N858RW · Emb ERJ170100SESDR CA090806013Wire Harness · unknownWHEN ACFT POWERED UP DURING SERVICING A FLASHING AMBER GOV LIGHT DISPLAYED ON ANNUNCIATOR PANEL. FAILURE CODE 123 CHECKED INDICATING "T4 FADEC L", GOING FURTHER INTO FADEC DATA -FAIL 1 CODE WAS 0020 (RAW T4.5 FAILURE) WAS DISPLAYED AND T4 INDICATION IN FADEC Aug 6, 2009 · Snias AS350B3SDR FDEA200907262807Wire Harness · damagedCLIMB 320 TO 340 AUTO THROTTLES ENGAGED NR3 ENG EXCEEDANCE HIGH EGT 1021, REQUIRED THROTTLE REDUCTION TO MAINTAIN EGT LIMITS. COMPLIED WITH EO 8-7720-7-5001. EGT PROBES ON NR 3 CHECKED GOOD. OPENED BORESCOPE PLUGS B3-1 AND B3-2 FOR QA ON NR 3 ENG. COMPLIEJul 26, 2009 · N302FE · Doug MD1030FSDR CA090715001Wire · burned(CAN) UPON ENGINE START ON GROUND CB`S POPED UPON 10 PERCENT ENGINE SPEED WHEN AUTO IGNITION CUT IN. THE WIRING AT THE STARTER WAS INSPECTED SERVICABLE. WIRING IN THE LT WING UNDER THE FAIRING HAD MULTIPLE BURNED WIRING. COMPANY IS NOW WORKING WITH M7 FOR OJul 12, 2009 · Swrngn SA227ACSDR TRBA2009073SUPWire Harness · failedDISCREP: ENGINE NR 1 FAILURE IN CRUISE FLIGHT - SHUT DOWN PROCEDURE. REMAINDER OF FLIGHT NORMAL AND ROUTINE. REPLACED ELECTRICAL HARNESS IAW 72-01-10. PERFORMED GROUND RUN UP PERFORMENCE CHECK IAW JIC 372-00-00-ERU-10040, JIC 73-23-61-RAI-10000 AND W/C 05-50Jul 1, 2009 · N410AT · Aerosp ATR72212SDR HALA2009041100143Connector · damagedETOPS SIGNIFICANT SYSTEM, ON NR 2 ENG FOUND CONNECTOR TO FUEL FILTER BYPASS SWITCH DAMAGE. REPLACED CONNECTOR D10994 PER AMM 71-51-00. FUNCTIONAL TEST GOOD PER AMM 71-00-00.Apr 11, 2009 · N592HA · Boeing 7673CBSDR NSVA2009014Connector · dirtyLEFT ENGINE OIL PRESS AT 178 PSI, ENGINE SHUTDOWN IN FLIGHT, DIVERTED TO KDTV DUE TO OIL PRESSURE. DISCONNECT P55 CONNECTOR OIL PRESS TRANSDUCER, CLEANED CONNECTOR AND RE-CONNECTED IAW AMM 70-00-15. OPS CHECK GOOD IAW AMM.Apr 3, 2009 · N196WQ · Bombdr DHC8402SDR USAA2009031990629Wire Harness · failedTHE FLIGHT ABORTED TAKEOFF DUE TO NR 2 ENGINE FAILURE. CREW REPORTED FLUCTUATION AT 80 PERCENT N1, THEN DROPPED OFF POWER. MAINTENANCE FOUND THE J8 HARNESS SWELLED DUE TO AN EARLIER LEAK ON THE HMU. REPLACED THE J8 HARNESS.Mar 16, 2009 · N179UW · Airbus A321211SDR CA090219014Wire Harness · damaged(CAN) SHORTLY AFTER T/O, THE ENGINE SUFFERED AN UNCOMMANDED DECREASE IN POWER. THE FLIGHT WAS ABORTED AND THE AIRCRAFT RETURNED TO BASE WITHOUT INCIDENT. THE DECREASE IN POWER WAS COMPENSATED BY THE OTHER ENGINE AND AT NO TIME DID THE ENGINE REVERT TO MANUAL NFeb 6, 2009SDR CA090115002Wire Harness · worn(CAN) ON NR1 ENGINE FOUND HARNESS W721 DAMAGED BEHIND FAN COWL AT 8 O`CLOCK POSITION. THE HARNESS DAMAGE WAS CAUSED BY THE RUB BETWEEN 2 ELECTRICAL HARNESSES W721 HARNESS REPLACED AND REPOSITIONED IAW B-777 AMM TASK 70-00-01-400-806-H-01. (TC NR 20090115002)Jan 9, 2009 · Boeing 777*SDR HNAA200911200392Connector · dirtyNR 2 ENGINE OIL TEMPERATURE FLUCTUATES IN FLIGHT. CLEAN CONNECTOR PLUG, OPS CHECK GOOD.Jan 7, 2009 · N980HA · Dhav DHC8102SDR TRBA2008117Wire Harness · openTHE ELECTRICAL CIRCUIT TO THE TORQUE PROBE NR 2 FROM THE EEC, USING A PORTATIVE OHM METER, WAS VERIFIED. THE CIRCUIT TORQUE NR 1 AND THE TORQUE SENSOR TEMP COMPENSATOR CIRCUIT WERE FOUND WITHIN THE MAINTENANCE MANUAL LIMITS. HOWEVER, BOTH CIRCUITS WERE SHOWIDec 22, 2008 · N407AT · Aerosp ATR72212SDR CA090115001Wire Harness · worn(CAN) ON NR 2 ENGINE FOUND HARNESS W729 DAMAGED BEHIND FAN COWL AT 6 O`CLOCK POSITION. THE DAMAGE WAS CAUSED BY THE HARNESS RUBBING ON EACH OTHER. THE HARNESS WAS CHANGED AND REPOSITIONED (TC NR 20090115001).Dec 16, 2008 · Boeing 777*SDR ASAA0853876Wire Harness · wornDURING OPERATIONAL CK OF HYDRAULIC PUMP ON NR 2 ENGINE FOUND THAT HYD PRESS WAS ZERO WITH PUMP SWITCH ON FOUND ENG HYD PUMP CONNECTOR DP1204 WORN. REPLACED MW0312 HARNESS REF IPC 71 51 03 01 AND AMM 71 51 03. OPS NML REF AMM 71 00 00 AND 73 21 00. ENG HYD PNov 21, 2008 · N587AS · Boeing 737890SDR CA081203010Wire Harness · damaged(CAN) THE ENG EXPERIENCED REPEATED EVENTS OF TORQUE FLUCTUATIONS BETWEEN THE 20TH AND 24TH OF OCTOBER FOR WHICH TROUBLESHOOTING HAD BEEN DONE. ON OCT. 27, THE PROBLEM RE-APPEARED AND WAS ACCOMPANIED BY NO RESPONSE TO THROTTLE MOVEMENTS. THE ENGINE WAS SHUTDOWNOct 27, 2008 · Aerosp ATR42*SDR 2008UALA05820Wire · burnedNR 2 ENG FOUND WIRES BURNED 6 INCHES BELOW CORE DISCONNECT D4216P. REPLACE WIRE W3538-202B-18, W3538-202R-1 8 AND SHIELD, PINS 5, 6, 7 AT D4216P TO IDG D10966 PINS 9 AND 10. REF WD 24-21-21. WIRE 561-0734 AOG NR R2902. REF WIRE LIST PG 1927. ROUTED WIRE FRSep 20, 2008 · N675UA · Boeing 767322SDR 08FDEA03276Wire Harness · failedSHORTLY AFTER T/O, AUTO THROTTLES DISENGAGED AND WOULD NOT RESET. SIMULTANEOUSLY, N1 FOR NUMBER 1 ENGINE FAILED (BOTH ANALOG AND DIGITAL). AUTO THROTTLE REMAINED OFF THE REST OF FLT. FOUND DUCT FOR T/R VALVE WITH A HOLE BLOWN THRU. ALSO, THE HARNESS FOR NAug 6, 2008 · N661FE · Airbus A300F4605RSDR A6WA200840544Wire Harness · damagedENG NR 1 SHUTDOWN IN FLIGHT, NO ASSOCIATED EICAS MESSAGES ILLUMINATED BEFORE SHUTDOWN. THRUST LEVERS WERE ABOVE IDLE AT APPROXIMATELY 80%. RAN QRH, TRIED TO RELIGHT. ENG RELIT FOR 15-20 SECONDS THEN GOT LOW OIL PRESSURE RED WARNING. DID PRECAUTIONARY SHUTDJul 15, 2008 · N445AW · Cndair CL6002B19SDR IXX2008F00001Connector · dirtyDURING CRUISE, NR 2 ENGINE FIRE WARNING AND BELL CAME ON INTERMITTEN FOR 1-2 SECONDS. THE CREW ACCOMPLISHED, RAN CHECK LIST AND SHUTDOWN NR (2) ENGINE. THE FIRE BELL STOPPED AFTER FIRE HANDLE WAS MOVED TO FULL FWD POSITION. THE FIRE BOTTLES WERE NOT DISCHAJul 1, 2008 · N830BX · Doug DC871FSDR VQI2008F00001Wire Harness · damagedIN NORMAL CRUISE, THE AIRCRAFT EXPERIENCED AN UNCOMMANDED SHUTDOWN OF THE NR 1 ENGINE. ECAM ENG1 FADEC A FAULT OCCURRED WITH ASSOCIATED MESSAGES. THE CREW RESTARTED THE ENGINE AFTER FOLLOWING QRH PROCEDURES . A/C DIVERTED INTO PDX WITH NO FURTHER FAULTS NOTED.May 14, 2008 · N527VA · Airbus A319111SDR B4V2008F00000Connector · arcedCONNECTOR IS NOT MAKING GOOD CONTACT AND CAUSING ARCING AND ENGINE TO QUIT. PROBABLE CAUSE IS AUTOMOTIVE QUALITY AND NOT OF THE THREADED TYPE. TO PREVENT RECURRENCE RECOMEND USING AVIATION THREADED TYPE PLUG. (K)Jan 19, 2008 · N4130M · Diamon DA42SDR HALA0700552Connector · dirtyETOPS SIGNIFICANT SYSTEM, RT PIMU MSG T5 CROSS CHECK FAIL A AND B CHANNEL FAULTED LEGS 1-4-16. CLEANED T5 CONNECTER PIMU BITE CHK OK PER FIM PIMU MSG INDEX PG 620.Dec 24, 2007 · N586HA · Boeing 7673G5SDR MALA070189Wire Harness · unknownDURING LANDING IN DTW, WHEN THE POWER LEVERS WERE RETARDED, THE RT PROP AUTOCOARSENED. CREW CONTINUED THE LANDING AND POWER RETURNED TO RT ENGINE DURING TAXI. REMOVED AND REPLACED RT ENGINE RT AIRFRAME HARNESS, PN: 7292533-681 AND STARTER GEN, PN: 23080-031,Nov 24, 2007 · N435XJ · Saab 340BSDR DL757071517Wire Harness · damagedON FINAL APPROACH CREW REPORTED THE LEFT ENGINE HAD A FLAME OUT AND SHUT DOWN BY ITSELF. CREW DID NOT NOTICE ANYTHING ABNORMAL BEFORE IT SHUTDOWN. INSPECTED INLET EXHAUST ON ENG, ALL NORMAL. FOUND WIRES OFF PRIMARY AND SECONDARY CHANNELS OFF PMA ORANGE WIRNov 20, 2007 · N696DA · Boeing 757232SDR FDKA200708432Connector · disconnectedFDM 6195 BUF (0444 PHX LCL) - ABORTED T/O DUE TO E-2 OIL IMPENDING BYPASS MESSAGE. MX FOUND OIL IMPENDING BYPASS INDICATOR C/P DISCONNECTED. RECONNECTED C/P, RAN ENGINE, NO OIL DEBRIS MESSAGE IN CMC. OPS GOOD.Aug 29, 2007 · N835MJ · Emb EMB145LRSDR HEEA116984Connector · malfunctionedAMBER GOV LIGHT ILLUMINATED PRIOR TO LANDING, UPON SHUTDOWN, ENGINE WOULD NOT REDUCE RPM FROM FLIGHT POSITION WHEN START SELECT SWITCH SET TO IDLE. ENGINE WOULD NOT RESTART. CLEANED CONNECTIONS AND REPLACED GOVERNOR FUSE, REPLACED FUSE HOLDER AND REPLACED EAug 17, 2007 · N972AE · Snias AS350B3SDR 2007UALA03216Wire Harness · damagedFOUND ENGINE HARNESS W0623 DAMAGED AT 9 O'CLOCK POSITION. BUNDLE MELTED THRU TO INNER WIRES. FOUND ENG HARNESS W0623 DAMAGED AT 9 O'CLOCK. BUNDLE MELTED THRU TO INNER WIRES. REPLACED HARNESS, READJUSTED CLAMPS, RAN ENGINE AND ALL CHECKED NORMALLY.Aug 16, 2007 · N214UA · Boeing 777222SDR 2007UALA02941Connector · damagedCREW REPORTS: LEFT ENG STARTED NORMAL, DURING RT ENG START, LEFT ENG SPOOL DOWN & FLAMED OUT, LEFT SPAR VALVE LIGHT CAME ON & LEFT VALVE LIGHT ALSO CAME ON. ON TROUBLESHOOTING FOUND ACTUATOR CONNECTOR PIN 5 BROKEN. REPINNED WIRE.Jul 31, 2007 · N518UA · Boeing 757222SDR DELA200700005Wire Harness · damagedLT ENGINE N1 LAGGED BEHIND RT ENGINE N1 ON TAKEOFF ROLL, AND ALSO LT ENGINE COMPUTER LIGHT CAME ON. FOUND (B) SOLENOID OF SERVO VALVE CONNECTOR HAD EXPOSED WIRE. RE-TERMINATED PINS (A) AND (B) OF CONNECTOR PLUG. CREW CONDUCTED HIGH POWER RUN AND HIGH SPEED Jun 27, 2007 · N431AS · Lear 35ASDR CA070618007Wire Harness · damaged(CAN) ACCESSORIES SERVICES PLANT 2. DURING BENCH CHECKING ACTIVITIES THE PART WAS EXHIBITING AN UNKNOWN CONFIGURATION. UNABLE TO DETERMINE THE MANUFACTURING SOURCE. THE PART WAS REPLACED WITH GENUINE PART. THIS PART WILL BE KEPT FOR 1 MONTH FOR EXAMINATION. Jun 18, 2007SDR NSVA20070142Wire Harness · wornL/R FUEL FLOW INDICATORS ERRATIC. FOUND BRACKET HOLDING START BLEED VALVE BROKEN. BLEED VALVE WORE THROUGH RT ENGINE "WHITE HARNESS." REMOVED AND REPLACED BRACKET AND HARNESS IAW AMM 71-50-00, PN OFF/ON (BRACKET), 5051T77G02, PN OFF/ON (HARNESS) 7292531.May 30, 2007 · N370PX · Saab 340BSDR HALA0700230Connector · dirtyETOPS SIGNIFICANT SYSTEM, RT ENG PIMU "MSG RT ENG EEC C2" MSG. PERFORMED CORRECTIVE ACTION FIM 71-PIMU PER PIMU MSG 353-19. CLEANED AND RETORQUED CONNECTORS. REPAIR CONFIRMATION CKS GOOD. RAN ENG NO MSG.May 27, 2007 · N586HA · Boeing 767300SDR CA070423004Wire Harness · chafed(CAN) SHORTLY AFTER T/O, THE RT ENGINE VIBRATION INDICATOR FLUCTUATED ERRATICALLY THE WENT TO DASHES MOMENTARILY THEN RETURNED TO NORMAL OPERATION. FLIGHT RETURNED FOR MAINTENANCE TROUBLESHOOTING. AFTER CHANGING THE ENGINE ACCELEROMETER AND SIGNAL CONDITIONEApr 21, 2007 · Cndair CL6002B19SDR DXTA200702003Terminal · broken(HIGH PRESS VALVE FAIL -R) CAS MESSAGE ILLUMINATED PRIOR TO ROTATION DURING TAKEOFF. CAS MESSAGE ONLY REMAINED ILLUMINATED FOR APPROX 15 MINS. DURING CLIMB-OUT, NR 1 ENG BEGAN TO SURGE WITH N1 FLUCTUATIONS OF 10-15 PERCENT FOR APPROX 20-30 SECONDS. ENG ANTI -Mar 7, 2007 · N384QS · Cessna 680CESDR RAIA00702023Connector · looseFLT NR 5587 - STL - NO FUEL FLOW ON NR 1 ENGINE DURING START. MAINTENANCE RESEATED CONNECTOR TO FADEC 1A & 1B. OPS CHECK GOOD.Feb 20, 2007 · N810HK · Emb EMB145LRSDR SWAA071020Connector · faultyINFLIGHT SHUTDOWN/AIRTURN BACK/DECLARED EMERGENCY. NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. REMAINED ON WITH THRUST LEVER CLOSED. ENGINE SHUTDOWN PER QRH. FOUND D404 CONNECTOR FAULTY. REMOVED AND REPLACED CONNECTOR PER MM.Feb 20, 2007 · N379SW · Boeing 7373H4SDR NSVA20070023Wire · brokenFLIGHT IDLE STOP LIGHT CAME ON DURING LANDING. TS IAW AMM 76-10-60 AND FOUND TWO BROKEN WIRES AT 6GA-J1 PINS L AND N REQUIRED WIRES IAW SAAB WM 20-20-00. REPAIRED BROKEN WIRING AT 6GA-J1 PINS L AND N IAW SWM 20-20-00. OPS CHECKS GOOD.Feb 2, 2007 · N311CE · Saab 340BSDR DL76L070047Wire · chafedDURING BRAKE RELEASE WHILE PUSHING THROTTLES FORWARD AT APPROX 1.3 EPR, THE RIGHT ENG OIL PRESSURE LIGHT ILLUMINATED AND PRESSURE GAUGE READ AT APPROX 213PSI. IMMEDIATE ABORT PERFORMED. AT IDLE RIGHT ENG OIL PRESS IS NORMAL APPROX 106 PSI. R ENG OIL PRESS EJan 19, 2007 · N173DN · Boeing 767332SDR QXEA200603021Relay · malfunctionedPDX - ON TAXI FOR FLIGHT 2501, RECEIVED A RIGHT ENGINE DEGRADE CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE REPLACED THE K20 AND K22 RELAYS ON PCB 3 IN THE JB-10 REF FIM 73-21-02. GROUND ENGINE AND OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICNov 23, 2006 · N614QX · Cndair CL6002C10SDR NSVA200600115Wire Harness · unknownRT ITT FLUX DURING CLIMB-OUT AND ENGINE SHUTDOWN. REMOVED AND REPLACED RT YELLOW HARNESS WITH SERVICEABLE PART IAW GE CT-7 71-00-00 PN ON/OFF 6068T54P02, OPS CHECK GOOD.Aug 1, 2006 · N203CJ · Saab 340BSDR 2006UALA01361Connector · looseRETURNED TO THE FIELD DUE TO LEFT ENGINE PARAMETER FLUCTUATIONS. NR 1 ENGINE EEC CONNECTOR LOCKING RING WAS DAMAGED AND REPLACED EEC. THIS EEC WAS INSTALLED ON JUNE 25, 2006.Jul 8, 2006 · N595UA · Boeing 757222SDR VNAA0606009Wire Harness · failedDURING TAKEOFF CHECK, RT ENGINE ITT FLUCTUATING. AIRCRAFT RETURNED TO GNV AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE INBOARD ITT HARNESS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.Jun 22, 2006 · N215PS · Cndair CL6002B19
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