JASC 2910

Service difficulty reports · 11,292

Reports filed under 2910 · Hydraulic System, Main, 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 = '2910'
  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 UALA2010122004650Hydraulic System · fluctuatesEICAS MESSAGE. C HYD SYS MAINT DISPLAYED. ACCOMPLISHED TROUBLESHOOTING ADDRESSING 'C' HYD MAINT MESSAGE. SYSTEM CHECKS GOOD PER TEST. PRESSURE STILL FLUCTUATES. REPLACED ADP MODULATING VALVE, NO HELP. REPLACED ADP PRESSURE REGULATOR AND SHUTOFF VALVE PER MM. Dec 19, 2010 · N668UA · Boeing 767322SDR USAA2010121393030Line · leakingFLT1021 - RETURNED TO FIELD AND DECLARED EMERGENCY LANDING. LANDING AND LOST NOSE WHEEL STEERING. FOUND NR 1 ENGINE THRUST REVERSER PRESSURE LINE LEAKING. REPLACED LINE WITH FLEX LINE PER AMM 20-17-03 AND EA 116831. SERVICED GREEN SYSTEM & OPERATIONAL CHEDec 18, 2010 · N102UW · Airbus A320214SDR DXTA2010122004369Hydraulic System · warning lightAFTER APPROX 50 MINUTES IN FLT, DURING CRUISE AT FL 380, AMBER HYD QTY LOW CAS ILLUMINATED. HYD PAGE QTY SHOWED COMBINED QTY JUST ABOVE LOW MARK. OVER THE NEXT 50 MIN IT SLOWLY DECREASED BELOW THE LOW MARK & WENT FROM WHITE TO RED. DURING APPROACH & LANDING, Dec 18, 2010 · N460QS · Gulstm GIVSDR NSVA2010230Pressure Switch · malfunctionedGEAR TOOK ABOUT 4 MINUTES TO COME UP HYD PUMP RAN CONTINOUSLY. RAN QRH CYCLED GEAR THEN CAME UP NORMALLY. COULD NOT DUPLICATE DISCREPENCY. REPLACED HYDRAULIC AUTO PRESSURE SWITCH. REPLACED HYDRAULIC RESEVOIR, BLED SYS AND SERVICED; PERFORMED NUMEROUS GEAR Dec 17, 2010 · N362PX · Saab 340BSDR UALA2010122004660Modulating Valve · faultyC HYD DEM PUMP LIGHT WITH GEAR RETRACT. ACCOMPLISHED FAULT ISOLATION PROCEDURE. ACP TROUBLESHOOTING IAW FIM. FAILED BLOCK 27 ON PAGE 173. WITH ADP IN AUTO AND CTR ELEC PUMPS OFF SHOULD HAVE MIN OF 2500 PSI WHILE OPERATING FLAPS FROM 5 THRU 30. HAD 1700 PSDec 17, 2010 · N653UA · Boeing 767322SDR UALA2010121704603Tube · damagedHYD LEAK FOUND ON ARR, FROM ACCESS PANEL F/O RT H-STAB. SUSPECT SECTION 72. REMOVED DAMAGED TUBING. CAPPED FOR BOTH ENDS AND REMOVED BOLTS ARE SECURED ORIGINAL POSITION. INSTALLED NEW TUBING AND LEAK CHECKED OK.Dec 16, 2010 · N204UA · Boeing 777222SDR FDEA201012164697Transducer · inoperative1 HOUR AFTER TAKEOFF, AT FL300 RECEIVED HYD PRESS 3 LOW LEVEL 1 ALERT, NR 3 HYD PRESSURE INDICATED 0 & NR 3 HYD QTY INDICATED 10.9 GALS, TURNED ON BOTH RMPS, NO HELP NR 3 PRESSURE STILL 0. DURING LANDING PHASE-RECEIVED HYD 3 PRESS LOW & HYD NR 3 FAIL LEVEL 2Dec 16, 2010 · N631FE · Doug MD11FSDR UALA2010121604598O-Ring · leakingNR 2 ENG PYLON ENG HYD MODULE, FWD MOST HYD UNION IS LEAKING 20 DPM WITH ENGINE RUNNING. REPLACED O-RING ON LEAKING UNION. SECURED ALL HYD LINES. BOLTS ON HYD MODULE NEED TO BE REINSTALLED AND CONNECTOR PLUG INSTALLED. REINSTALLED BOLTS AND RAN ENGINE, NODec 13, 2010 · N543UA · Boeing 757222SDR AALA20101213JFK02Shutoff Valve · crackedJFK - INFLIGHT ORD-LGA. CREW REPORTED LEFT HYDRAULIC SYSTEM QUANTITY VERY LOW. EMERGENCY DECLARED FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND SPOILER SHUT OFF VALVE CRACKED. REPLACED VALVE. SYSTEM GROUND CHECK NORMAL Dec 13, 2010 · N472AA · Doug DC982SDR USAA20101215BB089Hydraulic System · overservicedPHL - FLT 1012 EN ROUTE STT TO PHL. CREW REPORTS: STRONG ELECTRICAL SMELL IN AFT CABIN AFTER TAKEOFF. LESSER IN FORWARD CABIN. NO VISIBLE SMOKE. CLEARED IN 20 MINUTES. MAINTENANCE ACCOMPLISHED AMM AND FIM TASK INSPECTIONS. MAINTENANCE REPORTS: INSPECTDec 12, 2010 · N248AY · Boeing 767201SDR CA101214002Pcu · malfunctioned(CAN) AFTER LANDING CREW EXPERIENCED A HYDRAULIC SYSTEM FAILURE NECESSITATING A TOW FROM THE RUNWAY TO THE GATE. SPECIFICALLY: ON TOUCH DOWN, SPOILER FAULT THEN HYDRAULIC 2 LOW QUANTITY . FOUND 3 BOLTS SHEARED ON RT NR 5 SPOILER ACTUATOR CASE. NR 5 RT MFS PCDec 11, 2010 · Emb ERJ190100IGWSDR UALA2010121304541Switch · faultyRUDDER RATIO EICAS MSG. DUE TO REPORTS OF RUDDER RATIO MSG, PLEASE ACCOMPLISH FIM. START FROM BLOCK 1 AND ADDRESS ANY PROBLEMS. ACCOMPLISHED FIM. FOUND HYD SWITCH FAULT DISPLAYED. REPLACED LT PRESS SWITCH S27 IAW MM, OPS CHECK GOOD.Dec 11, 2010 · N672UA · Boeing 767322SDR P4YA2010121100001Hose · rupturedDURING A TRAINING FLIGHT, WHILE ON A MISSED APPROACH TO RUNWAY, THE FLIGHT CREW WAS UNABLE TO RETRACT FLAPS. IT WAS DETERMINED THAT THE ACFT LOST ALL HYD FLUID AND WAS UNABLE TO RUN ANY HYD SYS. AN EMERGENCY WAS DECLARED. UPON COMPLETION OF EMERGENCY AND NORMADec 11, 2010 · N1269J · Casa CN235SDR CA101210001Tube · worn(CAN) R HYD PRESS LOW AMBER. PILOT CALLED TO REPORT THE R HYD PRESS LOW AMBER CAS MESSAGE POSTED AFTER BEING AIRBORNE FOR OVER 4 HOURS. THE RH PRESSURE SHOWED 1400 PSI AND THE RH QUANTITY WAS ZERO. THE QRH WAS FOLOWED. THE FLIGHT WAS AN HOUR OUT OF AND DIVERTDec 9, 2010 · Bombdr BD1001A10SDR UALA2010120804484Line · leakingLEFT HYD SYS QTY INDICATES .68 RF ON STATUS AND EICAS PGS. FOUND LT SYS HYD QTY AT .40, SERVICED LT SYS TO FULL. FOUND EVIDENCE OF LARGE HYD LEAK IN TAIL. SUSPECT LT SYS RUDDER PCU OR LINE TO IT.Dec 8, 2010 · N656UA · Boeing 767322SDR CA101206022Servo · binding(CAN) THIS ACTUATOR WAS RECEIVED FOR REPAIR WITH COMMENTS "BINDING DURING INPUT". A FUNCTIONAL TEST WAS CARRIED OUT. DUE TO WEAR IN THE INPUT LINKAGE BUSHINGS AND BOLTS, THE SERVO VALVE TRAVEL WAS LIMITED ENOUGH TO RESTRICT THE SPEED OF THE ACTUATOR. WEAR IN TDec 6, 2010 · Bell 407SDR FDEA201012044594Line · leakingHYD YELLOW RESERVIOR LO LEVEL - ECAM QTY AND OVERHEAD GAUGE INDICATIONS SHOWED YELLOW SYS QTY. DECLARED TO RED DOT. YELLOW PUMP LO PRESS WITH SUBSEQUENT LOSS OF YELLOW SYS COMPONENTS FACT. HYD LINE FOUND LEAKING TO THE AILERON SERVO CONTROL, LINE HAS BEEN RDec 4, 2010 · N731FD · Airbus A300F4605RSDR CA101208009Filter · malfunctioned(CAN) LEFT-HAND HYDRAULIC FILTER CLOGGING INDICATOR BUTTON POPS WITH NO FAULTS FOUND. THIS HAS NOT RESULTED IN ANY LOSS OF HYDRAULIC POWER OR OTHER IN-FLIGHT FAILURE. EXTERNAL FILTER INDICATION ONLY. EUROCOPTER CANADA HAS GIVEN VERBAL INDICATION THAT THEY ARE Dec 3, 2010 · Snias AS350B3SDR DGCA10844Hydraulic System · low pressureLOST MAIN HYD SYS PRESSURE INDICATION. DECLARED AN EMERGENCY LANDING.Dec 3, 2010 · N570R · Rkwell NA26565SDR FDEA201012024539Line · crackedHYD 2 FAIL. BEHIND NR2 PYLON STRUCTURE PANEL 364KR FOUND NR2 HYD LINE CRACKED. REPAIRED SAME LINE IAW REF TO MM CHAP 20-10-01-2-0 PERMANENT PIPING REPAIR. MX PRACTICES WITH 3000 PSI APPLIED TO SYS, NO LEAKS FOUND. SYS OK FOR SERVICE. (CLOSED)Dec 2, 2010 · N528FE · Doug MD11FSDR 2010FA0001212Hydromech Unit · malfunctionedLOSS OF HYD POWER AND WITHOUT NR INDICATED.Dec 1, 2010 · Bell 206B3SDR UALA2010113004408Clamp · brokenBLUE HYD LOW QTY ECAM, FLIGHT DIVERTED. FOUND HYDRAULIC FLEX HOSE ASSY LEAKING AT BROKEN ATTACH CLAMP. PRESSURE LINE FROM BLUE PUMP, P/N AE707414-2 AOG# X3601. REPLACED BLUE SYS HYD PRESSURE LINE AND CLAMP FROM EMDP. PRESSURIZED AND LEAK CHECKED LINE. NO Nov 30, 2010 · N416UA · Airbus A320232SDR DXTA2010120104338Check Valve · failedUPON GEAR RETRACTION THE "LOW HYD FLO" ANNUNCIATOR RT SIDE ILLUMINATED AND REMAINED ON UNTIL THE GEAR WAS EXTENDED. RAN RT ENGINE SELECTED FLAPS DOWN, OPERATED SPEED BRAKES. DURING FLAP EXTENSION AND STAB MOVEMENT CYCLEC 2 OR 3 TIMES COULD NOT DUPICATE DISCNov 30, 2010 · N638QS · Cessna 560XLSDR CA101129008B-Nut · loose(CAN) WHILE ON A TEST FLIGHT, NOTICED THE RPM ON THE RIGHT ENGINE BEGIN TO DROOP. WHEN THE RPM DROPPED BELOW 94 PERCENT SELECTED THE CONDITION LEVER TO THE FEATHER POSITION AND SECURED THE ENGINE AS PER THE EMERGENCY CHECKLIST. THEN RETURNED TO RED DEER AND Nov 29, 2010 · Gulstm 690ASDR HALA2010112800569Pressure Switch · failedETOPS SIGNIFICANT SYSTEM, RT ELEC HYD PUMP IS INOP IN AUTO ON POSITION IS OK. ACCOMP FIM 29-11-00 FIG 105 REMOVED AND REPLACED ACMP PRESSURE SWITCH PER AMM29-11-18. OPS AND LEAK CK GOOD.Nov 29, 2010 · N580HA · Boeing 76733AERSDR DXTA2010112904325Line · leakingLEFT BRAKE GRABS HARD WHEN LIGHTLY APPLIED. FOUND LEAKING HYD LINE AT BRAKE FUSE. TIGHTENED & VERIFIED BRAKE HYD PRESSURES AT BRAKE METERING VALVE, RUDDER PEDALS & BRAKES IAW MM 32-42-00. OPS & LEAK CHECKED GOOD. TAXI CHECKED GOOD.Nov 26, 2010 · N922QS · Cessna 750SDR UALA2010112304328B-Nut · looseG SYS HYD ISSUE, RTFL. THE RT MLG DOOR BYPASS VLV (2518 GM), PORT 'C', 'B' NUT LOOSE. TIGHTENED AND ACCOMPLISHED LEAK CK. NO LEAKS NOTED. ACCOMPLISHED A RESET OF HANDLE AFTER A FREE FALL EXTENSION IAW MM.Nov 23, 2010 · N829UA · Airbus A319131SDR 2010FA0001202Relay · defectiveACFT WAS DEPARTING. THE GEAR HANDLE WAS SELECTED UP. THE HYD PUMP WAS NOT HEARD TO ACTIVATE AND THE HYD CAWS LIGHT ILLUMINATED 2-3 SECONDS LATER. THE LANDING GEAR LIGHTS STAYED IN THE "3 GREEN" POSITION. THE HYD POWER RELAY PN 974.09.26.112 WAS CONFIRMED TO BENov 23, 2010 · N669AF · Pilats PC1245SDR CA101209010Relief Valve · worn(CAN) THERMO RELIEF VALVE WAS RELIEVING HYD PRESSURE AT 1950 PSI. PRESSURE SWITCH WAS SET TO TURN PUMP OFF AT 2075 PSI. THERMO RELIEF VALVE REPLACED AND PRESSURE RELIEF VALVE WAS FOUND TO BE RELEAVING AT 2050 PSI. PRESSURE RELIEF VALVE REPLACED SYSTEM OPERATEDNov 21, 2010 · Beech 200BEECHSDR CA101122012Shutoff Valve · leaking(CAN) ELEC FLAP/SLAT MESSAGE AT CRUISE. DUE TO CTR HYD LEAK. FLAP/SLAT HYD SHUTOFF VALVE MODULE REPLACED AS PER AMM 29-11-00/201. LEAK CHECK AND FLT CONT OPS CHK, OK. MODULE INSTALLED DATE: 2004-01-13 OVERWEIGHT LANDING ACCOUNT OF MECHANICAL DIVERSION DUE Nov 20, 2010 · Boeing 767333SDR UHLA2010111900211Hydraulic Line · leakingAT FL360 RECEIVE "HYD QTY 1 LO" EICAS MESSAGE. SELECTED HYD SYNOPTIC PAGE ON MFD AND NOTICED THE HYD QTY 1 WAS AT 16 PERCENT AND RAPIDLY DROPPING. WITHIN MINUTES QUANTITY AND PRESSURE WERE AT 0 AND ASSOCIATED EICAS MESSAGE APPEARED. RAN QRH, DECLARED AN EMENov 19, 2010 · N207JQ · Emb ERJ170200LRSDR CA101122013Hose · ruptured(CAN) DURING APPROACH PILOT SELECTED GEAR DOWN AND THE LANDING GEAR FAILED TO EXTEND. PILOT SELECTED LANDING GEAR HANDLE TO THE UP POSITION THEN CYCLED THE GEAR HANDLE BACK TO THE DOWN POSITION AGAIN WITH A FAILURE OF THE GEAR TO EXTEND. APPROACH CANCELLED ANov 18, 2010 · Piper PA31SDR SWAA107143Line · chafedDIVERSION / DECLARED EMERGENCY. EN ROUTE ENGINE DRIVEN A NR 1 HYDRAULIC PUMP LIGHT FLICKERED AND THEN ILLUMINATED. FOUND ENGINE DRIVEN "A" SYS PRESSURE LINE CHAFED. REMOVED AND REPLACED LINE, PUMP AND FILTERS PER MM.Nov 17, 2010 · N367SW · Boeing 7373H4SDR UALA2010111704253Valve · failedAIRCRAFT BELLY SATURATED WITH HYDRAULIC FLUID FROM MLG TO TAIL. FOUND SLAT BYPASS VALVE SPRAYING FLUID WHEN SLATS ARE OPERATED. REPLACED VALVE WITH BORROWED PART. PART COMPATIBLE PER OLIPC. REPLACED AND OPS CK GOOD PER MM.Nov 16, 2010 · N543UA · Boeing 757222SDR UALA2010111504231Switch · inoperativeLEFT HYD SYSTEM PRESSURE SWITCH INOP. SUSPECT LEFT RESERVOIR HYD SYSTEM PRESSURE SWITCH, REPLACED S27. OPS CHECKS GOOD. NO FAULTS NOTED WITH RESERVOIR PRESS OR SYS PRESSURE.Nov 15, 2010 · N549UA · Boeing 757222SDR 2010F00241Pressure Switch · leakingABOUT 25 MILES OUT, ENROUTE, MEDICAL CREW INFORMED ME THAT THEY HAD HEARD A LOUD SOUND FOLLOWED BY A "THUD" THAT THEY FELT UNDERNEATH THE LT SIDE OF THE ACFT. DID NOT HEAR OF FEEL OR HEAR WHAT THEY HAD JUST EXPERIENCED, ASKED THEM TO SHOW SPECIFICALLY WHERE THNov 14, 2010 · N970NA · Pilats PC1245SDR UALA2010111504235Line · leakingSMOKE TYPE VAPOR EXITING AROUND RT PACK EXHAUST VENTS. FOUND HYD LEAK JUST FWD OF LEFT AIR COND BAY. TIGHTNED LOOSE CONNECTION AND CHECKED ALL OTHER HYD LINES IN AREA. LEAK STOPPED, CLEANED AREA OF ACCESS LIQUID USING RAGS. NO FUMES NOTED IN AIR CONDITIONINNov 14, 2010 · N543UA · Boeing 757222SDR 5APR577Y46Pressure Switch · malfunctionedLANDING GEAR WOULD NOT RETRACT. WHEN THE CONTROL HANDLE WAS PLACED BACK TO THE DOWN POSITION BOTH MLG LOCKED IN THE DOWN POSITION, BUT THE NLG DIDN’T AND THE HYD HAND PUMP HAD TO BE USED TO LOCK THE NLG DOWN. PROBLEM COULD NOT BE DUPLICATED BY MX. THE HYD PNov 13, 2010 · N669AF · Pilats PC1245SDR CA101126002Line · leakingSHORTLY AFTER TAKEOFF, THE LANDING GEARS WERE SELECTED UP, THEN A LOUD WHOOSHING SOUND WAS HEARD AND WHAT APPEARED AT THE TIME AS DESCRIBED BY THE PILOTS TO BE SMOKE COMING FROM BEHIND THE INSTRUMENT PANEL IN THE FLIGHT COMPARTMENT. SOON THEREAFTER IT WAS REANov 12, 2010 · Dhav DHC8301SDR CA101115013Line · cracked(CAN) DURING LEAK CHECK FOR DEFECT 949537 NR 2 ENGINE DRIVEN PUMP HYDRAULIC PRESSURE LINE P/N: CN627-2003-003 REPLACEMENT FOUND SUCTION LINE FOR NR 2 ENGINE DRIVEN PUMP HYDRAULIC CRACKED AT PYLON SIDE. DEFECT 949966 RAISED AND SUCTION LINE P/N: CN627-2005-001Nov 12, 2010 · Cndair CL600*SDR UALA2010111504233Seal · leakingHYD FLUID DRIPPING FROM FLAP FAIRING OUTBOARD LEFT MOTOR. NR 1 SPOILER ROD END SEAL LEAKING APPROX 1 TO 2 DROPS PER CYCLE. REPLACED ACTUATOR.Nov 12, 2010 · N547UA · Boeing 757222SDR DALA1032140926Hydraulic Line · leakingDURING THE LAST THIRD PART OF FLIGHT, CREW NOTICED A FAINT SMELL IN COCKPIT THAT CAUSED MILD EYE AND NOSE IRRITATION. THE F/A REPORTED NO SMELL IN CABIN. MX FOUND LT THRUST REVERSER RETURN LINE LEAKING. INSTALLED TEMP LINE REPAIR IAW MM 20-12-04-201. LEAK Nov 11, 2010 · N926DL · Doug MD88SDR AALA20101117TUL07O-Ring · brokenSCL - CREW REPORTED LEFT HYDRAULIC SYSTEM QUANTITY LOSS. EMERGENCY DECLARED RETURNED SCL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND VERTICAL STABILIZER HYDRAULIC MAINFOLD RETURN 3 O-RING BROKEN. REPLACED O-RING AND LEAK TESTED. SYSETM GNov 10, 2010 · N345AN · Boeing 767323SDR UALA2010111004178Line · leakingFOUND ON WALK AROUND HYDRO LEAKING FROM ADP C1 OUTPUT LINE. REPLACED C1 ADP PUMP PRESSURE LINE. LEAK CHECKS OKAY. SERVICED HYDRAULICS.Nov 10, 2010 · N214UA · Boeing 777222SDR UALA2010111004170O-Ring · leakingCTR HYD LEAK, FLIGHT DIVERTED. CENTER HYD QTY DROPPING TO .49. REFILL EICAS CENTER HYD SYS TURNED OFF. LEAKING O-RING ON RT CENTER HYDRAULIC ACCMP WAS CHANGED.Nov 10, 2010 · N677UA · Boeing 767322SDR R61A20100471Hydraulic System · malfunctionedCREW REPORTED HYD SYS 1 OVERTEMP MSG ON EICAS DURING CLIMB, DECLARED AN EMERGENCY AND RETURNED TO FIELD. MAINTENANCE T/S PER AMM AND REPORTED ACMP NR 1 WAS AT FAULT. MTX SWAPPED ACMP NR 1 WITH ACMP 3B AND PLACED ON MEL. A/C WAS THEN RETURNED TO SERVICE.Nov 7, 2010 · N812MD · Emb ERJ170100SUSDR A6WA201040812Fitting · leakingON TAKEOFF, NR2 MAIN TIRE BURST AS REPORTED BY CREW, ACFT RETURNED TO DEPARTURE, CREW REPORTED TO MX CONTROL, DID NOT LAND OVERWEIGHT. REF W/O 160575 FOR ALL WORK PERFORMED. FOUND NR2 BRAKE DISCONECT FITTING LEAKING. R & R FITTING AND NR1 AND NR2 TIRE AND BNov 5, 2010 · N453AW · Cndair CL6002B19SDR AALA20101103DFW05Shutoff Valve · failedDFW - RIGHT YAW DAMPER MESSAGE ALONG WITH TAIL HYDRAULIC VALVE MESSAGE DISPLAYED ON EICAS. EMERGENCY DECLARED LANDED DFW WITHOUT INCIDENT. REPLACED LEFT TAIL HYDRAULIC SHUTOFF VALVE AND GEN FIELD AND HYDRAULIC CONTROL PANEL. SYSTEM GROUND CHECKS NORMAL OPERNov 3, 2010 · N363AA · Boeing 767323SDR CA101104010Line · damaged(CAN) ON AN AMPHIBIOUS EQUIPPED AIRCRAFT, THE PILOT REPORTED A PROBLEM WITH THE WHEEL GEAR, THAT IT DID COME DOWN BUT THAT THE PUMP WOULD KEEP RUNNING. UPON INSPECTION BY MAINTENANCE PERSONNEL, A BLISTER WAS NOTED IN THE BLACK PLASTIC COVERING THE HYDRAULIC FNov 1, 2010 · Dhav DHC3SDR 2010FA0001171Line · failed(EBVR) FOUND NR 2 BRAKE SYSTEM CROSS CONNECTED, LT PEDAL OPERATES RT BRAKE, RT PEDAL OPERATES LT BRAKE. FOUND PLUMBING IN NOSE WHEEL SWAPPED. REF IPC 32-40-40-10, ITEMS 210 AND 290. CORREDTED PROBLEM BY CONNECTING LINES TO CORRECT LOCATIONS, FUNCTION CHECKNov 1, 2010 · N717LA · Amd FALCON50MYST
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