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FAA Service Difficulty Reports for Eclipse

Last post 04-28-2008, 10:23 AM by moriarty. 0 replies.
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  •  04-28-2008, 10:23 AM 1471

    FAA Service Difficulty Reports for Eclipse

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    FAA Service Difficulty reports for Eclipse.
    Date Tail S/N Hours Flights Unit Problem Subsystem Description
    7/29/07 116DJ 21 32 32 SENSOR FAULTY OIL TEMP RT ENG HIGH OIL TEMPERATURE CAS MESSAGE UPON LANDING. EXCEEDANCE (OIL TEMP) AFTER LANDING-ENGINE SHUTDOWN DURING TAXI. FOUND FAULTY MOT/MOP SENSOR REPLACED WITH NEW UNIT AND OPERATIONALLY CHECKED SATISFACTORY IAW EMM 79-30-04.
    8/3/07 109DJ 6 205 246 ACTUATOR MALFUNCTIONED T/E FLAPS FLAP FAIL CAS MESSAGE IN FLIGHT.  REMOVED AND REPLACED LT AND RT INBOARD FLAP ACTUATORS PER EA 500 AM CH 27-51-11.  RIGGED FLAP`S AND COMPLIED WITH SATISFACTORY FUNCTIONAL/OPERATIONAL CHECKS.
    8/22/07 131DJ 33 15 12 DISPLAY MALFUNCTIONED COCKPIT DURING TAXI FOR TAKEOFF, SMELLED SMOKE, MFD STARTED TO DIM, SMOKE BEGAN TO POUR OUT FROM UNDER PANEL, SHUT DOWN ENGINE AND TURNED OFF ALL ELECTRICS.  SUP REMOVED AND REPLACED MFD WITH A NEW UNIT PER EA 500 AMM 31-10-15.  INSPECTED ALL AREAS FORWARD OF MFD AND PFD'S TO INCLUDE HARNESSESS AND CONNECTORS NO DEFECTS OR DAMAGE NOTED.  PERFORMED ALL FUNCTIONAL CHECKS IAW AMM 31-10-00.  ALL CHECKS GOOD.
    8/29/07 130DJ 23 72 91 PROBE OBSTRUCTED PITOT/STATIC SYS ON INITIAL LEVEL OFF AT 4000 FT ACCELERATING TO 220 KEAS HAD AIRSPEED DISAGREE, YAW DAMP FAIL AND AUTO PILOT FAIL CAS MESSAGE.  AUTO PILOT DISENGAGE, AIRSPEED 224 LEFT 216 RIGHT.  SUP CLEANED PILOTS AND COPILOTS PITOT PROBES.  PERFORMED PITOT/STATIC VERIFICATION TEST.  SYSTEM OP'S CHECK GOOD, AIRSPEED/ALTITUDE MATCHED PERFECTLY IAW EA 500 AMM 34-10-00.
    9/8/07 119DJ 22 72 84 BEAM DAMAGED COCKPIT REPAIR OF FORWARD UPPER RIGHT WINDSHIELD BEAM PART NUMBER 53-111681-2005.  REPAIRED IAW ECLIPSE AVIATION SERVICE ENGINEERING MEMO, MEMO SEM 500-0076 REV A.
    9/8/07 109DJ 6 250 304 SKIN PANEL DAMAGED VERTICAL STAB VERTICAL STABILIZER LEADING EDGE PANEL HAS NUMEROUS DINGS THROUGH PAINT AND INTO COMPOSITE.  REPAIRED VERTICAL STABILIZER LEADING EDGE IAW EA500 AMM 20-09-00 AND SRM 51-70-01.  REFERENCE ECLIPSE AVIATION TECHNICAL SERVICE REGUEST FSR CASE 53-090507.
    9/10/07 119DJ 22 74 87 PROXIMITY SWITCH OUT OF ADJUST DOOR DOOR WARNING LIGHT ILLUMINATED AT TOP OF CLIMB (FL260, CABIN ALT. 3800', ROC -0) 30 MINUTES LATER ON DESCENT UPON REACHING 10,000 FT, LIGHT WENT OUT (2500 CABIN ALT AP: 5.4, ROC 0).  ADJUSTED AFT DOOR LOCK PROX SWITCH AND COMPLIED WITH DOOR TEST IAW EA500 AMM 52-00-00-071-011.
    9/25/07 135DJ 36 41 41 DISPLAY MALFUNCTIONED COCKPIT INTERMITTENT COM 1 TRANSMIT PROBLEM ON CLIMB OUT.  ON COM 2 DISPLAY ON L PFD, R PFD/COM.  WORKED NORMALLY UNTIL LEVEL AT CRUISE.  THEN UNABLE TO TR/RX ON COM 1 ON EITHER SIDE.  COM 2 FUNCTIONED NORMALLY, BUT THEN STUCK ON 121.8 (LAST FREQ IN ACTIVE).  ACTIVE (WINDOW) AND UNABLE TO SWAP FREQUENCY OR CHANGE STBY MORE THAN 1 MBZ 5 MINUTES LATER L PFD COM1/COM2 BUTTON CONTROLLED COM1/COM 2SELECTION ON R PFD. MINUTES LATER L PFD NAV FUNCTIONS FAILED INCLUDING NAV1,NAV2 WORKED BUT WAS UNCHANGEABLE IN FREQUENCY FIELDS. LANDING WHITE ADVISORY CAS "AVIONICS DATA BUSS FAIL".  REMOVED AND REPLACED LEFT PFD WITH A REPAIRED UNIT IAW EA500 AMM 31-10-16.  PERFORMED OPERATIONAL CHECKS OF LEFT PFD IAW EA500 AMM 31-00-00, NO DEF
    10/1/07 135DJ 36 43 44 COAX DEFECTIVE NR 1 COMM NR 1 COMM WOULD NOT TRANSMIT OR RECEIVE DURING FLIGHT.  HAPPENED DURING CLIMB FROM FL 090 TO 110.  FOUND BAD COMM NR 1 COAX CABLE.  REMOVED AND REPLACED COMM NR 1 COAX CABLE IAW EA500 AMM 23-10-00.  PERFORMED VOICE COMMUNICATION ADJUSTMENT TEST IAW EA500 AMM 23-10-00.  CHECKED GOOD.  RESECURED AND PERFORMED ADJUSTMENT TEST OF LEFT PFD IAW EA500 AMM 31-10-00.  OPS CHECK GOOD.  VERIFIED TRANSPONDER NR 1 AND NR 2 COMPLY WITH FAR 91.413 APPENDIX F.  PERFORMED ALTITUDE CORRELATION TEST PER PARAGRAPH C OF FAR PART 43 APPENDIX E.  NO DATA CORRESPONDENCE ERRORS FOUND FOR TRANSPONDERS NR 1 AND NR 2.
    10/2/07 119DJ 22 114 138 ADC OUT OF TOLERANCE ZONE 200 AIRSPEED DISAGREE CAUTION DURING TAKEOFF ROLL.  LEFT PFD INDICATED 55 KTS, RIGHT PFD INDICATED 65KTS. PERFORMED PITOT AND STATIC VERIFICATION TEST IAW EA500 AMM 34-10-00.  FAILED AT 6000 FEET AND 71 KNOTS.  REMOVED AND INSTALLED A NEW NR 2 AIR DATA COMPUTER IAW EA500 AMM 34-10-16.  PERFORMED FLIGHT ENVIRONMENT DATA ADJUSTMENT AND TEST IAW EA500 AMM 34-10-00.  OPS CHECK GOOD.
    10/4/07 119DJ 22 119 142 DISPLAY MALFUNCTIONED LT PFD BECAME PIXELATED ON FINAL APPROACH, COMPLETLEY UNUSEABLE, RT PFD DISPLAY WERE FINE. PROBLEM CLEARED UP FEW MINUTES LATER.  REMOVED AND REPLACED LT PFD IAW EA500 AMM 31-10-16.  PERFORMED DISPLAY AND CONTROL PANEL ADJUSTMENT/TEST IAW AMM 31-10-00 AND TRANSPONDER SYSTEM ADJUSTMENT/TEST IAW AMM 34-50-60. ALL CHECKS GOOD. VERIFIED NR 1 AND  NR 2 COMPLY WITH FAR 91.413, AND FAR 43 APPENDIX F. PERFORMED ALTITUDE REPORTING CORRELATION TEST IAW PARA.(C) OF FAR PART 43 APPENDIX E, NO DATA CORRESPONDENCE ERRORS FOUND FOR TRANSPONDER NR 1 AND NR 2.
    10/5/07 134DJ 35 89 88 CABLE OUT OF RIG YAW DAMPER ON T/O ROLL, APR ARMED, THE A/P INOP AND YAW DAMPER FAIL CAS CAME ON. ABORTED TAKEOFF.  CREW PERFORMED PROCEDURES IN QRH AND A/P TEST, ALL APPEARED NORMAL. SECOND T/O SAME.  CHECKED CABLE TENSIONS ON YAW, PITCH AND ROLL SERVO'S.  FOUND ROLL SERVO TO BE OUT OF LIMITS. YAW AND PITCH CHECKED WITHIN LIMITS. RIGGED ROLL SERVO CABLE IAW EA500 MM 27-00-01. PERFORMED AUTO FLIGHT SYSTEM ADJUSTMENT TEST IAW EA500 MM 22-00-00. SYSTEM OP'S CHECK GOOD.
    10/8/07 135DJ 36 WARNING MESSAGE ILLUMINATED AIRSPEED AIRSPEED DISAGREE CAS MESSAGE DURING TAKEOFF. RWY 09 KLAL, WINDS 060 AT 10 G15, MOD RAIN, XWIND 5-8 FROM LT, SPEEDS AT ABORT 68 LT PFD, 68 STBY, 74 RT PFD. SUPPLEMENTARY INFORMATION, PERFORMED FLIGHT ENVIRONMENT DATA ADJUSTMENT TEST IAW EA500 MM 34-10-00. SYSTEM GOOD TO SPECIFICATIONS.
    10/8/07 131DJ 33 ACTUATOR STUCK ELEVATOR TRIM AFTER  TAKEOFF "ELEVATOR TRIM TAB SPLIT " ADVISORY CAS APPEARED.  LT TAB MOVEMENT WAS NORMAL AND RT TAB WAS STUCK AT 10 PERCENT NOSE DOWN.  REMOVED AND REPLACED R/H ELEVATOR TRIM ACTUATOR I/A/W EA500 M/M 27-33-15. CHECKED ELEVATOR AND ELEVATOR TRIM RIG I/A/W EA500 M/M 27-00-01, RIG CHECK GOOD.
    10/11/07 135DJ 36 54 58 ACTUATOR FAILED ZONE 700 LANDED WITH LANDING GEAR FAIL CAS.  RIGHT MAIN GEAR NOT DOWN AND LOCKED.  REMOVED AND REPLACED RIGHT MAIN LANDING GEAR ACTUATOR, OPS CHECK GOOD IAW EA500 AMM 32-30-20.
    10/23/07 131DJ 33 74 90 SENSOR MALFUNCTIONED RT ENGINE SHUT DOWN RIGHT ENGINE, ACCT LOW OIL PRESSURE WARNING.  RIGHT ENGINE OPERATED AT WINDMILL RPM FOR APPROXIMATE 20 MINUTES.  RIGHT ENGINE PARAMETERS OTHER THAN OIL PRESSURE WERE NORMAL.  REMOVED AND REPLACED RIGHT ENGINE MOP/MOT SENSOR IAW P&WC EMM 79-30-04, AND RIGHT ENGINE ACS WIRING HARNESS IAW P&WC EMM 73-20-02.
    10/24/07 134DJ 35 101 101 ACTUATOR INOPERATIVE ZONE 300 ON PREFLIGHT CAS MESSAGE UNCOMMANDED TRIM, ELEVATOR SPLIT TRIM DISPLAYED.  REMOVED AND REPLACED RIGHT ELEVATOR PITCH TRIM ACTUATOR.  OPS CHECK GOOD IAW EA500 AMM 23-33-15.
    10/24/07 145DJ 57 9 6 BRAKE RESTRICTED LEFT VERY LITTLE LEFT BRAKE ON LANDING, PEDAL TO THE FLOOR, RIGHT BRAKE IS NORMAL.  PERFORMED BRAKE BLEEDING ON BOTH BRAKES IAW 32-40-00.  BRAKES OPERATE WITH NO DEFECTS NOTED IAW EA500 M/M 32-40-00.
    10/31/07 145DJ 57 12 13 MASTER CYLINDER LEAKING ZONE 700 LEFT BRAKE INOP.  REMOVED AND REPLACED PILOTS LEFT MASTER CYLINDER (LEAKING) WITH A NEW MASTER CYLINDER IAW EA500 AMM 32-41-11.  BLED AND SERVICED BRAKE SYSTEM IAW EA500 AMM 32-40-00.  TAXI CHECK GOOD.
    11/1/07 109DJ 6 292 349 ACTUATOR MALFUNCTIONED MLG LANDING GEAR FAIL AMBER CAS MESSAGE ILLUMINATED ON TAXI IN.  FLASHED NUMEROUS TIMES AND CUTOUT NUMEROUS TIMES.  REMOVED AND REPLACED RIGHT MLG ACTUATOR WITH A NEW UNIT IAW EA500 AMM 32-30-20.  PERFORMED NORMAL EXTENSION AND RETRACTION CHECK, AND EMERGENCY EXTENSION CHECK, ALL CHECKED GOOD IAW EA500 AMM 32-30-00.
    11/6/07 145DJ 57 14 17 BRAKE WEAK MLG LT BRAKE PEDAL WENT TO THE FLOOR ON LANDING.  RAPID PUMPING RESULTED IN SLIGHT BRAKE EFFECTIVENESS.  DID NOT TO FULL PEDAL UNTIL ON RAMP. SUPPLEMENTAL INFORMATION, REPLACED LT BRAKE WITH NEW BRAKE.  PERFORMED SATISFACTORY BLEED, LEAK, AND OP'S CHECK.  SERVICED BRAKE RESERVOIR I/A/W EA 500 M/M 32-41-15 AND EA SEM 500-0063 REV A.
    11/7/07 110DJ 7 387 477 LANDING GEAR MALFUNCTIONED LEFT UPON EXTENSION, LEFT MAIN LANDING GEAR REMAINS IN TRANSIT 15 SECONDS AFTER EXTENSION ( LONGER THAN OTHER TWO GEAR).  PERFORMED 10 GEAR CYCLES IAW EA500 AMM 32-30-00.  SYSTEM OPERATES SATISFACTORY WITH NO DEFECTS NOTED. ALSO TIMED GEAR DURING 10 CYCLES AND AVERAGED 9.5 SECONDS ON DOWN TRAVEL. PERFORMED  ADJUSTMENT TEST OF MAIN GEAR/DOORS IAW EA500 AMM 32-10-00 ALL CLEARANCES AND ADJUSTMENT FOUND TO BE WITH IN LIMITS.
    11/8/07 135DJ 36 80 95 TRIM SYSTEM MALFUNCTIONED PITCH NORMAL TAKEOFF GNV, ELECTRIC PITCH TRIM INOP ON CLIMB-OUT ( NO CAS MESSAGE). USED ALTERNATE PITCH TRIM FOR LANDING (FLAPS T/O POSITION).  PERFORMED FLIGHT CONTROLS ADJUSTMENT.  TEST FOR ELEVATOR AND ELEVATOR TRIM IAW EA 500 MM 27-00-00.  ALL TEST CHECK GOOD.  PERFORMED MFD (FLCS) FLIGHT CONTROL SYNOPTIC PAGE TRIM SYSTEM TEST IAW EA500 AMM 31-10-00 WITH PILOTS AND COPILOTS SIDE STICK WITH FLAPS AT TAKEOFF, LANDING, AND THROTTLES AT MAX.  SYSTEM CHECK GOOD.  NO DEFECTS NOTED.
    11/8/07 110DJ 7 388 478 LANDING GEAR MALFUNCTIONED RIGHT DURING EVALUATION FLIGHT, RIGHT MAIN GEAR INDICATED UNSAFE IN TRANSITION-TOOK APPROXIMATELY 20 SECONDS TO INDICATE GREEN.  FIRST EXTENSION NORMAL, SECOND EXTENSION WAS WHEN GEAR INDICATED UNSAFE AND 20 SECONDS TO GREEN, DOWN AND LOCKED.  PERFORMED EXTENSION AND RETRACTION TEST OF MLG SYSTEM IAW EA500 AMM 32-30-00, NO DEFECTS NOTED WITH GREEN INDICATIONS AND TIMING.
    11/9/07 115DJ 20 190 250 FIRE BOTTLE LEAKING RT NACELLE EVIDENCE OF FIRE SUPPRESSION AGENT LEAKING INTO RIGHT ENGINE.  SUPPLEMENTAL INFORMATION, CLEANED ENGINE IAW PWC EMM 71-00-00-108-808 AND PWC FSR RECOMMENDATION LETTER.
    11/19/07 145DJ 57 15 21 MASTER CYLINDER MALFUNCTIONED COPILOT BRAKE UPON LANDING IN BOCA, COPILOTS (RIGHT SIDE) LEFT BRAKE PEDAL HAD NO PRESSURE OR BRAKING, EVEN AFTER 2 OR 3 PUMPS.  SOME BRAKING WAS RESTORED AFTER 5-7 PUMPS ON CAPTAINS LEFT BRAKE PEDAL.  SUPPLEMENTAL INFORMATION, REPLACED COPILOTS LT MASTER CYLINDER WITH A NEW CYLINDER.  RETORQED PRESSURE B-NUT IN PEDESTAL FWD AREA.  PERFORMED SATISFACTORY BLEED, LEAK,  OP'S CHECK OF BRAKE SYSTEM IAW EA 500 M/M 32-41-11, 20-05-00, 32-40-00.
    12/20/07 132DJ 34 180 211 DOOR OUT OF ADJUST ZONE 800 PASSING THROUGH 18,000 FT, DOOR CAS MESSAGE CAME ON, DESCENDING THROUGH 9000 FT DOOR LIGHT WENT OUT.  PRESSURIZATION NORMAL.  PERFORMED CABIN PRESSURIZATION TEST IAW EA500 AMM 21-30-03.  FOUND PAX DOOR TO BE OUT OF ADJUSTMENT.  ADJUSTED PAX DOOR IAW EA500 AMM 52-00-00.  PERFORMED CABIN PRESSURIZATION TEST, NO UNSAFE DOOR CAS MESSAGE, NO OTHER DEFECTS NOTED IAW EA500 AMM 21-30-03.
    1/3/08 141DJ 55 84 112 TIRE FAILED NR 1 MLG NR 1 RT MAIN GEAR TIRE BLEW AT 60 KTS ON ROLLOUT ON LANDING, NO GRAB, NORMAL TOUCHDOWN.  NR 1 REMOVED RIGHT MAIN WHEEL ASSY.  INSPECTED AXLE, BRAKE ASSY AND HARD LANDING INDICATOR.  PERFORMED A GENERAL VISUAL INSPECTION OF GEAR ASSY.  INSTALLED A SERVICEABLE WHEEL ASSY IAW AMM 32-42-00.  NO DEFECTS AT THIS TIME.
    1/9/08 158DJ 74 9 6 INDICATION SYS SPLIT AIRSPEED MX LOG PG NR1404 DISC NR 1 AND WO NR1096 AIRSPEED DISAGREE CAS MESSAGE ON TAKEOFF ROLL. ABORTED TAKEOFF. SUPPLEMENTAL INFORMATION- PERFORMED FLIGHT ENVIRONMENT DATA ADJUSTMENT TEST FOR NR 1, NR 2 ADC'S AND LT AND RT PITOT/AOA PROBES IAW MM 31-10-00. ALL TESTS CHECK GOOD. NO DEFECTS NOTED. NO MORE THAN 1 KNOT SPLIT BETWEEN NR 1, NR 2, AIRSPEEDS. SUSPECT PREVIOUS (AIRSPEED DISAGREE) TO BE CAUSED BY MOISTURE.
    1/9/08 141DJ 55 95 127 BELLCRANK BINDING AILERONS MX LOG PG. NR 0829 DISC NR 3 STICK BINDS TOP CENTER 3 DEGREES TO EITHER SIDE OF CENTER WHEN INITIATING ROLL. NOTED IN FLIGHT, BOTH LT AND RT STICKS.  WO 1098, NRI 1. REMOVED AND REPLACED RT AILERON BELLCRANK AND JOINT ASSEMBLY IAW AMM 27-11-17. PERFORMED RIG CHECK IAW AMM 27-00-00. CHECKED WITHIN LIMITS.
    1/14/08 147DJ 59 70 75 CARTRIDGE LEAKING LT EXTINGUISHER LT ENGINE FIRE EXTINGUISHER CARTRIDGE PRESSURE IN RED BAND. EVIDENCE OF LEAKAGE INSIDE COWLINGS AND ON NUMEROUS PARTS OF THE ENGINE. SUPPLEMENTAL INFORMATION- REMOVED AND REPLACED LT ENGINE PYLON FIRE EXTINGUISHER CARTRIDGE IAW MM 26-20-00 REV NR 11 FIRE SUPPRESSION AGENT CLEANUP PROCEDURES AND EMM 05-50-00 AND 71-00-00.
    1/17/08 152DJ 71 35 32 ADC MALFUNCTIONED NR 1 AIR SPEED DISAGREE CAS MESSAGE AT 80 KTS.  15 KTS SPLIT, CAPTAIN SIDE FASTER.  REMOVED AND REPLACED NR 1 ADC IAW EA500 MM 34-10-15, 34-10-00, OPS CHECK GOOD.
    1/17/08 142DJ 56 56 76 INDICATOR MALFUNCTIONED AIRSPEED AIRSPEED DISAGREE AT 45 KTS. AIRSPEED CHECK AT 25 KTS ON T/O ROLL WAS OK, WIND 160/9 LIGHT RAIN. USED RUNWAY 11. SUPPLEMENTAL INFORMATION.  INSPECTED PITOT/STATIC DRAIN LINES, NO WATER FOUND. PERFORMED PITOT STATIC LEAK CHECK AND PITOT/STATIC PROBE VERIFICATION TEST IAW MM 31-10-00 ON BOTH ADC 1 AND ADC 2 SYSTEMS SIMULTANEOUSLY. ALL ALTITUDES AND AIRSPEEDS CHECKED GOOD. NO AIRSPEED DISAGREE CAS MESSAGE. NO DEFECTS NOTED.
    1/17/08 158DJ 74 13 13 TIRE FAILED MLG DISC NR 2-RT MAIN TIRE FAILED ON LANDING. SUPPLEMENTAL INFORMATION-REMOVED FAILED TIRE. INSPECTED RT AXLE, GEARDOOR,UNDER WING, FUSELAGE AND RT ENGINE. NO DEFECTS NOTED. INSTALLED SERVICEABLE WHEEL ASSY IAW MM 32-42-00. OK FOR SERVICE.
    1/18/08 161DJ 78 18 16 MASTER CYLINDER WEAK LT BRAKES LEFT BRAKE ON PILOT AND COPILOT FEELS SPONGY.  SUPPLEMENTAL INFORMATION, REMOVED AND REPLACED PILOTS LT BRAKE MASTER CYLINDER WITH NEW MASTER CYLINDER IAW EA 500 M/M 32-40-00.  OP'S CHECK GOOD.
    1/23/08 161DJ 78 21 18 MASTER CYLINDER WEAK LT BRAKES LEFT BRAKE SPONGY ON BOTH PILOT AND COPILOT POSITIONS.  REMOVED AND REPLACED CO-PILOTS LT MASTER CYLINDER WITH NEW MASTER CYLINDER IAW EA500 AMM 32-41-11. BLED BRAKES IAW EA 500 AMM 32-40-00.  OP'S CHECK AND LEAK CHECK GOOD.
    1/24/08 146DJ 58 93 114 WARNING MESSAGE FALSE ACTIVATION 7013348949 CAS MESSAGE AIRSPEED DISAGREE ON TAKEOFF, 70 KTS LIGHT RAIN CALM WINDS (ABORTED T/O).  PERFORMED FLIGHT ENVIRONMENT DATA ADJUSTMENT TEST IAW EA 500 M/M 34-10-00.  SYSTEM TEST AND CHECKS GOOD, NO DEFECTS NOTED.
    1/24/08 139DJ 54 70 83 CONNECTOR LOOSE CSP AFTER LIFT OFF, ON GEAR RETRACTION, GOT FOLLOWING INDICATIONS: FULL STALL WARNING, AIRSPEED MISCOMPARE, STICK PUSHER FAIL, CAPT'S AIRSPEED APPEARED NORMAL, F/O'S AIRSPEED WAS INDICATING 10-15 KTS SLOWER AND MATCHED NR 3 AIRSPEED.  STALL WARNING CONTINUED TO TOUCHDOWN.  AS PER PILOT THE 1ST OFFICERS DIGITAL READOUT WAS IN "RED" AND VARIED BETWEEN 120-115 KTS, AND STALL TAPE INDICATED UP TO 120 KTS, ALSO IN RED.  SUPPLEMENTAL INFORMATION, INSPECTED CENTER SWITCH PANEL IAW EA 500 AMM 31-10-11.  TIGHTENED CSP LT CONNECTOR 91A01P01 IAW EA 500 AMM 31-10-11.  PERFORMED CSP TEST IAW EA 500 AMM 31-10-00.  OP'S CHECK GOOD, NO DEFECTS NOTED.
    1/24/08 153DJ 72 31 35 ACTUATOR DEFECTIVE LT MLG LANDING GEAR FAIL CAS MESSAGE DISPLAYED IN FLIGHT AFTER GEAR RETRACTION.  LEFT MAIN GEAR INDICATED UNSAFE AFTER SELECTING GEAR HANDLE DOWN, THREE GREEN INDICATED (GEAR DOWN), LANDING UNEVENTFUL.  DAYJET WORK ORDER 1218, NRI 1.  TROUBLESHOT LANDING GEAR FOUND LEFT MLG ACTUATOR DEFECTIVE.  REMOVED AND REPLACED LEFT MLG ACTUATOR WITH NEW UNIT IAW EA 500 AMM 32-30-20.  PERFORMED ALL OPERATIONAL CHECKS OF LANDING GEAR SYSTEM IAW EA 500 AMM 32-30-00.  ALL SYSTEM CHECK WERE SATISFACTORY WITH NO DEFECTS NOTED.
    1/29/08 161DJ 78 31 28 BRAKE MALFUNCTIONED MLG LEFT BRAKE FEELS SPONGY ON BOTH PILOTS PEDALS.  PUMPING THE PEDAL DOES NOT BRING THE PRESSURE BACK.   ACCESSED ALL TUBING CONNECTIONS TO ALL LEFT BRAKE COMPONENTS, ALL TUBING RUNS CHECKED FOR SECURITY AND LEAKAGE, ALL CHECKED GOOD.  VERIFIED PROPER RESERVOIR SERVICE, REPLACED LEFT BRAKE WITH NEW UNIT AND PERFORMED A SATISFACTORY BLEED, LEAK AND OPS CHECK IAW EA500 MM 32-41-15.
    2/1/08 141DJ 55 127 167 BRAKE WEAK MLG MAX PEDAL DEFLECTION REQUIRED TO STOP, SPONGY FEEL ON BRAKES.  SERVICED BRAKE RESERVOIR AND BLED BRAKES, NO DEFECTS NOTED, IAW EA 500 MM 32-40-00.
    2/1/08 145DJ 57 106 132 PITOT HEAD FAILED ZONE 200 AT ABOUT 300 FT AGL ON T/O EXPERIENCED STALL WARNING CAS MESSAGE, AND AURAL WARNING PFD NR 1 A/S WAS 120KTS, PFD NR 2 A/S 145KTS AND MFD AS 145KTS, FOLLOWED BY A/S DISAGREE, STICK PUSHER CAS MESSAGE.  DAYJET WO NR 1283 NRI 1.  TROUBLESHOT SYSTEM FOUND BAD LEFT AND RIGHT PITOT.  AOA PROBES IAW EA500 AMM 34-00-00.  REPLACED PROBES IAW EA500 AMM 34-10-10. PERFORMED LEAK CHECK AND STATIC VERIFICATION CHECK IAW EA500 AMM 34-00-00.  ALL SYSTEMS CHECKED GOOD.
    2/4/08 146DJ 58 103 126 TIRE FLAT LT MLG DURING ROLLOUT, LEFT MAIN TIRE WENT FLAT.  SUPPLEMENTAL INFORMATION, REMOVED AND REPLACED LEFT MAIN WHEEL ASSY, INSPECTED FLAPS, ENGINE AND UNDERWING.  NO DAMAGE FOUND IAW EA 500 M/M 32-42-00.
    2/4/08 160DJ 77 42 43 PROBE MALFUNCTIONED PITOT/STATIC CENTER AIRSPEED AND ALTIMETER READS 200 FEET LOW AND 20 KNOTS RESPECTIVELY UP TO CRUISE ALTITUDE OF 2200 FEET.  REMOVED AND REPLACED STANDBY PITOT/STATIC PROBE WITH SERVICEABLE PROBE IAW EA500 AMM 34-10-12. PERFORMED STANDBY PITOT/STATIC VERIFICATION TEST.  OPS CHECK GOOD IAW EA500 AMM 34-10-00.
    2/4/08 153DJ 72 42 49 OUTFLOW VALVE DEFECTIVE ZONE 100 AT ALTITUDE THE DOOR LIGHT CAME ON, FOLLOWED BY CABIN DP HIGH LIGHT DP NOTED AS 8.6 PSI W/CABIN ALTITUDE INDICATING MUCH LOWER THAN NORMAL.  TURNED OFF THE AIR SOURCE SELECTOR AND DESCENDED.  CABIN ALTITUDE INDICATED, 500 FEET, EVEN AFTER DUMPING THE CABIN ON FINAL APPROACH, AND ON THE GROUND W/THE CABIN DOOR OPEN.  REFERENCE WORK ORDER 1296, NRI 1.  REPLACED SECONDARY OUTFLOW VALVE PER EA500 AMM 21-30-13. ADJUSTED DOOR SENSOR PER EA500 AMM 52-00-00. PERFORMED PRESSURIZATION TEST PER EA500 AMM 21-30-03.  OPS CHECK GOOD, NO FAULTS OR DEFECTS FOUND.
    2/5/08 139DJ 54 91 110 OUTFLOW VALVE DEFECTIVE ZONE 100 PRESSURIZATION OVER PRESSURIZING AT 18,000 FEET.  CABIN ALTITUDE READS +250 FEET AND 8.4 DIFFERENTIAL.  ON DECK WITH DOOR OPEN CABIN PRESSURE READS 600 FEET.  REFERENCE DAYJET WORK ORDER 1299, NRI 2.  REMOVED AND REPLACED PRIMARY OUTFLOW VALVE IAW EA500 AMM 21-30-12.  PERFORMED CPCS OUTFLOW VALVE ADJUSTMENT/TEST IAW EA500 AMM 21-30-01.  OPS CHECK GOOD.  PERFORMED PRIMARY AND SECONDARY OUTFLOW VALVE DELTA-P LIMITER TEST IAW EA500 AMM 21-30-03.  OPS CHECK GOOD.
    2/5/08 145DJ 57 108 134 TIRE FAILED ZONE 700 AFTER TOUCHDOWN, BOTH MAIN TIRES FAILED.  REMOVED UNSERVICEABLE WHEEL AND BRAKE ASSEMBLIES ON BOTH LEFT AND RIGHT LANDING GEAR.  INSPECTED LANDING GEAR, UNDER WINGS, FLAPS, AIRCRAFT, AND ENGINES BOTH LEFT AND RIGHT ON AIRCRAFT. NO DEFECTS NOTED. INSTALLED NEW SERVICEABLE BRAKE ASSEMBLIES AND INSTALL REPAIRED SERVICEABLE WHEEL ASSEMBLIES, BOTH LEFT AND RIGHT.  SERVICED AND BLED BRAKES.  WORK COMPLETED IAW EA500 AMM CHAPTER 32 PER 40, 41, 42.
    2/5/08 163DJ 81 19 18 PROXIMITY SWITCH OUT OF ADJUST PAX DOOR DOOR CAS MESSAGE ON AT 17,200 FEET ALTITUDE, DP 6.2, CABIN ALTITUDE 1750 FEET.  CAS MESSAGE OFF AT 10,000 FEET ALTITUDE, 1,000 FEET CABIN ALTITUDE AND 4 DP.  ADJUSTED FORWARD DOOR SENSOR, AND PRESSURIZED AIRCRAFT IAW EA500 AMM 52-00-00 AND 21-30-03.  NO CAS MESSAGE.  ALL CHECKS GOOD.
    2/5/08 132DJ 34 208 245 INDICATION SYS MALFUNCTIONED FUEL FUEL IMBALANCE CAS MESSAGE, AUTO TRANSFER LEFT TO RIGHT RESULTED IN FUEL BEING PUMPED OVERBOARD THROUGH RIGHT WING VENT DURING TAXI.  COMPLIED WITH WALK AROUND INSPECTION TO CHECK VENTS AND TANKS.  CONNECTED AMC TO AIRCRAFT IAW EA500 AMM 25-40-00 FOR GAUGING WET TEST ALL PROBES, CHECKED GOOD, ALSO COMPLIED WITH MFD FUEL SYNOPTIC TEST PAGE CHECK IAW EA500 AMM 31-10-00.  WITH ENGINES RUNNING COMPLIED WITH EA500 AMM FUEL SYSTEM CHECK 28-00-00, CHECKED GOOD.
    2/5/08 139DJ 54 91 110 ACTUATOR DEFECTIVE RUDDER TRIM UNCOMMANDED TRIM IN FLIGHT, ON GROUND.  ELEVATOR TRIM GOING UP AND DOWN AND SPLIT.  REFERENCE DAYJET WORK ORDER 1299, NRI 1 AND 3.  REFERENCE TSR 22-020608G AND NRI 1 FOR RUDDER TRIM ACTUATOR REPLACEMENT.  REMOVED AND REPLACED RUDDER TRIM ACTUATOR WITH NEW ACTUATOR IAW EA500 AMM 27-23-16.  PERFORMED OPERATIONAL CHECK OF RUDDER TRIM ACTUATOR IAW EA500 27-00-01.  OPS CHECK GOOD.
    2/6/08 162DJ 79 50 49 TIRE FAILED MLG NUMBER 1 TIRE FLAT ON LANDING.  REMOVED NR 1 WHEEL ASSEMBLY AND INSTALLED A SERVICEABLE WHEEL ASSEMBLY IAW EA500 AMM 32-42-00.
    2/7/08 158DJ 74 23 21 INDICATOR MALFUNCTIONED AIRSPEED ON TAKEOFF ROLL, NO AIRSPEED INDICATIONS ON LEFT PFD, MFD AND RIGHT PFD INDICATED UP TO 65KTS PRIOR TO ABORT.  CONNECTED BARFIELD DPS 450 TO AIRCRAFT IAW AMM 34-10-00-070-701 TO SIMULATE AIRSPEED ON LEFT PFD.  AIRSPEED CORRESPONDED WITH TEST BOX.  SUSPECT MOISTURE WAS PRESENT EARLIER.
    2/7/08 132DJ 34 208 245 PROBE DEFECTIVE ZONE 600 FUEL VENTING OVERBOARD ON RIGHT WING AFTER ENGINE START.  TOTALIZER READ 1,470 LBS, RIGHT WING INDICATED 680 LBS, LEFT WING 750 LBS.  VISUALLY JET WAS TOPPED OFF.  AFTER START JET AUTO TRANSFER FUEL FROM LEFT TO RIGHT.  DEFUELED AND SUMPED PER EA500 AMM 12-10-01.  PERFORMED FUEL PROBE CALIBRATION AND FUEL GAUGING TEST IAW EA500 AMM 28-40-00.  RIGHT SIDE FAILED TEST.  FOUND BAD PROBE IN BAY 9 AND 12. REMOVED AND REPLACED BAD PROBE IAW EA500 AMM 57-10-11.  PERFORMED ATP DATA ENTRY FOR NEW PROBES, DRY CALIBRATION AND WET CALIBRATION TEST PER EA500 AMM 28-40-00.  CHECKED GOOD.
    2/11/08 115DJ 20 289 387 FIRE BOTTLE LEAKING NR 2 NACELLE NR 2 ENGINE FIRE BOTTLE IS LEAKING, IT WAS LEAKING WHEN DISCONNECTED FOR 300 HOUR, NO EXTERNAL LEAK ON ENGINE.  REMOVED AND REPLACED WITH NEW RIGHT PHOSTREX BOTTLE IAW EA500 AMM 26-20-10.  INSPECTED ENGINE AND UPPER AND LOWER COWL FOR ANY PHOSTREX RESIDUE AND CLEANED AS REQUIRED.  FOLLOWING CLEANUP PROCEDURES IAW EA500 AMM 26-20-00.  SUPPRESSION AGENT CLEANUP PROCEDURES AND EMM 05-50-00-210-811, 05-50-16-021-801, AND 71-00-00.
    2/15/08 152DJ 62 90 95 WINDOW FRAME DAMAGED COCKPIT PART WAS DAMAGED IN MAINTENANCE, DURING WINDSHIELD REPLACEMENT
    2/15/08 152DJ 62 90 95 WINDOW FRAME DAMAGED FUSELAGE DAMAGED IN MAINT DURING WINDSHIELD REPLACEMENT.
    2/18/08 145DJ 57 121 148 WIRE HARNESS CHAFED APC FUEL GAUGING FAULT CAS MESSAGE.  ASSIGNED TO MDDR CONTROL NR 421.  A/C RELEASED PER MEL 28-01. OK FOR SERVICE.  REFERENCE DAYJET WORK ORDER 1396, NR-00001. TROUBLE SHOT FUEL GAUGING FAULT, FOUND HARNESS 39A01P05 OFF THE LEFT APC CHAFED AND TO BE DEFECTIVE.  REMOVED AND REPLACED HARNESS IAW EA500 WRM.  PERFORMED OPERATIONAL CHECKS IAW EA500 AMM 28-40-00, 71-00-00, AND 31-10-00, NO DEFECTS WERE NOTED.  FUEL GAUGING SYSTEM FUNCTION WITH NO DEFECTS NOTED.
    2/19/08 142DJ 56 75 99 AHRS MALFUNCTIONED ZONE 200 ON CLIMB-OUT , AHRS FAILED AND STICK PUSHER FAILED.  SUPPLEMENTAL INFORMATION, REMOVED AND INSTALLED AHRS NR 1 IAW EA 500 AMM 34-20-11.  PERFORMED ATTITUDE AND DIRECTION SYSTEM ADJUSTMENT TEST FOR AHRS.  SYSTEM CHECKS GOOD IAW 34-20-10.  DURING TROUBLESHOOTING ADC1 WAS ELECTRICALLY DISCONNECTED THEN RECONNECTED.  PERFORMED FLIGHT ENVIRONMENT DATA ADJUSTMENT TEST FOR ADC IAW EA 500 AMM 34-10-00.  ALL TESTS CHECK GOOD.  VERIFIED TRANSPONDER NR 1 AND NR 2 COMPLIED WITH FAR 91.413 AND FAR PART 43 APPENDIX F.  PERFORMED ALTITUDE REPORTING CORRELATION TEST PER PART (C) OF FAR 43 APPENDIX E.  NO DATA CORRESPONDENCE ERRORS FOUND FOR TRANSPONDERS NR 1 OR NR 2.
    2/19/08 153DJ 72 44 52 OUTFLOW VALVE DEFECTIVE ZONE 100 FIELD ELEVATION SET AT 200 FT', AIRCRAFT LANDED PRESSURIZED (2.0) PSI.  USED MAN/DUMP BUT COULD NOT DEPRESSURIZE EVEN AFTER ENGINE OF, FINALLY DEPRESSURIZED.  REFERENCE DAYJET WORK ORDER 1425, NRI 1.  REMOVED AND REPLACED PRIMARY AND SECONDARY OUTFLOW VALVES IAW EA500 AMM 21-30-12 AND 21-38-13.  OPS CHECK GOOD.
    2/21/08 146DJ 58 128 154 UNKNOWN UNKNOWN DURING T/O ROLL, CAS MESSAGE AIRSPEED DISAGREE AT 45KTS.  REFERENCE DAYJET WORK ORDER 1434, NR-00002.  CHECKED FOR WATER IN THE PITOT DRAINS IAW EA500 AMM 34-10-00.  NO WATER FOUND.  FOUND CODE 764 - AIRSPEED MISCOMPARE.  C/W  FLIGHT ENVIROMENT DATA ADJUSTMENT/TEST IAW EA500 AMM 34-10-00.  SYSTEM TEST AND CHECKS GOOD AT THIS TIME.  NO DEFECTS NOTED.
    2/22/08 163DJ 81 32 34 UNKNOWN UNKNOWN NR 1 ENGINE DURING T/O ROLL, NR 1 ENGINE OIL PRESSURE 8.2 PSI, AMBER, DISCONTINUED T/O.  PERFORMED ENGINE RUN OIL PRESSURE GOOD AT IDLE AND MAX POWER.  AT MAX POWER READ 5.2 ON LEFT ENGINE AND 4.9 ON RIGHT ENGINE.  OPS CHECK GOOD IAW EA500 AMM 71-00-00.
    2/23/08 141DJ 55 154 198 BELLCRANK BINDING AILERONS INSPECT LEFT AND RIGHT AILERON BELLCRANKS FOR CONDITION AND SECURITY.  INSPECTED AILERON CONTROLS FROM AFT SECTOR TO BELLCRANK AND FOUND RIGHT BELLCRANK WITH EXCESSIVE FRICTION SEE NR-00002.  REMOVED RIGHT AILERON TO GAIN ACCESS. REPLACED AILERON JOINT FITTING ASSEMBLY WITH NEW UNIT IAW EA500 AMM 27-11-18.  INSTALLED AILERON AND CHECKED FOR PROPER RIGGING IAW EA500 AMM 27-11-21.  CHECKED AILERON SYSTEM FOR FRICTION, NO DEFECTS NOTED.
    2/25/08 146DJ 58 129 156 MOTOR FAILED ELEVATOR TRIM ELEVATOR TRIM TAB SPLIT, UNABLE TO TRIM OFF PRESSURE DURING NORMAL FLIGHT THROUGH HAT SWITCH AND FLCS PAGE.  SUPPLEMENTAL INFORMATION, VERIFIED DISCREPANCY AND TROUBLESHOT A BAD LT ELEVATOR TRIM ACTUATOR.  REMOVED AND REPLACED LT ELEVATOR TRIM ACTUATOR.  ALL OP'S CHECKS SATISFACTORY IAW EA 500 AMM 27-33-15.
    2/25/08 136DJ 37 170 212 FIRE BOTTLE LEAKING RT NACELLE RIGHT ENGINE FIRE BOTTLE LEAKING.  REMOVED ENGINE COWLINGS AND PYLON PANELS, RIGHT SIDE FOR ACCESS.  REMOVED RIGHT FIRE BOTTLE IAW EA500 AMM 26-20-10.  INSTALLED A NEW RIGHT ENGINE FIRE BOTTLE IAW EA500 AMM 26-20-10.  RE INSTALLED ENGINE COWLINGS AND PYLON PANELS AS REQUIRED IAW EA500 AMM 26-20-10.
    2/26/08 139DJ 54 112 140 BELLCRANK BINDING AILERONS AILERONS STIFF, A/P HAS DIFFICULTY RESPONDING TO FD COMMANDS ALSO.  INSTALLED A NEW LEFT AILERON BELLCRANK IAW EA500 AMM 27-11-17.  INSTALLED A NEW LEFT AILERON JOINT ASSEMBLY IAW EA500 AMM 27-11-18.  C/W FLIGHT CONTROLS ADJUSTMENT/TEST (FUNCTIONAL CHECK) IAW EA500 AMM 27-00-00-071-801-B.
    2/27/08 142DJ 56 77 102 FLAP OUT OF ADJUST RIGHT FOUND RIGHT FLAP, OUTBOARD END TO BE .5 DEGREE HIGHER THAN THE INBOARD END AND THE WHOLE LEFT FLAP.  THIS IS WITHIN LIMITS, ADJUSTED TO MATCH THE INBOARD END AND THE LEFT FLAP IAW EA500 AMM 27-50-00.  RIG CHECKED BOTH AILERONS AND FOUND THEM TO BE THE SAME AND WITHIN AMM LIMITATIONS.  RIG CHECKED THE ELEVATOR AND ELEVATOR TRIM TABS AND FOUND THEM TO BE THE SAME AND TO BE WITHIN AMM LIMITS, PERFORMED ALL RIG CHECKS AND ADJUSTMENTS IAW EA500 AMM 27-00-00.  REFERENCE LOGBOOK PAGE 0897, ITEM 3.  EVALUATION FLIGHT UNSATISFACTORY.  IN CRUISE, FLAPS UP, 220 KNOTS, AILERON TRIM REQUIRED 41 PERCENT LWD.  WITH FLAPS LDG, 105 KTS, REQUIRED 37 PERCENT LWD.  PITCH TRIM NORMAL.  REFERENCE LOGBOOK PAGE 0898, ITEM 1, AND DAYJET WORK ORDER 1484, NR-00001.  ADJUSTED LEFT AND RIGHT AILERONS IAW EA500 AMM 27-00-00.  OPS CHECK GOOD.  REFERENCE LOGBOOK PAGE 0898, ITEM 2.  EVALUATION FLIGHT UNSATISFACTORY. REFERENCE LOGBOOK PAGE 0898, ITEM 3. AT 160 KTS, 3500", FLAPS UP, REQUIRED 23% LWD AILERON TRIM. AT 220 KTS, REQUIRED 91% LWD. SAME TRIM REQUIRED WITH YAW DAMPER OFF.
    2/29/08 161DJ 78 71 73 PROXIMITY SENSOR OUT OF ADJUST DOOR CLIMBING THROUGH FL 230, GOT DOOR WARNING CAS.  VISUALLY INSPECTED THE DOOR LOCKS (5 GREEN).  CAS CLEARED BELOW 10,000 FT, LANDING IN GNV.  INSPECTED DOOR PROX SENSOR.  FOUND SENSOR TO BE OUT OF ADJUSTMENT.  ADJUSTED SENSOR AND PERFORMED SENSOR TEST.  NO UNSAFE DOOR CAS MESSAGES NOTED.  TEST CHECKED GOOD IAW EA500 AMM 52-00-00.
    3/2/08 142DJ 56 78 104 SPRING DAMAGED AILERON TRIM REPLACED AILERON TRIM SPRING WITH NEW TRIM SPRING IAW AMM 27-11-20.  PERFORMED AILERON TRIM SYSTEM ADJUSTMENT/TES IAW AMM 27-00-01.  SYSTEM TEST AND CHECKS GOOD, NO DEFECTS NOTED.   ITEM 1.  FLIGHT WAS UNSATISFACTORY.  AT 220KTS 82 PERCENT OF TRIM WAS REQUIRED TO MAINTAIN STRAIGHT AND LEVEL FLIGHT.  AT 160 KTS 30 PERCENT TRIM (AILERON TRIM) WAS REQUIRED.   PERFORMED FLAP RIGGING IAW AMM 27-50-00 AND EA TSR 27-030408G.  RIG CHECKED GOOD.  VERIFIED FLAPS ARE AT 0 PERCENT.  EVALUATION FLIGHT UNSATISFACTORY.   AT 250 KTS REQUIRES AILERON TRIM IN EXCESS OF 101 PERCENT LWD.  AT 220 KTS, 37 PERCENT LWD.  AT 160 KTS, 23 PERCENT LWD.   FOUND RT FLAP TO HAVE EXCESSIVE PLAY, ADJUSTED FLAP IAW AMM 27-50-00.  FLAPS OPERATE NORMAL WITHIN LIMITS.  EVALUATION FLIGHT UNSATISFACTORY.  REQUIRES EXCESS LWD AILERON TRIM 250 KTS - 100 PERCENT LWD, 220 KTS - 34 PERCENT LWD 160 - 27 PERCENT LWD.
    3/4/08 153DJ 72 61 74 GPS MALFUNCTIONED DME AND GS INDICATIONS FAILED IN FLIGHT.  TRIED GNV, OCF, LAL BUT NO DME.  DURING RTB, DME AND GS CAME BACK INTERMITTENT.  SUPPLEMENTAL INFORMATION, PERFORMED GPS ADJUSTMENT TEST IAW EA 500 AMM 34-50-10.  NO DEFECTS NOTED AT THIS TIME.  PERFORMED A/C TAXI AND VERIFIED GROUND SPEED INDICATION ON BOTH PFD'S IAW EA500 AMM 9-20-00.
    3/4/08 163DJ 81 44 48 TRIM SYSTEM MALFUNCTIONED AILERONS WHILE HAND FLYING, AILERON TRIM DOES NOT SEEM TO WORK TO THE RIGHT EVEN WITH FULL DEFLECTION.  OK TO THE LEFT.  TRIM INDICATION MOVES OK.  SUPPLEMENTAL INFORMATION, PERFORMED AILERON TRIM FUNCTIONAL TEST IAW EA500 AMM 27-00-00 SUB TASK 27-00-00-071.  ALL CHECKS GOOD.  PERFORMED AILERON FRICTION CHECK IAW ECLIPSE TSR NR 27-030308G REV A DATED 03-03-08 ALL CHECKS GOOD.  SUPPLEMENTAL INFORMATION, REFERENCE LOGBOOK PAGE 1762, ITEM 2.  EVALUATION FLIGHT UNSATISFACTORY, LOGBOOK PAGE 1762, ITEM 3.  REQUIRES RWD AILERON TRIM AT HIGH AIRSPEEDS 250 KTS - 101 PERCENT RWD, 220 KTS - 84 PERCENT RWD, 200 KTS - 47 PERCENT RWD, 180 KTS AND BELOW, NO AILERON TRIM REQUIRED.  REFERENCE DAYJET WORK ORDER 1540, NR-00001,2,3.  COMPLIED WITH ECLIPSE TSR 27-030508G REV C.  NO DEFECTS NOTED.  PERFORMED AILERON FRICTION TEST, AILERON TENSION TEST AS PRESENTED IN SEC 12.3 PAGE 35 OF FLIGHT CONTROL RIGGING SPEC 27-109841 REV 5.  PERFORMED MEASUREMENT OF AILERON SKIN CONTOUR EAC AERO AE20 07-500-015.
    3/4/08 160DJ 77 55 60 AUTOPILOT SYS MALFUNCTIONED ON FLIGHT FROM SAV TO GNV DURING CRUISE, AUTO PILOT TRIMMED 79 PERCENT LWD.  AIRPLANE FLEW NORMALLY WITH A/P DISCONNECTED, 79 PERCENT LWD EARLIER LEGS, AILERON TRIM 0 TO 10 PERCENT LWD.  PERFORMED FLIGHT CONTROL CHECKS IAW EA500 AMM 27-00-00.  NO DEFECTS NOTED.
    3/7/08 142DJ 56 80 107 AILERON OUT OF RIG COMPLIED WITH ECLIPSE TSR 27-030508G REV C.  NO DEFECTS NOTED.  PERFORMED AILERON FRICTION TEST, AILERON TENSION TEST AS PRESENTED IN SEC 12.3, PAGE 35 OF FLT CONTROL RIGGING SPEC. 27-109846 REV. 5, PERFORMED MEASUREMENT OF AILERON SKIN CONTOUR EAC AERO 07-500 015 SDR REV C.  REFERENCE LOGBOOK PAGE 0901 ITEM 1.  EVAL FLIGHT UNSATISFACTORY, AIRCRAFT STILL REQUIRES EXCESSIVE AILERON TRIM.
    3/13/08 163DJ 81 45 50 SELECTOR SWITCH DEFECTIVE ELEVATOR TRIM ELEVATOR TRIM SPLIT - LEFT TAB FROZEN AT 7 PERCENT.  REMOVED AND REPLACED CENTER SWITCH PANEL WITH NEW UNIT.  PERFORMED TEST IAW EA500 AMM 31-10-00.  CSP TEST GOOD.
    3/13/08 163DJ 81 45 50 RUDDER OUT OF ADJUST AIRCRAFT REQUIRES 100 PERCENT RWD AT 252 KTS, WITH 16 PERCENT LEFT RUDDER.  REFERENCE WORK ORDER 1602, NR-00001.  PER TSR 27-030508G, REV C.  AIRCRAFT IS WITHIN SPECIFICATION AND NO FURTHER MAINTENANCE ACTION IS REQUIRED AT THIS TIME ON STATED CONDITION.
    3/13/08 142DJ 56 82 109 FLAP SYSTEM OUT OF ADJUST TE FLAPS AIRCRAFT REQUIRES 12 PERCENT LWD WITH 7 PERCENT RUDDER AT 160 KTS, 88 PERCENT LWD WITH 0 PERCENT RUDDER AT 160 KTS.  REFERENCE DAYJET WORK ORDER 1600, NR-00001.  TEMPORARILY INSTALLED 2 EACH GURNEY TABS ON THE RT WING FLAP IAW SEM 500-0096 REVISION B DATED 3/20/2008.  UPON COMPLETION OF TEST FLIGHT, IF PROBLEM IS CORRECTED, RETURN AIRCRAFT TO GNV SERVICE CENTER FOR PERMANENT ATTACHMENT OF GURNEY TABS IAW SEM 500-0096 REVISION B DATED MARCH 20, 2008.  REFERENCE LOGBOOK PAGE 0902, ITEM 1.  EVALUATION FLT COMPLETED, DATA FORWARDED TO MAINTENANCE ENGINEERING FOR REVIEW.  REFERENCE WORK ORDER 1676, NR-00001.  INSTALLED 2 GURNEY TABS ON RIGHT OUTBOARD FLAP TRAILING EDGE IAW SEM 500-0096 REVISION B.
    3/14/08 146DJ 58 139 173 STEERING SYS MALFUNCTIONED NLG TAKING THE RUNWAY AT A SLOW SPEED, AND STEERING DISPLACEMENT AT 10 PERCENT TO 15 PERCENT RATE OF TURN.  AIRCRAFT LOST STEERING CAPABILITY (CASTERED), TRY TO REENGAGE 2 TIMES, RETURN TO GATE.  REMOVED NOSE GEAR ASSEMBLY AND INSTALLED NEW ASSEMBLY IAW EA500 AMM 32-20-10 AND TSR 32-031708G.  PERFORMED NOSE GEAR AND DOORS ADJUSTMENT/TEST IAW EA500 AMM 32-20-00.  PERFORMED STEERING ADJUSTMENT/TEST IAW EA500 AMM 32-50-00.  ALL CHECKS GOOD.
    3/17/08 162DJ 79 99 112 BELLCRANK BINDING AILERON SYS IN FLIGHT AILERON FLIGHT CONTROL SIDE STICK FEELS VERY NOTCHY WHEN ROLLING LEFT OR RIGHT.  SUPPLEMENTAL INFORMATION-GAINED ACCESS TO RT AILERON JOINT, FOUND IT TO BE BINDING.  REPLACED JOINT AND BELLCRANK WITH NEW.  CHECKED LT AILERON JOINT AND FOUND IT TO BE FREE MOVING.  ALL WORK DONE IAW EA500 MM TR 27-1, 27-11-18 AND 27-11-17.  LT AND RT AILERON POS 4 PUSH RODS ARE BOTH SECURED AND SAFETIES IAW EA500 MM 27-11-16.  NO ROD ADJUSTMENTS WERE DONE.  ACCESS PANELS REINSTALLED IAW EA500 MM 06-50-00.  REMOVAL AND INSTALLATION OF RT AILERON DONE IAW EA500 MM 27-11-21.  PERFORMED FUNCTIONAL TEST (TRAVEL CHECKS) IAW EA500 MM 27-00-00-071-8-701-001.  NO DEFECTS NOTED.
    3/18/08 148DJ 61 156 185 BELLCRANK BINDING AILERON SYS FOUND LT AILERON JOINT AND BELLCRANK BINDING.  REMOVED LT AILERON, REPLACED LT BELLCRANK AND JOINT ASSY WITH NEW.  REINSTALLED LT AILERON.  VERIFIED RT AILERON DOES NOT HAVE ANY BINDING.  COMPLIED WITH SATISFACTORY OP'S CHECK OF LT BELLCRANK AND JOINT.  COMPLIED WITH TRAVEL CHECKS OF LT AND RT AILERONS.  NO DEFECTS NOTED.  ALL WORK DONE IAW EA500 MM 27-11-21, 27-11-17, TR 27-3, 27-11-18, AND 27-00-00.
    3/31/08 875NA 18 CONTROL TUBE OUT OF ADJUST PITCH TRIM AC EXPERIENCED A PITCH TRIM MALFUNCTION ON TAKEOFF ACCOMPANIED BY A WARNING MESSAGE.  AN EMERGENCY WAS DECLARED AND THE AC WAS RETURNED TO BASE.  PROBLEM WAS DUPLICATED ON THE GROUND.  AFTER TROUBLESHOOTING, IT WAS DETERMINED THAT A REPLACEMENT ACTUATOR SHOULD BE INSTALLED.  AFTER INSTALLING NEW PART, DEFECT STILL EXISTED.  FURTHER TROUBLESHOOTING REVEALED THAT THE CONTROL TUBES CONNECTED THE ACTUATOR TO THE CONTROL SURFACE WERE NOT SIMILARLY ADJUSTED.  THIS CONDITION CAUSED A BINDING OF THE SYS MECHANICS AND THE SUBSEQUENT FAILURE.  WHEN THE CONTROL TUBES WERE SIMILARLY ADJUSTED, THE SYSTEM OPERATED CORRECTLY ON GROUND AND IN SUBSEQUENT OPERATIONAL CHECK FLIGHT.  (K)
    4/1/08 158DJ 71 107 116 SWITCH OUT OF ADJUST PAX DOOR DURING CRUISE FLIGHT PASSENGER DOOR WARNING LIGHT CAS MESSAGE POSTED.  ADJUSTED FWD DOORS SWITCH LAW EA 500 AMM 52-00-00.  OPS CHECK GOOD LAW EA 500 AMM 21-30-03, CABIN PRESSURE VESSEL ADJ/TEST.
    4/9/08 156DJ 73 105 124 ADC FALSE INDICATION NR 1 AIRSPEED DISAGREE CAS MESSAGE DISPLAYED DURING TAKEOFF.  SUPPLEMENTAL INFORMATION, RESOLVED ON W/O: 1826 TASKCARD: NR-00001.  REMOVED NOSE ACCESS PANEL 211CT, PILOT'S AND CO-PILOTS SEATS, DRAINED PITOT/AOA PROBES IAW AMM SUBTASK 34-10-00-061-611-00; PERFORMED PITOT/AOA LEAK TEST IAW AMM SUBTASK 34-10-00-071-701-001.  TEST GOOD; PERFORMED PITOT AND STATIC VERIFICATION TEST IAW AMM SUBTASK 34-10-00-071-701-005.  FOUND LEFT PFD AIRSPEED TO BE OUT OF LIMITS AND SUSPECT FAULTY NR 1 ADC ME 0020195 04.08.08.  REMOVED UNSERVICEABLE ADC FROM NR 1 POSITION.  INSTALLED SERVICEABLE ADC, WHICH WAS REMOVED FROM N139DJ NR 1 POSITION, AND INSTALLED IN NR 1 POSITION IAW AMM 34-10-15.  COMPLETED ADJUSTMENT/TEST OF AIR DATA COMPUTER IAW AMM 34-10-00.
    4/10/08 158DJ 74 112 123 PITOT TUBE DEFECTIVE LEFT DURING T/O, RECEIVED AIRSPEED DISAGREE AND STICK PUSHER FAIL MESSAGE.  CPT AIRSPEED INDICATED 74 KTS ON TAXI IN AND 63 KTS STOPPED ON THE RAMP.  RESOLVED ON W/O:1834 TASKCARD: NR-00001.  REPLACED LT PITOT/AOA PROBE WITH NEW PROBE IAW AMM 34-10-10.  PERFORMED ADJUSTMENT/TEST IAW AMM 34-10-00.  TESTED AIR DATA SYSTEM IAW AMM 34-10-00, NO AIRSPEED DISAGREE, SYSTEM CHECKS GOOD, NO DEFECTS NOTED.
    4/15/08 150DJ 62 148 165 ACTUATOR MALFUNCTIONED RUDDER TRIM MOMENTARY APPLICATION OF RIGHT RUDDER TRIM RESULTED IN TRIM RUNNING AWAY FULL RIGHT.  UNABLE TO GET ANY FURTHER TRIM MOVEMENT.  REMOVED AND INSTALLED NEW RUDDER TRIM ACTUATOR IAW EA500 AMM 27-23-16.  RIGGED AND OP'S CHECKED RUDDER IAW EA500 AMM 27-00-01 AND 27-00-00.  NO DEFECTS NOTED.
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