STALLION TURBINE WALTER EXP.

Descripción

19 MAY 2006 STALL TESTING FUEL …….. 120 GAL = 840 lbs. + Pilot + Co pilot 350 1190 = 1200 lbs. Empty Wt ————-2600 = total 3800 lbs. Climb: 2,000 to 9,000 ft ( monitor ITT ; which rises as you climb ) 160KIAS 2000fpm ITT 600, N1 94%, Torque , N2 1850, FF 49g/h POWER OFF STALL 9,000 ft. Clean, gear retracted no flaps (inpending) 80KIAS, (actual) 78 KIAS Landing configuration gear down, full flaps: 65KIAS, 60 KIAS BEST GLIDE Power idle, prop full feather, gear retracted, no flaps 120 KIAS—————–800fpm 110 KIAS ————-900 fpm 100 KIAS—————–900 fpm NOTE: pitch very sensitive during flight. Avoid prop over speed. Advance prop slowly when coming out of feather: Monitor N2 ISOL practice: THROTTLE : … Idle CONDITION LEVER: …………..at detent ISOL SWICTH: …… On, quickly, use condition lever as throttle ITT decreasing, torque decreasing: FCU problem, go to ISOL ITT increasing, Torque decreasing: (crossing signals) BAD NEWS NEED TO SHUT DOWN ! FLT time 1.1 hrs fuel burned 33 gal / 281lbs Fuel remaining 87 gal 609 lbs 3 landings to fullstop

Avionica

AVIONICS: AUDIO PANEL Garmin GMA 340 MULTI-FUNCTION DISPLAY UPS apollo MX20 NAV/COM GPS Garmin GNS 430 NAV/COM UPS apollo SL 30 TRANSPONDER Garmin GTX 327 AUTO PILOT S-Tec 50 with interfaced GPSS and TURN BANK INDICATOR S-Tec ENCODER AK 551 ELT AK 450 ALTIMETER V.S.I. D.G.: Collins PN5223241 S/N 3008 HSI: Collins PN5222638001 S/N 1102 FLUX: Sperry PN6645-43 S/N L1730 VOR#2: Collins PN TA6224478001 S/N 1879 AS INDICATOR: Heritalia PN21060 S/N 1102 ARTIFICIAL HORIZON CHRONOMETER COMPASS 3 AXIS ELECTRIC TRIM: Rudder with indicator, Aileron and elevator trim at control stick Elevator trim with indicator ENGINE MONITORI NG: Electronics International RPM (N1) ITT Torque RPM (N2) Oil P/T Volts/Amps ELECTRIC FLAPS: FUEL ANUNCIATOR PANEL: collector tank low level indicator main tanks selector valve position indicators FUEL MONITORING SYSTEM: electronics international Fuel flow / pressure computer EI FP5 Fuel level / quantity with PC 300 probe in each wing tank FL20A S/N 61544 Flow Technology turbine flow meter S/N 84017357 w/ EI Foxboro interface unit BATTERY: Odyssey battery: PC925 (2) 24Volt system ANUNCIATOR PANEL: Low fuel, filter bypass, gen. fail, beta, ISOL, aft and fwd. chips DUAL SPEAKERS, 4 PL INTERCOM SYSTEM

Exterior

EXPERIMENTAL TURBINE STALLION N679PB Steel frame reinforcements, 1.59 gal. pressurized collector tank, 177 gal. total fuel capacity,(170 usable) total time 95 hours, 100 hour inspection to be completed before sale. AVIONICS: AUDIO PANEL Garmin GMA 340 MULTI-FUNCTION DISPLAY UPS apollo MX20 NAV/COM GPS Garmin GNS 430 NAV/COM UPS apollo SL 30 TRANSPONDER Garmin GTX 327 AUTO PILOT S-Tec 50 with interfaced GPSS and TURN BANK INDICATOR S-Tec ENCODER AK 551 ELT AK 450 ALTIMETER V.S.I. D.G.: Collins PN5223241 S/N 3008 HSI: Collins PN5222638001 S/N 1102 FLUX: Sperry PN6645-43 S/N L1730 VOR#2: Collins PN TA6224478001 S/N 1879 AS INDICATOR: Heritalia PN21060 S/N 1102 ARTIFICIAL HORIZON CHRONOMETER COMPASS 3 AXIS ELECTRIC TRIM: Rudder with indicator, Aileron and elevator trim at control stick Elevator trim with indicator ENGINE MONITORI NG: Electronics International RPM (N1) ITT Torque RPM (N2) Oil P/T Volts/Amps ELECTRIC FLAPS: FUEL ANUNCIATOR PANEL: collector tank low level indicator main tanks selector valve position indicators FUEL MONITORING SYSTEM: electronics international Fuel flow / pressure computer EI FP5 Fuel level / quantity with PC 300 probe in each wing tank FL20A S/N 61544 Flow Technology turbine flow meter S/N 84017357 w/ EI Foxboro interface unit BATTERY: Odyssey battery: PC925 (2) 24Volt system ANUNCIATOR PANEL: Low fuel, filter bypass, gen. fail, beta, ISOL, aft and fwd. chips DUAL SPEAKERS, 4 PL INTERCOM SYSTEM: ENGINE /PROP Walter 601- D turbine 90hrs since complete rebuild by Diemech Upgraded stacks (Exhaust gas extractor) Safe Start Limiter Fire Extinguishing System AVIA V 508E-AG/84in., 3 Blade Prop S/N 93065568 Inspection and dynamic balance Oct. 20 2006

Interior

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