VT-EEY - 1976 AEROSPATIALE ALOUETTE III

1976

AEROSPATIALE

ALOUETTE III

AH186

VT-EEY

Used

VFR

Aloutte III helicopter Mfd. by HINDUSTAN AEROAUTICS LTD; BANGALORE UNDER LICENSE FRO AEROSPSALE, FRANCE. FUEL CAPACITY 560 ltrs. TANK FULL. AVERAGE FUEL CONSUMPTION 175 TO 185 litrs.per hour. Single Turbine Engine

357100.0

STRUCTURE: *CABIN *FORWARD STRUCTURE ASSEMBLY (MONO-COQUE CONSTRUCTION) *CENTRAL SECTION (WELDED TUBE TRIANGULATED CONSTRUCTION) WITH FLAW DETECTION SYSTEM INSTALLED *TAIL BOOM (MONO-COQUE CONSTRUCTION) *STABILIZERS. *2 FORWARD DOORS, 2 REARSLIDING DOORS AND 2 BAGGAGE HOLD DOORS ON EITHER SIDE BAGGAGE HOLD. LANDING GEAR: *NON RETRACTABLE TRICYCLE WHEEL TYPE. *NON RIGID WITH OLE-PNEUMATIC SHOCK ABSORBERS. *SELF CENTERING STEER ABLE NOSE GEAR (45*) *DISC TYPE HYDRAULIC PARKING BRAKE ON EACHMAIN WHEEL. TRANSMISSION. *CENTRIFUGAL CUTCH-MAIN GEAR BOX WITH TWO OUTPUTS TO DRIVE MAIN ROTOR & TAIL ROTOR. ROTORS: MAIN *3 BLADES METAL CONSTRUCTION. 363 RPM *DIAMETER :11.020 METERS. CHORD 350MM. *AIRFOIL SECTION NACA63A OF 11,5% TWIST 6*30' TAIL *3 BLADES METAL CONSTRUCTION * DIAMETER 1.912 MTRS.,2001 RPM *AIRFOIL SECTION NACAOO.15 TO OO.18 ROTOR HEAD MAIN *FULLY ARTICULATED WITH HYDRAULIC DAMPERS IN DRAG PLANE TAIL *ARTICULATED TO PERMIT INCIDENCE AND FLAPPING FLIGHT CONTROL. *THREE CANNEL MAIN ROTOR CONTROLS WITH MIXING UNIT WITHCYCLIC AND COLLECTIVE STICKS,ASSISTED BYHYDRAULIC SERVO. *TAIL ROTOR CONTROLLED BY PEDDLE WITH HYDRAULIC VIBRATION DAMPER. *DUAL CONTROLS PILOT,CO-PILOT. ELECTRICAL SYSTEM. *ENGINE DRIVEN GENERATOR CUM STARTER4000 WATTS 28.5 VOLTS *A 40 A/H, 26 VOLT BATTERY *INTERNAL LIGHTING- 2 CABIN SWIVELLIGHTS, INSTRUMENT PANELEDGE LIGHTING. 3 POSITION LIGHTS-2 ROTRY ANTICOLLUSION LIGHTS- 1 RETRACTABLE LANDING LIGHT. FURNISHING. *2 FRONT SEATS AND 2 REAR BENCHES DIMENSIONS *LENTH 10.175 MTRS. *WIDTH AT ROTORS 9.600 MTRS. *WHEEL BASE 2.608 MTRS. *HEIGHT AT ROTORS HEAD 3.000 MTRS.

MAIN: MFD.BY HINDUSTANAERONAUTICS LT: INDIA *P/N H 3160.11.30.000.03 *HRS.DONE:2324:05 TAIL: MFD. BY HINDUSTAN AERONAUTICS LTD; INDIA. *P/N H3160.34.11.000.00 *HRS. DONE 1248:45

1750

3801

SNEW

SIGLE ENGINE. DATE OF MFG. 16-05-1976 *TYPE ARTOUSTE IIIB. MFD.BY HINDUSTAN AERONUTICS LTD; INDIA UNDER LICENSE TURBOMICA, FRANCE. *POWER MAX.AT 33500 RPM 420KW (563BHP) MAX. CONTINUES AT 33500 RPM 405 KW (543 BHP)

126

1750

SOH

ALL MANDATORY MODS AS PER DGCA (INDIA) DGAC (FRANCE) & FAA (USA) ARE COMPLIED. CONVERTED FROM SE3160-2100KGS.AUW, TO SA316B 2200 KGS.AUW

VHF 1.BENDIX / KING.......KTR-908 2.BENDIX..............RT241. ADF. BENDX / KING........KDF-806 ATC X-PONDER HONEYWELL BENDIX/KING KT76C ELT ARTEX..................100HM GPS GARMIN.................150 XL INTERCOM SYSTEM BENDIX / KING.......KMA 24H - 70

NONE

1999

1999

T2(800HRS / 4 YEARS) INSPECTION DUE 29-11-2003.