AS332 L - L1 conversion possible

Please feel free to download the datasheet of the helicopter mentioned above.

Datasheet AS332 L (456KB)

Actual product(s) may differ from photographs.

PRODUCTION YEAR: TSN: MISSION: AVAILABILITY:

1983 29,330 HOURS OFFSHORE IMMEDIATELY

LIST OF EQUIPMENTS:

Emergency floats (FP+RP) External life rafts HEEL HUMS Hoist (FP) Cargo Sling (FP) ELT C406N-HM Auxiliary Fuel tank (FP+RP)

Cabin: 18 passenger seats

LIST OF AVIONICS:

ADC B&D 9004 (*2)   GPS and FMS UNS-1D ADF Collins ADF 60   HSI Astronautics 133640 (*2) Altimeter 5934PAD-3 (*2)   Radio Altimeter Thales AHV 8 AP and AFCS SFIM 155   VHF Comm VHF-20A (*2) Transponder TDR-90   VHF FM Marine NP 138 Altitude Indicator ADI-77 (*2)   VHF Nav Collins VIR-31H (*2) Audio Team TB31   Weather radar Primus 700 Compass & AHRS CG-130 (*2)   DME Collins 40 CVR Combined CVFDR

COMPONENTS REMAINING TIMES: As of June 2012

Main gear box Main rotor blades (*4) Main rotor servo (*3) Intermediate gear box Tail gear box Engine 1 Makila 1A Engine 2 Makila 1A

794 / 3,000 hrs (TBO) 4,492 - 8.087 - 7,194 5,189 / 20,000 hrs (SLL) 2,241 - 160 - 2,206 / 3,000 hrs (TBO) 1,704 / 3,400 hrs (TBO) 3,491 / 3,500 hrs (TBO) 2,434 / 3,000 hrs (TBO) 1,555 / 3,000 hrs (TBO)

Inspection status: As of June 2012

FRESH G-CHECK

NOTES:

L/L1 Conversion possible FRESH PAINTING (WHITE) Aircraft is in good condition. No incident or Accident history Offered with Valid Export C of A We offer the Aircraft: “As is” Ex-Works North America

Aircraft availability subject to prior sale. Components remaining times, configuration and equipment subject to buyer's verfication prior to purchase.

Medium weight aircraft offering a high level of availability and a proven experience in all types of missions mainly offshore transport and SAR.

Please feel free to download the EUROCOPTER Technical Data of the AS332 L Helicopter

Technical Data AS332 L (3.7 MB)

MTOW: MAX RANGE WITH STANDARD FUEL TANK: STANDARD CONFIGURATION:

9,000 kg 841 km 2+20 pax

©Copyright all Helicopter photos courtesy of Eurocopter.

The data set forth in this document are general in nature and for information purpose only. They may vary with conditions. For performance data and operating limitations, reference must be made to the approval flight manual and all appropriate documents.

Subject AS332 L - L1 conversion possible, 1983, 29,330 hours

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