NFM-P users access the native user interface to perform all the end-to-end operations in the IP/ MPLS and L2 Ethernet domains running on the 7X50 router product families.

The Partenavia P.68, now Vulcanair P68, is a light aircraft designed by Luigi Pascale and initially built by Italian company Partenavia. It made its first flight on 25 May 1970, its type certification was granted on 17 November 1971 and was transferred to Vulcanair in 1998.

NSP Network Services Platform Network Functions Manager - Packet (NFM-P) Release 18.3 System Administrator Guide 3HE-14090-AAAA-TQZZA Issue 1 March 2018

It provides operating limitations, normal procedures, and emergency procedures for the aircraft. Key details include: - Engine and performance limitations, as well as airspeed, weight and balance limits. - Standard procedures for starting engines, takeoff, cruise, landing and securing the aircraft.

This document is an index of technical publications issued on June 13, 2022 for P.68 variant aircraft, including the Partenavia P.68 and AP68TP. It lists flight manuals, maintenance manuals, and maintenance manual supplements by aircraft type and serial number range, along with approval dates and revision numbers.

Sep 25, 2015 · P68 MMA can be deployed in observation and reconnaissance, airborne surveillance, maritime patrol, search and rescue (SAR), and homeland security missions in high-stress environments. It is cost-efficient and is believed to be a better alternative to helicopters for use in surveillance missions.

PARTENAVIA P68B VICTOR SECTION I – OPERATING LIMITATIONS ENGINES: Two Lycoming IO-360-A1B or Two Lycoming IO-360-A1B6 ENGINE LIMITS: For all operations 2700 RPM, 200 HP

The instructions in this manual provide informations necessary to perform main-tenance functions ranging from simple checks and replacement to a complete shop type repair. Refer to Table of Contents for page location of applicable sections.

P68 & P68B VICTOR FLIGHT MANUAL Appendix P/N NOR10.708-1 R.A.I. Approval No. 156014/T dated 23rd April 1979 Page 1 of 6 APPENDIX FOR MAXIMUM TAKE-OFF AND LANDING WEIGHT INCREASES SECTION 1 – GENERAL This appendix must be attached to the R.A.I. Approved Flight manual when the aircraft is operated

As a result the P.68 is a benign, docile and stable aircraft in the whole flight envelope with superior flight qualities which can only be appreciated once the aircraft is flown. The new P.68C is easily recognizable thanks to its pilot door, longer nose with more space for avionics and weather radar and its up turned wing tips.