|
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
1. FLIGHT MANAGEMENT SYSTEM (CONT'D)
The FMS thrust setting data is the primary means of information, provided two air data computers are available.
The FMS V speed data is the primary means of information, provided two flight management computers are available.
AR Certified Airplanes
The FMS V speed data is advisory only.
The following performance database, part number 815–9079–001, must be verified to be current and valid.
The following V speed database, part number 815-9174-001, must be verified to be current and valid.
On FAA Certified Airplanes incorporating SB 605–34–007:
The following V speed database, part number 815–9082–001, must be verified to be current and valid.
The FMS does not reduce available runway lengths for runways with displaced thresholds. When using FMS approach performance data for a runway with a displaced threshold, the pilot must manually enter the RWY LENGTH value with the actual available landing distance from a published chart.
When RWY LENGTH is manually entered, the FMS does not compute headwind/crosswind; these must be manually entered on the CDU.
LIMITATIONS Navigation Systems Limitations Vol. 1 02.09.3
REV 1, Dec 21/06
2. NAVIGATION OPERATIONAL APPROVALS
The FMS has been demonstrated capable of, and has been shown to meet the requirements for, the following operation:
Oceanic and remote
.
Use of the FMS with the GPS is approved for supplemental means of navigation source for oceanic and remote operations.
.
Use of the FMS with GPS has been found to comply with the requirements for GPS primary means of navigation in oceanic and remote airspace, when used in conjunction with the Collins prediction program 832–3443–008, or later applicable version, and with two operational GPS receivers and with two operational FMS systems. This does not constitute an operational approval.
North Atlantic (NAT) Minimum Navigational Performance Specification (MNPS) Airspace
.
Provided two FMS installations are operating with each receiving information from at least two inertial reference systems (IRS), the FMS has been demonstrated capable of flight into North Atlantic (NAT) minimum navigational performance specification (MNPS) airspace, and has been shown to meet the accuracy specification in accordance with AC 120–33 or AC 91–49.
NOTE
Compliance with the standards noted above does not constitute an operational approval.
Enroute and Terminal Navigation
.
Use of the FMS with the GPS is approved for supplemental means of navigation source for enroute and terminal operations.
.
The FMS installation meets the performance/accuracy criteria of AC 20–130A, Airworthiness Approval of Navigation or Flight Management Systems Integrating Multiple Navigation Sensors, for enroute and terminal area navigation.
中国公务机网 www.gongwuji.com
公务机翻译 www.aviation.cn
本文链接地址：庞巴迪挑战者605公务机机组操作手册 CL605-CHAPTER 2 -限制 LIMITATIONS(19)
| 
