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LIMITATIONS
02-04-02 Airplane Flight Manual DOT Approved Jul 31/2006
CSP 100-1 REV 6
SYSTEMS LIMITATIONS (Cont)
AVIONICS
DATALINK (If installed)
The DATALINK is approved for the transmission and receipt of messages that
will not create an unsafe condition if the message is improperly received. An
unsafe condition may exist if:
• The message or part of the message is delayed or not received
• The message is delivered to the wrong recipient
• The message content is corrupted
(Continued)
For aircraft on the Russian Federation (RF) and Commonwealth of
Independent States (CIS) countries’ registry:
NOTE: Referenced North American or European regulatory material is
in compliance with its RF and CIS countries’ equivalent.
COMMUNICATIONS
Flight in polar regions outside VHF coverage shall be allowed provided
forecast is favorable for HF radio waves propagation.
EFFECTIVITY
For aircraft not on the Russian Federation (RF) and Commonwealth of
Independent States (CIS) countries’ registry:
Crew actions based on messages such as pre-departure clearance, oceanic
clearance, digital automatic terminal information service, weight and balance,
take-off data (speeds, trim settings, runway distances) are prohibited
unless the approved operational procedures are used to verify that the message
is received by the intended recipient, that the message is valid, and that
the content is not corrupted.
For aircraft 20001 thru 20059 not incorporating Service Bulletin
SB100-34-18:
If the DATALINK system is used for clearances or other flight related
information, the crew must either monitor the DATALINK CDU page or
periodically check the DATALINK CDU page until the reply is received
and accepted. (Annunciation of incoming Datalink messages is provided
only by the ACTIVE ADVISORY prompt display on DATALINK CDU
pages).
EFFECTIVITY
LIMITATIONS
DOT Approved Jul 31/2006 Airplane Flight Manual 02-04-03
REV 6 CSP 100-1
SYSTEMS LIMITATIONS (Cont)
AVIONICS (Cont)
DATALINK (If installed) (Cont)
FLIGHT MANAGEMENT SYSTEM (FMS)
Use of the FMS V-speed data is prohibited for temperatures above ISA +33 ºC.
For aircraft on the Russian Federation (RF) and Commonwealth of
Independent States (CIS) countries’ registry:
NOTE: Use of DATALINK is not permitted for ATC purposes.
Crew actions based on messages such as digital automatic terminal information
service, weight and balance, take-off data (speeds, trim settings, runway
distances) are prohibited unless the approved operational procedures are
used to verify that the message is received by the intended recipient, that the
message is valid, and that the content is not corrupted.
EFFECTIVITY
For aircraft not on the Russian Federation (RF) and Commonwealth of
Independent States (CIS) countries’ registry:
Single FMS
- The FMS V-speed data (if installed) is advisory only and must be
verified with AFM data.
- V-speed database part number must be verified to be: 815-5961-
002.
Dual FMS (If installed)
- The FMS V-speed data (if installed) does not need to be verified with
the AFM, provided two Flight Management Computers are available.
- V-speed database part number must be verified to be: 815-5961-002.
EFFECTIVITY
For aircraft on the Russian Federation (RF) and Commonwealth of
Independent States (CIS) countries’ registry:
- The FMS V-speed data (if installed) does not need to be verified
with the AFM, provided both Flight Management Computers are
available.
- V-speed database part number must be verified to be: 815-5961-002.
EFFECTIVITY
LIMITATIONS
02-04-04 Airplane Flight Manual DOT Approved Jul 31/2006
CSP 100-1 REV 6
SYSTEMS LIMITATIONS (Cont)
AVIONICS (Cont)
FLIGHT MANAGEMENT SYSTEM (Cont)
The Collins FMS-5000 Flight Management System Operator’s Guide (Part
number 523-0780848-00XXXX dated May 15/2004, or later applicable
version) must be immediately available to the flight crew whenever navigation
is predicated on the use of the FMS.
The FMS is approved for use with software version [FMC SCID 832-4118-
018, or later applicable revision]. The software status in the FMS Operator’s
Guide must match that displayed on the equipment.
The performance database part number must be verified to be: 815-5959-002.
FMS range and fuel management information is advisory only.
When the batteries are removed, the FUEL USED on the FMS will indicate the
value from the previous flight. After re-installing the batteries, the FUEL
USED should be manually reset to zero.
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