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that are retrieved from the FMS database. The FMS must incorporate the current
update cycle. The pilot must verify approach waypoints for accuracy by reference to
current publications.
S The VNAV system information is not temperature compensated. FMS generated
altitudes and V-paths are not corrected for non-ISA conditions.
S The FMS meets the enroute, terminal and non-precision approach lateral performance
/ accuracy criteria of AC 20--130A.
S Operations with a VNAV final approach glidepath angle that exceeds 3.5 degrees are
prohibited.
S The approach must not be continued past the final approach fix if an FMS “NO APPR”
message is displayed on the PFD.
Airplane Flight Manual
CSP C-012 DOT Approved
REV 2, Feb 24/04
LIMITATIONS
Navigation Systems Limitations
02--09--2
1. FLIGHT MANAGEMENT SYSTEM (CONT’D)
S The FMS installation meets the airworthiness certification requirements of JAA
Temporary Guidance Leaflet No. 10, Airworthiness and Operational Approval for
Precision RNAV Operations in Designated European Airspace, except for the database
integrity requirements of TGL 10 section 8.2.
S Precision RNAV operations must not be conducted unless all of the required
equipment specified below is operational.
PRNAV REQUIRED EQUIPMENT LIST
EQUIPMENT REQUIREMENTS FOR PRNAV
FLIGHT MANAGEMENT COMPUTER (2)
<1214>
ONE (1) MUST BE OPERATIONAL.
FMS CONTROL DISPLAY UNIT (2)
<1214>
ONE (1) MUST BE OPERATIONAL.
VHF NAV (2), DME (2) One (1) VHF NAV and one (1) DME
must be operational.
VHF NAV (2), DME (2), GPS (2) <1027> One (1) VHF NAV and one (1) DME
must be operational, or one (1) GPS is operational.
IRS (2) <1025> One (1) must be operational.
IRS ONLY message must not be displayed.
Airplane Flight Manual
CSP C-012 DOT Approved
REV 3, May 03/05
LIMITATIONS
Navigation Systems Limitations
02---09---3
2. GLOBAL POSITIONING SYSTEM
S Options <1027> :
S Other approved navigation equipment appropriate to the route of flight (enroute and
terminal) must be installed and operating.
S The GPS may only be used for approach guidance if the reference coordinate data
system for the instrument approach is WGS--84 or NAD--83.
S The area navigation system used for IFR Class 1 navigation meets the performance /
accuracy criteria of AC 20--130A for enroute and terminal area navigation.
S Option <1027>:
S The dual GPS installation, when used in conjunction with the Prediction Program
832--3443--005 and with two operational FMS-4200 systems, has been found to
comply with the requirements of MNPS operations and as a primary means of
navigation in oceanic and remote airspace operations. Likewise, this compliance is
considered as meeting RNP-10 requirements, without time limitations.
NOTE
The demonstration of performance with the above
criteria does not constitute approval to conduct MNPS,
oceanic / remote airspace or RNP-10 operations.
Airplane Flight Manual
CSP C-012 DOT Approved
REV 3, May 03/05
Vol. 1 01--20--1
AIRPLANE GENERAL
Exterior REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
External Aircraft Dimensions <2224>
Figure 01---20---1
24 ft 1 in
(7.34 m)
109 ft 10.8 in (33.50 m)
118 ft 10.7 in (36.24 m)
8 ft 10 in
(2.69 m)
28 ft 4 in
(8.63 m)
36 ft 4 in
(11.07 m)
15 ft 11 in
(4.85 m)
6 ft 3 in (1.90 m)
3 ft (0.91 m)
24 ft 1 in
(7.34 m)
81 ft 6 in (24.85 m)
10 ft 7 in
(3.23 m)
5 ft 1 in (1.55 m)
6 ft 4 in 9 ft 6 in (2.89 m)
(1.93 m)
7 ft 1 in
(2.16 m)
Vol. 1 01--20--2
AIRPLANE GENERAL
Exterior REV 1, Jan 13/03
Flight Crew Operating Manual
CSP C--013--067
Engine Hazard Areas <2224>
Figure 01---20---2
100 mph
(161 km/h)
60 mph
(97 km/h)
7.7 ft
(4 m)
140 mph
(225 km/h)
140 mph
(225 km/h)
100 mph
(161 km/h)
60 mph
(97 km/h)
12 ft
(8 m)
LEGEND
Maximum thrust
Idle thrust
ENGINE EXHAUST
DANGER AREAWIDTH
TEMP. VELOCITY
IDLE 25 ft (8 m) 21 ft (6 m)
TAKE--OFF 37 ft (11 m) 36 ft (11 m)
(3)
(6)
(9.1)
(12.2)
(15.2 m)
(18.3)
(21.3)
(24.4)
(27.4)
(30.5 m)
(0 m)
10
20
30
40
50 ft
60
70
80
90
100 ft
0 ft
(3)
(6)
(9.1)
(12.2)
(15.2 m)
(18.3)
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