Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
1
DATE
:
10/15/2010
REVISION:
SECTION X
WEIGHT AND BALANCE PROCEDURE
135.23(b)
40
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
2
DATE
:
09/02/2010
REVISION:
39
LIST OF SUPERCEDE PAGES FOR SECTION X
SectionPage
Revision
Date
SectionPage
Revision
Date
X-I
Original
05/27/1994
X-30
39
09/02/2010
X-2
39
09/02/2010
X-31
39
09/02/2010
X-3
Original
05/05/2006
X-32
39
09/02/2010
X-4
Original
05/05/2006
X-33
39
09/02/2010
X-5
Original
05/27/1994
X-34
39
09/02/2010
X-6
39
09/02/2010
X-35
24
07/22/2002
X-7
34
06/18/2008
X-36
39
09/02/2010
X-8
39
09/02/2010
X-37
39
09/02/2010
X-9
39
09/02/2010
X-38
39
09/02/2010
X-10
15
07/22/1999
X-11
Original
05/27/1994
X-12
39
09/02/2010
X-13
39
09/02/2010
X-14
15
07/22/1999
X-15
39
09/02/2010
X-16
39
09/02/2010
X-17
15
07/22/1999
X-18
Original
05/27/1994
X-19
Original
05/27/1994
X-20
Original
05/27/1994
X-21
Original
05/27/1994
X-22
39
09/02/2010
X-23
39
09/02/2010
X-24
15
07/22/1999
X-25
39
09/02/2010
X-26
39
09/02/2010
X-27
15
07/22/1999
X-28
15
07/22/1999
X-29
39
09/02/2010
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
3
DATE
:
09/02/2010
REVISION:
39
WEIGHT AND BALANCE CONTROL
It is the responsibility of Vieques Air Link, Inc. to assure that each multi-engine aircraft
operated under the Air Carrier Certificate has a current and accurate empty weight and
empty C.G.
The Director of Maintenance will be responsible to investigate all weight changes in aircraft
to assure that the aircraft loading information is current and accurate and up to date. The
current empty weight and center of gravity of all single-engine and multi-engine aircraft will
be calculated from values established by actual weighing of the aircraft every 36 calendar
months.
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
4
DATE
:
01/01/2011
REVISION:
41
WEIGHT AND BALANCE PROCEDURES
The loading and Weight and Balance Computation procedures shall be in accordance with
the instructions contained in the appropriate sections of the FAA Approved Aircraft Manual
for the type of aircraft for which a load manifest must be prepared shall carry a copy of the
complete load manifest in the aircraft to its destination.
The company’s Weight and Balance System is designed to insure that the maximum
allowable weight will not be exceeded and the center of gravity will be within allowable
weight and balance information as well as the flight following information will be retained for
a period of 30 days at the company’s Main Office located at #358 Mellado Street, Vieques,
Puerto Rico.
DETERMINATION OF WEIGHT OF PASSENGERS AND CREW
Each passenger will approach the company scale to determine actual weight or solicited
(asked) passenger weight.
DETERMINATION OF WEIGHT OF CARGO AND BAGGAGE
Cargo and baggage weight will be taken by actual weighing:
CARRIAGE OF CARGO INCLUDING CARRY ON BAGGAGE
All cargo and baggage will be carried in the cargo compartment of the aircraft, except on a
Cargo Flight only; where that the cargo is carried in the passenger section of the aircraft in
accordance with the Aircraft Flight Manual.
Carry on baggage, such as a women’s or man’s purse, cameras, attaché cases and baby
supply bags, can be carried in the passenger’s compartment providing that they are of
average size and do not restrict the view of the passenger or restrict the free movement of
the passenger and can be easily carried on the lap.
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
5
DATE
:
09/02/2010
REVISION:
39
WEIGHT AND BALANCE PROCEDURES (Cont..)
FUEL COMPUTATIONS
The amount of fuel required for each flight must be computed including no less than 30
minutes of reserve during day time flight and no less than 45 minutes of reserve during night
time flights. The Aircraft Flight Manual should be used as reference for the computations of
the fuel consumption.
Appropriate Vieques Air Link, Inc., forms which are in accordance with F.A.A. approved
Flight Manual for all Weight and Balance computation are kept at all Vieques Air Link, Inc.
counters for Vieques Air Link’s aircrafts.
Prior to the start of any revenue flight, a complete flight manifest shall be prepared by
qualified ground personnel and signed by the Captain of First Office for two pilot operations
or by the Pilot in Command for single pilot operation. A complete flight manifest shall consist
shall consist of the following:
1. An approved company Weight and Balance form on which must be entered:
a.
b.
c.
d.
e.
f.
g.
h.
i.
j.
Date of flight
Flight number
Point of departure
Destination
Aircraft type and registration number
Aircraft operating weight of fuel, passenger, cargo and baggage.
Center of gravity moment (index) and limits.
Maximum allowable gross take-off weight.
Maximum landing weight when applicable.
Signature of person who prepared the Weight and balance attesting that the load
distribution confirms to company procedures.
k. Signature of a crewmember
l. Total number of passengers
m. Name of each passenger
2. Passenger ticket containing:
a. Flight number and date
b. Name of each passenger
3. The P.I.C. shall refer to his Operational Manual which contains the necessary forms
and he is responsible for the preparation of a flight manifest for all out of schedule
routes and charters.
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
6
DATE
:
09/02/2010
REVISION:
39
VIEQUES AIR LINK, INC.
FLIGHT MANIFEST
VAL FORM 001
DATE
A/C NUMBER
FROM
PASSENGERS NAMES
TO
Pax Weight
FLIGHT NO.
Seat
row
+
Moment
TIME
Moment
PIC
SIC
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
TOTAL PAX’S
TOTALS
TOTAL MOMENTS
PASSENGER COMPARMENT
Empty OP Weight
Passgers. Comp
Min. Mom.
Bagg Compt (Front)
Max. Mom.
Bagg Compt (Rear)
Corrected Moment
T ZWF
ZFW (MAX) (
)
Fuel Weight
Min. Mom.
Max. Mom.
T.O. Weight
Correction
Revised T.O. Weight
Max T.O. Weight
I CERTIFY THAT THE MAXIMUM ALLOWABALE
TAKE OFF WEIGHT FOR THIS FLIGHT IS
WITHIN THE ALLOWANCE SHOWN IN THE
AIRCRAFT FLIGHT MANUAL.
Signature of Pilot in Command
Remarks:
Prepared by:
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
7
DATE
:
01//01/2011
REVISION:
EMPTY WEIGHT AND MOMENT ISLANDERS
N663VL
E. W.
MOMENT
G. W.
N902VL
E. W.
MOMENT
G. W.
N903VL
E. W.
MOMENT
G. W.
N861VL
E. W.
MOMENT
G. W.
N904VL
E. W.
MOMENT
G. W.
Passenger
Med Evacuation
Cargo
4230
9446
6200
4250
1007
4130
9264
4150
1060
6200
4148
1081
3890
1021
3895
9601
6200
4010
1094
3890
1046
4040
936
6200
4038
958
3890
781
3970
955
6200
3990
995
3800
996
EMPTY WEIGHT AND MOMENT TRISLANDERS
16 Passengers
Med Evacuation
Cargo
6190
6200
5918
2048
2068
2052
9500
9500
9500
6200
6210
5928
2129
2023
2133
9500
9500
9500
N905VL
E. W
MOMENT
G. W
N906VL
E. W
MOMENT
G. W
N741VL
E. W.
MOMENT
G. W.
5053
9537
8750
N335VL
E. W.
MOMENT
G. W.
5087
9790
8750
EMPTY WEIGHT AND MOMENT CARAVANS
N742VL
E. W.
5078
MOMENT
9660
G. W.
8750
41
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
8
DATE
:
09/02/2010
REVISION:
39
INSTRUCTIONS FOR THE PREPARATION OF FLIGHT MANIFEST FOR BN-2AIRCRAFT (ISLANDER)
1.
2.
3.
4.
5.
6.
7.
8 thru 16.
17.
18 thru 26.
27 thru 35.
36 thru 44.
45 thru 54.
55.
56.
57.
58.
59.
60.
61.
62.
63.
64.
65.
66.
67.
68.
69.
70.
71.
72.
73.
74.
75.
76.
77.
78.
79.
80.
81.
82.
Date of flight
Aircraft Registration Number
Point of Departure
Destination
Number of schedule flight/flight status
Schedule Departure Time
Full Name of Pilot in Command
Full Name Passenger’s (From #1 thru #9)
Captain’s Actual Weight
Passenger’s Actual Weight
Passenger’s Seat Row Assigned
Positive Moment for Pilot and Passengers
Negative Moment for Pilot and Passengers
Total Passengers in Manifest
Total Crew and Passengers Weight
Total Positive Moment
Total Negative Moment
Total Adjusted Moment
Empty O.P. Weight
Total Crew and Passenger’s Weight
Total Baggage Weight
Total Zero Fuel Weight
Max. ZFW
Total Fuel Weight
Take-Off Weight
Last Minute Correction (Weight)
Revised Actual Take-off Weight
Max. T.O. Weight
Empty O.P. Moment
Total Adjusted Moment (see #59)
Total Baggage Moment
Total Zero Fuel Weight Moment
Total Fuel Moment
Take-off Moment
Last Minute Correction (Moment)
Revised Actual Take-Off Moment
Minimum and Maximum Limit Moment
Corrected Limit Moments (If Applicable)
Pilot in Command Signature
Agent’s Signature
Remarks or Comments in Flight
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
9
DATE
:
09/02/2010
REVISION:
39
VIEQUES AIR LINK, INC.
FLIGHT MANIFEST (ISLANDER)
VAL FORM 001
DATE
A/C NUMBER
FROM
TO
FLIGHT NO.
TIME
1
2
3
4
5
6
Seat
row
+
Moment
Moment
45
18
27
36
46
9
19
28
37
47
10
20
29
38
48
11
21
30
39
49
5
12
22
31
40
50
6
13
23
32
41
51
7
14
24
33
42
52
8
15
25
34
43
53
9
16
26
35
44
54
PASSENGERS NAMES
Pax Weight
7
17
8
2
3
4
PIC
SIC
1
10
11
12
13
14
15
16
55
TOTAL PAX’S
TOTALS
56
57
TOTAL MOMENTS
PASSENGER COMPARMENT
Empty OP Weight
6
0
7
0
Passgers. Comp
6
1
7
1
Bagg Compt (Rear)
6
2
7
2
T ZWF
6
3
7
3
Fuel Weight
6
5
7
4
T.O. Weight
6
6
7
5
Correction
6
7
7
6
Revised T.O. Weight
6
8
7
7
Max T.O. Weight
6
9
Min. Mom.
58
59
Max. Mom.
78
Bagg Compt (Front)
Corrected Moment
ZFW (MAX) ( 64)
Min. Mom.
Max. Mom.
I CERTIFY THAT THE MAXIMUM ALLOWABALE
TAKE OFF WEIGHT FOR THIS FLIGHT IS WITHIN
THE ALLOWANCE SHOWN IN THE AIRCRAFT
FLIGHT MANUAL.
80
Signature of Pilot in Command
Remarks:
82
79
Prepared by:
81
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
10
DATE
:
09/02/2010
REVISION:
PASSENGER ISLANDER - WEIGHT AND ARMS FORM
WEIGHT
LB.
70
80
90
100
110
120
130
140
150
160
170
180
190
200
210
220
230
240
250
260
270
280
290
300
PILOT OR
PASSENGER
SEAT ROW-1
STATION 89
-32
-36
-41
-45
-49
-54
-59
-63
-68
-72
-77
-81
-86
-90
-95
-99
-104
-108
-113
-118
-122
-127
-131
-136
SEAT ROW-2W
STATION 120
-11
-12
-14
-15
-17
-18
-20
-21
-23
-24
-26
-27
-29
-30
-32
-33
-35
-36
-38
39
-41
-42
-44
-45
SEAT ROW-3 SEAT ROW-4 SEAT ROW 5STATION 150 STATION 179 STATION 207
ALL MOMENTS ARE DIVIDED BY 100
+11
+31
+51
+12
+36
+58
+14
+40
+65
+15
+45
+73
+17
+49
+80
+18
+53
+87
+20
+58
+94
+21
+62
+101
+23
+67
+109
+24
+71
+116
+26
+75
+123
+27
+80
+130
+29
+84
+138
+30
+89
+145
+32
+93
+152
+33
+98
+160
+35
+102
+167
+36
+107
+174
+38
+111
+181
+39
+116
+189
+41
+120
+196
+42
+125
+203
+44
+129
+210
+45
+134
+218
WING TANK - STATION 161.5
WEIGHT LB.
50
100
150
200
250
300
350
400
ALL MOMENTS ARE DIVIDED BY 100
450
+122
500
+135
550
+149
600
+162
650
+176
700
+189
750
+203
800
+216
+14
+27
+41
+54
+68
+81
+95
+108
Baggage +120
20
40
60
80
100
150
+24
+48
+72
+96
+120
+180
Baggage +105
200
250
300
350
400
+240
+300
+360
+420
+480
20
40
60
80
100
150
+21
+42
+63
+84
+105
+158
200
250
300
350
400
+211
+264
+315
+367
+420
39
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
11
DATE
:
09/02/2010
REVISION:
39
ISLANDER - C.G. Limits Form
WEIGHT LB.
4000
4100
4200
4300
4400
4500
4600
4700
4800
4900
5000
5100
5200
5300
5400
5500
5600
5700
5800
5900
6000
6100
6200
C.G. LIMIT -IN
FWD
17.0
17.0
17.0
17.0
17.0
17.0
17.0
17.0
17.0
17.0
17.0
17.2
17.6
17.9
18.3
18.6
18.9
19.3
19.6
20.0
20.3
20.7
21.0
ALL MOMENTS ARE DIVIDED BY
100 LB. INC.
AFT
FWD
AFT
25.6
680
1024
25.6
697
1050
25.6
714
1075
25.6
731
1101
25.6
748
1126
25.6
765
1152
25.6
782
1178
25.6
799
1203
25.6
816
1229
25.6
833
1254
25.6
850
1280
25.6
877
1306
25.6
915
1331
25.6
949
1357
25.6
988
1382
25.6
1023
1408
25.6
1058
1434
25.6
1100
1460
BN-2
Limit
25.6
1137
1485
25.6
1180
1510
25.6 BN-2A
1218
1536
Limit
25.6
1263
1562
25.6
1302
1587
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
12
DATE
:
09/02/2010
REVISION:
39
INSTRUCTIONS FOR PREPARATION OF FLIGHT MANIFEST FOR BN-2 (ISLANDER w STRETCHER)
1.
2.
3.
4.
5.
6.
7.
8 thru 10.
11.
12.
13.
14 thru 16.
17.
18.
19.
20 thru 21.
22 thru 25.
26.
27.
28.
29.
30.
31.
32.
33.
34.
35.
36.
37.
38.
39.
40.
41.
42.
43.
44.
45.
46.
47.
48.
49.
50.
51.
52.
53.
Date of flight
Aircraft Registration Number
Point of Departure
Destination
Number of schedule flight/flight status
Schedule Departure Time
Full Name of Pilot in Command
Full Name Passenger’s
Name of Passenger in Stretcher
Name of Passenger in Pax Rear Seat
Pilot Actual Weight
Passenger’s Actual Weight
Passenger Stretcher Actual Weight
Rear Passenger Actual Weight
Passenger’s Seat Row Assigned
Positive Moment for Pilot and Passengers
Negative Moment for Pilot and Passengers
Total Passengers in Manifest
Total Crew and Passengers Weight
Total Positive Moment
Total Negative Moment
Total Adjusted Moment
Empty O.P. Weight
Total Crew and Passenger’s Weight
Total Baggage Weight
Total Zero Fuel Weight
Max. ZFW
Total Fuel Weight
Take-Off Weight
Last Minute Correction (Weight)
Revised Actual Take-off Weight
Max. T.O. Weight
Empty O.P. Moment
Total Adjusted Moment (see #30)
Total Baggage Moment
Total Zero Fuel Weight Moment
Total Fuel Moment
Take-off Moment
Last Minute Correction (Moment)
Revised Actual Take-Off Moment
Minimum and Maximum Limit Moment
Corrected Limit Moments (If Applicable)
Pilot in Command Signature
Agent’s Signature
Remarks or Comments in Flight
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
13
DATE
:
09/02/2010
REVISION:
39
VIEQUES AIR LINK, INC.
FLIGHT MANIFEST
VAL FORM 001
DATE
A/C NUMBER
FROM
TO
FLIGHT NO.
TIME
1
2
3
4
5
6
PASSENGERS NAMES
Pax Weight
PIC
7
13
Seat
row
1
+
Moment
Moment
22
SIC
8
14
1
23
1
9
15
19
24
2
10
16
19
25
3
11
17
STCH
20
4
12
18
RS
21
5
6
7
8
9
10
11
12
13
14
15
16
26
TOTAL PAX’S
TOTALS
27
28
30
TOTAL MOMENTS
PASSENGER COMPARMENT
Empty OP Weight
3
1
4
1
Passgers. Comp
3
2
4
2
Bagg Compt (Rear)
3
3
4
3
T ZWF
3
4
4
4
Fuel Weight
3
6
4
5
T.O. Weight
3
7
4
6
Correction
3
8
4
7
Revised T.O. Weight
3
9
4
8
Max T.O. Weight
4
0
Min. Mom.
29
Max. Mom.
49
Bagg Compt (Front)
Corrected Moment
ZFW (MAX) (35)
Remarks:
Min. Mom.
Max. Mom.
50
I CERTIFY THAT THE MAXIMUM ALLOWABALE
TAKE OFF WEIGHT FOR THIS FLIGHT IS
WITHIN THE ALLOWANCE SHOWN IN THE
AIRCRAFT FLIGHT MANUAL.
53
51
Signature of Pilot in Command
52
Prepared by:
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
14
DATE
:
09/02/2010
REVISION:
ISLANDER MEDICAL EVACUATION - WEIGHT AND ARMS FORM
WEIGHT
LB.
70
80
90
100
110
120
130
140
150
160
170
180
190
200
210
220
230
240
250
260
270
280
290
300
PILOT OR
PASSENGER
SEAT ROW-1
STATION 89
-32
-36
-41
-45
-49
-54
-59
-63
-68
-72
-77
-81
-86
-90
-95
-99
-104
-108
-113
-118
-122
-127
-131
-136
SEAT ROW-2W
STATION 120
-11
-12
-14
-15
-17
-18
-20
-21
-23
-24
-26
-27
-29
-30
-32
-33
-35
-36
-38
39
-41
-42
-44
-45
PATIENT IN
STRETCHER
STATION 183.6
+23
+26
+30
+33
+36
+40
+43
+46
+50
+53
+56
+60
+63
+66
+70
+73
+76
+79
+83
+86
+89
+93
+96
+99
REAR SEAT
STATION 01.6
+36
+41
+46
+51
+56
+61
+66
+72
+77
+82
+87
+92
+97
+102
+107
+112
+118
+123
+128
+133
+138
+143
+148
+153
WING TANK - STATION 161.5
WEIGHT LB.
50
100
150
200
250
300
350
400
ALL MOMENTS ARE DIVIDED BY 100
450
+122
500
+135
550
+149
600
+162
650
+176
700
+189
750
+203
800
+216
+14
+27
+41
+54
+68
+81
+95
+108
Baggage +120
20
40
60
80
100
150
+24
+48
+72
+96
+120
+180
Baggage +105
200
250
300
350
400
+240
+300
+360
+420
+480
20
40
60
80
100
150
+21
+42
+63
+84
+105
+158
200
250
300
350
400
+211
+264
+315
+367
+420
39
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
15
DATE
:
09/02/2010
REVISION:
39
INSTRUCTIONS FOR THE PREPARATION OF FLIGHT MANIFEST FOR MK-III TRISLANDER
1.
2.
3.
4.
5.
6.
7.
8.
9 thru 24.
25.
26.
27 thru 42.
43 thru 58.
59 thru 76.
77 thru 94.
95.
96.
97.
98.
99.
100.
101.
102.
103.
104.
105.
106.
107.
108.
109.
110.
111.
112.
113.
114.
115.
116.
117.
118.
119.
120.
121.
122.
123.
124.
Date of flight
Aircraft Registration Number
Point of Departure
Destination
Number of schedule flight/flight status
Schedule Departure Time
Full Name of Pilot in Command
Full Name of First Officer
Full Name Passenger’s (From #1 thru #16)
Captain’s Actual Weight
First Officer Actual Weight
Passenger’s Actual Weight
Passenger’s Seat Row Assigned
Positive Moment for Pilots and Passengers
Negative Moment for Pilots and Passengers
Total Passengers in Manifest
Total Crew and Passengers Weight
Total Positive Moment
Total Negative Moment
Total Adjusted Moment
Empty O.P. Weight
Total Crew and Passenger’s Weight
Total Baggage Weight (Front)
Total Baggage Weight (Rear)
Total Zero Fuel Weight
Max. ZFW
Total Fuel Weight
Take-Off Weight
Last Minute Correction (Weight)
Revised Actual Take-off Weight
Max. T.O. Weight
Empty O.P. Moment
Total Adjusted Moment (see #97)
Total Baggage Moment (Front)
Total Baggage Moment (Rear)
Total Zero Fuel Moment
Total Fuel Moment
Take-off Moment
Last Minute Correction (Moment)
Revised Actual Take-Off Moment
Minimum and Maximum Limit Moment
Corrected Limit Moments (If Applicable)
Pilot in Command Signature
Agent’s Signature
Remarks or Comments in Flight
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
16
DATE
:
09/02/2010
REVISION:
39
VIEQUES AIR LINK, INC.
FLIGHT MANIFEST (TRISLANDER)
VAL FORM 001
DATE
A/C NUMBER
FROM
TO
FLIGHT NO.
TIME
1
2
3
4
5
6
25
+
Moment
59
Moment
77
8
26
60
78
1
9
27
43
61
79
2
10
28
44
62
80
3
11
29
45
63
81
4
12
30
46
64
82
5
13
31
47
65
83
6
14
32
48
66
84
7
15
33
49
67
85
8
16
34
50
68
86
9
17
35
51
69
87
10
18
36
52
70
88
11
19
37
53
71
89
12
20
38
54
72
90
13
21
39
55
73
91
14
22
40
56
74
92
15
23
41
57
75
93
16
24
42
58
76
94
97
98
PASSENGERS NAMES
Pax Weight
PIC
7
SIC
95
TOTAL PAX’S
TOTALS
Seat
row
96
99
TOTAL MOMENTS
PASSENGER COMPARMENT
Empty OP Weight
1
0
0
1
1
1
Min. Mom.
Passengers. Comp
1
0
1
1
1
2
Bagg Compt (Front)
1
0
2
1
1
3
Bagg Compt (Rear)
1
0
3
1
1
4
T ZWF
1
0
4
1
1
5
Fuel Weight
1
0
6
1
1
6
T.O. Weight
1
0
7
1
1
7
Correction
1
0
8
1
1
8
Revised T.O. Weight
1
0
9
1
1
9
Max T.O. Weight
1
0
0
Max. Mom.
120
Corrected Moment
ZFW (MAX) ( 105)
Min. Mom.
Max. Mom.
I CERTIFY THAT THE MAXIMUM ALLOWABALE
TAKE OFF WEIGHT FOR THIS FLIGHT IS WITHIN
THE ALLOWANCE SHOWN IN THE AIRCRAFT
FLIGHT MANUAL.
122
Remarks:
11
Signature of Pilot in Command
124
Prepared by:
123
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
17
DATE
:
09/02/2010
REVISION:
39
TRISLANDER FLIGHT MANUAL
Table 4 - LOAD WEIGHTS AND MOMENTS – OCCUPANTS
(All Moments are divided by 100)
WEIGHT
*
*
ROW 1
ROW 2
*
ROW 3
ROW 4
*
ROW 5
ROW 6
*
ROW 7
ROW 8
ROW 9
30
-40
-31
-23
-14
-5
+4
+13
+22
+31
40
-54
-42
-30
-19
-7
+6
+18
+29
+41
50
-67
-52
-37
-23
-8
+7
+22
+36
+51
60
-80
-62
-45
-28
-10
+9
+26
+43
+61
70
-94
-73
-52
-32
-11
+10
+31
+50
+71
80
-107
-83
-59
-37
-13
+12
+35
+57
+81
90
-120
-93
-67
-41
-15
+13
+39
+65
+91
100
-134
-104
-74
-45
-16
+14
+44
+72
+102
110
-147
-114
-82
-50
-17
+16
+48
+79
+111
120
-160
-124
-89
-55
-19
+17
+52
+86
+122
130
-174
-134
-96
-60
-21
+19
+57
+93
+132
140
-187
-145
-104
-64
-22
+20
+61
+100
+142
150
-200
-155
-111
-69
-24
+21
+65
+107
+152
160
-214
-165
-118
-73
-25
+23
+70
+114
+162
170
-227
-176
-125
-77
-27
+24
+74
+122
+172
180
-240
-186
-133
-82
-29
+26
+78
+129
+182
190
-254
-196
-141
-87
-30
+27
+83
+136
+192
200
-267
-207
-148
-91
-32
+28
+87
+144
+203
210
-280
-217
-155
-96
-33
+30
+91
+150
+213
220
-294
-227
-163
-101
-35
+31
+96
+156
+224
230
-307
-238
-171
-105
-36
+33
+100
+165
+233
240
-321
-248
-178
-110
-38
+35
+105
+172
+243
250
-334
-258
-185
-115
-40
+36
+109
+179
+254
260
-348
-268
-192
-120
-42
+38
+114
+186
+264
270
-361
-279
-200
-124
-43
+39
+118
+193
+274
280
-374
-290
-208
-128
-44
+40
+122
+200
+284
290
-387
-300
-215
-133
-46
+41
+126
+207
+295
300
-400
-310
-222
-138
-48
+42
+130
+214
+305
16 PASSENGERS
* 9 PASSENGERS
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
18
DATE
:
09/02/2010
REVISION:
39
TRISLANDER FLIGHT MANUAL
Table 2 LOAD WEIGHTS AND MOMENTS - BAGGAGE (FRONT)
Weight
lb.
Mean Arm (Stn. 25.0)
All Moments are divided by 100
20
40
60
80
100
150
200
250
300
-41.9
-83.8
-125.7
-167.6
-209.5
-314.3
-419.0
-523.8
-628.5
Table 5 LOAD WEIGHTS AND MOMENTS - BAGGAGE (REAR)
Weight
lb.
20
40
60
80
100
150
200
250
300
350
400
450
500
550
600
650
700
Area aft of
Row 9
Station 378.5
All Moments are divided by 100
+28.8
+57.6
+86.4
+115.2
+144.0
+216.0
+288.0
+360.0
+432.0
+504.0
+576.0
Combined are aft
of Row 8
Station 360
+25.1
+50.2
+75.3
+100.4
+125.5
+188.3
+251.0
+313.8
+376.5
+439.3
+502.0
+564.8
+627.5
+690.3
+753.0
+815.8
+878.5
CAA Approved Doc FM/BN-2AIII/1
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
19
DATE
:
09/02/2010
REVISION:
TRISLANDER FLIGHT MANUAL
Table 3 LOAD WEIGHTS AND MOMENTS - FUEL AND OIL
Weight
lb.
50
100
150
200
250
300
350
400
450
500
550
600
650
700
750
800
Wing Tank
Station 261.5
All Moments are divided by 100
+14
+27
+41
+54
+68
+81
+95
+108
+122
+135
+149
+162
+176
+189
+203
+216
Tip Tank
Station 268.5
+17
+34
+51
+68
+85
+102
+119
Note:
The moment arm for combined wing and rear engine usable oil is + 52.6. The
relevant weight and moment/100 being 52.5 lb and 27.6 lb/in respectively.
Approved Doc FM/BN-2AIII/1
6th May 1971
39
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
20
DATE
:
09/02/2010
REVISION:
39
TRISLANDER FLIGHT MANUAL
Table 6 LOAD WEIGHTS AND MOMENTS - MOMENTS LIMITATIONS
Note:
Coupled with the C.G. envelope, Fig 4, the following Moment limitations apply:Weight
lb
6000
6100
6200
6300
6400
6500
6600
6700
6800
6900
7000
7100
7200
7300
7400
7500
7600
7700
7800
7900
8000
8100
8200
8300
8400
8500
8600
8700
8750
8800
8900
C.G. Limit - in.
Fwd
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.0
19.1
Aft
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.6
25.48
All Moments are divided by 100 - lb. in.
Fwd
Aft
1140
1536
1159
1562
1178
1587
1197
1613
1216
1638
1235
1664
1254
1690
1273
1715
1292
1741
1311
1766
1330
1792
1349
1818
1368
1843
1387
1869
1406
1894
1425
1920
1444
1916
1463
1971
1482
1997
1501
2022
1520
2048
1539
2074
1558
2099
1577
2125
1596
2150
1615
2176
1634
2202
1653
2227
1663
2240
1672
2253
1700
2268
D16 CAA Approved Doc FM/BN-2AIII/l
20th August 1976
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
21
DATE
:
09/02/2010
REVISION:
39
Table 6 LOAD WEIGHTS AND MOMENTS - MOMENTS LIMITATIONS
Note:
Coupled with the C.G. envelope, Fig 4, the following Moment limitations apply:Weight
lb
9000
9100
9200
9300
9400
9500
9600
9700
9800
9900
10000
C.G. Limit - in.
Fwd
Aft
19.2
25.37
19.3
25.25
19.36
25.2
19.4
25.1
19.5
25
19.6
24.92
19.7
24.85
19.75
24.75
19.83
24.67
19.92
24.58
20
24.5
All Moments are divided by 100 - lb. in.
Fwd
Aft
1728
2283
1756
2298
1781
2318
1804
2334
1833
2350
1862
2367
1891
2386
1916
2401
1943
2418
1972
2433
2000
2450
D16 CAA Approved Doc FM/BN-2AIII/l
20th August 1976
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
22
DATE
:
09/02/2010
REVISION:
39
INSTRUCTIONS FOR THE PREPARATION OF FLIGHT MANIFEST FOR MK-III TRISLANDER
1.
2.
3.
4.
5.
6.
7.
8.
9 thru 20.
21.
22.
23 thru 32.
33,
34.
35 thru 44.
45 thru 46.
47.
48.
49 thru 58.
59.
60.
61.
62.
63.
64.
65.
66.
67.
68.
69.
70.
71.
72.
73.
74.
75.
76.
77.
78.
79.
80.
81.
82.
83.
84.
85.
86.
87.
88.
Date of flight
Aircraft Registration Number
Point of Departure
Destination
Number of schedule flight/flight status
Schedule Departure Time
Full Name of Pilot in Command
Full Name of First Officer
Full Name Passenger’s (From #1 thru #16)
Captain’s Actual Weight
First Officer Actual Weight
Passenger’s Actual Weight
Passenger Stretcher Actual Weight
Rear Passenger Actual Weight
Passenger’s Seat Row Assigned
Positive Moment for Passengers
Positive Moment for Stretcher Passenger
Positive Moment for Rear Passenger
Negative Moment for Pilots and Passengers
Total Passengers in Manifest
Total Crew and Passengers Weight
Total Positive Moment
Total Negative Moment
Total Adjusted Moment
Empty O.P. Weight
Total Crew and Passenger’s Weight
Total Baggage Weight (Front)
Total Baggage Weight (Rear)
Total Zero Fuel Weight
Max. ZFW
Total Fuel Weight
Take-Off Weight
Last Minute Correction (Weight)
Revised Actual Take-off Weight
Max. T.O. Weight
Empty O.P. Moment
Total Adjusted Moment (see #97)
Total Baggage Moment (Front)
Total Baggage Moment (Rear)
Total Zero Fuel Moment
Total Fuel Moment
Take-off Moment
Last Minute Correction (Moment)
Revised Actual Take-Off Moment
Minimum and Maximum Limit Moment
Corrected Limit Moments (If Applicable)
Pilot in Command Signature
Agent’s Signature
Remarks or Comments in Flight
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
23
DATE
:
09/02/2010
REVISION:
39
VIEQUES AIR LINK, INC.
FLIGHT MANIFEST (TRISLANDER)
VAL FORM 001
DATE
A/C NUMBER
FROM
TO
FLIGHT NO.
TIME
1
2
3
4
5
6
PASSENGERS NAMES
Pax Weight
PIC
7
21
Seat
row
1
+
Moment
SIC
8
22
1
50
1
9
23
35
51
2
10
24
36
52
3
11
25
37
53
4
12
26
38
54
5
13
27
39
55
6
14
28
40
56
7
15
29
41
57
8
16
30
42
58
9
17
31
43
45
10
18
32
44
46
11
19
33
STCH
47
12
20
34
RS
48
Moment
49
13
14
15
16
59
TOTAL PAX’S
TOTALS
60
61
63
TOTAL MOMENTS
PASSENGER COMPARMENT
Empty OP Weight
6
4
7
5
Passengers. Comp
6
5
7
6
Bagg Compt (Front)
6
6
7
7
Bagg Compt (Rear)
6
7
7
8
T ZWF
6
8
7
9
Fuel Weight
7
0
8
0
T.O. Weight
7
1
8
1
Correction
7
2
8
2
Revised T.O. Weight
7
3
8
3
Max T.O. Weight
7
4
62
Min. Mom.
Max. Mom.
84
Corrected Moment
ZFW (MAX) (69)
Min. Mom.
Max. Mom.
85
I CERTIFY THAT THE MAXIMUM ALLOWABALE TAKE
OFF WEIGHT FOR THIS FLIGHT IS WITHIN THE
ALLOWANCE SHOWN IN THE AIRCRAFT FLIGHT
MANUAL.
86
88
Signature of Pilot in Command
Remarks:
Prepared by:
87
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
24
DATE
:
09/02/2010
REVISION:
39
TRISLANDER MEDICAL EVACUATION
LOAD WEIGHTS AND MOMENTS - OCCUPANTS AND STRETCHER
(ALL MOMENTS ARE ARE DIVIDED BY 100)
STRETCHER REAR SEAT
WEIGHT
30
40
50
60
70
80
90
100
110
120
130
140
150
160
170
180
190
200
210
220
230
240
250
260
270
280
290
300
ROW 1
ROW 2
ROW 3
ROW 4
-40
-54
-67
-80
-94
-107
-120
-134
-147
-160
-174
-187
-200
-214
-227
-240
-254
-267
-280
-294
-307
-321
-334
-348
-361
-374
-387
-400
-31
-42
-52
-62
-73
-83
-93
-104
-114
-124
-134
-145
-155
-165
-176
-186
-196
-207
-217
-227
-238
-248
-258
-268
-279
-290
-300
-310
-23
-30
-37
-45
-52
-59
-67
-74
-82
-89
-96
-104
-111
-118
-125
-133
-141
-148
-155
-163
-171
-178
-185
-192
-200
-208
-215
-222
-14
-19
-23
-28
-32
-37
-41
-45
-50
-55
-60
-64
-69
-73
-77
-82
-87
-91
-96
-101
-105
-110
-115
-120
-124
-128
-133
-138
ROW 5
STA. 282.3
STA. 300.3
-5
-7
-8
-10
-11
-13
-15
-16
-17
-19
-21
-22
-24
-25
-27
-29
-30
-32
-33
-35
-36
-38
-40
-42
-43
-44
-46
-48
+14
+19
+23
+28
+33
+37
+42
+47
+52
+56
+61
+66
+70
+75
+80
+85
+89
+94
+99
+104
+108
+113
+118
+122
+127
+132
+137
+141
+19
+26
+32
+39
+46
+52
+59
+65
+72
+78
+85
+92
+98
+105
+111
+118
+125
+131
+138
+144
+151
+157
+164
+171
+177
+184
+190
+197
ROW 9
+31
+41
+51
+61
+71
+81
+91
+102
+111
+122
+132
+142
+152
+162
+172
+182
+192
+203
+213
+224
+233
+243
+254
+264
+274
+284
+295
+305
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
25
DATE
:
09/02/2010
REVISION:
INSTRUCTIONS FOR PREPARATION OF CARGO FLIGHT MANIFEST FOR ISLANDER &
TRISLANDER
1.
2.
3.
4.
5.
6.
7.
8.
9 thru 11.
12.
13.
14 thru 16.
19 thru 21.
22 thru 26.
27.
28.
29.
30.
31.
32.
33.
34.
35.
36.
37.
38.
39.
40.
41.
42.
43.
44.
45.
46.
47.
48.
49.
50.
51.
52.
53.
54.
55.
56.
Date of flight
Aircraft Registration Number
Point of Departure
Destination
Number of schedule flight/flight status
Schedule Departure Time
Full Name of Pilot in Command
Full Name of First Officer
Name of Cargo
Captain’s Actual Weight
First Officer Actual Weight
Cargo Zones Actual Weight
Positive Moment for Pilots and Cargo
Negative Moment for Pilots and Cargo
Total Passengers in Manifest
Total Crew and Cargo Weight
Total Positive Moment
Total Negative Moment
Total Adjusted Moment
Empty O.P. Weight
Total Crew and Cargo Weight
Total Baggage Weight (Front)
Total Baggage Weight (Rear)
Total Zero Fuel Weight
Max. ZFW
Total Fuel Weight
Take-Off Weight
Last Minute Correction (Weight)
Revised Actual Take-off Weight
Max. T.O. Weight
Empty O.P. Moment
Total Adjusted Moment (see #97)
Total Baggage Moment (Front)
Total Baggage Moment (Rear)
Total Zero Fuel Moment
Total Fuel Moment
Take-off Moment
Last Minute Correction (Moment)
Revised Actual Take-Off Moment
Minimum and Maximum Limit Moment
Corrected Limit Moments (If Applicable)
Pilot in Command Signature
Agent’s Signature
Remarks or Comments in Flight
39
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
26
DATE
:
09/02/2010
REVISION:
39
VIEQUES AIR LINK, INC.
CARGO FLIGHT MANIFEST (ISLANDER & TRISLANDER)
VAL FORM 002
DATE
A/C NUMBER
FROM
TO
FLIGHT NO.
TIME
1
2
3
4
5
6
+
Moment
17
Moment
22
13
18
23
9
14
19
24
ZONE B
10
15
20
25
ZONE C
11
16
21
26
28
29
30
PASSENGERS NAMES
Pax Weight
PIC
7
12
SIC
8
ZONE A
27
TOTAL
PAX’S
TOTALS
Seat
row
1
31
TOTAL MOMENTS
PASSENGER COMPARMENT
Empty OP Weight
3
2
4
3
Passengers. Comp
3
3
4
4
Bagg Compt (Front)
3
4
4
5
Bagg Compt (Rear)
3
5
4
6
T ZWF
3
6
4
7
Fuel Weight
3
8
4
8
T.O. Weight
3
9
4
9
Correction
4
0
5
0
Revised T.O. Weight
4
1
5
1
Max T.O. Weight
4
2
Min. Mom.
Max. Mom.
52
Corrected Moment
ZFW (MAX) (37)
Min. Mom.
Max. Mom.
53
I CERTIFY THAT THE MAXIMUM ALLOWABALE
TAKE OFF WEIGHT FOR THIS FLIGHT IS
WITHIN THE ALLOWANCE SHOWN IN THE
AIRCRAFT FLIGHT MANUAL.
54
Signature of Pilot in Command
56
Remarks:
NOTE:
Prepared by:
55
Maximum Load Zone A (forward of front spar) not to exceed 1,000 lb. (453.6 kg), 1,500 lb. (680 kg) on
Trislander only.
Maximum load Zone B (between spars) not to exceed 820 lb. (371.97 kg)
Maximum load Zone C (AFT of rear spar) not to exceed 1,000 lb. (453.6 kg)
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
27
DATE
:
09/02/2010
REVISION:
CARGO ISLANDER BN2A-B
WEIGHTS AND ARMS FORM
Table 2 - LOAD WEIGHTS AND MOMENTS CARGO
Weight lb.
20
40
60
80
100
150
200
250
300
350
400
450
500
550
600
650
700
750
800
850
900
950
1000
Fwd of Front
Spar Station
122 (Zone A) 12.5
-3
-5
-8
-0
-13
-19
-25
-31
-38
-44
-50
-56
-63
-69
-75
-81
-88
-94
-100
-106
-113
-119
-125
CARGO BN2A-B
Baggage Bay
Between Spars Aft of Rear Spar Station 255.5
Station 162
Station 194
(Mod NBM483)
(Zone B) +27.5 (Zone C) +59.5
+121.5
+6
+11
+24
+11
+24
+48
+17
+36
+72
+22
+48
+96
+28
+60
+120
+41
+89
+181
+55
+119
+241
+69
+149
+301
+83
+179
+363
+96
+208
+422
+110
+238
+482
+124
+268
+138
+298
+151
+327
+165
+357
+179
+387
+193
+417
+206
+446
+220
+476
+506
+536
+565
+595
39
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
28
DATE
:
09/02/2010
REVISION:
39
CARGO TRISLANDER
WEIGHTS AND ARMS FORM
Weight lb.
Table 2 - LOAD WEIGHTS AND MOMENTS CARGO
All Moments are divided by 100
Fwd of Front Spar
Between Spars
Aft of Rear Spar
Station 175 (Zone A) Station 262 (Zone B) Station 294 (Zone C)
-59.5
+27.5
+59.5
20
40
60
80
100
150
200
250
300
350
400
450
500
550
600
650
700
750
800
850
900
950
1000
CARGO TRISLANDER
-11.0
-23.8
-35.7
-47.6
-59.5
-89.3
-119.0
-148.8
-178.5
-208.3
-238.0
-267.8
-297.5
-327.3
-357.0
-386.8
-416.5
-446.3
-476.0
-505.8
-535.5
-565.3
-595.0
+5.5
+11.0
+16.5
+22.0
+27.5
+41.0
+55.0
+68.8
+82.5
+96.3
+110.0
+123.8
+137.5
+151.3
+165.0
+178.8
+192.5
+206.3
+220.0
+11.9
+23.8
+35.7
+47.6
+59.5
+89.3
+119.0
+148.8
+178.5
+208.3
+238.0
+267.8
+297.5
+327.0
+357.0
+386.8
+416.5
+446.3
+476.0
+505.8
+535.5
+565.3
+595.0
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
29
DATE
:
09/02/2010
REVISION:
39
INSTRUCTIONS FOR THE PREPARATION OF FLIGHT MANIFEST FOR BN-2A/B,
BN2A MKIII/2 ON COMPUTER
1.
2.
3.
4.
5.
6.
7.
8.
9 thru 24.
25.
26.
27 thru 42.
43.
44.
45 thru 60.
61 thru 62.
63 thru 78.
79 thru 80.
81 thru 96.
97.
98.
99.
100.
101.
102.
103.
104.
105.
106.
107.
108.
109.
110.
111.
112.
113.
114.
115.
116.
Date of Flight (Computer enters date automatically)
Aircraft Registration Number (Company a/c are stored on Computer)
Point of Departure (Enter departure point or select from list of schedule flights)
Destination (Enter destination point or select from list of schedule flights)
Flight Number (Enter number or select from list of schedule flights)
Schedule Departure Time (Computer displays time based on schedule)
Full Name of Pilot in Command
Full Name of First Officer
Full Name Passenger’s
Captain’s Actual Weight
First Officer Actual Weight
Passenger’s Actual Weight
Baggage of Pilot in Command (if any)
Baggage of First Officer (if any)
Passenger’s Baggage Weight
Pilot and First Officer Seat Positions (Permanent position number 1)
Passenger’s Seats Designation (Done by Computer by Scientific Sort)
Negative Moment Pilot and First Officer (Done by Computer by Scientific Sort)
Passenger’s Moments (Done by Computer by Scientific Sort)
Empty O.P. Weight (Programmed with registration number of A/C)
Total Crew and Passenger’s Weight (Done automatically by Computer)
Total Baggage Weight (Calculated by Computer)
Total Zero Fuel Weight (Calculated by Computer)
Max. ZFW (Programmed with registration number of A/C)
Total Fuel Weight (Enter the Fuel in lbs.)
Take-Off Weight (Calculated by Computer)
Max. T.O. Weight (Programmed with registration number of A/C)
Empty O.P. Moment (Programmed with registration number of A/C)
Passenger Compartment Moment (Calculated by Computer)
Total Baggage Moment (Calculated by Computer)
Total Zero Fuel Weight Moment (Calculated by Computer)
Total Fuel Moment (Calculated by Computer)
Take-off Moment (Calculated by Computer)
Minimum Limit Moment (Depends on T-off Weight, Values retrieved from Computer)
Maximum Limit Moment (Depends on T-off Weight, Values retrieved from Computer)
Moments Maximum Deviation (Done Automatically by Computer )
Deviation (Done Automatically by Computer)
Pilot in Command Signature
Computer Operator Signature
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
30
DATE
:
09/02/2010
REVISION:
39
INSTRUCTIONS FOR THE PREPARATION OF
FLIGHT MANIFEST FOR BN-2A/B,
BN2A MKIII/2 ON COMPUTER (Cont.)
When all the data necessary for the weight and balance is entered the operator of the
computer press F10 on the keyboard where a menu is displayed to complete a print the
weight and balance.
If any correction is necessary before or after the manifest the computer operator just need to
move the cursor on the computer operator just need to move the cursor on the computer to
the field that need to be changed and press F10 on the keyboard and print the manifest
again.
To start a new manifest press F1 on the computer on the keyboard and all the data of the
previous manifest is erased.
If by any reason after the manifest is computed the aircraft is changed the programmer move
the cursor to the aircraft number field and change that number the computer automatically
change all the values pertinent to the aircraft.
NOTE 1:
This weight and balance program was prepared specifically for Vieques Air
Link, Inc. by a qualified computer programmer using the procedures
techniques and information from Britten Norman
NOTE 2:
Any necessary change will be complying by the programmer.
Name and address of programmer is available on request.
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
31
DATE
:
09/02/2010
REVISION:
39
VIEQUES AIR LINK, INC.
VAL FORM 001-A
DATE
FLIGHT MANIFEST (ISLANDER & TRISLANDER ON COMPUTER)
A/C NUMBER
1
FROM
2
TO
3
PASSENGERS NAMES
FLIGHT NO.
4
PAX WEIGHT
TIME
5
BAGGAGE
6
SEAT
MOMENT
PIC
7
25
43
61
79
SIC
8
26
44
62
80
1
9
27
45
63
81
2
10
28
46
64
82
3
11
29
47
65
83
4
12
30
48
66
84
5
13
31
49
67
85
6
14
32
50
68
86
7
15
33
51
69
87
8
16
34
52
70
88
9
17
35
53
71
89
10
18
36
54
72
90
11
19
37
55
73
91
12
20
38
56
74
92
13
21
39
57
75
93
14
22
40
58
76
94
15
23
41
59
77
95
16
24
42
60
78
96
WEIGHT
MOMENTS
MOMENT LIMIT
Empty OP Weight
97
105
Minimum:
111
Passengers. Comp
98
106
Maximum:
112
Bagg Comp
99
107
T ZWF
100
108
Max. Dev.:
113
ZFW (MAX) (101)
*
*
Deviation:
114
Fuel Weight
102
109
T.O. Weight
103
110
Max T.O. Weight
104
*
I CERTIFY THAT THE MAXIMUM ALLOWABALE TAKE OFF WEIGHT FOR THIS FLIGHT IS WITHIN THE ALLOWANCE SHOWN IN THE
AIRCRAFT FLIGHT MANUAL.
115
Signature of Pilot in Command
116
Prepared by:
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
32
DATE
:
09/02/2010
REVISION:
39
VIEQUES AIR LINK, INC.
FLIGHT MANIFEST (CARAVAN 208B)
VAL FORM 001 - B
DATE
A/C NUMBER
FROM
PASSENGERS NAMES
Weight
TO
1 | PIC
Multiply
by
.136
2
.136
3
.174
4
.174
5
.210
6
.210
7
.246
8
.246
9
.282
10
.282
Seat
Baggage Compartment Cabin Location
.344
Cargo Pod Zone A
.132
Cargo Pod Zone B
.182
Cargo Pod Zone C
.234
Cargo Pod Zone D
.288
Usable Fuel Weight
.203
Aircraft Empty Weight and Moment
xxxxx
Ramp Weight & Moment
xxxxx
FLIGHT NO.
Revised Ramp Weight & Moment
Fuel Allowance for Engine Start, Taxi, Run-Up
Take-off Weight and Moment
xxxxx
-35
xxxxx
xxxxx
Maximum Take-Off Weight 8,750 Pounds
TOTAL PAX’S
C EN T ER O F G R A V I T Y
LI M I T S
Moment
Correction
-7.2
TIME
POUNDS
4500
4600
4700
4800
4900
5000
5100
5200
5300
5400
5500
5600
5700
5800
5900
6000
6100
6200
6300
6400
6500
6600
6700
6800
6900
7000
7100
7200
7300
7400
7500
7600
7700
7800
7900
8000
8100
8200
8300
8400
8500
8600
8700
8800
AFT
810
820
840
860
880
900
920
930
950
960
980
1010
1020
1050
1070
1100
1120
1140
1160
1180
1200
1220
1240
1260
1280
1310
1330
1360
1380
1405
1425
1450
1470
1500
1520
1540
1570
1600
1620
1640
1670
1700
1720
1740
Remarks:
I CERTIFY THAT THE MAXIMUM ALLOWABLE TAKE OFF WEIGHT FOR THIS
FLIGHT IS WITHIN THE ALLOWANCE SHOWN IN THE AIRCRAFT FLIGHT MANUAL.
Signature of Pilot in Command
Prepared by:
FWD
920
940
960
980
1000
1020
1040
1060
1080
1100
1120
1140
1160
1180
1200
1230
1250
1270
1290
1310
1330
1350
1370
1390
1410
1430
1450
1475
1495
1515
1535
1555
1575
1600
1620
1640
1660
1680
1700
1720
1740
1760
1780
1790
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
33
DATE
:
09/02/2010
REVISION:
39
INSTRUCTIONS FOR THE PREPARATION OF FLIGHT MANIFEST FOR CARAVAN 208B
1.
2.
3.
4.
5.
6.
7.
8 thru 16.
17.
18 thru 26.
27.
28.
29.
30.
31.
32.
33.
34.
35.
36.
37.
38.
39 thru 47.
48.
49.
50.
51.
52.
53.
54.
55.
56.
57.
58.
59.
60.
61.
62.
63.
Date of flight
Aircraft Registration Number
Point of Departure
Destination
Number of schedule flight/flight status
Schedule Departure Time
Full Name of Pilot in Command
Full Name Passenger’s
Captain’s Actual Weight
Passenger’s Actual Weight
Baggage Compartment Cabin Location Weight
Cargo Pod Zone A Weight
Cargo Pod Zone B Weight
Cargo Pod Zone C Weight
Cargo Pod Zone D Weight
Usable Fuel Weight ( Enter in lbs.)
Aircraft Empty Weight
Ramp Weight
Correction Weight
Revised Ramp Weight
Take-Off Weight
Pilot Moment
Passenger’s Moment
Baggage Compartment Moment
Cargo Pod Zone A Moment
Cargo Pod Zone B Moment
Cargo Pod Zone C Moment
Cargo Pod Zone D Moment
Usable Fuel Weight Moment
Aircraft Empty Moment
Ramp Moment
Correction Moment
Revised Ramp Moment
Take-Off Moment
Center of Gravity Limits Table
Passenger’s Total
Remark Section
Pilot Signature
Prepared by Signature
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
34
DATE
:
09/02/2010
REVISION:
39
VIEQUES AIR LINK, INC.
FLIGHT MANIFEST (CARAVAN 208B)
VAL FORM 001 - B
DATE
A/C NUMBER
FROM
TO
FLIGHT NO.
TIME
1
2
3
4
5
6
Seat
PASSENGERS NAMES
Weight
1 | PIC
7
17
Multiply
by
.136
2
8
18
.136
39
3
9
19
174
40
4
10
20
.174
41
5
11
21
.210
42
6
12
22
.210
43
7
13
23
.246
44
8
14
24
.246
45
9
15
25
.282
46
10
16
26
.282
47
x
Baggage Compartment Cabin Location
27
.344
48
x
Cargo Pod Zone A
28
.132
49
x
Cargo Pod Zone B
29
.182
50
x
Cargo Pod Zone C
30
.234
51
x
Cargo Pod Zone D
31
.288
52
x
Usable Fuel Weight
32
.203
53
x
Aircraft Empty Weight and Moment
33
xxxxx
54
x
Ramp Weight & Moment
34
xxxxx
55
Correction
35
x
Revised Ramp Weight & Moment
36
xxxxx
57
x
Fuel Allowance for Engine Start, Taxi, Run-Up
-35 (fix)
xxxxx
-7.2
x
Take-off Weight and Moment
37
xxxxx
58
Moment
38
56
Maximum Take-Off Weight 8,750 Pounds
60
Remarks:
TOTAL PAX’S
61
C EN T ER OF GR A V IT Y
LI M I T S ( 59 )
POUNDS
4500
4600
4700
4800
4900
5000
5100
5200
5300
5400
5500
5600
5700
5800
5900
6000
6100
6200
6300
6400
6500
6600
6700
6800
6900
7000
7100
7200
7300
7400
7500
7600
7700
7800
7900
8000
8100
8200
8300
8400
8500
8600
8700
8800
A FT
810
820
840
860
880
900
920
930
950
960
980
1010
1020
1050
1070
1100
1120
1140
1160
1180
1200
1220
1240
1260
1280
1310
1330
1360
1380
1405
1425
1450
1470
1500
1520
1540
1570
1600
1620
1640
1670
1700
1720
1740
I CERTIFY THAT THE MAXIMUM ALLOWABLE TAKE OFF WEIGHT FOR THIS
FLIGHT IS WITHIN THE ALLOWANCE SHOWN IN THE AIRCRAFT FLIGHT MANUAL.
62
Signature of Pilot in Command
Prepared by:
63
FWD
920
940
960
980
1000
1020
1040
1060
1080
1100
1120
1140
1160
1180
1200
1230
1250
1270
1290
1310
1330
1350
1370
1390
1410
1430
1450
1475
1495
1515
1535
1555
1575
1600
1620
1640
1660
1680
1700
1720
1740
1760
1780
1790
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
35
DATE
:
09/02/2010
REVISION:
39
CARAVAN 208-B
Table 1 - LOAD WEIGHTS AND MOMENTS - OCCUPANTS
(ALL MOMENTS ARE DIVIDED BY 100)
Weight Seat 1 Seat 2 Seat 3 Seat 4 Seat 5 Seat 6 Seat 7 Seat 8 Seat 9 Seat 10
(135.5) (135.5) (173.9) (173.9) (209.9) (209.9) (245.9) (245.9) (281.9) (281.9)
30
4
4
5
5
6
6
7
7
8
8
40
5
5
7
7
8
8
10
10
11
11
50
7
7
9
9
11
11
12
12
14
14
60
8
8
10
10
13
13
15
15
17
17
70
10
10
12
12
15
15
17
17
20
20
80
11
11
14
14
17
17
20
20
23
23
90
12
12
16
16
19
19
22
22
25
25
100
14
14
17
17
21
21
25
25
28
28
110
15
15
19
19
23
23
27
27
31
31
120
16
16
21
21
25
25
30
30
34
34
130
18
18
23
23
27
27
32
32
37
37
140
19
19
24
24
29
29
34
34
39
39
150
20
20
26
26
32
32
37
37
42
42
160
22
22
28
28
34
34
39
39
45
45
170
23
23
30
30
36
36
42
42
48
48
180
24
24
31
31
38
38
44
44
51
51
190
26
26
33
33
40
40
47
47
54
54
200
27
27
35
35
42
42
49
49
56
56
210
29
29
37
37
44
44
52
52
59
59
220
30
30
38
38
46
46
54
54
62
62
230
31
31
40
40
48
48
57
57
65
65
240
33
33
42
42
50
50
59
59
68
68
250
34
34
44
44
53
53
62
62
71
71
260
35
35
45
45
55
55
64
64
73
73
270
37
37
47
47
57
57
66
66
76
76
280
38
38
49
49
59
59
69
69
79
79
290
39
39
51
51
61
61
71
71
82
82
300
41
41
52
52
63
63
74
74
85
85
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
36
DATE
:
09/02/2010
REVISION:
39
INSTRUCTIONS FOR THE PREPARATION OF FLIGHT MANIFEST FOR CARAVAN ON COMPUTER
1.
2.
3.
4.
5.
6.
7.
8 thru 16.
17.
18 thru 26.
27.
28.
29.
30.
31.
32.
33.
34.
35.
36.
37 thru 45.
46.
47 thru 55.
56.
57 thru 65.
66.
67.
68.
69.
70.
71.
72.
73.
74.
75.
76.
77.
78.
Date of flight (Computer enters date automatically)
Aircraft Registration Number (Company a/c are stored on Computer)
Point of Departure (Enter departure point or select from list of schedule flights)
Destination (Enter destination point or select from list of schedule flights)
Flight Number (Enter number or select from list of schedule flights)
Schedule Departure Time (Computer displays time based on schedule)
Full Name of Pilot in Command
Full Name Passenger’s (Enter each name of passengers in computer)
Captain’s Actual Weight
Passenger’s Actual Weight
Baggage Compartment Cabin Location Weight
Cargo Pod Zone A Weight (Calculated automatically by Computer)
Cargo Pod Zone B Weight (Calculated automatically by Computer)
Cargo Pod Zone C Weight (Calculated automatically by Computer)
Cargo Pod Zone D Weight (Calculated automatically by Computer)
Usable Fuel Weight (Enter fuel in lbs.)
Aircraft Empty Weight (Programmed and enter automatically when selection of a/c number)
Ramp Weight (Calculated automatically by Computer)
Fuel Allowance for Engine Start, Taxi, Run-Up (This subtracts automatically)
Pilot in Command Baggage Weight (if any)
Passengers Baggage Weight
Pilot Seat Position (Always assigned number 1)
Passenger’s Seats Designation (Done by Computer by Scientific Sort)
Pilot in Command Moment
Passenger’s Moment (Calculated by Computer)
Baggage Compartment Moment (Calculated by Computer)
Cargo Pod Zone A Moment (Calculated automatically by Computer)
Cargo Pod Zone B Moment (Calculated automatically by Computer)
Cargo Pod Zone C Moment (Calculated automatically by Computer)
Cargo Pod Zone D Moment (Calculated automatically by Computer)
Usable Fuel Moment (Enter the fuel pounds)
Aircraft Empty Moment (Programmed with registration number of A/C)
Ramp Moment (Calculated automatically by Computer)
Fuel Allowance for Engine Start, Taxi, Run-Up (This subtract automatically)
Remarks
Weights and Moments Limits (Calculated automatically by Computer)
Pilot in Command Signature
Computer Operator Signature
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
37
DATE
:
09/02/2010
REVISION:
39
INSTRUCTIONS FOR THE PREPARATION OF
FLIGHT MANIFEST FOR CARAVAN 208B
ON COMPUTER (Cont.)
When all the data necessary for the weight and balance is entered the operator of the
computer press F10 on the keyboard where a menu is displayed to complete a print the
weight and balance.
If any correction is necessary before or after the manifest the computer operator just need to
move the cursor on the computer operator just need to move the cursor on the computer to
the field that need to be changed and press F10 on the keyboard and print the manifest
again.
To start a new manifest press F1 on the computer on the keyboard and all the data of the
previous manifest is erased.
If by any reason after the manifest is computed the aircraft is changed the programmer move
the cursor to the aircraft number field and change that number the computer automatically
change all the values pertinent to the aircraft.
NOTE 1:
This weight and balance program was prepared specifically for Vieques Air
Link, Inc. by a qualified computer programmer using the procedures
techniques and information from Cessna (caravan)
NOTE 2:
Any necessary change will be complying by the programmer.
Name and address of programmer is available on request.
Operations Manual
Vieques Air Link, Inc.
Volume I
SECTION X
SECTION :
X
PAGE
:
38
DATE
:
09/02/2010
REVISION:
39
VIEQUES AIR LINK, INC.
FLIGHT MANIFEST (CARAVAN ON COMPUTER)
VAL FORM 001-B
DATE
A/C NUMBER
FROM
TO
FLIGHT NO.
TIME
1
2
3
4
5
6
PASSENGERS NAMES
PAX WEIGHT
BAGGAGE
SEAT
MOMENT
1 | PIC
7
17
36
46
56
2
8
18
37
47
57
3
9
19
38
48
58
4
10
20
39
49
59
5
11
21
40
50
60
6
12
22
41
51
61
7
13
23
42
52
62
8
14
24
43
53
63
9
15
25
44
54
64
10
16
26
45
55
65
X
Baggage Compartment Cabin Location
27
66
X
Cargo Pod Zone A
28
67
X
Cargo Pod Zone B
29
68
X
Cargo Pod Zone C
30
69
X
Cargo Pod Zone D
31
70
X
Usable Fuel Weight
32
71
X
Aircraft Empty Weight and Moment
33
XXXXX
72
X
Ramp Weight and Moment
34
XXXXX
73
X
Fuel Allowance for Engine Start, Taxi, Run-Up
35
XXXXX
74
Maximum Take-Off Weight 8,750 Pounds
Remarks:
WEIGHT AND MOMENTS LIMITS
TOW
Max. TOW
75
76
Max. AFT
Ramp
Max. FWD
I CERTIFY THAT THE MAXIMUM ALLOWABLE TAKE OFF WEIGHT FOR THIS
FLIGHT IS WITHIN THE ALLOWANCE SHOWN IN THE AIRCRAFT FLIGHT MANUAL.
77
Signature of Pilot in Command
78
Prepared by: