Supplement E6
Baggage Extension,
Baggage Tray
DA 40 AFM
DA 40 D AFM
0.1
RECORD OF REVISIONS
Rev. Reason
No.
Chap- Pager
ter
Doc. # 6.01.01-E
Doc. # 6.01.05-E
Rev. 0
Date of
revision
EASA Ap- ACG
proval No. Verification
09 Jan 2004
Date inserted
Signature
Page 9 - E6 - 1
Supplement E6
Baggage Extension,
Baggage Tray
DA 40 AFM
DA 40 D AFM
0.2
LIST OF EFFECTIVE PAGES
Chapter
Page
Date
9-E6-0
09 Jan 2004
9-E6-1
09 Jan 2004
9-E6-2
09 Jan 2004
9-E6-3
09 Jan 2004
1
9-E6-4
09 Jan 2004
2
9-E6-5
09 Jan 2004
3, 4A, 4B, 5
9-E6-6
09 Jan 2004
9-E6-7
09 Jan 2004
9-E6-8
09 Jan 2004
9-E6-9
09 Jan 2004
9-E6-10
09 Jan 2004
9-E6-11
09 Jan 2004
9-E6-12
09 Jan 2004
9-E6-13
09 Jan 2004
0
6
7, 8
Doc. # 6.01.01-E
Doc. # 6.01.05-E
Rev. 0
09 Jan 2004
Page 9 - E6 - 2
Supplement E6
Baggage Extension,
Baggage Tray
DA 40 AFM
DA 40 D AFM
0.3
TABLE OF CONTENTS
Page
1.
GENERAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9-E6-4
2.
OPERATING LIMITATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9-E6-5
3.
EMERGENCY PROCEDURES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9-E6-6
4A. NORMAL OPERATING PROCEDURES . . . . . . . . . . . . . . . . . . . . . . . . . 9-E6-6
4B. ABNORMAL OPERATING PROCEDURES . . . . . . . . . . . . . . . . . . . . . . . 9-E6-6
5.
PERFORMANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9-E6-6
6.
MASS AND BALANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9-E6-7
7.
DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS . . . . . . . . . . . 9-E6-13
8.
AIRPLANE HANDLING, CARE AND MAINTENANCE . . . . . . . . . . . . . . 9-E6-13
Doc. # 6.01.01-E
Doc. # 6.01.05-E
Rev. 0
09 Jan 2004
Page 9 - E6 - 3
Supplement E6
Baggage Extension,
Baggage Tray
DA 40 AFM
DA 40 D AFM
1. GENERAL
1.1
INTRODUCTION
This Supplement supplies the information necessary for the efficient operation of the
airplane when the Baggage Extension, with or without the Baggage Tray, is installed. The
baggage area including the Baggage Extension forms the Extended Baggage
Compartment. The information contained within this Supplement is to be used in
conjunction with the complete AFM.
This Supplement to the Airplane Flight Manual is a permanent part of the AFM and must
remain in the AFM at all times when the Extended Baggage Compartment is installed.
The implementation of the design change advisory OÄM 40-163 is prerequisite for the
use of the DA 40 / DA 40 D with the Extended Baggage Compartment. The implementation
of the design change advisory OÄM 40-164 is prerequisite for the use of the DA 40 / DA
40 D with the Baggage Tray. The Baggage Tray may not be used without the Extended
Baggage Compartment. Baggage cannot be carried unless the baggage net is used.
Doc. # 6.01.01-E
Doc. # 6.01.05-E
Rev. 0
09 Jan 2004
Page 9 - E6 - 4
Supplement E6
Baggage Extension,
Baggage Tray
DA 40 AFM
DA 40 D AFM
2. OPERATING LIMITATIONS
2.7
MASS (WEIGHT)
Max. load in forward baggage compartment alone :
45 kg
100 lb
Max. load in aft baggage compartment alone
:
18 kg
40 lb
Max. load, both baggage compartments together
:
45 kg
100 lb
Max. surface load in baggage compartments
:
75 kg/m²
15 lb/sq.ft.
2.15 LIMITATION PLACARDS
On Baggage Extension:
FORWARD BAGGAGE
COMPARTMENT
MAX. 45 kg [100 lb]
ARM: 3.89 m [153.1"]
AFT BAGGAGE
COMPARTMENT
MAX. 18 kg [40 lb]
ARM: 4.54 m [178.7"]
MAX. BAGGAGE TOTAL 45 kg [100 lb]
MAX. SURFACE LOAD: 75 kg/m² [15 lb/sq.ft.]
CAUTION: OBSERVE WEIGHT AND BALANCE LIMITATIONS
SEE AIRPLANE FLIGHT MANUAL CHAPTER 6
Doc. # 6.01.01-E
Doc. # 6.01.05-E
Rev. 0
09 Jan 2004
Page 9 - E6 - 5
Supplement E6
Baggage Extension,
Baggage Tray
DA 40 AFM
DA 40 D AFM
3. EMERGENCY PROCEDURES
No change.
4A. NORMAL OPERATING PROCEDURES
No change.
4B. ABNORMAL OPERATING PROCEDURES
No change.
5. PERFORMANCE
No change.
Doc. # 6.01.01-E
Doc. # 6.01.05-E
Rev. 0
09 Jan 2004
Page 9 - E6 - 6
Supplement E6
Baggage Extension,
Baggage Tray
DA 40 AFM
DA 40 D AFM
6. MASS AND BALANCE
6.1
INTRODUCTION
The Extended Baggage Compartment allows a baggage mass of 45 kg (100 lb) to be
carried when the baggage net is installed. The permissible mass and balance envelope
is not changed.
6.4
FLIGHT MASS AND CENTER OF GRAVITY
6.4.1 MOMENT ARMS
- Baggage
:
see diagram
AFT 4.54 m (178.7 in)
FORWARD 3.89 m (153.1 in)
3.25 m (128.0 in)
2.63 m (103.5 in)
2.30 m (90.6 in)
31 mm
(1.22 in)
1.00 m (39.4 in)
600 mm
(23.62 in)
2.194 m (86.4 in)
Doc. # 6.01.01-E
Doc. # 6.01.05-E
Rev. 0
09 Jan 2004
Page 9 - E6 - 7
Doc. # 6.01.01-E
Doc. # 6.01.05-E
Rev. 0
09 Jan 2004
50
100
150
25
50
75
100
125
150
175
10,000
100
20,000
200
400
500
40,000
Load Moment
30,000
300
50,000
[in.lb]
[kgm]
DA 40 D AFM
10
20
30
40
50
200
Fuel Quantity
[US gal] [liters]
200
225
Load Mass
[lb] [kg]
DA 40 AFM
Supplement E6
Baggage Extension,
Baggage Tray
6.4.2 LOADING DIAGRAM
Page 9 - E6 - 8
Supplement E6
Baggage Extension,
Baggage Tray
DA 40 AFM
DA 40 D AFM
6.4.3 CALCULATION OF LOADING CONDITION
DA 40 (Example)
CALCULATION OF
LOADING CONDITION
Your DA 40
Mass
[kg]
Moment
[kgm]
Mass
[kg]
Moment
[kgm]
[lb]
[in.lb]
[lb]
[in.lb]
781.1
1898.1
1722
164,750
2. Oil not added
Lever arm: 1.00 m (39.4 in)
-1.7
-1.7
-3.7
-146
3. Front seats
Lever arm: 2.30 m (90.6 in)
150
345
331
29,989
1. Empty mass (from Mass and
Balance Report)
4. Rear seats
Lever arm: 3.25 m (128.0 in)
70
227.5
154
19,712
5. Forward baggage compt.
Lever arm: 3.89 m (153.1 in)
25
97.2
55
8,421
6. Aft baggage compartment
Lever arm: 4.54 m (178.7 in)
10
45.4
22
3,931
7. Total mass & total moment
with empty fuel tanks
1034.4
2611.5
2280.3
226,657
8. On-board usable fuel
(0.72 kg/liter) (6.01 lb/US gal)
Lever arm: 2.63 m (103.5 in)
109.4
287.7
241
24,944
9. Total mass & total moment
with full fuel tanks
1143.8
2899.2
2521.3
251,600
(Total of 1.-6.)
(Total 7. plus 8.)
10. The total moments from rows 7 and 9 (2611.5 and 2899.2 kgm) (226,657 and 251,600
in.lb) must be divided by the related total mass (1034.4 and 1143.8 kg respectively)
(2280.3 and 2521.3 lb) and then located in Diagram 6.4.4 'PERMISSIBLE CENTER OF
GRAVITY RANGE'.
As in our example CG positions (2.525 m and 2.535 m respectively) (99.4 and 99.8
in) and masses fall into the permitted area, this loading condition is allowable.
Doc. # 6.01.01-E
Doc. # 6.01.05-E
Rev. 0
09 Jan 2004
Page 9 - E6 - 9
Supplement E6
Baggage Extension,
Baggage Tray
DA 40 AFM
DA 40 D AFM
6.4.4 PERMISSIBLE CENTER OF GRAVITY RANGE
Center of Gravity Position [in]
96
100
1150 kg / 2535 lb
1150
Flight Mass [kg]
98
1100
Normal
1050
1000
2600
2400
2200
980 kg / 2161 lb
950
2000
900
Utility & Normal
850
1800
800
750
2.40
102
Flight Mass [lb]
94
780 kg / 1720 lb
2.45
2.50
2.55
2.60
Center of Gravity Position [m]
CG
Envelope
Rear CG limit for
Long Range Tank
Doc. # 6.01.01-E
Doc. # 6.01.05-E
Rev. 0
09 Jan 2004
Page 9 - E6 - 10
160,000
180,000
Doc. # 6.01.01-E
Doc. # 6.01.05-E
220,000
FLIGHT MASS MOMENT [kgm]
200,000
FLIGHT MASS MOMENT [in.lb]
k
an k
e T Tan
g
n rd
Ra nda
g
n
ta
Lo or S
r
f
o it
it f
im r Lim
L
ar ea
Re R
Rev. 0
09 Jan 2004
1700
DA 40 D AFM
1800
1900
2000
2100
2200
2300
2400
2500
2550
FLIGHT MASS [lb]
er y
nt vit
"
e
"
.4 .0"
C ra ion
5"
9"
4.
G it
6. 98.4 100 102
9
9
f
/
/
/
/
o os
/
m
m m
P
m m
0
6
5
9
0
4
4
5 5
2.
2. 2.5 2. 2.
240,000
260,000
DA 40 AFM
Supplement E6
Baggage Extension,
Baggage Tray
6.4.5 PERMISSIBLE MOMENT RANGE
Page 9 - E6 - 11
FLIGHT MASS [kg]
Supplement E6
Baggage Extension,
Baggage Tray
DA 40 AFM
DA 40 D AFM
6.5
EQUIPMENT LIST AND EQUIPMENT INVENTORY
Additional equipment required for the operation with the extended baggage compartment:
* 1 extended baggage extension installed in accordance with OÄM 40-163
* 1 baggage net
Additional optional equipment:
* 1 baggage tray and lid installed in accordance with OÄM 40-164
Doc. # 6.01.01-E
Doc. # 6.01.05-E
Rev. 0
09 Jan 2004
Page 9 - E6 - 12
Supplement E6
Baggage Extension,
Baggage Tray
DA 40 AFM
DA 40 D AFM
7. DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS
7.7
BAGGAGE COMPARTMENT
The extended baggage compartment consists of the standard baggage compartment
behind the rear seats and the Baggage Extension mounted in the rear bulkhead.
The Baggage Extension has a door that may be hinged up to keep items from sliding aft
or hinged down to carry long items. The Baggage Extension also has a removable panel
in the bottom to allow access for inspection of the rear fuselage area.
The Baggage Tray may be installed in the bottom of the standard baggage compartment.
The lid of the Baggage Tray and the bottom of the Baggage Extension form a flat loading
surface. The lid has mounting provisions for the tow bar. The space under the lid may
be used to carry small items such as the gust lock and the fuel quantity measuring device.
Without the baggage net, no baggage may be loaded.
8. AIRPLANE HANDLING, CARE AND MAINTENANCE
No change.
Doc. # 6.01.01-E
Doc. # 6.01.05-E
Rev. 0
09 Jan 2004
Page 9 - E6 - 13