Carrier 1. SUPPLIERS’ CONTACT ADDRESSahm.yakutia.aero/docs/Dash8/AHM560 All fleet...

EDP-SYSTEM SEMI-PERMANENT DATA 1. SUPPLIERS’ CONTACT ADDRESS

Completed sheets and changes of basic data and procedure must be forwarded to: AHM560 group MAILING ADDRESS: 9, Bykovsky street, Yakutsk, Russian Federation TELETYPE ADDRESS: E-MAIL ADDRESS: [email protected] REMARKS:

2. CARRIER’S CONTACT ADDRESS MAILING ADDRESS: 9, Bykovskogo Street, Yakutsk, Russian Federation TELETYPE ADDRESS: E-MAIL ADDRESS: [email protected] REMARKS:

Completed by: M. Vasiliev Issue No.: 2 (Signature) Date: 24.06.2016

COMMUNICATION ADDRESSES

A Sheet 1

Carrier

R3

EDP-SYSTEM SEMI-PERMANENT DATA 3. AUTOMATICALLY PRODUCED DOCUMENTS (tick as required)

NOTOC

SEATPLAN

LOADPLAN

PASSENGER INFO LIST

LOADSHEET

LOADING INSTRUCTION/REPORT

4. MESSAGE REQUIREMENTS (tick as required) LDM Load Message AHM 583

ALI Abbreviated Load Information Message AHM 584

CPM Container/Pallet Distribution Message AHM 587

UCM ULD Control Message AHM 424 (dispatch only)

MVT Movement Messages AHM 730 and 780

DIV Diversion Message AHM 781

SOM Seats Occupied Message Recommended Practice 1712

PTM Passenger Transfer Message Recommended Practice 1718

PSM Passenger Service Message Recommended Practice 1715 (dispatch only)

TPM Teletype Passenger Manifest Recommended Practice 1717 (dispatch only)

PFS Passenger Final Sales Message Recommended Practice 1719 (dispatch only)

IDM Industry Discount Message Recommended Practice 1714

RQL Request List Message Recommended Practice 1709 (dispatch only)

PNL/ADL Passenger Name List, and Additions and Deletions List (Recommended Practice 1708) (acceptance only)

SAL Seats Available List Recommended Practice 1713 (acceptance only)

SLS Statistical Load Summary AHM 588

FMM Fuel Monitoring Message AHM 782

RQM Request Information Message AHM 783

UWS ULD/Bulk Load Weight Signal AHM 581(acceptance only)

5. MESSAGE ADDRESSES

Attach a complete address list for all messages mentioned under paragraph 4 above.

6. DEFINITION OF CLASS CODES

The following class naming convention shall be used throughout the document. Class codes: (e.g. F, Y, C, M, etc.)

Class 1

Class 2

Class 3 Y

Class 4

Class 5

7. DEFINITION OF UNITS OF MEASURE (tick as appropriate)

Weight Kg Lbs

Length Meters Inches

Volume Cu.mtr Cu.ft

Liquid Volume Liter US Gallon

8. MULTIPLE SHEETS NUMBERING

In the event of the requirements to produce multiple copies of the same sheets (e.g. C5, C9) establish an additional sequence identifier while keeping the original sheet number. E.g. C5a, C5b, etc, or C5.1, C5.2, etc.

Completed by: M. Vasiliev Issue No.: 2

(Signature) Date: 24.06.2016

COMMUNICATION ADDRESSES

A Sheet 2

Carrier

R3

EDP-SYSTEM SEMI-PERMANENT DATA

Section Sheet Multiple page identifier Sheet issue No. Date

YYYYMMDD

C 4 6 23.05.2018

C 5 6 23.05.2018

B 2 7 20.06.2018

B 3 7 20.06.2018

C 3 7 20.06.2018

C 7 7 20.06.2018

Attachment #1 7 20.06.2018

Attachment #2 7 20.06.2018

A 3 8 15.03.2018

A 4 8 15.03.2018

C 3 8 15.06.2018

Attachment #2 8 15.06.2018

A 3 9 21.12.2018

A 4 9 21.12.2018

C 3 9 21.12.2018

C 6 A,B,C 9 21.12.2018

Attachment #1 9 21.12.2018

Attachment #2 9 21.12.2018

C 3 10 28.08.2019

C 4 10 28.08.2019

C 6 A,B,C 10 28.08.2019

Attachment #2 10 28.08.2019

Attachment #3 10 28.08.2019

*If issue no. changes, “update complete document”, else “N/U/D section sheet paragraph”


LIST OF REVISIONS

A Sheet 3

Carrier

R3


Section Sheet Multiple page identifier Sheet issue No. Date YYYYMMDD

A 1 2 24.06.2016

A 2 2 24.06.2016

A 3 10 28.08.2019

A 4 10 28.08.2019

B 1 3 25.07.2017

B 2 7 20.06.2018

B 3 7 20.06.2018

C 1 2 24.06.2016

C 2 2 24.06.2016

C 3 10 28.08.2019

C 4 10 28.08.2019

C 5 6 23.05.2018

C 6 A,B,C 10 28.08.2019

C 7 7 20.06.2018

C 8 2 24.06.2016

C 9 2 24.06.2016

C 10 2 24.06.2016

C 11 2 24.06.2016

C 12 5 23.03.2018

C 13 5 23.03.2018

C 14 2 24.06.2016

D 1 3 25.07.2017

D 2 2 24.06.2016

D 3 2 24.06.2016

Attachment #1 9 21.12.2018

Attachment #2 10 28.08.2019

Attachment #3 10 28.08.2019

Completed by: M. Vasiliev Issue No.: 10

(Signature) Date: 28.08.2019

LIST OF EFFECTIVE SHEETS

A Sheet 4

Carrier

R3


1. PASSENGER AND BAGGAGE WEIGHTS

1.1 Standard / default passenger / cabin baggage weights

Standard/variations* Standard summer season weights

Standard winter season weights

* *

Average adult 75 kg 80 kg

Child 30 kg 30 kg

Infant 15 kg 15 kg

Cabin Baggage 10 kg 10 kg

Yes No

Cabin baggage weight is included in the above mentioned passenger weights.

Remarks: Summer season from last Sunday of March / to last Sunday of October

Winter season from last Sunday of October / to last Sunday of March

1.2 If passenger / cabin baggage weights vary by class, use the following table:

Class as appropriate Class 1 Class 2 Class 3 Class 4 Class 5 Class 6 Class 7

Average adult

Child

Infant

Cabin Baggage

Remarks: Flights to U.S. use piece concept: for Class 3: 1 bag – 23 kg.

for Class 2: 2 bags – 32 kg.

1.3 Checked baggage weight

Standard/variations* Standard * * * *

Weight per piece Actual

Weight per passenger Actual

* Variations may include domestic, international, charter, route, etc.

Remarks: Oversized baggage is treated as overweight baggage

1.4 Planning assumption

Route

Standard/variations* Standard * * * * * *

Average bags/pax 1.5

Average bag weight/pax 20

Average bag volume 0.12

if variations by route use separate table per route


GENERAL INFORMATION

B Sheet 1

Carrier

R3

EDP-SYSTEM SEMI-PERMANENT DATA 2. CREW AND CREW BAGGAGE WEIGHTS

2.1 Crew weights

Standard Male Female

Cockpit 85 kg

Cabin 75 kg

Crew hand baggage shall be included in the above crew weights.

Remarks: Standard crew 2/1 (2 pilots / 1 attendants) included in DOW

2.2 Crew Baggage Weights (other than hand baggage)

Cockpit Cabin

Shorthaul Actual Actual

Longhaul Actual Actual

Others*

*Specify conditions as appropriate.

Remarks: Maximum allowed cockpit and cabin crew free baggage weight 20 kg per person


GENERAL INFORMATION

AIRCRAFT DATA

B Sheet 2

Carrier

R3

EDP-SYSTEM SEMI-PERMANENT DATA 3. DRY OPERATING WEIGHT AND DRY OPERATING INDEX SPECIFICATIONS

(tick as appropriate)

DOW DOI Remarks

Item Incl. Excl. Incl. Excl.

Basic Weight

Cockpit Crew Standard 2

Cabin Crew Standard 1

Crew baggage

Pantry

Containers

Pallets

Potable Water 10 kg

Weapon box 42 kg in CPT2

Towbar 33 kg in CPT2

Remarks:


GENERAL INFORMATION

B Sheet 3

Carrier

R3


AIRCRAFT DATA C Sheet 1

A/C Type

DHC-8-300

Carrier

R3 1. BALANCE AND SPECIAL INFORMATION — OUTPUT ON LOADSHEET

1.5 Balance output (Reference AHM 517)

Please mark your requirements in respective box. Remarks

Basic Index BI

Dry Operating Index DOI

Deadload Index DLI

Deadload MAC MACDLW

Loaded Index at zero fuel weight LIZFW

Loaded Index at take-off weight LITOW

Loaded Index at landing weight LILAW

MAC — at zero fuel weight MACZFW

MAC — at take-off weight MACTOW

MAC — at landing weight MACLAW

Stabilizer trim setting at take-off STABTO*

*Specify ANU or AND as appropriate.

1.5.1 Passenger trim output

Please mark your requirements in respective box.

Remarks*

Class trim Not allowed

Cabin area trim 2nd priority

Seat row trim 1st priority

*Remarks: Indicate any other terminology to be printed on the loadsheet (Ref. AHM 517, 6.2, item 44).

1.6 Special Information

Specify the information to be entered in the lower parts of the EDP Loadsheet.

1.6.1 Captain’s information/notes, Center of Gravity limits, ramp weight, etc. (give examples). (Ref. AHM

517, 6.2, item 45.

1.6.2 Load message before LMC, if required, to be shown. (Ref. AHM 517, 6.2, item 46).


2.1 Examples and definitions

Index =

W = Weight, actual. Sta. = Station, horizontal distance in length units from station zero to the location. Ref. Sta. = Reference station/axis. Selected station around which all index values are calculated. K = Constant used as a plus value to avoid negative index figures C = Constant used as a denominator to convert moment values into index values. I = Index value corresponding to respective weight. MAC/RC = Length of Mean Aerodynamic Chord/Reference Chord in length units. LEMAC = Horizontal distance in length units from the station zero to location of the Leading Edge of the MAC/RC.

2.2 Index formula

Ref. Sta. at : 400 length units from zero.

K (constant) = 100

C (constant) = 10000

2.3 MAC/RC information

Length of MAC/RC = 85.5 length units.

LEMAC at : 378.37 length units from zero.

2.4 Stabilizer trim setting

For each required Thrust rating and/or Flap setting, or range of ratings/settings, supply

the following data:

Thrust rating or Range (from) (to)

Flaps setting or Range (from) 1 (to) 5

(Specify stabilizer settings for at least one weight if setting doesn’t change at different weights.)

(Specify at least minimum and maximum MAC/RC values.)

MAC/RC values




2. BASIC INDEX AND MAC/RC FORMULA

A/C Type

DHC-8-300

Carrier

R3

W (Sta. Ref. Sta.) C + K

% MAC/RC =

Weight

N/A




STANDART FLAP SETTING

A/C Type

DHC-8-300

Carrier

R3



A/C Type

DHC-8-300

Carrier

R3

3. AIRCRAFT REGISTRATIONS, WEIGHT AND INDEX DETAILS

DRY OPERATING WEIGHT BASIC WEIGHT (tick as appropriate)

Provide full list of registrations/tail numbers and adjustments to fleet weight/index

Fleet Weight: 12500 Fleet Index: 99.0

Registration/tail number

Weight Adjustment

Index Adjustment

Registration/tail number

Weight Adjustment

Index Adjustment

VQ-BVI -115 +0.8

VQ-BVJ -22 +1.5

VQ-BVH +198 -1.0

VP-BNS +81 +6.2

Note: Notification for data changes at short notice may also be made by means of data exchange message (AHM 562).




4. LIMITATIONS

A/C Type

DHC-8-300 Carrier

R3 4.1 Aircraft Weight Limitations

Operator defined maximum weights for:

Aircraft Reg./Tail Number

Ramp/Taxi Take-off Zero Fuel Landing

VQ-BVI 19595 19505 17917 19051

VQ-BVJ 19595 19505 17917 19051

VQ-BVH 19595 19505 17917 19051

VP-BNS 19595 19505 17917 19051




A/C Type

DHC-8-300 Carrier

R3 4.2 CG — Limits for Loadsheet

Purposes

Enter the forward and the aft balance limits in the boxes, commencing at the lowest possible operating weight and terminating at the highest possible operating weight to be checked.

IMPORTANT: If limits are affected and/or determined by passenger/fuel/version or other conditions, specify each set of limits on a separate sheet, entering the special condition(s) in the box.

FORWARD

Special condition if applicable

Specify applicability* Weight Index

Take-off

MTOW 19505 93.67

13608 88.02

10433 90.81

Landing

MLW 19051 93.23

13608 88.02

10433 90.81

Zero Fuel

MZFW 17917 96.98

13608 92.85

10433 95.64

AFT

Special condition if applicable

Specify applicability*

Weight Index

Take-off MTOW 19505 124.52

10433 113.11

Landing MLW 19051 123.95

10433 113.11

Zero Fuel MZFW 17917 113.24

10433 103.83

Note: A balance chart/trim sheet must be attached for check purposes as per AHM 519. State trim method (i.e. cabin area trim, cpt trim etc.)

Remarks:



AIRCRAFT DATA C Sheet 6A

A/C Type

DHC-8-300

Carrier

R3 5. EFFECT OF FUEL

(Tick as appropriate)

Remarks/Procedure Name

Standard Procedure

Non-standard Procedure

FUEL DENSITY: 0,8

Valid only for registration(s): VP-BNS

Fuel Weight Index

300 +0.25

600 +0.49

900 +0.74

1200 +0.98

1500 +1.23

1800 +1.48

2100 +1.72

2400 +1.97

2529* +2.07

Note:

*)Main tank – full(2529 kg)

**)Main+Long range tank – full(4561 kg)

Long Range fuel tank

Valid only for registration(s): VQ-BVI,

VQ-BVJ, VQ-BVH

Fuel Weight Index

2700 +2.21

3000 +2.46

3300 +2.71

3600 +2.95

3900 +3.20

4200 +3.44

4500 +3.69

4561** +3.74

Standard

Taxi Fuel Weight

Index

-100 -0,08



AIRCRAFT DATA C Sheet 6B

A/C Type

DHC-8-300

Carrier




Standard Procedure


FUEL DENSITY: 0,78


Fuel Weight Index

300 +0.25

600 +0.49

900 +0.74

1200 +0.98

1500 +1.23

1800 +1.48

2100 +1.72

2400 +1.97

2466* +2.02

Note:





VQ-BVJ, VQ-BVH

Fuel Weight Index

2700 +2.21

3000 +2.46

3300 +2.71

3600 +2.95

3900 +3.20

4200 +3.44

4447** +3.65

Standard

Taxi Fuel Weight

Index

-100 -0,08



AIRCRAFT DATA C Sheet 6C

A/C Type

DHC-8-300

Carrier




Standard Procedure


FUEL DENSITY: 0,82


Fuel Weight Index

300 +0.25

600 +0.49

900 +0.74

1200 +0.98

1500 +1.23

1800 +1.48

2100 +1.72

2400 +1.97

2592* +2.13

Note:





VQ-BVJ, VQ-BVH

Fuel Weight Index

2700 +2.21

3000 +2.46

3300 +2.71

3600 +2.95

3900 +3.20

4200 +3.44

4500 +3.69

4675** +3.83

Standard

Taxi Fuel Weight

Index

-100 -0,08




A/C Type

DHC-8-300

Carrier

R3 6. CREW

6.1 Number of cockpit crew seats and average location

Maximum number of cockpit seats

Length of arm from reference station

Index influence per weight unit

Captain & First Officer (2) - 321 - 0.0321

Observer (1) - 288 - 0.0288

Remarks: Pilots (Captain & First Officer) included in DOW

6.2 Number of cabin crew seats and location

Crew seats locations

Maximum No. of seats


Index influence per weight unit

FWD 1 - 244 - 0.0244

AFT 1 + 196 + 0.0196

(Rear fc. seat) 2 - 238 - 0.0238

Extra 2 + 163 + 0.0163

Remarks: Attendant (1) included in DOW

6.3 Crew Distribution/Crew Code

Crew Code

Cockpit Crew

Cabin Crew

Location* Location of Crew Baggage

2/2 2 1 FWD-1 Entry area Cabin

2/3 2 2 FWD-1 Entry area, AFT-1 Entry area Cabin

3/3 3 3 FWD-1 Entry area, AFT-1 Entry area, (Rear fc. seat)-1 Cabin

3/4 3 4 FWD-1 Entry area, AFT-1 Entry area, (Rear fc. seat)-2 Cabin

2/1 2 1 Configuration for Ferry flight, FWD-1 Entry area Cabin

3/1 3 1 Configuration for Ferry flight, FWD-1 Entry area Cabin

Remarks: Standart Crew 2/1 included in DOW Other Crew code DOW table in Attachment #2 Extra crew (Maintenance) – 2(1) located at Row 12 (A, C)




Configuration(s)

Y-50

A/C Type

DHC-8-300

Carrier

R3

7. GALLEY AND PANTRY

7.1 Galleys

Galley locations


Index influence

Length unit per weight unit

Galley G(AFT) + 212.7 + 0,0213

Remarks: 7.2 Pantry Weight/Pantry Code (normally used for above mentioned cabin configurations)

Pantry Code

Pantry Weight

Location *

“A” 62 kg G – 62 kg

“S” 47 kg G – 47 kg

“O” 33 kg G – 33 kg

Total

* Use the locations as under paragraph 7.1.

Remarks: Standard pantry weight code “A” with meal & equipment included in DOW

Code “A” used for full passenger capacity flight

Code “S” used for half passenger capacity flight

Code “O” used for ferry flights




Configuration(s)

Y-50

A/C Type

DHC-8-300

Carrier

R3 8. PASSENGER CABIN 8.1 Passenger Seats

Note: Fill in one table for each cabin configuration code.

Name of cabin section

Number of seats per cabin section Total per cabin section Class 1 Class 2 Class 3 Class 4 Class 5

OA 18 18

OB 16 16

OC 16 16

Total per class 50 50

Remarks:

8.2 Class/Cabin Sections

Class/Cabin Section Length of arm from reference station Index influence

length unit per weight unit

OA -153.55 -0.01536

OB -15.0 -0.00150

OC 114.50 0.01145




Configuration(s)

Y-50

A/C Type

DHC-8-300

Carrier

R3

8.3 Seating Layout

Show the passenger seating layout for the configurations given in the box at the top by inserting the seat row numbers and letters in the following table. For special seats use the description codes listed below.

B = Bassinet position P = Stretcher location

C = Crew seat Q = Quiet zone

E = Emergency exit S = Smoking

G = Groups T = Near toilet

H = Incapacitated passenger U = Unaccompanied minor

I = Infant preference rows/seats V = Seat left vacant/offered last

J = Rear facing seats W = No movie

K = Near galley X = No facility seat, e.g. no distinction

L = Leg space seat between smoking and non-smoking

M = Wheel chair Y = Not fitted

N = No smoking Z = Buffer zone

O = Over wing seat A = Aisle

Alpha /Characters —D, F, R, Blank, not used.


EDP-SYSTEM SEMI-PERMANENT DATA AIRCRAFT DATA

C Sheet 11A

Configuration(s)

Y-50

A/C Type

DHC-8-300

Carrier

R3 8.3.1 Seatplan Layout/Facilities and Row Index Influence

Class/ Cabin Section

Row

№.

Length of arm from reference

station

Index influence per weight unit +/-

. A C D F

OA

13 EJN EJN -238

- 0 0 2 3 8 0 1 ELN ELN ELN ELN -190 - 0 0 1 9 1 0 2 N N N N -158 - 0 0 1 5 9 0 3 N N N N -126 - 0 0 1 2 7 0 4 N N N N -95 - 0 0 0 9 5 0

OB

5 N N N N -63 - 0 0 0 6 3 0 6 N N N N -31 - 0 0 0 3 1 0 7 N N N N 1 0 0 0 0 1 0 8 N N N N 33 + 0 0 0 3 3 0

OC

9 N N N N 65 + 0 0 0 6 5 0 10 EN EN EN EN 99 + 0 0 0 9 9 0 11 N N N N 131 + 0 0 1 3 1 0 12 N N N N 163 + 0 0 1 6 3 0




Configuration(s)

Y-50

A/C Type

DHC-8-300

Carrier

R3 9. DETAILS FOR COMPARTMENT TRIM

Maximum Capacity

Compartment Number

Description Gross Weight Volume Length of arm from reference station

Index per kg x

* weight unit

CPT 1 AFT 793* 7.9***

238 0,023800

CPT 2 AFT 378** 286 0,028600

Security locker (DIP)

*** Volume information required for bulk compartments only in (cu/m).

Remarks: Maximum Allowable Weight of Cargo: 1) *TOTAL AFT (CPT1+2) – 923 kg (combined) 2) **Weapon box and Towbar is placed in CPT2 (details in section B3)

9.1 COMBINED LOAD LIMITS

Bay, CPT or Hold Bay, CPT or Hold Max combined weight

Remarks

CPT1 CPT2 923 kg

9.2 CUMULATIVE LOAD LIMITS Condition

Zone

Name From To

N/A

Note – Use +, -, or 0 to indicate forward, rearward or individual cumulative




Configuration(s)

Y-50

A/C Type

DHC-8-300

Carrier

R3 10. DETAILS FOR BAY/SECTION TRIM

Maximum Capacity

Bay/Section Gross Weight Volume * Length of arm from reference station

Index value per x* weight unit

1 793 7.9

238 + 0,023800

2 378 286 + 0,028600

Security Locker (DIP)

* Volume information required for bulk compartments only.

Note 1: Attach a plan for each compartment configuration.

Note 2: Use additional sheets as required.

10.1 LATERAL/ASYMMETRICAL LIMITATIONS

(Complete table or attach manufacturer’s formula)

Reference weight: TOW TAXI LDW

Lateral imbalance* Reference weight % MAC

N/A

* Define limitation




A/C Type

DHC-8-300

Carrier

R3 11. BALLAST

FIXED PROVISIONS FOR CARRYING BALLAST?

Yes No

If yes, specify below:

Location Weight Index

N/A

Remarks: The dry ballast is applied if necessary.

It is placed in compartments 1 or 2 under the additional order of the dispatcher of balance.



AIRCRAFT DATA D Sheet 1

A/C Type

DHC-8-300

Carrier

R3 1. CG — LIMITS 1.1 Ideal Trim Line at ZFW for Fuel Saving Purposes

Weight Index

10433 104.19

17917 107.2




A/C Type

DHC-8-300

Carrier

R3 2. UNIT LOAD DEVICES DETAILS

Maximum Capacity

Type Code Tare Weight Gross Weight Volume * Position or

height restriction Remarks

N/A

* Containers/Igloos only

Note: For pallets, specify height.

Indicated restriction means it cannot be loaded




A/C Type

DHC-8-300

Carrier

R3 3. SPECIAL LOAD

Attach relevant company regulations for special load (AVI, Dangerous Goods, etc.).

NOTE: Live animals to be loaded in hold 1

NOTE: Pets no more than 6 kg including cage (sides sum no more than 115 cm) are accepted in Cabin. Exceptions are seeing-eye dogs.


Attachment №1 SITATEX Addresses JSC ‘Air Company “Yakutia”

№ TYPE B LOCATION DISCRIPTION MAIL COMMENT

1 YKSFCR3 Yakutsk Operations Control Center

occ@ r3.aero

Vladislav Galushenko

2 YKSIDR3 Yakutsk Ground handling & Cargo Dept.

[email protected] Andei Illarionov

3 YKSSHR3 Yakutsk Schedule Dept. [email protected] Ivanka Klimiuk

4 YKSSDR3 Yakutsk Sale Dept. [email protected] Ludmila Kravchenko

MESSAGE ADDRESSES Attach a complete address list for all messages mentioned under paragraph 4 above.

LDM MVT PTM/BTM FTL PFS ETL PRL

YKSNPR3 YKSFCR3

YKSNPR3 YKSFCR3

QIFLPXS HDQRMR3

ATLXS1P YKSFCR3

For VKO transfer flights

VKOAPXH VKOAPXH

IATA E-CARGO MESSAGES

FFM FWB

[email protected], [email protected] or YKSNPR3

[email protected], [email protected] or YKSNPR3

Remark: Addresses of telegrams on a start are filled with signalmen, or airlines on each direction.

mailto:[email protected]




Attachment №2 VQ-BVI

CONDITION Weight,

Kg Arm, Inch

Moment, Kg-inch

B.I. %

MAC

CASE A 2 Pilots+1 C/As 12385 400 4951902 99,8 25,1

CASE B 2 Pilots+2 C/As 12460 401 4996602 101,2 26,5

CASE C 2 Pilots+3 C/As 12535 400 5008827 99,5 24,8

CASE E 2 Pilots+1 Observer+1 C/As 12470 398 4961422 97,3 22,8

CASE F 2 Pilots+1 Observer+2 C/As 12545 399 5006122 98,8 24,2

CASE G 2 Pilots+1 Observer+3 C/As 12620 398 5018347 97,0 22,5

CASE I 2 Pilots+4 C/As 12610 398 5021052 97,7 23,2

CASE J 2 Pilots+1 Observer+4 C/As 12695 396 5030572 95,2 20,9

CONDITION Weight,

Kg Arm, Inch

Moment, Kg-inch

B.I. %

MAC

CASE A1 2 Pilots+1 C/As+1Extra 12460 401 4994127 101,0 26,2

CASE B1 2 Pilots+2 C/As+1Extra 12535 402 5038827 102,5 27,6

CASE C1 2 Pilots+3 C/As+1Extra 12610 401 5051052 100,7 25,9

CASE E1 2 Pilots+1 Observer+1 C/As+1Extra 12545 399 5003647 98,6 23,9

CASE F1 2 Pilots+1 Observer+2 C/As+1Extra 12620 400 5048347 100,0 25,3

CASE G1 2 Pilots+1 Observer+3 C/As+1Extra 12695 399 5060572 98,2 23,7

CASE I1 2 Pilots+4 C/As+1Extra 12685 399 5063277 98,9 24,3

CASE J1 2 Pilots+1 Observer+4 C/As+1Extra 12770 397 5072797 96,5 22,1

CONDITION Weight,

Kg Arm, Inch

Moment, Kg-inch

B.I. %

MAC









VQ-BVJ

CONDITION Weight,

Kg Arm, Inch

Moment, Kg-inch

B.I. %

MAC

CASE A 2 Pilots+1 C/As 12478 400 4996338 100,5 25,8

CASE B 2 Pilots+2 C/As 12553 402 5041038 102,0 27,1

CASE C 2 Pilots+3 C/As 12628 400 5053263 100,2 25,5




CASE I 2 Pilots+4 C/As 12703 399 5065488 98,4 23,9


CONDITION Weight,

Kg Arm, Inch

Moment, Kg-inch

B.I. %

MAC









CONDITION Weight,

Kg Arm, Inch

Moment, Kg-inch

B.I. %

MAC









VQ-BVH

CONDITION Weight,

Kg Arm, Inch

Moment, Kg-inch

B.I. %

MAC

CASE A 2 Pilots+1 C/As 12698 398 5059433 98,0 23,5

CASE B 2 Pilots+2 C/As 12773 400 5104133 99,5 24,8

CASE C 2 Pilots+3 C/As 12848 398 5116358 97,7 23,2




CASE I 2 Pilots+4 C/As 12923 397 5128583 95,9 21,6


CONDITION Weight,

Kg Arm, Inch

Moment, Kg-inch

B.I. %

MAC









CONDITION Weight,

Kg Arm, Inch

Moment, Kg-inch

B.I. %

MAC









VP-BNS

CONDITION Weight,

Kg Arm, Inch

Moment, Kg-inch

B.I. %

MAC

CASE A 2 Pilots+1 C/As 12581 404 5083941 105,2 30,1

CASE B 2 Pilots+2 C/As 12656 405 5128641 106,6 31,4

CASE C 2 Pilots+3 C/As 12731 404 5140866 104,9 29,8




CASE I 2 Pilots+4 C/As 12806 402 5153091 103,1 28,1


CONDITION Weight,

Kg Arm, Inch

Moment, Kg-inch

B.I. %

MAC









CONDITION Weight,

Kg Arm, Inch

Moment, Kg-inch

B.I. %

MAC









Applicable for VQ-BVH, VQ-BVI, VQ-BVJ and VP-BNS

VQ-BVH VQ-BVI VQ-BVJ VP-BNS

Carrier 1. SUPPLIERS’ CONTACT ADDRESSahm.yakutia.aero/docs/Dash8/AHM560 All fleet...

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Transcript of Carrier 1. SUPPLIERS’ CONTACT ADDRESSahm.yakutia.aero/docs/Dash8/AHM560 All fleet...