Weight / Balance & Equipment List Revision Page # :1

DLK Aviation, Inc. - DK7R795J 2601 Cessna Lane Kennesaw GA 30144

WB ID # : 122 A/C Tail # : N207CL

Register Name : WRONG BROS CO Address : 37 MUSCOGEE AVENUE

City, State, PC : ATLANTA, GA 30305

770/427-4954 A/C Make : PIPER A/C Model : PA32R-300

A/C Serial # : 32R-770480

WO Ref # : 4495 WB Date : Sep-22-2004

This Aircraft has been re-weighed using the following computations. Reaction

Points Scale

Reading Tare Net Wei ht ht Arm / CG Moment

Right Main 801.00 0.00 801.00 Left Main 810.00 0.00 810.00

Sub Total Main 1611.00 109.80 176887.80

Nose / Tail 598.00 0.00 598.00 14.30 8551.40

Total as Weighed 2209.00 83.95 185439.20

Engine Oil

Un -useable Fuel 2: 00 93.60 2246.40

Other 1

Other 2

Other 3 -

Basic Empty Empty Weight 2233.00 1 84.05 187685.60

.RCRAFT GROSS WEIGHT = 3600.00 NEW USEFUL LOAD (computed) = 1367.00

Model / Part # Description of changes ( LB / IN) Weight CG/Arm Moment

Basic Empty Weight (from weighing) ->>> 2233.00 84.05 187685.60

NO ITEMS REMOVED

NO ITEMS INSTALLED

NEW DATA » NEW USEFUL LOAD = 1367.00 2233.00 84.05 187685.60

AIRCRAFT WEIGHTED EMPTY OF FUEL

SCALES CLBRATED 01-06-2004

Authorized Individual : 2•CR7' J FOR DLK AVIATION, INC.

SECTION 6

PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE

PA-32R-300, CHEROKEE LANCE

Weight (Lbs)

Arm Aft Datum

(Inches) Moment (In-Lbs)

c. Basic Empty Weight 2 1 33,012 811,e5- 187G85i6pc

Pilot and Front Passenger 85.5

Passengers (Center Seats) (Forward Facing) 118.1

Passengers (Center Seats) (Aft Facing) (Optional) 119.1

Passengers (Rear Seats) 157.6

Passenger (Jump Seat) (Optional) 118.1

Fuel (94 Gallon Maximum) 93.6

Baggage (Forward) 42.0

Baggage (Aft) 178.7

Moment due to Retraction of Landing Gear 819

Total Loaded Airplane

Totals must be within approved weight and C.G. limits. It is the responsibility of the airplane owner and the pilot to insure that the airplane is loaded properly. The Basic Empty Weight C.G. is noted on the Weight and Balance Data Form (Figure 6- 5 ). If the airplane has been altered, refer to the Weight and Balance Record for this information.

WEIGHT AND BALANCE LOADING FORM

Figure 6-11

REPORT: VB-840 ISSUED: AUGUST 20,1976 6-1 2

SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-32R-300, CHEROKEE LANCE

- T

1

3600

3400

3000

WE

IGH

T IN

POU

ND

S

2600

2200

1800

1400

76 78 SU 82 84 86 88 90 92 94 96

INCHES AFT OF DATUM

Moment due to retracting landing gear = +819 in. lbs.

C. G. RANGE AND WEIGHT

Figure 6-15

REPORT: VB-840 ISSUED: AUGUST 20, 1976 6-14

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PIPER AIRCRAFT CORPORATION PA-32R-300, CHEROKEE LANCE SECTION 6

WEIGHT AND BALANCE

600

550

500

450

400

350

300

250

200

150

100

50

5 10 15 20 25 30 35 40 45 50 55 60

MOMENT:1000 (POUNDS-INCHES)

LOADLNG GRAPH

Figure 6-13

ISSUED: AUGUST 20, 1976 REPORT: VB-840 6-13