înters winters aviation bvba aviation bcaa organisation

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înters Aviation =^=^^^ ^^^^=^^^= ^==^= \< = WINTERS AVIATION bvba BCAA ORGANISATION APPROVAL REF.: V.A. 94/16 ANTWERP AIRPORT LUCHTHAVENLEI 1 BUS 48 - 2100 DEURNE / ANTWERP (BELGIUM) TEL: +32 3 281 74 74 FAX: +32 3 281 72 13 WEIGHT AND BALANCE REPORT; REPORT N°: 2008/22 bis COMPLETED AT: EBAW OO-JET DATE: september 5, 2008 AIRCRAFTTYPE: Piper PA-28-161 PASSENGERS: _4_ (pilot inc.) COLOR: White & Red witn grey striping AIRCRAFTS/N: 2842282 LAST WEIGHED: PLACE & DATE OF CONSTRUCTION: Vero Beach, FL (United States) / January 12, 2007 NAfaE: WINTERS P. FUNCTION: INSPECTOR SIGNATURE; 1. EOUIPMENT DESCRIPTION MAKE: REVERE TYPE: A/S 37M-1 2. REFERENCE CALIBRATED: | April Ist, 2006 DATASHEETN 0 : REFERENCE LINE: LEVELING MEANS: 2A13 (Rev. 48 dated: August 7, 2006) 78,4" fwd of inbd intersection of straight & tappered sections two screws left side fuselage below window 3. EOUIPMENT A. INSTRUMENTS PFD Avidyne MFD Altimeter (back-up) AED [CED Attitude jndic. (back-up) Airspeed (back-up) magnetic compass •FADEC warning panel PAGE 1 Or 2 PAGES.

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întersAviation

=^=^^^ ^^^^=^^^= ^==^= \< =

WINTERS AVIATION bvbaBCAA ORGANISATION APPROVAL REF.: V.A. 94/16

ANTWERP AIRPORTLUCHTHAVENLEI 1 BUS 48 - 2100 DEURNE / ANTWERP (BELGIUM)TEL: +32 3 281 74 74 FAX: +32 3 281 72 13

WEIGHT AND BALANCE REPORT;

REPORT N°: 2008/22 bis

COMPLETED AT: EBAW

OO-JET

DATE: september 5, 2008

AIRCRAFTTYPE: Piper PA-28-161

PASSENGERS: _4_ (pilot inc.)

COLOR: White & Red witn grey striping

AIRCRAFTS/N: 2842282

LAST WEIGHED:

PLACE & DATE OF CONSTRUCTION: Vero Beach, FL (United States) / January 12, 2007

NAfaE: WINTERS P. FUNCTION: INSPECTOR

SIGNATURE;

1. EOUIPMENT DESCRIPTION

MAKE: REVERE

TYPE: A/S 37M-1

2. REFERENCE

CALIBRATED: | April Ist, 2006

DATASHEETN0 :REFERENCE LINE:LEVELING MEANS:

2A13 (Rev. 48 dated: August 7, 2006)78,4" fwd of inbd intersection of straight & tappered sectionstwo screws left side fuselage below window

3. EOUIPMENT

A. INSTRUMENTS

PFDAvidyne MFDAltimeter (back-up)

AED[CED

Attitude jndic. (back-up)Airspeed (back-up)magnetic compass

•FADEC warning panel

PAGE 1 Or 2 PAGES.

PAGE 2 OT2 PAGES.

SECTION 6WEIGHT AND BALANCE PA-28-161, WARRIOR III

Basic Empty Wcight

Pi lot and Front Passenger

Passcngers (Rear Scats)*

Fuel (48 Gallon Maximum)

Baggage* (200 Lbs. Maximum)

Ramp Wcight (2447 Lbs. Normal,2027 Lbs. Utility Maximum)

Fuel AllowanceFor Engine Start, Taxi and Run Up

Takeoff Weight (2440 Lbs. Normal,2020 Lbs. Utility Maximum)

Wcight(Lbs)

-7

Arm AftDatum

(Inches)

80.5

118.1

95.0

142.8

95.0

Moment(In-Lbs)

-665

Totals must bc wi th in approvcd weight and C.G. l imits. It is thé responsi-bility of thc airplane owner and thc pi lot to insure that thé airplane is loadedproperly. Thc Basic Empty Weight C.G. is noted on thé Weight and BalanceData Form (Figure 6-5). If thé airplane has been altcred, refer to thé Weightand Balance Record for this information.

*Utilily Category Opération - No baggage or alï passengers allowcd.

WEIGHT AND BALANCE LOADING FORMFigure 6-11

REPORT: VB-16106-12

ISSUED: JULY 12,1995

PA-28-161, WARRIOR IIISECTION 6

WEIGHT AND BALANCE

V)DZD

2

û

100

10 15 20 25 3O

MOMENT/1000 (POUNDS INCHES)

LOADING GRAPHFigure 6-13

ISSUED: JULY 12,1995 REPORT: VB-16106-13