PLATE NO.
15: AIRCRAFT ORTHOGRAPHIC
NAME: FRANCO, FRANCEZKA NOELLE P.
DRAWING AND SPECIFICATIONS
DATE: JUNE 29, 2022 PAGE: 1 OF 13
INSTRUCTOR: ENGR. JAYSON U. BAGA
GRADE: ISSUE NO: 1
Aircraft 1
Krunichev T-411
A. Weight (lbs, kg)
A.1 Gross Weight 1100 lbs (498, 95 kg)
A.2 Useful Loads
Pilot 170 lbs (77.11 kg)
Passenger/s 170 lbs (77.11 kg)
Baggage 78.25 lbs (35.49 kg)
Fuel Load 105.67 lbs (47.93 kg)
Oil Load 4.4 lbs (2 kg)
Total (A.2) 528.32 lbs (239.1 kg)
A.3 Empty Weight 544 kg (1,200 lb)
B. Dimension, Externa (Ft, m)
B.1 Wing Span 42 ft 8 ½ in (13.02 m)
B.2 Wing Chord at Root (CR) 3 ft 3 in (0.99 m)
B.3 Wing Chord at Tip (CT) 3 ft 3 in (0.99 m)
B.4 Wing Aspect Ratio 7.0
B.5 Length, Overall 31 ft 0 in (9.45 m)
B.6 Height Overall 8 ft 6 ¼ in (2.60 m)
B.7 Tail Plane Span 7 ft 9 in (2.35 in)
B.8 Wheel Track 8 ft 6 in (2.59 m)
B.9 Wheel Base 21 ft 4 in (6.50 m)
B.10 Propeller Diameter 6 ft 8 in (2.03 m)
B.11 Propeller Ground Clearance 1 ft (0.3 m)
B.12 Cabin Door, Height 2 ft 5 in (0.737 in)
Width 3 ft 3 in (0.92 m)
B.13 Wing Dihedral Angle 2o
B.14 Wing Swept-back Angle 0o
B.15 Tire Diameter, Main Gear 0.5 ft (0.15 m)
Nose Gear 0.43 ft (0.13 m)
B.16 Pontoon Float, or Similar
Devices
Length N/A
Height N/A
PLATE NO. 15: AIRCRAFT ORTHOGRAPHIC
NAME: FRANCO, FRANCEZKA NOELLE P.
DRAWING AND SPECIFICATIONS
DATE: JUNE 29, 2022 PAGE: 1 OF 13
INSTRUCTOR: ENGR. JAYSON U. BAGA
GRADE: ISSUE NO: 1
C. Areas (ft2, m2)
C.1 Wing (gross) 261.6 ft2 (24.30 m2)
C.2 Aileron (Total) 4.3 ft2 (0.4 m2)
C.3 Flaps (Total) 9.75 ft2 (0.91 m2)
C.4 Fin (Gross) 7.78 ft2 (0.72 m2)
C.5 Rudder 1.96 ft2 (0.18 m2)
C.6 Horizontal Stabilizer 13.03 ft2 (1.21 m2)
C.7 Elevator 8.01 ft2 (0.74 m2)
C.8 Fuselage (frontal) 9.92 ft2 (0.92 m2)
D. Loadings (appropriate units)
D.1 Wing Loading 69.1 kg/m2 (14.16 sq. ft)
D.2 Power Loading 6.27 kg/kW (10.30 lb/hp)
E. Engine (appropriate units)
E.1 Type and Model Vedeneyev M14P
E.2 Rated Maximum Horsepower 359 hp
E.3 Rated Maximum RPM 2,900 rpm
E.4 Fuel Consumption 13 l/hr
E.5 Fuel Type AV Gas 100/130
E.6 Number of Cylinder 9
E.7 Engine Dry Weight 139 lbs (63.15 kg)
F. Performance (appropriate
units)
F.1 Top Speed 138.09 mph (120 KCAS)
F.2 Cruising Speed 127 mph (110.36 KIAS)
F.3 Stalling Speed 70 mph (60.83 KCAS)
F.4 Maximum Rate of Climb at Sea 1.457 ft/min
Level
F.5 Service Ceiling 9,840 ft (3,000 m)
F.6 Absolute Ceiling 125,000 ft (3810 m)
F.7 Take-off Run 279 ft (85 m)
F.8 Landing Run 446 ft (136 m)
F.9 Range 648 nm
F.10 Endurance 3.7 hrs
PLATE NO. 15: AIRCRAFT ORTHOGRAPHIC
NAME: FRANCO, FRANCEZKA NOELLE P.
DRAWING AND SPECIFICATIONS
DATE: JUNE 29, 2022 PAGE: 1 OF 13
INSTRUCTOR: ENGR. JAYSON U. BAGA
GRADE: ISSUE NO: 1
Aircraft 2
Smolensk (Technoavia) SM-2000
A. Weight (lbs, kg)
A.1 Gross Weight 1100 lbs (498, 95 kg)
A.2 Useful Loads
Pilot 170 lbs (77.11 kg)
Passenger/s 170 lbs (77.11 kg)
Baggage 78.25 lbs (35.49 kg)
Fuel Load 105.67 lbs (47.93 kg)
Oil Load 4.4 lbs (2 kg)
Total (A.2) 528.32 lbs (239.1 kg)
A.3 Empty Weight 1,350 kg (2,976 lb)
B. Dimension, Externa (Ft, m)
B.1 Wing Span 38 ft 11 ¾ in (11.88 m)
B.2 Wing Chord at Root (CR) 3 ft 3 in (0.99 m)
B.3 Wing Chord at Tip (CT) 3 ft 3 in (0.99 m)
B.4 Wing Aspect Ratio 7.0
B.5 Length, Overall 30 ft 11 ½ in (9.435 m)
B.6 Height Overall 11 ft 2 ½ in (3.41 m)
B.7 Tail Plane Span 7 ft 9 in (2.35 in)
B.8 Wheel Track 10 ft 2 ¼ in (3.12 m)
B.9 Wheel Base 6 ft 4 ¼ in (1.95 m)
B.10 Propeller Diameter 8 ft 2 ½ in (2.50 m)
B.11 Propeller Ground Clearance 1 ft (0.3 m)
B.12 Cabin Door, Height 2 ft 11 ½ in (0.90 m)
Width 2 ft 11 ¼ in (1.20 m)
B.13 Wing Dihedral Angle 2o
B.14 Wing Swept-back Angle 0o
B.15 Tire Diameter, Main Gear 1 ft 4 in (0.4 m)
Nose Gear 11 in (0.28 in)
B.16 Pontoon Float, or Similar
Devices
Length N/A
Height N/A
PLATE NO. 15: AIRCRAFT ORTHOGRAPHIC
NAME: FRANCO, FRANCEZKA NOELLE P.
DRAWING AND SPECIFICATIONS
DATE: JUNE 29, 2022 PAGE: 1 OF 13
INSTRUCTOR: ENGR. JAYSON U. BAGA
GRADE: ISSUE NO: 1
C. Areas (ft2, m2)
C.1 Wing (gross) 261.6 ft2 (24.30 m2)
C.2 Aileron (Total) 4.3 ft2 (0.4 m2)
C.3 Flaps (Total) 9.75 ft2 (0.91 m2)
C.4 Fin (Gross) 7.78 ft2 (0.72 m2)
C.5 Rudder 1.96 ft2 (0.18 m2)
C.6 Horizontal Stabilizer 13.03 ft2 (1.21 m2)
C.7 Elevator 8.01 ft2 (0.74 m2)
C.8 Fuselage (frontal) 9.92 ft2 (0.92 m2)
D. Loadings (appropriate units)
D.1 Wing Loading 69.1 kg/m2 (14.16 sq. ft)
D.2 Power Loading 3.75 kg/kW (6.16 lb/shp)
E. Engine (appropriate units)
E.1 Type and Model Avia V-508E
E.2 Rated Maximum Horsepower 355 hp
E.3 Rated Maximum RPM 2,900 rpm
E.4 Fuel Consumption 13 l/hr
E.5 Fuel Type AV Gas 100/130
E.6 Number of Cylinder 7
E.7 Engine Dry Weight 139 lbs (63.15 kg)
F. Performance (appropriate
units)
F.1 Top Speed 138.09 mph (120 KCAS)
F.2 Cruising Speed 149 mph (129.477 KIAS)
F.3 Stalling Speed 72 mph (65.57 KCAS)
F.4 Maximum Rate of Climb at Sea 1,500 ft/min
Level
F.5 Service Ceiling 9,840 ft (3,000 m)
F.6 Absolute Ceiling 125,000 ft (3810 m)
F.7 Take-off Run 820 ft (250 m)
F.8 Landing Run 920 ft (280 m)
F.9 Range 324 nm
F.10 Endurance 3.7 hrs
PLATE NO. 15: AIRCRAFT ORTHOGRAPHIC
NAME: FRANCO, FRANCEZKA NOELLE P.
DRAWING AND SPECIFICATIONS
DATE: JUNE 29, 2022 PAGE: 1 OF 13
INSTRUCTOR: ENGR. JAYSON U. BAGA
GRADE: ISSUE NO: 1
Aircraft 3
Murphy JDM-8
A. Weight (lbs, kg)
A.1 Gross Weight 1100 lbs (498, 95 kg)
A.2 Useful Loads
Pilot 170 lbs (77.11 kg)
Passenger/s 170 lbs (77.11 kg)
Baggage 78.25 lbs (35.49 kg)
Fuel Load 105.67 lbs (47.93 kg)
Oil Load 4.4 lbs (2 kg)
Total (A.2) 528.32 lbs (239.1 kg)
A.3 Empty Weight 125-159 kg (275-350 lb)
B. Dimension, Externa (Ft, m)
B.1 Wing Span 20 ft 0 in (6.10 m)
B.2 Wing Chord at Root (CR) 3 ft 3 in (0.99 m)
B.3 Wing Chord at Tip (CT) 3 ft 3 in (0.99 m)
B.4 Wing Aspect Ratio 7.0
B.5 Length, Overall 30 ft 11 ½ in (9.435 m)
B.6 Height Overall 3 ft 11 in (1.19 m)
B.7 Tail Plane Span 7 ft 9 in (2.35 in)
B.8 Wheel Track 10 ft 2 ¼ in (3.12 m)
B.9 Wheel Base 6 ft 4 ¼ in (1.95 m)
B.10 Propeller Diameter 8 ft 2 ½ in (2.50 m)
B.11 Propeller Ground Clearance 1 ft (0.3 m)
B.12 Cabin Door, Height 2 ft 11 ½ in (0.90 m)
Width 2 ft 11 ¼ in (1.20 m)
B.13 Wing Dihedral Angle 2o
B.14 Wing Swept-back Angle 0o
B.15 Tire Diameter, Main Gear 1 ft 4 in (0.4 m)
Nose Gear 11 in (0.28 in)
B.16 Pontoon Float, or Similar
Devices
Length N/A
Height N/A
C. Areas (ft2, m2)
PLATE NO. 15: AIRCRAFT ORTHOGRAPHIC
NAME: FRANCO, FRANCEZKA NOELLE P.
DRAWING AND SPECIFICATIONS
DATE: JUNE 29, 2022 PAGE: 1 OF 13
INSTRUCTOR: ENGR. JAYSON U. BAGA
GRADE: ISSUE NO: 1
C.1 Wing (gross) 120 ft2 (11.13 m2)
C.2 Aileron (Total) 4.3 ft2 (0.4 m2)
C.3 Flaps (Total) 9.75 ft2 (0.91 m2)
C.4 Fin (Gross) 7.78 ft2 (0.72 m2)
C.5 Rudder 1.96 ft2 (0.18 m2)
C.6 Horizontal Stabilizer 13.03 ft2 (1.21 m2)
C.7 Elevator 8.01 ft2 (0.74 m2)
C.8 Fuselage (frontal) 9.92 ft2 (0.92 m2)
D. Loadings (appropriate units)
D.1 Wing Loading 69.1 kg/m2 (14.16 sq. ft)
D.2 Power Loading 3.75 kg/kW (6.16 lb/shp)
E. Engine (appropriate units)
E.1 Type and Model Rotax 277
E.2 Rated Maximum Horsepower 80 hp
E.3 Rated Maximum RPM 2,900 rpm
E.4 Fuel Consumption 13 l/hr
E.5 Fuel Type AV Gas 100/130
E.6 Number of Cylinder 1
E.7 Engine Dry Weight 139 lbs (63.15 kg)
F. Performance (appropriate
units)
F.1 Top Speed 138.09 mph (120 KCAS)
F.2 Cruising Speed 55 mph (47.794 KIAS)
F.3 Stalling Speed 30 mph (26.069 KCAS)
F.4 Maximum Rate of Climb at Sea 800 ft/min
Level
F.5 Service Ceiling 9,840 ft (3,000 m)
F.6 Absolute Ceiling 125,000 ft (3810 m)
F.7 Take-off Run 150 ft (46 m)
F.8 Landing Run 150 ft (46 m)
F.9 Range 324 nm
F.10 Endurance 3.7 hrs
PLATE NO. 15: AIRCRAFT ORTHOGRAPHIC
NAME: FRANCO, FRANCEZKA NOELLE P.
DRAWING AND SPECIFICATIONS
DATE: JUNE 29, 2022 PAGE: 1 OF 13
INSTRUCTOR: ENGR. JAYSON U. BAGA
GRADE: ISSUE NO: 1
Aircraft 4
Technochev JDM-2411
A. Weight (lbs, kg)
A.1 Gross Weight 1100 lbs (498, 95 kg)
A.2 Useful Loads
Pilot 170 lbs (77.11 kg)
Passenger/s 170 lbs (77.11 kg)
Baggage 78.25 lbs (35.49 kg)
Fuel Load 105.67 lbs (47.93 kg)
Oil Load 4.4 lbs (2 kg)
Total (A.2) 528.32 lbs (239.1 kg)
A.3 Empty Weight 125-159 kg (275-350 lb)
B. Dimension, Externa (Ft, m)
B.1 Wing Span 38 ft 11 ¾ in (11.88 m)
B.2 Wing Chord at Root (CR) 3 ft 3 in (0.99 m)
B.3 Wing Chord at Tip (CT) 3 ft 3 in (0.99 m)
B.4 Wing Aspect Ratio 7.0
B.5 Length, Overall 19 ft 3 in (5.87 m)
B.6 Height Overall 8 ft 6 ¼ in (2.60 m)
B.7 Tail Plane Span 7 ft 9 in (2.35 in)
B.8 Wheel Track 10 ft 2 ¼ in (3.12 m)
B.9 Wheel Base 6 ft 4 ¼ in (1.95 m)
B.10 Propeller Diameter 8 ft 2 ½ in (2.50 m)
B.11 Propeller Ground Clearance 1 ft (0.3 m)
B.12 Cabin Door, Height 2 ft 11 ½ in (0.90 m)
Width 2 ft 11 ¼ in (1.20 m)
B.13 Wing Dihedral Angle 2o
B.14 Wing Swept-back Angle 0o
B.15 Tire Diameter, Main Gear 1 ft 4 in (0.4 m)
Nose Gear 11 in (0.28 in)
B.16 Pontoon Float, or Similar
Devices
Length N/A
Height N/A
PLATE NO. 15: AIRCRAFT ORTHOGRAPHIC
NAME: FRANCO, FRANCEZKA NOELLE P.
DRAWING AND SPECIFICATIONS
DATE: JUNE 29, 2022 PAGE: 1 OF 13
INSTRUCTOR: ENGR. JAYSON U. BAGA
GRADE: ISSUE NO: 1
C. Areas (ft2, m2)
C.1 Wing (gross) 120 ft2 (11.13 m2)
C.2 Aileron (Total) 4.3 ft2 (0.4 m2)
C.3 Flaps (Total) 9.75 ft2 (0.91 m2)
C.4 Fin (Gross) 7.78 ft2 (0.72 m2)
C.5 Rudder 1.96 ft2 (0.18 m2)
C.6 Horizontal Stabilizer 13.03 ft2 (1.21 m2)
C.7 Elevator 8.01 ft2 (0.74 m2)
C.8 Fuselage (frontal) 9.92 ft2 (0.92 m2)
D. Loadings (appropriate units)
D.1 Wing Loading 69.1 kg/m2 (14.16 sq. ft)
D.2 Power Loading 3.75 kg/kW (6.16 lb/shp)
E. Engine (appropriate units)
E.1 Type and Model Rotax 277
E.2 Rated Maximum Horsepower 80 hp
E.3 Rated Maximum RPM 2,900 rpm
E.4 Fuel Consumption 13 l/hr
E.5 Fuel Type AV Gas 100/130
E.6 Number of Cylinder
E.7 Engine Dry Weight 139 lbs (63.15 kg)
F. Performance (appropriate
units)
F.1 Top Speed 138.09 mph (120 KCAS)
F.2 Cruising Speed 55 mph (47.794 KIAS)
F.3 Stalling Speed 30 mph (26.069 KCAS)
F.4 Maximum Rate of Climb at Sea 800 ft/min
Level
F.5 Service Ceiling 9,840 ft (3,000 m)
F.6 Absolute Ceiling 125,000 ft (3810 m)
F.7 Take-off Run 150 ft (46 m)
F.8 Landing Run 150 ft (46 m)
F.9 Range 324 nm
F.10 Endurance 3.7 hrs
