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1

Saturday, May 23rd 2009, 3:32am

Fuerza Aérea de Chile - Fighters

Types Operated:
- Accrisius F-12 "Aves" (1936) 202 planes (42 lost during Peruvian War)
- Spartan F-9 "Storm" (1934) - 144 planes remain in service as of 1938
- Spartan SP-34 "Cutlass" (1936) 64 planes
- FMA / ENAER I-01-IIB Buchon (1938) 106 planes delivered by Dec 1938, 38 on order for 1939
- FMA / ENAER I-02 Pulqui (1939) 108 planes ordered for 1939-1940.

2

Thursday, May 28th 2009, 7:57pm

Accrisius F-12 "Aves"

F1A Aves / Accrisius F-12 Aves
General characteristics
Wingspan: 39 ft (11.8 m)
Length: 31 ft, 6in (9.2 m)
Height: 10 ft (3.05 m)
Empty weight: 6,211 lbs
Loaded weight: 7,500 lbs
Engine: Spartan V-1300S V-12
Crew: 1
Armour: 8mm thick armoured bulkhead

Performance
Max. speed: 329 mph
Range: 641 nm (738 miles)
Service ceiling: 28,000 ft
Rate of climb: 1,617 fpm

Armament
- 6 × 12.7 mm in wings

3

Thursday, May 28th 2009, 7:58pm

Spartan F-9 "Storm"


Picture by James, aka "Hood"

F2S Storm / Spartan F-9 "Storm"
General characteristics
Length: 25 feet
Wingspan: 36 ft
Height:
Wing area: 192 sq ft
Weight: 4,150 lbs (maximum)
Crew: 1 (pilot)
Powerplant: 1xSpartan 700 (900hp)

Performance:
Speed: 301mph
Rate of climb: 3,091 ft/min
Ceiling: 25,000 feet
Range: 184 nm (212 miles)
Remarks:

4

Thursday, May 28th 2009, 7:59pm

Spartan SP-34 "Cutlass"

F3S Cutlass / Spartan SP-34 "Cutlass"
General characteristics:
Length: 46.5 ft
Wingspan: 72 ft
Height:
Wing area: 718 ft²
Weight: 16,721 lbs (empty), 22,000 lbs (loaded)
Crew: 2
Powerplant: 2x Ripon R-1200-012A (1,200hp at 15,000 ft)

Performance:
Speed: 305 mph
Rate of climb: 1,255 fpm
Ceiling: 24,500 ft
Range: 1,099 miles
Remarks:

Armament:
- 2x20mm cannon
- 3x 13mm HMG
- 2x 500lb underwing bombs

5

Sunday, November 22nd 2009, 4:08am

FMA/ENAER I-01-IIB Buchon


Drawing by somebody, via Hood, modified (roundels) by me.

F1F-2 Buchon / FMA I-01-IIB
F1E Buchon / ENAER I-01-IIB

Developed from the standard I-01-II this improved variant is for the dive-bomber/ fighter requirement with bomb-racks and dive-brakes. The version built by ENAER lacks the ventral armour originally proposed to the FMA. The FACH has ordered 144 I-01-IIBs for delivery across 1938 and 1939. I-01-IIBs are replacing Spartan F-9 Storms, which are being surplused out of the Air Force (many being sold or given to aviation clubs) or assigned to training roles.

Dimensions: span 10.05m; length 9.14; height 3.22m; wing area 176sq ft; wing loading 41 lb/sq ft; power loading 0.17 lb/hp
Structure: all-metal monocoque fuselage with I section fames and L section stringers with stressed light alloy covering, light alloy used for cantilever tail construction and tailplane covering. Cantilever metal wing with two steel spars, all-metal split flaps and aluminium framed ailerons with aluminium covering with two hydraulic dive-brakes. Rudder and elevators aluminium framed with aluminium covering. Retractable hydraulically raised main undercarriage with single oleo-pneumatic legs with twin pneumatic brakes and a retractable castoring tail wheel
Weights: empty 5,802lbs, maximum take-off 7,250lbs
Powerplant: one 1300hp Spartan 1300S V-12 inline engine with supercharger, maximum sea level output to 12,000ft
Performance: max speed 374mph at 15,000ft; service ceiling 21,500ft; rate of climb 2,325ft per minute at 1,500ft; range 311 miles full fuel load
Capacity: pilot in enclosed cockpit
Armament: four 13mm Browning HMG in wings and ventral bomb rack for one 250kg bomb and wing racks for either four 50kg or ten 15kg bombs
Equipment: full controls and navigation equipment including receiver/transmitter, reflector sight, Sperry autopilot and one flare chute

6

Sunday, November 22nd 2009, 4:13am

Fma / ENAER I-02

Future Project - FMA/ENAER I-02


[SIZE=1]Image by BadersBusCompany and Hood, with colors by me.[/SIZE]

F2F Pulqui / FMA I-02 Pulqui
F2E Pulqui / ENAER I-02 Pulqui
General characteristics:
Length: 10.3m (33.8 ft)
Wingspan: 10.6m (34.8 ft)
Height: 3.42m (11.2 ft)
Wing area: 197 ft²
Weight: 5,882 lbs (empty), 7,500 lbs (max takeoff)
Crew: 1
Powerplant: 1x 1300hp Spartan 1300S V-12 inline engine with supercharger, maximum sea level output to 15,000ft

Performance:
Speed: 414mph at 15,000 feet
Rate of climb: 2,598 feet per minute at 1,500ft
Ceiling: 35,000 feet
Range: 691 miles
Remarks: Pilot in enclosed cockpit armoured windscreen and 8mm thick armoured bulkhead behind

Armament:
- 4x 13mm MG
- 250-500lbs bomb

Order History:
- 108 planes delivered

7

Thursday, January 20th 2011, 5:32pm

F3E Caracara

ENAER F3E-1 Caracara Heavy Fighter
(licensed Petlyakov Pe-3bis with Spartan inlines)

General characteristics:
Crew: 2
Length: 13.5 m (44 ft 3 in)
Wingspan: 17.13 m (56 ft 2 in)
Height: 3.5 m (11 ft 6 in)
Wing area: 40.5 m2 (436 sq ft)
Empty weight: 6100 kg (13,450 lb)
Gross weight: 8,255 kg (18,200 lb)
Powerplant: 2 × FMA-Spartan 12V-1500S-SS V12 engines, 1,119 kW (1,500 hp) each
Propellers: 3-bladed

Performance:
Maximum speed: 603.5 km/h (375 mph; 325.9 kn) @ 5,050 metres (16,600 ft)
Range: 1,609 km (932 mi; 869 nmi)
Service ceiling: 9,500 m (31,168 ft)
Time to altitude: 6 minutes to 5,000 metres (16,000 ft)

Armament:
Guns:
- 2 × 20-mm cannon in the nose
- 2 × 13-mm machine guns in the nose
- 1 × 13-mm machine gun in dorsal position
- Bombs: up to 700 kg (1,543 lb)

Order History:
- 4 preproduction aircraft ordered and built 1939
- 54 production F3E-1 Caracaras ordered January 1940; delivered.

8

Monday, January 23rd 2012, 4:45pm

Chance-Vought F4U-4 / ENAER F4E-3



Vought F4U-4 Corsair / ENAER F4E-3 Corsair naval fighter
General characteristics
Wingspan: 41 ft (12.5m)
Length: 33 ft 4 in (10.16m)
Height: 14 ft 9 in (4.5m)
Wing Area: 314 ft² (29.2 m²)
Empty weight: 9,205 lbs (4,175 kg)
Gross weight: 12,420 lbs (5,630 kg)
Max Takeoff Weight: 14,670 lbs (6,650 kg)
Engine: 1 × Austral Incitatus 2W-31 (2,150hp takeoff, 1,950hp at 23,300ft / 7,100m, 2,450hp with water injection at sea level)
Crew: 1 (pilot)
Armour:

Performance
Max speed: 446 mph (718kph) @ 26,200 ft (7,990m)
Cruising speed: 215 mph (346 kph)
Range: 1,005 miles (1,620 km) normal range
Fuel:
- Internal fuel: 234 gal (US) / 886 liter tank
- Auxiliary fuel: two 150 gal (US) / 568 liter belly tanks
Service ceiling: 41,500 ft (12,650 m)
Rate of climb: 3,870 fpm (19.6 mps)

Armament
- 6 × 13 mm MGs in wings with 1,975 rounds
- Up to 4,000lb (454 kg) external stores including but not limited to 500lb, 1000lb, and 2000lb bombs, external auxiliary fuel tanks, 8x rockets on wings, 2x rockets on centerline

Notes
The ENAER F4E-3 is largely identical to the American F4U-4 Corsair, with ENAER working with Chance-Vought to improve the preceding Corsair design. Like the preceding F4E-2, ENAER built over 85% of the aircraft using indigenous development, although some difficult-to-manufacture parts were sourced from the US or Atlantis, The F4E-3 was highly regarded by the Armada, but the FACh ended up with first priority for ENAER's production, ordering ninety-six planes in late 1941.