Role Trainer
Propulsion\t1 Piston Engine
Engine Model\tLycoming AEIO-360
Engine Power\t134 kW\t180 hp
Speed\t241 km/h\t130 kts
Range\t1.141 km\t616 NM
Empty Weight\t700 kg\t1.543 lbs
max. Takeoff Weight\t1.050 kg\t2.315 lbs
Wing Span\t9,75 m\t32,0 ft
Wing Area\t13,2 m²\t142 ft²
Length\t7,50 m\t24,6 ft
Height\t2,81 m\t9,2 ft

* Crew: 1-2
* Length: 26 ft 11 in (8.21 m)
* Wingspan: 35 ft 10 in (10.92 m)
* Height: 8 ft 10 in (2.69 m)
* Wing area: 159 ft² (14.8 m²)
* Empty weight: 1,363 lb (618 kg)
* Loaded weight: 2,500 lb (1,134 kg)
* Powerplant: 1 × Continental IO-360-D, 210 hp (160 kW)
* Maximum speed: 125 knots (144 mph, 232 km/h)
* Range: 626 nm (720 mi, 1,159 km)
* Service ceiling: 17,000 ft (5,180 m)
* Rate of climb: 880 ft/min (4.47 m/s)

* Crew: Two
* Length: 28 ft 8½ in
* Wingspan: 33 ft 3⅞ in
* Height: 9 ft 7 in
* Wing area: 179.6 ft²
* Empty weight: 2,960 lb
* Max takeoff weight: 4,300 lb (T-34C-1 weapons trainer - 5,500 lb)
* Powerplant: 1 × Pratt & Whitney Canada PT6A-25 turboprop, 715 shp
* Never exceed speed: 280 knots
* Cruise speed: 214 knot max cruise at 17,000 ft
* Stall speed: 53 knotsflaps down, power off
* Range: 708 nmi at 180 knots and 20,000 ft
* Service ceiling: 30,000 ft
* Rate of climb: 1,480 ft/min
* g limit:+4.5, -2.3
Armament
* Hardpoints: 4 with a capacity of 600 lb inner, 300 lb outer, 1,200 lb

Role: Trainer, light attack
Crew: 2 in tandem
Length: 10.26 m
Wingspan: 10.59 m
Height: 3.68 m
Wing area: 16.01 m²
Empty weight: 1,910 kg
Max takeoff weight: 2,540 kg
Powerplant: 1 × Pratt & Whitney Canada PT6A-62, 950 hp
Maximum speed: 574 km/h
Range: 1,333 k at 7.620 m, max internal fuel
Service ceiling: 11,580 m
Rate of climb: 16.2 m/min

Engines: 1 Pratt &Whitney F100- PW-100 or -220 turbofan or I General Electric F110-GE-100 turbofan
Max power: F100-PW-220: 23,800 Ib static thrust F110-GE-100: 28,900 Ib static thrust
Internal fuel capacity: F-16 C: 6,972 Ib/approx 1,073 US galF-16 D: 5,785 Ib or approx 890 US gal
External fuel capacity: 6,760 Ib or approx 1,040 US gal
Empty: 18,238 Ib combat weight (50 % fuel and 2 Sidewinder AAMs)F100-PW-220: 26,250 Ib F110-GE-100: 27,350 Ib
Max takeoff: 42,300 Ib
Length: 49 ft 3 in
Height: 16 ft 8 in
Wing area: 300 ft2
Max speed: more than 1,146 kts or Mach 2 ceiling 60,000 ft
Radius: F-16 A, with 6 500-lb bombs, hi-lo-hi.
Internal fuel: 295 nm F-16 C, weapons load unspecified: more than 500 nm
Armament: 1 M61 20-mm multibarrel cannon with 515 rounds and 2 450-lb capacity wingtip launch rails for AAM and 6 wing, 1 belly, and 2
inlet weapons stations for AAM, bombs, air-toground missiles, fuel, rockets, chaff/flare dispensers, or electronics pods; of these:2 700-lb capacityouter wing pylons for AAM only 2 3,500-lb middle wing pylons AAM and other stores 2 4,500-lb inboard wing pylons for other stores only 1 2,200-lb capacity fuselage hardpoint for bombs,dispensers, or fuel2 900-lb inlet stub pylons for electronics pods
Radar: AN/APG-68 pulse- Doppler

Panjang: 21.935 mLebar sayap: 14.7 m
Tinggi: 6.36 m
Luas sayap: 62.0 m²
Bobot kosong: 17,700 kg
Bobot terisi: 24,900 kg
Mesin: 2× AL-31FL low-bypass turbofans
Dorongan kering: 7,600 kgf masing-masing
Dorongan dengan pembakar lanjut: 12,500 kgf masing2
Laju maksimum: Mach 2.0
Jarak jangkau: 3,000 km at altitude
Laju panjat: 230 m/s
Beban sayap: 401 kg/m²
Dorongan/berat: 1.0
Guns: 1 × GSh-30-1 gun
AAMs: 6 × R-27ER1 (AA-10C), 2 × R-27ET1 (AA-10D), 6 × R-73E (AA-11), 6 × R-77 RVV-AE(AA-12)
ASMs: 6 × Kh-31P/Kh-31A anti-radar missiles, 6 × Kh-29T/L laser guided missiles, 2 × Kh-59ME
Aerial bombs: 6 × KAB 500KR, 3 × KAB-1500KR, 8 × FAB-500T, 28 × OFAB-250-270

Kru: Satu
Panjang: 21,9 m
Lebar sayap: 14,7 m
Tinggi: 5,93 m
Bobot kosong: 16.380 kg
Bobot terisi: 23.000 kg
Mesin: 2× Lyulka AL-31F turbofan, 122,8 kN masing-masing
Laju maksimum: 2.500 km/jam (1.550 mph Mach 2.35)
Jarak jangkau: 1.340 km pada ketinggian air laut, 3.530 km pada ketinggian tinggi
Laju panjat: 325 m/s
Beban sayap: 371 kg/m²
1 x meriam GSh-30-1 30 mm, 150 butir peluru
8.000 kg (17.600 lb) pada 10 titik eksternal
6 R-27, 4 R-73
Su-27SM dapat menggunakan R-77 menggantikan R-27
Su-27IB dapat menggunakan peluru kendali anti-radiasi X-31, peluru kendali udara ke darat X-29L/T, serta bom KAB-150 dan UAB-500
AA-11 Archer / R-73
AA-10A/B/C/D/E Alamo-A/B/C/D/E / R-27R/T/RE/TE/AE
AS-16 Kickback SRAM/ Kh-15/C
Air bombs
KAB-500Kr
KAB-1500Kr
KAB-1500L / 1500F / 1500L-PR
KAB-500R
KAB-500KRU
ODAB-500
OEPS-27 Optronic sighting system for SU-27SK
AS-11 Kilter / Kh-58E
ZHUK FAMILY AIRBORNE RADARS

* Panjang: 40 ft 3 in
* Lebar sayap: 26 ft 6 in
* Tinggi: 15 ft
* Luas sayap: 259 ft²
* Airfoil: NACA 0008-1.1-25 root, NACA 0005-0.825-50 tip
* Bobot kosong: 10,450 lb
* Bobot terisi: 18,300 lb
* Mesin: 1× Pratt & Whitney J52-P8A turbojet, 9,300 lbf
* Laju maksimum: 585 kn (673 mph, 1,077 km/h)
* Jarak jangkau: 1,700 nmi
* Laju panjat: 8,440 ft/min
* Beban sayap: 70.7 lb/ft²
* Dorongan/berat: 0.51
* g-limit: -3/+8 g
* Senjata api: 2 × 20 mm Colt Mk 12 cannon, 100 rounds/gun
* Rudal:4×AIM-9 Sidewinder, AGM-45 Shrike ARM,MBDA Exocet, AGM-65 Mav ASM,AGM-62 Walleye glide bomb, AGM-12 Bullpup ASM
* Bom: 9,900 lb on five external hardpoints, Rockeye Mk.20 Cluster Bomb Unit, Rockeye Mk.7/APAM-59 Cluster Bomb Unit, Mk.81 and Mk.82 general-purpose bombs, various tactical nuclear missiles and bombs, Mk.76 practice bombs

* Mohon koreksinya atas berbagai kesalahan nama,jumlah,gambar dll
* Jenis pesawat sementara terbatas pada peswat latih,angkut,vvip,tempur yg aktif