OPS DAULAT, TUDM HAWK KILL MARKING : CROCO
PANGGILAN PERTIWI exclusive
TUDM HAWK KILL MARKING : Pilot callsign CROCO HAWk 208 M40-30
3 kali sortie 1st mk 82 dan 2nd n 3rd ngan crv7. Gambar credit kepada ARAMOS dan BANGER.
During the 2013 Lahad Datu standoff, five Hawk 208 together with three FA-18 Hornets were employed in an airstrike on the Royal Army of Sulu on March 5th, 2013, occupying part of Borneo, just before the Malaysian joint forces assault.
The Hawk 200 has the Adour 871 engine, combat wing, and some of the other combat kit of the Hawk 100, but along with the single seat configuration, which resulted in an entirely new fuselage from the cockpit forward, also features a still taller tailfin; an optional fixed in-flight refueling probe; and the Northrop-Grumman AN/APG-66H pulse-Doppler X-band multimode radar, with ten air-to-air and ten air-to-surface modes.
The Hawk 200 has eleven external store points with four underwing pylons, an under-fuselage pylon, and wingtip air-to-air missile stations. The range of external stores includes air-to-air missiles, a gunpod, rocket launchers, reconnaissance pod, retarded and free-fall bombs up to 540 kg, runway cratering, anti-personnel and light Armor bombs, cluster bombs, practice bomb and rocket carriers and external fuel tanks.
actual bombing pictures taken from Royal Malaysian Navy Ship in Kampung Tanduo during the opening assault of OPS DAULAT.
|Developing nation:||United Kingdom.|
|Production line:||Brough, East Yorkshire, UK.|
|Task:||multi-role light fighter.|
|First flight:||May 19, 1986, ZG200.|
|British Aerospace Hawk 200|
|Ejection seat:||Martin Baker Mk.10 LH.|
|Wing Span:||- 9,39 m.|
- 9,94 m with tip-mounted AIM-9 Sidewinder.
|Wing Area:||16,69 m².|
|Length fuselage:||11,33 m.|
|Length fuselage including probe:||12,07 m.|
|Tail plane span:||4,39 m.|
|Wheel track:||3,47 m.|
|Engines:||One Rolls Royce/Turboméca Adour Mk.871 turbofan rated 26.00 kN.|
|Weight:||- Empty: 4.450 Kg.|
- Internal fuel: 1.361 kg.
- External fuel: 2 x 591 liter drop tanks.
- max. ordnance 3.493 kg.
|Max. take off weight:||9.100 Kg.|
|Max. speed:||1.019 km/h at 2.440 m.|
|Service ceiling:||13.715 m.|
|Range:||- range 2.428 km without drop tanks.|
- ferry range 3.610 km with 3x 864 liter drop tanks.
- combat radius 1.234 km with one Sea Eagle missile and two drop tanks or 945 km on a lo-lo-lo reconnaissance mission with one reconnaissance pod and two drop tanks.
|Performance:||- max. rate of climb at sea level 3.508 m per minute.|
- take-off run to 15 m at max. take-off weight 2.134 m.
- landing run from 15 m at max. landing weight 854 m with brake chute.
- landing run from 15 m at max. landing weight 1.250 m without brake chute.
|Radar:||Northrop-Grumman AN/APG-66H pulse-Doppler X-band multimode radar.|
|Weapons:||- Aden 30 mm cannon with 120 rounds.|
- AIM-9L Sidewinder.
- AIM-120 AMRAAM.
- Sky Flash.
- AGM-65 Maverick.
- 9 x 240 kg bombs.
- 9 x 113 kg bombs.
- 5 x 540 kg bombs.
- cluster bombs.
- Paveway II Bombs.
- SNEB rocket pods.
- Sea Eagle missile.
- Marconi Sting Ray homing torpedo.
|Extra:||- Reconnaissance pod. |
- brake chute.