Tag Archives: helicopter

Data Teknis Kecelakaan Heli Puma di Bogor

Disadur dari okezone.com

Data Teknis Heli Nahas di Bogor

Sabtu, 13 Juni 2009 – 06:16 wib

JAKARTA – Jatuhnya helikopter milik TNI AU jenis Puma di Lanud Atang Sanjaya, Bogor, cukup menghenyakkan kembali banyak kalangan dan masyarakat. Pasalnya, berita jatuhnya heli di Cianjur masih hangat dalam ingatan.

Berbagai pertanyaan masih hinggap di benak banyak kalangan terkait penyebab heli buatan Perancis tersebut jatuh. Ketidaklaikan heli untuk melakukan penerbangan semakin menguat.

Berikut data teknis heli yang diperoleh:


Pic of the Sud Aviation / Aerospatiale SA 330 Puma

Tanggal kejadian : Jumat, 12 Juni 2009
Pukul : 14.13 WIB
Tempat Kejadian : Lanud Atang Sanjaya Bogor
Type Pesawat : SA-330 PUMA
Tile Number : HT 3306
Kesatuan : Skadron Udara 8 lanud ATS Bogor
Misi : Tes Flight
Rute Penerbangan : ATS – LOC – ATS
Awak Pesawat : 1. Mayor Pnb Sobic (pilot) alm
2. Lettu Pnb Wisnu (co Pilot) alm
3. Lettu Tek Ronny (Teknisi)
4. Serka Catur H (Jmu I) alm
5. Serka Efram (Jmu II)
6. Serka Ferdinand (Pjmu I)
7. Serda Dodi H (Spec) alm
Kondisi pesawat : Rusak berat
Korban : 1. Mayor Pnb Sobic (meninggal)
2. Lettu Pnb Wisnu (meninggal)
3. Serka Catur H (meninggal)
4. Serda Dodi H (meninggal)
5. 3 orang lainnya luka berat

Data Teknis

Type : SA-330 PUMA
Kegunaan : Multi Purpose
Pabrik : Turmomeca
Mesin : Tumo IV C
Pabrik Mesin : Perancis
Tahun Pembuatan : 1977
Dioperasikan TNI AU : 1978

Ukuran Pesawat

Panjang M/R blade : 7,5 m (24,6 ft)
Diameter putaran M/R : 18.217 m  959.77 ft)
Lebar M/R blade : 60 cm
Tinggi pesawat : 4.535 m (14.87 ft)
Panjang pesawat dari nose : 14.822 m (48.5 ft)
Diameter putaran T/R : 3.042 m (10 ft)

Kemampuan Muat

Jumlah awak pesawat : VFR 1 Pilot, IFR 2 Pilot
Kemampuan muat barang : 1500 Kg/ di dalam cabin
Kemampuan muat personel : – 10 orang VIP/VVIP
– 16 orang pasanger
Kemampuan evakuasi : 4 pasien tidur, 2 duduk
Berat kosong : 4200 Kg
Max take off weight : 7400 kg
Bahan bakar : Avtur JP-1

Kemampuan Terbang

Kecepatan jelajah : 120 Kts
Kecepatan maksimum : 167 Kts
Maksimum ketinggian : 16.500 feet
Jarak terbang : 270 nm
(Sukmo Wibowo/Trijaya/hri)

(Sumber : okezone.com, gambar dari http://www.militaryfactory.com)

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KNKT probes helicopter crash site in Pondok Cabe

The Jakarta Post ,  Jakarta   |  Thu, 01/29/2009 2:02 PM  |  Jakarta

Investigators examine the Super-Puma helicopter destroyed when it crashed at Pondok Cabe airfield in Tangerang, Banten, on Thursday. The crash early Thursday killed two technicians. The pilot and an on-board technician both survived. Antara/Prasetyo UtomoCrashed Chopper: Investigators examine the Super-Puma helicopter destroyed when it crashed at Pondok Cabe airfield in Tangerang, Banten, on Thursday. The crash early Thursday killed two technicians. The pilot and an on-board technician both survived. Antara/Prasetyo Utomo

Investigators from the National Transportation Safety Commission (KNKT) have arrived at Pondok Cabe airfield in Tangerang to investigate the helicopter crash that killed two technicians earlier Thursday.

The crash site, located in front of Pelita Air’s service hangar, was cordoned off and under police guard. Journalists were not allowed to enter the area.

The bodies of the victims, Ahmad Suparja (25) and Sri Setyobudi (42) were taken to Fatmawati Hospital in South Jakarta. The pilot of the twin engine Super-Puma helicopter, Rohman Hadi (50), and a technician who was inside the chopper, HM Hardi (52), survived, but were still suffering from shock.

South Jakarta Police chief Sr. Comr. Chairul Anwar said at the crash site the police had yet to figure out the chronology of the incident.

“What we know so far is they were doing a routine maintenance check. They started up the engine and the pilot began to lift the chopper when it suddenly collapsed,” Chairul told journalists, as quoted by tempointeraktif.com.

He said the helicopter’s blades had sliced through the two technicians. “It’s quite severe, they were cut in two,” he said. (dre)

Helicopter spesification, read here.

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Chopper Crashed; Spesification of Super Puma Chopper

Source : http://www.pelita-air.com

SUPER PUMA AS – 332C
MANUFACTURE :
AEROSPATIALE – IPTN 1983

POWER PLANT

Power Plant :2 (two) Turbomeca / Makila 1A (1756 HP Each)
Take Off Power :1662 SHP
Max. Contingengy Power :1515 SHP

SPECIFICATIONS

Seating Capacity :3 Cockpit + 17 Seat (airline), 18 Seat (troop)
Litter Capacity :6 Each
Avarage Cruise Speed :130 Kts
Speed with Slung Load :40 -80 Kts
Max. Speed (VNE) :150 Kts (WT > 8350 Kg)
:167 Kts (WT < 8350 Kg)
Fuel Consumption :600 Ltr/hr
Fuel Capacity :Internal Tank : 1880 Ltr
:External Tank : 700 Ltr
:Ferry Tank (1) : 475 Ltr
Max. Range (15” Reserve) :487 Nm / 904 Km
Ceiling (T/O & Landing) :15000 ft (WT < 8350 Kg)
:4000 ft (WT >8350 Kg)
Ceiling (Inflight) :20000 ft (WT < 8350 Kg)
:9500 ft (WT > 8350 Kg)
Max. Rate of Climb :1889 ft/min

DIMENSION

Rotor Blades :4 Fully Artriculated
Fuselage Length :15.53 M
Overall Length :18.7 M
Fuselage Width :3.380 M
Overall Height :4.94 M
Main Rotor Diameter :15.6 M
Tail Rotor Clearance :1.90 M
Cabin Doors Dimension :1.35 M x 1.35 M

LOADING INFORMATION

Max. Gross Weight :8600 Kg / 18900 Lb
Empty Weight – Std :4872 Kg / 10738 Lb
Usefuel Load – Int :3728 Kg / 8216 Lb
Usefuel Load – Ext :4478 Kg / 9869 Lb

HELIPAD SIZE

Size :20 x 20 M (Fato : 27.3 x 27.3 M )
Minimum Strenght :12.900 Kg

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