DAFTAR PUSTAKA Angkasa Pura Persero. PT ; Turning Area, Taxiway dan Apron Bandara BIM, Informasi Bandara Internasional Minangkabau. Basuki, Heru. 1986. Merancang Dan Merencanakan Lapangan Terbang Cetakan II. Bandung: Penerbit Alumni. Direktorat P.U. Jendral Bina Marga. No. 01/PD/BM/1983, Pedomanan Penentuan Tebal Perkerasan Lentur Jalan Raya, Badan Penerbit Pekerjaan Umum. Jakarta Departemen Pekerjaan Umum. 1987, Petunjuk Perencanaan Tebal Perkerasan Lentur Jalan Raya dengan Metode Analisa Komponen. Direktorat Jenderal Bina Marga, Jakarta. http://www.antaranews.com/berita/255364/lion-siap-layani-penumpang-umrah-daripadang Horonjeff, Robert & McKelvey Francis X, 1993. Perencanaan dan Perancangan Bandar Udara Edisi Ketiga Jilid I. http://infohaji.antaranews.com/berita/1316102972/pemerintah-ajukan-penambahankuota-haji-2012 http://www.airliners.net/aircraft-data/stats.main?id=136
http://digilib.mercubuana.ac.id/
Ihromi Faisal, 2008 ; Tugas Akhir Studi Pengembangan Geometrik Area Lapangan Terbang Juwata Kota Tarakan, Fakultas Teknik Sipil Malang. Kumpulan Foto-foto BIM yang dapat diapload melalui google.com Laporan Perencanaan Pekerjaan Sipil Sisi Udara, 2009. Desain Pengembangan Bandara Ketaping di Bandara Internasional Minangkabau. Padang: PT. DACREA AVIA. Muhammad Zein, Rusmali, 2010. Evaluasi Perencanaan Fasilitas Runway pada Bandara Internasional Minangkabau Kabupaten Padang Pariaman. Tugas Akhir Mahasiswa Teknik Sipil Universitas Islam Riau, Pekanbaru. Peraturan Direktur Jendral Perhubungan Udara No. SKEP/77/IV2005 Tentang Persayaratan Teknis Fasilitas Teknik Bandar Udara. Jakarta: Dirjen Perhubungan Udara. Peraturan Pemerintah Republik Indonesia No. 70 Tahun 2001 Tentang Kebandarudaraan. Jakarta: Sekretariat Negara Republik Indonesia. Proyek Pengembangan BIM. 2008. Pekerjaan Pengembangan Sisi Udara Turning Area, Taxiway dan Apron: PT. Persero Angkasa Pura II BIM. Padang.
http://digilib.mercubuana.ac.id/
Rajartnam Yayan ; Hardjasputra Harianto ; Giriana Monty, 2006 ; Studi Ilmiah Kelayakan Ekonomi Pengembangan Bandara Internasional Minangkabau. Mahsiswa S2 Univeritas Pelita Harapan, Jakarta.
Sandhyavitri, Ari. Tuafik, Hendra. 2005. Teori Dasar 1 Teknik Lapangan Terbang: Fakultas Teknik Sipil Universitas Riau. Pekanbaru. Tm, Suprapto. 2004. Bahan dan Struktur Jalan Raya; Biro Penerbit Teknik Sipil Universitas Gajah Mada. Yogyakarta. Yusuf, Muhamad, 2010 ; Tugas Akhir Analisa Metoda – Metoda Perencanaan Perkerasan Struktural Raunway Bandara, Fakultas Teknik Universitas Sumatera Utara.
http://digilib.mercubuana.ac.id/
Bab IV Perhitungan Perencanaan
Gambar Pesawat-Pesawat yang Landing di Bandar Udara Internasional Minangkabau Pesawat Rencana B-747-400
IV-1
http://digilib.mercubuana.ac.id/
Bab IV Perhitungan Perencanaan
Spesifikasi Teknis Pesawat B-747-400 KARAKTERISTIK Maximum Take Off Weight
Maximum Landing Weight
Operating Weight Empty Zero Full Weight
Runway Lenght
Length
Wingspan
Height
Wheelbase Tire pressure
SATUAN
MODEL B-747-400
Pounds
910000
Kilograms
412770
Pounds
564000
Kilograms
256000
Pounds
365800
Kilograms
166100
Pounds
526000
Kilograms
238800
Pounds
11000
Meters
3353
feet
231
meters
70,66
feet
211
meters
64,44
feet
63
meters
19,41
feet
84
meters
25,60
psi
205
Payload
362-490
VI-2
http://digilib.mercubuana.ac.id/
Bab IV Perhitungan Perencanaan
Pesawat Rencana B-737-300
VI-3
http://digilib.mercubuana.ac.id/
Bab IV Perhitungan Perencanaan
Spesifikasi teknis Pesawat B-737-300 KARAKTERISTIK Maximum Take Off Wight Maximum Take Landing Maximum Landing Weight Maximum Zero Fuel Weight Operating Empty Weight Length Wingspan Height Wheelbase Maximum Cruising Speed Maximum Seat Capacity Engines Maximum Paylod Maximum Fuel Capacity Take-off field length (S/L at 30 C) Tire pressure Landing field length
SATUAN MODEL B-737-300 Pounds 138500 Kilograms 62823 Pounds 124500 Kilograms 56470 Pounds 114000 Kilograms 51720 Pounds 105000 Kilograms 47625 Pounds 72100 Kilograms 32704 feet 109,53 meters 33,40 feet 94,75 meters 28,88 feet 36,50 meters 11,13 feet 40,83 meters 12,45 km/h 933 crews 6 pax 124 CFM56 Engines Pounds 35600 Kilograms 16150 Pounds 32030 Kilograms 14520 feet 7500 meters 2286 psi 166 feet 4700 meters
1433
VI-4
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Bab IV Perhitungan Perencanaan
Pesawat Fokker 100
VI-5
http://digilib.mercubuana.ac.id/
Bab IV Perhitungan Perencanaan
Spesifikasi Teknis Pesawat Fokker 100
KARAKTERISTIK Maximum Take Landing Maximum Take Off Weight Maximum Landing Weight Maximum Zero Fuel Weight Operating Empty Weight Length Wingspan Height Wheelbase Range Maximum Cruising Speed Maximum Seat Capacity Engines Maximum Paylod Maximum Fuel Capacity Maximum Pax Range
SATUAN
MODEL Fokker 100
Pounds Kilograms Pounds Kilograms Pounds Kilograms Pounds Kilograms Pounds Kilograms feet meters feet meters feet meters feet meters n miles Kilometers
99500 44680 101000 45810 88000 39915 81000 36740 54103 24541 116,52 35,54 92,03 28,08 27,87 8,50 45,93 14,01 2100 3889
km/h 845 crews 2 pax 100-107 Two RollsRoyce Tay Mk 65015 Pounds 26973 Kilograms 12235 Pounds 23300 Kilograms 10568 Km 2898 nm 1610
Take-off field length at MTOW, ISA, S/L (Flaps 15 0 )
feet meters
7500 2286
Take-off field length MTOW, ISA, S/L (Flaps 35 C 0 )
feet
4700
meters
1433 VI-6
http://digilib.mercubuana.ac.id/
Bab IV Perhitungan Perencanaan
Pesawat Fokker-50
Spesifikasi Teknis Pesawat Fokker-50 KARAKTERISTIK Maximum Take Off Weight Maximum Landing Weight Maximum Zero Fuel Weight Operating Empty Weight Length Wingspan Height Wheelbase Seat Capacity Engines Maximum Payload Maximum Fuel Weight Maximum Operating Altitude Take-Off Field Length at MTOW,ISA, S/L (Flaps 15) Take-Off Field Length at MTOW,ISA, S/L (Flaps 35)
SATUAN Pounds
MODEL F-50 45900
kilogram kilogram
20820 19731
kilogram 18144 kilogram 12383 meters 25,19 meters 29,00 meters 8,60 meters 9,74 pax 58 Pratt & Whitney Canada PW 120 B Turboprop kilogram 5760 kilogram 4123 feet
7620
meter
890
meter
1017 VI-7
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Bab IV Perhitungan Perencanaan
Pesawat Fokker 27
Spesifikasi Teknik Fokker 27
KARAKTERISTIK
SATUAN Pounds
MODEL F-27 Mk 500 45500
Maximum Take Off Weight Maximum Zero Fuel Weight Operating Empty Weight Length Wingspan Height Wheelbase Seat Capacity
kilogram
20639
Engines Range Maximum Payload Maximum Fuel Weight Maximum Operating Altitude Take-Off Field Length at 18143 kg (40000lb), ISA, S/L Take-Off Field Length at 16329 kag (36000 lb), S/L
kilogram 18597 kilogram 12701 meters 25,06 meters 29,00 meters 8,84 meters 9,74 pax 60 Two 1730 kW (2320ehp) Rolls Royce Dart Mk 5367R Turboprop driving four Blade Dowty Rotol propellers km 1315 kilogram 4123 kilogram 5896 feet
7620
meter
988
meter
1003
VI-8
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Bab IV Perhitungan Perencanaan
Pesawat Cassa 212
Spesifikasi Teknik Cassa 212
KARAKTERISTIK
SATUAN
MODEL C-212
Length
meters
16,15
Wingspan
meters
20,28
Height
meters
6,60
Wheelbase
meters
5,46
VI-9
http://digilib.mercubuana.ac.id/
Bab IV Perhitungan Perencanaan
VI-10
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