1. Theory of Flight 1.1 Aeroplane Aerodynamics and Flight ControlsOper terjemahan - 1. Theory of Flight 1.1 Aeroplane Aerodynamics and Flight ControlsOper Bahasa Indonesia Bagaimana mengatakan

1. Theory of Flight 1.1 Aeroplane A

1. Theory of Flight

1.1 Aeroplane Aerodynamics and Flight ControlsOperation and effect of:
roll control: ailerons and spoilers;
pitch control: elevators, stabilators, variable incidence stabilisers andcanards;
yaw control, rudder limiters;
Control using elevons, ruddervators;
High lift devices, slots, slats, flaps, flaperons;
Drag inducing devices, spoilers, lift dumpers, speed brakes;
Effects of wing fences, saw tooth leading edges;
Boundary layer control using, vortex generators, stall wedges or leading edgedevices;
Operation and effect of trim tabs, balance and antibalance (leading) tabs, servo tabs, spring tabs, mass balance, control surface bias, aerodynamicbalance panels;
1.2 High Speed Flight
Speed of sound, subsonic flight, transonic flight, supersonic flight, Machnumber, critical Mach number, compressibility buffet, shock wave,aerodynamic heating, area rule;
Factors affecting airflow in engine intakes of high speed aircraft;
Effects of sweepback on critical Mach number.

2. Airframe Structures — General Concepts

2.1 Airworthiness requirements for structural strength;
Structural classification, primary, secondary and tertiary;
Fail safe, safe life, damage tolerance concepts;
Zonal and station identification systems;
Stress, strain, bending, compression, shear, torsion, tension, hoop stress,fatigue;
Drains and ventilation provisions;
System installation provisions;
Lightning strike protection provision;
Aircraft bonding.
2.2 Construction methods of: stressed skin fuselage,formers, stringers, longerons, bulkheads, frames,doublers, struts, ties, beams, floor structures,reinforcement, methods of skinning, anticorrosiveprotection, wing, empennage and engineattachments;
Structure assembly techniques: riveting, bolting,bonding;
Methods of surface protection, such as chromating, anodising, painting;
Surface cleaning;
Airframe symmetry: methods of alignment andsymmetry checks.

3. Airframe Structures — Aeroplanes

3.1 Fuselage (ATA 52/53/56)
Construction and pressurisation sealing;
Wing, stabiliser, pylon and undercarriageattachments;
Seat installation and cargo loading system;
Doors and emergency exits: construction, mechanisms, operation andsafety devices;
Windows and windscreen construction and mechanisms.
3.2 Wings (ATA 57)
Construction;
Fuel storage;
Landing gear, pylon, control surface and high lift/drag attachments.
3.3 Stabilisers (ATA 55)
Construction;
Control surface attachment.
3.4 Flight Control Surfaces (ATA 55/57)
Construction and attachment;
Balancing — mass and aerodynamic.
3.5 Nacelles/Pylons (ATA 54)
Construction;
Firewalls;
Engine mounts.

4. Air Conditioning and Cabin Pressurisation (ATA 21)

4.1 Air supply
Sources of air supply including engine bleed, APU and ground cart;
4.2 Air Conditioning
Air conditioning systems;
Air cycle and vapour cycle machines;
Distribution systems;
Flow, temperature and humidity control system.
4.3 Pressurisation
Pressurisation systems;
Control and indication including control and safety valves;
Cabin pressure controllers;
Safety and warning devices;
Protection and warning devices.

5. Instruments/Avionic Systems

5.1 Instrument Systems (ATA 31)
Pitot static: altimeter, air speed indicator, vertical speed indicator;
Gyroscopic: artificial horizon, attitude director, direction indicator, horizontal situation indicator, turn and slip indicator, turn coordinator;
Compasses: direct reading, remote reading;
Angle of attack indication, stall warning systems;
Other aircraft system indication.
5.2 Avionic Systems
Fundamentals of system lay-outs and operation of:Auto Flight (ATA 22);
Communications (ATA 23);
Navigation Systems (ATA 34).

6. Electrical Power (ATA 24)

Batteries Installation and Operation;
DC power generation;
AC power generation;
Emergency power generation;
Voltage regulation;
Power distribution;
Inverters, transformers, rectifiers;
Circuit protection;External/Ground power.

7. Equipment and Furnishings (ATA 25)

7.1 Emergency equipment requirements;
Seats, harnesses and belts.
7.2 Cabin lay-out;Equipment lay-out;
Cabin Furnishing Installation;
Cabin entertainment equipment;
Galley installation;
Cargo handling and retention equipment;
Airstairs.

8. Fire Protection (ATA 26)

8.1 Fire and smoke detection and warning systems;
Fire extinguishing systems;System tests.
8.2 Portable fire extinguisher

9. Flight Controls (ATA 27)

Primary controls: aileron, elevator, rudder, spoiler;
Trim control;
Active load control;
High lift devices;
Lift dump, speed brakes;
System operation: manual, hydraulic, pneumatic, electrical, fly-by-wire;Artificial feel, Yaw damper, Mach trim, rudder limiter, gust locks systems;
Balancing and rigging;
Stall protection/warning system.

10. Fuel Systems (ATA 28)

System lay-out;
Fuel tanks;
Supply systems;
Dumping, venting and draining;
Cross-feed and transfer;
Indications and warnings;
Refuelling and defuelling;
Longitudinal balance fuel systems.

11. Hydraulic Power (ATA 29)

System lay-out;
Hydraulic fluids;
Hydraulic reservoirs and accumulators;
Pressure generation: electric, mechanical, pneumatic;
Emergency pressure generation;
Pressure Control;
Power distribution;
Indication and warning systems;
Interface with other systems.

12. Ice and Rain Protection (ATA 30)

Ice formation, classification and detection;
Anti-icing systems: electrical, hot air and chemical;
De-icing systems: electrical, hot air, pneumatic and chemical;
Rain repellant;
Probe and drain heating.
Wiper systems.

13. Landing Gear (ATA 32)

Construction, shock absorbing;
Extension and retraction systems: normal and emergency;
Indications and warning;
Wheels, brakes, antiskid and autobraking;
Tyres;
Steering.

14. Lights (ATA 33)

External: navigation, anti-collision, landing, taxiing, ice;Internal: cabin, cockpit, cargo;
Emergency.

15. Oxygen (ATA 35)

System lay-out: cockpit, cabin;
Sources, storage, charging and distribution;
Supply regulation;
Indications and warnings;

16. Pneumatic/Vacuum (ATA 36)

System lay-out;
Sources: engine/APU, compressors, reservoirs, ground supply;
Pressure control;
Distribution;
Indications and warnings;
Interfaces with other systems.

17. Water/Waste (ATA 38)

Water system lay-out, supply, distribution, servicing and draining;
Toilet system lay-out, flushing and servicing;
Corrosion aspects.

18. On Board Maintenance Systems (ATA 45)

Central maintenance computers;
Data loading system;
Electronic library system;
Printing;
Structure monitoring (damage tolerance monitoring).
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1. teori penerbangan 1.1 pesawat aerodinamis dan penerbangan ControlsOperation dan efek: Roll kontrol: ailerons dan spoiler; pitch kontrol: Elevator, stabilators, variabel insiden penyeimbang andcanards; yaw kontrol, limiters kemudi; Kontrol yang menggunakan elevons, ruddervators; Angkat tinggi perangkat, slot, bilah, flaps, flaperons; Tarik merangsang perangkat, spoiler, mengangkat damper, kecepatan rem; Efek dari sayap pagar, melihat tepi terkemuka gigi; Lapisan batas kontrol menggunakan, vortex Generator, irisan kios atau terkemuka edgedevices; Operasi dan efek dari tab trim, keseimbangan dan antibalance (terkemuka) tab, tab servo, musim semi tab, keseimbangan massa, kontrol permukaan bias, panel aerodynamicbalance; 1.2 penerbangan kecepatan tinggi Kecepatan suara, subsonik penerbangan, penerbangan transonic, penerbangan supersonik, Machnumber, kritis Mach jumlah, compressibility prasmanan, gelombang kejut, Penghangat Ruangan aerodinamis, peraturan daerah; Faktor-faktor yang mempengaruhi aliran udara di intake mesin pesawat kecepatan tinggi; Efek sweepback pada kritis Mach jumlah.2. airframe struktur — Konsep-konsep umum 2.1 kelaikan persyaratan untuk kekuatan struktural; Klasifikasi struktural, primer, sekunder dan tersier; Gagal hidup aman, aman, merusak toleransi konsep; Sistem identifikasi Zonal dan Stasiun; Stres, ketegangan, membungkuk, kompresi, geser, torsi, ketegangan, Ring stres, kelelahan; Saluran dan ventilasi ketentuan; Ketentuan pemasangan sistem; Sambaran petir perlindungan penyediaan; Aircraft bonding. 2.2 Construction methods of: stressed skin fuselage,formers, stringers, longerons, bulkheads, frames,doublers, struts, ties, beams, floor structures,reinforcement, methods of skinning, anticorrosiveprotection, wing, empennage and engineattachments; Structure assembly techniques: riveting, bolting,bonding; Methods of surface protection, such as chromating, anodising, painting; Surface cleaning; Airframe symmetry: methods of alignment andsymmetry checks.3. Airframe Structures — Aeroplanes 3.1 Fuselage (ATA 52/53/56) Construction and pressurisation sealing; Wing, stabiliser, pylon and undercarriageattachments; Seat installation and cargo loading system; Doors and emergency exits: construction, mechanisms, operation andsafety devices; Windows and windscreen construction and mechanisms. 3.2 Wings (ATA 57) Construction; Fuel storage; Landing gear, pylon, control surface and high lift/drag attachments. 3.3 Stabilisers (ATA 55) Construction; Control surface attachment. 3.4 Flight Control Surfaces (ATA 55/57) Construction and attachment; Balancing — mass and aerodynamic. 3.5 Nacelles/Pylons (ATA 54) Construction; Firewalls; Engine mounts.4. Air Conditioning and Cabin Pressurisation (ATA 21) 4.1 Air supply Sources of air supply including engine bleed, APU and ground cart; 4.2 Air Conditioning Air conditioning systems; Air cycle and vapour cycle machines; Distribution systems; Flow, temperature and humidity control system. 4.3 Pressurisation Pressurisation systems; Control and indication including control and safety valves; Cabin pressure controllers; Safety and warning devices; Protection and warning devices.5. Instruments/Avionic Systems 5.1 Instrument Systems (ATA 31) Pitot static: altimeter, air speed indicator, vertical speed indicator; Gyroscopic: artificial horizon, attitude director, direction indicator, horizontal situation indicator, turn and slip indicator, turn coordinator; Compasses: direct reading, remote reading; Angle of attack indication, stall warning systems; Other aircraft system indication. 5.2 Avionic Systems Fundamentals of system lay-outs and operation of:Auto Flight (ATA 22); Communications (ATA 23); Navigation Systems (ATA 34).6. Electrical Power (ATA 24) Batteries Installation and Operation; DC power generation; AC power generation; Emergency power generation; Voltage regulation; Power distribution; Inverters, transformers, rectifiers; Circuit protection;External/Ground power.7. Equipment and Furnishings (ATA 25) 7.1 Emergency equipment requirements; Seats, harnesses and belts. 7.2 Cabin lay-out;Equipment lay-out; Cabin Furnishing Installation; Cabin entertainment equipment; Galley installation; Cargo handling and retention equipment; Airstairs.8. Fire Protection (ATA 26) 8.1 Fire and smoke detection and warning systems; Fire extinguishing systems;System tests. 8.2 Portable fire extinguisher9. Flight Controls (ATA 27) Primary controls: aileron, elevator, rudder, spoiler; Trim control; Active load control; High lift devices; Lift dump, speed brakes; System operation: manual, hydraulic, pneumatic, electrical, fly-by-wire;Artificial feel, Yaw damper, Mach trim, rudder limiter, gust locks systems; Balancing and rigging; Stall protection/warning system.10. Fuel Systems (ATA 28) System lay-out; Fuel tanks; Supply systems; Dumping, venting and draining; Cross-feed and transfer; Indications and warnings; Refuelling and defuelling; Longitudinal balance fuel systems.11. Hydraulic Power (ATA 29) System lay-out; Hydraulic fluids; Hydraulic reservoirs and accumulators; Pressure generation: electric, mechanical, pneumatic; Emergency pressure generation; Pressure Control; Power distribution; Indication and warning systems; Interface with other systems.12. Ice and Rain Protection (ATA 30) Ice formation, classification and detection; Anti-icing systems: electrical, hot air and chemical; De-icing systems: electrical, hot air, pneumatic and chemical; Rain repellant; Probe and drain heating. Wiper systems.13. Landing Gear (ATA 32) Construction, shock absorbing; Extension and retraction systems: normal and emergency; Indications and warning; Wheels, brakes, antiskid and autobraking; Tyres; Steering.14. Lights (ATA 33) External: navigation, anti-collision, landing, taxiing, ice;Internal: cabin, cockpit, cargo; Emergency.15. Oxygen (ATA 35) System lay-out: cockpit, cabin; Sources, storage, charging and distribution; Supply regulation; Indications and warnings;16. Pneumatic/Vacuum (ATA 36) System lay-out; Sources: engine/APU, compressors, reservoirs, ground supply; Pressure control; Distribution; Indications and warnings; Interfaces with other systems.17. Water/Waste (ATA 38) Water system lay-out, supply, distribution, servicing and draining; Toilet system lay-out, flushing and servicing; Corrosion aspects.18. On Board Maintenance Systems (ATA 45) Central maintenance computers; Data loading system; Electronic library system; Printing; Structure monitoring (damage tolerance monitoring).
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