ATR 72-500 HANDS BOOK

ATR 72-500 PILOT HANDBOOK---------------------------------------------------------------------------------------------------------------------------------

LIMITATIONS

AIRCRAFT FAMILIARIZATIONS :

Length

: 27,166m (89ft 1,5in)

Wheel base: 10,77m (35ft 4in)

Span

: 27,050m (88ft 9 in)

Wheel Track : 4,100m (13ft 5in)Height

: 7, 650m (25ft 1in)

Clrc fslage/Prop: 0,82 m (2 ft 8in)CABIN/INTERIOR ACCOMMODATIONS

Max.cabin height: 1,910m (6ft 3in)Overall lenght: 19,210m (63ft 0,5in)Max.cabin width: 2,570m (8ft 5in)Max.floor width: 2,263m (7ft 5in)

Aisle width: 0,457m ( 18in)PERFORMANCE

TAKE-OFF FIELD LENGTH

SL,ISA,MTOW

: 1290m (4,232ft) 3000ft,ISA+10,MTOW

: 1570m (5,151ft)

LANDING FIELD LENGTH

SL,MLW

: 1070m (3,510ft)

MAX CRUISE SPEED

ISA, 17000 ft

: 276kt

MAXIMUM CEILING

: 25000ft

DESIGN WEIGHT LIMITATIONSMAXIMUM WEIGHTKGLB

TAXI22.97050.640

TAKE OFF22.80050.265

LANDING22.35049.273

ZERO FUEL20.80045.856

PASSENGERS BOARDING/DISEMBARKING

The tail prop must be installed before passengers boarding/disembarking.

A possible tip up should be taken info account from seven persons moving near the rear part of load aircraft.

CARGO DOOR OPS.Do not operate cargo door with a x-wind component of more than 45 kt.Stairway ops.MAX.OPERATING ALTITUDE :25.000 FTAIRSPEEDS MAX. OPERATING SPEED.

VMO = 250 kt

MMO = 0.55 MAX.DESIGN MANEUVERING SPEED VA/ VA = 175 kt

MAX.FLAPS EXTENDED VFE

FLAPS 15 185 kt

FLAPS 30 150 kt

MAX.LANDING GEARS EXTENDED

VLE = 185 kt

VLO RET = 160 kt

VLO LOW = 170 kt

MAX.ROUGH AIR SPEED VRA = 180 kt

MAX.WIPER OPS.SPEED VWO = 160 kt

MAX.TIRE SPEED : 165 kt (Ground speed)

STALL SPEEDS VSR See 2.01.03. P2

V1 LIMITED BY VMCG (FLAPS 15) See 2.01.03. P3

VMCA (FLAPS 15) See 2.01.03. P4

VMCL

FlapsVMCL (CAS)

30

1598 kt

98 kt

OPS.PARAMETERSENVIRONMENTAL ENVELOPE ( Altitude Zp/ft+OAT) See 2.01.03.P5

TAIL WIND LIMIT : 10 kt

X-WIND ON DRY RWY : 35 kt

MAX. MEAN RWY SLOPE : +/- 2%

For ops.on rwy slope be on 2% refer to 3.11.18

MIN.RWY WIDTH : 30 mtr

For narrow rwy ops. Refer to 3.11.10

POWER PLAN

THE ENGINE PW 127 F or PW 127 M

Certified for a 2750 SHP max. take off rating In normal ops.take off rating will be 2475 SHP (Reduced Take off or RTO) with an automatic power increase to 2750 SHP.

Max.Continuous Power 2500 SHP

Rotation : clockwise (looking forward)

100% Np : 1200 RPM

ENGINE PARAMETERSPOWER SETTINGTIME LIMITTQ(%)ITT

( C)

RESERVETAKE OFF10 mn(***)100(**)800

TAKE OFF5 mn90(**)(*)

MAXIMUM CONTINUOUSNONE(***)90.9(**)800

GROUND IDLE

HOTEL (4) MODE715

STARTING5 s950(2)

OTHER800

TRANSIENT5 s

20 s(1) (2)120840

20 mn

ITT Limits see 2.01.04. P3 Do not use engine 2 in HOTEL MODE without a qualified person (flight crew or maintenance) in the cockpit.

Max.HOTEL MODE tail wind is 10 kt

PROPELLERS

GROUND OPS. :

Engine run up must be perform into the wind.

Engine ground ops.with x-wind between 5-20 kt should not exceed 58% TQ.IN FLIGHT OPS.

NP bellow 82% in icing condt. is prohibited.STARTER

3 Starts with a 1 minute 30 seconds max.combined starter running time, followed by 4 minutes off.

OIL SYSTEM

Reserved take off : 55 to 65 psi, Temp. 0-125 C ( Same as take off, max.continous, H-MODE).

20 mn are authorized between 125 C and 140 C.NOTE :

Oil temp. maintain > 45 C to ensure inlet strut de-icing.

Oil temp maintain > 71 C to ensure fuel anti-icing protection in absence of the low fuel temp.indication.

FUEL SYSTEM

Jet A1

REFUELING : Max. pressure 3,5 bars (50 psi)USABLE FUEL : In each tank is 2500 kg (5510 lbs) total 5000kgUNBALANCE : 730 kg (1609 lbs)

FEEDING :

Each electric pump is able to supply 1 engine in whole flight envelope (5 psi)

1 electric pump and associated jet pump are able to supply both engine in whole flight envelope (jet pump 8,5 psi plus 30 seconds).

If jet pump drop < 5psi, the elect.pump is automatically on to supply engine. When low level (< 160kg remaining fuel onwing ctr box) is reach in one tank, its electrical pump is automatically actuated.

Feed low pressure illuminate < 4 psi FUEL CLOG light illuminate pressure < 45psi on corresponding HP pump fuel filter.FIRE PROTECTION Pulling the handle electrically causes:

1. PROPELLER

Feathering

2. FUEL

ENG LP VALVE closure

3. AIR

BLEED VALVE and HP VALVE closure

4. DE ICE

DE ICE VALVE and ISOLATION VALVE closure

5. ELEC

ACW and DC GEN deactivation

6. ALERT

SQUIB lights illumination

Detection for : each emgine fire, right nacelle overheat (on GRD only), each cargo compartment & toilets smoke, avionics compartment smoke.

EXTINGUISHING for : each engine, cockpit, cabin and each cargo compartment, toilets waste bin.

AIR PRESSURIZATION

Max. DP : 6.35 psi

Max. Negative DP : -0.5 psi

Max. DP for landing : 0.35 psi

Max. DP Pressure for OVBD valve full open selection : 1 psi

Max. Altitude for one bleed off operation : 20 000 ft

NORM MODE : On descent is -400 ft/mn, FAST (pressed in) 500 ft/mn

MANUAL MODE : MAN Rate -1500 ft/mn to +2500/mnELEVATION SET : -1500 FT AND 9900 FT

PNEUMATIC SYSTEM

The aircraft uses external air to supply :

1. The air conditioning & the ventilation systems

2. The pressurization system

3. The de-icing system Bleed auto closed, when: 1. Bleed duct OVHT

4. Eng. Fail (UP TRIM)

2. Bleed duct LEAK

5. Prop. BRK ON (left vlv only)

3. Eng. Fire handle

Air is generally bled from the low compressor stage (LP). At low engine speed when pressure from LP stage is insufficient, air source is automatically switched to the high compressor stage HP.(This may occur on ground and during descent at F.I).ELECTRICAL SYSTEM

Sources :1. MAIN (43 VDC A24V Ni-Cd) and EMERGENCY (15 VDC A24V Ni-Cd) Batteries.

2. Two (2) Engine-Driven DC starter/generators : 28 VDC and 400A.

3. Two AC Wild frequency generators 20KVA (consists two inverters/INV 500VA) :

Output voltage 115V +/- 4V and 26V +/- 1V Frequency 400Hz +/- 5Hz, type single phase.

4. Two External Power units (AC and DC), 28V but after load saving not less than 26V.

TRU 60A, 90A for 5 minutes.

In flight if OAT > ISA +25, Fl lvl limit to Fl 200. DC Eng.Driven > 45% NH = 61% ready used.

AC Acc Gear Box 66 % NP ACW ready used AC Pwr.

DC voltage indi : for battery without load : 25-28 volt, under load 23-28 volt.

DC current indi normal read for each GEN less than 300A.

HYDRAULIC

Hydraulic has 2 systems blue and green with 3 pumps; 2 Main and 1 Aux.Pump. Main pumps 3000 Psi pressurized by ACW elect.mtr driven pump. Aux.DC mtr driven Pump fitted with Blue cct and operate when MAIN lo press < 1500psi. Aux pump avail > 1600psi for Emergency and Pkg.Break Aux DC hyd.pump push button energize for 30 seconds.

Blue system supplies : 1.flap, 2.spoiler, 3.nose wheel steering, 4.prop.brake, 5.emerg and parking brake through specific accumulator.

Green system supplies : 1.landing gear, 2.normal brake. LO PR light ill.1500psi, LO LVL ill. < 2.5ltr.LANDING GEAR VLE = 185ktVLO RET = 160kt

VLO LOW = 170kt

Wheel steering angle is +/- 60 , Nose wheel deflection of +/- 91% is possible during towing with no press.in the system. Min.pavement width for 180 turn is 70ft (21.40m), Ex.: Left main wheel to right wing left turn (R4) is 64ft (19,74m) Left main wheel to nose A/C left turn 90 (R5) is 45ft (13,96m)

Left main wheel to nose wheel left turn 90 (R3) is 40ft (12,43m)

Centre of bailey to main wheel is 20ft (26,21m) = MW to MW 40ft (12,42m)* Fusible plugs are descend to release internal pressure when the wheel tempt exceeds 177C/350F

Antiskid system provided as soon as gear is down and locked, aircraft speed exceeds 10kts. Antiskid test pb : 6s on grd, 3s on air (the test is inhibited when wheel speed > 17kt)

Locked wheel protection for velocities > 23kts a speed differential of 50% or greater between the two speed signal, and thus in release of break.

Touch down protection : at main gear compression, the braking action is inhibited as long as wheel spin up < 35kt or for 5s. Brake temp over 150 C; BRK TEMP HOT ill. See 2.05.07. P7

MFC Take off with two or more failed MFC modules is prohibited. Has two separate electrical supply primary and alternate : From primary to alternate if primary V < 19 V and if alternate > 22 V

From alternate to primary if primary V > 22 V

AFCS It achieves : A/P function and/or Y/D, F/D function, Altitude Alert Mini height for A/P engagement after take off : 100ft

Mini height for use of either A/P or F/D : except during take off or executing an approach : 1000ft

VS or IAS mode during approach : 160ft

CAT1 APP mode

: 160ft

CAT2 see 2.02.04.P8

NAV MODE for VOR approach, using either A/P or F/D is authorized only if :

a co-located DME is available, and

DME HOLD is not selected

BANK pb : Hi Bank 27 , Lo Bank 15

TCS (Touch Ctr Steering) pb : Pitch Att.Re-synchronization limits +/- 15

Bank angles limits 6 35 , and will center if less than 6. At Bank greater 35 A/P will return 35.FLIGHT CONTROL

Holding with any flaps extended is prohibited in icing conditions (except for single engine ops). Spoiler deployed when aileron exceeds 2,5

TLU (Travel Limitation Unit : done through ADC when reaching 185kt during acceleration and when reaching 180kt during deceleration. FLAP UNLK spurious > 4 , Flaps Assymmetry > 6,7 during actuation.

ICING

All icing detection lights must be operative prior to flight into icing conditions at night

The ice detector must be operative for flight into icing conditions.

Icing conditions definition :

Visible moisture

Temp.SAT < 5 C on ground or at take off , TAT < 7 C in flight.

Visibility less than 1Sm In normal ops.the stick shaker threshold is set at -12 AOA with flaps 0, when ICING AOA light ON stick shaker threshold reduced at -7

- Icing Electrically : Windshields, Probe, Ice evidence, Propellers, Horns wing & Elevator, Electronic ice detector.

- De-Icing Pneumatically : Gas path de-icer, Engine air intake, Wing leading edge, Horizontal tail plane leading edge.

OXYGEN An excess altitude warning is activated if cabin alt.reaches 10000ft. Three (3) quick donning oxy.mask and smoke googles in the cockpit High pressure cylinder 3310L (115 cu.ft) supplies to distribution system/ nominal press.1850psi is reduced to 78psi in the distribution system.

Diluted oxygen provided 2 pilots and 1 obs.: 120mn at demand flow (N/normal position). In case of smoke or noxious gas emission oxygen provided 15mn at demand flow (100% position).

19 oxygen mask 30mn diluted oxy.supply. Two (2) portable oxy.bottles 120 L (4,25 cu) under press (1800psi) 30mn to both cabin attendants (under cab.seat).

See page 2.01.05 P2COCKPIT PHILOSOPHY

PB POSITIONBASIC FUNCTION

IN (DEPRESSED)

OUT (RELEASED)On, Auto, Normal

Off, Manual, Altn, Shut

COLORINDICATION

No light ill.except flow bars (DARK COCKPIT)

BLUE

GREEN

WHITE

AMBER

REDNormal basic operationTemporarily required system in normal operation

Back up or alternated system selected

Selection other than normal basic operation

Caution indication

Warning indication

INSTRUMENT MARKINGSRED ARC OR RADIAL LINE : MINIMUM AND MAXIMUM LIMITS

YELLOW ARC : CAUTION AREAGREEN ARC : NORMAL AREA

TCAS The fixed aircraft mock-up is surrounded with a 2mm loop.

ABV viewing : 2700ft below to 9900ft above.

BLW viewing : 2700ft above to 9900ft below. Intruder symbol :

TCAS RA : filled square (red) CORRECTIVE ACTION TO DO

TCAS TA : filled circle (amber) TRAFFIC, TRAFFIC. CPA is between 20-48 seconds. Proximity : filled diamond (Cyan) Tx in the Proximity Others : blank diamond (Cyan) Tx in the Visinity Arrow : climbing or descending greater than 500ft/mn.

TA may become RA within 15 seconds.

A typical TCAS II maneuver req.crew response within 5 seconds and G-forces of +/- 0,25G.

CABIN LIGHTINGThe general cabin illumination system must be used during not less than 15 minutes before each flight.ATPCS ARMING CONDITIONS :

- T/O or ON GRD: PWR MGT selector TO

ATPCS pb ON

Both PL above 49

Both TQ >46%

Aircraft on ground ( uptrim and auto feathering functions armed. - APP or IN FLT: PWR MGT selector TO

ATPCS pb ON

Both PL above 49

Both TQ >46%

Aircraft in flight ( auto feathering functions armed.

Armed ON GRD, uptrim is triggered and bleed vlv is shut off on the remaining engine, and autofeather is activated pd engine yg mati setelah 2,15s.

Armed IN FLT, autofeather is activated on the effected engine after 2,15s.

2,15s this feature enables to perform an acceleration stop without having autofeather in order to benefit from some reserving action on the failed engine. cancellation by: 1) PWR MGT other than TO, 2) ATPCS pb set to OFF, 3) both PL retarded.

CAUTION : If the engine is restarted, IT WILL BE NECESSARY TO SELECT PWR MGT to MCT position after relight in order to be able to UNFEATHER the propeller.

T/O CONFIG red light lt :1. FLT CTL when pitch trim and/or FLAPS not in TO configuration.2. AIL LOCK is illuminated : disagree the gust lock ctr and the actuator.

3. ENG when PWR MGT not in TO position.

4. TLU FAULT lt if not in LO SPD configuration.

5. Pressurization in AUTO position.T/O INHI( PRKG BRK, GPWS FAULT, MAINT.PANEL, ENG.oil, SMOKE warning & Associated Aurel Alert; cancel by : 1) one gear leg is not locked down, 2) by pressing RCL pb.

Pre-flight Preparations Procedure :

Shall Cx the following items :1. A/C Condition : Defect or DMI

2. NOTAMs : AED, RWY, TWY etc.

3. WX Briefing : T/O, EN RTE, DEST.,ALN.

4. Airport Infrastucture : At Destination/ALN.5. Specifics : Noise Abt. on Tx, TO or arrival.

6. Flight Planning : Via RTE, FL Time (limit W and cargo can add.or not).7. Fuel Planning : (plus icing and aln.1st or 2nd)

8. Flight Presentation : Ex.noise abt.when Tx

9. Flight Attendant Briefing :

Cx licence, schedule/revise, what day, job disc., emg.proc., time

TORQUE PRESET

NP = 86/82%Level flightApproach

3

Speed

180160140120VAPP

Gear

UPUPDOWNDOWNDOWN

Flaps

001530/3530/35

All engine torque

50%40%40%50%25%

All engine pitch

+1+1+2+2-1

Single engine torque

90%75%75%90%50%

Single engine pitch

+1+1+2+2-1

+/- 3% TQ ( +/- 1 percent slope; +/- 5% TQ ( 1 degree slope; +/- 5% ( +/- 10kt wind compn.BEST ANGLE AND BEST RATE SPEED

2 ENGINES

1 ENGINE

NORMAL

CONDITIONS

BEST ANGLE =

WHITE BUG

BEST RATE =

WHITE BUG +10WHITE BUG

ICING

CONDITIONS

RED BUG

WHITE BUG

SPEED BUGS

TAKE OFF BUGS :

Green Bug( V1set when V1 = VR (when rwy limited (set 12 oclock when not used)).

Yellow Bug( VRwhen limiting runway

V1/VR when non limiting runway

Speed Bug( V2 (Amber)White Bug( FLAPS RETRACTION SPEED (VmLBO), Normal Conditions.

Single engine climb speed Flaps 15 (VmLB15)

White Bug +10 ( HIGH BANK (VmHBO), Best climb rate speed Flaps 0

Red Bug( Icing Conditions; FLAPS RETRACTION SPEED (VmLBO)

Red Bug +10 ( Icing Conditions; HIGH BANK

CRUISE BUGS :White Bug( Nml Cond; DRIFT DOWN SPEED Flaps 0 MINI EN ROUTE (VmLBO)

Icing Cond; DRIFT DOWN SPEED Flaps 15 (VmLB15)

Red Bug( Icing Cond; MINI EN ROUTE Flaps 0 (VmLBO)

Speed Bug( Cruise speed (Amber)

APPROACH BUGS :

Yellow Bug( VGA = Greatest : VAPP no wind + 5kt or 1,1 Vmca

Speed Bug( (Amber) VAPP = VAPP no wind + wind factor

White Bug( FLAPS RETRACTION SPEED (VmLBO), Nml Conditions.

Single engine climb speed Flaps 15 (VmLB15)

White Bug +10 ( HIGH BANK (VmHBO), Best climb rate speed Flaps 0

Red Bug( Icing Cond; FLAPS RETRACTIONS SPEED (VmLBO)

Red Bug +10 ( Icing Cond; HIGH BANK

LIGHTS POLICY

NAV

Airplane electrically suplied

WINGS

Engine 2 running in Hotel mode

BEACON

Propeller rotation

TAXI & T/OAirplane taxing

LAND

Line up to FL 100

FL 100 to runway vacated

STROBES

Lining up and flight up to runway vacated LOGO

Company advertisement

BRIEFINGS Departure briefing :

All departure setting must be ready before performing briefing. Are you ready for departure briefing?

Status Weather conditions (icing, thunderstorm, wind)

A/C technical situation (technical concern, MEL restriction)

Specific flight items (NOTAMS, de-icing)

Taxi Taxi out description Specifics (contamination, taxiway closed) Runway in use and expected holding pointRunway- Limitations, specifications, bleed, anti-icing (fluid type)SID (Standard Instrument Departure) : When clearance departure is received from ATC, you must check it is in compliance with the expected SID :

a. Is actual SID in compliance with the prepared one?

b. Is altitude clearance in compliance with MSA/SID climb instruction?

c. Set squawk code.

If clearance is not amended, PF announces : no change.

Take-off briefing : Take-off RWY____, Weight____, V1____

If failure before____kt, I (you) stop the aircraft.

If failure at or after____kt, we continue HDG____, acc.alt.is____, MSA is____

The single engine flight path shall be read on FOS chart.

Example : FO will be PF in flight, so he performs the take-off briefing :

Are you ready for take-off briefing? Take-off runway 25L, weight 16 tons, V1 100kt, normal/icing condition. If failure before V1 you call STOP and stop the A/C. (etc are the same). Arrival briefing :

Top of descend (TOD)Expressed in distance (time for information) and MSA.

Particularities:

A/C DMI or push RCL

NOTAM

Airport equipment

Etc

Alternate and holding time:

Holding time before diversion

Wx at destination:Visi / RVR compare to minima : Airport accessible or not and icing orApproach procedure: (See and read App.Chart)

Radio-navigation setting : (for the final approach)LONG TRANSIT :

FCTM Internal inspection

02.02.03.P2

External inspection

02.02.03.P4

Preliminary cockpit preparation ( long transit)

02.02.03.P16

Final cockpit preparation

02.02.03.P22

SHORT TRANSIT :

FCTM External inspection

02.02.03.P4

Preliminary cockpit preparation (short transit)

02.02.03.P22 Final cockpit preparation

02.02.03.P24STARTING SEQUENCES* HOTEL MODE, Svc.DoorClosed, Wg.LightsOn, Prop.BrakeOn, Eng.Start Sel.A+b(AorB)Start Sw :

Timing (for 1.30s the 1st 3 start,next 4min off) Starter 2 Check on (30s maxi when starter off)* CL 2. FEATHER, TIMING.START

FUEL OPEN.. ITT should rise within 10s* ITT increasing.IGNITION (Timing stop)

- Check engine parameters

* NH increasing. OIL PRESS

* NH 45 % . Starter Off

ITT Max. Check, Timing Stop

* NH 61,5 %.... PARAMETER STABILIZED CM2( ENGSTARTOff, DC EXT PWR.Off/Disc, DC GEN2 FAULT.Extinguished, DC BTC. Check Closed, BLEED/ PACK/ X-VLV.Open - CM1. Check DC GEN 2 Voltage, Disconnect GPU.MISCELLANEOUS- Preparation for emergency landing or ditching :

1. Inform Cabin crew

2. Inform Passengers

3. Passangers preparation

4. Cabin preparation

5. Emergency equipment preparation

6. Final action :

Check all orders enforced

Inform the flight crew : Cabin ready for emergency landing (or ditching)

Seat down and fasten your harness after carrying out your own preparation.

An announcement is made by the Flight Crew 1 minute before the crash

Order the passengers to take the safety position 30 seconds before crash

A few seconds before crash order the passengers : brace-brace

7. Evacuation

- Refueling with passengers aboard :

> Passengers Instruction :

* No smoking (this order has to be repeated through the PA)

* No electrical switch operations

* No boarding or disembarking if the pax have not received the instructions

* Escape paths free from obstacles

> Cabin Instructions :

* Emergency lights ON or ARMED

* Opened doors equipped with stairs

* Curtains secured in open position

> Crew Instructions :

* Cabin survey by the Flight Attendants :

* Orders enforced (no smoking)

* Senior FA close to the main emergency exits

* Second FA in the front of the cabin

> Ground Instructions :

* No obstacle in front of the emergency exits

* Those responsible for refueling and airport safety service informed that pax are aboard

* Airport safety service available

* Extinguishing devices close to the aircraft- 5 syarat FA boleh melakukan evakuasi :

1. 10 detik tidak ada pemberitahuan dari cockpit

2. Pesawat berhenti

3. Mesin pesawat mati

4. Tidak ada api di luar pintu pesawat

5. Apabila pswt rusak berat atw when Dithcing air sdh masuk ke pesawat- Cara melakukan CPR /Nafas buatan 100x/mnt, 30/2x kasih nafas, RJP (di kejut listrik).- Sudden death harus ditolong within 6 mnt supaya hidup kembali.PRE-FLIGHT CHECK

Aircraft Systems :

1. Interphone

2. Smoke detectors

3. Automatic extinguishers

4. Emergency lights

5. Emergency exits

6. Lighted signs

7. Calls

8. Public Address (PA)Emergancy Equipment1. Seat belts

2. Safety instruction cards

3. First aid kits

4. Portable exthinguishers

5. Crash axe (if any)

6. Megaphone

7. Flash lights

8. Oxygen systems :

Sustenance oxygen

Protective breathing equipment

First aid oxygen (if any)

9. Life jackets (if any)10. Rafts (if any)

11. Survival kits (if any)

12. Emergency locator transmitter (if any)TAKE OFF SEQUENCEFlight

Events

CM 1CM 2

READY TO

TAKE OFF> ANNOUNCETAKE-OFF AT XXX OCLOCK

V1 XXX KT> DO TIMING.START

NOSE WHEEL STEERING.HANDED

Pls.NOTCH

> ANNOUNCE

SET POWER> DO

TIMING.START CONTROL WHEEL.HOLD TOWARD

WIND

ATPCS ARMED, POWER SET

70 KT READ ON THE STBY ASI & CM2 ASI

> ANNAOUNCE & DO : CHECK NOSE WHEEL STREERING. RELEASED

YOUR CONTROL / MY CONTROL> ANNOUNCE : 70 KTS

PNFPF

FL.CTRL.TRANSFER> ANN : I HAVE CONTROL

REACHING V1> ANN : V1CM1 : DO.PLs RELEASED

REACHING VR> ANN : ROTATE (YELLOW BUG)

DO : PITCH.ROTATE 10 & FOLLOW FD BARS

POSITIVE RATE> ANN : POSITIVE RATE

DO : L/G.Up; Y/D.On; Tx & TO Lt.Off

ORDER : GEAR UP

ALL LIGHTS OFF ON L/G PANEL> ANN : GEAR UP

CONT.ACCELERATE TO V2 + 5

REACHING ACC.ALT.> ANN : ACCELERATION ALTITUDE

DO :

* Two times tumb wheel * PLCx Notch

* PWR MGT-CL * BleedOff/On

* CxTQ % * Fine TuneV 170kts

> ANN : CLIMB SEQ.COMPLETE DO : PLCHECK IN THE NOTCH*

ORDER : CLIMB SEQUENCE

CRUISE PARAMETERSPNF reads SAT by depressing the SAT pb & determine the ISA deviation.

Ex. FL200, in std ISA Sea lvl 15*C & Decrease by 2* each 1000ft, pressing SAT is -25*.

So FL200 std temp.= 15*C-20x2*C=-25*C (Take FCOM/ QRH Compliance Crz Weight)FLIGHT FUEL MANAGEMENT

1. Fuel used versus distance (in Kg/Nm) = FF/GS

2. FU to DEST (in Kg) = actual FU + (dist.to go x Fuel used versus distance) = X

3. Remaining Fuel at Destination (in Kg) = FOB* - X = RF

4. Holding quantity (in Kg) = RF (alternate fuel + final reserve) = HF

5. Estimated maxi-holding time (in min) =

HF/10 for all other ATR type (i.e. 600kg/h**)

* FOB : Fuel On Board before engine start

**Please refer to FCOM for exact value

NORMAL GO-AROUNDFLIGHT EVENTSPNF

ANN. : MINIMUMPF

DA OR MDA (RUNWAY OR RAMP NOT IN SIGHT) OR OTHER EVENTS UNXXPECTED

WHEN FLAPS AT 15 ON THE FLAPS INDICATOR> DO :

TQs.CHECK/ADJUST GA

FLAPS 15.SELECTED

> ANN.: FLAPS 15, POWER SET> ANN.: GO-AROUND, SET POWER, FLAPS ONE NOTCH> DO :

- GA PB ON PL..DEPRESSED

- ROTATE.GA PITCH (+8 NOSE UP)

- PLs.ADVANCED TO RAMP

- CAVALRY CHARGE.CANCEL

POSITIVE RATE> ANN. : POSITIVE RATE, vsi + alt.incrs> DO :

- GEAR LEVER.UP

- HDG MODE.SELECTED

- LO BANK.SELECTED

- IAS.VGA SELECTED/WHITE BUG

- TAXI & T/O LIGHT.OFF

> ANN.: IAS XXX SET

> DO & ANN.: SET> ORDER : GEAR UP, HEADING, LOW BANK, IAS VGA (W/B)> ANN.: CHECK

> ORDER & DO : SET SPEED BUG VGA (W/B)

WHEN ALL LIGHTS OFF ON THE L/G PNL> ANN. : GEAR UP

REACHING ACC.ALT. NOTE : MINI 1000FT AGL OR HIGHER IF REQ.> ANN. : ACCELERATION ALTITUDE> DO : PL.RETARD TO THE NOTCH

> ORDER : CLIMB SEQUENCE

NB : CONT.AFTER T/O PROC.(i.e W/B OR R/B.FLAPS 0, dst.until after T/O C/L.

SINGLE ENGINE GO-AROUND*** From inisiate (MINIMUM) until GEAR UP are the same actions, but different when reach ACCELERATION ALTITUDE (follow the procedure bellow).FLIGHT EVENTSPNF

PF

REACH ACC. ALT MINI 1000ft AGL OR HIGHER IF REQUESTED > ANN. : ACCELERATION ALTITUDE> DO & ANN. :

ALT PB ON AFCS. DEPRESS

ALT GREEN

> DO & ANN. : SET

> ORDER : SET ALT> DO & ANN. :

ALT GREEN ON FMA..CHECK

CHECK

> ORDER AND DO

SET SPEED BUG WHITE BUG

REACHING WHITE BUG> ANN. : WHITE BUG> DO & ANN. :

IAS PB ON ADU.DEPRESS

IAS XXX SET

> DO & ANN. : PWR MGT.MCT

TORQUE ADJUSTED/CHECK IN THE

NOTCH MCT SET

> DO : FLAPS LEVERSET AS RQRD> ORDER : SET IAS> ORDER : SET MCT

> ORDER :

NORMAL CONDITIONS, FLAPS 0

OR

ICING CONDITIONS, REMAIN FLAPS 15

WHEN FLAPS AT EXPECTED POSITION ON FLAPS INDICATOR> ANN. : IN NORMAL CONDITIONSFLAPS 0

OR

IN ICING CONDITIONS

REMAIN FLAPS 15

ENGINE FLAME OUT AT TAKE-OFFFlight eventsPNF

PF

ENGINE FLAME OUTFirst crew detects failure announces loudly :

ENGINE FAILURE

POSITIVE RATE> ANN : POSITIVE RATEDO : ASSOCIATED ACTION

ORDER : GEAR UP

ACTIONS TRIGGERED BY PNF WITHOUT PF REQUEST, JUST AFTER GEAR RETRACTION SEQUENCEDO, CHECK & ANNOUNCEENG 2 (or 1) UPTRIMMEDENG 1(or 2) AUTOFEATHERED,

(TWO) BLEED FAULT LIT

If no UPTRIM, PF orders corrective actions before acceleration altitude

L/G PANEL ALL LIGHT OFF> ANN : GEAR UP

REACHING ACC.ALTITUDE> ANN : ACCELERATION ALTITUDEDO & ANN : ALT GREENDO & ANN : SETORDER : SET ALTORDER & DO : SET V BUG W/B

REACHING WHITE BUG> ANN : WHITE BUGDO & ANN : IAS XXX SET

DO & ANN : MCT SET

DO : FLAPS LEVERSET AS RQRDORDER : SET IASORDER : SET MCT

ORDER : NML CONDT.FLAPS 0/ICING CONDT.FLAPS REMAIN 15

WHEN FLAPS AT 0/15 ON INDI> ANN : FLAPS 0 or REMAIN FLAPS 15

WHEN FLIGHT PATH STABILIZED> DO & ANN. POINTED AT WITH FINGER PL CONFIRM CL1(or 2)?; FTHR THEN FUEL SO BLEED OFF IF NECESSARY, YES

OR NO?

MEMO ITEMS COMPLETE> DO, ANNOUNCE & POINTED : ENG.FLAME OUT AT TO C/L?

>ORDER, DO & ANN. :ENG.FLAME OUT AT TO MEMO ITEMS

PL 1 (or 2)?, FLIGHT IDLE

CONFIRM

BLEED OFF or BLEED ON

> REQ : ENG.FLAME OUT AT TO CL, RADIO MY SIDE

> TRANSMIT : PAN PAN 3X, CALL SIGN, ENG.F/O, I CALL U BACK

> C/L CHECK BY PNF : CONFIRM

PNF READS C/L> READ, CHECK, DO & ANNOUNCE :

> ANSWER; NO or YES

WHEN C/L COMPLETED> DO : CAP CLEARED> ANN & READ : AFTER TO C/L

> ANN : CHECKLIST COMPLETED> ANN : CLEAR CAP> REQ : AFTER TO C/L

> DO & ANNOUNCE :

SINGLE ENG.OPS.CHECKLIST?

> ANN : C/L COMPLETE RADIO MY SIDE

>ANN : SINGLE ENG.OPS.C/L!

C/L BY PNF, CONFIRM

>ANN : (When C/L COMPLETED),

RADIO YOUR SIDE

PF SUMS UP SITUATION> DO : INFORMATION> DO : SUM UP (Press Recall) DECISION

INFORMATION

SUMS UP : READY FOR ASSESSMENT?, GO HEAD

: TECHNICAL : WE HAVE.FAILURE, . ALL SYSTEM ARE AVAIL.

: OPERATIONAL : NO PERF.IMPACT, DEST.AIRPORT IS ACCESSIBLE.

: COMMERCIAL : NO CONSEQUENCE

PF ANN. : I SUGGEST WE (FO:YOU) CONTINUE (OR NO CONT.) TO DEST., &

WRITE IT DOWN IN MAINTENANCE LOG, NOBODY NEEDS TO BE

INFORMED, EXCEPT COMPANY, IF YOU AGREE.

CAPTAIN: I AGREE.ENGINE FIRE AFTER TAKE-OFFBasicly sama dgn engine flame-out tp perbedaan di ACC.ALTITUDE push INCREASE IAS TO W/B+ IN FLIGHT ENG. FIRE MEMO ITEMS-nya+ IN FLIGHT ENG. FIRE CHECKLIST-nya (s/d fire handle pulled and discharged).ENGINE FIRE B4 V1 & EMG. EVACUATION

Flight eventsCM 1CM 2

ENGINE FIRE

> ANN. LOUDLY : STOP!!

REDUCE PLs...GI/REV AS RQD BRAKES..FULL APPLICATION

> ANN : ENGINE FIRE CRC/MASTER WRNG....CANCELLED

CTRL WHEEL...HOLD AS REQUIRED

ATC (VHF1) CALLED

MAYDAY 3X, XXX (CALL SIGN), ENG. FIRE, ABORTED TAKE OFF.

> ANN. (on Public Address)

PLEASE, REMAIN SEATED, CABIN CREW AT STATION.

If possible, stop the aircraft to get the engine on fire head wind or to leeward

A/C STOPPED + PARKING BRAKE ON> DO : P/B ON

> ANN. & DO : ON GROUND ENG.FIRE MEMO ITEMS

> ANN. & REQUEST : MEMO ITEMS COMPLETE, ON GROUND ENG.FIRE C/L

> DO : CM1 ACTIONS. MONITOR

TIMING. START

> DO : QRH EMG. C/L. OPEN

CL REQ.BY CM1

FIRE NOT EXTINGUISHED

> ANSWER : YES

> REQUEST AND ANSWER :

ON GROUND EMER EVACUATION C/L> READ & ANN. : ON GROUND ENG.FIRE C/L AND PERFORMS C/L!!!> ANN : IF EVACUATION REQUIRED, YES OR NO?

> READ : ON GRD.EMG.EVACUATION PROC.(1.02). APPLY

ON GROUND EMER EVACUATION C/L

EVACUATION REQUIRED> ANN. : WE EVACUATE then on PA

EVACUATION, EVACUATION, EVACUATION

> DO & ANN. :

BATT TOGGLE SWITCH.. OFF

OFF

- MIN CABIN LIGHT.. ON

- FUEL PUMPS 1+2.. OFF> READ AND ANN. : ON GROUND EMER EVACUATION C/L> EVACUATION. INITIATE

> READ & ANN. :

BAT. OFF

EMERGENCY DESCENDFlight Events

PNFPF

ACCORDING TO FLIGHT EVENT OR MASTER WARNINGKAPITAN >> ORDER :

EMERGENCY DESCENT MEMO ITEMS

AUTOPILOT REMIND ENGAGED

>DO: O2 MASK+CREW COM... ESTB CAPT/COPIL OXY ON, RDO UR SIDE

- 02 PAX SUPPLY.ON- SEAT BELTS...ON- XPDR.7700>ANNOUNCE (ON PUBLIC ADDRESS)EMG DESCENT, REMAIN SEATED

> DO

- MINI SAFE ALTITUTE..CHECK

- ALT SEL....MSA SELECT

> ANN : MEMO ITEMS COMPLETE

> DO

CHECKLIST PREPARE

> ANN : EMG DESCENT CHECKLIST

>DO: 02 MASK+CREW COM.ESTB CAPT/COPIL OXY ON, RDO MY SIDE

- ALT.SEL LOWEST ALT.SELECT

- IAS MODE... SELECT

- HDG MODE.SELECT

- HDG KNOB...TURN +/-45

According to flight conditions

- PLs...FI

- CLs.MAX RPM/100% OVRD- FINE TUNE>ANNOUNCE (ON VHF1)

MAYDAY 3X, XXX (callsign), EMG. DESCENT, CONFIRM MSA.

> ORDER EMG DESCENT CHECKLIST

> DO

SPEED...ADJUST

Accdg. to potential structural damages

HEADINGADJUST

Accdg. To flight path (AWY, ATC).

(+/- 1000ft before SET IAS 210, CLs AUTO, HDG, Cx PARALEL).

APP. FL 100> DO: OXYGEN MASK....REMOVE

> ANN: BREATHING NORMALLY

> DO :

OXYGEN HATCH..CLOSE

OXYGEN TEST PBDEPRESS> ANNOUNCE YOU CAN REMOVE OXY MASK> DO

OXYGEN MASKREMOVE

OXYGEN HATCH..CLOSE

OXYGEN TEST PBDEPRESS

WHEN NORMAL RATE OF DESCENT AVAILABLEKAPITAN

> DO : FLIGHT ATTENDANT REPORT.REQUEST

ASSESMENT DECISION INFORMATION (A,B,C,D)

MEMO ITEMS1. IN FLIGHT ENG FIRE OR SEVERE MECHANICAL DAMAGE (1.02)PL affected sideF1

CL effected sideFTR THEN FUEL SO

FIRE HANDLE affected side.PULL

If condition persist after 10 seconds

FIRST AGENT affected side.DISCH

If condition persist after 30 seconds

SECOND AGENT affected side.DISCH

LAND ASAPSINGLE ENG OPERATION procedure (2.4)..APPLY2. ON GROUND ENG FIRE OR SEVERE MECHANICAL DAMAGE (1.02)PL 1 + 2..GI/REVERSE AS RQD

When aircraft stoppedPARKING BRAKE...ENGAGE

CL 1 + 2......FTR THEN FUEL SO

FIRE HANDLE affected side..PULL

If condition persistFIRST AGENT affected side .DISCH

If condition persist after 30 seconds

SECOND AGENT affected sideDISCH

If evacuation required ON GROUND EMER EVACUATION (1.02)..APPLYON GROUND EMER EVACUATION (1.02)AIRCRAFT/PARKING BRAKE..STOP/ENGAGE

AUTO PRESS ..DUMP

ATC (VHF 1).NOTIFY

CL 1 + 2FTR THEN FUEL SO

MIN CAB LIGHT...ON

CABIN CREW (PA)..NOTIFY

FIRE HANDLES 1 + 2...PULL

AGENTSAS RQD

ENG START ROTARY SELECTOR..OFF/START ABORT

FUEL PUMPS 1 + 2.OFF

EVACUATION (PA)..INITIATE

Before leaving aircraftBATOFF

3. ENG FIRE AT TAKE OFF (1.02A) When airborne

LDG GEAR ..UP

At Acceleration Altitude

PWR MGT ...MCT At VFTO

If normal condition

FLAPS ...0O If Icing conditionFLAPS ...MAINTAIN 15OPL affected side .FI

CL affected side .FTR THEN FUEL SO

FIRE HANDLE illuminated .....................................................PULL

If fire persist after 10 secondsFIRST AGENT affected side .....DISCH If fire persist after 30 secondsSECOND AGENT affected side DISCH

BLEED engine alive . OFF if necessary

LAND ASAPSINGEL ENG OPERATION procedure (2.04) . APPLY4. BOTH ENGINES FLAME OUT (1.03)PL 1 + 2..FI

If NH drops below 30% (no automatic relight)

CL 1 + 2 .FTR THEN FUEL SO

5. ENG FLAME OUT AT TAKE OFF (1.04)UPTRIM...CHECKAUTOFEATHER ....CHECK

If no UPTRIM PL 1 + 2....ADVANCE TO THE RAMP When airborneLDG GEAR ..UPBLEEDS 1 + 2 ...OFF, IF NOT FAULT At Acceleration Altitude

ALT .SET

At VFTOPL 1 + 2 ..IN THE NOTCH

PWR MGT MCT

IAS ..SET

If normal conditionFLAPS .0O If icing conditionFLAPS .MAINTAIN 15OPL affected side..FI

CL affected side..FTR THEN FUEL SO

BLEED engine alive..OFF if necessary

6. SMOKE (1.05)CREW OXY MASKS...ON/100%

GOGGLES..AS RQD

CREW COMMUNICATIONSESTABLISH

RECIRC FANS 1 + 2.OFF

APON

7. DUAL DC GEN LOSS (1.07)DC GEN 1 + 2.OFF then ON

If no generator recovered

HYD GREEN PUMP..OFF

TRU..ON

8. EMERGENCY DESCENT (1.07A)OXYGEN MASKS/CREW COMMUNICATIONS..AS RQD

GOOGLES..AS RQD

DESCENTINITIATE

PL 1 + 2.FICL 1 + 2100% OVRD

9. SEVERE ICING (1.09)MINIMUM ICING SPEED......INCREASE RED BUG by 10 kt

PWR MGTMCT

CL / PL..100 % MCT

AP (if engagedFIRMLY HOLD CONTROL WHEEL and DISENGAGE

SEVERE ICING CONDITIONS....ESCAPE

ATC.NOTIFY

10. RECOVERY AFTER STALL or ABNORMAL CONTROL (1.10)CONTROL WHEEL PUSH FIRMLY

If flaps 0O configuration

FLAPS 15OPWR MGT MCTCL/ PL ..100% / MCT

ATC NOTIFY

If flaps are extendend

PWR MGT .MCT

CL/PL ..100% / MCT

ATC ..NOTFY

11. UNRELIABLE AIRSPEED INDICATION (1.10)

AP/YD/FD BARS OFF/OFF/STBY

PITCH AND TQ .MAINTAIN

If at take off or GA below 1500 ft:

PITCH IMMEDIATELY ...8OICING / VOLCANIC ASHES CONDITIONS ..ESCAPE

12. ABNORMAL PARAMETERS DURING START (2.05) If ITT tends to exceed 900 C, or no ITT, or no NH

CL affected side FUEL SO

ENG START ROTARY SELECTOR..OFF / START ABORT

Then refer to relevant procedure: ...13. FIRE LOOP FAULT (2.06)

LOOP affected .OFF

14. ENG FLAME OUT (2.10)PL affected side.FI If NH drops below 30 % (no immediate relight)CL affected side FTR THEN FUEL SO

15. PEC FAULT (2.10A) If in short final approach (below 400ft RA)

GO AROUND procedure...APPLY

16. LO PITCH IN FLIGHT(2.11)PL affected side.FI

CL affected side...FTR THEN FUELS SO

17. FLAPS UNLK (2.21) If before V1

Take off.ABORT

If after V1

VR, V2..INCREASE BY 10 KT

If alarm occurs during approach

GO AROUND procedure..APPLY

VGA..INCREASE BY 10 KT

18. ELEVATOR JAM (2.23)CONTROL COLUMNS..UNCOUPLE

19. EFIS COMP (2.31)

If ROL, PIT, ATT, HDG cautions appears on EFISBOTH EADI, STBY HORIZON ....CROSSCHECK

WRONG INSTRUMENT ...IDENTIFY

ATT / HDG PB affected side ...DEPRESS AS RQD

CRUISING LEVEL INDONESIA FIRs AND UIRs IFR/VFR (BELOW FL 200)

RVSM AIRSPACE (Within- Designated Airspace)

IFR (ABOVE FL 200)

Standard communicationDistress (Emergency) messageUrgency (Abnormal) message

(a)MAYDAY; MAYDAY; MAYDAY; (a) PAN PAN; PAN PAN; PAN PAN;

(b) Name of the station addressed (when appropriate and time and circumstances permitting);

(c) Callsign;

(d) Type of aircraft;

(e) Nature of the emergency;

(f) Intention of the person-in-command;

Remember Light Philosophy:

Dark (no light) normal operation

Amber caution

Red emergency

White System is off

Blue status (switched temporary ON by crew)

Green backup (switched temporary ON by system)

Phylosophy; Never hurry; take time to analyze before acting1.Check system (analysis failure) Four check under taken for failure confirmation;

Control:system command in logical position? Reset?

Supply:supply source(s) available?

Circuit breakers:C/B pop out?

Lighting:bulb(s), digit(s) woking?

2.Reset policyAt PF discretion, one reset of a push button of failed system associated with amber caution for 3 seconds. Exceptions: LEAKS, LO LEVEL, EEC,PEC,BUS.

3.Circuit breaker policyIn flight;re-enggage a tripped c/b only if it is juged safe continuation of flight n recorded in maintenance logbook

On the ground;re-enggage c/b provided coordinated with the maintenance team

4.Checklist priorityEMERGENCY-NORMAL-ABNORMAL

Sum up / Decision / InformationSUM UP once C/L is complete PF sum up situation by taking into account three following aspect: T.O.C

Technical assessment: consider consequences of a failure on systems (fuel, electrical, hydraulic, air cond) (helped by pressing RCL push button).

Operational assessment: consider the possibility to land at destination or alternate depending on failure type (i.e degraded anti-icing system and icing conditions reported at destination)

Commercial assesement: consider passenger or crew casualties (e.g.: depressurization) and also in case of diversion, capacity to bring back passenger to destination airport (train, bus), in accordance with operator policy.

DECISION After performing the assessment, PF is able to suggest a decision, validated by Captain

CREW MUST ASSESS BEFORE MAKING A DECISION

INFORMATION

PF and PNF plan together the consequences of failure(s) encountered.

Then PNF inform, if necessary:

ATC - Passengers Flight Attendant - Airline flight operations

Windshear

Recovery procedure at take off:

Delay the take off, if a low windshear is reported, calculate VR,V2 at the maximum take-off weight available fo the day.

If windshear is experienced, do not change the configuration until safe speed and altitude are reached regardless of FD indication, increase pitch to 10degree.

When clear of obstacles, accelerat as much as possible and clear up the aircraft.

Climb at the normal climb speed.

Recovery procedure during an approach:

Initiate a normal go around procedure then increase to 10* pitch, regardless of FD indication.

Be aware of stick pusher.

Do not retract LDG Gear.

When positively climbing at a safe altitude, retract the gear and complete the go around procedure. (by two inst at least 5.,cx v/s increase)

Unusual attitude recovery

1.Stall Recovery, pls refer to AFM 4.05 p7, check-list!

Nose lower

Set Power

Flaps 15* (if a/c is in ldg config.,do not retract flaps to 15*)

2.Bounce Landing, NEVER push forward ctr column, do not try land, PERFORM G/A:

GA pitch

Set Power

Flaps ONE NOTCH, when speed > Vga

3.Hazardous positions; These flight maneuvers are the best procedure (extreme bank angle or extreme pitch att) May be encountered by flying into large aircraft wake vortex, a rotor downwind of a mountain range, sever turbulence or mechanical failure, etc

NOSE UP:

Eyebrow guidance to nose down

Simultaneously max power let nose lower (follow eyebrow if it appears)

With nose below horizon: roll out, stop descend, adjust power

NOSE DOWN:

Eyebrow guidance to nose up

Simultaneously power to flight idle/ level wings

Pull back smoothly (follow eyebrow if it appear)

With nose on horizon: stabilize, adjust power

Wake turbulence (turbulence encountered during approach or take off)

ATR BEHINDAPPROACHTAKE OFF

LIGHT/MEDIUM 3 NM

(2,5 NM according ATC)EXPECT TIME SEPARATION: 2 to 3 Min

HEAVY (>136 T) 4 NM (B-747)ACCORDING ICAO DOC 4444

Incapacitation

RECOGNITION:

If crew member does not respond appropriately to two verbal communication and comm.associated with a significant deviation from a standard flight profile

Other symptoms beginning active incap are:

Incoherent speech

Stranger behavior

Irregular breathing

Pale fixed facial expression

Jerky motion that are either delayed or too rapid

ACTION:

FLIGHT; Handling pilot shall following sequence n cx-list, use A/P n headset, safe flight path n announce I have control.

INCAPACITATION; must ensure incapacitated pilot cannot interfere with a/c control, call f.a to lock the sick pilot on his crew seat, f/a apply relevant procedure to unlock the system n provide first aid.

ORGANISATION AND COMMUNICATION;

Land asap on an adequate airport (priority landing) n req.medical assistance in flight;

MAYDAY, MAYDAY, MAYDAY, (CALLSIGN) EXPERIENCE CREW INCAPACITATION , REQ.MEDICAL ASSISTANCE ON LANDING

Terrain Avoidance Warning

A go-arround shall be initiated if the cause of the warning cannot be identified immediately.WHOOP WHOOP PULL UP-TERRAIN TERRAIN, TOO LOW TERRAIN AHEAD, PULL UP, OBSTACLE AHEAD, PULL UP

PL 1+2.GO ARROUND POWER

AUTO PILOT.OFF CLIMB or GO around initiate

Maintain wings leveled (Fly Pitch stick shacker / stall speed)

SINK RATE; Increasepitch n power to make the warning cease.

DONT SINK; Adjust pitch n power to maintain altitude or a positive climb gradient.

TOO LOW GEAR-TOO LOW FLAPS; Adapt aircraft configuration or perform G/A

GLIDE SLOPE; Resume (kembali) ke flight path to glide slope, or depress one of the two GPWS/GS push-buttons if approach is intentionnaly performed under glide slope.

TERRAIN AHEAD; Change flight path to avoid obstacle n make dwarning cease/stop

TCASTraffic Alert and Collision Avoidance System : TA and RA.

TA : Traffic Advisory indicate if it is climbing descending at greater than 500 feet per minute. TCAS will display a TA when CPA (Closest point of approach) is between 20 and 49 seconds with aural alert TRAFFIC, TRAFFIC.

RA : CORRECTIVE ACTION TO DO

A TA may become a RA within 15 seconds

A typical TCAS II maneuver requires crew response within 5 seconds and G-forces +/- 0.25G (karena persyaratan dari G-forces, RA tidak menanggapi apabl memakai A/P, mk A/P harus dimatikan dulu sebelumnya utk menanggapi RA.

Flight eventsPNFPF

WHEN RESOLUTION

OCCURS

DO : ATC CALL

IF CLIMB :PWR MGT..MCT

SEAT BELT..ONDO : AP DISCONNECT

ANN : I HAVE CONTROL

DO : PITCH.. INITIALY +/- 3

VSI GREEN ARC FOLLOW

POWER AS REQIURED

WHEN CLEAR OF CONFLICT

DO : ATCCALLDO :FLIGHT PATHRETURN TO

INITIAL FL

AP.ENGAGED

DO NOT FOLLOW F/D N NOT OVER REACTION A R/A XXX CTRL-CALL SIGN-TCAS CLIMB/DESCEND(ROGER), XXX CTRL-CALL SIGN- CLEAR OF CONFLICT RESUME TO FL/ALT (ROGEROR INSTRUCTIONS)

APM ( Aircraft Performance Monitoring)

APM allows improved ice accretion monitoring n enable to compare the aircraft theoretical drag with the in flight drag compute with the measure parameters, and therefore to detect if an abnormal loss of aircraft performance occurs.

CRUISE SPEED LOW (QRH normal procedure)

The speed in cruise is monitored and if an abnormal increase in drag induce (menyebabkan) an abnormal speed decrease of more than 10kts compare to the expected one, this message light on.

DEGRADED PERF. (QRH following failure procedure)

In crz or in climb,if an abnormal drag increase induce (menyebakan) a speed decrease or a loss of rate of climb, this alert is triggered in association with a single chime and a master CAUTION on the attention getter. In cruise, this occurs right after the CRUISE LOW SPEED.

INCREASE SPEED (QRH following failure procedure)

In cruise, climbor descend, if the drag is abnormally high and that IAS is lower the MSIS (Minimum Severe Icing Speed equivalent to red bug +10kts), this message flashes in association with a single chime and a master CAUTION on the attention getter. This occurs right after the DEGRADED PERF.

Cabin Briefing

1 Perkenalan post.masing2

2 Document2; - Rating masing2 (TAC)

- PASPOR

3 Revised/ schedule? Gmn? (Jam brp, hr ke brp dll)

4 Status pesawat (Reg,Parking, Type, Karakter, DMI)

5 Estimate pswt (delay/tidak) pswt drmn?

6 Flight Planed; Cuaca/menyangkut seving.

7 # Company policy;

Keep smile face

Embark and Disembark

Connecting pax

Akibat keterlambatan

# Termasuk barang2 yg volumenta besar, jika tdk cukup minta Ground staff taruh di bagasi.

8 Cabin Maintenance Cx

Ex. Door Emg. Cx secar fisik bisa operate atau tidak?

Emg. Brief; On Grd, Evac 5 syarat?

In Flt.

9 Bomb Treatment ( COM

Hi jack ( COM, plus Hi jack code i.e Spagety (its not on board) 7500)Unpressurized ( COM 7700 )

Comm. Fail (COM 7600, VFR 1200)

ODD

3000, 5000

7000, 9000

FL 130, TO

FL 190

EVEN

+500 4500,

6500,8500

FL 145, TO

FL 185

EVEN

4000 6000,

8000, 10000

FL 140, TO

FL 180

ODD

+500, 3500

5500, 7500

9500 TO

FL 195

FL 290

FL 310

FL 330

FL 350

FL 370

FL 390

FL 410

FL 300

FL 320

FL 340

FL 360

FL 360

FL 400

ODD

FLs 210

230

250

TO FL 270

THEN-

FLs 290

330

370

Etc.

EVEN

FLs 220

240

260

TO FL 280

THEN-

FLs 310

350

390

etc

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