Atr 72-500 Pilot Handbook

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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 LIMITATIONS

MAXIMUM WEIGHT KG LB TAXI 22.970 50.640 TAKE OFF 22.800 50.265 LANDING 22.350 49.273 ZERO FUEL 20.800 45.856 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.

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AIRSPEEDS

 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

VLORET = 160 kt

VLOLOW = 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

Flaps VMCL (CAS)

30

15 98 kt98 kt

OPS.PARAMETERS

ENVIRONMENTAL 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

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POWER

SETTING _LIMITTIME _(%)TQ _{( C)}ITT RESERVE TAKE OFF 10 mn(***) (**)100 800 TAKE OFF 5 mn 90 (**) (*) MAXIMUM CONTINUOUS NONE(***) 90.9(**) 800 GROUND IDLE HOTEL (4) MODE 715 STARTING 5 s 950 (2) OTHER 800 TRANSIENT 5 s 20 s(1) (2) 120 840 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.

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Jet A1

REFUELING : Max. pressure 3,5 bars (50 psi)

USABLE FUEL : In each tank is 2500 kg (5510 lbs) total 5000kg UNBALANCE : 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/mn

ELEVATION 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).

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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 = 185kt

VLORET = 160kt

VLOLOW = 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

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 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 ½ 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.

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 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 P2 COCKPIT PHILOSOPHY

PB POSITION BASIC FUNCTION

IN (DEPRESSED) OUT (RELEASED)

On, Auto, Normal Off, Manual, Altn, Shut

COLOR INDICATION

No light ill.except flow bars (DARK COCKPIT) BLUE

GREEN WHITE AMBER

RED

Normal basic operation

Temporarily required system in normal operation Back up or alternated system selected Selection other than normal basic operation

Caution indication Warning indication INSTRUMENT MARKINGS

RED ARC OR RADIAL LINE : MINIMUM AND MAXIMUM LIMITS YELLOW ARC : CAUTION AREA

GREEN 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 LIGHTING

The general cabin illumination system must be used during not less than 15 minutes before each flight.

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 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 2}nd₎

8. Flight Presentation : Ex.noise abt.when Tx 9. Flight Attendant Briefing :

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

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NP = 86/82% Level flight Approach 3

Speed 180 160 140 120 VAPP

Gear UP UP DOWN DOWN DOWN

Flaps 0 0 15 30/35 30/35

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 +10 WHITE BUG

ICING

CONDITIONS

RED BUG WHITE BUG

SPEED BUGS

 TAKE OFF BUGS :

Green Bug  V1 set when V1 = VR (when rwy limited (set 12 o’clock when not used)). Yellow Bug VR when 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

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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/O Airplane 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 point Runway

- 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”.

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- “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 or… Approach 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.P24

STARTING SEQUENCES

* “HOTEL MODE”, Svc.Door…Closed, Wg.Lights…On, Prop.Brake…On, 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 ENGSTART…Off, 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.

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- 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

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3. Automatic extinguishers 4. Emergency lights 5. Emergency exits 6. Lighted signs 7. Calls

8. Public Address (PA) Emergancy Equipment

1. 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 SEQUENCE

Flight Events

CM 1 CM 2

READY TO

TAKE OFF > ANNOUNCE“TAKE-OFF AT XXX O’CLOCK 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”

PNF PF

FL.CTRL.TRANSFER > ANN : “I HAVE CONTROL”

REACHING V1 > ANN : “V1”

CM1 : 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 * PL…Cx Notch * PWR MGT-CL * Bleed…Off/On * Cx…TQ % * Fine Tune…V 170kts > ANN : “CLIMB SEQ.COMPLETE”

DO : PL…CHECK IN THE NOTCH* ORDER : “CLIMB SEQUENCE”

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CRUISE PARAMETERS

PNF 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-AROUND FLIGHT EVENTS PNF ANN. : “MINIMUM” PF 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 EVENTS

PNF PF

REACH ACC. ALT MINI 1000ft AGL OR

HIGHER IF

> ANN. : “ACCELERATION ALTITUDE” > DO & ANN. :

ALT PB ON AFCS…. DEPRESS

> ORDER : “SET ALT” > DO & ANN. :

(15)

REQUESTED “ALT GREEN”

> DO & ANN. : “SET” > ORDER AND DO“CHECK”

“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 LEVER…SET 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 CONDITIONS

“FLAPS 0”

OR

IN ICING CONDITIONS

“REMAIN FLAPS 15”

ENGINE FLAME OUT AT TAKE-OFF

Flight events PNF PF

ENGINE FLAME

OUT First crew detects failure announces loudly :“ENGINE FAILURE” POSITIVE RATE > ANN : “POSITIVE RATE”

DO : ASSOCIATED ACTION

ORDER : “GEAR UP” ACTIONS TRIGGERED BY PNF WITHOUT PF REQUEST, JUST AFTER GEAR RETRACTION SEQUENCE

DO, CHECK & ANNOUNCE

“ENG 2 (or 1) UPTRIMMED ENG 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 ALTITUDE” DO & ANN : “ALT GREEN”

DO & ANN : “SET”

ORDER : “SET ALT”

ORDER & DO : “SET V BUG W/B”

REACHING WHITE BUG

> ANN : “WHITE BUG” DO & ANN : “IAS XXX SET” DO & ANN : “ MCT SET”

DO : FLAPS LEVER…SET AS RQRD

ORDER : “SET IAS” ORDER : “SET MCT”

ORDER : “NML CONDT.FLAPS

0/ICING CONDT.FLAPS REMAIN 15” WHEN FLAPS AT

0/15 ON INDI > ANN : “FLAPS 0 or REMAIN FLAPS15” 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

(16)

COMPLETED > ANN & READ : “AFTER TO C/L”

> ANN : “CHECKLIST COMPLETED” > 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-OFF

Basicly 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 events CM 1 CM 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

> READ AND ANN. : “ON GROUND

(17)

> 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

> EVACUATION…. INITIATE > READ & ANN. :

BAT…. OFF EMERGENCY DESCEND Flight Events PNF PF ACCORDING TO FLIGHT EVENT OR MASTER WARNING KAPITAN >> 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 HEADING………ADJUST 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 PB………DEPRESS

> ANNOUNCE

“YOU CAN REMOVE OXY MASK”

> DO

OXYGEN MASK…………REMOVE OXYGEN HATCH…………..CLOSE OXYGEN TEST PB………DEPRESS

WHEN NORMAL RATE OF DESCENT

AVAILABLE

KAPITAN

> DO : FLIGHT ATTENDANT REPORT….REQUEST ASSESMENT – DECISION – INFORMATION (A,B,C,D)

(18)

MEMO ITEMS

1. IN FLIGHT ENG FIRE OR SEVERE MECHANICAL DAMAGE (1.02) PL affected side………F1 CL effected side………FTR 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 ASAP

SINGLE ENG OPERATION procedure (2.4)………..APPLY

2. ON GROUND ENG FIRE OR SEVERE MECHANICAL DAMAGE (1.02) PL 1 + 2………..………GI/REVERSE AS RQD

 When aircraft stopped

PARKING BRAKE………..……….ENGAGE CL 1 + 2……….……..…………...FTR THEN FUEL SO FIRE HANDLE affected side…….……….PULL If condition persist

FIRST AGENT affected side ……….DISCH If condition persist after 30 seconds

SECOND AGENT affected side………DISCH If evacuation required

ON GROUND EMER EVACUATION (1.02)………..APPLY ON GROUND EMER EVACUATION (1.02)

AIRCRAFT/PARKING BRAKE………..STOP/ENGAGE AUTO PRESS ………..DUMP ATC (VHF 1)……….NOTIFY CL 1 + 2………FTR THEN FUEL SO MIN CAB LIGHT………...ON CABIN CREW (PA)………..NOTIFY FIRE HANDLES 1 + 2………...PULL AGENTS………AS RQD ENG START ROTARY SELECTOR………..OFF/START ABORT FUEL PUMPS 1 + 2……….OFF EVACUATION (PA)………..INITIATE  Before leaving aircraft

(19)

3. ENG FIRE AT TAKE OFF (1.02A)

LAND ASAP SINGEL ENG OPERATION procedure (2.04) ………. APPLY

4. 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………..….CHECK AUTOFEATHER ………..…..CHECK  If no UPTRIM

PL 1 + 2………....ADVANCE TO THE RAMP  When airborne

LDG GEAR ………..………UP BLEEDS 1 + 2 ………...OFF, IF NOT FAULT  At Acceleration Altitude

ALT ……….SET  At VFTO

PL 1 + 2 ………..IN THE NOTCH PWR MGT ………MCT IAS ………..SET If normal condition FLAPS ……….0O If icing condition FLAPS ……….MAINTAIN 15O PL affected side………..FI CL affected side………..FTR THEN FUEL SO BLEED engine alive………..………OFF if necessary  When airborne LDG GEAR …..………UP  At Acceleration Altitude PWR MGT ………...MCT  At VFTO  If normal condition FLAPS ……….………..0O  If Icing condition FLAPS ……….…..MAINTAIN 15O

PL affected side ……….………FI CL affected side ……….FTR THEN FUEL SO FIRE HANDLE illuminated ...PULL

If fire persist after 10 seconds

FIRST AGENT affected side ………...DISCH If fire persist after 30 seconds

SECOND AGENT affected side ………DISCH BLEED engine alive ………. OFF if necessary

(20)

6. SMOKE (1.05)

CREW OXY MASKS………...ON/100% GOGGLES………..AS RQD CREW COMMUNICATIONS………ESTABLISH RECIRC FANS 1 + 2……….OFF AP………ON 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 DESCENT………INITIATE PL 1 + 2……….FI CL 1 + 2………100% OVRD 9. SEVERE ICING (1.09)

MINIMUM ICING SPEED…………...INCREASE RED BUG by 10 kt PWR MGT………MCT CL / PL………..100 % MCT AP (if engaged…FIRMLY 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 ………15O

PWR MGT ………MCT CL/ 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 ………...8O

(21)

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 EFIS

BOTH 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)

EVEN +500 4500, 6500,8500 FL 145, TO FL 185 ODD 3000, 5000 7000, 9000 FL 130, TO FL 190

(22)

RVSM AIRSPACE Designated Airspace) IFR (ABOVE FL 200)

Standard communication

Distress (Emergency) message Urgency (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 acting

1.Check system (analysis failure) Four check under taken for failure confirmation; EVEN 4000 6000, 8000, 10000 FL 140, TO FL 180 ODD +500, 3500 5500, 7500 9500 TO FL 195 EVEN FLs 220 240 260 TO FL 280 THEN-FLs 310 350 390 etc ODD FLs 210 230 250 TO FL 270 THEN-FLs 290 330 370 Etc.

FL 300

FL 320

FL 340

FL 360

FL 400

FL 290

FL 310

FL 330

FL 350

FL 370

FL 390

FL 410

(23)

- 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 policy

At 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 policy

In 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 priority

EMERGENCY-NORMAL-ABNORMAL Sum up / Decision / Information

SUM 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.

(24)

-

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 BEHIND…

APPROACH

TAKE 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

(25)

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.

“DON’T 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 d’warning cease/stop

TCAS

Traffic 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”

(26)



A typical TCAS II maneuver requires crew response within 5 seconds and

G-forces +/- 0.25G (karena persyaratan dari G-G-forces, RA tidak menanggapi apabl

memakai A/P, mk A/P harus dimatikan dulu sebelumnya utk menanggapi RA.

Flight events

PNF

PF

WHEN RESOLUTION OCCURS DO : ATC… CALL IF CLIMB : PWR MGT………..MCT SEAT BELT………….….ON DO : AP… DISCONNECT ANN : “I HAVE CONTROL” DO : PITCH.. INITIALY +/- 3 VSI GREEN ARC… FOLLOW POWER… AS REQIURED WHEN CLEAR OF CONFLICT DO : ATC………CALL DO :

FLIGHT PATH……RETURN TO INITIAL FL AP……….ENGAGED