Pilatus PC-24 Ground Servicing Manual Download

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Fuel - Defuel and Drain Fuel

Preliminary Requirements and Safety Conditions

CAUTION

PUT ON PROTECTIVE CLOTHING AND SAFETY GOGGLES BEFORE YOU DO
WORK WITH FUEL. FUEL IS POISONOUS.

Recommended Support Equipment

Equipment

Recommended

Pilatus Part Number

Fuel drain tool

990.00.00.940 or Local supply

Defuel with Aircraft Pumps or by Suction

Fig. 2-2-1

and

Fig. 2-2-2

show the refuel / defuel compartments with the refuel panel and

placards.

Note

Do not use the aircraft batteries as the electrical power source for the fuel booster pumps.
When defueling with the fuel booster pumps, connect ground power then on the overhead
panel, select GPU ON.

Connect a Ground Power Unit (GPU) to the aircraft and energise the electrical system.

Note

Make sure that the fuel vehicle has the capacity to take the amount of fuel to be
removed.

Note

During the fuel system boot the FAIL light (red) will be on for approximately one
minute.

Follow the instructions given on the placard in the refuel / defuel compartment.

Section 2 - Aircraft Servicing

Ground Servicing Guide

Report No: 02484

Issue date: Apr 29, 2020

Page 2-2-1

PC24-A-A15-12-0010-00A-221A-A

Summary of Contents for PC-24

Page 1: ...0 This document contains recommended information for Fixed Base Operators when servicing the PC 24 aircraft The information contained herein is advisory In the event of any contradictions the AFM and...

Page 2: ...FM Front Matter Table of Contents Subject Page List of Effective Data Modules FM 1 1 Log of Revisions FM 2 1 Section FM Front Matter Ground Servicing Guide Report No 02484 Issue date Nov 30 2020 Page...

Page 3: ...Section FM Front Matter This Page Intentionally Left Blank Ground Servicing Guide Report No 02484 Issue date Nov 30 2020 Page FM 0 2...

Page 4: ...0001 00A 170A A Mooring 29 04 2020 A15 00 0200 00A 160A A Cargo Loading Unloading procedure 29 04 2020 A15 12 0001 00A 210A A Inflate Tires 29 04 2020 A15 12 0010 00A 221A A Fuel Defuel and Drain Fuel...

Page 5: ...Section FM Front Matter This Page Intentionally Left Blank Ground Servicing Guide Report No 02484 Issue date Nov 30 2020 Page FM 1 2 PC24 A A15 12 0001 00A 00SA A...

Page 6: ...icing Guide Initial Issue Issue 002 Revision 00 Dated Nov 30 2020 A15 12 0001 00A 030A A A15 12 0050 01A 250A A ACN Technical data added Windows Clean replaced with Windows Clean and apply rain repell...

Page 7: ...Section FM Front Matter This Page Intentionally Left Blank Ground Servicing Guide Report No 02484 Issue date Nov 30 2020 Page FM 2 2 PC24 A A15 12 0001 00A 003B A...

Page 8: ...Danger Areas 0 1 5 6 Runway Guidelines 0 1 7 7 Weight Guidelines 0 1 8 8 Revisions to the Ground Servicing Guide 0 1 8 Aircraft Classification Number 0 2 1 1 Aircraft Classification Number 0 2 1 2 Pa...

Page 9: ...Section 0 Introduction This Page Intentionally Left Blank Ground Servicing Guide Report No 02484 Issue date Nov 30 2020 Page 0 0 2...

Page 10: ...nd are familiar with basic jet aircraft systems common to aircraft of this type Therefore this document does not contain basic information that is considered prerequisite training It is the responsibi...

Page 11: ...must supervise the service personnel at all times during the servicing CAUTION If there is a problem during a procedure that could affect the safe operation or dispatch of the aircraft stop the proced...

Page 12: ...9 in 17 m 22 ft 4 5 in 6 8 m 17 ft 4 in 5 3 m 9 ft 10 in 3 m 10 ft 11 in 3 3 m Figure 0 1 1 Airplane Three View and Dimensions Section 0 Introduction Ground Servicing Guide Report No 02484 Issue date...

Page 13: ...DIUS 180 DEGREE TURN AS SHOWN 1 D B A E NOSEWHEEL RADIUS 26 ft 7 in 8 1 m OUTSIDE MAIN GEAR RADIUS 19 ft 5 in 5 9 m HORIZONTAL STABILIZER RADIUS 35 ft 5 in 10 8 m 2 ft 1 in 0 6 m C NOSE RADOME RADIUS...

Page 14: ...an be pulled into the engine by suction The aft danger area is from the jet exhaust of the engines Personnel can be burned by the hot jet exhaust and or pushed to the ground Any equipment or loose obj...

Page 15: ...SONNEL EQUIPMENT BEFORE ENGINE START AND OPERATION IN QUIET POWER MODE IDLE QPM IDLE VELOCITY DROPS TO 20 MPH AND PEAK TEMPERATURE IS 18 F OVER AMBIENT TM TM AREA TO BE CLEARED OF PERSONNEL EQUIPMENT...

Page 16: ...AFM Supplement 02442 Contaminated Runway Operation With gravel kit factory option installed Prepared dirt sand gravel runways dry and wet refer to AFM Supplement 02444 Dirt Sand Gravel Runway Operati...

Page 17: ...the Ground Servicing Guide 8 1 Revision Schedule From time to time as new information becomes available for the PC 24 aircraft Pilatus Aircraft Ltd will issue revised information and instructions to t...

Page 18: ...e Pavement Classification Number PCN A number expressing the bearing strength of a pavement for unrestricted operation Pavement Type F Flexible pavement for example asphalt R Rigid pavement for exampl...

Page 19: ...Navigate to the weight on the horizontal axis Navigate upwards to the appropriate Subgrade Strength line Navigate to the left to the vertical axis to find the ACN 3 Determine the main gear tyre press...

Page 20: ...0 000 5 5 5 4 5 4 3 5 3 2 5 2 1 5 ACN AIRCRAFT CLASSIFICATION NUMBER FLEXIBLE PAVEMENT Figure 0 2 1 Aircraft Classification Number Flexible Pavement Section 0 Introduction Ground Servicing Guide Repor...

Page 21: ...4 5 5 ACN EXAMPLE WEIGHT SUBGRADE ACN 15 000 LB D ULTRA LOW 3 7 AIRCRAFT CLASSIFICATION NUMBER RIGID PAVEMENT Figure 0 2 2 Aircraft Classification Number Rigid Pavement Section 0 Introduction Ground S...

Page 22: ...n the horizontal axis navigate upwards to the D ULTRA LOW subgrade strength line and then navigate to the left to the vertical axis to find the Aircraft Classification Number The result ACN is 3 7 3 T...

Page 23: ...Section 0 Introduction This Page Intentionally Left Blank Ground Servicing Guide Report No 02484 Issue date Nov 30 2020 Page 0 2 6 PC24 A A15 12 0001 00A 030A A...

Page 24: ...reliminary Requirements and Safety Conditions 1 2 1 2 Recommended Support Equipment 1 2 1 3 Parking Guidelines 1 2 2 Mooring 1 3 1 1 Preliminary Requirements and Safety Conditions 1 3 1 2 Recommended...

Page 25: ...Section 1 Ground Handling This Page Intentionally Left Blank Ground Servicing Guide Report No 02484 Issue date Nov 30 2020 Page 1 0 2...

Page 26: ...is can cause damage to the aircraft CAUTION Do not tow the aircraft with a towbarless tug if the gravel kit is installed A towbarless tug can damage the gravel kit CAUTION Do not use the aircraft brak...

Page 27: ...wed is clear of objects The passenger door and the cargo door are closed The brake pressure is sufficient Note A tow bar or towing equipment that fits correctly can be used Care must be taken to make...

Page 28: ...OWING ANGLE OPTION 2 B OPTION 1 ICN PC24 A A15000000 A S4080 07741 A 001 01 Figure 1 1 1 Towing the Aircraft Section 1 Ground Handling Ground Servicing Guide Report No 02484 Issue date May 13 2020 Pag...

Page 29: ...Section 1 Ground Handling This Page Intentionally Left Blank Ground Servicing Guide Report No 02484 Issue date May 13 2020 Page 1 1 4 PC24 A A15 10 0005 00A 174A A...

Page 30: ...tem covers and the ECS outlet cover The vapor cooling system and ECS outlet louver vanes can be easily damaged CAUTION Do not park the aircraft in direct sunlight during very hot weather conditions If...

Page 31: ...st Lock is set by the Flight Crew Install the tail strut at the position in Fig 1 2 1 Install a lock pin in each over wing emergency exit at the positions shown in Fig 1 2 2 Close and lock the passeng...

Page 32: ...4 A A15000000 A S4080 07778 A 001 01 Figure 1 2 1 Parking Tail Strut and Steering Bar Section 1 Ground Handling Ground Servicing Guide Report No 02484 Issue date May 13 2020 Page 1 2 3 PC24 A A15 10 0...

Page 33: ...SHOWN ICN PC24 A A15000000 A S4080 07779 A 001 01 Figure 1 2 2 Parking Emergency Exit Lock Pin Section 1 Ground Handling Ground Servicing Guide Report No 02484 Issue date May 13 2020 Page 1 2 4 PC24 A...

Page 34: ...TYPICAL D GAP 0 39 in 10 mm ICN PC24 A A15000000 A S4080 07780 A 001 01 Figure 1 2 3 Parking Air Data Probe Covers Section 1 Ground Handling Ground Servicing Guide Report No 02484 Issue date May 13 2...

Page 35: ...PC24 A A15120000 A S4080 07153 A 001 01 Figure 1 2 4 Parking Cockpit Cover Section 1 Ground Handling Ground Servicing Guide Report No 02484 Issue date May 13 2020 Page 1 2 6 PC24 A A15 10 0002 00A 170...

Page 36: ...C ICN PC24 A A15000000 A S4080 07781 A 001 01 Figure 1 2 5 Parking Nose Covers Section 1 Ground Handling Ground Servicing Guide Report No 02484 Issue date May 13 2020 Page 1 2 7 PC24 A A15 10 0002 00...

Page 37: ...H SHOWN B B ICN PC24 A A15000000 A S4080 07782 A 001 01 Figure 1 2 6 Parking Wing Covers Section 1 Ground Handling Ground Servicing Guide Report No 02484 Issue date May 13 2020 Page 1 2 8 PC24 A A15 1...

Page 38: ...LH SHOWN B C A A C F E ICN PC24 A A15000000 A S4080 07783 A 001 01 Figure 1 2 7 Parking Upper Rear Fuselage Covers Section 1 Ground Handling Ground Servicing Guide Report No 02484 Issue date May 13 2...

Page 39: ...H SHOWN H G H F ICN PC24 A A15000000 A S4080 07743 A 001 01 Figure 1 2 8 Parking Lower Rear Fuselage Covers Section 1 Ground Handling Ground Servicing Guide Report No 02484 Issue date May 13 2020 Page...

Page 40: ...parking 2 Recommended Support Equipment Equipment Recommended Pilatus Part Number Jack Point Adaptors 513 07 24 010 Jack Point Lugs 513 07 24 006 Mooring blocks minimum 400 lb 181 kg Local supply Rop...

Page 41: ...On a clay type soil or rock surface use six screw pickets Moor the aircraft as follows Remove and keep the three plugs Install the three jack point adaptors and jack point lugs Attach rope between ea...

Page 42: ...0 A S4080 07872 A 001 01 ICN PC24 A A15000000 A S4080 07872 A 001 01 Figure 1 3 1 Mooring Tie Down Points Section 1 Ground Handling Ground Servicing Guide Report No 02484 Issue date Apr 29 2020 Page 1...

Page 43: ...0 2 0 3 0 4 0 5 0 6 0 7 0 8 0 9 0 10 0 11 0 12 0 13 0 14 0 15 0 16 0 17 0 AIRCRAFT LONGITUDINAL AXIS M AIRCRAFT LATERAL AXIS M SPECIFIED TIE DOWN AREA ICN PC24 A A15000000 A S4080 07787 A 001 01 Figu...

Page 44: ...he cargo The minimum separation distance for a Large baggage restraint system and cargo is 9 8 in 250 mm Small baggage restraint system and cargo is 7 5 in 190 mm The long tie down straps must be posi...

Page 45: ...tion Type Maximum Weight Side Outboard 385 8 lb 175 kg Middle Inboard 440 9 lb 200 kg Full Width 771 6 lb 350 kg Section 1 Ground Handling Ground Servicing Guide Report No 02484 Issue date Apr 29 2020...

Page 46: ...DLE SIDE A TYPICAL MIDDLE ICN PC24 A A15000000 A S4080 05027 A 000 01 Figure 1 4 1 Cargo Tie Down Kit Configurations Section 1 Ground Handling Ground Servicing Guide Report No 02484 Issue date Apr 29...

Page 47: ...in 100 mm 9 8 in 250 mm 47 2 in 1200 mm LARGE BAGGAGE RESTRAINT SYSTEM CARGO CARGO 47 2 in 1200 mm ICN PC24 A A15000000 A S4080 05865 A 000 01 Figure 1 4 2 Cargo Baggage Clearance Section 1 Ground Han...

Page 48: ...GO DIMENSIONS 45 5 in 1 156 mm 47 2 in 1 200 mm ICN PC24 A A15000000 A S4080 05029 A 002 01 Figure 1 4 3 Maximum Cargo Dimensions and Strap Angle Section 1 Ground Handling Ground Servicing Guide Repor...

Page 49: ...Section 1 Ground Handling This Page Intentionally Left Blank Ground Servicing Guide Report No 02484 Issue date Apr 29 2020 Page 1 4 6 PC24 A A15 00 0200 00A 160A A...

Page 50: ...ing Guidelines 2 3 2 Windows Clean check and apply rain repellent 2 4 1 1 Preliminary Requirements and Safety Conditions 2 4 1 2 Recommended Support Equipment 2 4 1 3 Cleaning Guidelines 2 4 2 4 Rain...

Page 51: ...Weather Procedures Deicing Anti Icing 2 8 1 1 Preliminary Requirements and Safety Conditions 2 8 1 2 General 2 8 1 Section 2 Aircraft Servicing Ground Servicing Guide Report No 02484 Issue date Nov 3...

Page 52: ...SE AN INJURY TO PERSONNEL AND DAMAGE EQUIPMENT WARNING DO NOT RELEASE COMPRESSED GAS PRESSURE TOO QUICKLY IT CAN CAUSE SERIOUS INJURY CAUTION Do not service a hot tire Wait until the tire is at ambien...

Page 53: ...ire is more than 59 F 15 C it is recommended that the tire pressure is increased by the value given in the following table Table 2 1 1 Ambient Temperature Tire Pressure Ambient Temperature Decreased b...

Page 54: ...D C C CAP VALVE D CAP VALVE ICN PC24 A A15000000 A S4080 07791 A 001 01 Figure 2 1 1 Tires Fill Section 2 Aircraft Servicing Ground Servicing Guide Report No 02484 Issue date Apr 29 2020 Page 2 1 3 P...

Page 55: ...Section 2 Aircraft Servicing This Page Intentionally Left Blank Ground Servicing Guide Report No 02484 Issue date Apr 29 2020 Page 2 1 4 PC24 A A15 12 0001 00A 210A A...

Page 56: ...aft batteries as the electrical power source for the fuel booster pumps When defueling with the fuel booster pumps connect ground power then on the overhead panel select GPU ON 1 Connect a Ground Powe...

Page 57: ...0 LBS A B C B C TYPICAL D TYPICAL D A PC24 A A15120000 A S4080 07910 A 000 01 Figure 2 2 1 Refuel Defuel Compartment Section 2 Aircraft Servicing Ground Servicing Guide Report No 02484 Issue date Apr...

Page 58: ...B C TYPICAL D TYPICAL D A ICN PC24 A A15120000 A S4080 07907 A 000 01 Figure 2 2 2 Refuel Defuel Compartment with Suction Option Section 2 Aircraft Servicing Ground Servicing Guide Report No 02484 Iss...

Page 59: ...he aircraft 3 Install the fuel drain tool in a drain valve and drain the fuel from the left and right wing 4 Remove the fuel drain tool from the fuel drain 5 Disconnect the bonding lead from the waste...

Page 60: ...LVE FUEL DRAIN TOOL CONTAINER ICN PC24 A A15120000 A S4080 07909 A 000 01 Figure 2 2 3 Fuel Drain Tool Section 2 Aircraft Servicing Ground Servicing Guide Report No 02484 Issue date Apr 29 2020 Page 2...

Page 61: ...Section 2 Aircraft Servicing This Page Intentionally Left Blank Ground Servicing Guide Report No 02484 Issue date Apr 29 2020 Page 2 2 6 PC24 A A15 12 0010 00A 221A A...

Page 62: ...r pressure but gravity refueling can be used if pressure refueling is not possible Make sure that the correct fire fighting equipment and personnel are available at all times Conduct fueling operation...

Page 63: ...The approved fuel grades are Jet A ASTM D1655 17 Jet A 1 ATSM D1655 17 JP 8 MIL DTL 83133 Rev J TS 1 GOST 10277 86 Fig 2 3 1 shows the location of the refueling points Fig 2 3 2 shows the refuel defu...

Page 64: ...EL GRAVITY REFUEL ICN PC24 A A15000000 A S4080 01902 A 000 01 Figure 2 3 1 Fuel System Refueling Points Section 2 Aircraft Servicing Ground Servicing Guide Report No 02484 Issue date Apr 29 2020 Page...

Page 65: ...200 LB A B A B ICN PC24 A A15000000 A S4080 01616 A 003 01 Figure 2 3 2 Refuel Defuel Panel Section 2 Aircraft Servicing Ground Servicing Guide Report No 02484 Issue date Apr 29 2020 Page 2 3 4 PC24 A...

Page 66: ...placards in the refuel panel compartment A A ICN PC24 A A15000000 A S4080 07829 A 002 01 Figure 2 3 3 Fuel Refuel by Pressure Section 2 Aircraft Servicing Ground Servicing Guide Report No 02484 Issue...

Page 67: ...5 Put the refuel nozzle in the refuel filler opening 6 Fill the tank with the necessary fuel 7 Remove the refuel nozzle from the refuel filler opening 8 Install the filler cap 9 Disconnect the refuel...

Page 68: ...ER GRAVITY FILLER CAP FILLER CAP ADAPTER FUELING NOZZLE ICN PC24 A A15000000 A S4080 07830 A 001 01 Figure 2 3 4 Fuel Refuel by Gravity Section 2 Aircraft Servicing Ground Servicing Guide Report No 02...

Page 69: ...Fig 2 3 5 shows a typical drain valve 1 Do not move the aircraft for a minimum of 15 minutes 2 Connect a fuel tank drain reservoir to the drain valve 3 Drain a minimum of 0 44 pint 0 25 liter of fuel...

Page 70: ...DRAIN RESERVOIR DRAIN VALVE ICN PC24 A A15000000 A S4080 07831 A 001 01 Figure 2 3 5 Fuel Drain Water Section 2 Aircraft Servicing Ground Servicing Guide Report No 02484 Issue date Apr 29 2020 Page 2...

Page 71: ...Section 2 Aircraft Servicing This Page Intentionally Left Blank Ground Servicing Guide Report No 02484 Issue date Apr 29 2020 Page 2 3 10 PC24 A A15 12 0011 00A 211A A...

Page 72: ...WS CAUTION DO NOT CLEAN OR APPLY TREATMENT TO THE WINDSHIELD OR WINDOWS IN DUSTY OR SANDY CONDITIONS IN STRONG OR DIRECT SUNLIGHT CAUTION DO NOT USE WATER THAT IS PRESSURIZED THIS CAN CAUSE SCRATCHES...

Page 73: ...Windshield label MPG windshields Local supply Heat Blankets PPG windshield Local supply Protective film PPG windshields Local supply Heat blankets PPG windshields Local supply VAC power supply Local...

Page 74: ...e interior windows 4 Rain Repellent CAUTION THE AIRCRAFT CAN HAVE TWO DIFFERENT TYPES OF WINDSHIELDS INSTALLED AND IT IS IMPORTANT THAT THE CORRECT RAIN REPELLENT IS APPLIED INCORRECT RAIN REPELLENTS...

Page 75: ...pes Wipe windshield fully dry with clean paper wipes 2 Spray the windshield with Deionized water 3 If the water beads up in even sized droplets and runs off the windshield in straight clear lines or c...

Page 76: ...repellent satisfactory condition Figure 2 4 3 Windshields Rain repellent unsatisfactory condition Section 2 Aircraft Servicing Ground Servicing Guide Report No 02484 Issue date Nov 30 2020 Page 2 4 5...

Page 77: ...tween 41 and 68 F 5 and 30 C Protect the windshield from direct sun light rain snow and all other sources of possible contamination Sufficient ventilation is necessary to remove all airborne solvent v...

Page 78: ...THE OUTER SURFACE POLISH THE WINDOWS EVENLY A MAXIMUM OF TWO TIMES IF THE WINDOWS ARE POLISHED TOO MUCH THE ANTISTATIC LAYER CAN BE DAMAGED CAUTION DO NOT USE OTHER SOLVENT OR ABRASIVE MATERIAL IT CAN...

Page 79: ...of the polishing slurry has been removed 13 Discard the used paper wipes and the disposable gloves 14 Apply the surface activation solution as follows 14 1 Use a new pair of disposable gloves 14 2 Pre...

Page 80: ...towel and remove all the remaining unwanted rain repellent 15 7 Spray the windshield glass surface with deionized water and clean with a dry paper towel 15 8 Discard the used paper towel the paper wip...

Page 81: ...MATERIAL IT CAN CAUSE DAMAGED TO THE WINDSHIELD AND OR AIRCRAFT STRUCTURE Note Only the Master kit surface seal rain repellent and the Quick application kit surface seal is approved for the PPG windo...

Page 82: ...ual and the Ground Servicing Manual This guide gives the procedures to Apply the master kit surface seal Refer to Apply the master kit surface seal Apply the quick application kit surface seal optiona...

Page 83: ...y for a maximum of 2 times in a horizontal direction at rate of 1 ft 30cm between 2 and 3 sec Do not let the polishing slurry dry 1 6 3 If the surface becomes dry during polishing apply more polishing...

Page 84: ...reparation solution to make the gauze pads moist 5 Apply from the center to the edges Do not apply to the taped edges 6 Apply a thin film of the surface preparation solution around the edges 7 Discard...

Page 85: ...e used paper wipes and the disposable gloves 7 If no heat curing will be done do the steps that follow 1 Use a new pair of disposable gloves 2 Use clean paper wipes to wipe off the unwanted haze and r...

Page 86: ...is not too hot 11 Remove the masking tape and the heating blanket from the windshield 12 Remove the masking tape and the protective film from the windshield 13 Put the heating blanket and protective...

Page 87: ...s 2 5 If necessary apply more coating solution quick application kit to make the applicator pads moist 2 6 Apply from the center to the edges 2 7 Continue to apply the coating solution quick applicati...

Page 88: ...nal surface of the aircraft CAUTION Make sure to flush the aircraft surfaces in the direction of the airflow from nose to tail Do not point the hose at vents or openings in the aircraft structure This...

Page 89: ...r XE3 G Cleaner Hard Surface Cleaner Concentrate XG5 Cleaner Spray and Shine XC11 3 Cleaning Guidelines The following procedures give guidelines for Preparing the aircraft for cleaning Cleaning the ex...

Page 90: ...tled brush 3 Flush the area with clean water 4 If necessary repeat this process a maximum of three times until the surface is clean 5 Flush the aircraft tires with clean water and then if necessary mo...

Page 91: ...mixture of one part of cleaner Hard Surface Cleaner Concentrate XG5 or Spray and Shine XC11 to 20 parts of clean water 1 Use a spray bottle to apply the cleaner solution 2 Spray the applicable cleaner...

Page 92: ...ECS intake Fig 2 5 1 VCS outlets Fig 2 5 2 Ice detectors Fig 2 5 3 AOA sensors Fig 2 5 3 Pitot static probes Fig 2 5 3 OAT sensor Fig 2 5 3 2 Set the flaps to 0 Section 2 Aircraft Servicing Ground Ser...

Page 93: ...H SHOWN B C A A C F E ICN PC24 A A15000000 A S4080 07783 A 001 01 Figure 2 5 1 Parking Upper Rear Fuselage Covers Section 2 Aircraft Servicing Ground Servicing Guide Report No 02484 Issue date Apr 29...

Page 94: ...SHOWN H G H F ICN PC24 A A15000000 A S4080 07743 A 001 01 Figure 2 5 2 Parking Lower Rear Fuselage Covers Section 2 Aircraft Servicing Ground Servicing Guide Report No 02484 Issue date Apr 29 2020 Pa...

Page 95: ...TYPICAL D GAP 0 39 in 10 mm ICN PC24 A A15000000 A S4080 07780 A 001 01 Figure 2 5 3 Parking Air Data Probe Covers Section 2 Aircraft Servicing Ground Servicing Guide Report No 02484 Issue date Apr 29...

Page 96: ...o behind the aircraft interior surfaces CAUTION Do not clean the instrument panel with water or the soap solution This can damage the display screen anti glare coating 2 Recommended Support Equipment...

Page 97: ...clean the interior surfaces With a sponge moist with the clean water wipe the interior surfaces Carefully dry the interior surfaces with absorbent paper 3 2 Flight Deck CAUTION Before you clean the d...

Page 98: ...t when the cabin temperature is less than 36 Fahrenheit 2 Celsius If you deploy or operate the toilet when the cabin temperature is less than 36 Fahrenheit 2 Celsius damage can occur to the toilet com...

Page 99: ...TOILET ASSEMBLY SHOWN STOWED A B ICN PC24 A A150000 A S4080 00708 A 000 01 Figure 2 7 1 Vacuum Waste System Component Location Section 2 Aircraft Servicing Ground Servicing Guide Report No 02484 Issue...

Page 100: ...re 2 7 2 1 4 Remove the filler cap Figure 2 7 2 5 from the water tank Figure 2 7 2 3 5 Put the funnel Figure 2 7 2 4 in the water tank Figure 2 7 2 3 6 Note The maximum capacity of the water tank is 2...

Page 101: ...4 A A15380000 A S4080 05400 A 000 01 Figure 2 7 2 Water tank Fill using the funnel Sheet 1 of 2 Section 2 Aircraft Servicing Ground Servicing Guide Report No 02484 Issue date Apr 29 2020 Page 2 7 4 PC...

Page 102: ...er drain outlet Figure 2 7 3 2 is clear 5 Move the water drain handle Figure 2 7 3 1 to the open position 6 Make sure that the water drains into the container 7 When the flow of water from the water d...

Page 103: ...2 A B A B PC24 A A15120000 A S4080 07870 A 001 01 Figure 2 7 3 Water tank Drain Section 2 Aircraft Servicing Ground Servicing Guide Report No 02484 Issue date Apr 29 2020 Page 2 7 6 PC24 A A15 12 0060...

Page 104: ...t is less than 50 F 10 C and visible moisture in any form is present The aircraft must not takeoff with frost on these critical areas Wing leading edge and upper surface Windshield The aircraft must n...

Page 105: ...face until the aircraft attains a higher airspeed approximately 100 knots When the fluid shears from the surface it leaves only a thin film of fluid that will have a small impact on the performance Ty...

Page 106: ...ircraft must sprayed from the front Spraying from the rear can force fluid into aerodynamically quiet areas from where it may not be able to drain Tool Equipment Recommended Pilatus Part Broom Local s...

Page 107: ...luid be applied directly to the Air data probes Windshield and windows Air intakes Engine inlets Brakes Wheels Dry powdery snow can be removed by sweeping with a brush or broom Heavy wet snow can be r...

Page 108: ...be used This type of equipment with the fluid temperature limited to 160 F 70 C can be used to deice the aircraft Fig 2 8 1 shows a flowchart with the recommended deicing steps before the aircraft can...

Page 109: ...HE AIRCRAFT BEFORE TAKEOFF REVIEW THE AIRPORT ADVISORY INFORMATION FOR THE FLUID REQUIRED DEICING FLUID AVAILABLE DEICING LOCATION AND DISTANCE FROM RUNWAY DEICE THE AIRCRAFT DEICE ANTI ICE THE AIRCRA...

Page 110: ...bilizer should be thoroughly inspected 5 Deice the fuselage from the top centerline then outboard and downwards 6 If necessary use type I deicing fluid to aid the removal of the contamination Apply th...

Page 111: ...ed onto the brakes and wheels 1 With a brush remove the build up of slush ice or the accumulation of blown snow from the landing gear 2 Where contamination deposits have bonded to surfaces these can b...

Page 112: ...WHEELS ICE DETECTORS AVOID DIRECT SPRAYING OF DEICING FLUID ON THE FOLLOWING AREAS ENGINE INLETS WINDSHIELD CABIN WINDOWS RAM AIR INLETS PITOT STATIC PROBES AOA SENSORS Figure 2 8 2 Essential Aircraft...

Page 113: ...BRAKES WHEELS ICE DETECTORS AVOID DIRECT SPRAYING OF DEICING FLUID ON THE FOLLOWING AREAS ENGINE INLETS WINDSHIELD CABIN WINDOWS RAM AIR INLETS PITOT STATIC PROBES AOA SENSORS Figure 2 8 3 Essential...

Page 114: ...e Fuel tank and vents Landing gear 2 3 6 Pre Takeoff Check After the deicing anti icing procedure and before takeoff the pilot in command must do a pre takeoff check to make sure all critical surfaces...

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