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3.1

Clean the Exterior Surfaces

CAUTION

CLEANING AGENTS THAT ARE NOT LISTED CAN AFFECT THE RAIN-REPELLENT
PERFORMANCE OF THE WINDSHIELDS.

1

Flush the exterior surface of the windows with clean fresh water. Loosen dirt, sand or
mud if necessary. Do this with the tips of your fingers, and in the direction of the water
flow.

2

Make sure that there are no abrasive particles on the transparency, especially in the
corners of the windows.

3

With a sponge moist with: clean water or a mixture of 50% clean water and 50%
isopropanol or a weak soap solution, clean the windows.

4

Flush the surface thoroughly with clean fresh water and dry with a clean moist chamois
leather.

3.2

Clean the Interior Surfaces

CAUTION

DO NOT USE CLEANING AGENTS THAT ARE NOT LISTED. CLEANING AGENTS
THAT ARE NOT LISTED CAN CAUSE DAMAGE TO THE WINDSHIELDS AND
WINDOWS.

With a chamois leather moist with clean water or a weak soap solution, clean the 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 ARE NOT APPROVED BY PILATUS.

These procedures give guidelines for applying rain repellent treatment to the windshields.

4.1

Rain repellent coating inspection intervals

The durability of the rain repellent glass treatment is dependent on the repellent and its type of
application, aircraft utilization and operating conditions. Below table provides recommended
inspection intervals. Each operator shall establish by its type of rain repellent and its type of
aircraft operating conditions if the interval requires adjustment.

Rain Repellent Type

Recommended Inspection Interval

Surfex 100 (MPG windshields)

6 months / 300 flight hours

Surface Seal DSS4040 heat cure (PPG
windshields)

12 months / 600 flight hours

Surface Seal DSS4040 no heat cure (PPG
windshields)

6 months / 300 flight hours

Section 2 - Aircraft Servicing

Ground Servicing Guide

Report No: 02484

Issue date: Nov 30, 2020

Page 2-4-3

PC24-A-A15-12-0050-01A-250A-A

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Содержание PC-24

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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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