1. Manuals
  2. Brands
  3. Pilatus Manuals
  4. Aircrafts
  5. PC-24
  6. Ground servicing manual

Pilatus PC-24 Ground Servicing Manual

Hide thumbs Also See for PC-24:
Table of Contents

Advertisement

Quick Links

Download this manual
Ground Servicing Guide
Document Number 02484
Issue 002IRevision 04: Feb 27/ 2025
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 AMM shall
prevail over this document.
This document is not authority approved.

Advertisement

Table of Contents
loading
Need help?

Need help?

Do you have a question about the PC-24 and is the answer not in the manual?

Questions and answers

Related Manuals for Pilatus PC-24

Summary of Contents for Pilatus PC-24

  • Page 1 Document Number 02484 Issue 002IRevision 04: Feb 27/ 2025 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 AMM shall prevail over this document.
  • Page 2 This Page Intentionally Left Blank Ground Servicing Guide Report No: 02484 Issue date: Feb 27, 2025...
  • Page 3 Section FM - Front Matter SECTION FM Front Matter Table of Contents Subject Page List of Effective Data Modules FM-1-1 Log of Revisions FM-2-1 Ground Servicing Guide Report No: 02484 Issue date: Feb 27, 2025 Page FM-0-1...
  • Page 4 Section FM - Front Matter This Page Intentionally Left Blank Ground Servicing Guide Report No: 02484 Issue date: Feb 27, 2025 Page FM-0-2...
  • Page 5 Section FM - Front Matter List of Effective Data Modules All DMC are preceded with PC-24-A but for clarity this has been left out C = Changed data module N = New data module Data module code (DMC) Document title...
  • Page 6 Section FM - Front Matter This Page Intentionally Left Blank Ground Servicing Guide Report No: 02484 Issue date: Feb 27, 2025 Page FM-1-2...

  • Page 7: Log Of Revisions

    Section FM - Front Matter Log of Revisions Revision number Data Module Description and Date Code Issue 001 Revision PC-24 Ground Servicing Guide Initial Issue. 00 Dated May 14/2020 Issue 002 Revision A15-12-0001-00 ACN - Technical data added 00 Dated Nov A-030A-A...
  • Page 8 Section FM - Front Matter Revision number Data Module Description and Date Code Issue 002 Revision A15-10-0005-00 Gust lock removal no longer necessary for aircraft 04 Dated Feb A-174A-A towing 27/2025 A15-10-0006-00 New data module A-730A-A Ground Servicing Guide Report No: 02484 Issue date: Feb 26, 2025 Page FM-2-2...

  • Page 9: Table Of Contents

    Section 0 - Introduction SECTION 0 Introduction Table of Contents Subject Page Introduction 0-1-1 Copyright and Legal Statement 0-1-1 General 0-1-1 Purpose 0-1-1 Aircraft Dimensions 0-1-2 Danger Areas 0-1-5 Runway Guidelines 0-1-7 Weight Guidelines 0-1-8 Revisions to the Ground Servicing Guide 0-1-8 Aircraft Classification Number 0-2-1...
  • Page 10 Section 0 - Introduction This Page Intentionally Left Blank Ground Servicing Guide Report No: 02484 Issue date: Feb 27, 2025 Page 0-0-2...

  • Page 11: Introduction

    Pilatus Aircraft Ltd. In connection with the use of this document, Pilatus does not provide any express or implied warranties and expressly disclaims any warranty of merchantability or fitness for a particular purpose.

  • Page 12: Aircraft Dimensions

    Section 0 - Introduction CAUTION To prevent damage to the aircraft or equipment while away from home base / station, the flight crew must supervise the service personnel at all times during the handling and servicing of the aircraft. CAUTION If electrical power is required, only the flight crew can energize the electrical system.
  • Page 13 Section 0 - Introduction 9 ft 8 in. ( 2.9 m ) 55 ft 9 in. 22 ft 4.5 in. ( 17 m ) ( 6.8 m ) 17 ft 4 in. ( 5.3 m ) 23 ft 1 in. ( 7 m ) 55 ft 2 in.
  • Page 14 Section 0 - Introduction 2 ft 1 in. ( 0.6 m ) 60° 8 ft 5 in. ( 2.6 m ) PIVOT POINT 2 ft 1 in. ( 0.6 m ) A MINIMUM TAXIING SURFACE WIDTH OF 50 ft ( 15.2 m ) AND DIFFERENTIAL BRAKING ARE REQUIRED TO COMPLETE A MINIMUM RADIUS 180 DEGREE TURN AS SHOWN WING TIP RADIUS = 41 ft 4 in.

  • Page 15: Danger Areas

    Section 0 - Introduction Danger Areas When the engines are running, there are danger areas forward and aft of the engine nacelles (Fig. 0-1-3): − The forward danger area is from the engine intakes. Any loose equipment in this area can be pulled into the engine by suction.
  • Page 16 Section 0 - Introduction AIRCRAFT STATIC SEA LEVEL I.S.A. - NO WIND 49.5 ft 24.75 ft ( 15.1 m ) ( 7.55 m ) 20 ft ( 6.1 m ) RADIUS DANGER AIR INTAKE 7 ft 7 ft ( 2.1 m ) ( 2.1 m ) 60 ft 60 ft...

  • Page 17: Runway Guidelines

    Section 0 - Introduction Runway Guidelines Note A wet runway is defined as a runway which the surface is covered with: − Water, or a related substance, in a layer less than 1/8 in (3 mm) in depth − Sufficient moisture to give a reflective appearance, but without any significant area of standing water.

  • Page 18: Weight Guidelines

    Revisions to the Ground Servicing Guide 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 the latest registered owner or operator of the aircraft. This keeps the contents of the GSG current. This information may relate to, but is not limited to, approved aircraft modifications or improved knowledge, operating techniques or other guidance acquired through in-service experience.

  • Page 19: Aircraft Classification Number

    Y (tyre pressure limited to 145 psi) Z (tyre pressure limited to 73 psi) Note The PC-24 nose and main gear tyres have a service pressure of 58 respectively 73 psi (loaded). Therefore the PC-24 will never be tyre pressure limited.

  • Page 20: Determination Of Allowed Operation On Runway

    Section 0 - Introduction Determination of Allowed Operation on Runway To determine if an aircraft can operate without restrictions on a pavement, do as follows: From the Pavement Type Code, determine the: − Pavement Classification Number (PCN) − Pavement Type −...
  • Page 21 Section 0 - Introduction Figure 0-2-1: Aircraft Classification Number - Flexible Pavement Ground Servicing Guide Report No: 02484 Issue date: Nov 30, 2020 Page 0-2-3...
  • Page 22 Section 0 - Introduction Figure 0-2-2: Aircraft Classification Number - Rigid Pavement Ground Servicing Guide Report No: 02484 Issue date: Nov 30, 2020 Page 0-2-4...
  • Page 23 Section 0 - Introduction Example The example below describes how to determine if an aircraft can operate without restrictions on a pavement given the following conditions: − Pavement Type Code for a paved runway = PCN 20 / R / D / Y / T −...
  • Page 24 Section 0 - Introduction This Page Intentionally Left Blank Ground Servicing Guide Report No: 02484 Issue date: Nov 30, 2020 Page 0-2-6...
  • Page 25 Section 1 - Ground Handling SECTION 1 Ground Handling Table of Contents Subject Page Towing 1-1-1 Preliminary Requirements and Safety Conditions 1-1-1 Recommended Support Equipment 1-1-2 Towing Guidelines 1-1-2 Parking 1-2-1 Preliminary Requirements and Safety Conditions 1-2-1 Recommended Support Equipment 1-2-1 Parking Guidelines 1-2-2...

  • Page 26: Section 1 - Ground Handling

    Section 1 - Ground Handling This Page Intentionally Left Blank Ground Servicing Guide Report No: 02484 Issue date: Feb 27, 2025 Page 1-0-2...

  • Page 27: Towing

    Section 1 - Ground Handling Towing Preliminary Requirements and Safety Conditions WARNING ONLY TOW THE AIRCRAFT ON FIRM GROUND. THIS WILL HELP PREVENT INJURY TO PERSONNEL, DAMAGE TO EQUIPMENT, OR AIRCRAFT. WARNING OBEY THE TOWING VEHICLE MANUFACTURER'S INSTRUCTIONS BEFORE YOU TOW WITH A TOWBAR-LESS TUG.

  • Page 28: Recommended Support Equipment

    Section 1 - Ground Handling Recommended Support Equipment Equipment Recommended Pilatus Part Number Multi-head tow bar 990.00.00.904 Local supply Tow bar attachment-head 990.00.00.943 Local supply Wheel chocks 990.00.00.909 Local supply Towing Guidelines Make sure there are sufficient personnel to move the aircraft. It is recommended to have one person: −...
  • Page 29 Section 1 - Ground Handling MAXIMUM TOWING ANGLE OPTION 2 MAXIMUM TOWING ANGLE OPTION 1 ICN-PC24-A-A15000000-A-S4080-07741-A-001-01 Figure 1-1-1: Towing the Aircraft Ground Servicing Guide Report No: 02484 Issue date: Feb 26, 2025 Page 1-1-3...
  • Page 30 Section 1 - Ground Handling This Page Intentionally Left Blank Ground Servicing Guide Report No: 02484 Issue date: Feb 26, 2025 Page 1-1-4...

  • Page 31: Parking

    Section 1 - Ground Handling Parking Preliminary Requirements and Safety Conditions WARNING WHEN WORKING AT HEIGHT USE A SERVICEABLE PLATFORM OF THE CORRECT TYPE AND HEIGHT. MAKE SURE THAT THE PLATFORM IS STABLE. IF THE PLATFORM IS NOT STABLE, PERSONNEL CAN FALL, THIS CAN CAUSE DEATH OR INJURY TO PERSONNEL.

  • Page 32: Parking Guidelines

    Section 1 - Ground Handling Parking Guidelines Select a parking location: − On a hard, level surface − If possible, not in direct sunlight − Point the nose into the wind. When the aircraft is in the correct parking location: −...
  • Page 33 Section 1 - Ground Handling ICN-PC24-A-A15000000-A-S4080-07778-A-001-01 Figure 1-2-1: Parking - Tail Strut Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 1-2-3...
  • Page 34 Section 1 - Ground Handling LH SHOWN RH SIMILAR ICN-PC24-A-A15000000-A-S4080-07779-A-001-01 Figure 1-2-2: Parking - Emergency Exit Lock-Pin Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 1-2-4...
  • Page 35 Section 1 - Ground Handling 0.39 in. (10 mm) TYPICAL TYPICAL TYPICAL ICN-PC24-A-A15000000-A-S4080-07780-A-001-01 Figure 1-2-3: Parking - Air Data Probe Covers Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 1-2-5...
  • Page 36 Section 1 - Ground Handling NOTE: FOR AIRCRAFT WITH LITHIUM ION BATTERIES INSTALLED ICN-PC24-A-A15100000-A-S4080-07781-A-003-01 Figure 1-2-4: Parking - Nose Covers Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 1-2-6...
  • Page 37 Section 1 - Ground Handling LH SHOWN RH SIMILAR ICN-PC24-A-A15000000-A-S4080-07782-A-001-01 Figure 1-2-5: Parking - Wing Covers Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 1-2-7...
  • Page 38 Section 1 - Ground Handling NO STEP NO STEP TYPICAL LH SHOWN RH SIMILAR ICN-PC24-A-A15000000-A-S4080-07783-A-001-01 Figure 1-2-6: Parking - Upper Rear Fuselage Covers Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 1-2-8...
  • Page 39 Section 1 - Ground Handling LH SHOWN RH SIMILAR LH SHOWN RH SIMILAR ICN-PC24-A-A15000000-A-S4080-07743-A-001-01 Figure 1-2-7: Parking - Lower Rear Fuselage Covers Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 1-2-9...
  • Page 40 Section 1 - Ground Handling NOTE: FOR AIRCRAFT WITH LITHIUM ION BATTERIES INSTALLED ICN-PC24-A-A10000000-A-S4080-08959-A-002-01 Figure 1-2-8: Parking - Lithium Ion Battery 2 - Vent cover Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 1-2-10...
  • Page 41 Section 1 - Ground Handling ICN-PC24-A-A15120000-A-S4080-07153-A-001-01 Figure 1-2-9: Parking - Cockpit Cover Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 1-2-11...
  • Page 42 Section 1 - Ground Handling LH SHOWN RH SIMILAR ICN-PC24-A-A10000000-A-S4080-08961-A-001-01 Figure 1-2-10: Parking - Windhield inside covers Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 1-2-12...

  • Page 43: Mooring

    Section 1 - Ground Handling Mooring Applicable to all PC-24 aircraft: PC24 A Preliminary Requirements and Safety Conditions CAUTION Do not use the nose landing gear to moor the aircraft. This can cause damage to the aircraft. CAUTION Make sure that the rope is tight when it is attached to the aircraft and to the ground mooring points.
  • Page 44 Section 1 - Ground Handling Fig. 1-3-2 shows the tie-down areas. Create the six tie-down points in the tie-down area: − On a hard surface, use six mounting blocks − On a fine type soil, use six spike pickets − On a clay type soil or rock surface, use six screw pickets.
  • Page 45 Section 1 - Ground Handling TYPICAL ICN-PC24-A-A15000000-A-S4080-07872-A-001-01 ICN-PC24-A-A15000000-A-S4080-07872-A-001-01 Figure 1-3-1: Mooring - Tie-Down Points Ground Servicing Guide Report No: 02484 Issue date: Apr 29, 2020 Page 1-3-3...
  • Page 46 Section 1 - Ground Handling -0.5 -1.0 -1.5 -2.0 -2.5 -3.0 -3.5 -4.0 -4.5 -5.0 -5.5 -6.0 -6.5 -7.0 -7.5 -8.0 -8.5 -9.0 -9.5 10.0 11.0 12.0 13.0 14.0 15.0 16.0 17.0 AIRCRAFT LONGITUDINAL AXIS (M) SPECIFIED TIE-DOWN AREA ICN-PC24-A-A15000000-A-S4080-07787-A-001-01 Figure 1-3-2: Mooring - Tie-Down Areas Ground Servicing Guide Report No: 02484...

  • Page 47: Cargo - Loading/Unloading Procedure

    Section 1 - Ground Handling Cargo - Loading/Unloading procedure Applicable to all PC-24 aircraft: PC24 A General CAUTION MAKE SURE THE TAIL STRUT IS IN POSITION BEFORE YOU LOAD OR UNLOAD THE CARGO. IF THE TAIL STRUT IS NOT INSTALLED, DAMAGE TO THE AIRCRAFT CAN OCCUR.
  • Page 48 Section 1 - Ground Handling Select the Cargo Tie-Down Configuration Cargo must be symmetrically positioned in relation to the central axis of the aircraft and must not exceed the dimensions of the track fittings. Note Be careful when you load large items of baggage or cargo. The cargo door opening is 47.2 in (1,200 mm) by 47.2 in (1,200 mm).
  • Page 49 Section 1 - Ground Handling SIDE TYPICAL TYPICAL MIDDLE TYPICAL MIDDLE FULL WIDTH TYPICAL ICN-PC24-A-A15000000-A-S4080-05027-A-002-01 Figure 1-4-1: Cargo Tie-Down Kit Configurations Ground Servicing Guide Report No: 02484 Issue date: Jan 26, 2021 Page 1-4-3...
  • Page 50 Section 1 - Ground Handling 4 in ( 100 mm ) CARGO LARGE BAGGAGE 4 in RESTRAINT ( 100 mm ) CARGO SYSTEM 9.8 in ( 250 mm ) SMALL BAGGAGE 4 in RESTRAINT ( 100 mm ) CARGO SYSTEM 7.5 in ( 190 mm ) Figure 1-4-2: Cargo / Baggage Clearance...
  • Page 51 Section 1 - Ground Handling MAXIMUM CARGO STRAP ANGLE BETWEEN 10 AND 20 DEGREES MAXIMUM RECOMMENDED CARGO DIMENSIONS 45.5 in ( 1,156 mm ) ICN-PC24-A-A15000000-A-S4080-05029-A-002-01 Figure 1-4-3: Maximum Cargo Dimensions and Strap Angle Ground Servicing Guide Report No: 02484 Issue date: Jan 26, 2021 Page 1-4-5...
  • Page 52 Section 1 - Ground Handling This Page Intentionally Left Blank Ground Servicing Guide Report No: 02484 Issue date: Jan 26, 2021 Page 1-4-6...

  • Page 53: Ground Power Unit - Facility Requirements Associated With Servicing

    A Ground Power Unit (GPU), 28.5 Volt Direct Current (Vdc) is used to start the aircraft engines and to provide electrical power for servicing procedures. The requirements for a GPU for use with the Pilatus PC-24 are given in Table 1-5-1.
  • Page 54 Section 1 - Ground Handling This Page Intentionally Left Blank Ground Servicing Guide Report No: 02484 Issue date: Nov 08, 2024 Page 1-5-2...
  • Page 55 Section 2 - Aircraft Servicing SECTION 2 Aircraft Servicing Table of Contents Subject Page Ground Power Unit - Connect 2-1-1 Ground power unit 2-1-1 Connect the GPU to the aircraft 2-1-1 Disconnect the GPU from the aircraft 2-1-1 Inflate Tires 2-2-1 Preliminary Requirements and Safety Conditions 2-2-1...

  • Page 56: Subject

    Section 2 - Aircraft Servicing Subject Page Close up 2-6-4 Windows - Clean, check and apply rain repellent 2-7-1 Preliminary Requirements and Safety Conditions 2-7-1 Recommended Support Equipment 2-7-1 Cleaning Guidelines 2-7-2 Rain Repellent 2-7-3 Exterior - Clean 2-8-1 Preliminary Requirements and Safety Conditions 2-8-1 Recommended Support Equipment 2-8-2...

  • Page 57: Ground Power Unit - Connect

    A Ground Power Unit (GPU), 28.5 Volt Direct Current (Vdc) is used to start the aircraft engines and to provide electrical power for servicing procedures. The requirements for a GPU for use with the Pilatus PC-24 are given in Table 2-1-1.
  • Page 58 Section 2 - Aircraft Servicing This Page Intentionally Left Blank Ground Servicing Guide Report No: 02484 Issue date: Feb 26, 2025 Page 2-1-2...

  • Page 59: Inflate Tires

    Section 2 - Aircraft Servicing Inflate Tires Preliminary Requirements and Safety Conditions WARNING DO NOT POINT A COMPRESSED GAS OUTLET AT YOUR BODY OR AT OTHER PERSONNEL. THE COMPRESSED GAS CAN CAUSE INJURY TO PERSONNEL. WARNING DO NOT FILL A TIRE THAT IS DAMAGED. YOU CAN CAUSE AN EXPLOSION WHICH CAN KILL OR CAUSE AN INJURY TO PERSONNEL AND DAMAGE TO EQUIPMENT.

  • Page 60: Recommended Support Equipment

    Section 2 - Aircraft Servicing Recommended Support Equipment Equipment Recommended Pilatus Part Number Nitrogen cart Local supply Nitrogen, dry, minimum 97% purity Tire inflating gun Local supply 513.12.21.043 Tire Inflation Guidelines Check and inflate the tires as follows: Remove the cap from the inflation valve.
  • Page 61 Section 2 - Aircraft Servicing VALVE VALVE LH SHOWN RH SIMILAR ICN-PC24-A-A15000000-A-S4080-07791-A-001-01 Figure 2-2-1: Tires - Fill Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-2-3...

  • Page 62: Tire Markings

    Section 2 - Aircraft Servicing Tire markings Green paint dots are applied to new tires. The dots show the location of vent holes. Leakage from the vent holes is permitted. Refer to Fig. 2-2-2, views A and B. Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-2-4...
  • Page 63 Section 2 - Aircraft Servicing TYPICAL SIDEWALL VENTS TYPICAL DRY TIRE, VENT HOLE AND MARKING WET TIRE, SOAP SOLUTION OR LEAK DETECTION COMPOUND APPLIED. AIR ESCAPING ICN-PC24-A-A15120000-A-S4080-10189-A-001-01 Figure 2-2-2: Tires - Markings Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-2-5...
  • Page 64 Section 2 - Aircraft Servicing This Page Intentionally Left Blank Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-2-6...

  • Page 65: Stone Guard - Change

    Section 2 - Aircraft Servicing Stone guard - Change Preliminary Requirements and Safety Conditions Not applicable Tools and Support Equipment Not applicable Main Procedure This procedure contains the procedures that follow: − Remove the Quick-Release Stone Guard, Remove the Quick-Release Stone Guard −...
  • Page 66 Section 2 - Aircraft Servicing LH SHOWN RH SIMILAR LH SHOWN RH SIMILAR ICN-PC24-A-A15320000-A-S4080-08800-A-001-01 Figure 2-3-1: Quick-release stone guard - Remove and install Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-3-2...

  • Page 67: Fuel - Defuel And Drain Fuel

    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. 2-4-1 Fig.
  • Page 68 Section 2 - Aircraft Servicing TYPICAL 600 LBS 500 LBS 1100 LBS 1200 LBS TYPICAL REFUEL / DEFUEL PANEL PC24-A-A15120000-A-S4080-07910-A-002-01 Figure 2-4-1: Refuel / Defuel Compartment Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-4-2...
  • Page 69 Section 2 - Aircraft Servicing TYPICAL 600 LBS 500 LBS 1100 LBS 1200 LBS TYPICAL REFUEL / DEFUEL PANEL ICN-PC24-A-A15120000-A-S4080-07907-A-002-01 Figure 2-4-2: Refuel / Defuel Compartment with Suction Option Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-4-3...

  • Page 70: Drain Fuel

    Section 2 - Aircraft Servicing Drain Fuel Put a waste fuel container in position under the applicable drain valve. The waste fuel container capacity must be a minimum of 10 gallons (38 liters). Connect a bonding lead from the waste fuel container to the aircraft. Install the fuel drain tool in a drain valve and drain the fuel from the left and right wing.
  • Page 71 Section 2 - Aircraft Servicing LH SHOWN RH SIMILAR DRAIN VALVE FUEL DRAIN TOOL CONTAINER ICN-PC24-A-A15120000-A-S4080-07909-A-000-01 Figure 2-4-3: Fuel Drain Tool Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-4-5...
  • Page 72 Section 2 - Aircraft Servicing This Page Intentionally Left Blank Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-4-6...

  • Page 73: Refuel

    Section 2 - Aircraft Servicing Refuel Applicable to all PC-24 aircraft: PC24 A Preliminary Requirements and Safety Conditions CAUTION Do not use more than 60 pound per square inch (4.1 bar) at the fueling nozzle. Pressures more than 60 pound per square inch (4.1 bar) can cause damage to the fueling system components.

  • Page 74: Refueling Guidelines

    Section 2 - Aircraft Servicing Refueling Guidelines The information that follows gives guidance on: − Pressure refueling − Gravity refueling − Draining water from the fuel tanks. The approved fuel grades are: − Jet A (ASTM-D1655-17) − Jet A-1 (ATSM-D1655-17) −...
  • Page 75 Section 2 - Aircraft Servicing PRESSURE REFUEL / DEFUEL GRAVITY REFUEL GRAVITY REFUEL ICN-PC24-A-A15000000-A-S4080-01902-A-000-01 Figure 2-5-1: Fuel System - Refueling Points Ground Servicing Guide Report No: 02484 Issue date: Apr 29, 2020 Page 2-5-3...
  • Page 76 Section 2 - Aircraft Servicing 600 LB 500 LB 1100 LB 1200 LB ICN-PC24-A-A15000000-A-S4080-01616-A-003-01 Figure 2-5-2: Refuel / Defuel Panel Ground Servicing Guide Report No: 02484 Issue date: Apr 29, 2020 Page 2-5-4...
  • Page 77 Section 2 - Aircraft Servicing Pressure Refueling Follow the instructions given on the placards in the refuel panel compartment. ICN-PC24-A-A15000000-A-S4080-07829-A-002-01 Figure 2-5-3: Fuel - Refuel by Pressure Ground Servicing Guide Report No: 02484 Issue date: Apr 29, 2020 Page 2-5-5...
  • Page 78 Section 2 - Aircraft Servicing Gravity Refueling CAUTION Be careful when you work near the wing leading edges. The wing leading edges are easily damaged. Note This procedure is the same for the left and right fuel tanks. Connect the fueling vehicle ground lead to the aircraft ground point on the nose landing gear.
  • Page 79 Section 2 - Aircraft Servicing LEVER GRAVITY FILLER CAP FILLER CAP LH SHOWN ADAPTER RH SIMILAR FUELING NOZZLE GRAVITY FILLER CAP FILLER CAP ADAPTER ICN-PC24-A-A15000000-A-S4080-07830-A-001-01 Figure 2-5-4: Fuel - Refuel by Gravity Ground Servicing Guide Report No: 02484 Issue date: Apr 29, 2020 Page 2-5-7...
  • Page 80 Section 2 - Aircraft Servicing Drain Water CAUTION Do not start the engines if a large amount of contamination is found during the drain water procedure. Note This procedure is the same for the four drain valves. The two forward drain valves drain the left and right collector tanks.
  • Page 81 Section 2 - Aircraft Servicing LH SHOWN RH SIMILAR DRAIN VALVE FUEL TANK DRAIN RESERVOIR ICN-PC24-A-A15000000-A-S4080-07831-A-001-01 Figure 2-5-5: Fuel - Drain Water Ground Servicing Guide Report No: 02484 Issue date: Apr 29, 2020 Page 2-5-9...
  • Page 82 Section 2 - Aircraft Servicing This Page Intentionally Left Blank Ground Servicing Guide Report No: 02484 Issue date: Apr 29, 2020 Page 2-5-10...

  • Page 83: Engine Oil - Fill

    Section 2 - Aircraft Servicing Engine oil - Fill Preliminary Requirements and Safety Conditions WARNING DO NOT TOUCH THE ENGINE SURFACES IMMEDIATELY AFTER ENGINE OPERATION. THE ENGINE SURFACES ARE HOT. THIS CAN CAUSE DEATH OR INJURY TO PERSONNEL. WARNING ENGINE OIL IS TOXIC. PROTECTIVE CLOTHING MUST BE WORN WHEN HANDLING ENGINE OIL.

  • Page 84: Recommended Support Equipment

    − Mobil 254. It is permitted to mix the approved oils above, when necessary, because of normal oil consumption. Recommended Support Equipment Equipment Pilatus Part Number Absorbent paper Local supply “DO NOT OPERATE THE ENGINES” placard Local supply Funnel Local supply...

  • Page 85: Fill The Engine With Oil

    Section 2 - Aircraft Servicing Fill the engine with oil Note The oil filler cap is retained by a cable. Press down and turn the oil filler cap Figure 2-6-1 [1] anticlockwise to open. Remove the oil filler cap Figure 2-6-1 [1] from the top of the oil tank Figure 2-6-1 [2].

  • Page 86: Close Up

    Section 2 - Aircraft Servicing Close up Close the applicable LH/RH oil door on the engine nacelle. Refer to Fig. 2-6-1, views A and B. Flight crew must make sure that all access panels are closed correctly. Remove ladder or servicing platform from next to the applicable LH/RH engine nacelle. Remove all placards used in this procedure.
  • Page 87 Section 2 - Aircraft Servicing RH OIL DOOR ZONE 420 ZONE 330 ZONE 340 ZONE 410 LH OIL DOOR LH SHOWN RH SIMILAR ICN-PC24-A-A15120000-A-S4080-10622-A-001-01 Figure 2-6-1: Engine oil - Fill (Sheet 1 of 2) Ground Servicing Guide Report No: 02484 Issue date: Nov 08, 2024 Page 2-6-5...
  • Page 88 Section 2 - Aircraft Servicing FILLER CAP FILLER CAP NOT CLOSED CLOSED CORRECTLY BLUE MARKS BLUE MARKS NOT ALIGNED ALIGNED RED BAND NOT VISIBLE RED BAND VISIBLE PIN NOT LOCATED IN THE CORRECTLY GROOVE LOCATED IN THE GROOVE ICN-PC24-A-A15120000-A-S4080-10623-A-001-01 Figure 2-6-1: Engine oil - Fill (Sheet 2 of 2) Ground Servicing Guide Report No: 02484 Issue date: Nov 08, 2024...

  • Page 89: Windows - Clean, Check And Apply Rain Repellent

    THAT ARE NOT LISTED CAN CAUSE DAMAGE TO THE WINDOW ACRYLIC PANES AND THE WINDOW SEALS, AND CAN AFFECT THE RAIN-REPELLENT PERFORMANCE OF THE WINDSHIELDS. Recommended Support Equipment Equipment Recommended Pilatus Part Number Chamois leather Local supply Isopropyl (Isopropanol) Local supply Light soap (dish washing)

  • Page 90: Cleaning Guidelines

    Section 2 - Aircraft Servicing Equipment Recommended Pilatus Part Number Polishing slurry Local supply Master kit, Surfex 100 (MPG windshields) Local supply Surface activation concentrate / surface preparation Local supply solution Surface Seal DSS4040 (PPG and MPG windshields) Local supply...

  • Page 91: Rain Repellent

    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.
  • Page 92 Section 2 - Aircraft Servicing Rain repellent coating inspection intervals The durability of the: − Repellent type − Aircraft use − Operating conditions. The operator must make sure that the correct recommended inspection interval is used for the type of rain repellent, aircraft use and operating conditions. Refer to Table 2-7-1.
  • Page 93 Section 2 - Aircraft Servicing Check the condition of the rain repellent coating Make sure the windshield is clean as given in Cleaning Guidelines. Clean with Isopropanol and paper wipes. Wipe windshield fully dry with clean paper wipes. Spray the windshield with Deionized water). If the water “beads up”...
  • Page 94 Section 2 - Aircraft Servicing Figure 2-7-2: Windshields - Rain repellent (satisfactory condition) Figure 2-7-3: Windshields - Rain repellent (unsatisfactory condition) Apply the rain repellent coating Note Each new windshield and cockpit side window is supplied with rain repellent applied. This application procedure is applicable to windshields only.
  • Page 95 Section 2 - Aircraft Servicing The conditions that follow are applicable to all rain repellent application procedures: − Ambient temperature must be between 41 and 68 °F (5 and 30 °C) − Protect the windshield from direct sun light, rain, snow and all other sources of possible contamination −...
  • Page 96 Section 2 - Aircraft Servicing For the MPG windows use the Masterkit, Surfex 100, refer to: − https://www.boeingdistribution.com/ − https://aeroval.com/ref/287834/7137/ − https://www.globalparts.aero − https://www.sealdynamics.com Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-7-8...
  • Page 97 Section 2 - Aircraft Servicing Clean the windshield as follows: Make sure the windshield is clean as given in Cleaning Guidelines. Apply masking tape to the edges of the windshield, the weather seal and 0.25 in (6.0 mm) of the glass. Make sure that the masking tape gives a water tight seal.
  • Page 98 Section 2 - Aircraft Servicing 1.14.10 Discard the used paper wipes and the disposable gloves in a disposable bag. Note It is necessary to do this step in less than 10 minute to prevent contamination. Apply the rain repellent as follows: Use a new pair of disposable gloves.
  • Page 99 The heating blanket temperature is pre-set for the necessary curing temperature. Note Pilatus Aircraft Ltd. recommend you heat cure the windshield. If you do not heat cure the windshield the recommended rain repellent inspection interval is reduced. The recommended inspection interval is given in...
  • Page 100 Section 2 - Aircraft Servicing Clean the windshield as follows: Make sure the windshield is clean as given in Cleaning Guidelines. Apply masking tape to the edges of the windshield, the weather seal and 0.25 in (6.0 mm) of the glass. Make sure that the masking tape gives a water tight seal.
  • Page 101 Section 2 - Aircraft Servicing 2.4.3 Overlap the straight line strokes. 2.4.4 If necessary, apply more surface preparation solution to make the gauze pads moist. 2.4.5 Apply from the center to the edges. Do not apply to the taped edges. 2.4.6 Apply a thin film of the surface preparation solution around the edges.
  • Page 102 Section 2 - Aircraft Servicing 3.4.7 Do not use the gauze pads used at the edges to apply to the coating solution, master kit to the center. 3.4.8 Let the applied layer of coating solution, master kit dry for a minimum of 5 minutes.
  • Page 103 The heating blanket temperature is pre-set for the necessary curing temperature. Note Pilatus Aircraft Ltd. recommend you heat cure the windshield. If you do not heat cure the windshield the recommended rain repellent inspection interval is reduced. The recommended inspection interval is given in...
  • Page 104 Section 2 - Aircraft Servicing Polish the windshield as follows: Make sure the windshield is clean as given in Cleaning Guidelines. Apply masking tape to the edges of the windshield, the weather seal and 0.25 in (6.0 mm) of the glass. Make sure that the masking tape gives a water tight seal.
  • Page 105 Section 2 - Aircraft Servicing Put approximately 1/4 of the surface preparation solution on to some gauze pads to make them moist. Do not let the surface preparation solution drip from the gauze pads. Use the gauze pads and apply the surface preparation solution to the windshield glass surface as follows: 2.4.1 Start at the center of windshield glass surface.
  • Page 106 Section 2 - Aircraft Servicing 3.4.2 Apply a thin film of the coating solution, master kit with short, circular movements. 3.4.3 If necessary, apply more coating solution, master kit to make the gauze pads moist. 3.4.4 Apply from the center to the edges. 3.4.5 Apply a thin film of the coating solution, master kit with short, circular movements around the edges.
  • Page 107 For training on the procedure there is a product video in the master kit. Note Pilatus Aircraft Ltd. recommend you heat cure the windshield. If you do not heat cure the windshield the recommended rain repellent inspection interval is reduced. The recommended inspection interval is given in...
  • Page 108 Section 2 - Aircraft Servicing Prepare the windshield as follows: Make sure the windshield is clean as given in Cleaning Guidelines. Put on a new pair of disposable gloves. Prepare the coating solution, quick application kit, refer to the product manual in the quick application kit, surface seal.

  • Page 109: Exterior - Clean

    Section 2 - Aircraft Servicing Exterior - Clean Preliminary Requirements and Safety Conditions WARNING BE CAREFUL WHEN YOU USE THE CONSUMABLE MATERIALS. OBEY THE MANUFACTURER´S HEALTH AND SAFETY INSTRUCTIONS AND ALL THE APPLICABLE LOCAL INSTRUCTIONS. CONSUMABLE MATERIALS CAN BE DANGEROUS AND CAN CAUSE DEATH OR INJURY TO PERSONNEL AND / OR DAMAGE TO EQUIPMENT.

  • Page 110: Recommended Support Equipment

    Note In hot climates, it is recommended not to clean the aircraft during the hottest hours of the day. Recommended Support Equipment Tool / Equipment Recommended Pilatus Part Aircraft polish Nushine II S Clean water Local supply Cleaner Zero V.O.C. Degreaser XE3-G...
  • Page 111 Section 2 - Aircraft Servicing Table 2-8-1: Aircraft exterior wash intervals (continued from previous page) Aircraft in hanger Aircraft exterior wash intervals 3 months It is recommended that the water quality is within the specification that follows: Element Requirement Chloride concentration Less than 250 mg / l pH value 6.5 - 8.5...
  • Page 112 Section 2 - Aircraft Servicing Cleaning the Wing Leading Edge Use a lint-free cleaning cloth moist with the cleaning solvent to carefully clean the wing leading edge. Clean a small area of the wing leading edge at a time by rubbing the surface in the direction of the curve of the wing leading edge.
  • Page 113 Ground spoilers and spoiler mechanisms − Multi-function spoilers and spoiler mechanisms. If corrosion or damaged CPC is found, contact your service centre. The corrosion or damaged CPC must be repaired / restored according to PC-24 Aircraft Maintenance Manual. Ground Servicing Guide Report No: 02484...
  • Page 114 Section 2 - Aircraft Servicing Remove the covers from these items: − Engines (Fig. 2-8-1) − Environmental Control System (ECS) intake (Fig. 2-8-1) − Vapor Cooling System (VCS) outlets (Fig. 2-8-2) − Ice detectors (Fig. 2-8-3) − Angle of Attack (AOA) sensors (Fig.
  • Page 115 Section 2 - Aircraft Servicing NO STEP NO STEP TYPICAL LH SHOWN RH SIMILAR ICN-PC24-A-A15000000-A-S4080-07783-A-001-01 Figure 2-8-1: Parking - Upper Rear Fuselage Covers Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-8-7...
  • Page 116 Section 2 - Aircraft Servicing LH SHOWN RH SIMILAR LH SHOWN RH SIMILAR ICN-PC24-A-A15000000-A-S4080-07743-A-001-01 Figure 2-8-2: Parking - Lower Rear Fuselage Covers Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-8-8...
  • Page 117 Section 2 - Aircraft Servicing 0.39 in. (10 mm) TYPICAL TYPICAL TYPICAL ICN-PC24-A-A15000000-A-S4080-07780-A-001-01 Figure 2-8-3: Parking - Air Data Probe Covers Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-8-9...
  • Page 118 Section 2 - Aircraft Servicing NOTE: FOR AIRCRAFT WITH LITHIUM ION BATTERIES INSTALLED ICN-PC24-A-A15100000-A-S4080-07781-A-003-01 Figure 2-8-4: Parking - Nose Covers Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-8-10...
  • Page 119 Section 2 - Aircraft Servicing NOTE: FOR AIRCRAFT WITH LITHIUM ION BATTERIES INSTALLED ICN-PC24-A-A10000000-A-S4080-08959-A-002-01 Figure 2-8-5: Parking - Lithium Ion Battery 2 - Vent cover Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-8-11...
  • Page 120 Section 2 - Aircraft Servicing ACCEPTABLE CPC ARDROX AV 40 INSPECTION WITH A UV LIGHT Figure 2-8-6: Corrosion preventive compound around rivets and fasteners - Acceptable Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-8-12...

  • Page 121: Exterior - Clean With Water

    Section 2 - Aircraft Servicing Exterior - Clean with water CAUTION MAKE SURE THAT THE WATER USED TO CLEAN THE AIRCRAFT IS FREE FROM CONTAMINATION. IF THE WATER HAS CONTAMINATION IT CAN CAUSE CORROSION OR DAMAGE TO THE EXTERNAL SURFACE OF THE AIRCRAFT. CAUTION DO NOT USE HIGH PRESSURE WATER TO CLEAN THE EXTERNAL SURFACE OF THE AIRCRAFT.

  • Page 122: Recommended Support Equipment

    Cleaning Guidelines CAUTION MAKE SURE THAT THE WATER QUALITY FOR THE AIRCRAFT EXTERIOR CLEANING IS AS SPECIFIED BY PILATUS AIRCRAFT LTD. IF IT IS NOT, THE WATER CAN CAUSE CORROSION OR DAMAGE TO THE EXTERNAL SURFACE OF THE AIRCRAFT. The procedures that follow give guidelines to: −...
  • Page 123 Section 2 - Aircraft Servicing Prepare the Aircraft CAUTION DO NOT USE ADHESIVE TAPE TO COVER THE STATIC PORTS. IF YOU DO, RESIDUAL ADHESIVE CAN STAY ON THE STATIC PORT, ATTRACT CONTAMINATION AND CAUSE INCORRECT STATIC PRESSURE FOR AIRCRAFT SYSTEMS. Flight crew or authorized trained personnel - set the flaps to 33°.
  • Page 124 Section 2 - Aircraft Servicing Rinse the surface of the aircraft with water CAUTION MAKE SURE THAT THE DE-ICE FLUID RESIDUE DOES NOT GET INTO CAVITIES OR CAUSE A BLOCKAGE IN THE DRAIN HOLES. DE-ICE FLUID RESIDUE THAT HAS COLLECTED IN CAVITIES AND BLOCKED DRAIN HOLES CAN CAUSE DAMAGE TO THE AIRCRAFT.
  • Page 125 Section 2 - Aircraft Servicing Requirements after Job Completion Remove the cockpit covers from the items that follow. Refer to Fig. 2-9-2: − Ice detector (if installed) Figure 2-9-2 [3] − Angle of attack sensors Figure 2-9-2 [4] − Pitot probes Figure 2-9-2 [5] −...
  • Page 126 Section 2 - Aircraft Servicing ZONE 350 ZONE 420 ZONE 410 LH SHOWN RH SIMILAR Figure 2-9-1: Water rinse - Exterior covers, aft Ground Servicing Guide Report No: 02484 Issue date: Nov 08, 2024 Page 2-9-6...
  • Page 127 Section 2 - Aircraft Servicing ZONE 221 TYPICAL TYPICAL TYPICAL Figure 2-9-2: Water rinse - Exterior covers, cockpit Ground Servicing Guide Report No: 02484 Issue date: Nov 08, 2024 Page 2-9-7...
  • Page 128 Section 2 - Aircraft Servicing SECTION 4 SECTION 3 SECTION1 SECTION 2 SECTION 5 SECTION 6 Figure 2-9-3: Exterior aircraft zones Ground Servicing Guide Report No: 02484 Issue date: Nov 08, 2024 Page 2-9-8...

  • Page 129: Interior - Clean

    Section 2 - Aircraft Servicing Interior - Clean Applicable to all PC-24 aircraft: PC24 A Preliminary Requirements and Safety Conditions WARNING BE CAREFUL WHEN YOU USE THE CONSUMABLE MATERIALS. OBEY THE MANUFACTURER’S HEALTH AND SAFETY INSTRUCTIONS. CAUTION Do not clean fabric surfaces with a soap solution or water. This can inhibit the properties of the fireblock treatment applied to the fabric.

  • Page 130: Cleaning Guidelines

    Section 2 - Aircraft Servicing Cleaning Guidelines These procedures give guidelines for cleaning the interior surfaces of the cabin and flight deck. Cabin Use a vacuum cleaner to clean: − Seats − Floor − Seat tracks. If the seat track is covered by a carpet, clean where you can get access.

  • Page 131: Waste / Water System Servicing

    Section 2 - Aircraft Servicing Waste / Water System Servicing Applicable to all PC-24 aircraft: PC24 A Ground Servicing Guide Report No: 02484 Issue date: Apr 29, 2020 Page 2-11-1...

  • Page 132: Preliminary Requirements And Safety Conditions

    Section 2 - Aircraft Servicing Preliminary Requirements and Safety Conditions WARNING PUT ON PROTECTIVE CLOTHING, PROTECTIVE GOGGLES, AND GLOVED BEFORE YOU DO WORK ON THE WATER AND WASTE SYSTEM. THIS WILL HELP PREVENT INJURY OR DEATH. CAUTION Do not deploy or operate the toilet when the cabin temperature is less than 36 °Fahrenheit (2 °Celsius).
  • Page 133 Section 2 - Aircraft Servicing WATER DRAIN HANDLE RINSE PORT NOTE: VACUUM TOILET ASSEMBLY SHOWN STOWED DRAIN VALVE ICN-PC24-A-A150000-A-S4080-00708-A-000-01 Figure 2-11-1: Vacuum Waste System - Component Location Ground Servicing Guide Report No: 02484 Issue date: Apr 29, 2020 Page 2-11-3...
  • Page 134 Section 2 - Aircraft Servicing Drain the Waste Tank De-energise the electrical system. Open the vacuum waste system panel door, Fig. 2-11-1 shows the location of the waste system panel. Follow the instructions given on the placard on the vacuum waste panel door. Close the vacuum waste system panel.
  • Page 135 Section 2 - Aircraft Servicing ICN-PC24-A-A15380000-A-S4080-05400-A-000-01 Figure 2-11-2: Water tank - Fill using the funnel (Sheet 1 of 2) Ground Servicing Guide Report No: 02484 Issue date: Apr 29, 2020 Page 2-11-5...
  • Page 136 Section 2 - Aircraft Servicing ICN-PC24-A-A15380000-A-S4080-05414-A-000-01 Figure 2-11-2: Water tank - Fill using the funnel (Sheet 2 of 2) Drain the Water Tank De-energise the electrical system. Open the vacuum waste system panel door. Put a container with a minimum capacity of 2 Gallon (7.5 Liter) under the water drain outlet (Figure 2-11-3 [2]).
  • Page 137 Section 2 - Aircraft Servicing FRAME 18 PC24-A-A15120000-A-S4080-07870-A-001-01 Figure 2-11-3: Water tank - Drain Ground Servicing Guide Report No: 02484 Issue date: Apr 29, 2020 Page 2-11-7...
  • Page 138 Section 2 - Aircraft Servicing This Page Intentionally Left Blank Ground Servicing Guide Report No: 02484 Issue date: Apr 29, 2020 Page 2-11-8...

  • Page 139: Waste / Water System - Clean With Chemical Agent

    Section 2 - Aircraft Servicing Waste / Water System - Clean with chemical agent Preliminary Requirements and Safety Conditions WARNING BE CAREFUL WHEN YOU DO WORK ON THE ELECTRICAL SYSTEM OR A SYSTEM THAT USES THE ELECTRICAL POWER. MAKE SURE THAT IT IS SAFE BEFORE YOU APPLY ELECTRICAL POWER TO THE AIRCRAFT OR ENERGIZE THE AIRCRAFT ELECTRICAL SYSTEMS.
  • Page 140 Section 2 - Aircraft Servicing WARNING COMPONENTS WHICH HAVE BEEN IN CONTACT WITH SEWAGE ARE A HEALTH HAZARD. WASH THE PARTS WITH SOAP, HOT WATER AND SANITIZER. IF COMPONENTS ARE NOT PROPERLY WASHED INJURY TO PERSONNEL CAN OCCUR. WARNING COMPONENTS WHICH HAVE BEEN IN CONTACT WITH SEWAGE ARE A HEALTH HAZARD.

  • Page 141: Recommended Support Equipment

    Note Cleaning is recommended to reduce odors, discoloration, and scale buildup, even if the vacuum waste system is not used. Recommended Support Equipment Equipment Recommended Pilatus Part Number Acetic acid (vinegar) Local supply Antimicrobial soap Local supply Apron Local supply...
  • Page 142 Section 2 - Aircraft Servicing Clean the external components of the waste system, where access is available, as follows: Use fresh hot water, antimicrobial soap and a brush (non metallic) to clean the external surfaces of the: − Waste tank (Figure 2-12-1 [17]) −...
  • Page 143 Section 2 - Aircraft Servicing Clean the external components of the water system, where access is available, as follows: Use fresh hot water, antimicrobial soap and a brush (non metallic) to clean the external surfaces of the: − Water tank assembly (Figure 2-12-1 [23]) −...
  • Page 144 Section 2 - Aircraft Servicing Make approximately 2.5 US gallons (gal) (9.4 L) of water system disinfectant solution as follows: Mix eight parts water system disinfectant with one part citric acid by volume. Dilute the solution with water to a 100 parts per million (ppm) concentration. Mix the solution well and wait for five minutes.

  • Page 145: Return To Service

    Section 2 - Aircraft Servicing If necessary, use 0.26 gal (1 L) of warm water to flush remaining crushed ice. Drain the waste tank. Put 1.06 gal (4 L) of acetic acid (vinegar) in the toilet bowl (Figure 2-12-1 [6]). Keep the acetic acid in the toilet bowl (Figure 2-12-1 [6]) for 15 minutes.
  • Page 146 Section 2 - Aircraft Servicing FRAME 17 ICN-PC24-A-A15120000-A-S4080-09011-A-002-01 Figure 2-12-1: Water and waste system - Clean (Sheet 1 of 4) Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-12-8...
  • Page 147 Section 2 - Aircraft Servicing ICN-PC24-A-A15120000-A-S4080-09012-A-001-01 Figure 2-12-1: Water and waste system - Clean (Sheet 2 of 4) Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-12-9...
  • Page 148 Section 2 - Aircraft Servicing MSN 101 TO 150 ICN-PC24-A-A15120000-A-S4080-09013-A-001-01 Figure 2-12-1: Water and waste system - Clean (Sheet 3 of 4) Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-12-10...
  • Page 149 Section 2 - Aircraft Servicing MSN 150 AND UP ICN-PC24-A-A15120000-A-S4080-09014-A-001-01 Figure 2-12-1: Water and waste system - Clean (Sheet 4 of 4) Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-12-11...
  • Page 150 Section 2 - Aircraft Servicing This Page Intentionally Left Blank Ground Servicing Guide Report No: 02484 Issue date: Jan 31, 2023 Page 2-12-12...

  • Page 151: Cold Weather Procedures (Deicing / Anti-Icing)

    Section 2 - Aircraft Servicing Cold Weather Procedures (Deicing / Anti-Icing) Applicable to all PC-24 aircraft: PC24 A Preliminary Requirements and Safety Conditions WARNING THE DEICING AND ANTI-ICING PROCEDURES MUST BE DONE BY PERSONS THAT ARE FULLY TRAINED, QUALIFIED AND APPROVED IN THE USE OF DEICING / ANTI-ICING FLUIDS AND THE EQUIPMENT.
  • Page 152 Section 2 - Aircraft Servicing Deicing Methods In clear weather, it may be possible to manually remove all contamination to allow a safe takeoff and flight. Deicing fluids can also be used to quickly melt and remove frost or other ice formations.
  • Page 153 CAUTION The aircraft 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 supply Brush Local supply...
  • Page 154 Section 2 - Aircraft Servicing 2.3.2 Deicing CAUTION When ice, snow or slush is removed from the aircraft surface, care must be taken to prevent entry and accumulation of ice, snow or slush into intakes or control surface hinge areas. Note Deicing and anti-icing fluid may splash onto heated surfaces such as air data probes and engine nacelles which can produce significant vapor.
  • Page 155 Section 2 - Aircraft Servicing Mobile ground support equipment with the capability of heating deicing fluid and dispensing large quantities of fluid at high pressures can be used. This type of equipment with the fluid temperature limited to 160 °F (70 °C) can be used to deice the aircraft. Fig.
  • Page 156 Section 2 - Aircraft Servicing IS THERE ANY CONTAMINATION ( FROST, ICE, SNOW OR SLUSH ) ON THE WINGS, CONTROL SURFACES, ENGINE INLETS? IS THE TEMPERATURE LESS THAN 50 °F ( 10 °C ) AND VISIBLE MOISTURE OR ICING CONDITIONS ARE PRESENT? ( ICE, FROST, SLUSH OR SNOW ) ICING CONDITIONS PRESENT DURING DESCENT, APPROACH OR TAXI?
  • Page 157 Section 2 - Aircraft Servicing 2.3.3 Deicing / Anti-icing the Wings, Stabilizers and Fuselage Note Deicing / anti-icing can be done as a one or two step process. Step one is to deice the aircraft and step two, if necessary, is to anti-ice the aircraft before takeoff. The one step process applies heated deicing fluid to remove contamination and also provide some anti-icing protection.
  • Page 158 Section 2 - Aircraft Servicing 2.3.4 Deicing / Anti-icing the Landing Gear CAUTION The application of deicing / anti-icing fluid in the landing gear must be kept to a minimum. Deicing / anti-icing fluid must not be directed onto the brakes and wheels.
  • Page 159 Section 2 - Aircraft Servicing AVOID DIRECT SPRAYING OF DEICING FLUID ON THE FOLLOWING AREAS : ENGINE INLETS BRAKES RAM AIR INLETS WINDSHIELD WHEELS PITOT - STATIC PROBES CABIN WINDOWS ICE DETECTORS AOA SENSORS APPLY DEICING FLUID TO THESE AREAS DO NOT APPLY DEICING FLUID TO THESE AREAS REMOVE DEICING FLUID...
  • Page 160 Section 2 - Aircraft Servicing AVOID DIRECT SPRAYING OF DEICING FLUID ON THE FOLLOWING AREAS : ENGINE INLETS BRAKES RAM AIR INLETS WINDSHIELD WHEELS PITOT - STATIC PROBES CABIN WINDOWS ICE DETECTORS AOA SENSORS APPLY DEICING / ANTI - ICING FLUID TO THESE AREAS DO NOT APPLY DEICING / ANTI - ICING...
  • Page 161 Section 2 - Aircraft Servicing 2.3.5 Post Deicing Inspection After deicing / anti-icing a visual inspection, for contamination, must be done at these locations: − Air data probes − Wing leading edges, upper and lower surfaces, spoilers, aileron surfaces including the wing seals −...
  • Page 162 Section 2 - Aircraft Servicing This Page Intentionally Left Blank Ground Servicing Guide Report No: 02484 Issue date: May 13, 2020 Page 2-13-12...

  • Page 163: Unpaved Runway Conditions - Scheduled Inspection

    Section 2 - Aircraft Servicing Unpaved runway conditions - Scheduled inspection Applicable to all PC-24 aircraft: PC24 A Ground Servicing Guide Report No: 02484 Issue date: Feb 16, 2021 Page 2-14-1...

  • Page 164: Main Procedure

    Section 2 - Aircraft Servicing Main Procedure This procedure has these sections: − Scheduled Inspection every 10 Flights Scheduled Inspection every 10 Flights − Scheduled Inspection every 100 Flights Scheduled Inspection every 100 Flights. Scheduled Inspection every 10 Flights CAUTION LOOSE PROTECTIVE FOIL IS A FOD RISK.
  • Page 165 ● Loose or missing pieces. If contaminated, clean the affected area. If damage or loose items are found repair / replace / remove as necessary or contact an authorized Pilatus service center. Ground Servicing Guide Report No: 02484 Issue date: Feb 16, 2021...

  • Page 166: Requirements After Job Completion

    The MLG belly fairings. If contaminated, clean the affected area. If damage is found repair / replace as necessary or contact an authorized Pilatus service center. Requirements after Job Completion Remove all the equipment, tools and materials from the work area. Make sure that the work area is clean.
  • Page 167 Section 2 - Aircraft Servicing FRAME 9 FRAME 10 RIB 5 RIB 5 ICN-PC24-A-A15120000-A-S4080-07819-A-001-01 Figure 2-14-1: Unpaved runway conditions - Scheduled inspection zones Ground Servicing Guide Report No: 02484 Issue date: Feb 16, 2021 Page 2-14-5...
  • Page 168 Section 2 - Aircraft Servicing ICN-PC24-A-A15120000-A-S4080-09031-A-001-01 Figure 2-14-2: Unpaved runway conditions - Protective foil inspection (Sheet 1 of 4) Ground Servicing Guide Report No: 02484 Issue date: Feb 16, 2021 Page 2-14-6...
  • Page 169 Section 2 - Aircraft Servicing PROTECTION FILM ICN-PC24-A-A15120000-A-S4080-09032-A-001-01 Figure 2-14-2: Unpaved runway conditions - Protective foil inspection (Sheet 2 of 4) Ground Servicing Guide Report No: 02484 Issue date: Feb 16, 2021 Page 2-14-7...
  • Page 170 Section 2 - Aircraft Servicing FRAME 28 PROTECTION FILM NOTE: ADF ANTENNA SHOWN INSTALLED - OPTIONAL EQUIPMENT ICN-PC24-A-A15120000-A-S4080-09033-A-001-01 Figure 2-14-2: Unpaved runway conditions - Protective foil inspection (Sheet 3 of 4) Ground Servicing Guide Report No: 02484 Issue date: Feb 16, 2021 Page 2-14-8...
  • Page 171 Section 2 - Aircraft Servicing LH SHOWN RH SIMILAR PROTECTION FILM ICN-PC24-A-A15120000-A-S4080-09040-A-001-01 Figure 2-14-2: Unpaved runway conditions - Protective foil inspection (Sheet 4 of 4) Ground Servicing Guide Report No: 02484 Issue date: Feb 16, 2021 Page 2-14-9...
  • Page 172 Section 2 - Aircraft Servicing This Page Intentionally Left Blank Ground Servicing Guide Report No: 02484 Issue date: Feb 16, 2021 Page 2-14-10...

Table of Contents