Att.3_Paint Schemes 1 & 2.pdf

Perfecting Paint Schemes Since 1997

SCHEME I

Challenger 605 - N91

Paint Scheme Specification

Prepared for:

FAA

June 25, 2021

All dimensions used are only a guide.

Paint shop to determine final dimensions during the paint scheme layout.

COPYRIGHT © 2021 by Scheme Designers, Inc. - These drawings and paint schemes may only be used for the aircraft shown. Drawings and specifications shall be returned to the owner after the aircraft painting is complete. Reproduction of this scheme on another aircraft requires written permission of Scheme Designers, Inc.

www.schemedesigners.com 80 Broadway, Second Floor

Cresskill, NJ 07626, USA 201-569-7785 craig@schemedesigners.com

Aircraft Length Used: 821”

N91-6-25-21-0

Scheme Designers, Inc.

+1.201.569.7785 www.schemedesigners.com Copyright © 2021 by Scheme Designers, Inc.

Perfecting Paint Schemes Since 1997

Final Specifications Page 1

Challenger 605 - N91

FAA

Final Paint Scheme Design

White:

Matterhorn White

Jet Glo CM0570566

Blue:

Fighter Blue

Acry Glo W07445

Gold:

Antique Gold Metallic

Acry Glo H10512

Red:

Flight Red

Acry Glo W07432

Gray:

Aviation Gray

Acry Glo W00067 www.schemedesigners.com Copyright © 2021 by Scheme Designers, Inc.

Perfecting Paint Schemes Since 1997

Final Specifications Page 2

Challenger 605 - N91

FAA

NOTE:

The design on the right side of the aircraft is the mirror image of that on the left side.

Templates should be used to facilitate the layout from one side to the other.

Similar dimensions apply.

Right Side View www.schemedesigners.com Copyright © 2021 by Scheme Designers, Inc.

Perfecting Paint Schemes Since 1997

Final Specifications Page 3

Challenger 605 - N91

FAA

Fuselage Flow & Overall Notes

The cabin doors and the emergency exits have a 2” wide gray band along the inside edges of the doors and exits.

Where the door bands cross the blue and gold accent stripes, the edges of the door bands are separated from stripes by a 1/2” constant white outline.

See Left and Right profile views for additional detail.

NOTES:

The stripes are convex from the nose to below the center of the 4th cabin window, and concave from there aft. They both widen gradually as they flow aft. The stripes are separated from one another by a constant 1” white space.

www.schemedesigners.com Copyright © 2021 by Scheme Designers, Inc.

Perfecting Paint Schemes Since 1997

Final Specifications Page 4

Challenger 605 - N91

FAA

Flag & Registration

LEFT SIDE REGISTRATION

RIGHT SIDE REGISTRATION

The registration consists of 12” high rounded digits, Oangled aft on both sides at 15 . The digits are blue with a 1/4” white gap and a 1/2” gold drop shadow down and aft of each digit on both sides of the aircraft.

Paint masks are required. These are available from Scheme Designers, Inc. Contact Craig at 201-569-7785 or at craig@schemedesigners.com.

www.schemedesigners.com Copyright © 2021 by Scheme Designers, Inc.

Perfecting Paint Schemes Since 1997

Final Specifications Page 5

Challenger 605 - N91

FAA

RSVM Markings

12.6

CL

WL 100

WL 76

FS 1 85.5 FS220

1/2

1/2

NOTE 1:

The markings are applied in gray paint.

Markings are duplicated in a mirror position on the right side of the nose of the aircraft.

NOTE 2:

Distortion from the shape of the nose accounts for the upper forward marking shape. All four markings are identical in shape and size.

MARKINGS:

Individual Marking Dimensions www.schemedesigners.com Copyright © 2021 by Scheme Designers, Inc.

Perfecting Paint Schemes Since 1997

Final Specifications Page 6

Challenger 605 - N91

FAA

Nose

The blue stripe starts at a point at the nose cone trailing edge.

The gold stripe starts at a point 1” from the edge of the blue stripe.

20-1/2

2-3/4

2-3/4

7-3/4 www.schemedesigners.com Copyright © 2021 by Scheme Designers, Inc.

Perfecting Paint Schemes Since 1997

Final Specifications Page 7

Challenger 605 - N91

FAA

Forward Fuselage

14-3/4

2-1/2

1-1/2

3-1/4 www.schemedesigners.com Copyright © 2021 by Scheme Designers, Inc.

Perfecting Paint Schemes Since 1997

Final Specifications Page 8

Challenger 605 - N91

FAA

Mid-Fuselage

11-1/4

4-1/2

13-1/4

3-1/2

4-1/4 www.schemedesigners.com Copyright © 2021 by Scheme Designers, Inc.

Perfecting Paint Schemes Since 1997

Final Specifications Page 9

Challenger 605 - N91

FAA

Nacelle Area

The baseline of the registration is level when the aircraft is grounded.

It is vertically & horizontally centered on the nacelles.

8-3/4

6-3/4

10-1/4

5-1/4 www.schemedesigners.com Copyright © 2021 by Scheme Designers, Inc.

Perfecting Paint Schemes Since 1997

Final Specifications Page 10

Challenger 605 - N91

FAA

Tail

NOTE:

The flags are applied in red and blue paint using paint masks.

The gold stripe is a constant 1” from the edge of the blue.

It widens uniformly as it flows aft.

The horizontal tail is overall white.

2-3/4

9-3/4

20-1/2

17-1/2 37-1/4

8-1/2

5-1/2

7-1/4 www.schemedesigners.com Copyright © 2021 by Scheme Designers, Inc.

Perfecting Paint Schemes Since 1997

Final Specifications Page 11

Challenger 605 - N91

FAA

Wing Tip

11-3/4

3-3/4

25-1/2

3-1/2 The gold stripe is a constant 1” from the edge of the blue.

It widens uniformly aft.

NOTE:

The design on the inboard surface of the winglet is a mirror image of that on the outboard surface www.schemedesigners.com Copyright © 2021 by Scheme Designers, Inc.

Perfecting Paint Schemes Since 1997

Final Specifications Page 12

Challenger 605 - N91

FAA

Specification Notes

Paint Masks and Vinyl Decals

The specifications indicate where paint masks and/or vinyl decals are required.

These may be provided by Scheme Designers, Inc., by other paint masks/vinyl decal manufacturers or made internally by the paint shop.

If they are to be ordered from Scheme Designers, Inc.:

Contact Craig Barnett at Scheme Designers to Order.

Phone: 201-569-7785 E-mail: Craig@schemedesigners.com

If they are ordered from an alternate source, or made internally:

The drawings in the specifications PDF file are scalable. Extract elements to be paint masked or made into a vinyl decal, scale them to the dimensions indicated in the specifications and proceed to cut. Alternately, the overall length of the aircraft is provided on the cover page. The full drawing of the aircraft can be extracted from the PDF file, enlarged to the overall length provided, and then elements to be paint masked or made into decal can be extracted and cut.

Questions/Errors

While we strive to be as accurate as possible, errors may occur in specifications text or dimensions, or text may be unclear. If an error is found or suspected, or if any item in these specifications is not clearly understood, please call or e-mail Craig at Scheme Designers immediately to resolve the issue or to obtain an explanation.

Specification Notes

Dimensions:

Dimensions are in inches, unless otherwise specified.

When dimensions are specified with the word “from,” it implies the perpendicular distance from where it is measured. For example, “The black stripe starts at a point 1” the edge of the red stripe” implies from that the measurement to the starting point of the black stripe is measured the edge of the red stripe.perpendicular to

If a vertical distance is being specified, it will be specified as “ ” or below “ ” the element from where the measurement is being taken. For above example, “The black stripe starts at a point 1” the edge of the below red stripe” implies that the measurement to the starting point of the black stripe is measured from the red stripe. Similarly, a vertically horizontal measurement (parallel to the ground line) will be specified as “ ” or “ ” a particular reference.forward of aft of

Colors:

Colors are referred to throughout the document by a shortened name.

For example, an Acry Glo Black Velvet Metallic color is simply referred to as black. The reference to the actual color against the shortened name is provided on Page 1 of the specifications.

If a different paint type is being used to that specified on page 1, contact Scheme Designers, Inc. directly to determine an appropriate color match in the brand of paint being used.

If there is any reason to suspect an error in a color specification, either in the color name or part number, please contact Scheme Designers, Inc. immediately to verify the color specification.

Challenger 605

FAA

N91

Scheme Designers, Inc.

+1.201.569.7785 www.schemedesigners.com Copyright © 2021 by Scheme Designers, Inc.

SCHEME II

STRIPE START POINT

50.50 FWD OF AFT

WINDOW FRAME EDGE

STRIPE START POINT

30.25 BELOW LOWER

WINDSCREEN FRAME EDGE

STRIPE END POINT

13.00 FWD OF

TAILCONE SEAM

17.75 BETWEEN LOWER

SURFACE OF PYLON

(AT AFT, INBD EDGE)

TO UPPER EDGE

OF STRIPE

N86

STRIPE ROUGHLY

CENTERED ON

LEADING EDGE

OF SENSOR (REF)

SEE DETAIL B

0.75 STRIPE WIDTH

AT DOOR HANDLE

CENTER (REF)

1.25 STRIPE WIDTH

AT WINDOW

CENTER (REF)

SEE DETAIL A

SIDE VIEW

(NOT TO SCALE)

General Notes:

GN-1: This drawing specifies the color code of paint and clear coat to be used at various locations of the aircraft and includes positioning details for accents and other details. This drawing does not specify or modify the processes, procedures, or requirements for protective finishes which are established by the applicable aircraft or component maintenance manuals.

GN-2: Drawing geometry and dimensions are not to scale.

GN-3: Unless otherwise specified, dimensions are shown along the aircraft contour, i.e., the drawing views represent "flattened" views.

GN-4: Unless otherwise specified, dimensions that reference an aircraft feature (window frame, skin joint, etc) are taken from the nearest edge of the feature.

GN-5: Lifeline Attachment Bracket on RH upper wing (not shown) shall be painted PPG i4029 Sunfast Red (Reflectance = 11).

GN-6: Exterior general finishing anti-slip surfacing and external placards shall be in accordance with CL-601 Aircraft Maintenance Manual. Wing walk anti-slip surface color: PPG i6032 Aristo Blue with arrows painted in Sherwin-Williams 840180 Matterhorn White (Reflectance = 80).

GN-7: The following paint reflectance comparisons are given to show compliance: Contrast Difference (Pantone Match vs Medium Gray: 85-34 =51), Contrast Difference (Matterhorn White vs Aristo Blue: 80-6=74), Contrast Ratio (Matterhorn White vs Aristo Blue: 80/6=13.3) GN-8: Do not paint antennas.

Notes:

1.1 LH Side shown, RH side opposite, except for Main Entry Door (LH side only) and Emergency Exit Door (RH side only).

1.2 2.00" wide band around Main Entry door (LH Side only - as shown) and 2.00" wide band around Emergency Exit door (RH Side only - not shown). Color: Sherwin-

Williams Z00067 Medium Gray (Reflectance = 34) for both. See Detail C for gap requirements around both Main Entry and Emergency Exit doors.

1.3 Do not paint leading edges of wings/horizontal stabilizers/vertical stabilizer, engine inlet ring or exhaust cones. These areas to be polished.

1.4 Registration number ("N85", "N86", or "N87", as applicable) on each side of vertical stabilizer, positioned per Detail G. Letter height shall be 12.00 -12.10 inches.

Font shall be slanted 15 aft (from bottom to top), with rounded corners as shown. Color: PPG i6032 Aristo Blue (Reflectance = 6).

1.5 Primary aircraft paint color for fuselage, wings, winglets, vertical stabilizer, flaps, horizontal stabilizers, engine pylons, fuselage frame structure around entry door opening, inside of entry door/stairs/frame, inside/frame of equipment bay door, inside/frame of baggage door, inside/outside/frame of nose/main landing gear doors, and the areas of the engine cowls/thrust reverser that are detailed within this drawing: PPG Pantone Match 643 (Reflectance = 85).

1.6 Fuselage stripe and winglet accent: PPG i6032 Aristo Blue (Reflectance = 6)

0.75 STRIPE WIDTH

(REF)

1.4

1.1

1.2 1.3

SEE DETAIL C

1.5

1.6

1.3

1.3

SEE DETAIL G

SEE DETAIL E

FOR RVSM

DEMARCATION

SEE DETAIL D

FOR TAIL

CLEARCOAT

EQUIPMENT BAY DOOR

(CENTERLINE, REF)

REVISIONS

REV DESCRIPTION ENGINEER

A Added CL-604 to effectivity. J. Reid

B Added cowl details (sheets 7-9). Removed CL-604 from effectivity and from drawing title. Re-numbered drawing as -901 (Specification).

J. Reid

12345678

D

C

B

A A

B

C

D

8 7 6 5 4 3 2 1

SHEET 1 OF 9

INSTALLATIONTHE USE OF THIS DOCUMENT SHALL BE RESTRICTED TO

CONVEYANCE OF INFORMATION TO CUSTOMERS OR VENDORS

ONLY, NEITHER CLASSIFIED NOR UNCLASSIFIED DOCUMENTS

MAY BE REPRODUCED WITHOUT WRITTEN CONSENT OF THE

FEDERAL AVIATION ADMINISTRATION

FEDERAL AVIATION ADMINISTRATION

MIKE MONRONEY AERONAUTICAL CENTER

AIRCRAFT MAINTENANCE AND ENGINEERING DIVISION

WILL ROGERS WORLD AIRPORT, OKLAHOMA CITY, OK

PROJECT LEAD

DRAWN BY

CHECKED BY

J. Reid

APPROVAL:

DATE:

BREVISION:

5138, 5167, 5190EFFECTIVITY:

AIRCRAFT TYPE: Bombardier Inc. Model CL-600-2B16 (CL-601) ES-0001-901

1. SCALE: NONE

2. DIMENSIONS IN INCHES

3. BREAK ALL SHARP EDGES

4. ANGULAR TOL: X ± 1

5. LINEAR TOL: X.X ± 0.5

6. LINEAR TOL: X.XX ± 0.10

7. LINEAR TOL: X.XXX ± 0.005

CL-601 Paint Scheme

UNLESS OTHERWISE NOTED:

B. Jones J. Reid

Frederick E Wild-Jr

32.50

26.00

0.75 2.00

28.50

2.00 4.35

24.60

63.00

48.75

0.90

20.40

1.00 GAP

1.00 GAP

AFT WINDOW (REF)

DETAIL A

(NOT TO SCALE)

WINDOW

FRAME EDGE

(TYP)

FUSELAGE STRIPE

1.6

12345678

D

C

B

A A

B

C

D

8 7 6 5 4 3 2 1

SHEET 2 OF 9

INSTALLATIONTHE USE OF THIS DOCUMENT SHALL BE RESTRICTED TO

CONVEYANCE OF INFORMATION TO CUSTOMERS OR VENDORS

ONLY, NEITHER CLASSIFIED NOR UNCLASSIFIED DOCUMENTS

MAY BE REPRODUCED WITHOUT WRITTEN CONSENT OF THE

FEDERAL AVIATION ADMINISTRATION

FEDERAL AVIATION ADMINISTRATION

MIKE MONRONEY AERONAUTICAL CENTER

AIRCRAFT MAINTENANCE AND ENGINEERING DIVISION

WILL ROGERS WORLD AIRPORT, OKLAHOMA CITY, OK

PROJECT LEAD

DRAWN BY

CHECKED BY

J. Reid

APPROVAL:

DATE:

B

See First Sheet

See First Sheet

REVISION:

5138, 5167, 5190EFFECTIVITY:

AIRCRAFT TYPE: Bombardier Inc. Model CL-600-2B16 (CL-601) ES-0001-901

1. SCALE: NONE

2. DIMENSIONS IN INCHES

3. BREAK ALL SHARP EDGES

4. ANGULAR TOL: X ± 1

5. LINEAR TOL: X.X ± 0.5

6. LINEAR TOL: X.XX ± 0.10

7. LINEAR TOL: X.XXX ± 0.005

CL-601 Paint Scheme

UNLESS OTHERWISE NOTED:

B. Jones

21.60

0.10

0.25 GAP

0.25 GAP 0.10

1.10 2.00

3.80

7.00

0.50

1.20

4.75

SKIN JOINT (REF)

PARALLEL ( 1 )

DETAIL B

(NOT TO SCALE)

FUSELAGE

STRIPE (REF)

SKIN JOINT

(REF)

1.6

WINGLET ACCENT

RIVETS (REF)

12345678

D

C

B

A A

B

C

D

8 7 6 5 4 3 2 1

SHEET 3 OF 9

INSTALLATIONTHE USE OF THIS DOCUMENT SHALL BE RESTRICTED TO

CONVEYANCE OF INFORMATION TO CUSTOMERS OR VENDORS

ONLY, NEITHER CLASSIFIED NOR UNCLASSIFIED DOCUMENTS

MAY BE REPRODUCED WITHOUT WRITTEN CONSENT OF THE

FEDERAL AVIATION ADMINISTRATION

FEDERAL AVIATION ADMINISTRATION

MIKE MONRONEY AERONAUTICAL CENTER

AIRCRAFT MAINTENANCE AND ENGINEERING DIVISION

WILL ROGERS WORLD AIRPORT, OKLAHOMA CITY, OK

PROJECT LEAD

DRAWN BY

CHECKED BY

J. Reid

APPROVAL:

DATE:

B

See First Sheet

See First Sheet

REVISION:

5138, 5167, 5190EFFECTIVITY:

AIRCRAFT TYPE: Bombardier Inc. Model CL-600-2B16 (CL-601) ES-0001-901

1. SCALE: NONE

2. DIMENSIONS IN INCHES

3. BREAK ALL SHARP EDGES

4. ANGULAR TOL: X ± 1

5. LINEAR TOL: X.X ± 0.5

6. LINEAR TOL: X.XX ± 0.10

7. LINEAR TOL: X.XXX ± 0.005

CL-601 Paint Scheme

UNLESS OTHERWISE NOTED:

0.60 0.50

GAPS REQUIRED TO

MEET REFLECTANCE

CONTRAST REGULATION

LH - 4 PLACES AT MAIN ENTRY DOOR

RH - 4 PLACES AT EMERGENCY EXIT DOOR

FUSELAGE STRIPE

(REF)

DETAIL C

(NOT TO SCALE)

DOOR FRAME

BAND (REF)

12345678

D

C

B

A A

B

C

D

8 7 6 5 4 3 2 1

SHEET 4 OF 9

INSTALLATIONTHE USE OF THIS DOCUMENT SHALL BE RESTRICTED TO

CONVEYANCE OF INFORMATION TO CUSTOMERS OR VENDORS

ONLY, NEITHER CLASSIFIED NOR UNCLASSIFIED DOCUMENTS

MAY BE REPRODUCED WITHOUT WRITTEN CONSENT OF THE

FEDERAL AVIATION ADMINISTRATION

FEDERAL AVIATION ADMINISTRATION

MIKE MONRONEY AERONAUTICAL CENTER

AIRCRAFT MAINTENANCE AND ENGINEERING DIVISION

WILL ROGERS WORLD AIRPORT, OKLAHOMA CITY, OK

PROJECT LEAD

DRAWN BY

CHECKED BY

J. Reid

APPROVAL:

DATE:

B

See First Sheet

See First Sheet

REVISION:

5138, 5167, 5190EFFECTIVITY:

AIRCRAFT TYPE: Bombardier Inc. Model CL-600-2B16 (CL-601) ES-0001-901

1. SCALE: NONE

2. DIMENSIONS IN INCHES

3. BREAK ALL SHARP EDGES

4. ANGULAR TOL: X ± 1

5. LINEAR TOL: X.X ± 0.5

6. LINEAR TOL: X.XX ± 0.10

7. LINEAR TOL: X.XXX ± 0.005

CL-601 Paint Scheme

UNLESS OTHERWISE NOTED:

0.60 0.50

2.10 2.00

2.10 2.00

0.60 0.50

N86 5.1

Notes:

5.1 LH and RH Sides: Clear coat checkered area of vertical stabilizer/rudder and lower surface of horizontal stabilizer/elevator using P/N 03-X-96 clear coat (customer provided). Do not polish clear-coated areas. Do not apply clear coat to upper surface of horizontal stabilizer.

5.2 LH and RH Sides: Paint four corners of a boundary box to mark the RVSM-Critical zone. Fuselage stations (FS) and water lines (WL) indicated correspond to the interior edges of the corner marks. Color: PPG i6032 Aristo Blue.

DETAIL F

CORNER MARK

(ROTATE AS REQ'D)

5.2

SEE DETAIL F

DETAIL D

(NOT TO SCALE)

DETAIL E

(NOT TO SCALE)

0.60 0.50

2.10 2.00

2.10 2.00

0.60 0.50

12345678

D

C

B

A A

B

C

D

8 7 6 5 4 3 2 1

SHEET 5 OF 9

INSTALLATIONTHE USE OF THIS DOCUMENT SHALL BE RESTRICTED TO

CONVEYANCE OF INFORMATION TO CUSTOMERS OR VENDORS

ONLY, NEITHER CLASSIFIED NOR UNCLASSIFIED DOCUMENTS

MAY BE REPRODUCED WITHOUT WRITTEN CONSENT OF THE

FEDERAL AVIATION ADMINISTRATION

FEDERAL AVIATION ADMINISTRATION

MIKE MONRONEY AERONAUTICAL CENTER

AIRCRAFT MAINTENANCE AND ENGINEERING DIVISION

WILL ROGERS WORLD AIRPORT, OKLAHOMA CITY, OK

PROJECT LEAD

DRAWN BY

CHECKED BY

J. Reid

APPROVAL:

DATE:

B

See First Sheet

See First Sheet

REVISION:

5138, 5167, 5190EFFECTIVITY:

AIRCRAFT TYPE: Bombardier Inc. Model CL-600-2B16 (CL-601) ES-0001-901

1. SCALE: NONE

2. DIMENSIONS IN INCHES

3. BREAK ALL SHARP EDGES

4. ANGULAR TOL: X ± 1

5. LINEAR TOL: X.X ± 0.5

6. LINEAR TOL: X.XX ± 0.10

7. LINEAR TOL: X.XXX ± 0.005

CL-601 Paint Scheme

UNLESS OTHERWISE NOTED:

44.00

30.75

DETAIL G

(NOT TO SCALE)

REFERENCE BOUNDARY

AROUND REG. NUMBER

(REF ONLY)

CENTER POINT OF

REFERENCE BOUNDARY

(REF ONLY)

1.4

12345678

D

C

B

A A

B

C

D

8 7 6 5 4 3 2 1

SHEET 6 OF 9

INSTALLATIONTHE USE OF THIS DOCUMENT SHALL BE RESTRICTED TO

CONVEYANCE OF INFORMATION TO CUSTOMERS OR VENDORS

ONLY, NEITHER CLASSIFIED NOR UNCLASSIFIED DOCUMENTS

MAY BE REPRODUCED WITHOUT WRITTEN CONSENT OF THE

FEDERAL AVIATION ADMINISTRATION

FEDERAL AVIATION ADMINISTRATION

MIKE MONRONEY AERONAUTICAL CENTER

AIRCRAFT MAINTENANCE AND ENGINEERING DIVISION

WILL ROGERS WORLD AIRPORT, OKLAHOMA CITY, OK

PROJECT LEAD

DRAWN BY

CHECKED BY

J. Reid

APPROVAL:

DATE:

B

See First Sheet

See First Sheet

REVISION:

5138, 5167, 5190EFFECTIVITY:

AIRCRAFT TYPE: Bombardier Inc. Model CL-600-2B16 (CL-601) ES-0001-901

1. SCALE: NONE

2. DIMENSIONS IN INCHES

3. BREAK ALL SHARP EDGES

4. ANGULAR TOL: X ± 1

5. LINEAR TOL: X.X ± 0.5

6. LINEAR TOL: X.XX ± 0.10

7. LINEAR TOL: X.XXX ± 0.005

CL-601 Paint Scheme

UNLESS OTHERWISE NOTED:

Exterior Surfaces Only

Exterior Surfaces Only 1.5

Exterior Surfaces, Interior Surfaces and Frame 1.5

Exterior Surfaces, Interior Surfaces and Frame 1.5

1.5

Interior Surfaces No Topcoat

Exterior Surfaces, Interior Surfaces and Frame 1.5

12345678

D

C

B

A A

B

C

D

8 7 6 5 4 3 2 1

SHEET 7 OF 9

INSTALLATIONTHE USE OF THIS DOCUMENT SHALL BE RESTRICTED TO

CONVEYANCE OF INFORMATION TO CUSTOMERS OR VENDORS

ONLY, NEITHER CLASSIFIED NOR UNCLASSIFIED DOCUMENTS

MAY BE REPRODUCED WITHOUT WRITTEN CONSENT OF THE

FEDERAL AVIATION ADMINISTRATION

FEDERAL AVIATION ADMINISTRATION

MIKE MONRONEY AERONAUTICAL CENTER

AIRCRAFT MAINTENANCE AND ENGINEERING DIVISION

WILL ROGERS WORLD AIRPORT, OKLAHOMA CITY, OK

PROJECT LEAD

DRAWN BY

CHECKED BY

J. Reid

APPROVAL:

DATE:

B

See First Sheet

See First Sheet

REVISION:

5138, 5167, 5190EFFECTIVITY:

AIRCRAFT TYPE: Bombardier Inc. Model CL-600-2B16 (CL-601) ES-0001-901

1. SCALE: NONE

2. DIMENSIONS IN INCHES

3. BREAK ALL SHARP EDGES

4. ANGULAR TOL: X ± 1

5. LINEAR TOL: X.X ± 0.5

6. LINEAR TOL: X.XX ± 0.10

7. LINEAR TOL: X.XXX ± 0.005

CL-601 Paint Scheme

UNLESS OTHERWISE NOTED:

No Topcoat

Leading Edge Not Painted

Inlet Area 1.5

Exterior SurfaceOnly (Except Leading Edge) 1.5

Flange Not Painted (Brightwork)

No Topcoat on Interior Surfaces, Cascades, and Frame

No Topcoat on Interior Surfaces, Cascades, and Frame

1.5

Exterior Surface (Except Brightwork)

12345678

D

C

B

A A

B

C

D

8 7 6 5 4 3 2 1

SHEET 8 OF 9

INSTALLATIONTHE USE OF THIS DOCUMENT SHALL BE RESTRICTED TO

CONVEYANCE OF INFORMATION TO CUSTOMERS OR VENDORS

ONLY, NEITHER CLASSIFIED NOR UNCLASSIFIED DOCUMENTS

MAY BE REPRODUCED WITHOUT WRITTEN CONSENT OF THE

FEDERAL AVIATION ADMINISTRATION

FEDERAL AVIATION ADMINISTRATION

MIKE MONRONEY AERONAUTICAL CENTER

AIRCRAFT MAINTENANCE AND ENGINEERING DIVISION

WILL ROGERS WORLD AIRPORT, OKLAHOMA CITY, OK

PROJECT LEAD

DRAWN BY

CHECKED BY

J. Reid

APPROVAL:

DATE:

B

See First Sheet

See First Sheet

REVISION:

5138, 5167, 5190EFFECTIVITY:

AIRCRAFT TYPE: Bombardier Inc. Model CL-600-2B16 (CL-601) ES-0001-901

1. SCALE: NONE

2. DIMENSIONS IN INCHES

3. BREAK ALL SHARP EDGES

4. ANGULAR TOL: X ± 1

5. LINEAR TOL: X.X ± 0.5

6. LINEAR TOL: X.XX ± 0.10

7. LINEAR TOL: X.XXX ± 0.005

CL-601 Paint Scheme

UNLESS OTHERWISE NOTED:

Not Painted (Brightwork)

Not Painted (Brightwork)

Not Painted (Brightwork) Areas (4 pl)

Not Painted (Brightwork) Areas (4 pl)

Exterior Surface (Except Brightwork)

1.5

Exterior Surface (Except Brightwork)

1.5

Inteior and Frame Surfaces AFT of Firewall Seal Not Painted

Inteior and Frame Surfaces AFT of Firewall Seal Not Painted

Interior Surfaces and Cowl Frame

FORWARD of Firewall Seal Only

1.5

Interior Surfaces and Cowl Frame

FORWARD of Firewall Seal Only

1.5

12345678

D

C

B

A A

B

C

D

8 7 6 5 4 3 2 1

SHEET 9 OF 9

INSTALLATIONTHE USE OF THIS DOCUMENT SHALL BE RESTRICTED TO

CONVEYANCE OF INFORMATION TO CUSTOMERS OR VENDORS

ONLY, NEITHER CLASSIFIED NOR UNCLASSIFIED DOCUMENTS

MAY BE REPRODUCED WITHOUT WRITTEN CONSENT OF THE

FEDERAL AVIATION ADMINISTRATION

FEDERAL AVIATION ADMINISTRATION

MIKE MONRONEY AERONAUTICAL CENTER

AIRCRAFT MAINTENANCE AND ENGINEERING DIVISION

WILL ROGERS WORLD AIRPORT, OKLAHOMA CITY, OK

PROJECT LEAD

DRAWN BY

CHECKED BY

J. Reid

APPROVAL:

DATE:

B

See First Sheet

See First Sheet

REVISION:

5138, 5167, 5190EFFECTIVITY:

AIRCRAFT TYPE: Bombardier Inc. Model CL-600-2B16 (CL-601) ES-0001-901

1. SCALE: NONE

2. DIMENSIONS IN INCHES

3. BREAK ALL SHARP EDGES

4. ANGULAR TOL: X ± 1

5. LINEAR TOL: X.X ± 0.5

6. LINEAR TOL: X.XX ± 0.10

7. LINEAR TOL: X.XXX ± 0.005

CL-601 Paint Scheme

UNLESS OTHERWISE NOTED: