Appendix A - CL-601 Paint Scheme, Rev C.pdf

STRIPE START POINT

33.25" FWD OF AFT

EDGE OF WINDOW

BRIGHTWORK

STRIPE START POINT

32.75" BELOW LOWER

EDGE OF WINDSCREEN

BRIGHTWORK

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

APPROX

0.6" STRIPE WIDTH

AT DOOR HANDLE

CENTER (REF)

APPROX

1.2" 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)

APPROX

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

C Moved stripe start point down and aft to avoid AOA placard and better match CL-605. J. Reid

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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:

C

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 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

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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:

C

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:

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)

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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:

C

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)

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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:

C

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

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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:

C

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

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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:

C

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

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

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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:

C

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

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)

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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:

C

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

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

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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:

C

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