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DEPARTMENT OF TRANSPORT MINISTÈRE DES TRANSPORTS

MASTER MINIMUM EQUIPMENT LIST LISTE PRINCIPALE D'ÉQUIPEMENT MINIMAL

Aircraft – Aéronef Revision No - No de révision: TR 79 Page

Canadair CL-600-2B19/-2C10/-2D15/-2D24/-2E25 Date: Dec 15/10 1 of 3

TEMPORARY REVISION No. 79

LETTER OF TRANSMITTAL

Based on TCCA CRJ MMEL Rev. 20

REASON FOR ISSUE:

• The MMEL Temporary Revision 79 is based on the TCCA approved TRS No 37. − TRS No 37 introduces item 27-51-04 Slat Disconnect Detection System for the CL-600-2E25 model.

INSTRUCTIONS FOR INSERTION OF THIS TEMPORARY REVISION:

(1) Insert the pages of this Temporary Revision in the MMEL as instructed at the top of the page. (2) Record the insertion of this Temporary Revision on the Record of Temporary Revision page. (3) Retain this page for record purposes.

LIST OF PAGES AFFECTED BY THIS TEMPORARY REVISION TpRv-13 27-6






INSERT IN MMEL FACING PAGE TpRv-13

RECORD OF TEMPORARY REVISIONS

Retain this index in the front of the manual. When Temporary Revisions are issued or cancelled, enter the date you insert each revision in your manual.

Temp Rev#

Pages Affected

TC approval Description of Revision Date Incorporated Signature

79 27-6 TRS No. 37 Walter Istchenko, Chief, Flight Test for Minister of Transport, 15 December 2010.

TRS No 37 introduces item 27-51-04 Slat Disconnect Detection System for the CL-600-2E25 model.






INSERT IN MMEL FACING PAGE 27-6

1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 27 – FLIGHT CONTROLS 4. Remarks or Exceptions Remarques ou exceptions

51-04 Slat Disconnect

Detection System

1) (600-2C10, 600-2D15, 600-2D24 without ModSum 670T30446)

A 1 0 (M) May be inoperative as indicated by “SLAT FAULT” status message provided:

a) Slats are inspected once each flight day to ensure no mechanical disconnect is present, and

b) Repairs are made within three flight days.

2) (600-2C10, 600-2D15, 600-2D24 with ModSum 670T30446), (600-2E25)

A 1 0 (M)(O) May be inoperative as indicated by “SLAT FAULT” status message provided:

a) Slats are inspected once each flight day to ensure no mechanical disconnect is present,

b) Slats are inspected before next flight to ensure no mechanical disconnect is present if 0g or negative g is encountered as result of pilot maneuvering in last flight, and

c) Repairs are made within three flight days.

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INTENTIONALLY LEFT BLANK








REASON FOR ISSUE:

• The MMEL Temporary Revision 80 is based on the TCCA approved TRS No 36. − TRS No 36 introduces single pack dispatch reliefs and removes operational limitation of ISA+30 in

APU related reliefs (two pack configurations) for the CL-600-2E25 model.



LIST OF PAGES AFFECTED BY THIS TEMPORARY REVISION TpRv-13 21-1, 21-14, 21-16, 21-18, 21-21. 26-2, 26-3, 26-7. 28-1. 36-1, 36-2, 36-4, 36-8, 36-10. 49-1, 49-2, 49-3, 49-4, 49-5.









Temp Rev#

Pages Affected


80 21-8 TRS No. 36 Walter Istchenko, Chief, Flight Test for Minister of Transport, 17 December 2010.

TRS No 36 introduces single pack dispatch reliefs and removes operational limitation of ISA+30 in APU related reliefs (two pack configurations) for the CL-600-2E25 model.







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 21 – AIR CONDITIONING 4. Remarks or Exceptions Remarques ou exceptions

22-01 Recirculation Fans 1) 600-2C10 C 2 0 (M) May be inoperative provided affected fan(s) is

deactivated.

2) 600-2D15, 600-2D24

C 2 0 (M) May be inoperative provided: a) Affected fan(s) is deactivated, b) Inlet Cargo Air SOV is operative or secured

CLOSED, c) AIR CONDITIONING Cargo switch is selected

to OFF, and d) Live animals are not carried in cargo

compartment.

3) 600-2E25 C 2 0 (M)(O) May be inoperative provided: a) Affected fan is deactivated, and b) Both Air Conditioning Packs are operative.

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51-01 Air Conditioning

Packs (cont’d)

4) 600-2E25

C 2 1 (O) RH pack may be inoperative provided: a) RH pack is selected OFF, b) Ram Air SOV is verified operative, c) Operations are conducted at or below FL 250, d) Ground operation for Left Air Conditioning Pack

is conducted using APU bleed, e) Operations are not conducted in known or

forecast icing conditions, and f) Operations are conducted in accordance with

AFM Supplement (Air Conditioning – Single Pack Operation).

| | | | || || |||

C 2 1 (O) RH pack may be inoperative provided: a) RH pack is selected OFF, b) Operations are conducted at or below FL 250, c) Ram Air SOV is verified operative, d) Ground operation for Left Air Conditioning Pack

is conducted using engine bleed, e) Operation is limited to temperature below

ISA+10, and f) Operations are conducted in accordance with


| | | | || || |||

(cont’d)






INSERT IN MMEL FACING PAGE 21-14 (cont’d)



Packs (cont’d)

4) 600-2E25 (cont’d)

C 2 1 (O) LH pack may be inoperative provided: a) LH pack is selected OFF, b) Ram Air SOV is verified operative, c) Operations are conducted at or below FL 250, d) Ground operation for Right Air Conditioning

Pack is conducted using APU bleed, e) Operations are not conducted in known or



| | | | || || |||


Pack is conducted using engine bleed, e) Operation is limited to temperature below



| | | | || || |||








51-02 Flow Control Valve

(FCV) (cont’d)

3) 600-2E25 C 2 1 (M)(O) RH FCV may be inoperative provided: a) Valve is secured CLOSED, b) RH pack is selected OFF, c) Operations are conducted at or below FL 250, d) Ram Air SOV is verified operative, e) Ground operation for Left Air Conditioning Pack

is conducted using APU bleed, f) Operations are not conducted in known or

forecast icing conditions, and g) Operations are conducted in accordance with


| | | | | || || |||

C 2 1 (M)(O) RH FCV may be inoperative provided: a) Valve is secured CLOSED, b) RH pack is selected OFF, c) Operations are conducted at or below FL 250, d) Ram Air SOV is verified operative, e) Ground operation for Left Air Conditioning Pack

is conducted using engine bleed, f) Operation is limited to temperature below

ISA+10, and g) Operations are conducted in accordance with


| | | | | || || |||

(cont’d)









(FCV) (cont’d)

3) 600-2E25 (cont’d)

C 2 1 (M)(O) LH FCV may be inoperative provided: a) Valve is secured CLOSED, b) LH pack is selected OFF, c) Operations are conducted at or below FL 250, d) Ram Air SOV is verified operative, e) Ground operation for Right Air Conditioning

Pack is conducted using APU bleed, f) Operations are not conducted in known or



| | | | | || || |||


Pack is conducted using engine bleed, f) Operation is limited to temperature below



| | | | | || || |||









System (cont’d)

3) 600-2C10, 600-2D15, 600-2D24

C 1 1 System redundancy may be degraded as indicated by “L PACK FAULT” and/or “R PACK FAULT” status messages provided the associated Air Conditioning Pack(s) is considered inoperative.

4) 600-2E25 C 1 1 System redundancy may be degraded as indicated by “L PACK FAULT” or “R PACK FAULT” status message provided the associated Air Conditioning Pack is considered inoperative.

||||








52-01 Ram Air SOV

(cont’d)

4) 600-2E25 C 1 0 (M)(O) May be inoperative OPEN provided: a) Ram Air SOV is deactivated OPEN, b) LH Air Conditioning Pack is operative, c) RH Air Conditioning Pack is selected OFF, d) Operations are conducted at or below FL 250, e) Ground operation for Left Air Conditioning Pack

is conducted using APU bleed, f) Operations are not conducted in known or



| | | | | || || |||

C 1 0 (M)(O) May be inoperative OPEN provided: a) Ram Air SOV is deactivated OPEN, b) LH Air Conditioning Pack is operative, c) RH Air Conditioning Pack is selected OFF, d) Operations are conducted at or below FL 250, e) Ground operation for Left Air Conditioning Pack




| | | | | || || |||








52-03 Ram Air Regulating

Valve (RARV) (600-2D15, 600-2D24, 600-2E25)

C 2 1 One may be inoperative provided associated Air Conditioning Pack is considered inoperative.

|







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 26 – FIRE PROTECTION 4. Remarks or Exceptions Remarques ou exceptions

12-01 APU Fire Detection

Loops

1) 600-2B19 C 2 1 Same.

C 2 0 Same.

2) 600-2C10, 600-2D15, 600-2D24, 600-2E25

2 1 NOTE: Item included for clarification only. Relief for single APU Fire Loop failure is covered by item 26-00-01.

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C 2 0 Both loops (A and B) may be inoperative provided the APU is considered inoperative.

3) 600-2C10, 600-2D15, 600-2D24

C 2 0 (M) May be inoperative provided: a) APU is used on ground (for engine start only), b) APU access doors are opened, c) APU is visually monitored, d) APU is pneumatically loaded only, and e) Total APU operating time shall not exceed

5 minutes.

(cont’d)








12-01 APU Fire Detection

Loops (cont’d)

4) 600-2E25

C 2 0 (M)(O) May be inoperative provided: a) APU is used on ground (for engine start only), b) APU access doors are opened, c) APU is visually monitored, d) APU is pneumatically loaded only, and e) Total APU operating time shall not exceed

5 minutes.

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22-01 APU Fire

Extinguishing System

1) 600-2B19 C 1 0 May be inoperative provided APU is considered inoperative.

2) 600-2C10, 600-2D15, 600-2D24, 600-2E25

C 1 0 May be inoperative provided APU is considered inoperative.

|

3) 600-2C10, 600-2D15, 600-2D24

C 1 0 (M) May be inoperative provided: a) APU is used on ground (for engine start only), b) APU access doors are opened, c) APU is visually monitored, d) APU Fire Detection System is operative, e) APU is pneumatically loaded only, and f) Total APU operating time shall not exceed 5

minutes.

4) 600-2E25 C 1 0 (M)(O) May be inoperative provided: a) APU is used on ground (for engine start only), b) APU access doors are opened, c) APU is visually monitored, d) APU Fire Detection System is operative, e) APU is pneumatically loaded only, and f) Total APU operating time shall not exceed 5

minutes.

|







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 28 – FUEL 4. Remarks or Exceptions Remarques ou exceptions

13-01 APU Fuel Feed

SOV

1) 600-2B19 C 1 0 (M) May be inoperative CLOSED provided APU is considered inoperative.

2) 600-2C10, 600-2D15, 600-2D24, 600-2E25

C 1 0 (M) May be inoperative CLOSED provided APU is considered inoperative.

|

C 1 0 (M)(O) May be inoperative OPEN provided: a) APU is used for engine starting on ground only, b) APU is shutdown after one engine start, c) APU is not used in flight, d) APU Fire Detection System is operative, and e) APU Fire Extinguishing System is operative.







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 36 – PNEUMATIC 4. Remarks or Exceptions Remarques ou exceptions

11-02 Pressure Regulating

SOV (PRSOV)

1) 600-2C10 C 2 1 Same.

2) 600-2D15, 600-2D24

C 2 1 Same.

3) 600-2E25 C 2 1 (M)(O) May be inoperative provided: a) Associated PRSOV is secured CLOSED, b) Opposite HPV is operative, c) Opposite Engine Cowl Anti-Ice SOV is

operative, d) Operations are conducted at or below FL 250, e) Ground operation for Air Conditioning is

conducted using APU bleed, f) Operations are not conducted in known or


AFM Supplements (Operations with Airplane Systems Inoperative).

| | | || | || || |||








11-03 High Pressure Valve

(HPV)

1) 600-2C10 C 2 1 Same.

2) 600-2D15, 600-2D24

C 2 1 Same.

3) 600-2E25 C 2 1 (M)(O) May be inoperative provided: a) Associated HPV is secured CLOSED, b) Opposite Engine Cowl Anti-Ice SOV is

operative, c) Operations are conducted at or below FL 250, d) Ground operation for Air Conditioning is

conducted using APU bleed, e) Operations are not conducted in known or



| | || | || || |||








12-02 Bleed Air

ISOL Valve (Cross-Bleed Valve)

1) 600-2C10 C 1 0 Same.

2) 600-2D15, 600-2D24

C 1 0 Same.

3) 600-2E25 C 1 0 (M)(O) May be inoperative OPEN provided: a) ISOL valve is secured OPEN, b) Bleed valves selector switch is selected to

MANUAL, c) PRSOV and HPV on selected side are

operative, d) Operations are conducted at or below FL 250, e) Ground operation for Air Conditioning is

conducted using APU bleed, f) Operations are not conducted in known or



| | || || | || || |||








21-06 Air Leak Detection

System (600-2C10, 600-2D15, 600-2D24, 600-2E25) (cont’d)

3) Bleed Loops (cont’d)

b) Left (600-2D15, 600-2D24)

C 2 0 Same.

c) Left (600-2E25)

C 2 0 (O) Both loops (A and B) may be inoperative provided: a) At least one Right Bleed Loop (A or B) is

operative, b) Both PRSOV are operative, c) Both HPV are operative, d) Both Engine Cowl Anti-Ice SOV are operative, e) Right Air Conditioning Pack is operative, f) Operations are conducted at or below FL 250, g) Ground operation for Right Air Conditioning

Pack is conducted using engine bleed, h) Operations are not conducted in known or

forecast icing conditions, and i) Operations are conducted in accordance with

AFM Supplements (Operations with Airplane Systems Inoperative) and (Air Conditioning – Single Pack Operation).

| || | | | | | || || ||||

(cont’d)








21-06 Air Leak Detection



e) Right (600-2D15, 600-2D24)

C 2 0 Same.

f) Right (600-2E25)

C 2 0 (O) Both loops (A and B) may be inoperative provided: a) At least one Left Bleed Loop (A or B) is

operative, b) Both PRSOV are operative, c) Both HPV are operative, d) Both Engine Cowl Anti-Ice SOV are operative, e) Left Air Conditioning Pack is operative, f) Operations are conducted at or below FL 250, g) Ground operation for Left Air Conditioning Pack

is conducted using APU or engine bleed, h) Operations are not conducted in known or

forecast icing conditions, and i) Operations are conducted in accordance with

AFM Supplements (Operations with Airplane Systems Inoperative) and (Air Conditioning – Single Pack Operation).

| || | | | | | || || ||||







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 49 – APU 4. Remarks or Exceptions Remarques ou exceptions

10-01 Auxiliary Power Unit

(APU)

1) 600-2B19 C 1 0 Same.

C 1 0 Same.

2) 600-2C10, 600-2D15, 600-2D24

C 1 0 Same

C 1 0 Same.

3) 600-2E25 C 1 0 (M)(O) May be inoperative provided: a) APU is deactivated, b) Intake door is visually verified CLOSED, c) Both Integrated Drive Generators (IDG) are

operative, and d) Cabin occupants limited per table.

|

(cont’d)








10-01 Auxiliary Power Unit

(APU) (cont’d)

3) 600-2E25 (cont’d)

C 1 0 (M)(O) May be inoperative provided: a) APU is deactivated, b) Aircraft speed is limited to 220 knots, c) Both Integrated Drive Generators (IDG) are

operative, and d) Cabin occupants limited per table.

|








14-01 APU Air Intake Door

Linear Actuator (cont’d)

2) 600-2C10, 600-2D15, 600-2D24

C 1 0 Same.

3) 600-2E25 C 1 0 (O) May be inoperative provided: a) APU is not used, b) Aircraft speed is limited to 220 knots, and c) Both Integrated Drive Generators (IDG) are

operative.

| |

4) 600-2C10, 600-2D15, 600-2D24

C 1 0 Same

C 1 0 Same.

5) 600-2E25 C 1 0 (M)(O) May be inoperative provided: a) Intake door is deactivated OPEN, b) APU is operated continuously during flight or

aircraft speed is limited to 220 knots if APU is OFF, and

c) AFM performance corrections for APU ON are applied.

| |

(cont’d)








14-01 APU Air Intake Door

Linear Actuator (cont’d)

5) 600-2E25 (cont’d)

C 1 0 (M)(O) May be inoperative provided: a) Intake door is deactivated CLOSED, and b) APU is considered inoperative.

|

43-01 APU START/STOP “START/AVAIL” Switch Light (light function only)

C 1 0

51-01 APU Load Control Valve (LCV)

1) 600-2B19 C 1 0 (M) May be inoperative provided it is secured CLOSED. NOTE: The APU is available as a source of electrical

power only, if required.

2) 600-2C10, 600-2D15, 600-2D24

C 1 0 (M) May be inoperative CLOSED provided Bleed Valves are selected to “Manual” on the Bleed Air Control Panel. NOTE: The APU is available as a source of electrical


3) 600-2E25 C 1 0 (M)(O) May be inoperative CLOSED provided Bleed Valves are selected to “Manual” on the Bleed Air Control Panel. NOTE: The APU is available as a source of electrical


| | | |








61-02 APU

Sub-system (600-2C10, 600-2D15, 600-2D24, 600-2E25)

B 1 0 (O) May be inoperative as indicated by ”APU FAULT” status message on ground provided:

a) APU is operative (start and shutdown normally), and

b) Flight operations are not dependent on use of APU.

|



Aircraft – Aéronef Revision No - No de révision: TR 80-1 Page

Canadair CL-600-2B19/-2C10/-2D15/-2D24/2E25 Date: Nov 28/11 1 of 8

TEMPORARY REVISION No. 80-1


Based on TCCA CRJ MMEL Rev. 20 and TR 80 REASON FOR ISSUE:

• The MMEL Temporary Revision 80-1 is based on the TCCA approved TRS No 38. − In the TRS No 38, for single pack dispatch relief using APU bleed, limitation for operations in known

or forecast icing conditions is made specific to ground operation, − Also, new item 32-60-01 Proximity Sensing System is introduced.


(1) Remove and discard the pages 4 of 24, 5 of 24, 6 of 24, 7 of 24, and 9 of 24 of TR 80 and replace with pages 3 of 8, 4 of 8, 5 of 8, 6 of 8, and 7 of 8 of TR80-1.


LIST OF PAGES AFFECTED BY THIS TEMPORARY REVISION TpRv-13 21-14, 21-16, 21-21. 32-6.






INSERT IN MMEL

FACING PAGE TpRv-13

RECORD OF TEMPORARY REVISIONS Retain this index in the front of the manual. When Temporary Revisions are issued or cancelled, enter the date you insert each revision in your manual. Temp Rev#

Pages Affected


80-1 21-14, 21-16, 21-21, 32-6

TRS No. 38 Walter Istchenko, Chief, Flight Test for Minister of Transport, 21 November 2011.

- In the TRS No 38, for single pack dispatch relief using APU bleed, limitation for operations in known or forecast icing conditions is made specific to ground operation,

- Also, new item 32-60-01 Proximity Sensing System is introduced.






REMOVE AND DISCARD PAGE 4 OF 24 OF TR 80 AND

INSERT THIS PAGE IN MMEL FACING PAGE 21-14



Packs (cont’d)

4) 600-2E25

C 2 1 (O) RH pack may be inoperative provided: a) RH pack is selected OFF, b) Ram Air SOV is verified operative, c) Operations are conducted at or below FL 250, d) Ground operation for Left Air Conditioning Pack

is conducted using APU bleed, e) Ground operations are not conducted in known

or forecast icing conditions, and f) Operations are conducted in accordance with


|

C 2 1 (O) RH pack may be inoperative provided: a) RH pack is selected OFF, b) Operations are conducted at or below FL 250, c) Ram Air SOV is verified operative, d) Ground operation for Left Air Conditioning Pack

is conducted using engine bleed, e) Operation is limited to temperature below



(cont’d)







INSERT THIS PAGE IN MMEL FACING PAGE 21-14 (cont’d)



Packs (cont’d)

4) 600-2E25 (cont’d)


Pack is conducted using APU bleed, e) Ground operations are not conducted in known



|


Pack is conducted using engine bleed, e) Operation is limited to temperature below












(FCV) (cont’d)

3) 600-2E25 C 2 1 (M)(O) RH FCV may be inoperative provided: a) Valve is secured CLOSED, b) RH pack is selected OFF, c) Operations are conducted at or below FL 250, d) Ram Air SOV is verified operative, e) Ground operation for Left Air Conditioning Pack

is conducted using APU bleed, f) Ground operations are not conducted in known

or forecast icing conditions, and g) Operations are conducted in accordance with


|

C 2 1 (M)(O) RH FCV may be inoperative provided: a) Valve is secured CLOSED, b) RH pack is selected OFF, c) Operations are conducted at or below FL 250, d) Ram Air SOV is verified operative, e) Ground operation for Left Air Conditioning Pack




(cont’d)







INSERT THIS PAGE IN MMEL FACING PAGE 21-16 (cont’d)



(FCV) (cont’d)

3) 600-2E25 (cont’d)


Pack is conducted using APU bleed, f) Ground operations are not conducted in known



|


Pack is conducted using engine bleed, f) Operation is limited to temperature below











52-01 Ram Air SOV

(cont’d)

4) 600-2E25 C 1 0 (M)(O) May be inoperative OPEN provided: a) Ram Air SOV is deactivated OPEN, b) LH Air Conditioning Pack is operative, c) RH Air Conditioning Pack is selected OFF, d) Operations are conducted at or below FL 250, e) Ground operation for Left Air Conditioning Pack

is conducted using APU bleed, f) Ground operations are not conducted in known



|

C 1 0 (M)(O) May be inoperative OPEN provided: a) Ram Air SOV is deactivated OPEN, b) LH Air Conditioning Pack is operative, c) RH Air Conditioning Pack is selected OFF, d) Operations are conducted at or below FL 250, e) Ground operation for Left Air Conditioning Pack









INSERT IN MMEL

FOLLOWING PAGE 32-6

1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 32 – LANDING GEAR 4. Remarks or Exceptions Remarques ou exceptions

60-01 Proximity Sensing

System (600-2C10, 600-2D15, 600-2D24, 600-2E25 with Modsum 670T31999)

C 1 1 System redundancy may be degraded as indicated by “PROX SYS FAULT 2” status message.

||||||||




Canadair CL-600-2B19/-2C10/-2D15/-2D24/2E25 Date: Apr 24/13 1 of 2



Based on TCCA CRJ MMEL Rev. 20 REASON FOR ISSUE:

• The MMEL Temporary Revision 81-1 rescinds TR 81. INSTRUCTIONS FOR INSERTION OF THIS TEMPORARY REVISION:

(1) Remove and discard all pages of TR 81. (2) Record the removal of Temporary Revision 81 and the insertion of this Temporary Revision on the

Record of Temporary Revision page. (3) Retain this page for record purposes.

LIST OF PAGES AFFECTED BY THIS TEMPORARY REVISION TpRv-13




Canadair CL-600-2B19/-2C10/-2D15/-2D24/2E25 Date: Apr 24/13 2 of 2




Retain this index in the front of the manual. When Temporary Revisions are issued or cancelled, enter the date you insert each revision in your manual. Temp Rev#

Pages Affected


81-1 N/A TRS No. 41-1 Walter Istchenko, Chief, Flight Test for Minister of Transport, 24 April 2013

TCCA rescinded TR 81.




Canadair CL-600-2B19/-2C10/-2D15/-2D24/2E25 Date: Mar 20/13 1 of 3




REASON FOR ISSUE:

• The MMEL Temporary Revision 82 is based on the TCCA approved TRS No 42. − TRS No 42, modify the dispatch condition to include the Electronic Display Unit (EDU) for the

Electronic Flight Bag Systems Mounting Device. INSTRUCTIONS FOR INSERTION OF THIS TEMPORARY REVISION:


LIST OF PAGES AFFECTED BY THIS TEMPORARY REVISION TpRv-13 46-1.









Temp Rev#

Pages Affected


82 46-1 TRS No. 42 Jim Martin, for Chief, Flight Test for Minister of Transport, 22 February 2013.

TRS No 42, modify the dispatch condition to include the Electronic Display Unit (EDU) for the Electronic Flight Bag Systems Mounting Device.







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 46 – INFORMATION SYSTEMS 4. Remarks or Exceptions Remarques ou exceptions

20-01 Electronic Flight Bag

Systems (EFBs) (Class 2) ***

1) Data Connectivity

C 2 0 (O) May be inoperative provided alternative procedures are established and used.

D 2 0 May be inoperative provided procedures do not require its use.

2) Power Connection

C 2 0 (O) May be inoperative provided alternative procedures are established and used.

D 2 0 May be inoperative provided procedures do not require its use.

3) Mounting Device (including Electronic Display Unit (EDU))

C 2 0 (M)(O) May be inoperative provided: a) Associated EDU and hardware is secured by an

alternate means or removed from the aircraft, and

b) Alternative procedures are established and used.

||||||

D 2 0 (M) May be inoperative provided: a) Associated EDU and hardware is secured by an

alternate means or removed from the aircraft, and

b) Procedures do not require its use.

|








REASON FOR ISSUE:

• The MMEL Temporary Revision 83 is based on the TCCA approved TRS No 40. − TRS No 40, dispatch condition has been changed to add QFE or non QFE operations.



LIST OF PAGES AFFECTED BY THIS TEMPORARY REVISION TpRv-13 21-8 22-1.









Temp Rev#

Pages Affected


83 21-8 22-1

TRS No. 40, Walter Istchenko, Chief Flight Test for Minister of Transport, 28 June 2012.

TRS No 40, for item 21-33-01, ‘non-QFE flight operation’ was added to sub-item 1) CPAM (2B19). Also, Item 22-10-01 NOTE 3 for the 600-2B19 model has been added.








33-01 Cabin Pressure

Monitoring Sub-system

1) Cabin Pressure Acquisition Module (CPAM) (600-2B19)

C 1 0 (M) May be inoperative for non-QFE flight operation provided:

a) Both Automatic Cabin Pressurization Controllers are operative, and

b) Operations are conducted at or below FL 300.

| |

2) Cabin Pressure

Control Panel (CPCP) Pressure Monitoring Function (600-2C10, 600-2D15, 600-2D24, 600-2E25)

A 1 0 (O) May be inoperative as indicated by “CPAM FAIL” status message provided:

a) Both Automatic Cabin Pressure Controllers are operative,

b) Emergency depress system is verified operative,

c) Operations are conducted at or below FL 300, and

d) Repairs are made within one flight day.







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 22 – AUTO FLIGHT 4. Remarks or Exceptions Remarques ou exceptions

10-01 Autopilot System 1) 600-2B19 C 1 0 Except where enroute operations or approach

procedures require its use, may be inoperative provided Altitude Alerting system is operative. NOTE 1: Autopilot is required for RVSM Operations. NOTE 2: Relief for inoperative individual flight

guidance operational modes is provided by MMEL Item 22-10-02 Flight Directors.

NOTE 3: Autopilot is required for QFE Operations when the altimeter setting at destination/alternate airport is expected to be 950 mb or lower.

| | | | | | | | | | | | |

2) 600-2C10,

600-2D15, 600-2D24 600-2E25)

C 1 0 Except where enroute operations or approach procedures require its use, may be inoperative provided Altitude Alerting system is operative. NOTE 1: Autopilot is required for RVSM Operations. NOTE 2: Relief for inoperative individual flight

guidance operational modes is provided by MMEL Item 22-10-02 Flight Directors.

| | | |




Canadair CL-600-2B19/-2C10/-2D15/-2D24/-2E25 Date: Nov 05/2013 1 of 7

TEMPORARY REVISION No 84

LETTER OF TRANSMITTAL Based on TCCA CRJ MMEL Rev. 20

REASON FOR ISSUE:

• The MMEL Temporary Revision 84 is based on the TCCA accepted TRS No 39 Rev. 2. − TRS#39 Rev. 2 modifies the items that follow:

21-51-05: Note is modified to address different failure modes of pressure transducer. 27-51-04: Addition of Proviso, requiring slat mechanical disconnects inspection if 0g or

negative g is encountered as result of pilot maneuvering 35-20-01: New set of proviso added provided flight is conducted at or below 10,000 feet

MSL. 52-11-01: Item modified to address Power Assist Sub-system and Counterbalance Sub-

system.


(1) Remove and discard page 3 of 3.of TR 79. (2) Insert the pages of this Temporary Revision in the MMEL as instructed at the top of the page. (3) Record the insertion of this Temporary Revision on the Record of Temporary Revision page. (4) Retain this page for record purposes.

LIST OF PAGES AFFECTED BY THIS TEMPORARY REVISION: TpRv-13 21-18 27-6 35-2 52-1









Temp Rev #

Pages Affected

EASA Acceptedl Description of Revision Date Incorporated Signature

84 21-18 27-6 35-2 52-1

TRS No.39 Rev 2 Walter Istchenko, Chief, Flight Test for Minister of Transport, 29 October 2013

TRS#39 Rev. 2 modifies the items that follow:

21-51-05: Note is modified to address different failure modes of pressure transducer.

27-51-04:Addition of Proviso, requiring slat mechanical disconnects inspection if 0g or negative g is encountered as result of pilot maneuvering.

35-20-01:New set of proviso added provided flight is conducted at or below 10,000 feet MSL.

52-11-01:Item modified to address Power Assist Sub-system and Counterbalance Sub-system.








51-05 Pack Supply Pressure

Indication (600-2B19)

C 2 0 (O)

NOTE: Pack Supply Pressure Readout on the

EICAS ECS Synoptic Page may show amber dashes and the pack flowline may show black with white outlines.

| | |






REMOVE AND DISCARD PAGE 3 OF 3 OR TR 79 INSERT THIS PAGE IN MMEL FACING PAGE 27-6

1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 27 – FLIGHT CONTROLS 4. Remarks or Exceptions Remarques ou exceptions

51-04 Slat Disconnect

Detection System (600-2C10, 600-2D15, 600-2D24 600-2E25)

A 1 0 (M)(O) May be inoperative as indicated by “SLAT FAULT” status message provided:

a) Slats are inspected once each flight day to ensure no mechanical disconnect is present,

b) Slats are inspected before next flight to ensure no mechanical disconnect is present if 0g or negative g is encountered as result of pilot maneuvering in last flight, and

c) Repairs are made within three flight days.

| | | | | | | | | |







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 35 – OXYGEN 4. Remarks or Exceptions Remarques ou exceptions

20-01 Passenger Oxygen System

B 1 0 (O) May be inoperative provided: a) All components of cabin pressurization warning

and indicating systems are operative, b) Operations are conducted so that minimum

enroute altitude is at or below 13,000 ft MSL, c) Operations are conducted at or below FL 250, d) Portable oxygen units are provided for all crew

members and for 10 percent of the passengers for half an hour (supplemental oxygen),

e) Operational procedures are established to ensure that passengers are appropriately briefed to accommodate revised equipment, and

f) Both Air Conditioning Packs are verified operative.

B 1 0 May be inoperative provided flight is conducted at or

below 10,000 feet MSL. | |

1) Automatic

Deployment B 1 0 (M) May be inoperative provided:

a) Manual deployment is operative, and b) Operations are conducted at or below FL 300.

2) Passenger

Service Units (PSU)

(cont’d)

D - 0 (M)(O) Individual PSUs may be inoperative with no flight altitude restriction provided:

c) Associated seats are blocked and placarded to prevent occupancy,

d) PSUs for flight attendant locations operate normally, and

e) No more than two consecutive banks of seats and their adjacent banks of seats have an inoperative PSU (forward and aft, left and right).







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 35 – OXYGEN 4. Remarks or Exceptions Remarques ou exceptions

20-01 Passenger Oxygen System

(cont’d) 3) Automatic

Opening Feature of Door Latches

B - - (M)(O) May be inoperative provided: a) The door is confirmed inoperative unlatched, b) The door is secured closed, c) The PSU oxygen system is operative, d) The flight remains at or below FL300, e) The manual deployment system is operative, f) No more than two consecutive banks of seats

and their adjacent banks of seats have an inoperative automatic opening feature, and

g) Occupants are briefed on oxygen mask access.

NOTE: The method of door closure must not hinder

ready access to the first aid oxygen outlet.







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 52 – DOORS 4. Remarks or Exceptions Remarques ou exceptions

11-01 Passenger Door Power Assist System

1) Power Assist Sub-system

C 1 0 (M)(O) May be inoperative provided: a) Door is verified manually operative (opens and

closes) without any interference, b) Counterbalance Forward and Aft sides are

operative, and c) Alternate procedures are established and

used.

| | | | | | | |

2) Counterbalance

Sub-system |

| a) Forward side C 1 0 (M)(O) May be inoperative provided:

a) Door is verified manually operative (opens and closes) without any interference,

b) Counterbalance Aft side is operative, and c) Alternate procedures are established and

used.

| | | | | | |

b) Aft side C 1 0 (M)(O) May be inoperative provided:

a) Door is verified manually operative (opens and closes) without any interference,

b) Counterbalance Forward side is operative, and

c) Alternate procedures to control manually the support wheel or to support door with cable kit are established and used.

| | | | | | | | |




Canadair CL-600-2B19/-2C10/-2D15/-2D24/-2E25 Date: Apr 20/2015 1 of 3



REASON FOR ISSUE:

• The MMEL Temporary Revision 85 is based on the TCCA accepted TRS No 44. - Proviso b) added to monitor fuel level (balance) and quantity during flight, - Item re-introduced for the 600-2C10 model, and - New item introduced for the 600-2D15, 600-2D24, and 600-2E25 models.



LIST OF PAGES AFFECTED BY THIS TEMPORARY REVISION: TpRv-13 73-2









Temp Rev #

Pages Affected

TCCA Accepted Description of Revision Date Incorporated Signature

85 73-2 TRS No.44, Walter Istchenko, Chief, Flight Test for Minister of Transport, 13 April 2015

- Proviso b) added to monitor fuel level (balance) and quantity during flight,

- Item re-introduced for the

600-2C10 model, and - New item introduced for

the 600-2D15, 600-2D24, 600-2E25 models.







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 73 – ENGINE FUEL & CONTROL 4. Remarks or Exceptions Remarques ou exceptions

31-03 Fuel Low Pressure

Indicating Systems A 2 1 (O) May be inoperative provided:

a) Both Fuel Boost Pumps are operative, b) Monitor fuel level and quantity during flight,

and c) Repairs are made within two days.

NOTE: Fuel system check valve test

(First flight of day – Before Engine Shutdown) is waived for the inoperative fuel low pressure indication.

| | |




Canadair CL-600-2B19/-2C10/-2D15/-2D24/2E25 Date: Sep 15/15 1 of 14




REASON FOR ISSUE:

• The MMEL Temporary Revision 86 is based on the TCCA approved TRS No 45. − TRS No 45, dispatch condition modified for altitude operations at FL310 with single pack.



LIST OF PAGES AFFECTED BY THIS TEMPORARY REVISION TpRv-13 21-13; 21-15; 21-16, 21-20, 21-21 36-1; 36-2; 36-4; 36-8; 36-10









Temp Rev#

Pages Affected


86 21-13, 21-15, 21-16, 21-20, 21-21, 36-1, 36-2, 36-4, 36-8, and 36-10.

TRS No. 45, Walter Istchenko, Chief Flight Test for Minister of Transport, 28 May 2015.

- TRS No. 45 reworks various items to provide related additional provisos to cater for operations wherein the airplane is dispatched with a single pack inoperative at higher altitude operations.









Packs

3) 600-2D15, 600-2D24

C 2 1 (O) RH pack may be inoperative provided: a) RH pack is selected OFF, b) Operations are conducted at or below FL 250, c) Ram Air SOV is either verified operative or

deactivated OPEN, and d) Operations are conducted in accordance with

AFM Supplement (Performance Penalties for Operation with Airplane Systems Inoperative).

| |

C 2 1 (O) RH pack may be inoperative provided:

a) RH pack is selected OFF, b) Operations are conducted at or below FL 310, c) Maximum number of cabin occupants (including

Flight Attendants) is equal to or less than 82, d) Ram Air SOV is either verified operative or

deactivated OPEN, e) Operations are conducted in accordance with

AFM Supplement (Performance Penalties for Operation with Airplane Systems Inoperative), and

f) Operations are conducted in accordance with AFM Supplement (Air-conditioning - Airplane Dispatch in Single Pack Configuration).

| | | | | | | | | | | | | |









Packs (cont’d)

3) 600-2D15, 600-2D24

(cont’d)

C 2 1 (O) LH pack may be inoperative provided: a) LH pack is selected OFF, b) Operations are conducted at or below FL 250, c) Ram Air SOV is verified operative, and d) Operations are conducted in accordance with


| |

C 2 1 (O) LH pack may be inoperative provided:

a) LH pack is selected OFF, b) Operations are conducted at or below FL 310, c) Maximum number of cabin occupants (including

Flight Attendants) is equal to or less than 82, d) Ram Air SOV is verified operative, e) Operations are conducted in accordance with


f) Operations are conducted in accordance with AFM Supplement (Air-conditioning - Airplane Dispatch in Single Pack Configuration).

| | | | | | | | | | | | |

C 2 0 Same.









(FCV)

2) 600-2D15, 600-2D24

C 2 1 (M)(O) RH FCV may be inoperative provided: a) Valve is secured CLOSED, b) RH pack is selected OFF, c) Opposite Air Conditioning Pack is operative, d) Operations are conducted at or below FL 250, e) Ram Air SOV is either verified operative or

deactivated OPEN, and f) Operations are conducted in accordance with


| |

C 2 1 (M)(O) RH FCV may be inoperative provided:

a) Valve is secured CLOSED, b) RH pack is selected OFF, c) Opposite Air Conditioning Pack is operative, d) Operations are conducted at or below FL 310, e) Maximum number of cabin occupants (including

Flight Attendants) is equal to or less than 82, f) Ram Air SOV is either verified operative or

deactivated OPEN, g) Operations are conducted in accordance with


h) Operations are conducted in accordance with AFM Supplement (Air-conditioning - Airplane Dispatch in Single Pack Configuration).

| | | | | | | | | | | | | | |

(cont’d)









(FCV) (cont’d)

2) 600-2D15, 600-2D24

(cont’d)

C 2 1 (M)(O) LH FCV may be inoperative provided: a) Valve is secured CLOSED, b) LH pack is selected OFF, c) Opposite Air Conditioning Pack is operative, d) Operations are conducted at or below FL 250, e) Ram Air SOV is verified operative, and f) Operations are conducted in accordance with


| |

C 2 1 (M)(O) LH FCV may be inoperative provided: a) Valve is secured CLOSED, b) LH pack is selected OFF, c) Opposite Air Conditioning Pack is operative, d) Operations are conducted at or below FL 310, e) Maximum number of cabin occupants (including

Flight Attendants) is equal to or less than 82, f) Ram Air SOV is verified operative, g) Operations are conducted in accordance with


h) Operations are conducted in accordance with AFM Supplement (Air-conditioning - Airplane Dispatch in Single Pack Configuration).

| | | | | | | | | | | | | | |

C 2 0 Same.








52-01 Ram Air SOV

3) 600-2D15, 600-2D24

C 1 0 (M)(O) May be inoperative OPEN provided: a) Ram Air SOV is deactivated OPEN, b) LH Air Conditioning Pack is operative, c) RH Air Conditioning Pack is selected OFF, d) Operations are conducted at or below FL 250,

and e) Operations are conducted in accordance with


| |

C 1 0 (M)(O) May be inoperative OPEN provided:

a) Ram Air SOV is deactivated OPEN, b) LH Air Conditioning Pack is operative, c) RH Air Conditioning Pack is selected OFF, d) Operations are conducted at or below FL 310, e) Maximum number of cabin occupants (including

Flight Attendants) is equal to or less than 82, f) Operations are conducted in accordance with


g) Operations are conducted in accordance with AFM Supplement (Air-conditioning - Airplane Dispatch in Single Pack Configuration).

| | | | | | | | | | | | | |

C 1 0 Same.







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 36 – PNEUMATIC 4. Remarks or Exceptions 11-02 Pressure Regulating

SOV (PRSOV)

2) 600-2D15, 600-2D24

C 2 1 (M)(O) May be inoperative provided: a) Associated PRSOV is secured CLOSED, b) Opposite HPV is operative, c) Opposite Engine Cowl Anti-Ice SOV is

operative, d) APU is operative, e) APU Load Control Valve is operative, f) Operations are conducted at or below FL 250, g) Operations are not conducted in known or

forecast icing conditions, and h) Operations are conducted in accordance with


| |

C 2 1 (M)(O) May be inoperative provided: a) Associated PRSOV is secured CLOSED, b) Opposite HPV is operative, c) Opposite Engine Cowl Anti-Ice SOV is

operative, d) APU is operative, e) APU Load Control Valve is operative, f) Operations are conducted at or below FL 310, g) Maximum number of cabin occupants (including

Flight Attendants) is equal to or less than 82, h) Operations are not conducted in known or

forecast icing conditions, i) Operations are conducted in accordance with


j) Operations are conducted in accordance with AFM Supplement (Air-conditioning - Airplane Dispatch in Single Pack Configuration).

| | | | | | | | | | | | | | | | | | |







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 36 – PNEUMATIC 4. Remarks or Exceptions 11-03 High Pressure Valve

(HPV)

2) 600-2D15, 600-2D24

C 2 1 (M)(O) May be inoperative provided: a) Associated HPV is secured CLOSED, b) Opposite Engine Cowl Anti-Ice SOV is

operative, c) APU is operative, d) APU Load Control Valve is operative, e) Operations are conducted at or below FL 250, f) Operations are not conducted in known or



| |

C 2 1 (M)(O) May be inoperative provided: a) Associated HPV is secured CLOSED, b) Opposite Engine Cowl Anti-Ice SOV is

operative, c) APU is operative, d) APU Load Control Valve is operative, e) Operations are conducted at or below FL 310, f) Maximum number of cabin occupants (including

Flight Attendants) is equal to or less than 82, g) Operations are not conducted in known or

forecast icing conditions, h) Operations are conducted in accordance with


i) Operations are conducted in accordance with AFM Supplement (Air-conditioning - Airplane Dispatch in Single Pack Configuration).

| | | | | | | | | | | | | | | | | |







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 36 – PNEUMATIC 4. Remarks or Exceptions 12-02 Bleed Air

ISOL Valve (Cross-Bleed Valve)

2) 600-2D15, 600-2D24

C 1 0 (M)(O) May be inoperative OPEN provided: a) ISOL valve is secured OPEN, b) Bleed source selector switch is selected either

to L ENG or R ENG, c) Bleed valves selector switch is selected to

MANUAL, d) PRSOV and HPV on selected side are

operative, e) Operations are conducted at or below FL 250, f) Operations are not conducted in known or



| |

C 1 0 (M)(O) May be inoperative OPEN provided: a) ISOL valve is secured OPEN, b) Bleed source selector switch is selected either

to L ENG or R ENG, c) Bleed valves selector switch is selected to

MANUAL, d) PRSOV and HPV on selected side are

operative, e) Operations are conducted at or below FL 310, f) Maximum number of cabin occupants (including

Flight Attendants) is equal to or less than 82, g) Operations are not conducted in known or

forecast icing conditions, h) Operations are conducted in accordance with


i) Operations are conducted in accordance with AFM Supplement (Air-conditioning – Airplane Dispatch in Single Pack Configuration).

|| | | | | | | | | | | | | | | | | |







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 36 – PNEUMATIC 4. Remarks or Exceptions 21-06 Air Leak Detection

System (600-2C10, 600-2D15, 600-2D24, 600-2E25)

3) Bleed Loops b) Left

(600-2D15, 600-2D24)


operative, b) Right PRSOV is operative, c) Right HPV is operative, d) Right Air Conditioning Pack is operative, e) Bleed source selector switch is selected to the

R ENG, f) Bleed Air ISOL Valve is operative and selected

CLOSED, g) Bleed valves selector switch is selected to

MANUAL, h) APU is operative, i) APU Load Control Valve is operative, j) Cross bleed start procedure is not used for

engine start, k) Operations are conducted at or below FL 250, l) Operations are not conducted in known or

forecast icing conditions, and m) Operations are conducted in accordance with


| |










b) Left (600-2D15, 600-2D24) (cont’d)


operative, b) Right PRSOV is operative, c) Right HPV is operative, d) Right Air Conditioning Pack is operative, e) Bleed source selector switch is selected to the

R ENG, f) Bleed Air ISOL Valve is operative and selected



engine start, k) Operations are conducted at or below FL 310, l) Maximum number of cabin occupants (including

Flight Attendants) is equal to or less than 82, m) Operations are not conducted in known or

forecast icing conditions, n) Operations are conducted in accordance with


o) Operations are conducted in accordance with AFM Supplement (Air-conditioning - Airplane Dispatch in Single Pack Configuration).

| | | | | | | | | | | | | | | | | | | | | | | | |










e) Right (600-2D15, 600-2D24)


operative, b) Left PRSOV is operative, c) Left HPV is operative, d) Left Air Conditioning Pack is operative, e) Bleed source selector switch is selected to the L

ENG, f) Bleed Air ISOL Valve is operative and selected



engine start, k) Operations are conducted at or below FL 250, l) Operations are not conducted in known or

forecast icing conditions, and m) Operations are conducted in accordance with


| |







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 36 – PNEUMATIC

4. Remarks or Exceptions

21-06 Air Leak Detection System (600-2C10, 600-2D15, 600-2D24, 600-2E25) (cont’d)


e) Right (600-2D15, 600-2D24) (cont’d)


operative, b) Left PRSOV is operative, c) Left HPV is operative, d) Left Air Conditioning Pack is operative, e) Bleed source selector switch is selected to the L

ENG, f) Bleed Air ISOL Valve is operative and selected



engine start, k) Operations are conducted at or below FL 310, l) Maximum number of cabin occupants (including

Flight Attendants) is equal to or less than 82, m) Operations are not conducted in known or

forecast icing conditions, n) Operations are conducted in accordance with


o) Operations are conducted in accordance with AFM Supplement (Air-conditioning - Airplane Dispatch in Single Pack Configuration).

| | | | | | | | | | | | | | | | | | | | | | |




Canadair CL-600-2B19/-2C10/-2D15/-2D24/2E25 Date: Dec 14/15 1 of 3



REASON FOR ISSUE:

• The MMEL Temporary Revision 87 is based on the TCCA accepted TRS No 47. - Item 22-22-01: A new type of malfunction applicable to Yaw Damper (YD) linear-

actuator Part Number (P/N) 622-9968-001, was found on the CRJ700/705/900 aircraft models.

Thus, this TRS splits the aircraft models and introduces dispatch conditions with or without production Modsum 670T122231 or equivalent SB 670BA−22−007 for the CRJ700/705/900 aircraft models only.




THIS PAGE INTENTIONALLY LEFT BLANK









Temp Rev #

Pages Affected

TCCA Approved Description of Revision Date Incorporated Signature

87 22-4 TRS No.47, Walter Istchenko, Chief, Flight Test for Minister of Transport, 13 November 2015

- Item 22-22-01: A new type of malfunction applicable to Yaw Damper (YD) linear-actuator Part Number (P/N) 622-9968-001, was found on the CRJ700/705/900 aircraft models.

Thus, this TRS splits the aircraft models and introduces dispatch conditions with or without production Modsum 670T122231 or equivalent SB 670BA−22−007 for the CRJ700/705/900 aircraft models only.







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 22 – AUTOFLIGHT 4. Remarks or Exceptions Remarques ou exceptions

22-01 Yaw Dampers 1) (600-2C10,

600-2D15, 600-2D24)

|

a) Without Modsum

670T122231 or SB 670BA−22−007

2 2 Must be operative for dispatch. | | | | |

b) With Modsum

670T122231 or SB 670BA−22−007

C 2 1 (M) May be inoperative provided the affected damper is verified not engaged.

| | | |

2) (600-2E25) C 2 1 (M) May be inoperative provided the affected damper

is verified not engaged. |






LETTER OF TRANSMITTAL Based on TCCA CRJ MMEL Rev. 20 and TR 80-1

REASON FOR ISSUE:

• The MMEL Temporary Revision 88 is based on the TCCA accepted TRS No 46. - Item 21-51-01, 21-51-02, and 21-52-01, for single pack dispatch relief using engine

bleed, operation is limited to temperature below ISA+10 is made specific to ground operation.


(1) Remove and discard the pages 3 of 8, 4 of 8, 5 of 8, 6 of 8, and 7 of 8 of TR 80-1 and replace with pages 3 of 7, 4 of 7, 5 of 7, 6 of 7, and 7 of 7 of TR88.


LIST OF PAGES AFFECTED BY THIS TEMPORARY REVISION: TpRv-13 21-14, 21-16, and 21-21.









Temp Rev #

Pages Affected


88 21-14, 21-16, and 21-21

TRS No.46, Walter Istchenko, Chief, Flight Test for Minister of Transport, 15 December 2015

- Item 21-51-01, 21-51-02, and 21-52-01, for single pack dispatch relief using engine bleed, operation is limited to temperature below ISA+10 is made specific to ground operation.






REMOVE AND DISCARD PAGE 3 OF 8 OF TR 80-1 AND INSERT THIS PAGE IN MMEL FACING PAGE 21-14


51-01 Air Conditioning Packs (cont’d)

4) 600-2E25 C 2 1 (O) RH pack may be inoperative provided:

a) RH pack is selected OFF, b) Ram Air SOV is verified operative, c) Operations are conducted at or below FL 250, d) Ground operation for Left Air Conditioning




C 2 1 (O) RH pack may be inoperative provided:

a) RH pack is selected OFF, b) Operations are conducted at or below FL 250, c) Ram Air SOV is verified operative, d) Ground operation for Left Air Conditioning

Pack is conducted using engine bleed, e) Ground operation is limited to temperature

below ISA+10, and f) Operations are conducted in accordance with


|

(cont’d)







(cont’d)


51-01 Air Conditioning Packs (cont’d)

4) 600-2E25

(cont’d)


a) LH pack is selected OFF, b) Ram Air SOV is verified operative, c) Operations are conducted at or below FL 250, d) Ground operation for Right Air Conditioning



AFM Supplement (Operations with Airplane Systems Inoperative).


a) LH pack is selected OFF, b) Ram Air SOV is verified operative, c) Operations are conducted at or below FL 250, d) Ground operation for Right Air Conditioning

Pack is conducted using engine bleed, e) Ground operation is limited to temperature

below ISA+10, and f) Operations are conducted in accordance with

AFM Supplement (Operations with Airplane Systems Inoperative).

|








51-02 Flow Control Valve (FCV) (cont’d)

3) 600-2E25 C 2 1 (M)(O) RH FCV may be inoperative provided:

a) Valve is secured CLOSED, b) RH pack is selected OFF, c) Operations are conducted at or below FL 250, d) Ram Air SOV is verified operative, e) Ground operation for Right Air Conditioning




C 2 1 (M)(O) RH FCV may be inoperative provided:

a) Valve is secured CLOSED, b) RH pack is selected OFF, c) Operations are conducted at or below FL 250, d) Ram Air SOV is verified operative, e) Ground operation for Right Air Conditioning

Pack is conducted using engine bleed, f) Ground operation is limited to temperature

below ISA+10, and g) Operations are conducted in accordance with


|

(cont’d)







(cont’d)

1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 21 – AIR CONDITIONING 4. Remarks or Exceptions Remarques ou exceptions 51-02 Flow Control Valve

(FCV) (cont’d)

3) 600-2E25

(cont’d)

C 2 1 (M)(O) LH FCV may be inoperative provided:

a) Valve is secured CLOSED, b) LH pack is selected OFF, c) Operations are conducted at or below FL 250, d) Ram Air SOV is verified operative, e) Ground operation for Right Air Conditioning




C 2 1 (M)(O) LH FCV may be inoperative provided:

a) Valve is secured CLOSED, b) LH pack is selected OFF, c) Operations are conducted at or below FL 250, d) Ram Air SOV is verified operative, e) Ground operation for Right Air Conditioning




|








52-01 Ram Air SOV (cont’d)

4) 600-2E25 C 1 0 (M)(O) May be inoperative OPEN provided:

a) Ram Air SOV is deactivated OPEN, b) LH Air Conditioning Pack is operative, c) RH Air Conditioning Pack is selected OFF, d) Operations are conducted at or below FL 250, e) Ground operation for Left Air Conditioning




C 1 0 (M)(O) May be inoperative OPEN provided: a) Ram Air SOV is deactivated OPEN, b) LH Air Conditioning Pack is operative, c) RH Air Conditioning Pack is selected OFF, d) Operations are conducted at or below FL 250, e) Ground operation for Left Air Conditioning




|




Canadair CL-600-2B19/-2C10/-2D15/-2D24/-2E25 Date: May 24/2016 1 of 3



REASON FOR ISSUE:

• The MMEL Temporary Revision 89 is based on the TCCA accepted TRS No 49. - New optional item 34-54-02 for ADS-B Out is introduced for the CL-600-2C10, CL-600-

2D15, CL-600-2D24, and CL-600-2E25 models.











Retain this index in the front of the manual. When Temporary Revisions are issued or cancelled, enter the date you insert each revision in your manual. Temp Rev #

Pages Affected


89 34-7 TRS No. 49, Walter Istchenko, Chief, Flight Test for Minister of Transport, 04 April 2016

New optional item 34-54-02 for ADS-B Out is introduced for the CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2E25 models.







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 34 – NAVIGATION 4. Remarks or Exceptions Remarques ou exceptions

54-02 Automatic Dependent

Surveillance – Broadcast (ADS-B Out) (600-2C10, 600-2D15, 600-2D24 600-2E25) ***

C 2 0 (O) May be inoperative where routine procedures require its use provided alternate procedures are established and used.

NOTE: Any ADS-B Out function which operates

normally may be used.

D 2 0 May be inoperative provided operating regulations do not require its use.




Canadair CL-600-2B19/-2C10/-2D15/-2D24/-2E25 Date: July 04/2016 1 of 5



REASON FOR ISSUE:

• The MMEL Temporary Revision 90 is based on the TCCA approved TRS No 43. - New Item introduced as part of Bombardier Take-Off Safety Enhancement (TOSE) long term

action plan.



LIST OF PAGES AFFECTED BY THIS TEMPORARY REVISION: TpRv-13 30-1 and 30-5









Temp Rev #

Pages Affected


90 30-1, and 30-5

TRS No. 43, Walter Istchenko, Chief, Flight Test for Minister of Transport, 14 September 2015

Item 30-12-01 introduces SB 601R-30-034 on the 600-2B19 model and corrects editorial error in reference to AFM Supplement

Item 30-12-09 600-2B19 with SB 601R-30-034. New item introduced as part of Bombardier Take-Off Safety Enhancement (TOSE) long term action plan.







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 30 – ICE AND RAIN PROTECTION 4. Remarks or Exceptions Remarques ou exceptions

12-01 Wing Anti-Ice Modulating and SOVs (Wing Anti-Ice Valve)

C 2 0 (M) Both may be inoperative provided: a) Valves are secured CLOSED, b) Operations are not conducted in known or

forecast icing conditions, and c) Both Ice Detection Systems are operative.

1) (600-2B19 without

SB 601R-30-034) C 2 1 (M) May be inoperative CLOSED provided:

a) Valve is secured CLOSED, and b) 14th Stage ISOL Valve is operative and

selected OPEN.

| | | |

2) (600-2B19 with

SB 601R-30-034) C 2 1 (M) May be inoperative CLOSED provided:

a) Valve is secured CLOSED, b) 14th Stage ISOL Valve is operative and

selected OPEN, c) Low Temperature Ground Wing Anti-Ice

System is considered inoperative, and d) Wing Anti-Ice System is operative.

| | | | | | |

3) (600-2C10,

600-2D15, 600-2D24 without ModSum 670T11216)

C 2 1 (M)(O) May be inoperative CLOSED provided: a) Air Conditioning Pack on the affected side is

operative and is operated continuously throughout flight,

b) Wing Cross Bleed Valve is operative, c) Wing cross bleed selector switch is selected to

the opposite side (FROM LEFT or FROM RIGHT), and

d) Operations are conducted in accordance with AFM Supplement (Performance Penalties for Operations with Airplane Systems Inoperative).

|

(cont’d)







(cont’d)


12-01 Wing Anti-Ice Modulating and SOVs (Wing Anti-Ice Valve) (cont’d)

4) (600-2C10,

600-2D15, 600-2D24 with ModSum 670T11216), (600-2E25)

C 2 1 (M) May be inoperative CLOSED provided: a) Wing Cross Bleed Valve is operative, b) Wing cross bleed selector switch is selected to

the opposite side (FROM LEFT or FROM RIGHT), and

c) Operations are conducted in accordance with AFM Supplement (Performance Penalties for Operations with Airplane Systems Inoperative).

|








12-09 Low Temperature Ground Wing Anti-Ice System (LTGWAIS) (600-2B19 with SB 601R-30-034)

C 1 0 (M)(O) May be inoperative provided: a) The SUPP GND WING ANTI-ICE SYS OFF

switch is selected to OFF, b) Wing Anti-Ice System is operative, and c) Operations are conducted in accordance with

AFM Supplement (Performance Penalties for Operations with Airplane Systems Inoperative).

| | | | | | | |

C 1 0 (M)(O) May be inoperative as indicated by TEMP ‘FAIL

LO’ amber light on SUPP GND WING ANTI-ICE panel provided:

a) The SUPP GND WING ANTI-ICE SYS OFF switch is selected to OFF,

b) Wing Anti-Ice System is operative, and c) Operations are conducted in accordance with


| | | | | | | | | |

C 1 0 (M)(O) May be inoperative as indicated by TEMP ‘FAIL

HI’ amber light on the SUPP GND WING ANTI-ICE panel provided:

a) The SUPP GND WING ANTI-ICE SYS OFF switch is selected to OFF,

b) Wing Anti-Ice System is operative, and c) Operations are conducted in accordance with


| | | | | | | | | |




Canadair CL-600-2B19/-2C10/-2D15/-2D24/-2E25 Date: April 03/2017 1 of 3



REASON FOR ISSUE:

• The MMEL Temporary Revision 91 is based on the TCCA accepted TRS No 50. - New STD Button sub item 34-12-01 3) for Integrated Standby Instruments System (ISIS) is

introduced for the CL-600-2B19, CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2E25 models.












Temp Rev #

Pages Affected


91 34-1 TRS No. 50, Walter Istchenko, Chief, Flight Test for Minister of Transport, 15 March 2017

New STD Button sub item 34-12-01 3) for Integrated Standby Instruments System (ISIS) is introduced for the CL-600-2B19, CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2E25 models.







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 34 – NAVIGATION 4. Remarks or Exceptions Remarques ou exceptions

12-01 Integrated Standby

Instruments (ISI) (600-2B19***, 600-2C10, 600-2D15, 600-2D24, 600-2E25)

1) NAV Function C 1 0 Same. 2) Attitude Function B 1 0 Same. 3) STD Button *** C 1 0 (O) May be inoperative provided ISI BARO knob

operates normally. | |







REASON FOR ISSUE:

• The MMEL Temporary Revision 92 is based on the TCCA accepted TRS No 51. - New Controller to Pilot Data Link Communication (CPDLC) - Link 2000+ sub item 23-22-01

1) for Aircraft Communications Addressing and Reporting System (ACARS) is introduced for the CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2E25 models.












Temp Rev #

Pages Affected


92 23-1 TRS No. 51, Walter Istchenko, Chief, Flight Test for Minister of Transport, 15 March 2017

New Controller to Pilot Data Link Communication (CPDLC) sub item 23-22-01 1) for Aircraft Communications Addressing and Reporting System (ACARS) is introduced for the CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2E25 models.







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 23 – COMMUNICATION 4. Remarks or Exceptions Remarques ou exceptions

22-01 Aircraft

Communications Addressing and Reporting System (ACARS) ***

C 1 0 Same.

D 1 0 Same. 1) Controller Pilot

Data Link Communication (CPDLC) - Link 2000+ *** (600-2C10 600-2D15 600-2D24 600-2E25)

C 1 0 (O) May be inoperative where routine procedures require its use provided alternate procedures are established and used.

| | | | | | | | | |

D 1 0 May be inoperative provided operating regulations do

not require its use.

| |







REASON FOR ISSUE:

- The MMEL Temporary Revision 93 is based on the TCCA accepted TRS No 52. - The updated item 52-31-01 for balance springs includes remark for (M) procedure and

clarification for deactivation of the affected spring introduced for the CL-600-2B19, CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2E25 models.












Temp Rev #

Pages Affected


93 52-3 TRS No. 52, Walter Istchenko, Chief, Flight Test for Minister of Transport, 17 May 2017.

Item 52-31-01 (Balance Springs) is updated to include remark for (M) procedure and clarification for deactivation of the affected spring introduced for the CL-600-2B19, CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2E25 models.







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 52– DOORS 4. Remarks or Exceptions Remarques ou exceptions

31-01 Balance Springs

1) Cargo Compartment Door (600-2B19)

C 2 1 (M) May be inoperative provided door is verified operative (opens and closes) without interference and affected spring is deactivated. NOTE: Door may close faster.

| |

2) Aft Cargo

Compartment Door (600-2C10, 600-2D15, 600-2D24, 600-2E25)

C 2 1 (M) May be inoperative provided door is verified operative (opens and closes) without interference and affected spring is deactivated. NOTE: Door may close faster.

| |




Canadair CL-600-2B19/-2C10/-2D15/-2D24/-2E25 Date: December 14/2017 1 of 3



REASON FOR ISSUE:

• The MMEL Temporary Revision 94 is based on the TCCA accepted TRS No 54. - The updated item 24-50-04 for Cockpit Power Outlets and USB Ports System is introduced

for CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2E25 models.












Temp Rev #

Pages Affected


94 24-13 TRS No. 54, Walter Istchenko, Chief, Flight Test for Minister of Transport, 13 December 2017.

The item 24-50-04 (Cockpit Power Outlets and USB Ports System) is introduced for CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2E25 models.







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 24 – ELECTRICAL POWER 4. Remarks or Exceptions Remarques ou exceptions

50-04 Cockpit Power Outlets

and USB Ports System *** (600-2C10, 600-2D15, 600-2D24 600-2E25)

D 1 0 (M) May be inoperative provided the power supply system for the power outlets and USB ports is deactivated.

| | | | | | |




Canadair CL-600-2B19/-2C10/-2D15/-2D24/-2E25 Date: January 15/2018 1 of 3



REASON FOR ISSUE:

• The MMEL Temporary Revision 95 is based on the TCCA accepted TRS No 55. - The updated item 33-41-01 for Landing Lights is introduced for CL-600-2C10, CL-600-2D15,

CL-600-2D24, and CL-600-2E25 models.












Temp Rev #

Pages Affected


95 33-5 TRS No. 55, Walter Istchenko, Chief, Flight Test for Minister of Transport, 10 January 2018.

New optional relief for the Nose Landing Light (LED) item 33-41-01 is introduced for CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2E25 models.







1. 2. Number Installed System & Sequence No Item Nombre d'articles installés No de système/série article 3. Number Required For Dispatch Nombre d'articles à expédier 33 – LIGHTS 4. Remarks or Exceptions Remarques ou exceptions

41-01 Landing Lights

1) 600-2B19

C 4

3

Same.

C 4 2 Same. C 4 0 Same. 2) 600-2C10,

600-2D15, 600-2D24, 600-2E25

a) Nose Light

(Incandescent) C 1 0 Same.

| C 1 0 Same. b) Nose Light

(LED) ***

C 1 0 May be inoperative provided: a) Both Wing Landing Lights are operative, and b) Both Taxi/Recognition Lights are operative.

NOTE: The light is considered inoperative with more than two individual LEDs inoperative.

| | | | |

C 1 0 May be inoperative provided aircraft is not operated at

night.

NOTE: The light is considered inoperative with more than two individual LEDs inoperative.

| | | |

c) Wing Lights C 2 1 One may be inoperative provided the associated

Taxi/Recognition Light is operative. |

C 2 0 Both may be inoperative provided aircraft is not

operated at night.

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