U.S. DEPARTMENT OF TRANSPORTATION 

FEDERAL AVIATION ADMINISTRATION 

In the Matter of: 

MN Airlines, LLC d/b/a 

Sun Country Airlines. 

) 

) 

) 

) 

) 

) 

FAA Docket No. CP-FDMS-2015-2444 

Case No. 2014-GL-15-0030 

Administrative Law Judge J.E. Sullivan 

RULE 26(a)(l) INITIAL DISCLOSURES OF MN AIRLINES, LLC d/b/a SUN 

COUNTRY AIRLINES 

MN Airlines, LLC d/b/a Sun Country Airlines, Respondent, by and through its 

undersigned counsel, for its initial disclosures pursuant to F.R.C.P. 26(a)(l) state as follows: 

A. Fact Witnesses 

1. Thomas Groshans 

2. Kevin Kaiser 

3. Heidi De Hoogh 

4. Ron Bums 

5. Brenda Bouma 

6. Ashtyn Kupser 

7. Jim Duffy 

8. Steve Dykhuizen 

9. David Benner 

10. Todd LaSalle 

11. Glen Bloomquist 

12. Anthony Sasso 

13. Doug Jolmson 

14. Craig Hiram 

15. Jolm Spanjers 

16. Craig Seppala 

B. Documents 

Please see enclosed. 

c. Damages 

Not Applicable. 

D. Insurance 
Not Applicable. 

Dated this_!_ 

-

day of January, 2016~---

Donald Chance Mark, Jr. (#67659) 

Fafinski Mark & Johnson, P.A. 

775 Prairie Center Drive, Suite 400 

Flagship Corporate Center 

Eden Prairie, MN 55344 

Telephone: 952-995-9500 

Facsimile: 952-995-9577 
CERTIFICATE OF SERVICE 

I hereby certify that on the~ day of January, 2016, I served, via facsimile, a copy of 

the foregoing Initial Disclosures in the Matter of MN Airlines, LLC d/b/a Sun Country Airlines, 

FAA Docket No. CP-FDMS-20 15-2444, Case No. 2014-GL-15-0030, upon: 

Lauren Hoyson, Esq., Complainant's Counsel 

Federal Aviation Administration 

Great Lakes Regional Counsel's Office 

2300 East Devon Avenue, Suite 479 

Des Plaines, IL 60018 

Telephone: 847-294-7165 

Facsimile: 847-294-7498 

Honorable J.E. Sullivan, Administrative Law Judge 

Office of Hearings, M-20 

U.S. Department of Transportation 

1200 New Jersey Avenue, S.E. (E11-310) 

Washington, DC 20590 

Telephone: 202-366-6941 

Facsimile: 202-366-7536 

In addition, I have sent for filing, via U.S. Mail, the original and one copy of the 

foregoing Answer to: 

Hearing Docket 

Federal Aviation Administration 

Attention: Hearing Docket Clerk, AGC-430 

Wilbur Wright Building, Suite 2W1000 

800 Independence Avenue, S.W. 

Washington, DC 20591 

Wendy J. Flan ry, Legal Asststant 

Fafinski Mark & Johnson, P.A. 
-sun country an-l1nes 

Nov 25,2014 Transmittal 

MELfCDL 

B-T3T 

1 

To: All holders ofMN Airlines d/b/a Sun Country Airlines MELICDL Manual. 

Subject: MELICDL Manual Revision. 

Revision Number: 42 

Revision Date: Nov 25, 2014 

This revision reflects the most current information available to Sun Country Airlines through the 

subject revision date. The following revision highlights explain changes in this revision. 

THE FOLLOWING INFORMATION IS EFFECTIVE UPON RECEIPT UNLESS OTHERWISE 

NOTED. 

Revision Highlights 

Generally, revision bars are displayed adjacent to all technical and non-technical changes. However, 

highlights are written only for technical revisions. In some sections, the information may have been 

extensively rewritten for clarity, in these cases a highlight is written, but change bars may not be provided. Revision bars will not be provided on pages issued for the purpose of repagination or formatting only 

Add means that a new MEL item has been added to the SCA MEL. 

Replace means remove existing MEL item and replace with revised MEL item pages. 

Delete means the remove and destroy the MEL item. 

Revision Highlights 

Item MMEL DDG SCA Instruction Highlights 

LEP-0.1 - X Replace Updated List of Effective Pages. 

LEP-0.8 

1-0.1 - 1-0.2 X Replace Introduction 

Revised to current revision approval. 

4-0.1 - 4-0.4 X Replace Equipment Addendum 

Added aircraft 820SY and 821SY equipment. 

23-0.1 - 23- X Replace Updated Table of Contents. 

0.2 

23-10.1 - 23- X Replace 23-10 Cockpit Voice Recorder System 

10.2 (CVR) 

Added items for Recorder Independent Power 

Supplies. 

23-27.1 - 23- X Add 23-27 Data Link Communication 

27.2 Added item for aircraft Data Link equipment. 

25-6.1 - 25- X Replace 25-6 Passenger Seat(s) 

6.2 Incorporated interim revision. 
MEL/CDL 

B-T3T 

2 

Item 

25-10.1 - 25-

10.10 

27-4.1 - 27-

4.4 

27-7.1 - 27-

7.2 

27-8.1 - 27-

8.2 

34-0.1 - 34-

0.2 

34-54.1 - 34.54.2 

34-55.1 - 34.55.2 

35-4.1 - 35.4.2 

47-1.1 - 47.1.2 

73-4.1 - 73-

4.2 

74-1.1 - 74-

1.2 

57-0-0.1 -57-

0-0.2 

57-31-1.1 -

57-31-1.2 

MMEL DDG SCA 

X 

X 

X 

X 

X 

X 

X 

X 

X 

X 

X 

X 

X 

-sun country a!tl!nes 

Transmittal Nov 25,2014 

Instruction Highlights 

Replace 25-10 Non-Essential Equipment and 

Furnishing (NEF) 

Incorporated interim revision and added PSK 

and window drain hose items. 

Replace 27-4 Leading Edge Flap/Slat Position Light 

Systems 

Added Maintenance Procedure for aircraft 

820SY and 821SY. 

Replace 27-7 Auto Speed Brake System 

Added provisions for aircraft 820SY and 

821SY. 

Replace 27-8 Flap Load Limiter System 

Added Maintenance Procedure for aircraft 

820SY and 821SY. 

Replace Updated Table of Contents. 

Add 34-54 Integrated Standby Flight Display 

(ISFD) 

Added MEL item for ISFD equipment. 

Add 34-55 Vertical Situation Display (VSD) 

Added MEL item for VSD equipment. 

Replace 35-4 Portable Oxygen Dispensing Units 

(Bottle and Mask) 

Added 820SY and 821 SY qualifiers. 

Replace 47-1 Nitrogen Generation System (NGS) 

Revised F IC deferral item. 

Replace 73-4 Fuel Filter Differential Pressure 

Warning Systems 

Incorporated interim revision. 

Replace 7 4-1 Ignition Systems 

Revised Maintenance Procedure. 

Replace Updated Table of Contents. 

Add Split Scimitar Winglet Ventral Strake 

Added MEL item for split scimitar equipment. 

Nov 25,2014 

PAGENO. DATE 

Title Page 

Table of Contents 

MEL/CDL-0.1May 29,2014 

MELICDL-0.2May 29, 2014 

Record of Revisions 

ROR-0.1 May29, 2014 

ROR-0.2 May 29,2014 

ROR-0.3 May29, 2014 

ROR-0.4 May29, 2014 

List Of Effective Pages 

*LEP-0.1 Nov 25,2014 

*LEP-0.2 Nov 25,2014 

*LEP-0.3 Nov25, 2014 

*LEP-0.4 Nov 25, 2014 

*LEP-0.3 Nov 25,2014 

*LEP-0.4 Nov25,2014 

*LEP-0.5 Nov25, 2014 

*LEP-0.6 Nov 25,2014 

*LEP-0.7 Nov 25,2014 

*LEP-0.8 Nov25,2014 

Introduction 

*1-0.1 Nov 25,2014 

1-0.2 May 29,2014 

Definitions & Preamble 

2-0.1 May29, 2014 

2-0.2 May 29, 2014 

2-0.3 May 29,2014 

2-0.4 May29, 2014 

2-0.5 May29, 2014 

2-0.6 May 29,2014 

I 

List of Effective Pages 

PAGE NO. DATE 

2-0.7 May 29,2014 

2-0.8 May 29,2014 

Practices 

3-0.1 May 29,2014 

3-0.2 May 29,2014 

3-0.3 May 29,2014 

3-Q.4 May 29,2014 

3-0.5 May 29,2014 

3-0.6 May 29,2014 

3-0.7 May 29,2014 

3-0.8 May 29,2014 

Equipment Addendum 

'4-0.1 Nov 25,2014 

*4-0.2 Nov 25,2014 

*4-0.3 Nov 25,2014 

4-0.4 Ju1 01, 2014 

Minimum 

Equipment List 

Air Conditioning-21 

21-0.1 May 29,2014 

21-0.2 May 29,2014 

21-l.l May 29,2014 

21-1.2 May 29,2014 

21-1.3 May 29,2014 

21-1.4 May 29,2014 

21-2.1 May 29,2014 

21-2.2 May 29,2014 

21-3.1 May 29,2014 

21-3.2 May 29,2014 

21-5.1 May 29,2014 

21-5.2 May 29,2014 

PAGE NO. 

21-7.1 

21-7.2 

21-8.1 

21-8.2 

21-9.1 

21-9.2 

21-10.1 

21-10.2 

21-1l.l 

21-11.2 

21-12.1 

21-12.2 

21-13.1 

21-13.2 

21-14.1 

21-14.2 

21-15.1 

21-15.2 

21-16.1 

21-16.2 

21-17.1 

21-17.2 

21-18.1 

21-18.2 

21-19.1 

21-19.2 

21-2l.l 

21-21.2 

21-21.3 

21-21.4 

21-24.1 

DATE PAGE NO. 

May 29,2014 21-24.2 

May 29,2014 21-25.1 

May 29,2014 21-25.2 

May 29,2014 21-26.1 

May 29,2014 21-26.2 

May 29,2014 21-27.1 

May 29,2014 21-27.2 

May 29,2014 21-3l.l 

May 29,2014 21-31.2 

May 29,2014 21-32.1 

May29,2014 21-32.2 

May 29,2014 21-33.1 

May 29,2014 21-33.2 

May 29,2014 21-34.1 

May 29,2014 21-34.2 

May29, 2014 21-35.1 

May 29,2014 21-35.2 

May 29,2014 21-36.1 

May 29,2014 21-36.2 

May29, 2014 21-38.1 

May 29,2014 21-38.2 

May 29,2014 21-39.1 

May 29,2014 21-39.2 

May 29,2014 21-39.3 

May 29,2014 21-39.4 

May 29,2014 21-40.1 

May 29,2014 21-40.2 

May 29,2014 21-4l.l 

May 29,2014 21-41.2 

May 29,2014 21-42.1 

May 29,2014 21-42.2 

MEL/CDL 

B-737 

LEP-0.1 

DATE 

May 29,2014 

May 29,2014 

May 29,2014 

May 29,2014 

May29, 2014 

May29, 2014 

May 29,2014 

May 29,2014 

May29, 2014 

May29, 2014 

May29, 2014 

May 29,2014 

May29, 2014 

May29, 2014 

May 29,2014 

May 29,2014 

May29, 2014 

May 29,2014 

May 29,2014 

May29,2014 

May 29,2014 

May 29,2014 

May 29,2014 

May 29,2014 

May 29,2014 

May29, 2014 

May 29,2014 

May 29,2014 

May 29,2014 

May 29,2014 

May 29,2014 

FAAApprove~d~: ________ O~ri~g~in~a~l~s~ig~n~e~d~an~d~d=a=te~d~by~G~l~cnn==~B~l~oo~m~g~u=is~t ____________________ __ 

Principal Operations Inspector 
NIEL/CDL 

B-737 -~sun country a1rl1nes 

LEP-0.2 List of Effective Pages Nov 25,2014 

PAGE NO. DATE PAGE NO. DATE PAGE NO. DATE PAGE NO. DATE 

21-43.1 May 29,2014 22-16.1 May 29, 2014 23-14.1 May 29,2014 24-7.1 May 29,2014 

21-43.2 May 29,2014 22-16.2 May 29,2014 23-14.2 May 29,2014 24-7.2 May 29,2014 

21-44.1 May 29,2014 22-17.1 May 29, 2014 23-15.1 May 29,2014 24-8.1 May 29,2014 

21-44.2 May 29,2014 22-17.2 May 29, 2014 23-15.2 May 29,2014 24-8.2 May 29,2014 

21-50.1 May 29,2014 22-18.1 May 29,2014 23-16.1 May 29,2014 24-9.1 May 29,2014 

21-50.2 May 29,2014 22-18.2 May 29,2014 23-16.2 May 29,2014 24-9.2 May 29,2014 

Auto Flight-22 22-19.1 May 29,2014 23-17.1 May 29,2014 24-11.1 May 29,2014 

22-0.1 May 29,2014 22-19.2 May 29,2014 23-17.2 May 29,2014 24-11.2 May 29,2014 

22-0.2 May 29,2014 22-20.1 May29, 2014 23-18.1 May 29,2014 24-12.1 May 29,2014 

22-1.1 May 29,2014 22-20.2 May 29,2014 23-18.2 May 29,2014 24-12.2 May 29,2014 

22-1.2 May 29,2014 Communications-23 23-19.1 May29, 2014 24-14.1 May 29,2014 

22-2.1 May 29,2014 *23-0.1 Nov 25,2014 23-19.2 May 29,2014 24-14.2 May 29,2014 

22-2.2 May 29,2014 23-0.2 May29, 2014 23-20.1 May 29,2014 24-15.1 May 29,2014 

22-3.1 May 29,2014 23-1.1 May 29,2014 23-20.2 May 29,2014 24-15.2 May 29,2014 

22-3.2 May 29,2014 23-1.2 May 29,2014 23-21.1 May 29,2014 24-16.1 May 29,2014 

22-4.1 May 29,2014 23-2.1 May 29,2014 23-21.2 May 29,2014 24-16.2 May 29,2014 

22-4.2 May 29,2014 23-2.2 May29, 2014 23-23.1 May 29,2014 24-17.1 May 29,2014 

22-5.1 May 29,2014 23-3.1 May 29,2014 23-23.2 May 29,2014 24-17.2 May 29,2014 

22-5.2 May 29,2014 23-3.2 May 29,2014 23-26.1 May 29,2014 24-18.1 May 29,2014 

22-8.1 May 29,2014 23-4.1 May 29,2014 23-26.2 May 29,2014 24-18.2 May 29,2014 

22-8.2 May 29,2014 23-4.2 May29, 2014 *23-27.1 Nov25, 2014 24-19.1 May 29,2014 

22-9.1 May 29,2014 23-6.1 May 29,2014 '23-27.2 Nov 25, 2014 24-19.2 May 29,2014 

22-9.2 May 29,2014 23-6.2 May 29,2014 Electrical Power-24 Equipment Furnishings-25 

22-10.1 May 29,2014 23-9.1 May 29,2014 24-0.1 May 29,2014 25-0.1 May 29,2014 

22-10.2 May 29,2014 23-9.2 May 29,2014 24-0.2 May 29,2014 25-0.2 May 29,2014 

22-11.1 May 29,2014 *23-10.1 Nov 25, 2014 24-1.1 May 29,2014 25-3.1 May 29,2014 

22-11.2 May 29,2014 23-10.2 May 29,2014 24-1.2 May 29,2014 25-3.2 May 29,2014 

22-14.1 May 29,2014 23-11.1 May 29,2014 24-2.1 May 29,2014 25-4.1 May 29,2014 

22-14.2 May29, 2014 23-11.2 May 29, 2014 24-2.2 May 29,2014 25-4.2 May 29, 2014 

22-15.1 May 29,2014 23-12.1 May 29,2014 24-3.1 May 29,2014 25-5.1 May 29,2014 

22-15.2 May 29,2014 23-12.2 May 29, 2014 24-3.2 May 29,2014 25-5.2 May 29,2014 

FAA Approved,.,: ______ Origif!al signed and dated by Glenn Bloomquist 

Principal Operations Inspector 
$sun country a1rl1nes 

Nov 25,2014 List of Effective Pages 

PAGE NO. DATE PAGE NO. DATE PAGE NO. DATE 

*25-6.1 Nov 25,2014 25-99.1 May 29,2014 26-16.2 May 29,2014 

25-6.2 Nov26, 2014 25-99.2 May 29,2014 26-18.1 May 29,2014 

25-9.1 May 29,2014 Fire Protection-26 26-18.2 May 29,2014 

25-9.2 May29, 2014 26-0.1 May 29,2014 26-19.1 May29, 2014 

*25-10.1 Nov 25,2014 26-0.2 May 29,2014 26-19.2 May 29,2014 

*25-10.2 Nov25,2014 26-l.l May 29,2014 26-19.3 May 29,2014 

*25-10.3 Nov 25,2014 26-1.2 May29, 2014 26-19.4 May 29,2014 

*25-10.4 Nov 25, 2014 26-2.1 May 29,2014 Flight Controls-27 

*25-10.5 Nov 25, 2014 26-2.2 May 29,2014 27-0.1 May 29,2014 

*25-10.6 Nov 25,2014 26-3.1 May 29,2014 27-0.2 May 29,2014 

*25-10.7 Nov25, 2014 26-3.2 May 29,2014 *27-4.1 Nov25, 2014 

*25-10.8 Nov 25, 2014 26-4.1 May 29,2014 *27-4.2 Nov 25, 2014 

*25-10.9 Nov 25, 2014 26-4.2 May 29,2014 *27-4.3 Nov 25, 2014 

*25-10.10 Nov 25,2014 26-6.1 May 29,2014 *27-4.4 Nov25, 2014 

25-1l.l May 29,2014 26-6.2 May29, 2014 *27-7.1 Nov 25, 2014 

25-11.2 May 29,2014 26-7.1 May 29,2014 *27-7.2 Nov 25,2014 

25-12.1 May 29,2014 26-7.2 May 29,2014 *27-8.1 Nov25, 2014 

25-12.2 May 29,2014 26-8.1 May 29,2014 27-8.2 May 29,2014 

25-16.1 May 29,2014 26-8.2 May 29,2014 27-9.1 May 29,2014 

25-16.2 May 29,2014 26-9.1 May 29,2014 27-9.2 May 29,2014 

25-17.1 May 29,2014 26-9.2 May 29,2014 27-10.1 May 29,2014 

25-17.2 May 29,2014 26-9.3 May 29,2014 27-10.2 May 29,2014 

25-18.1 May29, 2014 26-9.4 May 29,2014 27-10.3 May 29,2014 

25-18.2 May 29, 2014 26-10.1 May 29,2014 27-10.4 May 29,2014 

25-20.1 May 29,2014 26-10.2 May 29,2014 27-1l.l May 29,2014 

25-20.2 May29, 2014 26-12.1 May29, 2014 27-11.2 May 29,2014 

25-2l.l May 29,2014 26-12.2 May 29,2014 27-12.1 May 29,2014 

25-21.2 May 29,2014 26-13.1 May 29,2014 27-12.2 May 29,2014 

25-22.1 May 29,2014 26-13.2 May 29,2014 27-14.1 May 29,2014 

25-22.2 May 29, 2014 26-15.1 May 29,2014 27-14.2 May 29,2014 

25-24.1 May 29,2014 26-15.2 May 29,2014 27-16.1 May 29,2014 

25-24.2 May 29,2014 26-16.1 May 29,2014 27-16.2 May 29,2014 

PAGE NO. 

27-17.1 

27-17.2 

27-20.1 

27-20.2 

27-20.3 

27-20.4 

27-2l.l 

27-21.2 

MEL/CDL 

B-T3T 

LEP-0.3 

DATE 

May 29,2014 

May29, 2014 

May 29, 2014 

May 29,2014 

May 29,2014 

May29, 2014 

May 29,2014 

May29, 2014 

Fuei-28 

28-0.1 May 29, 2014 

28-0.2 May29, 2014 

28-l.l May29, 2014 

28-1.2 May 29,2014 

28-2.1 May 29,2014 

28-2.2 May 29,2014 

28-2.3 May 29,2014 

28-2.4 May 29,2014 

28-3.1 May 29,2014 

28-3.2 May 29,2014 

28-3.3 May29, 2014 

28-3.4 May 29,2014 

28-4.1 May 29,2014 

28-4.2 May 29,2014 

28-5.1 May 29,2014 

28-5.2 May 29,2014 

28-6.1 May 29,2014 

28-6.2 May 29,2014 

28-7.1 May 29,2014 

28-7.2 May 29,2014 

28-8.1 May 29,2014 

28-8.2 May 29,2014 

28-9.1 May 29,2014 

FAA Approve~: ----------'O"'r"'ig,ic>n«al,_s/.'il'>g«ne:::d~an~d~d«at~e~dc'b~y'-G=le=.-nn=B=lo""o"'m~q'!'u=-'i"-st,_ _______ _ 

Principal Operations Inspector 
MEL/CDL 

B-737 

LEP-0.4 

PAGE NO. DATE 

28-9.2 May 29,2014 

28-10.1 May 29,2014 

28-10.2 May 29,2014 

28-12.1 May 29,2014 

28-12.2 May 29,2014 

28-16.1 May 29,2014 

28-16.2 May 29,2014 

28-17.1 May 29,2014 

28-17.2 May 29,2014 

28-21.1 May 29,2014 

28-21.2 May 29,2014 

28-22.1 May 29,2014 

28-22.2 May 29,2014 

Hydraulic Power-29 

29-0.1 May 29,2014 

29-0.2 May 29,2014 

29-2.1 May 29,2014 

29-2.2 May 29,2014 

29-3.1 May 29,2014 

29-3.2 May 29,2014 

29-4.1 May 29,2014 

29-4.2 May 29,2014 

29-5.1 May 29,2014 

29-5.2 May 29,2014 

29-7.1 May 29,2014 

29-7.2 May 29,2014 

29-9.1 May 29,2014 

29-9.2 May 29,2014 

29-10.1 May 29,2014 

29-10.2 May 29,2014 

29-11.1 May 29,2014 

-sun country airlines 

List of Effective Pages Nov 25,2014 

PAGE NO. DATE PAGE NO. DATE PAGE NO. DATE 

29-11.2 May 29,2014 30-6.2 May29, 2014 31-9.2 May 29,2014 

29-12.1 May 29, 2014 30-7.1 May 29,2014 31-10.1 May 29,2014 

29-12.2 May 29,2014 30-7.2 May 29,2014 31-10.2 May 29,2014 

29-13.1 May 29,2014 30-8.1 May 29,2014 31-11.1 May 29,2014 

29-13.2 May 29,2014 30-8.2 May 29,2014 31-11.2 May 29,2014 

29-15.1 May 29,2014 30-9.1 May 29,2014 31-14.1 May 29,2014 

29-15.2 May 29,2014 30-9.2 May 29,2014 31-14.2 May29, 2014 

29-16.1 May 29,2014 30-11.1 May 29,2014 Landing Gear-32 

29-16.2 May 29,2014 30-11.2 May 29,2014 32-0.1 May 29,2014 

29-17.1 May 29,2014 30-12.1 May29, 2014 32-0.2 May 29,2014 

29-17.2 May 29,2014 30-12.2 May29, 2014 32-2.1 May29, 2014 

29-18.1 May 29,2014 30-13.1 May 29,2014 32-2.2 May 29,2014 

29-18.2 May 29,2014 30-13.2 May 29,2014 32-4.1 May 29,2014 

Ice & Rain Protcction-30 30-17.1 May 29,2014 32-4.2 May 29,2014 

30-0.1 May 29,2014 30-17.2 May29, 2014 32-7.1 May 29,2014 

30-0.2 May 29,2014 30-18.1 May29,2014 32-7.2 May29, 2014 

30-1.1 May 29,2014 30-18.2 May29, 2014 32-8.1 May29, 2014 

30-1.2 May 29,2014 30-19.1 May 29,2014 32-8.2 May 29,2014 

30-1.3 May 29,2014 30-19.2 May 29,2014 32-10.1 May 29,2014 

30-1.4 May 29,2014 Indicating/Recording 32-10.2 May29, 2014 

Systems-31 

30-2.1 May 29,2014 32-12.1 May29, 2014 

31-0.1 May 29,2014 

30-2.2 May 29,2014 32-12.2 May 29,2014 

31-0.2 May29, 2014 

30-3.1 May 29,2014 32-13.1 May 29,2014 

31-1.1 May29, 2014 

30-3.2 May29, 2014 32-13.2 May 29,2014 

31-1.2 May 29,2014 

30-3.3 May 29,2014 32-14.1 May29, 2014 

31-2.1 May 29,2014 

30-3.4 May 29,2014 32-14.2 May 29,2014 

31-2.2 May 29,2014 

30-4.1 May 29,2014 32-15.1 May 29,2014 

31-7.1 May29, 2014 

30-4.2 May 29,2014 32-15.2 May 29,2014 

31-7.2 May 29,2014 

30-5.1 May 29,2014 32-15.3 May29, 2014 

31-8.1 May 29,2014 

30-5.2 May 29, 2014 32-15.4 May 29,2014 

31-8.2 May 29,2014 

30-6.1 May 29,2014 32-17.1 May 29,2014 

31-9.1 May29, 2014 

}1\AApproved~:~----------~O~r~ig~i~n~a~ls~i~g~n~ed~an~d~d~a=te~d~b~y~G~le~n=n~B=lo~o~m~g~u~i~st~----------------­

Principal Operations Inspector 
Nov 25,2014 List of Effective Pages 

PAGE NO. DATE PAGE NO. DATE PAGE NO. 

32-17.2 May 29, 2014 33-12.1 May 29,2014 34-5.2 

32-19.1 May 29. 2014 33-12.2 May 29,2014 34-7.1 

32-19.2 May 29,2014 33-14.1 May 29,2014 34-7.2 

32-20.1 May 29,2014 33-14.2 May 29, 2014 34-11.1 

32-20.2 May29, 2014 33-15.1 May 29,2014 34-11.2 

32-21.1 May 29, 2014 33-15.2 May 29,2014 34-12.1 

32-21.2 May 29, 2014 33-16.1 May 29,2014 34-12.2 

Lights-33 33-16.2 May 29,2014 34-13.1 

33-0.1 May 29,2014 33-17.1 May 29,2014 34-13.2 

33-0.2 May 29,2014 33-17.2 May 29,2014 34-14.1 

33-1.1 May 29,2014 33-18.1 May 29, 2014 34-14.2 

33-1.2 May 29, 2014 33-18.2 May 29,2014 34-15.1 

33-2.1 May 29, 2014 33-19.1 May 29,2014 34-15.2 

33-2.2 May 29,2014 33-19.2 May 29,2014 34-16.1 

33-3.1 May 29,2014 33-20.1 May 29,2014 34-16.2 

33-3.2 May 29, 2014 33-20.2 May 29,2014 34-17.1 

33-4.1 May 29,2014 33-23.1 May 29, 2014 34-17.2 

33-4.2 May 29, 2014 33-23.2 May 29,2014 34-18.1 

33-5.1 May 29, 2014 33-25.1 May 29,2014 34-18.2 

33-5.2 May 29,2014 33-25.2 May 29,2014 34-20.1 

33-6.1 May 29,2014 Navigation-34 34-20.2 

33-6.2 May 29,2014 '34-0.1 Nov 25,2014 34-23.1 

33-7.1 May29, 2014 34-0.2 May 29,2014 34-23.2 

33-7.2 May 29,2014 34-1.1 May 29,2014 34-25.1 

33-8.1 May 29,2014 34-1.2 May 29,2014 34-25.2 

33-8.2 May 29,2014 34-2. I May 29,2014 34-26.1 

33-9.1 May 29,2014 34-2.2 May 29,2014 34-26.2 

33-9.2 May 29,2014 34-3.1 May 29, 2014 34-31.1 

33-10.1 May 29, 2014 34-3.2 May 29,2014 34-31.2 

33-10.2 May 29,2014 34-4.1 May 29,2014 34-32.1 

33-11.1 May 29,2014 34-4.2 May 29,2014 34-32.2 

33-11.2 May 29, 2014 34-5.1 May 29,2014 34-35.1 

DATE 

May 29,2014 

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'34-54.1 

'34-54.2 

'34-55.1 

'34-55.2 

34-98.1 

34-98.2 

34-99.1 

34-99.2 

MEL/CDL 

B-737 

LEP-0.5 

DATE 

May29, 2014 

May 29,2014 

May 29,2014 

May29, 2014 

May29, 2014 

May29, 2014 

May 29,2014 

May 29,2014 

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May29, 2014 

May 29,2014 

Nov 25,2014 

Nov 25, 2014 

Nov 25, 2014 

Nov 25,2014 

May 29,2014 

May 29,2014 

May 29, 2014 

May29, 2014 

Oxygen-35 

35-0.1 May 29,2014 

35-0.2 May 29,2014 

FAAApprovcd~:~~~~~~~O~ri£g~in~a~l~s~ig~n~e~d~an~d=da==te=d~bLy~G~l~e~nn~B~l~oo=m~q~u~is~t~~~~~~~~~ 

Principal Operations Inspector 

MEL/CDL 

B-737 

LEP-0.6 

PAGE NO. DATE 

35-2.1 May 29, 2014 

35-2.2 May 29,2014 

35-3.1 May 29,2014 

35-3.2 May 29,2014 

*35-4.1 Nov 25,2014 

35-4.2 Nov 25,2014 

35-5.1 May 29,2014 

35-5.2 May 29,2014 

35-6.1 May 29,2014 

35-6.2 May 29,2014 

Pneumatic-36 

36-0.1 May 29,2014 

36-0.2 May 29, 2014 

36-1.1 May 29,2014 

36-1.2 May 29,2014 

36-2.1 May 29,2014 

36-2.2 May 29,2014 

36-3.1 May 29,2014 

36-3.2 May 29,2014 

36-4.1 May 29,2014 

36-4.2 May 29,2014 

36-5.1 May 29,2014 

36-5.2 May 29,2014 

36-6.1 May 29, 2014 

36-6.2 May 29,2014 

36-8.1 May 29,2014 

36-8.2 May 29,2014 

36-9.1 May 29,2014 

36-9.2 May 29,2014 

Water/Waste- 38 

38-0.1 May 29,2014 

-sun country a1rl1nes 

List of Effective Pages Nov 25,2014 

PAGE NO. DATE PAGE NO. DATE PAGE NO. DATE 

38-0.2 May29, 2014 49-7.2 May 29,2014 52-17.4 May 29,2014 

38-1.1 May 29,2014 49-8.1 May 29,2014 52-18.1 May 29,2014 

38-1.2 May 29,2014 49-8.2 May29, 2014 52-18.2 May 29,2014 

38-2.1 May 29,2014 49-9.1 May 29,2014 52-20.1 May29, 2014 

38-2.2 May 29,2014 49-9.2 May 29,2014 52-20.2 May29,2014 

Information Systems~46 49-12.1 May 29,2014 52-22.1 May 29,2014 

46-0.1 May 29,2014 49-12.2 May 29,2014 52-22.2 May 29, 2014 

46-0.2 May 29,2014 49-15.1 May29, 2014 52-23.1 May 29,2014 

46-1.1 May 29,2014 49-15.2 May 29,2014 52-23.2 May 29,2014 

46-1.2 May 29,2014 49-16.1 May 29,2014 Engine Fuel & Control-73 

46-1.3 May 29,2014 49-16.2 May29, 2014 73-0.1 May 29,2014 

46-1.4 May 29,2014 Doors-52 73-0.2 May 29,2014 

Iuert Gas System- 47 52-0.1 May29, 2014 *73-4.1 Nov 25,2014 

47-0.1 May 29,2014 52-0.2 May 29,2014 73-4.2 May 29,2014 

47-0.2 May 29,2014 52-1.1 May 29,2014 73-5.1 May29, 2014 

*47-1.1 Nov 25,2014 52-1.2 May29,2014 73-5.2 May 29,2014 

47-1.2 May29, 2014 52-3.1 May29, 2014 73-6.1 May 29, 2014 

Airborne Auxiliary 

52-3.2 May29, 2014 73-6.2 May 29,2014 

Power-49 52-5.1 May29, 2014 73-10.1 May 29,2014 

49-0.1 May 29,2014 52-5.2 May29, 2014 73-10.2 May 29,2014 

49-0.2 May29,2014 52-6.1 May 29,2014 73-11.1 May29, 2014 

49-1.1 May 29,2014 52-6.2 May 29,2014 73-11.2 May29, 2014 

49-1.2 May 29,2014 52-7.1 May29, 2014 lgnition-74 

49-2.1 May 29,2014 52-7.2 May29, 2014 74-0.1 May 29,2014 

49-2.2 May 29,2014 52-9.1 May29, 2014 74-0.2 May 29,2014 

49-4.1 May29, 2014 52-9.2 May29, 2014 74-1.1 May 29,2014 

49-4.2 May 29,2014 52-15.1 May 29,2014 '74-1.2 Nov25,2014 

49-5.1 May 29,2014 52-15.2 May 29,2014 Engine Indicating-77 

49-5.2 May 29,2014 52-17.1 May29, 2014 

77-0.1 May29, 2014 

49-6.1 May29, 2014 52-17.2 May 29,2014 

77-0.2 May29, 2014 

49-6.2 May 29,2014 52-17.3 May 29,2014 

77-2.1 May 29,2014 

49-7.1 May 29,2014 

FAAApproved~=------------~O~r~igzi~n=al~s~i~gi~1e~d:~an~d~d~ffi~e~d~b~y_G~Ie~nn~B~Io~o~rn~qlu~i=st~--------------· 

Principal Operations Inspector 
sun country a!n111es 

Nov 25,2014 List of Effective Pages 

PAGE NO. DATE 

-

PAGE NO. DATE 

77-2.2 May 29, 2014 30·1 0-1.1 May 29, 2014 

77·5.1 May 29,2014 30·1 0-1.2 May 29,2014 

77·5.2 May 29,2014 Table of Contents Landing Gear~ 32 

77·9.1 May 29,2014 CDL·O·O.l May 29,2014 32·0·0.1 May 29,2014 

77-9.2 May 29,2014 CDL·0·0.2 May 29,2014 32-0·0.2 May 29,2014 

Exhaust-78 General 32-10·2.1 May 29,2014 

78·0.1 May 29,2014 CDL-1.1 May 29,2014 32·10·2.2 May 29,2014 

78·0.2 May 29,2014 CDL-1.2 May 29,2014 32-10·3.1 May 29,2014 

78·1.1 May 29,2014 Air conditioning- 21 

32·10·3.2 May29, 2014 

78-1.2 May 29,2014 

21·0·0.1 

32·10·4.1 

May 29,2014 

May 29,2014 

78·7.1 May 29,2014 32·1 0·4.2 May 29,2014 

21·0·0.2 May 29,2014 

78·7.2 May 20,2014 

21·5J.l.l 

32·10·5.1 

May 29,2014 

May 29,2014 

Oil-79 32-10-5.2 May 29,2014 

21-51-1.2 May 29,2014 

79·0.1 May 29,2014 32-10-6.1 May 29,2014 

21·51·2.1 May 29,2014 

79·0.2 May 29,2014 32·10·6.2 May 29,2014 

21·51·2.2 May 29,2014 

79·1.1 May 29,2014 32-10·7.1 May29, 2014 

Communication - 23 

79·1.2 May 29,2014 32-10· 7.2 May29, 2014 

23·0·0.1 May 29,2014 

79·2.1 May 29,2014 32-10-8.1 May 29,2014 

23·0·0.2 May 29,2014 

79·2.2 May 29,2014 32·1 0·8.2 May 29,2014 

23-60-1.1 May 29,2014 

79·4.1 May 29,2014 32-41·2.1 May29, 2014 

23·60-1.2 May 29,2014 

79·4.2 May 29,2014 32-41·2.2 May 29,2014 

23·61·1.1 May 29,2014 

Starting-SO 32-41·3.1 May 29,2014 

23·6J.l.2 May 29,2014 32·41·3.2 May 29,2014 

80·0.1 May 29,2014 Fuel· 28 

80-0.2 May 29,2014 Lights· 33 

28·0·0.1 May 29,2014 

80-1.1 May 29,2014 33·0·0.1 May29, 2014 

28·0·0.2 May 29,2014 

80-1.2 May 29,2014 33·0·0.2 May 29,2014 

28·16·1.1 May 29,2014 

80·2.1 May 29,2014 33-40-1.1 May 29,2014 

28-16·1.2 May 29,2014 

80-2.2 May 29,2014 33-40-1.2 May 29,2014 

Ice & Rain Protection- 30 33-40·2.1 May29, 2014 80·3.1 May 29,2014 

30·0·0.1 May 29, 2014 33-40-2.2 May 29,2014 80·3.2 May 29,2014 

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MELjCDL 

B-T3T 

LEP-0.7 

DATE 

May 29,2014 

May 29,2014 

May 29,2014 

May29, 2014 

May29,2014 

May 29,2014 

May 29,2014 

May 29,2014 

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Water/Waste- 38 

38·0·0.1 May 29,2014 

38·0-0.2 May 29,2014 

38-17·1.1 May 29,2014 

38·17-1.2 May29, 2014 

Auxiliary Power Unit- 49 

49·0·0.1 May 29,2014 

49·0·0.2 May29, 2014 

49-15·1.1 May29, 2014 

49-15·1.2 May29, 2014 

Doors- 52 

52·0·0.1 May 29,2014 

52·0·0.2 May 29,2014 

52·10-1.1 May 29,2014 

52·10·1.2 May 29,2014 

52-40·6.1 May 29,2014 

52·40·6.2 May29, 2014 

52-40·8.1 May 29,2014 

52·40·8.2 May 29,2014 

52-40·9.1 May 29,2014 

52-40·9.2 May29,2014 

52-40-10.1 May 29,2014 

FAAApproved~:~----------~O~ri~g~in~a~l~si~·g~n~e~d~a~n~d~d~a~te~d~b~y~G~l~enn~~D~lo~o~m~q~ut~·s~t ________________ __ 

Principal Operations Inspector 
MEL/CDL 

B-737 

LEP-0.8 

PAGE NO. DATE 

52-40-10.2 May29, 2014 

Stabilizers -55 

55-0-0.1 May 29,2014 

55-0-0.2 May 29,2014 

55-10-1.1 May 29,2014 

55-10-1.2 May 29,2014 

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Wings- 57 

*57-0-0.1 Nov 25,2014 

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57-30-8.1 May 29,2014 

List of Effective Pages 

PAGE NO. DATE PAGE NO. DATE 

57-30-8.2 May 29,2014 57-53-5.2 May 29,2014 

57-31-1.1 Nov 25,2014 57-53-6.1 May 29, 2014 

*57-31-1.2 Nov 25,2014 57-53-6.2 May 29,2014 

57-41-4.1 May 29,2014 57-53-7.1 May 29,2014 

57-41-4.2 May 29,2014 57-53-7.2 May 29,2014 

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57-41-13.2 May 29,2014 57-54-8.2 May 29,2014 

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57-51-1.2 May29, 2014 57-54-9.2 May 29,2014 

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57-53-3.2 May 29,2014 57-54-10.2 May 29,2014 

57-53-5.1 May 29,2014 57-71-1.1 May 29,2014 

FAA Approvedcc: ______ _.cOccr"'ig"'i""n"'alc.:~igned and dated by Glenn Bloomquist 

Principal Operations Inspector 

Nov 25,2014 

PAGE NO. DATE 

57-71-1.2 May 29,2014 

Exhaust -78 

57-0-0.1 May 29,2014 

57-0-0.2 May 29,2014 

78-30-1.1 May 29,2014 

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78-32-2.2 May 29,2014 
$sun cou~try dll"llllSS 

Nov 25,2014 

General 

Introduction 

MELjCDL 

B-T3T 

1-0.1 

Sun Country Airlines (SCA) has established policies and practices in accordance with 14 CFR 

121.628 and Operations Specification D095 for the use of the Minimum Equipment List (MEL) and 

the Configuration Deviation List (CDL). This manual interfaces with other Sun Country Airlines departments and manuals, including: 

SCA General Maintenance Manual 

SCA Flight Operations Manual 

14 Code of Federal Regulations (CFRs) 

SCA has also established an amplified MELICDL which is an extension of the Master MEL as published by the Flight Operations Evaluation Board (FOEB), and the CDL as published by Boeing Corporation. The amplified MELICDL published by SCA is in compliance with, or is in some cases, 

more restrictive than the information from which it is derived. 

The established policies and practices govern the dispatch of an aircraft with certain equipment either inoperative or missing. Approvals presented herein have been prepared to meet requirements of 

current 14 CFRs and are applicable to the 737 aircraft operated by SCA. Compliance with the policies and practices stated in this manual is mandatory. 

Approvals 

The approval signatures below grant Sun Country Airlines authorization to utilize SCA Revision 42, 

737 MELICDL in operations of such aircraft. Items within this MEL/CDL are no less restrictive 

than the FAA Approved MMEL, revision 56, dated November 19,2012 and include Boeing Dispatch Deviations Guide (DDG) Revision 51, dated November 30, 2012. 

Approved: 

Original signed and dated by: 

Duane Franklund 

SCA, Director QC 

Kevin Kaiser Glenn Bloomquist 

SCA, Sr. Director of Flight Opera- FAA, POI 

tions 
MEL/CDL 

B-T3T 

1-0.2 Introduction 

Intentionally 

Blank 

-sun country airlines 

May 29,2014 

country airlines 

Nov 25,2014 

General 

Equipment Addendum 

This equipment addendum is intended to provide a common location for Sun Country Airlines 737 MELICDL users to id

installed equipment by aircraft registration number. "Yes" indicates that the system or item is installed. "Yes (#)" indicate

of systems or items is installed. "No" indicates that the system or item is not installed. 

B737-700 

EQUIPMENT ADDENDUM 

MEL Item 710SY 711SY 712SY 713SY 714SY 715SY 716SY 

23-3-a 

Yes Yes No No No No Yes 

#3VHF 23-3-1 

VHFComm No No Yes (2) Yes (2) No No No 

Control Pnl 

23-3-2 

Yes (3) Yes (3) No No Yes (3) Yes (3) Yes (3) 

Radio Tuning Pnl 

23-11 

HF Yes (1) Yes (1) Yes (1) Yes (1) No No Yes (2) Communication 

Systems 

27-20 Speed 

Brake Load 

Alleviation Yes Yes No No Yes Yes Yes 

System (Winglets 

Installed) 

28-2-1 

No No No No No No No 

UFI 

28-3-2-a Auto No Yes No No Yes Yes No Shutoff 

28-7-4 

No Yes No No Yes Yes No 

SB 737-28A1206 

33-11 Single 

Navigation Lights Dual Dual Dual Dual Single (L) Dual 

Dual (R) 
MEL/CDL 

B-T3T 

4-0.2 

MEL Item 

33-19-1 

Escape Path 

Lighting 

34-15-4 

Autotilt/MultiScan Radar 

46-1-7 

Electronic Flight 

Bag 

B737-800 

MEL Item 

23-3-a 

#3 VHF 

23-3-1 

VHFComm 

Control Pnl 

23-3-2 

Radio Tuning Pnl 

23-11 

HFComms 

7IOSY 

Incandescent 

Yes 

Class 3 

SOISY 

Yes 

No 

Yes (3) 

Yes (2) 

EQUIPMENT ADDENDUM 

711SY 712SY 713SY 714SY 

Photolu- Photolu- Photolu- Incandes- mines- mines- minescent 

cent cent cent 

Yes No No Yes 

Class 3 Class 3 Class 3 Class I 

S04SY SOSSY SOSSY S09SY 

Yes Yes Yes Yes 

No No No No 

Yes (3) Yes (3) Yes (3) Yes (3) Yes (2) Yes (2) Yes (2) Yes (2) 

Equipment Addendum 

715SY 716SY 

Photolu- Photolumines- minescent cent Strips 

Yes Yes 

Class 3 Class 3 

EQUIPMENT ADDENDUM 

SI3SY SI4SY SISSY SI6SY 

No Yes Yes Yes 

Yes (2) No No Yes (2) 

No Yes (3) Yes (3) No 

Yes(!) Yes (2) Yes (2) Yes(!) 

SI7SY SISSY SI9SY 

Yes Yes Yes 

No No No 

Yes (2) Yes (3) Yes (3) Yes (2) Yes (2) Yes(!) 

*
4ltsun country a1rilnes 

Nov 25,2014 

MEL Item 801SY 804SY 

27-20 Speed 

Brake Load 

Alleviation Yes No 

System (Winglets 

Installed) 

28-2 UFI Yes Yes 

28-3-2-a Auto No No Shutoff 

28-7-4 

No No 

SB 737-28Al206 

33-11 

Navigation Dual Dual 

Lights 

33-19-1 

Inc an- IncanEscape Path descent descent 

Lighting 

34-15-4 

Autotilt/Multi- Yes Yes 

Scan Radar 

46-1-7 

Electronic Flight Class 3 Class 3 

Bag 

805SY 

No 

Yes 

No 

No 

Dual 

fucandescent 

Yes 

Class 3 

Equipment Addendum 

EQUIPMENT ADDENDUM 

808SY 809SY 813SY 814SY 815SY 

No No No No No 

No No Yes Yes No 

Yes Yes No No No 

Yes Yes No No No 

Dual Dual Dual Dual Dual 

Photolu- Photolu- Photolumines- In can- In can- mines- mines- descent descent 

cent cent cent 

Yes Yes Yes Yes Yes 

Class 1 Class 3 Class 3 Class 3 Class 3 

816SY 817SY 818SY 819SY 

No No No No 

Yes Yes No No 

No No Yes Yes 

No Yes Yes Yes 

Dual Dual Dual Dual 

Photolu- Seat Photolu- Photolu

mines- Mounted mines- minescent LED cent cent 

No Yes Yes Yes 

Class 3 Class 3 Class 3 Class 1 
'<!; 

0 

' "'" 
sun country airlines 

Nov 25,2014 

Communications-23 

Table of Contents 

MELjCDL 

B-737 

23-0.1 

23-1 Flight Deck Speaker System .................................................................................. 23-1.1 

23-2 Passenger Address System ..................................................................................... 23-2.1 

23-3 Communications Systems - VHF .......................................................................... 23-3.1 

23-4 Crewmember Interphone System ......................................................................... 23-4.1 

23-6 Selective Call System (SELCAL) .......................................................................... 23-6.1 

23-9 A CARS/Printer System ......................................................................................... 23-9.1 

23-10 Cockpit Voice Recorder System (CVR) ........................................................... 23-10.1 

23-11 High Frequency Communication Systems (HF) .............................................. 23-11.1 

23-12 Emergency Locator Transmitter (ELT) ........................................................... 23-12.1 

23-14 Flight Deck Headsets Earphones/Headphones and Boom Microphones ...... 23-14.1 

23-15 Pre-recorded Passenger Announcement System ............................................. 23-15.1 

23-16 Pnsh-To-Talk (PTT) Switches ........................................................................... 23-16.1 

23-17 Flight Deck Hand Microphones ........................................................................ 23-17.1 

23-18 Satellite Communication System (SATCOM) ................................................. 23-18.1 

23-19 Alerting System (AudioNisual) ........................................................................ 23-19.1 

23-20 Handset Systems ................................................................................................. 23-20.1 

23-21 Electronic Visual Surveillance Systems ............................................................ 23-21.1 

23-23 Multipurpose Interactive Display Unit (MIDU) .............................................. 23-23.1 

23-26 Avionica secureLINK Airborne Wireless Router (STC03151AT) ................ 23-26.1 

23-27 Data Link Communication ................................................................................ 23-27.1 

MEL/CDL 

B-737 

23-0.2 Table of Contents 

Intentionally 

Blank 

country airlines 

May 29,2014 
-sun country awlrnes 

Nov 25,2014 Communications 

MEL/CDL 

B-T3T 

23-10.1 

23-10 Cockpit Voice Recorder System (CVR) 

SYSTEM INTV QUANTITY F/C REMARKS OR EXCEPTIONS 

INSTL/RQD 

23-10-1 A 1 0 y May be inoperative provided: 

Aircraft with- a) Flight Data Recorder (FDR) operates normalout Recorder ly, and 

Independent b) Repairs are made within three flight days. 

Power Supply 

(RIPS) 

23-10-2 A I 0 y (M) May be inoperative provided: 

Aircraft with a) Flight Data Recorder (FOR) operates normalRecorder In- ly, 

dependent b) RIPS circuit breaker is pulled and collared, 

Power Supply c) A 15 minute interval after pulling of the c/b is 

(RIPS) achieved before departure, and 

(N820SY and d) Repairs are made within three days. 

N821SY on- NOTE: CVR is inoperative with the RIPS c/b pulled ly) and collared. 

23-10-2-a c 1 0 N (M) May be inoperative provided: 

Recorder In- a) CVR operates normally, and 

dependent b) RIPS battery is removed. 

Power Supply 

(RIPS) 

(N820SY and 

N821SY only) 

PLACARD 

As appropriate. 

MAINTENANCE CMl 

For item 23-10-2, deactivate RIPS (AMM 23-00-00/901): 

I. Open and collar RIPS circuit breaker. 

For item 23-10-2-a, remove RIPS battery (AMM 23-00-00/901): 

1. Remove battery from RIPS. 

2. Cover battery pack connector on the RIPS charger assembly with an electrical connector cap. 

3. Secure electrical connector cap to charger assembly with tape. 
MEL/CDL 

B-737 

23-10.2 Communications 

Intentionally 

Blank 

country airlines 

May 29,2014 
sun country airlines 

Nov 25,2014 Communications 

MEL/CDL 

B-737 

23-27.1 

23-27 Data Link Communication 

SYSTEM INTV QUANTITY F/C REMARKS OR EXCEPTIONS 

INSTL/RQD 

23-27-2 D 1 0 y May be inoperative. 

(N820SY/ NOTE:Any portion of the system that operates nor- N821SY on- mally may be used. ly) 

PLACARD 

As appropriate. 
NIEL/CDL 

B-737 

23-27.2 Communications 

Intentionally 

Blank 

country airlines 

Nov 25,2014 

country awl1nes 

MEL/CDL 

B-T3T 

Nov 25,2014 Equipment and Furnishings 25-6.1 

25-6 Passenger Seat(s) 

SYSTEM INTV QUANTITY F/C REMARKS OR EXCEPTIONS 

INSTL/RQD 

25-6 c - - y May be inoperative provided: 

a) Seat does not block an Emergency Exit, 

b) Seat does not restrict any passenger from access to the main aircraft aisle, and 

c) The affected seat(s) are blocked and placarded "DO NOT OCCUPY". 

NOTE 1 :A seat with an inoperative seat belt is considered inoperative. 

NOTE 2:Inoperative seat(s) do not affect the required number of Flight Attendants. 

NOTE 3:Affected seat(s) may include the seat(s) behind and/or adjacent outboard seats. 

25-6-1 D - - N (M) May be inoperative and seat occupied provided 

Recline seat is secured in the up-right position. 

Mechanism 

25-6-1-a D - - y May be inoperative and seat occupied provided seat 

Recline is immovable in the up-right position. 

Mechanism 

25-6-2-a D - - N (M) May be inoperative or missing and seat occupied 

Armrests with provided: 

Recline a) Arm rest does not block an Emergency Exit, 

Mechanism b) Arm rest does not restrict any passenger from 

access to the main aircraft aisle, and 

c) If armrest is missing, seat is secured in full 

upright position. 

NOTE: If the armrest has a de-lethalization pad built 

into the back side of the armrest, the row directly behind the missing or inoperative armrest must also be considered inoperative per 

MEL Item 25-6. 
MEL/CDL 

B-T3T 

sun country airlines 

25-6.2 Equipment and Furnishings Nov 25,2014 

25-6 Passenger Seat(s) 

SYSTEM INTV QUANTITY F/C REMARKS OR EXCEPTIONS 

INSTL/RQD 

25-6-2-b D - - y May be inoperative or missing and seat occupied 

Armrests provided: 

without Re- a) Arm rest does not block an Emergency Exit, 

cline Mecha- and 

nism b) Arm rest does not restrict any passenger from 

access to the main aircraft aisle. 

NOTE: If the armrest has a de-lethalization pad built 

into the back side of the armrest, the row directly behind the missing or inoperative armrest must also be considered inoperative per 

MEL Item 25-6. 

25-6-3 c - - y (O)May be inoperative provided: 

Underseat a) Baggage is not stowed under seat with inopBaggage Re- erative restraining bar, 

straining Bars b) Associated seat is placarded "DO NOT 

STOW BAGGAGE UNDER THIS SEAT", 

and 

c) Procedures are established to alert Cabin 

Crew of inoperative restraining bar. 

PLACARD 

As appropriate- DO NOT STOW BAGGAGE UNDER THIS SEAT or SEAT RECLINE INOP or 

DO NOT OCCUPY or ARM REST INOP. 

MAINTENANCE (M) 

Refer to the seat manufacturer's information for securing seat in upright position. 

For an inoperative underseat baggage restraining bar, ensure cabin crew is notified of the inoperative 

restraining bar and that baggage is not to be placed under the associated seat. 
I 

sun country airlines 

MELfCDL 

B-737 

Nov 25,2014 Equipment and Furnishings 25-10.1 

25-10 Non-Essential Equipment and Furnishing (NEF) 

SYSTEM INTV 

25-10 D 

25-10N --

PLACARD 

25-10: As appropriate 

25-1 ON: Not required 

NEF Information 

QUANTITY F/C REMARKS OR EXCEPTIONS 

INSTL/RQD 

- 0 y May be inoperative, damaged or missing. 

- 0 y May be inoperative, damaged or missing. This item 

does not require a placard and must be annotated on 

the MDDR Log Sheet located in the back of the Logbook binder. It will not be listed on the Dispatch Release. 

The NEF Approved List below lists the defects which have been analyzed and approved for deferral 

under MEL 25-10 or 25-1 ON. The NEF Rejected List lists items that have been analyzed and found 

to be not eligible for deferral under the NEF program. If the defect/equipment in question is not listed 

in either the NEF Approved List or the NEF Rejected List, Maintenance Control must analyze the 

defect per the NEF Process Flowchart in the Practices section of the MEL to determine whether it is 

eligible for deferral. 

See Non-Essential Equipment and Furnishings (NEF) Policies and Procedures, in the Practices section of the MEL for additional NEF details. 

NEF Approved List Qtems with N code are deferred nnder 25-lON) 

. 

Cabin General · .. · 

.· 

Item Code Repair Procedures/Remarks 

Interval . . . 

Boarding music N 120 days 

Bulkhead/sidewall literature pock- N 120 days Must not present hazard to passengers or 

ets dirty, worn, damaged or missing crew or impede emergency egress. One 

passenger information card must be available for each seat assembly. 

Cabin handset cradle damaged 120 days 

(handset fully operational) 

Cabin temperature sensor grill cover N 5 days 
MEL/CDL 

B-T3T 

country airlines 

25-10.2 Equipment and Furnishings Nov 25,2014 

Cabin General 

Item Code Repair Procedures/Remarks 

Interval 

Cabin vanity mirrors N 120 days Must not present hazard to passengers or 

crew. 

Carpet worn or tom N 120 days Must not present hazard to passengers or 

crew or impede emergency egress 

Coat hangers N 120 days 

CPR Mask (spare) 120 days Does not include masks from EEMK or 

EMGK 

Divider curtain tie backs damaged, 120 days (M) Secure curtain in fully open position 

tom or missing so as not to impede emergency egress or 

remove curtain and stow in closet. 

Divider curtain snaps broken or N 120 days 

missing 

Divider curtain tom or missing N 120 days 

Door liner cracked or damaged N 120 days Must not present hazard to passengers or 

crew or impede emergency egress. 

Door slide bustle dirty or scuffed N 120 days 

Door slide bustle minor damage N 120 days Must not present hazard to passengers or 

crew or impede emergency egress. 

Door slide pressure gauge lens N 120 days Must not present hazard to passengers or 

cracked crew or impede emergency egress. Pressure must be readable. 

Emergency Services Kit (ESK) 10 days Place placard on checklist inside ESK 

Floor covering worn or tom N 120 days Must not present hazard to passengers or 

crew or impede emergency egress 

Gap seal (decorative foam around N 120 days 

bulkheads, galleys, lavatories) missing or loose 

Ground service electrical outlet cov- N 120 days 

ers damaged or missing 

Jumpseat cover fabric tom N 120 days 

Lavatory occupied lights 120 days 

Magazine rack latch/lock broken N 120 days 

Passenger Entertainment System 120 days --
couqtry a1r11nes 

MEL/CDL 

B-T3T 

Nov 25,2014 Equipment and Furnishings 25-10.3 

Cabin General 

Item Code Repair Procedures/Remarks 

Interval . 

Safety demo equipment - safety 120 days One complete set must still be onboard the 

belt, life vest and oxygen mask airplane 

Seat number placards N 120 days 

Seat track covers loose, damaged or 120 days (M) Any exposed wiring must be protectmissmg ed. Must not present hazard to passengers 

or crew or impede emergency egress. 

Flight Crew may not defer if wiring is exposed. 

Sharps container 120 days 

Sidewall panel soiledldirty N 120 days 

Sidewall panel damaged N 120 days 

Stowage bin snubber damaged or N 120 days 

missmg 

Stowage bin latch bezel trim dam- N 120 days Must not present hazard to passengers or 

aged or missing crew 

Stowage bin exterior fmish dirty/ N 120 days 

worn/damagedlchipped 

Wall covering torn, damaged or N 120 days Must not present hazard to passengers or 

missing crew or impede emergency egress. 

Window crazedldirty N 120 days Does not apply to entry/service doors 

Window moisture between panes N 120 days Does not apply to entry/service doors 

Window trim missing or loose N 120 days Must not present hazard to passengers or 

crew or impede emergency egress. 

Seats ..... .. · . 

Item Code Repair Procedures/Remarks 

. Interval ·· . 

Flight attendant seat gasper vent in- N 120 days 

operative 

Headrest damaged N 120 days Must not present hazard to passengers or 

crew or impede emergency egress. 

MEL/CDL 

B-737 

-sun country airlines 

25-10.4 Equipment and Furnishings Nov 25,2014 

Seats 

Item Code Repair Procedures/Remarks 

Interval ·. 

Life Vest pouch worn/soiled N 120 days Must not be torn and velcro must be secured 

Passenger information cards dam- N 120 days At least one is required per seat assembly 

aged or missing 

PSU air vent inoperative N 120 days 

PSU attendant call inoperative N 120 days 

PSU panel minor damage, soiled/ N 120 days 

dirty (PSU operates normally) 

Reading light lens/covers loose or N 120 days Must not present hazard to passengers or 

damaged, (light operates normally) crew or impede emergency egress. 

Reading lights need adjustment N 120 days 

Seat ashtray missing N 120 days 

Seat ashtray will not open or close N 120 days 

Seat back cover soiled/dirty N 120 days 

Seat back cover torn/worn N 120 days 

Seat belt soiled/dirty N 120 days 

Seat bottom cushion soiled/dirty N 120 days 

Seat bottom cushion tom/worn N 120 days 

Seat back pocket sags or spring bro- N 120 days 

ken 

Seat belt extensions missing N 120 days 

Seat trim items, anmest pads, cov- N 120 days Must not present hazard to passengers or 

ers crew or impede emergency egress. If the 

annrest has a de-lethalization pad, refer to 

MEL25-6-2-a or 25-6-2-b. 

Tray table - Damaged table/latch N 120 days Must not present hazard to passengers or 

crew or impede emergency egress. 

Tray table needs adjustment N 120 days Must not present hazard to passengers or 

crew or impede emergency egress. 

Tray table soiled/dirty N 120 days 
country airlines 

MEL/CDL 

B-737 

Nov 25, 2014 Equipment and Furnishings 25-10.5 

Galleys 

Item Code Repair Procedures/Remarks 

Interval 

Coffee maker hot plate inoperative 120 days (M) Pull and secure associated circuit 

breaker 

Coffee maker hot plate light inoper- 120 days (M) Pull and secure associated circuit 

ative breaker 

Coffee maker inoperative, over- 120 days (M) Pull and secure associated circuit 

flowing or C/B popping breaker 

Coffee maker leaking 120 days (M) Isolate leak by shutting off associated 

galley water supply. Pull and secure associated circuit breaker. 

Coffee maker light inoperative 120 days (M) Pull and secure associated circuit 

breaker 

Coffee maker skillet missing N 120 days 

Counter shelf damaged 120 days (M) Secure shelf if it is loose. Install "Do 

not use" placard on shelf. 

Counter shelf stuck N 120 days Must not present hazard to passengers or 

crew or impede emergency egress. 

Galley drain drains slowly N 120 days 

Galley drain noisy N 120 days 

Galley floor covering worn/tom/ N 120 days Must not present hazard to passengers or 

buckled crew or impede emergency egress. 

Galley gasper vents inoperative N 120 days 

Galley storage compartment lock N 120 days Door latches must still be operational 

broken 

Galley storage compartment minor N 120 days 

damage 

Galley storage compartment hold N 120 days 

open rods 

Galley storage compartment will N 120 days 

not open 

Galley water spigots will not tum on 120 days 

Oven door won't open 120 days 
MEL/CDL 

B-T3T 

$-sun country atrltnes 

25-10.6 Equipment and Furnishings Nov 25,2014 

Galleys 

Item Code Repair Procedures/Remarks 

Interval 

Ovens and controls 120 days (M) Pull and secure associated circuit 

breaker. 

PSK missing N 120 days 

Waste container pull handle N 120 days 

Work light N 120 days 

Work table damaged 120 days 

Work table will not stay upright 120 days Must not present hazard to passengers or 

crew or impede emergency egress . 

Lava.tories ·.·. ·.·. .. : ... • ,< . 

: 

... . • . 

· .. 

. :··. 

Prilcedrires/Remarks . 

Item < Code Repair ' 

. . •• ·.·.·. , .•.. '.: .. ·. Inte~~l · .. ·•· ··•··· .. , .•. .. · ........... . ·. ·.·.· . .•. · .. ·. .•... :· .... ,:. ... . ·~· 

Amenity holder missing or broken N 120 days 

Kleenex holder missing or broken N 120 days 

Lavatory air grill cover missing or N 120 days 

broken 

Lavatory deodorizer holder missing N 120 days 

or broken 

Lavatory diaper changing table in- 120 days (M) If table is damaged, verify that it is 

operative secure. Install "Do not use" placard on tab1e. 

Lavatory door hard to open or close N 120 days 

Lavatory door interior ashtray miss- N 120 days 

mg 

Lavatory door lock inoperative 120 days (M) (0) Lavatory door locks may be inoperative provided lavatory door latches 

closed. 

Lavatory door Occupied display N 120 days 

Lavatory door spring inoperative N 120 days 

Lavatory drain drains slowly N 120 days 

Lavatory drain noisy N 120 days 
sun country airlines 

MELjCDL 

B-737 

Nov 25,2014 Equipment and Furnishings 25-10.7 

Lavatories 

Item Code Repair Procedures/Remarks 

Interval . 

Lavatory gasper vents inoperative N 120 days 

Lavatory hot or cold faucet indica- N 120 days 

tors missing or broken 

Lavatory interior wall trim/cover- N 120 days 

ings damaged 

Lavatory mirror cracked N 120 days Must not present hazard to passengers or 

crew 

Lavatory paper towel holders bra- N 120 days 

ken or missing 

Lavatory passenger assist handles N 120 days 

broken or missing 

Lavatory attendant call inoperative N 120 days 

Lavatory sanitizer dispensers bra- N 120 days 

ken or missing 

Lavatory sink stopper inoperative N 120 days 

Lavatory spigot/faucet will not tum 120 days 

on 

Lavatory vanity lights inoperative N 120 days 

Lavatory waste container door will N 120 days 

not open 

Lavatory water dispenser drain N 120 days 

clogged 

Lavatory water heater inoperative 120 days (M) If applicable, position heater switch 

to OFF. Pull and secure associated circuit 

breaker. 

Shroud Upper Collar N 120 days 

Toilet bowl strong odor N 120 days 

Toilet paper holder broken N 120 days 

Toilet paper holder missing N 120 days 

Toilet seat cover damaged 120 days 
MELjCDL 

B-737 

sun country airlines 

25-10.8 Equipment and Furnishings Nov 25,2014 

Flight Deck 

Item Code Repair Procedures/Remarks 

Interval 

CDU Line Select Key rubber cap N 120 days Line Select Key must be functional 

miSS JUg 

Flight deck access compartment N 120 days (M) Verify that door can still be secured 

latches missing/inoperative closed with latches. If not, remove contents and secure door closed. 

Flight deck ashtrays N 120 days 

Flight deck coat or hat hooks N 120 days 

Flight deck cup holder or insert N 120 days (M) If missing, inspect open cavity to endamaged or missing sure there are no foreign objects present. 

Use suitable tape to secure openmg 

closed. 

Flight deck door hold-open device N 120 days 

Flight deck gasper vents N 120 days 

Flight deck knobs loose (but fully N 120 days 

functional) 

Flight deck seat bottom cushion soft N 120 days 

or flat 

Flight deck seat covers soiled or N 120 days 

worn 

Flight deck spring clip (document N 120 days 

holder) inoperative or missing 

Flight deck storage compartments I N 120 days (M) Verify that compartment door closes 

doors inoperative properly. If not, remove contents and secure door closed. 

Flight deck sunshades or clips darn- N 120 days 

aged, inoperative or missing 

Flight deck vanity mirror cracked N 120 days Must not present a hazard to crew 

Instrument panel foot tread trim N 120 days 

worn 

Landing Gear lever knob cracked N 120 days Knob must remain attached and not present a hazard to crew. 

Nav I Comm panel frequency win- N 120 days Crack must not hinder visibility of fredow glass cracked quency or present a hazard to flight crew. 

$-sun country a1r11nes 

MELjCDL 

B-737 

Nov 25,2014 Equipment and Furnishings 25-10.9 

Flight Deck 

Item Code Repair Procedures/Remarks 

Interval . 

PI A Handset hinged mount bracket N 120 days Handset must be stowed. 

broken or damaged 

Spare bulb kit and contents incom- N 120 days 

plete or missing 

Trim - seat, glareshield, walls, etc. N 120 days Must not present hazard to crew or imdamaged or worn pede emergency egress 

Window clip holder damaged or N 120 days Must not present a hazard to crew 

mtssmg 

Window drain hose missing N 120 days 

Yoke chart clip damaged or inoper- N 120 days 

ative 

Yoke checklist reminder indicator N 120 days 

missing 

Yoke thumb wheel reminder inop- N 120 days 

erative 

Ge[leral . . ·.·· . 

I . I 

Item Code .Repair Procedures/Remarks .· 

. ·· · . 

Inte.rv:H ... ... 

Non-required exterior placards - de- N 120 days 

graded but legible 

Non-required exterior placards - N 120 days 

missing or illegible 

Engine cowl hold open rod N 120 days 

Cargo Compartment Insulation N 120 days 

Blanket tom or missing 

GPU Door latch return spring bro- N 120 days Door must close and secure normally 

ken or missing 
MEL/CDL 

B-737 

25-10.10 

Service Bays 

Equipment and Furnishings 

country airlines 

Nov 25,2014 

Item Code Repair Procedures/Remarks 

Interval 

Compartment light lens cracked N 120 days 

Dust cover caps, chains or lanyards N 120 days 

Hold open rods or lanyards N 120 days 

Hold open rod or lanyard storage de- N 120 days 

ViCe 

NEF Rejected List 

The following items are not eligible for deferral under the Approved NEF Program. 

1. Exterior lavatory ashtrays 

2. Onboard wheelchair 

3. Crew safety harness worn or frayed 

4. Ll, L2, Rl, R2 door assist handles broken, missing, loose 

5. EFB screen cracked 

6. Aileron trim switch guard (tab) broken/damaged/missing 

7. Elevator trim switch guard broken/damaged/missing (on yoke) 
iltsun country atrltnes 

Nov 25,2014 Flight Controls 

MELJCDL 

B-T3T 

27-4.1. 

27-4 Leading Edge Flap/Slat Position Light Systems 

SYSTEM INTV QUANTITY F/C REMARKS OR EXCEPTIONS 

INSTL/RQD 

27-4-a c 1 0 y Aft overhead panel LE Devices Annunciator panel 

Aft System may be inoperative provided forward panel lights operate normally. 

27-4-2 c 1 0 N (M) Forward panel lights may be inoperative providForward Sys- ed: 

tern a) Aft overhead panel LE Devices Annunciator 

panel operates normally and is used to verify 

proper LE Device position, and 

b) A placard is installed to indicate proper positions for flap configuration in use. 

27-4-6 c 8 7 N (M) (O)Indication lights on the forward panel and in 

Leading Edge addition indication lights for one leading edge slat, exSlat Indica- cept for slats 4 and 5, on overhead annunciator panel 

tions may be inoperative provided: 

(-700) a) Normal operation is verified by the flight crew 

before each takeoff and landing, 

b) Maximum speed is limited to 300 KIAS at/below FL 200 or .65 Mach above FL 200, 

c) All remaining indications on the overhead annunciator panel operate normally, and 

d) Stall warning operation of both systems is verified to operate normally. 

e) A placard is installed to indicate proper positions for flap configuration in use. 

27-4-7 c 8 7 N (M) (O)Indication lights on the forward panel and in 

Leading Edge addition indication lights for one leading edge slat, exSlat Indica- cept for slats 3, 4, 5, and 6, on overhead annunciator 

tions panel may be inoperative provided: 

(-800) a) Normal operation is verified by the flight crew 

before each takeoff and landing, 

b) Maximum speed is limited to 300 KIAS at/below FL 200 or .65 Mach above FL 200, 

c) All remaining indications on the overhead annunciator panel operate normally, and 

d) Stall warning operation of both systems is verified to operate normally. 

e) A placard is installed to indicate proper positions for flap configuration in use. 
MELjCDL 

B-737 

27-4.2 Flight Controls 

sun country airlines 

Nov 25,2014 

NOTE: Associated wing illumination light may be required for verification of normal operation of 

the leading edge slats. 

PLACARD 

For inoperative forward panel lights, affected lights- INOP 

For inoperative annunciator panel, overhead annunciator panel- INOP 

For inoperative indicators for one slat on both panels, affected annunciator panel lights- INOP- VISUALLY CONFIRM POSITION 

MAINTENANCE (Ml 

MEL 27-4-2: FORWARD POSITION INDICATOR LIGHTS INOPERATIVE (AMM 27-00-00/ 

901): 

1. Cycle the flaps. 

2. Verity that the LE DEVICES annunciator panel (P5) operates normally during flap extension 

and retraction. 

NOTE: If an annunciator panel TRANSIT light fails to illuminate while the corresponding device is in motion, then this light must be considered inoperative. 

3. Remove the bulbs from the associated forward position indicator light(s) on the center instrument panel, P2. 

4. Use this data to make a placard and put it adjacent to the annunciator panel: 

All exceptN820SY/N821SY 

A. Flap positions 1 thru 5: 

1) All slats in EXT position. 

2) LE flaps extended. 

B. Flap positions 10 thru 40: 

1) All slats in FULL EXT position. 

2) LE flaps extended. 

N820SYIN821SY only 

A. Flap positions 1 thru 25: 

1) All slats in EXT position. 

2) LE flaps extended. 

B. Flap positions 30 and 40: 

1) All slats in FULL EXT position. 

2) LE flaps extended. 
sun country ' ,, a:nrnes 

Nov 25,2014 Flight Controls 

MEL/CDL 

B-T3T 

27-4.3 

MEL 27-4-6 or MEL 27-4-7: FORWARD POSITION INDICATOR LIGHTS INOPERATIVE 

AND ONE SLATS ANNUNCIATOR PANEL LIGHT INOPERATIVE (AMM 27-00-00/901): 

NOTE: For the -700, slat indications for slats 4 and 5 are not allowed to be inoperative due to the 

inability to visually verify their position from the flight deck For the -800, slat indications 

for slats 3, 4, 5 and 6 are not allowed to be inoperative due to the inability to visually verify 

their position from the flight deck 

L Cycle the flaps, 

2, Verify that the remaining LE DEVICES annunciator panel (P5) lights operate normally during 

flap extension and retraction. 

NOTE 1 :If an annunciator panel TRANSIT light fails to illuminate while the corresponding 

device is in motion, then this light must be considered inoperative, 

NOTE 2:This item is applicable to inoperative leading edge SLAT indications and not the 

leading edge FLAP indications on the LE DEVICES annunciator paneL Dispatch is 

not allowed if the LE DEVICES annunciator panel FLAP lights do not illuminate 

properly and the forward panellight(s) are inoperative, 

3. Remove the bulbs from the associated forward position indicator light(s) on the center instrument panel, P2. 

4. Use this data to make a placard and put it adjacent to the annunciator panel: 

All exceptN820SY/N821SY 

A. Flap positions 1 thru 5: 

1) All slats in EXT position. 

2) LE flaps extended. 

B. Flap positions 10 thru 40: 

1) All slats in FULL EXT position. 

2) LE flaps extended. 

N820SY/N821SY only 

A. Flap positions 1 thru 25: 

1) All slats in EXT position. 

2) LE flaps extended, 

B. Flap positions 30 and 40: 

1) All slats in FULL EXT position. 

2) LE flaps extended. 

5, Determine which TE flap position( s) causes the inoperative slat indication. 

NOTE: If faulty indication is intennittent or cannot be replicated on the ground, use FSEU 

BITE to determine if an FSEU input has been recently faulty, If FSEU BITE (Flight 

Leg 0) indicates fault message codes 27-81200 through 27-81223 or 27-81225 through 

MEL/CDL 

B-737 

27-4.4 Flight Controls 

sun country airlines 

Nov 25,2014 

27-81236, open and collar the Stall Warning Asymmetry Mode circuit breaker on the 

Pl8-2 Panel. IfFSIM BITE does not yield one of these fault codes because the fault 

indication light(s) flashes ON/OFF for an instant such that the fault does not latch, and 

the applicable slat can be confirmed to be stationary in the position where the intermittent indication was observed, then open and collar the Stall Warning Asymmetry Mode 

circuit breaker. 

6. Set flaps to the position which produces the faulty indication. 

7. Verify that the leading edge and trailing edge devices are in the correct position. 

8. Verify normal operation of both Stall Warning Systems: 

NOTE I: (All exceptN820SY/N821SY) If the inoperative slat indication occurs at more than 

one flap position, repeat the procedure to verify normal operation of both Stall Warning Systems at Flaps 0, Flaps I and Flaps 10. 

NOTE 2: (N820SY/N821SY only) If the inoperative slat indication occurs at more than one 

flap position, repeat the procedure to verify normal operation of both Stall Warning 

Systems at Flaps 0, Flaps I and Flaps 30. 

A. Verify that hydraulic system B pressure is between 2900 and 3100 psi. 

B. Push and hold STALL WARNING TEST NO. I and NO.2 switch on the stall warning 

test module (P5 Overhead Panel). 

C. Check that the control column stick shakers operate normally. 

D. If both stick shakers fail to operate normally, open and collar the Stall Warning Asymmetry Mode circuit breaker on the P 18-2 Panel if not already accomplished in step 5 above, 

and then repeat test in steps B and C. 

9. If the stick shaker tests are normal the airplane can be dispatched. 

OPERATIONS (0) 

MEL 27-4-6 or MEL 27-4-7: Forward position indicator lights inoperative and one SLATS annunciator panel light inoperative: 

I. Verify leading edge slat position for the inoperative indication before each takeoff and landing. 

2. Limit airspeed: 

A. At or below FL 200, limit airspeed to 300 KIAS. 

B. Above FL 200, limit airspeed to 0.65 Mach. 

C. Reference QRH, Performance Inflight Section, VREF table for information on maintaining minimum maneuvering speeds. 

3. Flight plan will be generated using "Leading Edge Slat" (LES) profile to account for speed restrictions. 

NOTE: With FMC update 10.7 or later, VNAV will limit the speed target to 230 KIAS unless speed 

intervention is used. 
country airlines 

MELJCDL 

B-737 

Nov 25,2014 Flight Controls 27-7.1 

27-7 Auto Speed Brake System 

SYSTEM INTV QUANTITY F/C 

INSTL/RQD 

REMARKS OR EXCEPTIONS 

27-7-1 c I 0 Y (M) (O)May be inoperative provided: 

(all except 

N820SY, 

N821SY) 

27-7-2 

(N820SY, 

N821SY only) 

PLACARD 

c I 0 y 

a) System is deactivated, 

b) Operations are conducted in accordance with 

AFM, and 

c) For aircraft with Blended Winglet with Speed 

Brake Load Alleviation System, the Speed 

Brake Load Alleviation System is considered 

inoperative. 

NOTE !:Refer to Equipment Addendum, item 27-20 

Speed Brake Load Alleviation System 

(Winglets Installed), to determine which aircraft have Speed Brake Load Alleviation System installed. 

NOTE 2:Aircraft with Speed Brake Load Alleviation 

System installed must also be dispatched using MEL 27-20 Speed Brake Load Alleviation 

System (Winglets Installed). 

(M) (O)May be inoperative provided: 

a) System is deactivated, 

b) Appropriate performance adjustments are applied, and 

c) For aircraft with Blended Winglet with Speed 

Brake Load Alleviation System, the Speed 

Brake Load Alleviation System is considered 

inoperative. 

NOTE:N820SY and N821 SY do not have Speed Brake 

Load Alleviation System installed. 

Speed brake control lever- AUTO SPD BRK INOP 

MAINTENANCE (M) 

For item 27-7-1: Prepare the airplane for flight with the auto speed brake system inoperative (AMM 

27-00-00190 1): 

I. Verify manual speed brake operation. 

2. Open and collar P6 panel circuit breaker FLIGHT CONTROL AUTO SPEED BRAKE. 

For item 27-7-2: Prepare the airplane for flight with the auto speed brake system inoperative (AMM 

27-00-001901 ): 
MEL/CDL 

B-737 

27-7.2 Flight Controls 

sun country airlines 

Nov 25,2014 

1. Verify manual speed brake operation. NOTE: Extend flaps prior to moving speed brake lever 

beyond FLIGHT DETENT position. 

2. Open and collar P6 panel circuit breaker FLIGHT CONTROL AUTO SPEED BRAKE. 

OPERATIONS (0) 

1. InOPS, select AUTO SPOILER SYSTEM: INOPERATIVE from the MEL input screen. This 

will account for the takeoff and landing performance penalties. 

2. Prior to takeoff, ensure that speed brake lever is in full down detent. 

3. Extend speedbrakes manually for rejected takeoff or landing. 

A. For rejected takeoff: 

1) Simultaneously close thrust levers, disengage the autothrottles and apply manual 

wheel brakes or verify operation of auto brakes. 

2) Manually raise SPEED BRAKE lever. 

3) Apply the maximum amount of reverse thrust consistent with conditions. 

B. For landing, use the SPEED BRAKE DO NOT ARM non-normal checklist 

4. The auto brakes may not disarm when the speed brake lever is stowed. Auto brakes may be disarmed by positioning AUTO BRAKE select switch to OFF, applying brakes manually or advancing the thrust levers. 
sun country airlines 

Nov 25,2014 Flight Controls 

MEL/CDL 

B-737 

27-8.1 

27-8 Flap Load Limiter System 

SYSTEM INTV QUANTITY F/C REMARKS OR EXCEPTIONS 

INSTL!RQD 

27-8-4 c 1 0 y (O)May be inoperative provided: 

(-700) a) Flaps are not extended beyond Flaps 30 at gross 

weights above 93,480 lb, and 

b) Flaps are not extended beyond Flaps 15 at gross 

weights above 104,403 lb. 

27-8-5 c I 0 y (O)May be inoperative provided: 

(-800) a) Flaps are not extended beyond Flaps 30 at gross 

weights above 93,995 Ib, and 

b) Flaps are not extended beyond Flaps 15 at gross 

weights above 104,875 lb. 

27-8-6 c 1 0 y (O)May be inoperative provided: 

(-800SFP) a) Flaps are not extended beyond Flaps 30 at gross 

(N820SY, weights above 95,800 lb, and 

N821SY on- b) Flaps are not extended beyond Flaps 15 at gross 

ly) weights above 105,000 lb, and 

c) Flaps are not extended beyond Flaps 10 at gross 

weights above 135,800 lb. 

PLACARD 

Flap handle and/or flap position indicator- LOAD LIMITER INOP- FLAPS ARE NOT TO BE EXTENDED BEYOND FLAPS 15/30 AS APPLICABLE. 

OPERATIONS CO) 

InOPS, select Flap Load Limiter: INOPERATIVE from the MEL input screen. This will force the 

Dispatch Landing calculations to be based on flaps I 5. 
NIEL/CDL 

B-T3T 

27-8.2 Flight Controls 

Intentionally 

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May 29,2014 
-sun country awl1nes 

Nov 25,2014 

Navigation-34 

Table of Contents 

MELjCDL 

B-T3T 

34-0.1 

34-1 Mach Indications .................................................................................................... 34-1.1 

34-2 Mach/Airspeed Warning Systems ......................................................................... 34-2.1 

34-3 Altimeter Vibrators - Standby Altimeter ............................................................. 34-3.1 

34-4 Static Air Temperature Indication ....................................................................... 34-4.1 

34-5 Total Air Temperature Indication ........................................................................ 34-5.1 

34-7 Standby Horizon Indicator .................................................................................... 34-7.1 

34-11 Non-Stabilized Magnetic Compass ................................................................... 34-11.1 

34-12 Flight Director Systems ...................................................................................... 34-12.1 

34-13 Distance Measuring Equipment Systems ......................................................... 34-13.1 

34-14 Marker Beacon Receiver System ...................................................................... 34-14.1 

34-15 Weather Radar ................................................................................................... 34-15.1 

34-16 Radio Compass Systems (ADF) ......................................................................... 34-16.1 

34-17 VHF Navigation Systems (YO RilLS) ............................................................... 34-17.1 

34-18 ATC Transponders and Automatic Altitude Reporting Systems .................. 34-18.1 

34-20 Radio Altimeter Systems .................................................................................... 34-20.1 

34-23 True Airspeed Indication ................................................................................... 34-23.1 

34-25 Altitude Alerting System .................................................................................... 34-25.1 

34-26 Enhanced Ground Proximity Warning System (EGPWS) ............................ 34-26.1 

34-31 Speed Cursor Remote Drive .............................................................................. 34-31.1 

34-32 Instrument Transfer Switching System ........................................................... 34-32.1 

34-35 Inertial Reference Systems (IRS) ...................................................................... 34-35.1 

34-36 Flight Management Computer System (FMCS) .............................................. 34-36.1 

34-37 Windshear Detection and Guidance Systems .................................................. 34-37.1 

34-38 Pitch Limit Indication (PLI) .............................................................................. 34-38.1 

34-40 Traffic Collision and Avoidance System (TCAS) ............................................ 34-40.1 

34-42 Radio Magnetic Indicators (RMI) - PFD/ND .................................................. 34-42.1 

34-43 Radio Height Alert ............................................................................................. 34-43.1 

34-45 Global Positioning System (GPS) ...................................................................... 34-45.1 

34-47 ILS Beam Deviation Lights ............................................................................... 34-47.1 

34-48 EFIS Control Panel ............................................................................................ 34-48.1 

34-49 Right IRS DC Power Supply System ................................................................ 34-49.1 

34-54 Integrated Standby Flight Display (ISFD) ....................................................... 34-54.1 

34-55 Vertical Situation Display (VSD) ...................................................................... 34-55.1 

34-98 ETOPS ................................................................................................................. 34-98.1 

34-99 RVSM .................................................................................................................. 34-99.1 
MEL/CDL 

B-737 

34-0.2 Table of Contents 

Intentionally 

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May 29,2014 
sun country airlines 

Nov 25,2014 Navigation 

MELjCDL 

B-737 

34-54.1 

34-54 Integrated Standby Flight Display (ISFD) 

SYSTEM INTV QUANTITY F/C REMARKS OR EXCEPTIONS 

INSTL/RQD 

34-54-1-a B 1 0 y May be inoperative provided: 

Attitude Dis- a) Operations are conducted in Day VMC only, 

play and 

b) Operations are not conducted into known or 

forecast over-the-top conditions. 

34-54-1-b D 1 0 y May be inoperative. 

ILS Indication 

34-54-1-c c 1 0 y May be inoperative. 

Heading Display 

34-54-1-d D 1 0 y May be inoperative provided operations do not require 

Metric Altim- its use. 

eter Display 

34-54-1-e c 1 0 y May be inoperative. 

Dedicated 

Battery 

PLACARD 

As appropriate. 
MELjCDL 

B-737 

34-54.2 Navigation 

Intentionally 

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Nov 25,2014 
ncountry airlines 

Nov 25;2014 Navigation 

MEL/CDL 

B·T3T 

34-55.1 

34-55 Vertical Situation Display (VSD) 

SYSTEM INTV QUANTITY F/C REMARKS OR EXCEPTIONS 

INSTL/RQD 

34-55 D 1 I o y May be inoperative. 

PLACARD 

As appropriate. 
MEL/CDL 

B-T3T 

34-55.2 Navigation 

Intentionally 

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country airlines 

Nov 25,2014 

country airlines 

Nov 25,2014 Oxygen 

MEL/CDL 

B-737 

35-4.1 

35-4 Portable Oxygen Dispensing Units (Bottle and Mask) 

SYSTEM INTV QUANTITY F/C REMARKS OR EXCEPTIONS 

INSTL/RQD 

35-4 D 7 3 y (M) Any in excess of those required may be unservice-

(-700) able or missing provided: 

a) Required distribution of serviceable bottles is 

maintained throughout aircraft by ensuring botties are equally divided between forward and 

aft cabin stowage areas (if the number of required bottles is odd, the odd bottle may be 

placed forward or aft), and 

b) Bottles not properly serviced are replaced, serviced or removed at the next available maintenance facility. 

35-4-1 D 8 4 y (M) Any in excess of those required may be unservice-

(-800 Non- able or missing provided: 

ETOPS and a) Required distribution of serviceable bottles is 

N820SY/ maintained throughout aircraft by ensuring botN821SY) ties are equally divided between forward and 

aft cabin stowage areas (if the number of required bottles is odd, the odd bottle may be 

placed forward or aft), and 

b) Bottles not properly serviced are replaced, serviced or removed at the next available maintenance facility. 

35-4-2 D 13 - y (M) (O)Any in excess of those required may be unser-

(-800 ETOPS viceable or missing provided: 

except a) Required distribution of serviceable bottles is 

N820SY/ maintained throughout aircraft by ensuring botN821SY) ties are equally divided between forward and 

aft cabin stowage areas (if the number of required bottles is odd, the odd bottle may be 

placed forward or aft), and 

b) Bottles not properly serviced are replaced, serviced or removed at the next available maintenance facility. 

c) For operations other than Greenland, the minimum required quantity is four ( 4) bottles. 

d) For Greenland Operations, minimum oxygen 

bottle quantities are based upon the passenger 

count. See Operations (0) procedure below. 

NOTE !:Any unit with less than 1000 psi is considered unserviceable for dispatch. Any unit with 
MEL/CDL 

B-737 

sun country airlines 

35-4.2 Oxygen Nov 25,2014 

more than 1000 psi, but less than 1500 psi, should be placed on MTI. 

NOTE 2:The use of an oxygen mask renders the associated unit unserviceable for dispatch. 

PLACARD 

As appropriate 

MAINTENANCE (M) 

l. Place the SCM-14 placard on the face of the pressure gauge and remove the mask. 

2. Ensure required distribution of serviceable units is maintained throughout the airplane by ensuring bottles are equally divided between forward and aft cabin stowage areas (if the number 

of required bottles is odd, the odd bottle may be placed forward or aft). Stowage areas may 

include floor mounting stowage units (doghouses), overhead bins, etc. 

3. Until an unserviceable bottle can be removed from the airplane at the next available maintenance facility, it must be stowed in a location where it will not be used by mistake and associated locator placards for inoperative units must be removed or obscured. 

OPERATIONS (0) 

This item is applicable only to aircraft planned to operate over Greenland. This can be verified by 

confirming that 13 oxygen bottles are installed. 

Minimum oxygen bottle quantities required for operations over Greenland are based upon: 

I. Sun Country Airlines Greenland Depressurization Procedures, 

2. Depressurization at 45W, operating at 14,000 feet for up to 29 minutes, and 

3. Oxygen bottles for up to ( 4) four flight attendants. 

Passenger Count Minimum Oxygen Bottle Quantity 

0-18 5 

19-36 6 

37-54 7 

55-72 8 

73-90 9 

91-108 10 

109-126 11 

127-144 12 

145-162 13 
country airlines 

Nov 25,2014 Inert Gas System 

MELjCDL 

B-737 

47-1.1 

47-1 Nitrogen Generation System (NGS) 

SYSTEM INTV QUANTITY FIC REMARKS OR EXCEPTIONS 

INSTL/RQD 

47-1-1 A - 0 N (M) May be inoperative provided: 

Nitrogen a) NGS shutoff valve is deactivated closed, aud 

Generation b) Repairs are made within ten (1 0) flight days. 

System 

47-1-1-a c - 0 y May be inoperative. 

Nitrogen 

Generation 

Degraded 

MAINTENANCE (M) 

For either the amber INOPERATIVE- UNSERVICEABLE indicator light illuminated or for no 

operability indicator lights illuminated, deactivate the N GS shutoff valve in the closed position 

(AMM 47-00-00/901). 
NIEL/CDL 

B-737 

47-1.2 Inert Gas System 

Intentionally 

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May 29,2014 
sun country airlines 

Nov 25, 2014 Engine Fuel and Control 

73-4 Fuel Filter Differential Pressure Warning Systems 

NIEL/CDL 

B-T3T 

73-4.1 

SYSTEM INTV QUANTITY F/C REMARKS OR EXCEPTIONS 

INSTL/RQD 

73-4-2 c 2 1 N (M) One may be inoperative provided the malfunction 

is verified to be in the warning system. 

PLACARD 

Affected fuel FILTER ICING or FILTER BYPASS light- INOP 

MAINTENANCE (M) 

VerifY that the malfunction is in the fuel filter bypass warning system: 

1. If the FILTER BYPASS light illuminates with the engine not operating, the fuel filter bypass 

warning system is faulty. Proceed to step 3 below to replace the fuel filter. 

NOTE: To energize the system with the engine not operating, position the Engine START 

Switch to CONT. 

2. If the FILTER BYPASS light does NOT illuminate with the engine not operating, perform the 

following: 

A. If Fuel FILTER BYPASS light was ON prior to engine shutdown, check EEC BITE-RECENT FAULTS for a "FUEL FILTER SIGNALS DISAGREE" fault message (AMM 73-

21-00). 

1) If this fault message is present, proceed to step 3 below to replace the fuel filter. 

2) If the fault message is not present, use FIM 73-05 Task 801 -Fuel FILTER BYPASS 

Light is ON, to identifY if there is a malfunction in the fuel bypass warning system. 

B. If Fuel FILTER BYPASS light is inoperative OFF, do EEC TEST, AMM task 73-21-00-

700-804-FOO. 

NOTE:Remaining indication lights in the EEC test should illuminate normally. 

3. Replace fuel filter with a new filter (AMM 73-11-02). 

NOTE: Except forETOPS operations, one flight is permitted prior to filter replacement provided that fuel drained from filter housing drain plug is free of visible, gross contamination. 

OPERATIONS NOTE 

Ifthe remaining FILTER BYPASS light illuminates, assume both engine fuel filters have an impending bypass condition. 

MEL/CDL 

B-T3T 

73-4.2 Engine Fuel and Control 

Intentionally 

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May 29,2014 
sun country airlines 

May 29,2014 

74-1 Ignition Systems 

SYSTEM INTV QUANTITY 

INSTLIRQD 

74-1-2-a B 2 1 

Left Ignition 

Systems 

74-1-2-a-1 c 2 0 

Left Ignition 

Systems 

74-1-2-b B 2 I 

Right Ignition Systems 

74-1-2-b-1 c 2 0 

Right Ignition Systems 

F/C 

y 

y 

N 

N 

MEL/CDL 

B-737 

Ignition 74-1.1 

REMARKS OR EXCEPTIONS 

One may be inoperative provided: 

a) Ignition Select Switch remains in BOTH position, and 

b) Right ignition systems operate normally. 

(O)Except forETOPS operations, may be inoperative 

provided: 

a) Ignition Select Switch remains in BOTH position, 

b) Associated engine right ignition system operates normally, and 

c) For ETOPS aircraft only, ETOPS statns is 

downgraded per MEL Item 34-98-1. 

(M) (O)One may be inoperative provided: 

a) Ignition Select Switch remains in BOTH position, 

b) Left ignition systems operate normally, and 

c) Associated engine left igniter is connected to 

AC Standby Bus by an acceptable configuration. 

(M) (O)Except forETOPS operations, may be inoperative provided: 

a) Ignition Select Switch remains in BOTH position, 

b) Associated engine left ignition systems operate 

normally, and 

c) Associated engine left igniter is connected to 

AC Standby Bus by an acceptable configuration, and 

d) For ETOPS aircraft only, ETOPS statns is 

downgraded per MEL Item 34-98-1. 

NOTE I :Dispatch is not permitted if the ignition failure is due to an EEC right igniter fault (AMM 

74-00-00, EEC BITE Igniters Test). 

NOTE 2:When using MEL Items 74-1-2-a-1 and 74-1-2-b-1, refer to MEL Item 34-98 ETOPS. 

PLACARD 

Ignition Select Switch- OPERATE IN BOTH ONLY 
MEL/CDL 

B-T3T 

74-1.2 

MAINTENANCE fM) 

Ignition 

sun country air~Jines 

Nov 25,2014 

1. Right Ignition System(s), connect the LEFT igniter to AC Standby Bus (AMM 74-00-00/901). 

A. Open applicable Pl8-2 (#I ENG) or P6-2 (#2 ENG) Panel circuit breakers: 

I) Engine No. I- ENGINE 1 IGNITION RIGHT and ENGINE I IGNITION LEFT 

2) Engine No.2- ENGINE 2 IGNITION RIGHT and ENGINE 2 IGNITION LEFT 

B. VerifY that start levers are in the CUTOFF position and start switch is in the OFF position. 

C. Open fan cow I on affected engine. 

WARNING: MAKE SURE THE IGNITION EXCITERS ARE DE-ENERGIZED BEFORE 

WORKING ON THE IGNITION SYSTEM. WAIT FOR A MINIMUM OF FIVE 

MINUTES TO RELEASE THE IDGH VOLTAGE FROM IGNITION EXCITER. 

D. Disconnect LEFT/RIGHT power supply cables from the LEFT/RIGHT ignition exciter. 

E. Connect cables as follows: 

1) LEFT power supply cable to RIGHT exciter. 

2) RIGHT power supply cable to LEFT exciter. 

F. Close circuit breakers opened in Step 2A. 

G. Perform Audible Test oflgnition System - EEC BITE. 

H. Close fan cowl on affected engine. 

OPERATIONS (0) 

Normal operation of the operable ignition system may be confirmed as follows: 

1. Position ignition switch to IGN R for starting the associated engine. 

2. After engine start, position ignition switch to IGN BOTH. 
esun country airlines 

Nov 25,2014 

Wings- 57 

Table of Contents 

MEL/CDL 

B-T3T 

57-0-0.1 

Flap Track Fairing Tail Cone, Outboard Flaps ..................................................... 57-10-3.1 

Flap Track Fairing Tail Cones, Inboard Flaps ....................................................... 57-10-4.1 

Flap Support Fairings No.1 and No.8 (Outboard Flap) ....................................... 57-10-5.1 

Wing Vortex Generators ........................................................................................... 57-30-6.1 

Jacking Point Panels .................................................................................................. 57-30-7.1 

Slat Actuator Fairing Panels ..................................................................................... 57-30-8.1 

Split Scimitar Winglet Ventral Strake ..................................................................... 57-31-1.1 

Slat Main Track Seal Door ....................................................................................... 57-41-4.1 

Slat Skin Tabs CIT Auxiliary Arms ......................................................................... 57-30-8.1 

Slat Sponge Seals ....................................................................................................... 57-41-9.1 

Slat Bnlb Seals .......................................................................................................... 57-41-10.1 

Slat End Seals (Outboard End, Slats 1 & 8) .......................................................... 57-41-11.1 

Wing Leading Edge Vortilons ................................................................................ 57-41-12.1 

Slat Spanwise Lower Flex Skin .............................................................................. 57-41-13.1 

Sponge Rubber Air Dam in Overwing Bolt Cover Cavity ..................................... 57-51-1.1 

Inboard Flap, Inboard Seal Plate ............................................................................. 57-53-3.1 

Inboard Flap, Inboard Flap Track Slot Landing Door Assembly ........................ 57-53-5.1 

Inboard Flap, Inboard Flap Track Slot Landing Door Seals ................................ 57-53-6.1 

Outboard Flap Leading Edge Vortex Generators .................................................. 57-53-7.1 

Aerodynamic Seal CIT Krueger Flap (Fwd) Inboard Fixed Leading Edge ......... 57-54-3.1 

Aerodynamic Seal CIT Krueger Flap (Aft) ............................................................. 57-54-4.1 

Aerodynamic Seal CIT Krueger Flap (Inboard Fixed Leading Edge) ................. 57-54-5.1 

Aerodynamic Seal Retainer CIT (Krueger Flap- Fwd) ......................................... 57-54-6.1 

Aerodynamic Seal Retainer CIT (Krueger Flap- Aft) ........................................... 57-54-7.1 

Aerodynamic Seal Retainer Assembly CIT (Krueger Flap- Aft) ......................... 57-54-8.1 

Bnlb Seal CIT Krueger Flap (Aft) ............................................................................ 57-54-9.1 

Seal-Blade, Inboard Krueger Flap, Spanwise, Aft ............................................... 57-54-10.1 

Spoiler 1, 2, 3, 10, 11, 12 Seals .................................................................................. 57-71-1.1 
NIEL/CDL 

B-T3T 

57-0-0.2 Table of Contents 

Intentionally 

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country 

aWI!IleS 

May 29,2014 

~ S~n .country ~A.rlrnes• 

Nov 25, 2014 Configuration Deviation List 

NUMBER: 57-31-1 

ITEM:Split Scimitar Winglet Ventral Strake 

MODEL: All 

NUMBER OF ITEM INSTALLED FOR (MODEL): 2 

CDL 

B-T3T 

57-31-1.1 

Both split scimitar winglet ventral strakes may be removed. Flight with one split scimitar winglet 

ventral strake removed is not authorized. 

Performance shall be limited to Blended Winglet performance with both ventral strakes removed. 

Time with both ventral strakes removed shall be limited to 10 calendar days. 

Maximum Take-off weight shall be less than 168,500 pounds. 
CDL 

B-T3T 

57-31-1.2 Configuration Deviation List Nov 25, 2014 

Intentionally Blank 
May 24, 2012 Operational information 

Equipment Failure 

(On the Ground) 

QRH 

8-737 

01.7.1 

Condition: Any Equipment Failure during engine start 

and prior to Takeoff. 

1 Verify that the system controls are set correctly. 

2 If applicable, accomplish the appropriate 

Non-Normal Checklist. After completion, resume 

this checklist. 

Note: All subsequent steps must be completed in 

coordination with Maintenance Control. 

3 Contact Maintenance Control. 

If circuit breaker(s) tripped: 

,.. ,..Go to Circuit Breaker Tripped (Reset) 

checklist, Step 3 on page 01.4.5 

4 Consult Minimum Equipment List (MEL). 
QRH 

8-737 0 Sun --·""~· Country 

Airlines 

01.7.2 Operational Information Pend, 2013 

1!£1 i. &<m!Pl\lent!J1l!Jl\W!1I€!:IDml>t.G~~!tHB!ll 

5 Choose one: 

If unable to comply with the conditions and 

limitations of the MEL return to gate . 

•••• 

If able to comply with the conditions and 

limitations of the MEL and the Captain, 

Maintenance Control, and Dispatch agree 

the flight is safe, the flight may continue to 

destination. 

~~Go to step 6 

1

6 Prior to flight the failed item will be entered into the 

Aircraft Maintenance logbook and placed on MEL. 

Note: At the direction of Maintenance control, 

complete the ACTION column of the 

Aircraft Maintenance Logbook. Include a 

brief description of the item/system, MEL 

No., Placard No., CAT letter, MDDR No., 

and state "Maintenance Control Notified". 

Note: If the conditions for a flight are changed to 

the extent the original dispatch/flight 

release is no longer valid, a new or· 

amended release is required. See the 

FOM; Chapter 3, Section 3 "Dispatch 

Release Validity" . 

••••