### 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 LawJudge 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 ofJanuary,



# 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 ofJanuary, 2016, I served, via facsimile, a copy of the foregoing Initial Disclosures in the Matter ofMN Airlines, LLC d/b/a Sun Country Airlines, FAA DocketNo. 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 LawJudge Office ofHearings, M-20 U.S. Department ofTransportation 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 ofthe 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.

# -suncountry 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, revisionbars are displayed adjacentto all technical and non-technical changes. However, highlights are written only for technical revisions. In some sections, the information may have been extensively rewrittenfor clarity, inthese cases ahighlight is written, butchange barsmaynotbe provided. Revisionbars will notbe provided onpages issued for the purpose ofrepagination orformatting only Add means that a newMEL item has been added to the SCA MEL. Replace means remove existing MEL item and replace with revised MEL itempages. Delete means the remove and destroy the MEL item.
Revision Highlights
Item MMEL DDG SCA Instruction Highlights LEP-0.1


## - X Replace Updated List ofEffective 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 EquipmentAddendum Added aircraft 820SY and 821SY equipment. 23-0.1



## - 23- X Replace Updated Table ofContents. 0.2 23-10.1

- 23- X Replace 23-10 CockpitVoice Recorder System 10.2 (CVR) Added items for RecorderIndependentPower Supplies. 23-27.1

- 23- X Add 23-27 DataLink Communication 27.2 Added item for aircraft DataLink 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 

# -suncountry 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 27-4LeadingEdgeFlap/SlatPositionLight Systems Added Maintenance Procedure for aircraft 820SY and 821SY. Replace 27-7 Auto SpeedBrake 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 ofContents. Add 34-54 Integrated StandbyFlightDisplay (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 74-1 Ignition Systems Revised Maintenance Procedure. Replace Updated Table ofContents. Add Split ScimitarWinglet Ventral Strake Added MEL item for split scimitar equipment.Nov 25,2014

PAGENO. DATE TitlePage Table ofContents MEL/CDL-0.1May 29,2014 MELICDL-0.2May 29, 2014 Record ofRevisions ROR-0.1 May29, 2014 ROR-0.2 May 29,2014 ROR-0.3 May29, 2014 ROR-0.4 May29, 2014

List OfEffectivePages *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 ofEffective 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

EquipmentAddendum '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 ofEffective Pages Nov 25,2014

PAGE NO. DATE PAGE NO. DATE PAGENO. 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

# $suncountry a1rl1nes Nov 25,2014 

### List ofEffective 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 Nov25, 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 

# -suncountry airlines List ofEffective 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 InspectorNov 25,2014 

### List ofEffective 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 May 29,2014 May 29,2014 May 29,2014 May 29,2014 May 29,2014 May 29,2014 May 29,2014 May 29,2014 May 29,2014 May 29,2014 May 29,2014 May 29,2014 May 29,2014 May 29,2014 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 May 29,2014 May 29,2014 May 29,2014 May 29,2014 May 29,2014 May 29,2014 PAGE NO. 34-35.2 34-36.1 34-36.2 34-37.1 34-37.2 34-38.1 34-38.2 34-40.1 34-40.2 34-42.1 34-42.2 34-43.1 34-43.2 34-45.1 34-45.2 34-47.1 34-47.2 34-48.1 34-48.2 34-49.1 34-49.2 '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 May 29,2014 May 29,2014 May29, 2014 May 29,2014 May 29,2014 May 29,2014 May 29,2014 May29, 2014 May29,2014 May 29,2014 May 29, 2014 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 

# -suncountry a1rl1nes List ofEffective 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

## ofEffective Pages

PAGENO. DATE



# - PAGE NO. DATE 77-2.2 May 29, 2014 30·1 0-1.1 May 29, 2014 77·5.1 May 29,2014 30·10-1.2 May 29,2014 77·5.2 May 29,2014 Table ofContents 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 32·10·4.2 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 32·10·8.2 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 30·0·0.2 May 29,2014 33·40·3.1 May 29,2014 PAGE NO. 33-40-3.2 33-43-1.1 33-43-1.2 33-43·2.1 33-43·2.2 33-43-3.1 33-43-3.2 33·5J.l.1 33·51-1.2 

### 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 May 29,2014 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 55-30-1.1 May 29,2014 55-30-1.2 May 29,2014 Wings- 57 *57-0-0.1 Nov 25,2014 57-0-0.2 May 29, 2014 57-10-3.1 May 29,2014 57-10-3.2 May 29,2014 57-10-4.1 May 29,2014 57-10-4.2 May 29,2014 57-10-5.1 May 29,2014 57-10-5.2 May 29,2014 57-30-6.1 May29, 2014 57-30-6.2 May29, 2014 57-30-7.1 May 29,2014 57-30-7.2 May 29,2014 57-30-8.1 May 29,2014 

### List ofEffective 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 57-30-8.1 May 29,2014 57-54-3.1 May 29,2014 57-30-8.2 May 29,2014 57-54-3.2 May 29,2014 57-41-9.1 May 29,2014 57-54-4.1 May 29,2014 57-41-9.2 May 29,2014 57-54-4.2 May 29,2014 57-41-10.1 May 29,2014 57-54-5.1 May 29,2014 57-41-10.2 May 29,2014 57-54-5.2 May 29,2014 57-41-11.1 May 29,2014 57-54-6.1 May 29,2014 57-41-11.2 May29, 2014 57-54-6.2 May 29,2014 57-41-12.1 May 29,2014 57-54-7.1 May 29,2014 57-41-12.2 May 29,2014 57-54-7.2 May29, 2014 57-41-13.1 May 29,2014 57-54-8.1 May 29, 2014 57-41-13.2 May 29,2014 57-54-8.2 May 29,2014 57-51-1.1 May 29,2014 57-54-9.1 May 29,2014 57-51-1.2 May29, 2014 57-54-9.2 May 29,2014 57-53-3.1 May 29,2014 57-54-10.1 May 29,2014 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 78-30-1.2 May 29,2014 78-30-4.1 May 29,2014 78-30-4.2 May 29,2014 78-30-5.1 May 29,2014 78-30-5.2 May 29,2014 78-31-4.1 May 29,2014 78-31-4.2 May29, 2014 78-31-5.1 May 29,2014 78-31-5.2 May29, 2014 78-31-6.1 May 29,2014 78-31-6.2 May 29,2014 78-31-7.1 May 29,2014 78-31-7.2 May29, 2014 78-31-8.1 May 29,2014 78-31-8.2 May29, 2014 78-32-2.1 May 29,2014 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 ofthe Minimum EquipmentList (MEL) and the ConfigurationDeviationList (CDL). This manual interfaces with other Sun CountryAirlines departments and manuals, including: SCA General Maintenance Manual SCA Flight Operations Manual 14 Code ofFederal Regulations (CFRs) SCAhas also established an amplifiedMELICDL which is an extension ofthe MasterMEL as published bythe FlightOperationsEvaluationBoard (FOEB), andthe CDL as publishedbyBoeingCorporation. 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 ofan aircraft with certain equipment either inoperative ormissing. Approvalspresentedhereinhave beenpreparedto meetrequirements of current 14 CFRs and are applicable to the 737 aircraft operated by SCA. Compliance with the policies and practices stated inthis manual is mandatory. Approvals The approval signatures below grant Sun CountryAirlines authorizationto utilize SCARevision42, 737 MELICDL in operations ofsuch aircraft. Items within this MEL/CDL are no less restrictive than theFAAApproved 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 ofFlight Opera- FAA, POI tions

### MEL/CDL B-T3T 

### 1-0.2 

### Introduction

Intentionally Blank 

# -suncountry airlines May 29,2014countryairlinesNov25,2014GeneralEquipmentAddendumMELjCDLB-T3T4-0.1ThisequipmentaddendumisintendedtoprovideacommonlocationforSunCountryAirlines737MELICDLuserstoidentifyvariationsrelatingtoinstalledequipmentbyaircraftregistrationnumber."Yes"indicatesthatthesystemoritemisinstalled."Yes(#)"indicatesthatthespecifiednumberofsystemsoritemsisinstalled."No"indicatesthatthesystemoritemisnotinstalled.B737-700EQUIPMENTADDENDUMMELItem710SY711SY712SY713SY714SY715SY716SY23-3-aYesYesNoNo NoNoYes#3VHF23-3-1VHFCommNo NoYes(2)Yes(2)No No NoControlPnl23-3-2Yes(3)Yes(3)NoNoYes(3)Yes(3)Yes(3)RadioTuningPnl23-11HFYes(1)Yes(1)Yes(1)Yes(1)NoNoYes(2)CommunicationSystems27-20SpeedBrakeLoadAlleviationYesYesNoNoYesYesYesSystem(WingletsInstalled)28-2-1NoNoNoNo NoNoNoUFI28-3-2-aAutoNoYesNoNoYesYesNoShutoff28-7-4NoYesNoNoYesYesNoSB737-28A120633-11SingleNavigationLightsDualDual Dual DualSingle(L)DualDual(R)MEL/CDLB-T3T4-0.2MELItem33-19-1EscapePathLighting34-15-4Autotilt/MultiScanRadar46-1-7ElectronicFlightBagB737-800MELItem23-3-a#3VHF23-3-1VHFCommControlPnl23-3-2RadioTuningPnl23-11HFComms7IOSYIncandescentYesClass3SOISYYesNoYes(3)Yes(2)EQUIPMENTADDENDUM711SY712SY 713SY 714SYPhotolu-Photolu-Photolu-Incandes-mines-mines- minescentcent cent centYesNo NoYesClass3Class3Class3ClassIS04SYSOSSYSOSSYS09SYYesYesYesYesNoNoNo NoYes(3)Yes(3)Yes(3)Yes(3)Yes(2)Yes(2)Yes(2)Yes(2)EquipmentAddendum715SY716SYPhotolu-Photolumines-minescentcentStripsYesYesClass3Class3EQUIPMENTADDENDUMSI3SYSI4SYSISSYSI6SYNoYes YesYesYes(2)NoNoYes(2)NoYes(3)Yes(3)NoYes(!)Yes(2)Yes(2)Yes(!)SI7SYSISSYSI9SYYes Yes YesNoNoNoYes(2)Yes(3)Yes(3)Yes(2)Yes(2)Yes(!)*suncountryairlinesNov25,2014S20SYS21SYTAVSOOYesYes YesNoNo NoYes(3) 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 Dualfucandescent 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- Photolumines- Mounted mines- minescent LED cent cent

No Yes Yes Yes

Class 3 Class 3 Class 3 Class 1 820SY No No Yes Yes DualPhotoluminescent Yes Class 1 NIELjCDL B-737 4-0.3 821SY TAV 800
No As Inst No No Yes As Inst Yes Yes Dual DualPhotolumines- In can-

descent

cent Yes No Class 1 Class 1'<!; 0' 

# "'"

# sun country airlines Nov 25,2014 

### Communications-23 Table ofContents MELjCDL 

### B-737 

### 23-0.1

23-1 Flight DeckSpeaker 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 ACARS/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 DeckHeadsets 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 FlightDeckHand 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 ElectronicVisual Surveillance Systems ............................................................ 23-21.1 23-23 Multipurpose Interactive Display Unit (MIDU)
..............................................23-23.1 23-26 Avionica secureLINKAirborne Wireless Router (STC03151AT)
................ 23-26.1 23-27 Data LinkCommunication ................................................................................23-27.1

### MEL/CDL 

### B-737 

### 23-0.2 Table ofContents

Intentionally Blank 

# country airlines May 29,2014

# -suncountry 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 OREXCEPTIONS 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 withinthree 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 ofthe c/b is (RIPS) achieved before departure, and (N820SY and d) Repairs are made withinthree 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) CVRoperates 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 OREXCEPTIONS 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 OREXCEPTIONS 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 andplacarded "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 ofFlight 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) 

### Maybe inoperative ormissing and seatoccupied Armrests with provided: Recline a) Arm rest does not block an Emergency Exit, Mechanism b) Armrest does notrestrict anypassengerfrom access to the main aircraft aisle, and c) If armrest is missing, seat is secured in full upright position. NOTE:Ifthe armrest has a de-lethalization padbuilt into the back side ofthe armrest, the row directly behindthe missing or inoperative armrest must also be considered inoperative per MEL Item 25-6.

### MEL/CDL 

### B-T3T 

# suncountry airlines 25-6.2 Equipment and Furnishings Nov 25,2014 

### 25-6 Passenger Seat(s) SYSTEM INTV QUANTITY F/C REMARKS OREXCEPTIONS 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) Armrest does notrestrict any passengerfrom access to the main aircraft aisle. NOTE:Ifthe armrest has a de-lethalization pad built into the back side ofthe 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 ofinoperative 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 uprightposition. For an inoperativeunderseatbaggage restrainingbar, ensure cabin crewis notified ofthe inoperative restraining bar and that baggage is notto be placed under the associated seat.I 

# sun country airlines MELfCDL B-737 Nov 25,2014 

### Equipmentand Furnishings 25-10.1 

### 25-10 Non-Essential Equipment and Furnishing (NEF) SYSTEM INTV
25-10 D 25-10N

--

PLACARD 25-10: As appropriate 25-1ON: Not required NEF Information QUANTITY F/C REMARKS OREXCEPTIONS INSTL/RQD



## - 0 y Maybe 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 ofthe Logbook binder. Itwill not be listed on the Dispatch Release.

TheNEF ApprovedList below lists the defects whichhave been analyzed andapproved for deferral under MEL 25-10 or 25-1ON. TheNEF Rejected List lists items thathave been analyzed and found to be not eligiblefor deferral undertheNEF program. Ifthedefect/equipmentinquestion is notlisted in either the NEF Approved List or the NEF Rejected List, Maintenance Control must analyze the defectpertheNEF Process Flowchartin the Practices section ofthe MELto determine whether it is eligible for deferral. SeeNon-Essential Equipment and Furnishings (NEF) Policies andProcedures, in the Practices section ofthe 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 notpresent hazard to passengers or ets dirty, worn, damaged ormissing 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) Cabintemperature 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 Coathangers 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 curtaintom 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 outletcov- 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 setmust stillbe onboardthe belt, life vest and oxygen mask airplane Seat numberplacards N 120 days Seat track covers loose, damaged or 120 days (M) Any exposed wiring must be protectmissmg ed. Mustnotpresenthazard to passengers or crew or impede emergency egress. Flight Crew may not defer ifwiring 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 betweenpanes 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 

# -suncountry 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 requiredper 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 backpocket 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. Ifthe annresthas a de-lethalizationpad, refer to MEL25-6-2-a or 25-6-2-b. Tray table

- Damagedtable/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 hotplate 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 leakby shutting offassociated 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 shelfdamaged 120 days (M) Secure shelfifit is loose. Install "Do not use" placard on shelf. Counter shelfstuck 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 Galleywater spigots willnottum on 120 days Oven door won't open 120 days

### MEL/CDL B-T3T 

# $-suncountry 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 containerpull 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) Iftable is damaged, verify that it is operative secure. Install "Do not use" placard ontab1e. 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)Lavatorydoorlocks maybe 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 ormissing Lavatory passenger assist handles N 120 days broken ormissing 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 

# suncountry 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 miSSJUg 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) Ifmissing, inspect open cavityto 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 seatbottom 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. Ifnot, 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 notpresent 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 hazardto 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.

# $-suncountry a1r11nes MELjCDL B-737 Nov 25,2014 

### EquipmentandFurnishings 25-10.9 FlightDeck 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 notpresent 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 Holdopenrod orlanyard 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)

# iltsuncountry 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 OREXCEPTIONS 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 takeoffand 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 annunciatorpanel operate normally, and d) Stall warning operation ofboth 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 indicationlights 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 verifiedby the flight crew before eachtakeoffand 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 ofboth systems is verifiedto operate normally. e) A placard is installed to indicate proper positions for flap configuration in use.

### MELjCDL 

### B-737 

### 27-4.2 

### Flight Controls 

# suncountry airlines Nov 25,2014 NOTE:Associated wing illumination light may be required for verification ofnormal operation of the leading edge slats. 

### PLACARD For inoperative forward panel lights, affected lights- INOP For inoperative annunciatorpanel, overhead annunciator panel- INOP Forinoperative indicators for one slatonboth panels, affected annunciatorpanel lights- INOP- VISUALLY CONFIRMPOSITION 

### 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:Ifan annunciatorpanel TRANSIT light fails to illuminate whilethe 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 instrumentpanel, P2. 4. Use this datato make aplacard and put it adjacent to the annunciator panel: All exceptN820SY/N821SY A. Flappositions 1thru 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 inEXTposition. 2) LE flaps extended. B. Flap positions 30 and 40: 1) All slats in FULL EXT position. 2) LE flaps extended.

# suncountry ' 

### ,, 

## 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 ANNUNCIATORPANEL 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 thatthe remaining LEDEVICES annunciatorpanel (P5) lights operate normally during flap extension and retraction. NOTE 1

### :Ifan annunciator panel TRANSIT light fails to illuminate while the corresponding device is inmotion, thenthis lightmust 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 instrumentpanel, P2. 4. Use this data to make aplacard and putit adjacentto 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 1thru 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 ifan FSEU input has been recently faulty, IfFSEU 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 

# suncountry 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 ofthese fault codes because the fault indication light(s) flashes ON/OFF for an instant such thatthe fault does not latch, and the applicable slat can be confirmed to be stationary inthe positionwhere the intermittent indicationwas observed, then open and collarthe Stall WarningAsymmetryMode circuit breaker. 6. Set flaps to the positionwhich produces the faulty indication. 7. Verify thatthe leading edge and trailing edge devices are in the correctposition. 8. Verify normal operation ofboth Stall Warning Systems: NOTE I: (All exceptN820SY/N821SY) If

### the inoperative slat indication occurs at more than one flap position, repeatthe procedureto verifynormal operation ofboth Stall Warning Systems at Flaps 0, Flaps I and Flaps 10. NOTE 2: (N820SY/N821SY only) Ifthe inoperative slat indication occurs at more than one flap position, repeat the procedure to verify normal operation ofboth Stall Warning Systems atFlaps 0, Flaps I and Flaps 30. A. Verifythat 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 thatthe control column stick shakers operate normally. D. Ifboth stick shakers fail to operate normally, open and collarthe Stall WarningAsymmetry Mode circuit breaker onthe P 18-2 Panel ifnot already accomplished in step 5 above, and then repeattest in steps B and C. 9. Ifthe 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 annunciatorpanel light inoperative:

I. 

### Verify leading edge slatposition for the inoperative indicationbefore eachtakeoffand 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. Flightplan will be generated using "LeadingEdge Slat" (LES) profile to accountfor speed restrictions. NOTE: With FMC update 10.7 or later, VNAV will limitthe speedtargetto 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 aircrafthave SpeedBrake LoadAlleviation System installed. NOTE 2:Aircraft with Speed Brake Load Alleviation System installed must also be dispatched usingMEL 27-20SpeedBrake 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 andN821 SY do nothave SpeedBrake Load Alleviation System installed.

Speed brake control lever- AUTO SPD BRKINOP MAINTENANCE (M) For item 27-7-1: Prepare the airplane for flight withthe auto speedbrake 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 withthe auto speed brake system inoperative (AMM 27-00-001901):

### MEL/CDL B-737 

### 27-7.2 Flight Controls 

# suncountry airlines Nov 25,2014
1. Verify manual speed brake operation. NOTE: Extend flaps priorto 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, selectAUTO SPOILER SYSTEM: INOPERATIVE fromthe MEL input screen. This will account for the takeoffand landing performance penalties. 2. Prior to takeoff, ensure that speed brake lever is in full down detent. 3. Extend speedbrakes manually for rejected takeoffor landing. A. Forrejected takeoff: 1) Simultaneously close thrust levers, disengage the autothrottles and apply manual wheel brakes or verify operation ofautobrakes. 2) Manually raise SPEED BRAKE lever. 3) Apply the maximum amount ofreverse thrust consistent with conditions. B. For landing, use the SPEED BRAKEDO NOT ARM non-normal checklist 4. The autobrakes maynotdisarm whenthe speedbrake leveris stowed. Auto brakes maybe disarmed by positioning AUTO BRAKE select switch to OFF, applying brakes manually or advancing the thrust levers.

# suncountry 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 OREXCEPTIONS INSTL!RQD 27-8-4 

## c 1 0 y (O)May be inoperative provided: (-700) a) Flaps are notextendedbeyondFlaps 30 atgross weights above 93,480 

### lb, and b) Flaps are notextended beyondFlaps 15 atgross weights above 104,403 

### lb. 27-8-5 

## c I 0 

### y (O)May be inoperative provided: (-800) a) Flaps are notextended beyondFlaps 30 at gross weights above 93,995 Ib, and b) Flaps are notextendedbeyondFlaps 15 at gross weights above 104,875 lb. 27-8-6 

## c 1 0 

### y (O)May be inoperative provided: (-800SFP) a) Flaps are notextendedbeyondFlaps 30 atgross (N820SY, weights above 95,800 

### lb, and N821SY on- b) Flaps are notextendedbeyondFlaps 15 at gross ly) weights above 105,000 

### lb, and c) Flaps arenotextendedbeyondFlaps 10 at gross weights above 135,800 

### lb. PLACARD Flap handle and/or flap position indicator- LOAD LIMITERINOP- FLAPS ARENOTTO BEEXTENDED BEYOND FLAPS 15/30 AS APPLICABLE. OPERATIONS CO) InOPS, selectFlap Load Limiter: INOPERATIVE from the MEL input screen. This will force the Dispatch Landing calculations to be based on flaps I5.

### NIEL/CDL 

### B-T3T 

### 27-8.2 Flight Controls

Intentionally Blank 

# sun country ail-lines May 29,2014

# -suncountry awl1nes Nov 25,2014 

### Navigation-34 Table ofContents MELjCDL 

### B-T3T 

### 34-0.1

34-1 Mach Indications

.................................................................................................... 34-1.1 34-2 Mach/Airspeed Warning Systems

......................................................................... 34-2.1 34-3 AltimeterVibrators

- StandbyAltimeter

............................................................. 34-3.1 34-4 Static AirTemperature Indication

....................................................................... 34-4.1 34-5 TotalAirTemperature Indication

........................................................................ 34-5.1 34-7 StandbyHorizon Indicator

.................................................................................... 34-7.1 34-11 Non-Stabilized Magnetic Compass

................................................................... 34-11.1 34-12 Flight Director Systems

...................................................................................... 34-12.1 34-13 DistanceMeasuring Equipment Systems

......................................................... 34-13.1 34-14 MarkerBeacon Receiver System

...................................................................... 34-14.1 34-15 WeatherRadar

................................................................................................... 34-15.1 34-16 Radio Compass Systems (ADF)

......................................................................... 34-16.1 34-17 VHF Navigation Systems (YORilLS)

............................................................... 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 GroundProximity Warning System (EGPWS)

............................ 34-26.1 34-31 Speed CursorRemote Drive

.............................................................................. 34-31.1 34-32 Instrument Transfer Switching System

........................................................... 34-32.1 34-35 InertialReference Systems (IRS)

...................................................................... 34-35.1 34-36 Flight Management ComputerSystem (FMCS)

.............................................. 34-36.1 34-37 WindshearDetection 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 HeightAlert

............................................................................................. 34-43.1 34-45 GlobalPositioning System (GPS)

...................................................................... 34-45.1 34-47 ILS Beam Deviation Lights

............................................................................... 34-47.1 34-48 EFIS Control Panel

............................................................................................ 34-48.1 34-49 RightIRS DC Power Supply System

................................................................ 34-49.1 34-54 Integrated StandbyFlight 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 ofContents

Intentionally Blank 

# sun country ali-lines May 29,2014

# suncountry airlines Nov 25,2014 

## Navigation MELjCDL 

### B-737 

### 34-54.1 

### 34-54 Integrated Standby Flight Display (ISFD) SYSTEM INTV QUANTITY F/C REMARKS OREXCEPTIONS 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 Maybe inoperative provided operations do notrequire 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 Blank 

# suncountry airlines 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 Blank 

# 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 OREXCEPTIONS INSTL/RQD 35-4 D 7 3 y (M) Any in excess ofthose required may beunservice- (-700) able or missing provided: a) Required distribution of serviceable bottles is maintainedthroughout aircraftby ensuring botties are equally divided between forward and aft cabin stowage areas (if the number ofrequired bottles is odd, the odd bottle may be placed forward or aft), and b) Bottles notproperly serviced are replaced, serviced or removed at the next available maintenance facility. 35-4-1 D 8 4 y (M) Any in excess ofthose required may be unservice- (-800 Non- able ormissingprovided: ETOPS and a) Required distribution of serviceable bottles is N820SY/ maintainedthroughout aircraftby ensuring botN821SY) ties are equally divided between forward and aft cabin stowage areas (if the number ofrequired 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 ofthose required may be unser- (-800 ETOPS viceable or missingprovided: except a) Required distribution of serviceable bottles is N820SY/ maintainedthroughout aircraftby ensuringbotN821SY) ties are equally divided between forward and aft cabin stowage areas (if the number of required bottles is odd, the odd bottle may be placedforward 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 

# suncountry airlines 35-4.2 

## Oxygen Nov 25,2014

more than 1000 psi, but less than 1500 psi, should beplaced on MTI. NOTE 2:The use ofan oxygen mask renders the associated unit unserviceable for dispatch. 

### PLACARD As appropriate 

### MAINTENANCE (M)

l. Place the SCM-14 placard onthe face ofthe pressure gauge and remove the mask. 2. Ensure required distribution ofserviceable units is maintained throughoutthe airplane by ensuring bottles are equally divided between forward and aft cabin stowage areas (ifthe number ofrequired 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 itwill notbe used by mistake and associated locatorplacards 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 shutoffvalve is deactivated closed, aud Generation b) Repairs are made within ten (10) 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 NGS shutoff valve in the closed position (AMM 47-00-00/901).

### NIEL/CDL 

### B-737 

### 47-1.2 

## Inert 

## Gas System

Intentionally Blank 

# sun country air'lines May 29,2014

# suncountry 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 OREXCEPTIONS 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 orFILTER BYPASS light- INOP MAINTENANCE (M) VerifY thatthe malfunction is in the fuel filter bypass warning system:

1. Ifthe 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 energizethe system withthe engine not operating, positionthe Engine START Switch to CONT. 2. Ifthe FILTERBYPASS light does NOT illuminate withthe engine not operating, perform the following: A. IfFuel FILTERBYPASS light was ONprior to engine shutdown, check EEC BITE-RECENTFAULTS for a "FUELFILTER SIGNALS DISAGREE" fault message (AMM 73- 21-00). 1) Ifthis fault message is present, proceed to step 3 below to replace the fuel filter. 2) Ifthe faultmessage is notpresent, use FIM 73-05 Task 801 -FuelFILTERBYPASS Light is ON, to identifY ifthere is a malfunction in the fuel bypass warning system. B. IfFuel FILTERBYPASS light is inoperative OFF, do EEC TEST, AMMtask 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 drainplug is free ofvisible, 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 Blank 

# suncountry airlines May 29,2014

# suncountry 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 OREXCEPTIONS


### 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 leftignition 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 downgradedper MEL Item 34-98-1. NOTE I:Dispatch is notpermitted ifthe 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. RightIgnition System(s), connectthe LEFTigniterto AC Standby Bus (AMM 74-00-00/901). A. Open applicable Pl8-2 (#I ENG) orP6-2 (#2 ENG) Panel circuit breakers: 

### I) Engine No. 

### I- ENGINE 

### 1IGNITION RIGHT and ENGINE I IGNITION LEFT 2) Engine No.2- ENGINE 2 IGNITION RIGHT and ENGINE 2 IGNITION LEFT B. VerifY that startlevers are in the CUTOFF position and start switch is inthe OFF position. C. Open fan cowI 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 THEIDGH VOLTAGEFROM IGNITION EXCITER. D. DisconnectLEFT/RIGHTpower supply cables from the LEFT/RIGHT ignition exciter. E. Connect cables as follows: 1) LEFTpower supply cable to RIGHT exciter. 2) RIGHT power supply cable to LEFT exciter. F. Close circuitbreakers opened in Step 2A. G. PerformAudible Test oflgnition System

- EEC BITE. H. Close fan cowl on affected engine. OPERATIONS (0) Normal operation ofthe 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 switchto IGN BOTH.

# esuncountry airlines Nov 25,2014 

### Wings- 57 Table ofContents 

### MEL/CDL B-T3T 

### 57-0-0.1

Flap Track Fairing Tail Cone, Outboard Flaps

.....................................................57-10-3.1 Flap TrackFairing 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 ScimitarWingletVentral Strake

.....................................................................57-31-1.1 Slat Main Track SealDoor

.......................................................................................57-41-4.1 Slat Skin Tabs CITAuxiliaryArms

.........................................................................57-30-8.1 Slat Sponge Seals

.......................................................................................................57-41-9.1 SlatBnlb Seals

..........................................................................................................57-41-10.1 SlatEnd Seals (Outboard End, Slats 1 & 8)

..........................................................57-41-11.1 Wing Leading Edge Vortilons

................................................................................57-41-12.1 Slat SpanwiseLower Flex Skin

..............................................................................57-41-13.1 Sponge RubberAirDam in Overwing Bolt Cover Cavity

.....................................57-51-1.1 InboardFlap, Inboard SealPlate

.............................................................................57-53-3.1 Inboard Flap, Inboard Flap TrackSlotLanding Door Assembly

........................57-53-5.1 InboardFlap, Inboard Flap TrackSlotLanding Door Seals

................................57-53-6.1 Outboard Flap Leading EdgeVortex Generators

..................................................57-53-7.1 Aerodynamic Seal CITKrueger Flap (Fwd) Inboard Fixed Leading Edge

.........57-54-3.1 Aerodynamic Seal CITKruegerFlap (Aft)

.............................................................57-54-4.1 Aerodynamic Seal CITKrueger Flap (Inboard Fixed Leading Edge)

.................57-54-5.1 Aerodynamic Seal Retainer CIT (KruegerFlap- Fwd)

.........................................57-54-6.1 Aerodynamic Seal Retainer CIT (KruegerFlap- Aft)

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

.........................57-54-8.1 Bnlb Seal CITKruegerFlap (Aft)

............................................................................57-54-9.1 Seal-Blade, Inboard KruegerFlap, 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 Blank 

# country aWI!IleS May 29,2014

# ~**S~n** .country**~A.rlrnes•** Nov 25, 2014 

## Configuration Deviation List

NUMBER: 57-31-1 ITEM:Split Scimitar WingletVentral Strake MODEL: All NUMBER OF ITEMINSTALLED 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 BlendedWinglet performance with both ventral strakes removed. Time withbothventral strakes removed shall be limitedto 10 calendar days. MaximumTake-offweight shall be less than 168,500 pounds.

### CDL B-T3T 

### 57-31-1.2 

## Configuration Deviation List Nov 25, 2014

Intentionally BlankMay 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

. 

# •••• Ifable 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 Priorto 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: Ifthe 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"

. 

# ••••