background image

MAULE AEROSPACE TECHNOLOGY, INC. 

AIRPLANE FLIGHT MANUAL 

MAULE

 

MX-7-180B

 

Page ii 

LOG OF SUPPLEMENTS 

 

SUP. 

NO. 

NO. OF 
PAGES 

DESCRIPTION

 

APPROVAL 

DATE 

Installation of EDO 248B2440 Floats - Maule Dwg 9145A. 

Rev. A 

08/19/02 

Installation of Aqua 2200 Floats per STC No. SA253CH. 

Rev'd 

03/23/95 

Operation and limitation of aircraft when Model M-6-180 is modified to a MX-7-180B - Maule 
Modification Kit No. 22. 

04/03/97 

20 

Inst. of Wipline 2350 Amphibious Floats - Maule Drawing 9178A.    

Rev. C 

08/19/02 

English to Metric Conversion Charts - required in aircraft when registered in Canada

01/23/98 

Inst. of S-TEC System 30 Two Axis Autopilot ST-810-30 (14v) - Maule Dwg 9197A

(Land)

 

01/21/00 

Inst. of S-TEC System 30 Two Axis Autopilot ST-810-30 (14v) - Maule Dwg 9197A

(Sea)

 

01/21/00 

Inst. of S-TEC System 50 Two Axis Autopilot ST-609-50 (

28v

) - Maule Dwg 9200A

02/14/00 

Inst. of S-TEC System 55 Two Axis Autopilot ST-620 (14v) - Maule Dwg 9196A

(Land)

 

04/04/00 

Inst. of S-TEC System 55 Two Axis Autopilot ST-620 (14v) - Maule Dwg 9196A

 (Sea)

 

04/04/00 

10 

Inst. of S-TEC System 20 Single Axis Autopilot ST-810-20 (14v) - Maule Dwg 9197A

(Land)

 

03/20/00 

11 

Inst. of S-TEC System 20 Single Axis Autopilot ST-810-20 (14v) - Maule Dwg 9197A

(Sea)

 

03/20/00 

12 

Inst. of S-TEC System 20 Single Axis Autopilot ST-820-20 (

28v

) - Maule Dwg 9201A

03/20/00 

13 

Inst. of S-TEC System 40 Single Axis Autopilot ST-418-40 (14v) - Maule Dwg 9193A

10/29/01 

14 

Inst. of S-TEC System 40 Single Axis Autopilot ST-609-40 (

28v

) - Maule Dwg 9200A

10/29/01 

Inst. of S-TEC System 20 Single Axis Autopilot ST-872-20 (

28v

) - Maule Dwg 9211A

(Land)

  06/25/01 

Inst. of S-TEC System 30 Two Axis Autopilot ST-872-30 (

28v

) - Maule Dwg 9211A

(Land)

 

06/25/01 

Inst. of S-TEC System 20 Single Axis Autopilot ST-872-20 (

28v

) - Maule Dwg 9211A

(Sea)

 

06/25/01 

Inst. of S-TEC System 30 Two Axis Autopilot ST-872-30 (

28v

) - Maule Dwg 9211A.  

(Sea)

 

06/25/01 

Inst. of S-TEC System 50 Two Axis Autopilot ST-418-50 (14v) - Maule Dwg 9193A.  Rev. A 

10/14/04 

Inst. of S-TEC System 20 Single Axis Autopilot ST-873-20 (14/

28v

) - Maule Dwg 9212A

10/15/01 

Inst. of S-TEC System 30 Two Axis Autopilot ST-873-30 (14/

28v

) - Maule Dwg 9212A.  

10/15/01 

Installation of Apollo MX20 Multi-Function Display - Maule Drawing 7265A. 

08/15/02 

Installation of GARMIN GNS-430 (GPS/NAV/COMM) System - Maule Dwg 7205A

01/03/01 

Installation of GARMIN GNC-300XL (GPS/COMM) System - Maule Drawing 7207A

01/03/01 

Installation of GARMIN GNC-250XL (GPS/COMM) System - Maule Drawing 7209A

01/03/01 

Installation of Bendix-King KLX-135A (GPS/COMM) System - Maule Drawing 7219A

01/03/01 

Installation of GARMIN GNC-420 (GPS/COMM) System - Maule Drawing 7251A

06/30/03 

Installation of GARMIN GNS-530 (GPS/NAV/COMM) System - Maule Drawing 7253A

06/30/03 

Installation of GARMIN GTX-330 Mode S Transponder Traffic Information System (TIS) 
Maule Drawing 7255A

06/30/03 

Operation of aircraft when Micro AeroDynamics Vortex Generator System is installed in 
accordance with Maule Drawing 9177A

12/16/05 

 
 
 

Summary of Contents for MX-7-180B

Page 1: ...HIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES FAA APPROVED ____________________________________ Manager Aircraft Certification Office Federal Aviation Administration Atlanta Georgia USA DATE...

Page 2: ...ons Placard from page 6 Deleted Fuel Capacity numbers from Fuel Transfer Pump Switch Placard and added note for Tank Configuration Parking Brake OFF to 3 2 D BEFORE TAKEOFF Added Unusable Fuel weight...

Page 3: ...PI EDM 900 930 ______________________________ Manager Southeast Flight Test Section AIR Atlanta GA Date _____________________________ Corrected Max Weight and C G Limits from 2400 to 2500 lbs Correcte...

Page 4: ...8 40 14v Maule Dwg 9193A 10 29 01 14 7 Inst of S TEC System 40 Single Axis Autopilot ST 609 40 28v Maule Dwg 9200A 10 29 01 4 Inst of S TEC System 20 Single Axis Autopilot ST 872 20 28v Maule Dwg 9211...

Page 5: ...ts 8 3 3 Normal Flight Operations 11 3 4 Door Off Operation 13 3 5 Noise Level 13 3 6 Anti Collision Light 13 SECTION IV EMERGENCY PROCEDURES 4 1 Emergency Basic Rules 14 4 2 Engine Emergency Shut Dow...

Page 6: ...ment Change Sheet 24 Required Equipment List Provided for each Airplane SECTION VI AIRCRAFT SERVICING HANDLING AND MAINTENANCE 6 1 Introduction 25 6 2 Airplane Inspection Period 25 6 3 Preventive Main...

Page 7: ...MAULE AEROSPACE TECHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE MX 7 180B SECTION I GENERAL Page 1...

Page 8: ...atum Wing Leading Edge It is the responsibility of the pilot to assure that the airplane is property loaded Refer to the Weight and Balance Data for baggage cargo loading recommendations and loading C...

Page 9: ...d Airspeeds IAS AIRSPEED INDICATOR MARKINGS 161K 185 mph Yellow Arc Caution Range 129 161K 149 185 mph Green Arc Normal Operating Range 53 129K 61 149 mph White Arc Flap Operating Range 41 85K 47 98 m...

Page 10: ...g Limit 500 F Oil Temperature Green Arc Normal Operating Range 140 F 245 F Red Radial Operating Limit 245 F Oil Pressure Green Arc Normal Operating Range 55 to 95 PSI Yellow Arc Caution Range 25 to 55...

Page 11: ...is airspeed is not marked on the airspeed indicator The following placards are in the cockpit in clear view of the pilot MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN COMPLIANCE WITH THE OPERATING...

Page 12: ...BOTH RIGHT GAL The following placard is located on the instrument panel at the optional auxiliary tank transfer FUEL TRANSFER PUMPS PUSH FOR AUX QUANT PUSH FOR AUX QUANT LEFT RIGHT 900 930 units are i...

Page 13: ...ECK HINGES CONTROL ATTACHMENTS Top CHECK FOR WRINKLES AS INDICATION OF INTERNAL DAMAGE Left Wing Main Fuel Tank Drain Left Wing Aux Fuel Tank Drain if installed DRAIN 1 DRAIN 1 Left Wing Tip Nav Light...

Page 14: ...R Right Stabilizer CHECK ATTACHMENT POINTS STRUT Right Elevator CHECK HINGE POINTS Rudder CHECK HINGE POINTS CONTROL ATTACHMENT NAV LIGHT Tailwheel CHECK FOR INFLATION ATTACHMENTS REMOVE TIEDOWN Left...

Page 15: ...D ALT SWITCHES TURN OFF AND EXIT AIRCRAFT After Starting CHECK OIL PRESSURE IF OIL PRESSURE DOES NOT EXCEED 25 PSI WITHIN 30 SECONDS SHUT DOWN ENGINE Alternator CHECK CHARGING Radios other electrical...

Page 16: ...REEDOM AND PROPER TRAVEL Mixture Control FULL RICH Control FULL INCREASE RPM Carburetor Air Control PUSH COLD Engine Instruments RECHECK IN NORMAL RANGE Radios AS DESIRED Altimeter SET Attitude Indica...

Page 17: ...ng Flap Settings are available Flap Handle Position Flap Position Handle Full Down 7 First Notch 0 Second Notch 24 Third Notch 40 Fourth Notch 48 RECOMMENDED FLAP SETTINGS Flap settings are given in n...

Page 18: ...TALL WARNING LIGHT IS INOPERATIVE WHEN THE BATTERY SWITCH IS OFF LANDINGS TAKEOFFS trated crosswind component is 10K 12 mph and flap extension should be limited to 0 fully retracted with such crosswin...

Page 19: ...h front doors are installed with the rear passenger door or rear passenger and baggage doors off When doing so observe the following additional limitations Maximum airspeed 109K 125 mph Maximum bank a...

Page 20: ...EROSPACE TECHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE MX 7 180B EMERGENCY PROCEDURES EMERGENCY BASIC RULES To assist the pilot when an emergency occurs three basic rules are established which apply to...

Page 21: ...93 Rev D dated MAULE AEROSPACE TECHNOLOGY INC SECTION IV AIRPLANE FLIGHT MANUAL EMERGENCY PROCEDURES MAULE MX 7 180B ENGINE FAILURE AFTER TAKEOFF OR FORCED LANDING Establish 72K 83 mph IAS with flaps...

Page 22: ...ery altitude Notify appropriate controlling agency if appropriate Determine control difficulty airspeed by slowing down while flying straight ahead Do not allow the aircraft to stall Make full stop la...

Page 23: ...rly The empty weight empty weight center of gravity and useful load are listed below for this airplane as delivered from the factory If the airplane has been aircraft log and or aircraft records for t...

Page 24: ...th the tailwheel elevated to place the airplane in approximately the flight attitude Place a level on the leveling mark and leveling lug on the bottom of the right wing near height of the tailwheel un...

Page 25: ...es b Moment inch pounds W x C G i e Moment _____________ x ____________ ___________inch lbs EXAMPLE OF WEIGHT AND BALANCE CALCULATION FOR LOADED AIRCRAFT An airplane with an empty weight of 1383 lbs a...

Page 26: ...MAULE AEROSPACE TECHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE MX 7 180B SECTION V WEIGHT AND BALANCE FORM 63 PAGE 20...

Page 27: ...MAULE AEROSPACE TECHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE MX 7 180B This page 21 has been deleted by revision C FORM 63 PAGE 21 SECTION V WEIGHT AND BALANCE...

Page 28: ...MAULE AEROSPACE TECHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE MX 7 180B SECTION V WEIGHT AND BALANCE FORM 63 PAGE 22...

Page 29: ...MAULE AEROSPACE TECHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE MX 7 180B SECTION V WEIGHT AND BALANCE FORM 63 PAGE 23...

Page 30: ...RM MOMENTS Previous Aircraft Empty A New Empty Weight ______________________lbs B New Empty Center of Gravity ______________ins C New Empty Weight C G Moment ___________in lbs D New Useful Load ______...

Page 31: ...rator is responsible for Airworthiness Directives AD that may be issued from time to time Reference should be made to FAR 91 and FAR 43 requirements for properly certified agency or personnel to accom...

Reviews: