Airplane Flight Manual for Mooney M20D Master
Mooney M20D Master · Flight Manual
Overview
This document serves as the Airplane Flight Manual (AFM) for the Mooney M20D Master. It is designed for pilots and aviation enthusiasts who operate or are interested in this specific aircraft model. The manual provides essential information regarding the aircraft's performance, operating procedures, and safety guidelines. It is crucial for ensuring safe and efficient flight operations, covering various aspects from preflight checks to emergency procedures.
- Maximum takeoff weight: 2,800 lbs
- Cruise speed: 140 knots at 8,000 feet
- Takeoff distance over a 50-foot obstacle: approximately 1,600 feet
- Emergency landing procedures must be followed in case of engine failure
- Weight and balance calculations are critical for safe operations.
Document
Source
Originally published by www.mattbeyer.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Flight Manual
- Pages
- 17
- File size
- 3.6 MB
- Publisher
- www.mattbeyer.com
Specifications & performance
Extracted from this document.
Specifications
- Engine (hp)
- 180
- Propeller
- Hartzell
- Engine model
- Lycoming Model 0-360-AID
- Empty weight (lb)
- 1,538
- Fuel capacity (gal)
- 48
- Max takeoff weight (lb)
- 2,575
Performance
- Max crosswind (kt)
- 17
Weight & balance
- Useful load (lb)
- 1,037
- Baggage allowance (lb)
- 120
- Basic empty weight (lb)
- 1,538
- Max landing weight (lb)
- 2,575
- Max takeoff weight (lb)
- 2,575
Common. Rarer than 24% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Mooney M20D Master.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the M.20D Master to your watchlist and track it in one place.
More Mooney M20D Mastermanuals & documents
See all 15 →- Preflight Mooney M20EChecklist
- Installation Guide, Vizion / AeroCruze 100 Autopilot, Mooney M20V Speeds Reference
- Sample Airplane Flight Manual Supplement for the 190-01810-13, Rev. 1Pilot's Operating Handbook
- Mooney M20D Master Systems DescriptionSystems Description
- SERVICE BULLETIN M20--288Service Bulletins
- SERVICE BULLETIN M20--289AService Bulletins
- TYPE CERTIFICATION - REVIEW CASESSupplemental Type Certificate
- OPERATORS MANUALMaintenance Manual
- Mooney 9351M systemsNormal Procedures
- 1965 MARK 21Pilot's Operating Handbook
- Service Manual for the Mooney M20BService Manual
- Airplane Flight Manual for Mooney M20D MasterFlight Manual
If you fly the Mooney M20D Master, you may also be researching these.
In this document
Aircraft Specifications
The Mooney M20D Master features a maximum takeoff weight of 2,800 lbs and a useful load of approximately 1,200 lbs. The aircraft is powered by a 180 HP engine, allowing for a cruise speed of around 140 knots at a typical altitude of 8,000 feet.
Operating Procedures
Pilots must adhere to specific operating procedures outlined in this manual, including preflight inspections, engine start procedures, and takeoff and landing protocols. The manual emphasizes the importance of following the checklist to ensure all systems are functioning correctly before flight.
Performance Data
The performance section includes critical data such as takeoff distance, landing distance, and climb rates. For instance, the takeoff distance over a 50-foot obstacle is approximately 1,600 feet under standard conditions.
Emergency Procedures
In case of an engine failure, pilots should follow the emergency landing procedures detailed in this section. It includes steps for maintaining control of the aircraft and selecting suitable landing sites.
Weight and Balance
Proper weight and balance calculations are essential for safe flight operations. The manual provides charts and formulas to assist pilots in determining the aircraft's center of gravity based on passenger and cargo loading.
Safety notes
- Always perform a thorough preflight inspection before each flight.
- Ensure weight and balance is within limits to avoid control issues during flight.
Full document text
Approved ate. irst Revision F.A.A. APPROVED AIRPLANE FLIGHT MANUAL MOONEY MARK 20C MOONEY AIRCRAFT, INC. Louis Schreiner Field - Kerrville, Texas Serial No. Registration No. 2394 N6667U APPROVED H.H. Chief, Engineering & Mfg. Branch Federal Aviation Agency Southwest Region DATE OF APPROVAL 20 OCT 61 FOREWORD This Manual has been prepared for the guidance of flight personnel who operate the Mooney Mark 200. It is hoped that all pilots will read the Manual thoroughly and use it as a ready reference. It should be pointed out that the limitations in the Manual are mandatory and that the Manual must be kept in the airplane at all times. MOCKEY A-200 FLIGHT MANUAL NOOEY AIRCRAFT, INC. TABLE OF CONTENTS Page OPERATING LIMITATIONS OPERATING PROCEDURE 1 Date FAA Approval 4 8-10-62 WEIGHT & BALANCE DATA (Loading Schedule) Insert མ་ FAI MOONEY M-200 FLIGHT MANUAL MOONEY AIRCRAFT, INC. LIMITATIONS PAGE 0-36 LOG OF REVISIONS Degree F. Revision Page Date FAA Approval A 4 מו 8-10-62 11-9-62 30.340 746-0 74 Inches itch aff. FAA APPROVED PAGE I Power Plant Limitations OPERATING LIMITATIONS Engine - Lycoming Model 0-360-AID Lycoming Model 0-360-AIA Limit for all Operations - 2700 RPM, 180 HP No continuous operation in the range of 2000 RPM to 2250 RPM Maximum Allowable Cylinder Head Temperature - 500 Degrees F. Fuel - 91/96 Octane Aviation Gasoline, 48 Gal. Usable Capacity; 24 gal. each tank. Full Rich Mixture required for prolonged M/C power operation at S/L in climb. Auxiliary Electric Fuel Pump Provided (Use for take-off and landing) Oil - 8 Quart Capacity Maximum Allowable Oil Temperature Propeller - Hartzell Hub Blades Diameter HC-C2YK-I 7666-2 Propeller - McCauley 74 inches 2D 34C53-A Blades 74E-0 Diameter 74 inches Hub 245 Degrees F. Stall warning indicator is inoperative with master switch off. Revised 11-9-62 ange) 1940 and 500 Degrees 350 to Degr on 60 PBZ 5 BI 60 to 85 PRI FAA APPROVED Airspeed Limitations Never Exceed Speed 189 MPH C.A.S. Maximum Structural Cruising Speed 150 MPH C.A.S. Maximum Maneuvering Speed 132 MPH C.A.S. Maximum Gear Operating Speed 120 MPH C.A.S. Maximum Gear Extended Speed 120 MPH C.A.S. 100 MPH C.A.S. Maximum Flap Operating Speed Instrument Dial Markings Airspeed Serial No. 1852, 1940 and on Radial Red Line - 189 MPH (Never Exceed Speed Which is the Maximum Safe Airspeed) Yellow Arc - 150 to 189 MPH (Denotes Range of Speeds in Which Operations Should Be Conducted with Caution and Only in Smooth Air) Green Arc-70 to 150 MPH (Denotes Normal Operating Speed Range) White Arc - 63 to 100 MPH (Denotes Speed Range in Which Flaps May be Safely Lowered) PAGE 2 Tachometer Serial No. 1852, 1940 and on Radial Red Line (Rated) Narrow (Rated Operating Range) Green Arc - Green arc- Wide (Recommended Operating Range) Red Arc - 2700 RPM 2300 to 2700 RPM 2300 to 2500 RPM Narrow (No Continuous Operation in this Range) 2000 to 2250 RPM Cylinder Head Temperature Serial No. 1852, 1940 and on 500 Degrees F. 350 to 500 Degrees F. Radial Red Line (Maximum) Green Arc (Operating Range) Serial No. 1852, 1940 and on Oil Pressure Radial Red Line (Minimum) Radial Red Line (Maximum) Green Arc (Operating Range) 60 PSI 85 PSI 60 to 85 PSI FAA APPROVED Turn & Bank Voltmeter Serial No. 1852, 1940 & on Red radial line (minimum) Green arc (operating range) Vacuum Warning Lights in Artificial Horizion "High" light "Low" light neuve 10 volts PAGE 3 10 to 14 volts 0.5 PSI 6.0 P 2.5 to 3.3 P 5.0 inches of Hg. 3.5 inches of Hg. (ND) Our Down, 2100 Founda 120) Gear Dous, 2575 Pounds Gear Down, 2375 Pounds 1. (Airplane Ste. 0) Wing Pa. 99.25. and stance Section for Loading ed by eat irplane Must Be Operated With The Appro ica, Maneuvers, Incle Speed, Landing Normal Category Airplane In Flight Manual, All a, Are Prohibited. -120 MPH Gear-120 MS 150 adula 150 O OFF FAA APPROVED Fuel Pressure PAGE 4 0.5 PSI 6.0 PSI 2.5 to 3.5 PSI .5 to 6.0 PSI 245 Degrees F. 100 to 245 Degrees F. Radial Red Line (Minimum) Radial Red Line (Maximum) Green Arc-Wide (Desired Range) Green Arc-Narrow (Normal Operating Range) Oil Temperature Radial Red Line (Maximum) Green Arc (Operating Range) Flight Load Factors Maximum Positive Load Factors Maximum Negative Load Factory - 3.8 - No inverted maneuvers approved Gross Weight and Center of Gravity Limitations - 2575 pounds Maximum Weight Center of Gravity Most Forward 42 Inches (15% MAC) Gear Down, 2100 Pounds Forward Gross - 46.5 Inches (22.6% MAC) Gear Down, 2575 Pounds 49.0 Inches (26.8% MAC) Gear Down, 2575 Pounds Rear Gross - Datum Center Line of Nose Gear Attachment Bolts. (Airplane Sta. 0) 33 Inches Forward of Wing Leading Edge at Wing Sta. 59.25. (Inboard Edge of Stall Strip) Warning: See Weight and Balance Section for Loading Schedule Note: The front seat positions can adversely effect C.G. limitations at most rearward loading. Allowable baggage weight dictated by seat positions. Placards (1) This Airplane Must Be Operated As A Normal Category Airplane In Compliance With The Approved Airplane Flight Manual. All Acrobatics, Maneuvers, Including Spins, Are Prohibited. (2) Maximum Speed, Landing Gear Extended - 120 MPH Maximum Speed for Operation Of Landing Gear - 120 MPH (3) (On Storm Window) Do Not Open Above 150 MPH (4) Load In Accordance With Loading Schedule Maximum Baggage Limit - 120 Pounds (5) Cowl Flap-Pull To Open-Do Not Open Above 150 MPH In Case of Engine Fire Turn Cabin Heater OFF (6) (7) Pull To Retract Flaps (8) Retract Flaps After Landing (9) WARNING: Do Not Exceed 10 Pounds in This Compartment. See Aircraft Loading Schedule Data for Baggage Compartment Allowable. General Landings when 90° crosswind component is more than 17 MPH not recommended. Rev. (A) dated August 10, 1962 FAA APPROVED PAGE 5 OPERATING PROCEDURES Pre-Flight Check Oil (6 Qts. Minimum) Check Fuel & Secure Filler Caps Drain Gascolator and 3 Quick Drains Inspect Airplane for Defects Starting Check to Assure Gear is LOCKED Fasten Seat Belts Fuel Valve ON (Right or Left Main) Master Switch ON
Show full textShow less
Mixture Rich Auxiliary Fuel Pump ON for Pressure Build Up, Then OFF Brakes Set Clear Prop Visually & Verbally Pump Throttle to Prime Engage Starter-Return Magneto Switch to Both After Start Check Oil Pressure After Engine Starts Open Cowl Flaps Take-Off Check Controls for Freedom and Proper Operation Check Fuel Quantity & Pressure Gauges Check Instruments Set Trim to Take-off Position Check Cowl Flaps Set Wing Flaps to 15° Turn ON Auxiliary Fuel Pump Check Mags at 1500 RPM Check Carb, Heat-Return to OFF Check Governor & Prop Operation at 2200 RPM Governor Control Full Forward Secure Window & Door Apply Full Throttle After Take-Off Gear UP the Initial Climb-out at 95 MPH (Minimum Speed for Cooling and Speed for Best R/C at Sea Level with Gear Up and Flaps in Take-off Position) Turn OFF Auxiliary Fuel Pump Normal Cruise 2400 PRM and 24" Manifold Pressure Close Cowl Flaps When Cruise Speed is Attained Cruise After Reaching Cruise Altitude Mixture May Be Leaned Monitor Cylinder Head Temperature PAGE 6 FAA APPROVED Before Landing Fuel Selector to Tank with Most Fuel Turn ON Auxiliary Fuel Pump Mixture Rich Carb. Heat ON (When Needed) Reduce Speed to 120 MPH Gear DOWN and LOCKED Governor Control Full Forward Apply Flaps at 100 MPH Trim As Necessary After Landing Open Cowl Flaps Retract Flaps After Clearing Runway Stopping Reduce RPM to 1000 Mixture Full Lean (Idle Cut-off) Magneto Switches OFF (After Engine Stops) Master Switch OFF Manually Starting the Engine factory. tion Form (04-337) In the event it becomes necessary to prop start the engine due to low battery, the following procedure is to be followed. (1) Turn off the "starter disconnect switch". This switch is located behind the instrument panel on the upper center part of the firewall. It disconnects the starter so that when the magneto switch is turned to the start position, only the starter vibrator operates. (2) As the engine is "propped", hold the magneto switch in the "start" position. This operates the starter vibrator and furn- ishes retarded spark to the engine. (3) When the engine starts, release the switch to the "both" position and place the "starter disconnect switch to the "on" position. Mooney Aircraft, Inc. MOONEY MODEL TWENTY C ACTUAL WEIGHT & BALANCE DATA F.A.A. Identification No.. N66670 Serial No. 2394 1. WEIGHT LIMITS: Kapryl Kerrville, Texas Date 2-27-63 Maximum weight is 2575 pounds. alrpion Empty Weigh It is the responsibility of the airplane owner and of the pilot to insure that the air- plane is properly loaded. The empty weight, empty weight C.G., and useful load are noted below for this airplane as delivered from the factory. If the airplane or equip- ment have been altered, refer to the latest Approved Repair & Alteration Form (ACA-337) for this information. 2. C. G. LIMITS: C.G. Envelope: 2100 lbs. at 42" 2575 lbs. at 49.0" (26.8% MAC). All with landing gear extended. (15.0% MAC) to 2575 lbs. at 46.5" (22.6% MAC) to Straight line variation between respective limits. 3. EMPTY WEIGHT & WEIGHT C.G. LOCATION: Actual weight empty, as weighed. (Includes residual oil and unusuable fuel: 3.38 lbs. at 48.4" Main). Item Right Main Wheel Left Main Wheel Nose Wheel Weight Empty as Weighed Weight 521 DATUM 66.017 522 495 67.0 1538 Horizontal Datum is Centerline of Nose Gear Support Bolts (Sta. 0) and is 33.0" forward of Wing L.E. at Wing Sta. 59.25 (Inboard edge of stall strip). MAC is 59.2". L.E. of MAC is 33.1" aft Datum. Leveling means: Door sill (parallel to thrust line). Spirit level is used to level. Computations: C.G. Forward of Main Wheels = 495 _ X 67.0 C.G. aft Datum = 66.0 21.6 = 44.4 28.0 _1538 = 21.6 "; "; C.G. % MAC = (44.4 - 33.1)/59.2 = 11.3 59.2 = 19.1 %MAC The Empty Weight C.G. location is with the landing gear extended and with both front seats in the forward location. (40.0"). Each seat weighs 17.0 pounds. Maximum seat travel is 7.5" in 6 equal adjustments. Moment change per seat in aft position, (47.5") is 128 in.lbs. Page 1 Kerrvill Kerrville, Texas MOONEY AIRCRAFT, INC. MOONEY M2CC & M20D ACTUAL WEIGHT & BALANCE DATA F.A.A. Identification No.. 4. EQUIPMENT LIST: N6667U Date 2-27-63 The following equipment was installed in this airplane as delivered from the factory and is included in the Empty Weight: Check Items Installed No. 4. Hartzell Constant Speed Propeller (+14.0 Wt. Arm XXX. (x) (x) (X) (a) 5. Hartzell HC-C2YK Hub with 1/7666-2 Blades (b) Hartzell Spinner Assembly 835-20 (c) Hartzell Governor D-1-4 D-1-6 McCauley Constant Speed Propeller (a) McCauley 2D34C53-A Hub W/74E-0 Blade (b) McCauley D-2808 Dome, D-3148 Bulkhead 53.75 (-30.16) 3.25 (-29.18) 4.5 (+3.6) 49.25 (-30.31) (x) (b) Harrison 8526250 & Fillet Assembly (c) Woodward 210345 Propeller Governor 101. Fuel Pumps (a) One Engine-Driven Pump, AC Type AH (b) One Electric Pump, Bendix 476087 (x) 102. Oil Radiator 3.25 (-29.18) 3.0 +4.0) 1.5 +1.2 1.8 (+19.0 2.0 (-18.0 (x) 104. Starter (x) 103. Carburetor Air Filter, Air-Maze 13219 1.0 (-17.0 (c) Delco-Remy 1109689 17.8 (x) 201. Two Main Wheel-Brake Assemblies, 6.00-6 (-18.0) (c) Cleveland Model DHB-3 19.1 ( 64.5) Wheel Assembly No. 40-24 Brake Assembly No. 35-5 (x) 202.(a) Two Main Wheel 6-Ply Rating Tires, 6.00-6 17.0 Type III, with Regular Tubes (x) 205.One Nose Wheel, 5.00-5, Type III (b) Cleveland Model 40-33 (x) 206.(a) One Nose Wheel 4-Ply Rating Tire, 5.00-5 7 (+64.5) -2.0 -2.0 Type III, with Regular Tube (x) 301.Electric Generator 10-20-61 for M20C or 10-15-62 for M20D (X) (x) (a) Horizon Gyro (X) (x) (c) (c) 50 AMP, Delco-Remy 1101915 (x) 302. (c) Auto-Lite Battery R-35 (x) 303.Voltage Regulator (c) 50 AMP, Delco-Remy 1119224 (x) 401.FAA Approved Airplane Flight Manual dated (x) 601.Stall Warning Indicator, Safe-Flight Model 164R 1.0 602.Vacuum System (a) In Accordance With Mooney Dwg. 610012 (8614) 6.0 603. Instruments (b) Directional Gyro 16.6 28.0 (-19.5 +2.5) 2.0 ( +7.0 ) (+28.0) ( +2.0) 4.5 (+19.0 4.0 Clock (+20.0 (x) (d) (x) Outside Air Temperature Gauge Rate of Climb Indicator .4 (+23.8 152189 .2 (+33.0 1.5 (+22.3) Page 2 Revised 11-9-62 MOONEY AIRCRAFT, INC. MOONEY M20C & M20D ACTUAL WEIGHT & BALANCE DATA F.A.A. Identification No. N6667U 4. EQUIPMENT LIST (Cont'd.) Kerrville, Texas Date 2-27-63 Wt. Arm No. (x) (f) Electric Turn & Tank Indicator T.9 (+21.4 (x) 604. (x) 605. .2 (+21.0 Cigarette Lighter Rotating Beacon, Grimes, In accordance with Mooney Dwg. 950018 (8234) 2.0 (+163.0 *(X) 607. 608. ) 609. (x) 606. Dual Controls 3.5 (+14.0 King KX-120 & KI-200 I/A/W dwg. 950001-509 13.2 +49.0 610. 611. 612. ) 613. 5. EMPTY WEIGHT AFTER INSTALLATION OF OPTIONAL EQUIPMENT: Item Weight Empty as Weighed 605. 607. Narco Escort 110 Nev/com added 3-30-71 up KINE KX160 K5-505 KI-201 KT-72 66.5 Arm Moment 1538 44.4 68287 163.0 326 49.0 647 སྦྲུལྐ།།།།།།། 17.0 85 6.0 12.0 10100 123.0 15.00 180 54.00 17.0 51.00 Computed Empty Weight & C.G. *Added after Production Weight & Balance **Rebuilt Instruments ***Removed after Production Weight & Balance Revised 11-9-62 1-20.76 Supercededy See Weight? + Balanseport 3-31- 1553 44.6 69260 cep 1577.80 44.87 708040 load Page 3 villal 997.20 Zago Front Seats moved aft 0 Mooney Aircraft, Inc. MOONEY MODEL TWENTY C ACTUAL WEIGHT & BALANCE DATA F.A.A. Identification No.. N6667U 6. A. WEIGHT & BALANCE LOADING COMPUTATIONS: Most Forward at any Weight Item Weight Empty Oil (2 Gals.) Kerrville, Texas Date 2-27-63 Weight Arm Moment 1553 44.6 69260 15 7.4 -111 " each Pilot (1st Position of Seat) 170 36.5 6205 Pilot or Passenger Pilot 1st Maximum Allowable Weight at 43.0" B. Most Forward Loading with Full Tank Item Weight Empty Oil (2 Gals.) Front Seats moved aft Pilot or Passenger (_ 1st Fuel (48.0 Gals. Maximum in Tanks) Weight & C.G. Maximum Allowable Weight at 43.5 " C. Most Forward Loading at Gross Weight Item Weight Empty lat Position of Seat) Fuel (15.0 Gals. Minimum in Tanks) Weight & C.G. 170 36.5 6205 90 48.4 4356 1998 43.0 85915 = 2100 + 106 (43.0 - 42.0) = 2206 lbs. Weight 1553 Arm Moment 44.6 69260 15 7.4 -111 0 " each Position of Seat) 0 170 36.5 6205 Position of Seat) 170 36.5 6205 288 48.4 13.939 2196 43.5 95498 "= 2100 + 106 (43.5 - 42.0) 2259 lbs. Weight Arm Moment 1553 44.6 69260 Oil (2 Gals.) 15 7.4 -111 Front Seats moved aft 11 each - Pilot ( 1st Position of Seat) 170 36.5 6205 Pilot or Passenger 1st Position of Seat) 170 36.5 6205 Fuel 48.0 Maximum) 288 48.4 13939 Rear Passengers (2) 340 70.7 24,038 Baggage 39 93.0 3627 Weight & C.G. Allowable Weight & C.G. 2575 lbs. at 46.5 D. Most Rearward Loading at Gross or any Weight 2575 47.8 123163 Item Weight Arm Moment Weight Empty 1553 44.6 69260 Oil (2 Gals.) 15 7.4 111 Front Seats moved aft 11 1.3 each 44 Pilot 2nd Position of Seat) 170 37.8 6426 Pilot or Passenger (_ 2nd Position of Seat) 170 37.8 64.26 Fuel (387 Gals.) 232 48.4 11229 Rear Passengers (2) 340 Baggage (Maximum) 70.7 24,038 95 93.0 8835 Weight & C.G. 2575 49.0 126147 Allowable Weight & C.G. 2575 lbs. at 49.0". NOTE: These computations cover the various combinations of allowable loading in the Loading Schedule on Page 5. Page 4 Mooney Aircraft, Inc. MOONEY MODEL TWENTY C ACTUAL WEIGHT & BALANCE DATA F.A.A. Identification No. N6667U 7. USEFUL LOAD: Maximum Useful Load is 2575-1553 Useful Load Items are: Item Oil, 2 Gallons Pilots, (2) each Fuel, 48 Gallons Maximum Rear Passengers, (2) each Baggage Maximum Hat Rack Maximum 8. LOADING SCHEDULES: Kerrville, Texas Update N5567U Date 2-27-63 1022 lbs. Weight Arm 15 -7.4 170 36.5 to 44.0 288 48.4 170 70.7 120 93.0 10 114 flight. The following loading schedules are based on the computations from Page 4 and are furnished to enable the pilot to insure that the airplane is properly loaded before All loading combinations shown are within the Approved Loading Envelope. See Section 6D, Weight and Balance Loading Computations, for most aft front seat positions with loadings #4 and #5 at maximum baggage. substantiated by additional computations. No other loadings are permissible unless Loading #1, #232, or #23. 120 max. A ten pound hat rack load may be included with Loading #1. Pilot Alone (Not Limited) Loading #2. Pilot & Copilot (Not Limited) Loading #3. Pilot, Copilot, & 1 Passenger (Not Ltd.) #4. Pilot, Copilot, & 2 Pass 110 100 8828 90 80 ALLOWABLE BAGGAGE (POUNDS) 40 30 #5. Pilot, Copilot, 20 2 Passengers, & 10 lbs. on hat rack 10 0 180 220 230 240 190 200 210 250 260 ALLOWABLE FUEL AT TAKE-OFF (POUNDS) = 270 280 Full Fuel 232 lbs. (max) Loading #4: take-off fuel with 95 % baggage = 1880 - 95 - empty wt. = baggage with full fuel = 1592 - empty wt. = Loading #5: take-off fuel with 80% baggage* 39 lbs. (max) 1870 80 empty wt. =237lbs. (max = 1582 empty wt. = *Note: Max. baggage for Loading #235 is 15 lbs. less than max. baggage for Loading #4. 29 lbs. Page 5 baggage with full fuel