Duke Marquis Winglets - Royal Air Inc
CESSNA 310F · Training Manual
Overview
This document provides essential weight and balance information for the Beechcraft 60 Duke. It is intended for pilots and aviation personnel who need to ensure that the aircraft is loaded within its weight limits for safe operation. The document outlines the maximum weight capacities, loading procedures, and calculations necessary to maintain proper balance during flight. Understanding these parameters is crucial for flight safety and compliance with aviation regulations.
- Maximum takeoff weight: 4,500 lbs
- Ensure center of gravity is within limits for safe operation
- Follow loading procedures to maintain balance
Document
Source
Originally published by royalairinc.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Training Manual
- Pages
- 7
- File size
- 612 KB
- Publisher
- royalairinc.com
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In this document
Maximum Weight Limits
The Beechcraft 60 Duke has a maximum takeoff weight of 4,500 lbs. This section details the maximum weight for passengers, cargo, and fuel to ensure safe operation.
Loading Procedures
Proper loading procedures are outlined to ensure that the aircraft's center of gravity remains within limits. This includes guidelines on how to distribute weight among passengers and cargo.
Weight Calculation Examples
This section provides examples of how to calculate the total weight and balance of the aircraft based on various loading scenarios, ensuring pilots can make informed decisions before flight.
Safety notes
- Improper loading can lead to loss of control during flight
- Always verify weight calculations before flight
Full document text
Duke Marquis Winglets N277MC Shown left, Duke P-365 after completion of the BLR, Duke Mar- quis Winglet Modifica- tion. The Winglets.can be installed on either... dry or wet tip models and require 20-30 man hours to complete, plus paint. Flight test results have shown that the Duke Marquis Winglet 'installation will; Improve climb performance Improve cruise fuel efficiency... Reduce lift induced drag Lower stall speeds Lower Vmc Raise single engine ceiling. Improve stall characteristics Improve handling & stability Reduce takeoff & landing distance Look cool Winglets must be installed in conjunction with our Vortex Generator kit, and will be com pletely compatible with our new wet tips, when available. Boundary Layer Research, Inc. "Vortex Generator Specialists" Performance Plus™ Duko See reverse for performance improvements Below, a close up of. the winglet as installed" (note clean lines). The Winglet is constructed using the latest in com- posite technologies and incorporates a copper bonding screen for pro tection against lighting strikes. The Winglet is designed to withstand loads of 3 1/2 times flight test limits. BEECHCRAFT DUKE MARQUIS WINGLETS 60/A60/B60 PERFORMANCE SPECIFICATIONS Stock Baseline P-340 BLR Performance The BLR Difference Max. Ramp Wt. 6814 7039 +225 Gross Takeoff Wt. 6775 7000 +225 Min. SE Vmc - 85 72 -13 Min. SE-Flaps 15° N/A 67 N/A Stall clean Vs - 82 76 -6 Stall dirty- Vso 76 67 -9 Liftoff - Vlof 94 77 -17 Liftoff-Flaps 15° N/A 72 N/A ROC-Twin (fpm) 850 1200 +350 - ROC Single (fpm) 305 370 +65 Short Fld Approach 99 77 -22 TAS @ FL260 205 212 +7 Speed shown in KIAS Weight shown in pounds Notes: 1. Company test data and FAA-Approved numbers. See AFMS for certified performance. 2. Stall speeds are certified at new gross weight, forward CG and zero thrust. 3. Vmc is certified at light weight, aft CG and windmilling propeller. 4. Vlof=Vmc + 5 KIAS; Short Field = 1.15 x Vso & Vref = 1.3 x Vso at maximum landing weight. 5. Kit installation time is approximately thirty man-hours on wet tip airplanes, twenty man-hours on late-style dry tip airplanes, plus airspeed dial face change. Winglets not compatible with early style dry wing tips. 6. Kit includes comprehensive installation manual, FAA-Approved Flight Manual Supplement, 2 winglets, hardware, dial faces and all necessary documentation, including Supplemental Type Certificate (STC). 7. BLR gross weight increase vortex generator kit installation is required. 8. Funds quoted in US dollars, plus shipping & handling. FAA- & CAA-Approved STC#SA00112SE Complete Kit $10,750 TO 701 HIT 8046 1.02 BLR BOUNDARY LAYER RESEARCH, INC. BLR VORTEX GENERATOR TECHNOLOGY SAFETY PERFORMANCE ♦ PROFIT Vortex Generators have become the standard value-added performance modification in general, commercial and military aviation today Boundary Layer Research, Inc., is the industry leader in the design, testing and certification of this airflow technology and its associated benefits. Additionally, BLR is known for its exceptional worldwide customer service and dealer support. Discovered over 60 years ago by the British, the benefits of this airflow technology were brought to the commercial market in 1987. Most of the men and women on the engineering and flight test team which pioneered the practical application of this discovery are associated now with Boundary Layer Research. Company President Bob Desroche flew the first Baron-equipped prototype during its initial development, certified the majority of the models now available and is still designing, testing and certifying new models today. All kits consist of small highly engineered aluminum tabs that are glued onto the wing aft of the leading edge in very precise locations Installations on twin-engine aircraft incorporate VGs on the vertical tail for improved rudder authority and many kits utilize riveted strakes to improve the airflow around the engine nacelle and wing attach intersections. Various kits incorporate additional aft body strakes and/or small delta fins to create much needed airflow modification. Each model-specific kit is designed to optimize the airflow over the wing. The VGs energize the airflow by spinning it into tiny vortices which travel over the wing and compress the boundary layer. This compression delays the onset of a stall by forcing airflow separation further aft along the wing chord, thus allowing the wing to achieve a higher angle of attack before actual stall separation occurs. A pronounced stall buffet occurs as a result of controlled separation, and when complete separation does occur it is designed to be docile As a result of each kit's installation, operators realize immediate benefits. Many models receive a certified increase in useful loads, each receives much improved aileron response in all flight configurations especially leading into and throughout the stall, as well as a virtual elimination of Vmc for twins due to it's being reduced to or below the stall speed Low speed performance is achieved with no measurable loss of speed in cruise flight on properly rigged aircraft ⇒ Increased useful load (most models) > Elimination of Vme (most models) Increased aileron effectiveness in all flight configurations Shorter takeoffs and landings with steeper climbouts and approaches → Decreased tire and brake wear → No speed loss in cruise flight on properly rigged aircraft ⇒ Approved for known-icing aircraft Easy one-day installation No Weight and Balance revision required No additional maintenance required → FAA-Approved with an STC for each model 3125 100th St SW, Hangar C75-5 Everett, WA 98204 800-257 4847 CALL 1-800-257-4847 425-353 6591 fax 355 3045 MAY-07-98 16:02 AM BLE, INC. 425 355 3046 F.03 May 1998 BOUNDARY LAYER BLR RESEARCH, INC. Price List ENGINE-OUT WARNINGS SYSTEMS: Low Thrust Detector System Item# Model/Description/Highlights List Price STC# 101-1100 1 NEW 1.TDS - All Piston Twins - Notice of impending engine failure SA1007NW $2,995
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BEECHCRAFT SERIES: Vortex Generator Kits, Winglets, Wet Tips, Body Strakes, Accessories Item# BD IV BD IVW BD-1W BD-IW BD-1AR BD-1AS BD-18 BD IU BB IS BT IS Model/Description/Highlights Duke VG Kit - 8 knot reduction in Vmc Duke 190 Plus VG Kit - 190 lb. Gross Weight Increase Duke Marquis Winglets - Increased wing aspect ratio/Climb/Cruise NEW Duke Wet Tip Tank - 30 gallon usable fuel upgrade Duke Dual Aft Body Strakes - Increased Stability/Vmc reduction Duke Boarding Assist Strap Black, Gold Duke Spring Thing - Baggage Door Assembly Duke VG Kit Upgrade to Gross Weight Increase Baron Spring Thing Baggage Door Assembly - TravelAir Spring Thing - Baggage Door Assembly STC# List Price SA5273NM $1,950 SA5761NM $3,750 SA00112SE $9,750 SA00479S $15,000 SA00370SE $2,950 N/A $65 N/A $65 SA5761NM Call N/A $65 N/A $65 CESSNA SERIES: Operational Weight Increases, Gear Kits, Vortex Generator Kits, Skylights, Accessories Model/Description/Highlights NEW Conquest II 441 - 315 lb. Operational Weight Increases Golden Eagle 421C 129 lb. Gross Weight Increase Item# CC-2W STC# List Price SA00487SH $5,995 C-1\ SA00015SE $2,950 C-1V CAVA Golden Eagle 421B 129 lb. Gross Weight Increase (0201 and on) Golden Eagle 421, 42LA - 14 mph reduction in Vme SA00074SL $2,950 SA00329SE $1,750 C-2V Chancellor 414A 355 lb. Gross Wt. Incr. w/no Zero Fuel Wt. hrnut SA5672NM $2,950 C-35 414-40 lb. Ramp Weight Increase SA5900NM $1,995 C2V C-3V 402C 360 lb. Gross Weight Increase & 355 Lb. Zero Fuel Weight Incr. SA5673NM $2,950 402B 40 lb. Ramp Weight Increase SA5900NM $1,995 C-3VA 402, 402A - 40 lb. Ramp Weight Increase SA5900NM $1,995 C3VA 401, 401A, 401B - 40 lb. Ramp Weight Increase SA5900NM $1,995 C-4V 340A 315 lb. Gross Weight Increase & 230 lb. Zero Fuel Weight Incr. SA5198NM $2,950 C-4V 340 330 lb. Gross Weight Increase SA5198NM $2,950 CAVA C-5V 335 - 315 lb. Gross Weight Incr. & 230 lb. Zero Fuel Weight Increase 320E, 320F 279 lb. Gross Weight Increase SA5198NM $2,250 SA5757NM $1,995 C-5V 320D 274 lb. Gross Weight Increase SA5757NM $1,995 C-GV T310R 184 . Gross Weight Incr. & 385 lb. Zero Fuel Weight Incr. SA5163NM $2,495 C-6VA (2.7V 310R 150 lb. Gross Weight Increase & 360 lb. Zero Fuel Weight Incr. T310Q 184 lb. Gross Weight Increase SA5163NM $2,495 SA5756NM $2,495 3125 100th St. SW, Hangar C75-5 Everett, WA 98204 800-257 4847 425-353-6591 1. Ace 3042 TIMT-07 70702 HTT FLR TRE. BL BOUNDARY LAYER BLR RESEARCH, INC. Price List 439 955 8046 F.04 May 1998 CESSNA SERIES: Operational Weight Increases, Gear Kits, Vortex Generator Kits, Skylights, Accessories Model/Description/Highlights STC# List Price Item# C-7V 310Q 75 lb. Gross Weight Increase SA5756NM $2,495 C-7V T310P - 284 lb. Gross Weight Increase SA5756NM $2,495 C-7V 310K, 310L, 310N, 310P - 100 lb. Gross Weight Increase SA5756NM $2,495 C-8V 310-8 mph reduction in Vinc ST00049SH $1,200 C-8V 310D, 310F 3 mph reduction in Vmc ST00049SE $995 C-8V 310C 11 mph reduction in Vmc C-8V 310A, 310B - 9 mph reduction in Vmc C-8V 310 - 20 mph reduction in Vmc CS-18 300 & 400 Series - Nacelle Baggage Locker Springs C-9V C-9V C-10V C-ITT 100 Series Tooltote - Baggage Door Storage Unir C-1SLW C-1S C-1HI A185F - 5 knot reduction in stall speeds/Better roll response 180J, 180K 10 knot reduction in stall speeds/Better roll response 120, 140.5 mph reduction in stall speeds 100 Series Skylights - Overhead window kit - Greenhouse Style Spring Thing Baggage door assembly C-1CC Cabin Covers Exterior Protection - All models Headliners Various Styles/Colors · All models . ST00049SF. $995 ST00049SE $1,200 ST00049SF. $995 N/A $150 SA00165SE $1,495 SA00165SE $1,495 N/A Call N/A Call SA00123SE $495 N/A $99 SA4379NM Call N/A $65 DEHAVILLAND SERIES: Vortex Generator Kit Item#f Model/Description/Highlights DB IV DHC-2 Mk I Beaver - Greatly Improves Stall Characterishes List Price STC# SA00200SH $1,950 PIPER SERIES: Operational Weight Increases, Vortex Generator Kits, Landing Gear Kits Model/Description/Highlights STC# List Price Item# PC-1V PC-1G PN-IV PN1V Chieftain PA-31-350, T1020 - 368 lb. Gross Weight Increase VG Kit Chieftain PA-31-350, T1020 - 368 lb. Landing Weight Increase Navajo PA-31-325 C/R - 340 lb. Gross Weight Increase Navajo PA-31-310 - 340 lb. Gross Weight Increase SA00192SE $3,450 SA002025 $2,500 SA00048SE $3,950 SA00047SE $3,950 PN-1V CP.11 SA00047SE $3,450 SA00039SE $3,950 SA00202SE $2,500 CP-IN SA00038SE $3,950 SA00037SE $3,950 $1,000 Navajo PA-31-310 w/wing lockers 230 lb. Gross Weight Increase Panther II PA-31-350 200 lb. Gross Weight Increase PC-1GP Panther II PA-31-350 - 200 lb. Landing Weight Increase Panther I PA-31-325 C/R - 200 lb. Gross Weight Increase Panther PA-31-310 - 200 lb. Gross Weight Increase Colemill/BLR Panther - Upgrade existing VG Kit NEW Aerostar Spring Thing - Baggage door assembly Seneca III, IV PA-34-220T-3 knot reduction in Vinc Seneca II PA-34-2001' 168 lb. Zero Fuel Weight Increase CP 1\ C”-UP PA-IS PS-IV PS-IV Various N/A $65 SA00109ST. $2,950 SA00109SH $2,950 3125 100th St SW, Hangar C75-5 Everett, WA 98204 800 257-4847 425-353 8591 fax 355 3046 BLR BOUNDARY BOUNDARY LAYER RESEARCH, INC. Price List PIPER SERIES: Operational Weight Increases, Vortex Generator Kits, Landing Gear Kits Item# SC 1V SC-2V Model/Description/Highlights Super Cub PA-18, PA-19 - Shorter Landing/Eliminates "Moose Stall" Cruiser J-5, PA-12, PA-14 Shorter Landing/Eliminates "Moose Stall" PMA PARTS/REPLACEMENTS/SERVICE Item# • Model/Description/Highlights RK 1 VG Repaint Kit Complete replacement VG Kit VG Repair Kit Spare VGs, Glue, etc. RK-2 PUR-1 STC# May 1998 List Price SA00275SF $1,495 SA00467SE $1,495 STC# List Price PMA $250 PMA $100 1C01530 Documents/Paperwork Upgrades & Replacements. Delta Fin - Replacement parts Various Models N/A $150 Various $50 DFC-1 DFC-2 DFC-3 Dial Face Change - Per owner supplied instrument Piston Models Dial Face Change - Per owner supplied instrument Turbine Model, Dial Face Replacement parts New $100 New $120 New $50 CH2026-1 Torque Link Replacement - Gear Kit parts PMA $300 CH2021 1 Spacer Tube Replacement Gear Kit parts PMA $100 Various Low Thrust Detector System Heated Sensor Probes 102-2100-1 Low Thrust Detector System - Bench Test & Recalibrate 102-3100-1 Low Thrust Detector System Repair & Recalibrate 102-4100-1 Low Thrust Detector System - Exchange/Upgrade Unit N/A $500 PMA $375 N/A $145 N/A $295 Page 3 of 3 L 3125 100th St SW, Hangar C75-5 Everett, WA 98204 800 257-4847 425 353-659: fax 355 3046 27-50-00 Page 202 Nov 2/73 FLAP SETTINGS Approach 15° from Neutral Full Down- 30° from Neutral 1. Flap Motor Gearbox 2. Flap Shaft and Housing 3. Flap Actuator 4. Limit Switches BEECHCRAFT DUKE 60 SERIES MAINTENANCE MANUAL - FLAP SYSTEM for right 125 kits min 5000' runway For left 135k+ FLAP TRANSMITTER AND POSITION INDICATORS 3 DN- 1. Transmitter 2. Flap Actuator FLAP LIMIT SWITCHES TRANSIT 1. Down Limit Switch 2. Up Limit Switch 3. 14° Limit Switch *4. 16° Limit Switches 000 3. Indicator UP APH DN *4. Indicator Lights No flaps ina Furn Keep handon flap handle - Neverfill up or down -No flapinturn -Intermidate stop. TO ADJUST, LOOSEN MOUNTING BOLTS AND MOVE FORE AND AFT, OR ROTATE SLIGHTLY. Flap System Figure 201 *INDICATOR LIGHTS AND (2) 16° LIMIT SWITCHES ARE IN- STALLED ON SERIALS P-247 AND AFTER. 60-161-1A
What's in the CESSNA 310F TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.
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