P68 & P68B VICTOR FLIGHT MANUAL
PARTENAVIA P-68 B · Weight & Balance
Overview
This document is an appendix to the R.A.I. Approved Flight Manual for the Partenavia P-68 B aircraft, detailing maximum take-off and landing weight increases. It includes weight limits, center of gravity limits, and airspeed limitations relevant to the aircraft's operation.
- Maximum Take-off Weight: 4387 Pounds (1990 Kilograms)
- Maximum Landing Weight: 4167 Pounds (1890 Kilograms)
- Aft Center of Gravity Limit: 20.7 Inches
- Forward Center of Gravity Limit: 13.03 Inches at maximum weight
- Maneuvering Speed (VA): 130 KIAS
- Performance data may be obtained from the basic Flight Manual
- Stall speeds vary with angle of bank and flap settings
- Best rate of climb speed is 90 KIAS
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at alfako.be. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Weight & Balance
- Year ·
- 1979
- File size ·
- 523 KB
- Copy found at ·
- alfako.be
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Maximum landing weight (lb) ·
- 4167
- Maximum takeoff weight (lb) ·
- 4387
Performance
- Stall speed 0 deg kias ·
- 66
- Stall speed 15 deg kias ·
- 63
- Stall speed 35 deg kias ·
- 61
- Best rate of climb speed kias ·
- 90
V-speeds
- VA_KIAS ·
- 130
Weight & balance
- Aft cg limit (in) ·
- 20.7
- Forward cg limit (in) ·
- 13.03
What is the P68 & P68B VICTOR FLIGHT MANUAL?
The P68 & P68B VICTOR FLIGHT MANUAL is a weight & balance for the PARTENAVIA P-68 B, dated 1979.
What year was the P68 & P68B VICTOR FLIGHT MANUAL published?
The P68 & P68B VICTOR FLIGHT MANUAL — the PARTENAVIA P-68 B weight & balance on file — is dated 1979.
Common. More common than 89% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the PARTENAVIA P-68 B.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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In this document
General
This section outlines the maximum take-off and landing weights for the aircraft and states that this appendix overrides the basic Aircraft Flight Manual in case of conflicts.
Limitations
Details airspeed limitations including the maneuvering speed and weight and center of gravity limits for safe operation.
Performance
Notes that performance data not included in this appendix can be found in the basic Flight Manual and provides stall speeds under various conditions.
Weight and Balance
Specifies weight limits and center of gravity limits necessary for safe flight operations.
Emergency Procedures
No changes are noted in this section.
Normal Procedures
No changes are noted in this section.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
P68 & P68B VICTOR FLIGHT MANUAL Appendix P/N NOR10.708-1 R.A.I. Approval No. 156014/T dated 23rd April 1979 Page 1 of 6 APPENDIX FOR MAXIMUM TAKE-OFF AND LANDING WEIGHT INCREASES SECTION 1 – GENERAL This appendix must be attached to the R.A.I. Approved Flight manual when the aircraft is operated at the following weights: a. Maximum Take-off: 4387 Pounds (1990 Kilograms) b. Maximum Landing: 4167 Pounds (1890 Kilograms) For Limitations, Procedures and Performance data not contained in this appendix, consult the basic Aircraft Flight Manual. NOTE: The Limitations, Performance Data and Information in this appendix must be considered as overriding the basic Aircraft Flight Manual where there is any conflict between the Appendix and Flight Manual. SECTION 2 – LIMITATIONS AIRSPEED LIMITATIONS a. Manoeuvring Speed, VA ………………………………………………………………………. 130 KIAS (126 KCAS) P68 & P68B VICTOR FLIGHT MANUAL Appendix P/N NOR10.708-1 R.A.I. Approval No. 156014/T dated 23rd April 1979 Page 2 of 6 WEIGHT AND CENTRE OF GRAVITY LIMITS Weight Limits: a. Maximum Take-off Weight: 4387 Pounds (1990 Kilograms) b. Maximum Landing Weight: 4167 Pounds (1890 Kilograms) Centre of Gravity Limits: a. Aft Limit: 20.7 Inches /34% M.A.C.) Aft of Datum at all weights b. Forward Limits: 13.03 Inches (21.4% M.A.C.) Aft of datum at 4387 Pounds 10.20 Inches (16.8% M.A.C.) Aft of datum at 3527 Pounds or less with straight line variation between these points. Datum Location is at the Wing Leading Edge. FIGURE 2-1 P68 & P68B VICTOR FLIGHT MANUAL Appendix P/N NOR10.708-1 R.A.I. Approval No. 156014/T dated 23rd April 1979 Page 3 of 6 SECTION 3 – EMERGENCY PROCEDURES No Changes SECTION 4 – NORMAL PROCEDURES No Changes SECTION 5 – PERFORMANCE NOTE: The Performance Data not included in this Appendix, may be obtained from Performance Charts in the basic Flight Manual, by extrapolating the variation with weight up to 4387 pounds. STALL SPEEDS CONDITIONS: 1. Throttle – IDLE 2. MAXIMUM take-off Weight – 4387 Pounds. ANGLE OF BANK 0° 20° 40° 60° FLAPS KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS 0° 66 65 68 67 76 74 95 92 15° 63 61 65 63 73 70 90 86 35° 61 58 63 59 69 65 85 80 P68 & P68B VICTOR FLIGHT MANUAL Appendix P/N NOR10.708-1 R.A.I. Approval No. 156014/T dated 23rd April 1979 Page 4 of 6 RATE OF CLIMB – MAXIMUM CLIMB CONDITIONS: 1. 2700 RPM and Full Throttle 2. Mixture – FULL RICH up to 5000 feet. At higher altitude, lean for smooth operation. Do not exceed 435 °F (224 °C) C.H.T. 3. Flaps – UP 4. Best rate of Climb Speed – 90 KIAS P68 & P68B VICTOR FLIGHT MANUAL Appendix P/N NOR10.708-1 R.A.I. Approval No. 156014/T dated 23rd April 1979 Page 5 of 6 RATE OF CLIMB – SINGLE ENGINE CONDITIONS: 5. 2700 RPM and Full Throttle 6. Mixture – FULL RICH up to 5000 feet. At higher altitude, lean for smooth operation. Do not exceed 435 °F (224 °C) C.H.T. 7. Flaps – UP 8. Best rate of Climb Speed – 88 KIAS P68 & P68B VICTOR FLIGHT MANUAL Appendix P/N NOR10.708-1 R.A.I. Approval No. 156014/T dated 23rd April 1979 Page 6 of 6 SECTION 6 – WEIGHT AND BALANCE CENTER OF GRAVITY MOMENT ENVELOPE