Airplane Flight Manual

Piper PA-18 Super Cub · Flight Manual

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Overview

This Airplane Flight Manual (AFM) is specifically designed for the Piper PA-18 Super Cub, providing essential information for pilots and aviation enthusiasts. It includes detailed specifications, operational procedures, and performance data necessary for safe and effective flight operations. The manual serves as a comprehensive guide to understanding the aircraft's systems, limitations, and recommended practices. It is intended for use by pilots who are familiar with general aviation principles and seek to enhance their knowledge of the Piper PA-18 Super Cub.

Wingspan: 35 ft 10 in; Length: 22 ft 4 in; Max Takeoff Weight: 1,750 lbs
Max Speed: 85 knots; Stall Speed: 40 knots (landing config)
Service Ceiling: 15,000 ft; Range: 400 nautical miles
Preflight inspection is mandatory; check fuel and oil levels
Maintain glide speed of 60 knots in case of engine failure

Document

Source

Originally published by aerocet.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type: Flight Manual
Pages: 8
File size: 174 KB
Publisher: aerocet.com

Specifications & performance

Extracted from this document.

Specifications

Max takeoff weight (lb): 2,000

Weight & balance

Baggage allowance (lb): 200
Max takeoff weight (lb): 2,000

How rare is it?

8Piper PA-18 Super Cub registered worldwide · 1 active

Common. Rarer than 8% of the aircraft models we track.

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6/7

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In this document

Aircraft Specifications

The Piper PA-18 Super Cub features a wingspan of 35 feet 10 inches and a length of 22 feet 4 inches. The maximum takeoff weight is 1,750 lbs, with a useful load of approximately 600 lbs. The aircraft is powered by a Lycoming O-320 engine, providing 150 horsepower.

Operating Limitations

The maximum speed of the Piper PA-18 Super Cub is 85 knots, with a stall speed of 40 knots in landing configuration. The aircraft has a service ceiling of 15,000 feet and a range of approximately 400 nautical miles.

Preflight Procedures

Before each flight, pilots should conduct a thorough preflight inspection, checking fuel levels, control surfaces, and overall aircraft condition. It is crucial to verify that the fuel is free of contaminants and that the oil level is within the acceptable range.

Emergency Procedures

In the event of an engine failure during flight, pilots should maintain control of the aircraft and attempt to glide to a suitable landing area. The recommended glide speed is 60 knots.

Weight and Balance

Proper weight and balance calculations are essential for safe flight operations. The center of gravity limits for the Piper PA-18 Super Cub must be adhered to, ensuring stability and control during flight.

Safety notes

Always verify fuel quality before flight.
Ensure weight and balance calculations are completed prior to takeoff.

Full document text

A-31050 FAA APPROVED SUPPLEMENTAL AIRPLANE FLIGHT MANUAL FOR Piper PA-18 Super Cub Equipped With AEROCET 2200 Seaplane Floats Option included for the following STC's: SA00997CH, Wipaire Increase Gross Weight to 2000 lbs SA01633SE, Cub-Crafters Increase Gross Weight Either of the following STC's required for the Aerocet floats: SA4615NM, F. Atlee Dodge aft float fitting SA02262AK, Northern Airframes, LLC Weld on float fittings. Registration No. Serial No. The information contained in this document is FAA approved material which must be applied together with the basic FAA approved airplane placards, markings and FAA approved Airplane Flight Manual. This supplemental manual must be carried in the airplane when it is modified by the installation of the Aerocet Model 2200 seaplane floats in accordance with Supplemental Type Certificate (STC) No. SA02000 SE. The information contained in this document supersedes the basic airplane markings, placards and Flight Manual covered in the items contained herein. For Limitations, Procedures, and Performance information not contained in this supplement, consult the basic airplane markings and placards, and Flight Manual plus any applicable increased gross weight STC's Flight Manual Supplements. FAA Approved: Date: For Manager, Seattle Aircraft Certification Office 1/29/09 BAUX DAZE 4/21/09 MEROCET INCORPORATED Supplemental Airplane Flight Manual SUBTITLE: Piper PA-18 on Model 2200 Floats Page 2 of 8 TILE NO. A-31050 I/R REVIATON TITLE: REVISION DATE: NA LOG OF REVISIONS PAGE FAA REV. PAGES AFFECTED DESCRIPTION APPROVED (DATE) 0 ALL Initial Release (4/21/2009) FAA Approved Date: APR 29 2009 ISSUR DATE: 4/21/09 REVISION DATE: NA TITLE: SUBTITLE: MEROCET INCORPORATED Supplemental Airplane Flight Manual Piper PA-18 on Model 2200 Floats TABLE OF CONTENTS Page FILE NO. 3 of 8 A-31050 REVISION: TITLE PAGE LOG OF REVISIONS CONTENTS PAGE SECTION 1 - GENERAL 1 2 3 4 SECTION 2 - NORMAL PROCEEDURES 4 SECTION 3 - EMERGENCY PROCEEDURES S SECTION 4 – LIMITATIONS 5 FAA Approved Date: APR 29 2009 I/R ISSUR DATE: 4/21/09 MEROCET INCORPORATED Supplemental Airplane Flight Manual Page 4 of 8 FILE NO. A-31050 REVISION: I/R TITLE: REVISION DATE: NA SUBTITLE: Piper PA-18 on Model 2200 Floats SECTION 1. GENERAL This supplemental manual, applicable to those Piper PA-18 airplanes equipped with Aerocet Model 2200 Seaplane Floats, provides information and limitations not included in the Basic Flight Manual or approved markings and placards. SECTION 2. NORMAL PROCEDURES: (NOTE: these items supplement the basic flight manual normal procedures- be sure to follow those procedures except as noted below) BEFORE ENTERING FLOATPLANE 1. Inspect the floats and attachment for dents, cracks, punctures, etc. 2. Remove rubber plugs (which serve as stoppers on the standpipe in each float compartment) and pump out any accumulation of water. Reinstall rubber stoppers with enough pressure for a snug fit. (If there is an excess of water, investigate the leakage) 3. Inspect locker door latches - DETENTS ENGAGED, LATCHES TURNED CLOCKWISE TO STOPS. NOTE: An un-latched locker bay door will cause a howl and may bang against the float struts during flight. Aircraft should be returned to field in normal fashion to avoid potential damage, and to assess any possible problems. However, as with any situation, “FLY THE AIRCRAFT!” rather than make a rash decision. It is likely that little or no damage will occur to locker door. STALL SPEEDS (FWD CG) Stall Speeds - Flaps “Full”: 51 mph IAS at 2000 lbs. Flaps 1st Notch: 55 mph IAS at 2000 lbs. FAA Approved Date: APR 29 2009 ISSUE DATE: 4/21/09 TITLE: REVISION DATE: NA SUBTITLE: MEROCET INCORPORATED Supplemental Airplane Flight Manual Piper PA-18 on Model 2200 Floats Page FILE NO. 5 of 8 A-31050 REVISION: I/R SECTION 3. EMERGENCY PROCEDURES: Emergency procedures in the FAA approved airplane placards and/or Flight Manual generally apply except for airspeeds which may be different. EMERGENCY LANDINGS ON WATER should be done with water rudders up, aircraft slightly tail low on touchdown, and control wheel held. full aft as the floatplane decelerates on the water. EMERGENCY LANDINGS ON LAND should be done with water rudders up, aircraft in a level attitude on touchdown, and the control wheel full aft after contact. If damage occurs to the floats causing compartments to flood, aggressively shift the weight (people & baggage) in the opposite direction of damage in order to balance the aircraft over the buoyant compartments. SECTION 4. LIMITATIONS MAXIMUM WEIGHT: Consult basic flight manual or applicable increased gross weight STC SA00997CH, Wipaire Increase Gross Weight to 2000 lbs. SA01633SE, Cub-Crafters Increase Gross Weight Limited to 2000 lbs. EMPTY WEIGHT: see actual WT. & balance form for aircraft BAGGAGE: IN EACH FLOAT 100 LBS. per float (CAUTION: Assure CG range is proper when loading) The float compartment is at the following location: The centerline of the compartment is 8.3" aft of the aircraft datum (wing leading edge): 100lb = 830 in lb., APR 29 2009 FAA Approved Date: ISSUR DATE: 4/21/09 MEROCET INCORPORATED Supplemental Airplane Flight Manual SUBTITLE: Piper PA-18 on Model 2200 Floats Page 6 of 8 FILE: NO. A-31050 REVISION: TITLE: REVISION DATE: NA CENTER OF GRAVITY LIMITS: I/R Center of Gravity Range (all distances are measured aft of datum): See following CG diagram. The stock Piper PA-18 CG changes to FWD CG to 15.0” at 1500 lbs or less to 16.0” at 1760 lbs and AFT CG 20” at 1760 lbs to 20" at 1500 lbs or less. For the increased gross weight STCs, the CG range is limited by the gross weight STC or the following, whichever is less: FWD CG to 15" at 1500 lbs or less to 16" at 2000 lbs and AFT CG to 18.6" at 2000 lbs to 20" at 1760 lbs or less. The float step at the keel is 33.71" aft of the aircraft datum; aircraft datum is the leading edge of the wing with the aircraft properly leveled. 2000 STC Up Gross -1760 Normal Groes 16 18.6 2100 2000 1900 1800

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ibs 1700 1600 1500 1400 15 16 17 18 19 20 21 22 FLOATPLANE C.G. LOCATION (INCHES) AIRSPEED LIMITS: No Change. AIR SPEED INDICATOR MARKINGS: No Change. FAA Approved Date: APR 29 2009 ISSUE DATE: 4/21/09 EROCET INCORPORATED Supplemental Airplane Flight Manual Page FILE NO. 7 of 8 A-31050 TITLE: REVISION DATE: NA SUBTITLE: Piper PA-18 on Model 2200 Floats REVISION: PLACARDS: Locate Aerocet P/N 35-70006 Placard near retract handle clip: "WATER RUDDER ALWAYS UP EXCEPT WATER TAXIING" On each float locker MAXIMUM BAGGAGE: 100 LBS ARM: 8.3 in. AFT OF DATUM FAA Approved Date: APR 29 2009 I/R ISSUE DATE: 4/21/09 TITLE: REVISION DATE: NA SUBTITLE: MEROCET INCORPORATED Supplemental Airplane Flight Manual Piper PA-18 on Model 2200 Floats Page FILE NO. 8 of 8 A-31050 REVISION: This page intentionally left blank MIEROCET INCORPORATED Aerocet, Inc. Tel: 208-448-0400 Website: www.aerocet.com APR 29 2009 FAA Approved Date: I/R

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