AD/PA-30/35 Amdt 1 - Aircraft Flight Manual, Flight into Icing Conditions

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Piper PA-30 & 39 (Twin Comanche) Series Aeroplanes

 

AIRWORTHINESS DIRECTIVE


For the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/PA-30/35 and issues the following AD under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

 

AD/PA-30/35

Amdt 1


Aircraft Flight Manual, Flight into Icing Conditions 7/2000

 

Applicability: Models PA30, PA39, and PA40. Requirement:  Revise:

  1. The Limitations Section of the aircraft's Aircraft Flight Manual (AFM) by incorporating the following:

 

"WARNING"

Severe icing may result from environmental conditions outside of those for which the aircraft is certificated.

 

Flight in freezing rain, freezing drizzle, or mixed icing conditions (super cooled liquid water and ice crystals) may result in:

 

  • ice build-up on protected surfaces and exceed the capability of the ice protection system, or

 

  • ice forming aft of the protected surfaces.

This ice may not be shed using the ice protection systems, and may seriously degrade the performance and controllability of the aircraft.

 

During flight, severe icing conditions that exceed those for which the aircraft is certificated shall be determined by the visual cues described below. If one or more of these visual cues exists, immediately request priority handling from Air Traffic Control to facilitate a route or an altitude change to exit the icing conditions. The cues are:

 

  • unusually extensive ice accumulation on the airframe and windscreen in areas not normally observed to collect ice, and/or

 

  • accumulation of ice on the upper surface of the wing aft of the protected area, and/or

 

  • accumulation of ice on the engine nacelles and propeller spinners farther aft than normally observed.

 

 

Since the auto-pilot, when installed and operating, may mask tactile cues that indicate adverse changes in handling characteristics, use of the auto-pilot is prohibited when any of the visual cues specified above exist, or when unusual lateral trim requirements or auto-pilot trim warnings are encountered while the aircraft is in icing conditions.

 

All wing icing inspection lights must be operative prior to flight into known or forecast icing conditions at night. This direction supersedes any relief provided  by any Minimum Equipment List.

 

 

 

2.     The Normal Procedures Section of the AFM by incorporating the following:

 

THE FOLLOWING WEATHER CONDITIONS MAY BE CONDUCIVE TO SEVERE IN-FLIGHT ICING:

  • Visible rain at temperatures below 0 degrees Celsius ambient air temperature;
  • Droplets that splash or splatter on impact at temperatures below 0 degrees Celsius ambient air temperature.

 

PROCEDURES FOR EXITING A SEVERE ICING

ENVIRONMENT: (These procedures are applicable to all flight phases from take-off to landing.)

 

Monitor the ambient air temperature.

 

While severe icing may form at temperatures as cold as -18 degrees Celsius, increased vigilance is warranted at temperatures around freezing when visible moisture is present.

If the visual cues which are specified in the Limitations Section of the AFM for identifying severe icing conditions are observed, accomplish the following:

 

  • Immediately request priority handling from Air Traffic Control to facilitate a route or an altitude change to exit the severe icing conditions in order to avoid extended exposure to flight conditions more severe than those for which the aircraft has been certificated.

 

  • Avoid abrupt and excessive manoeuvring that may exacerbate control difficulties.

 

  • Do not engage the autopilot.
  • If the autopilot had previously been engaged, hold the control wheel firmly and disengage the autopilot.

 

  • If an unusual roll response or un-commanded roll control movement is observed, reduce the angle-of-attack.

 

  • Do not extend flaps when holding in icing conditions. Operation with flaps extended can result in a reduced wing angle-of-attack, with the possibility of ice forming on the upper surface further aft on the wing than normal, possibly aft of the protected area.

 

  • If the flaps are extended, do not retract them until the airframe is clear of ice.
  • Report these weather conditions to Air Traffic Control.

Note 1: Certificate of Registration holders should initiate action to ensure notification of this change is conveyed to any person who may operate their aircraft as pilot in command.

 

Note 2: FAA AD 99-14-01 refers.

 

Certification for accomplishment of this Directive may be carried out:

 

  1. after a copy of this Directive is included in the appropriate sections of the aircraft's AFM; and

 

b.     may be carried out at a minimum, by the holder of a private pilot's licence.

 

 

Compliance: Within 30 days after the Effective date of this Amendment.

 

This Amendment becomes effective on 13 July 2000.

 

Background:  This Directive is issued to minimise the potential hazards associated with operating the aircraft in severe icing conditions by providing more clearly defined procedures and limitations associated with such conditions.

 

Amendment 1 is issued to correct a word processing error in the initial issue.

 

The original issue of this Airworthiness Directive became effective on 23 March 2000.


 

Bernard Malcolm Hole

Delegate of the Civil Aviation Safety Authority 31 May 2000

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


The above AD is notified in the Commonwealth of Australia Gazette on 14 June 2000.

Overview

The Civil Aviation Safety Authority Act 1998 was enacted to provide a legal framework for regulating civil aviation safety in Australia. This legislation was introduced to address the need for a cohesive and comprehensive approach to civil aviation safety, encompassing aircraft, operators, personnel, and infrastructure. The Act empowers the Civil Aviation Safety Authority (CASA) to issue airworthiness directives, such as the Piper PA-30 and 39 (Twin Comanche) Series Aeroplanes Airworthiness Directive, to ensure that aircraft meet safety standards and to address any identified hazards. This particular Airworthiness Directive, issued under subregulation 39.1 (1) of the Civil Aviation Regulations 1998, aims to mitigate the risks associated with operating these aircraft in severe icing conditions by updating the Aircraft Flight Manual with more defined procedures and limitations. The policy objective is to enhance flight safety by providing clear guidance on handling severe icing conditions, thereby reducing the potential hazards faced by pilots and passengers.

Scope and Application

This Airworthiness Directive (AD) applies to Piper PA-30, PA-39, and PA-40 series aeroplanes, which includes any aircraft of these models registered in Australia. The AD mandates specific revisions to the Aircraft Flight Manual (AFM) of these aircraft, ensuring that the Limitations and Normal Procedures sections are updated to include more detailed information about flying into and out of severe icing conditions. The AD requires these updates to be made within 30 days from the effective date of the amendment, which is 13 July 2000. The AD is issued under the authority of the Civil Aviation Safety Regulations 1998 and is applicable to all aircraft of the specified models, regardless of the operator or the specific circumstances of their operation. The AD does not explicitly exclude any aircraft, operators, or situations but ensures that all such aircraft must comply with the updated AFM requirements to mitigate the risks associated with in-flight icing conditions. The AD may be subject to further interpretation and enforcement through subordinate instruments issued by the Civil Aviation Safety Authority.

Key Provisions

The Airworthiness Directive (AD) AD/PA-30/35 (Amdt 1) issued by the Civil Aviation Safety Authority (CASA) mandates specific actions to be taken to address safety concerns related to the Piper PA-30 and 39 (Twin Comanche) series aeroplanes. The directive requires the revision of the aircraft’s Aircraft Flight Manual (AFM) to include updated procedures and warnings concerning flight into icing conditions (sections 1 and 2). Specifically, the Limitations Section of the AFM must be updated to warn of the dangers of severe icing conditions that may exceed the aircraft's certification, including the necessity to request priority handling from Air Traffic Control to exit these conditions. Additionally, the Normal Procedures Section must be revised to include detailed weather conditions that may lead to severe in-flight icing and specific procedures for exiting severe icing environments. These procedures include monitoring ambient air temperature, avoiding abrupt manoeuvring, refraining from using the autopilot, and managing flap operations. The directive is applicable to models PA30, PA39, and PA40 and requires compliance within 30 days of the effective date of the amendment, which is 13 July 2000. The obligations imposed by this AD on aircraft operators and pilots are substantial. Operators must ensure that a copy of the directive is included in the appropriate sections of the aircraft's AFM. This includes the integration of new warnings and procedures into the manual to inform pilots of the risks associated with flying in severe icing conditions. Furthermore, pilots must adhere strictly to the updated procedures outlined in the AFM, such as avoiding the use of the autopilot in icing conditions and immediately requesting assistance from Air Traffic Control when visual cues of severe icing are observed. Operators are also required to notify all relevant personnel, including pilots in command, of these changes to ensure widespread awareness and compliance. Failure to comply with the AD/PA-30/35 (Amdt 1) can result in significant safety risks and potential legal consequences. Although the directive itself does not explicitly state penalties for non-compliance, violations of airworthiness directives can lead to enforcement actions by CASA. Such actions may include fines, suspension or revocation of aircraft certificates, and potential criminal charges if the non-compliance results in an accident or incident. The severity of these consequences underscores the importance of adhering to the AD to maintain the airworthiness and safety of the aircraft in question.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.