AD/Y12/8 - Aircraft Flight Manual, Flight into Icing Conditions
In ForceCTH
Jurisdiction
Commonwealth
Collection
legislative instrument
Plain English Summary
4/10 complexity
This Directive requires operators of Harbin Y12II aircraft to amend the Airplane Flight Manual to add specific icing limitations and procedures: immediate activation and cycling of de‑icing boots, visual cues that define “severe” icing, autopilot and flap restrictions in those conditions, and a requirement that wing‑icing inspection lights be serviceable for night flights into known or forecast icing. Operators must update AFMs and notify/train crews within 20 days; operators bear compliance and maintenance costs, pilots must change in‑flight behaviour, and CASA enforces the rule.
This Airworthiness Directive (AD), AD/Y12/8, addresses operational procedures and Airplane Flight Manual (AFM) limitations for Harbin Y12 Series aeroplanes, specifically all Y12II aeroplanes. The Directive is issued by a delegate of the Civil Aviation Safety Authority (CASA) under subregulation 39.1(1) of the Civil Aviation Regulations 1998 (CAR 1998), and takes effect on 20 March 2003. The Directive requires operators to revise the CAAC and FAA‑approved AFM by incorporating prescribed text into the Limitations and Normal Procedures sections, and to notify and ensure flight crew awareness (Requirement; Note 2; Compliance; Background).
Mechanically, the Directive mandates three core changes to AFM content: (1) explicit de‑icing boot activation and operation instructions for wing and tail leading edge pneumatic de‑icing boot systems; (2) a set of WARNINGS and visual cues identifying severe icing conditions, together with specific restrictions on autopilot use and an operational requirement for wing icing inspection lights at night; and (3) normal‑procedures material describing weather conditions conducive to severe icing and step‑by‑step procedures for exiting severe icing environments (Requirement, paragraphs 1-3; Note 3). Compliance must be completed within 20 days of the AD’s effective date unless already accomplished (Compliance).
The AD records a stated policy purpose: “to minimise the potential hazards associated with operating the aircraft in severe icing conditions by providing more clearly defined procedures and limitations” (Background). It also cross‑references an earlier China AD (CAD2000‑Y012‑02 Amdt 39‑2824) and calls for operators to take steps to notify crew and to insert a copy of the Directive in the AFM if desired (Note 1; Note 2; Note 3). The text explicitly states that the wing icing inspection lights requirement “supersedes any relief provided by the Master Minimum Equipment List” (Limitations, wing inspection lights note).
Current sections
Direct links to the current provisions in AD/Y12/8 - Aircraft Flight Manual, Flight into Icing Conditions.
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (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/Y12/8 Aircraft Flight Manual, Flight into Icing Conditions 3/2003
AD/Y12/8 Aircraft Flight Manual, Flight into Icing Conditions 3/2003
Applicability: All Y12II aeroplanes.
Requirement: 1. Revise the CAAC and FAA approved Airplane Flight Manual (AFM) by incorporating the following into the Limitations Section of the AFM:
“Except for certain phases of flight where the AFM specifies that de-icing boots should not be used (e.g. take-off, final approach, and landing), compliance with the following is required.
Wing and Tail Leading Edge Pneumatic De-icing Boot System, if installed, must be activated:
At the first sign of ice formation anywhere on the aircraft, or upon annunciation from an ice detector system, whichever occurs first; and
ii. The system must either be continued to be operated in the automatic cycling mode, if available; or the system must be manually cycled as needed to minimize the ice accretion on the airframe.
b. The wing and tail leading edge pneumatic de-icing boot system may be deactivated only after leaving icing conditions and after the airplane is determined to be clear of ice.”
2. Revise the CAAC and FAA approved Airplane Flight Manual (AFM) by incorporating the following into the Limitations Section of the AFM:
“WARNING
“WARNING
“WARNING
Severe icing may result from environmental conditions outside of those for which the airplane is certificated. Flight in freezing drizzle, or mixed icing conditions (supercooled liquid water and ice crystals) may result in ice build-up on protected surfaces exceeding the capability of the ice protection system, or may result in 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 airplane.
Harbin Y12 Series Aeroplanes
Harbin Y12 Series Aeroplanes
Harbin Y12 Series Aeroplanes
AD/Y12/8 (Continued)
During flight, severe icing conditions that exceed those for which the airplane is certificated shall be determined by the following visual cues. If one or more of these visual cues exists, immediately request priority handling from Air Traffic Control (ATC) to facilitate a route or an altitude change to exit the icing conditions:
Unusually extensive ice accumulation on the airframe and windshield in areas not normally observed to collect ice.
b. Accumulation of ice on the lower surface of the wing aft of the protected area.
c. Accumulation of ice on the engine nacelles and propeller spinners farther aft than normally observed.
Since the autopilot, when installed and operating, may mask tactile cues that indicate adverse changes in handling characteristics, use of the autopilot is prohibited when any of the visual cues specified above exist, or when unusual lateral trim requirements or autopilot trim warnings are encountered while the airplane is in icing conditions.
All wing icing inspection lights must be operative prior to flight into known or forecast icing conditions at night. (NOTE: This supersedes any relief provided by the Master Minimum Equipment List).”
3. Revise the CAAC and FAA-approved AFM by incorporating the following into the Normal Procedures Section of the AFM:
“THE FOLLOWING WEATHER CONDITIONS MAY BE
“THE FOLLOWING WEATHER CONDITIONS MAY BE CONDUCIVE TO SEVERE IN FLIGHT ICING
“THE FOLLOWING WEATHER CONDITIONS MAY BE CONDUCIVE TO SEVERE IN FLIGHT ICING
Visible rain at temperatures below 0 degrees Celsius ambient air temperature.
b. Droplets that splash or splatter on impact at temperature below 0 degrees Celsius ambient air temperature.
PROCEDURES FOR EXITING THE SEVERE ICING
PROCEDURES FOR EXITING THE SEVERE ICING ENVIRONMENT:
PROCEDURES FOR EXITING THE SEVERE ICING ENVIRONMENT:
These procedures are applicable to all flight phases from takeoff to landing.
Source text
Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.
AIRWORTHINESS DIRECTIVE AIRWORTHINESS DIRECTIVE
AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (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/Y12/8 Aircraft Flight Manual, Flight into Icing Conditions 3/2003
Applicability: All Y12II aeroplanes.
Requirement: 1. Revise the CAAC and FAA approved Airplane Flight Manual (AFM) by incorporating the following into the Limitations Section of the AFM:
“Except for certain phases of flight where the AFM specifies that de-icing boots should not be used (e.g. take-off, final approach, and landing), compliance with the following is required.
Wing and Tail Leading Edge Pneumatic De-icing Boot System, if installed, must be activated:
At the first sign of ice formation anywhere on the aircraft, or upon annunciation from an ice detector system, whichever occurs first; and
ii. The system must either be continued to be operated in the automatic cycling mode, if available; or the system must be manually cycled as needed to minimize the ice accretion on the airframe.
b. The wing and tail leading edge pneumatic de-icing boot system may be deactivated only after leaving icing conditions and after the airplane is determined to be clear of ice.”
2. Revise the CAAC and FAA approved Airplane Flight Manual (AFM) by incorporating the following into the Limitations Section of the AFM:
“WARNING “WARNING
“WARNING
Severe icing may result from environmental conditions outside of those for which the airplane is certificated. Flight in freezing drizzle, or mixed icing conditions (supercooled liquid water and ice crystals) may result in ice build-up on protected surfaces exceeding the capability of the ice protection system, or may result in 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 airplane.
Who decides and who must act is clear on the face of the Directive. CASA, through its delegate (signed by James Coyne), issues the AD. The legal obligation to revise the AFM and to ensure crew awareness falls on operators of Y12II aeroplanes. Flight crew and ATC are named as operational actors required to follow the procedures set out in the AFM (Requirement; Note 2).
Main concepts
Applicability: the AD applies to all Harbin Y12II aeroplanes. The Directive is prescriptive about the AFM content and pilots’ operational responses to icing, rather than requiring hardware modification or decommissioning. The main technical and operational concepts in the Directive are:
De‑icing boot activation and operation. The AFM must require activation of wing and tail leading edge pneumatic de‑icing boots at the first sign of ice formation or upon ice detector annunciation; boots should either remain in automatic cycling mode or be manually cycled as needed; deactivation permitted only after leaving icing conditions and after the aeroplane is determined to be clear of ice (Requirement 1, quoted passages).
Severe icing recognition and pilot response. The Directive adds WARNINGS describing that freezing drizzle and mixed icing conditions can produce ice beyond the protection system’s capability, or create ice aft of protected surfaces that cannot be shed. It defines concrete visual cues to identify icing that exceeds certification: unusually extensive ice on airframe and windshield, ice on wing lower surface aft of protected area, and ice on engine nacelles and propeller spinners farther aft than normal (Requirement 2).
Autopilot prohibition when certain conditions are present. Where the visual cues exist, or where unusual lateral trim requirements or autopilot trim warnings occur in icing conditions, use of the autopilot is prohibited; autopilot may mask tactile cues and thereby delay pilot recognition of adverse handling characteristics (Requirement 2).
Night operations equipment requirement. The AD requires all wing icing inspection lights to be operative prior to flight into known or forecast icing conditions at night, explicitly superseding any MMEL relief (Requirement 2 note).
Normal procedures for exiting severe icing. The AFM must contain a list of weather conditions conducive to severe in‑flight icing (e.g., visible rain below 0°C, droplets that splash or splatter on impact below 0°C) and a set of stepwise procedures applicable to all flight phases to exit severe icing. Procedures include requesting priority handling from ATC to change route/altitude, avoiding abrupt manoeuvres, not engaging the autopilot, holding control wheel and disengaging autopilot if engaged, reducing angle‑of‑attack if uncommanded roll occurs, not extending flaps when holding in icing, not retracting flaps until clear of ice if already extended, and reporting conditions to ATC (Requirement 3).
Temporal and procedural compliance mechanics. The AD becomes effective on 20 March 2003 and requires compliance within 20 days of the effective date unless previously accomplished (Compliance). The Directive permits a copy to be inserted in AFM to accomplish the amendment (Note 3) and urges operators to notify flight crew members (Note 2).
These concepts frame an operational regime that is procedural rather than equipment‑modification based. The balance struck by the Directive is to change pilot behaviour, AFM content, and dispatch conditions rather than mandate hardware changes on the fleet.
Who it affects
The Directive identifies three discrete groups with obligations or duties: operators of Harbin Y12II aeroplanes, flight crew operating those aeroplanes, and Air Traffic Control as an operational facilitator.
Operators: The Directive is addressed to operators of Y12II aeroplanes. Operators are required to revise the CAAC and FAA‑approved AFM for their aeroplanes by incorporating the specified text into the Limitations and Normal Procedures sections (Requirement 1-3). Operators must ensure action is taken “unless previously accomplished, within 20 days of the effective date of this Directive” (Compliance). Note 2 instructs that operators “should initiate action to notify and ensure that flight crew members are aware of the change,” a managerial responsibility sitting with operators.
Flight crew: The AFM changes impose new in‑flight duties and constraints on pilots. Pilots must activate and cycle de‑icing boots at the first sign of ice or upon ice detector annunciation, follow the new warnings and visual cue recognition regime, comply with the autopilot prohibitions where applicable, adhere to flaps and angle‑of‑attack guidance, and follow the specified procedures for exiting severe icing. The AFM material makes explicit that certain autopilot usage is prohibited when the visual cues are present or when autopilot trim warnings occur (Requirement 1-3).
Air Traffic Control (ATC): The Directive requires flight crews to “immediately request priority handling from Air Traffic Control to facilitate a route or an altitude change to exit the icing conditions” when severe icing visual cues are observed and to request priority handling in the normal procedures for exiting severe icing. Thus ATC becomes an operational actor responding to pilot requests to expedite route or altitude changes in icing events (Requirement 2, Requirement 3).
Maintenance and dispatch personnel: The requirement that “All wing icing inspection lights must be operative prior to flight into known or forecast icing conditions at night” affects maintenance and pre‑flight dispatch decisions. The Directive expressly supersedes any MMEL relief that might otherwise permit dispatch with inoperative wing icing inspection lights, thus shifting responsibility to ensure operability before night icing flights (Requirement 2).
CASA and its delegate: The AD is issued by CASA under CAR 1998, with a specific delegate signature (James Coyne) on 3 February 2003. The delegate is the deciding official who imposed the requirement; CASA is the regulator enforcing compliance through its regulatory framework (opening paragraph; delegate signature; Background).
The Directive does not require changes to certification status, crew complements, or equipment beyond operation and AFM text. It is limited in applicability to Y12II aeroplanes and does not purport to govern other types or fleets.
Key duties and rights
Key duties created or reinforced by the Directive are as follows, quoted and paraphrased according to the AD’s structure:
AFM revision duty. Operators must revise the CAAC and FAA‑approved AFM to include the specified Limitations and Normal Procedures material. This is an affirmative managerial duty: the AFM must incorporate the text provided by the Directive (Requirement 1-3).
De‑icing boot operation duty. The AFM must require that the wing and tail leading edge pneumatic de‑icing boot system, if installed, is activated at the first sign of ice or upon annunciation from an ice detector system, and must either be kept in automatic cycling mode if available or manually cycled as needed; deactivation only after leaving icing and confirming the airframe is clear of ice (Requirement 1).
Severe icing recognition and response duties. The AFM must carry WARNINGS that identify environmental conditions that can produce severe icing beyond certification, with explicit visual cues and required pilot responses. The pilot duty is to request priority handling from ATC to change route or altitude immediately when the visual cues are present (Requirement 2).
Autopilot limitation duty. The AFM must prohibit autopilot use when the defined visual cues exist, or when unusual lateral trim requirements or autopilot trim warnings occur while in icing conditions. The Directive explains the rationale: autopilot may mask tactile cues of adverse handling characteristics (Requirement 2).
Night dispatch equipment duty. The AFM must state that all wing icing inspection lights must be operative prior to flight into known or forecast icing conditions at night. This overrides any MMEL relief allowing dispatch with these lights inoperative (Requirement 2, note).
Operational procedure duties. The AFM must contain Normal Procedures that require crews to monitor ambient temperature, request priority handling, avoid abrupt manoeuvres, not engage the autopilot, hold the control wheel and disengage autopilot if engaged, reduce angle‑of‑attack if uncommanded roll occurs, manage flap extension/retraction with specific constraints in icing conditions, and report the weather conditions to ATC (Requirement 3).
Rights and discretionary space in the Directive:
Operator discretion as to method of AFM amendment. Note 3 indicates a practical mechanism: “A copy of this Directive maybe inserted in the AFM to accomplish the amendment to the AFM.” This gives operators a concrete, permitted method to comply without necessarily producing a newly printed AFM revision.
Pilot discretionary judgement in detection. The core activation duty for de‑icing boots is tied to the “first sign of ice formation anywhere on the aircraft, or upon annunciation from an ice detector system, whichever occurs first.” That wording leaves detection partly dependent on pilot judgement (visual or tactile cues) unless an ice detector annunciates, in which case the duty is mechanical/automatic.
ATC facilitation role. Pilots have a procedural right to request priority handling from ATC to facilitate exiting icing conditions; ATC’s role is to respond operationally to such requests. The Directive places the onus on pilots to request and on ATC to facilitate, rather than mandating specific ATC actions.
Non‑express duties and omitted sanctions:
The AD itself does not specify civil or criminal penalties or the enforcement mechanism details in its text. It is issued under the statutory authority of CAR 1998 subregulation 39.1(1), which confers regulatory force; the AD does not, however, set out penalty parameters or enforcement procedures within its text (opening paragraph; Compliance).
Penalties and enforcement
The Directive is issued under the authority of CAR 1998 subregulation 39.1(1), and the signature of a CASA delegate (James Coyne) appears on the document. That establishes the AD as a regulatory instrument within CASA’s statutory remit (opening paragraph; signature block). The Directive does not itself set out penalties, fines, or explicit enforcement steps in the text provided.
What is present on the face of the Directive is procedural enforcement content: a compliance deadline and a clear instruction that the AFM be amended to include specified text. Compliance is required “unless previously accomplished, within 20 days of the effective date of this Directive.” The Directive’s effective date is 20 March 2003 and the AD was signed on 3 February 2003 (Compliance; effective date statements; delegate signature). The AD was notified in the Commonwealth of Australia Gazette on 26 February 2003, which serves as a public notification mechanism (final paragraph).
Because the Directive itself does not prescribe penalties, the likely enforcement pathway is by CASA regulatory enforcement under CAR 1998 and related enforcement provisions, but that is not detailed in the Directive text. The AD imposes binding operational requirements on operators and flight crew through the AFM amendment obligation and the procedural duties that AFM will impose on pilots. Enforcement would ordinarily be effected via CASA surveillance, audits, and enforcement mechanisms under the broader regulatory framework, but the AD itself contains only the directive and the compliance deadline, not a schedule of sanctions.
The AD also contains a specific operational override: the instruction that wing icing inspection lights must be operative prior to night flights into known or forecast icing conditions “supersedes any relief provided by the Master Minimum Equipment List.” That language has immediate operational effect for dispatch and maintenance decisions; it transfers the decision authority away from MMEL relief and back to the AFM/AD requirement. Non‑compliance with that sentence would directly contradict the AD’s operational requirement even if an MMEL permitted dispatch.
In sum, the AD establishes legally binding procedural obligations under CASA’s AD authority, prescribes a short compliance timeframe, and uses public notification via the Gazette. It does not enumerate penalties or enforcement steps in its text; enforcement would therefore rely on CASA’s statutory enforcement mechanisms outside the AD wording.
How it interacts with other laws
The Directive identifies its statutory provenance: it is issued under subregulation 39.1(1) of CAR 1998. That citation establishes the AD’s place within the Civil Aviation Regulations framework and indicates that the AD is an instrument issued under that regulation (opening paragraph).
The AD also interacts explicitly with other regulatory and certification instruments:
CAAC and FAA AFMs. The Directive requires revision of “the CAAC and FAA approved Airplane Flight Manual (AFM)” for the aeroplane. The instruction to amend AFMs approved by foreign authorities recognises the dual or multinational certification pathways applicable to the Harbin Y12 series and imposes changes that operators must incorporate into those approved manuals (Requirement 1-3).
China AD CAD2000‑Y012‑02 Amdt 39‑2824. The AD notes that “China AD CAD2000‑Y012‑02 Amdt 39‑2824 refers,” indicating a cross‑reference to an earlier or parallel airworthiness directive issued by the Chinese aviation authority (Note 1). That cross‑reference signals an interaction between CASA’s AD and a foreign authority’s AD addressing similar issues.
Master Minimum Equipment List (MMEL). The Directive contains an explicit interaction clause: “All wing icing inspection lights must be operative prior to flight into known or forecast icing conditions at night. (NOTE: This supersedes any relief provided by the Master Minimum Equipment List).” That sentence displaces any MMEL‑based relief that might otherwise permit dispatch with inoperative wing icing inspection lights before night flights into known or forecast icing conditions. Practically, that changes decision‑making at dispatch and maintenance: MMEL relief cannot be used to override the AD’s operational requirement in the described circumstances (Requirement 2).
Air Traffic Control procedures. The AD instructs pilots to request priority handling from ATC to enable route or altitude changes to exit severe icing conditions. That creates an interface between flight operations obligations and ATC services: the AD does not change ATC law but expects ATC to facilitate pilots’ requests in icing emergencies (Requirement 2, Requirement 3).
AFM amendment mechanisms. Note 3 allows operators to insert a copy of the Directive into the AFM “to accomplish the amendment to the AFM.” That choice interacts with AFM approval and record‑keeping processes in that operators may use the Directive copy insertion as the practical method of compliance instead of a formal reissue of the AFM.
The Directive does not purport to change the certification basis for the aircraft, require supplemental type certificates, or mandate hardware alteration. It is procedural and operational in its requirements, inserting specific AFM text and pilot procedures into the regulatory compliance environment. Any enforcement or penalties for non‑compliance would fall under CAR 1998 enforcement mechanisms and CASA policy, neither of which are detailed in the AD text itself.
Amendment history
The text of the Directive contains very limited material that could be described as an amendment history. What is present:
The AD explicitly refers to China AD CAD2000‑Y012‑02 Amdt 39‑2824 as a related document: “Note 1: China AD CAD2000‑Y012‑02 Amdt 39‑2824 refers.” This references an earlier or parallel airworthiness directive issued by the Chinese authority which is relevant background. The AD does not provide the text of that China AD, nor does it indicate any change to this Australian AD based upon it beyond the cross‑reference (Note 1).
The AD contains an internal supersession statement regarding the Master Minimum Equipment List: the requirement that wing icing inspection lights be operative prior to night flights into known or forecast icing conditions “supersedes any relief provided by the Master Minimum Equipment List.” That sentence functions as an immediate and explicit amendment to any existing MMEL relief that would permit dispatch with those lights inoperative in the specified circumstances (Requirement 2 note).
The AD itself becomes effective on 20 March 2003 and specifies a compliance window: “Unless previously accomplished, within 20 days of the effective date of this Directive.” There is no indication within this AD of subsequent amendments, revocations, or revisions to AD/Y12/8 beyond its issuance. The AD’s issuance date (signed 3 February 2003) and Gazette notification date (26 February 2003) are recorded; effective date is 20 March 2003 (delegate signature block; final paragraph; Compliance).
Note 3 provides a mechanism to implement the AFM amendment: “A copy of this Directive maybe inserted in the AFM to accomplish the amendment to the AFM.” That procedural allowance effectively constitutes an operational amendment method authorised by CASA for the AFM content.
No further amendment history is included in the text provided. The AD does not record supersessions of prior CASA ADs, nor does it include an explicit amendment log within the Directive text. Any subsequent amendments to AD/Y12/8, if they exist, are not recorded within this document.
Litigation history
The Directive itself does not record any litigation history, judicial review, or challenges to its content or issuance. The document lists no cases, no appeals, and no legal proceedings. It cross‑references a China AD but does not cite judicial treatment of the AD or related operational disputes.
Where litigation history is absent from a directive, the document serves as a primary regulatory instrument and the absence of recorded litigation in the text means that users of the AD must look outside this document to determine whether legal challenges or enforcement actions have occurred. The AD does record its formal issuance and notification steps (delegate signature dated 3 February 2003; Gazette notification 26 February 2003) which are the typical administrative steps that can be relied on in any subsequent legal proceedings, but the AD itself contains no litigation or adjudicative record.
In short, the provided Directive contains no litigation history. Any enquiries regarding subsequent compliance enforcement, challenges, or legal interpretation would need to be addressed using external records not contained in this document.
Gotchas
This AD contains specific operational requirements and drafting choices that impose concentrated operational consequences. The following are practical, source‑grounded points that operators, pilots, and compliance professionals should note carefully:
Short compliance window. The AD requires AFM revision “within 20 days of the effective date” unless previously accomplished. The effective date is 20 March 2003 (Compliance). A 20‑day window for AFM revision, crew notification, insertion, and training is brief and may require rapid procedural and administrative action by operators.
AFM wording is prescriptive and detailed. The specified text includes imperative obligations (for example, activation of de‑icing boots “at the first sign of ice formation anywhere on the aircraft, or upon annunciation from an ice detector system,” and autopilot prohibitions). Operators must ensure the AFM’s wording exactly,or at least substantively,matches the Directive’s instructions to satisfy compliance, and the Directive authorises insertion of a copy of the AD into the AFM as a permissible method (Requirement 1-3; Note 3).
Detection uncertainty and pilot judgement. The duty to activate de‑icing boots at “the first sign of ice formation” relies on pilot detection unless an ice detector annunciates. This creates a dependency on human judgement and sensory detection, which can vary with weather, visibility, crew experience, and reliance on autopilot (Requirement 1). The Directive acknowledges that autopilot may mask tactile cues, and it therefore prohibits autopilot use when visual cues are present.
Autopilot prohibition increases pilot workload. The AD prohibits autopilot use where the listed visual cues exist or when unusual lateral trim requirements or autopilot trim warnings occur while in icing conditions. That shifts handling to manual control in potentially demanding circumstances and may increase pilot workload, especially during phases such as holding or descent. Operators must incorporate this into crew training and operational planning (Requirement 2).
MMEL relief removed for a specific item. The AD explicitly supersedes MMEL relief for wing icing inspection lights prior to night flights into known or forecast icing conditions. Operators who habitually dispatch with MMEL relief for these lights must change their dispatch logic and maintenance priorities accordingly (Requirement 2 note).
Flap management can affect approach and holding. The AD forbids extending flaps while holding in icing conditions and directs that if flaps are extended they should not be retracted until the airframe is clear of ice. This affects standard approach and holding procedures and may require changes to approach planning and minima in icing forecasts (Requirement 3).
Ambiguities in “severe icing”. The AD supplies visual cues to identify severe icing but operational judgements remain (for example, what constitutes “unusually extensive ice” or “farther aft than normally observed”). Identifying severe icing triggers a set of mandatory responses including requesting priority handling from ATC; therefore operators should ensure clear crew guidance and training to reduce variability in decision‑making (Requirement 2).
Practical insertion permitted but may not satisfy all approval processes. Note 3 allows a copy of the Directive to be inserted in the AFM to accomplish the amendment. While this is a practical compliance option, operators should confirm that such insertion meets their AFM approval/recording requirements under other regulatory instruments or corporate procedures before relying on it as a long‑term solution (Note 3).
Interaction with foreign approvals. The AFM to be amended is the CAAC and FAA approved AFM. Operators should ensure that amendments are reflected in the versions of the AFM accepted by those authorities, or at least that the insertion of this AD into the AFM is acceptable to the relevant approving authority. The AD itself requires amendment of those AFMs but does not describe the process for updating approvals.
Reporting and ATC reliance. The AD requires pilots to “report these weather conditions to Air Traffic Control.” Reliance on ATC to facilitate exits from icing conditions is subject to ATC traffic management constraints. Pilots must both request and rely on priority handling, but actual routing/altitude changes may be constrained by ATC traffic or airway structures.
Each of these “gotchas” derives directly from the AD text and indicates points where operational, training, dispatch, maintenance, or procedural adjustments will be necessary.
How to comply
Compliance is an operator‑centred, time‑sensitive programme consisting of documented AFM amendment, crew notification and training, maintenance/dispatch checks, and procedural implementation. The Directive provides a specific compliance pathway and a permissible insertion mechanism. Practical steps, grounded exclusively in the Directive, are:
Confirm applicability and effective date. Determine whether the operator’s fleet includes any Y12II aeroplanes, note the Directive’s effective date (20 March 2003) and the compliance timeframe (“unless previously accomplished, within 20 days of the effective date of this Directive”) (Applicability; Compliance).
Amend the AFM. Incorporate the exact text required by the Directive into the Limitations section and the Normal Procedures section of the CAAC and FAA‑approved AFM. The required content is set out under Requirement paragraphs 1-3 and includes:
De‑icing boot activation and cycling instructions (Requirement 1).
WARNINGS concerning severe icing, the visual cues list, autopilot prohibition conditions, and the wing icing inspection lights night operability requirement (Requirement 2).
Normal procedures for recognising conditions conducive to severe icing and stepwise procedures for exiting the severe icing environment (Requirement 3).
Use permitted insertion if needed. Note 3 allows a copy of the Directive to be inserted into the AFM to accomplish the amendment. Operators may use this route for rapid compliance, but should ensure that such insertion is recorded and accessible to crews in the AFM (Note 3).
Notify and train flight crew. As Note 2 states, operators “should initiate action to notify and ensure that flight crew members are aware of the change.” Implement a crew notification and training plan that covers:
Activation criteria for de‑icing boots.
Recognition of the specified visual cues for severe icing.
Autopilot limitations and procedures to disengage and manage manual handling.
Flap management rules in icing conditions.
Procedures for requesting priority handling from ATC and for reporting icing to ATC.
Monitoring of ambient temperature guidance, including the note that severe icing may occur down to −18°C and increased vigilance at temperatures around freezing (Requirement 3).
Update dispatch and maintenance checklists. Ensure that pre‑flight and dispatch procedures reflect the new requirement that “all wing icing inspection lights must be operative prior to flight into known or forecast icing conditions at night,” and ensure that MMEL relief is not used to circumvent this requirement (Requirement 2 note).
Operationalise pilot duties. Ensure that flight crews follow the AFM‑inserted steps in flight, including:
Activating de‑icing boots at first sign of ice or ice detector annunciation and maintaining cycling until clear;
Requesting priority handling from ATC immediately when visual cues of severe icing appear;
Avoiding abrupt manoeuvres, not engaging the autopilot when the specified cues exist, holding the control wheel and disengaging autopilot if engaged, reducing angle‑of‑attack for unusual roll responses, and managing flaps per the AFM instructions (Requirement 1-3).
Recordkeeping and audit. Document the AFM amendment, the notification to crew, and any training activities to support compliance evidence. If a copy of the Directive is inserted into the AFM, record that step and make the AD insert readily available to crews.
Coordinate with approving authorities. Because the Directive requires revision of CAAC and FAA‑approved AFMs, operators should ensure that their method of compliance (AFM insertion or formal AFM revision) is acceptable to those approving authorities and that records reflect the AD‑driven change.
Monitor and report. Ensure that crews file any reports required by the AFM (for example, reporting observed severe icing conditions to ATC), and retain records of any ATC priority handling requests and icing encounters for safety monitoring and regulatory oversight.
Implement maintenance prioritisation. Given the AD’s MMEL supersession for wing icing inspection lights in night icing flights, maintenance planners should prioritise the repair or assurance of these lights so as not to restrict operation during forecast or known night icing conditions.
Completion of these steps within the 20‑day compliance window satisfies the Directive’s stated timeline, unless the operator had already accomplished the required AFM changes. Note that while Note 3 permits an AFM insertion as a compliant route, operators should ensure that crew training and dispatch processes treat the insertion as an effective and accessible AFM amendment.
Part “THE FOLLOWING WEATHER CONDITIONS MAY BE“THE FOLLOWING WEATHER CONDITIONS MAY BE CONDUCIVE TO SEVERE IN FLIGHT ICING
Harbin Y12 Series Aeroplanes Harbin Y12 Series Aeroplanes
Harbin Y12 Series Aeroplanes
AD/Y12/8 (Continued)
During flight, severe icing conditions that exceed those for which the airplane is certificated shall be determined by the following visual cues. If one or more of these visual cues exists, immediately request priority handling from Air Traffic Control (ATC) to facilitate a route or an altitude change to exit the icing conditions:
Unusually extensive ice accumulation on the airframe and windshield in areas not normally observed to collect ice.
b. Accumulation of ice on the lower surface of the wing aft of the protected area.
c. Accumulation of ice on the engine nacelles and propeller spinners farther aft than normally observed.
Since the autopilot, when installed and operating, may mask tactile cues that indicate adverse changes in handling characteristics, use of the autopilot is prohibited when any of the visual cues specified above exist, or when unusual lateral trim requirements or autopilot trim warnings are encountered while the airplane is in icing conditions.
All wing icing inspection lights must be operative prior to flight into known or forecast icing conditions at night. (NOTE: This supersedes any relief provided by the Master Minimum Equipment List).”
3. Revise the CAAC and FAA-approved AFM by incorporating the following into the Normal Procedures Section of the AFM:
“THE FOLLOWING WEATHER CONDITIONS MAY BE “THE FOLLOWING WEATHER CONDITIONS MAY BE CONDUCIVE TO SEVERE IN FLIGHT ICING
“THE FOLLOWING WEATHER CONDITIONS MAY BE CONDUCIVE TO SEVERE IN FLIGHT ICING
Visible rain at temperatures below 0 degrees Celsius ambient air temperature.
b. Droplets that splash or splatter on impact at temperature below 0 degrees Celsius ambient air temperature.
PROCEDURES FOR EXITING THE SEVERE ICING PROCEDURES FOR EXITING THE SEVERE ICING ENVIRONMENT:
PROCEDURES FOR EXITING THE SEVERE ICING ENVIRONMENT:
These procedures are applicable to all flight phases from takeoff to landing.
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AD/Y12/8 (Continued)
Monitor the ambient air temperature. While severe icing may form at temperature as cold as -18 degrees Celsius, increased vigilance is warranted at temperatures around freezing with visible moisture present. If the visual cues 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 altitude change to exit the severe icing conditions in order to avoid extended exposure to flight conditions more severe than those for which this airplane has been certificated.
b. Avoid abrupt and excessive manoeuvring that may exacerbate control difficulties.
c. Do not engage the autopilot.
d. If the autopilot is engaged, hold the control wheel firmly and disengage the autopilot.
e. If an unusual roll response or uncommanded roll control movement is observed, reduce the angle-of-attack.
f. 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 lower surface further aft on the wing than normal, possibly aft of the protected area.
g. If the flaps are extended, do not retract them until the airframe is clear of ice.
h. Report these weather conditions to Air Traffic Control.”
Note 1: China AD CAD2000-Y012-02 Amdt 39-2824 refers.
Note 2: Operators should initiate action to notify and ensure that flight crew members are aware of the change.
Note 3: A copy of this Directive maybe inserted in the AFM to accomplish the amendment to the AFM.
Compliance: Unless previously accomplished, within 20 days of the effective date of this Directive.
This Airworthiness Directive becomes effective on 20 March 2003.
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AD/Y12/8 (Continued)
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.
James Coyne
Delegate of the Civil Aviation Safety Authority 3 February 2003
The above AD is notified in the Commonwealth of Australia Gazette on 26 February 2003.