AD/BEECH 1900/47 - Elevators

The AD rests on a small set of technical and administrative concepts. The text itself identifies the following as the primary elements to be understood and acted upon:

• Applicability by model and serial number. The AD lists the particular Beechcraft 1900 models and serial-number ranges to which it applies. The exact text reads: "Model 1900 aircraft, serial number UA-3. Model 1900C aircraft, serial number UB-1 through UB-74, UC-1 through UC-174. Model 1900C aircraft, serial numbers UD-1 through UD-6. Model 1900D aircraft, serial numbers UE-1 through UE-439." Those serial-numbered subsets determine who must comply.

• Inspection targets. The AD differentiates two inspection targets: (a) "elevator hinge support attachments" on both left and right elevators, to be checked for loose or missing rivets; and (b) "elevator hinge joints" and the "clearance of each elevator to its stabiliser," to be checked for looseness and incorrect clearance.

• Reference technical standards. The AD does not provide the detailed inspection or repair steps itself. Instead it requires following Raytheon Aircraft Company Safety Communique No. 261 and, specifically, the Raytheon Maintenance Manual Chapter 5-20-07 and Structural Repair Manual Chapter 51-40-02. These documents are incorporated by reference for technical procedure.

• Remedy mandate and flight limitation. The AD establishes remedial actions and ties them directly to the aircraft’s ability to fly: if loose or missing rivets are evident, "replace affected rivets before further flight"; if hinge looseness or incorrect clearance is evident, "correct the discrepancies before further flight." The AD therefore conditions continued flight on successful completion of prescribed repairs.

• Compliance timing. The directive fixes a compliance interval of "within 50 hours time in service after 4 October 2005" for each inspection, making the inspection window short and actionable.

• Cross-reference to FAA action. The AD states "Note: FAA AD 2005-18-21 Amdt 39-14262 refers," signalling alignment or reliance on a contemporaneous FAA airworthiness action and an international regulatory reference point.

• Safety trigger. The background recites an incident,binding elevator control column during takeoff,linked to missing and loose rivets and rubbing of the elevator counterweight horn against the horizontal stabiliser. The incident is the proximate factual trigger for the AD’s prescriptive measures.

Those concepts together create an instrument that prescribes a technical inspection, references manufacturer technical materials for execution, requires immediate rectification of defects as a condition of flight, applies to precisely listed serial-numbered aeroplanes, and imposes a rapid compliance deadline.

The AD identifies by model and serial number the discrete set of aircraft to which it applies. Operators, maintenance organisations, and owners that possess or service the listed Beechcraft 1900 series aeroplanes are the parties directly affected. The applicability language in the AD reads:

• Model 1900 aircraft, serial number UA-3.
• Model 1900C aircraft, serial number UB-1 through UB-74, UC-1 through UC-174.
• Model 1900C aircraft, serial numbers UD-1 through UD-6.
• Model 1900D aircraft, serial numbers UE-1 through UE-439.

That enumeration means compliance obligations attach to each individual aeroplane within those serial-number brackets. The AD’s technical actions are maintenance tasks, so the immediate actors who must carry out the inspections and repairs are maintenance engineers and certifying staff working for the operator or for contracted maintenance organisations. The AD requires following Raytheon Aircraft Company guidance (Safety Communique No. 261 and specific manual chapters), and so those who provide maintenance must have access to and apply those Raytheon documents.

Pilots and flight crews are affected indirectly: the AD responds to a flight-safety event (a binding elevator control column during takeoff) and links remedial action to whether an aircraft may continue to be flown. The AD specifies that where defects are found the rivets must be replaced and discrepancies corrected "before further flight," making the flight crew’s ability to operate the aircraft contingent on maintenance outcomes.

Regulatory actors are implicated by authorship and issuance. The AD is signed by David Villiers, "Delegate of the Civil Aviation Safety Authority," and is presented as a CASA directive effective 4 October 2005. That identifies CASA as the issuing regulator and the delegate as the decision agent for issuance. The AD also refers to an FAA AD (FAA AD 2005-18-21 Amdt 39-14262), so manufacturers, operators and maintenance organisations operating in jurisdictions influenced by FAA directives may need to consider the related FAA instrument.

The AD does not list exemptions, alternative compliance procedures, or delegated approval processes within the text provided. It does not specify who pays for inspections or repairs; operationally, that financial responsibility normally falls to the aircraft owner or operator, but the AD itself only prescribes the technical and timing obligations and the "before further flight" condition.

The AD sets out clear duties for owners/operators and maintenance personnel of the listed Beechcraft 1900 series aeroplanes. The principal duties as stated in the AD are:

• To inspect "all elevator hinge support attachments on both left and right elevators for loose or missing rivets" following Raytheon Aircraft Company Safety Communique No. 261 and the Raytheon Aircraft Company Maintenance Manual, Chapter 5-20-07 and Structural Repair Manual, Chapter 51-40-02. If loose or missing rivets are evident, the AD requires replacement of the affected rivets "before further flight."

• To inspect the "elevator hinge joints for looseness and the clearance of each elevator to its stabiliser" under the same Raytheon references. If looseness or incorrect clearance is evident, the AD requires correction of the discrepancies "before further flight."

• To perform both inspections within 50 hours time in service after 4 October 2005.

These duties are prescriptive in both process (inspect following specific Raytheon materials) and outcome (replace rivets/correct discrepancies before further flight). The AD conditions continued operation on successful remediation of the identified defects; the phrase "before further flight" operates as an operational restriction until maintenance action is completed.

The AD does not state procedural rights such as appeal, exemption, extension, alternative means of compliance (AMOC), or an administrative review process within its own text. It likewise does not include express rights to recover costs or to seek reimbursement. The AD contains a “Note: FAA AD 2005-18-21 Amdt 39-14262 refers,” but does not itself incorporate FAA processes for AMOCs or other administrative procedures.

Because the AD mandates following Raytheon technical documents, a practical right conferred to operators is access to the specified manufacturer guidance as the technical standard for compliance. The AD does not itself provide the technical content, so the right to rely on the Raytheon documents to demonstrate compliance is implicit in the AD’s requirement language.

Procedurally, the AD sets a short compliance timeframe , 50 hours time in service , which constrains scheduling of maintenance. The AD does not itself provide for staged compliance, temporary operations under limited conditions, or an extended window, nor does it state any exceptions for aircraft that have already undergone similar inspections; the duty as written applies to the listed serials within the prescribed timeframe.

In short, the AD imposes specific, outcome-focused maintenance duties tied to a short compliance period and references manufacturer materials as the operative technical standards; it does not, in the provided text, articulate rights of exemption, appeal, or cost recovery.

The AD text as provided does not itself set out penalties, sanctions or an enforcement mechanism in statutory terms. It is presented as an Airworthiness Directive issued by the Civil Aviation Safety Authority, signed by a CASA delegate (David Villiers) and effective 4 October 2005. The AD prescribes mandatory inspections and repair-before-flight obligations, but contains no express penalty clauses in the provided text.

Key enforcement-relevant features that do appear in the AD are procedural and conditional:

• Compliance timing is fixed: both inspections are to be completed "within 50 hours time in service after 4 October 2005." That creates a defined compliance deadline.

• Remedy obligations are tied to flight status: if certain defects (loose or missing rivets, hinge looseness, incorrect clearance) are found, the AD requires replacement or correction "before further flight." That conditions continued airworthiness on the completion of specified maintenance.

• The AD references FAA AD 2005-18-21 Amdt 39-14262. That cross-reference may indicate a parallel track of regulatory requirements in another jurisdiction but the AD does not itself describe enforcement interactions.

The absence of explicit penalties in the text means that any penalty regime, enforcement process or sanction for non-compliance would be found in the wider statutory or regulatory framework governing aviation safety and the exercise of CASA’s enforcement powers, none of which are reproduced or incorporated in the AD text provided. The AD itself is an instrument that imposes obligations; whether non-compliance triggers administrative enforcement, grounding notices, certificate actions, monetary penalties, or criminal offences depends on separate statutory provisions and CASA’s enforcement policy, which are not part of the text you supplied.

For practitioners assessing risk, the operative enforcement signals in the AD are the strict timing and the before-flight condition: failure to carry out the inspections within 50 hours or to replace/correct defects before further flight would leave the aircraft in a state that the AD identifies as non-compliant with this directive. The AD’s linkage of defects to flightworthiness (through the "before further flight" language) is the primary operational lever within the document itself.

The AD explicitly refers to an FAA airworthiness directive, stating "Note: FAA AD 2005-18-21 Amdt 39-14262 refers." That is the only cross-jurisdictional or external regulatory reference contained in the text. The AD also requires maintenance work to be performed in accordance with Raytheon Aircraft Company Safety Communique No. 261 and specific chapters of Raytheon’s Maintenance Manual and Structural Repair Manual. These references function as incorporated technical standards for the AD’s execution.

Beyond those express references, the AD does not purport to amend, repeal, or otherwise modify any other statute, regulation or rule in the text provided. The AD is a standalone directive specifying inspections and remedial action for affected Beechcraft 1900 aeroplanes and ties compliance to a date and a number of flight hours. The AD’s formal status as an instrument issued by the Civil Aviation Safety Authority situates it within the broader Australian aviation safety regulatory regime, but the AD text does not reproduce or restate the underlying statutory authority for CASA’s issuance power, nor does it set out how it interacts procedurally with airworthiness certificate regimes, operational approvals, or maintenance record-keeping obligations.

The practical interfaces to other legal or regulatory instruments that are apparent from the AD’s content are:

• Manufacturer technical documents as the operative technical standard. The AD requires compliance with Raytheon Safety Communique No. 261 and specific manual chapters. Those documents are thereby incorporated by reference as the technical means of compliance.

• An FAA counterpart AD. The FAA reference suggests parallel or corroborating action taken by another regulator; that may be relevant to operators or maintenance organisations that operate in multiple jurisdictions or rely on FAA airworthiness determinations. The AD itself contains no detail on how any differences between the CASA AD and the FAA AD are to be reconciled.

• Implicit connection to operator obligations on airworthiness and continued operation. The AD’s "before further flight" remedial requirement links the AD to operational decisions about whether an aircraft may be flown pending maintenance, but the AD does not specify the legal mechanics (for example, whether a non-compliant aircraft must be grounded by an enforcement notice) that would be used by CASA under the broader aviation safety framework.

In the provided text there are no references to broader statutory penalties, alternative compliance approvals, exemptions, or amendment mechanisms. Those interactions would need to be located in the supporting statutory or regulatory framework outside this document.

The AD text includes an identifying reference "AD/BEECH 1900/47" and sheet data "12/2005 DM" but does not record prior versions or a chain of amendments in the document provided. The AD states: "This Airworthiness Directive becomes effective on 4 October 2005" and is dated and signed 29 September 2005. There is no express amendment history, supersession clause or indication of earlier ADs being replaced or modified within the content you supplied.

The single temporal marker in the text is the effective date and the compliance window: inspections must be done "within 50 hours time in service after 4 October 2005." The AD also contains a note referencing FAA AD 2005-18-21 Amdt 39-14262, but does not state whether that FAA AD amends or is amended by other instruments.

In the absence of any listed amendments or revision notes in the provided text, the following factual observations can be drawn strictly from the document:

• The AD becomes effective on 4 October 2005; there is no prior effective date listed.

• The AD appears as a distinct issuance numbered "AD/BEECH 1900/47" and dated "12/2005 DM," which may be an internal or catalogue identifier, but no earlier AD numbers or superseded documents are included in the text.

• No subsequent amendments, revocations, replacements or continuations are recorded in the supplied material.

If a reader requires a complete amendment trail, the AD as supplied does not contain it, so one would need to consult CASA’s official AD register or subsequent ADs,sources which are outside the material provided here,to determine whether this instrument was later amended, superseded or revoked. The document provided, standing alone, contains only the original issuance data and the effective date.

The AD text provided contains no litigation history. It does not reference any judicial decisions, disputes, appeals, or legal challenges relating to the issuance, scope or application of this directive. The only adjudicative or administrative signatory information given is the signature block: "David Villiers, Delegate of the Civil Aviation Safety Authority, 29 September 2005."

Because the supplied document contains solely the directive and an explanatory background incident report, and no subsequent commentary on legal challenges or case law, there is no litigation history recorded within the AD itself. The AD does include a factual background concerning an incident reported to the FAA (binding elevator control column during takeoff; missing and loose rivets; rubbing of the elevator counterweight horn), but that is a safety incident narrative rather than a description of litigation.

Practitioners seeking litigation or adjudicative history connected to this AD will not find such information in the text provided. Any record of enforcement actions, disputes over compliance, civil or criminal prosecutions, or administrative appeals associated with this AD would be located outside the supplied document and are not reflected in the material you provided.

The AD contains several features and drafting choices that warrant careful attention by operators, maintenance organisations and legal advisers. These items are drawn strictly from the AD text and its operative mechanics.

• Narrow applicability by serial number. The AD applies only to the specifically enumerated serial numbers. The precision of the serial ranges means that compliance duties attach only to those aircraft. Operators must verify exact serial numbers; the AD lists UA-3, multiple UB, UC, UD ranges for Model 1900C and a wide UE range for Model 1900D. Misreading the serial ranges could lead to under- or over-compliance.

• Both left and right elevators. The requirement reads "Inspect all elevator hinge support attachments on both left and right elevators." The AD therefore requires a bilateral inspection even if the reported incident occurred on a single side. Failure to inspect both sides would not satisfy the AD’s terms.

• Two distinct inspection tasks with identical compliance windows. Although the two inspections concern related hardware, the AD separates them: one task is checking hinge support attachments for loose/missing rivets, the other is checking hinge joints for looseness and elevator-to-stabiliser clearance. Both must be done within 50 hours TIS after 4 October 2005. Operational planners must ensure both tasks are scheduled and recorded within that interval.

• "Before further flight" requirement for defects. The AD’s remedial language is categorical: if loose or missing rivets are evident, replace affected rivets "before further flight"; if hinge looseness or incorrect clearance is evident, "correct the discrepancies before further flight." That phrasing converts the discovery of a defect into an immediate operational constraint. Any decision to ferry an aircraft, or to defer repairs, would not comply with the AD as written.

• Reliance on Raytheon documentation. The AD requires following Raytheon Safety Communique No. 261 and specific manual chapters. Access to those documents, and use of the exact procedures they prescribe, is a compliance precondition. Operators must ensure the versions referenced are the correct ones and that maintenance personnel are trained and authorised to follow them.

• Short compliance interval. The 50 hours time in service deadline is brief and may impose urgent scheduling needs. Aircraft that are frequently used might reach that clock quickly; aircraft that are idle still have a 50-hour limit from the effective date. The AD does not provide staged compliance or extensions within the text.

• Cross-reference to FAA AD. The AD notes "FAA AD 2005-18-21 Amdt 39-14262 refers." This is useful for aligning technical expectation, but the AD does not import FAA procedures, nor does it state whether equivalency or divergence exists. Operators with international operations need to note that the CASA AD is an independent instrument even where it mirrors FAA action.

• Formatting and duplication in the source. The applicability paragraph in the supplied text has punctuation and line breaks that could cause reading errors (multiple model 1900C entries, punctuation). Care should be taken to read the serial ranges exactly as printed to identify affected aircraft.

• No procedural detail on documentation. The AD mandates inspections and repairs but does not specify the form of maintenance documentation, sign-off or record retention required to evidence compliance. Operators must therefore pay attention to general maintenance-recording obligations under applicable regulatory frameworks, even though such obligations are not spelled out in this AD.

Each of these points is dictated by the AD’s wording. They translate into operational risks if overlooked: scheduling errors, incomplete inspections, use of incorrect technical guidance, or failure to effect repairs prior to flight.

The AD prescribes a short, concrete compliance sequence that operators and maintenance organisations must follow. The steps below are derived directly from the AD language and should be carried out in that order and within the timeframes specified.

1. Verify applicability. Confirm the aircraft model and serial number against the AD’s applicability list. The AD applies to: Model 1900 serial number UA-3; Model 1900C serial numbers UB-1 through UB-74 and UC-1 through UC-174; Model 1900C serial numbers UD-1 through UD-6; and Model 1900D serial numbers UE-1 through UE-439.

2. Schedule inspections within the compliance window. Both inspections must be completed "within 50 hours time in service after 4 October 2005." Plan maintenance slots to ensure both tasks are performed within that interval.

3. Follow the prescribed technical references. For both inspections, the AD requires following Raytheon Aircraft Company Safety Communique No. 261 and Raytheon’s technical manuals: Maintenance Manual, Chapter 5-20-07 and Structural Repair Manual, Chapter 51-40-02. Obtain the exact versions of those documents referenced by the AD and ensure maintenance personnel are authorised to use them.

4. Conduct inspection A: hinge support attachments. Inspect all elevator hinge support attachments on both the left and right elevators for loose or missing rivets. Use the Raytheon procedures to determine acceptable rivet condition and inspection technique.

5. Take immediate remedial action A: rivet replacement. If loose or missing rivets are evident on any hinge support attachment, replace the affected rivets before further flight. Ensure replacement rivets and techniques conform to the Raytheon Structural Repair Manual procedures cited in the AD.

6. Conduct inspection B: hinge joints and clearances. Inspect the elevator hinge joints for looseness and measure/check the clearance of each elevator to its stabiliser, using the Raytheon guidance cited.

7. Take immediate remedial action B: correct discrepancies. If hinge looseness or incorrect clearance between the elevator and stabiliser is evident, correct those discrepancies before further flight. Apply the Structural Repair Manual procedures required by the AD for repairs and any necessary rigging.

8. Record the work. Although the AD does not prescribe specific paperwork, maintain contemporaneous maintenance records showing dates, personnel, the Raytheon documents used, findings, and corrective actions taken. These records will be needed to demonstrate compliance in the event of regulatory query.

9. Re-inspection/follow-up. The AD requires an initial inspection within 50 hours but does not describe a recurring schedule. Consider, consistent with the Raytheon guidance and the wider airworthiness regime, whether follow-up inspections or modifications are recommended in the Raytheon Communique; implement any such steps as appropriate.

10. Consider cross-jurisdictional compliance. The AD notes an FAA AD that refers. If the aircraft operates under other national jurisdictions or registries, check whether the FAA AD or equivalent instruments impose additional or different steps and reconcile actions accordingly.

11. Do not resume flight until remedied. For any defects found, the AD’s remedial language is explicit: replace or correct "before further flight." No limited or conditional allowance to ferry the aircraft is contained in the text.

12. Liaise with regulator if uncertain. The AD does not state an alternative means of compliance or appeal process in the text provided. If an operator considers an alternative method to meet the AD’s safety aim, the operator should consult CASA or seek formal guidance in accordance with the regulator’s processes (not described in the AD itself).

Following these steps, in the order and within the timeframe prescribed by the AD, implements its requirements as written. The AD’s references to Raytheon documents make access to those manufacturer materials an essential part of compliance.