Airworthiness Directive 2013-14-09

one-time
Official AD 2013-14-09 · FR doc 2013-18771 · 2013-08-06 · airframe

Airworthiness Directives; Bombardier, Inc. Airplanes

What this AD requires

We are superseding airworthiness directive (AD) 2012-14-04 for certain Bombardier, Inc. Model DHC-8-100, -200, and -300 series airplanes. AD 2012-14-04 required replacing certain parking brake accumulators. This new AD retains this requirement. This new AD also requires installing restraint devices around the parking brake accumulator end caps. We are issuing this AD to prevent failure of a parking brake accumulator screw cap or end cap resulting in loss of the number 2 hydraulic system and damage to airplane structures, which could adversely affect the controllability of the airplane.

Which aircraft AD 2013-14-09 applies to

Models-101, -102, -103, -106, -201, -202, -301, -311, -315, DHC-8
Serial-conditional — narrows to serials 003–?.

Applies to serial numbers 003 and subsequent (open-ended). NOTE: the applicability text returned by prep_slice.py for this AD was a mis-sliced excerpt (Costs of Compliance / Regulatory Findings section, concerning a parking brake accumulator, superseding AD 2012-14-04). The fields above were sourced from the AD's actual Applicability paragraph via federalregister.gov (FR Doc 2013-18771, 78 FR 47543, published 2013-08-20).

Whether AD 2013-14-09 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

How AD compliance is recorded

A valid compliance record (14 CFR 43.9) states:

Method of complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 2013-14-09 complied with on your aircraft?

Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.

Look up a tail number →Read the full directive (Federal Register)

Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.