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PROPOSED AD TRUE FLIGHT HOLDINGS LLC: Docket No. FAA-2021-1017; Project Identifier AD-2021-00495-A.
(a) COMMENTS DUE DATE

    The FAA must receive comments on this airworthiness directive (AD)  by
    January 18, 2022.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies to True Flight Holdings LLC Model AA-1, AA-1A,  AA-1B,
    AA-1C,  AA-5,  AA-5A,  and   AA-5B  airplanes,  all  serial   numbers,
    certificated in any category.

(d) SUBJECT

    Joint Aircraft System Component (JASC) Code 5330, Fuselage Main, Plate
    /Skin; 5512, Horizontal Stabilizer, Plate/Skin; 5522, Elevator, Plates
    /Skin Structure; 5532, Vertical Stabilizer, Plates/Skin; 5542, Rudder,
    Plate/Skin; 5730, Wing, Plates/Skins.

(e) UNSAFE CONDITION

    This AD was prompted by  corrosion and delamination of the  horizontal
    stabilizer bondlines. The FAA is issuing this AD to detect and address
    cracks, buckles, corrosion, delamination, rust, and previous repair of
    the wings,  fuselage, and  stabilizers. The  unsafe condition,  if not
    addressed,  could  result  in  reduced  structural  integrity  of  the
    affected airplane  component with  consequent loss  of control  of the
    airplane.

(f) COMPLIANCE

    Comply with this AD within the compliance times specified,  unless al-
    ready done.

(g) INSPECTION OF BONDLINES OF THE WINGS, STABILIZERS, AND AFT FUSELAGE

    Within 100 hours time-in-service after  the effective date of this  AD
    or within  12 months  after the  effective date  of this AD, whichever
    occurs first,  and thereafter  at intervals  not to  exceed 12 months,
    inspect  the  wings,  stabilizers,  and  aft  fuselage  for   bondline
    separation,  corrosion,  and  previous repair  and take  all necessary
    corrective action before further flight in accordance with  paragraphs
    A.1. through A.7.  in True Flight  Aerospace Service Bulletin  SB-195,
    Revision A, dated June 1, 2021. Pay particular attention to the  areas
    listed in paragraphs (g)(1) through (3) of this AD.

(1) Bondlines of the horizontal stabilizer outboard rib  at  the  elevator
    bearing support assembly.

(2) Bondlines of the elevator trim tab inboard rib.

(3) Bondlines and previous repairs  of the trailing edges  of the elevator
    trim tabs, elevators, rudder, ailerons, and wings.

(h) SPECIAL FLIGHT PERMITS

    Special flight permits are prohibited.

(i) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

(1) The  Manager,  Atlanta ACO Branch,  FAA,  has the authority to approve
    AMOCs for this AD, if requested  using the procedures found in 14  CFR
    39.19. In  accordance with  14 CFR  39.19, send  your request  to your
    principal  inspector  or  local Flight  Standards District  Office, as
    appropriate. If  sending information  directly to  the manager  of the
    certification  office,  send  it  to  the  attention  of  the   person
    identified in paragraph (j)(1) of this AD.

(2) Before using any approved AMOC,  notify your appropriate principal in-
    spector, or lacking  a principal inspector,  the manager of  the local
    flight standards district office/certificate holding district office.

(j) RELATED INFORMATION

(1) For  more information  about this AD,  contact  Fred Caplan,  Aviation
    Safety Engineer, Atlanta ACO Branch FAA, 1701 Columbia Avenue, College
    Park, GA 30337;  phone:  (404) 474-5507;  fax:  (404) 474-5606; email:
    frederick.n.caplan@faa.gov.

(2) For service information  identified  in this AD,  contact  True Flight
    Holdings LLC,  2300 Madison Highway, Valdosta, GA 31601;  phone: (229)
    242-6337; email: info@trueflightaerospace.com.  You may view this ref-
    erenced service information at the FAA, Airworthiness Products Section
    Operational Safety Branch, 901 Locust, Kansas City, MO 64106.  For in-
    formation on the availability of this material at the FAA,  call (816)
    329-4148.

Issued on November 23, 2021. Lance T Gant, Director, Compliance & Airworth
-iness Division, Aircraft Certification Service.

DATES: The FAA must receive comments  on this proposed AD  by  January 18,
2022.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2021-1017; Project Identifier AD-2021-00495-A]
RIN 2120-AA64

Airworthiness Directives; True Flight Holdings LLC Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

-----------------------------------------------------------------------

SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for all True Flight Holdings LLC Model AA-1, AA-1A, AA-1B, AA-1C, AA-5,
AA-5A, and AA-5B airplanes. This proposed AD was prompted by the report
of an accident of an airplane with bondline corrosion and delamination
of the horizontal stabilizers. This proposed AD would require
inspecting the wings, fuselage, and stabilizers for bondline
separation, corrosion, and previous repair. This AD would also require
repairing or replacing parts and applying corrosion inhibitor as
necessary. The FAA is proposing this AD to address the unsafe condition
on these products.

DATES: The FAA must receive comments on this proposed AD by January 18,
2022.

ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions
for submitting comments.
Fax: (202) 493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
For service information identified in this NPRM, contact True
Flight Holdings LLC, 2300 Madison Highway, Valdosta, GA 31601; phone:
(229) 242-6337; email: info@trueflightaerospace.com. You may view this
service information at the FAA, Airworthiness Products Section,
Operational Safety Branch, 901 Locust, Kansas City, MO 64106. For
information on the availability of this material at the FAA, call (816)
329-4148. It is also available at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-1017.

Examining the AD Docket


You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-1017; or in person at
Docket Operations between 9 a.m. and 5 p.m., Monday through Friday,
except Federal holidays. The AD docket contains this NPRM, any comments
received, and other information. The street address for Docket
Operations is listed above.

FOR FURTHER INFORMATION CONTACT: Fred Caplan, Aviation Safety Engineer,
Atlanta ACO Branch, FAA, 1701 Columbia Avenue, College Park, GA 30337;
phone: (404) 474-5507; fax: (404) 474-5606; email:
frederick.n.caplan@faa.gov.

SUPPLEMENTARY INFORMATION:

Comments Invited

The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under ADDRESSES. Include ``Docket No. FAA-2021-1017; Project Identifier
AD-2021-00495-A'' at the beginning of your comments. The most helpful
comments reference a specific portion of the proposal, explain the
reason for any recommended change, and include supporting data. The FAA
will consider all comments received by the closing date and may amend
this proposal because of those comments.
Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
https://www.regulations.gov, including any personal information you
provide. The agency will also post a report summarizing each
substantive verbal contact received about this NPRM.

Confidential Business Information


CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this NPRM contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this NPRM, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this NPRM. Submissions containing CBI should be sent to Fred
Caplan, Aviation Safety Engineer, Atlanta ACO Branch, FAA, 1701
Columbia Avenue, College Park, GA 30337. Any commentary that the FAA
receives which is not specifically designated as CBI will be placed in
the public docket for this rulemaking.

Background

The FAA received a report of an accident involving a True Flight
Holdings LLC Model AA-5 airplane that occurred on January 19, 2021.
During flight, the outboard elevator attach bracket on the horizontal
stabilizer detached, causing loss of elevator control, flutter, and
significant damage to the airplane. An investigation identified
corrosion and delamination of the airplane skin bondlines around the
area of the horizontal stabilizer where the elevator attach bracket was
attached, as well as on the trailing edge of the elevator trim tab.
Field reports have identified additional instances of corrosion and
delamination of skin bondlines around the horizontal stabilizer and
other primary structures.
Model AA-1, AA-1A, AA-1B, AA-1C, AA-5, AA-5A, and AA-5B airplanes
are similar in design and are constructed using a metal-to-metal
bonding process. While the bond adhesive remains structurally sound
throughout the aging process, factors such as corrosion and freezing
moisture may compromise the structural integrity of some of the bond
joints. This can lead to delamination of the skin from the primary
structure.
Field reports indicate that bondline inspections are not being
adequately performed during routine inspections, which emphasize a
visual scanning for problem areas. However, damage can exist with no
visual indications, and a mechanic might miss damage in a hidden area.
The FAA has determined that a more thorough inspection procedure is
necessary to reliably identify corrosion and delamination of bondlines
in these critical areas.
This condition, if not addressed, could result in reduced
structural integrity of the affected airplane component, with
consequent loss of control of the airplane. The FAA is proposing this AD to
address the unsafe condition on these products.

FAA's Determination

The FAA is issuing this NPRM after determining that the unsafe
condition described previously is likely to exist or develop on other
products of the same type design.

Related Service Information Under 1 CFR Part 51


The FAA reviewed True Flight Aerospace Service Bulletin SB-195,
Revision A, dated June 1, 2021 (True Flight SB-195A). This service
information specifies procedures for inspecting the primary structure
and flight controls for bondline separation and corrosion and repairing
or replacing parts and applying corrosion inhibitor as necessary.
This service information is reasonably available because the
interested parties have access to it through their normal course of
business or by the means identified in ADDRESSES.

Other Related Service Information

The FAA also reviewed True Flight Aerospace Service Kit 125,
Revision B. This service information specifies procedures for repairing
bondline delamination of flight controls and structures.

Proposed AD Requirements in This NPRM

This proposed AD would require accomplishing the actions specified
in True Flight SB-195A as already described, except as discussed under
``Differences Between the AD and the Service Information.''

Differences Between This Proposed AD and the Service Information

This proposed AD would only require the Part A inspections, and not
the Part B inspection, from True Flight SB-195A. In addition, True
Flight SB-195A specifies reporting information to the manufacturer, and
this proposed AD would not.

Costs of Compliance

The FAA estimates that this AD, if adopted as proposed, would
affect 2,466 airplanes of U.S. registry.
The FAA estimates the following costs to comply with this proposed
AD:

Estimated costs

Action
Labor cost
Parts cost
Cost per airplane
Cost on U.S. operators
Inspect for delamination and corrosion 8 work-hours x $85 per hour = $680 per inspection cycle Not applicable $680 per inspection cycle $1,676,880 per inspection cycle

The FAA estimates that it would take 3 work-hours at $85 per work-
hour to do the proposed corrosion inhibitor treatment. Parts would cost
$104 for a total proposed cost of $359 per airplane. In addition, there
could be a wide range of areas that may require repair (fuselage,
stabilizers, and wings) for the delaminated bondlines and/or corrosion
with potential replacement of the entire component. The FAA has no way
of determining the number of airplanes that might need these repairs or
the exact costs for corrective actions needed as a result of the
proposed inspection, as the damage may vary significantly from airplane
to airplane.

Authority for This Rulemaking

Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on products identified in this rulemaking action.

Regulatory Findings

The FAA determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would not
have a substantial direct effect on the States, on the relationship
between the national government and the States, or on the distribution
of power and responsibilities among the various levels of government.
For the reasons discussed above, I certify this proposed
regulation:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Would not affect intrastate aviation in Alaska, and
(3) Would not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.

The Proposed Amendment

Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

1. The authority citation for part 39 continues to read as follows:

Authority: 49 U.S.C. 106(g), 40113, 44701.

Sec. 39.13 [Amended]

2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive: