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PROPOSED AD HOFFMANN GMBH & CO. KG: Docket No. FAA-2022-0980; Project Identifier MCAI-2022-00448-P.
(a) COMMENTS DUE DATE

    The FAA  must receive  comments on  this airworthiness  directive (AD)
    action by September 15, 2022.

(b) AFFECTED ADS

    This  AD  replaces AD  2021-23-17,  Amendment 39-21815  (86  FR 68905,
    December 6, 2021) (AD 2021-23-17).

(c) APPLICABILITY

    This AD applies  to Hoffmann GmbH  & Co. KG  (Hoffmann) model HO-V  72
    propellers.

(d) SUBJECT

    Joint  Aircraft  System  Component  (JASC)  Code  6114,  Propeller Hub
    Section.

(e) UNSAFE CONDITION

    This AD was  prompted by reports  of cracks at  different positions on
    two affected  propeller hubs.  The FAA  is issuing  this AD to prevent
    failure of the propeller hub. The unsafe condition, if not  addressed,
    could result in release of the propeller, damage to the airplane,  and
    injury to persons on the ground.

(f) COMPLIANCE

    Comply  with this  AD within  the compliance  times specified,  unless
    already done.

(g) REQUIRED ACTIONS

(1) Before the next flight after December 22, 2020  (the effective date of
    AD 2020-25-05, Amendment  39-21347 (85 FR  78702, December 7,  2020)),
    amend the  emergency or  abnormal procedures  section of  the existing
    aircraft flight  manual by  inserting this  text: "Abnormal  propeller
    vibrations: As applicable, reduce engine RPM."

(2) Before the next flight  after January 10, 2022  (the effective date of
    AD  2021-23-17),  and thereafter,  before  the next  flight  after any
    flight  where  abnormal propeller  vibrations  have been  experienced,
    visually inspect  propeller hub  HO-V 72  ( )  ( )-(  )-( ) for cracks
    using  paragraph  2.1 of  Hoffmann  Propeller GmbH  &  Co. KG  Service
    Bulletin SB E53, Rev. D,  dated February 18, 2021 (Hoffmann  Propeller
    SB E53 Rev. D).

(3) Within 20 flight hours (FHs)  after  January 10, 2022  (the  effective
    date  of  AD  2021-23-17),   perform  a  non-destructive  test   (NDT)
    inspection of propeller hub  HO-V 72 ( )  ( )-( )-( )  using paragraph
    2.3 of Hoffmann Propeller SB E53 Rev. D.

(4) During each overhaul  of  propeller hub  HO-V 72 ( ) ( )-( )-( ) after
    January 10, 2022 (the effective date of AD 2021-23-17), perform an NDT
    inspection using paragraph 2.3 of Hoffmann Propeller SB E53 Rev. D.

(5) Within 30 days after the effective date of this AD, review the mainte-
    nance  records  to confirm  the  propeller blade  retention  nuts were
    tightened at the last in-shop  maintenance visit to the torque  values
    in paragraph 5 of Hoffmann  Propeller Service Bulletin SB057 C,  dated
    February 22, 2022 (Hoffmann Propeller SB057 C).

(6) If, during the records review required by paragraph (g)(5) of this AD,
    it is  determined that  the propeller  blade retention  nuts were  not
    tightened to the  torque values in  paragraph 5 of  Hoffmann Propeller
    SB057 C, or  it cannot be  confirmed if the  propeller blade retention
    nuts were tightened  to the torque  values in paragraph  5 of Hoffmann
    Propeller SB057 C, perform the following actions:

(i) Within 90 FHs  after the effective date of this AD,  tighten each pro-
    peller blade  retention nut  to the  torque values  in paragraph  5 of
    Hoffmann  Propeller SB057  C,  using  paragraphs 6  and 7  of Hoffmann
    Propeller Service Bulletin SB059 B, dated February 23, 2022.

(ii) Before the next flight after the effective date of this AD and there-
     after, before each flight until the propeller blade retention nut  is
     tightened to the torque values  in paragraph 5 of Hoffmann  Propeller
     SB057 C, as required by paragraph (g)(6)(i) of this AD, confirm  that
     there is no  axial play in  the blade retention  system by inspecting
     the propeller blade for shake. If any axial play is detected,  remove
     the  propeller from  service and  perform  an  NDT inspection  of the
     propeller hub using paragraph 2.3  of Hoffmann Propeller SB E53  Rev.
     D.

(7) If, during any inspection  required  by  paragraph (g)(2), (3), (4) or
    (6)(ii) of this AD, any crack is detected,  replace propeller hub HO-V
    72 ( ) ( )-( )-( ) with a part eligible for installation.

(h) DEFINITION

    For the purpose of  this AD, a "part  eligible for installation" is  a
    propeller hub HO-V 72 ( ) ( )-( )-( ) with zero hours time since  new,
    or a propeller  hub HO-V 72  ( ) (  )-( )-( )  that has passed  an NDT
    inspection using paragraph 2.3 of Hoffmann Propeller SB E53 Rev. D.

(i) NON-REQUIRED ACTIONS

(1) Sending the propeller to Hoffmann for investigation,  as  contained in
    paragraph 2.1 of Hoffmann Propeller SB E53 Rev. D,  is not required by
    this AD.

(2) Reporting propeller hubs with cracks to Hoffmann, as contained in par-
    agraph 2.3 of Hoffmann Propeller SB E53 Rev. D,  is  not  required  by
    this AD.

(j) CREDIT FOR PREVIOUS ACTIONS

(1) You may take credit  for the initial visual inspection and NDT inspec-
    tion of the propeller hub  required by paragraphs (g)(2), (3), and (4)
    of this AD if you performed  any of these actions  before  January 10,
    2022  (the effective date of AD 2021-23-17)  using  Hoffmann Propeller
    GmbH & Co. KG SB E53,  Rev. A,  dated October 9, 2020;  Rev. B,  dated
    October 14, 2020; or Rev. C, dated December 9, 2020.

(2) You may take credit for the records review  to  confirm  the propeller
    blade retention nuts were tightened  to the torque values as  required
    by paragraph (g)(5) of this  AD, and the tightening of  each propeller
    blade retention nut as required  by paragraph (g)(6)(i) of this  AD if
    you performed any of these  actions before the effective date  of this
    AD during the last in-shop maintenance visit using Hoffmann  Propeller
    Service Bulletin SB057 B,  dated February 8, 2022;  Hoffmann Propeller
    Service  Bulletin  SB059  A,  dated  February  11,  2022;  or Hoffmann
    Propeller Service Bulletin SB059 B, dated February 23, 2022.

(k) SPECIAL FLIGHT PERMIT

    A special flight permit may be issued in accordance with 14 CFR 21.197
    and 21.199 to  operate the airplane  to a service  facility to perform
    the NDT inspection. Special  flight permits are prohibited  to perform
    the visual inspection of the propeller hub.

(l) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

(1) The  Manager,  Boston 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 (m)(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.

(m) RELATED INFORMATION

(1) For more information about this AD,  contact Michael Schwetz, Aviation
    Safety Engineer, Boston ACO Branch FAA, 1200 District Avenue, Burling-
    ton, MA 01803;  phone: (781) 238-7761;  email: 9-AVS-AIR-BACO-COS@faa.
    gov.

(2) Refer to European Union Aviation Safety Agency  (EASA)  AD  2022-0061,
    dated April 4, 2022, for more information. You may examine the EASA AD
    in the AD docket at www.regulations.gov  by searching for and locating
    it in Docket No. FAA-2022-0980.

(3) For service information identified in this AD, contact Hoffmann GmbH &
    Co. KG, Kupferlingstrasse 9, 83022,  Rosenheim, Germany;  phone: +49 0
    8031 1878 0; email: info@hoffmann-prop.com; website: https://hoffmann-
    prop.com. You may view this referenced service information at the FAA,
    Airworthiness Products Section,  Operational Safety Branch,  1200 Dis-
    trict Avenue, Burlington, MA 01803. For information on the availabili-
    ty of this material at the FAA, call (817) 222-5110.

Issued on July 22, 2022.  Christina Underwood, Acting Director, Compliance
& Airworthiness Division, Aircraft Certification Service.

DATES: The FAA must receive comments on this proposed AD  by September 15,
2022.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2022-0980; Project Identifier MCAI-2022-00448-P]
RIN 2120-AA64

Airworthiness Directives; Hoffmann GmbH & Co. KG Propellers

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD)
2021-23-17, which applies to all Hoffmann GmbH & Co. KG (Hoffmann)
model HO-V 72 propellers. AD 2021-23-17 requires amending the existing
aircraft flight manual (AFM) by inserting abnormal propeller vibration
instructions, visual inspection and non-destructive test (NDT)
inspection of the propeller hub and, depending on the results of the
inspections, replacement of the propeller hub with a part eligible for
installation. Since the FAA issued AD 2021-23-17, further investigation
by the manufacturer revealed that cracks found on propeller hubs likely
resulted from propeller blade retention nuts that were not tightened
using published service information during blade installation. This
proposed AD would retain the required actions of AD 2021-23-17. This
proposed AD would also require a maintenance records review and,
depending on the results of the maintenance records review, tightening
of each propeller blade retention nut to specific torque values.
Depending on the results of the maintenance records review, this
proposed AD would require physically inspecting the propeller blade for
shake. If any axial play is detected during the performance of the
inspection, this proposed AD would require the removal of the propeller
from service and the performance of an NDT inspection of the propeller
hub. 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 September
15, 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 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 Hoffmann
GmbH & Co. KG, Kupferlingstrasse 9, 83022, Rosenheim, Germany;
phone: +49 0 8031 1878 0; email: info@hoffmann-prop.com; website:
https://hoffmann-prop.com. You may view this service information at the
FAA, Airworthiness Products Section, Operational Safety Branch, 1200
District Avenue, Burlington, MA 01803. For information on the
availability of this material at the FAA, call (817) 222-5110.

Examining the AD Docket

You may examine the AD docket at www.regulations.gov by searching
for and locating Docket No. FAA-2022-0980; 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, the mandatory
continuing airworthiness information (MCAI), any comments received, and
other information. The street address for Docket Operations is listed
above.

FOR FURTHER INFORMATION CONTACT: Michael Schwetz, Aviation Safety
Engineer, Boston ACO Branch, FAA, 1200 District Avenue, Burlington, MA
01803; phone: (781) 238-7761; email: 9-AVS-AIR-BACO-COS@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-2022-0980; Project Identifier
MCAI-2022-00448-P'' 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
the 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
www.regulations.gov, including any personal information you provide.
The agency will also post a report summarizing each substantive verbal
contact we receive about this proposed AD.

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
Michael Schwetz, Aviation Safety Engineer, Boston ACO Branch, FAA, 1200
District Avenue, Burlington, MA 01803. 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 issued AD 2021-23-17, Amendment 39-21815 (86 FR 68905,
December 6, 2021), (AD 2021-23-17), for all Hoffmann GmbH & Co. KG
model HO-V 72 propellers. AD 2021-23-17 was prompted by reports of
cracks at different positions on two affected propeller hubs. AD 2021-
23-17 requires amending the existing AFM by inserting abnormal
propeller vibration instructions, visual inspection and NDT inspection
of the propeller hub and, depending on the results of the inspections,
replacement of the propeller hub with a part eligible for installation.
The agency issued AD 2021-23-17 to prevent failure of the propeller
hub.

Actions Since AD 2021-23-17 Was Issued

Since the FAA issued AD 2021-23-17, the European Union Aviation
Safety Agency (EASA), which is the Technical Agent for the Member
States of the European Community, has issued EASA AD 2022-0061, dated
April 4, 2022 (referred to after this as ``the MCAI''), to address the
unsafe condition on these products. The MCAI states:

Cracks have been reported at different positions on two affected
parts, both installed on Slingsby T67 ``Firefly'' aeroplanes. One
crack was found during scheduled inspection, the other crack during
an unscheduled inspection after abnormal vibrations occurred.
Subsequent investigation determined that improper tightening of
blade nuts has caused or contributed to those events.
This condition, if not detected and corrected, could lead to in-
flight propeller detachment, possibly resulting in damage to the
aeroplane and/or injury to persons on the ground.
To address this potential unsafe condition, Hoffmann Propeller
issued the SB, providing applicable instructions, and EASA issued
Emergency AD 2020-0226-E (later revised [to EASA AD 2020-0226R1]) to
require inspections of affected parts and, depending on findings,
replacement. That AD also required, for certain aeroplanes,
amendment of the applicable Aircraft Flight Manual (AFM).
Since that [EASA] AD was issued, further investigation revealed
that not all propeller blade nuts were tightened in accordance with
the Hoffman Propeller blade nut tightening procedure B2.23 which
requires a certain over-torquing and loosening of the blade nut to
limit a preload reduction due to material settlement. Prompted by
this development, Hoffmann Propeller issued SB057 (incorporating
blade nut tightening procedure B2.23) providing torquing
instructions, and SB58 providing instructions for setting correct
counterweight angles. Additionally, Hoffmann Propeller issued the
torque tightening SB (referencing SB57 and SB58) providing
inspections and corrective action instructions.
For the reasons described above, this [EASA] AD retains the
requirements of EASA AD 2020-0226R1, which is superseded, and
requires additional blade checks, inspections, and re-tightening of
the propeller blade nuts.

You may obtain further information by examining the MCAI in the AD
docket at www.regulations.gov by searching for and locating Docket No.
FAA-2022-0980.

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 the following service information:
Hoffmann Propeller Service Bulletin SB057 C, dated
February 22, 2022. This SB specifies procedures for tightening the
propeller blade retention nut.
Hoffmann Propeller Service Bulletin SB059 B, dated
February 23, 2022. This SB specifies procedures for tightening the
propeller blade retention nut with the correct torque and inspecting
the propeller blade for shake.
This proposed AD would also require Hoffmann Propeller GmbH & Co.
KG Service Bulletin SB E53 Rev. D, dated February 18, 2021, which was
previously approved by the Director of the Federal Register for
incorporation by reference on January 10, 2022 (86 FR 68905, December
6, 2021). The service bulletin describes procedures for visual and NDT
inspections of the propeller hub for cracks.
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 reviewed the following service information:
Hoffmann Propeller Service Bulletin SB058 A, dated
February 2, 2022. This SB specifies the updated definition of the
counterweight angle.

Proposed AD Requirements in This NPRM

This proposed AD would retain all of the requirements of AD 2021-
23-17. This proposed AD would also require a maintenance records review
and, depending on the results of the maintenance records review,
tightening of each propeller blade retention nut to specified torque
values. Depending on the results of the maintenance records review,
this proposed AD would require initial and repetitive physical
inspections of the propeller blade for shake. If any axial play is
detected during inspection, this proposed AD would require the removal
of the propeller from service and the performance of an NDT inspection
of the propeller hub.

Costs of Compliance

The FAA estimates that this AD, if adopted as proposed, would
affect 35 propellers installed on 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 product
Cost on U.S. operators
Amend AFM 1 work-hour x $85 per hour = $85
$0
$85
$2,975
Visually inspect propeller hub 1 work-hour x $85 per hour = $85
0
85
2,975
NDT inspect propeller hub 8 work-hours x $85 per hour = $680
0
680
23,800
Review maintenance records 0.5 work-hours x $85 per hour = $42.50
0
42.50
1,487.50

The FAA estimates the following costs to do any necessary actions
that would be required based on the results of the proposed
inspections. The agency has no way of determining the number of
aircraft that might need these actions:

On-Condition Costs

Action
Labor cost
Parts cost
Cost per product
Replace propeller hub 5 work-hours x $85 per hour = $425
$1,600
$2,025
Inspect propeller blade for shake 0.25 work-hours x $85 per hour = $21.25
0
21.25
Tighten propeller blade retention nuts 2 work-hours x $85 per hour = $170
0
170

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 that the 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:

a. Removing Airworthiness Directive 2021-23-17, Amendment 39-21815 (86
FR 68905, December 6, 2021); and

b. Adding the following new airworthiness directive: