Airworthiness Directives; Aspen Avionics, Inc.

[Federal Register Volume 85, Number 148 (Friday, July 31, 2020)]
[Rules and Regulations]
[Pages 45990-45993]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2020-16592]


=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2020-0723; Project Identifier AD-2020-00586-Q; 
Amendment 39-21192; AD 2020-16-08]
RIN 2120-AA64


Airworthiness Directives; Aspen Avionics, Inc.

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments.

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

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for 
certain Aspen Avionics, Inc., Evolution Flight Display (EFD) EFD1000 
Emergency Backup Display, EFD1000 Multi-Function Display, and EFD1000 
Primary Flight Display systems installed on various airplanes. This AD 
imposes operating restrictions on these display systems by revising the 
Limitations section of the airplane flight manual (AFM). This AD was 
prompted by an automatic reset occurring when the display internal 
monitor detects a potential fault, causing intermittent loss of 
airspeed, attitude, and altitude information during flight. The FAA is 
issuing this AD to address the unsafe condition on these products.

DATES: This AD is effective August 17, 2020.
    The FAA must receive comments on this AD by September 14, 2020.

ADDRESSES: You may send comments, using the procedures found in 14 CFR 
11.43 and 11.45, by any of the following methods:
    <bullet> Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
    <bullet> Fax: 202-493-2251.
    <bullet> 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.
    <bullet> Hand Delivery: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE, Washington, DC 20590, between 9 a.m. and 5 p.m., 
Monday through Friday, except Federal holidays.

Examining the AD Docket

    You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2020-
0723; 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 final rule, the regulatory evaluation, any comments received, and 
other information. The street address for the Docket Operations is 
listed above. Comments will be available in the AD docket shortly after 
receipt.
    For service information identified in this final rule, contact 
Aspen Avionics, Inc. at either address: 5001 Indian School Rd. NE, 
Suite 100, Albuquerque, NM 87110; or 19820 N 7th Street, Suite 150, 
Phoenix, AZ 85024; telephone: 1 (888) 992-7736; internet: https://aspenavionics.com/contact/.

FOR FURTHER INFORMATION CONTACT: Mahmood Shah, Aerospace Engineer, Fort 
Worth ACO Branch, FAA, 10101 Hillwood Pkwy, Fort Worth, TX 76177; 
phone: 817-222-5133; fax: 817-222-5960; email: [email protected].

SUPPLEMENTARY INFORMATION:

Discussion

    On February 25, 2020, Aspen Avionics, Inc. (Aspen), notified the 
FAA of 35 instances of software interacting with a graphics processing 
chip defect and causing an automatic reset to occur on Aspen EFD1000 
Emergency Backup Display, EFD1000 Multi-Function Display, and EFD1000 
Primary Flight Display systems. The reset occurs when the display 
internal monitor detects a potential fault. The display will go black 
and then it will restart, which lasts about 50 seconds. In 
installations where multiple Aspen EFDs serve as the primary and backup 
attitude, altitude, and airspeed displays instead of independent 
instruments; this repeat resetting may affect both Aspen units, 
resulting in loss of all attitude, altitude, and airspeed information 
during the reset period. Loss of all airspeed, attitude, and altitude 
information during flight may cause a loss of control of the airplane 
in instrument meteorological conditions (IMC) or at night. The actions 
required by this AD will restrict operations to flight under visual 
flight rules (VFR) and prohibit night operations to allow safe 
operation in the event of a loss of flight display functionality.

[[Page 45991]]

Related Service Information

    The FAA reviewed Aspen Operator Advisory OA2020-01, dated March 3, 
2020. This document advises operators of the automatic reset event and 
provides recommended operating limitations.
    The FAA also reviewed Aspen Service Bulletin Number: SB2020-01, 
dated April 1, 2020. This document provides instructions for updating 
the EFD software to correct the automatic reset issue. This AD does not 
apply to airplanes that are compliant with this service information.

FAA's Determination

    The FAA is issuing this AD because it evaluated all the relevant 
information and determined the unsafe condition described previously is 
likely to exist or develop in other products of the same type design.

AD Requirements

    This AD requires revising the AFM limitations section to add 
language restricting operations to Day VFR only, either by making a pen 
and ink change or by inserting a copy of this AD.

FAA's Justification and Determination of the Effective Date

    An unsafe condition exists that requires the immediate adoption of 
this AD without providing an opportunity for public comments prior to 
adoption. The FAA has found that the risk to the flying public 
justifies waiving notice and comment prior to adoption of this rule 
because intermittent loss of attitude, altitude, and airspeed 
information during flight could result in loss of control of the 
airplane in IMC or at night. The required corrective actions must be 
accomplished before further flight, which does not allow the time 
necessary for the public to comment and for publication of the final 
rule. Therefore, the FAA finds good cause that notice and opportunity 
for prior public comment are impracticable. In addition, for the reason 
stated above, the FAA finds that good cause exists for making this 
amendment effective in less than 30 days.

Comments Invited

    This AD is a final rule that involves requirements affecting flight 
safety and was not preceded by notice and an opportunity for public 
comment. However, we invite you to send any written data, views, or 
arguments about this final rule. Send your comments to an address 
listed under the ADDRESSES section. Include the Docket Number FAA-2020-
0711 and Product Identifier MCAI-2020-00719-A at the beginning of your 
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 we receive, without change, to 
https://www.regulations.gov, including any personal information you 
provide. The FAA will also post a report summarizing each substantive 
verbal contact we receive about this final rule.

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 AD 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 AD, 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 AD. Submissions containing CBI should be sent to Mahmood 
Shah, Aerospace Engineer, Fort Worth ACO Branch, FAA, 10101 Hillwood 
Pkwy, Fort Worth, TX 76177. Any commentary that the FAA receives which 
is not specifically designated as CBI will be placed in the public 
docket for this rulemaking.

Costs of Compliance

    The FAA estimates that this AD affects 900 airplanes of U.S. 
registry.
    The FAA estimates the following costs to comply with this AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                     Cost per      Cost on U.S.
               Action                         Labor cost            Parts cost        product        operators
----------------------------------------------------------------------------------------------------------------
Revise Flight Manual...............  0.25 work-hour x $85.00 per           $0.00          $21.25      $19,125.00
                                      hour = $21.25.
----------------------------------------------------------------------------------------------------------------

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 Flexibility Act

    The requirements of the Regulatory Flexibility Act (RFA) do not 
apply when an agency finds good cause pursuant to 5 U.S.C. 553 to adopt 
a rule without prior notice and comment. Because FAA has determined 
that it has good cause to adopt this rule without notice and comment, 
RFA analysis is not required.

Regulatory Findings

    This AD will not have federalism implications under Executive Order 
13132. This AD will 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 this AD:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866, and
    (2) Will not affect intrastate aviation in Alaska.

List of Subjects in 14 CFR Part 39

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

Adoption of the Amendment

    Accordingly, under the authority delegated to me by the 
Administrator,

[[Page 45992]]

the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
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]

0
2. The FAA amends Sec.  39.13 by adding the following new airworthiness 
directive (AD):

2020-16-08 Aspen Avionics, Inc.: Amendment 39-21192; Docket No. FAA-
2020-0723; Project Identifier AD-2020-00586-Q.

(a) Effective Date

    This AD is effective August 17, 2020.

(b) Affected ADs

    None.

(c) Applicability

    (1) This AD applies to Aspen Avionics, Inc., Evolution Flight 
Display (EFD) EFD1000 Primary Flight Display part number (P/N) 910-
00001-011, EFD1000 Multi-Function Display P/N 910-00001-012, and 
EFD1000 Emergency Backup Display P/N 910-00001-017 units that meet 
both conditions in paragraphs (c)(1)(i) and (ii) of this AD.
    (i) Software version 2.10 or 2.10.1 is installed;
    (ii) Independent attitude, altitude, and airspeed back-up 
instruments are not installed.
    (2) These flight display units may be installed on, but are not 
limited to, the following airplanes, certificated in any category:
    (i) Aermacchi S.p.A. Model S.205-18/F, S.205-18/R, S.205-20/F, 
S.205-20/R, S.205-22/R, S.208, and S.208A airplanes;
    (ii) Aeronautica Macchi S.p.A. Model AL 60 (previously 
designated as Model LASA 60), AL 60-B, AL 60-C5, and AL 60-F5 
airplanes;
    (iii) Aerostar Aircraft Corporation Model PA-60-600 (Aerostar 
600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P), and PA-
60-602P (Aerostar 602P) airplanes;
    (iv) Alexandria Aircraft, LLC (type certificate previously held 
by Bellanca, Inc.), Model 14-19, 14-19-2, 14-19-3, 14-19-3A, 17-30, 
17-30A, 17-31, 17-31A, 17-31ATC, and 17-31TC airplanes;
    (v) American Champion Aircraft Corp. Model 402, 7ECA, 7GCAA, 
7GCBC, 7KCAB, 8GCBC, and 8KCAB airplanes;
    (vi) CEAPR (type certificate previously held by APEX) Model CAP 
10 B airplanes;
    (vii) Cirrus Design Corporation Model SR20 and SR22 airplanes;
    (viii) Commander Aircraft Corporation (type certificate 
previously held by CPAC, Inc.) Model 112, 112B, 112TC, 112TCA, 114, 
114A, 114B, and 114TC airplanes;
    (ix) Consolidated Vultee Aircraft Corporation, Stinson Division 
Model V-77 (Army AT-19) airplanes;
    (x) Cougar Aircraft Corporation (type certificate previously 
held by SOCATA, S.A.) Model GA-7 airplanes;
    (xi) Diamond Aircraft Industries Inc. Model DA20-A1 and DA20-C1 
airplanes;
    (xii) Diamond Aircraft Industries Inc. (type certificate 
previously held by Diamond Aircraft Industries GmbH) Model DA 40 and 
DA 40 F airplanes;
    (xiii) Discovery Aviation, Inc. (type certificate previously 
held by Liberty Aerospace Incorporated), Model XL-2 airplanes;
    (xiv) Dynac Aerospace Corporation Model Aero Commander 100, Aero 
Commander 100A, Aero Commander 100-180, Volaire 10, and Volaire 10A 
airplanes;
    (xv) EADS-PZL ``Warszawa-Okecie'' S.A. (type certificate 
previously held by Panstwowe Zaklady Lotnicze) Model PZL-104 WILGA 
80, PZL-104M WILGA 2000, PZL-104MA WILGA 2000, PZL-KOLIBER 150A, and 
PZL-KOLIBER 160A airplanes;
    (xvi) Extra Flugzeugproduktions- und Vertriebs- GmbH (type 
certificate previously held by Extra Flugzeugbau GmbH) Model EA 300, 
EA 300/L, EA 300/S, EA 300/200, and EA 300/LC airplanes;
    (xvii) Frakes Aviation Model G-44 (Army OA-14, Navy J4F-2), G-
44A, and SCAN Type 30 airplanes;
    (xviii) FS 2003 Corporation (type certificate previously held by 
The New Piper Aircraft, Inc.) Model PA-12 and PA-12S airplanes;
    (xix) GROB Aircraft AG (type certificate previously held by GROB 
Aerospace GmbH i.l.) Model G115, G115A, G115B, G115C, G115C2, G115D, 
G115D2, G115EG, and G120A airplanes;
    (xx) Helio Aircraft, LLC, Model H-250, H-295 (USAF U-10D), H-391 
(USAF YL-24), H-391B, H-395 (USAF L-28A and U-10B), H-395A, H-700, 
H-800, HST-550, HST-550A (USAF AU-24A), and HT-295 airplanes;
    (xxi) Interceptor Aviation Inc. (type certificate previously 
held by Interceptor Aircraft Corporation) Model 200, 200A, 200B, 
200C, 200D, and 400 airplanes;
    (xxii) Lockheed Martin Aeronautics Company Model 402-2 
airplanes;
    (xxiii) Maule Aerospace Technology, Inc. (type certificate 
previously held by Maule Aircraft Corporation), Model Bee Dee M-4, 
M-4, M-4C, M-4S, M-4T, M-4-180C, M-4-180S, M-4-180T, M-4-210, M-4-
210C, M-4-210S, M-4-210T, M-4-220, M-4-220C, M-4-220S, M-4-220T, M-
5-180C, M-5-200, M-5-210C, M-5-210TC, M-5-220C, M-5-235C, M-6-180, 
M-6-235, M-7-235, M-7-235A, M-7-235B, M-7-235C, M-7-260, M-7-260C, 
M-7-420A, M-7-420AC, M-8-235, MT-7-235, MT-7-260, MT-7-420, MX-7-
160, MX-7-160C, MX-7-180, MX-7-180A, MX-7-180AC, MX-7-180B, MX-7-
180C, MX-7-235, MX-7-420, MXT-7-160, MXT-7-180, and MXT-7-180A 
airplanes;
    (xxiv) Mooney Aircraft Corporation Model M22 airplanes;
    (xxv) Mooney International Corporation (type certificate 
previously held by Mooney Aviation Company, Inc.) Model M20, M20A, 
M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20M, M20R, 
M20S, M20TN, M20U, and M20V airplanes;
    (xxvi) Pacific Aerospace Ltd. (type certificate previously held 
by Found Aircraft Canada, Inc.) Model FBA-2C, FBA-2C1, and FBA-2C2 
airplanes;
    (xxvii) Pilatus Aircraft Ltd. Model PC-6, PC-6-H1, PC-6-H2, PC-
6/350, PC-6/350-H1, PC-6/350-H2, PC6/A, PC-6/A-H1, PC-6/A-H2, PC-6/
B-H2, PC-6/B1-H2, PC-6/B2-H2, PC-6/B2-H4, PC-6/C-H2, and PC-6/C1-H2 
airplanes;
    (xxviii) Piper Aircraft, Inc. (type certificate previously held 
by The New Piper Aircraft, Inc.), Model PA-18, PA-18 ``105'' 
(Special), PA-18 ``125'' (Army L-21A), PA-18 ``135'' (Army L-21B), 
PA-18 ``150,'' PA-18A, PA-18A ``135,'' PA-18A ``150,'' PA-18AS 
``125,'' PA-18AS ``135,'' PA-18AS ``150,'' PA-18S, PA-18S ``105'' 
(Special), PA-18S ``125,'' PA-18S ``135,'' PA-18S ``150,'' PA-19 
(Army L-18C), PA-19S, PA-20, PA-20 ``115,'' PA-20 ``135,'' PA-20S, 
PA-20S ``115,'' PA-20S ``135,'' PA-22, PA-22-108, PA-22-135, PA-22-
150, PA-22-160, PA-22S-135, PA-22S-150, PA-22S-160, PA-23, PA-23-
160, PA-23-235, PA-23-250, PA-24, PA-24-250, PA-24-260, PA-24-400, 
PA-28-140, PA-28-150, PA-28-151, PA-28-160, PA-28-161, PA-28-180, 
PA-28-181, PA-28-201T, PA-28-235, PA-28-236, PA-28R-180, PA-28R-200, 
PA-28R-201, PA-28R-201T, PA-28RT-201, PA-28RT-201T, PA-28S-160, PA-
28S-180, PA-30, PA-32-260, PA-32-300, PA-32-301, PA-32-301FT, PA-32-
301T, PA-32-301XTC, PA-32R-300, PA-32R-301 (HP), PA-32R-301 (SP), 
PA-32R-301T, PA-32RT-300, PA-32RT-300T, PA-32S-300, PA-34-200, PA-
34-200T, PA-34-220T, PA-39, PA-40, PA-44-180, PA-44-180T, PA-46-
310P, and PA-46-350P airplanes;
    (xxix) Polskie Zaklady Lotnicze Spolka zo.o. (type certificate 
previously held by PZL MIELEC) Model PZL M26 01 airplanes;
    (xxx) Revo, Incorporated Model Colonial C-1, Colonial C-2, Lake 
LA-4, Lake LA-4A, Lake LA-4P, Lake LA-4-200, and Lake Model 250 
airplanes;
    (xxxi) Robert E. Rust, Jr. (type certificate previously held by 
Robert E. Rust), Model DHC-1 Chipmunk Mk 21, DHC-1 Chipmunk Mk 22, 
and DHC-1 Chipmunk Mk 22A airplanes;
    (xxxii) Sierra Hotel Aero, Inc. (type certificate previously 
held by Navion Aircraft LLC), Model Navion (Army L-17A), Navion A 
(Army L-17B and L-17C), Navion B, Navion D, Navion E, Navion F, 
Navion G, and Navion H airplanes;
    (xxxiii) Slingsby Aviation Ltd. Model T67M260 and T67M260-T3A 
airplanes;
    (xxxiv) SOCATA (type certificate previously held by Socata 
Groupe Aerospatiale) Model MS 880B, MS 885, MS 892A-150, MS 892E-
150, MS 893A, MS 893E, MS 894A, MS 894E, Rallye 100S, Rallye 150ST, 
Rallye 150T, Rallye 235C, Rallye 235E, TB 9, TB 10, TB 20, TB 21, 
and TB 200 airplanes;
    (xxxv) Spartan Aircraft Company Model 7W (Army UC-71) airplanes;
    (xxxvi) SST FLUGTECHNIK GmbH Model EA 400 and EA 400-500 
airplanes;
    (xxxvii) Swift Museum Foundation, Inc. (type certificate 
previously held by Univair Aircraft Corporation), Model GC-1A and 
GC-1B airplanes;
    (xxxviii) Symphony Aircraft Industries Inc. (type certificate 
previously held by Ostmecklenburgische Flugzeugbau GmbH), Model OMF-
100-160 and SA 160 airplanes;

[[Page 45993]]

    (xxxix) Textron Aviation Inc. (type certificate previously held 
by Cessna Aircraft Company) Model 120, 140, 140A, 150, 150A, 150B, 
150C, 150D, 150E, 150F, 150G, 150H, 150J, 150K, 150L, 150M, 152, 
170, 170A, 170B, 172, 172A, 172B, 172C, 172D, 172E, 172F (USAF T-
41A), 172G, 172H (USAF T-41A), 172I, 172K, 172L, 172M, 172N, 172P, 
172Q, 172R, 172RG, 172S, 175, 175A, 175B, 175C, 177, 177A, 177B, 
177RG, 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 
180K, 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 
182K, 182L, 182M, 182N, 182P, 182Q, 182R, 182S, 182T, 185, 185A, 
185B, 185C, 185D, 185E, 206, 206H, 207, 207A, 210, 210A, 210B, 210C, 
210D, 210E, 210F, 210G, 210H, 210J, 210K, 210L, 210M, 210N, 210R, 
210-5 (205), 210-5A (205A), 310, 310A (USAF U-3A), 310B, 310C, 310D, 
310E (USAF U-3B), 310F, 310G, 310H, 310I, 310J, 310J-1, 310K, 310L, 
310N, 310P, 310Q, 310R, 320, 320A, 320B, 320C, 320D, 320E, 320F, 
320-1, 335, 336, 337, 337A, 337B, 340, 340A, A150K, A150L, A150M, 
A152, A185E, A185F, E310H, E310J, LC40-550FG, LC41-550FG, LC42-
550FG, P172D, P206, P206A, P206B, P206C, P206D, P206E, P210N, P210R, 
R172E (USAF T-41B, USAF T-41C and D), R172F (USAF T-41D), R172G 
(USAF T-41C and D), R172H (USAF T-41D), R172J, R172K, R182, T182, 
T182T, T206H, T207, T207A, T210F, T210G, T210H, T210J, T210K, T210L, 
T210M, T210N, T210R, T303, T310P, T310Q, T310R, TP206A, TP206B, 
TP206C, TP206D, TP206E, TR182, TU206A, TU206B, TU206C, TU206D, 
TU206E, TU206F, TU206G, U206, U206A, U206B, U206C, U206D, U206E, 
U206F, and U206G airplanes;
    (xl) Textron Aviation Inc. (type certificate previously held by 
Beechcraft Corporation), Model 19A, 23, 35, 35R, 35-33, 35-A33, 35-
B33, 35-C33, 35-C33A, 36, 45 (YT-34), 50 (L-23A), 56TC, 58, 58A, 
58P, 58PA, 58TC, 58TCA, 76, 95, 95-55, 95-A55, 95-B55, 95-B55A, 95-
B55B (T-42), 95-C55, 95-C55A, A23, A23A, A23-19, A23-24, A24, A24R, 
A35, A36, A36TC, A45 (T-34A, B-45), A56TC, B19, B23, B24R, B35, 
B36TC, B50 (L-23B), B95, B95A, C23, C24R, C35, C50, D35, D45 (T-
34B), D50 (L-23E), D50A, D50B, D50C, D50E, D50E-5990, D55, D55A, 
D95A, E33, E33A, E33C, E35, E50 (L-23D, RL-23D), E55, E55A, E95, 
F33, F33A, F33C, F35, F50, G33, G35, G50, H35, H50, J35, J50, K35, 
M19A, M35, N35, P35, S35, V35, V35A, and V35B airplanes;
    (xli) The Boeing Company (type certificate previously held by 
Rockwell International) Model AT-6 (SNJ-2), AT-6A (SNJ-3), AT-6B, 
AT-6C (SNJ-4), AT-6D (SNJ-5), AT-6F (SNJ-6, SNJ-7), BC-1A, and T-6G 
airplanes;
    (xlii) The King's Engineering Fellowship (TKEF) Model 44 
airplanes;
    (xliii) The Waco Aircraft Company Model YMF airplanes;
    (xliv) Topcub Aircraft, Inc., Model CC18-180 and CC18-180A 
airplanes;
    (xlv) True Flight Holdings LLC (type certificate previously held 
by Tiger Aircraft LLC) Model AA-1, AA-1A, AA-1B, AA-1C, AA-5, AA-5A, 
AA-5B, and AG-5B airplanes;
    (xlvi) Twin Commander Aircraft LLC (type certificate previously 
held by Twin Commander Aircraft Corporation) Model 500, 520, 560, 
and 560A airplanes;
    (xlvii) Univair Aircraft Corporation Model 108, 108-1, 108-2, 
108-3, and 108-5 airplanes;
    (xlviii) Viking Air Limited (type certificate previously held by 
Bombardier Inc. and deHavilland Inc.) Model DHC-2 Mk. I, DHC-2 Mk. 
II, and DHC-2 Mk. III airplanes;
    (xlix) Vulcanair S.p.A. (type certificate previously held by 
Partenavia Costruzioni Aeronautiche S.p.A.) Model AP68TP-300 
``Spartacus,'' AP68TP-600 ``Viator,'' P.68, P.68 ``Observer,'' P.68 
``Observer 2,'' P.68B, P.68C, P.68C-TC, and P.68TC ``Observer'' 
airplanes;
    (l) WSK PZL Mielec and OBR SK Mielec Model PZL M20 03 airplanes;
    (li) W.Z.D. Enterprises Inc. (type certificate previously held 
by JGS Properties, LLC) Model 11A and 11E airplanes;
    (lii) Zenair Ltd. Model CH2000 airplanes; and
    (liii) Zlin Aircraft a.s. (type certificate previously held by 
Moravan a.s.) Model Z-143L and Z-242L airplanes.

(d) Subject

    Joint Aircraft System Component (JASC)/Air Transport Association 
(ATA) of America Code 3410, FLIGHT ENVIRONMENT DATA; 3420, ATTITUDE 
AND DIRECTION DATA SYSTEM.

(e) Unsafe Condition

    This AD was prompted by an automatic reset occurring when the 
display internal monitor detects a potential fault causing 
intermittent loss of airspeed, attitude, and altitude information 
during flight. The FAA is issuing this AD to address the software 
interacting with a graphics processing chip defect. The unsafe 
condition, if not addressed, could result in intermittent loss of 
airspeed, attitude, and altitude information during flight with 
consequent loss of airplane control.

(f) Compliance

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

(g) Required Actions

    (1) Before further flight, revise the limitations section of the 
airplane flight manual (AFM) for your airplane by inserting a copy 
of this AD or by making a pen and ink change to add: ``Operation 
under Instrument Flight Rules (IFR) or night Visual Flight Rules 
(VFR) is prohibited.''
    (2) The action required by paragraph (g)(1) of this AD may be 
performed by the owner/operator (pilot) holding at least a private 
pilot certificate and must be entered into the aircraft records 
showing compliance with this AD in accordance with 14 CFR 43.9(a)(1) 
through (4) and 14 CFR 91.417(a)(2)(v). The record must be 
maintained as required by 14 CFR 91.417. This authority is not 
applicable to aircraft being operated under 14 CFR part 119.

(h) Special Flight Permit

    Special flight permits are prohibited.

(i) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Fort Worth 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).
    (2) Before using any approved AMOC, notify your appropriate 
principal inspector, or lacking a principal inspector, the manager 
of the local flight standards district office/certificate holding 
district office.

(j) Related Information

    For more information about this AD, contact Mahmood Shah, 
Aerospace Engineer, Fort Worth ACO Branch, FAA, 10101 Hillwood Pkwy, 
Fort Worth, TX 76177; phone: 817-222-5133; fax: 817-222-5960; email: 
[email protected].

    Issued on July 24, 2020.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification 
Service.
[FR Doc. 2020-16592 Filed 7-30-20; 8:45 am]
BILLING CODE 4910-13-P

The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T01:57:32.682900+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256

95ba036ea060094b28567be943e94b6799b2871f79aa39bab9eb6f0b5c3c116a

Text SHA-256

fcbace48f4a89c5dce2e11df13df0a4af9650db48d644c2171a81151ecdbb865