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2020-03-20 THE BOEING COMPANY: Amendment 39-19844; Docket No. FAA-2020-0098; Product Identifier 2020-NM-011-AD.
(a) EFFECTIVE DATE

    This AD is effective February 18, 2020.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies to The Boeing Company airplanes,  certificated  in any
    category, as identified in paragraphs (c)(1) through (9) of this AD.

(1) Model MD-11 and MD-11F airplanes modified by supplemental type certif-
    icate (STC) ST01895WI.

(2) Model 717-200 airplanes modified by STC ST04416AT.

(3) All Model 737-8 and 737-9 airplanes.

(4) All  Model  737-600, -700, -700C, -800, -900, and -900ER  series  air-
    planes.

(5) Model 747-400 and 747-400F series airplanes modified by STC ST01892WI.

(6) Model 757-200, -200PF, -200CB, and -300 series airplanes  modified  by
    STC ST04436AT.

(7) Model 767-200, -300, -300F, -400ER, and -2C series airplanes  modified
    by STC ST04436AT or ST01883WI.

(8) All Model 777-200, -200LR, -300, and -300ER series airplanes.

(9) All Model 777F series airplanes.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 34, Navigation.

(e) UNSAFE CONDITION

    This AD was prompted by reports of the loss of global positioning sys-
    tem  (GPS) data  or  degraded  GPS positional  accuracy while  using a
    certain  multi-mode receiver  (MMR).  The  FAA is  issuing this  AD to
    address the  loss of  GPS data  and degraded  GPS positional accuracy,
    which, during  a high-precision  approach with  this GPS  error, could
    result in controlled flight into terrain.

(f) COMPLIANCE

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

(g) AIRPLANE FLIGHT MANUAL (AFM) REVISION

    For airplanes equipped  with Collins GLU-2100 MMR,  part number  (P/N)
    822-2532-100,  having  any  applicable  GLU-2100  operational software
    (OPS) identified in figure 1 to paragraph (g) of this AD installed: At
    the applicable time specified in paragraphs (g)(1) and (2) of this AD,
    revise  the  limitations   or  certificate  limitations   section,  as
    applicable, of the existing  AFM to include the  information specified
    in figure 2 to paragraph (g)  of this AD and revise the  procedures or
    normal  procedures  section, as  applicable,  of the  existing  AFM to
    include the information specified in figure 3 to paragraph (g) of this
    AD.  This  may  be done  by inserting  a copy  of figures  2 and  3 to
    paragraph (g) of this AD into the existing AFM.

(1) For Model 737-8 and 737-9 airplanes: Before further flight.

(2) For  all  airplanes  except  Model 737-8 and 737-9 airplanes: Within 7
    days after the effective date of this AD.

              FIGURE 1 TO PARAGRAPH (G) – AFFECTED OPS SOFTWARE           
    ______________________________________________________________________
    AIRPLANES                                   OPS SOFTWARE NUMBER
    ______________________________________________________________________
    Model 777-200, 777-200LR, 777-300,            COL4D-0087-0002
    777-300ER, and 777F series airplanes

    Model 737-600, 737-700, 737-700C,             COL4E-0087-0001
    737-800, 737-900, and 737-900ER series
    airplanes; and Model 737-8, and 737-9
    airplanes

    All airplanes                                 COL48-0087-0700

    Model MD-11, MD-11F, and 717-200              COL49-0087-0701
    airplanes; and Model 737-600, 737-700,
    737-700C, 737-800, 737-900, 737-900ER,
    747-400F, 747-400, 757-200, 757-200PF,
    757-200CB, 757-300, 767-200, 767-300,
    767-300F, 767-400ER, 767-2C, 777-200,
    777-200LR, 777-300, 777-300ER, and
    777F series airplanes
    ______________________________________________________________________


    FIGURE 2 TO PARAGRAPH (G) – AFM–LIMITATIONS OR CERTIFICATE LIMITATIONS
    ______________________________________________________________________
    ELECTRONICS – GLOBAL LANDING UNIT (GLU)
    (REQUIRED BY AD 2020-03-20)

    Operations that  require less than 0.3 RNP  (For  example,  0.1, 0.11,
    0.15, etc.)  in the region identified  below are prohibited  with GLU-
    2100 OPS software number COL4D-0087-0002, COL4E-0087-0001, COL48-0087-
    0700, or COL49-0087-0701 installed.

    Exception:  Anchorage (PANC) approach procedures  that allow less than
    RNP 0.3 are authorized provided the instructions outlined in the Elec-
    tronics – Global Landing Unit Section of Normal Procedures Chapter are
    followed.

    Note:  Currently,  Fairbanks (PAFA) and Anchorage (PANC)  are the only
    airports in the region  with an RNP approach that requires better than
    0.3 nmi performance.

    Region bounded by the following coordinates:
    ______________________________________________________________________
        LATITUDE RANGE (DEGREES)            LONGITUDE RANGE (DEGREES)
    ______________________________________________________________________
            80 N to 70 N                     40 E to 40 W
            70 N to 69 N                     134.5 E to 134.38 W
            69 N to 68 N                     134.5 E to 137.28 W
            68 N to 67 N                     134.5 E to 139.50 W
            67 N to 66 N                     134.5 E to 141.58 W
            66 N to 65 N                     134.5 E to 144.23 W
            65 N to 64 N                     134.5 E to 145.48 W
            64 N to 63 N                     134.5 E to 146.44 W
            63 N to 62 N                     134.5 E to 148.33 W
            62 N to 61 N                     134.5 E to 149.50 W
            61 N to 60 N                     134.5 E to 150.35 W
            60 N to 59 N                     134.5 E to 151.00 W
            59 N to 58 N                     134.5 E to 151.40 W
            58 N to 57 N                     134.5 E to 152.62 W
            57 N to 56 N                     134.5 E to 153.42 W
            56 N to 30 N                     154 E to 154 W
            30 N to 5 N                      163 E to 163 W
            5 N to 10 S                      166 E to 166 W
            10 S to 15 S                     170 E to 170 W
    ______________________________________________________________________


                        ILLUSTRATION (Figure 2)


      FIGURE 3 TO PARAGRAPH (G) – AFM – PROCEDURES OR NORMAL PROCEDURES   
    ______________________________________________________________________
    ELECTRONICS – GLOBAL LANDING UNIT (GLU)
    (REQUIRED BY AD 2020-03-20)

    To  conduct  an approach procedure  with  GLU-2100 OPS software number
    COL4D-0087-0002, COL4E-0087-0001, COL48-0087-0700, or COL49-0087-0701,
    installed at Anchorage (PANC)  with less than 0.3 RNP,  accomplish the
    following prior to dispatch in accordance with AC 90-101A:

    Perform a RNP GPS prediction  to ensure  the predicted availability of
    GPS Horizontal Integrity Limit (HIL)  is  less  than  MAX HIL  for the
    planned operation time frame at Anchorage (PANC).

    MAX HIL = 1.8 (RNP – 0.0726 nm) for LNAV with A/P engaged
    MAX HIL = 1.8 (RNP – 0.0926 nm) for LNAV with F/D

    ______________________________________________________________________

(h) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

(1) The  Manager,  Seattle 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 identi-
    fied in paragraph (i) of this AD. Information may be emailed to:
    9-ANM-Seattle-ACO-AMOC-Requests@faa.gov.

(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.

(3) An AMOC that provides  an acceptable level of safety  may be used  for
    any repair, modification, or alteration  required by this AD if  it is
    approved by The Boeing Company Organization Designation  Authorization
    (ODA) that  has been  authorized by  the Manager,  Seattle ACO Branch,
    FAA,  to  make those  findings.  To be  approved,  the repair  method,
    modification  deviation,  or   alteration  deviation  must   meet  the
    certification  basis   of  the   airplane,  and   the  approval   must
    specifically refer to this AD.

(i) RELATED INFORMATION

    For more information about this AD,  contact  David Sumner,  Aerospace
    Engineer, Systems and Equipment Section, FAA, Seattle ACO Branch, 2200
    South 216th St.,  Des Moines, WA 98198;  phone and fax:  206-231-3538;
    email: david.sumner@faa.gov.

(j) MATERIAL INCORPORATED BY REFERENCE

    None.

Issued  on  February 12, 2020.  Gaetano A. Sciortino,  Deputy Director for
Strategic  Initiatives,  Compliance  &  Airworthiness  Division,  Aircraft
Certification Service.

FOR FURTHER INFORMATION CONTACT: David Sumner, Aerospace Engineer, Systems
and Equipment Section, FAA,  Seattle ACO Branch, 2200 South 216th St., Des
Moines, WA 98198; phone and fax: 206-231-3538; email: david.sumner@faa.gov
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2020-0098; Product Identifier 2020-NM-011-AD; Amendment
39-19844; AD 2020-03-20]
RIN 2120-AA64

Airworthiness Directives; The Boeing Company Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments.

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

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain The Boeing Company Model MD-11, MD-11F, and 717-200 airplanes,
all Model 737-8 and 737-9 airplanes, all Model 737-600, -700, -700C, -
800, -900, and -900ER series airplanes, certain Model 747-400 and 747-
400F series airplanes, certain Model 757 and 767 airplanes, and all
Model 777 airplanes. This AD requires revising the existing airplane
flight manual (AFM) to include a limitation to prohibit operations that
require less than 0.3 required navigational performance (RNP) within a
specified area for airplanes having a certain multi-mode receiver (MMR)
with certain software installed. This AD was prompted by reports of the
loss of global positioning system (GPS) data or degraded GPS positional
accuracy while using a certain MMR. The FAA is issuing this AD to
address the unsafe condition on these products.

DATES: This AD is effective February 18, 2020.
The FAA must receive comments on this AD by April 3, 2020.

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.

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-
0098; 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 Docket Operations (phone:
800-647-5527) is listed above. Comments will be available in the AD
docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: David Sumner, Aerospace Engineer,
Systems and Equipment Section, FAA, Seattle ACO Branch, 2200 South
216th St., Des Moines, WA 98198; phone and fax: 206-231-3538; email:
david.sumner@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

In December 2019, the FAA received reports of the loss of GPS data
or degraded GPS positional accuracy while using a certain MMR with
certain software installed. An investigation determined that within a
certain region of the world, operational software (OPS), number COL4D-
0087-0002, COL4E-0087-0001, COL48-0087-0700, or COL49-0087-0701, if
installed on Collins GLU-2100 MMR, part number (P/N) 822-2532-100,
could result in a GPS positional error. The affected area occurs in a
funnel shaped region of the world that mainly extends +/- 20 degrees on
either side of 180 degrees West Longitude, and encompasses the Northern
Hemisphere to 10 degrees Latitude in the Southern Hemisphere. When an
airplane is within this affected region, the software should map the
computed ionospheric pierce point (IPP) to the correct hemisphere, but
the software is not doing that. The consequences of the GPS error are:
An annunciated loss of GPS output, where the Global
Navigation Satellite System (GNSS) bus becomes inactive anywhere from a
few seconds to up to 40 minutes.
Un-annunciated reduced positional accuracy in the affected
region when the Satellite-Based Augmentation System (SBAS) ionosphere
corrections are improperly applied. The positional error will be
bounded to 0.3 nautical miles, but may not be bounded by the horizontal
protection level (HPL) that is output by the GNSS.
This improper mapping within the OPS, if not addressed, could,
during a high-precision approach with a GPS error, result in controlled
flight into terrain.

FAA's Determination

The FAA is issuing this AD because the agency 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 existing airplane flight manual to
include a limitation to prohibit operations that require less than 0.3
RNP within a specified area for airplanes having a certain MMR with
certain software installed.

Interim Action

The FAA considers this AD interim action. Collins is currently
developing a software update that will further address the unsafe
condition identified in this AD. Once this software update is
developed, approved, and available, the FAA might consider additional
rulemaking.

Justification for Immediate Adoption and Determination of the Effective
Date


Section 553(b)(3)(B) of the Administrative Procedure Act (APA) (5
U.S.C.) authorizes agencies to dispense with notice and comment
procedures for rules when the agency, for ``good cause,'' finds that
those procedures are ``impracticable, unnecessary, or contrary to the
public interest.'' Under this section, an agency, upon finding good
cause, may issue a final rule without seeking comment prior to the
rulemaking. Similarly, Section 553(d) of the APA authorizes agencies to
make rules effective in less than thirty days, upon a finding of good
cause.
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 foregoing notice and comment prior to adoption of this rule
because, as described in the Discussion section of this AD, the loss of
GPS data, or degraded GPS positional accuracy, during a high-precision
approach with a GPS positional error, could result in controlled flight
into terrain. Given the significance of the risk presented by this
unsafe condition, it must be immediately addressed.
Accordingly, notice and opportunity for prior public comment are
impracticable and contrary to the public interest pursuant to 5 U.S.C.
553(b)(3)(B). In addition, for the reasons stated above, the FAA finds
that good cause exists pursuant to 5 U.S.C. 553(d) 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, the FAA invites 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-
0098 and Product Identifier 2020-NM-011-AD at the beginning of your
comments. The FAA specifically invites comments on the overall
regulatory, economic, environmental, and energy aspects of this final
rule. The FAA will consider all comments received by the closing date
and may amend this final rule 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 FAA will also post a report summarizing each substantive
verbal contact the agency receives about this final rule.

Confidential Business Information

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 David Sumner, Aerospace Engineer, Systems and Equipment
Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA
98198; phone and fax: 206-231-3538; email: david.sumner@faa.gov. Any
commentary that the FAA receives which is not specifically designated
as CBI will be placed in the public docket for this rulemaking.

Regulatory Flexibility Act (RFA)

The requirements of the 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 the FAA has determined that it has good cause to adopt
this rule without notice and comment, RFA analysis is not required.

Costs of Compliance

Although the FAA estimates the number of airplanes identified in
the applicability of this AD as 3,200 airplanes of U.S. registry, the
AFM revision specified in this AD is required only for the airplanes
having a configuration identified in paragraph (g) of this AD. The FAA
estimates that 409 airplanes of U.S. registry are affected by the AFM
revision specified in paragraph (g) of this AD.
The FAA estimates the following costs to comply with this AD:

Estimated Costs

Action
Labor cost
Parts cost
Cost per product
Cost on U.S. operators
AFM revision 1 work-hour x $85 per hour = $85
$0
$85
$34,765

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

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, the FAA amends 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 (AD):