81 FR 56472 - Special Conditions: Bombardier Aerospace Inc. Model BD-700-2A12 and BD-700-2A13 Airplanes; Automatic Speed Protection for Design Dive Speed
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 81, Issue 162 (August 22, 2016)
Federal Aviation Administration
Federal Register Volume 81, Issue 162 (August 22, 2016)
| Page Range | 56472-56474 | |
| FR Document | 2016-19993 |
[Federal Register Volume 81, Number 162 (Monday, August 22, 2016)] [Rules and Regulations] [Pages 56472-56474] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2016-19993] [[Page 56472]] ======================================================================= ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 25 [Docket No. FAA-2016-4137; Special Conditions No. 25-631-SC] Special Conditions: Bombardier Aerospace Inc. Model BD-700-2A12 and BD-700-2A13 Airplanes; Automatic Speed Protection for Design Dive Speed AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final special conditions; request for comments. ----------------------------------------------------------------------- SUMMARY: These special conditions are issued for the Bombardier Aerospace Inc. (Bombardier) Model BD-700-2A12 and BD-700-2A13 airplanes. These airplanes will have a novel or unusual feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This design feature is associated with a reduced margin between design cruising speed, VC /MC , and design diving speed, VD / MD , based on the incorporation of a high-speed-protection system that limits nose-down pilot authority at speeds above VD /MD . The applicable airworthiness regulations do not contain adequate or appropriate safety standards for these design features. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards. DATES: This action is effective on Bombardier on August 22, 2016. We must receive your comments by October 6, 2016. ADDRESSES: Send comments identified by docket number FAA-2016-4137 using any of the following methods:Federal eRegulations Portal: Go to http://www.regulations.gov/ and follow the online instructions for sending your comments electronically. Mail: Send comments to Docket Operations, M-30, U.S. Department of Transportation (DOT), 1200 New Jersey Avenue SE., Room W12-140, West Building Ground Floor, Washington, DC, 20590-0001. Hand Delivery or Courier: Take comments to Docket Operations in Room W12-140 of the West Building Ground Floor at 1200 New Jersey Avenue SE., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. Fax: Fax comments to Docket Operations at 202-493-2251. Privacy: The FAA will post all comments it receives, without change, to http://www.regulations.gov/, including any personal information the commenter provides. Using the search function of the docket Web site, anyone can find and read the electronic form of all comments received into any FAA docket, including the name of the individual sending the comment (or signing the comment for an association, business, labor union, etc.). DOT's complete Privacy Act Statement can be found in the Federal Register published on April 11, 2000 (65 FR 19477-19478), as well as at http://DocketsInfo.dot.gov/. Docket: Background documents or comments received may be read at http://www.regulations.gov/ at any time. Follow the online instructions for accessing the docket or go to Docket Operations in Room W12-140 of the West Building Ground Floor at 1200 New Jersey Avenue SE., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. FOR FURTHER INFORMATION CONTACT: Mark Freisthler, FAA, Airframe and Cabin Safety Branch, ANM-115, Transport Airplane Directorate, Aircraft Certification Service, 1601 Lind Avenue SW., Renton, Washington, 98057- 3356; telephone 425-227-1119; facsimile 425-227-1232. SUPPLEMENTARY INFORMATION: Comments Invited We invite interested people to take part in this rulemaking by sending written comments, data, or views. The most helpful comments reference a specific portion of the special conditions, explain the reason for any recommended change, and include supporting data. We will consider all comments we receive on or before the closing date for comments. We may change these special conditions based on the comments we receive. Background On May 30, 2012, Bombardier applied for an amendment to type certificate no. T00003NY to include the new Model BD-700-2A12 and BD- 700-2A13 airplanes. These airplanes are derivatives of the Model BD-700 series of airplanes currently approved under type certificate no. T00003NY, and are marketed as the Bombardier Global 7000 (Model BD-700- 2A12) and Global 8000 (Model BD-700-2A13). These airplanes are ultra- long-range, executive-interior business jets. Type Certification Basis Under the provisions of Title 14, Code of Federal Regulations (14 CFR) 21.101, Bombardier must show that the Model BD-700-2A12 and BD- 700-2A13 airplanes meet the applicable provisions of the regulations listed in type certificate no. T00003NY, or the applicable regulations in effect on the date of application for the change, except for earlier amendments as agreed upon by the FAA. If the Administrator finds that the applicable airworthiness regulations (i.e., 14 CFR part 25) do not contain adequate or appropriate safety standards for the BD-700-2A12 and BD-700-2A13 airplanes because of a novel or unusual design feature, special conditions are prescribed under the provisions of Sec. 21.16. Special conditions are initially applicable to the model for which they are issued. Should the type certificate for that model be amended later to include any other model that incorporates the same novel or unusual design feature, or should any other model already included on the same type certificate be modified to incorporate the same novel or unusual design feature, these special conditions would also apply to the other model under Sec. 21.101. In addition to the applicable airworthiness regulations and special conditions, the Model BD-700-2A12 and BD-700-2A13 airplanes must comply with the fuel-vent and exhaust-emission requirements of 14 CFR part 34, and the noise certification requirements of 14 CFR part 36. The FAA issues special conditions, as defined in 14 CFR 11.19, in accordance with Sec. 11.38, and they become part of the type- certification basis under Sec. 21.101. Novel or Unusual Design Features The Bombardier Model BD-700-2A12 and BD-700-2A13 airplanes will have a novel or unusual design feature associated with a high-speed- protection system that limits nose-down pilot authority at speeds above V D /MD . Discussion Bombardier's high-speed-protection system limits nose-down pilot authority at speeds above VC /MC , and prevents the airplane from actually performing the maneuver required under Sec. 25.335(b)(1). Section 25.335(b)(1) is an analytical envelope condition that was originally adopted in Part 4b of the Civil Air Regulations to provide an acceptable speed margin between design cruise [[Page 56473]] speed and design dive speed. Flutter-clearance design speeds and airframe design loads are impacted by the design dive speed. While the initial condition for the upset specified in the rule is 1g level flight, protection is afforded for other inadvertent overspeed conditions as well. Section 25.335(b)(1) is intended as a conservative enveloping condition for potential overspeed conditions, including non- symmetric ones. To establish that potential overspeed conditions are enveloped, Bombardier must demonstrate that any reduced speed margin, based on the high-speed-protection system, will not be exceeded in inadvertent or gust-induced upsets resulting in initiation of the dive from non-symmetric attitudes; or that the airplane is protected, by the flight-control laws, from getting into non-symmetric upset conditions. Bombardier must conduct a demonstration that includes a comprehensive set of conditions, as described in these special conditions. These special conditions are necessary to address Bombardier's proposed high-speed-protection system. These special conditions identify various symmetric and non-symmetric maneuvers that will ensure that an appropriate design dive speed is established. Symmetric (pitching) maneuvers are specified in Sec. 25.331, ``Symmetric maneuvering conditions.'' Non-symmetric maneuvers are specified in Sec. 25.349, ``Rolling conditions,'' and in Sec. 25.351, ``Yaw maneuver conditions.'' These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards. Applicability As discussed above, these special conditions are applicable to the Model BD-700-2A12 and BD-700-2A13 airplanes. Should Bombardier apply at a later date for a change to the type certificate to include another model incorporating the same novel or unusual design feature, these special conditions would apply to the other model as well. Conclusion This action affects only certain novel or unusual design features on two model series of airplanes. It is not a rule of general applicability. The substance of these special conditions has been subjected to the notice and comment period in several prior instances and has been derived without substantive change from those previously issued. It is unlikely that prior public comment would result in a significant change from the substance contained herein. Therefore, the FAA has determined that prior public notice and comment are unnecessary, and good cause exists for adopting these special conditions upon publication in the Federal Register. The FAA is requesting comments to allow interested persons to submit views that may not have been submitted in response to the prior opportunities for comment described above. List of Subjects in 14 CFR Part 25 Aircraft, Aviation safety, Reporting and recordkeeping requirements. The authority citation for these special conditions is as follows: Authority: 49 U.S.C. 106(g), 40113, 44701, 44702, 44704. The Special Conditions Accordingly, pursuant to the authority delegated to me by the Administrator, the following special conditions are issued as part of the type certification basis for Bombardier Model BD-700-2A12 and BD- 700-2A13 airplanes. 1. In lieu of compliance with Sec. 25.335(b)(1), if the flight- control system includes functions that act automatically to initiate recovery before the end of the 20-second period specified in Sec. 25.335(b)(1), VD /MD must be determined from the greater of the speeds resulting from special conditions 1(a) and 1(b), below. The speed increase occurring in these maneuvers may be calculated if reliable or conservative aerodynamic data are used. a. From an initial condition of stabilized flight at VC / MC , the airplane is upset so as to take up a new flight path 7.5 degrees below the initial path. Control application, up to full authority, is made to try to maintain this new flight path. Twenty seconds after initiating the upset, manual recovery is made at a load factor of 1.5g (0.5 acceleration increment), or such greater load factor that is automatically applied by the system with the pilot's pitch control neutral. Power, as specified in Sec. 25.175(b)(1)(iv), is assumed until recovery is initiated, at which time power reduction and the use of pilot-controlled drag devices may be used. b. From a speed below VC /MC , with power to maintain stabilized level flight at this speed, the airplane is upset so as to accelerate through VC /MC at a flight path 15 degrees below the initial path (or at the steepest nose-down attitude that the system will permit with full control authority if less than 15 degrees). The pilot's controls may be in the neutral position after reaching VC /MC and before recovery is initiated. Recovery may be initiated three seconds after operation of the high-speed warning system by application of a load of 1.5g (0.5g acceleration increment), or such greater load factor that is automatically applied by the system with the pilot's pitch control neutral. Power may be reduced simultaneously. All other means of decelerating the airplane, the use of which is authorized up to the highest speed reached in the maneuver, may be used. The interval between successive pilot actions must not be less than one second. 2. It must also be demonstrated that the speed margin, established as above, will not be exceeded in inadvertent or gust-induced upsets resulting in initiation of the dive from non-symmetric attitudes, unless the airplane is protected, by the flight-control laws, from getting into non-symmetric upset conditions. The upset maneuvers described in Advisory Circular 25-7C, ``Flight Test Guide for Certification of Transport Category Airplanes,'' section 8, paragraph 32, sub-paragraphs c(3)(a) and (b), may be used to comply with this requirement. 3. The probability of any failure of the high-speed-protection system that would result in an airspeed exceeding those determined by special conditions 1 and 2, above, must be less than 10-\5\ per flight hour. 4. Failures of the system must be annunciated to the pilots. Airplane flight-manual instructions must be provided that reduce the maximum operating speeds, VMO /MMO . With the system failed, the operating speed must be reduced to a value that maintains a speed margin between VMO /MMO and VD /MD , and that is consistent with showing compliance with Sec. 25.335(b) without the benefit of the high-speed- protection system. 5. Dispatch of the airplane with the high-speed-protection system inoperative could be allowed under an approved minimum equipment list that would require airplane flight-manual instructions to indicate reduced maximum operating speeds, as described in special condition 4, above. In addition, the flight-deck display of the reduced operating speeds, as well as the overspeed warning for exceeding those speeds, must be equivalent to that of the normal airplane with the high-speed- protection system operative. Also, it must be shown that no additional hazards are introduced with the high-speed-protection system inoperative. [[Page 56474]] Issued in Renton, Washington, on August 11, 2016. Paul Bernado, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2016-19993 Filed 8-19-16; 8:45 am] BILLING CODE 4910-13-P
![56472 Federal Register / Vol. 81, No. 162 / Monday, August 22, 2016 / Rules and Regulations
DEPARTMENT OF TRANSPORTATION Privacy: The FAA will post all Type Certification Basis
comments it receives, without change, Under the provisions of Title 14, Code
Federal Aviation Administration to http://www.regulations.gov/, of Federal Regulations (14 CFR) 21.101,
including any personal information the Bombardier must show that the Model
14 CFR Part 25 commenter provides. Using the search BD–700–2A12 and BD–700–2A13
[Docket No. FAA–2016–4137; Special function of the docket Web site, anyone airplanes meet the applicable provisions
Conditions No. 25–631–SC] can find and read the electronic form of of the regulations listed in type
all comments received into any FAA certificate no. T00003NY, or the
Special Conditions: Bombardier docket, including the name of the applicable regulations in effect on the
Aerospace Inc. Model BD–700–2A12 individual sending the comment (or date of application for the change,
and BD–700–2A13 Airplanes; signing the comment for an association, except for earlier amendments as agreed
Automatic Speed Protection for Design business, labor union, etc.). DOT’s upon by the FAA.
Dive Speed complete Privacy Act Statement can If the Administrator finds that the
be found in the Federal Register applicable airworthiness regulations
AGENCY: Federal Aviation
published on April 11, 2000 (65 FR (i.e., 14 CFR part 25) do not contain
Administration (FAA), DOT.
19477–19478), as well as at http:// adequate or appropriate safety standards
ACTION: Final special conditions; request DocketsInfo.dot.gov/.
for comments. for the BD–700–2A12 and BD–700–
Docket: Background documents or 2A13 airplanes because of a novel or
SUMMARY: These special conditions are comments received may be read at unusual design feature, special
issued for the Bombardier Aerospace http://www.regulations.gov/ at any time. conditions are prescribed under the
Inc. (Bombardier) Model BD–700–2A12 Follow the online instructions for provisions of § 21.16.
and BD–700–2A13 airplanes. These accessing the docket or go to Docket Special conditions are initially
airplanes will have a novel or unusual Operations in Room W12–140 of the applicable to the model for which they
feature when compared to the state of West Building Ground Floor at 1200 are issued. Should the type certificate
technology envisioned in the New Jersey Avenue SE., Washington, for that model be amended later to
airworthiness standards for transport- DC, between 9 a.m. and 5 p.m., Monday include any other model that
category airplanes. This design feature through Friday, except Federal holidays. incorporates the same novel or unusual
is associated with a reduced margin design feature, or should any other
FOR FURTHER INFORMATION CONTACT:
between design cruising speed, VC/MC, model already included on the same
and design diving speed, VD/MD, based Mark Freisthler, FAA, Airframe and
Cabin Safety Branch, ANM–115, type certificate be modified to
on the incorporation of a high-speed- incorporate the same novel or unusual
protection system that limits nose-down Transport Airplane Directorate, Aircraft
Certification Service, 1601 Lind Avenue design feature, these special conditions
pilot authority at speeds above VD/MD. would also apply to the other model
The applicable airworthiness SW., Renton, Washington, 98057–3356;
telephone 425–227–1119; facsimile under § 21.101.
regulations do not contain adequate or In addition to the applicable
appropriate safety standards for these 425–227–1232.
airworthiness regulations and special
design features. These special SUPPLEMENTARY INFORMATION: conditions, the Model BD–700–2A12
conditions contain the additional safety and BD–700–2A13 airplanes must
standards that the Administrator Comments Invited
comply with the fuel-vent and exhaust-
considers necessary to establish a level We invite interested people to take emission requirements of 14 CFR part
of safety equivalent to that established part in this rulemaking by sending 34, and the noise certification
by the existing airworthiness standards. written comments, data, or views. The requirements of 14 CFR part 36.
DATES: This action is effective on most helpful comments reference a The FAA issues special conditions, as
Bombardier on August 22, 2016. We specific portion of the special defined in 14 CFR 11.19, in accordance
must receive your comments by October conditions, explain the reason for any with § 11.38, and they become part of
6, 2016. recommended change, and include the type-certification basis under
ADDRESSES: Send comments identified supporting data. § 21.101.
by docket number FAA–2016–4137 We will consider all comments we Novel or Unusual Design Features
using any of the following methods: receive on or before the closing date for
• Federal eRegulations Portal: Go to The Bombardier Model BD–700–2A12
comments. We may change these special and BD–700–2A13 airplanes will have a
http://www.regulations.gov/ and follow
conditions based on the comments we novel or unusual design feature
the online instructions for sending your
receive. associated with a high-speed-protection
comments electronically.
• Mail: Send comments to Docket Background system that limits nose-down pilot
Operations, M–30, U.S. Department of authority at speeds above VD/MD.
Transportation (DOT), 1200 New Jersey On May 30, 2012, Bombardier applied
for an amendment to type certificate no. Discussion
Avenue SE., Room W12–140, West
Building Ground Floor, Washington, T00003NY to include the new Model Bombardier’s high-speed-protection
DC, 20590–0001. BD–700–2A12 and BD–700–2A13 system limits nose-down pilot authority
• Hand Delivery or Courier: Take airplanes. These airplanes are at speeds above VC/MC, and prevents
comments to Docket Operations in derivatives of the Model BD–700 series the airplane from actually performing
Room W12–140 of the West Building of airplanes currently approved under the maneuver required under
Lhorne on DSK30JT082PROD with RULES
Ground Floor at 1200 New Jersey type certificate no. T00003NY, and are § 25.335(b)(1).
Avenue SE., Washington, DC, between 9 marketed as the Bombardier Global 7000 Section 25.335(b)(1) is an analytical
a.m. and 5 p.m., Monday through (Model BD–700–2A12) and Global 8000 envelope condition that was originally
Friday, except Federal holidays. (Model BD–700–2A13). These airplanes adopted in Part 4b of the Civil Air
• Fax: Fax comments to Docket are ultra-long-range, executive-interior Regulations to provide an acceptable
Operations at 202–493–2251. business jets. speed margin between design cruise
VerDate Sep<11>2014 15:11 Aug 19, 2016 Jkt 238001 PO 00000 Frm 00002 Fmt 4700 Sfmt 4700 E:\FR\FM\22AUR1.SGM 22AUR1](https://thefederalregister.org/doc/81_FR_56634/page/1.svg)
![56474 Federal Register / Vol. 81, No. 162 / Monday, August 22, 2016 / Rules and Regulations
Issued in Renton, Washington, on August Ground Floor at 1200 New Jersey (Model BD–700–2A12) and Global 8000
11, 2016. Avenue SE., Washington, DC, between 9 (Model BD–700–2A13). These airplanes
Paul Bernado, a.m. and 5 p.m., Monday through are ultra-long-range, executive-interior
Acting Manager, Transport Airplane Friday, except Federal holidays. business jets.
Directorate, Aircraft Certification Service. • Fax: Fax comments to Docket
Type Certification Basis
[FR Doc. 2016–19993 Filed 8–19–16; 8:45 am] Operations at 202–493–2251.
BILLING CODE 4910–13–P Privacy: The FAA will post all Under the provisions of Title 14, Code
comments it receives, without change, of Federal Regulations (14 CFR) 21.101,
to http://www.regulations.gov/, Bombardier must show that the Model
DEPARTMENT OF TRANSPORTATION including any personal information the BD–700–2A12 and BD–700–2A13
commenter provides. Using the search airplanes meet the applicable provisions
Federal Aviation Administration function of the docket Web site, anyone of the regulations listed in type
can find and read the electronic form of certificate no. T00003NY, or the
14 CFR Part 25 all comments received into any FAA applicable regulations in effect on the
[Docket No. FAA–2015–6359; Special docket, including the name of the date of application for the change,
Conditions No. 25–633–SC] individual sending the comment (or except for earlier amendments as agreed
signing the comment for an association, upon by the FAA.
Special Conditions: Bombardier Inc. business, labor union, etc.). DOT’s If the Administrator finds that the
Model BD–700–2A12 and BD–700– complete Privacy Act Statement can be applicable airworthiness regulations
2A13 Airplanes; Airplane Electronic- found in the Federal Register published (i.e., 14 CFR part 25) do not contain
System Security Protection From on April 11, 2000 (65 FR 19477–19478), adequate or appropriate safety standards
Authorized Internal Access as well as at http://DocketsInfo.dot. for the BD–700–2A12 and BD–700–
AGENCY: Federal Aviation gov/. 2A13 airplanes because of a novel or
Administration (FAA), DOT. Docket: Background documents or unusual design feature, special
comments received may be read at conditions are prescribed under the
ACTION: Final special conditions; request
http://www.regulations.gov/ at any time. provisions of § 21.16.
for comments.
Follow the online instructions for Special conditions are initially
SUMMARY: These special conditions are accessing the docket, or go to Docket applicable to the model for which they
issued for the Bombardier Inc. Operations in Room W12–140 of the are issued. Should the type certificate
(Bombardier) Model BD–700–2A12 and West Building Ground Floor at 1200 for that model be amended later to
BD–700–2A13 airplanes. These New Jersey Avenue SE., Washington, include any other model that
airplanes will have novel or unusual DC, between 9 a.m. and 5 p.m., Monday incorporates the same novel or unusual
design features, specifically, digital through Friday, except Federal holidays. design feature, or should any other
systems architecture composed of FOR FURTHER INFORMATION CONTACT: model already included on the same
several connected data networks that Varun Khanna, FAA, Airplane and type certificate be modified to
will have the capability to allow Flight Crew Interface, ANM–111, incorporate the same novel or unusual
connectivity of the passenger-service Transport Airplane Directorate, Aircraft design feature, these special conditions
computer systems to the airplane Certification Service, 1601 Lind Avenue would also apply to the other model
critical systems and data networks. The SW., Renton, Washington 98057–3356; under § 21.101.
applicable airworthiness regulations do telephone 425–227–1298; facsimile In addition to the applicable
not contain adequate or appropriate 425–227–1149. airworthiness regulations and special
safety standards for this design feature. SUPPLEMENTARY INFORMATION: conditions, the Model BD–700–2A12
These special conditions contain the
Comments Invited and BD–700–2A13 airplanes must
additional safety standards that the
comply with the fuel-vent and exhaust-
Administrator considers necessary to We invite interested people to take emission requirements of 14 CFR part
establish a level of safety equivalent to part in this rulemaking by sending 34, and the noise certification
that established by the existing written comments, data, or views. The requirements of 14 CFR part 36.
airworthiness standards. most helpful comments reference a
The FAA issues special conditions, as
DATES: This action is effective on specific portion of the special
defined in 14 CFR 11.19, in accordance
Bombardier on August 22, 2016. We conditions, explain the reason for any
with § 11.38, and they become part of
must receive your comments by October recommended change, and include
the type-certification basis under
6, 2016. supporting data.
§ 21.101.
ADDRESSES: Send comments identified We will consider all comments we
by docket number FAA–2015–6359 receive on or before the closing date for Novel or Unusual Design Features
using any of the following methods: comments. We may change these special
The Model BD–700–2A12 and BD–
• Federal eRegulations Portal: Go to conditions based on the comments we
receive. 700–2A13 airplanes will incorporate the
http://www.regulations.gov/ and follow
following novel or unusual design
the online instructions for sending your
Background feature:
comments electronically.
• Mail: Send comments to Docket On May 30, 2012, Bombardier applied Digital systems architecture composed
Operations, M–30, U.S. Department of for an amendment to type certificate no. of several connected data networks.
Transportation (DOT), 1200 New Jersey T00003NY to include the new Model This network architecture and
Lhorne on DSK30JT082PROD with RULES
Avenue SE., Room W12–140, West BD–700–2A12 and BD–700–2A13 configuration may be used for, or
Building Ground Floor, Washington, DC airplanes. These airplanes are interfaced with, a diverse set of
20590–0001. derivatives of the Model BD–700 series functions, including:
• Hand Delivery or Courier: Take of airplanes currently approved under • Flight-safety-related control,
comments to Docket Operations in type certificate no. T00003NY, and are communication, and navigation systems
Room W12–140 of the West Building marketed as the Bombardier Global 7000 (airplane-control domain);
VerDate Sep<11>2014 15:11 Aug 19, 2016 Jkt 238001 PO 00000 Frm 00004 Fmt 4700 Sfmt 4700 E:\FR\FM\22AUR1.SGM 22AUR1](https://thefederalregister.org/doc/81_FR_56634/page/3.svg)
Document Created: 2018-02-09 11:38:07
Document Modified: 2018-02-09 11:38:07
| Category | Regulatory Information | |
| Collection | Federal Register | |
| sudoc Class | AE 2.7: GS 4.107: AE 2.106: | |
| Publisher | Office of the Federal Register, National Archives and Records Administration | |
| Section | Rules and Regulations | |
| Action | Final special conditions; request for comments. | |
| Dates | This action is effective on Bombardier on August 22, 2016. We must receive your comments by October 6, 2016. | |
| Contact | Mark Freisthler, FAA, Airframe and Cabin Safety Branch, ANM-115, Transport Airplane Directorate, Aircraft Certification Service, 1601 Lind Avenue SW., Renton, Washington, 98057- 3356; telephone 425-227-1119; facsimile 425-227-1232. | |
| FR Citation | 81 FR 56472 | |
| CFR Associated | Aircraft; Aviation Safety and Reporting and Recordkeeping Requirements |
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