Special Conditions: Embraer S.A., Model ERJ 190-100 ECJ Airplane; Flight-Accessible Class C Cargo Compartment, 46539-46542 [E8-18474]
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BILLING CODE 4810–33–C
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. NM391; Special Conditions No.
25–273–SC]
Federal Aviation
Administration (FAA), DOT.
ACTION: Final special conditions.
jlentini on PROD1PC65 with RULES
AGENCY:
SUMMARY: These special conditions are
issued for the Embraer S.A. Model ERJ
190–100 ECJ airplane. This airplane will
have novel or unusual design features
15:34 Aug 08, 2008
Jkt 214001
FOR FURTHER INFORMATION CONTACT:
Jayson Claar, FAA, Airframe/Cabin
Safety Branch, ANM–115, Transport
Airplane Directorate, Aircraft
Certification Service, 1601 Lind
Avenue, SW., Renton, Washington
98057–3356; telephone 425–227–2194;
facsimile 425–227–1232.
SUPPLEMENTARY INFORMATION:
Special Conditions: Embraer S.A.,
Model ERJ 190–100 ECJ Airplane;
Flight-Accessible Class C Cargo
Compartment
VerDate Aug<31>2005
associated with access during flight of
the main deck Class C cargo
compartment. The applicable
airworthiness regulations do not contain
adequate or appropriate safety standards
for this design feature. 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: Effective Date: September 10,
2008.
Background
Embraer S.A., made the original
application for certification of the ERJ
190 on May 20, 1999. The Embraer
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application includes six different
models, the initial variant being
designated as the ERJ 190–100. The
application was submitted concurrently
with that for the ERJ 170–100, which
received an FAA type certificate (TC) on
February 20, 2004. Although the
applications were submitted as two
distinct TCs, the airplanes share the
same conceptual design and general
configuration. On July 2, 2003, Embraer
S.A., submitted a request for an
extension of its original application for
the Embraer S.A., Model ERJ 190 series,
with a new application date of May 30,
2001, for establishing the type
certification basis. The FAA
certification basis was adjusted to reflect
this new reference date. In addition,
Embraer has elected to voluntarily
comply with certain 14 CFR part 25
amendments introduced after the May
30, 2001, application date.
On May 30, 2001, Embraer S.A.,
amended the application to include the
Embraer S.A., Model ERJ 190–100 ECJ.
The Embraer S.A., Model ERJ 190–100
ECJ is a derivative of the Embraer S.A.,
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ER11AU08.009
Dated: August 5, 2008.
John C. Dugan,
Comptroller of the Currency.
[FR Doc. E8–18410 Filed 8–8–08; 8:45 am]
46539
ER11AU08.008
Federal Register / Vol. 73, No. 155 / Monday, August 11, 2008 / Rules and Regulations
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46540
Federal Register / Vol. 73, No. 155 / Monday, August 11, 2008 / Rules and Regulations
Model ERJ 190 which is approved under
Type Certificate No. A57NM. The
Embraer S.A., Model ERJ 190–100 ECJ is
a low wing, transport-category aircraft
powered by two wing-mounted General
Electric CF34–10E6 turbofan engines.
The airplane is a 19 passenger regional
jet with a maximum take off weight of
54,500 kilograms (120,151 pounds). The
maximum operating altitude and speed
are 41,000 feet and 320 knots calibrated
air speed (KCAS)/0.82 MACH,
respectively. The Embraer S.A., Model
ERJ 190–100 ECJ design includes an
accessible main deck Class C cargo
compartment.
The regulations consider that a ‘‘cargo
compartment’’ is not intended for access
during flight by the traveling public.
The intent of the Class C cargo
compartment was that it be a selfcontained, isolated compartment
intended to carry baggage and/or cargo.
It was not intended for access during
flight. Access into a cargo compartment
inherently carries with it an increased
level of risk as baggage or cargo could
shift, a decompression could occur in
the compartment, or a fire could
develop during the flight. The FAA
considers that any of these threats are
beyond passengers’ capabilities. In
addition, there are security concerns
with in-flight access to baggage and/or
cargo placed in the Class C cargo
compartment.
The FAA acknowledges that an
allowance was made specifically for
crew access into a Class B cargo
compartment for the express purpose of
fire fighting. Passengers’ access during
flight into aft Class B cargo
compartments has been permitted in the
past for other small aircraft that are
operated under part 91 and 135
operations. Passengers’ quick access to
luggage has been allowed because of the
limited duration for use and limited
number of passengers possibly affected.
These approvals were granted before the
increased security concerns and the new
regulations imposed by the
Transportation Security Administration
(TSA) to address the security concerns.
The FAA gave no consideration to a
flight-accessible Class C cargo
compartment when the classification
was first developed, as no manufacturer
had ever proposed to incorporate such
a feature into their design. Inherently a
‘‘cargo compartment’’ was not intended
for access, especially by the traveling
public.
The FAA acknowledges that a
previous Embraer airplane, the Embraer
S.A., Model EMB 135BJ, has a flightaccessible Class C cargo compartment
that was approved using an equivalent
level of safety finding. The Embraer
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15:34 Aug 08, 2008
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S.A., Model EMB 135BJ design is
similar to the proposed design for the
ERJ 190–100 ECJ. The Embraer S.A.,
Model EMB 135BJ approval was granted
before the increased security concerns
and the new regulations imposed by the
TSA to address security concerns. We
have determined that because the
existing airworthiness standards do not
contain adequate or appropriate safety
standards, relative to cargo
compartment accessibility by passengers
during flight, special conditions are the
appropriate method for this and all
future accessible Class C cargo
compartments.
Type Certification Basis
Under the provisions of § 21.101,
Embraer S.A. must show that the
Embraer S.A., Model ERJ 190–100 ECJ
meets the applicable provisions of the
regulations incorporated by reference in
Type Certificate No. A57NM or the
applicable regulations in effect on the
date of application for the change to the
ERJ 190–100 ECJ. The regulations
incorporated by reference in the type
certificate are commonly referred to as
the ‘‘original type certification basis.’’
If the Administrator finds that the
applicable airworthiness regulations
(i.e., part 25) do not contain adequate or
appropriate safety standards for the
Embraer S.A., Model ERJ 190–100 ECJ
because of a novel or unusual design
feature, special conditions are
prescribed under the provisions of
§ 21.16.
In addition to the applicable
airworthiness regulations and special
conditions, the Embraer S.A., Model ERJ
190–100 ECJ 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 § 11.19, under § 11.38, and
they become part of the type
certification basis under § 21.101.
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 or similar novel
or unusual design feature, or should any
other model already included on the
same type certificate be modified to
incorporate the same or similar novel or
unusual design feature, the special
conditions would also apply to the other
model under § 21.101.
Novel or Unusual Design Features
The Embraer S.A., Model ERJ 190–100
ECJ will incorporate a novel or unusual
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design feature of in-flight access to a
Class C cargo compartment.
Discussion
The FAA considers that Class C cargo
compartment access during flight may
impact the isolation of the passenger
cabin from the cargo compartment,
which is needed to protect the
passengers from any fire and smoke that
may start within the cargo compartment,
as required by § 25.857(c). In addition,
in-flight access to the Class C
compartment creates unique hazards
resulting from passengers having access
to cargo and baggage in the
compartment. These hazards include
safety for the persons entering the cargo
compartment, possible hazards to the
airplane as a result of this access, and
security concerns with access to the
baggage and/or cargo. These special
conditions provide additional
requirements necessary to ensure
sufficient cabin isolation from fire and
smoke in this unusual design
configuration, and for passenger safety
while occupying the Class C
compartment during flight.
Security
The FAA has been in contact with the
TSA to understand the security
concerns with passengers having access
in-flight to baggage and/or cargo, and
specifically with regard to unscreened
(checked) baggage/cargo. The TSA has
provided the following information to
clarify the regulations concerning access
to cargo compartments by passengers.
Aircraft operators holding operating
certificates under 14 CFR part 119 for
scheduled passenger operations, public
charter passenger operations, and private
charter passenger operations must have an
aircraft operator security program. For U.S.
flag carriers 49 CFR 1544 regulates the
operator security program. Specifically, 49
CFR 1544.101(a)–(i) describes the type of
program an aircraft operator must adopt
depending on the type of aircraft operation.
For the vast majority of operations in-flight
access to checked baggage and/or cargo by
passengers is NOT permitted by the aircraft
operator security program. Aircraft operators
should contact their Principal Security
Inspector (PSI) concerning in-flight access to
checked baggage and/or cargo by passengers.
For airplanes not operated for hire or
offered for common carriage (e.g.,
operation under FAA operating rules 14
CFR parts 91 or 125), flight-accessibility
to baggage and/or cargo placed in the
Class C cargo compartment is controlled
by the operator of the airplane. This
provision does not preclude the
operator from receiving remuneration to
the extent consistent with 14 CFR parts
125 and 91, subpart F, as applicable.
These airplane operators do not hold
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operating certificates under 14 CFR part
119.
For airplanes operated for hire or for
common carriage (e.g., operation under
FAA operating rules 14 CFR part 119),
the TSA regulations provided in 49 CFR
1544.203 prohibit in-flight access to
checked baggage and cargo. Checked
baggage and cargo do not pass through
the screening required of carry-on
baggage, and thus may introduce a
security concern if passengers are
provided in-flight access.
Note: These special conditions are specific
to the in-flight accessible Class C cargo
compartment. Security requirements for
occupants and for baggage/cargo placed in
other locations continue to be subject to the
screening requirements and operator’s
security program as identified in 49 CFR
1544.
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Fire Protection and Alerting
It is the FAA’s position that the threat
of fire is of paramount concern, and
therefore prompt crew action to fight the
fire must be taken to prevent a fire from
threatening the safety of the airplane.
For Class C cargo compartments, the
means of controlling a fire is by flooding
the compartment with an extinguishing
agent. These extinguishing agents are
hazardous to humans. In the event of
smoke detection, the flightcrew should
ensure that the cargo compartment is
not occupied before they discharge the
extinguishing agent. To address this
concern, a warning system is provided
to the flight crew to alert them when a
person is in the cargo compartment.
After the extinguishing agent has been
discharged into the compartment, there
must be a means of alerting a person(s)
not to enter the compartment. It must be
located adjacent to the entry/exit door
that provides access into the
compartment. Access into the cargo
compartment must be prevented after
discharge of the extinguishing agent to
prevent persons from being exposed to
the extinguishing agent and to keep the
extinguishing agent in the compartment
to control the fire.
Passengers in the cabin are alerted
when oxygen is needed. A person in the
cargo compartment would not be alerted
when oxygen is needed. To address this
concern, an aural and visual indication
system within the cargo compartment is
required to alert the person(s) that
oxygen is required. An oxygen
dispensing unit must be provided
adjacent to the entry door into the cargo
compartment to have oxygen readily
available for the person leaving the
compartment. The oxygen supply lines
must not be routed into the cargo
compartment because that would
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15:34 Aug 08, 2008
Jkt 214001
provide a source of oxygen to the cargo
which would feed a fire.
Cargo Restraint
If a net is used as the primary means
of retention of the cargo, an untrained
person accessing a cargo compartment
may not be capable of securing the net
correctly to maintain the retention of the
cargo. The improperly restrained cargo
could be a hazard in flight to the safe
operation of the airplane and a hazard
to the occupants under crash load
conditions.
Discussion of Comments
A notice of proposed special
conditions No. 25–08–05–SC for the
Embraer S.A., Model ERJ 190–100 ECJ
airplanes was published in the Federal
Register on April 21, 2008 (73 FR
21286).
A comment was received from
Embraer S.A.
Requested change: Embraer agreed
with all proposed special conditions
except for the private use only
limitation in Condition No. 8. Embraer
noted that 49 CFR 1544.203(d)(2)
requires the operator to prevent access
to checked baggage. Embraer also noted
that because the ERJ 190–100 ECJ Class
C cargo compartment is accessible inflight, all baggage placed there is not
checked baggage, but rather is
considered accessible subject to the
screening requirements of 49 CFR
1544.201. Embraer proposed to include
guidance in the ERJ 190–100 ECJ
operational publications describing the
applicable TSA regulations and how the
accessible main deck Class C
compartment should be treated in
compliance with those regulations.
Embraer further noted that the security
issue is relevant to in-flight baggage
accessibility, and is not related to the
unique feature (built-in fire
extinguishing) of the ERJ 190–100 ECJ
Class C compartment, and that many
other airplanes have been certified since
the EMB–135BJ with flight accessible
compartments, without any private use
limitations. Embraer believes that the
private use, not-for-hire limitation
proposed by the FAA is not necessary
and, if imposed, would preclude the ERJ
190–100 ECJ from operating in the
charter market. Embraer proposed that
when all of the in-flight accessible
cargo/baggage is screened as carried on
baggage/cargo, the airplane should be
permitted to be operated for hire and for
common carriage.
FAA Disposition: We partially agree
with the Embraer comments. When all
of the occupants and in-flight accessible
baggage/cargo are subject to the
accessible baggage screening
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46541
requirements identified in 49 CFR part
1544 there would not be a need to limit
the operation of the airplane to private
use, not for common carriage. We have
revised Condition No. 8 to allow
operation for hire and common carriage
when the occupants and the baggage/
cargo that is accessible in-flight are
subject to the screening requirements of
49 CFR part 1544. It should be noted
that the screening of the occupants and
carry on baggage is addressed by the
operators’ security program as identified
in 49 CFR part 1544. AFM Limitations
are necessary to ensure that flight crews
are aware of the unique security
requirements associated with in-flight
accessible compartments when
operating for hire or for common
carriage. The FAA has imposed similar
limitations on other programs initiated
since increased security requirements
were introduced, and intends to
continue to do so for future projects that
introduce in-flight accessible cargo
compartments, regardless of the
classification of those compartments per
14 CFR 25.857.
Applicability
As discussed above, these special
conditions are applicable to the Embraer
S.A., Model ERJ 190–100 ECJ. Should
Embraer S.A. apply at a later date for a
change to the type certificate on the
same type certificate to include another
model incorporating the same novel or
unusual design feature, the special
conditions would apply to that model as
well.
Conclusion
This action affects only certain novel
or unusual design features on the
Embraer S.A., Model ERJ 190–100 ECJ
airplanes. It is not a rule of general
applicability.
List of Subjects in 14 CFR Part 25
Aircraft, Aviation safety, Reporting
and recordkeeping requirements.
I The authority citation for these
special conditions is as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701,
44702, 44704.
The Special Conditions
I 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 Embraer S.A. Model ERJ 190–
100 ECJ airplanes.
1. There must be a clear, visual
message in the cockpit to advise the
flightcrew when the main deck Class C
cargo compartment is occupied.
2. There must be means provided to
keep the cargo door open while the
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Federal Register / Vol. 73, No. 155 / Monday, August 11, 2008 / Rules and Regulations
cargo compartment is occupied. There
must be a placard located on or adjacent
to the cargo door instructing occupants
that the door must be closed and latched
at all times except when someone is in
the cargo compartment. This placard
must also instruct the person entering
the cargo compartment to keep the door
open when they are in the cargo
compartment and to immediately close
and latch the door when they exit the
cargo compartment.
3. There must be a (on/off) visual
advisory/warning stating ‘‘Do Not
Enter’’ (or similar words) to be located
outside of and on or near the main entry
door/hatch to the main deck cargo
compartment. The advisory/warning is
to be controlled from the flight deck.
4. There must be an aural and visual
warning provided in the baggage
compartment to alert an occupant when
an oxygen mask must be donned
immediately.
5. Oxygen dispensing units must be
automatically presented and
immediately available to an occupant(s)
of the baggage compartment when they
exit the compartment. For these special
conditions, immediately available
means the oxygen dispensing units are
located in the passenger cabin near the
main entry door/hatch to the main deck
cargo compartment (no oxygen supply
lines are allowed to be routed into the
compartment). The number of oxygen
dispensing units must be equal to the
number of occupants allowed in the
cargo compartment. There must be a
placard located on or adjacent to the
cargo door instructing occupants of the
maximum number of occupants allowed
in the cargo compartment.
6. For cargo and baggage placed in the
baggage compartment whose primary
retention means is by net, the net must
be constructed so that the means of
opening and closing or securing the net
is easily identified and operated.
7. These special conditions apply to
main deck accessible Class C cargo
compartments with volumes of 10 m3 or
less. Class C cargo compartments that
are accessible to passengers with a
volume greater than 10 m3 may be
approved, but would likely require
additional limitations or provisions to
mitigate the larger volume. Note that
there may also be a maximum volume
above which access is not acceptable.
8. Operational limitations: The
airplane has operational limitations
associated with the level of screening
required for baggage/cargo that is placed
in the in-flight accessible Class C cargo
compartment. These limitations must be
documented in the Airplane Flight
Manual (AFM).
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(a) When the airplane is not operated
for hire or offered for common carriage
screening of the baggage/cargo placed in
the in-flight accessible Class C
compartment is the responsibility of the
operator of the airplane. This provision
does not preclude the operator from
receiving remuneration to the extent
consistent with 14 CFR parts 125 and
91, subpart F, as applicable.
(b) When the airplane is operated for
hire or operated for common carriage,
the baggage/cargo placed in the in-flight
accessible Class C compartment is
subject to the screening requirements
and operators security program as
identified in 49 CFR part 1544.
Issued in Renton, Washington, on July 31,
2008.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E8–18474 Filed 8–8–08; 8:45 am]
Certification Office, FAA, 2601
Meacham Blvd., Fort Worth, Texas
76137–4298; telephone: (817) 222–5146;
fax: (817) 222–5960.
SUPPLEMENTARY INFORMATION:
Discussion
AD 2008–02–04, Amendment 39–
15334 (73 FR 3618, January 22, 2008),
affects Eclipse Model EA500 airplanes
and currently:
• Requires incorporating a
modification of the angle of attack
(AOA) probe;
• Limits the applicability to airplanes
under S/N 000065; and
• Retains the operating limitations
from AD 2007–13–11 until the
modification is incorporated.
BILLING CODE 4910–13–P
The FAA incorrectly referenced the
issue date as ‘‘January 9, 2007’’ instead
of ‘‘January 9, 2008.’’ This document
corrects the issue date.
DEPARTMENT OF TRANSPORTATION
Need for the Correction
Federal Aviation Administration
This correction is needed to reflect
the correct issue date on the AD.
14 CFR Part 39
[Docket No. FAA–2007–29316; Directorate
Identifier 2007–CE–078–AD; Amendment
39–15334; AD 2008–02–04]
RIN 2120–AA64
Airworthiness Directives; Eclipse
Aviation Corporation Model EA500
Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; correction.
AGENCY:
SUMMARY: This document makes a
correction to Airworthiness Directive
(AD) 2008–02–04, which was published
in the Federal Register on January 22,
2008 (73 FR 3618), and applies to all
Eclipse Aviation Corporation (Eclipse)
Model EA500 airplanes. This AD
requires incorporating a modification of
the angle of attack (AOA) system, limits
the applicability to airplanes under S/N
000065, and retains the operating
limitations from AD 2007–13–11 until
the modification is incorporated. The
FAA incorrectly referenced the issue
date of the AD as ‘‘January 9, 2007’’
instead of ‘‘January 9, 2008.’’ This
document corrects the issue date.
DATES: The effective date of this AD
remains February 26, 2008, since the
incorrect reference of the issue date of
AD 2008–02–04 does not affect
compliance.
FOR FURTHER INFORMATION CONTACT: Al
Wilson, Flight Test Pilot, Airplane
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Correction of Publication
Accordingly, the publication of
January 22, 2008 (73 FR 3618), which
was the subject of FR Doc. E8–751, is
corrected as follows:
Section 39.13
[Corrected]
On page 3619, in the third column, in
the sixth and seventh lines from the
bottom, under the heading § 39.13
[Amended], replace ‘‘January 9, 2007’’
with ‘‘January 9, 2008.’’
Action is taken herein to correct this
reference in the AD.
The effective date of this AD remains
February 26, 2008, since the incorrect
reference of the issue date of AD 2008–
02–04 does not affect compliance.
Issued in Kansas City, Missouri, on August
1, 2008.
James E. Jackson,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E8–18227 Filed 8–8–08; 8:45 am]
BILLING CODE 4910–13–P
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Agencies
[Federal Register Volume 73, Number 155 (Monday, August 11, 2008)]
[Rules and Regulations]
[Pages 46539-46542]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E8-18474]
=======================================================================
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. NM391; Special Conditions No. 25-273-SC]
Special Conditions: Embraer S.A., Model ERJ 190-100 ECJ Airplane;
Flight-Accessible Class C Cargo Compartment
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final special conditions.
-----------------------------------------------------------------------
SUMMARY: These special conditions are issued for the Embraer S.A. Model
ERJ 190-100 ECJ airplane. This airplane will have novel or unusual
design features associated with access during flight of the main deck
Class C cargo compartment. The applicable airworthiness regulations do
not contain adequate or appropriate safety standards for this design
feature. 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: Effective Date: September 10, 2008.
FOR FURTHER INFORMATION CONTACT: Jayson Claar, FAA, Airframe/Cabin
Safety Branch, ANM-115, Transport Airplane Directorate, Aircraft
Certification Service, 1601 Lind Avenue, SW., Renton, Washington 98057-
3356; telephone 425-227-2194; facsimile 425-227-1232.
SUPPLEMENTARY INFORMATION:
Background
Embraer S.A., made the original application for certification of
the ERJ 190 on May 20, 1999. The Embraer application includes six
different models, the initial variant being designated as the ERJ 190-
100. The application was submitted concurrently with that for the ERJ
170-100, which received an FAA type certificate (TC) on February 20,
2004. Although the applications were submitted as two distinct TCs, the
airplanes share the same conceptual design and general configuration.
On July 2, 2003, Embraer S.A., submitted a request for an extension of
its original application for the Embraer S.A., Model ERJ 190 series,
with a new application date of May 30, 2001, for establishing the type
certification basis. The FAA certification basis was adjusted to
reflect this new reference date. In addition, Embraer has elected to
voluntarily comply with certain 14 CFR part 25 amendments introduced
after the May 30, 2001, application date.
On May 30, 2001, Embraer S.A., amended the application to include
the Embraer S.A., Model ERJ 190-100 ECJ. The Embraer S.A., Model ERJ
190-100 ECJ is a derivative of the Embraer S.A.,
[[Page 46540]]
Model ERJ 190 which is approved under Type Certificate No. A57NM. The
Embraer S.A., Model ERJ 190-100 ECJ is a low wing, transport-category
aircraft powered by two wing-mounted General Electric CF34-10E6
turbofan engines. The airplane is a 19 passenger regional jet with a
maximum take off weight of 54,500 kilograms (120,151 pounds). The
maximum operating altitude and speed are 41,000 feet and 320 knots
calibrated air speed (KCAS)/0.82 MACH, respectively. The Embraer S.A.,
Model ERJ 190-100 ECJ design includes an accessible main deck Class C
cargo compartment.
The regulations consider that a ``cargo compartment'' is not
intended for access during flight by the traveling public. The intent
of the Class C cargo compartment was that it be a self-contained,
isolated compartment intended to carry baggage and/or cargo. It was not
intended for access during flight. Access into a cargo compartment
inherently carries with it an increased level of risk as baggage or
cargo could shift, a decompression could occur in the compartment, or a
fire could develop during the flight. The FAA considers that any of
these threats are beyond passengers' capabilities. In addition, there
are security concerns with in-flight access to baggage and/or cargo
placed in the Class C cargo compartment.
The FAA acknowledges that an allowance was made specifically for
crew access into a Class B cargo compartment for the express purpose of
fire fighting. Passengers' access during flight into aft Class B cargo
compartments has been permitted in the past for other small aircraft
that are operated under part 91 and 135 operations. Passengers' quick
access to luggage has been allowed because of the limited duration for
use and limited number of passengers possibly affected. These approvals
were granted before the increased security concerns and the new
regulations imposed by the Transportation Security Administration (TSA)
to address the security concerns.
The FAA gave no consideration to a flight-accessible Class C cargo
compartment when the classification was first developed, as no
manufacturer had ever proposed to incorporate such a feature into their
design. Inherently a ``cargo compartment'' was not intended for access,
especially by the traveling public.
The FAA acknowledges that a previous Embraer airplane, the Embraer
S.A., Model EMB 135BJ, has a flight-accessible Class C cargo
compartment that was approved using an equivalent level of safety
finding. The Embraer S.A., Model EMB 135BJ design is similar to the
proposed design for the ERJ 190-100 ECJ. The Embraer S.A., Model EMB
135BJ approval was granted before the increased security concerns and
the new regulations imposed by the TSA to address security concerns. We
have determined that because the existing airworthiness standards do
not contain adequate or appropriate safety standards, relative to cargo
compartment accessibility by passengers during flight, special
conditions are the appropriate method for this and all future
accessible Class C cargo compartments.
Type Certification Basis
Under the provisions of Sec. 21.101, Embraer S.A. must show that
the Embraer S.A., Model ERJ 190-100 ECJ meets the applicable provisions
of the regulations incorporated by reference in Type Certificate No.
A57NM or the applicable regulations in effect on the date of
application for the change to the ERJ 190-100 ECJ. The regulations
incorporated by reference in the type certificate are commonly referred
to as the ``original type certification basis.''
If the Administrator finds that the applicable airworthiness
regulations (i.e., part 25) do not contain adequate or appropriate
safety standards for the Embraer S.A., Model ERJ 190-100 ECJ because of
a novel or unusual design feature, special conditions are prescribed
under the provisions of Sec. 21.16.
In addition to the applicable airworthiness regulations and special
conditions, the Embraer S.A., Model ERJ 190-100 ECJ 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 Sec. 11.19, under
Sec. 11.38, and they become part of the type certification basis under
Sec. 21.101.
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 or similar
novel or unusual design feature, or should any other model already
included on the same type certificate be modified to incorporate the
same or similar novel or unusual design feature, the special conditions
would also apply to the other model under Sec. 21.101.
Novel or Unusual Design Features
The Embraer S.A., Model ERJ 190-100 ECJ will incorporate a novel or
unusual design feature of in-flight access to a Class C cargo
compartment.
Discussion
The FAA considers that Class C cargo compartment access during
flight may impact the isolation of the passenger cabin from the cargo
compartment, which is needed to protect the passengers from any fire
and smoke that may start within the cargo compartment, as required by
Sec. 25.857(c). In addition, in-flight access to the Class C
compartment creates unique hazards resulting from passengers having
access to cargo and baggage in the compartment. These hazards include
safety for the persons entering the cargo compartment, possible hazards
to the airplane as a result of this access, and security concerns with
access to the baggage and/or cargo. These special conditions provide
additional requirements necessary to ensure sufficient cabin isolation
from fire and smoke in this unusual design configuration, and for
passenger safety while occupying the Class C compartment during flight.
Security
The FAA has been in contact with the TSA to understand the security
concerns with passengers having access in-flight to baggage and/or
cargo, and specifically with regard to unscreened (checked) baggage/
cargo. The TSA has provided the following information to clarify the
regulations concerning access to cargo compartments by passengers.
Aircraft operators holding operating certificates under 14 CFR
part 119 for scheduled passenger operations, public charter
passenger operations, and private charter passenger operations must
have an aircraft operator security program. For U.S. flag carriers
49 CFR 1544 regulates the operator security program. Specifically,
49 CFR 1544.101(a)-(i) describes the type of program an aircraft
operator must adopt depending on the type of aircraft operation. For
the vast majority of operations in-flight access to checked baggage
and/or cargo by passengers is NOT permitted by the aircraft operator
security program. Aircraft operators should contact their Principal
Security Inspector (PSI) concerning in-flight access to checked
baggage and/or cargo by passengers.
For airplanes not operated for hire or offered for common carriage
(e.g., operation under FAA operating rules 14 CFR parts 91 or 125),
flight-accessibility to baggage and/or cargo placed in the Class C
cargo compartment is controlled by the operator of the airplane. This
provision does not preclude the operator from receiving remuneration to
the extent consistent with 14 CFR parts 125 and 91, subpart F, as
applicable. These airplane operators do not hold
[[Page 46541]]
operating certificates under 14 CFR part 119.
For airplanes operated for hire or for common carriage (e.g.,
operation under FAA operating rules 14 CFR part 119), the TSA
regulations provided in 49 CFR 1544.203 prohibit in-flight access to
checked baggage and cargo. Checked baggage and cargo do not pass
through the screening required of carry-on baggage, and thus may
introduce a security concern if passengers are provided in-flight
access.
Note: These special conditions are specific to the in-flight
accessible Class C cargo compartment. Security requirements for
occupants and for baggage/cargo placed in other locations continue
to be subject to the screening requirements and operator's security
program as identified in 49 CFR 1544.
Fire Protection and Alerting
It is the FAA's position that the threat of fire is of paramount
concern, and therefore prompt crew action to fight the fire must be
taken to prevent a fire from threatening the safety of the airplane.
For Class C cargo compartments, the means of controlling a fire is
by flooding the compartment with an extinguishing agent. These
extinguishing agents are hazardous to humans. In the event of smoke
detection, the flightcrew should ensure that the cargo compartment is
not occupied before they discharge the extinguishing agent. To address
this concern, a warning system is provided to the flight crew to alert
them when a person is in the cargo compartment.
After the extinguishing agent has been discharged into the
compartment, there must be a means of alerting a person(s) not to enter
the compartment. It must be located adjacent to the entry/exit door
that provides access into the compartment. Access into the cargo
compartment must be prevented after discharge of the extinguishing
agent to prevent persons from being exposed to the extinguishing agent
and to keep the extinguishing agent in the compartment to control the
fire.
Passengers in the cabin are alerted when oxygen is needed. A person
in the cargo compartment would not be alerted when oxygen is needed. To
address this concern, an aural and visual indication system within the
cargo compartment is required to alert the person(s) that oxygen is
required. An oxygen dispensing unit must be provided adjacent to the
entry door into the cargo compartment to have oxygen readily available
for the person leaving the compartment. The oxygen supply lines must
not be routed into the cargo compartment because that would provide a
source of oxygen to the cargo which would feed a fire.
Cargo Restraint
If a net is used as the primary means of retention of the cargo, an
untrained person accessing a cargo compartment may not be capable of
securing the net correctly to maintain the retention of the cargo. The
improperly restrained cargo could be a hazard in flight to the safe
operation of the airplane and a hazard to the occupants under crash
load conditions.
Discussion of Comments
A notice of proposed special conditions No. 25-08-05-SC for the
Embraer S.A., Model ERJ 190-100 ECJ airplanes was published in the
Federal Register on April 21, 2008 (73 FR 21286).
A comment was received from Embraer S.A.
Requested change: Embraer agreed with all proposed special
conditions except for the private use only limitation in Condition No.
8. Embraer noted that 49 CFR 1544.203(d)(2) requires the operator to
prevent access to checked baggage. Embraer also noted that because the
ERJ 190-100 ECJ Class C cargo compartment is accessible in-flight, all
baggage placed there is not checked baggage, but rather is considered
accessible subject to the screening requirements of 49 CFR 1544.201.
Embraer proposed to include guidance in the ERJ 190-100 ECJ operational
publications describing the applicable TSA regulations and how the
accessible main deck Class C compartment should be treated in
compliance with those regulations. Embraer further noted that the
security issue is relevant to in-flight baggage accessibility, and is
not related to the unique feature (built-in fire extinguishing) of the
ERJ 190-100 ECJ Class C compartment, and that many other airplanes have
been certified since the EMB-135BJ with flight accessible compartments,
without any private use limitations. Embraer believes that the private
use, not-for-hire limitation proposed by the FAA is not necessary and,
if imposed, would preclude the ERJ 190-100 ECJ from operating in the
charter market. Embraer proposed that when all of the in-flight
accessible cargo/baggage is screened as carried on baggage/cargo, the
airplane should be permitted to be operated for hire and for common
carriage.
FAA Disposition: We partially agree with the Embraer comments. When
all of the occupants and in-flight accessible baggage/cargo are subject
to the accessible baggage screening requirements identified in 49 CFR
part 1544 there would not be a need to limit the operation of the
airplane to private use, not for common carriage. We have revised
Condition No. 8 to allow operation for hire and common carriage when
the occupants and the baggage/cargo that is accessible in-flight are
subject to the screening requirements of 49 CFR part 1544. It should be
noted that the screening of the occupants and carry on baggage is
addressed by the operators' security program as identified in 49 CFR
part 1544. AFM Limitations are necessary to ensure that flight crews
are aware of the unique security requirements associated with in-flight
accessible compartments when operating for hire or for common carriage.
The FAA has imposed similar limitations on other programs initiated
since increased security requirements were introduced, and intends to
continue to do so for future projects that introduce in-flight
accessible cargo compartments, regardless of the classification of
those compartments per 14 CFR 25.857.
Applicability
As discussed above, these special conditions are applicable to the
Embraer S.A., Model ERJ 190-100 ECJ. Should Embraer S.A. apply at a
later date for a change to the type certificate on the same type
certificate to include another model incorporating the same novel or
unusual design feature, the special conditions would apply to that
model as well.
Conclusion
This action affects only certain novel or unusual design features
on the Embraer S.A., Model ERJ 190-100 ECJ airplanes. It is not a rule
of general applicability.
List of Subjects in 14 CFR Part 25
Aircraft, Aviation safety, Reporting and recordkeeping
requirements.
0
The authority citation for these special conditions is as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701, 44702, 44704.
The Special Conditions
0
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 Embraer S.A. Model ERJ 190-100 ECJ
airplanes.
1. There must be a clear, visual message in the cockpit to advise
the flightcrew when the main deck Class C cargo compartment is
occupied.
2. There must be means provided to keep the cargo door open while
the
[[Page 46542]]
cargo compartment is occupied. There must be a placard located on or
adjacent to the cargo door instructing occupants that the door must be
closed and latched at all times except when someone is in the cargo
compartment. This placard must also instruct the person entering the
cargo compartment to keep the door open when they are in the cargo
compartment and to immediately close and latch the door when they exit
the cargo compartment.
3. There must be a (on/off) visual advisory/warning stating ``Do
Not Enter'' (or similar words) to be located outside of and on or near
the main entry door/hatch to the main deck cargo compartment. The
advisory/warning is to be controlled from the flight deck.
4. There must be an aural and visual warning provided in the
baggage compartment to alert an occupant when an oxygen mask must be
donned immediately.
5. Oxygen dispensing units must be automatically presented and
immediately available to an occupant(s) of the baggage compartment when
they exit the compartment. For these special conditions, immediately
available means the oxygen dispensing units are located in the
passenger cabin near the main entry door/hatch to the main deck cargo
compartment (no oxygen supply lines are allowed to be routed into the
compartment). The number of oxygen dispensing units must be equal to
the number of occupants allowed in the cargo compartment. There must be
a placard located on or adjacent to the cargo door instructing
occupants of the maximum number of occupants allowed in the cargo
compartment.
6. For cargo and baggage placed in the baggage compartment whose
primary retention means is by net, the net must be constructed so that
the means of opening and closing or securing the net is easily
identified and operated.
7. These special conditions apply to main deck accessible Class C
cargo compartments with volumes of 10 m3 or less. Class C
cargo compartments that are accessible to passengers with a volume
greater than 10 m3 may be approved, but would likely require
additional limitations or provisions to mitigate the larger volume.
Note that there may also be a maximum volume above which access is not
acceptable.
8. Operational limitations: The airplane has operational
limitations associated with the level of screening required for
baggage/cargo that is placed in the in-flight accessible Class C cargo
compartment. These limitations must be documented in the Airplane
Flight Manual (AFM).
(a) When the airplane is not operated for hire or offered for
common carriage screening of the baggage/cargo placed in the in-flight
accessible Class C compartment is the responsibility of the operator of
the airplane. This provision does not preclude the operator from
receiving remuneration to the extent consistent with 14 CFR parts 125
and 91, subpart F, as applicable.
(b) When the airplane is operated for hire or operated for common
carriage, the baggage/cargo placed in the in-flight accessible Class C
compartment is subject to the screening requirements and operators
security program as identified in 49 CFR part 1544.
Issued in Renton, Washington, on July 31, 2008.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E8-18474 Filed 8-8-08; 8:45 am]
BILLING CODE 4910-13-P