Federal Register - June 8, 2021
Versión en texto ¿Qué es?Dateas es un sitio independiente no afiliado a entidades gubernamentales. La fuente de los documentos PDF aquí publicados es la entidad gubernamental indicada en cada uno de ellos. Las versiones en texto son transcripciones no oficiales que realizamos para facilitar el acceso y la búsqueda de información, pero pueden contener errores o no estar completas.
Fuente: Federal Register
Federal Register / Vol. 86, No. 108 / Tuesday, June 8, 2021 / Rules and Regulations
30385
mode, which may cause the airspeed to drop significantly below the safe operating speed, possibly resulting in reduced control of the airplane.
20211102 MHI RJ Aviation ULC Type Certificate Previously Held by Bombardier, Inc.: Amendment 39
21564; Docket No. FAA20210098;
Project Identifier MCAI202001121T.
1 Model CL6002B19 Regional Jet Series 100 & 440 airplanes.
2 Model CL6002C10 Regional Jet Series 700, 701 & 702 airplanes.
3 Model CL6002C11 Regional Jet Series 550 airplanes.
4 Model CL6002D15 Regional Jet Series 705 airplanes.
5 Model CL6002D24 Regional Jet Series 900 airplanes.
6 Model CL6002E25 Regional Jet Series 1000 airplanes.
a Effective Date This airworthiness directive AD is effective July 13, 2021.
d Subject Air Transport Association ATA of America Code 22, Auto Flight.
b Affected ADs This AD replaces AD 20192207, Amendment 3919786 85 FR 439, January 6, 2020 AD 20192207.
e Reason This AD was prompted by a report that during the Automatic Flight Control System AFCS ALTS CAP, V ALTS CAP, or V
ALTV CAP mode, the flight guidance/
autopilot does not account for engine failure while capturing an altitude. The FAA is issuing this AD to address an engine failure, if it occurs during or before a climb while in ALTS CAP, V ALTS CAP, or V ALTV CAP
Within 60 days after the effective date of this AD: Revise the existing AFM to include the information in Subject 2, AUTOMATIC
FLIGHT CONTROL SYSTEM AFCS, of Section 0208, System Limitations, of Chapter 2, LIMITATIONS; and Subject 1.C, Engine Failure in Climb During ALTS
CAP, or Subject 1.D, Engine Failure in Climb During V ALTS CAP or V ALTV
CAP, of Section 0502, In-flight Engine Failures, of Chapter 5, ABNORMAL
PROCEDURES; as applicable; of the applicable AFM identified in figure 1 to paragraph g of this AD.
39.13
Amended
2. The FAA amends 39.13 by:
a. Removing Airworthiness Directive AD 20192207, Amendment 39
19786 85 FR 439, January 6, 2020; and b. Adding the following new AD:
c Applicability This AD applies to the MHI RJ Aviation ULC airplanes identified in paragraphs c1
through 6 of this AD, certificated in any category, all manufacturer serial numbers.
f Compliance Comply with this AD within the compliance times specified, unless already done.
g Revision of the Airplane Flight Manual AFM
Figure 1 to paragraph g - AFM Revision
CL-600-2B 19
CL-600-2C10
CL-600-2Cll
Bombardier CRJ Series Regional Jet Model CL-600-2C10 Series 700, 701, 702 and CL-600-2Cl 1 Series 550
AFM, CSP B-012
Revision 31, dated May 8, 2020
CL-600-2D24
Bombardier CRJ Series Regional Jet Model CL-600-2D24 Series 900 and CL-600-2D15 Series 705 AFM, CSP
C-012, Volume 1
Revision 24, dated March 27, 2020
CL-600-2E25
Bombardier CRJ Series Regional Jet Model CL-600-2E25 Series 1000
AFM, CSP D-012
Revision 23, dated February 14, 2020
h Credit for Previous Actions This paragraph provides credit for actions required by paragraph g of this AD, if those
VerDate Sep<11>2014
AFM Revision
Bombardier CRJ Series Regional Jet Revision 73, dated Model CL-600-2B19 AFM, CSP A-012, January 3, 2020
Volume 1
CL-600-2D15
jbell on DSKJLSW7X2PROD with RULES
Bombardier AFM
15:53 Jun 07, 2021
Jkt 253001
actions were performed before the effective date of this AD, using the applicable AFM
PO 00000
Frm 00011
Fmt 4700
Sfmt 4700
specified in figure 2 to paragraph h of this AD.
E:FRFM08JNR1.SGM
08JNR1
ER08JN21.015
MHI RJ Aviation ULC Airplane Model
