Textron Aviation Inc. 750 (Citation X): certification basis
Basis entries as written on the TCDS
-
REG
T00007WI
FAA Type Certification Data Sheet No.
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
-
REG
See FAA Type Certificate Data Sheet No. T00007WI
State of Design Airworthiness Authority Certification Basis
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
-
REG
JAR‐25, Change 13, effective 5 October 1989, Orange Paper 90/1, effective 11 May 1990, Orange Paper 91/1, effective 12 April 1991, Orange Paper 93/1, effective 8 March 1993 JAR AWO Change 1, effective 29 Nov. 1985 and JAR AWO Change 2, effective 01 August 1996 NPA AWO‐5, CAT. II NPA AWO‐9, CAT. II JAR APU Change 2, 26 September 1983, (Note: APU is classified as non‐essential on this aircraft.)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
-
REG
JAA IL‐23 RVSM, effective April 1994.
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
-
REG
NPA 25G‐255 Issue 1 from 28 August 1992, Flight Manuals – General NPA 25B‐240 Landing performance in abnormal configurations
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
-
◆ SPECIAL
CRI A‐01 Thrust reversers (TGM/25/01) Yawing manoeuvring conditions (INT/POL/25/8)
-
◆ SPECIAL
SC B‐07 Accelerate‐Stop Distances and Related Performance Matters, 16 February 1993 (INT/POL/25/5)
-
◆ SPECIAL
SC B‐08 Performance Calculator (CPCalc) (TGL‐OPS Leaflet No. 36)
-
◆ SPECIAL
SC C‐03 Interaction of Systems with Structures (TGM/GEN/01; NPA 25C‐199)
-
◆ SPECIAL
SC C‐04 Ground Gust (TGM/GEN/01)
-
◆ SPECIAL
SC C‐10 Personal injury criteria for dynamic testing of Single Place Side‐Facing Seats
-
◆ SPECIAL
SC D‐01 Worn Brakes (INT/POL/25/6)
-
◆ SPECIAL
SC D‐02 Protection from the effects of HIRF (INT/POL/25/2)
-
◆ SPECIAL
SC D‐03 Protection from the Effects of Lightning Strike; Direct Effects (INT/POL/25/3)
-
◆ SPECIAL
SC D‐04 Protection from the Effects of Lightning Strike; Indirect Effects (INT/POL/25/4)
-
◆ SPECIAL
SC D‐09 Special Conditions for operation to 51000 feet Altitude
-
◆ SPECIAL
SC D‐11 Side‐facing Divan
-
◆ SPECIAL
SC F‐01 Basic RNAV (B‐RNAV) Systems Airworthiness Approval (TGL/3 Rev 1)
-
◆ SPECIAL
SC F‐10 Enhanced Vision System (INT/POL/25/2; (INT/POL/25/4))
-
EXEMPT
Engine‐out lateral trim requirements of § 25.161(d) (FAA exemption number 6431)
-
EXEMPT
(Ref: CRI A‐01)
-
ELOS
ESF B‐04 High Altitude Minimum Speed System
-
ELOS
ESF D‐05 Towing, towbarless towing
-
ELOS
ESF D‐06 Emergency Exit Marker and Location Signs
-
ELOS
ESF D‐07 Ditching Emergency Exits for Passengers
-
ELOS
ESF D‐08 Cabin Pressurization‐High Altitude Take‐off and Landing Operations
-
ELOS
ESF D‐10 Emergency Exit Access
-
ELOS
ESF D‐12 Width of Aisle
-
ELOS
ESF D‐13 Testing Standard for Thermal Acoustic Insulation
-
ELOS
ESF K‐01 Approach Flight Path – Automatic Control, Audible Warning
-
OTHER
CRI A‐03 Noise requirements: ICAO Annex 16, Volume I, 3rd edition
-
OTHER
CRI A‐03 Emission requirements: ICAO Annex 16, Volume II, 2nd edition