UNITED KINGDOM
CIVIL AVIATION AUTHORITY
FA 63
Issue 1
August 1995
HS 125 Series 1
HS125 Series 3
HS125 Series 400
HS125 Series 600
HS125 Series 700
BAe125 Series 800
BAe125 Series 1000
Hawker 800 Series
Hawker 1000 Series
TYPE CERTIFICATE DATA SHEET No. FA63
This data sheet which is part of CAA Type Certificate No. FA63 prescribes conditions and limitations under
which the product, for which the type certificate was issued, meets the airworthiness requirements of the Civil
Aviation Authority.
NOTE:As a consequence of Type Certificate transfer from Raytheon Corporate Jets, Inc. to Raytheon
Aircraft Company on 1st August 1995, Type Certificate number BA9 and its associated data sheet have
been superseded by this document for control of 125 products imported into the United Kingdom.
UK Certification from 1st August 1995 is based on FAA Certification together with compliance with UK
Additional Requirements for Import (see page 2).
TYPE CERTIFICATE HOLDER: BEECH AIRCRAFT CORPORATION
Also known as RAYTHEON AIRCRAFT COMPANY
9709 East Central
Wichita
Kansas 67206
United States of America
MANUFACTURER: Up to and including Hawker 1000 Series, Raytheon Corporate Jets, Inc.
and predecessor companies.
Hawker 800XP Raytheon Corporate Jets, Inc.
AIRCRAFT TYPE/ HS 125 Series 1-521
MODEL NUMBER(S): HS 125 Series 1-522
HS125 Series 1/S-522
HS125 Series 1/R-522
HS125 Series 3/R
HS125 Series 3/RA
HS125 Series 3/RB
HS125 Series F3/RA
HS125 Series F3
2 FA63
Issue 1
Aircraft Type/Model Nos continued:
HS125 Series 400/1
HS125 Series 401
HS125 Series 402
HS125 Series 403
HS125 Series F400
HS125 Series 600/1
HS125 Series 600/2
HS125 Series 600/3
HS125 Series F600
Hawker 800XP
TYPE DESIGN DEFINITION: HS125 Series 1 Document No. DO/AW/125/T.C.1
HS125 Series 3 Document No. DO/AW/125/T.C.1
HS125 Series 400 Document No. DO/AW/125/T.C.1
HS125 Series 600 Document No. DO/AW/125-600/T.C.1
HS 125 Series 700 Document No. DO/AW/125-700/ FAA/T.C.1
BAe125 Series 800 Document No. DO/AW/125-800/ FAA/T.C.1
(See Note 1)
BAe125 Series 1000 Document No. CJE-HPA-G-260-AW1660
(See Note 2)
Hawker 800 Document No. DO/AW/125-800/FAA/T.C.1
Hawker 1000 Document No. CJE-HPA-G-260-AW1660
Hawker 800XP Document No.RAE-HSC-F-258-AW95000147
CERTIFICATION BASIS: FAA certification basis as presented by FAA Type Certificate Data
Sheet number A3EU together with UK Additional Requirements for
Import.
CERTIFICATION CATEGORY: Transport Category (Passenger)
Private Category
PERFORMANCE CATEGORY: Group A
FLIGHT MANUAL: HS125 Series 1 HS 1.1
HS125 Series 1 HS 1.2
1-521 HS 1.2
1-522 HS 1.3
1S-522 HS 1.3
1R-522 HS 1.3
HS125 Series 3 HS 1.3
3/R HS 1.3
3/RA HS 1.3
3/RB HS 1.3
F3 HS 1.12
HS125 Series 400 HS 1.5
400B/1 HS 1.5
401 HS 1.5
403 HS 1.5
F400 HS 1.5
3 FA63
Issue 1
Flight Manual continued:
HS125 Series 600 HS 1.7
600/1 HS 1.7
600/2 HS 1.7
600/3 HS 1.7
F600 HS 1.8
HS125 Series 700 HS 1.8
BAe 125 Series 800 HS 1.15
BAe 125 Series 1000 HS 1.18
Hawker 800 HS 1.15
Hawker 1000 HS 1.18
Hawker 800XP HS 1.21
ENGINE: Engine TCDS No.
HS125 Series 1 Two Bristol Siddley Viper 520 1024
1-521 Two Bristol Siddley Viper 521 1025
1-522 Two Bristol Siddley Viper 522 1033
HS125 Series 3 Two Bristol Siddley Viper 522 1033
3/R Two Bristol Siddley Viper 522 1033
3/RA Two Bristol Siddley Viper 522 1033
3/RB Two Bristol Siddley Viper 522 1033
HS125 Series 400 Two Bristol Siddley Viper 522 1033
400/1 Two Bristol Siddley Viper 522 1033
401 Two Bristol Siddley Viper 522 1033
403 Two Bristol Siddley Viper 522 1033
F400 Two Garrett TFE 731-3R-1H E6WE
HS125 Series 600 Two Rolls Royce (Bristol Engine Division) Viper 601
F600 Two Garrett AiResearch TFE 731-3R-1H E6WE
HS125 Series 700 Two Garrett AiResearch TFE 731-3R-1H E6WE
BAe 125 Series 800 Two Garrett Turbine Engine Co. TFE 731-5R-1H E6WE
BAe 125 Series 1000 Two Pratt & Whitney PW305B E35NE
Hawker 800 Two Garrett Turbine Engine Co. TFE 731-5R-1H E6WE
Hawker 1000 Two Pratt & Whitney PW305B E35NE
Hawker 800XP Two Allied Signals Engines TFE 731-5BR-1H E6WE
4 FA63
Issue 1
MAXIMUM WEIGHTS:
Series 1 Model 1-521 Model 1-521
with modification
252022
Maximum taxying weight 20,800 lb (9,434 kg) 21,200 lb (9,616 kg) 21,400 lb (9,707 kg)
Maximum take-off weight 20,500 lb (9,298 kg) 21,200 lb (9,616 kg) 21,200 lb (9,616 kg)
Maximum Landing weight 19,550 lb (8,868 kg) 19,550 lb (8,868 kg) 19,550 lb (8,868 kg)
Maximum zero fuel weight 13,000 lb (5,889 kg) 13,000 lb (5,889 kg) 13,200 lb (5,987 kg)
Model 1-521 with Model 1/S-522 Model 1/S-522 with
Mod. 256423 Mod. 252022
Maximum taxying weight 21,200 lb (9,616 kg) 21,200 lb (9,616 kg) 21,900 lb (9,934 kg)
Maximum take-off weight 19,500 lb (8,868 kg) 21,200 lb (9,616 kg) 21,700 lb( 9,833 kg)
Maximum Landing weight 18,100 lb (8,210 kg) 19,500 lb (8,845 kg) 19,550 lb (8,868 kg)
Maximum zero fuel weight 13,000 lb (5,889 kg) 13,000 lb (5,889 kg) 13,700 lb (6,214 kg)
Model 1/S-522 with Model 1/S-522 with Model 1/S-522& Series 3
Mods. 251302 & 251303 Mods.251883 & 251867 with Mods 251700 &
255640
Maximum taxying weight 21,200 lb (9,616 kg) 21,700 lb (9,833 kg) 22,300 lb (10,115 kg)
Maximum take-off weight 21,200 lb (9,616 kg) 21,700 lb (9,833 kg) 22,200 lb (10,069 kg)
Maximum Landing weight 20,000 lb (9,071kg) 19,550 (8,868 kg) 19,550 lb (8,868 kg)
Maximum zero fuel weight 13,500 lb (6,123kg) 13,500 lb (6,123 kg) 13,200 lb (5,987 kg)
Series 3 Series 3 with Mods. Series 3 with
251302 & 251314 modification 252022
Maximum taxying weight 21,400 lb (9,707 kg) 21,700 lb (9,833 kg) 21,900 lb (9,934 kg)
Maximum take-off weight 21,200 lb (9,616 kg) 21,700 lb (9,833 kg ) 21,700 lb (9,833 kg)
Maximum Landing weight 20,000 lb (9,071 kg) 20,000 lb (9,071 kg) 20,000 lb (9,071 kg)
Maximum zero fuel weight 13,500 lb (6,123 kg) 13,500 lb (6,123 kg) 13,700 lb (6,214 kg)
Model 3R Model 3/RA Model 3/RB
Maximum taxying weight 22,800 lb (10,342 kg) 23,100 lb (10,478 kg) 23,300 lb (10,569 kg)
Maximum take-off weight 22,700 lb (10,296 kg) 22,800 lb (10,342 kg) 23,300 lb (10,569 kg)
Maximum Landing weight 20,000 lb (9,071 kg) 20,000 lb (9,071 kg) 20,000 lb (9,071 kg)
Maximum zero fuel weight 13,700 lb (6,214 kg) 14,200 lb (6,441 kg) 14,200 lb (6,441kg)
Model F3 Model F3 with HS 125 Series 400
Modification 259224
Maximum taxying weight 21,900 lb (9,934 kg) 21,900 lb (9,934 kg) 23,300 lb (10,569 kg)
Maximum take-off weight 21,700 lb (9,833 kg) 21,700 lb (9,833 kg) 23,300 lb (10,569 kg)
Maximum Landing weight 20,000 lb (9,071 kg) 20,000 lb (9,071 kg) 20,000 lb ( 9,071 kg)
Maximum zero fuel weight 13,700 lb (6,214 kg) 13,800 lb (6,260 kg) 14,200 lb ( 6,441 kg)
Model 401 Models 403 and F400 HS 125 Series 600
Maximum taxying weight 23,600 lb (10,705 kg) 23,800 lb (10,795 kg) 25,000 lb (11,340 kg)
Maximum take-off weight 23,600 lb (10,705 kg) 23,600 lb (10,705 kg) 25,000 lb (11,340 kg)
Maximum Landing weight 20,000 lb ( 9,071 kg) 20,000 lb ( 9,071 kg) 22,000 lb ( 9,979 kg)
Maximum zero fuel weight 14,500 lb ( 6,571 kg) 14,700 lb ( 6,668 kg) 15,550 lb ( 7,053 kg)
5 FA63
Issue 1
HS 125 Series 600 with HS 125 Series 700 HS 125 Series 700
modification 252320 and variant model F600 with modification
258332
Maximum taxying weight 25,500 lb (11,567 kg) 25,000 lb (11,340 kg) 25,500 lb (11,567 kg)
Maximum take-off weight 25,500 lb (11,567 kg) 24,800 lb (11,249 kg) 25,500 lb (11,567 kg)
Maximum landing weight 22,000 lb (9,979 kg) 22,000 lb ( 9,979 kg) 22,000 lb ( 9,979 kg)
Maximum zero fuel weight 16,050 lb (7,280 kg) 16,050 lb ( 7,280 kg) 16,050 lb ( 7,280 kg)
HS 125 Series 700 with BAe 125 Series 800 BAe 125 Series 800
modification 258825 with modification
253169A
Maximum taxying weight 25,000 lb (11,340 kg) 27,520 lb (12,483 kg) 27,520 lb (12,483 kg)
Maximum take-off weight 24,800 lb (11,249 kg) 27,400 lb (12,429 kg) 27,400 lb (12,429 kg)
Maximum Landing weight 22,000 lb (9,979 kg) 23,350 lb (10,592 kg) 23,350 lb ( 10,592 kg)
Maximum zero fuel weight 16,300 lb (7394 kg) 17,520 lb ( 7,947 kg) 18,000 lb ( 8,165 kg)
BAe Series 800 Hawker 800 Hawker 800XP
with modification with modification
259865A 25B047A & 25B059A
Maximum taxying weight 27,520 lb (12,483 kg) 26,866 lb (12,186 kg) 28,120lb (12,755 kg)
Maximum take-off weight 26,453 lb (11,999 kg) 26,866 lb (12,186 kg) 28,000lb (12701 kg)
Maximum Landing weight 23,350 lb (10,592 kg) 23,350 lb (10,592 kg) 23,350lb (10,592kg)
Maximum zero fuel weight 17,520 lb ( 7,947 kg) 18,450 lb ( 8,369 kg) 18,450lb (8369 kg)
BAe 125 Series 1000 BAe 125 Series 1000
with modification
253379A
Maximum taxying weight 31,100 lb (14,107 kg) 31,100 lb (14,107 kg)
Maximum take-off weight 31,000 lb (14,062 kg) 31,000 lb (14,062 kg)
Maximum Landing weight 25,000 lb (11,340 kg) 25,000 lb (11,340 kg)
Maximum zero fuel weight 19,800 lb ( 8,981 kg) 20,300 lb ( 9,208 kg)
NUMBER OF WHEELS AND MAXIMUM TYRE PRESSURES
Number of wheels in the nose-wheel unit: 2
Number of main-wheel units: 2
Number of wheels in each main-wheel unit: 2
DIMENSIONS:
SERIES 1, 3 and 400 Ft M
Length 47ft 5in 14.45
Wingspan 47 ft 14.33
Height 16ft 6in 5.03
Wing area 353ft2 32.8
SERIES 600 Ft M
Length 50ft 5.75in 15.39
Wingspan 47 ft 14.33
Height 17ft 3in 5.26
Wing area 353ft2 32.80
6 FA63
Issue 1
Dimensions cont’d
SERIES 700 Ft M
Length 50ft 8.55in 15.46
Wingspan 47 ft 14.33
Height 17ft 7in 5.36
2
Wing area 353ft 32.8
SERIES 800 and 800XP Ft M
Length 51ft 1.64in 15.59
Wingspan 51ft 4.5in 15.66
Height 17ft 5in 5.31
Wing area 374ft2 34.75
SERIES 1000 Ft M
Length 53ft 10.64in 16.43
Wingspan 51ft 4.5in 15.66
Height 17ft 1in 5.21
Wing area 374ft2 34.75
MINIMUM CREW:
HS 125 Series 400 The minimum flight crew is two, consisting of one pilot and one other person
HS 125 Series 600 holding a flight crew licence. This other person is required to operate the
HS 125 Series 700 emergency MANUAL CABIN ALTITUDE CONTROL which is not accessible to
& variants the pilot. For flights within controlled airspace, this other person shall hold a
Private Pilot's Licence or a Commercial Pilot's Licence or a Senior Commercial
Pilot's Licence or an Airline Transport Pilot's Licence or a Flight Navigator's
Licence, together with a Flight Radio Telegraphy or Telephony Operator's
Licence.
BAe 125 Series 800 The minimum flight crew is two pilots.
BAe 125 Series 1000 The minimum flight crew is two pilots.
Hawker 800XP The minimum flight crew is two pilots.
MAXIMUM OCCUPANTS/PASSENGERS:
Number of persons, including crew, for the HS 125 Series 600, the variant model F600, the HS 125 Series 700,
the BAe 125 Series 800, BAe 125 Series 1000 and Hawker 800XP is not to exceed 17.
Number of persons, including crew, for the HS 125 Series 400 and the variant models 401, 403 and F400 is not
to exceed 11.
OPERATING LIMITATIONS: See associated Airplane Flight Manuals
MANDATORY MAINTENANCE See related Maintenance Manual references
INSTRUCTIONS:
7 FA63
Issue 1
NOISE: Series 1 CAA Noise Type Certificate
1 29
1R 28
1/S - 522 27
1/R-522 26
1-522 24
3 23
3/RA 25
3/RC 21
400 19
F400, F3/RA 20
403 22
600 1&2
F600 18 & 88
700 16 & 84
800 63
1000 146
NOTE 1: Where the designation BAe 125 Series 800 is referenced in this document the designation
Hawker 800 equally applies.
NOTE 2: Where the designation BAe 125 Series 1000 is referenced in this document the designation
Hawker 1000 equally applies.
- END -
