by Damien Burke
Switch No. 4
Check STBY, return to NORM
Switch No. 3
EMER (3 min warm up). I/C N warning
PANEL, INSTRMTS, and GENERAL lighting
As required
100% OXY/AIRMIX switch
As required
A.D.C. mix switch
ADC MIX
Anti-g stop-cock lever
On (forward)
Anti-g control valve
Set H or L, press TEST button
A.V.S. temperature control
Inoperative
A.V.S. flow control
Inoperative
UHF ST/BY switch
Hold at TEST, check emer. UHF Switch No. 3 to R + G
H.F. (if fitted)
Check radio, and aerial change-over
SEAT
Mask / jerkin
Mask – check by pressing inboard button
Jerkin – check by lifting guard and pressing both buttons
Regulator change-over lever
Select stand-by regulator, check for at least 18 sec., no OXY warning. Return to main regulator
Emergency oxygen control
Fully home
BEFORE STARTING
Confirm cockpit checks complete
AFTER-STARTING CHECKS
No. 2 engine ground idle:
No. 2 H.P. turb. air temp.
Warning lamps out, Indicators functioning
No. 2 Rear Bearing temp.
Warning lamps out, Indicators functioning
No. 2 Oil inlet temp.
Indicators functioning
No. 2 Flowmeter
Indicators functioning
No. 2 Nozzle position
Closed
No. 2 Rear bearing diff. press.
For ground use only
No. 1 engine ground idle:
As per No. 2 engine
Fuel panel:
FLIGHT TIME REMAINING
Indicator functioning
FUEL REMAINING
Indicator functioning
Ess. a.c. busbar frequency meter
398 +/- 8 c.p.s.
Brake pressure gauges
Pressures 1 and 2 PORT, 1 and 2 STBD, between - 1750psi
I.P. alignment switch
To FLIGHT when alignment complete
A.V.C.U.
Set variation to zero, resynchronize
C.W.P.
All warnings out. Press to test.
Canopy
Select CLOSE, pull closed; push down latching handle, check mechanical indicators LOCKED and selector moves to OPEN
Canopy jettison handle
Remove pin and stow
Seat
Remove pins and stow
BEFORE TAKE-OFF CHECKS
Fuel
Check contents
Instrumentation switch panel
Switch according to Flight Test Schedule
Altimeter
Set QNH, ‘drome ht. +/- 20ft.
Artificial horizon
Erected
Compass and heading indicator
Check against runway hdg.
Tacan
Check BRG and DIST readout
Oxygen
Contents/press., 100% OXY/AIRMIX as required. Flow indicator operating.
Canopy
Check LOCKED
Harness
Tight and locked
C.W.P.
All warnings out
TAKE-OFF CHECKS
(engines at max dry)
Brake pressures
1,750psi max.
No. 1 and 2 H.P. turb. air temp.
Warning lamp out. Temps within Flight Clearance Note limits
No. 1 and 2 Rear bearing temp.
Warning lamp out. Temps within Flight Clearance Note limits
No. 1 and 2 Oil inlet temp.
Temps within Flight Clearance Note limits
No. 1 and 2 Flowmeters
Check functioning
No. 1 and 2 Nozzle positions
Open to max. dry position
Brakes released. Reheat on :
No. 1 and 2 Nozzle positions
Fully open
BEFORE LANDING CHECKS
Undercarriage
Check down through downward sight
Fuel
Check contents and c.g. position
Brake pressure
1,750psi max.
Harness
Tight and locked
AFTER LANDING CHECKS
Brake temperatures
Check
Brake pressures
1,750psi max.
SHUT-DOWN CHECKS
(ground power on)
Instrumentation master switch
Leave on
Engineering tape recorder
Leave running
B.S.E. RECORDER
All switches off
Crash recorder
Check off
Tank switches
All OFF
Downward sight
AZIMUTH control pushed in, switch OFF
Rapid start panel
All switches off
I.P. alignment switch
STANDBY (aircraft must not be moved for at least 20 min.)
Canopy jettison handle
Safety pin fitted
Seat
Safe for parking
Cockpit lighting
Off
BRITISH AIRCRAFT CORPORATION
(PRESTON DIVISION)
T.S.R. 2
(XR219 & 220)
FLIGHT REFERENCE CARDS (3)
EMERGENCY DRILLS
(1) AIRCRAFT ENGINE AND AFCS
FAILURES
ISSUE 2, JUNE 1964
INCORPORATING AMENDMENT LIST 6, APRIL 1965
Issued by - Technical Publications Dept.,
WARTON AERODROME, LANCS.
BARRIER ENGAGEMENT
Call for barrier
Throttles COCK OFF
Nosewheel on ground
Steer by differential braking (n/w steering lost)
Enter between verticals, centre if possible
Steady braking throughout
Parking brake on at rest
Lox cock shut (navigator)
Note :- N/w steering may be regained by selecting U/C EMERG.
FIRE DRILLS; ABANDONING
PREPARE TO ABANDON THE AIRCRAFT IF ANY FIRE
WARNING PERSISTS 3 MINUTES AFTER TAKING ACTION
ENG FIRE WARNING
Throttle
COCK OFF
L.P. COCK
CLOSED
Speed
Reduce if possible
Extinguisher
Operate
Return to base, using SINGLE ENGINE RECOVERY
Note: No further extinguishant is available.
REHEAT FIRE WARNING
Throttle
IDLE
Extinguisher
Operate
Return to base, avoiding use of reheat
Note: Extinguishant still available on other side
EJECTION
Recommended speed
250knots
Maximum speed
500knots
Full auto sequence
above 300knots
Individual (navigator first)
below 300knots
Canopies first
below 75knots
Straight and level or climbing
Above 42,000ft. DEPRESS for 30 seconds if possible
FAILURE OF AUTO-SEPARATION :-
Press button and lift EMERGENCY HARNESS RELEASE handle to full extent; roll out of seat, pull ‘chute D-ring
Note :-
EMERGENCY oxygen not available when separated from seat
TAKE-OFF ENGINE FAILURES
1. At or below V stop :-
Throttles
IDLE
Parachute
Pull ONCE to stream
Brakes
Apply fully
Barrier
Call to raise
2. Above V stop :-
No immediate action
Accelerate to 220knots, climb into circuit
Dead engine
COCK OFF
Approach as in SINGLE ENGINE RECOVERY
Strain gauge warning :-
Leave for up to 20 seconds, then see IN-FLIGHT ENGINE FAILURES (9)
IN-FLIGHT ENGINE FAILURES
1. Mechanical defect, Nozzle runaway open, OIL warning :-
Throttle
COCK OFF
L.P. COCK
CLOSE
Use SINGLE-ENGINE RECOVERY
2. Nozzle runaway closed :-
Throttle back to dry range. No further use of reheat.
3. THROT warning, No throttle response, RPM fluctuating :-
DO NOT MOVE THROTTLE LEVER (TCU failure)
Emergency throttle switch
EMERG
NOZZLE OV/RIDE switch
MAX.DRY
Check RPM and temperature within limits
TO CANCEL REHEAT :-
Reduce to approx 95% RPM (NOT below) on d.c. throttle
Throttle lever back to dry range
Reheat cannot be reselected
NOTE:-
(a) No automatic P3, top temperature or acceleration control or RPM governing on d.c. throttle. Handle engine with care and monitor frequently, especially when climbing or decelerating.
(b) If THROT warning appeared suddenly, or together with GEN warning, make one attempt only to regain normal control, after stabilizing engine.
4. P3 warning
Throttle back to clear
5. Nozzle area fluctuating :-
Cancel reheat if in use
If unsuccessful, select MAX DRY.
If still unsuccessful, select EMERG throttle.
6. AUX. DR warning :-
Reduce speed to below 300knots
Return to base
7. REHEAT extinguishes or fails to light :-
Cancel selection
Attempt re-selection after 8 seconds minimum
If no light-up within 3 seconds, cancel
8. TCV warning :-
Throttle: IDLE
(a) IF WARNING GOES OUT :- (failed open)
Engine may be used for cruise if warning stays out
Expect reappearance of warning when reducing IAS
Shut down for approach and landing.
(b) IF WARNING REMAINS :- (failed closed)
Switch OFF associated generator unless other has failed; wait 5 seconds and RESET
Leave throttle at IDLE until TCV warning goes out
9. Strain gauge warning (NOT 220)
Return to base at min. RPM on both engines
Navigator cancel and reset warning
RELIGHTING
FLAMEOUT :-
IMMEDIATE RELIGHT :-
Throttle
Slam to IDLE
Fueldraulic PUMP switch
X-OVER
Start / relight
Press and hold
IF NO RELIGHT WITHIN 15 SECONDS :-
Throttle
COCK OFF
NORMAL RELIGHT after 1 minute.
NORMAL RELIGHT :-
Speed
Above 250kt
Below 350kt / 0.9M
Height
Below 35,000 feet
Throttle
COCK OFF
WINDMILL RELIGHT switch
Aft (assist) below 18% RPM
Fwd. (guarded) above 18% RPM
Fueldraulic PUMP switch
X-OVER
Start / relight
Press and hold
Throttle
Slowly to IDLE in about 10 seconds
NO RELIGHT WITHIN 15 SEC. OF REACHING IDLE
OR
TURBINE TEMPERATURE EXCEEDS 550°C
Throttle
COCK OFF
Try again after 1 minute.
CONSISTENT FAILURE TO RELIGHT :-
Suspect throttle runaway closed (no THROT warning)
Relight on d.c. throttle (below).
DOUBLE FLAMEOUT :-
Throttles
Slam to IDLE
IMMEDIATE RELIGHT on both engines; if neither lights,
Speed
Above 250knots
Commence fast descent to 35,000ft.
Restrict flying controls operation to a minimum
NORMAL RELIGHT on one engine only, at or below 35,000ft. When one engine is running, relight the other.
RELIGHT ON D.C. THROTTLE :-
EMERG switch
EMERG (THROT warning)
Throttle
COCK OFF
D.C. throttle switch
‘close’ for 30 seconds
NOZZLE OV/RIDE switch
MAX. DRY
WINDMILL RELIGHT switch
Aft (assist) below 18% RPM
Fwd. (guarded) above 18% RPM
Fueldraulic PUMP switch
X-OVER
Start / relight
Press and hold
Throttle
To red mark
D.C. throttle switch
‘open’ slowly (i.e. not continuously)
IF NO RELIGHT WITHIN 20 SECONDS
(of start of D.C. throttle opening)
OR TURBINE TEMPERATURE EXCEEDS 550°C
Throttle
COCK OFF
D.C. throttle switch
‘close’ for 30 seconds
Try again after 1 minute
AFTER RELIGHT :-
Fueldraulic PUMP switch
NORM (220 ONLY)
Ensure WINDMILL RELIGHT switches forward / guarded
SINGLE-ENGINE RECOVERY
Note :- Gearbox X-OVER is limited to 8 minutes with the LP COCK CLOSED. (No limit with cock OPEN)
1. IMMEDIATELY :-
GEARBOX drive
DIS
GEN. CONTROL switch
OFF
EM. GEN switch
To remaining HYD system
Warnings
OIL, CONT, SERV. GEN on
(Stay at fueldraulic PUMP
X-OVER regardless)
Autobalance master switch
GAUGE
Check CROSSFEED cock OPEN
c.g. meters
Both at G.
2. RECOVERY
Cruise at 330kt (subject to M limitation)
Specific range increases with altitude and M.
Maintain c.g. position by MAN. TRANS as necessary
Navigator eliminates resulting BAL warnings with AUTO reset.
3. DOWNWIND, BEFORE UNDERCARRIAGE SELECTION :-
GEARBOX drive
X-OVER
Warnings
CONT, SERV out
4. APPROACH (NORMAL DOUBLE DATUM)
Remaining engine
Reheat
Flaps
20°
Air brakes
IN
Approach at 190kt; touchdown 180knots
5. APPROACH ON D.C. THROTTLE
Remaining engine
Maximum dry thrust
Flaps
20°
Air brakes
IN
Undercarriage
Delay DOWN until long finals
Speeds
230kt downwind, 210kt reducing to 200 on approach; 190kt touchdown.
6. AFTER SECOND GEN WARNING
No possible action
Emergency generator only remains
Cancel reheat before any hydraulic selection
No simultaneous hydraulic selections
Proceed as for 3 : (Normal U/C DOWN operative).
7. AFTER SECOND CONT WARNING :-
GEARBOX DRIVE
X-OVER
Warnings
CONT, SERV out
8. AFTER SECOND SERV WARNING :-
EM. GEN switch
Dead engine HYD system
(GEARBOX drive to X-OVER if second GEN warning appears).
GEARING: 0
Reduce speed
Pitch and yaw feel lost
To select air brakes or flaps :-
GEARBOX DRIVE
X-OVER, make selection and return to DIS
To select undercarriage :-
GEARBOX DRIVE
X-OVER
U/C selector
DOWN (1 or 2 greens)
U/C EMERG
EMERG.