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- (i) APU master switch - OFF ( IF APU NOT REQUIRED FOR BLEED )
- (ii) DC ESS ON BAT and AC EMER. ON INV lts - OFF
- (iii) CM1 ND comes back.
- (iv) Fuel X-feed open.
- APU start is possible below FL200.
- Landing gear extension, by gravity only, to avoid ST.BY GEN tripping.
- With LAND RECOVERY ON - SLATS, FLAPS, A/SKID and GRD SPOILERS 1,4,6,7 are available.
- Check BUS EQPT list , note down the systems not available for approach.
- Ask for Radar Vector, or home to VOR, do not home to NDB, as ADF is not available.
- Nose wheel steering is not available. Ask for tow truck, after landing.
- If on ST.BY.GEN., the equipment and Indications given below are available.
- During descent, increase the cockpit temp. to approx surface (OAT) temp. As window heat is lost, when descending the OAT will increase but windows are cold thus fogging will take place on the window, which will restrict the visibility. By increasing the cockpit temp the windows will also get warm and remain clear.
- Since IRS 2 is lost (IRS warn light flashing on MSU ), select ATT mode on MSU 2 and SYS 2 and STS HDG on ISDU and enter heading (wing level ).
FLT CNTR ENG. NAV/FLT INST.
PITCH TRIM 1 EGT PFD 1
YAW DAMPER 1 N1 ND 1
PITCH FEEL 1 START VALVE IRS 1 & 3
RUDDER TRAVEL 1 IGN. B ALT 1
VOR / ILS 1
FUEL FMS 1
QTY IND. ATC / VHF 1
CTR L.PUMP, INR 2L DME 1
ISOL VALVES
FLIGHT ON BATTERY ONLY
- IGNITION.............CONT. RELIGHT
- Use Elevator and Rudder with care above 170 kts (Low speed)
- Fuel feed by gravity (All pumps are lost )
- ST.BY. GEN. fault light illuminate on ELEC panel
- Max flight time (Bat. capacity 25 AH charged at 70%) - 38 mts. Beyond 30 min. total loss of electrical power may occur, leading to loss of Slats / Flaps extension.
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