Appendix 1 - Acceptable ODR Tables

Definitions	ODR Training Level
“HO” = Handout	A
“ST” = Slide/tape presentations “TCBI” = Tutorial computer based instruction “SU” = Stand-up Instructors “VT” = Video tapes	B
“ICBI” = Interactive computer based instruction “CSS” = Cockpit system simulators “CPT” = Cockpit procedures trainers “PTT” = Part task trainers “FTD 2-5” = Flight training devices (level 2-5)	C
“FTD 6-7” = Flight training devices (level 6-7) “SIM A-B” = Simulators (level A or B)	D
“SIM C-D” = Simulators (level C or D) “ACFT” = Aircraft	E

Notes

An “X” in an ODR table column indicates that any of the training methods listed for that level are acceptable. If a specific instruction method is specified in an ODR table column, it must be used.

“ C* ” in the Checking column of the ODR tables requires use of training devices specified in “Training LVL C” column of ODR table

 

Difference Aircraft: GV-SP Base Aircraft: GIV-X Approved By ( POI )____________________________				Compliance Method
				Training				CHK / CURR
Design	Remarks	FLT CHAR	PROC CHNG	LVL A	LVL B	LVL C	LVL D	CHK	CURR
20 Aircraft General	Performance Max T.O. Weight 91,000 lb Increase of 17,100 lb	No	No	X				A	A
23 Communications	Selcal Test and CVR Test switches relocated	No	Minor	X				A	A
27 Flight Controls	Split flight controls added	Yes	Minor			CSS or CPT or PTT or FTD 5		A	A
27 Flight Controls	Trailing edge contours (TECs) added to inboard trailing edge of flaps	No	No	X				A	A
27 Flight Controls	No Alternate Flap Switch	No	Minor	X				A	A
27 Flight Controls	Standby rudder and nose wheel steering on AUX pump capability	No	Minor		X			A	A
27 Flight Controls	Spoiler Control switch added. Lateral Control Switch deleted.	Yes	Minor		X			B	A
27 Flight Controls	Vortex generators added to lower horizontal stabilizer surfaces and upper elevator surfaces	No	Minor	X				A	A
28 Fuel	Heated Fuel Return System	No	Minor		X			A	A
29 Hydraulic Power	Aux Hydraulic Boost Pump added	No	No	X				A	A
30 Ice and Rain	Pitot Probe Heat System changed.	No	Minor	X				A	A
32 Landing Gear	4 brake wear indicator pins vs. 2 and WOW switches	No	Minor	X				A	A
49 APU	Different APU installed. RE220 vs. 36-150 both supplied by Honeywell.	No	Minor		X			A	A
49 APU	Bleeds off takeoff capability added.	No	Major		X			A	A
70 Powerplant	BR710 installed vs. Tay 611-8C	No	Minor		X			A	A
78 Engine Exhaust	Thrust Reverser Manual Stow switches (2) installed	No	Minor		X			A	A
Limitations	Max Takeoff Weight increased to 91,000 lb from 73,900 lb. Max Landing Weight increased to 75,300 lb from 66,000 lb. Fuel quantity 41,300 lb vs. 29,500 lb APU and Engine limitations differences.	No	No	X				A	A

 

 

Difference Aircraft: GV-SP Base Aircraft: GIV-X Approved By ( POI )____________________________				Compliance Method
				Training				CHK / CURR
Maneuver	Remarks	FLT CHAR	PROC CHNG	LVL A	LVL B	LVL C	LVL D	CHK	CURR
Normal Takeoff	Bleeds Off	No	Minor	X				A	A

 

 

Difference Aircraft: GV-SP Base Aircraft: GIV-X Approved By ( POI )____________________________				Compliance Method
				Training				CHK / CURR
System	Remarks	FLT CHAR	PROC CHNG	LVL A	LVL B	LVL C	LVL D	CHK	CURR
23 Communications	Selcal and CVR test switches different test methodology	No	Minor	X				A	A
27 Flight Controls	Spoiler Control switch added. Lateral Control Switch deleted.	Yes	Minor		X			B	A
30 Ice and Rain	Pitot Probe Heat System changed.	No	Minor	X				A	A
49 APU	Different APU installed. RE220 vs. 36-150 both supplied by Honeywell.	No	Minor		X			A	A
49 APU	Starter assisted airstart capability for main engines	No	Major		X			A	A
49 APU	Bleeds off takeoff capability added	No	No		X			A	A
70 Powerplant	Thrust increased by 1,535 lb to 15,385 lb	No	No	X				A	A

 

 

Difference Aircraft: GIV-X Base Aircraft: GV-SP Approved By ( POI )____________________________				Compliance Method
				Training				CHK / CURR
Design	Remarks	FLT CHAR	PROC CHNG	LVL A	LVL B	LVL C	LVL D	CHK	CURR
20 Aircraft General	Performance Max T.O. Weight 17,100 lb decrease to 73,900 lb	No	No	X				A	A
23 Communications	Selcal Test and CVR Test switches relocated	No	Minor	X				A	A
27 Flight Controls	Alternate Flap Control switch added	No	Minor		X			A	A
27 Flight Controls	No split flight controls	Yes	Minor		X			A	A
27 Flight Controls	Trailing Edge Contours not installed	No	No	X				A	A
27 Flight Controls	No standby rudder and no nose wheel steering on AUX pump capability	Yes	Minor		X			A	A
27 Flight Controls	Lateral Control switch added. Spoiler Control Switch deleted.	Yes	Minor		X			B	A
27 Flight Controls	Vortex generators deleted from lower horizontal stabilizer surfaces and upper elevator surfaces	No	Minor	X				A	A
28 Fuel	No Heated Fuel Return System installed	No	Minor	X				A	A
29 Hydraulic Power	Aux Hydraulic Boost Pump deleted	No	No	X				A	A
30 Ice and Rain	Pitot Probe Heat System changed.	No	Minor	X				A	A
32 Landing Gear	2 brake wear indicator pins vs. 4	No	Minor	X				A	A
49 APU	Different APU installed. RE220 vs. 36-150 both supplied by Honeywell.	No	Minor		X			A	A
49 APU	No Bleeds Off takeoff capability	No	No	X				A	A
70 Powerplant	Tay 611-8C installed vs. BR710.	No	Minor		X			A	A
78 Engine Exhaust	No Manual Thrust Reverser Stow switches installed.	No	Minor	X				A	A
Limitations	Max T.O. Weight decreased by 17,100 lb to 73,900 lb. Max landing weight decreased to 66,000 lb. Fuel quantity 29,500 lb vs. 41,300 lb APU and engine limitations differences.	No	No	X				A	A

 

 

Difference Aircraft: GIV-X Base Aircraft: GV-SP Approved By ( POI )____________________________				Compliance Method
				Training				CHK / CURR
Maneuver	Remarks	FLT CHAR	PROC CHNG	LVL A	LVL B	LVL C	LVL D	CHK	CURR
None	None	No	No

 

 

Difference Aircraft: GIV-X Base Aircraft: GV-SP Approved By ( POI )____________________________				Compliance Method
				Training				CHK / CURR
System	Remarks	FLT CHAR	PROC CHNG	LVL A	LVL B	LVL C	LVL D	CHK	CURR
23 Communications	Selcal and CVR test switches different test methodology	No	Minor	X				A	A
27 Flight Controls	Lateral Control switch added. Spoiler Control Switch deleted.	Yes	Minor		X			B	A
30 Ice and Rain	Pitot Probe Heat System changed.	No	Minor	X				A	A
49 APU	Different APU installed. RE220 vs. 36-150 both supplied by Honeywell.	No	Minor		X			A	A
49 APU	No Bleeds Off takeoff capability	No	Minor	X				A	A
70 Powerplant	Thrust decreased 1,535 lb to 13,850 lb	No	No	X				A	A

 

 

Difference Aircraft: GV Base Aircraft: GIV-X Approved By ( POI )____________________________				Compliance Method
				Training				CHK / CURR
Design	Remarks	FLT CHAR	PROC CHNG	LVL A	LVL B	LVL C	LVL D	CHK	CURR
20 Aircraft General	Performance Max T.O. Weight 90,500 lb Increase of 16,600 lb	No	No	X				A	A
20 Aircraft General	Observer seat and location changed.	No	No		VT			A	A
21 ECS	Outflow valve changed to butterfly valve.	No	Minor	X				A	A
24 Electrical Power	Revised Location of PDB circuit breaker panels	No	Minor	X				A	A
27 Flight Controls	Split flight controls added	Yes	Minor			CSS or CPT or PTT or FTD 5		A	A
27 Flight Controls	No Alternate Flap Switch	No	Minor	X				A	A
27 Flight Controls	Standby Rudder installed with nose wheel steering on the AUX pump capability (including AUX pump ground spoiler pressure)	Yes	Minor		X			A	A
27 Flight Controls	Spoiler Control switch added. Lateral Control Switch deleted.	Yes	Minor		X			B	A
27 Flight Controls	Vortex generators added to lower horizontal stabilizer surfaces and upper elevator surfaces	No	Minor	X				A	A
28 Fuel	Heated Fuel Return System added	No	Minor		X			A	A
29 Hydraulic Power	Aux Hydraulic Boost Pump added	No	No	X				A	A
30 Ice and Rain	Pitot Probe Heat System changed.	No	Minor	X				A	A
32 Landing Gear	4 brake wear indicator pins vs. 2 and WOW switches	No	Minor	X				A	A
49 APU	Different APU installed with capability for APU assisted main engine airstart and different electrical load capabilities.	No	Minor		X			A	A
52 Doors	Main Door moved aft 24 inches	No	No	X				A	A
52 Doors	Aft Lav Dump Door relocated	No	No	X				A	A
70 Powerplant	BR710 vs. Tay 611-8C Installed	No	Minor		X			A	A
78 Engine Exhaust	Thrust Reverser Manual Stow Switches (2) installed.	No	Minor		X			A	A
Limitations	Max Takeoff Weight increased to 90,500 lb from 73,900 lb.	No	No	X				A	A

 

 

Difference Aircraft: GV Base Aircraft: GIV-X Approved By ( POI )____________________________				Compliance Method
				Training				CHK / CURR
Maneuver	Remarks	FLT CHAR	PROC CHNG	LVL A	LVL B	LVL C	LVL D	CHK	CURR
None	None	No	No

 

 

Difference Aircraft: GV Base Aircraft: GIV-X Approved By ( POI )____________________________				Compliance Method
				Training				CHK / CURR
System	Remarks	FLT CHAR	PROC CHNG	LVL A	LVL B	LVL C	LVL D	CHK	CURR
22 Autoflight	TOGA Flight Director Command Bars initiate at 12 degrees vs. 8 degrees on GIV-X.	No	No	X				A	A
23 Communications	New Audio System	No	No			X		A	A
23 Communications	Radio Tuning Through RFMU	No	Yes			X		A	A
27 Flight Controls	Spoiler Control switch added. Lateral Control Switch deleted.	Yes	Minor		X			B	A
30 Ice and Rain	Pitot Probe Heat System changed.	No	Minor	X				A	A
31 Indicating / Recording Systems	Standby Engine Instrument on RFMU	No	Minor	X				A	A
31 Indicating / Recording Systems	DAU (Data Acquisition Unit) and FWC (Fault Warning Computer) replaces MAU (Modular Avionics Unit)	No	Minor	X				A	A
31 Indicating / Recording Systems	Display Controller	No	Minor			X		A	A
31 Indicating / Recording Systems	Electronic Checklist Auto Pop-up Feature enabled	No	Minor		ST , TCBI or VT			A	A
34 Navigation	IRS on/off switches deleted and replaced with MSU switches	No	Minor		X			A	A
34 Navigation	EICAS FMS Joystick Panel	No	None		X			A	A
34 Navigation	6 Display Units vs. 4 Display Units	No	Minor			X		B	A
34 Navigation	No CCD s Used in Conjunction with Displays	No	Minor			X		B	A
34 Navigation	HSI on RFMU	No	Minor		X			A	A
34 Navigation	LaserTrack	No	Minor			X		B	A
34 Navigation	Standby Flight instruments have different design and location	No	Minor	X				A	A
49 APU	Different APU installed with capability for APU assisted main engine airstart and different electrical load capabilities.	No	Minor		X			A	A
70 Powerplant	Thrust increased by 900 lb to 14,750 lb	No	No	X				A	A

 

 

Difference Aircraft: GIV-X Base Aircraft: GV Approved By ( POI )____________________________				Compliance Method
				Training				CHK / CURR
Design	Remarks	FLT CHAR	PROC CHNG	LVL A	LVL B	LVL C	LVL D	CHK	CURR
20 Aircraft General	Performance Max T.O. Weight 73,900 lb Decrease of 16,600 lb	No	No	X				A	A
20 Aircraft General	Observer seat and location changed.	No	No		VT			A	A
21 ECS	Outflow valve changed to thrust recovery outflow valve.	No	Minor	X				A	A
23 Communications	Selcal test and CVR test switches relocated	No	Minor	X				A	A
24 Electrical Power	Revised Location of PDB circuit breaker panels	No	Minor	X				A	A
27 Flight Controls	No Standby Rudder installed or nose wheel steering on the AUX pump capability	Yes	Minor		X			A	A
27 Flight Controls	No split flight controls	Yes	Minor	X				A	A
27 Flight Controls	Lateral Control switch added. Spoiler Control Switch deleted.	Yes	Minor		X			B	A
27 Flight Controls	Vortex generators deleted from lower horizontal stabilizer surfaces and upper elevator surfaces	No	Minor	X				A	A
27 Flight Controls	Alternate Flap Switch added	No	Minor		X			A	A
28 Fuel	No Heated Fuel Return System	No	Minor	X				A	A
29 Hydraulic Power	No Aux Hydraulic Boost Pump	No	No	X				A	A
30 Ice and Rain	Pitot Probe Heat System changed.	No	Minor	X				A	A
49 APU	Different APU installed with no capability for APU assisted main engine airstart and different electrical load capabilities.	No	Minor		X			A	A
52 Doors	Main Door moved forward 24 inches	No	No	X				A	A
52 Doors	Aft Lav Dump Door relocated	No	No	X				A	A
Limitations	Max Takeoff Weight decreased to 73,900 lb from 90,500 lb. Fuel Quantity 29,500 lb vs. 41,300 lb APU and engine limitations differences	No	Minor	X				A	A

 

 

Difference Aircraft: GIV-X Base Aircraft: GV Approved By ( POI )____________________________				Compliance Method
				Training				CHK / CURR
Maneuver	Remarks	FLT CHAR	PROC CHNG	LVL A	LVL B	LVL C	LVL D	CHK	CURR
None	None	No	No

 

 

Difference Aircraft: GIV-X Base Aircraft: GV Approved By ( POI )____________________________				Compliance Method
				Training				CHK / CURR
System	Remarks	FLT CHAR	PROC CHNG	LVL A	LVL B	LVL C	LVL D	CHK	CURR
22 Autoflight	TOGA Flight Director Command Bars initiate at 8 degrees vs. 12 degrees on GV.	No	No	X				A	A
23 Communications	New Audio System	No	Minor			X		A	A
23 Communications	Radio Tuning Through MCDU and graphically	No	Minor		X			A	A
27 Flight Controls	Lateral Control switch added. Spoiler Control Switch deleted.	Yes	Minor		X			B	A
30 Ice and Rain	Pitot Probe Heat System changed.	No	Minor	X				A	A
31 Indicating / Recording Systems	Electronic Checklist Auto Pop-up Feature deleted	No	Minor	X				A	A
31 Indicating / Recording Systems	Standby Engine Instruments on MCDU	No	Minor	X				A	A
31 Indicating / Recording Systems	DAU (Data Acquisition Unit) and FWC (Fault Warning Computer) replaced by MAU (Modular Avionics Unit)	No	Minor	X				A	A
31 Indicating / Recording Systems	Display Controller	No	Minor			X		A	A
34 Navigation	IRS MSU switches deleted and replaced with on/off switches	No	Minor	X				A	A
34 Navigation	4 Display Units vs. 6 Display Units	No	Minor			X		B	A
34 Navigation	Added Dual CCD s used in Conjunction with Displays	No	Minor			X		B	A
34 Navigation	LaserTrack removed	No	Minor	X				A	A
34 Navigation	Standby Flight instruments have different design and location	No	Minor		X			A	A
34 Navigation	MCDU on Emergency Power	No	Minor		X			B	A
49 APU	Different APU installed with no capability for APU assisted main engine airstart and different electrical load capabilities.	No	Minor		X			A	A
70 Powerplant	Thrust decreased by 900 lb to 13,850 lb	No	No	X				A	A

 

 

Difference Aircraft: GV-SP Base Aircraft: G-V Approved By ( POI )____________________________				Compliance Method
				Training				CHK / CURR
Design	Remarks	FLT CHAR	PROC CHNG	LVL A	LVL B	LVL C	LVL D	CHK	CURR
20 Aircraft General	Performance Max T.O. Weight 91,000 lb Increase of 500 lb	No	No	X				A	A
21 ECS	Outflow valve changed to thrust recovery outflow valve.	No	No	X				A	A
24 Electrical Power	Revised Location of PDB circuit breaker panels	No	Minor	X				A	A
25 Equipment / Furnishings	Redesign and relocation of cockpit observer’s seat to behind Co-Pilot’s seat	No	No		X			A	A
27 Flight Controls	Trailing edge contours (TECs) added to inboard trailing edge of flaps	No	No	X				A	A
38 Water & Waste	Fuselage conformal fresh water tank	No	Minor	X				A	A
38 Water & Waste	Relocation of vacuum lavatory waste tank from baggage compartment to above APU	No	No	X				A	A
49 APU	Bleeds off takeoff capability added	No	Major		X			A	A
52 Doors	Main Door moved forward 24 inches	No	No	X				A	A
52 Doors	Aft Lav Dump Door relocated	No	No	X				A	A
53 Fuselage	27 Boundary Layer Energizers added above the canopy	No	No	X				A	A
56 Windows	Addition of 7th cabin window	No	No	X				A	A
57 Wings	7 Vortex Generators relocated outboard on each wing	No	No	X				A	A
Limitations	Max Takeoff Weight increased to 91,000 lb from 90,500 lb.	No	No	X				A	A

 

 

Difference Aircraft: GV-SP Base Aircraft: G-V Approved By ( POI )____________________________				Compliance Method
				Training				CHK / CURR
Maneuver	Remarks	FLT CHAR	PROC CHNG	LVL A	LVL B	LVL C	LVL D	CHK	CURR
Normal Takeoff	Bleeds Off	No	Minor	X				A	A

 

 

Difference Aircraft: GV-SP Base Aircraft: G-V Approved By ( POI )____________________________				Compliance Method
				Training				CHK / CURR
System	Remarks	FLT CHAR	PROC CHNG	LVL A	LVL B	LVL C	LVL D	CHK	CURR
22 Autoflight	TOGA Flight Director Command Bars initiate at 8 degrees vs. 12 degrees on GV.	No	No	A				A	A
23 Communications	New Audio System	No	Minor			X		A	A
23 Communications	Radio Tuning Through MCDU and graphically	No	No		X			A	A
31 Indicating/ Recording Systems	Electronic Checklist Auto Pop-up Feature deleted	No	Minor Non Normal	X				A	A
31 Indicating/ Recording Systems	DAU (Data Acquisition Unit) and FWC (Fault Warning Computer) replaced by MAU (Modular Avionics Unit)	No	Minor	X				A	A
31 Indicating/ Recording Systems	Standby Engine Parameters available on #1 MCDU only	No	Minor	X				A	A
31 Indicating/ Recording Systems	Different formatting on some synoptic displays	No	Minor		X			A	A
34 Navigation	IRS MSU switches deleted and replaced with on/off switches	No	Minor	X				A	A
34 Navigation	4 Display Units Vs 6 Display Units with different formatting.	No	Major			X		B	A
34 Navigation	Added Dual CCD ’s Used in Conjunction with Displays	No	Minor			X		B	A
34 Navigation	Display controllers have different menus.	No	Minor			X		A	A
34 Navigation	Standby Flight instruments have different design and location	No	Major		X			B	A
34 Navigation	Display Unit Controller has 4 overhead switches instead of 3	No	Major		X			B	A
34 Navigation	RNP and Estimated Position Uncertainty (EPU) is displayed on PFD	No	Minor		X			A	A
34 Navigation	MCDU on Emergency Power	No	Minor		X			B	A
49 APU	Bleeds off takeoff capability added	No	Minor		ST , TCBI , SU VT			A	A
70 Powerplant	Thrust increased by 635 lb to 15,385 lb	No	No	HO				A	A

 

 

Difference Aircraft: G-V Base Aircraft: GV-SP Approved By ( POI )____________________________				Compliance Method
				Training				CHK / CURR
Design	Remarks	FLT CHAR	PROC CHNG	LVL A	LVL B	LVL C	LVL D	CHK	CURR
20 Aircraft General	Performance Max T.O. Weight 500 lb. decrease to 90,500 lb	No	No	X				A	A
21 ECS	Outflow valve changed to butterfly style.	No	No	X				A	A
24 Electrical Power	Revised location of PDB's and associated circuit breakers.	No	Minor	X				A	A
25 Furnishings	Redesign and relocation of cockpit observer’s seat to behind Captain’s seat	No	No		X			A	A
27 Flight Controls	Trailing Edge Contours not installed	No	No	X				A	A
38 Water & Waste	Non-fuselage conformal fresh water tank	No	No	X				A	A
38 Water “& Waste	Relocation of vacuum lavatory waste tank from above APU to baggage compartment	No	No	X				A	A
49 APU	No Bleeds Off takeoff capability	No	Minor	X				A	A
52 Doors	Main Door moved aft 24 inches	No	No	X				A	A
52 Doors	Aft Lav Dump Door relocated	No	No	X				A	A
53 Fuselage	27 Boundary Layer Energizers removed from the canopy	No	No	X				A	A
56 Windows	Removal of 7th cabin window	No	No	X				A	A
57 Wings	7 Vortex generators relocated inboard on each wing	No	No	X				A	A
Limitations	Max T.O. Weight decreased by 500 lb to 90,500 lb	No	No	X				A	A

 

 

Difference Aircraft: G-V Base Aircraft: GV-SP Approved By ( POI )____________________________				Compliance Method
				Training				CHK / CURR
Maneuver	Remarks	FLT CHAR	PROC CHNG	LVL A	LVL B	LVL C	LVL D	CHK	CURR
None		No	No

 

 

Difference Aircraft: G-V Base Aircraft: GV-SP Approved By ( POI )____________________________				Compliance Method
				Training				CHK / CURR
System	Remarks	FLT CHAR	PROC CHNG	LVL A	LVL B	LVL C	LVL D	CHK	CURR
22 Autoflight	TOGA Flight Director Command Bars initiate at 12 degrees vs. 8 degrees on GV-SP.	No	No	X				A	A
23 Communications	New audio system	No	Minor			X		A	A
23 Communications	Radio tuning accomplished through RFMU 's	No	Minor			X		A	A
31 Indicating/ Recording Systems	Electronic Checklist has Auto pop-up Feature vs. passive checklist on GV-SP	No	Minor		X			A	A
31 Indicating/ Recording	MAU replaced by DAU and FWC	No	Minor			X		B	A
31 Indicating/ Recording Systems	Engine Parameters available on either RFMU	No	Minor	X				A	A
31 Indicating/ Recording Systems	Different formatting on some synoptic displays	No	Minor		X			A	A
34 Navigation	EICAS FMS Joystick Panel	No	None		X			A	A
34 Navigation	LaserTrack	No	Minor			X		B	A
34 Navigation	IRS on/off switches replaced with IRS MSU switches	No	Minor		X			A	A
34 Navigation	6 Display Units Vs 4 Display Units with different formatting	No	Minor			X		B	A
34 Navigation	No CCD 's installed	No	Minor			X		B	A

 

 

Difference Aircraft: GV-SP Base Aircraft: G-V Approved By ( POI )____________________________				Compliance Method
				Training				CHK / CURR
System	Remarks	FLT CHAR	PROC CHNG	LVL A	LVL B	LVL C	LVL D	CHK	CURR
34 Navigation	Display controllers have different menus	No	Minor			X		B	A
34 Navigation	Standby Flight instruments have different design and location	No	Minor	X				A	A
34 Navigation	Display Unit Controller has 3 overhead switches instead of 4	No	Minor			X		B	A
34 Navigation	RNP and Estimated Position Uncertainty (EPU) are not displayed on PFD	No	Minor		X			B	A
49 APU	No bleeds off takeoff capability	No	Minor	X				A	A
70 Powerplant	Thrust reduced 635 lb to 14,750 lb	No	No	X				A	A