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 FTD5   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 FTD5   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 CCDs 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 CCDs 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
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