Appendix 3 - Example ODR Tables

The following ODR tables are provided:

 

B-777-300ER to B-787-8 Design
DESIGN OPERATOR DIFFERENCES REQUIREMENTS
DIFFERENCE AIRCRAFT:         787-8
BASE AIRCRAFT:               777-300ER
COMPLIANCE METHOD
TRAINING CHKG/CURR
General Differences Flt char Proc chg A B C D E FLT CHK REC EXP
GENERAL LONG RANGE No No HND
OUT
           
DIMENSIONS 787-8
  • Length = 186 feet 1 inches (56.74 meters)
  • Height = 55 feet 6 inches (16.92 meters)
  • Wing Span = 197 feet 4 inches (60.12 meters)
Nose gear to main gear = 74 feet 9 inches (22.80 meters)
No No HND
OUT
           
FLIGHT DECK FLIGHT DECK ARRANGEMENT
PFD/ND format, large displays

PILOT'S FIELD OF VIEW:
Pilot eye height (above ground)
minor differences

Flight deck overhead hatch
No No HND
OUT
           
CABIN 787 max passenger capacity  is variable by customer choice No No HND OUT            
CARGO BULK CARGO
Left side
No No HND OUT            
ENGINES Rolls Royce Trent 1000
General Electric GEN X
No Yes HND OUT            
LIMITATIONS  WEIGHT/CG DIFFERENCE
  • Size/type/system limitations
VMO/MMO
  • Per placard
Max slats speed, stalling speed, VMCA, VMCG
No Yes HND OUT            

 

B-777-300ER to B-787-8 Systems
SYSTEM OPERATOR DIFFERENCES REQUIREMENTS
DIFFERENCE AIRCRAFT: 787-8
BASE AIRCRAFT: 777-300ER
COMPLIANCE METHOD
TRAINING CHKG/CURR
System Differences Flt char Proc chg A B C D E FLT CHK REC EXP
21 – AIR
CONDITIONING
CONTROLS AND INDICATORS
  • Panel layout

PACKS:
  • Electric compressors

ALTERNATE VENTILATION:
  • New Function
EQUIPMENT COOLING:
  • Forward and Aft System
  • Smoke EICAS message
CARGO HEAT SYSTEM:
  • Switch types
  • Automated functions
No YES   C
B
T
         
21 - PRESSURIZATION

SYSTEM,CONTROLS & INDICATORS:

  • Same as 777
No No              
22- AUTOFLIGHT MODE CONTROL PANEL
  • MCP 2 line windows (Speed, Heading, and Altitude)
    • Future uplink feature
  • Integrated Approach Navigation
  • Bank limit selector

AFDS FLIGHT MODE ANNUCIATIONS:
  • Same except addition of Integrated Approach Navigation and GLS

AUTOMATIC FLIGHT APPROACH AND LANDING:
  • Same except addition of Integrated Approach Navigation and GLS
No Yes   C
B
T
         
23- COMMUNICATIONS CONTROLS AND INDICATORS:
  • New Tuning Control Panel (TCP)

VHF, HF, PA, CABIN/FLIGHT AND SERVICE INTERPHONE
  • Control resides in Tuning Control Panel (TCP)

SATCOM
  • Control resides in Tuning Control Panel (TCP)

AUDIO CONTROL PANEL
  • Same except PA MIC switch function
No Yes   C
B
T
         
24- ELECTRICAL POWER ELECTRICAL CONTROL PANEL
  • System architecture – functionally equivalent
  • No bus tie switches
  • Additional Engine Generator and Drive Disconnect switches
  • Additional APU Generator switch
  • Additional external power switches

AC ELECTRICAL
  • Four Engine Starter Generators
  • Two APU Starter Generators
  • No backup generators

AC ELECTRICAL POWER DISTRIBUTION
  • No flight instrument transfer busses

DC ELECTRICAL
  • System architecture – functionally equivalent

BATTERY/STANDBY POWER SYSTEM
  • System architecture – functionally equivalent

AUTOLAND
  • System architecture – functionally equivalent
No Yss   C
B
T
         
25- EQUIPMENT/FURNISHING FLIGHT DECK GENERAL ARRANGEMENT:
  • Non-opening number two windows
  • Flight deck door controls to aisle stand and alerting on EICAS
  • Overhead hatch
  • C/Bs panels location – Main display system
No Yss H
N
D

O
U
T
           
25- EMERGENCY EVAC EMERGENCY EVACUATION PANEL
  • Same functions – Integrated aisle stand panel
No No H
N
D

O
U
T
           
26- FIRE PROTECTION APU FIRE CONTROLS AND INDICATORS:
  • Same panel/location
  • More automation

CARGO FIRE CONTROLS AND INDICATORS:
  • Same panel/location
  • Additional automation for composite structure protection
No Yes H
N
D

O
U
T
           
27 – FLIGHT CONTROLS PRIMARY FLIGHT CONTROL SURFACES
  • Roll: different mix same roll effect

FLIGHT CONTROL SYSTEMS
  • Roll - Roll rate command – same handling
  • Yaw - Yaw rate command – same handling

FLIGHT ENVELOPE PROTECTION:
  • Enhanced Stall Protection (ESP)

STABILIZER TRIM:
  • Electrical back-up trim control
  • Electrically actuated

TRIM INDICATORS:
  • Indicator location on primary EICAS display
  • Aileron trim eliminated

THRUST ASYMMETRY COMPENSATION:
  • No TAC Switch – available full time
  • Embedded in flight control law
  • Yaw rate based

FLAP LOAD RELIEF
  • Functionally equivalent but different threshold sensing

ALTERNATE FLAP OPERATION
  • Alternate mode – minor differences

CRUISE FLAPS SYSTEM
  • New performance enhancement system with EICAS message
No Yes H
N
D

O
U
T
           
28- FUEL FUEL TANKS:
  • Fuel Tank Capacities,
    • Left Main    37,500 lbs
    • Right Main   37,500 lbs
    • Center   150,800 lbs
    • Total Fuel   225,800 lbs
      (33,700 US GAL)
  • Fuel tank inerting system

CONTROLS AND INDICATORS:
  • Panel layout – minor differences
  • One Crossfeed
  • Fuel balance switch

FUEL PUMPS:
  • Center tank pump operation – minor differences
No Yes   C
B
T
         
29 – HYDRAULIC POWER CONTROLS AND INDICATORS:
  • Panel layout

HYDRAULIC SYSTEMS:
  • 5000 psi

CENTER HYDRAULIC SYSTEM
  • No Air-driven demand pumps
  • Electric pumps

 
No Yes H
N
D
           
30 - ICE AND RAIN WIPER PANEL
  • Same panel location
  • Washer switches

WING ANTI-ICE
  • Electric heater blankets
No Yes H
N
D

O
U
T
           
31- FLIGHT INSTRUMENT DISPLAYS EFIS CONTROL PANEL PFD/ND CONTROLS
  • Map switches moved to soft controls - minor
  • ND mode selector – rotary control display selection
  • ND range selector - .5 – 1280 NM

DISPLAY SELECT PANEL
  • Panel layout
  • four DSPs
  • Synoptic soft switches – software menu
  • EICAS display position switch

PFD/MFD SELECTOR
  • PFD/MFD functionally similar to INBD DSPL selector
  • Different location

INSTRUMENT SOURCE SELECTORS
  • Air data/attitude different switch type
  • NAV switch eliminated
  • DSPL CTRL switch eliminated

CURSOR CONTROL
  • Minor differences - additional rotary control

DISPLAY FORMATS:
  • Enhanced large format capabilities
  • Clock integrated in display format
  • Airport map
  • Vertical Situation Display (VSD)

STANDBY FLIGHT INSTRUMENTS
  • Same instrument minor relocation
No Yes     F
B
T
       
31- FLIGHT INSTRUMENT DISPLAYS HEAD UP DISPLAY (HUD):
  • Dual installation
No Yes

 

    F
F
S
     
32- LANDING GEAR MAIN GEAR:
  • Twin tandem bogie assembly (4 wheels)
  • No aft axle steering

NOSE WHEEL STEERING TILLER:
  • Steer by wire - Functionally equivalent
  • Nose gear cut-out switch

BRAKES:
  • System operation – functionally equivalent
  • Electric brakes
  • Battery indication vs. accumulator
No Yes H
N
D

O
U
T
           
34 – NAVIGATION CONTROL DISPLAY UNIT
  • Display based CDU
  • Cursor Controls
  • Message/Help window

FLIGHT MANAGEMENT SYSTEM
  • Added design features

INERTIAL REFERENCE SYSTEM
  • Air data system separate

TRANSPONDER PANEL
  • Control integrated into the Tuning Control Panel (TCP)

WEATHER RADAR CONTROL PANEL
  • Control integrated into the Tuning Control Panel (TCP)

Alternate NAV
  • Function in Tuning Control Panel (TCP)

 
No Yes   C
B
T
         
36- PNEUMATIC BLEED AIR CONTROL PANEL
  • Eliminated
                 
49- APU SYSTEM OPERATION
  • No Bleed Air
  • No Air Turbine Starter - Electric starter

Starter Duty cycle Limitation
No No H
N
D

O
U
T
           
52- DOORS DOORS:
  • Eight entry doors - same
No No H
N
D

O
U
T
           
70- POWER PLANT ENGINES:
  • GE & RR - engine type design differences
No Yes H
N
D

O
U
T
           
73- ENGINE FUEL AND CONTROL EEC SYSTEM
  • Functionally equivalent
No No H
N
D

O
U
T
           
77- ENGINE INDICATING INDICATORS
  • RR Engine - TPR replaces EPR
No Yes   C
B
T
         
78- EXHAUST THRUST REVERSER SYSTEM
  • Same
No No              
80 STARTING CONTROLS AND INDICATORS
  • Panel layout
  • System operation
  • Electric starter
  • Starter Duty cycle Limitation
No Yes   C
B
T
         
                     
                     
 
B-777-300ER to B-787-8 Maneuver
MANEUVER OPERATOR DIFFERENCES REQUIREMENTS TABLE
DIFFERENCE AIRCRAFT: 787-8
BASE AIRCRAFT: 777-300ER
COMPLIANCE METHOD
TRAINING CHKG/CURR
Maneuver Differences Flt char Proc chg A B C D E FLT CHK REC EXP
Exterior Preflight Minor differences No No HND
OUT
           
Preflight Procedures Minor Differences due to systems No Yes HND
OUT
           
Before Start Procedures Minor differences No Yes   CB
T
         
Taxi Minor differences (Airport Map) No Yes   CB
T
         
HUD operations Minor Differences all phases of flight No Yes       FFS   D A
Engine failure/V1 Minor differences (TAC embedded in control law) No No              
ILS/GLS Normal No differences (GLS added) No No              
Go-Around (All Eng) Minor differences (LNAV auto engage) No No HND
OUT
           
ILS Eng Inop Minor differences (TAC embedded in control law) No No              
Go-Around (One Eng) Minor differences (TAC embedded in control law) No No              
Manual Landing (One Eng) Minor differences (TAC embedded in control law) No No              
Non-ILS app Minor differences (Integrated Approach Navigation) No Yes     FBT     C  
B-787-8 to B-777-300ER Design
DESIGN OPERATOR DIFFERENCES REQUIREMENTS TABLE
DIFFERENCE AIRCRAFT: 777-300ER
BASE AIRCRAFT: 787-8
COMPLIANCE METHOD
TRAINING CHKG/CURR
General Differences Flt char Proc chg A B C D E FLT CHK REC EXP
GENERAL LONG RANGE  No No HND
OUT
           
DIMENSIONS 777-300ER
  • Length = 242 feet 4 inches (73.9 meters)
  • Height = 60 feet 10 inches (18.54 meters)
  • Wing Span = 212 feet 7 inches (64.8 meters)
  • Nose gear to main gear = 102 feet 5 inches (31.2 meters)
No No HND
OUT
           
FLIGHT DECK FLIGHT DECK ARRANGEMENT
  • PFD/ND format, smaller displays

PILOT'S FIELD OF VIEW:
  • Pilot eye height (above ground)
  • minor differences
  • Flight deck windows
No No HND
OUT
           
CABIN 777 max passenger capacity is variable by customer choice No No HND
OUT
           
CARGO BULK CARGO
  • Right side
No No HND
OUT
           
ENGINES General Electric Model GE90-115B No Yes HND
OUT
           
LIMITATIONS WEIGHT/CG DIFFERENCE
  • Size/type/system limitations

VMO/MMO
  • Per placard
Max slats speed, stalling speed, VMCA, VMCG
No Yes HND
OUT
           
 
B-787-8 to B-777-300ER Systems
SYSTEM OPERATOR DIFFERENCES REQUIREMENTS TABLE
DIFFERENCE AIRCRAFT: 777-300ER
BASE AIRCRAFT: 787-8
COMPLIANCE METHOD
TRAINING CHKG/CURR
System Differences Flt char Proc chg A B C D E FLT CHK REC EXP
21 – AIR CONDITIONING CONTROLS AND INDICATORS
  • Panel layout

PACKS:
  • Engine Bleed Air

ALTERNATE VENTILATION:
  • N/A

EQUIPMENT COOLING:
  • Forward System Only

CARGO HEAT SYSTEM:
  • Switch types
  • Automated functions

SYSTEM,CONTROLS & INDICATORS:
  • Same as 787

 
No Yes   C
B
T
         
22- AUTOFLIGHT MODE CONTROL PANEL
  • MCP single windows (speed, heading, and altitude)
  • Bank limit selector

AFDS FLIGHT MODE ANNUCIATIONS:
  • Same except no Integrated Approach Navigation or GLS

AUTOMATIC FLIGHT APPROACH AND LANDING:
  • Same except no Integrated Approach Navigation or GLS
No Yes
 
C
B
T
         
23- COMMUNICATIONS CONTROLS AND INDICATORS:
  • Radio Tuning Panel
VHF, HF, SATCOM, PA, CABIN/FLIGHT AND SERVICE INTERPHONE
  • Controlled by audio control panel
  • Tuning on radio control panel (VHF and HF)
AUDIO CONTROL PANEL
  • Same except PA MIC switch function
No Yes
 
C
B
T
         

24- ELECTRICAL POWER

ELECTRICAL CONTROL PANEL
  • System architecture – functionally equivalent
  • Bus tie switches
  • One Engine Generator and Drive Disconnect switch per engine
  • One APU Generator switch
  • Two external power switches

AC ELECTRICAL
  • Two Engine Starter Generators
  • One APU Starter Generators
  • Two backup generators

AC ELECTRICAL POWER DISTRIBUTION
  • Two flight instrument transfer busses
DC ELECTRICAL
  • System architecture – functionally equivalent
BATTERY/STANDBY POWER SYSTEM
  • System architecture – functionally equivalent

AUTOLAND
  • System architecture – functionally equivalent
No Yes
 
C
B
T
         
25- EQUIPMENT/ FURNISHING FLIGHT DECK GENERAL ARRANGEMENT:
  • Two opening number two windows
  • Flight deck access system switch to flight deck side door post
  • C/Bs panels location – overhead panel
No Yes H
N
D

O
U
T
 
           
25- EMERGENCY EVAC EMERGENCY EVACUATION PANEL
  • Same functions – Integrated aisle stand panel
No No H
N
D

O
U
T
 
           
26- FIRE PROTECTION APU FIRE CONTROLS AND INDICATORS:
  • Same panel/location
  • Less automation
No Yes H
N
D

O
U
T
 
           

27 – FLIGHT CONTROLS

PRIMARY FLIGHT CONTROL SURFACES
  • Roll: different mix same roll effect

FLIGHT CONTROL SYSTEMS
  • Roll - Roll rate command – same handling
  • Yaw - Yaw rate command – same handling

FLIGHT ENVELOPE PROTECTION:
  • Functionally equivalent

STABILIZER TRIM:
  • Alternate pitch trim levers

TRIM INDICATORS:
  • Pitch trim on Control Stand
  • Aileron trim on control wheel/column
  • Rudder trim on aft aisle stand

THRUST ASYMMETRY COMPENSATION:
  • TAC Switch on overhead panel
  • Engine thrust based

FLAP LOAD RELIEF
  • Functionally equivalent but different threshold sensing

ALTERNATE FLAP OPERATION
  • Alternate mode – minor differences
No Yes H
N
D

O
U
T
 
           
28- FUEL FUEL TANKS:
  • Fuel Tank Capacities
    • Left Main   69,000 lbs
      • (31,300 kgs)
    • Left Main    69,000 lbs
      • (31,300 kgs)
    • Center   182,800 lbs
      • (82,900 kgs)
    • Total Fuel   320,800 lbs
      • (145,500 kgs)
    • (470,890 US GAL)
  • Nitrogen generating system (NGS)

CONTROLS AND INDICATORS:
  • Panel layout – minor differences
  • Two Crossfeed
  • No fuel balance switch

FUEL PUMPS:
  • Center tank pump operation – minor differences
No Yes C
B
T
 
           
29 – HYDRAULIC POWER CONTROLS AND INDICATORS:
  • Panel layout

HYDRAULIC SYSTEMS:
  • 3000 psi

CENTER HYDRAULIC SYSTEM
  • Two air-driven demand pumps
  • Two electric pumps
No Yes H
N
D

O
U
T
 
           
30- ICE AND RAIN WIPER PANEL
  • Same panel location
  • Washer switches

WING ANTI-ICE
  • Bleed air heats three midwing leading edge slats on each wing
No Yes H
N
D

O
U
T
 
           
31- FLIGHT INSTRUMENT DISPLAYS EFIS CONTROL PANEL PFD/ND CONTROLS
  • Map switches on EFIS panel
  • ND mode selector – EFIS control panel
  • ND range selector – 10 - 640 NM

DISPLAY SELECT PANEL (DSP)
  • Panel layout
  • One DSP

INBOARD DISPLAY CONTROLS
  • functionally similar to PFD/MFD selector
  • Different location

HEAD UP DISPLAY (HUD):
  • None
No Yes
 
  F
B
T
       
32- LANDING GEAR MAIN GEAR:
  • Each gear has six wheels in tandem pairs
  • Has aft axle steering

NOSE WHEEL STEERING TILLER:
  • Hydraulic powered - Functionally equivalent

BRAKES:
  • System operation – functionally equivalent
  • Hydraulic brakes
  • Brake accumulator pressure indicator

 
No Yes

H
N
D

O
U
T
 

           
34 – NAVIGATION CONTROL DISPLAY UNIT
  • Conventional CDU

FLIGHT MANAGEMENT SYSTEM
  • Functionally equivalent

AIR DATA INERTIAL REFERENCE SYSTEM (ADIRU)
  • One ADIRU, one SAARU, eight air data modules

TRANSPONDER PANEL
  • On aft aisle stand

WEATHER RADAR CONTROL PANEL
  • On aft aisle stand

Alternate NAV
  • CDUs can be used if both FMCs fail

 
No Yes C
B
T
 
           
36- PNEUMATIC BLEED AIR CONTROL PANEL
  • Overhead panel
   
 
           
49- APU SYSTEM OPERATION
  • Bleed Air and electric power
  • Air Turbine Starter

 
No No H
N
D

O
U
T
 
           
52- DOORS DOORS:
  • Eight entry doors - same
No No H
N
D

O
U
T
           
70- POWER PLANT ENGINES:
  • GE90-115B - engine type design differences
No Yes H
N
D

O
U
T
 
           
73- ENGINE FUEL AND CONTROL EEC SYSTEM
  • Functionally equivalent
No No H
N
D

O
U
T
           
77- ENGINE INDICATING INDICATORS
  • GE Engines - N1 replaces TPR
No Yes
 
C
B
T
 
         
78- EXHAUST THRUST REVERSER SYSTEM
  • Same
No No
 
           
80 STARTING CONTROLS AND INDICATORS
  • Panel layout
  • System operation
  • Pneumatic starter
  • Starter Duty cycle limitation monitored automatically
No Yes
 
C
B
T
         
B-787-8 to B-777-300ER Maneuver
MANEUVER OPERATOR DIFFERENCES REQUIREMENTS TABLE
DIFFERENCE AIRCRAFT: 777-300ER
BASE AIRCRAFT: 787-8
COMPLIANCE METHOD
TRAINING CHKG/CURR
Maneuver Differences Flt char Proc chg A B C D E FLT CHK REC EXP
Exterior Preflight Minor differences No No HND
OUT
 
           
Preflight Procedures Minor Differences due to systems No Yes HND
OUT
 
           
Before Start Procedures Minor differences No Yes
 
CBT          
Taxi Minor differences (Airport Map on EFB) No Yes
 
CBT          
HUD operations None    
 
           
Engine failure/V1 Minor differences (TAC off) No No
 
  FFS        
ILS/GLS Normal  No differences (no GLS) No No
 
           
Go-Around (All Eng) Minor differences No Yes HND
OUT
 
           
ILS Eng Inop Minor differences (TAC off) No No
 
  FFS        
Go-Around (One Eng) Minor differences No No
 
  FFS        
Manual Landing (One Eng) Minor differences (TAC off) No No
 
  FFS        
Non-ILS app Minor differences (no Integrated Approach Navigation) No Yes
 
           
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