NIIN Output Data
Definition:
A HOLLOW BODY USED TO TRANSPORT AIR TO VARIOUS PARTS OF THE AIRCRAFT FOR THE PURPOSE OF HEATING, COOLING, PRESSURIZING, DE-ICING, AND THE LIKE. IT MAY INCLUDE FLANGE(S), BRACKET(S), AND THE LIKE FOR MOUNTING PURPOSES. EXCLUDES PIPES USED IN AIRCRAFT EXHAUST SYSTEMS AND PIPES USED IN NON-AIRCRAFT APPLICATIONS. EXCLUDES PIPE, EXHAUST AND PIPE, AIR CONDITIONING-HEATING.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| L5338270-001 | 43999 | A | 3 | 2 | 2 | SB |
CAGE Information
| Code | Company |
|---|---|
| 43999 | BOEING COMPANY THE DBA BOEING DIV DE |
Federal Supply Class
Title
AIRCRAFT AIR CONDITIONING, HEATI
Inclusions:
INCLUDES CABIN SUPERCHARGING EQUIPMENT; CANISTERS; CYLINDER ASSEMBLIES; MASKS; FIXED OXYGEN SYSTEM; SPECIALLY DESIGNED AIRCRAFT VALVES; CABIN PRESSURE REGULATORS; HEAT EXCHANGERS; AIR EXPANSION TURBINES; AIRCRAFT HEATERS; VENTILATING SYSTEM COMPONENTS; AIR CONDITIONING AND HEATING DUCT ASSEMBLIES; THERMAL DE-ICING EQUIPMENT; CABIN AND COMPARTMENT PRESSURIZING EQUIPMENT; AIR DIFFUSERS; CABIN PRESSURE SELECTORS; LIQUID OXYGEN CONVERTERS.
Exclusions:
EXCLUDES OXYGEN PRESSURE SIGNALS AND WARNING DEVICES; TUBING; GROUND TYPE HEATERS AND COOLERS; PRESSURIZING EQUIPMENT OTHER THAN THAT USED FOR CABIN AND COMPARTMENT PRESSURIZATION; FLUID DE-ICING EQUIPMENT; VALVES SPECIFICALLY DESIGNED FOR USE WITH AIRCRAFT ENGINES, GUIDED MISSILES, AND GUIDED MISSILE ENGINES.
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| FEAT | SPECIAL FEATURES | PCONSIST OF WEB TUBE; WEB,ALUMINUM ALLOY SHEET 6061-0 PER QQ-A-250/11; FLANGE,ALUMINUM ALLOY SHEET 6061-0; TUBE 1.250 IN. OD; WEB 0.600 IN. LG,O.O4O IN. THK,0.380 IN WD; FLANGE 1.500 IN. LG,0.040 IN. THK,1.500 IN. WD |
| AGAV | END ITEM IDENTIFICATION | B-1B AIRCRAFT |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | WW-T-700/6 FED SPEC SINGLE MATERIAL RESPONSE |
| CZEJ | AIRCRAFT STATION NUMBER | YF325.7 |
| CZDJ | AIRCRAFT LOCATION | CREW AIR OVERHEAD SUPPLY |
| ABHP | OVERALL LENGTH | 3.500 INCHES NOMINAL |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-1B |
| MATT | MATERIAL | ALUMINUM ALLOY 6061 |
| ABPX | MATERIAL THICKNESS | 0.035 INCHES NOMINAL |