NIIN Output Data
Definition:
A MIRROR, USUALLY WITH A FRAME AND BRACKET(S) AND/OR ARM(S), FOR ADJUSTABLE MOUNTING IN A POSITION TO REFLECT VISIBILITY IN A SPECIFIED DIRECTION.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 826BANM | 75595 | F | 5 | 9 | 2 | SB | ||
| ST9M610-1 | 76301 | A | 3 | 2 | 2 | SB | ||
| 94063-1 | 1YBJ4 | A | 5 | 2 | 6 | ZZ | ||
| 94063-1 | 86175 | A | 5 | 2 | 2 | ZZ | ||
| P-1164 | 75595 | F | 5 | 9 | 4 | 9Z |
CAGE Information
| Code | Company |
|---|---|
| 1YBJ4 | MOYER & ASSOCIATES INC |
| 75595 | SWEDLOW INC LIBERTY MIRROR DIV |
| 76301 | BOEING COMPANY THE DBA BOEING |
| 86175 | GKN AEROSPACE TRANSPARENCY SYSTEMS I |
Federal Supply Class
Title
MISCELLANEOUS AIRCRAFT ACCESSORI
Inclusions:
INCLUDES CONTROL ASSEMBLIES, PUSH-PULL; BRACE, POSITIONING CARGO RAMP STOWED ON BOARD; COCKPIT MOUNTED CONTROL QUADRANTS; ACTUATORS, ELECTRO-MECHANICAL AND MECHANICAL; VENTILATORS; RELIEF TUBES; MAP HOLDERS; AERIAL GLIDER TOWING ACCESSORIES ATTACHED TO AIRCRAFT; BELTS, SAFETY AND LAP; HARNESS, SHOULDER AND SAFETY; LITTER ATTACHING SUPPORTS;ELECTRIC WINDSHIELD WIPERS;AIRCRAFT ONBOARD INERT GAS GENERATORS;AIRCRAFT FURNITURE;AIRCRAFT MOUNTED WINCHES AND HOISTS;IN-FLIGHT REFUELING SYSTEM COMPONENTS, INCLUDING FUEL COMPONENTS;AIRCRAFT CURTAINS;CABLE TENSION REGULATORS;SUN VISORS;REAR-VIEW MIRRORS;MECHANICAL TRANSMISSIONS, GEARBOXES AND CONSTANT SPEED DRIVES SPECIALLY DESIGNED FOR AIRCRAFT.
Exclusions:
EXCLUDES ENGINE MOUNTED CONTROL ASSEMBLIES; FITTED COVERS, AIRCRAFT PYLONS; HELICOPTER ROTER BRAKE SYSTEM COMPONENTS; HELICOPTER AUTOMATIC STABILIZATION EQUIPMENT.
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| SURF | SURFACE TREATMENT | ANODIZED OR ZINC CHROMATE |
| AYQM | MOUNTING LOCATION | INSIDE |
| ALKE | FRAME WIDTH | 2.100 INCHES NOMINAL |
| ALKD | FRAME LENGTH | 6.950 INCHES NOMINAL |
| BWDW | MIRROR SHAPE | ARC |
| ALGC | MOUNTING CONFIGURATION | BALL STUD WITH 0.500 IN. DIA BALLAND 0.025 IN.-2B EXT THD STUD |