SCREW,DRIVE
Screws
Application: COMMUNICATIONS TERMINAL, SATELLITE AN/GSC-39(V)1; ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); TRAINER, B-1B AIRCRAFT; SYSTEMS, JP-5 AVIATION FUELS; AIRBORNE MOBILE DIR AIR SPT CTL (2ID), 02M JUL83)(AN/UYQ-3A); CLOSE IN WEAPON SYSTEM (CIWS-PHALANX); ENGINE, AIRCRAFT TF33-PW-102 (C135E, EC-135H/K/P); AIRCRAFT, (AC-130H, MC-130H, EC-130E, HC-130); SUPPORT EQUIPMENT, B-1 AIRCRAFT; GUN, 5-IN./54 CAL, MK-54; GUIDED MISSILE LAUNCHING SYS
Technical characteristics
13 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| AASU | HEAD HEIGHT | INCHES MINIMUM 0.041 AND INCHES MAXIMUM 0.049 |
| AASL | HEAD DIAMETER | INCHES MINIMUM 0.118 AND INCHES MAXIMUM 0.127 |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | OVERALL FED SPEC ALL TREATMENT RESPONSES QQ--416 TY 2 CL 3 |
| AASB | FASTENER LENGTH | INCHES NOMINAL 0.188 |
| CBBL | FEATURES PROVIDED | CASE-HARDENED |
| CRGF | NONMACHINE THREAD STYLE | |
| CTYF | NONMACHINE NOMINAL THREAD DIAMETER | INCHES 0.073 |
| MATT | MATERIAL | OVERALL STEEL |
| SFTT | SURFACE TREATMENT | OVERALL CADMIUM AND CHROMATE |
| AASK | HEAD STYLE | |
| AGAV | END ITEM IDENTIFICATION | COMMUNICATIONS TERMINAL, SATELLITE AN/GSC-39(V)1; ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); TRAINER, B-1B AIRCRAFT; SYSTEMS, JP-5 AVIATION FUELS; AIRBORNE MOBILE DIR AIR SPT CTL (2ID), 02M JUL83)(AN/UYQ-3A); CLOSE IN WEAPON SYSTEM (CIWS-PHALANX); ENGINE, AIRCRAFT TF33-PW-102 (C135E, EC-135H/K/P); AIRCRAFT, (AC-130H, MC-130H, EC-130E, HC-130); SUPPORT EQUIPMENT, B-1 AIRCRAFT; GUN, 5-IN./54 CAL, MK-54; GUIDED MISSILE LAUNCHING SYS |
| AAVM | PILOT LENGTH | INCHES NOMINAL 0.047 |
| AAVL | PILOT DIAMETER | INCHES MINIMUM 0.060 AND INCHES MAXIMUM 0.063 |
Supersedes
This item replaces cancelled NIINs 001989424 · 004481613 · 008281677 · 008036225 · 007969521 · 013170423 · 013168949. An older drawing citing one of those numbers resolves here.