FLIGHT INSTRUMENTS AVIONICS Parts 6610-01-128-2428 through 6610-01-131-4484 |
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We solve sourcing challenges for parts like 6610-01-128-2428, 6610-01-128-7748, 6610-01-129-1053, 6610-01-129-3952, 6610-01-129-3953, 6610-01-129-4642, 6610-01-129-4967, 6610-01-129-6420, 6610-01-129-7097, 6610-01-129-7814 -- hard to find, long lead time, and obsolete part requirements.
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| Part number | Description | Category | Details |
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6610-01-128-2428 | PENDULUM ARM ASSEMB | | |
6610-01-128-7748 | ACCELEROMETER, ELECTRICAL, LINEAR | REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY SOURCE CONTROL DWG |
| 6610-01-129-1053 | ADAPTER, ECCENTRIC MOTOR | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY 2024-T4,QQ-A-250/4;0.560 TO 0.562 IN. DIA;0.040 IN. TH |
| 6610-01-129-3952 | PITOT-STATIC TUBE | MOUNTING METHOD | FLANGE |
| 6610-01-129-3953 | TRANSMITTER, ANGLE OF ATTACK | ELECTRICAL HEATING ELEMENT | NOT PROVIDED |
| 6610-01-129-4642 | TRANSDUCER ASSEMBLY | | |
| 6610-01-129-4967 | STRIP, COATED | | |
| 6610-01-129-6420 | COMPUTER, AIR DATA | INPUT INTELLIGENCE TYPE | PRESSURE |
| 6610-01-129-7097 | RECORDER, SIGNAL DATA | REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY SOURCE CONTROL DWG |
| 6610-01-129-7814 | COUNTERWEIGHT | III END ITEM IDENTIFICATION | 6610004466856 |
| 6610-01-129-7865 | PLATE, MOUNTING, BRUSH BLOCK | GENERAL CHARACTERISTICS ITEM DESCRIPTION | 1.600 IN. LG;0.4925 IN. W;0.062 IN. TH;ALUMINUM ALLOY 6061-T6,QQ-A-250/11;2 HOLES 0.096 DIA |
| 6610-01-129-8215 | AIR SPEED ASSEMBLY | GENERAL CHARACTERISTICS ITEM DESCRIPTION | METAL CASE; PAINTED FINISH; 3.750IN. LG; 3.500 IN. W; 5.500 IN. H; CONNECTOR TERMINATION; FOUR BOLT MTD ON 3.625 IN. BY 2.938 IN. MTG CENTERS |
| 6610-01-129-8404 | COMPUTER, AIR DATA | INTELLIGENCE INPUT METHOD | ELECTRICAL |
| 6610-01-130-0744 | INDICATOR SUBASSEMBLY, ATTITUDE | COMPONENT TYPE AND QUANTITY | 2 EYELET AND 1 INDICATOR AND 4 LAMP AND 2 NUT AND 4 POST AND 2 PRINTED WIRING BOARD AND 1 RESISTOR AND 21 SCREW AND 2 SHIM AND 6 SPACER AND 8 TERMINAL AND 8 WASHER |
| 6610-01-130-0746 | COVER, REAR | | |
| 6610-01-130-2672 | WEIGHT, SPECIAL, COUNTERBALANCE | III END ITEM IDENTIFICATION | AIRCRAFT MODEL F-18 |
| 6610-01-130-2788 | STOP, PITCH | III END ITEM IDENTIFICATION | AIRCRAFT MODEL AV-8C |
| 6610-01-130-2826 | CALIBRATION CARD, AIRSPEED | GENERAL CHARACTERISTICS ITEM DESCRIPTION | VINYL CHLORIDE POLYMER L-P-535,PRESSURE SENSITIVE BACKING,LETTERING SHALL BE 10 POINT UPPER CASE,NUMERALS SHALL BE 12 POINT,3.120 IN. LG,0.800 IN. W,0.015 IN. THK |
| 6610-01-130-2829 | INDICATOR, STICK POSITION | GENERAL CHARACTERISTICS ITEM DESCRIPTION | 2.000 IN. LG; 2.000 IN. W; 8.900 IN. MAX H; MARKED L,F,R,A,STICK POSITION,TEST,DIM; ELAPSED TIME INDICATOR ON REAR,4 DIGITS |
| 6610-01-130-4489 | ROTATING BRACKET ASSEMBLY | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ROTATING BRACKET 1;CLUSTER-SPUR GEAR 1;SPUR GEAR 1;TORSION SPRING 1;ELECTRICAL CONTACT RING 1 |
| 6610-01-130-5101 | BUTTON | | |
| 6610-01-130-7057 | RECORDER, SIGNAL DATA | RECORDING METHOD | TAPE |
| 6610-01-130-8885 | COMPUTER, ALTITUDE | III END ITEM IDENTIFICATION | MODEL A4M ACFT |
| 6610-01-131-2636 | THUMPER INSERT, ALTIMETER | III END ITEM IDENTIFICATION | ALTIMETER,PRESSURE |
| 6610-01-131-4484 | BEZEL AND CASE ASSEMBLY | | |
