All-in-One Report Demo (NSN: 5340016991107, Part Number: 50354)
Supplier Parts Availability - item details and contact information for suppliers holding stock
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Overhaul / Repair Capabilities
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Part # Description |
Cond. |
Company Name Phone Fax |
Address |
Last Update |
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50-354 LAP BELT
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NS |
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PANAMA |
2024-09-25 |
50-354 PLATE: INSTRUCTION
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NE |
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PANAMA |
2024-09-25 |
50-354 DOUBLER
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NE |
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PANAMA |
2024-09-25 |
50-354 "NAMEPLATE, INST"
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NS |
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PANAMA |
2024-09-25 |
50-354 FRAME ASSY
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NE |
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PANAMA |
2024-09-25 |
50-354 "COLLINS AEROSPACE 50-354 INSTRUCTION PLATE, FOR FIXED WING
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NE |
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PANAMA |
2024-09-25 |
50-354 SEAT BELT
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NS |
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PANAMA |
2024-09-25 |
50-354 TRANSAIR PAX SEAT BELT
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NS |
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PANAMA |
2024-09-25 |
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Master Cross Reference Data (MCRD) - alternate part numbers for national stock numbers
NSN Description MCRL Information
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5340016991107
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SEAT,HELICAL COMPRESSION SPRING
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INC: 24328
HMIC: P
ESDC:
ENAC:
Cancelled By: |
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FAA PMA - Alternate Part Numbers/Manufacturers approved by the Federal Aviation Administration
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PMA Part #
(Replacement For OEM PN) |
Approval Means Description |
PMA Holder |
Model Eligibility |
Shoulder harness
(Airbus 503543-205)
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Details Available
503543-205 |
Details Available
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Airbus (A300, B4-601, B4-603, B4-620, B4-605R, B4-622R, F4-605R)
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Restraint System Assembly
(503543-401)
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Details Available
503543-401 |
Details Available
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Airbus (A300 B4-601, B4-603, B4-620, B4-605R, B4-622R, F4-605R)
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Restraint System Assembly
(503543-403)
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Details Available
503543-403 |
Details Available
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Boeing (767-300)
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Technical Characteristics - detailed information such as measurements and material type for national stock numbers
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NSN
Item Name |
Technical Characteristics |
5340-016991107
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SEAT,HELICAL COMPRESSION SPRING |
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Management Data - US Gov't supply management data (costs, storage, etc.)
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NSN Item Name |
Management Data |
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5340-016991107
 SEAT,HELICAL COMPRESSION SPRING
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PMIC |
Criticality |
ADPE |
ESDC |
HMIC |
DEML |
A |
X |
0 |
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P |
A |
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