Quality Control Inspector
Resume:
Carlos Vasquez
Miami, FL *****
ad5dt2@r.postjobfree.com
Authorized to work in the US for any employer
Work Experience
QC Inspector
Owl Aerospace - Hollywood, FL
August 2017 to Present
QUALITY CONTROL INSPECTOR.
AOG Shipping, Receiving, Invoicing, Packing List, FedEx, UPS, DHL, AA Online AWB.
• Hazmat Declaration.
• Harmonized System Tariff Classification (HS code)
• Electronic Export Information (EEI)
• Employer Identification Number (EIN)
• Export Administration Regulations (EAR)
• Export Control Classification Numbers (ECCN)
• Harmonized Code
• Incoterms
• International Air Waybill
• International Traffic in Arms Regulations (ITAR)
• Schedule B Code
• Shipper's Export Declaration (SED)
• Military Aircraft’s
• F-16
• C-130
• Helicopters MD-500
• Arava IAI Aircraft
• Commercial Aircraft’s
• Boeing
• Airbus
• Embraer
• Foreign Government Aircraft
• Beechcraft, Cessna by Textron Aviation
As Receiving Inspector I am responsible to the Director of Quality for the efficient determination of Airworthiness of all Aircraft Parts and Materials Received by the Repair Station; In addition the Receiving Inspector is Responsible for: The physical condition of the parts and Materials at the time of Reception By the Repair Inspection.
Ensure the completed and correct documentation accompany all the Parts and Materials. Ensure The Airworthines Condition and Proper traceability. QC Inspector
Lan Airlines - Miami, FL
May 2001 to May 2012
• QUALITY CONTROL INSPECTOR
• AOG SERVICE 24 Hours
• B-777, B-767 B-737, B-727 A-340, A-319, A-320, DC-8.
• Well versed in Engines Pre-Inspection.
As Quality Control Inspector I am responsible to the Director of Quality for the efficient determination of Airworthiness of all Aircraft Parts and Materials Received by the Repair Station; In addition the Receiving Inspector is Responsible for: The physical condition of the parts and Materials at the time of Reception By the Repair Inspection.
Ensure the completed and correct documentation accompany all the Parts and Materials. Ensure The Airworthines Condition and Proper traceability. 1. Ensure that Airworthy SUP and defective parts are properly identified and placed in a specific segregated place.
2. The receiving inspection process is intended to certify that all aeronautical parts and materials intended for use in maintaining aircraft meets the requirements of traceability and certification. The aim is to establish sufficient traceability to establish that the part(s) were manufactured under Title 14 of the Code of Federal Regulations (14 CFR) part 21, were previously determined to be airworthy under 14 CFR part 43, produced to established industry or U.S. Government standards or accepted foreign standards. 3. For this a physical inspection and document review for all parts and materials received will be done and recorded in the appropriate documentation and/or the “Operators” control system. This is to ensure that the parts or material are eligible to be installed on any of the associated aircraft. NOTE: This does not relieve the responsibility of the Maintenance Organization in regards to the airworthiness requirements of the parts and/or materials of the local Airworthiness Authority for each aircraft registration
4 -All incoming product will be inspected by the Receiving Inspector prior to its storage and/or availability for use by maintenance personnel using the following procedure: A-Obvious damage. If damage is found the part or material will be rejected, this will be indicated as such in the system and the part will be placed in the Quarantine designated area. a) Examine the part for installed plugs and caps on port openings and electrical connections, corrosion, discoloration of material, loose or missing rivets, bent rods or controls, correct placement of safeties, nicks,
scratches, dents presence and security of any required data plate or evidence of mishandling b) Any part placed in Quarantine must remain isolated until either the discrepancy is resolved or the part is
properly returned to the manufacturer or vender.
a. Parts in Quarantine maybe temporarily accessed for information or required actions; however unless final disposition and action is taken, the part must be returned to the quarantine area once the required action has been satisfied. This must be prior to the completion of the current tour of duty. b. Parts removed from Quarantine must be documented in the turnover log with the reason for removal and time the part was returned to Quarantine.
1. Physically check the quantities, part number, serial number, and other product markings or identifications are correct and consistent with the documentation of the outsource organization. a) Shipments of bolts, nuts, rivets or other standard hardware received in quantities will be checked to ensure
manufacturer’s certification is included, as applicable 1. Check Documentation, Purchase Orders, Work Orders, Teardown Reports, Certification Documents, etc., applicable to the products, but not limited to as follows: 2. a) FAA Form 8130-3, Airworthiness Approval Tag, JAA Form 1 (prior to 11/28/04), EASA Form 1 (after 11/28/04), or Transport Canada Form 24-0078.
b) Shop Report or Teardown report of work accomplished during the shop visit. 1. Verify compliance with applicable AD’s by comparing the certification Documents with the Company Approved program, and/or the Purchase Order sent by The Company to vendors. 2. If the 8130 or Teardown report indicates an AD was accomplish to the part, but the PO or the System doesn’t show the request for this AD, Quarantine the part and contact the Purchasing Department. 3. If the PO or System request a task for AD Compliance but Part documentation doesn’t have the compliance, Quarantine the part and contact Purchasing Department. COMMERCIAL TRACEABILITY
1. AS RECEIVING INSPECTOR must verify that documents such as PO’s, invoices, packing list and/or ATA 106 forms should have the material traceable from the current purchase to approved source of manufacturing or last major repair (overhaul), from all associated vendors. AIRWORTHINESS TRACEABILITY (performed by RECEIVING INSPECTOR 4-Items that require certification form 8130-3:
a.
The part coming from the manufacturers or external repair facilities must have the original certificates or certified copies.
b.
Verify under what standard the certificate was issued. You can accept the following equivalents, depending on whether the part will be stored in inventory or for installation on a specific aircraft registration (if do not know the destination of the party, use the criteria used for storage): c.
If the 8130-3 (or equivalent) form indicates the compliance with an AD (Airworthiness Directive), notify the Airworthiness Management by SYSAID to complete the corresponding control tasks. The component will be quarantined until an answer is received. In cases of an AOG during non-business hours, you may request Support from Production Engineering.
d.
Verify that the facility is approved to issue the certificate. If you have doubts, you can go to the following websites:
1. http: //AVInfo.faa.gov/repairstation.asp or
2. http://www.aviationsuppliers.org/.
3. Certificates issued by 121 operators are not acceptable. e- If the 8130-3 (or equivalent) form is marked with the acronym "PMA", you must check in the Operators Control System (Part-Details) that the box "PMA Part" is activated. f.
You may accept Forms marked "PROTOTYPE" only if they have been previously validated by the Operators Projects Engineering.
g.
For repaired/ tested components with Hard-Time controls, you should obtain the traceability back to new or overhauled condition, as applicable, or have the information tracing to “New” or “Last Overhaul” written on the 8130-3. Verify the information in the Operators Control System. 5-Items that require the issuance of a Certificate of Conformance (C of C) - Also performed by the RECEIVING INSPECTOR:
Note: Form 8130-3 or equivalent is also an acceptable means to establish the conformance of a part, component, or material.
a. The ATA Form 106 is acceptable as a Certificate of Conformance, only if issued by the material manufacturer.
b. The certificate of conformance must indicate a statement which identifies the Acceptable Data under which the product has been certified (i.e. standard, drawing) c. If the documentation indicates a batch/lot number, it must match the physical number on the component, either by printing, engraved or painted. Additionally you must have a tag attached to component/part or attached to the packaging.
d. The amount of material or parts received cannot exceed the quantity indicated on the C of C. 1. Materials repaired/tested/overhauled/calibrated (not new), their certificates must indicate or come with:
a. Work Order (work order).
b. Workshop Teardown Report, with the details of the work performed. c. The work accomplished "without observations" in accordance with the technical data (or equivalent wording).
1. The raw materials which require flammability testing must come with an attached copy of flammability test for the associated batch being received; indicating compliance with FAA/EC 25.853 requirements. 2. The following materials which require compliance with a TSO must have the compliance standard printed legibly on the label, data plate, or physically on the material: Seats / TSO-C39 (9g) or TSO-127 (16g) Belts / TSO-C22 Floating cushion / TSO-C72c
Lifejackets / TSO-C13
Life raft / TSO-C12 Slide / TSO-C69
Trolleys / TSO-C175
1. You must ensure that materials’ requiring mechanical and/or chemical testing indicates the reference values of the results. In addition they must be found within the acceptable ranges. 1. Verify that the kits have a list that itemizes in detail all of the composing sub-elements. QC Inspector
Education
Associate in Aviation
AeroAndes
January 1987 to June 1989
Some college
Skills
• Quality Control
• Quality Inspector
• Inspection
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