Delivery Inspection Checklist - Attachment 7.XLS
XLS spreadsheet 46 KB Posted
- Attached to
- AIRCRAFT LEASING Federal contract opportunity
- Solicitation number
- djms-11-jpt-r-0023
About this file
STATEMENT OF WORK - ATTACHMENT 7
View the file
Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| Statement of Work - May 2011.doc | DOC document | |
| AMENDMENT 0001 - QUESTIONS RESPONSES.doc | DOC document | |
| Attachment 3 - Leased-Charter Flight Personnel Data Sheet.pdf | ||
| Attachment 2 - GSE.doc | DOC document | |
| Attachment 8 - Subcontracting Plan Requirements.doc | DOC document | |
| Attachment 5 - Performance Measurement and Reporting.doc | DOC document | |
| Pre-Award Inspection Checklist - Attachment 6.XLS | XLS spreadsheet | |
| COMBINED SYNOPSIS - SOLICITATION.pdf | ||
| Attachment 1 - JPATS GMM-Rev2.pdf | ||
| Attachment 4 - Lease Plane Flight Log.pdf |
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Text version
DIChecklist
| Unacceptable | Acceptable | ||
| H. Aircraft Requirements Configuration | |||
| H.1. | Has the Contractor provided? | ||
| 1 | U.S. Registered Aircraft with Standard Certificate of Airworthiness | ||
| H.2. | Specific Minimum Requirements: has the Contractor provided? | ||
| 1 | Brand Name (MD-83 or 737-400) aircraft or Equal | ||
| H.3. | Has the contractor provided aircraft that: | ||
| 1 | Meet specifications of their original Type Cerificate IAW Title 14 CFR Part 25 | ||
| 2 | Are certified for day, night, VFR, IFR operations and flight into known icing conditions. | ||
| 3 | Have cockpit and cabin instrumentation, placards, labeled and readable in English language | ||
| 4 | Have documentation that each has not sustained any substantial damage NTSB Subpart A, Gnrl. 830.2 | ||
| 5 | Are equipped with an APU, supplying ground power, engine starts, grnd.cooling / heating | ||
| 6 | Are equipped with a minimum of three lavatories, configured for external servicing | ||
| 7 | Are of a narrow-body, single aisle design / configuration | ||
| 8 | Are of a standard 2 and 3 or a 3 and 3 seating configuration | ||
| 9 | Have a manufacture date no earlier than 1991 and total cycles since new not exceeding 39,000 | ||
| H.4. | |||
| 1 | General: Has the Contractor provided? | ||
| A | All documentation and manuals for operation of all aircraft flight systems | ||
| B | Aircraft equipped with emergency overwater passenger operations IAW Title 14 Part 121 | ||
| C | An approved electronic system for calculating/determining center of gravity (CG) prior to flight | ||
| that is compatible with Microsoft Windows Operating System as | |||
| installed in a Motion Computing Tablet or equivalent | |||
| D | Compliance with all published FAA Airworthiness Directives/ Mfgr. Mandatory/Alert Service Bulletins. | ||
| E | Compliance with all calendar, flight hour, and cycle maintenance inspections / events from | ||
| a manufacturer or FAA approved maintenance program | |||
| F | Aircraft with takeoff, climb and cruise performance equal to or greater than the MD-83 aircraft | ||
| G | Aircraft with operational range capability equal to or greater than the MD-83 aircraft with std. 3 tank config. | ||
| 2 | Avionic / Navigation / Auto Flight System: Has the Contractor provided? | ||
| A | A single or dual FMS with a data base containing worldwide navigation data. | ||
| In addition, the airport data base will incorporate all airports with an instrument approach procedure and a | |||
| runway greater than 5000 feet in length in the geographic area defined as the Continental | |||
| United States, Alaska, Hawaii, Canada, Latin America and South America. | |||
| B | FMS software version the same for each model aircraft with the most recent version | ||
| NOTE: Contractor will be responsible for maintaining and providing current data | |||
| C | A FMS fully integrated / interfaced with and receiving navigational data / inputs from a minimum of two | ||
| IRS, or two AHARS, as applicable, a minimum of one GPS or a minimum of two radio navigation systems. | |||
| The system must be FAA certified with performance capabilities as detailed in the SOW. | |||
| D | A Flight Guidance / Autopilot System | ||
| E | Three digital VHF tranceivers communiatons systems with a minimum of 760 channels | ||
| with 8.33 KHZ spacing | |||
| F | Two (2) digital VHF, VOR/LOC navigation receivers | ||
| G | Two (2) glide slope receivers with a minimum of 40 receive channels | ||
| H | One (1) marker beacon receiver systems | ||
| I | Two (2) digital ADF navigation systems | ||
| J | Enhanced GPWS system with low level wind shear detection and TAWS capability | ||
| K | TCAS II system incorporating revision 7 | ||
| L | Two (2) air data computers | ||
| M | Two (2) radio altimeter systems | ||
| N | One (1) digital flight data recorder | ||
| O | One (1) digital cockpit voice recorder | ||
| P | Two (2) mode S Transponders | ||
| Q | Two DME systems with NAV-1 and NAV-2 channeling | ||
| R | One (1) altitude preselect / alerter system | ||
| S | All equipment and components necessary for certification for flight operations in RVSM airspace | ||
| T | One (1) wiring system (coax) and antenna capable of supporting a cockpit mounted Aircell ST3100 | ||
| Iridium Telecommunications system | |||
| U | EFIS both pilot and copilot sides with: EADI with integrated airspeed format display and EHSI utilizing | ||
| a heading up and not track up display format | |||
| V | Digital autothrottle system | ||
| W | Standardized cockpit layout and associated navigational equipment and instrumentation | ||
| Unacceptable | Acceptable | ||
| 3 | Equipment. Has the Contractor provided? | ||
| A | Operational forward self-contained and powered airstairs | ||
| B | An operational Class C fire detection and supression system in all cargo compartments | ||
| C | Operational thrust reversers | ||
| D | Compliance with noise level requirements established in Title 14 CFR Part 36 Stage 3 | ||
| E | Single point refueling capability | ||
| 4 | Cabin Configuration / Furnishing. Has the Contractor provided? | ||
| A | A minumum of 148 forward facing, tourist class, seats installed with the maximum pitch possible | ||
| NOTE: Must meet Title 14 CFR Part 121 standard | |||
| B | A cabin with class partitions removed | ||
| C | A cabin compliant with Title 14 CFR Part 121 burn criteria | ||
| D | A reinforced flight deck door meeting the standard for a Title 14 CFR Part 121 commercial carrier | ||
| E | A cabin with all seat-back tray tables removed | ||
| F | A cabin with all ashtrays removed and appropriate blanking plate sinstalled in their place | ||
| G | A cabin with all seat backs locked n their full upright position with the exception of the first two rows | ||
| and emerency exit rows | |||
| H | Provisions for storage of JPATS ice chests and bottled water in galleys with appropriate | ||
| tie downs or reinforced web strapping | |||
| 5 | Exterior. Has the Contractor provided? | ||
| A | An aircraft with no logo trademark characteristic of a commercial air carrier | ||
| B | An aircraft with an appropriately assigned U.S. registration number applied IAW Title 14 Part 45 | ||
| Remarks: | |||
| Delivery Inspection Performed By / Date: | |||
| Maintenance: | |||
| Operations: | |||
| Contractor Representative Receipt of Inspection / Date: |
&CAttachment 7 Delivery Inspection Checklist &C
Attch 2
&CEvaluation Plan Attachment 2 Technical Evaluation (factor 62) Page &P of &N
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