What it approves
Installation of ESL special mission configuration. (DHC-7-103 S/N 104, DHC-7-102 S/N 048)
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
Number SA1049NE This certificate issued to Sierra Nevada Corporation/Integrated Mission Systems.
18635 Jarkey Drive Hagerstown, MD 21742
Part 25 of the Federal Aviation Regulations.
Original Product -- Type Certificate Number : A20EA Make : DeHavilland
Model : DHC-7-102, s/n 048 DHC-7-103, s/n 104
Installation of ESL Special Mission Configuration in accordance with the following Field Aviation Co. Inc. Drawing Lists at the issue levels indicated:
a) FACi Drawing List 33666, Issue 1, dated September 28, 1992 (Survey/Navigation System Installation).
b) FACi Drawing List 33664, Issue 1, dated October 1, 1992 (Antenna Matrix System Installation).
c) FACi Drawing List 33662, Issue 2, dated June 19, 1993 (MTOW Increase Structural Provisions).
d) FACi Drawing List 33665, Issue 2, dated March 20, 1993 (Cabin Interior Mission Equipment Installation).
e) FACi Drawing List 33669, Issue 1, dated October 1, 1992 (Cabin Interior Liner Installation).
1. The life limited items and inspection requirements are as specified in Chapter 5 of FACi Maintenance Manual Supplement, p/n FACi-6700-110 (ESL Special Mission Equipment).
Date of application : November 14, 1991
Date of issuance : February 11, 1993 Date reissued : September 28, 1993, April 16, 2003 April 23, 2004, May 5, 2006
Date amended : April 2, 1993, August 27, 1993
( Signature) Anthony Socias Manager New York Aircraft Certification Office
(Title)
FAA Form 8110-2-1(10-69) Page 2 of 2
Number SA1049NE Date of Reissuance: May 5, 2006
2. Aircraft Weight Limits:
Maximum Ramp Weight: 47100 lbs.
Maximum Take Off Weight: 47000 lbs.
Maximum Landing Weight:
Flaps 25º : 45000 lbs.
Flaps 45º: 42000 lbs.
Maximum Zero Fuel Weight: 39000 lbs.
3. Aircraft Center of Gravity Limits:
Forward Limit:
Up to 42000 lbs: 25% M.A.C.
From 42000 lbs. to 47000 lbs: Varies linearly from:
25% to 30% M.A.C.
From 47000 lbs. to 47100 lbs: 30% M.A.C.
Aft Limit:
At all weights: 40% M.A.C.
4. Maximum Passenger Capacity:
Essential Crew Only – No Passengers.
Maximum Number of Occupants:
Pilot, co-pilot and 9 additional persons as limited by approved seating configuration.
5. For additional limitations and conditions on S/N 048, see Supplemental Type Certificate Number SA1045NE, Cargo Door Installation.
6. The following documents, at the revision status indicated, are required with this modification:
a) Field Aviation Co. Inc. Flight Manual Supplement, p/n FACi-6700-109 (Survey Navigation System, Cabin Interior Mission Equipment and Antenna Matrix System Installation), Rev. 8, DOT approved June 30, 1993.
b) Field Aviation Co. Inc. Flight Manual Supplement, p/n FACi-6700-125 (Delco Carousel IV-E INS and GPS System Installation), Rev. 2, DOT approved January 29, 1993.
c) Field Aviation Co. Inc. Flight Manual Supplement, p/n FACi-6700-119 (M.T.O.W. Increase Modification), Rev. 2, DOT approved June 30, 1993.
d) Field Aviation Co. Inc. Flight Manual Supplement, p/n FACi-6700-110 (ESL Special Mission Equipment), Rev. 3, DOT approved June 30, 1993.
7. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written permission of that permission.
8. Compatibility of this design change with previously approved modifications must be determined by the installer.
…END…
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