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COMPONENT HISTORY FORMPART NAME
Blade Assy, M/R
MANUFACTURER
Bell
PART NUMBER SERIAL NUMBER
205-015-150-101 A-FS340
RETIREMENT LIFE
10,000 Mrs
OVERHAUL LIFE
N/A
NOTES
Ref. Form 2408-16
INSTALLATION REMOVALDATE N#OR
LOCATION
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INSTALLATI
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DATE
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REMOVAL
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MODIFICATION MANDATORY SERVICE BULLETIN
DATE MOD.# SIGNATURE & LICENSE DATE S/B NUMBER SIGNATURE & LICENSE
OVERHAULS - REPAIRS -ADJUSTMENTS - REPLACEMENTS
DATE TSN SIGNATURE & LICENSE
fY3./ rr
"form 1200 Rotorcraft Inc.KQTR784F
Box 453 (Hwy 63 & 117)Black Rock, AR 72415
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Work Order_i22— N 9 ̂ ^1614
Date Received ^ Date Released
Customer Name /// ̂ ^ S— ^ ^Address ^7&///^oJi f' PoaA f /7IY—nS
S IolJcSPart name
Part No. ^ OS- n/-3--/S£>-/O/
Serial Number A-S^3VO 4 A-J^S.399 ^Special Instructions a/^ Ae/^n hs /7 J>CL ia /7 ce
Work Accqmpjished
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FORM 1200
306it. o
3003.0 37"
Rotorcraft Inc.KQTR784F
Box 453 (Hwy 63 & 117)Black Rock, AR 72415
Work Order _ /3 N9^7-2007
Date Received
Customer Name
'-/3
///in Of 3 /~ X/7CDate Released
Address o^/^^d-, ^ ̂ ^ ̂ /Part name. XePart No. 2as~e>/3~/3o-Jol
Serial Number
Special Instructions (J
Work Accomplished, jFJpi 4L ^/^/]-/4sr)A^9'99 7Ai/^ns^/0 aL MA FUd, . /^o'A/ynfn^A
4/7 f9' 04. -/w.^ f/Tm
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1. Approving National AviationAuthority/Country:
FAA/UNITED STATES
2.
AUTHORIZED RELEASE CERTIFICATEFAA Form 8130-3. AIRWORTHINFXS APPROVAL TAG
3. Form Tracking Number:
07-94-1614
4. Organization Name and Address:
RotorCraft Inc.
Box 453 (Hwy 63 & 117)Black Rock, AR 72415
5. Work Order/Contract/Invoice
Number:
07-94-1614
6. Item: 7. Description: 8. Part Number: 9. Eligibility: * 10. Quantity: 11. Serial/Batch Number: 12. Status/Work:
1 Main Rotor Blade 205-015-150-101 Bell UH-1 series 1 A-FS 340 Inspected/Repaired
13. Remarks:
Work Order # 07-94-1614 prescribing the actuai work performed is attached.
The prescribed work was performed in accordance with FAA approved data.
14. Certifies the items identified above were manufactured in conformity to:
[m Approved design data and are in condition for safe operation.
CH Non-approved design data specified in Block 13.
19. ^ 14 CFR 43.9 Return to Service LJ Other regulation specified in Block 13
Certifies that unless otherwise specified in block 13, the work identified in Block 12and described in Block 13 was accomplished in accordance with Title 14, Code ofFederal Regulations, part 43 and in respect to that work, the items are approved forreturn to service.
15. Authorized Signature: 16. Approval/Authorization No.: 20. Authoriz^^ignature|^^^^^_^^^^^^^ 21. Approval/Certificate No.:
KQTR784F
17. Name (Typed or Printed): 18. Date: 22. Naine'^(Typed or Printed):Jail's F. Propst
23. Date (m/d/y):1-16-08
User/Installer ResoonsibilitiesIt is important to understand that the existence of this document alone does not automatically constitute authority to install the part/component/assembly.
Where the user/installer performs work in accordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country specified
Bl^kl'' ®s'®ntial that the user/installer ensures that his/her airworthiness accepts parts/components/assemblies from the airworthiness authority of the countiy specified inStatements in Blocks 14 and 19 do not constitute installation certification. In all cases, aircraft maintenance records must contain an installation certification issued in accordance withthe .national regulations by the user/installer before the aircraft may be flown.
FAA Form 8130-3 (6-01) *Installer must cross-check eligibility with applicable technical data. NSN: 0052-00-012-9005
I. Approving Civil AviationAuthority/Country:
FAA/United States AUTHORIZED RELEASE CERTIFICATEFAA Form 8130-3, AIRWORTHINESS APPROVAL TAG
3. Form Tracking Number:
13-37-2007
4. Organization Name and Address:
Rotorcraft Inc. Box 453 Black Rock, AR 72415
5. Work Ordcr/Contract/Invoice
Number:
13-37-2007
6. Item: 7. Description: 8. Part Number: 9. Quantity: 10. Serial Number: 11. StatusAVork:
1 Main Rotor Blade 205-015-150-101 1 A-FS 340 Inspected/Repaired
12. Remarks:
A general description of the work performed is attached as form 1200; Under the part description listed in blocks 6,7,8,10 and 11 as applicable.
A complete description of work performed is on file at the above referenced organization under the work order and system tracking reference numberindicated in blocks 3 and 5.
NOTICE: An Airworthiness Directive may apply to the article(s) described hereon. The installer is responsible for ensuring complete compliance with any
applicable Airworthiness Directives..
Part Total Time (As supplied by owner) 3082.0 Hrs
13a. Certifies the items identified above were manufactured in conformity to:
II] Approved design data and are in a condition for safe operation.Q Non-approved design data specified in Block 12.
14a. iZI 14 CFR 43.9 Return to Service Q Other regulation specified in Block 12
Certifies that unless otherwise specified in Block 12, the work identified in Block 11and described in Block 12 was accomplished in accordance with Title 14, Code ofFederal Regulations, part 43 and in respect to that work, the items are approved forreturn to service.
13h. Authorized Signature: 13c. ApprovaFAuthorization No.: 14b. Authopz^ Signature: 14e. Approval/Certificate No.:
KQTR784F
13d. Name (Typed or Printed): 13e. Date (dd/mmm/yyyy): Ijt^Name (Typed or Printra):
James F. Propst
]4e. Date (dd/mmm/yyyy):
10-04-2014
User/Installer Responsibilities
It is important to understand that the existence of this document alone does not automatically constitute authority to install the aircraft engine/propeller/article.
Where the user/installer performs work in accordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country specified inBlock 1, it is essential that the user/installer ensures that his/her airworthiness authority accepts aircraft engiue(s)/propeller(s)/article(s) from the airworthiness authority of the countryspecified in Block 1.
Statements in Blocks 13a and 14a do not constitute installation certification. In all cases, aircraft maintenance records must contain an installation certification issued in accordance with thenational regulations by the user/installer before the aircraft may he flown.
FAA Form 8130-3 (02-14) NSN: 0052-00-012-9005
o\
SERVICEABLE
MAINTENANCE RELEASE
THE AIRCRAFT AND/OR COMPONENT
IDENTIFIED ON REVERSE SIDE WAS
REPAIRED AND INSPECTED IN ACCORDANCE
WITH CURRENT REGULATIONS OF THE
FEDERAL AVIATION ADMINISTRATION AND IS
APPROVED FOR RETURN TO SERVICE.
PERTINENT DETAILS OF THE REPAIRS ARE
ON FILE AT THIS REPAIR STATION UNDER
Work Order No. QT-Q^-I ft l U
Dated 12-3-07
Inspected By James F. Propst
Remarks Inspected/Repaired
spx per Work Order.
ROTORCRAFT INC.Box 453 (Hwy 63 & 117)
BLACK ROCK, AR 72415
KQTR784F
SERVICEABLE
OManufacturer Bell Helicopter
Part Name Main Rotor Blade
Part No 205-015-150-101 , Serial No. A-FS 340
Owner Billings Flying Service, Inc.
Total Time
Inspector
943.1 TSO 943.1
Date 1—16—08
Additional Remarks On Reverse Side
oSERVICEABLE
MAINTENANCE RELEASE
THE AIRCRAFT AND/OR COMPONENTIDENTIFIED ON REVERSE SIDE WAS
REPAIRED AND INSPECTED IN ACCORDANCE
WITH CURRENT REGULATIONS OF THE
FEDERAL AVIATION ADMINISTRATION AND ISAPPROVED FOR RETURN TO SERVICE.PERTINENT DETAILS OF THE REPAIRS AREON FILE AT THIS REPAIR STATION UNDER
Work Order No. 1 3-37-7.007
Dated S-8-13
Inspected By —Jsmes F.—Propst
Remarks I^ispected/Repaired
per 'fAjork order.
ROTORCRAFT INC.BOX 453 (HWY 63 & 117)BLACK ROCK, AR 72415
KQTR784F
SERVICEABLE
Manufacturer ^ell Fgligppter
oPart Name Wain •Rn-Hnr- -nl aHo
Part Mffg05-01 5-1 50-1 01 Serial No.. A-FS 340
Owner Billings Flying Service, Inc.
Total Time =— —ISO.
Inspectoc
.0^
Pete 4 ~ ̂ 0-1 4
Additional Remarks On Reverse Side