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TRANSCRIPT
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YEAR: RECORDING TACH -----
TODAYS I TOTAL FLIGHT TIME IN ----···--
u e scr1puon 01 1nspect1ons, Testa, Repa· -:::~-------- -Entries must be endorsed with Name, Rating and c''•rt~,.nd Alteratio-" ~
e 1 1cate Nunu..-. ' ··•~rot
~ SERVICES, INC. l'l{0 .. 1~SSION,\L NO~-ni:STltU(1'1VE F.XAMINA'rlONs
FAA REPAlR STATION FS6R546N
MAINTENANCE RELEASE FORM ......-- -- · ·- ·• · - · ----- -------------------P(>~crt~in~c;n,;--;cl;;c;;;luiliils~o~f-;i.lh:c 7:in::sp=cc~ti~ons:--nr-c
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Natrona Avionics under: n I c 11\ th15 1t~rs1 Customer
Work Order Number l 9. 705.413 Mnkc Cessna -
Description of Component Inspected Moue\ 2\0M -I Carrv Thru Spar
Scriul Number 2\0618S2 -.,
Registration Number N210WV
The aircraft, uirframe, nircran engine, propeller, or appliance identified nbove was inspected as described below in accordo.nce wilh cum Regulations of the Federal Aviation Administration. Only those items recorded as "nccept". "nccept11b\e11 or ns "no discrepnncics" on tht inspection document(s) are approved for return to service.
Description of Inspection: Eddy Current per Cessna Service Letter SEL-57-06. ..... ~ ·----Refer to inspection report for any and all discrepancies.
2354705 8/\9/19
Repairman Number Ontc
15552 E. Fremont Dr., Unit A 106 - Centennial, CO 80112 - (303) 741-05l8
DATEI
RECORDING TACH TIME
TODAYS FllGHT
TOTAL TIME IN SERVICE
'¾HS
De~cription of Inspections, Tests, Repairs and Alterations Entnes must be endorsed with Name, Rating and Certificate Number ot Technician or Repair Facility. (See back pages for other specific entries.)
}iAT E 10/25/2019 N210WV TACH: 581.2 TTAF: 3629.5 · ,. , _ _. ALLY INSPECTED CARRY THROUGH SPAR AREA PRIOR TO OWNER REINSTALLING H!:ADLINER. NO CORROSION FOUND ON SPAR OR ANY OTHER METAL IN THE AREA. OWNER PREVIOUSLY HAD SPAR EDDY CURRENT INSPECTED WITH ALL INDICATIONS GOOD. SEE PREVIOUS LOG ENTRY FOR DETAILS. ALL PULLEYS AND CABLES ABOVE HEADLINER LOOK -GOOD. REPLACE PILOT SIDE SCAT TUBING TO VENTS .. ............. .... ......... ... .. ....... END.
BRUCE MCWHORTER A&P 3690658
Bighorn Airways, Inc Date: 2/05/2020; Aircraft: N210WV; Type: C210; S/N: 21061852; Hobbs:; Tach: 588.60; Total Time: Shop Order#: RS20-0015 1 Alternator does not work. Found alternator capacitor wire grounding out to case. Repaired wire. System op-checks good. REF Cessna 21 o MM Chapter 17.
This aircraft,airframe,engine,propeller and/or appliance identified above was repaired and/or inspected in accordance with current regulations of the FAA and ir respect to the work performed is approved for return to service IAW FAR 43.9 & FAR 43.11,as applicable. Reference above listed Bighorn Airways shop order for details of work performed
~ Bighorn Airways.Inc CRS# BIGR467C
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Autopilots Cehttal, Inc~ FAA Certified RS #CM2R747K
SCALE CORRECTIONS Altimeter Add Algebraically
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I 1 Approving Civil Aviation
I Authority/Country:
2. AUTHORIZED RELEASE CERTIFICATE
3. Form Tracking Number
AV2&-~3~3 I FANUNITED STATES FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG
' -t: Organization Name and Address: AUTOPILOTS CENTRAL, INC. 5. Wor1( Order/ContracVlnvoice
FM CRS #CM2R747K
f o Item· 7. Oescri tion: HANGAR 23 TULSA INT'L AIRPORT• TULSA, OKLAHOMA 74115 Number: Same #3
8. Part Number: 9. Quanti 10. Serial Number: 11 . Status/Work:
c~ ro ·12. Remarks:
Reference attached service shop report for work performed. C-53e>A 13a. Certifies the items identified above were manufactured in conformity to: 14a.18114 CFR 43.9 Return to Service D Other regulation specified in Block 12
O Approved design data and are in condition tor safe operation.
O Non-approved design data specified in Block 12.
13b. Authorized Signature: 13c. ApprovaVAuthorization No.:
13d. Name (Typed or Printed): 13e. Date (dd/mmm/yyyy):
Certifies that unless otherwise specified in Block 12, the work identified in Block 11 and described in Block 12 was accomplished in accordance with
Title 14, Code of Federal Regulations, part 43 and in respect to that work,
the items are approved for return to service.
14c. ApprovaVCertificate No.:
CM2R747K 14e. Date (dd/mmm/yyyy):
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 in Block 1, it is essential that the user/installer ensures that his/her airworthiness authority accepts aircraft engine(s)/propeller(s)/article(s)
from the airworthiness authority of the country specified in Block 1.
Statements in Blocks 13a and 14a do not constitute installation certification. In all cases, aircraft maintenance records must contain an instaHation certification
issued in accordance with the national regulations by the user/installer before the aircraft may be flown.
FAA Form 8130-3 (02-14) NSN: 0052-00-012-9005
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-----1 ___ --1. _ _ __j_ ___ __j_ ___ ______________ _____ _
Bighorn Airways, Inc . ft· Nz1owv- Type: C210; SIN: 21061852; Hobbs:; Tach: 600.00; Total Time· 3648.30
. 3/13/2020; A1rcra . , oate #· RS20-0028 . . . . . . . ShOP Or~er · AD 2020.03-16 (effective 3/9/2020) by perforrmng v1~ual inspection of carry-thru spar with a 10X magnification lens for corrosion, cracks and 1. complied wr~D 2020_03_ 10 para. (g). No discrepancies found. Venfi~ eddy current inspection of Carry-Thru Spar was complied with IAW AD 2020-03-16 damage as~~ (2) by compliance with Cessna SEL-57-06 by NOE Services W.0 . 19-706-413 on 8/19/2019, no discrepancies found. Applied corrosion para. (h~:~tings IAW AD2020-03-_16 para. (i) a~d Cessna SEL-57-08R1 steps 9_and 1 O. . . . protectiify that this aircraft's pitoVstatic system, altimeter, ATC Transponder and altitude reporting system has been inspected and tested to 30000 feet m 2. Ice: ce with FAR Part 43 Appendix E&F and found to comply with FAR Part 91 .411 ,91 .413, and 91 .227. ac~r a~ed GTX 345R transponder encoder to primary static system IAW GARMIN STC# SA01714WI. Leak checks good. ;: R~:oved overhead interior. Overhead interior left down per owner's request.
This aircraft.airframe,engine,propeller and/or appliance identified above was repaired and/or inspected in accordance with current regulations of the FAA and in respect to the work performed is approved for return to service IAW FAR 43.9 & FAR 43.11 ,as applicable.
Reference above listed Bighorn Airways shop order for details of work performed
Bighorn Airways.Inc CRS# BIGR467C
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JJ- BlgHom Airway• N# 210WV 912 W. Brundego Lano Serini# 21061852
___________ Sheridan WY 82801 --~lrfra_m.!!-~ [ ntr1 __ _ _ Datt: 6'1112020 ______ Tech: 818.1 ACTT: 3414.A
'" l 1'~ \ ( 1ff Anhme ~ coble with RG 400. Referunood AC 43 13-21:3 ch 3 Pora, 311 Rofur~ od Garrflin (JH-J/ tY., IM 11;)vf{1.ll f. :-, "-<111 •i Oat'ed DGcoolber 31, 2019 and Garmin GNS 430W IM 190-003!J6-02 Rev M Oated June 30, 201/ . All OfJ1J gwJ TNs attra, ~irtrlme,eogine,propoller and/or appliance identified abovo was repaired a11d/or inspoctad In acr..ordarice w,th c;.meflf ,~,. ~,
the FAA and in respect to the work performed Is approved for return to service IAW FAR 43,9 & FAR 43.11.~ ~ ~ Reference Bighorn Airways Work Order 200109 for d~tails of work performE,d
~ -< - Bighorn Airways ---·--- ~ · ---- - CRSBtGR46ic
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(!) 912 W. Brundage Lane Serial# 21061852 9
.r . ~- Sheridan WY 82801 Airframe Log Entry
[ oate! /20/2020 Tach: 638.2 ACrr· 3676 5
__ , 1 lnstailaj test~ TKS con~rol panel. System op-<:h~ks 9~-~IN off/on: CT464, SIN off/on: AST08A1035. REF STC SA00631
w1_ • - ·- -
This aircraft, airframe ,engine, propeller and/or appliance identified above was repaired and/or inspected in acco d 'th .
the FAA and in respect to the wori< performed is approved for return to s; rvice IAW FAR 43.9 & FA~4a3n~ w, cu,~enbt re<Julations of
f . h A' W . ,,as app ica le >-""'.l~- e erence 19 orn 1rways ork Order 200149 for details of work performed
Bighorn Airways 1 1
CRSBIGR467C
i1 BigHorn Airways 912 W. Brundage Lane
Sheridan WY 82801
N# 210WV Serial# 21061852
Airframe Log Entry _ __,[ Date: 7/20/2020 Tach: 638.4 ACTT: 3686.7
1. Adjusted Rh landing gear down and locked switch. Replaced landing gear down and locked light IAW Cessna 210 service manual sections and
Cessna WDM DWG #1270709 Operational checks good.
2. Replaced NAV light switch with new switch. IAW C210 service manual p.17-5. Operational check good
Th,s aircraft, airframe ,engine, propeller and/or appliance identified above was repaired and/or inspected in accordance with current regulations of
the FAA and in respect to the wori< performed is approv€'d for return to servi~ lAW FAR 43 9 & FAR 43 11,as applicable
~~ce Bighorn Airways Work Order 200159 for details of work performed.
?Justineion Bighorn Airways CRSBIGR467C
[oate: 6/10/2020 Tach: 614.8 ACTT: 3663.1
-- 1 Inspected VOR diplexor, splitter, antenna and cablining. No defects found. Tested GTN-750 and GNS-430 VOR. Took RF sign~I down to -
47 dbm on test set, both units passed VOR test Found VOR Identifier audio weak dnd unrPadable on GTN-750. Reseated Audio panel
-- correctly audio sounds good. Referenced Garmin GTN-750 STC IM 190-01007-A3 Rev '14 dated December 31, 2019.
I certify that this aircraft is in an airwo,thy condition and all of the noted discrepancies have been corrected or deferrel1
-- ,.,. r_r, Reference Bighorn Airways Work Order 200103 for details of work performed
•----~Justin Olson Bighorn Airways CRSBiGR467C
YEAR:
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TODAYS FLIGHT
TOTAL TIME IN SERVICE
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