NLG Overhaul.pdf
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- Solicitation number
- 15M30026RA3700011
About this file
This is an FAA Form 8130-3, Airworthiness Approval Tag, issued by Summit Aerospace in Miami, Florida, certifying the overhaul and release to service of a Boeing 737 nose landing gear assembly (Part Number 65-73762-21, Serial Number T2200P1540). The work order number is 55033827, and the FAA Certificate of Release from Service (CRS) number is E6QR207X, dated August 3, 2018. The overhaul was performed in accordance with EASA Part 145 Approval No. EASA.145.5462 and complies with Title 14 CFR Part 43 for return to service authorization.
The documentation includes comprehensive historical life-limited component data for all subassemblies within the nose gear assembly, tracking part numbers, serial numbers, cycle service hours (CSO and CSN), life limits, remaining cycles, and previous operators including Canadian North and WebJet. Service bulletins AD 2000-08-17 and AD 2003-07-12 were embodied during the overhaul, including mandatory installation of updated light assembly components per SB 737-33-1129 and incorporation of SB 737-32-1322. The certification by authorized personnel (Luis Mazuelos) confirms the component is in condition for safe operation and ready for installation, though end users must obtain their own installation certification per national regulations before aircraft operation.
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1. Approving Civil Aviation 2. AUTHORIZED RELEASE CERTIFICATE 3. Form Tracking Number:
Authority/Country:
FAA/UNITED STATES FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG 26630
4. Organization Name and Address: 5. Work Order/Contract/Invoice Number
SUMMIT AEROSPACE 1260 NW 57 AVE MIAMI, FL 33126 Phone:305/267-6400 (E6QR207X) 55033827 / PENDING
6. Item: 7. Description: 8. Part Number: 9. Quantity: 10. Serial Number: 11. Status/Work:
1 NOSE GEAR ASSY 65-73762-21 1 T2200P1540 OVERHAULED
i2. Remarks: Manual#: 737-322148 RevDate: Jul 1,2018 Rev#: 90 ManufBOEING ATA: 32-21-48 Overhauled in accordance with the data identified herein.
Details of the work performed are on file.
CSN:36,667 CS0:-0- LAST OPERATOR:CANADIAN NORTH
Certifies that the work specified in block 11/12 was carried out in accordance with EASA Part 145 and in respect to that work the component is considered ready for release to service under EASA Part 145 Approval no. EASA.145.5462
13a. Certifies the items identified above were manufactured in conformity to: I 4a. lK] 14 CFR 43.9 Return to Service 1K] Other regulation specified in Block 12
D _Approved design data _and are in condition f~r safe operation. Certifies that unless otherwise specified in Block 12, the work identified in Block
D Non-approved design data specified in Block 12. 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.
13b. Authorized Signature: 13c. Appro~al/Authorization No.: ~--n 14c. Approval/Certificate No.: .
E6QR207X - ..
J 3e. Date ( dd/mmm/yyyy):
C 13d. Name (Typed or Printed) l,J4c( i.<t::..:.-. ,., .. .ffyped or Printed) 14e. Date (dd/mmm/yyyy):
LUIS MAZUELOS 03/Aug/2018 •. P " . -· J.
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 pe,rforms work in accordance with the national regulations of an Airworthiness Authority different than the Airworthiness Authority of the country specified in block l, it is essential that the user/installer ensures that his/her Airworthiness Authority accepts aircraft engine(s)/propeller(sYarticle(s) from the Airworthiness Authority of the country specified in block l.
Statements in block 13a and 14a do not constitute installation cenification. In all cases aircraft maintenance records must contain an installation certification issued in accordance with national regulations by the user/installer before the aircraft may be flown.
FAA Form 8130-3 (02-14) NSN: 0052-00-012-900S su, M~
SETTING A NEW STANDARD FOR SUPPORT
DESCRIPTION: NOSE GEAR ASSEMBLY
PART NUMBER: 65•73762•21
SERIAL NUMBER: T2200P1540
Off Log
Part Number Serial Number cso CSN
85C25876-2 CPT0194ETN 8,736 36,667
65-46210-28 CPT0581BAC 8,736 36,667
85-46210-38 CPI0017 8,736 36,667
65-48215-22 ETM4656 8,736 36,667
65-46219-1 96-179242 8,736 36,662
65-48226-9 96-173242-1A 8,736 36,662
65C25707-1 96-79242 8,736 36,662
65-46221-4 96-179242 8,736 36,662
69-36622-3 MAE796JNN 8,736 16,289
65-46288-13 YK817 9,137 42,593
65-46288- ZB426 9,137 39,111
65-46203-26 PT1777 9,137 35,621
69-61383-4 WBK1791 8.736 13,840
69-61383-4 WBK1892 8,736 13,840
69-72696-4 96-179242-1 8,736 36,662
69-72696-4 96-179242-2 8,736 36,662
BACB30LM10CD52 96-179242 8,736 24,632
65-46230-13 E547 8,736 33,096
65-80051-18 S17010 8,736 36,662
69-35391-2 AV00109 3,168 3,168
69-35394-4 Sl5280 557 557
69-35394-4 Sl8562 557 557
69-35396-2 PFG 6,736 36,662
65-46240-11 YW826 5,648 40,221
65-46242-11 YF076 8,736 44,313
69-35385-2 ZC304 8,736 23,575
69-53297-2 011-870 8,736 6,736
69-35398-2 810 8,736 26,652
69-41248-2 426 8,736 26,652
® :1
QUALITY CONTROL:, _____ _
SUM-QC-LLP-F02 REV 1 NOV. 17, 2016
Life Limit
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
75,000
HISTORICAL LIFE LIMITED COMPONENTS
MODEL: 737
Remaining Part Description Part Number Serial Number
Cycles
38.333 OUTER CYLINDER 65C25676-2 CPT0194ETM
38,333 STEERING PLATE - UPPER 65-46210-28 CPT0561BAC
38,333 STEERING PLATE T LOWER 65-46210-38 CPI0017
36,333 INNER CYLINDER 65-46215-22 ETM4658
36,338 METERING PIN 85-46219-2 96-179242
36,338 SUPPORT TUBE 65-46226-11 96-173242-1A
36,338 ORIFICE SUPPORT STEM 65C25707-1 96-79242
36,336 GLAND NUT ASSY 65-46221-4 96-179242
56,711 ORIFICE PLATE- UPPER 69-36622-3 MAE796JNN
32,407 TORSION LINK - UPPER 65-46288-13 CPT0923-SNM
35,889 TORSION LINK - LOWER 65-46288-13 CPT1583-SNM
39,179 STEERING COLLAR 65-46203-24 CPT1777ETM
61 ,160 BOLT - STEERING COLLAR 69-61383-4 95-179109-1
61 ,160 BOLT - STEERING COLLAR 69-61383-4 BFGM3712
38,338 TORSION LINK PIN 69-72696-4 96-179242-1
38,338 TORSION LINK PIN 69-72698-4 96-179242-2
50,368 TORSION LINK APEX SOLT BACB30LM1 OCD52 96-179242
41,904 LOWER DRAG BRACE 65-46230-13 E547
38,338 UPPER DRAG BRACE 65-80051-18 S17010
71,832 PIN • DRAG BRACE CENTER 69-35391-2 AV00109
74,443 PIN- UPPER DRAG BRACE 69-35394-4 YU753
74,443 PIN- UPPER DRAG BRACE 69-35394-4 DL127
38,338 BOLT • LOWER DRAG BRACE 69-35396-2 PFG
34,779 LOCK BRACE 65-46240-11 YW826
30,687 LOCK LINK 65-46242-11 YF076
51,425 SHAFT • AFTER LOCK MECH. 69-35385-1 ZC304
66,264 SHAFT (LOCK LINK) 69-53297-2 011-870
48,348 TRUNNION PIN - LH 69-35398-2 610
48,348 TRUNNION PIN • RH 69-41248-2 Sl205
On Log
CSN Life Umit
36,667 75,000
36,667 75,000
36,667 75,000
36,667 75,000
36,662 75,000
36,662 75,000
36,662 75,000
36,662 75,000
18,289 75,000
42,869 75,000
26,075 75,000
35,821 75,000
51,159 75,000
54,991 75,000
36,662 75,000
36,662 75,000
24,632 75,000
33,096 75,000
36,662 75,000
3,168 75,000
44,606 75,000
37,596 75,000
36,662 75,000
40,221 75,000
44,313 75,000
23,575 75,000
8,738 75,000
26,652 75,000
55,762 7S.000
FAA CRS E6~.,_l207X
CUSTOMER: Summit
W /0: 55033827
BOEING DWG. 65C73762
Remaining Last Operator WO Cycles , 38,333 CANADIAN 55033827
38,333 CANADIAN 55033827
38,333 CANADIAN 55033827
38,333 CANADIAN 55033827
38,338 CANADIAN 55033827
38,338 CANADIAN 55033827
38,338 CANADIAN 55033827
38,338 CANADIAN 55033827
56,711 CANADIAN 55033827
32,131 WEBJET 7503494
48,925 WEBJET 7503495
39,179 CANADIAN 55033627
23,841 WEBJET 55033827
20,009 WEBJET 55033827
38,338 CANADIAN 55033827
38,338 CANADIAN 55033827
50,368 CANADIAN 55033827
41,904 CANADIAN 55033827
36,338 CANADIAN 55033827
71,832 CANADIAN 55033827
30,194 AMERICAN P0:55038605
37,404 DELTA P0:55038670
38,338 CANADIAN 55033827
34,779 CANADIAN 55033627
30,687 CANADIAN 55033627
51,425 CANADIAN 55033627
66,264 CANADIAN 55033627
48,348 CANADIAN 55033827
19,218 WEBJET 7503493
DATE: u-:::: , ,z.,~t°'"V'"' F I lofl
SUMM~
SETIING A NEW STANDARD FOR SUPPORT
SERVICE BULLETINS AND SERVICE LETTERS
DESCRIPTION: NOSE LANDING GEAR
PART NUMBER: 65-73762-21
SERIAL NUMBER: T2200P1540
SB/SL Rev. Modification Subject
DAMAGE TO THE LIGHT ASSEMBLY. Mandates installation of AD 2000-08-17 - light assembly PIN 50-0199-9, 50-0199-11, 50-0128-1A, 50-0128-
1MA, 50-128-3A, or50-0128-3MA. Ref. SB 737-33-1129.
AD 2003-07-12 - Incorporates SB 737-32-1322.
e) ., QUALITY CONTROL ______ _
SUM-QC-S8-F01 REV O NOV 17, 2016
Previously Embodied
FAA CRS E6QR207X
MODEL: 737-300/500
CUSTOMER: Summit
W/0: 55033827
Embodied at Overhaul
X
X
Remark
Ref. SB 33-1129
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