# Pacific Aerospace Service Bulletin PACSB/2C/001

Copy: Revision 1 ("DCA-FBA-4_PAL PACSB-2C-001 Issue 1 dated 25 September 2018"), 4 pages: PDF https://openairdocs.org/files/sha256/5c/b4/5cb46f36beff4b0a1d5b9a6b1a3fe68a742c8585313ed9096df39a84ea1eeeca; text https://openairdocs.org/service-documents/pacific-aerospace/pacsb-2c-001/file/5cb46f36beff.md. Rights: © Pacific Aerospace. Filed by the FAA in regulations.gov docket FAA-2019-0047; AD 2019-02-02 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.

## Details

- Manufacturer: [Pacific Aerospace](https://openairdocs.org/service-documents/pacific-aerospace.md)
- Type: Service bulletin (Service Bulletin)
- Number: PACSB/2C/001
- Latest revision known: PACSB/2C/001, Issue 1, dated September 25, 2018 (OpenAirDocs)
- Page: https://openairdocs.org/service-documents/pacific-aerospace/pacsb-2c-001

## ADs that cite it (1) (OpenAirDocs)

Newest first, with the revision each names, as OpenAirDocs read it from the AD's text.

- [AD 2019-02-02](https://openairdocs.org/ad/2019-02-02.md), effective Feb 27, 2019: Revision 1

## Text (4 pages)

Rights: © Pacific Aerospace. Filed by the FAA in regulations.gov docket FAA-2019-0047; AD 2019-02-02 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. Some pages are OCR from a scan. OCR can misread letters and numbers. Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1

Issued: 2
 
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25 Septembe
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VATOR 
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RENCE 
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### Page 2

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ACSB / 2C
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NSURE 
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C / 001 
SSUE 1 
mber 2018 
a. Retain 
pushrod 
nters on 
internal 
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to that 
ure that

### Page 3 (OCR)

PACIFICAEROSPACE  PACSB / 2C / 001
ISSUE 1
Re-install the push rod assembly.
10)  On the 2C3 and 2C4 aircraft, reconnect the spring to the elevator pushrod assembly
(Refer to Figure 2).
11)  Check the elevator deflections specified in Tables 27-80-01 and 27-80-02, following the
procedures specified in Section 27-30-01 of the Maintenance Manual FAC2-M200.
ASSEMBLY ELEVATOR (REF)
ELEVATOR PUSHROD ASSEMBLY
(P/N C305-1)
HORIZONTAL
STABILIZER (REF)
HORIZONTAL STABILIZER AREA (REF)
ELEVATOR PUSHROD ASSEMBLY
(P/N C305-1)
DETAIL A
DETAIL B
FIGURE 1  ELEVATOR PUSHROD ASSEMBLY - INSTALLATION
HORIZONTAL STABILIZER  TRIM ARM  HORIZONTAL STABILIZER (REF)  ASSEMBLY (P/N C305-1)  ELEVATOR PUSHROD  ASSEMBLY (P/N C305-1)  ELEVATOR PUSHROD
SPRING (REF)
SPRING (REF)
Landplane Configuration, s/n 300-306  Landplane Configuration, s/n 307 onwards
ELEVATOR PUSHROD
ASSEMBLY (P/N C305-1)  ELEVATOR PUSHROD
ASSEMBLY (P/N C305-1)
SPRING (REF)
SPRING (REF)
Floatplane Configuration, s/n 300-306  Floatplane Configuration, s/n 307 onwards
FIGURE 2  SPRING REMOVAL (2C3 & 2C4 ONLY)
Issued: 25 September 2018  Page 3 of 4

### Page 4

Pa
3. 
4. 
 
age 4 of 4 
 
 
 
 
 
 
 
CERTI
Record 
 
 
MATER
 Boil e
 CA 1
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
F
FICATION
compliance
RIAL REQ
ed linseed o
1000 Non-C
FIGURE 3 
N 
e with this S
QUIRED 
oil, ACF-50 A
Chromate Co
ELEVAT
Service Bull
Anti-corrosi
orrosion Inh
 
TOR PUSH
etin in the A
ion compou
hibitive Join
ROD ASSE
Aircraft Log 
und or equiv
nting Compo
 P A
Issued
EMBLY 
Book. 
valent. 
ound (from 
ACSB / 2C
IS
d: 25 Septem
 
PPG Aeros
C / 001 
SSUE 1 
mber 2018 
space).

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