# AD 2008-02-18: Pick-up collar support and nylon screws

- Type: Airworthiness directive
- Status: Current
- Products: BRS-172 parachute recovery system (Ballistic Recovery Systems STC SA01679CH or SA01999CH)
- Effective: February 28, 2008
- Published: January 24, 2008, 73 FR 4051–4053
- Issued: January 16, 2008
- Issued as: Final rule
- Superseded by: Nothing supersedes this AD
- Product type: Aircraft, Small airplane
- Amendment: 39-15348
- Docket: FAA-2007-29317 (https://www.regulations.gov/docket/FAA-2007-29317)
- Project: 2007-CE-079-AD
- Registered aircraft: 30,787 may be affected, by airframe or engine model (OpenAirDocs)
- Official PDF: https://openairdocs.org/files/sha256/da/3c/da3cdf5610d708b4bb6ef16c8677dc517865e2669229ede79ebeecee87e488f1 (from https://www.govinfo.gov/content/pkg/FR-2008-01-24/pdf/E8-1130.pdf)
- Federal Register: https://www.federalregister.gov/documents/2008/01/24/E8-1130/airworthiness-directives-cessna-aircraft-company-172-and-182-series-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5347E48E2DF1A5F1862573DA0059A97C.0001
- DRS record last changed: May 30, 2024
- Page: https://openairdocs.org/ad/2008-02-18

## Summary

We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company 172 series airplanes with the BRS-172 Parachute System installed via Supplemental Type Certificate (STC) No. SA01679CH and Cessna Aircraft Company 182 series airplanes that are equipped with the BRS-182 Parachute System installed via STC No. SA01999CH. This AD requires you to replace the pick-up collar support and nylon screws for the BRS-172 and BRS-182 Parachute System. This AD results from notification by Ballistic Recovery Systems, Inc. (BRS) that the pick-up collar assembly may prematurely move off the launch tube and adversely affect rocket trajectory during deployment. We are issuing this AD to prevent premature separation of the collar, which could result in the parachute failing to successfully deploy.

## The airworthiness directive

### Adoption of the Amendment

Accordingly, under the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows:

1. The authority citation for part 39 continues to read as follows:

2. FAA amends § 39.13 by adding the following new AD:

2008-02-18 Cessna Aircraft Company: Amendment 39-15348; Docket No. FAA-2007-29317; Directorate Identifier 2007-CE-079-AD.

### (a) Effective Date

  (a) This AD becomes effective on February 28, 2008.

### (b) Affected ADs

  (b) None.

### (c) Applicability

  (c) This AD applies to the following airplane models, all serial numbers, certificated in any category, that are equipped with:

  (1) BRS-172 Parachute System installed via Supplemental Type Certificate (STC) No. SA01679CH, or

  (2) BRS-182 Parachute System installed via STC No. SA01999CH.


| Cessna 172 models | Cessna 182 models |
| --- | --- |
| 172 | 182G |
| 172A | 182H |
| 172B | 182J |
| 172C | 182K |
| 172D | 182L |
| 172E | 182M |
| 172F (USAF T-41A) | 182N |
| 172G | 182P |
| 172H (USAF T-41A) | 182Q |
| 172I | 182R |
| 172K | 182S |
| 172L | 182T |
| 172M | T182 |
| 172N | T182T |
| 172P |  |
| 172Q |  |
| 172R |  |
| 172S |  |
| R172J |  |
| R172K |  |

### (d) Unsafe Condition

  (d) This AD results from notification by Ballistic Recovery Systems, Inc. (BRS) that the pick-up collar assembly may prematurely move off the launch tube and adversely affect rocket trajectory during deployment. We are issuing this AD to prevent premature separation of the collar. This condition could result in the parachute failing to successfully deploy.

### (e) Compliance

  (e) To address this problem, you must do the following, unless already done:

*—*

| Actions | Compliance | Procedures |
| --- | --- | --- |
| Remove and replace the pick-up collar support and two retaining screws | Within the next 25 hours time-in-service after February 28, 2008 (the effective date of this AD) | (i) For Cessna 172 series airplanes follow BRS SB 07-01, dated June 8, 2007. (ii) For Cessna 182 series airplanes, follow BRS SB 07-02, dated June 8, 2007. |

### (f) Alternative Methods of Compliance (AMOCs)

  (f) The Manager, Chicago Aircraft Certification Office, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Gregory Michalik, Senior Aerospace Engineer, FAA, 2300 East Devon Avenue, Des Plaines, Illinois, 60018; telephone: (847) 294-7135; fax: (847) 294-7834; e-mail: gregory.michalik@faa.gov. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO.

### (g) Material Incorporated by Reference

  (g) You must use Ballistic Recovery Systems, Inc. Service Bulletin No. 07-01, dated June 8, 2007, for Cessna 172 series airplanes; or Ballistic Recovery Systems, Inc. Service Bulletin No. 07-02, dated June 8, 2007, for Cessna 182 series airplanes; to do the actions required by this AD, unless the AD specifies otherwise.

  (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51.

  (2) For service information identified in this AD, contact Ballistic Recovery Systems, Inc., 300 Airport Road, South Saint Paul, MN 55075-3551; telephone: (651) 457-7491; fax: (651) 457-8651.

  (3) You may review copies at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 64106; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.

## Rule preamble

### Dates

This AD becomes effective on February 28, 2008.

On February 28, 2008, the Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD.

### Addresses

For service information identified in this AD, contact Ballistic Recovery Systems, Inc., 300 Airport Road, South Saint Paul, MN 55075-3551; telephone: (651) 457-7491; fax: (651) 457-8651.

To view the AD docket, go to U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590, or on the Internet at http://www.regulations.gov. The docket number is FAA-2007-29317; Directorate Identifier 2007-CE-079-AD.

### For further information contact

Gregory Michalik, Senior Aerospace Engineer, 2300 East Devon Avenue, Room 107, Des Plaines, Illinois 60018; telephone: (847) 294-7135; fax: (847) 294-7834.

### Discussion

On November 2, 2007, we issued a proposal to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) to include an AD that would apply to certain Cessna Aircraft Company 172 and 182 series airplanes that are equipped with the BRS-172 and BRS-182 Parachute System. This proposal was published in the Federal Register as a notice of proposed rulemaking (NPRM) on November 2, 2007 (72 FR 62143). The NPRM proposed to require the replacement of the pick-up collar support and screws for the BRS-172 and BRS-182 Parachute System.

### Comments

We provided the public the opportunity to participate in developing this AD. We received no comments on the proposal or on the determination of the cost to the public.

### Conclusion

We have carefully reviewed the available data and determined that air safety and the public interest require adopting the AD as proposed except for minor editorial corrections. We have determined that these minor corrections:

• Are consistent with the intent that was proposed in the NPRM for correcting the unsafe condition; and

• Do not add any additional burden upon the public than was already proposed in the NPRM.

### Costs of Compliance

We estimate that this AD affects 54 airplanes in the U.S. registry.

We estimate the following costs to do the modification:

*—*

| Labor cost | Parts cost | Total cost per airplane | Total cost on U.S. operators |
| --- | --- | --- | --- |
| 1 work-hour × $80 per hour = $80 | Not Applicable | $80 | $4,320 |

Note:

BRS will provide warranty credit to the extent noted in Ballistic Recovery Systems, Inc. Service Bulletins SB 07-01 and SB 07-02, both dated June 8, 2007.

### Authority for This Rulemaking

Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, Section 106 describes the authority of the FAA Administrator. Subtitle VII, Aviation Programs, describes in more detail the scope of the agency's authority.

We are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701, “General requirements.” Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this AD.

### Regulatory Findings

We have determined that this AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government.

For the reasons discussed above, I certify that this AD:

1. Is not a “significant regulatory action” under Executive Order 12866;

2. Is not a “significant rule” under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and

3. Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act.

We prepared a summary of the costs to comply with this AD (and other information as included in the Regulatory Evaluation) and placed it in the AD Docket. You may get a copy of this summary by sending a request to us at the address listed under ADDRESSES. Include “Docket No. FAA-2007-29317; Directorate Identifier 2007-CE-079-AD” in your request.

## Affected data sheets (3) (OpenAirDocs)

The type certificate data sheets whose models the AD names.

- [TCDS 3A12](https://openairdocs.org/tcds/3A12): Textron Aviation Inc.; names 18 of 18 models: 172F (USAF T-41A), 172M, 172Q, 172R, 172K, 172G, 172A, 172L…
- [TCDS 3A13](https://openairdocs.org/tcds/3A13): Textron Aviation Inc.; names 14 of 23 models: 182J, 182P, 182L, 182G, 182Q, 182N, 182M, 182H…
- [TCDS 3A17](https://openairdocs.org/tcds/3A17): Textron Aviation Inc.; names 2 of 12 models: R172K, R172J

## Registered aircraft it may apply to (OpenAirDocs)

Matched by airframe and engine model; the AD's applicability may narrow it by serial number, part number or equipment.

- Aircraft: 30,787 (30,787 by airframe model, 0 by engine model)
- Makers: Cessna 29,103, Textron 1,682, Cessna Wren 2

Models with the most aircraft:

- [Cessna 172M](https://openairdocs.org/model/cessna-172m): 3,573 aircraft (airframe model)
- [Cessna 172N](https://openairdocs.org/model/cessna-172n): 3,138 aircraft (airframe model)
- [Cessna 182P](https://openairdocs.org/model/cessna-182p): 2,099 aircraft (airframe model)
- [Cessna 172S](https://openairdocs.org/model/cessna-172s): 1,915 aircraft (airframe model)
- [Cessna 172](https://openairdocs.org/model/cessna-172): 1,805 aircraft (airframe model)
- [Cessna 182Q](https://openairdocs.org/model/cessna-182q): 1,565 aircraft (airframe model)
- [Textron 172S](https://openairdocs.org/model/textron-172s): 1,239 aircraft (airframe model)
- [Cessna 172P](https://openairdocs.org/model/cessna-172p): 1,111 aircraft (airframe model)
- [Cessna 172K](https://openairdocs.org/model/cessna-172k): 1,026 aircraft (airframe model)
- [Cessna 182T](https://openairdocs.org/model/cessna-182t): 969 aircraft (airframe model)
- [Cessna 172L](https://openairdocs.org/model/cessna-172l): 857 aircraft (airframe model)
- [Cessna T182T](https://openairdocs.org/model/cessna-t182t): 781 aircraft (airframe model)
- [Cessna 172H](https://openairdocs.org/model/cessna-172h): 780 aircraft (airframe model)
- [Cessna 172G](https://openairdocs.org/model/cessna-172g): 722 aircraft (airframe model)
- [Cessna 172F](https://openairdocs.org/model/cessna-172f): 717 aircraft (airframe model)
- [Cessna 172R](https://openairdocs.org/model/cessna-172r): 683 aircraft (airframe model)
- [Cessna R172K](https://openairdocs.org/model/cessna-r172k): 653 aircraft (airframe model)
- [Cessna 172E](https://openairdocs.org/model/cessna-172e): 617 aircraft (airframe model)
- [Cessna 182S](https://openairdocs.org/model/cessna-182s): 606 aircraft (airframe model)
- [Cessna 182J](https://openairdocs.org/model/cessna-182j): 487 aircraft (airframe model)

All 42 models: https://openairdocs.org/ad/2008-02-18/models.md
Every aircraft: https://openairdocs.org/ad/2008-02-18/aircraft.md

## Related documents

- [Proposed rule FAA-2007-29317](https://openairdocs.org/proposed/FAA-2007-29317): Notice of proposed rulemaking (NPRM), published Nov 2, 2007
- [STC SA01679CH](https://openairdocs.org/stc/SA01679CH): Install BRS-172 parachute recovery system.. Ballistic Recovery Systems Inc., Named in the applicability
- [STC SA01999CH](https://openairdocs.org/stc/SA01999CH): Install BRS-182 parachute recovery system.. Ballistic Recovery Systems Inc., Named in the applicability

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