# AD 88-09-05 R1: Labels Marking Lavatory - Type: Airworthiness directive - Status: Current - Products: Bombardier DHC-8-101, DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311 and DHC-8-315 - Effective: October 21, 1996 - Published: September 16, 1996, 61 FR 48612–48613 - Issued as: Final rule - Superseded by: Nothing supersedes this AD - Product type: Aircraft, Large airplane - Amendment: 39-9745 - Docket: 95-NM-266-AD - Registered aircraft: 68 may be affected, by airframe or engine model (OpenAirDocs) - Official PDF: https://openairdocs.org/files/sha256/97/dd/97ddac191e90e598a14d9be262031f60f0930be911361463166b928039f735a5 (from https://www.govinfo.gov/content/pkg/FR-1996-09-16/pdf/96-22598.pdf) - Federal Register: https://www.federalregister.gov/documents/1996/09/16/96-22598/airworthiness-directives-de-havilland-model-dhc-8-100-series-airplanes - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A49EBED25CB95307862569ED0055CDAF.0001 - DRS record last changed: May 30, 2024 - Page: https://openairdocs.org/ad/88-09-05-R1 ## The airworthiness directive 88-09-05 R1 DE HAVILLAND, INC.: Amendment 39-9745. Docket 95-NM-266-AD. Revises AD 88-09-05, Amendment 39-5908. Applicability: Model DHC-8 series airplanes, serial numbers 3 through 79 inclusive, on which Modification 8/0757 has not been installed; certificated in any category. NOTE 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (b) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it. Compliance: Required as indicated, unless accomplished previously. To prevent inadvertent opening of the airstair door and consequent depressurization of the airplane, accomplish the following: (a) Within 60 days after June 10, 1988 (the effective date of AD 88-09-05, amendment 39-5908), replace the labels marking the location and means of opening the lavatory, in accordance with the Accomplishment Instructions of de Havilland Service Bulletin 8-11-14, Revision `A', dated July 31, 1987; or Revision `B', dated July 1, 1988, or Revision `C', dated September 29, 1995. (b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, New York Aircraft Certification Office (ACO), FAA, Engine and Propeller Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, New York ACO. NOTE 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the New York ACO. (c) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. (d) The replacement shall be done in accordance with de Havilland Service Bulletin 8- 11-14, Revision `A', dated July 31, 1987; or de Havilland Service Bulletin 8-11-14, Revision `B', dated July 1, 1988; or de Havilland Service Bulletin 8-11-14, Revision `C', dated September 29, 1995. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from Bombardier, Inc., Bombardier Regional Aircraft Division, Garratt Boulevard, Downsview, Ontario, Canada M3K 1Y5. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the FAA, New York Aircraft Certification Office, Engine and Propeller Directorate, 10 Fifth Street, Third Floor, Valley Stream, New York; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. (e) This amendment becomes effective on October 21, 1996. ## Affected data sheets (1) (OpenAirDocs) The type certificate data sheets whose models the AD names. - [TCDS A13NM](https://openairdocs.org/tcds/A13NM): De Havilland Aircraft of Canada Limited; names 9 of 16 models: DHC-8-101, DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311… ## 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: 68 (68 by airframe model, 0 by engine model) - Makers: Bombardier 31, Dehavilland 28, Boeing Of Canada/Dehav Div 6, Boeing 3 Models with the most aircraft: - [Dehavilland DHC-8-202](https://openairdocs.org/model/dehavilland-dhc-8-202): 17 aircraft (airframe model) - [Bombardier DHC-8-315](https://openairdocs.org/model/bombardier-dhc-8-315): 15 aircraft (airframe model) - [Bombardier DHC-8-202](https://openairdocs.org/model/bombardier-dhc-8-202): 14 aircraft (airframe model) - [Dehavilland DHC-8-106](https://openairdocs.org/model/dehavilland-dhc-8-106): 4 aircraft (airframe model) - [Boeing DHC-8-102](https://openairdocs.org/model/boeing-dhc-8-102): 3 aircraft (airframe model) - [Boeing Of Canada/Dehav Div DHC-8-311](https://openairdocs.org/model/boeing-of-canada-dehav-div-dhc-8-311): 3 aircraft (airframe model) - [Boeing Of Canada/Dehav Div DHC-8-106](https://openairdocs.org/model/boeing-of-canada-dehav-div-dhc-8-106): 2 aircraft (airframe model) - [Bombardier DHC-8-201](https://openairdocs.org/model/bombardier-dhc-8-201): 2 aircraft (airframe model) - [Dehavilland DHC-8-201](https://openairdocs.org/model/dehavilland-dhc-8-201): 2 aircraft (airframe model) - [Dehavilland DHC-8-103](https://openairdocs.org/model/dehavilland-dhc-8-103): 2 aircraft (airframe model) - [Dehavilland DHC-8-315](https://openairdocs.org/model/dehavilland-dhc-8-315): 2 aircraft (airframe model) - [Boeing Of Canada/Dehav Div DHC-8-102](https://openairdocs.org/model/boeing-of-canada-dehav-div-dhc-8-102): 1 aircraft (airframe model) - [Dehavilland DHC-8-102](https://openairdocs.org/model/dehavilland-dhc-8-102): 1 aircraft (airframe model) All 13 models: https://openairdocs.org/ad/88-09-05-R1/models.md Every aircraft: https://openairdocs.org/ad/88-09-05-R1/aircraft.md ## Related documents - [Proposed rule 95-NM-266-AD](https://openairdocs.org/proposed/95-NM-266-AD): Notice of proposed rulemaking (NPRM), published Jul 3, 1996 Its text cites no advisory circulars or STCs. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.