James D. Morton, Jr. v. James E. Dow, Acting Administrator, Federal Aviation Administration, and National Transportation Safety Board

525 F.2d 1302
CourtCourt of Appeals for the Tenth Circuit
DecidedOctober 21, 1975
Docket75--1088
StatusPublished
Cited by21 cases

This text of 525 F.2d 1302 (James D. Morton, Jr. v. James E. Dow, Acting Administrator, Federal Aviation Administration, and National Transportation Safety Board) is published on Counsel Stack Legal Research, covering Court of Appeals for the Tenth Circuit primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
James D. Morton, Jr. v. James E. Dow, Acting Administrator, Federal Aviation Administration, and National Transportation Safety Board, 525 F.2d 1302 (10th Cir. 1975).

Opinion

WILLIAM E. DOYLE, Circuit Judge.

This is a review of a decision of the Federal Aviation Administrator revoking the petitioner Morton’s airworthiness certificate for what purported to be a rebuilt Bell Helicopter, Model 205A — 1. This review is pursuant to 49 U.S.C. §§ 1429 and 1486.

An aircraft belonging to Arizona Helicopters, Inc. crashed and was totally destroyed on August 14, 1972. Little was salvaged except the log book and the identification plate. These, however, were used to build a new helicopter, and for the obtaining of a new registration number. This latter was changed from N2236W to N6208N.

Meanwhile, on August 23, 1973, Arizona Helicopters had conveyed the salvage together with the new number to petitioner. 11^ was Morton who constructed the new aircraft and affixed the log book and identification plate of the destroyed one.

Based on a previous airworthiness certificate, Morton contacted an FAA employee and showed him a copy of the 1969 airworthiness certificate together with the change in registration number. He represented that he had lost his original airworthiness certificate and asked the employee to issue him a replacement. All of this was without mentioning that the helicopter bearing No. N2236W had been destroyed. The employee, who had known Morton previously, issued the replacement .certificate without further ado.

After it had been in service for two months, Bell Helicopters learned of it and made a complaint to FAA. The FAA in turn on February 28, 1974, issued an emergency order of revocation of the airworthiness certificate for the aircraft. As a result, Morton was unable to fly the helicopter from that time on.

In March 1974, notice of appeal was filed to the National Transportation Safety Board seeking review of the revocation order. Morton waived the emergency procedures in order to serve personal convenience. Thereupon, the Administrative Law Judge denied motions for discovery and clarification of the emergency order. The matter came to trial on November 18, 1974, and at the conclusion of that trial, on November 22, 1974, the Administrative Law Judge issued an oral decision affirming the emergency order. His decision was appealed to the National Transportation Safety Board, and on March 27, 1975, the Board affirmed the emergency order.

The action of the FAA, the Administrative Law Judge and the National Transportation Safety Board did not proceed on the basis that a deception had been perpetiated on the FAA in order to get that body to issue a replacement airworthiness certificate. Why, we do not *1305 know. It would seem simple to so proceed. One would suppose that implicit in an application of this sort would be that the aircraft is the identical one which had been originally certificated. Once it became apparent that it was not, it would seem that the action taken on the false assumption could be easily undone as void or at least voidable. There is no need, however, to clear up this mystery because the government agency continued the fiction by the simple expedient of ruling that the aircraft for which an airworthiness certificate had been issued did not comply with the type certificate for a Bell Helicopter Model 205A-1.

I.

49 U.S.C. § 1423 vests in the Administrator of the FAA power to issue type certificates for aircraft. This certificate pertains to the design of the aircraft and once a general design is type certificated, all other craft built according to that design are entitled to type certificates. An applicant can obtain a type certificate if the aircraft design complies with the airworthiness requirements of 14 C.F.R. Parts 23-35 and a test shows that it is safe. The type certificate includes the design, the operating limitations, the certified data sheet and the FAA regulations. These are effective until suspended, revoked or otherwise terminated, and are freely transferable provided notice is given to the FAA. 14 C.F.R. § 21.47. Some modifications to an aircraft compel the issuance of a new type certificate. Other “major changes” require only a supplemental type certificate. 14 C.F.R. §§ 21.113-21.119.

As noted, the Administrator’s determination that the craft conforms to its type certificate, plus his determination that the aircraft is in a safe condition entitles it to an airworthiness certificate. 49 U.S.C. § 1423(c). A new aircraft is, of course, entitled to the type certificate without exception. 14 C.F.R. § 21.83, but other aircraft are not entitled to an airworthiness certificate unless the owner presents evidence as set forth in the regulations. See 14 C.F.R. § 21.181(1). Once issued, however, the airworthiness certificate continues as long as maintenance, preventive maintenance and alterations are performed in accordance with the regulations. 14 C.F.R. § 21.181(1). An airworthiness certificate is transferred with the craft. 14 C.F.R. § 21.179.

Morton’s contentions are:

First, that the procedures that we have outlined violate his constitutional rights — deprive him of due process of law and are contrary to the Administrative Procedure Act;

Second, that at the trial the complaint was insufficient, the evidence was irrelevant and was also insufficient to support the findings;

Third, that the Administrator was es-topped to revoke his airworthiness certificate;

Fourth, that the Administrative Law Judge was obligated to furnish an opportunity to eliminate the non-conformance of the helicopter with the type certificate.

We have considered the various aspects of the due process arguments and conclude that they are wholly without merit. We see nothing invalid in the authority given in 49 U.S.C. § 1429 to the Administrator to revoke an airworthiness certificate in an emergency and without a hearing. Thus, it has been held that agencies can take emergency action where danger to the public is present. 1 Inherent in an aircraft is dan *1306 ger if it does not meet prescribed standards. This helicopter, though purporting to be a Bell 205A — 1, was not such an aircraft. We are not able to say that the Administrator did not have sufficient grounds to summarily suspend the certificate.

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