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510 

14 CFR Ch. I (1–1–24 Edition) 

§ 135.417 

(6) Apparent cause of the failure, 

malfunction or defect (e.g., wear, 
crack, design deficiency, or personnel 
error). 

(7) Other pertinent information nec-

essary for more complete identifica-
tion, determination of seriousness, or 
corrective action. 

(f) A certificate holder that is also 

the holder of a type certificate (includ-
ing a supplemental type certificate), a 
Parts Manufacturer Approval, or a 
Technical Standard Order Authoriza-
tion, or that is the licensee of a type 
certificate need not report a failure, 
malfunction, or defect under this sec-
tion if the failure, malfunction, or de-
fect has been reported by it under § 21.3 
or § 37.17 of this chapter or under the 
accident reporting provisions of 49 CFR 
part 830 of the regulations of the Na-
tional Transportation Safety Board. 

(g) No person may withhold a report 

required by this section even though 
all information required by this section 
is not available. 

(h) When the certificate holder gets 

additional information, including in-
formation from the manufacturer or 
other agency, concerning a report re-
quired by this section, it shall expedi-
tiously submit it as a supplement to 
the first report and reference the date 
and place of submission of the first re-
port. 

[Doc. No. 16097, 43 FR 46783, Oct. 10, 1978, as 
amended by Amdt. 135–102, 70 FR 76979, Dec. 
29, 2005; Doc. No. FAA–2022–1355; Amdt. Nos. 
135–143; 87 FR 75848, Dec. 9, 2022] 

§ 135.417 Mechanical interruption 

summary report. 

Each certificate holder shall mail or 

deliver, before the end of the 10th day 
of the following month, a summary re-
port of the following occurrences in 
multiengine aircraft for the preceding 
month to the responsible Flight Stand-
ards office: 

(a) Each interruption to a flight, un-

scheduled change of aircraft en route, 
or unscheduled stop or diversion from a 
route, caused by known or suspected 
mechanical difficulties or malfunctions 
that are not required to be reported 
under § 135.415. 

(b) The number of propeller 

featherings in flight, listed by type of 
propeller and engine and aircraft on 

which it was installed. Propeller 
featherings for training, demonstra-
tion, or flight check purposes need not 
be reported. 

[Doc. No. 16097, 43 FR 46783, Oct. 10, 1978, as 
amended by Amdt. 135–60, 61 FR 2616, Jan. 26, 
1996; Docket FAA–2018–0119, Amdt. 135–139, 83 
FR 9175, Mar. 5, 2018] 

§ 135.419 Approved aircraft inspection 

program. 

(a) Whenever the Administrator finds 

that the aircraft inspections required 
or allowed under part 91 of this chapter 
are not adequate to meet this part, or 
upon application by a certificate hold-
er, the Administrator may amend the 
certificate holder’s operations speci-
fications under § 119.51, to require or 
allow an approved aircraft inspection 
program for any make and model air-
craft of which the certificate holder 
has the exclusive use of at least one 
aircraft (as defined in § 135.25(b)). 

(b) A certificate holder who applies 

for an amendment of its operations 
specifications to allow an approved air-
craft inspection program must submit 
that program with its application for 
approval by the Administrator. 

(c) Each certificate holder who is re-

quired by its operations specifications 
to have an approved aircraft inspection 
program shall submit a program for ap-
proval by the Administrator within 30 
days of the amendment of its oper-
ations specifications or within any 
other period that the Administrator 
may prescribe in the operations speci-
fications. 

(d) The aircraft inspection program 

submitted for approval by the Adminis-
trator must contain the following: 

(1) Instructions and procedures for 

the conduct of aircraft inspections 
(which must include necessary tests 
and checks), setting forth in detail the 
parts and areas of the airframe, en-
gines, propellers, rotors, and appli-
ances, including emergency equipment, 
that must be inspected. 

(2) A schedule for the performance of 

the aircraft inspections under para-
graph (d)(1) of this section expressed in 
terms of the time in service, calendar 
time, number of system operations, or 
any combination of these. 

(3) Instructions and procedures for 

recording discrepancies found during 

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511 

Federal Aviation Administration, DOT 

§ 135.422 

inspections and correction or deferral 
of discrepancies including form and 
disposition of records. 

(e) After approval, the certificate 

holder shall include the approved air-
craft inspection program in the manual 
required by § 135.21. 

(f) Whenever the Administrator finds 

that revisions to an approved aircraft 
inspection program are necessary for 
the continued adequacy of the pro-
gram, the certificate holder shall, after 
notification by the Administrator, 
make any changes in the program 
found by the Administrator to be nec-
essary. The certificate holder may pe-
tition the Administrator to reconsider 
the notice to make any changes in a 
program. The petition must be filed 
with the representatives of the Admin-
istrator assigned to it within 30 days 
after the certificate holder receives the 
notice. Except in the case of an emer-
gency requiring immediate action in 
the interest of safety, the filing of the 
petition stays the notice pending a de-
cision by the Administrator. 

(g) Each certificate holder who has 

an approved aircraft inspection pro-
gram shall have each aircraft that is 
subject to the program inspected in ac-
cordance with the program. 

(h) The registration number of each 

aircraft that is subject to an approved 
aircraft inspection program must be in-
cluded in the operations specifications 
of the certificate holder. 

[Doc. No. 16097, 43 FR 46783, Oct. 10, 1978, as 
amended by Amdt. 135–104, 71 FR 536, Jan. 4, 
2006] 

§ 135.421 Additional maintenance re-

quirements. 

(a) Each certificate holder who oper-

ates an aircraft type certificated for a 
passenger seating configuration, ex-
cluding any pilot seat, of nine seats or 
less, must comply with the manufac-
turer’s recommended maintenance pro-
grams, or a program approved by the 
Administrator, for each aircraft en-
gine, propeller, rotor, and each item of 
emergency equipment required by this 
chapter. 

(b) For the purpose of this section, a 

manufacturer’s maintenance program 
is one which is contained in the main-
tenance manual or maintenance in-
structions set forth by the manufac-

turer as required by this chapter for 
the aircraft, aircraft engine, propeller, 
rotor or item of emergency equipment. 

(c) For each single engine aircraft to 

be used in passenger-carrying IFR op-
erations, each certificate holder must 
incorporate into its maintenance pro-
gram either: 

(1) The manufacturer’s recommended 

engine trend monitoring program, 
which includes an oil analysis, if appro-
priate, or 

(2) An FAA approved engine trend 

monitoring program that includes an 
oil analysis at each 100 hour interval or 
at the manufacturer’s suggested inter-
val, whichever is more frequent. 

(d) For single engine aircraft to be 

used in passenger-carrying IFR oper-
ations, written maintenance instruc-
tions containing the methods, tech-
niques, and practices necessary to 
maintain the equipment specified in 
§§ 135.105, and 135.163 (f) and (h) are re-
quired. 

(e) No certificate holder may operate 

a single engine aircraft under IFR, car-
rying passengers, unless the certificate 
holder records and maintains in the en-
gine maintenance records the results of 
each test, observation, and inspection 
required by the applicable engine trend 
monitoring program specified in (c) (1) 
and (2) of this section. 

[Doc. No. 16097, 43 FR 46783, Oct. 10, 1978, as 
amended by Amdt. 135–70, 62 FR 42374, Aug. 6, 
1997] 

§ 135.422 Aging airplane inspections 

and records reviews for multien-

gine airplanes certificated with 

nine or fewer passenger seats. 

(a) 

Applicability. 

This section applies 

to multiengine airplanes certificated 
with nine or fewer passenger seats, op-
erated by a certificate holder in a 
scheduled operation under this part, 
except for those airplanes operated by 
a certificate holder in a scheduled op-
eration between any point within the 
State of Alaska and any other point 
within the State of Alaska. 

(b) 

Operation after inspections and 

records review. 

After the dates specified 

in this paragraph, a certificate holder 
may not operate a multiengine air-
plane in a scheduled operation under 
this part unless the Administrator has 
notified the certificate holder that the