2700

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DIFFUSER,AIR,AIRCRAFT HEATING AN

NELLCOR PURITAN BENNETT LLC DBA COVIDIEN DIV COVIDIENATA 21

Where to Buy

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Documentation

General information based on part classification, not a certification determination. Your operator's quality manual governs.

OEM / Production Approval Holder Part8130-3 Eligible

What to ask the seller for

  • FAA Form 8130-3 from the PAH or an authorized release traceable to the PAH
  • Manufacturer's CofC if a Form 8130-3 was not issued

Governing reference: FAA Order 8130.21J

PMA Alternatives

No PMA alternatives found for this part. This does not mean none exist — only that none are currently in our database.

Supplemental Type Certificates15 found

FAA-approved modifications that reference this part number

SA02483CH ↗Don P. Maxwell
Rev: 2023-08-11

Modify aircraft to utilize full 310 BHP @ 2700 rpm rated power of existing installed Teledyne Continental Motors (TCM) TSIO-550-G engine.

Aircraft: M20TN

SE792NW ↗4J's Aviation
Rev: 2019-07-26

Modification of a Lycoming0-235-L2C, or 0-235-L2A engine to increase HP rating from 115-HP at 2700 rpm to a continuous125 HP at 2800 rpm.

Aircraft: O-235-L2A, O-235-L2C

SA1391CE ↗Artic Barnabas Ministries
Rev: 2018-04-23

Cutting and reattaching the left and right lower engine cowling with AN 2700-4 cam locks.

Aircraft: PA-23-250

SA2251CE ↗Textron Aviation Inc.
Rev: 2018-03-09

Installation of a B & D Model 2700 Cabin and Cockpit Display System.

Aircraft: 650

SA02193CH ↗Mooney International Corp
Rev: 2017-11-14

Power increase to 310 BHP by Installation of Powerlite STC SE02930AT or CMI IO-550N Engine rated at 310 BHP/2700 RPMs and Hartzell Propeller Model PHC-J3YF-1RF/F7693DF(B)-2 propeller

Aircraft: M20R, M20S, M20U

ST02177LA ↗Rockwell Collins Inc
Rev: 2015-12-07

Installation of Rockwell Collins Model 6605 Head-Up Display (HUD-6605) and Enhanced Vision System (EVS) CMA-2600i Infrared Sensor System (ISS) or HUD and Enhanced Flight Vision System (EFVS) CMA-2700

Aircraft: CL-600-2B16 (CL-604)

SH516AL ↗Airglas Inc.
Rev: 2012-08-16

Installation of Airglas model L-2700-369 skis

Aircraft: 369HE, 369HM, 369HS

SA2375SW-D ↗RAM Aircraft Limited Partnership
Rev: 2008-08-25

Installation of Lycoming 0-320-D2G, 0-320-D2J, or 0-320-E2D (as modified by STC SE3692SW-D) engine rated for 160 h.p. take-off and 150 h.p. METO for models 1721, 172K, 172L, and 172M according to RAM Dwg. Rl 7201 Rev. F dated 12/9/86; or installation of Lycoming 0-320-D2G, 0-320-D2J, or 0-320-E2D (as modified by STC SE3692SW-D) engine rated for 160 h.p. take-off and 145 h.p. METO for models 172D, 172E, 172F, 172G, and 172H according to RAM Dwg. 17202, Rev. K dated 12/9/86; or installation of Lycoming 0-320-D2G, 0-320-D2J or 0-320-E2D (as modified by STC SE3692SW-D) engine (160 h.p., 2700 r.p.m) in model 172N according to RAM Dwg. 17203, Rev. L dated 12/9/86; or later FAA approved revision.

Aircraft: 172D, 172E, 172F (USAF T-41A), 172G +6 more

SE09104SC-D ↗RAM Aircraft Limited Partnership
Rev: 2008-08-24

Modify Teledyne Continental TSIO-520-NB engine. Maximum continuous power is 335 hp at 2700 rpm and 38.0 inches Hg manifold pressure. This mod is limited to Teledyne Continental motors model TSIO-520-NB engines modified per STC SE4327SW.

Aircraft: TSIO-520-NB

SE4327SW-D ↗RAM Aircraft Limited Partnership
Rev: 2008-08-19

Increase all operations power rating to 325 horse power (HP) at 40 inches of manifold pressure (MP) and 2700 RPM.

Aircraft: TSIO-520-NB

SA3674WE ↗Rogerson ATS
Rev: 2008-05-12

Installation of 2700 gallon auxiliary fuel tanks in forward and aft cargo compartments. (727-17)

Aircraft: 727

SE3877NM ↗Kai V. Nielsen
Rev: 2008-01-08

Modification of a Lycoming O-235-L2C engine to increase the horsepower rating from 115 HP @ 2700 RPM to a continuous 125 HP @ 2800 RPM

Aircraft: O-235-L2C

SE4327SW ↗RAM Aircraft Limited Partnership
Rev: 2001-10-08

Increase all operation power rating to 325 horsepower (hp) at 40 inches of manifold pressure (MP) and 2700 RPM.

Aircraft: TSIO-520-NB

SE00988CH ↗Precision Engine
Rev: 1999-02-08

Modify Lycoming aircraft engine Model O-235-C2C rated at maximum continuous 108 hp at 2600 rpm and 6.75:1 compression ratio to maximum continuous 115 at 2700 rpm and 8.5:1 compression ratio.

Aircraft: O-235-C2C

ST0684SE ↗Flight Dynamics, Inc
Rev: 1996-05-02

Installation of HUD guidance system (HGS), Model 2700. (DO 328-100 MOD 10 CONFIGURATION)

Aircraft: Do 328-100

Airworthiness Directives

Synced 40 days ago (09/27/2026)

No Active Airworthiness Directives

No FAA or EASA ADs are linked to this part number. Always verify against the aircraft's maintenance records before install.

Service Difficulty Reports

No Service Difficulty Reports

No failure reports found for this part number in the FAA SDR database.

Suspect-Parts Alerts (SUP/UPN)

No Suspect-Parts Alerts

This manufacturer is not named in any active FAA Suspect Unapproved Parts (SUP/UPN) notification.

NSN Cross-References1 NSN — DLA WebFLIS

National Stock Numbers assigned to this part number by the U.S. Defense Logistics Agency

NSNStandardized NameFSCDLA List Price (gov't catalog)CAGE / Manufacturer
1660-01-052-4874DIFFUSER,AIR,AIRCRAFT HEATING AN1660—7Y988NELLCOR PURITAN BENNETT LLC DBA COVIDIEN DIV COVIDIEN

DLA PUBLOG published list price — government procurement catalog, not a commercial market price. Prices may differ from current commercial availability.

Government Award Prices

U.S. government contract award prices from FPDS — unit prices for NSN purchases by DoD/DLA agencies

No government contract award price data found for this part number.

Identifiers

Manufacturer

NELLCOR PURITAN BENNETT LLC DBA COVIDIEN DIV COVIDIEN

Source

DLA WebFLIS

ATA Chapter

21

Type

OEM

Part ID: nsn:2700 | Source: DLA WebFLIS | Last updated: 2026-11-07