# N215WE: 1984 Boeing 727-2S2F

- Status: Valid registration
- Airframe: [Boeing 727-2S2F](https://openairdocs.org/model/boeing-727-2s2f) (registry code 1384081, 124 seats)
- Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049)
- Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (Pratt & Whitney) (OpenAirDocs)
- Serial number: 22936
- Year built: 1984
- Type: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Experimental, showing compliance
- Airworthiness date: June 3, 2026
- Certificate issued: November 21, 2011
- Expires: November 30, 2027
- Mode S code: A1CE0E
- Registered owner: [International Trading Company Of Yukon Inc](https://openairdocs.org/faa-owner/INTERNATIONAL%20TRADING%20COMPANY%20OF%20YUKON%20INC)
- Location: [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City)
- Owner type: Non-citizen corporation
- Owner's area on the map: 35.5813° N, 97.5737° W: Placed by OpenAirDocs at the center of ZIP code 73120, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=215WE
- Page: https://openairdocs.org/aircraft/N215WE

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Pratt & Whitney JT8D-17 model are included.

## ADs that may apply (OpenAirDocs): 35 in force

### Matched by airframe (Boeing 727-2S2F)

None in force.

### Matched by engine (Pratt & Whitney JT8D-17 series)

- [AD 2011-03-01](https://openairdocs.org/ad/2011-03-01): Critical life- limited parts · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 9 more. Effective Mar 4, 2011
- [AD 2010-21-17](https://openairdocs.org/ad/2010-21-17): Fan blade · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-17 and 3 more. Effective Nov 12, 2010
- [AD 2009-24-01](https://openairdocs.org/ad/2009-24-01): Fan blade · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-17 and 5 more. Effective Jan 4, 2010
- [AD 2006-17-07 R1](https://openairdocs.org/ad/2006-17-07-R1): High pressure compressor (HPC) front hubs and HPC disk · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Nov 2, 2006
- [AD 2005-17-16](https://openairdocs.org/ad/2005-17-16): Critical life-limited rotating parts · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 17 more. Effective Sep 30, 2005
- [AD 2003-12-07](https://openairdocs.org/ad/2003-12-07): 12th Stage high pressure compressor · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Jul 18, 2003
- [AD 2003-05-07](https://openairdocs.org/ad/2003-05-07): Low pressure compressor (LPC) · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Apr 17, 2003
- [AD 2001-15-18](https://openairdocs.org/ad/2001-15-18): Stage Compressor Disks · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 6 more. Effective Sep 4, 2001
- [AD 99-01-08](https://openairdocs.org/ad/99-01-08): Stage 7 through Stage 15 High-Pressure Compressor (HPC) Disks · Pratt & Whitney Division JT3D-1, JT3D-1-MC6, JT3D-1-MC7 and 30 more. Effective Jan 5, 1999
- [AD 98-21-24](https://openairdocs.org/ad/98-21-24): Compressor Disks · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 17 more. Effective Nov 16, 1998
- [AD 98-04-39](https://openairdocs.org/ad/98-04-39): Combustion Chamber Outer Case · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Feb 25, 1998
- [AD 97-19-12](https://openairdocs.org/ad/97-19-12): Hub Inspection · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 9 more. Effective Nov 18, 1997
- [AD 97-19-14](https://openairdocs.org/ad/97-19-14): Low Pressure Turbine (LPT) Blade Sets · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 9 more. Effective Oct 24, 1997
- [AD 96-23-14](https://openairdocs.org/ad/96-23-14): Combustion Chamber Outer Cases · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Jan 2, 1997
- [AD 95-26-03](https://openairdocs.org/ad/95-26-03): High Pressure Compressor Disks · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Jan 11, 1996
- [AD 86-09-02 R2](https://openairdocs.org/ad/86-09-02-R2): Combustion Chamber Liners · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Nov 17, 1995
- [AD 95-16-07](https://openairdocs.org/ad/95-16-07): High Pressure Compressor (HPC) Disks · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 11 more. Effective Sep 11, 1995
- [AD 95-10-10](https://openairdocs.org/ad/95-10-10): Compressor Fan Hub · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 6 more. Effective Jul 21, 1995
- [AD 94-25-07](https://openairdocs.org/ad/94-25-07): Combustion Chamber Outer Case · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Mar 30, 1995
- [AD 95-02-16](https://openairdocs.org/ad/95-02-16): Fuel Nozzle and Support Assembly · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 17 more. Effective Feb 21, 1995
- [AD 94-20-09](https://openairdocs.org/ad/94-20-09): Low Pressure Turbine Blade Sets · Pratt & Whitney Division JT8D-15A, JT8D-17A and JT8D-17AR. Effective Nov 14, 1994
- [AD 91-24-14](https://openairdocs.org/ad/91-24-14): Bearing Seal Spacer · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Jan 21, 1992
- [AD 89-25-11](https://openairdocs.org/ad/89-25-11): Fan Blade Retaining Plates · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 6 more. Effective Jan 15, 1990
- [AD 86-08-04 R1](https://openairdocs.org/ad/86-08-04-R1): HPC Removable Sleeve Spacers · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Nov 4, 1986
- [AD 86-02-52 R1](https://openairdocs.org/ad/86-02-52-R1): Combustion Chamber · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Apr 14, 1986
- [AD 85-19-51 R1](https://openairdocs.org/ad/85-19-51-R1): Second Stage Turbine Disk · Pratt & Whitney Division JT8D-15, JT8D-17 and JT8D-17R. Effective Dec 26, 1985
- [AD 78-17-02 R3](https://openairdocs.org/ad/78-17-02-R3): Compressor Front Hubs · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 6 more. Effective Mar 30, 1984
- [AD 80-15-51](https://openairdocs.org/ad/80-15-51): Engine Rear Compressor Front Hubs · Pratt & Whitney Division JT8D-209, JT8D-1, JT8D-11 and 11 more. Effective Aug 21, 1980
- [AD 77-16-12](https://openairdocs.org/ad/77-16-12): Low Turbine Shaft · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 8 more. Effective Aug 31, 1977
- [AD 75-05-06](https://openairdocs.org/ad/75-05-06): Fuel Manifold Leakage · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Feb 24, 1977
- [AD 70-26-05](https://openairdocs.org/ad/70-26-05): First Stage Compressor Rotor Blades · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Dec 29, 1970
- [AD 70-25-08](https://openairdocs.org/ad/70-25-08): Seventh Stage Compressor Rotor Disc · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Dec 15, 1970
- [AD 70-11-03](https://openairdocs.org/ad/70-11-03): Sixth Stage Compressor Discs · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Jun 12, 1970
- [AD 70-02-02](https://openairdocs.org/ad/70-02-02): Sixth Stage Compressor Rotor Disc · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Apr 15, 1970
- [AD 76-12-06](https://openairdocs.org/ad/76-12-06): Second Stage Fan Blades · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-17 and 1 more

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N215WE.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20150413006859I](https://openairdocs.org/incident/20150413006859I), Apr 13, 2015: Boeing 727-2S2F (N215WE), Fwa, IN, No damage. Enroute crew declared emergency due to smoke & oder in cockpit diverted to Fwa. Unable to control RH pack temp due to previous trouble shooting causing pack…

## Service difficulty reports (40)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR VGCA20260917001](https://openairdocs.org/sdr/VGCA20260917001), Sep 17, 2026: ENGINE. MAKING METAL. ENGINE OIL BYPASS INDICATION. METAL IN OIL FILTER
- [SDR VGCA20251024009](https://openairdocs.org/sdr/VGCA20251024009), Oct 24, 2025: SKIN PANEL. DAMAGED. R/H HORIZONTAL STABILIZER UPPER T/E DAMAGED PANEL 65-20659-24 BETWEEN ELEV. STA. 99.79 AND 173.21
- [SDR VGCA20251024020](https://openairdocs.org/sdr/VGCA20251024020), Oct 24, 2025: FRAME. PUNCTURED. FUSELAGE FRAME INNER CHORD SCREW DAMAGE AT BS 1110 BETWEEN STRINGER 25R AND 28R.
- [SDR VGCA20251024019](https://openairdocs.org/sdr/VGCA20251024019), Oct 24, 2025: FRAME. PUNCTURED. FUSELAGE FRAME INNER CHORD SCREW DAMAGE AT BS 1090 BETWEEN STRINGER 26R AND 28R
- [SDR VGCA20251024018](https://openairdocs.org/sdr/VGCA20251024018), Oct 24, 2025: FRAME. DENTED. FUSELAGE FRAME INNER CHORD DENT AT BS 1070 BETWEEN STRINGER 25R AND 29R
- [SDR VGCA20251024017](https://openairdocs.org/sdr/VGCA20251024017), Oct 24, 2025: FRAME. DENTED. FUSELAGE FRAME INNER CHORD DENT AT BS 1050 BETWEEN STRINGER 26R AND 28R
- [SDR VGCA20251024016](https://openairdocs.org/sdr/VGCA20251024016), Oct 24, 2025: FLOORBEAM. CORRODED. FUSELAGE FLOOR STABILIZER BEAM MULTIPLE SPOTS CORROSION AT BL 0 BETWEEN BS 449.94 AND BS 720+9.94
- [SDR VGCA20251024015](https://openairdocs.org/sdr/VGCA20251024015), Oct 24, 2025: FRAME. GOUGED. FUSELAGE FRAME INNER CHORD GOUGED AT BS 1130 BETWEEN STRINGER 26L AND 28L
- [SDR VGCA20251024014](https://openairdocs.org/sdr/VGCA20251024014), Oct 24, 2025: FRAME. GOUGED. FUSELAGE FRAME INNER CHORD GOUGED AT BS 1110 BETWEEN STRINGER 26L AND 28L
- [SDR VGCA20251024013](https://openairdocs.org/sdr/VGCA20251024013), Oct 24, 2025: FRAME. PUNCTURED. FUSELAGE FRAME INNER CHORD PUNCTURED AT BS 1090 BETWEEN STRINGER 26L AND 28L
- [SDR VGCA20251024012](https://openairdocs.org/sdr/VGCA20251024012), Oct 24, 2025: SKIN. DENTED. FUSELAGE SKIN GOUGE/DENT REPAIRED BELOW MCD BETWEEN BS 460 AND BS 620, AND BETWEEN STRINGER 15L-20L
- [SDR VGCA20251024011](https://openairdocs.org/sdr/VGCA20251024011), Oct 24, 2025: FRAME. PUNCTURED. FUSELAGE FRAME INNER CHORD PUNCTURED AT BS 1070 BETWEEN STRINGER 26L AND 29L
- [SDR VGCA20251024010](https://openairdocs.org/sdr/VGCA20251024010), Oct 24, 2025: SHEAR TIE. CORRODED. FUSELAGE FRAME BOTTOM CHORD CORROSION DAMAGE AT BS 970 BETWEEN STRINGER 28R AND 29R.
- [SDR VGC2025F00000](https://openairdocs.org/sdr/VGC2025F00000), Oct 24, 2025: FRAME. CORRODED. FUSELAGE FRAME BOTTOM CHORD CORROSION DAMAGE AT BS 970 BETWEEN STRINGER 28R AND 29R
- [SDR VGCA202511254009](https://openairdocs.org/sdr/VGCA202511254009), Oct 24, 2025: SKIN PANEL. DAMAGED. R/H HORIZONTAL STABILIZER UPPER T/E DAMAGED PANELS 65-20659-24 BETWEEN ELEV. STA. 99.79 AND 173.21 REPAIRED AND INSTALLED I.A.W. V1 AEROSPACE DOC. NO. R24-02464
- [SDR VGCA202511254008](https://openairdocs.org/sdr/VGCA202511254008), Oct 24, 2025: SKIN PANEL. DAMAGED. RIGHT HORIZONTAL STABILIZER UPPER T/E DAMAGED PANELS 65-20658-24 BETWEEN ELEV. STA. 99.79 AND 173.21 REPAIRED AND INSTALLED IAW. R24-02464-001, REVISION 6 ,DATE
- [SDR VGCA20251024007](https://openairdocs.org/sdr/VGCA20251024007), Oct 24, 2025: BEAM. CORRODED. R/H SIDE H-STAB. TRAILING EDGE BEAM UPPER SURFACE CORROSION REPAIRED BY REPLACEMENT OF R/H TRAILING EDGE UPPER BEAM ENTIRE LENGTH BETWEEN ELEVATOR STATION 10 AN
- [SDR VGCA20251024006](https://openairdocs.org/sdr/VGCA20251024006), Oct 24, 2025: FLOORBEAM. CORRODED. FUSELAGE TRANSVERSE FLOOR BEAM UPPER FLANGE CORROSION DAMAGE AT BS 740 BETWEEN LBL 45 AND LBL 62
- [SDR VGCA20251024005](https://openairdocs.org/sdr/VGCA20251024005), Oct 24, 2025: FRAME. DENTED. FUSELAGE FRAME INNER CHORD DENTED AT BS 1050 BETWEEN STRINGER 25L AND 28L
- [SDR VGCA20251024004](https://openairdocs.org/sdr/VGCA20251024004), Oct 24, 2025: FRAME. CRACKED. FUSELAGE FRAME INNER CHORD CRACK AT BS 660 BETWEEN STRINGER 27L AND 27R
- [SDR VGCA20251024003](https://openairdocs.org/sdr/VGCA20251024003), Oct 24, 2025: FRAME. CRACKED. FUSELAGE FRAME INNER CHORD CRACK AT BS 640 BETWEEN STRINGER 28L AND 27R
- [SDR VGCA20251024002](https://openairdocs.org/sdr/VGCA20251024002), Oct 24, 2025: FRAME. DENTED. FUSELAGE FRAME INNER CHORD DENT AT BS 1148 BETWEEN STRINGER 25R AND 28R
- [SDR VGCA20251024001](https://openairdocs.org/sdr/VGCA20251024001), Oct 24, 2025: FRAME. DENTED. FUSELAGE FRAME INNER CHORD DENTS AT BS 1130 BETWEEN STRINGER 24R AND 28R
- [SDR VGCA20230323001](https://openairdocs.org/sdr/VGCA20230323001), Mar 23, 2023: GEARBOX. LEAKING. #2 ENGINE PRECAUTIONARY SHUTDOWN DUE TO LOW OIL PRESSURE. FOUND LOOSE FASTENER ON MAIN ACCESORY GEARBOX CAUSING OIL LOSS.
- [SDR VGCA20230213002](https://openairdocs.org/sdr/VGCA20230213002), Feb 13, 2023: STUB FRAME. DAMAGED. MISSDRILLED HOLES IN VERTICAL FLANGE OF LEFT STUB BEAM LOWER CHORD PART NUMBER 65-86355-3 AT STATION 783.95
- [SDR VGCA20230213001](https://openairdocs.org/sdr/VGCA20230213001), Feb 13, 2023: FRAME. SCRATCHED. DAMAGED HOLE / DEEP SCRATCH AT THE LOWEST HOLE OF THE INBOARD CHORD OF THE LH FRAME PART NUMBER 65-16326-139 AT STATION 783.95
- [SDR VGCA20201028001](https://openairdocs.org/sdr/VGCA20201028001), Oct 28, 2020: PROXIMITY SENSOR. INTERMITTENT. DURING APPROACH WITH THE GEAR SELECTED DOWN, LEFT GEAR UNSAFE LIGHT ILLUMINATED WITH NO GREEN LIGHT. NOSE AND RIGHT GEAR INDICATE SAFE. DOORS LIGHT INDICATES NO
- [SDR VGCA202009098302](https://openairdocs.org/sdr/VGCA202009098302), Aug 31, 2020: FLOORBEAM. CORRODED. CORROSION ON FLOOR BEAM LOWER FLANGE AT STATION 950D LBL 20.
- [SDR VGCA2020090983101](https://openairdocs.org/sdr/VGCA2020090983101), Aug 31, 2020: SPAR. CORRODED. CORROSION ON WING CENTER SECTION FRONT SPAR LOWER CHORD BETWEEN LBL 3.25 AND RBL 10.25.
- [SDR VGCA20180108001](https://openairdocs.org/sdr/VGCA20180108001), Jan 8, 2018: LOCKING PLATE. CORRODED. WHILE GAINING ACCESS TO PERFORM AD 2008-22-12F, FOUND THE HORIZONTAL STABILIZER HINGE BEARING RETAINER LOCKING PLATE HAD A BROKEN BOLT. REMOVED THE STABILIZER T
- [SDR VGCA20150526001](https://openairdocs.org/sdr/VGCA20150526001), May 26, 2015: WEB. CRACKED. DURING THE UNRELATED ACCOMPLISHMENT OF AD 2014-21-09 PARAGRAPH H DISCOVERED BOTH LT & RT WEB OF ELEVATOR QUADRANT ASSEMBLIES CRACKED. R & R BOTH WEBS.
- [SDR VGCA20150413001](https://openairdocs.org/sdr/VGCA20150413001), Apr 13, 2015: A/C PACK. OVERHEATED. AIR CONDITIONING PACK OVERHEAT.
- [SDR VGCA20140609001](https://openairdocs.org/sdr/VGCA20140609001), Jun 9, 2014: SKIN. DENTED. FUSELAGE SKIN DENTED BETWEEN STATIONS 344 & 351 LT ABOVE STRINGER 19L.
- [SDR VGCA20140605001](https://openairdocs.org/sdr/VGCA20140605001), Jun 5, 2014: SKIN. DAMAGED. SUSPECTED LIGHTNING STRIKE ON RIVET AT STATION 680, STRINGER 3L RESULTING IN FUSELAGE SKIN DAMAGE.
- [SDR VGCA20120521006](https://openairdocs.org/sdr/VGCA20120521006), May 21, 2012: KEELBEAM. CORRODED. CORROSION ON LWR INBD FLANGE OF STR 28R AND 28L FWD OF DELTA KEEL AT STA 740.
- [SDR VGCA20120521005](https://openairdocs.org/sdr/VGCA20120521005), May 21, 2012: FLOORBEAM. CORRODED. CORROSION ON FWD CARGO PIT FLOOR SUPPORT STA 537 RBL8 AND RBL13.
- [SDR VGCA20120521004](https://openairdocs.org/sdr/VGCA20120521004), May 21, 2012: KEEL. CORRODED. CORROSION ON KEEL LT SIDE BESIDE STA 740.
- [SDR VGCA20120521003](https://openairdocs.org/sdr/VGCA20120521003), May 21, 2012: WEB. DAMAGED. DAMAGED FLOOR WEB AT BS 1130, RBL 24 UNDER SEAT TRACK ON MAIN CARGO DECK.
- [SDR VGCA20120521002](https://openairdocs.org/sdr/VGCA20120521002), May 21, 2012: FRAME. CORRODED. CORROSION ON FRAME BS 228 RBL 4 - LBL 4 INSIDE FWD ACCESS FOUND BEYOND LIMITS.
- [SDR VGCA20120521001](https://openairdocs.org/sdr/VGCA20120521001), May 21, 2012: SILL. CORRODED. CORROSION ON MAIN CARGO DOOR SILL.

## STCs that may be installed (OpenAirDocs) (17)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (Pratt & Whitney JT8D-17 series)

- [STC SE2930SO](https://openairdocs.org/stc/SE2930SO): Installation of an alternate gearbox cover seal utilizing an aluminum retainer .040-inch thick with a molded-in-place elastomeric seal contoured to fit the main housing/cover flange interface. Parker O-Seal Division. Lists JT8D Series
- [STC SE497NE](https://openairdocs.org/stc/SE497NE): Installation of oil tank filler neck check valve assembly. Aviation Components Support
- [STC SE3916NM](https://openairdocs.org/stc/SE3916NM): Installation of CADC bleed valve supports brackets, P/N B10002 or RB10003, as a replacement part for P&W P/N 578273. Aeroparts Mfg & Repair. Lists JT8D Series
- [STC SE79WE](https://openairdocs.org/stc/SE79WE): Installation of CADC bleed valve support brackets, P/N B10001 or RB10006, as a replacement part for P&W P/N 493317 used on JT8D-1, -5, -7, -9, -9A, -15 and -17 engines. Aeroparts Mfg & Repair. Lists JT8D Series
- [STC SE00049AT-D](https://openairdocs.org/stc/SE00049AT-D): Installation of Intermediate Compressor Case (JT8D SERIES). Aero Component Technologies. Lists JT8D Series
- [STC SE00048AT-D](https://openairdocs.org/stc/SE00048AT-D): Modification of compressor intermediate case diaphragm to permit acceptable of a 7th stage airseal ring. Aero Component Technologies. Lists JT8D-17A
- [STC SE59GL](https://openairdocs.org/stc/SE59GL): Installation of O-ring face seal P/N-s 1-1337-700, -701, 1-1633-700, -701, 1-1738-700, -701; and/or 1-2233-700, 701. Rexnord, Inc
- [STC SE86WE](https://openairdocs.org/stc/SE86WE): Replace the airoils on P&WA P/Ns 495051, 478351, 583751, 653851, 653951, 572451, 583351, 653751, 653151, 676951, 728951, 709951, 710751, 627751, 737271, 578551, 738271, 747171, 792871, 786471, 583751, 777971, 780591, 782571, 793181, 799771, 794481, 794491 , 798781, and 799191. Chromizing Company
- [STC SE557NE](https://openairdocs.org/stc/SE557NE): Installation of oil tank shuttle valve. Stockbridge William D
- [STC SE2666SO](https://openairdocs.org/stc/SE2666SO): Modification of the anti-ice mount bracket. Cook Airtomic
- [STC SE593NE](https://openairdocs.org/stc/SE593NE): Installation of a Select Controls Inc. Engine Oil Shuttle Valve, P/N 2057-1-001. (See Eligibility List). Basken Valve Corporation. Lists JT8D Series
- [STC SE1930SO](https://openairdocs.org/stc/SE1930SO): Installation of power control shaft bushing. Cook Airtomic Division. Lists JT8D Series
- [STC SE83WE](https://openairdocs.org/stc/SE83WE): Installation of heat shield assembly P/N 408-007 as a replacement part for P&W P/N499941 or 749609 used on JT8D-1, -5, -7, -9, -9A, -15 and -17 engines. Hughes Helicopter. Lists JT8D Series
- [STC SE84WE](https://openairdocs.org/stc/SE84WE): Installation of heat shield assembly 408-008 as a replacement part for P&W No. 586918 used on JT8D-1, -5, -7, -9, -9A, -15 and -17 engines. Hughes Helicopter. Lists JT8D Series
- [STC SE67WE](https://openairdocs.org/stc/SE67WE): Installation of fuel control rod end bearings. Triumph Corporation. Lists JT8D Series
- [STC SA2627WE](https://openairdocs.org/stc/SA2627WE): Installation of fuel control rod end bearings. Triumph Corporation. Lists JT8D Series
- [STC SE5058NM](https://openairdocs.org/stc/SE5058NM): Incorporation of feather seals into platforms of the first stage nozzle guide vanes, P&W P/N 653751, 737271, 738271, 747171, 792871, 786471, and 798771. Chromizing Company

## Related

- Other Boeing 727-2S2F aircraft: https://openairdocs.org/model/boeing-727-2s2f/aircraft.md
- The Pratt & Whitney JT8D-17 series engine: https://openairdocs.org/engine/pratt-whitney-jt8d-17-series.md

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