# N464FE: 1976 Boeing 727-225, registration cancelled 2012-10-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 12, 2012
- Status when cancelled: Valid registration
- Airframe: [Boeing 727-225](https://openairdocs.org/model/boeing-727-225) (registry code 1384077)
- Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 21288
- Year built: 1976
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: November 19, 1976
- Certificate issued: September 22, 1992
- Last registry action: May 3, 2012
- Mode S code: A5A8F9
- Owner when cancelled: [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION)
- Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis)
- Owner type: Corporation
- Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N464FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=464FE
- Page: https://openairdocs.org/deregistered/N464FE-2012-10-12

From the FAA registry file of October 28, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 727-225: https://openairdocs.org/model/boeing-727-225.md

## Service difficulty reports (225, newest 50)

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

- [SDR FDEA201006182051](https://openairdocs.org/sdr/FDEA201006182051), Jun 18, 2010: LINE. LEAKING. LOST "A" SYSTEM HYDRAULICS AT FL 250. ENG 1 & 2 FLUID SHUTOFF CLOSED FOR 30 MINUTES WITH ENGINE NR 1 & 2 OPERATING. FOUND SPOILER HYD FLUID RETURN LINE NEAR WIN
- [SDR FDEA201004131198](https://openairdocs.org/sdr/FDEA201004131198), Apr 13, 2010: RIB. CRACKED. NR 3 SLAT 2ND FROM INBD RIB IS CRACKED AT SLAT STA 128. REMOVED CRACKED RIB, FABRICATED NEW RIB USING 7075-O .032 DIMS 18" X 6", HEAT TREATED TO T6 CONDITION IA
- [SDR FDEA201004041077](https://openairdocs.org/sdr/FDEA201004041077), Apr 4, 2010: STRINGER. DAMAGED. AFT PIT STRINGER HAS DOUBLE DRILLED HOLES STA 970 STR 28L REMOVED PREVIOUS REPAIR SPLICE AND PRODUCTION SPLICE, REMOVED DAMAGED STRINGER SECTION, LOCATED AND DR
- [SDR FDEA201003301031](https://openairdocs.org/sdr/FDEA201003301031), Mar 30, 2010: SKIN. GOUGED. UPON REMOVAL OF INTERCOSTAL FOUND GOUGE IN FUSELAGE SKIN FWD OF BS 970 BTWN STR 30 AND STR 29R. REMOVED GOUGE AND CORROSION AND FOUND OUT OF LIMITS, REMOVED PRE
- [SDR FDEA201003281121](https://openairdocs.org/sdr/FDEA201003281121), Mar 28, 2010: SKIN. DAMAGED. MAIN CARGO AREA STA 660 BETWEEN STR 3L AND 4L NO EDGE DISTANCE ON FASTENERS. CUT OUT DAMAGED AREA DIMS 3" X 3.4", FABRICATED TRIPLER USING 2024T-3 .100 PO 90091
- [SDR FDEA201003271026](https://openairdocs.org/sdr/FDEA201003271026), Mar 27, 2010: FLOORBEAM. DAMAGED. STA 1166 FLOORBEAM HAS DOUBLE DRILLED HOLES LBL 25. CUT OUT DAMAGED AREA, FABRICATED NEW UPPER CHORD USING BAC1505-100617 7075T-73 PO 29103139 DIMS 11 5/8" X 2"
- [SDR FDEA201003271021](https://openairdocs.org/sdr/FDEA201003271021), Mar 27, 2010: SKIN. DAMAGED. RT WING OTBD FORE FLAP, INBD L/E WBL 309 TO WBL 314 HAS 2 DEEP GOUGES FROM CONTACT WITH SPOILER PULLEY BOLTS. GOUGES OUT OF LIMITS IAW SRM 57-50-2 ,CUT OUT 2 DA
- [SDR FDEA201003261016](https://openairdocs.org/sdr/FDEA201003261016), Mar 26, 2010: STRUCTURE. CORRODED. CORROSION ON NOSE WHEEL WELL RT MID-CHORD, REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED CHORD, LOCATED AND DRILLED NEW CHORD PN 65-19862-20 PO 20017288 AN
- [SDR FDEA201003261017](https://openairdocs.org/sdr/FDEA201003261017), Mar 26, 2010: SILL. DAMAGED. C-2 DOOR CUT-OUT LOWER SILL HAS PILLOWING AT BS 970. REMOVED PREVIOUS REPAIR, REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED CHORD IAW SRM 51-30-2, LOCATED 
- [SDR FDEA201003261018](https://openairdocs.org/sdr/FDEA201003261018), Mar 26, 2010: SKIN. CORRODED. CORROSION ON SKIN FROM STA 580 TO 600 BETWEEN STR 27L AND 28L. THIS NR WAS INCOPORATED IN REPAIR.
- [SDR FDEA201003251010](https://openairdocs.org/sdr/FDEA201003251010), Mar 25, 2010: FRAME. CORRODED. C-2 DOOR CUTOUT AFT FRAME BS 990, UPPER FLANGE IS CORRODED WITH EXFOLIATION ON LOWER SURFACE BTWN STR. 26R-25R. REMOVED CORROSION AND FOUND OUT OF LIMITS, CUT O
- [SDR FDEA201003251009](https://openairdocs.org/sdr/FDEA201003251009), Mar 25, 2010: SKIN. DAMAGED. L-1 DOOR LOWER LIGHTNING HOLE INNER SKIN IS DAMAGED. ROUTED OUT DAMAGE ON L-1 DOOR INNER SKIN LIGHTNING HOLE, DIM .1250" IAW SRM 51-10-1, FABRICATED REPAIR DOUB
- [SDR FDEA201003251008](https://openairdocs.org/sdr/FDEA201003251008), Mar 25, 2010: SKIN. CRACKED. L-1 DOOR LOWER LIGHTNING HOLE INNER DOOR SKIN IS CRACKED. ROUTED OUT DAMAGE ON L-1 DOOR INNER SKIN LIGHTNING HOLE DIM .1250" IAW SRM 51-10-1 FABRICATED REPAIR D
- [SDR FDEA201003251007](https://openairdocs.org/sdr/FDEA201003251007), Mar 25, 2010: SKIN. CRACKED. L-1 DOOR LOWER LIGHTNING HOLE INNER DOOR SKIN HAS UNREPAIRED CRACK, STOP DRILLED. ROUTED OUT DAMAGE AT L-1 DOOR LOWER LIGHTNING HOLE INNER DOOR SKIN DIM 3/4" X 
- [SDR FDEA201003241218](https://openairdocs.org/sdr/FDEA201003241218), Mar 24, 2010: SKIN. DAMAGED. FASTENERS WITH IMPROPER SPACING STA 440 STR 10L. CUT OUT DAMAGED AREA DIMS 11" X 9.4", FABRICATED 3 FILLERS USING 2024T-3 .063 DIMS 11" X 6.75", 9.75" X 11" AND
- [SDR FDEA201003240986](https://openairdocs.org/sdr/FDEA201003240986), Mar 24, 2010: SKIN. DAMAGED. C-2 DOOR EXTERIOR SKIN HAS ROUTE OUT GREATER THAN .100" AT FWD LOWER CORNER. CUT OUT DAMAGED AREA DIM 3 1/2" X 1 1/2" ON C-2 DOOR FWD LOWER CORNER OF SKIN IAW S
- [SDR FDEA201003240982](https://openairdocs.org/sdr/FDEA201003240982), Mar 24, 2010: STRINGER. CORRODED. FWD PIT- CORROSION AROUND DOME NUT IN STRINGER 27R AT BS 705. CORROSION OUT OF LIMITS, REMOVED DAMAGED STRINGER, FABRICATED FILLER USING BAC1498-144 7075T-6 PO 
- [SDR FDEA201003241049](https://openairdocs.org/sdr/FDEA201003241049), Mar 24, 2010: SHEAR TIE. CORRODED. CORROSION ON SHEAR TIE AT STA 720C STR'S 28R AND 27R. CORROSION OUT OF LIMITS, REMOVED SHEAR TIE, FABRICATED NEW SHEAR TIE USING 2024T-3 .040 PO NR 9009253 DIMS
- [SDR FDEA201003240988](https://openairdocs.org/sdr/FDEA201003240988), Mar 24, 2010: SUPPORT. CRACKED. CRACK ON SUPPORT ANGLE INSIDE RT ELEVATOR PANEL 9405. REMOVED CRACKED ZEE STIFFENER, FABRICATED NEW ZEE STIFFENER USING 2024T-3 .032 PO NR 9009378 DIMS 18 INCH 
- [SDR FDEA201003240985](https://openairdocs.org/sdr/FDEA201003240985), Mar 24, 2010: SKIN. MISREPAIRED. PREVIOUS REPAIR LOCATED AT STA 1223 STR 23R REQUIRES EVALUATION IAW EO 7-5100-7-5005 PH. REPAIR HAS BLIND FASTENERS INSTALLED. REMOVED BLIND FASTENERS AND INSTA
- [SDR FDEA201003240977](https://openairdocs.org/sdr/FDEA201003240977), Mar 24, 2010: SHEAR TIE. CORRODED. FWD PIT- CORROSION ON SHEAR TIE AT BS 720, AFT SIDE, BETWEEN STRINGERS 28R AND 28L. CORRSION OUT OF LIMITS, REMOVED DAMAGED SHEAR TIE, FABRICATED NEW SHEAR TIE 
- [SDR FDEA201003240987](https://openairdocs.org/sdr/FDEA201003240987), Mar 24, 2010: WEB. CRACKED. FWD CARGO CUTOUT, STA 620, BETWEEN STR 24R AND 25R, CRACKED WEB. CUT OUT DAMAGED SECTION OF WEB, FABRICATED NEW FILLER USING 7075T-6 .071 PO 9009353 DIMS 6" X 4
- [SDR FDEA201003230981](https://openairdocs.org/sdr/FDEA201003230981), Mar 23, 2010: STRINGER. CORRODED. FWD PIT BS 740 STR 27R IS CORRODED AT AFT END. CORROSION OUT OF LIMITS, CUT OUT DAMAGED STRINGER SECTION, FABRICATED NEW STRINGER SECTION USING BAC1498-147 7075
- [SDR FDEA201003230983](https://openairdocs.org/sdr/FDEA201003230983), Mar 23, 2010: SHEAR TIE. CORRODED. FWD PIT- CORROSION ON SHEAR TIE AT BS 720A (FWD SIDE) BETWEEN STRINGERS 28L AND 27L. REMOVED CORROSION ON SHEAR TIE, FWD SIDE BS 720A BETWEEN STRINGERS 28L AND 
- [SDR FDEA201003230984](https://openairdocs.org/sdr/FDEA201003230984), Mar 23, 2010: SHEAR TIE. CORRODED. FWD PIT- CORROSION ON SHEAR TIE AT BS 720B, BETWEEN STRINGERS 28L AND 27L. REMOVED CORROSION ON SHEAR TIE BS 720B BETWEEN STR 28L AND 27L. ORIGINAL THICKNESS .0
- [SDR FDEA201003230966](https://openairdocs.org/sdr/FDEA201003230966), Mar 23, 2010: STRINGER. CORRODED. FWD PIT STA 564 STRINGER 26L CORRODED. CUT OUT DAMAGED STRINGER DIMS 19" X 3" IAW SRM 53-10-3, FABRICATED FILLER USING BAC1498-140 7075T-6 PO 2910023 DIMS 19" X
- [SDR FDEA201003230972](https://openairdocs.org/sdr/FDEA201003230972), Mar 23, 2010: SHEAR TIE. CORRODED. FWD PIT - CORROSION ON SHEAR TIE AT BS 720A, FWD SIDE, BETWEEN STRINGERS 26R AND 25R. CORROSION OUT OF LIMITS, REMOVED DAMAGED SHEAR TIE, FABRICATED NEW SHEAR T
- [SDR FDEA201003230969](https://openairdocs.org/sdr/FDEA201003230969), Mar 23, 2010: WEB. GOUGED. MCD CUTOUT INNER WEB IS GOUGED IN SEVERAL SPOTS FROM BS 620 - 640 BTWN STR 4L-5L. REMOVED INNER SKIN AND 2 EACH SPLICER TO MAIN CARGO DOOR AFT UPPER AREA IAW SR
- [SDR FDEA201003230967](https://openairdocs.org/sdr/FDEA201003230967), Mar 23, 2010: SHEAR TIE. CORRODED. FWD PIT - CORROSION ON SHEAR TIE AT BS 585, BETWEEN STRINGERS 27R AND 26R - MARKED. REMOVED FRAME TO BS 585 BETWEEN STR 27R AND 26R IAW SRM 51-30-2 FABRICATED N
- [SDR FDEA201003220980](https://openairdocs.org/sdr/FDEA201003220980), Mar 22, 2010: STRINGER. CORRODED. FWD PIT- STRINGER 26R IS CORRODED AT BS 740. CORROSION OUT OF LIMITS, CUT OUT DAMAGED STRINGER SECTION, FABRICATED NEW STRINGER SECTION USING BAC1498-147 7075T-
- [SDR FDEA201003210970](https://openairdocs.org/sdr/FDEA201003210970), Mar 21, 2010: ANGLE. CRACKED. LT WING T/E FALSE SPAR CHORD ANGLE CRACKED WBL 118. TRIMMED OUT DAMAGE, FABRICATED NEW INBD WEB SECTION USING 7075T-6 .032 PO NR 9009201 DIMS 12 1/8 INCH BY 9 1
- [SDR FDEA201003201152](https://openairdocs.org/sdr/FDEA201003201152), Mar 20, 2010: SKIN. DAMAGED. FASTENERS WITH IMPROPER SPACING STA 440, STRINGER 19L. CUT OUT DAMAGED AREA, HFEC INSPECTED CUT OUT AND EXISTING HOLES WITH NO DEFECTS NOTED IAW NDTM 51-00-00. 
- [SDR FDEA201003201025](https://openairdocs.org/sdr/FDEA201003201025), Mar 20, 2010: FLANGE. CORRODED. SURFACE CORROSION ON FUSELAGE STRUCTURE FLANGE AND MONTING BRACKETS FOR FUSELAGE PANEL AFT OF NWW STA 351. CORROSION OUT OF LIMITS, REMOVED, LOCATED AND DRILLED
- [SDR FDEA201003201024](https://openairdocs.org/sdr/FDEA201003201024), Mar 20, 2010: STRUCTURE. CORRODED. AFT CARGO BS 950 LOWER CHORD ANGLE IS CORRODED WITH EXFOLIATION BTWN STR 29L- STR 28L. CORROSION OUT OF LIMITS, REMOVED CHORD, LOCATED AND DRILLED NEW CHORD PAR
- [SDR FDEA201003200979](https://openairdocs.org/sdr/FDEA201003200979), Mar 20, 2010: ANGLE. CORRODED. FWD PIT- 740 BULKHEAD LOWER CHORD ANGLE IS CORRODED BETWEEN STRINGERS 28R AND 27R. REMOVED DAMAGED ANGLE SUPPORT IAW SRM 51-30-2, FABRICATED ANGLE SUPPORT USING
- [SDR FDEA201003191191](https://openairdocs.org/sdr/FDEA201003191191), Mar 19, 2010: SKIN. MISREPAIRED. FASTENERS WITH IMPROPER SPACING FWD PIT STA 540, STR 27L CUT OUT DAMAGED AREA THRU SKIN MCD STA 540 STR 27L IAW SRM 53-30-3, FIG 1B FABRICATED STRUCTURAL FILLER
- [SDR FDEA201003190963](https://openairdocs.org/sdr/FDEA201003190963), Mar 19, 2010: STRINGER. CORRODED. AFT PIT- CORROSION IN STRINGER 27L FROM BS 1005 TO 1010.
- [SDR FDEA201003190935](https://openairdocs.org/sdr/FDEA201003190935), Mar 19, 2010: SEAT TRACK. CORRODED. SEAT TRACK CORRODED BS 1142-1165 BL0. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION USING 7075T6510, DIMS 44.7500 INCHES LONG IA
- [SDR FDEA201003180881](https://openairdocs.org/sdr/FDEA201003180881), Mar 18, 2010: SKIN. CRACKED. LT OTBD FOREFLAP, CARRIAGE ATTACH FITTING WBL 348 AREA, CUTOUT, SKIN FWD OF FITTING CRACKED. TRIMMED OUT DAMAGED AREA (DIM: .2500"X.2500") IAW SRM 51-10-1. FABR
- [SDR FDEA201003180960](https://openairdocs.org/sdr/FDEA201003180960), Mar 18, 2010: STRUCTURE. CRACKED. AFT A/S LOWER TORQUE BOX LIGHTENING HOLE CRACKED LT SIDE BS 1326.
- [SDR FDEA201003180902](https://openairdocs.org/sdr/FDEA201003180902), Mar 18, 2010: ANGLE. CRACKED. NR 7 SLAT LOWER T/E CHORD ANGLE REPAIR DOUBLER AT INBD UPSTOP PAD IS CRACKED. REMOVED NR 7 SLAT T/E CHORD IAW SRM 57-30-2. LOCATED AND DRILLED NEW T/E CHORD. BA
- [SDR FDEA201003180928](https://openairdocs.org/sdr/FDEA201003180928), Mar 18, 2010: SKIN. MISREPAIRED. PREVIOUS REPAIR LOCATED AT STA 390 STR 25L REQUIRES EVALUATION IAW EO 7-5100-7-5005 PT1. EVALUATION DETERMINED THE EXISTING REPAIR REQUIRES REPLACEMENT. REMOVED
- [SDR FDEA201003180927](https://openairdocs.org/sdr/FDEA201003180927), Mar 18, 2010: STRINGER. PUNCTURED. FWD CARGO AREA, BS 520, STR 21L, STRINGER HAS PUNCTURE. CUT OUT DAMAGED STRINGER DIMS 14" X 3", FABRICATED FILLER USING BAC1498-140 7075T-6. PO NR 2910023 DIMS 
- [SDR FDEA201003180926](https://openairdocs.org/sdr/FDEA201003180926), Mar 18, 2010: STRINGER. DAMAGED. FWD CARGO AREA, BS 600, STR 21L, STRINGER HAS DOUBLE DRILLED HOLE. CUT OUT DAMAGED STRINGER DIMS 13" X 3", FABRICATED FILLER USING BAC1498-140 7075T-6 PO NR 291
- [SDR FDEA201003180925](https://openairdocs.org/sdr/FDEA201003180925), Mar 18, 2010: TRIPLER. MISMANUFACTURED. MCD TRIPLER HAS NUMEROUS FASTENERS WITH IMPROPER SPACING STA 460 STR'S 22L TO 24L. CUT OUT DAMAGED AREAS DIM (13.6250 X 2.7500") AND (2.2500" X 1.7500") IAW PF 
- [SDR FDEA201003180921](https://openairdocs.org/sdr/FDEA201003180921), Mar 18, 2010: SKIN. MISMANUFACTURED. FASTENERS WITH IMPROPER SPACING FWD PIT STA 675 STR 25L. CUT OUT DAMAGE AREA THRU SKIN TO STA 675 STR 25L IAW SRM 51-10-1. FABRICATED REPAIR PARTS STRUCTURAL FI
- [SDR FDEA201003180920](https://openairdocs.org/sdr/FDEA201003180920), Mar 18, 2010: SKIN. MISMANUFACTURED. FASTENERS WITH IMPROPER SPACING SKIN FWD PIT STA 600 STR 27L. CUT OUT DAMAGE AREA THRU SKIN STA 600 STR 27L-28L IAW B727 PF 53-30-3 FIG 1B. FABRICATED REPAIR PA
- [SDR FDEA201003180919](https://openairdocs.org/sdr/FDEA201003180919), Mar 18, 2010: SKIN. MISMANUFACTURED. FASTENERS WITH IMPROPER SPACING FWD PIT STA 620 STR 27L. CUT OUT DAMAGED AREAS, FABRICATED REPAIR DOUBLER USING 2024T-3 .080 DIMS 89" X 29.5", TRIPLER USING 202
- [SDR FDEA201003180918](https://openairdocs.org/sdr/FDEA201003180918), Mar 18, 2010: SKIN. MISMANUFACTURED. FASTENERS WITH IMPROPER SPACING FWD PIT STA 640 STR 27L. CUT OUT DAMAGE AREA TO SKIN STA 640 STR 27L. FABRICATED STRUCTURAL FILLER, DOUBLER AND TRIPLER IAW SRM 
- [SDR FDEA201003180917](https://openairdocs.org/sdr/FDEA201003180917), Mar 18, 2010: SKIN. MISMANUFACTURED. FASTENERS WITH ZERO ED FWD PIT STA 680 STR 22L.

All 225: https://openairdocs.org/deregistered/N464FE-2012-10-12/reports.md

## FAA accident and incident reports (2)

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 20081023849569I](https://openairdocs.org/incident/20081023849569I), Oct 23, 2008: Boeing 727225 (N464FE), Wichita, KS, No damage. (-23) On October 23, 2008, at 23:37 local time the flight crew for federal express corp operating a Boeing 727 as flight number FDC1305 departed Wichita,…
- [Incident 20041027026589I](https://openairdocs.org/incident/20041027026589I), Oct 27, 2004: Boeing 727225 (N464FE), Kansas City, MO. (-23) On October 27, 2004 federal express flight 1336 a 727-225A aborted its takeoff roll at about 60 kt due to an unknown problem (a loud mechanical noise).…

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