# N134FE: 1968 Boeing 727-25C, registration cancelled 2002-10-15 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 15, 2002 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 727-25C](https://openairdocs.org/model/boeing-727-25c) (registry code 138400H) - 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) (OpenAirDocs) - Serial number: 19852 - Year built: 1968 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: April 8, 1982 - Certificate issued: July 2, 1980 - Last registry action: September 19, 2000 - Mode S code: A08A8F - 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/N134FE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=134FE - Page: https://openairdocs.org/deregistered/N134FE-2002-10-15 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 727-25C: https://openairdocs.org/model/boeing-727-25c.md ## Service difficulty reports (21) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 00FDEA00007](https://openairdocs.org/sdr/00FDEA00007), Jan 5, 2000: WARNING LIGHT. ILLUMINATED. 00-7 - AFTER T/O, NR 1 HYD SYS A PUMP LIGHT FLICKERED. HYD SYS 'A' QUANTITY WENT TO ZERO. REMOVED AND REPLACED BOTH CASE DRAIN FILTERS NO METAL FOUND PER 727-10 - [SDR 97FDEA00826](https://openairdocs.org/sdr/97FDEA00826), Nov 11, 1997: KEEL BEAM. CORRODED. WHILE WORKING NR 0091 FOUND CORROSION AT KEEL BEAM VERTICAL FLANGE BS 874, RBL 6.5, WL 142. *S/D* REPAIRED KEEL BEAM VERTICAL FLANGE BS 874, RBL 6.5, WL 142 IAW - [SDR 97FDEA00825](https://openairdocs.org/sdr/97FDEA00825), Nov 11, 1997: KEEL BEAM. CORRODED. CORROSION ON KEEL BEAM STR 29 LT, BS 1066, WL 148. *S/D* REPAIRED KEEL BEAM STR 29 LT, BS 1060 TO 1080, WL 148 PER FED-EX EA 7-5310-36873. - [SDR 97FDEA00796](https://openairdocs.org/sdr/97FDEA00796), Oct 31, 1997: FITTING. CRACKED. AFT CARGO DOOR BOTTOM FWD STOP PIN FITTING IS CRACKED ON THE LOWER FLANGES. *S/D* REMOVED AND INSTALLED NEW AFT CARGO DOOR BOTTOM FORWARD STOP FITTING. ALL WORK - [SDR 97FDEA00723](https://openairdocs.org/sdr/97FDEA00723), Oct 10, 1997: INTERCOSTAL. CRACKED. AFT CARGO DOOR FWD HINGE ARM MOUNT INTERCOSTAL IS CRACKED AT MOUNT UPPER ATTACH BOLT. *S/D* REMOVED FWD HINGE ARM AND INTERCOSTAL. DRILLED REPLACEMENT INTERCOST - [SDR 97FDEA00715](https://openairdocs.org/sdr/97FDEA00715), Oct 7, 1997: BEAM. CRACKED. AFT CARGO DOOR NR 5 TRANSVERSE BEAM HAS TWO CRACKS IN OUTBD RADIUS; ONE APPROX .5 LONG THE OTHER APPROX 1.5 LONG. *S/D* REMOVED AND INSTALLED NEW AFT CARGO DOOR - [SDR 97FDEA00714](https://openairdocs.org/sdr/97FDEA00714), Oct 7, 1997: FLOORBEAM. CORRODED. CORROSION (C53-224-08) ON FLOORBEAM UNDER NUT PLATE BS 1150, LBL 58, WL 208. *S/D* FABRICATED AND INSTALLED REPAIR PARTS FOR FLOORBEAM AT BS 1130, LBL 60, WL 20 - [SDR 97FDEA00713](https://openairdocs.org/sdr/97FDEA00713), Oct 7, 1997: SKIN. CORRODED. DURING ROUTINE LFEC INSP, NOTED AREA OF GREATER THAN 10 PERCENT MATERIAL LOSS IN FWD SKIN BS 441 CIRCUMFERENTIAL BUTT SPLICE, BETWEEN STR 3R AND 4R (MARKED IN R - [SDR 97FDEA00706](https://openairdocs.org/sdr/97FDEA00706), Oct 6, 1997: BULKHEAD WEB. CRACKED. EVIDENCE OF A CRACK AT FASTENER FWD SIDE OF BS 178 PRESSURE BULKHEAD WL 236, RBL 10. *S/D* REPAIRED DAMAGED PRESSURE BULKHEAD BS 178, WL 236, RBL 10 PER FED-EX - [SDR 97FDEA00705](https://openairdocs.org/sdr/97FDEA00705), Oct 3, 1997: SHEAR TIE. CRACKED. CRACKED SHEAR TIE AT BS 990 I/B SIDE OF LT KEEL BEAM WL 138. *S/D* REMOVED DAMAGE, FABRICATED REPAIR PARTS, ALODINED, PRIMED AND INSTALLED PER FED-EX SRM 51-30- - [SDR 96FDEA01605](https://openairdocs.org/sdr/96FDEA01605), Oct 24, 1996: INDICATION. MALFUNCTIONED. ON INITIAL LANDING GEAR EXTENSION, NOSE GEAR DID NOT INDICATE DOWN AND LOCKED. RAN CHECK LIST AFTER GO AROUND ON SECOND EXTENSION INDICATED DOWN AND LOCKED. NOS - [SDR 96FDEA01474](https://openairdocs.org/sdr/96FDEA01474), Sep 13, 1996: CONNECTOR. DIRTY. ON FLAP RETRACTION FROM 2 DEGREES TO 0 DEGREES THE AMBER LEADING EDGE FLAP LIGHT REMAINED ON. SECOND OFFICER'S AUXILIARY PANEL POSITION INDICATOR SHOWED THAT TH - [SDR 95FDEA00852](https://openairdocs.org/sdr/95FDEA00852), Jun 21, 1995: CASTING. CRACKED. LIGHT CORROSION ON HEAVY CARGO DOOR CASTING STA 620 ON UNDERSIDE OF LEG, AFT SIDE OF 620 INCLUDING CORRODED GOUGE. HFEC'D AREA, APPROXIMATELY A 1.50 INCH CRACK, - [SDR 95FDEA00855](https://openairdocs.org/sdr/95FDEA00855), Jun 20, 1995: FLOORBEAM. CORRODED. FS 344 LBL 6-14 CORROSION ON TOP LEG OF FLOORBEAM. INSTALLED FLOORBEAM CAP PER 53-10-8. - [SDR 95FDEA00858](https://openairdocs.org/sdr/95FDEA00858), Jun 8, 1995: FITTING. CRACKED. MAIN CARGO DOOR AFT CAM SUPPORT FITTING CRACKED. REPLACED FITTING WITH 65-26680-5 IN PLACE OF ORIGINAL - 3 FITTINGS OBSOLETE PER EA NR 7-5230-25056. - [SDR 95FDEA00857](https://openairdocs.org/sdr/95FDEA00857), Jun 8, 1995: FITTING. CRACKED. RIGHT STA 870 CRACK ABOVE STR 10 EXTENDING UNDER SPLICE PLATE - AFT SIDE OF 870 FORGING. REPAIRED BS 870 TERMINAL FITTING AS PER BOEING SB 727-53-0. - [SDR 95FDEA00856](https://openairdocs.org/sdr/95FDEA00856), Jun 7, 1995: FLOOR BEAM. CORRODED. CORROSION ON TOP OF LEG ON FLOORBEAM (TOP LEG) STA 480 RBL 18-20. BLENDED OUT CORROSION ON TOP LEG OF FLOORBEAM, BLENDED OUT AREA 2.0 INCHES X .75 INCH WIDE, AT - [SDR 95FDEA00854](https://openairdocs.org/sdr/95FDEA00854), Jun 7, 1995: SPAR WEB. CORRODED. CENTER WING BOX AFT SPAR WEB SKIN AT UPPER CHORD HAS FOUR EACH FASTENERS WITH POPPED HEADS AND ONE READY TO POP, TOTAL FIVE. WEB SKIN IS BULGED AT APPROX RBL 50 - [SDR 95FDEA00853](https://openairdocs.org/sdr/95FDEA00853), Jun 7, 1995: FLOOR BEAM. CORRODED. FS 360 RBL 19-20. CORROSION ON FLOORBEAM AROUND FLOORBOARD ATTACH SCREW HOLE. REPAIRED PER AA ESO 11782 FEDEX EA NR 7-5310-25029. - [SDR 95FDEA00851](https://openairdocs.org/sdr/95FDEA00851), Jun 7, 1995: FLOOR BEAM. CORRODED. CORROSION ON TOP OF FLOORBEAM AROUND FLOORBOARD ATTACH SCREW HOLE, BS 360 RBL 20-22. BLENDED OUT CORROSION ON TOP LEG OF FLOORBEAM. BLEND OUT AREA IS 2.0 INCHES - [SDR 95FDEA00850](https://openairdocs.org/sdr/95FDEA00850), Jun 6, 1995: FITTING. CRACKED. UPPER LOBE CARGO DOOR: CARGO DOOR AFT CAM SUPPORT FITTING CRACKED BETWEEN 2ND AND 3RD RIVET IN WEB AT INBD ROW OF FASTENERS. REMOVED AND REPLACED CASTING PER ES ## Other aircraft with N134FE - [Registered now](https://openairdocs.org/aircraft/N134FE): Boeing 767-3S2F, S/N 43550, built 2016 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.