# N267FE: 1979 Boeing 727-233, registration cancelled 2012-10-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 12, 2012
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 727-233](https://openairdocs.org/model/boeing-727-233) (registry code 138408A)
- Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs)
- Serial number: 21673
- Year built: 1979
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: February 9, 2005
- Certificate issued: January 28, 2005
- Last registry action: January 15, 2008
- Mode S code: A29980
- Owner when cancelled: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP)
- 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/N267FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=267FE
- Page: https://openairdocs.org/deregistered/N267FE-2012-10-12

From the FAA registry file of October 29, 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 727-233: https://openairdocs.org/model/boeing-727-233.md

## Service difficulty reports (121, newest 50)

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

- [SDR FDEA201205031738](https://openairdocs.org/sdr/FDEA201205031738), May 3, 2012: LIGHT. DETACHED. EMERGENCY LIGHT OVER COCKPIT DOOR CAME UNATTACHED FROM ATTACHMENT ON TAKE OFF ROLL. REINSTALLED COCKPIT EMERGENCY LIGHT ASSY IAW MM 33-50-001-2-0. OPS CHECKED N
- [SDR FDEA201006152020](https://openairdocs.org/sdr/FDEA201006152020), Jun 15, 2010: STRINGER. CORRODED. CORROSION IN CHANNEL -STRINGER 27L, STA 950 - 950C. CUT OUT SECTION OF STRINGER 27L FROM BS 950A PLUS 10" TO 950C PLUS 10", 38 3/4" IN LENGTH, IAW SRM, REV 103,
- [SDR FDEA201006142002](https://openairdocs.org/sdr/FDEA201006142002), Jun 14, 2010: RIB. GOUGED. UPON REMOVAL OF NO. 7 SLAT, FOUND OB END CAP RIB CHAFFED AND GOUGED, EXTERIOR SURFACE. REMOVED DAMAGE OB RIB AND FABRICATED NEW RIB FROM 2024O .040 HEATED TREAT
- [SDR FDEA201006142000](https://openairdocs.org/sdr/FDEA201006142000), Jun 14, 2010: RIB. GOUGED. UPON REMOVAL OF NR 7 SLAT FOUND IB END CAP RIB CHAFED AND GOUGED, EXTERIOR SURFACE REMOVED DAMAGED IB RIB, FABRICATED NEW RIB FROM 2024O .040 APPROX DIM: 15 3/4
- [SDR FDEA201006121972](https://openairdocs.org/sdr/FDEA201006121972), Jun 12, 2010: SKIN. DAMAGED. UPON REMOVAL OF BLIND FASTENER AT BS 950E, AT STRINGER 26L TO 25L, FOUND DOUBLE DRILLED HOLE. CUT OUT DAMAGED AREA OF SKIN, DIMENSIONS 4" X 4" IAW SRM 53-30-3 F
- [SDR FDEA201006101937](https://openairdocs.org/sdr/FDEA201006101937), Jun 10, 2010: WEB. CRACKED. AFT AIRSTAIRS RT LOWER TORQUE BOX WEB AT BS 1243 HAS UPPER LIGHTNING HOLE CRACKED. CUTOUT DAMAGED AREA APPROX DIM: 5/8" X 3/8", FABRICATED REPAIR DOUBLER FROM 7
- [SDR FDEA201006101936](https://openairdocs.org/sdr/FDEA201006101936), Jun 10, 2010: WEB. CRACKED. AFT AIRSTAIR RT LOWER TORQUE BOX WEB AT BS 1243 HAS LOWER LIGHTNING HOLE CRACKED. CUTOUT DAMAGED AREA APPROX DIM: 5/8" X 3/8", FABRICATED REPAIR DOUBLER FROM 70
- [SDR FDEA201006101946](https://openairdocs.org/sdr/FDEA201006101946), Jun 10, 2010: SHEAR TIE. CRACKED. CRACKED SHEAR TIE - STA 950E AT STR 26L. REMOVED SHEAR TIE 26L IAW SRM, REV 103, 51-30-2. FABRICATED SHEAR TIE USING BAC1505-100261 7075-T6511, 7 3/8" LONG IAW 
- [SDR FDEA201006091908](https://openairdocs.org/sdr/FDEA201006091908), Jun 9, 2010: STRINGER. CRACKED. RT WING, WS 629 STR 9 HAS A CRACK. STOP DRILLED CRACK DIM: .0187" IAW EO 7-5710-7-4322 PART 1. FABRICATED REPAIR ANGLES FROM AND10134-2001 7075T6 DIM: 10.6" X 2
- [SDR FDEA201006091917](https://openairdocs.org/sdr/FDEA201006091917), Jun 9, 2010: SKIN. CORRODED. CORROSION IN SKIN BS 600, STR 28L. CUTOUT DAMAGED AREA APPROX DIM: 2.5" X 1" AND FABRICATED REPAIR DOUBLER FROM 2024T3 .100 APPROX DIM: 8 3/4" X 12 5/8". INSTAL
- [SDR FDEA201006081873](https://openairdocs.org/sdr/FDEA201006081873), Jun 8, 2010: SEAT TRACK. CORRODED. CORROSION SEAT TRACK SECTION BS 1130-BS 1176, RBL 25. REMOVED CORRODED SEAT TRACK AT BS 1130 - BS 1176 RBL 25 IAW SRM 51-30-2 FOUND CORROSION OUT- OF-LIMITS IAW
- [SDR FDEA201006081871](https://openairdocs.org/sdr/FDEA201006081871), Jun 8, 2010: SKIN. GOUGED. MAIN CARGO AREA, MAIN CARGO INNER SKIN, BS 620 - 640, STR 4L GOUGED. REMOVED DAMAGE MAIN CARGO DOOR INNER SKIN FROM BS 594- BS 642 STR 9L - STR 4L, FABRICATED N
- [SDR FDEA201006081900](https://openairdocs.org/sdr/FDEA201006081900), Jun 8, 2010: INTERCOSTAL. CORRODED. CORROSION IN STR 28L AT BS 600. CUTOUT DAMAGED AREA APPROX DIM: 17" IN LENGTH, AND FABRICATED NEW STRINGER SECTION FROM BAC 1498-141 APPROX DIM: 17" IN LENGTH A
- [SDR FDEA201006071859](https://openairdocs.org/sdr/FDEA201006071859), Jun 7, 2010: SKIN. CORRODED. CORROSION ON SKIN UNDER INTERCOSTAL AT BS 970 BETWEEN STR 28L AND 27L. CUT OUT DAMAGE, 15 1/4" X 2 7/8" ON SKIN AT BS 950E TO 970 BETWEEN STRINGER 28L AND 27L I
- [SDR FDEA201006051840](https://openairdocs.org/sdr/FDEA201006051840), Jun 5, 2010: FLOORBEAM. CORRODED. CORROSION TOP OF FLOORBEAM MAIN CABIN BS 620 BETWEEN LBL 25 - LBL 45. CUT-OUT DAMAGED AREA AT TOP OF FLOOR BEAM BS 620 LBL 25 -LBL 45 APPROX DIM: 3" 5/8 X 1". F
- [SDR FDEA201006051839](https://openairdocs.org/sdr/FDEA201006051839), Jun 5, 2010: FLOORBEAM. CORRODED. CORROSION FLOORBEAM TOP FLANGE BS 1130, RBL 35. CUT-OUT DAMAGED AREA APPROX DIM: 3" X 1" 1/4, FABRICATED REPAIR PARTS, ANGLE APPROX DIM 11" 1/8 X 3", FABRICATED
- [SDR FDEA201006041825](https://openairdocs.org/sdr/FDEA201006041825), Jun 4, 2010: FITTING. CORRODED. CORROSION ON LOWER CHORD AT BS 950, STRINGER 30. REMOVED LOWER CHORD SPLICE AT BS950, BL 0, IAW SRM, REV 103, 51-30-2. LOCATED, DRILLED AND DEBURRED LOWER CHORD
- [SDR FDEA201006041821](https://openairdocs.org/sdr/FDEA201006041821), Jun 4, 2010: STRINGER. CORRODED. CORROSION ON STR 27L BETWEEN BS 950F AND 970. REMOVED SECTION OF STRINGER 38 1/2" IN LENGTH IAW B727 SRM, REV 103, 53-10-3 FIG 1. FABRICATED (2)EA. STRINGER SEC
- [SDR FDEA201006031833](https://openairdocs.org/sdr/FDEA201006031833), Jun 3, 2010: SKIN. DAMAGED. MAIN CARGO AREA, BS 660, BETWEEN STR 3L -4L. FASTENERS WITH NO SPACING. DAMAGED AT TEAR STRAP AND SKIN BS 660 STR 3L - 4L DIM: 3" X 2" 1/2 - 2" 1/2 X 1". FABRIC
- [SDR FDEA201006031812](https://openairdocs.org/sdr/FDEA201006031812), Jun 3, 2010: STRINGER. CORRODED. CORROSION ON STRINGER 29L, FROM BS 950B TO 950C. REMOVED FASTENERS IAW SRM 51-30-2. REMOVED CORROSION FROM STR 29L IAW SRM 51-10-6. UT INSPECTED AREA IAW NDTM 5
- [SDR FDEA201006031810](https://openairdocs.org/sdr/FDEA201006031810), Jun 3, 2010: ANGLE. CRACKED. RT WING INBD MID FLAP LOWER T/E CHORD ANGLE IS CRACKED, 2 PLACES, WBL 100. R & R DUE TO DELAMINATION ON SNRM NR N00544, WO NR00048343.
- [SDR FDEA201006031809](https://openairdocs.org/sdr/FDEA201006031809), Jun 3, 2010: STRUCTURE. CRACKED. NR 7 SLAT T/E CHORD CRACKED AT INBD UP STOP. REMOVED NR 7 SLAT LOWER CHORD IAW SRM 51-30-2. FABRICATED NEW CHORD USING BAC1514-1559, 2024-T3511, 113.7500", IAW 
- [SDR FDEA201006031801](https://openairdocs.org/sdr/FDEA201006031801), Jun 3, 2010: SEAT TRACK. CORRODED. CORROSION SEAT TRACK FLANGE MAIN CABIN BS 680 TO BS 620, LBL 45. REMOVED DAMAGED SEAT TRACK SECTION FROM BS 480 - 690 LBL 45 AND FABRICATED NEW SEAT TRACK SECTI
- [SDR FDEA201006021802](https://openairdocs.org/sdr/FDEA201006021802), Jun 2, 2010: STRUCTURE. CORRODED. CORROSION AT REINFORCEMENT CHORD, BS 1176, MAIN CABIN, LBL 46. REMOVED REINFORCEMENT CHORD BS 1176, LBL 46, IAW SRM 51-30-2 AND FABRICATED NEW REINFORCEMENT CHO
- [SDR FDEA201006011764](https://openairdocs.org/sdr/FDEA201006011764), Jun 1, 2010: FITTING. CORRODED. CORROSION BS 740 FITTING EXTERIOR FUSELAGE KEELBEAM AREA LBL 10. REMOVED KEEL BEAM FITTING AT BS 740 LBL 10 IAW SRM 51-30-2 REV 103 AND FABRICATED FITTING FROM 
- [SDR FDEA201006011758](https://openairdocs.org/sdr/FDEA201006011758), Jun 1, 2010: STRINGER. CRACKED. CRACK AFT END OF STRINGER 27L AT BS 740, AC DISTRIBUTION COMPARTMENT. CUT OUT DAMAGED SECTION OF STR 27L AT BS 740, 11.5" LONG IAW SRM, REV 103, 53-10-3 FIG 1. 
- [SDR FDEA201005311747](https://openairdocs.org/sdr/FDEA201005311747), May 31, 2010: ANGLE. CRACKED. CRACKED ANGLE CHORD FALSE SPAR AT NR 8 SPOILER ACTUATOR ATTACH FITTING. CUT OUT DAMAGED SECTION OF WEB, 9.5" IAW DWG SR27-57-038, REV C. FABRICATED NEW DOUBLER 
- [SDR FDEA200911133948](https://openairdocs.org/sdr/FDEA200911133948), Nov 13, 2009: ACTUATOR. LEAKING. COMPLETE LOSS OF SYS A HYDRAULICS DURING FLAP RETRACTION. FOUND ACTUATOR ABOVE TAIL SKID LEAKING OUT OF THE HSG. ORDERING NEW ACTUATOR. R&R TAIL SKID ACTUATOR P
- [SDR 08FDEA00336](https://openairdocs.org/sdr/08FDEA00336), Jan 31, 2008: FLOORBEAM. DAMAGED. MAIN DECK FLOORBEAM, UPPER CHORD FWD FLG, IS MISDRILLED, BS 480, LBL 62, WL 208 ACCOMPLISHED HFEC, NO DEFECTS NOTED. APPLIED SEALANT TO AFFECTED HOLE. REF FED E
- [SDR 08FDEA00333](https://openairdocs.org/sdr/08FDEA00333), Jan 30, 2008: SKIN. DENTED. AFT LOWER EXTERIOR FUSELAGE, SKIN CREASED WITH SMALL GOUGE, STA 1183 5", 2" BELOW STR 20L. REMOVED DAMAGE AREA OF SKIN. HFEC CUTOUT, NO DEFECTS NOTED. FABRICATE
- [SDR 08FDEA00330](https://openairdocs.org/sdr/08FDEA00330), Jan 30, 2008: CHANNEL. CRACKED. MAIN CARGO DOOR SILL, HAT CHANNEL, ATTACHED TO FLOORBEAM HAS A CRACK AT FASTENER HOLE AS MARKED, LOCATED AT STA 540 8", LBL 61", WL 208". REPLACED DAMAGED HAT C
- [SDR 08FDEA00279](https://openairdocs.org/sdr/08FDEA00279), Jan 25, 2008: FLOORBEAM. CORRODED. CORROSION ON LOWER AFT SIDE OF FLOORBEAM TO CAP AT FLOORBOARD ATTACH FWD HOLE AT FS 720D, LBL 48, WL 208. REMOVED CORROSION AND FLOORBEAM WAS FOUND TO BE OUT OF
- [SDR 08FDEA00277](https://openairdocs.org/sdr/08FDEA00277), Jan 25, 2008: SKIN. CRACKED. CRACK IN UPPER RIGHT WING OUTBD PANEL AT WBL 602.5, OF OUTBD AILERON REPAIRED UPPER WING OUTBD. PANEL AT WBL 602.5 REF EA NR 7-5720-113964. THIS IS CLASSIFIED A
- [SDR 08FDEA00257](https://openairdocs.org/sdr/08FDEA00257), Jan 24, 2008: ANGLE. CORRODED. CORROSION AT SEVERAL AREAS ON AFT WALL GILL LINER PANEL FRAME AT STA 1166 AROUND CAMLOC RECEPTACLE HOLES FRONT AND BACK SIDE. LOWER AFT CARGO COMPARTMENT REMOVE
- [SDR 08FDEA00241](https://openairdocs.org/sdr/08FDEA00241), Jan 23, 2008: RIB. CRACKED. LT WING, FWD SPAR, STA 467, LE RIB, UPPER RADIUS CRACKED. REMOVED BLEED AIR DUCT TO GAIN ACCESS. REMOVE WEB AT STA 467 ON FWD SPAR. FABRICATED WEB REF BAC DWG 6
- [SDR 08FDEA00240](https://openairdocs.org/sdr/08FDEA00240), Jan 23, 2008: BRACKET. CRACKED. RT WING O/B MOST UPPER TRAILING EDGE PANEL I/B SIDE SPOILER SEAL BRACKET CRACKED AT AFT EDGE AND AT SPOILER DOWN STOP PAD CUTOUT. REMOVED CRACKED BRACKET AND FA
- [SDR 08FDEA00239](https://openairdocs.org/sdr/08FDEA00239), Jan 23, 2008: FRAME. CORRODED. LWR FWD CARGO PIT FRAME UPPER FLANGE HAS SURFACE CORROSION, AFT SIDE STA. 720D ABOVE STR 26R. FOUND FRAME TO BE OUT OF LIMITS. CUT OUT DAMAGE AND REPAIRED FRAME
- [SDR 08FDEA00238](https://openairdocs.org/sdr/08FDEA00238), Jan 23, 2008: FRAME. CORRODED. LWR FWD CARGO PIT FRAME, UPPER FLANGE HAS SURFACE CORROSION, AFT SIDE OF STA 720D ABOVE STR 26L. FRAME DAMAGE FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGE, FABRICA
- [SDR 08FDEA00236](https://openairdocs.org/sdr/08FDEA00236), Jan 23, 2008: FLOORBEAM. CORRODED. MAIN DECK FLOORBEAM UPPER "T" CAP CORRODED, BS 950D, RBL 9-23 THIS SDR WAS ENTERED IN ERROR AND WILL NOT BE USED. THIS IS A DUPLICATE OF SDR NR 08-0235. THIS SD
- [SDR 08FDEA00235](https://openairdocs.org/sdr/08FDEA00235), Jan 23, 2008: FLOORBEAM. CORRODED. MAIN DECK FLOORBEAM UPPER TEE CAP CORRODED, BS 950D, RBL 9-23. REMOVED CORROSION. OUT OF LIMITS IAW SM 53-10-8, SRM 51-10-6. DISPLACED SEAT TRACK BS 950-950F RB
- [SDR 08FDEA00234](https://openairdocs.org/sdr/08FDEA00234), Jan 23, 2008: FLOORBEAM. CORRODED. MAIN DECK FLOORBEAM UPPER TEE CAP CORRODED, BS 950D, LBL 10-13. REMOVED CORROSION. FOUND OUT OF LIMITS IAW PF SRM 53-10-1 FIG 4C. REPAIRED DAMAGED FLOORBEAM IAW
- [SDR 08FDEA00233](https://openairdocs.org/sdr/08FDEA00233), Jan 23, 2008: SEAT TRACK. CORRODED. SEAT TRACK CORRODED, STA 880-950, RBL 47 REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED SEAT TRACK. FABRICATED NEW SEAT TRACK, ALODINED AND PRIMED AND IN
- [SDR 08FDEA00221](https://openairdocs.org/sdr/08FDEA00221), Jan 22, 2008: INTERCOSTAL. CRACKED. LEFT LOWER FUSELAGE "B" SYSTEM HYD COMPARTMENT HYDRAULIC LINE SUPPORT INTERCOSTAL CRACKED 3 AREAS IN RADIUS, STA 950A PLUS 4, TO 950A PLUS 7 JUST O/B OF RESERVO
- [SDR 08FDEA00220](https://openairdocs.org/sdr/08FDEA00220), Jan 22, 2008: RIB. CRACKED. NR 2 FLAP TRACK MID FRG AFT RIB IS CRACKED REMOVED CRACKED RIB REF SRM 51-30-2 P1, PRIMED AND PAINT FLAP TRACK FRG, REF 51-10-2 PG 1-4. INSTALLED REPLACEMENT RI
- [SDR 08FDEA00219](https://openairdocs.org/sdr/08FDEA00219), Jan 22, 2008: FRAME. CORRODED. CORROSION AT SEVERAL AREAS ON AFT WALL GILL LINER PANEL UPPER FRAME AT STA 1166, AROUND CAM LOC RECEPTACLE HOLES FRONT AND BACK FABRICATED UPPER FRAME AT STA 11
- [SDR 08FDEA00218](https://openairdocs.org/sdr/08FDEA00218), Jan 22, 2008: STRINGER CLIP. TORN. CABIN BS 660, S 5L STRINGER CLIP TORN. REMOVED STRINGER CLIP, TRANSFERRED HOLD TO NEW CLIP. INSTALLED NEW STRINGER CLIP REF SRM 51-30-2. THIS IS CLASSIFIED AS A
- [SDR 08FDEA00217](https://openairdocs.org/sdr/08FDEA00217), Jan 22, 2008: FLOOR SUPPORT. CRACKED. AFT CARGO PIT CAP STRIP, 950D TO 990 LT, CRACKED AT FASTENER HOLE FABRICATED NEW CAP STRIP. REF BOEING DWG NR 65-67278/SRM 51-20-1 FIG 2/SRM 51-10-1, PG 12. TRE
- [SDR 08FDEA00216](https://openairdocs.org/sdr/08FDEA00216), Jan 22, 2008: INTERCOSTAL. CORRODED. MAIN CARGO DECK INTERCOSTAL CORRODED, BS 1030-1050, LBL 19 REMOVED CORROSION AND FOUND OUT OF LIMITS. MATERIAL THICKNESS IS .071". REMAINING MATERIAL IS .051", 
- [SDR 08FDEA00212](https://openairdocs.org/sdr/08FDEA00212), Jan 22, 2008: BRACKET. CRACKED. RT WING, NR 6 FLAP TRACK FAIRING, O/B SKATE ANGLE ATTACH BRACKET, CRACKED AT I/B AFT SIDE REMOVED RT WING NR 6, FLAP TRACK FAIRING O/B SKATE ANGLE ATTACH BRACKE
- [SDR 08FDEA00211](https://openairdocs.org/sdr/08FDEA00211), Jan 22, 2008: LINK. CORRODED. MAIN DECK 1L DR CUTOUT LWR HINGE RADIUS LINK IS CORRODED. INSTALLED NEW RADIUS LINK, REF MM 52-11-001-PG 2, OPS CHECKED GOOD THIS IS CLASSIFIED AS A MINOR REPAI

All 121: https://openairdocs.org/deregistered/N267FE-2012-10-12/reports.md

## Other aircraft with N267FE

- [Registered now](https://openairdocs.org/aircraft/N267FE): Boeing 767-300F, S/N 66866, built 2023

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