# N168FE: 1966 Boeing 727-22, registration cancelled 2007-06-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 28, 2007 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 727-22](https://openairdocs.org/model/boeing-727-22) (registry code 1384002) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Serial number: 18865 - Year built: 1966 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: February 10, 1989 - Certificate issued: January 3, 1989 - Last registry action: May 15, 2007 - Mode S code: A10FE8 - 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/N168FE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=168FE - Page: https://openairdocs.org/deregistered/N168FE-2007-06-28 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 727-22: https://openairdocs.org/model/boeing-727-22.md ## Service difficulty reports (26) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 04FDEA03385](https://openairdocs.org/sdr/04FDEA03385), Dec 7, 2004: SWITCH. MALFUNCTIONED. AT FL280, LE AMBER LIGHT ILLUMINATED (WING ANTI-ICE ON). NO ROLL OR DIRECTIONAL CENTRAL PROBLEM NOTED. NR 2 FLAP ON FE PNL L AMBER. SLOWED DOWN TO 230 KTS, CLOS - [SDR 03FDEA02042](https://openairdocs.org/sdr/03FDEA02042), Dec 4, 2003: BELLCRANK. DAMAGED. COMPLY WITH EA 7-5230-73854A DOOR MAIN CARGO DOOR TORQUE TUBE ELONGATED HOLES REPAIR BS 489 THROUGH BS 610. COMPLIED WITH EA 7-5230-73854A DOOR-MAIN CARGO DOOR - [SDR 03FDEA01639](https://openairdocs.org/sdr/03FDEA01639), Sep 26, 2003: DUCT. LOOSE. ON CLIMBOUT NR 3 GENERATOR BREAKER TRIPPED. OBSERVED GENERATOR DRIVE OIL TEMP PEGGED ON THE HIGH SIDE. COMPLIED WITH CSD HIGH OIL TEMP PROCEDURE AND CSD FAILED - [SDR 01FDEA00262](https://openairdocs.org/sdr/01FDEA00262), Apr 7, 2001: SUPPORT. CRACKED. DURING ROUTINE INSP, FLOORBEAM SUPPORT STRAP AT BS 304, STR 18R, RBL 35 FOUND CRACKED. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2. - [SDR 01FDEA00261](https://openairdocs.org/sdr/01FDEA00261), Apr 7, 2001: SEAT TRACK. CORRODED. DURING ROUTINE INSP, FWD LWR CARGO BIN LT SEAT TRACK FOUND CORRODED AT BS 680. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-5. - [SDR 01FDEA00260](https://openairdocs.org/sdr/01FDEA00260), Apr 7, 2001: FLOORBEAM. CORRODED. DURING ROUTINE INSP, BS 660 FLOORBEAM FOUND CORRODED AT NR 5 SEAT TRACK. CUT OUT DAMAGED AREA. FAB AND INSTALL REPAIR PER IAW BAC 727 SRM 53-10-8. - [SDR 01FDEA00259](https://openairdocs.org/sdr/01FDEA00259), Apr 7, 2001: FLOORBEAM. CORRODED. DURING ROUTINE INSP, BS 640 FLOORBEAM FOUND CORRODED AT 5 SEAT TRACK. CUT OUT DAMAGED AREA. FAB AND INSTALL REPAIR PER IAW BAC 727 SRM 53-10-8. - [SDR 01FDEA00227](https://openairdocs.org/sdr/01FDEA00227), Mar 24, 2001: SKIN. CORRODED. N 164 DUR ROUTINE INSP, FUSELAGE SKIN FND CORRODED AT BS 400, STR 3R AND 4R. ** S/D ** STRIPPED AREA. LFEC IND NO CORROSION LOSS PER LOSS IAW 727 NDT MANUAL PAR - [SDR 01FDEA00229](https://openairdocs.org/sdr/01FDEA00229), Mar 24, 2001: SUPPORT FITTING. CRACKED. N 650 DUR ROUTINE INSP, UPR AND LWR LUGS OF THE UPR RUDDER ROD SUPPORT FITTING LOCATED ON THE VERTICAL STABILIZER REAR SPAR FND CRACKED. ** S/D ** HFEC IND NO C - [SDR 01FDEA00228](https://openairdocs.org/sdr/01FDEA00228), Mar 24, 2001: RIB. CRACKED. DURING ROUTINE INSP HFEC IND THE LWR RUDDER, THRUST HINGE RIB FITTING WAS CRACKED AT FWD RIGHT SIDE. *S/D* REMOVED AND REPLACED RUDDER THRUST HINGE RIB PER IAW - [SDR 01FDEA00230](https://openairdocs.org/sdr/01FDEA00230), Mar 24, 2001: INTERCOSTAL. CRACKED. DURING ROUTINE INSP, INTERCOSTAL AT BS 738 AT THE NR 5 SEAT TRACK FOUND CRACKED. *S/D* STOP DRILLED INTERCOSTAL. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 5 - [SDR 00FDEA00896](https://openairdocs.org/sdr/00FDEA00896), Dec 21, 2000: DOWNLOCK SWITCH. FAULTY. ON APRROACH IN INDIANA, NO GREEN LIGHT ON NOSE GEAR INDICATOR. RECYCLED GEAR NOSE GEAR IND SHOW GREEN AFT A DELAY. ** S/D ** CLEAN & TREAT DOWN & LOCK POSITION - [SDR 00FDEA00320](https://openairdocs.org/sdr/00FDEA00320), May 5, 2000: WARNING LIGHT. ILLUMINATED. AFT T/O WITH FLAPS FULLY RETRACTED, NR 2 LEADING EDGE FLAP AND LEADING EDGE (AMBER) LIGHT ILLUM ON FWD PANEL. - [SDR 98FDEA00650](https://openairdocs.org/sdr/98FDEA00650), Oct 13, 1998: DOUBLER. CORRODED. WHILE WORKING NR0186, FOUND INTERNAL DOUBLER AT BS 961 TO 990, STR 28 TO 29 RT TO BE CORRODED AND OUT OF LIMITS PER SRM. - [SDR 98FDEA00649](https://openairdocs.org/sdr/98FDEA00649), Oct 13, 1998: CHORD. CORRODED. WHILE WORKING NR 0213 FOUND CORROSION ON FAIL-SAFE CHORD, BS 380 BETWEEN STR 25 TO 26 RT. *S/D* REPAIRED FAIL-SAFE CHORD BS 380 BETWEEN STR 25-26 RT IAW FEDEX S - [SDR 98FDEA00644](https://openairdocs.org/sdr/98FDEA00644), Oct 8, 1998: STRINGER. CORRODED. UPON REMOVAL OF LT KEEL BEAM ON NR 0190, FOUND CORROSION IN STR AT BS 1080, LBL 8, WL 138, STR 29L. *S/D* REPAIRED STR 29L, BS 1082-1098, LBL 8, WL 138 PER FED- - [SDR 98FDEA00640](https://openairdocs.org/sdr/98FDEA00640), Oct 7, 1998: BEAM. CORRODED. WHILE WORKING NR 424, FOUND CORROSION ON 25 G-BEAM AT BS 264, WL 208, RBL 8 TO BE OUT OF LIMITS. *S/D* REMOVED AND REPLACED 25 G-BEAM, BS 264, WL 208, LBL 18 TO - [SDR 98FDEA00619](https://openairdocs.org/sdr/98FDEA00619), Oct 5, 1998: STRINGER. CORRODED. NR 0211 CORROSION (C53-224-03-1/2) TOP OF STR 26 FROM BS 381-400, LBL 29, WL 156 IN FWD E/E BAY. REMOVED AND REPLACED STR 26L FROM BS 384-413, LBL 29, WL 156 PE - [SDR 98FDEA00618](https://openairdocs.org/sdr/98FDEA00618), Oct 5, 1998: STRINGER. CORRODED. CORROSION (C53-224-03-1/2) ON UPPER SURFACE OF STR 26R, BS 380, RBL 16, WL 152. *S/D* REMOVED AND REPLACED CORRODED STR BS 360-385, STR 26R, WL 152 PER FED-EX S - [SDR 98FDEA00597](https://openairdocs.org/sdr/98FDEA00597), Sep 28, 1998: KEEL BEAM. CORRODED. CORROSION ON RT KEEL BEAM AT BS 1040, WL 138, AFT CARGO BAY. *S/D* REMOVED AND REPLACED RT KEEL BEAM AT BS 1040 TO BS 961 WL 138 PER FEDEX EA 7-5330-42225. - [SDR 98FDEA00596](https://openairdocs.org/sdr/98FDEA00596), Sep 28, 1998: BEAM. CORRODED. CORROSION UNDER NUT PLATE ON FLANGE OF LONGITUDINAL BEAM BS 798, LBL 25, WL 208. *S/D* REMOVED AND REPLACED LONGITUDINAL BS 798, LBL 25, WL 208 PER FED-EX SRM 5 - [SDR 98FDEA00595](https://openairdocs.org/sdr/98FDEA00595), Sep 28, 1998: KEEL BEAM. CORRODED. CORROSION ON LT KEEL BEAM AT BS 1030, WL 138, LBL 12 IN THE AFT CARGO BAY. *S/D* REMOVED AND REPLACED LT KEEL BEAM AT BS 961-1087, WL 138, LBL 8 PER FEDEX. - [SDR 96FDEA01694](https://openairdocs.org/sdr/96FDEA01694), Nov 27, 1996: SWITCH SPACER. MISSING. NR 2 LEADING EDGE FLAP FAILED TO RETRACT AFTER TAKEOFF. FOLLOWED CHECKLIST WITH NO RESULTS, RETURNED TO PORTLAND. REMOVED AND REPLACED NR 2 FLAP SWITCH, FOUND S - [SDR 96FDEA01179](https://openairdocs.org/sdr/96FDEA01179), Jun 25, 1996: GUSSET. CRACKED. CABIN INTERIOR - FS 783.5 RIB SUPPORT GUSSET BELOW FLOOR LEVEL, IS CRACKED AT LOWER INBOARD CORNER, JUST ABOVE WING SKIN, CRACK APPROX 1 INCH. CRACKED GUSSET RE - [SDR 96FDEA01181](https://openairdocs.org/sdr/96FDEA01181), Jun 24, 1996: BELL FRAME. CRACK. FORWARD CARGO CRACK IN BELL FRAME, STA 680 BETWEEN STR 26-27L. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-40-4, PG 12-17. - [SDR 96FDEA01180](https://openairdocs.org/sdr/96FDEA01180), Jun 24, 1996: FLOOR BEAM. CORROSION. MAIN CARGO CORROSION ON FLOOR BEAM AT SCREW HOLES FROM LBL 45 - 54, STA 344. REMOVED CORROSION PER SRM 53-10-1. INSTALLED FLOOR BEAM REPAIR PER SRM 53-10-8 AND ## Other aircraft with N168FE - [Registered now](https://openairdocs.org/aircraft/N168FE): Boeing 767-300F, S/N 63100, built 2018 --- 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.