# N107FE: 1967 Boeing 727-22C, registration cancelled 2006-08-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 10, 2006
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 727-22C](https://openairdocs.org/model/boeing-727-22c) (registry code 138400F)
- Serial number: 19202
- Year built: 1967
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, transport
- Airworthiness date: June 30, 1967
- Certificate issued: October 2, 1978
- Last registry action: December 16, 2003
- Mode S code: A01F37
- 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: Co-owned
- 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/N107FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=107FE
- Page: https://openairdocs.org/deregistered/N107FE-2006-08-10

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 727-22C: https://openairdocs.org/model/boeing-727-22c.md

## Service difficulty reports (55, newest 50)

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

- [SDR 05FDEA02294](https://openairdocs.org/sdr/05FDEA02294), Aug 6, 2005: CHANNEL. CRACKED. RIGHT WING TRAILING EDGE AT AFT SPAR AREA 3 EA CLOSE OUT PANEL SUPPORTS ARE CRACKED LOCATED UNDER NR 12 & 13 SPOILER PANELS. REMOVED AND REPLACED 3 EACH CHANNEL
- [SDR 05FDEA00092](https://openairdocs.org/sdr/05FDEA00092), Jan 14, 2005: RIB. CRACKED. STABILIZER-ELEVATOR HINGE SUPPORT RIB INSPEC - S/B 727-55A0091 R1 COMPLY WITH EO 7-5510-7-5001. FOUND CRACK IN RIB AT ELEVATOR STA 50.50 DURING INSPECTION IAW E
- [SDR 04FDEA00216](https://openairdocs.org/sdr/04FDEA00216), Jan 24, 2004: STIFFENER. CORRODED. LEFT WHEEL WELL BULKHEAD STA 950 LOWER -TEE CHORD IS CORRODED. REMOVED AND REPLACED CHORD IAW SRM 51-30-2 ON N/R N00126 WO 24581 AT MAE.
- [SDR 04FDEA00214](https://openairdocs.org/sdr/04FDEA00214), Jan 23, 2004: SKIN. CORRODED. FUSELAGE SKIN BULGE AT STA 1163 STRINGER 18L & 19L. REMOVED CORROSION IAW SRM 51-10-6, FABRICATED & INSTALLED REPAIR DOUBLER IAW EA 7-5330-73867A.
- [SDR 04FDEA00202](https://openairdocs.org/sdr/04FDEA00202), Jan 22, 2004: INTERCOSTAL. DAMAGED. AFT PIT BS 1080 TO 1050 AT STR 26R INTERCOSTAL DAMAGED AND HOLES ELONGATED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-30-2. NEW INTERCOSTAL FABRICATED ON TRAV
- [SDR 04FDEA00184](https://openairdocs.org/sdr/04FDEA00184), Jan 16, 2004: SUPPORT ANGLE. CRACKED. LOWER NOSE COMPT DOOR CUTOUT SUPPORT ANGLE IS CRACKED AT FS 203 RBL 11. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-30-2 AT MAE ON N/R N00687.
- [SDR 04FDEA00183](https://openairdocs.org/sdr/04FDEA00183), Jan 16, 2004: WEB. CRACKED. UPPER DECK, CARGO DOOR UPPER BOX WEB FINGERS ARE CRACKED AT STA 490 AND 500 STR 2L. REMOVED DAMAGED WEB AND INSTALLED NEW WEB IAW SRM 51-30-2.
- [SDR 04FDEA00182](https://openairdocs.org/sdr/04FDEA00182), Jan 16, 2004: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK AT APPROX RBL 24 FS 1140 TO 1183 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2 AT MAE ON N/R N00448.
- [SDR 04FDEA00181](https://openairdocs.org/sdr/04FDEA00181), Jan 16, 2004: FLOOR SUPPORT. CRACKED. AFT LOWER PIT BS 970 TO 990 BETWEEN STR 29 AND LT KEEL BEAM CRACKED FLOOR SUPPORT AND CORRODED NUT PLATES. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 53-10-5 AT
- [SDR 03FDEA02208](https://openairdocs.org/sdr/03FDEA02208), Dec 16, 2003: COUPLER. FAILED. LOWER YAW DAMPER RUNAWAY - LT AND RT AFTER TAKEOFF - LYD SWITCH TURNED OFF. REMOVED AND REPLACED LOWER YAW DAMP COUPLER IAW 727-100 MM CH 22-11-131-4. OPS CHECK
- [SDR 03FDEA01408](https://openairdocs.org/sdr/03FDEA01408), Sep 3, 2003: SWITCH. FALSE INDICATION. NOSE GEAR DID NOT INDICATE SAFE AFTER PLACING LANDING GEAR HANDLE DOWN. CYCLED LANDING GEAR LEVER. NOSE GEAR INDICATED SAFE AFTER APPROX 10 - 15 SEC. RED UNSAFE
- [SDR 03FDEA00126](https://openairdocs.org/sdr/03FDEA00126), Feb 14, 2003: COALESCER BAG. CONTAMINATED. AFTER GEAR RETRACTION, CREW BECAME AWARE OF AN ACRID ODOR WHICH INTENSIFIED. INITIAL ODOR WAS OF BURNING RUBBER OR A SMOLDERING WIRE BUNDLE. CREW WENT ON OXYGEN
- [SDR 02FDEA00703](https://openairdocs.org/sdr/02FDEA00703), Oct 2, 2002: ACTUATOR. FAILED. DURING FLAP RETRACTION NR 2 SLAT ON RIGHT WING REMAINED EXTENDED WITH FLAP LEVER IN UP POSITION. QRH PROCEDURES WERE FOLLOWED AND FLAPS WERE CYCLED BACK TO 5 ON
- [SDR 02FDEA00513](https://openairdocs.org/sdr/02FDEA00513), Jul 23, 2002: OIL FILTER. DAMAGED. NR 1 ENGINE, HIGH OIL TEMP (OFF SCALE HIGH) FOUND BAD CONNECTION AT OIL TEMP SENSOR. PER CREW INFO WINDMILLING WAS LESS THAN 30 MIN. FOUND BROKEN WIRE AT C/P ON
- [SDR 01FDEA00503](https://openairdocs.org/sdr/01FDEA00503), Jun 26, 2001: SKIN. CORRODED. N 371 DUR ROUTINE INSP FUSELAGE SKIN FND CORRODED FROM BS 425-440 BETWEEN STR 3L AND 4L. R&R & FAB SKIN PER IAW BAC 727 SRM 53-30-3.
- [SDR 01FDEA00502](https://openairdocs.org/sdr/01FDEA00502), Jun 26, 2001: FITTING. CORRODED. N 773 DUR ROUTINE INSP, NLG DOOR UPR LINK FITTING BS 227.8 FND CORRODED. R&R FITTING IAW BAC 727 SRM 51-30-2.
- [SDR 01FDEA00453](https://openairdocs.org/sdr/01FDEA00453), Jun 18, 2001: SUPPORT. CRACKED. DURING ROUTINE INSP THE NR 1 SEAT TRACK SUPPORT AT BS 860 FOUND CRACKED. *S/D* REMOVED AND REPLACED SUPPORT PER IAW BAC 727 SRM 51-30-2.
- [SDR 01FDEA00414](https://openairdocs.org/sdr/01FDEA00414), Jun 11, 2001: PRESSURE PANEL. CRACKED. DURING ROUTINE INSP LT SIDE WEB IN NOSE WHEEL WELL WAS FOUND CRACKED AT BS 1260. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.
- [SDR 01FDEA00413](https://openairdocs.org/sdr/01FDEA00413), Jun 11, 2001: WEB. CRACKED. DURING ROUTINE INSP, LT SIDE WEB IN AIRSTAIR COMPT FOUND CRACKED AT LIGHTENING HOLE AT BS 1263. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-40-2, 51-
- [SDR 01FDEA00412](https://openairdocs.org/sdr/01FDEA00412), Jun 11, 2001: FITTING. CRACKED. DURING ROUTINE INSP, RT ELEVATOR TAB ROD FITTING FOUND CRACKED. *S/D* REMOVED AND REPLACED RIGHT ELEVATOR TAB PER IAW BAC 727 MM 27-30-011-2.
- [SDR 01FDEA00401](https://openairdocs.org/sdr/01FDEA00401), Jun 11, 2001: BEAM. CRACKED. DURING ROUTINE INSP BS 1183 BULKHEAD VERTICAL BEAM AT LBL 27 FOUND CRACKED AT WL 263. *S/D* REMOVED AND REPLACED PER VERTICAL BEAM PER IAW FEDEX EO 7-5310-7-234
- [SDR 01FDEA00411](https://openairdocs.org/sdr/01FDEA00411), Jun 11, 2001: WEB. CRACKED. DURING ROUTINE INSP, RT SIDE WEB IN AFT AIRSTAIR AREA FOUND CRACKED AT BS 1283. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 BAC 727 SRM 51-40-2, 51-30-2.
- [SDR 01FDEA00410](https://openairdocs.org/sdr/01FDEA00410), Jun 11, 2001: TIE CLIP. CRACKED. DURING ROUTINE INSP, STR TIE CLIP AT BS 312, STR 4R FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.
- [SDR 01FDEA00409](https://openairdocs.org/sdr/01FDEA00409), Jun 11, 2001: TIE CLIP. CRACKED. DURING ROUTINE INSP, STR TIE CLIP AT BS 328, STR 14R FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.
- [SDR 01FDEA00408](https://openairdocs.org/sdr/01FDEA00408), Jun 11, 2001: SKIN. CRACKED. DURING ROUTINE INSP, LT FWD EMERGENCY EXIT HATCH UPPER INNER SKIN FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 52-00-3, 51-30-2.
- [SDR 01FDEA00407](https://openairdocs.org/sdr/01FDEA00407), Jun 11, 2001: BULKHEAD. CRACKED. DURING ROUTINE INSP, HFEC IND TWO CRACKS IN BS 1183 BULKHEAD WEB AT WL 283. *S/D* REMOVED AND REPLACED WEB PER IAW FEDEX EO 7-5310-7-5000 PARTS 2 & 4.
- [SDR 01FDEA00406](https://openairdocs.org/sdr/01FDEA00406), Jun 11, 2001: BULKHEAD. CRACKED. DURING ROUTINE INSP, HFEC IND CRACK IN BS 1183 BULKHEAD WEB AT WL 283, RBL 17.8. *S/D* REMOVED AND REPLACED PER IAW FEDEX EO 7-5310-7-5000 PARTS 3 & 5.
- [SDR 01FDEA00405](https://openairdocs.org/sdr/01FDEA00405), Jun 11, 2001: FITTING. CRACKED. DURING ROUTINE INSP, HFEC IND CRACK IN FASTENER HOLES IN ROW 3, LT BS 870 FITTING AT STR 9L. *S/D* HFEC IND NO CRACKS PER IAW BAC 727 NDT MANUAL PART 6.
- [SDR 01FDEA00404](https://openairdocs.org/sdr/01FDEA00404), Jun 11, 2001: FLOORBEAM. CRACKED. DURING ROUTINE INSP FLT DECK FLOORBEAM WEB AT BS 299, LBL 6 FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB WEB PER IAW BAC 727 SRM 51-20-1, SRM 51-30-2.
- [SDR 01FDEA00403](https://openairdocs.org/sdr/01FDEA00403), Jun 11, 2001: RIB. CRACKED. DURING ROUTINE INSP LWR RUDDER, LWR THRUST HINGE RIB FOUND CRACKED AT FASTENER COMMON TO FIN REAR SPAR. *S/D* HFEC IND CRACK TERMINATED. REMOVED, REPLACED AND F
- [SDR 01FDEA00402](https://openairdocs.org/sdr/01FDEA00402), Jun 11, 2001: SUPPORT. CRACKED. DURING ROUTINE INSP THE NR 1 SEAT TRACK SUPT AT BS 840 FOUND CRACKED.
- [SDR 99FDEA00053](https://openairdocs.org/sdr/99FDEA00053), Feb 2, 1999: BATTERY. DISCHARGED. ENTRY DOOR EMERGENCY LIGHT BURNED OUT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ON FORWARD ENTRY DOOR. SYS OPER CK GOOD IAW FEDEX MM 33-50-0.
- [SDR 98FDEA00726](https://openairdocs.org/sdr/98FDEA00726), Dec 5, 1998: PUMP. FAILED. DURING CLIMBOUT, NR 2 LOW OIL PRESS/FILTER BYPASS LIGHT CAME ON. OIL PRESS DROPPED TO ZERO, TEMP WAS OK. SHUTDOWN ENG PER RED TABS WITHIN 4 TO 5 MIN. *S/D* REMO
- [SDR 96FDEA01550](https://openairdocs.org/sdr/96FDEA01550), Sep 26, 1996: HYD LINE. CRACKED. IN-FLIGHT AT FL 280, NR 1 ENGINE HYDRAULIC PUMP LIGHT STARTED BLINKING WITH FLUCTUATION IN PRESSURE. TWO SECONDS LATER, NR 2 ENGINE HYD PRESS LIGHT BLINKED, THE
- [SDR 96FDEA01432](https://openairdocs.org/sdr/96FDEA01432), Sep 3, 1996: TRACK. CORRODED. CORROSION ON O/B OF TRACK STA 840 RBL 48. INSTALLED DOUBLER PER EA 7531-0-28823 AND 51-10-1.
- [SDR 96FDEA01426](https://openairdocs.org/sdr/96FDEA01426), Aug 22, 1996: INTEGRAL RIB. CRACKED. LT 870 INTEGRAL RIB FWD CRACK FROM O/B HOLE TO EDGE. INSTALLED BATHTUB FITTING PER EA NR 7-5310-28832.
- [SDR 96FDEA01430](https://openairdocs.org/sdr/96FDEA01430), Aug 21, 1996: SKIN. CORRODED. UPPER SURFACE CENTER WING SECTION, CENTER WING SKIN HAS HEAVY CORROSION AT LT AFT CORNER SECTION UNDER PRESS. SEAL TRACK APPROX 6 INCH AREA, THREE PLACES FS 850
- [SDR 96FDEA01428](https://openairdocs.org/sdr/96FDEA01428), Aug 15, 1996: ANGLE. CORRODED. FLOOR BOARD SUPPORT ANGLE CORRODED AT STA 344 26 TO 45 LBL FLOOR BEAM. REMOVED CORROSION AND INSTALLED CAP STRIP REPAIR PER SRM 51-10-1.
- [SDR 96FDEA01431](https://openairdocs.org/sdr/96FDEA01431), Aug 14, 1996: ANGLE. CORRODED. CABIN INTERIOR, FS 1176 REINFORCEMENT CHORD ANGLE HAS HEAVY TO SEVERE CORROSION. FLOOR LEVEL BETWEEN BL 44 TO 46 LT. REMOVED DAMAGED PORTION OF CHORD ANGLE, INS
- [SDR 96FDEA01429](https://openairdocs.org/sdr/96FDEA01429), Aug 14, 1996: SEAT TRACK. CORRODED. CORROSION ON O/B OF TRACK STA 840 RBL 48. INSTALLED DOUBLER PER EA 7531028823.
- [SDR 96FDEA01427](https://openairdocs.org/sdr/96FDEA01427), Aug 14, 1996: SPLICE PLATE. CORRODED. CORROSION UNDER WING TO FUSE SPLICE PLATE LT SIDE AFT CORNER OF TANK BS 870 LBL 70.5. CUT OUT CORROSION, INSTALLED REPAIR PER EA 7-5710-28845.
- [SDR 96FDEA01361](https://openairdocs.org/sdr/96FDEA01361), Aug 13, 1996: DOUBLER. CRACKED. FOUND CRACK AT FWD ENTRY DOOR CUT OUT FRAME UPPER HINGE AREA. INSTALLED DOUBLER AS PER SRM 53-10-4 FIG 2.
- [SDR 96FDEA01360](https://openairdocs.org/sdr/96FDEA01360), Aug 13, 1996: FLANGE. CORROSION. NR0176, MAIN CARGO HAS CORR ON STR 5L STA 1148 TO 1166. REMOVED CORR SRM 51-10-6 OUT OF LIMITS, CUT REPAIR PARTS FOR INSIDE FLANGE REPAIR PER SRM 53-10-3.
- [SDR 96FDEA1359](https://openairdocs.org/sdr/96FDEA1359), Aug 12, 1996: DOUBLER. CRACKED. RT 870 INTERGRAL RIB FWD CRACKED FROM O/B HOLE TO EDGE. THE 2ND CRACK O/B OF O/B HOLE CRACKED FROM EDGE THROUGH RADIUS INTO AFT LWR HOLE OF O/B FLANGE. INSTALLE
- [SDR 96FDEA01353](https://openairdocs.org/sdr/96FDEA01353), Aug 12, 1996: FLOOR BEAM. CORROSION. MAIN CARGO CORROSION ON FLOOR BEAM AT STA 312 LBL 19. INSTALLED AND COMPLETED FLOOR BEAM REPAIR STA 312 LBL 19 PER SRM 53-10-8.
- [SDR 96FDEA01352](https://openairdocs.org/sdr/96FDEA01352), Aug 12, 1996: STRINGER. CORRODED. FORWARD CARGO BS 720 STR 23R HEAVY CORROSION INSIDE STRINGER ON LOWER LEG. REMOVED CORROSION AND INSTALLED STRINGER REPAIR PER SRM 53-10-3.
- [SDR 96FDEA01338](https://openairdocs.org/sdr/96FDEA01338), Aug 7, 1996: WINDOW POST. CRACKED. CRACK AT F/O'S NR 1 WINDOW O/B POST AT UPPER CORNER. CRACK LENGTH VERIFIED BY NDT HFEC, CRACK WAS STOP DRILLED AND VERIFIED BY NDT HFEC REPAIR DOUBLER INSTALLED
- [SDR 96FDEA01318](https://openairdocs.org/sdr/96FDEA01318), Aug 4, 1996: STRINGER. CORROSION. NR0440, FWD CARGO BS 720 STR 23R HEAVY CORROSION INSIDE STR ON LOWER LEG. *S/D* REMOVED CORROSION AND INSTALLED STRINGER REPAIR PER 53-10-3.
- [SDR 96FDEA01317](https://openairdocs.org/sdr/96FDEA01317), Aug 2, 1996: FLOOR BEAM. CORROSION. NR0436, FWD CARGO BS 600 BL 0 TO RBL 24 HEAVY CORROSION ON LOWER SIDE OF LOWER LEG OF MAIN CARGO FLOOR BEAM. *S/D* INSTALLED FLOOR BEAM REPAIR PER SRM 53-10-8.
- [SDR 96FDEA01314](https://openairdocs.org/sdr/96FDEA01314), Aug 2, 1996: FITTING. CRACKED. STR END FITTING CRACKED STA 740 STR 5R. REMOVED AND REPLACED STR END FITTING PER 51-10-01.

All 55: https://openairdocs.org/deregistered/N107FE-2006-08-10/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB NYC93IA065](https://openairdocs.org/ntsb/NYC93IA065), Mar 23, 1993: Boeing 727-100 (N107FE), Newark, NJ, incident, no damage. Probable cause: THE PILOT'S MISUNDERSTANDING OF LANDING RUNWAY, AND THE FAILURE OF THE LOCAL CONTROLLER TO ADEQUATELY MONITOR THE PROGRESS OF THE FLIGHT. FACTORS WHICH CONTRIBUTED TO THE INCIDENT WERE: THE FAILURE…

## FAA accident and incident reports (5)

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 20030214005729I](https://openairdocs.org/incident/20030214005729I), Feb 14, 2003: Boeing 72722C (N107FE), Indianapolis, IN. (-23) After gear retraction crew became aware of an acrid odor which intensified. Smelled like burning rubber of smoldering wire bundle. The crew went on…
- [Incident 19981205042239I](https://openairdocs.org/incident/19981205042239I), Dec 5, 1998: Boeing 72722C (N107FE), Rochester, MN. (-5) During climb #2 eng. Low oil/filter bypass light came on, #2 eng. Oil pressure dropped to zero, temp. Was within limits. The eng. Operated in this…
- [Incident 19850814044059I](https://openairdocs.org/incident/19850814044059I), Aug 14, 1985: Boeing 72722C (N107FE), Peoria, IL. Aircrafts left main gear went off side of runway during rollout. Struck runway lights.
- [Incident 19811102082879I](https://openairdocs.org/incident/19811102082879I), Nov 2, 1981: Boeing 72722C (N107FE), Houston, TX, Minor damage. During climbout a bird struck an engine. Oil pressure dropped. Pilot returned to Houston.
- [Incident 19811031082019I](https://openairdocs.org/incident/19811031082019I), Oct 31, 1981: Boeing 72722C (N107FE), Houston, TX, Minor damage. Number 3 engine stalled and overtemped on takeoff and was shutdown. Aircraft returned. Turbine had failed.

## Other aircraft with N107FE

- [Registered now](https://openairdocs.org/aircraft/N107FE): Boeing 767-3S2F, S/N 44377, built 2014

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