# N102FE: 1967 Boeing 727-22C, registration cancelled 2004-08-26

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 26, 2004
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 727-22C](https://openairdocs.org/model/boeing-727-22c) (registry code 138400F)
- Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044)
- Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 19193
- Year built: 1967
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: April 17, 1967
- Certificate issued: March 30, 1978
- Last registry action: September 16, 2003
- Mode S code: A00CA4
- 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/N102FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=102FE
- Page: https://openairdocs.org/deregistered/N102FE-2004-08-26

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

## Service difficulty reports (37)

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

- [SDR 00FDEA00480](https://openairdocs.org/sdr/00FDEA00480), Jul 20, 2000: JACKSCREW. DAMAGED. ON T/O AND DURING FLAP RETRACTION I/B FLAPS STUCK JUST PRIOR TO FLAPS 2 ON GAUGE CAUSING SPLIT TRAILING EDGE FLAP MALFUNCTION. RED TABS PROC COMPLIED WITH. FOUN
- [SDR 00FDEA00325](https://openairdocs.org/sdr/00FDEA00325), May 9, 2000: ACTUATOR. INOPERATIVE. AT CR ''A'' SYSTEM HYD QTY WENT TO ZERO, GEAR UP AND FLAPS UP. SHUT OFF ENGINE PUMPS (1 & 2) AND FLUID SHUT OFF (1 & 2) CRANKED GEAR DOWN. *S/D* REMOVED AND REP
- [SDR 00FDEA00245](https://openairdocs.org/sdr/00FDEA00245), Apr 14, 2000: SMOKE. DETECTED. CREW REPORTS SMOKE/FUMES IN COCKPIT, EMERGENCY DECLARED. *S/D* REMOVED AND REPLACED NR 1 & 2, 02 BOTTLES PER IAW MM 35-10.
- [SDR 98FDEA00223](https://openairdocs.org/sdr/98FDEA00223), Mar 31, 1998: OUTFLOW VALVE. FAILED. AIRCRAFT WILL NOT PRESSURIZE IN NORMAL OR AUTOMATIC. NO AUTHORITY WITH MANUAL WITH FULL INCREASE PRESSURE. CABIN VERTICAL SPEED INDICATOR FULL CLIMB THROUGHOUT.
- [SDR 98FDEA00033](https://openairdocs.org/sdr/98FDEA00033), Jan 14, 1998: CONNECTOR. DIRTY. THE RIGHT GEAR DOOR REMAINED OPEN AFTER GEAR HANDLE WAS PLACED UP. AFTER 2 MIN THE GEAR WAS RECYCLED PER RED TABS. THE RIGHT GEAR DOOR CONSISTENTLY IS SLOW TO C
- [SDR 97FDEA00100](https://openairdocs.org/sdr/97FDEA00100), Feb 11, 1997: DOUBLER. CORRODED. NR 0578 031, CORROSION (C53-221-01) ON COCKPIT FLOOR AND ON ATTACHED ANGLE AT BS 225, RBL 20 TO 26. *S/D* REMOVED CORROSION ON COCKPIT FLOOR AND ATTACHED ANGLE 
- [SDR 97FDEA00099](https://openairdocs.org/sdr/97FDEA00099), Feb 11, 1997: FRAME. CORRODED. NR 0633 030, CORROSION (53-221-01) AT FRAME STA 227 AFT O/B ANGLE, WL 235 RT. *S/D* REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED
- [SDR 97FDEA00095](https://openairdocs.org/sdr/97FDEA00095), Feb 7, 1997: CEILING SUPPORT. CORRODED. NR 0357 028. CORROSION (C53-111-01) ON CENTER CEILING SUPPORT FROM BS 660 TO BS 500, WL 200 BL ZERO. REMOVED CORROSION FROM CEILING SUPPORT STABILIZER BS 500 TO
- [SDR 97FDEA00082](https://openairdocs.org/sdr/97FDEA00082), Feb 1, 1997: FLOORBEAM. CORRODED. NR 0283 027. CORROSION C53-224-01(1) ON FLOORBEAM UPPER FLANGE BOTTOM FWD SIDE AT BS 360, LBL 56, WL 207.8. REPAIRED FLOORBEAM AT BS 360, LBL 56, WL 208. CORROS
- [SDR 97FDEA00074](https://openairdocs.org/sdr/97FDEA00074), Jan 27, 1997: SHEAR TIE. CRACKED. NR 0707 021. WHILE WORKING NR 0083, FOUND CRACKED SHEAR TIE AT BS 278, STR 26 LT. CRACKED SHEAR TIE AT BS 278. STRINGER 26 LT FABRICATED NEW SHEAR TIE AND INSTA
- [SDR 97FDEA00073](https://openairdocs.org/sdr/97FDEA00073), Jan 27, 1997: CLIP. CORRODED. NR 0703 022. WHILE WORKING NR 00831 FOUND STRINGER CLIP AT BS 295 STR 26 TO BE CORRODED BEYOND LIMITS. REMOVED AND FABRICATED STRINGER CLIP I.A.W. FED-EX SRM 72
- [SDR 97FDEA00089](https://openairdocs.org/sdr/97FDEA00089), Jan 25, 1997: STRINGER. CORRODED. NR 0122 025 CORROSION (C53-224-01,3) ON STRINGER 4 RT AT BS 978 TO 1040 AND BS 1090 TO 1110. *S/D* REMOVED AND REPLACED STRINGER 4 RT FROM BS 950 TO 1120 IAW FE
- [SDR 97FDEA00069](https://openairdocs.org/sdr/97FDEA00069), Jan 23, 1997: STRINGER. CORRODED. NR 0705 019. WHILE WORKING NR 0083 FOUND STR 25 LT TO BE CORRODED BEYOND LIMITS BS 310. REMOVED CORRODED STRINGER FROM BS 295 TO BS 360 STR 25 LT AND INSTALLED 
- [SDR 97FDEA00068](https://openairdocs.org/sdr/97FDEA00068), Jan 23, 1997: SKIN. CORRODED. NR 0706 017. WHILE WORKING NR 00083, FOUND SKIN AT BS 225-360 STR 25 LT-28 LT TO BE CORRODED BEYOND LIMITS. REMOVED CORRODED SKIN FROM BS 225-360, STR 25 LT AND
- [SDR 97FDEA00067](https://openairdocs.org/sdr/97FDEA00067), Jan 23, 1997: ANGLE. CORRODED. NR 0704 018 WHILE WORKING NR 0083 FOUND LOWER FLANGE OF LT LOWER NOSE ANGLE TO BE CORRODED AROUND NUTPLATE HOLES BS 330 TO 350. *S/D* LT LOWER NOSE ANGLE AND TE
- [SDR 97FDEA00077](https://openairdocs.org/sdr/97FDEA00077), Jan 22, 1997: STRINGER. CRACKED. NR 0701 023 NR 6 RT STRINGER CRACKED AT BS 400. *S/D* CUT OUT DAMAGED NR 6 STRINGER FROM BS 390 TO BS 410, FABRICATED AND INSTALLED REPAIR PARTS PER FED-EX SRM 
- [SDR 97FDEA00063](https://openairdocs.org/sdr/97FDEA00063), Jan 22, 1997: FRAME. DENTED. NR 0508 013 DAMAGED FRAME AT BS 990 BETWEEN STR 526-R AND 527-R. *S/D* REMOVED DAMAGED AREA OF 1 BY 1.75. FABRICATED REPAIR DOUBLER IAW 727 FED-EX SRM 51-40-3. 
- [SDR 97FDEA00062](https://openairdocs.org/sdr/97FDEA00062), Jan 22, 1997: FRAME. DENTED. NR 0509 014 DAMAGED FRAME AT BS 1010 BETWEEN STR 27 AND 26 RT. *S/D* REMOVED DAMAGED, FABRICATED REPAIR PARTS AND INSTALLED IAW FED-EX SRM 51-40-3 AT BS 1010 BE
- [SDR 97FDEA00060](https://openairdocs.org/sdr/97FDEA00060), Jan 22, 1997: STRINGER. CORRODED. NR 0125 16 CORROSION (C53-224-01,3) ON STRINGER 4 LT BS 990 TO 1030 AND BS 1080 TO 1110. *S/D* FOUND CORROSION ON STRINGER 4 LT TO BE OUT OF LIMITS AT BS 1050 T
- [SDR 97FDEA00079](https://openairdocs.org/sdr/97FDEA00079), Jan 21, 1997: STRINGER. CRACKED. NR 0700 024 NR 5 RT STRINGER CRACKED AT BS 400. *S/D* CUT OUT DAMAGED NR 5 STRINGER FROM BS 390 TO BS 410, FABRICATED AND INSTALLED REPAIR PARTS PER FED-EX SRM 
- [SDR 97FDEA00061](https://openairdocs.org/sdr/97FDEA00061), Jan 21, 1997: SKIN. CORRODED. NR 0345 015. CORROSION (C53-224-01) ON INTERNAL SKIN AT BS 560-580, STR 1-9 RT, BS 540-560 BETWEEN STR 3 LT AND 4 RT, BS 500-520 BETWEEN STR 3 LT AND 2 LT BS, 4
- [SDR 97FDEA00053](https://openairdocs.org/sdr/97FDEA00053), Jan 20, 1997: SKIN. DAMAGE. NR 0237 007. SKIN CREASED AT ST 188, WL 181 RT, BS 180 TO 185, WL 179 AND BS 198, WL 182 RT. REMOVED DAMAGED SKIN AND FABRICATED REPAIR PARTS. INSTALLED FILLERS
- [SDR 97FDEA00056](https://openairdocs.org/sdr/97FDEA00056), Jan 18, 1997: CHORD. CORRODED. NR 0687 010. WHILE WORKING CUSTOMER CARD NR 0083 FOUND CORROSION ON CHORD BS 219, LBL 26, WL 173. REMOVED OLD CHORD, FABRICATED NEW CHORD PARTS, ALODINED, PRIME
- [SDR 97FDEA00054](https://openairdocs.org/sdr/97FDEA00054), Jan 17, 1997: FLOORBEAM. CORRODED. NR 0516 009. CORROSION (53-111-01) UNDER NUTPLATE AT BS 1050, LBL 19, WL 200. ACCOMPLISHED REPAIR TO FLOORBEAM AT BS 1050, LBL 19 AND RBL 30, WL 200 PER FED-EX 
- [SDR 97FDEA00044](https://openairdocs.org/sdr/97FDEA00044), Jan 12, 1997: SKIN. CORRODED. NR 0615 006. CORROSION (C53-221-01) AT STA 245 UNDER CAPTAIN'S NR 3 WINDOW, WL 227. REMOVED CORROSION 3 INCH BY 4 INCH BY .049 INCH FROM ORIGINAL THICKNESS OF .
- [SDR 97FDEA00041](https://openairdocs.org/sdr/97FDEA00041), Jan 12, 1997: FLOORBEAM. CORROSION. NR 0515 005 CORROSION (C53-111-01) UNDER NUTPLATE AT BS 1148, RBL 1, WL 200. *S/D* CORROSION WAS FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM AT BS 1148, WL 20
- [SDR 97FDEA00040](https://openairdocs.org/sdr/97FDEA00040), Jan 10, 1997: FLOORBEAM. CORROSION. NR 0284 004 CORROSION (C53-224-01,1) ON FLOORBEAM AROUND NUTPLATE HOLES BS 380 LBL 45 TO 55, WL 207.5. *S/D* REPAIRED FLOORBEAM BS 380, LBL 31 TO LBL 70, WL 208
- [SDR 97FDEA00098](https://openairdocs.org/sdr/97FDEA00098), Jan 9, 1997: FLOORBEAM. CORRODED. NR 0288 029, CORROSION (C53-224-01,1) ON FLOORBEAM BS 640, LBL 12, WL 208 AND BLI AROUND FLOORBOARD FASTENER HOLES. *S/D* REPAIRED BEAM AT BS 640, LBL 60 TO RBL
- [SDR 97FDEA00031](https://openairdocs.org/sdr/97FDEA00031), Jan 9, 1997: SKIN. CORROSION. NR 083 003 CORROSION (C53-100-01) AT LAP LT STA 211 TO STA 259.5 STRINGER 25. *S/D* REMOVED CORROSION FROM SKIN AT LAP STA 211 TO STA 259.5, STR 19 TO 24 LT AND
- [SDR 97FDEA00083](https://openairdocs.org/sdr/97FDEA00083), Jan 8, 1997: ANGLE. DOUBLE HOLES. NR 0637 026. WHILE WORKING 7-5300-7-230YM1 PT 3, FOUND EXISTING DOUBLE HOLE IN L-ANGLE BS 925-950, LBL 63, WL 200. REMOVED L- ANGLE. FABRICATED NEW ANGLE, DRILL
- [SDR 97FDEA00058](https://openairdocs.org/sdr/97FDEA00058), Jan 8, 1997: FRAME. CRACKED. NR 0609 012 FWD LT OVERWING EXIT LOWER WENCE FRAME, HAS A CRACK BETWEEN FASTENER HOLES AT O/B EDGE OF FRAME THAT ATTACHES TO OUTER SKIN. *S/D* REMOVED AND REPLA
- [SDR 97FDEA00057](https://openairdocs.org/sdr/97FDEA00057), Jan 8, 1997: BULKHEAD ANGLE. CRACKED. NR 0618 011 CORROSION BS 178 BULKHEAD L-ANGLE LBL 28, WL 208 TO WL 224. *S/D* REMOVED CORROSION AND FOUND CHORD L-ANGLE TO BE CRACKED. REMOVED CHORD AND REPLACE
- [SDR 97FDEA00030](https://openairdocs.org/sdr/97FDEA00030), Jan 8, 1997: STRINGER. CORROSION. NR 0595 002 CORROSION (C53-224-01) ON STRINGER 4 RT BS 460 TO 360. *S/D* REMOVED DAMAGED STR 4 RT, BS 410 TO 450. FABRICATED NEW PARTS AND INSTALLED PER FED-EX 
- [SDR 97FDEA00070](https://openairdocs.org/sdr/97FDEA00070), Jan 7, 1997: STRINGER. CORRODED. NR 0353 020. CORROSION (C53-224-01) ON STRINGER 2 RT BS 560-BS 520. REMOVED CORRODED STRINGER 2 RT FROM BS 510-570 AND FABRICATED AND INSTALLED REPAIR PARTS ON 
- [SDR 97FDEA00055](https://openairdocs.org/sdr/97FDEA00055), Jan 6, 1997: SKIN. CORRODED. NR 0356 008. CORROSION (C53-224-05) ON UPPER SURFACE OF CENTER WING TANK AT BS 757, RBL 65, WL 204. REMOVED CORROSION AND REPAIRED I.A.W. FED-EX E.A. NR 7-5710-
- [SDR 97FDEA00027](https://openairdocs.org/sdr/97FDEA00027), Jan 6, 1997: FRAME. CORRODED. NR 0367 001 CORROSION (C53-111-01, 2) ON TOP OF FRAME AT BS 680, WL 156, LBL 20.5. *S/D* CORROSION FOUND TO BE OUT OF LIMITS. REMOVED CORRODED MATERIAL AND REPA
- [SDR 95FDEA01135](https://openairdocs.org/sdr/95FDEA01135), Aug 17, 1995: ADI. FAILED. CAPTAIN'S ADI FAILED DURING CLIMB OUT IN NORMAL POSITION, AND ALSO FAILED IN AUXILIARY POSITION. REPLACED CAPTAIN'S ADI. OPS CK NORMAL ON GROUND.

## Other aircraft with N102FE

- [Registered now](https://openairdocs.org/aircraft/N102FE): Boeing 767-3S2F, S/N 42707, built 2013

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