# N151FE: 1967 Boeing 727-22, registration cancelled 2007-07-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 16, 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-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044)
- Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 19147
- Year built: 1967
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: October 12, 1967
- Certificate issued: September 11, 1987
- Last registry action: September 19, 2006
- Mode S code: A0CE68
- 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/N151FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=151FE
- Page: https://openairdocs.org/deregistered/N151FE-2007-07-16

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

## Service difficulty reports (46)

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

- [SDR 06FDEA04137](https://openairdocs.org/sdr/06FDEA04137), Nov 29, 2006: SHUTOFF VALVE. FAILED. LOST PRESSURIZATION AT FL 260. COMPLIED WITH QRH, A/C DID NOT PRESSURIZE AUTO OR MANUAL. TROUBLESHOT TO LT PAC S/O VALVE INOP. PWR TO VALVE. REMOVED AND REPLACE
- [SDR 05FDEA01746](https://openairdocs.org/sdr/05FDEA01746), Jun 29, 2005: INDICATOR. FALSE INDICATION. NR 3 FUEL GAGE ERRONEOUS INDICATION, AT T/O SHOWED 11.1, SHORTLY INTO FLIGHT GAGE DROPPED 5K LBS. AT CRUISE FLT BOOST PUMPS ILLUMINATED. UPON LANDING AT KFSD, N
- [SDR 05FDEA00081](https://openairdocs.org/sdr/05FDEA00081), Jan 12, 2005: ACTUATOR. LEAKING. UPON GEAR RETRACT AFTER T/O RED RT GEAR LIGHT ILLUMINATED & AMBER RT MLG DOOR LIGHT ON S/O PANEL ILLUMINATED. MOVED GEAR HANDLE TO DOWN POS. 3 GREEN DOWN/LOCKED
- [SDR 05FDEA00020](https://openairdocs.org/sdr/05FDEA00020), Jan 4, 2005: SPLICE. CRACKED. STRINGER 4R SPLICE IS CRACKED ON EACH SIDE OF FRAME AT STA 480. REMOVED AND REPLACED STRINGER 4R SPLICE AT STA 480 IAW SRM 51-10-1.
- [SDR 05FDEA00019](https://openairdocs.org/sdr/05FDEA00019), Jan 4, 2005: RIB. CRACKED. SECOND INBOARD RIB IS CRACKED IN LEADING EDGE OF NR 5 SLAT. REMOVED AND REPLACED RIB IAW SRM 51-10-1.
- [SDR 04FDEA03505](https://openairdocs.org/sdr/04FDEA03505), Dec 29, 2004: RIB. CRACKED. RIGHT HORIZONTAL STAB ELEVATOR STATION 17.20, INBOARD RIB CRACK RUNS FROM RIVET ON UPPER. REMOVED RIB IAW SRM 51-30-2 & SB 727-55A0091. INSTALLED NEW RIB WITH P
- [SDR 04FDEA03437](https://openairdocs.org/sdr/04FDEA03437), Dec 17, 2004: FRAME. CORRODED. FLT CREW COMPARTMENT LEFT SIDE AT FS 227.8 FRAME HAS 2 EACH AREAS OF CORROSION ABOVE AND BELOW OXYGEN PANEL. REMOVED DAMAGE AREA IAW SRM 51-40-2, MADE NEW WEB F
- [SDR 04FDEA03433](https://openairdocs.org/sdr/04FDEA03433), Dec 17, 2004: WEB. CHAFED. LT WING NR 3 L/E FLAP INBD ANTI-ICE DUCT CHAFING FLAP. REMOVED & REPLACED WEB IAW SRM 51-30-2, NEW WEB FABBED FROM 2024-T3 .050, BATCH 814135, FOUND INNER SKIN 
- [SDR 04FDEA03432](https://openairdocs.org/sdr/04FDEA03432), Dec 17, 2004: WEB. CHAFED. LT WING NR 3 L/E FLAP INBD ANTI-ICE DUCT CHAFING FLAP. REMOVED & REPLACED WEB IAW SRM 51-30-2, NEW WEB FABBED FROM 2024-T3 .050, BATCH 814135, FOUND INNER SKIN 
- [SDR 04FDEA03204](https://openairdocs.org/sdr/04FDEA03204), Nov 24, 2004: WARNING SYSTEM. ACTIVATED. RECEIVED GND PROX WARNING ON TAKEOFF. PERFORMED ESCAPE MANEUVER USING FIREWALL POWER. FUEL WAS DUMPED TO MAX LDG WT. NO EMERGENCY WAS DECLARED. OTHER FLIGHT INF
- [SDR 04FDEA00166](https://openairdocs.org/sdr/04FDEA00166), Jan 15, 2004: CONNECTOR. CONTAMINATED. ON APPROACH, UPON LOWERING LANDING GEAR, NOSE GEAR INDICATED UNSAFE (RED GEAR LIGHT ON, GREEN LIGHT OUT). RAN EMERGENCY PROCEDURES, CYCLED GEAR AND GOT 3 DOWN I
- [SDR 02FDEA00521](https://openairdocs.org/sdr/02FDEA00521), Jul 25, 2002: SHEAR TIE. CORRODED. CORROSION ON SHEAR TIE AT BS 968, RBL 3-5, WL 150. REPAIRED SHEAR TIE IAW SRM.
- [SDR 02FDEA00508](https://openairdocs.org/sdr/02FDEA00508), Jul 20, 2002: SHEAR TIE. GOUGED. SHEAR TIE GOUGED AT BS 540, JUST BELOW STR 14R. REPAIRED SHEAR TIE BS 540 BELOW STR 14R IAW SRM 53-10-4, 53-10-2.
- [SDR 02FDEA00289](https://openairdocs.org/sdr/02FDEA00289), Apr 25, 2002: ALTIMETER. FAILED. CAPT'S ALTIMETER GOT OFF FLAG ON CLIMBOUT, ALSO GOT OFF FLAG IN ALTITUDE ALERT BOX, WHEN OFF FLAG SHOWING, ALTIMETER DIDN'T MOVE. REMOVED AND REPLACED CAPT'S AL
- [SDR 01FDEA00966](https://openairdocs.org/sdr/01FDEA00966), Nov 6, 2001: LINE. BLOWN. NR 1 ENGINE STRUT OVERHEAD LIGHT CAME ON. REMOVED AND REPLACED BLOWN T/R HOSE IN NR 1 PYLON AREA. NO LEAKS NOTED. OK FOR SERVICE.
- [SDR 01FDEA00964](https://openairdocs.org/sdr/01FDEA00964), Nov 2, 2001: CLAMP. LOOSE. NR 1 ENG STRUT OVERHEAD LIGHT ILLUM. SECURED CLAP AND CONNECTOR PER MM 36-00-000-5. OPS CHECK OK.
- [SDR 01FDEA00951](https://openairdocs.org/sdr/01FDEA00951), Nov 1, 2001: CLAMP. LOOSE. 01-357 #1 ENG STRUT OVERHEAT ILLUM IN GLT. TIGHTENED CLAMP ON HIGH PRESS MODULATING VALVE (SHUTOFF).
- [SDR 01FDEA00178](https://openairdocs.org/sdr/01FDEA00178), Mar 7, 2001: FILTER. DIRTY. NR 3 OIL BYPASS LIGHT CAME ON. COMPLIED WITH RED TABS AND SHUTDOWN ENGINE. OIL PRESS AND TEMP NORMAL. *S/D* CHANGE FILTER PER 727-100 MM 79-00-000-2, CHANGE OIL
- [SDR 00FDEA00144](https://openairdocs.org/sdr/00FDEA00144), Mar 8, 2000: FRAME. CORRODED. NR 833, WHILE WORKING NR-0525 FOUND CORROSION ON AFT CARGO DOOR FRAME FWD FRAME WEB STR 26 RT AREA MARKED.
- [SDR 00FDEA00119](https://openairdocs.org/sdr/00FDEA00119), Feb 29, 2000: SKIN. CORRODED. NR 112 SKIN BULGING AT LOWER NOSE CHORD BS 328, RBL 20, JUST ABOVE NOSE GEAR STRUT DOOR CUTOUT (C53-100-01). REPAIRED PER FEDEX EA 7-5330-50011.
- [SDR 00FDEA00090](https://openairdocs.org/sdr/00FDEA00090), Feb 18, 2000: FRAME. CORRODED. WHILE WORKING NR 112 FOUND CORROSION ON NOSE CHORD AT BS 343, RBL 20, WL 149.
- [SDR 00FDEA00089](https://openairdocs.org/sdr/00FDEA00089), Feb 18, 2000: WEB. CORRODED. NR 693 CORROSION (C57-571-01-01) ON L/W FRONT SPAR WEB AT FUEL CELL PANEL CUT OUT 7340, FWD AND AFT WEB SURFACE WS 182. REMOVED AND REPLACED CORROSION PER FEDEX
- [SDR 00FDEA00082](https://openairdocs.org/sdr/00FDEA00082), Feb 16, 2000: FRAME. CORRODED. NR 113 - CORROSION AT INNER CHORD BS 292, RBL22, WL 154, AS SEEN THROUGH LIGHTENING HOLE INSIDE NOSE WW (C53-100-01).
- [SDR 00FDEA00077](https://openairdocs.org/sdr/00FDEA00077), Feb 14, 2000: STRAP. BENT. WHILE WORKING NRC-805 (FUSELAGE 194) FOUND STABILIZER STRAP BS 1030-1130, STR 27R TO BE BENT AND HAS DOUBLE HOLES. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-3
- [SDR 00FDEA00076](https://openairdocs.org/sdr/00FDEA00076), Feb 14, 2000: WEB. GOUGED. WHILE WORKING NR 805 (FUSELAGE 194) FOUND VERTICAL WEB TO BE GOUGED IN SEVERAL LOCATIONS BS 1057-1110, STR 27 RT. *S/D* REMOVED AND REPLACED, ALODINED, PRIMED A
- [SDR 00FDEA00063](https://openairdocs.org/sdr/00FDEA00063), Feb 9, 2000: FRAME. CORRODED. WHILE WORKING NR 113, FOUND SHEAR TIE AT BS 320, RBL 18-21, WL 151 TO BE CORRODED. *S/D* REPAIRED IAW FEDEX SRM 53-10-4 FIG 15.
- [SDR 00FDEA00062](https://openairdocs.org/sdr/00FDEA00062), Feb 9, 2000: FRAME. CORRODED. WHILE WORKING NR 112 FOUND HORIZONTAL CHORD CORRODED BS 348, WL 168, RBL 16. *S/D* REMOVED AND REPLACED CHORD PER IAW FEDEX SRM 51-30-2.
- [SDR 00FDEA00061](https://openairdocs.org/sdr/00FDEA00061), Feb 7, 2000: SKIN. CORRODED. CORROSION AND FASTENERS PULLED THRU OUTER SKIN AT BOTTOM SIDE OF CARGO CUTOUT BS 1065 - 1090, STR 26R. *S/D* REPAIRED AFT CARGO DOOR PER FEDEX EA 7-5330-50016.
- [SDR 00FDEA00040](https://openairdocs.org/sdr/00FDEA00040), Jan 27, 2000: SHEAR TIE. CORRODED. WHILE WORKING NR 0113, FOUND SHEAR TIE AT BS 344, RBL 21-24, WL 151 TO BE CORRODED. *S/D* REPAIRED IAW FEDEX SRM 53-10-4, FIG 11.
- [SDR 00FDEA00039](https://openairdocs.org/sdr/00FDEA00039), Jan 27, 2000: FRAME. GOUGED. MAIN CARGO DOOR REPAIR DOUBLER ON LWR AFT SIDE FRAME WAS GOUGED. *S/D* REMOVED AND REPLACED ALODINED, PRIMED AND INSTALLED PER FEDEX SRM 51-10-2, 51-30-8, 51-20
- [SDR 00FDEA00034](https://openairdocs.org/sdr/00FDEA00034), Jan 25, 2000: FRAME. CRACKED. CRACKED FRAME BS 1050 BETWEEN STR 26 RT & 27 RT. *S/D* REMOVED AND REPLACED PER FEDEX EA 7-5310-47886.
- [SDR 00FDEA00033](https://openairdocs.org/sdr/00FDEA00033), Jan 25, 2000: SKIN. CRACKED. NR 805 - CORROSION AND FASTENERS PULLED THROUGH OUTER SKIN, BOTTOM SIDE OF CARGO DOOR CUT-OUT BS 1065-1090, STR 26R.
- [SDR 00FDEA00035](https://openairdocs.org/sdr/00FDEA00035), Jan 24, 2000: BULKHEAD. DAMAGED. WHILE WORKING 71C101-02, FOUND STRUCTURAL DAMAGE AT BS 227.8, LBL 12, WL 163 ON PRESSURE BULKHEAD. *S/D* REMOVED AND REPLACED PER SRM 51-40-2 FIG 1.
- [SDR 00FDEA00026](https://openairdocs.org/sdr/00FDEA00026), Jan 18, 2000: FLOORBEAM. CORRODED. NR 705 - CORROSION (C53-224-01(1)) ON UPPER CHORD OF FLOORBEAM AT BS 620 BL0- LBL 24, WL 208. REMOVED AND REPLACED PER FEDEX SRM 53-10-8, 53-10-2.
- [SDR 00FDEA00019](https://openairdocs.org/sdr/00FDEA00019), Jan 17, 2000: SKIN. CORRODED. NR 368 - NR 3 K-FLAP TO BULLNOSE I/B BONDING JUMPER HAS CORROSION UNDER ITS WASHERS AT BOTH ATTACH PTS. REPAIRED AND ATTACH PT IAW FEDEX DWG SR 27-57-010 AND SR
- [SDR 00FDEA00018](https://openairdocs.org/sdr/00FDEA00018), Jan 17, 2000: WEB. CRACKED. NR 223 - LT TORQUE BOX WEB LOWER LIGHTENING HOLE AT BS 1297 IS CRACKED. REMOVED AND REPLACED DOUBLER IAW FEDEX SRM 51-40-2.
- [SDR 00FDEA00017](https://openairdocs.org/sdr/00FDEA00017), Jan 17, 2000: CHORD. CORRODED. NR 235 - CORROSION ON REINFORCEMENT CHORD BS1176, LBL 20, WL 208.
- [SDR 00FDEA00016](https://openairdocs.org/sdr/00FDEA00016), Jan 17, 2000: FLOORBEAM. CORRODED. NR 657 - CORROSION (C53-224-02) ON BS 680 FLOORBEAM WL 208, LBL 10.5 AT FASTENER HOLE. REPAIRED FLOORBEAM PER IAW FEDEX SRM 53-10-8 FIG 8.
- [SDR 00FDEA00015](https://openairdocs.org/sdr/00FDEA00015), Jan 17, 2000: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM UPPER TEE BS 640, RBL 27-52, WL 208.
- [SDR 00FDEA00014](https://openairdocs.org/sdr/00FDEA00014), Jan 12, 2000: FRAME. CRACKED. BS 620 FRAME CRACKED IN RADIUS OF STR 20R CUTOUT. *S/D* REMOVED AND REPLACED FRAME, FAB DOUBLER FILLER AND WEB ANGLE, ALODINED, PRIMED SEALED IAW FEDEX EA 7-531
- [SDR 97FDEA00664](https://openairdocs.org/sdr/97FDEA00664), Sep 18, 1997: CLIP. CRACKED. NR 3 AND NR 4 LEFT HAND STRINGER CLIPS AT BS 1050 ARE CRACKED. *S/D* REMOVED CRACKED STRINGER CLIPS AT NR 3 AND NR 4 LT STRINGER AT BS 1050. INSTALLED NEW STRIN
- [SDR 97FDEA00651](https://openairdocs.org/sdr/97FDEA00651), Sep 11, 1997: CHORD. CORRODED. CORROSION (C53-224-08) ON REINFORCEMENT CHORD AT BS 1176.9, RBL 48 AND RBL 37, WL 208. *S/D* FOUND TO BE OUT OF LIMITS. REPLACED SEGMENT OF REINFORCEMENT CHORD 
- [SDR 97FDEA00648](https://openairdocs.org/sdr/97FDEA00648), Sep 11, 1997: SPOILER. DELAMINATED. NR 0195 004 NR 2 SPOILER TRAILING EDGE IS DELAMINATED. REPAIRED NR 2 SPOILER IAW FED-EX SRM 57-50-06.
- [SDR 97FDEA00647](https://openairdocs.org/sdr/97FDEA00647), Sep 11, 1997: SKIN. DELAMINATED. LEFT WING I/B FOREFLAP HAS 6 X 6 AREA OF DELAMINATION ON UPPER I/B END. *S/D* REMOVED DAMAGED SKIN AND REPAIRED IAW FED SRM 51-40-6, LT I/B FOREFLAP.
- [SDR 97FDEA00644](https://openairdocs.org/sdr/97FDEA00644), Sep 10, 1997: FLAP. DELAMINATED. NR 0248 002 LEFT WING I/B MIDFLAP T/E WEDGE HAS AREA OF DELAMINATION ON O/B END. REMOVED DAMAGED AREA 9.25 BY 4 ON UPPER SURFACE OVERLAYED WITH RESIN IMPREGNATE
- [SDR 97FDEA00643](https://openairdocs.org/sdr/97FDEA00643), Sep 10, 1997: FLAP. DELAMINATED. NR 0249 001 RIGHT WING O/B MIDFLAP T/E WEDGE HAS TWO AREAS OF DELAMINATION ON UPPER SKIN. REMOVED DAMAGE 9 BY 3.5 OVERLAYED WITH RESIN IMPREGNATED FIBERGLASS VA

## Other aircraft with N151FE

- [Registered now](https://openairdocs.org/aircraft/N151FE): Boeing 767-300F, S/N 43630, built 2017

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