# N184FE: 1966 Boeing 727-22, registration cancelled 2002-10-15 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 15, 2002 - Status when cancelled: Valid registration - 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: 18870 - Year built: 1966 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: April 24, 1966 - Certificate issued: August 14, 1989 - Last registry action: November 16, 1999 - Mode S code: A1500A - Owner when cancelled: [Federal Express Corpoation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPOATION) - 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/N184FE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=184FE - Page: https://openairdocs.org/deregistered/N184FE-2002-10-15 From the FAA registry file of October 27, 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 (21) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 99FDEA00034](https://openairdocs.org/sdr/99FDEA00034), Jan 30, 1999: LANDING GEAR. VIBRATED. VIBRATION IN THE AREA OF NOSE WHEEL AND A FLICKER OF A RED DOOR LIGHT ABOVE GEAR HANDLE. WHEN GEAR LEVER WAS RAISED NO ADDITIONAL VIB WERE FELT. INSPECTED NOSE - [SDR 98FDEA00451](https://openairdocs.org/sdr/98FDEA00451), Jul 11, 1998: SWITCH. MALFUNCTIONED. 98-0176 STA-MEM: AFTER TAKEOFF WHEN GEAR WAS RAISED, THE GREEN NLG LIGHT AND RED GEAR DOOR LIGHT FOR NOSE GEAR REMAINED ON. AFM PROCEDURES WERE FOLLOWED BUT NO - [SDR 98FDEA00448](https://openairdocs.org/sdr/98FDEA00448), Jul 9, 1998: SWITCH. INOP. STA-MEM: NOSE GEAR UNSAFE. RECYCLED 4 TIMES, FOURTH TIME AFTER 3 MINUTES DELAY GOT GREEN LIGHT. NOSE ALIGNMENT STRIPE SAFE. REPEAT. INSTALLED (3) GEAR LOCK PINS - [SDR 98FDEA00350](https://openairdocs.org/sdr/98FDEA00350), May 15, 1998: RETRACT MECH. LACK OF LUBE. ON FINAL, NOSE GEAR DID NOT INDICATE DOWN (NO GREEN LIGHT) WHEN GEAR DOWN WAS INITIALLY SELECTED. GEAR HANDLE RECYCLED AND ALL GEAR INDICATED NORMAL DOWN AND LO - [SDR 97FDEA00849](https://openairdocs.org/sdr/97FDEA00849), Nov 20, 1997: PANEL. MALFUNCTION. 97-0237 NOSE GEAR DID NOT INDICATE DOWN SAFE (GREEN LIGHT NOT ON.) NOSE GEAR LIGHT WOULD NOT TEST. GEAR DOOR LIGHT TRANSITIONED NORMALLY WITH EXTENSION AND RETR - [SDR 97FDEA00806](https://openairdocs.org/sdr/97FDEA00806), Nov 4, 1997: KEEL BEAM. CORRODED. NR 0388 016 CORROSION ON THE L/H KEEL BEAM BETWEEN SKIN BS 1065. *** S/D *** REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED DAMAGED PORTION BS 1057 TO 1087. RE - [SDR 97FDEA00801](https://openairdocs.org/sdr/97FDEA00801), Nov 3, 1997: SHEAR TIE. CORRODED. NR 0446 014 CORROSION (C53-113-01(2)) IN THE SHEAR TIE BS 990, BETWEEN STRINGERS 29 & 30 R/H. *** S/D *** REPAIRED SHEAR TIE AT BS 990, RBL 6, WL 151 IAW FED-EX - [SDR 97FDEA00800](https://openairdocs.org/sdr/97FDEA00800), Nov 3, 1997: SPLICE. CORRODED. NR 0421 015 CORROSION IN THE STRINGER SPLICE AT BS 1057, STR 28 R/H. *** S/D *** REMOVED STRINGER SPLICE AT BS 1057. REMOVED STRINGER END PIECE AT BS 1040-1057. - [SDR 7FDEA00791](https://openairdocs.org/sdr/7FDEA00791), Oct 29, 1997: SHEAR TIE. CRACKED. NR 0427 013 CORROSION (C53-113-01(2)) ON THE SHEAR TIE AT BS 1130 OUTBOARD OF STRINGER 29L. *** S/D *** REMOVED SHEAR TIE. FABRICATED NEW SHEAR TIE. INSTALLED P - [SDR 97FDEA00784](https://openairdocs.org/sdr/97FDEA00784), Oct 28, 1997: FLOORBEAM. CORRODED. NR 0253 009 CORROSION (C53-224-06) ON FLOORBEAM BS 344, RBL 15-LBL 60, WL 208. UPPER CHORD OF 344 FLOORBEAM, RBL 65 TO LBL 65, WL 208 WAS FOUND TO BE OUT OF LIM - [SDR 97FDEA00783](https://openairdocs.org/sdr/97FDEA00783), Oct 28, 1997: FRAME. CRACKED. NR 0412 010 AFT CARGO BAY AT BS 1130, STR 26L THE FRAME IS CRACKED IN THE J SECTION. *** S/D ***INSTALLED DOUBLER ON FRAME AT 26L BS 1130 AFT CARGO BAY AS PER F - [SDR 97FDEA00782](https://openairdocs.org/sdr/97FDEA00782), Oct 28, 1997: RIB. CORRODED. NR 0083 011 NR 2 K-FLAP CORRODED AT I/B BONDING JUMPER TO BULLNOSE. REMOVED CORROSION ON NR 2 K-FLAP I/B BULLNOSE ATTACH (LOWER) POINT FLANGE THICKNESS .140. RE - [SDR 97FDEA00781](https://openairdocs.org/sdr/97FDEA00781), Oct 28, 1997: RIB. CORRODED. NR 0173 012 CORROSION AT BONDING WIRE UPPER AND LOWER ATTACH POINTS ON NR 4 K-FLAP BULLNOSE, O/B END. REMOVED CORROSION AT BONDING WIRE UPPER AND LOWER ATTACH P - [SDR 97FDEA00777](https://openairdocs.org/sdr/97FDEA00777), Oct 27, 1997: FLOORBEAM. CORRODED. NR 0103 008 CORROSION (C53-224-06) ON FLOORBEAM BS 328, LBL 37, WL 208. REMOVED CORROSION (C53-224-06) FOUND TO BE OUT OF LIMITS. REPAIRED BS 328, LBL 37, WL 20 - [SDR 97FDEA00776](https://openairdocs.org/sdr/97FDEA00776), Oct 27, 1997: STRINGER. CRACKED. NR 0417 007 AFT CARGO BAY AT BS 1113, STRINGER 28 R/H IS CRACKED ON INBOARD SIDE. *** S/D *** REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, ALODINED, PRIMED AN - [SDR 97FDEA00771](https://openairdocs.org/sdr/97FDEA00771), Oct 23, 1997: STRINGER. CORRODED. CORROSION (C53-113-01, 2) ON INBOARD SIDE OF STRINGER 28 RT, BS 1130. *S/D* REMOVED AND REPLACED STRINGER 28 RT IAW FED-EX SRM 53-10-3 FIG 1 SHT 1 WORK ACCOMPLI - [SDR 97FDEA00768](https://openairdocs.org/sdr/97FDEA00768), Oct 21, 1997: SPAR CHORD. CORRODED. CORROSION (C53-224-05) WING CENTER SECTION FRONT SPAR LOWER CHORD RBL 25, BS 740. *S/D* FOUND CORROSION OUT OF LIMITS. REMOVED WING CENTER SECTION FRONT SPAR LO - [SDR 97FDEA00761](https://openairdocs.org/sdr/97FDEA00761), Oct 17, 1997: WEDGE. DELAMINATED. RT WING O/B MIDFLAP T/E WEDGE IS DELAMINATED 24 FROM I/B END AND AT THE NR 2 AFT FLAP TRACK, UPPER AND LOWER SURFACE. *S/D* FOUND CORROSION ON T/E WEDGE SPAR TO - [SDR 97FDEA00760](https://openairdocs.org/sdr/97FDEA00760), Oct 17, 1997: WEDGE. DELAMINATED. LT WING I/B MIDFLAP T/E WEDGE IS DELAMINATED AT 20 FROM I/B END, UPPER AND LOWER SURFACE. *S/D* FOUND CORROSION ON T/E WEDGE SPAR TO BE OUT OF LIMITS. REMOVED A - [SDR 97FDEA00755](https://openairdocs.org/sdr/97FDEA00755), Oct 16, 1997: BONDING JUMPER. CORRODED. NR 2 K-FLAP BULLNOSE CORRODED ON O/B BONDING JUMPER. *S/D* REMOVED CORROSION AND REPAIRED NR 2 K-FLAP O/B BULLNOSE BONDING JUMPER UPPER ATTACH POINT IAW FED-EX - [SDR 97FDEA00742](https://openairdocs.org/sdr/97FDEA00742), Oct 15, 1997: WEDGE. DELAMINATED. NR 0079 001, R/W I/B MIDFLAP T/E WEDGE IS DELAMINATED 16 FROM I/B END. ## Other aircraft with N184FE - [Registered now](https://openairdocs.org/aircraft/N184FE): Boeing 767-300F, S/N 63115, built 2020 --- 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.