# N196FE: 1967 Boeing 727-22, registration cancelled 2002-10-15

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 15, 2002
- 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: 19145
- Year built: 1967
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: August 30, 1967
- Certificate issued: November 30, 1990
- Last registry action: September 19, 2000
- Mode S code: A17EF7
- 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/N196FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=196FE
- Page: https://openairdocs.org/deregistered/N196FE-2002-10-15

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 (43)

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

- [SDR 99FDEA00239](https://openairdocs.org/sdr/99FDEA00239), Jun 24, 1999: HINGE. LOOSE. 99-146 - WHEN LEFT ELEVATOR IS DEFLECTED UP IT MAKES A POPPING SOUND AND BOWS OUT THE LWR ACCESS PNL ON STAB FWD OF ELEVATOR. REMOVED AND REPLACED BALANCE PANEL
- [SDR 99FDEA00072](https://openairdocs.org/sdr/99FDEA00072), Feb 19, 1999: SHEAR TIE. CORRODED. CORROSION (C53-113-01, 2) ON SHEAR TIE BS 990, LBL 17, WL 140. *S/D* REMOVED, FABBED AND INSTALLED NEW SHEAR TIE BS 990, LBL 17, WL 140 IAW FEDEX SRM 53-10-04.
- [SDR 99FDEA00070](https://openairdocs.org/sdr/99FDEA00070), Feb 19, 1999: SHEAR TIE. CRACKED. NR 244 - SHEAR TIE ON WEB AT BS 336 HAS CRACK IND IN UPPER O/B RADIUS OF CUT OUT FOR STR 25 AND 26 RT.
- [SDR 99FDEA00061](https://openairdocs.org/sdr/99FDEA00061), Feb 15, 1999: WEB. CORRODED. CORROSION (C53-113-0 1/2) ON VERTICAL WEB AND ATTACH BRACKET, BS 987 TO 990, STR 28 RT, WL 140. * S/D* REMOVED AND REPLACED VERTICAL WEB AND ATTACH BRACKET BS 9
- [SDR 98FDEA00015](https://openairdocs.org/sdr/98FDEA00015), Jan 8, 1998: PNEUMATIC DUCT. BLOWN. REJECTED TAKEOFF AT 85 KNOTS DUE TO NR 3 ENGINE FIRE WARNING. COMPLETED ENGINE FIRE CHECK LIST AND REJECTED TAKEOFF CHECK LIST. REJECTED TAKEOFF BRAKE COOLING C
- [SDR 96FDEA01423](https://openairdocs.org/sdr/96FDEA01423), Sep 2, 1996: FRAME. CRACKED. NR 0255 AND 037, CRACK ON FRAME AT BS 1110, STR 27R, RBL 22 WL 153.
- [SDR 96FDEA01420](https://openairdocs.org/sdr/96FDEA01420), Aug 30, 1996: SKIN. CORRODED. REMOVE AND INSTALLED NEW BELLY SKIN FROM BS 950 TO 1080.45, STR 26 LT TO 26 RT DUE TO MULTIPLE REPAIRS REQUIRED. REMOVED AND REPLACED BELLY SKIN FROM BS 950 TO 
- [SDR 96FDEA01418](https://openairdocs.org/sdr/96FDEA01418), Aug 29, 1996: WEB. CORROSION. WHILE WORKING NR O610, FOUND CORROSION ON WEB UNDER STIFFENER, STA 310, WL 184. REMOVED CORRODED WEB, FABRICATED NEW WEB AND SPLICE AT BS 294 TO BS 315, RBL 12 
- [SDR 96FDEA01401](https://openairdocs.org/sdr/96FDEA01401), Aug 23, 1996: FLOOR BEAM. CORROSION. NR-0618 032, CORROSION (C53-111-01, -2) ON FLOOR BEAM STA 680 RBL 20 TO LBL 20 WL 200 FWD BAY.
- [SDR 96FDEA1395](https://openairdocs.org/sdr/96FDEA1395), Aug 22, 1996: STRINGER. CORRODED. NR0711 AND 031, WHILE WORKING ON NR0698 FOUND CORROSION ON STRINGER 30 BS 964.
- [SDR 96FDEA01395](https://openairdocs.org/sdr/96FDEA01395), Aug 22, 1996: STRINGER. CORRODED. NR0711 AND 031, WHILE WORKING ON NR0698 FOUND CORROSION ON STRINGER 30 BS 964. *S/D* REMOVED CORROSION ON SIR 30 BS 964, OUT OF LIMITS IAW FEDEX SRM 53-10-01. R
- [SDR 96FDEA01394](https://openairdocs.org/sdr/96FDEA01394), Aug 22, 1996: SHEAR TIE. CORRODED. NR 0648 AND 030, CORROSION ON CHORD BS 350 RBL 18 TO LBL 18 WL 148 UNDER NUTPLATES.
- [SDR 96FDEA01385](https://openairdocs.org/sdr/96FDEA01385), Aug 19, 1996: ANGLE. CORRODED. NR0698 AND 029, CORROSION ON KEEL BEAM SUPPORT ANGLE AT BS 950 LBL TO RBL 5 WL 138.
- [SDR 96FDEA01383](https://openairdocs.org/sdr/96FDEA01383), Aug 19, 1996: SHEAR TIE. CORRODED. NR0673 AND 028, WHILE WORKING NR0668 FOUND BULGE IN BETWEEN SKIN AND FRAME AT BS 1030 BETWEEN STR 18 TO 19L.
- [SDR 96FDEA01382](https://openairdocs.org/sdr/96FDEA01382), Aug 19, 1996: FITTING. CORRODED. NR0360 AND 027, CORROSION (C57-581-01-1) LT WING O/B AILERON CONTROL ROD FITTING ON AILERON IS CORRODED. *S/D* REMOVED AND REPLACED LT WING O/B AILERON CONTROL 
- [SDR 96FDEA01381](https://openairdocs.org/sdr/96FDEA01381), Aug 19, 1996: DOUBLER. CORROSION. NR0696 AND 002, CORROSION ON SKIN SPLICE DOUBLER AT BS 1080 FROM RBL 23 TO LBL 32 WL 140. ALSO, (P/N 65-18387-15). *S/D* REMOVED CORROSION ON SKIN SPLICE DOUBLE
- [SDR 96FDEA01380](https://openairdocs.org/sdr/96FDEA01380), Aug 19, 1996: STRINGER. CORRODED. NR0129 AND 025, CORROSION (C53-224-02, -1) ON STR 6L BS 700 TO 680. *S/D* CORROSION ON STR NR 6L BS 700 TO 680 WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10
- [SDR 96FDEA01379](https://openairdocs.org/sdr/96FDEA01379), Aug 19, 1996: STRINGER. CRACKED. NR0672 AND 024, WHILE WORKING NR201 FOUND STR TO BE CRACKED AT BS 1082 WL 138 STR 29L.
- [SDR 96FDEA01378](https://openairdocs.org/sdr/96FDEA01378), Aug 19, 1996: SHEAR TIE. CRACKED. NR0681 AND 023, CRACKED SHEAR TIE AT BS 970 BETWEEN STR 29 TO 30R.
- [SDR 96FDEA01377](https://openairdocs.org/sdr/96FDEA01377), Aug 19, 1996: SHEAR TIE. CRACKED. NR0682 AND 022, CRACKED SHEAR TIE AT BS 970 BETWEEN STR 28 TO 29R. *S/D* REMOVED CRACKED SHEAR TIE AND REPLACED IAW FEDEX SRM 51-30-2.
- [SDR 96FDEA01376](https://openairdocs.org/sdr/96FDEA01376), Aug 19, 1996: SHEAR TIE. CRACKED. NR0683 AND 021, CRACKED SHEAR TIE AT BS 990 BETWEEN STR 29 TO 30R.
- [SDR 96FDEA01375](https://openairdocs.org/sdr/96FDEA01375), Aug 19, 1996: SHEAR TIE. CORRODED. NR0689 AND 020, CORROSION ON SHEAR TIE AT BS 170 BETWEEN STR 28 TO 29R.
- [SDR 96FDEA01374](https://openairdocs.org/sdr/96FDEA01374), Aug 19, 1996: SHEAR TIE. CORRODED. NR0690 AND 019, CORROSION ON SHEAR TIE AT BS 990 BETWEEN STR 29 TO 30L. *S/D* REPAIRED SHEAR TIE AT BS 990 BETWEEN STRINGER 29 LEFT AND 30 LEFT AS PER FEDEX SRM
- [SDR 96FDEA01384](https://openairdocs.org/sdr/96FDEA01384), Aug 16, 1996: CLIP. CRACKED. NR0119 AND 018, CRACKED STR CLIP AT BS 970 STR 16R. *S/D* REMOVED CRACKED STRINGER CLIP AT BS 970 STRINGER 16 RT AND REPLACED WITH NEW IAW FEDEX SRM 51-30-2.
- [SDR 96FDEA01372](https://openairdocs.org/sdr/96FDEA01372), Aug 16, 1996: FLOOR BEAM. CORRODED. NR0550 AND 017, CORROSION (C53-224-01, -1) ON FLOOR BEAM UPPER CHORD BS 344 LBL 65 RBL 17 WL 208.
- [SDR 96FDEA01367](https://openairdocs.org/sdr/96FDEA01367), Aug 15, 1996: FORMER. CORRODED. NR 0664 AND 016. WHILE WORKING NR 0647, DISCOVERED CORROSION ON RT LOWER SKIN FORMER ANGLE AT BS 951, RBL 8 WL 138. ****S/D**** COMING.
- [SDR 96FDEA01366](https://openairdocs.org/sdr/96FDEA01366), Aug 15, 1996: FLOOR BEAM. CORRODED. NR 0627 AND 015. CORROSION C53-224-01(1) AND BARE METAL ON BS 560 BEAM FROM LBL 62 - RBL 24 WL 208.1. ******S/D**** COMING.
- [SDR 96FDEA01365](https://openairdocs.org/sdr/96FDEA01365), Aug 14, 1996: STIFFENER. CORROSION. NR 0611 AND 014. CORROSION C53-111-01 ON HORIZONTAL STIFFENER STA 310 RBL 12 WL 178. ****S/D****** COMING.
- [SDR 96FDEA01364](https://openairdocs.org/sdr/96FDEA01364), Aug 14, 1996: STIFFENER. CORROSION. NR 0607 AND 013. CORROSION C53-111-01(1) ON HORIZONTAL STIFFENER STA 314 RBL 12 WL 178. ****S/D***** COMING.
- [SDR 96FDEA01363](https://openairdocs.org/sdr/96FDEA01363), Aug 14, 1996: FRAME. CORRODED. NR 0623 AND 012. CORROSION C53-111-01 ON FRAME STA 700 STR 27L - R WL 156. ****S/D***** COMING.
- [SDR 96FDEA01357](https://openairdocs.org/sdr/96FDEA01357), Aug 13, 1996: CHORD. CORRODED. NR0562 AND 011, CORROSION (C53-224-08) ON 1176.9 REINFORCEMENT CHORD AT LBL 63 WL 208.1 OUT OF LIMITS PER FEDEX SRM 53-10-01.
- [SDR 96FDEA01356](https://openairdocs.org/sdr/96FDEA01356), Aug 13, 1996: KEEL BEAM. CORRODED. NR0647 AND 010, CORROSION (C53-100-3) BETWEEN SKIN AND KEEL BEAM BS 1062 STR 29R. *S/D* REMOVED AND REPLACED RT KEEL BEAM STR 29R FROM BS 960 TO BS 1090 PER SB 
- [SDR 96FDEA01355](https://openairdocs.org/sdr/96FDEA01355), Aug 13, 1996: NOSE CHORD. CORROSION. NR0610 AND 009, CORROSION (C53-111-01, -1) ON RT UPPER NOSE CHORD STA 312, 318, 330 RT WL 168 DOG HOUSE. *S/D* REMOVED AND REPLACED RT MID NOSE CHORD BS 294 TO 
- [SDR 96FDEA01422](https://openairdocs.org/sdr/96FDEA01422), Aug 12, 1996: STRINGER. CORRODED. NR 0597 AND 036, BULGE IN SKIN AT BS 1157, STR 27 L.
- [SDR 96FDEA01336](https://openairdocs.org/sdr/96FDEA01336), Aug 8, 1996: WEB. CORRODED. NR0633 AND 008, CORROSION (C53-221-01) ON WEB AND OUTBOARD CF FRAME STA 227.8 RBL 42 WL 211 TO 233. *S/D* REPAIRED WEB AT STA 227 TO 8, RBL 42, WL 227.
- [SDR 96FDEA01335](https://openairdocs.org/sdr/96FDEA01335), Aug 8, 1996: FLOOR BEAM. CORRODED. NR0560 AND 007, CORROSION (C53-224-01, -3) ON BS 1110 BEAM RBL 26 TO 45 WL 208.1. *S/D* CUT OUT CORROSION AND INSTALLED REPAIR ON BS 1110 BEAM RBL 26 TO 45 WL 2
- [SDR 96FDEA01334](https://openairdocs.org/sdr/96FDEA01334), Aug 8, 1996: SKIN. DELAMINATED. NR0577 AND 006, UPPER RUDDER TAB LOWER SURFACE RT AND LT HAS AREAS OF DELAMINATION. *S/D* REPAIRED UPPER RUDDER TAB LOWER SURFACE RT AND LT PER FEDEX SRM 51-40-
- [SDR 96FDEA01326](https://openairdocs.org/sdr/96FDEA01326), Aug 7, 1996: FLOOR BEAM. CORRODED. NR 0114 AND 005. CORROSION C53-111-01(3) ON FLOOR BEAM UNDER NUTPLATES AT BS 1050 FROM LBL 32 - RBL 41, WL 200 (AFT BAY). *****S/D***** COMING.
- [SDR 96FDEA01325](https://openairdocs.org/sdr/96FDEA01325), Aug 7, 1996: FLOOR BEAM. CORRODED. NR0111 AND 004, CORROSION (C53-111-01, -3) ON FLOOR BEAM UNDER NUTPLATES AT BS 1110 WL 200 LBL 32 TO RBL 43 AFT BAY. *S/D* REPAIRED FLOOR BEAM AT BS 1110, WL 20
- [SDR 96FDEA01324](https://openairdocs.org/sdr/96FDEA01324), Aug 7, 1996: FRAME. CORROSION. NR 0176 AND 003. CORROSION C53-111-01(3) ON FRAME AT BS 1057, RBL 30, WL 149. ****S/D**** COMING.
- [SDR 96FDEA01323](https://openairdocs.org/sdr/96FDEA01323), Aug 6, 1996: KEEL BEAM. CORRODED. NR0201 AND 002, BS 1050 STR 29L LBL 6 THERE IS A BULGE IN SKIN. *S/D* REMOVED AND REPLACED LT KEEL BEAM STR 296 FROM BS 960 TO BS 1090 PER SB 727-53-0179.
- [SDR 96FDEA1313](https://openairdocs.org/sdr/96FDEA1313), Aug 5, 1996: SKIN. DELAMINATION. NR0012 AND 001, RIGHT WING I/B AFT FLAP HAS TEMPORARY REPAIR THAT NEEDS TO BE MADE PERMANENT. *S/D* REPAIRED RIGHT WING I/B AFT FLAP IAW FEDEX SRM 51-40-6.
- [SDR 96FDEA01247](https://openairdocs.org/sdr/96FDEA01247), Jul 3, 1996: SKIN. LIGHTNING STRIKE. NR 0430, 026, 4 LIGHTNING STRIKES BS 182 TO 192, LT WL 225 TO 227.

## Other aircraft with N196FE

- [Registered now](https://openairdocs.org/aircraft/N196FE): Boeing 767-300F, S/N 63126, built 2021

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