# N192FE: 1966 Boeing 727-22, registration cancelled 2007-05-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 2, 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 series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Serial number: 19085
- Year built: 1966
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: March 26, 2004
- Certificate issued: March 17, 2004
- Last registry action: March 20, 2007
- Mode S code: A1701B
- 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/N192FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=192FE
- Page: https://openairdocs.org/deregistered/N192FE-2007-05-02

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

## Service difficulty reports (53, newest 50)

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

- [SDR 06FDEA1958](https://openairdocs.org/sdr/06FDEA1958), May 17, 2006: SKIN. CORRODED. LOWER SKIN OF LEFT HORIZONTAL STAB HAS NUMEROUS AREAS OF CORROSION FROM STAB TIP TO I/B END, FWD SRAP TO AFT SPAR. REPAIRED PER FED EX EA 7-5510-102242.
- [SDR 06FDEA1941](https://openairdocs.org/sdr/06FDEA1941), May 17, 2006: BEAM. CHAFED. WHILE GETTING AND OK TO CLOSE, FOUND RT ELEVATOR RUB BLOCK SPACER LOOSE AND CHAFING INTO LOWER TRAILING EDGE BEAM AT ELEV STA 118.13 . REPAIRED RT HORIZ STAB LO
- [SDR 06FDEA1928](https://openairdocs.org/sdr/06FDEA1928), May 15, 2006: DOOR FRAME. CORRODED. LEFT AFT EMERGENCY EXIT SEAL FRAME CORRODED. FOUND CORROSION ON SEAL FRAME TO BE OUT OF LIMITS. REMOVED AND REPLACED LT AFT EMERGENCY EXIT HATCH PER MM 52-21-00
- [SDR 06FDEA1911](https://openairdocs.org/sdr/06FDEA1911), May 12, 2006: ATTACH FITTING. CORRODED. NR 2 FLAP TRACK FWD ATTACH FITTING IS CORRODED. REMOVED, REPAIRED AND REINSTALLED NR 2 FLAP TRACK FWD ATTACH FITTING IAW OHM 20-50-01 ANS FED EX EA 7-5710-96623
- [SDR 06FDEA1800](https://openairdocs.org/sdr/06FDEA1800), May 11, 2006: SKIN. DAMAGED. LT HORIZONTAL STAB HAS A BLEND OUT THAT EXCEEDS SRM LIMITS AT STAB STA 77.1, .500 FWD OF THE EDGE OF THE T/E SKIN. REPAIRED LT HORIZONTAL STAB LWR SKIN PER FED 
- [SDR 06FDEA1799](https://openairdocs.org/sdr/06FDEA1799), May 11, 2006: SKIN. CORRODED. FOUND LOWER SKIN OF RIGHT HORIZONTAL STAB HAS NUMEROUS AREAS OF CORROSION FROM STAB TIP TO IB END, FWD SPAR TO AFT SPAR. REPAIRED PER FED EX EA 7-5510-102242.
- [SDR 06FDEA1777](https://openairdocs.org/sdr/06FDEA1777), May 10, 2006: SKIN. DENTED. LWR FWD CARGO DOOR FWD EDGE OF EXTERIOR SKIN HAS SEVERAL DENTS. *S/D* REMOVED AND REPLACED LWR FWD CARGO DOOR IAW FED EX MM 52-31-000-4.
- [SDR 06FDEA1738](https://openairdocs.org/sdr/06FDEA1738), May 8, 2006: ATTACH FITTING. UNKNOWN. N01182 COMPLY WITH EO 7-5710-7-2314D PT5- WINGS MLG TRUNION ATTATCH FITTING MODIFICATION SB 727-57A0132R3 AD 2004-18-08, LT SIDE. COMPLIED WITH FED EX EO 7-5710
- [SDR 06FDEA1724](https://openairdocs.org/sdr/06FDEA1724), May 5, 2006: FITTING. CRACKED. WHILE INSPECTING BS 870 RT TERMINAL FITTING PER FED EX EO 7-5310-7-3663 03 PART 4 FOUND CRACK INDICATION IN ROW 3 HOLE NR 5. REPAIRED DAMAGED HOLE BS 870 TERMIN
- [SDR 06FDEA1702](https://openairdocs.org/sdr/06FDEA1702), May 4, 2006: FRAME. GOUGED. LWR FWD CARGO DOOR CUTOUT AFT SIDE FRAME IS GOUGED FWD OF LATCH FITTING STR 23 RT. REPAIRED LOWER FWD CARGO DOOR CUTOUT AFT SIDE FRAME IAW FED EX EA 7-5310-9951
- [SDR 06FDEA1703](https://openairdocs.org/sdr/06FDEA1703), May 4, 2006: SKIN. CORRODED. LT WING, I/B MID FLAP UPPER SKIN IS CORRODED, 4 INCHES FROM T/E AND 12 INCHES AND 58 INCHES FROM I/B END. *S/D* REMOVED & REPLACED FLAP PER FED EX MM 27-51-013.
- [SDR 06FDEA1697](https://openairdocs.org/sdr/06FDEA1697), May 3, 2006: FLAP TRACK. DAMAGED. NR 6 FLAP TRACK AFT ATTACH FITTING DAMAGED OB BARREL NUT HOLE. REMOVED AND REPLACED NR 6 FLAP TRACK AFT O/B ATTACH FITTING PER SRM 51-30-02 AND SRM 51-20-01.
- [SDR 06FDEA1655](https://openairdocs.org/sdr/06FDEA1655), May 1, 2006: FLOORBEAM. CORRODED. FOUND 1110 FLOORBEAM CORRODED ON LOWER FLANGE LBL 30 TO RBL 30. REMOVED AND REINSTALLED AFT CARGO BAY CEILING PANELS BS 1110 TO BS 1170 AND REMOVED AND REINSTAL
- [SDR 06FDEA1664](https://openairdocs.org/sdr/06FDEA1664), May 1, 2006: SUPPORT FITTING. CORRODED. NR 1 ENG PYLON ON FWD ENG MOUNT CASTING O/B OF PYLON HAS CORROSION ON FWD AND AFT SIDES IN SEVERAL AREAS. COMPLIED WITH FED EX EA 7-5410-99512 ON NR 1 ENGINE PY
- [SDR 06FDEA1663](https://openairdocs.org/sdr/06FDEA1663), May 1, 2006: SUPPORT FITTING. CORRODED. NR 1 ENG PYLON HAS CORROSION ON FWD ENG SUPPORT FITTING WEB FWD LWR I/B JUST ABOVE LWR HORIZONTAL FLANGE COMMON TO EO 7-5410-7-3304 P9 PAGE 12 FIG 2. *S/D* COMP
- [SDR 06FDEA1662](https://openairdocs.org/sdr/06FDEA1662), May 1, 2006: FLANGE. CORRODED. NR 1 ENG PYLON ON FWD ENG SUPPORT HORIZONTAL FLANGE HAS CORROSION ON UPPER FWD EDGE. *S/D* COMPLIED WITH FED EX EA 7-5410-99512.
- [SDR 06FDEA1612](https://openairdocs.org/sdr/06FDEA1612), Apr 26, 2006: STRINGER CLIP. CORRODED. STA 380 STR 19L CORROSION ON STR CLIP. *S/D* REMOVED AND REPLACED STRINGER CLIP AT BS 380, STR 19L, PER SRM 51-30-2.
- [SDR 06FDEA1578](https://openairdocs.org/sdr/06FDEA1578), Apr 24, 2006: SHEAR TIE. CRACKED. FOUND CRACK IN OEM SHEAR TIE AT BS 520 ABOVE STR 22L. REPAIRED OEM SHEAR TIE AT BS 520 ABOVE STR 22L IAW SRM 53-10-04.
- [SDR 06FDEA1576](https://openairdocs.org/sdr/06FDEA1576), Apr 24, 2006: SHEAR TIE. CORRODED. STA 1030 STR 29R, CORROSION ON FRAME OUTBOARD FLANGE. *S/D* REMOVED AND REPLACED SHEAR TIE ON BS 1030, STR 29R FRAME OUTBOARD FLANGE IAW SRM 53-10-4.
- [SDR 06FDEA1577](https://openairdocs.org/sdr/06FDEA1577), Apr 24, 2006: STRUCTURE. CRACKED. BS 961, RBL 10, STR 29R AT BS 961, RBL 10, STR 29R, STRUCTURE IS CRACKED. REMOVED DAMAGE AND REPAIRED CHORD PER SRM 51-40-04.
- [SDR 06FDEA1566](https://openairdocs.org/sdr/06FDEA1566), Apr 21, 2006: FRAME. CORRODED. STA 970 BETWEEN STR 29L AND STR 30, CORROSION ON FRAME OUTBOARD FLANGE. *S/D* REPAIRED PER SRM 53-10-4.
- [SDR 06FDEA1486](https://openairdocs.org/sdr/06FDEA1486), Apr 17, 2006: SKIN. DELAMINATED. RIGHT WING I/B FORE FLAP DELAMINATED MID SPAN ON UPPER SURFACE. *S/D* REPAIRED DELAM ON UPPER SURFACE ON RIGHT WING I/B FORE FLAP PER SRM 51-40-20.
- [SDR 06FDEA1455](https://openairdocs.org/sdr/06FDEA1455), Apr 14, 2006: WEB. GOUGED. FOUND FUSELAGE BS 480 TO 640, STR 3L, CARGO DOOR SURROUND WEB GOUGED IN NUMEROUS AREAS. ALL WORK ACCOMPLISHED IAW FEDEX EA 7-5330-99510.
- [SDR 06FDEA1422](https://openairdocs.org/sdr/06FDEA1422), Apr 12, 2006: WEB. CORRODED. FOUND CORROSION ON FLOOR WEB, BS 1130 TO 1176 RBL 49 TO 63, WL 208. REPAIRED FLOOR WEB AT BS 1130 TO 1176 RBL 49 TO 63, WL 208 IAW SRM 51-40-02.
- [SDR 06FDEA1360](https://openairdocs.org/sdr/06FDEA1360), Apr 10, 2006: BULKHEAD. CRACKED. CRACK IN BULKHEAD AT BS 870, LBL 12, WL 138. *S/D* REPAIRED CRACK IN BULKHEAD BS 870, LBL 12, WL 138 IAW SRM 53-10-9 FIG 4.
- [SDR 06FDEA1359](https://openairdocs.org/sdr/06FDEA1359), Apr 10, 2006: BULKHEAD. CRACKED. CRACK IN BULKHEAD AT BS 870, RBL 12, WL 138. *S/D* REPAIRED CRACK IN BULKHEAD BS 870 RBL 12 WL 138 IAW SRM 53-10-9 FIG 4.
- [SDR 06FDEA1358](https://openairdocs.org/sdr/06FDEA1358), Apr 10, 2006: SUPPORT ANGLE. CRACKED. FOUND CRACK ON LOWER SUPPORT ANGLE AT BS 870 LBL 12 WL 138. REPAIRED CRACKED ANGLE AT BS 870 RBL 12 WL 138 IAW SRM 54-10-9.
- [SDR 06FDEA1363](https://openairdocs.org/sdr/06FDEA1363), Apr 10, 2006: KEELBEAM. CORRODED. STA 1030 - 1050 STR 29R HAS CORROSION ON STR FLANGE.
- [SDR 06FDEA1362](https://openairdocs.org/sdr/06FDEA1362), Apr 10, 2006: KEELBEAM. CORRODED. FOUND STA 1034 STR 29L, CORROSION ON STR FLANGE AT RIVET TAIL.
- [SDR 06FDEA1361](https://openairdocs.org/sdr/06FDEA1361), Apr 10, 2006: WEB. TOOL DAMAGE. FOUND DRILL START BEHIND VERTICAL STIFFENER ON FWD SIDE OF 870 WEB.
- [SDR 06FDEA1337](https://openairdocs.org/sdr/06FDEA1337), Apr 7, 2006: WEB. CORRODED. FOUND CORROSION ON FLOOR WEB, BS 1155, RBL 41, WL 208. REPAIRED PER SRM 51-40-02.
- [SDR 06FDEA1335](https://openairdocs.org/sdr/06FDEA1335), Apr 7, 2006: GUSSET. DAMAGED. UPON REMOVAL OF SHEAR WEB AT BS 1176, FOUND GUSSET TO BE DAMAGED AROUND LUG AT BS 1176, WL 208, LBL 18. *S/D* REMOVED AND REPLACED GUSSET BS 1176, LBL 18, WL 20
- [SDR 06FDEA1336](https://openairdocs.org/sdr/06FDEA1336), Apr 7, 2006: SKIN. DENTED. FOUND FUSELAGE SKIN DENT BS 693, 5" BELOW STR 26R. REPAIRED PER SRM 53-30-3.
- [SDR 06FDEA1334](https://openairdocs.org/sdr/06FDEA1334), Apr 7, 2006: SKIN. CORRODED. RT HORIZONTAL STABILIZER CORROSION REMOVAL DAMAGE IS OUT OF LIMITS AT RT STAB STA 120, .5 INCHES AFT OF THE LE SPAR AND FWD EDGE OF THE SKIN NECESSITATING A REP
- [SDR 06FDEA1333](https://openairdocs.org/sdr/06FDEA1333), Apr 7, 2006: SKIN. CORRODED. FOUND RT HORIZONTAL STABILIZER CORROSION REMOVAL DAMAGE IS OUT OF LIMITS AT RT STAB STA 116.5, 9.5 INCHES AFT OF THE LE SPAR AND FWD EDGE OF THE SKIN NECESSITAT
- [SDR 06FDEA1332](https://openairdocs.org/sdr/06FDEA1332), Apr 7, 2006: SKIN. CHAFED. UPON REMOVAL OF FAIRING 3509 FOR ACCESS FOUND EXTERNAL FUSELAGE SKIN CHAFED AT FAIRING CONTACT LINE, BS 1110-1130 BETWEEN STR 25 AND 26 LEFT. REPAIRED PER SRM 5
- [SDR 06FDEA1321](https://openairdocs.org/sdr/06FDEA1321), Apr 6, 2006: STRINGER. CORRODED. FOUND STA 970 - 1030, CORROSION IN STR 30 AT RIVET TAILS. REPAIRED STR 30 PER SRM 53-10-3.
- [SDR 06FDEA1313](https://openairdocs.org/sdr/06FDEA1313), Apr 5, 2006: FLAP TRACK. CORRODED. NR 6 FLAP TRACK IS CORRODED AT SAFETY BOLT HOLE. REPLACED NR 6 FLAP TRACK IAW TASK CARD 27X5708-03.
- [SDR 06FDEA1307](https://openairdocs.org/sdr/06FDEA1307), Apr 4, 2006: ANGLE. CORRODED. STA 348 LBL 17 WL 149, CORROSION ON LOWER NOSE ANGLE (AFT OF NLG). REMOVED AND REPLACED CHORD AT STA 348 LBL 17 WL 149 IAW SRM 51-30-2.
- [SDR 06FDEA1279](https://openairdocs.org/sdr/06FDEA1279), Apr 3, 2006: FRAME. CORRODED. FOUND STA 1070 BETWEEN STR 28L AND 29L, CORROSION ON FRAME OUTBOARD FLANGE. REPAIRED FRAME BS 1070 STR 28L TO 29L IAW SRM 53-10-4.
- [SDR 06FDEA1300](https://openairdocs.org/sdr/06FDEA1300), Apr 3, 2006: FLAP TRACK. CORRODED. NR 8 FLAP TRACK FWD LUG IS CORRODED. REPLACED NR 8 FLAP TRACK IAW TASK CARD 27X5710-03.
- [SDR 06FDEA1299](https://openairdocs.org/sdr/06FDEA1299), Apr 3, 2006: SKIN. DAMAGED. FOUND STA 342, 4" BELOW STR 21L SKIN HAS SHARP PROTRUSION, FROM APPARENT INTERNAL IMPACT. REPAIRED DAMAGE AT STA 342 4" BELOW STR 21L IAW SRM 53-30-3 FIG 13A.
- [SDR 06FDEA1281](https://openairdocs.org/sdr/06FDEA1281), Apr 3, 2006: FLAP TRACK. CORRODED. NR 7 FLAP TRACK CORRODED AT FWD END. REPLACED NR 7 FLAP TRACK IAW TASK CARD 27X5709-03.
- [SDR 06FDEA1280](https://openairdocs.org/sdr/06FDEA1280), Apr 3, 2006: WEB. CORRODED. FOUND CORROSION ON FLOOR WEB, BS 1146 TO 1173, LBL 7 TO 14, WL 208. REPLACED FLOOR WEB, BS 1146-1173 WL 208 PER SRM 51-30-2, 51-10-2, 51-20-4.
- [SDR 06FDEA1246](https://openairdocs.org/sdr/06FDEA1246), Mar 27, 2006: SKIN. DENTED. N00969 DENT IN SKIN, BS 748, JUST BELOW STR2R. REPAIRED DENT PER FED EX E.A. 7-5330-96624
- [SDR 06FDEA1247](https://openairdocs.org/sdr/06FDEA1247), Mar 27, 2006: SKIN. DENTED. FOUND DENT IN SKIN, BS 1084, 1" ABOVE STR 2L TO 4" ABOVE STR 4L. ALL WORK ACCOMPLISHED IAW FED EX EA 7-5330-99514 FOUND TO BE A MAJOR REPAIR
- [SDR 05FDEA02746](https://openairdocs.org/sdr/05FDEA02746), Sep 4, 2005: SKIN. DAMAGED. EXTERNAL FUSELAGE SKIN HAS POPPED AND CRACKED FASTENERS ALONG STR 25 LEFT, BS 1166-1183. REPAIRED DAMAGED FUSELAGE SKIN BS 1166-1183 AT STR 25-STR 27 PER FED EX
- [SDR 05FDEA02706](https://openairdocs.org/sdr/05FDEA02706), Aug 29, 2005: SKIN. CRACKED. EXTERNAL FUSELAGE SKIN HAS POPPED AND CRACKED FASTENERS ALONG STR 25 LEFT, BS 1166 - 1183. REPAIRED DAMAGED FUSELAGE SKIN BS 1166-1183 AT STR 25-STR 27 PER FED 
- [SDR 05FDEA02705](https://openairdocs.org/sdr/05FDEA02705), Aug 29, 2005: SKIN. DENTED. WHILE WORKING ON AIRCRAFT, RAN INTO AIRCRAFT N192FE. DENTED AT BS 1203L TO 1223L IN BETWEEN STRINGERS 19 & 20, GOUGED AT BS 1203L TO 1223L IN BETWEEN STRINGERS 
- [SDR 05FDEA02425](https://openairdocs.org/sdr/05FDEA02425), Aug 11, 2005: PITOT LINE. OBSTRUCTED. AFTER TAKE F/O NOTED AIRSPEED INDICATOR STOPPED ACCELERATING BEYOND 140 KTS AS CAPTAIN LEVEL AT 3000, F/O ALTIMETER READ 2000 F/O AIRSPEED INOP FLAG CAME INTO V

All 53: https://openairdocs.org/deregistered/N192FE-2007-05-02/reports.md

## Other aircraft with N192FE

- [Registered now](https://openairdocs.org/aircraft/N192FE): Boeing 767-300F, S/N 63123, built 2021

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