# N190FE: 1966 Boeing 727-22, registration cancelled 2007-03-01

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 1, 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: 19083
- Year built: 1966
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: June 20, 1966
- Certificate issued: November 18, 1989
- Last registry action: March 15, 2005
- Mode S code: A168AD
- 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/N190FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=190FE
- Page: https://openairdocs.org/deregistered/N190FE-2007-03-01

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 (55, newest 50)

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

- [SDR 05FDEA02689](https://openairdocs.org/sdr/05FDEA02689), Aug 26, 2005: FITTING. MISDRILLED. LEFT AND RIGHT LOWER FORWARD TRUNNION TEE ATTACHED FITTINGS PART NUMBER 65-19257-6 /5/7/8, REQUIRES REWORK, REFERENCE:EO/7-5710-7-2314D PT-4. REWORKED LEFT AND 
- [SDR 04FDEA01900](https://openairdocs.org/sdr/04FDEA01900), Jul 1, 2004: INTERCOSTAL. CRACKED. FWD CARGO COMPARTMENT INTERCOSTAL IS CRACKED AT STRINGER 22R BS 572 THRU BS 580. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-1.
- [SDR 04FDEA01899](https://openairdocs.org/sdr/04FDEA01899), Jul 1, 2004: SKIN. BULGED. SKIN BULGE AT BS 1180 STRINGER 26L THRU STRINGER 23L. REPAIRED AREA IAW EA 7-5330-79539.
- [SDR 04FDEA01233](https://openairdocs.org/sdr/04FDEA01233), May 12, 2004: WARNING LIGHT. ILLUMINATED. NOSE GEAR DOWN LIGHT (GREEN) DID NOT ILLUMINATE WHEN GEAR LOWERED, CAME ON AFTER NOSE GEAR PIN INSTALLED. ADDITIONAL INFO FROM DEBRIEFING CREW. EXTREME PRECIPIT
- [SDR 04FDEA00002](https://openairdocs.org/sdr/04FDEA00002), Jan 1, 2004: CONNECTOR. CONTAMINATED. UNSAFE NOSE GEAR INDICATION - NO GREEN LIGHT. RAN PROCEDURE PER QRH. RECYCLED GEAR. VIEWED NOSE GEAR PORT WITH A GEAR DOWN & LOCKED INDICATION NORMAL. NOSE GEAR
- [SDR 99FDEA00465](https://openairdocs.org/sdr/99FDEA00465), Sep 27, 1999: BELLFRAME. DAMAGED. NR 685 - DENTS IN UPPER FLANGE RADIUS OF BELLFRAME AT BS 1050 ABOVE STR 26L IN AFT CARGO. CUT OUT DAMAGED AND INSTALL FILLER AND DOUBLER PER SRM 53-10-4 AND EA 
- [SDR 99FDEA00464](https://openairdocs.org/sdr/99FDEA00464), Sep 22, 1999: STRINGER. CORRODED. STR 30 IS CORRODED BETWEEN BS 1148 AND 1166 IN AFT CARGO. REMOVED AND REPLACED STR 30 PER SRM 53-10-3.
- [SDR 99FDEA00478](https://openairdocs.org/sdr/99FDEA00478), Sep 21, 1999: SPLICE. CORRODED. NR 118 - UPPER LOBE BS 344 LBL 45- LBL 60 CORROSION AROUND FLOORBOARD ATTACH HOLES UPPER LEG OF FLOORBEAM. INSTALLED UPPER CHORD SPLICE PER DRAWING SR 27-53-007
- [SDR 99FDEA00477](https://openairdocs.org/sdr/99FDEA00477), Sep 21, 1999: COVER. CORRODED. NR 782 - RT WING RT STUB TANK PLATE LAND NEEDS RESIDUE REMOVED FWD SPAR ACCESS. CORROSION REMOVED AND REPLACED AREA PER EA NR 75710-45413 DATED 9-29-99 SEEN NR 
- [SDR 99FDEA00466](https://openairdocs.org/sdr/99FDEA00466), Sep 21, 1999: CASTING. SCORED. NR 999 - LT WING BS 870 FWD AND AFT BOTTLE PIN CASTINGS ARE SCORED, AFT CASTING HAS 2 PREVIOUSLY BLENDED (DISHED OUT) AREAS (MARKED). REMOVED SCORING AND BLENDI
- [SDR 99FDEA00476](https://openairdocs.org/sdr/99FDEA00476), Sep 20, 1999: KEEL BEAM. CRACKED. NR 794 - KEEL BEAM LWR LT CHORD CRACKED IN RADIUS AT BS 954. STOP DRILLED CRACK AND INSTALL DOUBLER PER EA NR7-531045391 DATED 15 SEP 99.
- [SDR 99FDEA00462](https://openairdocs.org/sdr/99FDEA00462), Sep 10, 1999: BOTTLE PIN. CORRODED. RT FWD BOTTLE BOLT (SPAR TERMINAL PIN) HAS CORROSION. REMOVED AND REPLACED NEW BOTTLE BOLT PIN SEALED.
- [SDR 99FDEA00067](https://openairdocs.org/sdr/99FDEA00067), Feb 18, 1999: BULB. FAILED. LT MAIN LANDING GEAR LIGHT DID NOT COME ON WHEN GEAR LOWERED. COMPLIED WITH RED TABS. REPLACED BOTH BULBS IN LT MAIN GEAR IND PER CHAPTER 20 STANDARD PRACTICES.
- [SDR 98FDEA00769](https://openairdocs.org/sdr/98FDEA00769), Dec 29, 1998: VALVE. FAILED. LOST ALL SYS A UPON GEAR RETRACT, SHUT OFF VALVES FOR 33 MIN. REMOVED AND REPLACED LEFT MAIN GEAR LOCK PER MM 32-32-031-4, A SYS RETURN FILTER PER MM 29-11, NR 
- [SDR 98FDEA00497](https://openairdocs.org/sdr/98FDEA00497), Aug 11, 1998: COMPUTER. MALFUNCTIONED. STICK SHAKER AFTER TAKEOFF DURING FIRST FLAP RETRACTION 165 KIAS. OCCURRED INTERMITTENTLY AT ALL ALTITUDES AND AIRSPEEDS UNTIL LANDING, PITCH APPROX 8 DEG UP. *
- [SDR 98FDEA00226](https://openairdocs.org/sdr/98FDEA00226), Apr 1, 1998: SWITCH. FAILED. MAIN CARGO DOOR LIGHT CAME ON SHORTLY AFTER TAKEOFF. REPLACED LOCK ROD SWITCH AND ADJUSTED PER MAINTENANCE MANUAL 52-70-09, OPERATIONAL CHECKS GOOD.
- [SDR 97FDEA00562](https://openairdocs.org/sdr/97FDEA00562), Aug 18, 1997: FRAME. CRACKED. CRACK INDICATIONS NOTED (DAMAGED HOLE) BS 970, STR 27L AND 27R, AFT CARGO BAY LOWER LOBE. *S/D* REMOVED AREA OF DAMAGE .5 BY .5 BY .071 AT BS 970, STR 27L AND 2
- [SDR 97FDEA00536](https://openairdocs.org/sdr/97FDEA00536), Aug 14, 1997: FRAME. CRACKED. NR 0372 004 CRACK INDICATION NOTED AT TOOLING HOLE BS 1110, STR 26L AFT CARGO BAY LOWER LOBE. REMOVED .5 FT BY .3 FROM AREA AROUND TOOLING HOLE. REPAIRED IAW FE
- [SDR 97FDEA00535](https://openairdocs.org/sdr/97FDEA00535), Aug 14, 1997: FRAME. DAMAGED. NR 0370 006 WHILE WORKING EO 7-5310-7-2354E2 PT 2, FOUND DAMAGED HOLES ON FRAME BS 1090, LBL 17, WL 150. REMOVED DAMAGED AREA OF .425 BY .550 AND .500 BY .750 O
- [SDR 97FDEA00534](https://openairdocs.org/sdr/97FDEA00534), Aug 14, 1997: FITTING. CORRODED. NR 0271 005 - R/W I/B AILERON, I/B TAB FITTING CORRODED (AREA MARKED).
- [SDR 97FDEA00521](https://openairdocs.org/sdr/97FDEA00521), Aug 8, 1997: SHEAR TIE. CORRODED. CORROSION (C53-113-01, 2) BS 1168, AFT SHEAR TIE LBL 15 TO RBL 10 WL 164 BETWEEN STR 27R TO 27L. *S/D* REMOVED CORRODED SHEAR TIE AT BS 1168, LBL 15 TO RBL 10, 
- [SDR 97FDEA00520](https://openairdocs.org/sdr/97FDEA00520), Aug 8, 1997: MID FLAP. DELAMINATED. RIGHT WING I/B MID FLAP T/E WEDGE IS DELAMINATED AT 22 INCHES FROM I/B END. *S/D* REMOVED 9 BY 4 OF DAMAGED SKIN AND CORE, 22 INCHES FROM I/B END OF RIGHT WING 
- [SDR 97FDEA00504](https://openairdocs.org/sdr/97FDEA00504), Aug 6, 1997: SKIN. DELAMINATED. NR 0011 001 R/W I/B FOREFLAP HAS DELAMINATION DENT APPROXIMATELY 48 I/B O/B END. REPAIRED R/W I/B FOREFLAP DELAMINATION DENT APX 48 I/B OF O/B END IAW FED-EX SR
- [SDR 97FDEA00335](https://openairdocs.org/sdr/97FDEA00335), Jun 10, 1997: HYD FILTER. DIRTY. ON TAKEOFF, FIRST OFFICER FELT THAT HYDRAULIC PRESSURE TO ELEVATOR WAS LOST DURING GEAR RETRACTION. SAME THING OCCURED ON LANDING IN BFM WHEN SPEED BRAKES WERE 
- [SDR 96FDEA01307](https://openairdocs.org/sdr/96FDEA01307), Jul 31, 1996: SEQUENCE VALVE. LEAKING. LOSS OF SYS A-HYD ON GEAR RETRACTION. A-PUMPS RAN FOR 7 MINUTES WITHOUT FLUID. REMOVED AND REPLACED NR 1 AND NR 2 ENG HYD PUMPS PER MM 29-11-33. REMOVED AND REP
- [SDR 95FDEA00230](https://openairdocs.org/sdr/95FDEA00230), Mar 12, 1995: FRAME. DOUBLE HOLE. AT BS 970 STR 27R WL 157 THERE IS A DOUBLE HOLE IN THE FRAME. REPAIRED FRAME AT BS 970 STR 27R WL 157 PER FEDEX 51-40-3.
- [SDR 95FDEA00245](https://openairdocs.org/sdr/95FDEA00245), Mar 10, 1995: FITTING. CRACKED. UPPER RUDDER TAB ACTUATING ROD SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED CRACKED UPPER RUDDER TAB ACTUATING ROD SUPPORT FITTING.
- [SDR 95FDEA00244](https://openairdocs.org/sdr/95FDEA00244), Mar 10, 1995: FRAME. GOUGED. GOUGE ON FRAME AT BS 680 STR 14L. REMOVED AND REPLACED DAMAGED AREA PER FEDEX SRM 51-40-3.
- [SDR 95FDEA00243](https://openairdocs.org/sdr/95FDEA00243), Mar 10, 1995: STRINGER TIE. CRACKED. FRAME TO STRINGER TIE CRACKED AT BS 680 STR 11L. REMOVED, FABRICATED AND REPLACED STR TIE AT BS 680 STR 11L.
- [SDR 95FDEA00242](https://openairdocs.org/sdr/95FDEA00242), Mar 10, 1995: STRINGER. CORRODED. CORROSION (72C237-02) ON STRINGER AT BS 1150-1160 STR 7L. FOUND CORROSION TO BE OUT OF LIMITS. REPAIRED STR AT BS 1150-1160 IAW SRM 53-10-3 AND 51-40-3.
- [SDR 95FDEA00241](https://openairdocs.org/sdr/95FDEA00241), Mar 10, 1995: STRINGER. CRACKED. STR 25R IS CRACKED AT BS 420. REPAIRED STR 25R AT BS 420 IAW SRM 53-10-3 FIG 1 DETAIL II.
- [SDR 95FDEA00240](https://openairdocs.org/sdr/95FDEA00240), Mar 10, 1995: FLOOR BEAM. CORRODED. CORROSION (72C235-2) ON 344 FLOOR BEAM RBL 15 WL 208 UNDER NUTPLATE HOLE. CORROSION PERMIATED THROUGH BEAM AND HAT CHANNEL OUT OF LIMITS PER FEDEX SRM 53-10-1 R
- [SDR 95FDEA00239](https://openairdocs.org/sdr/95FDEA00239), Mar 10, 1995: SEAT TRACK. CORRODED. CORROSION (72C235-02) ON SEAT TRACK BS 740 LBL 25. CORROSION FOUND TO BE OUT OT LIMITS, REMOVED AND REPLACED SEAT TRACK FROM BS 710-740 IAW SRM 53-10-5.
- [SDR 95FDEA00238](https://openairdocs.org/sdr/95FDEA00238), Mar 10, 1995: SEAT TRACK. CORROSION. CORROSION ON SEAT TRACK BS 480 RBL 25 WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 480-510 RBL 25 WL 208.
- [SDR 95FDEA00237](https://openairdocs.org/sdr/95FDEA00237), Mar 10, 1995: SEAT TRACK. CORROSION. CORROSION ON SEAT TRACK BS 470-484 LBL 45 WL 208. REPLACED SEAT TRACK FROM BS 480-510 LBL 45 WL 208 AND CLEANED CORROSION ON TRACK FLANGE AT BS 470 PER FEDEX SR
- [SDR 95FDEA00236](https://openairdocs.org/sdr/95FDEA00236), Mar 10, 1995: SEAT TRACK. CORRODED. CORROSION (72C235-02) ON SEAT TRACK BS 344-350 RBL 25. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-10-1.
- [SDR 95FDEA00235](https://openairdocs.org/sdr/95FDEA00235), Mar 10, 1995: SEAT TRACK. CORROSION. CORROSION ON SEAT TRACK BS 870 RBL 25 WL 208 OUT OF LIMITS PER SRM 51-10-01 1 INCH BY 1 INCH BY .035 ORIGINAL THICKNESS .090. REMOVED AND REPLACED SEAT TRACK BS
- [SDR 95FDEA00234](https://openairdocs.org/sdr/95FDEA00234), Mar 10, 1995: BULKHEAD. DENTED. DENT IN PRESSURE BULKHEAD BS 950 RBL 23 WL 153. REPAIRED DENT IN BS 950 CENTER BULKHEAD AT RBL 23 WL 153 PER FEDEX SRM 53-10-9 FIG 4.
- [SDR 95FDEA00233](https://openairdocs.org/sdr/95FDEA00233), Mar 10, 1995: CLIP. DAMAGED. CRACK AND OR HOLE DAMAGE IN LEFT BS 870 TERMINAL FITTING ROW 1 HOLE NR 1. DETERMINED BY HFEC THAT DAMAGE TO FRAME TO STRINGER CLIP TO BE MECHANICAL TOOLING DAMA
- [SDR 95FDEA00232](https://openairdocs.org/sdr/95FDEA00232), Mar 10, 1995: SEAT TRACK. WORN. F/E'S AFT SEAT TRACK IS WORN. REMOVED AND REPLACED F/E'S AFT SEAT TRACK.
- [SDR 95FDEA00231](https://openairdocs.org/sdr/95FDEA00231), Mar 10, 1995: FRAME. DOUBLE HOLE. AT BS 990 STR 27R WL 148 THERE IS A DOUBLE HOLE IN THE FRAME. REPAIRED FRAME AT BS 990 STR 27R WL 157 PER FEDEX SRM 51-40-3.
- [SDR 95FDEA00229](https://openairdocs.org/sdr/95FDEA00229), Mar 10, 1995: STRINGER. GOUGED. BS 500 WL 190 STR 19R STR IS GOUGED ON LOWER SIDE CHANNEL. REMOVED GOUGED STR 19 BS 500 WL 190 AND INSTALLED NEW STR PER FEDEX SRM 53-10-3.
- [SDR 95FDEA00226](https://openairdocs.org/sdr/95FDEA00226), Mar 10, 1995: SKIN. DAMAGED. 9503-11 LEFT HORIZONTAL STABILIZER INTERSPAR SKIN (LWR SURFACE) IS DAMAGED BETWEEN STAB STA 151.81 AND STAB 169.81. REPAIRED DAMAGED AREA ON LEFT HORIZONTAIL ST
- [SDR 95FDEA00225](https://openairdocs.org/sdr/95FDEA00225), Mar 10, 1995: FITTING. CRACKED. BS 870 TERMINAL FITTING ROW 2 HOLES NR 3 AND NR 4 HAVE CRACK INDICATION NOTED RT SIDE. REPAIRED CRACK BETWEEN HOLES 3 AND 4, ROW 2 IN BS 870 TERMINAL FITTING RT
- [SDR 95FDEA00224](https://openairdocs.org/sdr/95FDEA00224), Mar 10, 1995: SKIN. CORRODED. GREATER THAN 10 PERCENT MATERIAL LOSS INDICATION NOTED AT BS 441 CIRCUMFERENTIAL SPLICE FWD SKIN PANEL BETWEEN STR 1920R. REPAIRED AFT UPR SKIN STA 440 STR 19 I
- [SDR 95FDEA00223](https://openairdocs.org/sdr/95FDEA00223), Mar 10, 1995: SKIN. GOUGED. GOUGES IN SKIN AT F/O'S WINDSHIELD WIPER MOUNT AND JUST BELOW O/B SIDE OF NR 1 WINDOW. BLENDED GOUGE AT SKIN BELOW F/O'S WINDSHIELD WIPER. INSTALLED DOUBLER PER
- [SDR 95FDEA00222](https://openairdocs.org/sdr/95FDEA00222), Mar 10, 1995: STIFFENER. CORRODED. CORROSION IN E/E BAY ON FRAME STIFFENER AT BS 300 LBL 38 WL 169. PART OUT OF LIMIT REMOVED .070 BY .1250 BY .5 INCH CORROSION, REMOVED AND REPLACED STIFFENER ST
- [SDR 95FDEA00221](https://openairdocs.org/sdr/95FDEA00221), Mar 10, 1995: STRINGER. DAMAGED. MECHANICAL DAMAGE ON STR 8L BS 802. REMOVED DAMAGED .5 INCH SECTION OF STR 8L FROM BS 802, FABRICATED AND INSTALLED PART PER FEDEX SRM 53-10-3.
- [SDR 95FDEA00220](https://openairdocs.org/sdr/95FDEA00220), Mar 10, 1995: STRINGER. CRACKED. STR 21R IS CRACKED AT BS 400. REPAIRED STR 21R AT BS 400 IAW FEDEX SRM 53-10-01.
- [SDR 95FDEA00219](https://openairdocs.org/sdr/95FDEA00219), Mar 10, 1995: FLOORBEAM. CORRODED. CORROSION (71C709-02) IN NUTPLATE HOLES ON LOWER FLANGE OF FLOORBEAM AT BS 1110 RBL 3-47 WL 200. REPAIRED BS 1110 FLOORBEAM RBL 3-47 WL 200 AS PER FEDEX EA 7-53

All 55: https://openairdocs.org/deregistered/N190FE-2007-03-01/reports.md

## Other aircraft with N190FE

- [Registered now](https://openairdocs.org/aircraft/N190FE): Boeing 767-300F, S/N 63121, built 2020

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