- Registered owner
- Federal Express Corp
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 22909
- Year built
- 1986
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Certificate issued
- February 8, 2011
- Expires
- February 28, 2030
- Mode S code
- ADD324
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 316
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1983 | 1 |
|---|---|
| 1985 | 7 |
| 1986 | 8 |
| 1987 | 7 |
| 1988 | 7 |
| 1989 | 11 |
| 1990 | 12 |
| 1991 | 14 |
| 1992 | 15 |
| 1993 | 8 |
| 1994 | 9 |
| 1995 | 6 |
| 1996 | 6 |
| 1997 | 7 |
| 1998 | 9 |
| 1999 | 8 |
| 2000 | 7 |
| 2001 | 13 |
| 2002 | 8 |
| 2003 | 11 |
| 2004 | 10 |
| 2005 | 20 |
| 2006 | 12 |
| 2007 | 8 |
| 2008 | 15 |
| 2009 | 5 |
| 2010 | 7 |
| 2011 | 6 |
| 2012 | 8 |
| 2013 | 13 |
| 2014 | 6 |
| 2015 | 3 |
| 2016 | 8 |
| 2017 | 7 |
| 2018 | 11 |
| 2019 | 4 |
| 2020 | 8 |
| 2021 | 4 |
| 2022 | 8 |
| 2023 | 3 |
| 2024 | 6 |
| 2025 | 7 |
| 2026 | 7 |
See all 360 ADs
Information bulletins that may apply · 13
Advisory, not mandatory.
Airframe · Boeing 757-232
SAIB 2026-09HYDRAULIC POWER, Hydraulic Power Transfer Unit SystemSAIB 2025-02DOORS, Main Deck Cargo DoorSAIB 2025-01HYDRAULIC POWER SYSTEM, Fatigue Failure of Hydraulic Flexible HosesSAIB NM-20-07Navigation - Glideslope SystemSAIB NE-19-03Escape Slide Maintenance Tasks and Intervals - JASC 2565SAIB NM-18-33Engine Fuel and ControlSAIB NM-17-17Oxygen SystemSAIB NM-17-10Maintenance PracticesSAIB NM-15-03Flight ControlsSAIB NM-10-24Hydraulic Motors: Hydraulic Motor Generator (HMG) Inadvertent Lock-outSAIB NM-09-03Engine Fuel and Control - Implementing Fuel Tank System Airworthiness LimitationsSAIB NM-07-14M10444 APU/Cargo Fire Control Panel (APU/CFCP)SAIB NM-06-57Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.NTSB investigations
No NTSB investigations matched to N990FDMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Boeing 757-232 aircraft
FAA incident reports
No FAA accident or incident reports matched to N990FDMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Boeing 757-232 aircraft
Service difficulty reports · 143
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FDEA202512122239Torque Tube · damagedWHEN CONFIGURING AFTER START SETTING FLAPS TO 5 RECEIVED LE SLAT DISAG EICAS. UPON INSPECTION FOUND THE CONTROL CABLE INPUT FOR THE LE SLAT PDU BROKEN AND FRAYED. THE CABLE IS IDENTIFIED AS LESA IAW FIM 27-81, FAULT TREE 803, FIGURE 104, & IPC 27-51-25-0SDR FDEA202511112160Skin · delaminatedLH HORIZONTA STABILIZER UPPER SKIN HAS POSSIBLY DELAMINATION STAB STA 104.248 AREA APPLIED PERMANENT REPAIR AT LH HORIZONTAL STABILIZER UPPER SKIN I.A.W B757 SRM 55-10- 01-1A, TABLE I, NOTE 'A' AND "I", FIG 101, SHEET 2, I.A.W B757 SRM 51-70-10-2RSDR FDEA202511112159Skin · dentedRH HORIZONTAL STABILIZER LOWER SURFACE HAS TWO DENTS STAB STA 176.249 AREA TWO DENTS FOUND OUT OF LIMITS AT RH HORIZONTAL STABILIZER LOWER SURFACE STAB STA 176.248. AND APPLIED PERMANENT REPAIR I.A.W B757 SRM 55-10-01-1A, TABLE I, NOTE 'I' FIG 101, SHEET 3
See all 143 reportsSTCs that may be installed · 721
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.