# N918FD: 1989 Boeing 757-23A

- Status: Valid registration
- Airframe: [Boeing 757-23A](https://openairdocs.org/model/boeing-757-23a) (registry code 1384967, 178 seats)
- Engine: [Rolls-Royce RB211-535E4 series](https://openairdocs.org/engine/rolls-royce-rb211-535e4-series) (registry code 54223)
- Data sheets: [TCDS A2NM](https://openairdocs.org/tcds/A2NM) (The Boeing Company), [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs)
- Serial number: 24290
- Year built: 1989
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 27, 2009
- Certificate issued: April 30, 2008
- Expires: April 30, 2030
- Mode S code: ACB4E4
- Registered owner: [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 is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=918FD
- Page: https://openairdocs.org/aircraft/N918FD

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Rolls-Royce RB211-535E4 model are included.

## ADs that may apply (OpenAirDocs): 20 in force

### Matched by airframe (Boeing 757-23A)

None in force.

### Matched by engine (Rolls-Royce RB211-535E4 series)

- [AD 2024-10-06](https://openairdocs.org/ad/2024-10-06): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jun 27, 2024
- [AD 2020-08-03](https://openairdocs.org/ad/2020-08-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective May 18, 2020
- [AD 2017-24-08](https://openairdocs.org/ad/2017-24-08): Fuel control/Turbine engines · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jan 16, 2018
- [AD 2016-03-04](https://openairdocs.org/ad/2016-03-04): Life-limited rotating parts · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Mar 15, 2016
- [AD 2013-23-17](https://openairdocs.org/ad/2013-23-17): High-pressure (HP) and intermediate-pressure (IP) turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-C-37 and 3 more. Effective Dec 11, 2013
- [AD 2013-16-23](https://openairdocs.org/ad/2013-16-23): Cracked and distorted FCL metering panel · Rolls-Royce RB211-524B-02, RB211-524B2-19, RB211-524B3-02 and 13 more. Effective Oct 8, 2013
- [AD 2012-25-09](https://openairdocs.org/ad/2012-25-09): Intermediate-pressure (IP) turbine discs · Rolls-Royce RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19 and 10 more. Effective Feb 6, 2013
- [AD 2012-02-11](https://openairdocs.org/ad/2012-02-11): LP turbine stage 1, 2, and 3 discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Mar 6, 2012
- [AD 2009-20-14](https://openairdocs.org/ad/2009-20-14): Eddy current inspection (ECI) · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Nov 17, 2009
- [AD 2008-20-04](https://openairdocs.org/ad/2008-20-04): HP turbine discs · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 26 more. Effective Nov 3, 2008
- [AD 2006-11-05 R2](https://openairdocs.org/ad/2006-11-05-R2): High pressure compressor (HPC) · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 21, 2008
- [AD 2007-14-07](https://openairdocs.org/ad/2007-14-07): Fluorescent penetrant inspections (FPI) · Rolls-Royce RB211-524B-02, RB211-524B-B-02, RB211-524B2-19 and 21 more. Effective Aug 16, 2007
- [AD 2006-17-12](https://openairdocs.org/ad/2006-17-12): High pressure (HP) turbine discs · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 3 more. Effective Sep 27, 2006
- [AD 2004-19-04](https://openairdocs.org/ad/2004-19-04): Critical Life-Limited Rotating Engine Parts · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Nov 1, 2004
- [AD 2004-01-21](https://openairdocs.org/ad/2004-01-21): Frount engine mount housing · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 27, 2004
- [AD 2003-10-03 R1](https://openairdocs.org/ad/2003-10-03-R1): High pressure (HP) turbine discs · Rolls-Royce RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jun 20, 2003
- [AD 2001-19-05](https://openairdocs.org/ad/2001-19-05): High Speed Gearbox Drive · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Oct 11, 2001
- [AD 2000-09-14](https://openairdocs.org/ad/2000-09-14): Radial Drive Steady Bearings · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Jul 11, 2000
- [AD 97-02-12](https://openairdocs.org/ad/97-02-12): Fuel Flow Governor (FFG) · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Apr 4, 1997
- [AD 87-25-04](https://openairdocs.org/ad/87-25-04): Fuel Quantity Indication System · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Dec 8, 1987

### Historical (superseded or no longer in force)

- [AD 2015-17-21](https://openairdocs.org/ad/2015-17-21) (historical): High-pressure turbine (HPT) disks · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Dec 2, 2015
- [AD 2014-24-08](https://openairdocs.org/ad/2014-24-08) (historical): Fuel leaks · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jan 6, 2015
- [AD 2013-19-18](https://openairdocs.org/ad/2013-19-18) (historical): LPT stage 2 disc failure · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Nov 7, 2013
- [AD 2013-19-17](https://openairdocs.org/ad/2013-19-17) (historical): Failure of rotating life limited parts · Rolls-Royce RB211-535E4-B-37. Effective Nov 7, 2013
- [AD 2011-11-08](https://openairdocs.org/ad/2011-11-08) (historical): LP Turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Jun 30, 2011
- [AD 2008-22-24](https://openairdocs.org/ad/2008-22-24) (historical): Low pressure compressor (LPC) fan blade · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Dec 9, 2008
- [AD 2006-11-05 R1](https://openairdocs.org/ad/2006-11-05-R1) (historical): Disc assemblies · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective May 1, 2007
- [AD 2006-11-05](https://openairdocs.org/ad/2006-11-05) (historical): High pressure compressor (HPC) stage 3 disc assemblies · Rolls-Royce RB211-22B-02, RB211-524B-02, RB211-524B-B-02 and 24 more. Effective Jun 27, 2006
- [AD 2005-02-05](https://openairdocs.org/ad/2005-02-05) (historical): Low Pressure Compressor (LPC) Fan Blade Roots · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Feb 11, 2005
- [AD 2004-26-03](https://openairdocs.org/ad/2004-26-03) (historical): High pressure (HP) turbine discs · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 3 more. Effective Jan 13, 2005
- [AD 2004-01-20](https://openairdocs.org/ad/2004-01-20) (historical): High pressure compressor (HPC) · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 24, 2004
- [AD 2003-17-15](https://openairdocs.org/ad/2003-17-15) (historical): Low pressure (LP) turbine stage 2 discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Oct 2, 2003
- [AD 2003-12-15](https://openairdocs.org/ad/2003-12-15) (historical): LPC fan blade roots · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jul 30, 2003
- [AD 2003-10-03](https://openairdocs.org/ad/2003-10-03) (historical): High Pressure (HP) turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jun 20, 2003
- [AD 2002-23-08](https://openairdocs.org/ad/2002-23-08) (historical): Low Pressure (LP) Turbine Stage 2 Discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Dec 30, 2002
- [AD 2001-23-02](https://openairdocs.org/ad/2001-23-02) (historical): High Pressure Turbine Disks · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 2 more. Effective Dec 24, 2001
- [AD 98-07-07](https://openairdocs.org/ad/98-07-07) (historical): Fuel System Tube Assembly · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Apr 29, 1998
- [AD 86-07-01](https://openairdocs.org/ad/86-07-01) (historical): Outer Combustion Case Inspection · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective May 16, 1986

## Information bulletins (advisory) (1 in force)

- [SAIB 2026-11](https://openairdocs.org/saib/2026-11): Theft of Turbofan Engine Parts before Mutilation. Issued Jun 8, 2026

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA23WA363](https://openairdocs.org/ntsb/DCA23WA363), Jul 16, 2023: Boeing 757-23A (N918FD), Tel Aviv, Israel, substantial damage

## FAA accident and incident reports

None matched to N918FD.

## Service difficulty reports (190, newest 50)

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

- [SDR FDEA202508291579](https://openairdocs.org/sdr/FDEA202508291579), Aug 29, 2025: FRAME. CRACKED. CRACK INDICATIONS FOUND IN STA 1640 AT S-14R BOTTOM I/B OPEN HOLE APROX AT 8 O' CLOCK LOOKING AFT AND TWO CRACK INDICATIONS IN UPPER O/B OPEN HOLE APROX AT 6 & 
- [SDR FDEA202508281562](https://openairdocs.org/sdr/FDEA202508281562), Aug 28, 2025: SKIN. DELAMINATED. LH WING LEADING EDGE SKIN AREA CRACKED BETWEEN WS 150.5 AND 204.50 (#5 LEADING EDGE SLAT AREA ) PERFORMED TAP TEST ON LH WING L/E DELAMINATION FOUND DIM L= 18.5
- [SDR FDEA202501270142](https://openairdocs.org/sdr/FDEA202501270142), Jan 27, 2025: LENS. DETACHED. L EXTERNAL EMERGENCY LIGHT COVER DETACHED. IAW AMM 33-51-06-2-1 EA TF-3350-T0313211 L EMERG LIGHT LENS REATTACHED IAW SPM AND AMM 33-51-06-2-1 TESTED OK.
- [SDR FDEA202501270141](https://openairdocs.org/sdr/FDEA202501270141), Jan 27, 2025: LENS. DETACHED. EXTERNAL EMERGENCY LIGHT COVER DETACHED. IAW AMM 33-51-06-2-1 EA TF-3350-T0313211 L EMERG LIGHT LENS REATTACHED IAW SPM AND AMM 33-51-06-2-1 TESTED OK.
- [SDR FDEA202501270140](https://openairdocs.org/sdr/FDEA202501270140), Jan 27, 2025: LENS. DETACHED. EXTERNAL LH EMER. LIGHT LENSE DETACHED. L EMERG LIGHT LENS REATTACHED IAW SPM AND AMM 33-51-06-2-1 TESTED OK ADD CLEARED
- [SDR FDEA202412021762](https://openairdocs.org/sdr/FDEA202412021762), Dec 2, 2024: GUARD. DAMAGED. EMERGENCY EXIT LIGHTS ARE UNARMED WHEN EMERGENCY EXIT LIGHT SWITCH IS CLOSED. FOUND SWITCH GUARD SPRING LOAD OUTSIDE OF THE SWITCH, REPOSITIONED THE SPRING, PER
- [SDR FDEA202408081109](https://openairdocs.org/sdr/FDEA202408081109), Aug 8, 2024: SKIN. CORRODED. FOUND EXFOLIATION CORROSION ON EXTERIOR SKIN SURFACE ADJACENT TO L/H APY DOOR FWD HINGE POINT AREA COMPLIED WITH MAJOR REPAIR CLASSIFICATION. E.A. #-F-5330-T038
- [SDR FDEA202407251057](https://openairdocs.org/sdr/FDEA202407251057), Jul 25, 2024: RELAY. FAILED. NOSE L/G COMPONENTS INSPECTION REQUIRED TO CONFIRM NO DAMAGES. NOSE GEAR COMPONENTS VISUAL INSPECTION PERFORMED. NO OBVIOUS DAMAGES OBSERVED. ALSO NOSE GEAR STE
- [SDR FDEA202407251056](https://openairdocs.org/sdr/FDEA202407251056), Jul 25, 2024: RELAY. FAILED. RUNWAY ENGINE START. INSTEAD OF STABILIZING AT IDLE, THE RPM AND THRUST INCREASED WITH NO THROTTLE INPUT AND THROTTLES AT IDLE AND CONTINUED TO INCREASE RAPIDLY
- [SDR FDEA202404300520](https://openairdocs.org/sdr/FDEA202404300520), Apr 30, 2024: FAN. FAILED. OIL BURNING SMOKE BELOW 5000FEET WITH LOW POWER SETTING. R & R L/H RECIRCULATION FILTER AND FAN, REVERSED MEL 21-25-01-02 & MEL 21-58-07, RECONNECTED WIRE ON PL
- [SDR FDEA202404230272](https://openairdocs.org/sdr/FDEA202404230272), Apr 23, 2024: GIRT BAR. OUT OF ALIGNMENT. LIGHT ON LEFT CREW ENTRY DOOR INOP. FACT 23APR24 08:51 AMS AMM: 25-66-10-2 AMM: 25-66-11-2 RELAMP NO HELP. FOUND SLIDE VERY HARD TO ARM AND GIRTBAR FITTINGS NOT
- [SDR FDEA202310231791](https://openairdocs.org/sdr/FDEA202310231791), Oct 23, 2023: WEB. MISALIGNED. REMOVE FRAME REPAIR AT STA 1360 L/H AFT CARGO FRAME PER EA # F-5310-TO376446 REPAIR PREFORMED PER EA # F-5310-T0376446 P 1. EO TITLE: FUSELAGE - MAIN - FRAME - 
- [SDR FDEA202310121757](https://openairdocs.org/sdr/FDEA202310121757), Oct 12, 2023: FLOORBOARD. DAMAGED. MAIN CABIN FLOORBOARD PANEL 231 MAF IN ZONE 230 DAMAGED. FABRICATED MAIN CABIN FLOORBOARD 231 MAF ON VT MAE TRAVELER # T23/1709112 IAW DWG SRZ-25-005 REV R MAJO
- [SDR FDEA202310121756](https://openairdocs.org/sdr/FDEA202310121756), Oct 12, 2023: FLOORBOARD. DAMAGED. MAIN CABIN FLOORBOARD 231 MEF IN ZONE 230 DAMAGED. FABRICATED MAIN CABIN FLOORBOARD PANEL 231MEF ON VT MAE TRAVELER # T23/1709132 IAW DWG SRZ-25-005 REV R MAJOR
- [SDR FDEA202310121751](https://openairdocs.org/sdr/FDEA202310121751), Oct 12, 2023: FLOOR PANEL. DAMAGED. ZONE 220 COURIER FLOORBOARD 221 MBF DAMAGED. FABRICATED ZONE 220 FLOORBOARD 221 MBF ON VT MAE TRAVELER # T23/1707219 IAW DWG SRZ-25-005 REV R MAJOR REPAIR.
- [SDR FDEA202310121750](https://openairdocs.org/sdr/FDEA202310121750), Oct 12, 2023: FLOOR PANEL. DAMAGED. MAIN CABIN FLOORBOARD PANEL 231MFF IN ZONE 230 DAMAGED FABRICATED MAIN CABIN FLOORBOARD PANEL 231MFF ON VT MAE TRAVELER # T23/1709136 IAW DWG SRZ-25-005 REV R M
- [SDR FDEA202310121749](https://openairdocs.org/sdr/FDEA202310121749), Oct 12, 2023: FLOOR PANEL. DAMAGED. MAIN CABIN FLOORBOARD PANEL 231MBF IN ZONE 230 DAMAGED. FABRICATED MAIN CABIN FLOORBOARD PANEL 231MBF ON VT MAE TRAVELER # T23/1709121 IAW DWG SRZ-25-005 REV R 
- [SDR FDEA202310111746](https://openairdocs.org/sdr/FDEA202310111746), Oct 11, 2023: SEAT TRACK. CORRODED. MAIN DECK CARGO FLOOR SEAT TRACK FLANGE HAS SEVERAL CORROSION LOC BET STA 1180 AND 122 RBL 45. SEAT TRACK WAS REMOVED, FABRICATED AND INSTALLED ON MAIN DECK CAR
- [SDR FDEA202310111745](https://openairdocs.org/sdr/FDEA202310111745), Oct 11, 2023: SEAT TRACK. CORRODED. MDC SAET TRACK BETWEEN BS 1420 AND 1540 AT LBL 45.50 HAS LIGHT SURFACE CORROSION SEAT TRACK WAS REPAIRED BETWEEN STA 1480 TO 1540 AND LBL 45.50 IAW B757 SRM 53-
- [SDR FDEA202310111744](https://openairdocs.org/sdr/FDEA202310111744), Oct 11, 2023: FLOORBOARD. DAMAGED. MAIN CABIN FLOORBOARD PANEL 252 MTF DAMAGED FABRICATED MAIN CABIN FLOORBOARD PANEL 252 MTF ON VT MAE TRAVELER # T23/1709138 IAW DWG SRZ-25-005 REV R MAJOR REPAI
- [SDR FDEA202307171230](https://openairdocs.org/sdr/FDEA202307171230), Jul 17, 2023: RUDDER. DAMAGED. THE WINGTIP OF A MANEUVERING AIRCRAFT STRUCK THE RIGHT HAND SIDE LOWER SECTION OF THE RUDDER STRUCTURE, PENETRATING THE RUDDER SKIN SURFACE AND HONEYCOMB CORE. 
- [SDR FDEA202212243010](https://openairdocs.org/sdr/FDEA202212243010), Dec 24, 2022: SEAL. DAMAGED. AT CRUISE FL370, NOTICED LOUD NOISE COMING FROM FORWARD AIRCRAFT LEFT, SUSPECTED LEAKY DOOR SEAL. CABIN ALTITUDE DISPLAYED 9100 WITH A SLIGHT CLIMB AND OUTFLOW 
- [SDR FDEA202212082890](https://openairdocs.org/sdr/FDEA202212082890), Dec 8, 2022: BATTERY. FAILED. FOUND APU BATTERY OVERHEATED AND FUMES ON IT DURING APU BITE TEST ON ECU. BATTERY INMEDIATELY DISCONNECTED AND FIRE BRIGADE ADVISED. INSTALLED NEW APU BATTERY I
- [SDR FDEA202211152784](https://openairdocs.org/sdr/FDEA202211152784), Nov 15, 2022: SCREW. LOOSE. ON APPROACH TO 26L WITH THE LT AUTOPILOT ENGAGED, RECEIVED MULTIPLE FAILURES, INCLUDING EICAS MESSAGES & INDICATIONS: AUTOPILOT FAIL, BLEED ISLN VAL, LT YAW DAM
- [SDR FDEA202209292386](https://openairdocs.org/sdr/FDEA202209292386), Sep 29, 2022: LIGHT. LOOSE. DURING PREFLIGHT UNARMED LIGHT CAME OUT OF EMERGENCY LIGHTS MODULE ON OVERHEAD PANEL FOUND KORRY LIGHT ASSY BROKEN. R&R KORRY ASSY IAW AMM 33-13-00-2 AND SWPM 2
- [SDR FDEA202203030408](https://openairdocs.org/sdr/FDEA202203030408), Mar 3, 2022: NONE. FAILED. EMERGENCY EXIT LIGHT ARMING SWITCH WIRE BROKEN. DOES NOT ARM LIGHTS WHEN TOGGLE SWITCH CLOSED. FOUND THE SPRING OF THE SAFE GUARD SWITCH BROKEN. OIL 03MAR22 14:
- [SDR FDEA202202260378](https://openairdocs.org/sdr/FDEA202202260378), Feb 26, 2022: NONE. NONE. MDIS 918 33-50 3520 26FEB22 LGG FACT U DURING SERVICE CHECK FOUND L1 SLIDE LIGHT INOP. RELAMPED L1 SLIDE LIGHT IAW AMM 33-51-06-2-1, LIGHT OPERATIONAL.
- [SDR FDEA202111222974](https://openairdocs.org/sdr/FDEA202111222974), Nov 22, 2021: SKIN. DAMAGED. FUSELAGE BELLY SKIN AT BS 1460 TO 1480 BETWEEN STRINGER 29L AND 29R THERE IS A DOUBLER AND A TRIPLER INSTALLED UNDER THE VHF ANTENAN. REPAIR REQUIRES EVALUATION
- [SDR FDEA202111222972](https://openairdocs.org/sdr/FDEA202111222972), Nov 22, 2021: NONE. DAMAGED. FOUND 20 4EA HOLES DRILLED AND UNUSED ON AFT PLATE BETWEEN STA 1681-1700 ON BL 0 THE DAMAGED SECTION OF THE AFT DECK PLATE WAS TRIMMED OUT PER SRM 51-10-02, THE
- [SDR FDEA202111222970](https://openairdocs.org/sdr/FDEA202111222970), Nov 22, 2021: NONE. CORRODED. FOUND CORROSION ON UPPER CHORD OF FLOOR BEAM AT STA 1681 LBL 40 TO RBL 40 UNDER SHEAR WEB THE FLOOR BEAM UPPER CHORD FWD FLANGE WAS REPAIRED WITH 2 ANGLES, 1 FI
- [SDR FDEA202111182976](https://openairdocs.org/sdr/FDEA202111182976), Nov 18, 2021: SKIN. DAMAGED. EMPENNAGE , TAIL CONE UPPER SURFACE LEFT HAND SIDE , CIRCULAR DUBLER REPAIR ON EXTERNAL SKIN FORWARD OF THE APU EXHAUST OUTLET AT BS 1980, REPAIR REQUIRES EVALU
- [SDR FDEA202111182975](https://openairdocs.org/sdr/FDEA202111182975), Nov 18, 2021: SKIN. DAMAGED. APU COMPARTMENT R/H SIDE , CIRCULAR DOUBLER REPAIR ON INNER SKIN AT BS 1925 AND INCHES FROM THE PANEL LOWER EDGE REPAIR REQUIRES EVALUATION TO DETERMINE IF IT W
- [SDR FDEA202111182973](https://openairdocs.org/sdr/FDEA202111182973), Nov 18, 2021: NONE. UNKNOWN. FORWARD LOWER CARGO FLOOR,RIGHT HAND SIDE Z CHANNEL HAS A REPAIR SPLICE AT BS 710. REPAIR REQUIRES EVALUATION TO DETERMINE IF IT WAS ACCOMPLISHED IN ACCORDANCE 
- [SDR FDEA202110252971](https://openairdocs.org/sdr/FDEA202110252971), Oct 25, 2021: FLOORBEAM. CORRODED. FOUND CORROSION ON STA 1640 ON UPPER CHORD OF FLOOR BEAM BETWEEN LBL 45 TO RBL 45 THE CORREDED UPPER CHORD WAS REMOVED AND DISCARDED A NEW REPAIR UPPER CHORD P/
- [SDR FDEA202110242977](https://openairdocs.org/sdr/FDEA202110242977), Oct 24, 2021: WEDGE. DAMAGED. DURING C-DUCT REMOVEL R/H INBD L/H SLAT DAMAGED PERFORMED REPAIR PER EA F-5750-T0365723A REP DIM. 5.2" X 7" REP. LOC. ISS 137 AT T/E. PERFORMED HOT BOND REPAIR 
- [SDR FDEA2020082091946](https://openairdocs.org/sdr/FDEA2020082091946), Aug 19, 2020: MECHANISM. LACK OF LUBE. DURING WALKAROUND FOUND DOOR L1 NOT ABLE TO OPERATE FROM THE OUTSIDE HANDLE. ABLE TO OPEN THE L1 DOOR BUT EXTERIOR HANDLE BUTTERFLY STICKY AND HARD TO MOVE. TRI
- [SDR FDEA2020051530931](https://openairdocs.org/sdr/FDEA2020051530931), May 13, 2020: LIGHT. INOPERATIVE. L/H FOWARD ENTRY DOOR "SLIDE" LIGHT FOUND TO BE INOP AS DOOR WAS CLOSED RE-LAMPED L/H FWD DOOR ARM/SLIDE IAW STANDARD PRACTICES ELECTRICAL. TEST OK
- [SDR FDEA2020041760752](https://openairdocs.org/sdr/FDEA2020041760752), Apr 16, 2020: COLLAR. WORN. L1 DOOR INOP GUST LOCK INOP. SPARES KIT CONTAINS 10-N6008-1 TWO PIECE COLLAR ASSEMBLY TOGETHER WITH 10-N6009-1 CATCH ASSEMBLY. 10-N0244-7 IS INTERCHANGEABLE WIT
- [SDR FDEA202002210363](https://openairdocs.org/sdr/FDEA202002210363), Feb 21, 2020: GUST LOCK. CRACKED. LEFT CREW ENTRY GUST LOCK HAS SMALL PIECE CRACKED OFF. REMOVED AND REPLACED COLLAR AND CATCH ASSY AS PER AMM 52-11-08-8. OPS CHECK OK. MEL CLOSED PLACARDS REMOV
- [SDR FDEA2019100322398](https://openairdocs.org/sdr/FDEA2019100322398), Oct 2, 2019: DOOR FRAME. CRACKED. MDCC L2 DOOR FRAME CRACKED AT THE UPPER HINGE CUTOUT. REPAIRED THE DOOR FRAME BS 680 - 700 IAW SRM 52-10-02-2R, REPAIR 1 & EA F-5210-T0321335 A P2. CLASSIFIED A
- [SDR FDEA2019100322397](https://openairdocs.org/sdr/FDEA2019100322397), Oct 2, 2019: DOOR FRAME. CRACKED. MDCC RT NR 2 DOOR FRAME CRACKED AT THE UPPER HINGE CUTOUT. REPAIRED THE DOOR FRAME BS 680 - 700 IAW SRM 52-10-02-2R, REPAIR 1. CLASSIFIED AS A MAJOR REPAIR IAW 
- [SDR FDEA2019082872032](https://openairdocs.org/sdr/FDEA2019082872032), Aug 27, 2019: VALVE. FAILED. ABORTED TAKEOFF AT 70 KTS DUE TO RT ENG BLEED OFF EICAS.EICAS WENT AWAY WITH THROTTLES AT IDLE.ON TAXIBACK SAME EICAS WHENEVER THROTTLES PUSHED UP. REMOVED AND 
- [SDR FDEA2018092542667](https://openairdocs.org/sdr/FDEA2018092542667), Sep 24, 2018: FLOORBOARD. DENTED. FLOORBOARD DENTED AT B/S 830 LBL 50 CARRIED OUT EVALUATION OF FLOORBOARD DENTED ON UPPER DECK BS830 LBL 50 AS PER SRM 53-00-50-1A REV 125. DAMAGE WAS FOUND TO B
- [SDR FDEA2018092512663](https://openairdocs.org/sdr/FDEA2018092512663), Sep 21, 2018: DOOR FRAME. DAMAGED. GOUGE DAMAGE FOUND ON B-STA 231-25 BL O FRAME FROM CONTACT WITH MEC ACCESS DOOR LATCH PIN REPAIRED IAW SRM 53-00-07-2R REPAIR 7. THIS IS A MAJOR REPAIR.
- [SDR FDEA2018091432521](https://openairdocs.org/sdr/FDEA2018091432521), Sep 13, 2018: HYDRAULIC LINE. LEAKING. ON SHORT FINAL, L HYD QTY WENT TO ZERO. AS WE WERE FULLY CONFIGURED, WE OPTED TO LAND AND STOP ON THE RUNWAY. PTU KICKED IN ABOUT 150 AGL. WE CAME TO A STOP RAN
- [SDR FDEA201805091199](https://openairdocs.org/sdr/FDEA201805091199), May 9, 2018: COMPUTER. MALFUNCTIONED. MCP WENT BLANK EXCEPT FOR IAS, HDG AND ALT. WHEN GS WAS SELECTED FLIGHT DIRECTORS SUDDENLY COMMANDED A CLIMBING LEFT TURN, WHICH WAS TOTALLY INCONSISTENT. WE TU
- [SDR FDEA201710032840](https://openairdocs.org/sdr/FDEA201710032840), Oct 3, 2017: STRUCTURE. CORRODED. LT PYLON CORROSION ON ACCESS PANEL 433GR CUTOUT AREA CARRIED OUT REPAIR TO CORROSION ON LT PYLON AROUND ACCESS PANEL 433GR CUTOUT IAW SRM 54-50-01-1A ALLOWABLE 
- [SDR FDEA201710032839](https://openairdocs.org/sdr/FDEA201710032839), Oct 3, 2017: FLOORBEAM. CORRODED. EVIDENCE OF CORROSION FOUND RBL 2.90 FLOORBEAM LOCATED AFT CARGO COMPARTMENT BETWEEN STA 1330 AND STA 1440. CARRIED OUT REPAIR TO FLOORBEAM AT STA 1330 RBL 2.90
- [SDR FDEA201709252843](https://openairdocs.org/sdr/FDEA201709252843), Sep 25, 2017: WEB. CRACKED. CRACK ON FLOOR WEB AT BS 580, LBL 47. CARRIED OUT REPAIR TO CRACKED FLOOR WEB AT STA 580 LBL 47 IAW EA F-5330-T0335604.
- [SDR FDEA201709232680](https://openairdocs.org/sdr/FDEA201709232680), Sep 23, 2017: FLOOR SUPPORT. CORRODED. EVIDENCE OF CORROSION FOUND AT RBL 10.45, FLOOR SUPPORT LOCATED IN THE AFT CARGO BAY BETWEEN BS 1330 AND 1440. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-53, REPA

All 190: https://openairdocs.org/aircraft/N918FD/reports.md

## STCs that may be installed (OpenAirDocs) (6)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Boeing 757-23A)

- [STC ST01162NY](https://openairdocs.org/stc/ST01162NY): Installation of Literature Pockets. Magee Plastics Company. Lists 757 Series
- [STC ST01675CH](https://openairdocs.org/stc/ST01675CH): Installation of Butterfly Valve Ring AIR23028 in starter control valves, part number 775538 or 799700. Cook Airtomic. Lists 757 Series
- [STC ST02296AT](https://openairdocs.org/stc/ST02296AT): Upgrade existing HF Voice Communication System to provide HF datalink capability. ARINC, Inc. Lists 757 Series
- [STC SA01916AT](https://openairdocs.org/stc/SA01916AT): Manufacture of Tray Carrier P/N 1839-501. BFE Services. Lists 757 Series
- [STC SA1258EA](https://openairdocs.org/stc/SA1258EA): Installation of Cosco model78-( ) child restraint system. (172M S/N 17263459 - 17267584). Miller Stuart R. Lists 757 Series

### Approved for the engine (Rolls-Royce RB211-535E4 series)

- [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc. Lists RB211-535E4-37

## Related

- Other Boeing 757-23A aircraft: https://openairdocs.org/model/boeing-757-23a/aircraft.md
- The Rolls-Royce RB211-535E4 series engine: https://openairdocs.org/engine/rolls-royce-rb211-535e4-series.md

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