# N919FD: 1990 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 RB211535E4B37](https://openairdocs.org/engine/rolls-royce-rb211535e4b37) (registry code 54054)
- 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: 24636
- Year built: 1990
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, normal
- Airworthiness date: November 19, 2008
- Certificate issued: January 16, 2008
- Expires: May 31, 2029
- Mode S code: ACB89B
- 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=919FD
- Page: https://openairdocs.org/aircraft/N919FD

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.

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

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

None in force.

### Matched by engine (Rolls-Royce RB211535E4B37)

- [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 DCA18WA088](https://openairdocs.org/ntsb/DCA18WA088), Jan 30, 2018: Boeing 757 23A (N919FD), Tel Aviv, Israel, incident, no damage

## FAA accident and incident reports

None matched to N919FD.

## Service difficulty reports (203, 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 FDEA202608261232](https://openairdocs.org/sdr/FDEA202608261232), Aug 26, 2026: FRAME. CRACKED. RIGHT, BS 1640 FUSELAGE FRAME WEB AT STRINGER 14R UPPER INBD CRACK INDICATION AT 2:00 O'CLOCK, AROUND THE BOTTOM INBD HOLE WITH TWO CRACK INDICATIONS AT 2:00 O'
- [SDR FDEA202608251224](https://openairdocs.org/sdr/FDEA202608251224), Aug 25, 2026: SKIN PANEL. CRACKED. LH WING NR 3 SLAT MAIN TRACK SUPPORT AREA LOWER SURFACE SKIN WITH CRACKED. COVE PANEL WITH CRACK AT LH WING # 3 SLAT MAIN TRACK SUPPORT AREA LOWER SURFACE WAS R
- [SDR FDEA202608131118](https://openairdocs.org/sdr/FDEA202608131118), Aug 13, 2026: FLOORBEAM. CORRODED. MAIN CABIN FLOORBEAM AT BS 1200 BETWEEN BL 0 TO LBL 24.75 WITH CORROSION FLOORBEAM SECTION OUT OF LIMITS AT MAIN CABIN B.S 1200 BETWEEN LBL 5 TO LBL 11 WAS REPA
- [SDR FDEA202608121116](https://openairdocs.org/sdr/FDEA202608121116), Aug 12, 2026: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK BEWTEEN BS 1060 TO 1080 RBL 45.50 WITH CORROSION MAIN CABIN SEAT TRACK SUPPORT (UPPER CHORD) BETWEEN STA 1040-1080 WITH CORROSION OUT OF L
- [SDR FDEA202608121115](https://openairdocs.org/sdr/FDEA202608121115), Aug 12, 2026: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK BETWEEN BS 1180 TO BS 1200 LBL 24.75 OUTB FLANGE WITH CORROSION REMOVED CORROSION AT MAIN CABIN SEAT TRACK AT STA 1180 TO 1200 LBL 24.75 I
- [SDR FDEA202608081101](https://openairdocs.org/sdr/FDEA202608081101), Aug 8, 2026: SKIN. DAMAGED. EVALUATE EXISTING DOUBLER REPAIR ON RH INBOARD MAIN FLAP LOWER SURFACE, NEAR MF STA 147.00 FOR RSC TRACKING PURPOSE ONLY EXISTING REPAIR ON RH INBOARD MAIN FLAP
- [SDR FDEA202608081100](https://openairdocs.org/sdr/FDEA202608081100), Aug 8, 2026: SKIN. DAMAGED. EVALUATE EXISTING COMPOSITE REPAIR AT LT ELEVATOR UPPER SURFACE T/E, OUTBOARD AREA. REPAIRED AT LH ELEVATOR UPPER SURFACE T/E, OUTBOARD AREA WAS EVALUATED UNDER
- [SDR FDEA202603220365](https://openairdocs.org/sdr/FDEA202603220365), Mar 22, 2026: SKIN. CORRODED. #2 ENG. L/H FUSELAGE EXTERIOR COMPOSITE PANEL HAS CORROSION ON OUTER ALUMINUM SKIN AT FWD LWR CORNER NEAR APU PLENUM DRAIN. APPROX. STA. 1904 REF. BOEING DWG. 1
- [SDR FDEA202409211334](https://openairdocs.org/sdr/FDEA202409211334), Sep 21, 2024: SKIN. DENTED. INCOMING A/C DAMAGE JUST BELOW AND FWD OF THE MAIN CARGO DOOR. DENT MEASURING APPROX 2"X3" AND MAX DEPTH OF 0.0119. LOCATED 2" AFT OF FS460 JUST BELOW STR 18L. 
- [SDR FDEA202409111303](https://openairdocs.org/sdr/FDEA202409111303), Sep 11, 2024: FLOORBOARD. DAMAGED. MAIN DECK CARGO COMPT FLOORBOARD PANEL 252 MWF IN ZONE 250 DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 252MWF ON VTMAE TRAVELER T24/1774253 IAW DRAWING SRZ-25
- [SDR FDEA202409111302](https://openairdocs.org/sdr/FDEA202409111302), Sep 11, 2024: FLOORBOARD. DAMAGED. MAIN DECK CARGO COMPT FLOORBOARD PANEL 251 MWF IN ZONE 250 DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 251MWF ON VTMAE TRAVELER T24/1774230 IAW DRAWING SRZ-25
- [SDR FDEA202409111301](https://openairdocs.org/sdr/FDEA202409111301), Sep 11, 2024: FLOORBOARD. DAMAGED. MAIN DECK FLOORGOARD PANEL 251MXF IN ZONE 250 DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 251MXF ON VTMAE TRAVELER #T24/1774251 IAW SRZ-25-005 REVISION R DRAW
- [SDR FDEA202406010758](https://openairdocs.org/sdr/FDEA202406010758), Jun 1, 2024: SUPPORT. DAMAGED. L/H WING, AFT FAIRING SUPPORT INBD MAIN FLAP FITTING IS LOOSE. FOUND AFT MOUNT HOLE DAMAGED IN LH I/B LWR MAIN FLAP FOR FAIRING SUPPORT BRACKET. REPAIRED DAMAGE
- [SDR FDEA202403280391](https://openairdocs.org/sdr/FDEA202403280391), Mar 28, 2024: WINDOW. CRACKED. WHILE IN CRUISE FLIGHT FL360, CAPTAIN SIDE FRONT WINDSCREEN ARCED FOLLOWED BY SHATTERING WITH OUTER PAIN. RAN QRH, ARCING CONTINUED. POSSIBLE DEFORMED WINDOW WI
- [SDR FDEA202403150295](https://openairdocs.org/sdr/FDEA202403150295), Mar 15, 2024: TRANSMISSION. CONTAMINATED. TE FLAP DISAGREE MESSAGE FOLLOWING SELECTION OF FLAPS 1. FLAPS INDICATED UP. COMPLETED QRH. DECLARED EMERGENCY. LANDED FLAPS 20. PERFORMED FIM 27-51 FT 808, NO 
- [SDR FDEA202403150294](https://openairdocs.org/sdr/FDEA202403150294), Mar 15, 2024: BOTTLE. FAILED. R1 DOOR SLIDE ASSIST BOTTLE EXTINGUISHED DURING OPENING OF R1 DOOR. REMOVED AND REPLACED R1 DOOR EMERGENCY POWER RESERVOIR CYLINDER. REPLACED R1 DOOR SLIDE IAW 
- [SDR FDEA202308141406](https://openairdocs.org/sdr/FDEA202308141406), Aug 14, 2023: CHARGER. FAILED. MDIS 919 33-50 5583 13AUG23 SHV FACT U DURING SERVICE CHECK FOUND L1 DOOR INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP FACT 14AUG23 20:34 SHV U AMM: 33-51-07-02 
- [SDR FDEA202212022866](https://openairdocs.org/sdr/FDEA202212022866), Dec 2, 2022: NONE. NONE. DUE TO WRI 25-60/5015 AND A POSSIBLE SAFTEY CONCERN OF THE NORMAL OPERATION OF THE R1 DOOR SLIDE WHEN OPENING FROM THE EXTERIOR. R1 DOOR, TO INCLUDE THE SLIDE, 
- [SDR FDEA202211302858](https://openairdocs.org/sdr/FDEA202211302858), Nov 30, 2022: RESERVOIR. FALSE ACTIVATION. UPON BLOCK IN PILOTS REQUEST MAINTENANCE TO OPEN R1 DOOR FROM OUTSIDE DUE TO INDICATION MEL. WHEN OPENING DOOR BOTTLE DISCHARGED AND SLIDE FELL OUT OF BUSTLE BU
- [SDR FDEA202211302856](https://openairdocs.org/sdr/FDEA202211302856), Nov 30, 2022: LIGHT. MALFUNCTIONED. R1 SLIDE LIGHT DOES NOT EXTINGUISH WHEN DISARMING DOOR. ACCOMPLISHED GIRT BAR ESCAPE SLIDE ARM & DISARMED OPERATION IAW AMM 25-66-00-10 & 25-66-01-4. ALL INDICA
- [SDR FDEA202211042729](https://openairdocs.org/sdr/FDEA202211042729), Nov 4, 2022: FRAME. CRACKED. WHILE PERFORMING HFEC INSP OF FRAME WEB INBD OF STRINGER S-26L AT BODY STATION 1460, FOUND CRACK INDICATON ON INBD HOLE AT 6:O,CLOCK. ACCOMPLISHED REPAIR PER EA
- [SDR FDEA202210272679](https://openairdocs.org/sdr/FDEA202210272679), Oct 27, 2022: FLOORBOARD. DENTED. MAIN CARGO FLOOR PANEL 241MMF IS DAMAGE. FABRICATED ZONE 240 FLOORBOARD 241MMF ON VTMAE TRAVELER # T22/1641931 IAW DWG SRZ- 25-005 REVISION R. PART MARK PER GMM
- [SDR FDEA202210252666](https://openairdocs.org/sdr/FDEA202210252666), Oct 25, 2022: FLOORBOARD. DELAMINATED. ZONE 220 FLOORBOARD 221 BF IS DELAMINATED. FABRICATED COURIER AREA FLOORBOARD 221BF FROM TRAVELER T22/1640838 IAW DWG SRZ-25- 005. PART MARKED IAW GMM 07-01-100
- [SDR FDEA202210252665](https://openairdocs.org/sdr/FDEA202210252665), Oct 25, 2022: FLOORBOARD. DELAMINATED. ZONE 220 FLOORBOARD 221 MBF IS DAMAGED. FABRICATED COURIER AREA FLOORBOARD 221 MBF FROM TRAVELER T22/1641793 IAW DWG SRZ- 25-005. PART MARKED IAW GMM 07-01-1001
- [SDR FDEA202208181994](https://openairdocs.org/sdr/FDEA202208181994), Aug 18, 2022: HOSE. LEAKING. AT 300FT ON LANDING, WE EXPERIENCED A L HYD QTY MESSAGE, FOLLOWED BY L HYD SYS PRESS UPON LANDING. HYD QTY SHOWS 0.00. DUE TO L HYD SYS TOTAL LOST OF FLUID, INT
- [SDR FDEA202206031372](https://openairdocs.org/sdr/FDEA202206031372), Jun 3, 2022: SKIN. DENTED. CROWN SKIN HAS OUTWARD DENTS LEFT AND RIGHT OF STRINGER 1 JUST FORWARD OF STA 418. REPAIRED DENTED CROWN SKIN PER EA F-5330-T036881
- [SDR FDEA202103060583](https://openairdocs.org/sdr/FDEA202103060583), Mar 6, 2021: PLUG. LOOSE. AT CRUISE AT FL350 THE RIGHT AND TOTAL QTY INDICATIONS ARE INTERMITTENT. AT OTHER TIMES THE RIGHT QTY INDICATION FLUTUATED - 1,000 POUNDS. DIVERTED TO SIN AND M
- [SDR FDEA202010282669](https://openairdocs.org/sdr/FDEA202010282669), Oct 28, 2020: SPAR. CORRODED. RIGHT HAND WING LEFT HAND TRAILING EDGE OUTBOARD MAIN FLAP REAR SPAR UPPER CHORD FOUND CORROSION AT AROUND WBL 387 OUTBOARD OF NR 7 FLAP TRACK. EA F-5750-T03576
- [SDR FDEA202010262652](https://openairdocs.org/sdr/FDEA202010262652), Oct 26, 2020: SEAT TRACK. CORRODED. MAIN DECK, CARGO SEAT TRACK FOUND CORROSION AT STATION 876, RBL 45.5 MAIN DECK STATION 876 RBL 45.5. CARGO SEAT TRACK CORROSION REPAIRED, AS PER B757 SRM 53-00-
- [SDR FDEA201810303052](https://openairdocs.org/sdr/FDEA201810303052), Oct 30, 2018: CROSSBEAM. CORRODED. MDCC CROSSBEAM CORRODED B/W STA1640, LBL24.75-LBL45.5. THIS IS A MINOR REPAIR, CLOSE THE SDR.
- [SDR FDEA201810303051](https://openairdocs.org/sdr/FDEA201810303051), Oct 30, 2018: CROSSBEAM. CORRODED. MDCC CROSSBEAM CORRODED B/W STA1680,RBL0-RBL24.75. REPAIRED THE CORRODED CROSSBEAM AT MDCC STA1680,RBL0-RBL24.75 PER B757 SRM51- 40-02 AND SRM53-60-51 REPAIR 3.
- [SDR FDEA201810303049](https://openairdocs.org/sdr/FDEA201810303049), Oct 30, 2018: SEAT TRACK. CORRODED. MDCC SEAT TRACK CORRODED B/W STA1620-STA1640,LBL45.5. REPLACED THE CORRODED SEAT TRACK AT MDCC STA1540-STA1640,LBL45.5 PER B757 SRM51-40-02. MAJOR REPAIR IAW FE
- [SDR FDEA201810303048](https://openairdocs.org/sdr/FDEA201810303048), Oct 30, 2018: SEAT TRACK. CORRODED. MDCC SEAT TRACK CORRODED B/W STA 1180-STA 1200, LBL 45.5. REPLACED THE CORRODED SEAT TRACK AT MDCC STA1180-STA1240,LBL45.5 PER B757 SRM51-40-02. MAJOR REPAIR IA
- [SDR FDEA201712283461](https://openairdocs.org/sdr/FDEA201712283461), Dec 28, 2017: SLIDE. UNWANTED DEPLOY. L1 SLIDE WAS DEPLOYED BEFORE DEPARTURE. REMOVED AND REPLACED THE SLIDE IAW MM 25-66-01-4.
- [SDR FDEA201612164471](https://openairdocs.org/sdr/FDEA201612164471), Dec 16, 2016: MODULE. MALFUNCTIONED. AFTER LANDING, COMING OUT OF TURN ONTO TAXIWAY, NOSE WHEEL STEERING WAS UNRESPONDING FEELS AS THOUGH NWS TILLER WAS BINDING. PERFORMED RIGGING CHECK AND SYSTEM 
- [SDR FDEA201610243680](https://openairdocs.org/sdr/FDEA201610243680), Oct 24, 2016: SKIN. DAMAGED. LEFT ELEVATOR DAMAGED ON UPPER SURFACE. REPAIRED IAW EA F-5520-T0329101 P1.
- [SDR FDEA201610213674](https://openairdocs.org/sdr/FDEA201610213674), Oct 21, 2016: SKIN. DAMAGED. LIGHTNING STRIKE ON FUSELAGE SKIN AT BS 402, 1.5'' ABOVE 24R REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01, FIG 201, REPAIR 6, SECTION I, REV 118.
- [SDR FDEA201610213673](https://openairdocs.org/sdr/FDEA201610213673), Oct 21, 2016: SKIN. DAMAGED. LIGHTNING STRIKE AT BS 282, 29'' BELOW LAPJOINT STR 20R. REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01, FIG 201, REPAIR 6, SECTION I, REV 118.
- [SDR FDEA201610213672](https://openairdocs.org/sdr/FDEA201610213672), Oct 21, 2016: SKIN. DAMAGED. LIGHTNING STRIKE AT BS 535, 2.5'' ABOVE STR 23 RT. REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01 FIG 201, REPAIR 6 ,SECTION I, REV 118.
- [SDR FDEA201610213671](https://openairdocs.org/sdr/FDEA201610213671), Oct 21, 2016: SKIN. DAMAGED. LIGHTNING STRIKE AT BS 692, 1.5'' BELOW STR 21R. REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01 FIG 201, REPAIR 6, SECTION I REV 118.
- [SDR FDEA201610213670](https://openairdocs.org/sdr/FDEA201610213670), Oct 21, 2016: SKIN. DAMAGED. LIGHTNING STRIKE AT BS 329, 1.5'' ABOVE STR 24 RT. REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01 FIG 201 REPAIR 6 SECTION I REV 118.
- [SDR FDEA201610213669](https://openairdocs.org/sdr/FDEA201610213669), Oct 21, 2016: SKIN. DAMAGED. LIGHTNING STRIKE AT BS 370, 1.5'' ABOVE STR 24RT. REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01 FIG 201 REPAIR 6, SECTION I REV 118.
- [SDR FDEA201610213668](https://openairdocs.org/sdr/FDEA201610213668), Oct 21, 2016: SKIN. DAMAGED. LIGHTNING STRIKE AT BS 409, 1.5'' ABOVE STR 24R. REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01 FIG 201, REPAIR 6 SECTION I REV 118.
- [SDR FDEA201610113686](https://openairdocs.org/sdr/FDEA201610113686), Oct 11, 2016: SKIN. DAMAGED. LIGHTNING STRIKE AT BS 468, 0.5" ABOVE STR 23R ON FUSELAGE SKIN. CARRIED OUT REPAIR IAW SRM 53-00-01 FIG 201 REPAIR 15 REV118
- [SDR FDEA201610113681](https://openairdocs.org/sdr/FDEA201610113681), Oct 11, 2016: WEDGE. DELAMINATED. DELAMINATION FOUND IN THE RT OTBD SLAT NR 7 T/E WEDGE UPPER AND LOWER SURFACE AT IB END. REMOVED AND REPLACED IAW AMM 27-81-02 ACCOMPLISHED EA F-5750-T0329030.
- [SDR FDEA201605251730](https://openairdocs.org/sdr/FDEA201605251730), May 25, 2016: STEERING SYS. OUT OF RIG. DURING TAKEOFF, AFTER ENGAGING THE THRUST TILE, THE ACFT WOULD NOT HOLD CENTERLINE. REJECTED TAKEOFF 08 L CDG. BOTH THRUST LEVERS WERE ALIGNED, RUDDER & AILERON
- [SDR FDEA201602020421](https://openairdocs.org/sdr/FDEA201602020421), Feb 2, 2016: SWITCH. DIRTY. ON TAKEOFF, AT APPROX 40 KTS, MASTER CAUTION ILLUMINATED WITH CHIMES, AUTO THROTTLE DISC, DISPLAYED ON EICAS. TAKEOFF WAS REJECTED. FOLLOWED QRH PROCEDURES, ALE
- [SDR FDEA201511253790](https://openairdocs.org/sdr/FDEA201511253790), Nov 25, 2015: WINDOW. CRACKED. DURING CRUISE, LT FWD WINDOW ARCING & THEN OUTER PANE CRACKED. R & R NR 1 FLIGHT DECK WINDSHIELD IAW AMM 56-11-01-4. PERFORMED WINDOW HEATING SYS TEST, TEST PAS
- [SDR FDEA201510303412](https://openairdocs.org/sdr/FDEA201510303412), Oct 30, 2015: CYLINDER. INOPERATIVE. RIGHT DOOR OPEN WITH GIRT BAR ACTIVATED, BUT NO ACTIVATION SLIDE, NOT POSSIBLE TO ARM DOOR. R & R R1 DOOR EMER POWER CYLINDER IAW AMM 52-11-30-4-0. REINSTALLED 
- [SDR FDEA201510063087](https://openairdocs.org/sdr/FDEA201510063087), Oct 6, 2015: UNKNOWN. ODOR. HEAVY BURNING ELEC SMELL IN COCKPIT WHEN ENCOUNTERING HEAVY RAIN & TURBULENCE FL360. ACCOMPLISHED EVIDENCE OF SMELL IAW MM:05-51-56-2, RUN APU WITH PACKS, INSPE

All 203: https://openairdocs.org/aircraft/N919FD/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 RB211535E4B37)

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

## Related

- Other Boeing 757-23A aircraft: https://openairdocs.org/model/boeing-757-23a/aircraft.md
- The Rolls-Royce RB211535E4B37 engine: https://openairdocs.org/engine/rolls-royce-rb211535e4b37.md

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