# N938FD: 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: 24292
- Year built: 1989
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 19, 2013
- Certificate issued: July 25, 2012
- Expires: July 31, 2028
- Mode S code: AD03E2
- 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=938FD
- Page: https://openairdocs.org/aircraft/N938FD

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

None matched to N938FD.

## FAA accident and incident reports

None matched to N938FD.

## Service difficulty reports (87, 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 FDEA202310301815](https://openairdocs.org/sdr/FDEA202310301815), Oct 30, 2023: STATIC INVERTER. BURNED. MDIS 938 24-22 9631 30OCT23 IND FACT U UPON POWERING UP AIRCRAFT, NOTICED AN ACRID SMELL IN COCKPIT WITH ASSOCIATED STBY INVERTER EICAS MSG. PART 30OCT23 16:24 
- [SDR FDEA202307271317](https://openairdocs.org/sdr/FDEA202307271317), Jul 27, 2023: UNKNOWN. SHEARED. MDIS 938 32-42 9432 27JUL23 BUR FACT U AT PUSHBACK #7 MLG TIRE BLEW, UPON INSPECTION FOUND EIGHT TIE BOLTS HAD SHEARED OFF. 5 R/I 27JUL23 04:06 BUR U REASON COD
- [SDR FDEA202304070588](https://openairdocs.org/sdr/FDEA202304070588), Apr 7, 2023: SKIN. DAMAGED. R/H EXTERIOR FUSELAGE SKIN DOUBLER HAS 2EA DENTS BETWEEN BS 540 AND BS 560 AND STRINGER S-22R AND STRINGER S23R REPAIRED PER FEDEX EA # F-5330-165083-P3
- [SDR FDEA202304060575](https://openairdocs.org/sdr/FDEA202304060575), Apr 6, 2023: ANGLE. CORRODED. AREA OF AFT CARGO COMPARTMENT, MAIN CABIN FLOOR SUPPORT STRUCTURE AND NUTSTRIP ARE CORRODED BETWEEN STA 1701 AND 1720 APPROX RBL 13 REMOVED AND REPLACED ANGLE (
- [SDR FDEA202304060573](https://openairdocs.org/sdr/FDEA202304060573), Apr 6, 2023: ANGLE. CORRODED. AREA OF THE BULK CARGO COMPARTMENT, MAIN CABIN FLOOR SUPPORT STRUCTURE AND NUTSTRIP ARE CORRODED BETWEEN STA 1701 AND 1720 APPROX LBL5 REMOVED AND REPLACED ANGL
- [SDR FDEA202304060572](https://openairdocs.org/sdr/FDEA202304060572), Apr 6, 2023: ANGLE. CORRODED. AREA AFT OF THE BULK CARGO COMPARTMENT, MAIN CABIN FLOOR SUPPORT STRUCTURE & NUT STRIP ARE CORRODED BETWEEN STA 1701 & 1720 APPROX RBL 5 REMOVED AND REPLACED FL
- [SDR FDEA202304060571](https://openairdocs.org/sdr/FDEA202304060571), Apr 6, 2023: PANEL. DELAMINATED. R.WING L/E PANEL 611DB HAS COMPOSITE DAMAGE ON MULTIPLE AREAS. ACCOMPLISHED PERMANENT REPAIR ON R/W L/E PANEL 611DB COMPOSITE DAMAGE PER B757 SRM 57-41-01-4R, 5
- [SDR FDEA202304060570](https://openairdocs.org/sdr/FDEA202304060570), Apr 6, 2023: PANEL. DELAMINATED. #1 PYLON PANEL 432AL AFT 2 CORNERS ARE DELAMINATED AND DAMAGED. ACCOMPLISHED PERMANENT REPAIR OF PANEL PER B757 SRM 51-40-02, 54-50-70-0G, 51-70-17-0G AND BOEIN
- [SDR FDEA202303300525](https://openairdocs.org/sdr/FDEA202303300525), Mar 30, 2023: STRAP. CRACKED. #2 ENG I/B T/R L/E RADIAL STRAP IS CRACKED AT APPROX 8 0CLOCK POS. REMOVED AND REPLACED PER B757 AMM 78-31-20-8
- [SDR FDEA202302090243](https://openairdocs.org/sdr/FDEA202302090243), Feb 9, 2023: UNKNOWN. UNKNOWN. PDIS 938 52-10 9099 09FEB23 PHX FACT U ON FO S PRE-FLIGHT FO DISCOVERED R1 DOOR SLIDE CABLE EXPOSED. CALLED MX TO VERIFY AND CHECK THAT IT WOULD NOT CATCH ON TH
- [SDR FDEA202206011356](https://openairdocs.org/sdr/FDEA202206011356), Jun 1, 2022: SURVIVAL KIT. OUT OF POSITION. R1 DOOR EMERGENCY SLIDE SURVIVAL KIT STRAP NOT STOWED PROPERLY. REMOVED SLIDE COVER AND PROPERLY STOWED THE R1 DOOR EMERGENCY SLIDE SURVIVAL KIT STRAP AND INSTA
- [SDR FDEA202205101167](https://openairdocs.org/sdr/FDEA202205101167), May 10, 2022: GIRT BAR. DIRTY. PDIS 938 25-60 8387 10MAY22 SJO FACT U ENTRY DOOR KNUCKLE BUSTER WILL NOT DEPLOY WHEN ARMING DOOR. FACT 10MAY22 01:43 SJO U INSPECTED L1 ENTRY DOOR AND REMOVED 
- [SDR FDEA202203030406](https://openairdocs.org/sdr/FDEA202203030406), Mar 3, 2022: HOSE. FAILED. L HYD QTY L HYD SYS PRESS TE FLAP DISAGREE COMPLIED WITH QRH, DECLARED EMERGENCY. LANDED RWY 31, SHUTDOWN ON RWY. PERFORMED EDP INSPECTION/CHECK REF AMM 29-11-0
- [SDR FDEA202105051128](https://openairdocs.org/sdr/FDEA202105051128), May 5, 2021: SEAT TRACK. CORRODED. DOT# 106-12, MAIN CARGO COMPT APPROX. STA. 1340, RBL 45.50 SEAT TRACK HAS CORROSION. CUT OUT DAMAGE SEAT TRACK FROM STA 1300 TO STA 1350 RBL 45.5 IAW SRM 53-00-
- [SDR FDEA202105051119](https://openairdocs.org/sdr/FDEA202105051119), May 5, 2021: FLOOR PANEL. DELAMINATED. COURIER FLOOR PANEL 221BF DELAMINATED. FABRICATED COURIER FLOOR PANEL 221BF ON VTMAE TRAVELER #T21/1548308 IAW FEDEX DWG. DWG. NO. SRZ-25-005 REV. R CAT "A" MAJ
- [SDR FDEA202105051118](https://openairdocs.org/sdr/FDEA202105051118), May 5, 2021: FLOOR PANEL. DELAMINATED. COURIER FLOOR PANEL 221AF DELAMINATED. FABRICATED COURIER FLOOR PANEL 221AF ON VTMAE TRAVELER #T21/1548307 IAW FEDEX DWG DWG NO. SRZ-25-005 REV R. CAT "A" MAJOR
- [SDR FDEA202105051117](https://openairdocs.org/sdr/FDEA202105051117), May 5, 2021: FLOOR PANEL. DELAMINATED. COURIER FLOOR PANEL 222MAF DELAMINATED. FABRICATED FLOOR PANEL 222MAF ON VTMAE TRAVELER #T21/1548305 IAW DWG SRZ-25-005 REV REV R CAT "A" MAJOR REPAIR.
- [SDR FDEA202105051116](https://openairdocs.org/sdr/FDEA202105051116), May 5, 2021: FLOOR PANEL. DELAMINATED. COURIER FLOOR PANEL 221MBF DELAMINATED. FABRICATED COURIER FLOOR PANEL 221MBF ON VTMAE TRAVELER #T21/1548304 IAW DWG SRZ- SRZ-25-005 REV R CAT "A" MAJOR REPAIR.
- [SDR FDEA202105051114](https://openairdocs.org/sdr/FDEA202105051114), May 5, 2021: FLOOR PANEL. DELAMINATED. COURIER 222AF FLOOR PANEL DELAMINATED. FABRICATED 222AF COURIER FLOOR PANEL ON VTMAE TRAVELER #T21/1548306 IAW DWG SRZ-25- SRZ-25-005 REV R, CAT "A" MAJOR REPAI
- [SDR FDEA2020071311485](https://openairdocs.org/sdr/FDEA2020071311485), Jul 11, 2020: UNKNOWN. MALFUNCTIONED. DURING POWER TRANSFER ON SHUTDOWN, ALL SCREENS WENT BLANK AND LEFT ENGINE POWER WAS INCREASING WITH THE THRUST LEVER AT IDLE. BLOCK IN FUEL 10.0 CREW DEBRIEFED 
- [SDR FDEA2020021070284](https://openairdocs.org/sdr/FDEA2020021070284), Feb 7, 2020: VALVE. LEAKING. 30 MINUTES INTO FLIGHT AT FL340 EXPERIENCED "CABIN ALTITUDE" ALERT. NOTED A DIFFERENTIAL OF 6.0 WITH CABIN ALT OF 11,000. RAN QRH AND PROCEEDED TO KICT AT 10.00
- [SDR FDEA202002070280](https://openairdocs.org/sdr/FDEA202002070280), Feb 7, 2020: SELECTOR. FAILED. CABIN ALTITUDE WARNING ANNUNCIATED AT CRUISE FL370. VERIFIED CABIN ALT, DON MASKS. QRH COMPLIED WITH DECENT TO 15,000. CABIN PRES STABILIZED. CLIMBED TO FL250 C
- [SDR FDEA201904180847](https://openairdocs.org/sdr/FDEA201904180847), Apr 18, 2019: STRINGER. GOUGED. STRINGER 1 HAS EXISTING GOUGE NEAR HILOCK COLLAR APPOX STA. 1505 AND ELONGATED FASTENER HOLE AT EXISTING HILOCK APPROX STA. 1515. CUT OUT DAMAGED SECTION OF MAI
- [SDR FDEA2018102973033](https://openairdocs.org/sdr/FDEA2018102973033), Oct 27, 2018: SHUTOFF VALVE. MALFUNCTIONED. CABIN ALT WANING -LOSS OF PRESSURIZATION AT FL310 ON CLIMB OUT. HAD MEL 77-12-03 (N3 TACHOMETER NR 1 ENG) AND RAN QRH FOR L ENG BLEED OFF EICAS MSG. APPROX 10 M
- [SDR FDEA201710213022](https://openairdocs.org/sdr/FDEA201710213022), Oct 21, 2017: CONTROL UNIT. FAILED. SPOILER ALERT ILLUMINATED ON THE EICAS AND OVERHEAD. ALL HYDRAULICS GOOD. NO ROLL OR BUFFET. PERFORMED BITE TEST OF THE SMCS AND FOUND 2R SCM FAULT ON THE LAST 
- [SDR FDEA201710132926](https://openairdocs.org/sdr/FDEA201710132926), Oct 13, 2017: ACTUATOR. MISSING. SLIDE LIGHT ABOVE THE R1 DOOR FOUND INOPERATIVE WITH DOOR CLOSED AND SLIDE HANDLE IN ARMED POSITION. FOUND THE PROXIMITY SENSOR -A S10216. PROXIMITY ACTUATOR MI
- [SDR FDEA201706131635](https://openairdocs.org/sdr/FDEA201706131635), Jun 13, 2017: INDICATOR. OBSTRUCTED. ARMING INDICATION IS NOT POPPING OUT CORRECTLY. IT WAS CORRECTLY INDICATING AT PUSH BACK. BUT TOOK A FEW TRIES. FOUND THAT THE L1 DOOR ARM INDICATOR STICKER WAS
- [SDR FDEA201704281295](https://openairdocs.org/sdr/FDEA201704281295), Apr 28, 2017: STIFFENER. CRACKED. RT WW AFT PRESSURE BULKHEAD LWR INBD STIFFENER CRACKED. REMOVED THE STIFFENER LOCATED, DRILLED NEW AND INSTALLED IAW SRM 51-40-02-0G AND SRM 51-40-05-0G.
- [SDR FDEA201704281293](https://openairdocs.org/sdr/FDEA201704281293), Apr 28, 2017: STIFFENER. CRACKED. LEFT MLG WW AFT PRESSURE BULKHEAD LOWER INBD STIFFENER CRACKED. REMOVED THE STIFFENER. LOCATED, DRILLED A NEW STIFFENER AND INSTALLED IAW SRM 51-40-02-0G, AND S
- [SDR FDEA201704201244](https://openairdocs.org/sdr/FDEA201704201244), Apr 20, 2017: SKIN. DENTED. FUSELAGE SKIN HAS THREE PROTUDING DENTS IN EXTERNAL SKIN LOWER FUSELAGE AT BS 520 AND TWO INCHES INBD OF STRINGER 26L. SKIN REPAIRED IAW EA F-5330-T0332752 P1.
- [SDR FDEA201612304580](https://openairdocs.org/sdr/FDEA201612304580), Dec 30, 2016: MODULE. INOPERATIVE. DURING DECENT, AUTOPILOT FAILED TO CAPTURE ALTITUDE (5000'). ALT WARNING WORKED. R&R THE STAB TRIM ASSY MODULE, PASSES MCDP TEST 65 AS WELL AS MCDP GROUND TEST 
- [SDR FDEA201507082177](https://openairdocs.org/sdr/FDEA201507082177), Jul 8, 2015: SWITCH. STUCK. WHILE TROUBLESHOOTING ACARS SYS, FOUND L1 DOOR SWITCH S10094 STUCK IN THE CLOSED POSITION. OPERATIONS CHECKED OK.
- [SDR FDEA201504161244](https://openairdocs.org/sdr/FDEA201504161244), Apr 16, 2015: DOUBLER. DAMAGED. APU FWD BULKHEAD RT SIDE HAS A DAMAGED AND GOUGED PREVIOUS REPAIR. REMOVED DAMAGE DOUBLER IAW SRM 51-40-02, FABRICATED NEW DOUBLER IAW SRM 53-80-08-2R, INSTALLE
- [SDR FDEA201407111715](https://openairdocs.org/sdr/FDEA201407111715), Jul 11, 2014: SLIDE RAFT. PARTIAL DEPLOY. AFTER DISARMING CREW ENTRY DOOR 1R SLIDE PARTIALLY DEPLOYED UPON OPENING DOOR. REMOVED AND REPLACED THE R1 DOOR SLIDE/RAFT
- [SDR FDEA201407111714](https://openairdocs.org/sdr/FDEA201407111714), Jul 11, 2014: HANDLE. LOOSE. L1 DOOR HANDLE PLASTIC, TOP RT IS LOOSE. SECURED THE L1 DOOR ASSIST HANDLE PER B757 AMM.
- [SDR FDEA201304100763](https://openairdocs.org/sdr/FDEA201304100763), Apr 10, 2013: SKIN. CHAFED. AFT FUSELAGE SKIN BELOW STRINGER 9L AFT OF BULKHEAD BS 1787, EXT SURFACE CHAFED BY STAB FAIRING. COMPLIED WITH EA F-5330-T0300225, CAT "A" MAJOR REPAIR.
- [SDR FDEA201304050732](https://openairdocs.org/sdr/FDEA201304050732), Apr 5, 2013: SKIN. DENTED. FUSELAGE SKIN DENTED BS 443 AT S15R. A SKIN REPAIR WAS ACCOMPLISHED IAW EA 757 -5331-16-F4106, REV. MAJOR REPAIR
- [SDR FDEA201304020711](https://openairdocs.org/sdr/FDEA201304020711), Apr 2, 2013: SKIN. MISREPAIRED. LT WING, NR 2 SLAT COVE PANEL INBD OF OTBD DRIVE TRACK MISREPAIRED. R & R, NR 2 SLAT, INBD OF OTBD DRIVE TRACK, COVE SKIN IAW DWG 114N4026 AND INSTALLED IAW SRM
- [SDR FDEA201303300692](https://openairdocs.org/sdr/FDEA201303300692), Mar 30, 2013: STRUCTURE. DAMAGED. OTBD FLAP LT WING BETWEEN STA 565 -600 HAS ELONGATED HOLE. A REPAIR WAS ACCOMPLISHED IAW EA 757-5753 -16 -F4116, REV-. MAJOR REPAIR.
- [SDR FDEA201303290687](https://openairdocs.org/sdr/FDEA201303290687), Mar 29, 2013: SKIN. FAILED. TWO MISDRILLED HOLES AT VERTICAL STAB LT PANEL 322DL ATTACHMENT. COMPLIED WITH EA F-5530-TO300208. MAJOR REPAIR.
- [SDR FDEA201303280684](https://openairdocs.org/sdr/FDEA201303280684), Mar 28, 2013: SKIN. CRACKED. R2 DOOR FWD FRAME FACE HINGE CUTOUT CRACKED A REPAIR WAS ACCOMPLISHED ON R2 DOOR FWD FRAME UPPER HINGE CUTOUT IAW EA 757-5211-16-F4100 REV, MAJOR REPAIR.
- [SDR FDEA201303200633](https://openairdocs.org/sdr/FDEA201303200633), Mar 20, 2013: SKIN. DENTED. INCOMING EXTERNAL FUSELAGE SKIN DENTED BS 1618, BETWEEN S17-18L, REPAIRED IAW EA 757-5361-16-F4111, REV. MAJOR REPAIR.
- [SDR FDEA201303150583](https://openairdocs.org/sdr/FDEA201303150583), Mar 15, 2013: INTERCOSTAL. CORRODED. AFT CARGO DOOR FRAME BS 1380-1400 INTERCOSTAL CORRODED. REPAIRED IAW EA 757-5360-16-F4146. MAJOR REPAIR
- [SDR FDEA201303150577](https://openairdocs.org/sdr/FDEA201303150577), Mar 15, 2013: STIFFENER. GOUGED. BS 1180 BULKHEAD STIFFENER, LBL 45.57 WL 182, GOUGED. BLENDED GOUGE ON STA 1180 BULKHEAD IAW SRM 51-10-02. L= 1.25 W= .75 D= .046 ORIGINAL MATERIAL .107 OUT OF 
- [SDR FDEA201303150582](https://openairdocs.org/sdr/FDEA201303150582), Mar 15, 2013: SKIN. DENTED. EXTERNAL FUSELAGE SKIN BS 1701-1720 BETWEEN S28-29R DENTED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL III. REPAIRED IAW SRM 53-00-01 FIG 201.
- [SDR FDEA201303130564](https://openairdocs.org/sdr/FDEA201303130564), Mar 13, 2013: SKIN. CORRODED. NR 1 PYLON INSIDE AREA, INBD SKIN IS CORRODED TWO PLACES. ACCOMPLISHED EA F- 5450- TO300125.
- [SDR FDEA201303130563](https://openairdocs.org/sdr/FDEA201303130563), Mar 13, 2013: SKIN. DENTED. FUSELAGE SKIN DENTED BS 550 BETWEEN S-18R TO S-19R. A SKIN DENT REPAIR BS 540-560, STRINGER S18-20R WAS ACCOMPLISHED IAW EA 757-5331-16-F 4088, REV.
- [SDR FDEA201303080528](https://openairdocs.org/sdr/FDEA201303080528), Mar 8, 2013: SKIN. DENTED. FUSELAGE SKIN DENTED BS 395 BETWEEN S-16R TO S-17R FOUND TO BE OUT OF LIMITS IAW SRM 53-00-010, FIG 101, DETAIL III. REPAIRED IAW SRM 53-00-01, REPAIR 16. MAJOR
- [SDR FDEA201303070513](https://openairdocs.org/sdr/FDEA201303070513), Mar 7, 2013: SKIN. CORRODED. NR 2 PYLON INTERNAL SKIN SURFACES LT SIDE FROM PPS 138 - 174, HAS SIGN OF CORROSION. REPAIRED IAW EA F-5450-T0300141. MAJOR REPAIR
- [SDR FDEA201303060504](https://openairdocs.org/sdr/FDEA201303060504), Mar 6, 2013: SKIN. CORRODED. NR 2 PYLON LEFT SKIN PANEL 443GL CUTOUT, EDGE CORRODED. REPAIRED IAW EA F-5450-T0300094. MAJOR REPAIR

All 87: https://openairdocs.org/aircraft/N938FD/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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