# N961FD: 1991 Boeing 757-2Y0

- Status: Valid registration
- Airframe: [Boeing 757-2Y0](https://openairdocs.org/model/boeing-757-2y0) (registry code 138492A, 178 seats)
- Engine: [Rolls-Royce RB211-535E4 series](https://openairdocs.org/engine/rolls-royce-rb211-535e4-series) (registry code 54223)
- Data sheets: [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs)
- Serial number: 25268
- Year built: 1991
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 14, 2012
- Certificate issued: October 28, 2011
- Expires: October 31, 2027
- Mode S code: AD605E
- Registered owners: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Attn: Michael Wilson](https://openairdocs.org/faa-owner/ATTN%3A%20MICHAEL%20WILSON)
- 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=961FD
- Page: https://openairdocs.org/aircraft/N961FD

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 757-2Y0)

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 N961FD.

## FAA accident and incident reports

None matched to N961FD.

## Service difficulty reports (80, 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 FDEA202403070260](https://openairdocs.org/sdr/FDEA202403070260), Mar 7, 2024: RESERVOIR. LOW PRESSURE. L1 DOOR EMERGENCY POWER RESERVOIR NEEDS SERVICING. OUT OF GREEN BAND RANGE. INSPECTED L1 DOOR POWER RESERVOIR REF AMM 52-11-30-6-0. RESEVOIR PRESSURE GAUGE IS I
- [SDR FDEA202310161769](https://openairdocs.org/sdr/FDEA202310161769), Oct 16, 2023: GUST LOCK. DAMAGED. MDIS 961 52-10 9274 13OCT23 MEM FACT U L1 DOOR GUST LOCK BROKEN. MEL 13OCT23 06:26 MEM U RELEASED FOR SERVICE PER MEL : 52-11-01-A CATEGORY : B EXPIRATION : 16O
- [SDR FDEA202301130089](https://openairdocs.org/sdr/FDEA202301130089), Jan 13, 2023: RELAY. FAILED. ON APPROACH, TE LIGHT WITH TE FLAP DISAGREE MESSAGE, WHEN FLAPS SET TO 25. CONFIRMED FLAP HANDLE IN DETENT. COMPLIED WITH QRH FOR SUBSEQUENT APPROACH & LANDING.
- [SDR FDEA202209222356](https://openairdocs.org/sdr/FDEA202209222356), Sep 22, 2022: FSEU. FAILED. MOVING FLAP LEVER FROM 20 TO 25 A TRAILING EDGE FLAP DISAGREE EICAS MESSAGE DISPLAYED. QRH COMPLIED WITH AND EMERGENCY DECLARED. EMERGENCY DECLARED. REMOVED AND
- [SDR FDEA202206081394](https://openairdocs.org/sdr/FDEA202206081394), Jun 8, 2022: GUST LOCK. DAMAGED. MDIS 961 52-10 8137 08JUN22 MEM OPEN U L1 DOOR GUST LOCK BROKEN MEL 08JUN22 05:17 MEM U RELEASED FOR SERVICE PER MEL : 52-11-01-A CATEGORY : B EXPIRATION : 11JU
- [SDR FDEA202205101176](https://openairdocs.org/sdr/FDEA202205101176), May 10, 2022: ROD. SHEARED. DURING TAXI-IN, NOTICED RIGHT NOSE GEAR DOOR, OPEN AND SWINGING. UPON BLOCK-IN, FOUND RIGHT NOSE GEAR ACTUATING ROD, REF IPC 32-22-02-01 FIG 1, ITEM 40, BROKEN 
- [SDR FDEA202203090775](https://openairdocs.org/sdr/FDEA202203090775), Mar 9, 2022: NONE. NONE. EMERGENCY/ UNARMED LIGHT INOP RELAMPED THE EMERGENCY "UNARMED" ANNUNCIATION LIGHT OPS CK GOOD PER B 757 AMM 33-51-00-5. AC OK FOR SERVICE.
- [SDR FDEA202012233202](https://openairdocs.org/sdr/FDEA202012233202), Dec 23, 2020: AUTOPILOT SYS. INOPERATIVE. TEST FLIGHT: ON CLIMB OUT WITH CENTER AUTO PILOT ON, STAB TRIM WENT FULL UP. DISENGAGE AUTO PILOT AND WAS ABLE TO CONTROL TRIM. HAPPENED TWICE MORE ON CLIMBOUT.
- [SDR FDEA202012093089](https://openairdocs.org/sdr/FDEA202012093089), Dec 9, 2020: FLOOR SUPPORT. CORRODED. AFT CARGO INTERCOSTAL HAS CORROSION ON LOWER OUTBOARD SIDE AT RBL-5 STA 1417. REMOVED INTERCOSTAL AT AFT CARGO STA 1417 RBL 5 AND EVALUATED AND FOUND OUT OF LIM
- [SDR FDEA202012053044](https://openairdocs.org/sdr/FDEA202012053044), Dec 5, 2020: CUSP WEB. CORRODED. MAIN CABIN RT CUSP WEB CORRODED BETWEEN STA 580 AND STA 600. REMOVED CORROSION AT MAIN CABIN RT CUSP WEB BETWEEN STA 580 TO STA 600 AND AFTER EVALUATION FOUND C
- [SDR FDEA202012053043](https://openairdocs.org/sdr/FDEA202012053043), Dec 5, 2020: CUSP WEB. CORRODED. MAIN CABIN RT CUSP WEB CORRODED BETWEEN STA 600 TO 620. REMOVED CORROSION AT MAIN CABIN RT CUSP WEB BETWEEN STA. 600 TO 620 AND EVALUATED ORIGINAL MAT .036", MA
- [SDR FDEA202012053042](https://openairdocs.org/sdr/FDEA202012053042), Dec 5, 2020: FAILSAFE. CORRODED. MAIN CABIN LT SIDE JUST ABOVE STR 17 STA 1520 ON FRAME CORRODED. COMPLIED WITH FEDEX EA NR F-5310-T0358418 P1. FUSELAGE-MAINFRAME-STA 1520 FAILSAFE CHORD CORROS
- [SDR FDEA202012043026](https://openairdocs.org/sdr/FDEA202012043026), Dec 4, 2020: SHIM. CRACKED. MAIN CARGO FLOOR SUPPORT SHIM DAMAGED AT STA 1058 BETWEEN LBL 24 AND LBL 45. REMOVED SHIM (COVER PLATE) AT MAIN CARGO FLOOR SUPPORT STA 1058 BETWEEN LBL 24 AND 
- [SDR FDEA202012023015](https://openairdocs.org/sdr/FDEA202012023015), Dec 2, 2020: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK FLANGE HAS CORROSION AT RBL 45 STA 1540. REMOVED CORROSION AT MAIN CABIN SEAT TRACK FLANGE RBL 45 STA 1540 AND AFTER EVALUATION FOUND SEAT
- [SDR FDEA202012023014](https://openairdocs.org/sdr/FDEA202012023014), Dec 2, 2020: SEAT TRACK. CORRODED. MAIN CABAIN STA 1540 LBL 45 SEAT TRACK FLANGE CORRODED. REMOVED CORROSION AT MAIN CABIN STA 1540 LBL 45 SEAT TRACK FLANGE AND AFTER EVALUATION FOUND SEAT TRACK 
- [SDR FDEA202012023013](https://openairdocs.org/sdr/FDEA202012023013), Dec 2, 2020: CREASE BEAM. CORRODED. MAIN CABIN RT SIDE STA 450 TO 665 CREASE BEAM CORRODED. REMOVED CORROSION AT MAIN CABIN RT SIDE CREASE BEAM BETWEEN STA 450 TO 665 AND AFTER EVALUATION FOUND CR
- [SDR FDEA202009192256](https://openairdocs.org/sdr/FDEA202009192256), Sep 19, 2020: COMPRESSOR. STALLED. PDIS 961 71-00 6706 19SEP20 ONT OPEN U LOGPAGES:3339293 AFTER TAKEOFF, AFTER SELECTING VNAV/CLIMB POWER, RIGHT ENGINE EXPERIENCED STRONG COMPRESSOR STALLS WITH 
- [SDR FDEA20200731732](https://openairdocs.org/sdr/FDEA20200731732), Jul 30, 2020: HANDLE. LACK OF LUBE. TE FLAP DISAGREE ON BASE TURN TO FINAL, WHEN GOING FROM FLAPS 20 TO 25. NO HISTORY PAST 90 DAYS. AFTER DEBREIFING CREW NO 'TE DISAGREE LIGHT' OR EICAS MESSAGE P
- [SDR FDEA202007211599](https://openairdocs.org/sdr/FDEA202007211599), Jul 21, 2020: COVER. LOOSE. SLIDE COVER ON L1 DOOR IS LOOSE. REPLACED DAMAGE POTED INSERTS ON UPPER HINGE COVER PANEL IAW AMM 25-00-00-8. INSTALLED SERVICEABLE SLIDE COVER IAW AMM 25-66-01
- [SDR FDEA2020030970502](https://openairdocs.org/sdr/FDEA2020030970502), Mar 7, 2020: UNKNOWN. ODOR. FUMES IN COCKPIT ON TAKEOFF ROLL TILL ABOUT 5K FT. REQUIRED CREW TO DON O2 MASK IMMEDIATELY AFTER TAKEOFF. ODOR OF BURNT RUBBER/ENG SMELL MAINLY ON CAPTAINS SID
- [SDR FDEA201812053433](https://openairdocs.org/sdr/FDEA201812053433), Dec 5, 2018: ACTUATOR. FAILED. PDIS 961 27-80 5336 05DEC18 LEVEL 10000 FT, 220 KIAS AND SLOWING, RECEIVED EICAS " LE SLAT DISAGREE" AND DISCRETE "LEADING EDGE" WHILE EXTENDING FLAPS 1. EMERGE
- [SDR FDEA2018120653433](https://openairdocs.org/sdr/FDEA2018120653433), Dec 5, 2018: ACTUATOR. FAILED. PDIS 961 27-80 5336 05DEC18 LEVEL 10000 FT, 220 KIAS AND SLOWING, RECEIVED EICAS " LE SLAT DISAGREE" AND DISCRETE "LEADING EDGE" WHILE EXTENDING FLAPS 1. EMERGE
- [SDR FDEA201811173272](https://openairdocs.org/sdr/FDEA201811173272), Nov 17, 2018: STRINGER. CRACKED. MAIN CABIN STA 1505 STR 1 CRACKED. REMOVED DAMAGED SECTION DIM 12" STA 1500 IAW SRM 53-00-03-2R REPAIR 2 FIG 201 DET 1. REMOVED FWD SECTION ON STR 1 FROM STA 14
- [SDR FDEA201711223298](https://openairdocs.org/sdr/FDEA201711223298), Nov 22, 2017: BOTTLE. DISCHARGED. NR 1 PASSENGER DOOR ASSIST BOTTLE DISCHARGED, REQUIRES SERVICING. REMOVED AND REPLACED CYLINDER EMERGENCY POWER RESERVOIR IAW MM 52-11-30-4.
- [SDR FDEA201709162581](https://openairdocs.org/sdr/FDEA201709162581), Sep 16, 2017: FSEU. MALFUNCTIONED. TRAILING EDGE FLAP DISAGREE LIGHT. LOCKED AT 20 DEGREES. COMPLIED WITH QRH. PERFORMED FSEU BITE PROCEDURE IAW FIM 27-51-00, FIG 104, FOUND NO CURENT FAULTS FOR 
- [SDR FDEA201708032108](https://openairdocs.org/sdr/FDEA201708032108), Aug 3, 2017: SEAT TRACK. DAMAGED. LOCK ON CENTERLINE BETWEEN STRINGERS 3L-R FOUND DAMAGED AT SEAT TRACK. REMOVED LOCK AND PLACED IN COURRIER COMPT. LOCK ID D611 MEL 29JUN17 18:59 SEAT TRACK LOBE
- [SDR FDEA201703290998](https://openairdocs.org/sdr/FDEA201703290998), Mar 29, 2017: TRANSMITTER. MALFUNCTIONED. AFTER TAKEOFF RECEIVED A LE SLAT DISAGREE EICAS. PERFORMED QRH. COMPLIED WITH LANDING PROCEDURES. REMOVED AND REPLACED LEADING EDGE PDU TRANSMITTER.
- [SDR FDEA201703291000](https://openairdocs.org/sdr/FDEA201703291000), Mar 29, 2017: FUEL SYS. LEAKING. LEFT WING INBOARD DRY BAY CENTER FORWARD DRAIN HAS A RUNNING FUEL LEAK.
- [SDR FDEA201703240986](https://openairdocs.org/sdr/FDEA201703240986), Mar 24, 2017: WARNING MESSAGE. FALSE ACTIVATION. LE SLAT DISAGREE EICAS MESSAGE AS FLAP EXTENDED TO FLAPS 1, WENT THROUGH QRH PROCEDURE WHICH LEAD TO A LE SLAT ASSYMETRY ISSUE. PERFORMED QRH PROCEDURE FOR LE S
- [SDR FDEA201703010723](https://openairdocs.org/sdr/FDEA201703010723), Mar 1, 2017: CONNECTOR. UNSECURE. DURING CRUISE FLIGHT AT FL390, A RAT UNLOCKED EICAS MESSAGE AND RAT UNLOCKED LIGHT IN RAT SWITCH ILLUMINATED. FIVE MINUTES LATER BOTH WARNINGS WERE NO LONGER DI
- [SDR FDEA201610273707](https://openairdocs.org/sdr/FDEA201610273707), Oct 27, 2016: SKIN. DELAMINATED. RIGHT WING OB FLAP TOP SECTON INBD SIDE REPAIR DISBONED. REPAIRED IAW SRM 57-53-01-2R FIG 201, SRM 51-70-10 REPAIR 4, AND SRM 51-70-10-2R PARA 20, FIG 208.
- [SDR FDEA201610273714](https://openairdocs.org/sdr/FDEA201610273714), Oct 27, 2016: DOOR FRAME. CRACKED. R2 DOOR UPPER HINGE CUTOUT IS CRACKED. LOCATED AND INSTALLED REPAIR DOUBLER PN 143N6158-12 AT R2 DOOR UPPER HINGE CUT OUT IAW SRM 52-10-02-2R. COMPLIED WITH EA 
- [SDR FDEA201507312445](https://openairdocs.org/sdr/FDEA201507312445), Jul 31, 2015: DOOR. DELAMINATED. LEFT MLG DOOR DELAMINATED. MISSING SECTION CRAZ COMPLY WITH EA F-5280-T0319221 REV NR POS P3. R & R MLG DOOR IAW MM 32-12-01-4 & EA F-5280-T0319221.
- [SDR FDEA201507192271](https://openairdocs.org/sdr/FDEA201507192271), Jul 19, 2015: BRACKET. LOOSE. L1 DOOR SLIDE COVER LOOSE. TIGHTENED SLIDE COVER ATTACH BRACKETS, AND INSTALLED SLIDE COVER FOR L1 DOOR IAW AMM 52-11-02-4.
- [SDR FDEA201505201570](https://openairdocs.org/sdr/FDEA201505201570), May 20, 2015: BRAKE. LACK OF LUBE. RECEIVED TE FLAP DISAGREE EICAS MSG ON APPROACH WHEN MOVING FLAPS FROM 20' TO 25'. RETRACTED FLAP HANDLE TO 20' IAW GO AROUND PROCEDURES, RAN QRH & LANDED FLAPS
- [SDR FDEA201411253894](https://openairdocs.org/sdr/FDEA201411253894), Nov 25, 2014: SKIN. DENTED. FUSELAGE HAS A DENT AT BS 525 BETWEEN STRINGERS 26 - 27L. REPAIRED IAW EA F-5330-T0313598 REV P1. MAJOR REPAIR.
- [SDR FDEA201407091672](https://openairdocs.org/sdr/FDEA201407091672), Jul 9, 2014: LIGHT. INOPERATIVE. DURING PREFLIGHT CHECK, FOUND R1 DOOR EMER SLIDE LIGHT INOPERATIVE. RELAMPED R1 DOOR SLIDE LIGHT, OPERATIONS CHECKED NORMAL.
- [SDR FDEA201407091671](https://openairdocs.org/sdr/FDEA201407091671), Jul 9, 2014: PIN. BACKED OUT. DURING PREFLIGHT, FOUND L1 DOOR EMER SLIDE LIGHT INOPERATIVE. REMOVED LIGHT ASSEMBLY & CHECKED VOLTAGE TO LIGHT WITH EMER LIGHTS ON, THERE IS NO POWER TO L1 SLI
- [SDR FDEA201302250457](https://openairdocs.org/sdr/FDEA201302250457), Feb 25, 2013: BATTERY. INOPERATIVE. DOOR EMERGENCY EXIT LIGHTS WILL NOT TEST. R & R L1 EMERGENCY EXIT BATTERY PACK IAW MM 33-51-07-2. OPS CHECKED NORMAL.
- [SDR FDEA201212104273](https://openairdocs.org/sdr/FDEA201212104273), Dec 10, 2012: WEB. DAMAGED. MAIN DECK- CARGO DOOR CUTOUT ON FUSELAGE SILL AREA LOWER SILL WEB HAS A PUNCTURE LOCATED JUST AFT OF NR 1 DOOR LATCH FITTING. A REPAIR WAS ACCOMPLISHED ON THE L
- [SDR FDEA201212054250](https://openairdocs.org/sdr/FDEA201212054250), Dec 5, 2012: TRACK. FAILED. THE CARGO HANDLING SYS, ROLLER RAILS WILL NOT LOCK INTO THE SEAT TRACK CROWNS BETWEEN STA, S660-780 RBL 24.75 AND 45.5. DISCEPANT SEAT TRACKS ARE INCOMING. DUE 
- [SDR FDEA201212044245](https://openairdocs.org/sdr/FDEA201212044245), Dec 4, 2012: SKIN. CORRODED. LT INBD FLAP, FRONT INBD PANEL HAS CORROSION. REMOVED CORROSION ON LT INBD FLAP INBD PANEL IAW-SRM-51-10-02. CHECK LIMIT ORIG MAT .125 MAT LOSS .030 FOUND OUT O
- [SDR FDEA201211214119](https://openairdocs.org/sdr/FDEA201211214119), Nov 21, 2012: STRINGER CLIP. CORRODED. FOUND CORROSION AT BS 1661 S26R STINGER CLIP. REPAIRED IAW SRM 53-00-03 REPAIR 2.
- [SDR FDEA201211144019](https://openairdocs.org/sdr/FDEA201211144019), Nov 14, 2012: SKIN. DENTED. DENT IN FUSELAGE AT BS 380 STRINGER 4R A FUSELAGE EXTERNAL SKIN REPAIR WAS ACCOMPLISHED BETWEEN STA 377-418 IAW EA 757-5311-16-F3939 REV- . MAJOR REPAIR.
- [SDR FDEA201211093928](https://openairdocs.org/sdr/FDEA201211093928), Nov 9, 2012: SKIN. DENTED. SKIN DENTED BS 1630 BETWEEN S17 TO 18R. DENT REPAIRED IAW EA 757-5361-16-F3919. MAJOR REPAIR.
- [SDR FDEA201211093926](https://openairdocs.org/sdr/FDEA201211093926), Nov 9, 2012: SKIN. MISREPAIRED. FUSELAGE SKIN MISREPAIRED BS 395 BETWEEN S1 TO 3L. REPAIRED IAW EA 757-5311-16-F3891, REV-.
- [SDR FDEA201211083914](https://openairdocs.org/sdr/FDEA201211083914), Nov 8, 2012: STRINGER. CORRODED. STRINGER 17R BS 1420-1440 CORRODED REPAIRED EA 757-5361-16-F3901. MAJOR REPAIR.
- [SDR FDEA201211073904](https://openairdocs.org/sdr/FDEA201211073904), Nov 7, 2012: PANEL. CORRODED. NR 2 SLAT COVE PANEL JUST BELOW INBD MAIN TRACK FITTING HAS CORROSION. REMOVED CORROSION ON COVE PANEL IAW SRM 51-10-02. REMOVED .019 FROM ORIGINAL THICKNESS OF
- [SDR FDEA201211023813](https://openairdocs.org/sdr/FDEA201211023813), Nov 2, 2012: STRUCTURE. MISREPAIRED. CARGO DOOR LWR FWD CORNER MISREPAIRED. REPAIRED IAW-SRM-52-30-01 FIG.201 REPAIR 4 THIS IS A CAT."B" REPAIR,MAJOR.
- [SDR FDEA201211013808](https://openairdocs.org/sdr/FDEA201211013808), Nov 1, 2012: SKIN. DAMAGED. LEFT WING TOP OTBD WINGTIP HAS A LIGHTING STRIKE. FOUND LIGHTENING STRIKE TO BE ON SCREW AND SPLICE STRAP. REMOVED AND REPLACED OUTBOARD RIB LT WING SPLICE STRA

All 80: https://openairdocs.org/aircraft/N961FD/reports.md

## STCs that may be installed (OpenAirDocs) (1)

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 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 757-2Y0 aircraft: https://openairdocs.org/model/boeing-757-2y0/aircraft.md
- The Rolls-Royce RB211-535E4 series engine: https://openairdocs.org/engine/rolls-royce-rb211-535e4-series.md

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