# N970FD: 1997 Boeing 757-28A

- Status: Valid registration
- Airframe: [Boeing 757-28A](https://openairdocs.org/model/boeing-757-28a) (registry code 1384976, 249 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: 28166
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 5, 2013
- Certificate issued: October 24, 2012
- Expires: October 31, 2028
- Mode S code: AD8426
- 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=970FD
- Page: https://openairdocs.org/aircraft/N970FD

From the FAA registry file of October 20, 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 757-28A)

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 N970FD.

## FAA accident and incident reports

None matched to N970FD.

## Service difficulty reports (70, newest 50)

As reported by operators and repair stations.

- [SDR FDEA202605050561](https://openairdocs.org/sdr/FDEA202605050561), May 5, 2026: MODULE. FAULTED. AFTER TAKEOFF, GEAR DISAGREE AND GEAR DOORS EICAS MESSAGES APPEARED ACCOMPANIED BY AN AUDIBLE AND TACTILE INDICATION THAT THE GEAR AND/OR GEAR DOORS WERE NOT RE
- [SDR FDEA202506030833](https://openairdocs.org/sdr/FDEA202506030833), Jun 3, 2025: SKIN. CRACKED. L/T WING # 2 SLAT POSSIBLE CRACK ON SKIN AT BACK SIDE ON LOWER AREA OF O/B MAIN TRACK TRIMMED DAMAGE AREA, LH WING # 2 SLAT O/B MAIN TRACK IAW B757 SRM 57-43-01
- [SDR FDEA202506030832](https://openairdocs.org/sdr/FDEA202506030832), Jun 3, 2025: SKIN. CRACKED. LE SLAT NO 9 INTERNAL SKIN WITH CRACK REMOVED L/E SLAT NO 9 INTERNAL SKIN PANEL IAW B757 SRM 51-40-02-0G, FORMED TRIMMED, LOCATED, DRILLED AND INSTALLED NEW SKI
- [SDR FDEA202506030831](https://openairdocs.org/sdr/FDEA202506030831), Jun 3, 2025: SKIN. CRACKED. L/T WING # 1 SLAT POSSIBLE CRACK ON SKIN AT BACK SIDE ON LOWER AREA OF I/B MAIN TRACK TRIMMED OUT DAMAGE AREA L/T WING # 1 SLAT ON SKIN AT I/B MAIN TRACK IAW B7
- [SDR FDEA202506030830](https://openairdocs.org/sdr/FDEA202506030830), Jun 3, 2025: SKIN. CRACKED. LE SLAT NO 8 INTERNAL SKIN WITH CRACK REMOVED SKIN PANEL L/E SLAT NO 8 IAW B757 SRM 51-40-02-0G FORMED, TRIMMED, LOCATED DRILLED AND INSTALL NEW SKIN PANEL IAW 
- [SDR FDEA202307281329](https://openairdocs.org/sdr/FDEA202307281329), Jul 28, 2023: UNKNOWN. UNKNOWN. R-3 DOOR, STRINGER CLIP DEFORMED AT STRINGER S-13R BETWEEN BS 1340 AND BS 1360. REMOVED AND REPLACED DEFORMED STRINGER CLIP IAW B757 SRM 51-40-02 AND BACDWG 146
- [SDR FDEA202307261306](https://openairdocs.org/sdr/FDEA202307261306), Jul 26, 2023: RETAINER. CRACKED. R/H MLG TRUNNION DOOR SEAL RETAINER IS CRACKED.. REMOVED SEAL AND RETAINER, FABRICATED NEW RETAINER PER BAC DWG 113N8200 AND FEDEX EA # F-3210- T0375397 TITLE :
- [SDR FDEA202307251292](https://openairdocs.org/sdr/FDEA202307251292), Jul 25, 2023: SLAT. DELAMINATED. #3 SLAT UPPER SURFACE TRAILING EDGE WEDGE HAS AN AREA OF DISBOND LOCATED 52" FROM THE OUTBOARD EDGE AND 4" FROM THE TRAILING EDGE. APPROX 2.5" IN DIAMETER. REPA
- [SDR FDEA202307201254](https://openairdocs.org/sdr/FDEA202307201254), Jul 20, 2023: UNKNOWN. UNKNOWN. MAIN CABIN - FLOOR PANEL AT STA 440 TO STA 560 , LBL24 TO LBL 45 IS SATURATED IN HYDRAULIC FLUID REMOVED, FABRICATED AND REPLACED FLOOR PANEL IAW B757 AMM 53-01
- [SDR FDEA202211012702](https://openairdocs.org/sdr/FDEA202211012702), Nov 1, 2022: SKIN. DAMAGED. WHILE WORKING #1 O/B T/R C DUCT CHANGE FOUND DAMAGE ON UPPER PORTION OF INBOARD #1 ENG FAN COWL REPAIRED IAW EA F-7110-T0371402 THIS IS A MAJOR REPAIR
- [SDR FDEA202204191001](https://openairdocs.org/sdr/FDEA202204191001), Apr 19, 2022: COLLAR. CRACKED. L1 DOOR HOLD OPEN LOCK COLLAR BROKEN. REMOVED AND REPLACED L1 DOOR OPEN LOCK REF AMM 52-11-08-4. OPS CHECK GOOD.
- [SDR FDEA202204191000](https://openairdocs.org/sdr/FDEA202204191000), Apr 19, 2022: GUST LOCK. FAILED. MDIS 970 52-10 7067 19APR22 DAY OPEN U R1 DOOR HOLD OPEN LOCK COLLAR BROKEN FACT 21APR22 18:02 MEM R1 DOOR HOLD OPEN LOCK (MPN: 654N0244-8) REPLACED REF B757 AM
- [SDR FDEA202203300780](https://openairdocs.org/sdr/FDEA202203300780), Mar 30, 2022: VALVE. NONE. L-ENG ANT-ICE EICAS MESSAGE DISPLAYED ALONG WITH VALVE LIGHT ON L ENGINE ANTI ICE SWITCH DISPLAYED DURING DESCENT WHEN SELECTED ON AND STAYED ON FOR REMAINDER O
- [SDR FDEA202101160132](https://openairdocs.org/sdr/FDEA202101160132), Jan 16, 2021: VALVE. INOPERATIVE. NR 5 BRAKE INOPERABLE FUNCTIONS NORMALLY IN ALTERNATE (LT HYD SYS). REPLACED LEFT ANTISKID SHUTTLE VALVE MODULE, IAW 757 MM 32-42-07-4. OPERATIONS AND LEAK CHEC
- [SDR FDEA202010230330](https://openairdocs.org/sdr/FDEA202010230330), Oct 23, 2020: CASE. CORRODED. #1 ENG AT 9 O`CLOCK LP COMPRESSOR CASE OUTER SURFACE HAS CORROSION IN EXCESS OF 10 AROUND (FWD) MATING FLANGE TO INLET (UNDER KEVLAR WRAP). REMOVED AND REPLACED
- [SDR FDEA202007081461](https://openairdocs.org/sdr/FDEA202007081461), Jul 8, 2020: GUST LOCK. MALFUNCTIONED. L ENTRY DOOR GUST LOCK DOES NOT LATCH IN THE RELEASE POSITION.
- [SDR FDEA201907091515](https://openairdocs.org/sdr/FDEA201907091515), Jul 9, 2019: BRACKET. DAMAGED. WIC 5782600-00-01 AGING AIRCRAFT INSPECTION- LT I/B MAIN FLAP O/B SIDE OF #3 FLAP TRACK FWD BRACKET HAS ELONGATED HOLES. REMOVED ,FABRICATED AND INSTALLED NEW B
- [SDR FDEA201907011451](https://openairdocs.org/sdr/FDEA201907011451), Jul 1, 2019: FLOOR SUPPORT. CORRODED. MAIN CABIN BETWEEN STA.1680-1720, BL.0 - RBL.54 FLOOR SUPPORT WEB CORRODED. REMOVED CORROSION FROM M/C AFT DECK WEB STA.1680 - 1720 , BL.0 - RBL.54, MAX MATERIA
- [SDR FDEA201907011449](https://openairdocs.org/sdr/FDEA201907011449), Jul 1, 2019: SKIN. CORRODED. CORROSION, APU LT ACCESS DOOR FUSELAGE CUTOUT STRUCTURE FWD END, APPROX. BS.1887.5, INNER SURFACE, JUST AFT OF THE APU FIREWALL. COMPLIED WITH EA#F-5330-T034775
- [SDR FDEA201907011442](https://openairdocs.org/sdr/FDEA201907011442), Jul 1, 2019: FLOORBEAM. CORRODED. COCKPIT STA.345 BETWEEN LBL5-LBL 24 FLOORBEAM CORRODED. CORROSION ON EXISTING FLOORBEAM "T "CAP REPAIR OUT OF LIMITS, REMOVED EXISTING "T" CHORD ANGLE & REPAIR 
- [SDR FDEA201907011450](https://openairdocs.org/sdr/FDEA201907011450), Jul 1, 2019: SKIN. CORRODED. CORROSION APU RT ACCESS DOOR FUSELAGE CUTOUT STRUCTURE FWD END, APPROX. BS.1887.5, INNER SURFACE, JUST AFT OF THE APU FIREWALL. EVAL. CORROSION DAMAGE WITH 100%
- [SDR FDEA201907011448](https://openairdocs.org/sdr/FDEA201907011448), Jul 1, 2019: FRAME. GOUGED. INSIDE FWD ACC. COMPARTMENT, FRAME AT STA. 231.25 HAS A GOUGE IN UPPER RADIUS AT BL.0. CUT OUT DAMAGE & FABRICATED AND INSTALLED FRAME REPAIR AT STA. 231.25 BL.
- [SDR FDEA2019021430395](https://openairdocs.org/sdr/FDEA2019021430395), Feb 13, 2019: HANDLE. OBSTRUCTED. COULD NOT ARM SLIDE ON RIGHT HAND ENTRY DOOR. RELOCATED CORD DIDN'T LET CLOSE PROPERLY, OPERATE DOOR SEVERAL TIMES , OPS CKS NORMAL REF AMM 52-11-01-6.
- [SDR FDEA201806071418](https://openairdocs.org/sdr/FDEA201806071418), Jun 7, 2018: STATIC LINE. TANGLED. RIGHT FORWARD ENTRY DOOR WILL NOT FULLY DISARM. SLIDE ARM LIGHT WILL EXTINGUISH, BUT EVACUATION SLIDE LEVER WILL NOT MOVE FULLY TO THE DISARM POSITION. FOUND ST
- [SDR FDEA201709222674](https://openairdocs.org/sdr/FDEA201709222674), Sep 22, 2017: PLUNGER. DAMAGED. RAMP REPORTED THE MAIN CARGO DOOR WILL NOT CLOSE. FOUND THE TIP MISSING FROM PLUNGER ON MAIN CARGO DOOR SEQUENCE VALVE. REPLACED THE TIP IAW SRM 51-40-02. MAIN 
- [SDR FDEA201705241502](https://openairdocs.org/sdr/FDEA201705241502), May 24, 2017: BOTTLE. EMPTY. L1 DOOR WAS ARMED, CREW ATTEMPTED TO OPEN DOOR, L1 EMERGENCY ASSIST BOTTLE DEPLETED SLIDE DID NOT DEPLOY.
- [SDR FDEA201612114381](https://openairdocs.org/sdr/FDEA201612114381), Dec 11, 2016: WARNING LIGHT. FALSE ACTIVATION. AT LEVEL OFF, RECEIVED A CTR L FUEL PUMP ALERT WITH 5.1 OF FUEL IN CENTER TANK. REACTIVATED LT CTR OVERRIDE FUEL PUMP. AUDIBLE CHECKED THE LT CTR OVERRIDE PUMP 
- [SDR FDEA201609213326](https://openairdocs.org/sdr/FDEA201609213326), Sep 21, 2016: WINDOW. FAILED. AT CRUISE FL290, A LOUD BANG WAS HEARD THEN ARCING & SHATTERING OF FO'S FORWARD WINDOW. REPLACED RT FWD WINDOW. OK FOR SERVICE.
- [SDR FDEA201507212287](https://openairdocs.org/sdr/FDEA201507212287), Jul 21, 2015: FSEU. INOPERATIVE. ON DEPARTURE, WHEN SELECTING FLAPS UP, HAD A LE DISAGREE EICAS. FLAP INDICATOR SHOWED STUCK BETWEEN 1 DEGREE & UP. PERFORMED CHECKLIST & RETURNED TO DEPARTURE. 
- [SDR FDEA201506201930](https://openairdocs.org/sdr/FDEA201506201930), Jun 20, 2015: SKIN. DENTED. PROTRUDING DENT STATION 523 AT STRINGER 26L. COMPLIED WITH EA F-5330-TO318148 PART 1 FUSELAGE PLATES & SKIN. REPAIR AT STATION 523 BETWEEN STRINGERS 26L - 27L.
- [SDR FDEA201506201929](https://openairdocs.org/sdr/FDEA201506201929), Jun 20, 2015: SKIN. DENTED. TWO EACH DENTS STATION 490 BELOW 27L. COMPLIED WITH EA F-5330-TO318149 PART 1 FUSELAGE PLATES & SKINS. REPAIR AT STATION 490 BETWEEN STRINGERS 27L - 28L.
- [SDR FDEA201506161821](https://openairdocs.org/sdr/FDEA201506161821), Jun 16, 2015: SKIN. DENTED. LEFT AILERON UNDER SIDE HAS SMALL DENT. BONDED REPAIRED IAW SRM 51-70-17 PG 14/15 PARA 4, 57-60-01-212. OPS CHECKED GOOD IAW AMM 27-11-00-0.
- [SDR FDEA201312203031](https://openairdocs.org/sdr/FDEA201312203031), Dec 20, 2013: BOLT. OUT OF POSITION. AFTER LANDING GOT FLAP LE SLAT AYSYM EICAS MESSAGE BETWEEN UP & 1 POSITION. NR 1 FLAP, SLAT ELEX UNIT BITE SHOWS RT SLAT DRIVE. NR 2 UNIT SHOWS RT SLAT XMITTER.
- [SDR FDEA201308081809](https://openairdocs.org/sdr/FDEA201308081809), Aug 8, 2013: WIRE. LOOSE. EMERGENCY EXIT SIGN ABOVE R1 DOOR INOPERATIVE. FOUND R1 DOOR EMERGENCY EXIT LIGHT WIRE NR 1 NOT PROPERLY SEATED AT QUICK DISCONNECT, RESEATED WIRE IAW SMP. R1 D
- [SDR FDEA201307231638](https://openairdocs.org/sdr/FDEA201307231638), Jul 23, 2013: BATTERY PACK. INOPERATIVE. SLIDE ILLUMINATION LIGHT AND CENTER EMERGENCY EXIT SIGN INOPERATIVE. R & R EMERGENCY LIGHT POWER SUPPLY ASSY IAW AMM 33-51-07-2. OPS CHECKED GOOD.
- [SDR FDEA201306251413](https://openairdocs.org/sdr/FDEA201306251413), Jun 25, 2013: SKIN. CRACKED. LT WING NR 3 SLAT, AT INBD TRACK, JUST OUTBOARD, COVE SKIN CRACKED, COVE SKIN FOUND TO BE OUT OF LIMITS IAW-SRM-57-43-01, FIG 101, SHEET (2 OF 4) NOTE B, NO CRA
- [SDR FDEA201306131370](https://openairdocs.org/sdr/FDEA201306131370), Jun 13, 2013: CREASE BEAM. CRACKED. CREASE BEAM OTBD ANGLE CRACKED AT BS 1641, S17L. REPAIRED CREASE BEAM IAW EA 757-5361-16-F4175. MAJOR REPAIR.
- [SDR FDEA201306131271](https://openairdocs.org/sdr/FDEA201306131271), Jun 13, 2013: SKIN. DEBONDED. LEFT WING INBD FLAP, TOP OTBD PANEL LOWER SURFACE, DISBONDED. REPAIRED SKIN IAW SRM 51-70-10. REPAIR 4. MAJOR REPAIR
- [SDR FDEA201305311154](https://openairdocs.org/sdr/FDEA201305311154), May 31, 2013: SKIN. MISREPAIRED. FUSELAGE SKIN BS 395-418 BETWEEN S2-4L MISREPAIRED. REPAIRED IAW EA F-5330-T0300578. MAJOR REPAIR
- [SDR FDEA201305311153](https://openairdocs.org/sdr/FDEA201305311153), May 31, 2013: STRINGER FITTING. CORRODED. LOWER LOBE STR 26L AFT END ATTACHMENT FITTING HAS CORROSION BS 1720. REMOVED CORROSION ON STRINGER 26L END FITTING IAW SRM 51-10-02, ORIGINAL THICKNESS .090, RE
- [SDR FDEA201305221068](https://openairdocs.org/sdr/FDEA201305221068), May 22, 2013: SKIN. DAMAGED. RT WING INBD FLAP, TOP OTBD PANEL, LOWER SURFACE HONEYCOMB EDGE VOID. REPAIRED IAW SRM 51-70-10. REPAIR 4. CAT "A" MAJOR REPAIR.
- [SDR FDEA201305211057](https://openairdocs.org/sdr/FDEA201305211057), May 21, 2013: FITTING. WORN. BS 935, BL 0, FITTING HAS ONE OVERSIZED HOLE OF 0.352 IN DIAMETER. THE MATING FLOOR STRUCTURE HAS SAME HOLE SIZE AT SAME LOCATION AT STA 935, BL0. REPAIR WAS AC
- [SDR FDEA201305161011](https://openairdocs.org/sdr/FDEA201305161011), May 16, 2013: SKIN. DENTED. EXTERNAL FUSELAGE SKIN BS 1600-1620 BETWEEN S25-26R HAS TWO DENTS. . BS 1613 BETWEEN S26-25R A=0.6 Y=.045 A/Y= 13.33 OUT OF LIMITS. REPAIRED IAW SRM-53-00-01, F
- [SDR FDEA201305151005](https://openairdocs.org/sdr/FDEA201305151005), May 15, 2013: SKIN. CORRODED. NR 1 SLAT COVE SKIN LWR EDGE CORRODED. REMOVED CORROSION IAW-SRM-51-10-02 ON NR 1 SLAT COVE SKIN LWR EDGE, CHECKED LIMIT .050 MAT. LOSS .009, FOUND OUT OF LIMIT
- [SDR FDEA201305140982](https://openairdocs.org/sdr/FDEA201305140982), May 14, 2013: FITTING. CRACKED. NR 2 PYLON STRUT TO DIAGONAL BRACE FITTING RT SIDE AFT INBD HOLE SHOWS CRACK INDICATION AT THE 4:30 POS IN THE ALUMINUM BULKHEAD ONLY. COMPLIED WITH EA F-5450-T
- [SDR FDEA201305100969](https://openairdocs.org/sdr/FDEA201305100969), May 10, 2013: SKIN. MISREPAIRED. SKIN MISREPAIRED BS 1700 -1720 S15-16L. REPAIRED IAW EA F-5330-T0300418, CAT "B" MAJOR REPAIR.
- [SDR FDEA201305070932](https://openairdocs.org/sdr/FDEA201305070932), May 7, 2013: SKIN. GOUGED. LEFT FUSELAGE EXTERNAL SKIN HAS GOUGES AT STA. 1862 , S9L.
- [SDR FDEA201304270871](https://openairdocs.org/sdr/FDEA201304270871), Apr 27, 2013: FRAME. CRACKED. MAIN CABIN BS 760 BETWEEN S8- 9R FRAME IS CRACKED. FOUND CRACKED AT FAST HOLE , CRACKED IS NOT ALLOWED IAW SRM 53- 00-07, REPAIRED FRAME IAW SRM 53-00-07, REPAI
- [SDR FDEA201304240849](https://openairdocs.org/sdr/FDEA201304240849), Apr 24, 2013: SKIN. CRACKED. NR 2 SLAT COVE SKIN, OSS 677.5 CRACKED AT FASTENER. REMOVED CRACKED NR 2 SLAT COVE SKIN IAW-SRM-51-40-02, REPLACED CRACKED COVE SKIN WITH NEW COVE SKIN IAW-SRM-
- [SDR FDEA201304230834](https://openairdocs.org/sdr/FDEA201304230834), Apr 23, 2013: SKIN. CRACKED. NR 1 SLAT COVE SKIN , OSS 736.7, CRACKED AT FASTENER. REMOVED CRACKED NR 1 SLAT COVE SKIN, IAW-SRM-51-40-02, FOUND OUT OF LIMITS, IAW-53-00-71. REPLACED CRACKED

All 70: https://openairdocs.org/aircraft/N970FD/reports.md

## Related

- Other Boeing 757-28A aircraft: https://openairdocs.org/model/boeing-757-28a/aircraft.md
- STCs for the Boeing 757-28A: https://openairdocs.org/model/boeing-757-28a/stcs.md
- The Rolls-Royce RB211-535E4 series engine: https://openairdocs.org/engine/rolls-royce-rb211-535e4-series.md

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From OpenAirDocs.org, an independent open copy of FAA and NTSB data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.