# N914FD: Boeing 757-28A - Status: Valid registration - Airframe: [Boeing 757-28A](https://openairdocs.org/model/boeing-757-28a) (registry code 1384976, 249 seats) - Serial number: 24367 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Certificate issued: February 24, 2009 - Expires: August 31, 2029 - Mode S code: ACA608 - 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=914FD - Page: https://openairdocs.org/aircraft/N914FD 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): 0 in force ### Matched by airframe (Boeing 757-28A) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N914FD. ## FAA accident and incident reports None matched to N914FD. ## Service difficulty reports (168, 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 FDEA202603040310](https://openairdocs.org/sdr/FDEA202603040310), Mar 4, 2026: GIRT BAR. DIRTY. PDIS 914 52-10 5125 03MAR26 23:10 OGG FACT L1 ENTRY DOOR WOULD NOT SHOW DISARM. DISARM LEVER DID NOT COMPLETELY DISARM (LEVER AND KNUCKLE BLOCKER) REQUIRED MAIN - [SDR FDEA202509091673](https://openairdocs.org/sdr/FDEA202509091673), Sep 9, 2025: FLOORBEAM. CORRODED. MAIN DECK CABIN FLOORBEAM A STA.1680 HAS POSSIBLE SIGN OF CORROSION. ACCOMPLISHED REPAIRS ON FINAL E.A. #F5310-T0384709 COMPLIED WITH FUSE. MAINFRAME- REPAIR OF - [SDR FDEA202509071640](https://openairdocs.org/sdr/FDEA202509071640), Sep 7, 2025: FITTING. CRACKED. WHILE ACCOMPLISHING F-5730-E034006 P13 OPEN HOLE INSPECTION OF THE #1 ENGINE DRAG LINK FITTING HOLE #13 HAS CRACKIN SKIN WORK ACCOMPLISHED ON FINAL EA 3F-5730-T - [SDR FDEA202509071639](https://openairdocs.org/sdr/FDEA202509071639), Sep 7, 2025: FITTING. CRACKED. WHILE ACCOMPLISHING F-5730-E034006 P14 OPEN HOLE INSPECTION OF THE #2 ENGINE DRAG LINK FITTING HOLE #4 HAS CRACK IN FITTING LAYER. WORK ACCOMPLISHED ON FINAL EA - [SDR FDEA202509071638](https://openairdocs.org/sdr/FDEA202509071638), Sep 7, 2025: FITTING. CRACKED. WHILE ACCOMPLISHING F-5730-E034006 P14 OPEN HOLE INSEPCTION OF THE #2 ENGINE DRAG LINK FITTING HOLE #2 HAS CRACKED IN SKIN. WORK ACCOMPLISHED ON FINAL EA #F-573 - [SDR FDEA202509071637](https://openairdocs.org/sdr/FDEA202509071637), Sep 7, 2025: FITTING. CRACKED. WHILE ACCOMPLISHING F-5730-E034006 P14 OPEN HOLE INSPECTION OF THE #2 ENGINE DRAG LINK FITTING HOLE #8 HAS CRACKIN SKIN/FITTING. WORK ACCOMPLISHED ON FINAL EA#F - [SDR FDEA202509031615](https://openairdocs.org/sdr/FDEA202509031615), Sep 3, 2025: SWITCH. FAILED. EMERGENCY TEST LIGHT SWITH INOP REMOVED AND REPLACED EMERGENCY LIGHT SWITCH IAW SWPM 20-84-18, OPS CHECK IAW B757 AMM 33-51-00-5 TEST GOOD. - [SDR FDEA202508281559](https://openairdocs.org/sdr/FDEA202508281559), Aug 28, 2025: SEAT TRACK. CORRODED. MAIN DECK CABIN RBL 58.22 SEAT TRACK FROM STA 1560 TO 1620 HAS CORROSION I/B - OTBD. REMOVED AND REPLACED WITH NEW SEAT TRACK AT RBL 58, STA 1420 - 1620 IAW SRM - [SDR FDEA202508281558](https://openairdocs.org/sdr/FDEA202508281558), Aug 28, 2025: ANGLE. CORRODED. FLIGHT DECK, AFT LT CORNER BROWN PAINT AREA, VERTICAL WALL ANGLE CORRODED 3 AREAS, AT FLOOR LEVEL. REMOVED, FABRICATED, INSTALLED FLIGHT DECK, AFT LT CORNER ANG - [SDR FDEA202508221528](https://openairdocs.org/sdr/FDEA202508221528), Aug 22, 2025: CHANNEL. CORRODED. COURIER AREA FLOOR STRUCTURE AFT LH CORNER "Z" CHANNEL AT AFT DRAIN FOR L1 DOOR CORRODED. INSTALLED FABRICATED CHANNEL AT COURIER AREA FLOOR STRUCTURE AFT LOWER - [SDR FDEA202508221527](https://openairdocs.org/sdr/FDEA202508221527), Aug 22, 2025: CREASE BEAM. CORRODED. MAIN DECK CABIN RBL 64.20 SUPPORT FLOOR FROM STA 1540 TO 1620 HAS CORROSION. REPAIRED FLOOR SUPPORT CREASE BEAM AT MAIN CABIN STA 1540 TO 1620 RBL 64.20 IAW SRM - [SDR FDEA202508191505](https://openairdocs.org/sdr/FDEA202508191505), Aug 19, 2025: FLOORBOARD. DAMAGED. MAIN CARGO COMPT ZONE 230 FLOORBOARD PANEL 231 MTF DAMAGED. FABRICATED MAIN CARGO COMPT. ZONE 230 FLOORBOARD 231 MTF VTMAE ON TRAVELER # T25/1826241 IAW DWG 118 - [SDR FDEA202508191504](https://openairdocs.org/sdr/FDEA202508191504), Aug 19, 2025: FLOORBOARD. DELAMINATED. MAIN DECK CABIN AFT R/H STA 1681 PNL 252MWF DELAMINATED. FABRICATED MAIN CARGO COMPT. ZONE 250 FLOORBOARD 252MWF VTMAE ON TRAVELER # T25/1826237 IAW DWG 1186418 - [SDR FDEA202502110217](https://openairdocs.org/sdr/FDEA202502110217), Feb 11, 2025: LAMP. FAILED. EMERGENCY PANEL DISCHARGE LIGHT INOP. SWPM: 20-84-18 REPLACED LIGHT ASSEMBLY. PER SWPM 20-84-18. OPS CHECKS GOOD. - [SDR FDEA202406090786](https://openairdocs.org/sdr/FDEA202406090786), Jun 9, 2024: GUST LOCK. DAMAGED. L1 GUST LOCK STUCK UP AND WILL NOT LOCK DOOR IN PLACE. REMOVED AND REPLACED L1 DOOR GUST LOCK PER ABOVE REFERENCE. OPS CHK GOOD. A/C OK FOR SERVICE. - [SDR FDEA202404200482](https://openairdocs.org/sdr/FDEA202404200482), Apr 20, 2024: COLLAR. FAILED. WHILE DOWN-POWERING THE AIRCRAFT FOR LAYOVER, DISCOVERED THE L1 DOOR HOLD-OPEN LOCK COLLAR BROKEN. AMM: 52-11-08-4 R/R L1 HOLD OPEN LOCK IN REF TO ABOVE. A/C OK - [SDR FDEA202310031695](https://openairdocs.org/sdr/FDEA202310031695), Oct 3, 2023: SKIN. CRACKED. #2 PYLON AFT LOWER HEAT SHIELD SKIN IS CRACKED @ APPROX. PPS 295 REMOVED #2 PYLON AFT LOWER HEAT SHIELD AND INSTALLED NEW HEAT SHIELD P/N 313N5042-11 PER BAC DW - [SDR FDEA202310031690](https://openairdocs.org/sdr/FDEA202310031690), Oct 3, 2023: HEAT SHIELD. CRACKED. #2 PYLON AFT HEAT SHIELD SKIN @ APPROX. PPS 285 IS CRACKED. REPAIRED #2 PYLON AFT HEAT SHIELD SKIN PER FEDEX EA F-5480-T0376253 TITLE: NACELLES/PYLON - FILLETS/ - [SDR FDEA202309281668](https://openairdocs.org/sdr/FDEA202309281668), Sep 28, 2023: LOUVER. CRACKED. #1 PYLON LOUVERED PRE-COOLER PANEL R33CL IS CRACKED. ACCOMPLISH WELD REPAIR ON PANEL PER FEDEX EA # F-5450-T0376289 P1 TITLE: NACELLES/PYLON - WINGS PYLON/STRUT - [SDR FDEA202309271661](https://openairdocs.org/sdr/FDEA202309271661), Sep 27, 2023: SPLICE. CORRODED. MAIN CABIN STA 1070, LH CUSP AREA, FITTING EXFOLIATED NEAR FRAME REMOVED AND REPLACED SPLICE FITTING IAW B757 DWG 144N5340 REV A. PART FABRICATED ON NR N00218. - [SDR FDEA202309271660](https://openairdocs.org/sdr/FDEA202309271660), Sep 27, 2023: COMPRESSOR. DELAMINATED. #1 ENG RH SIDE TEFLON SLEEVE (KEVLAR PROTECTIVE COATING) HAS SEPERATION OF THE EDGES ON THE COVERING OT THE COMPRESSOR CASING BETWEEN 5 AND 6 O'CLOCK POSITIONS. - [SDR FDEA202309271659](https://openairdocs.org/sdr/FDEA202309271659), Sep 27, 2023: COMPRESSOR. TORN. #1 ENG RH SIDE TEFLON SLEEVE (KEVLAR PROTECTIVE COATING) TORN BETWEEN 5 AND 6 O'CLOCK POSITIONS ACCOMPLISHED PERMANENT REPAIR ON #1 ENG RH SIDE TEFLON SLEEVE BE - [SDR FDEA202309251645](https://openairdocs.org/sdr/FDEA202309251645), Sep 25, 2023: FLAP. CHAFED. LEFT WING I/B MAIN FLAP LOWER SURFACE AT MLG AFT TRUNNION FAIRING CONTACT HAS CHAFFING WEAR MARKS. EVALUATED L/W I/B MAIN FLAP LE LOWER SURFACE CHAFFED AND FOUN - [SDR FDEA202309201628](https://openairdocs.org/sdr/FDEA202309201628), Sep 20, 2023: PANEL. CRACKED. RIGHT HORIZONTAL PANEL 345BB CRACKED. EVALED PANEL CRACK FOUND TO BE IN TEDLAR ONLY, NO COMPOSITE DAMAGE NOTED, NO REPAIR REQUIRED IAW B757 SRM 55-10-01-1A, 55- - [SDR FDEA202309201627](https://openairdocs.org/sdr/FDEA202309201627), Sep 20, 2023: PANEL. CRACKED. LH HORIZONTAL T/E PANEL 335BB CRACKED. ACCOMPLISHED PERMANENT REPAIR TO LEFT HORIZONTAL T/E PANEL 335BB IAW FEDEX B757 SRM 55-10-01-1A, 51-70-05-0G,55-10-01-2R - [SDR FDEA202111142856](https://openairdocs.org/sdr/FDEA202111142856), Nov 14, 2021: FLOOR PANEL. DELAMINATED. COURIER AREA FLOOR BOARD 222MAF DELAMINATED. FABRICATED FLOOR BOARD 222MAF ON VTMAE TRAVELER # T21/1581211 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR. - [SDR FDEA202111142855](https://openairdocs.org/sdr/FDEA202111142855), Nov 14, 2021: FLOOR PANEL. DELAMINATED. COURIER AREA FLOOR BOARD 222AF DELAMINATED. FABRICATED FLOOR BOARD 222AF ON VTMAE TRAVELER #T21/1581209 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR. - [SDR FDEA202111142854](https://openairdocs.org/sdr/FDEA202111142854), Nov 14, 2021: FLOOR PANEL. DELAMINATED. COURIER AREA FLOOR BOARD 221AF DELAMINATED. FABRICATED FLOOR BOARD 221AF ON VTMAE TRAVELER # T21/1581201 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR. - [SDR FDEA202111142853](https://openairdocs.org/sdr/FDEA202111142853), Nov 14, 2021: FLOOR PANEL. DELAMINATED. COURIER AREA FLOOR BOARD 221MBF DELAMINATED. FABRICATED FLOOR BOARD 221MBF ON VTMAE TRAVELER #T21/1581231 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR. - [SDR FDEA202111142852](https://openairdocs.org/sdr/FDEA202111142852), Nov 14, 2021: FLOOR PANEL. DELAMINATED. COURIER AREA FLOOR BOARD 221BF DELAMINATED. FABRICATED FLOOR BOARD 221BF ON VTMAE TRAVELER #T21/1581218 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR. - [SDR FDEA202111112822](https://openairdocs.org/sdr/FDEA202111112822), Nov 11, 2021: FLOOR PANEL. DAMAGED. FLOOR PANEL 241MQF DAMAGED AT FWD RIGHT HAND CORNER. FABRICATED ZONE 240 FLOOR BOARD 241MQF ON VT MAE TRAVELER T21/1582439 IAW DWG SRZ-25-005 REVISION R. MAJOR - [SDR FDEA202111112820](https://openairdocs.org/sdr/FDEA202111112820), Nov 11, 2021: NONE. DAMAGED. FLOOR PANEL 242MFF DAMAGED. FABRICATED ZONE 240 FLOOR BOARD 242MFF ON VT MAE TRAVELER T21/1582446 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIR - [SDR FDEA202111102813](https://openairdocs.org/sdr/FDEA202111102813), Nov 10, 2021: NONE. DAMAGED. FLOOR PANEL 241MEF IS DAMAGED ON RIGHT FWD CORNER. FABRICATED ZONE 240 FLOOR BOARD 241MEF ON VT MAE TRAVELER T21/1582438 IAW DWG SRZ- 25-005 REV R. MAJOR REPAIR - [SDR FDEA2019062411403](https://openairdocs.org/sdr/FDEA2019062411403), Jun 21, 2019: BATTERY. INOPERATIVE. DURING PRE-FLIGHT, CREW REPORTED AN ODOR SOMETHING LIKE SMOKE IN THE COCKPIT. RELEASED FOR SERVICE APU BATTERY INOPERATIVE. APU INOPERATIVE. SWAPPED APU BATTERY - [SDR FDEA2019060311193](https://openairdocs.org/sdr/FDEA2019060311193), May 31, 2019: GCU. FAULTED. PDIS 914 24-20 9178 30MAY19 MNL OPEN U LOGPAGES:2951455 DURING DESCENT INTO RPLL, THE FOLLOWING EICAS INDICATIONS DISPLAYED: R GEN, R BUS, R UTILITY BUS, R EEC. - [SDR FDEA201711083206](https://openairdocs.org/sdr/FDEA201711083206), Nov 8, 2017: FRAME. CRACKED. MAIN CABIN FRAME (STUBFRAME) CRACKED AT UPPER RADIUS STA 580 LBL 44.5. REMOVED AND REPLACED IAW DWG 657N4311, REV-. - [SDR FDEA201711083197](https://openairdocs.org/sdr/FDEA201711083197), Nov 8, 2017: FRAME. GOUGED. FRAME REPAIR GOUGED AT FWD ACCESSORY BAY ENTRY FWD FRAME BS 231 BL 0. REMOVED AREA OF DAMAGE. REMOVED AND FABRICATED A NEW REPAIR ANGLE AND FILLER IAW SRM 53-00 - [SDR FDEA201610033471](https://openairdocs.org/sdr/FDEA201610033471), Oct 3, 2016: INSERT. MISSING. DURING FIRST OFFICER`S PREFLIGHT, NOTICED PART OF RIGHT ENTRY DOOR HANDLE MISSING. REPLACED THE DOOR HANDLE INSERT, IAW MM 52-11-02-4. OPS CHECKED NORMAL. - [SDR FDEA201510283401](https://openairdocs.org/sdr/FDEA201510283401), Oct 28, 2015: ANGLE. GOUGED. MAIN CABIN STATION 324, RBL 62, ANGLE GOUGED AT EDGE FWD INBD SIDE. REMOVED ANGLE, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04-1A DETAIL IV. FABRICATED NEW ANGLE - [SDR FDEA201510283398](https://openairdocs.org/sdr/FDEA201510283398), Oct 28, 2015: WEB. GOUGED. MAIN CABIN, BETWEEN STATION 310 - 324, RBL 62, WEB GOUGED AT EDGE FWD INBD SIDE. REMOVED EB FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04-1A DETAIL I. FABRICATED W - [SDR FDEA201510223314](https://openairdocs.org/sdr/FDEA201510223314), Oct 22, 2015: SEAT TRACK. CORRODED. MAIN CABIN STATION 365 TO 337, SEAT TRACK FLANGES HAS CORROSION, RBL 31.5. REMOVED CORROSION IAW SRM 51-10-02. EVALUATED AREAS OUT OF LIMITS, FABRICATED TWO EAC - [SDR FDEA201510223313](https://openairdocs.org/sdr/FDEA201510223313), Oct 22, 2015: FILLER. CORRODED. MAIN CABIN STATION 376, LBL 9, FLOORBEAM SUPPORT HAS CORROSION. REMOVED CORROSION ON 3471-79 FILLER IAW SRM 51-10-0. REWORKED ON THE FILLER IS STRUCTURALLY ACCE - [SDR FDEA201510213298](https://openairdocs.org/sdr/FDEA201510213298), Oct 21, 2015: FLOORBEAM. CORRODED. MAIN CABIN STATION 377, BETWEEN LBL 19 & LBL 36, FLOORBEAM HAS CORROSION. REMOVED CORROSION ON FLOORBEAM IAW SRM 51-10-02. EVALUATED NO LIMITS FOR CORROSION REM - [SDR FDEA201510183274](https://openairdocs.org/sdr/FDEA201510183274), Oct 18, 2015: FLOOR SUPPORT. CRACKED. MAIN CABIN APPROX STATION 1678, BL0, FLOOR SUPPORT CRACKED AT NUTPLATE HOLE. - [SDR FDEA201510173267](https://openairdocs.org/sdr/FDEA201510173267), Oct 17, 2015: SHEAR WEB. CORRODED. MAIN CABIN SHEAR WEB HAS CORROSION, BS 1684 TO 1700, RBL 5 - RBL 8. REMOVED CORROSION IN AREA AT MAIN CABIN SHEAR WEB, EVALUATED AREA ORIGINAL MAT .071", REM MA - [SDR FDEA201510163263](https://openairdocs.org/sdr/FDEA201510163263), Oct 16, 2015: SKIN. DAMAGED. RIGHT WING AILERON, OTBD UPPER SURFACE HAS LIGHTNING STRIKE DAMAGE. REMOVED, FABRICATED & INSTALLED CONDUCTIVE FRAME ON RT AILERON ASSEMBLY, NO DAMAGE FOUND ON - [SDR FDEA201510163258](https://openairdocs.org/sdr/FDEA201510163258), Oct 16, 2015: FLOORBEAM. CORRODED. MAIN CABIN STATION 324 FLOORBEAM HAS CORROSION, RBL 54 TO RBL 64. REMOVED CORROSION IAW SRM 51-10-02, EVALUATED NO LIMITS FOR CORROSION REMOVAL ON PREVIOUS REPA - [SDR FDEA201510163257](https://openairdocs.org/sdr/FDEA201510163257), Oct 16, 2015: SKIN. DENTED. FUSELAGE HAS 2 EACH DENTS, STATION 1612, JUST BELOW STRINGER 26L LAP JOINT. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01-1A DETAIL III. CUT OUT DAMAGED AREA, FABR - [SDR FDEA201510143207](https://openairdocs.org/sdr/FDEA201510143207), Oct 14, 2015: FLOORBEAM. CORRODED. MAIN CABIN FLOORBEAM HAS CORROSION STATION 365, RBL 56. REMOVED CORROSION IAW SRM 51-10-02, EVALUATED AREA OUT OF LIMITS FOR CORROSION ON PREVIOUS REPAIR. REMOV - [SDR FDEA201510103162](https://openairdocs.org/sdr/FDEA201510103162), Oct 10, 2015: DOOR FRAME. DAMAGED. FORWARD E & E BAY DOOR CUT OUT BS 231, FRAME DENTED & GOUGED AT BL 0. REMOVED DAMAGE IAW EA F-5310-T0320728 P1. FABRICATED REPAIR PART IAW EA F-5310-T0320728 P1 All 168: https://openairdocs.org/aircraft/N914FD/reports.md ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Boeing 757-28A aircraft: https://openairdocs.org/model/boeing-757-28a/aircraft.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.