# N936FD: 1985 Boeing 757-2T7 - Status: Valid registration - Airframe: [Boeing 757-2T7](https://openairdocs.org/model/boeing-757-2t7) (registry code 138491A, 239 seats) - Serial number: 23293 - Year built: 1985 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 5, 2010 - Certificate issued: December 2, 2008 - Expires: February 28, 2029 - Mode S code: ACFC74 - 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=936FD - Page: https://openairdocs.org/aircraft/N936FD 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 757-2T7) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N936FD. ## FAA accident and incident reports None matched to N936FD. ## Service difficulty reports (229, 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 FDEA202312141942](https://openairdocs.org/sdr/FDEA202312141942), Dec 14, 2023: COUPLING. DAMAGED. AT CRUIRE AT FL 340 HAD A LT ENGINE FIRE (L ENG FIRE) AND OVERHEAT (L ENG OVERHEAT) INDICTION ON EICAS , LT FIRE HANDLE AND LEFT CONTOL LEVER. NO UNUSUAL LT ENG - [SDR FDEA202311161857](https://openairdocs.org/sdr/FDEA202311161857), Nov 16, 2023: FLEX LINE. LEAKING. IN SHORT FINAL AFTER FULLY CONFIGURED, L HYD SYS PRESS EICAS CAME ON. LANDED WITH ROLL TO RIGHT, NO NOSE WHEEL STEERING. FACT 15NOV23 23:59 MEM U AMM: 20-10-10- - [SDR FDEA202309141597](https://openairdocs.org/sdr/FDEA202309141597), Sep 14, 2023: SKIN. DAMAGED. DURING DVI INSPECTION OF L/E SKIN REPAIR ON #3 SLAT ON HECO CARD 9019, FOUND 2 BLIND FASTENERS THAT WERE LOOSE AND LOCKING PINS WERE NOT FLUSH WITH THE FASTENER - [SDR FDEA202309131593](https://openairdocs.org/sdr/FDEA202309131593), Sep 13, 2023: SKIN. CORRODED. #1 PYLON PANEL 433HR HAS CORROSION ON AFT SURFACE OF THE PANEL FABRICATED NEW PANEL PER BAC DWG 311N5049 REV C AND FEDEX EA # F-5430-T0376029 TITLE: NACELLS/PYL - [SDR FDEA202309131592](https://openairdocs.org/sdr/FDEA202309131592), Sep 13, 2023: COMPRESSOR. LOOSE. #1 ENG FAN CASE AREA PROTECTIVE PLASTIC COVER FOR KEVLAR SEPERATING FROM COMPRESSOR CASING AT FWD EDGE SEVERAL PLACES REPAIRED #1 ENGINE LP COMPRESSOR CASE TEFL - [SDR FDEA202309131591](https://openairdocs.org/sdr/FDEA202309131591), Sep 13, 2023: COMPRESSOR. TORN. #2 ENGINE LP COMPRESSOR CASE KEVLAR WRAPPING FWD EDGE, PROTECTIVE PLASTIC COVER TORN AT 4 O'CLOCK POSITION. REPAIRED #2 ENGINE LP COMPRESSOR CASE TEFLON SLEEVE - [SDR FDEA202309131590](https://openairdocs.org/sdr/FDEA202309131590), Sep 13, 2023: COMPRESSOR. LOOSE. #2 ENG LP COMPRESSOR CASE KEVLAR WRAPPING PROTECTIVE PLASTIC COVER, SEVERAL REPAIRS PATCHTAPE PEELING OFF. REPAIRED #2 ENGINE LP COMPRESSOR CASE TEFLON SLEEVE W - [SDR FDEA202309111572](https://openairdocs.org/sdr/FDEA202309111572), Sep 11, 2023: ATTACH ANGLE. CRACKED. LOWER FRAME ATTACH CLIP IS CRACKED IN LH MLG WHEEL WELL, ON AFT SIDE OF FRAME @ APPROX. STA 1064 LBL 30 REMOVED AND REPLACED CRACKED CLIP WITH NEW CLIP P/N 654N - [SDR FDEA202309101570](https://openairdocs.org/sdr/FDEA202309101570), Sep 10, 2023: FLOOR SUPPORT. CRACKED. AFT PIT CARGO COMPARTMENT FLOOR STRINGER HAS A CRACK ON STA 1340 RBL 7.55 REPAIRED AFT PIT CARGO COMPARTMENT FLOOR STRINGER STA 1340 RBL 7.55 IAW B757 SRM 53-00 - [SDR FDEA202309031543](https://openairdocs.org/sdr/FDEA202309031543), Sep 3, 2023: SLAT. DELAMINATED. DISBOND INDICATION FOUND 5" OUTBOARD ON TOP SIDE OF SLAT #2 T/E WEDGE. REPAIRED #2 SLAT T/E WEDGE BY REMOVING DAMAGED AREA OS UPPER SKIN LOCATED 5.5" FROM I/B E - [SDR FDEA202309031542](https://openairdocs.org/sdr/FDEA202309031542), Sep 3, 2023: SLAT. DELAMINATED. DISBOND INDICATION FOUND 93" OUTBOARD ON TOP SIDE OF SLAT #3 T/E WEDGE. REPAIRED #3 SALT T/E WEDGE UPPER SKIN DISBONDED AREA 93" FROM I/B END, 5375 FROM T/E IAW - [SDR FDEA202309031541](https://openairdocs.org/sdr/FDEA202309031541), Sep 3, 2023: SLAT. DELAMINATED. DISBOND INDICATION FOUND 67" OUTBOARD ON TOP SIDE OF #3 TE WEDGE. REPAIRED #3 SLAT T/E UPPER SKIN DISBOND 67.5 FROM I/B END, 6.25" FROM T/E IAW B757 SRM 57- 43- - [SDR FDEA202308291538](https://openairdocs.org/sdr/FDEA202308291538), Aug 29, 2023: PANEL. CRACKED. L.WING L/E PANEL 521AB HAS A CRACK AT THE EDGE OF THE PANEL EVALUATED, CLEANED, SANDED, REMOVED DAMAGE, ON L/E PANEL 521AB AND REPAIRED IAW B757 SRM 57-41-01-2R - [SDR FDEA202303010354](https://openairdocs.org/sdr/FDEA202303010354), Mar 1, 2023: GUIDE ARM. FAILED. ENTRY DOOR WILL NOT CLOSE PROPERLY. APPEARS A HINGE IS NOT ALIGNED CORRECTLY. COMPLETED INSTALL OF L1 ENTRY DOOR GUIDE ARM. ALL ADJUSTMENTS AND OPS CHECKS GOOD. - [SDR FDEA202302220333](https://openairdocs.org/sdr/FDEA202302220333), Feb 22, 2023: NONE. NONE. PDIS 936 27-50 1303 22FEB23 MSP FACT U TE FLAP DISAGREE BETWEEN 5-15. RAN QRH AND LANDED MSP. ***EMERGENCY DECLARED*** FACT 22FEB23 13:11 MSP U FIM: 21-51-00-81 - [SDR FDEA202110252611](https://openairdocs.org/sdr/FDEA202110252611), Oct 25, 2021: FRAME. UNKNOWN. COMPLY WITH EA FOR FRAME REPAIR STA. 1640 RH COMPLIED WITH EA #T F-5310-138502E P9 EA TITLE FUSELAGE-MAINFRAME-EXISTING FRAME REPAIR OF BS 1640, WL 208.10 RIGHT - [SDR FDEA202110212587](https://openairdocs.org/sdr/FDEA202110212587), Oct 21, 2021: NONE. CRACKED. CRACKED FLOOR BEAM @ STA. 580,LBL 45. REPAIRED FLOOR BEAM AT STA 580 LBL 45 PER E.A. # F-5310-T0364468 P1 AND SR DRAWING # 57-53-004 E.A. TITLE FUSELAGE-MAINFRA - [SDR FDEA202110152541](https://openairdocs.org/sdr/FDEA202110152541), Oct 15, 2021: SEAT TRACK. CRACKED. SEAT TRACK AT STA 580, LBL 45, FLANGE HAS A CRACK. REPAIRED SEAT TRACK LBL45 AT STA 530 - 680 IAW EA# F-5321-T0364473, FUSELAGE - CARGO FLOOR - SECTION 43 - MCD - [SDR FDEA202110082498](https://openairdocs.org/sdr/FDEA202110082498), Oct 8, 2021: NONE. DAMAGED. ZONE 220 FLOOR BOARD 222MDF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MDF ON VT MAE TRAVELER T21/1575353 IAW DWG SRZ 25-005 REVISION R. MAJOR REPAIR - [SDR FDEA202110082497](https://openairdocs.org/sdr/FDEA202110082497), Oct 8, 2021: NONE. DAMAGED. EDGE DAMAGE NOTED ON FLOOR PANEL 242MEF BOTTOM SIDE. FABRICATED FLOOR BOARD 242MEF ON VT MAE TRAVELER T21/1577548 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR - [SDR FDEA202110082496](https://openairdocs.org/sdr/FDEA202110082496), Oct 8, 2021: NONE. DAMAGED. ZONE 220 FLOOR BOARD 222MAF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MAF ON VT MAE TRAVELER T21/1575476 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIR - [SDR FDEA202110082495](https://openairdocs.org/sdr/FDEA202110082495), Oct 8, 2021: NONE. DAMAGED. ZONE 220 FLOOR BOARD 221MBF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221MBF ON VT MAE TRAVELER T21/1575357 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR - [SDR FDEA202110082494](https://openairdocs.org/sdr/FDEA202110082494), Oct 8, 2021: NONE. DAMAGED. ZONE 220 FLOOR BOARD 222MEF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MEF ON VT MAE TRAVELER T21/1575352 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR - [SDR FDEA202110082493](https://openairdocs.org/sdr/FDEA202110082493), Oct 8, 2021: NONE. DAMAGED. ZONE 220 FLOOR BOARD 221AF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VT MAE TRAVELER T21/1575471 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIR - [SDR FDEA202110082492](https://openairdocs.org/sdr/FDEA202110082492), Oct 8, 2021: NONE. DAMAGED. ZONE 220 FLOOR BOARD 222BF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222BF ON VT MAE TRAVELER T21/1575359 IAW DWG SRZ- 25-005 REVISION R MAJOR REPAIR - [SDR FDEA202101090028](https://openairdocs.org/sdr/FDEA202101090028), Jan 9, 2021: INDICATOR. NO INDICATION. PRE-DEPARTURE UNABLE TO ARM L1 DOOR. NO SLIDE LIGHT. COMPLIED WITH INSPECTION & TEST OF GIRT BAR HANDING MECHANISM IAW MM 25-66-10-2. ALL CHECKED NORMAL . ARM L - [SDR FDEA202011252964](https://openairdocs.org/sdr/FDEA202011252964), Nov 25, 2020: TRANSMISSION. TRIPPED. TRAILING EDGE FLAP DISAGREE BETWEEN 20&25 W/FLAP HANDLE IN 25 DETENT. COMPLIED W/QRH EMERGENCY DECLARED. ACCOMPLISHED FIM 27-51-00-815-808 FIG 105. FOUND RT INB - [SDR FDEA201910112605](https://openairdocs.org/sdr/FDEA201910112605), Oct 11, 2019: CUSP WEB. CORRODED. MAIN CARGO AREA STA 1450 RH CUSP WEB CORRODED. REMOVED,FABRICATED AND INSTALLED NEW CUSP WEB IAW DWG 146N5590. - [SDR FDEA201910112604](https://openairdocs.org/sdr/FDEA201910112604), Oct 11, 2019: SKIN. DENTED. EXTERIOR FUSELAGE SKIN DENTED AT STA 408 BETWEEN STRINGER 10L AND 11L REPAIRED PER EA# F-5310-T0349762-P1 - [SDR FDEA201910112592](https://openairdocs.org/sdr/FDEA201910112592), Oct 11, 2019: SKIN. DENTED. LOWER AFT CARGO FUSELAGE AT BS 1635 BETWEEN STR27R AND 28R HAS PITTING CORROSION ON INTERNAL SURFACE ACOMPLISHED WORK IAW EA F-5310-T0349844 - [SDR FDEA2019101102590](https://openairdocs.org/sdr/FDEA2019101102590), Oct 10, 2019: SLAT TRACK. CORRODED. LEFT WING #3 SLAT INBD TRACK WORN AND PITTED. REMOVED AND REPLACED #3 SLAT IB MAINTRACK REF B757 AMM 27-81-12-4. ADJUSTMENT OF #3 TRACK IS ACCOMPLISHED ON NR N0 - [SDR FDEA2019101102584](https://openairdocs.org/sdr/FDEA2019101102584), Oct 10, 2019: ATTACH ANGLE. CORRODED. L/W L/E PNL ATTACH STRUCTURE AT STA 532 HAS INTERGRANULAR CORROSION REMOVED AND REPLACED ANGLE PER B757 SRM 51-40-02 AND DWG #114N2151 - [SDR FDEA2019101102583](https://openairdocs.org/sdr/FDEA2019101102583), Oct 10, 2019: ATTACH ANGLE. CORRODED. LEFT WING L/E PANEL ATTACH ANGLE AT WS 478 HAD INTERGRANULAR CORROSION. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-40-02, AND DWG 114N2151. - [SDR FDEA201910092528](https://openairdocs.org/sdr/FDEA201910092528), Oct 9, 2019: SKIN. CORRODED. LT WING NR 3 SLAT LEADING EDGE IS CORRODED APPROXIMATELY 32 IN OUTBOARD OF THE INBOARD EDGE IN THE UNPAINTED SURFACE. REPAIRED PER B757 SRM 57-43-01-2R. - [SDR FDEA2019101092528](https://openairdocs.org/sdr/FDEA2019101092528), Oct 9, 2019: SKIN. CORRODED. LEFT WING NR 3 SLAT L/E WAS CORRODED APPROX 32 INCHES OTBD OF THE INBD EDGE IN THE UNPAINTED SURFACE. REPAIRED THE SLAT IAW SRM 57-43-01-2R. - [SDR FDEA2019101092536](https://openairdocs.org/sdr/FDEA2019101092536), Oct 9, 2019: GEAR. CORRODED. LEFT WING NR 4 SLAT OTBD TRACK DRIVE MOTOR SPROCKET TEETH PITTED. REMOVED AND REPLACED NR 4 SLAT OTBD ROTARY ACTUATOR SPROCKET IAW AMM 27-81-18-4. OPS CHECKED G - [SDR FDEA201910092538](https://openairdocs.org/sdr/FDEA201910092538), Oct 9, 2019: SPROCKET. CORRODED. LEFT WING NR 4 SLAT INBD TRACK DRIVE MOTOR SPROCKET TEETH PITTED. REMOVED AND REPLACED THE NR 4 SLAT INBD ROTARY ACTUATOR SPROCKET IAW AMM 57-81-18-4. OPS CHECK - [SDR FDEA2019101092537](https://openairdocs.org/sdr/FDEA2019101092537), Oct 9, 2019: SPROCKET. CORRODED. LEFT WING NR 3 SLAT INBD TRACK DRIVE MOTOR SPROCKET TEETH PITTED. REMOVED AND REPLACED NR 3 SLAT INBD ROTARY ACTUATOR SPROCKET IAW AMM 27-81-18-4. OPS CHECK GOO - [SDR FDEA2019101092533](https://openairdocs.org/sdr/FDEA2019101092533), Oct 9, 2019: SLAT TRACK. CORRODED. LEFT WING NR 3 SLAT OTBD TRACK WORN AND PITTED. REMOVED AND REPLACED THE NR 3 SLAT OTBD TRACK IAW AMM 27-81-12-4. OPS CHECKED GOOD IAW AMM 57-81, 81-18-4. - [SDR FDEA2019101092542](https://openairdocs.org/sdr/FDEA2019101092542), Oct 9, 2019: SPLICE. CORRODED. LEFT WING T/E OTBD PANEL SPLICE STRIP, JUST AFT OF THE AILERON WAS CORRODED. REMOVED AND REPLACED THE SPLICE STRIP IAW SRM 51-40-02, AND DWG 113N1640, REV B. - [SDR FDEA2019101092539](https://openairdocs.org/sdr/FDEA2019101092539), Oct 9, 2019: STRIKER. DELAMINATED. LMLG DOOR AFT UPSTOP PAD IS WORN. REMOVED AND REPLACED STRIKER PLATE IAW SRM 51-10-02, DWG 149N6002, AND SRM 51-70-06-0G. REMOVED DAMAGED PLIES AND BONDED REPAI - [SDR FDEA2019101092535](https://openairdocs.org/sdr/FDEA2019101092535), Oct 9, 2019: STRIKER. DELAMINATED. RIGHT MLG DOOR LOWER UPSTOP PAD HAD COMPOSITE MATERIAL DELAMINATION. REMOVED DAMAGE AND STRIKER PLATE, BONDED NEW POTTING AND REPAIR PLIES AND STRIKER PLATE IAW - [SDR FDEA2019101092532](https://openairdocs.org/sdr/FDEA2019101092532), Oct 9, 2019: SLAT TRACK. CORRODED. LEFT WING NR 4 SLAT INBD TRACK WORN AND PITTED. REMOVED AND REPLACED THE NR 4 SLAT INBOARD TRACK IAW AMM 27-81-12-4. ADJUSTMENT AND OPS CHECK ACCOMPLISHED ON SN - [SDR FDEA2019101092529](https://openairdocs.org/sdr/FDEA2019101092529), Oct 9, 2019: WEDGE. CORRODED. LEFT WING NR 5 SLAT LOWER T/E WEDGE WAS DELAMINATED AT THE INBD AFT CORNER. REPLACED THE SLAT. - [SDR FDEA2019101092527](https://openairdocs.org/sdr/FDEA2019101092527), Oct 9, 2019: ATTACH ANGLE. CORRODED. RIGHT WING NR 9 SLAT LOWER T/E WEDGE ATTACH ANGLE IS CORRODED AND THE T/E WEDGE WAS BULGING WITH FASTENERS PULLING THROUGH AT THREE LOCATIONS. REPLACED THE SLAT - [SDR FDEA2019101082502](https://openairdocs.org/sdr/FDEA2019101082502), Oct 8, 2019: SKIN. DENTED. APU COMPARTMENT RT DOOR OUTER SURFACE IS CREASED. REPAIRED APU RT DOOR OUTER SKIN IAW EA F-5240-T0349703. - [SDR FDEA2019101082501](https://openairdocs.org/sdr/FDEA2019101082501), Oct 8, 2019: SKIN. DENTED. APU COMPARTMENT LT DOOR OUTER SURFACE IS BULGED. REPAIRED APU DOOR OUTER SURFACE IAW EA F-5240-T0349685. - [SDR FDEA2019101082499](https://openairdocs.org/sdr/FDEA2019101082499), Oct 8, 2019: SKIN. DENTED. ETERIOR FUSELAGE SKIN IS DENTED AT APPROX BS 1630 ON STR17R. REMOVED EFECTED FASTENERS PREFORMED HFEC TO OPEN HOLES AND EFECTED AREA FOUND NO CRACKS. OVERSIZED - [SDR FDEA201908091828](https://openairdocs.org/sdr/FDEA201908091828), Aug 9, 2019: UNKNOWN. UNKNOWN. MOD TYPE T MOD NO. F-5730-T0348437 REV NO. PS P2 WINGS - PLATES AND SKINS - LH WING T.E. SKIN PANEL W BL 235 TO 300 - CRACKS AND COMPLY WITH E..A. F-5730-T03484 - [SDR FDEA201907081509](https://openairdocs.org/sdr/FDEA201907081509), Jul 8, 2019: BATTERY. DISCHARGED. DURING PRE-DEPARTURE CHECK, FOUND NUMEROUS EMERGENCY EXIT SIGNS AND R1 EXTERIOR LIGHT INOP. ATTEMPTED TO CHARGE EMERGENCY LIGHT BATTERIES USING SHIP'S POWER FOR All 229: https://openairdocs.org/aircraft/N936FD/reports.md ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Boeing 757-2T7 aircraft: https://openairdocs.org/model/boeing-757-2t7/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.