FEDERAL EXPRESS CORPORATION

Operated by FEDERAL EXPRESS CORP (per NTSB report)

Operated by FEDERAL EXPRESS CORP (per NTSB report)

Operated by FEDERAL EXPRESS CORP (per NTSB report)

Operated by FEDERAL EXPRESS CORP (per NTSB report)

Operated by Federal Express Corporation (per NTSB report)

Operated by Federal Express (per NTSB report)

Operated by Federal Express (per NTSB report)

Operated by Federal Express (per NTSB report)

Operated by FEDERAL EXPRESS CORP (per NTSB report)

Operated by FEDERAL EXPRESS CORP (per NTSB report)

Operated by FEDERAL EXPRESS CORP (per NTSB report)

Operated by FEDERAL EXPRESS CORP (per NTSB report)

Operated by FEDERAL EXPRESS CORPORATION (per NTSB report)

Operated by FEDERAL EXPRESS CORP (per NTSB report)

Operated by FEDERAL EXPRESS CORP (per NTSB report)

Operated by FEDERAL EXPRESS CORP (per NTSB report)

L1 DOOR ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT REMAINS ILLUMINTED WHEN SLIDE IS DISARMED. MEL 01JUL26 05:26 IND RELEASED FOR SERVICE PER MEL : 25-66-05-A CATEGORY : C EXPIRATION : 11JUL26 "MEL 25-66-05-A: L1 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS - INOP. VERIFY AND RECORD IN AML/EAML THAT ASSOCIATED SLIDE IS VISUALLY VERIFIED ENGAGED PRIOR TO EACH DEPARTURE." PER MEL 25-66-05-A, ENGAGEMENT OF ASSOCIATED SLIDE HAS BEEN VISUALLY VERIFIED. AC OK FOR SERVICE.

[MAIN DECK STUB FRAME IS CRACKED AT UPPER FLANGE AT 580 LBL 45.50 MAIN DECK STUB FRAME CRACKED AT UPPER FLANGE STA 580 LBL 45.50, 2026-07-01] ORG WRI 979 25-50 0563 MAIN CARGO DECK LEFT O/B SEAT TRACK DAMAGED AT STATION 579. LOCK ID B579. REPLACED SEGMENT USING E.A.#:F-5310-T0387768 PART: 1 (P1) TITLE: FUSELAGE - MAINFRAME - SEAT TRACK SPLICE REPAIR FROM STA 530 TO STA 610 AT LBL 45 ALONG WITH 757 SRM 53-00-52- 2R AND DRW 657N3399.

LH WING LOWER SURFACE (NEAR FOOTSTOOL FITTING) HAS SEVERAL WEAR MARKS. C/W EA 1-5730-T0387611

L1 DOOR ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT REMAINS ILLUMINTED WHEN SLIDE IS DISARMED. AMM: 25-66-11-2, AMM: 25-66-10-2, AMM: 25-66-01-6, RELEASED IMPEDED PROXIMITY SWITCH ON L1 DOOR GIRT BAR SYSTEM. L1 DOORSLIDE LIGHT NOW OPERATES NORMALLY.

DURING CURRENT DROP-IN VISIT IN IND, THE FLOOR BEAM SEGMENT AT STA 580 AND LBL 45 WAS FOUND CRACKED UNDER THE LBL 45 SEAT TRACK. CREATED EA E.A.#: F-5310-T0387857 TITLE: FUSELAGE - MAINFRAME - STA 580 AND LBL 45 STUB FLOOR BEAM CRACKED REPAIR PER DRAWING SR57-53-004 (FORM 8110-3 APPROVAL ATTACHED) - TRACKING EA PART 1 PROVIDES DOCUMENTATION OF THE REPAIR BEING PERFORMED PER FEDEX DRAWING SR57-53-004. PART 2 PROVIDES INSPECTIONS/TRACKING FOR REPAIR. THIS IS A CATEGORY B REPAIR. THIS IS A MAJOR REPAIR REPLACEMENT OF SEGMENT DONE ON NR 27 WO 92512

MAIN DECK CARGO COMPARTMENT,L/H FLOOR PANEL 231QFF HAS PUNCTURE DAMAGE. FABRICATED NEW FLOOR PANEL 231QFF, MPN: 143T5876-19, LBL 9.13 LBL 77.5, STA 654.22-784.22 IN REF.TO BOEING DWG 143T5876-19, AND SR67-53-009. THIS IS A MAJOR REPAIR.

PUNCTURE ON FLOOR PANEL 241AFF MDC FLOOR PANEL 241AFF MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94.

TWO PUNCTURES ON FLOOR PANEL 241WFF STA 1050, MDC FLOOR PANEL 241WFF STA 1050 MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025

PUNCTURE ON FLOOR PANEL 231NFF MDC FLOOR PANEL 231NFF MDC WAS REPAIRED IAW SRM 53-00-50-2R FIG 4-B FIG 201 SHEET 2 REV 94.

MAIN DECK CARGO COMPARTMENT, R/H OUTBD FLOOR PANEL 232NFF HAS PUNCTURE DAMAGE. FABRICATED NEW FLOOR PANEL 232NFF, RBL 86.5 - RBL 77.5, BS 654 22 - 675 IAW DWG 143T5876-20, AND SRM 67-53-009. PERFORMED. THIS IS A MAJOR REPAIR. FOR INSTALLATION OF THIS PANEL REFER TO WO# 92339, NR# 279.

MAIN DECK CARGO COMPARTMENT, L/H FLOOR PANEL 241KFFHAS PUNCTURE DAMAGE. JM10 FABRICATED NEW FLOOR PANEL 241KFF, MPN: 145T5876-8, LBL 77.5 - LBL 89.5, STA 821 - 933 IN REF. TO BOEING DWG 145T5876-8, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. FOR INSTALLATION OF THIS PANEL REFER TO WO# 92339 NR# 283.

R1 EMERGENCY LIGHT DOESN'T STAY ON FOR THE COMPLETE LIGHT TEST. L1 LIGHT NORMAL. AMM 33-51-07-2 REMOVED POWER SUPPLY BATTERY PACK, HAS POWER AT POWER SUPPLY, REPLACED BATTERY PACK, OPS NORMAL. OK TO CONTINUE.

MAIN DECK CARGO COMPARTMENT, CENTER FLOOR PANEL 251LFF HAS PUNCTURE DAMAGE. REPAIRED FLOOR PANEL 251LFF, RBL 11- LBL 11, BS 1263-1267 IAW SRM 53-00-50-2R, FIG 201, REPAIR 1 SHT 1, AND DWG 146T5869-127. THIS IS A MAJOR REPAIR. THIS FLOOR PANEL WAS REPAIRED ON AIRCRAFT.

MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 251BFF DENTED WITH DELAMINATION. JM11 REPAIRED FLOOR PANEL 251BFF, MPN: 146T5869-155, LBL 11- LBL 33, BS 1160-11166 IAW SRM 53-00-50-2R, FIG 201, REPAIR 1 SHT 1, AND DWG 146T5869-155. THIS IS A MAJOR REPAIR. THIS FLOOR PANEL WAS REPAIRED ON AIRCRAFT.

PUNCTURE ON FLOOR PANEL 232DFF MDC FLOOR PANEL 232DFF MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94. DEC 15/2025

RIGHT WING INB MAIN FLAP TRAILING EDGE OTBD SECTION, UPPER AND LOWER SURFACE SHOWS MULTIPLE DENTS APPLIED PERMANENT REPAIR AT UPPER AND LOWER SURFACE ON RH WING INBD MAIN FLAP TRAILING EDGE IAW SRM 57-53-01-2R REP 1, DETAIL I, FIG 201, SHEET 2 AND SRM 51-70-10- 2R, REP 4.

PUNCTURED FLOOR PANEL 252MFF FLOOR PANEL 252MFF WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025.

PUNCTURED FLOOR PANEL 242UFF MDC FLOOR PANEL 242UFF MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025

PUNCTURED (2E/A) FLOOR PANEL 241WFF, BS 1000. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV 94 DEC 15/2025

PUNCTURED ON FLOOR PANEL241JFF BS 933. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4-B, FIG 201, SHEET 2, REV 94 DEC 15/2025

PUNCTURED (5 E/A) FLOOR PANEL 242VFF, BS 1000, THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R P R 4-B, FIG 201, SHEET 2, REV 94 DEC 15/2025.

FSS DISPLAY SHOWS UNARMED STATUS WHILE INFLIGHT. AMM: 26-90-03-2 EA: H-2624-T0387831 C/W E.A. H-2624-T0387831 TO RE-PIN D2166D PIN G8 TO F8. REACTIVATED FSS SYSTEM PER AMM REF ABOVE. CLOSED ALL DOORS AND SYSTEM PASSED AUTO ARM. NO FURTHER DEFECTS NOTED. PLACARD REMOVED. THIS ACTION CLEARS MEL.

EXISTING REPAIR ON HORIZONTAL PRESSURE DECK UPPER SURFACE BETWEEN FR51-FR52,Y0~- Y450 REQUIRES EVALUATION FOR CONFORMITY.

EXISTING REPAIR ON FUSELAGE FRAME FR0 BETWEEN 8-9 O'CLOCK REQUIRES EVALUATION FOR CONFORMITY.

AFTER LOWERING MLG THERE WAS A DISTINCT ELECTRICAL BURNING ODOR. EXPERIENCED THIS ABOUT 2 WEEKS AGO ON THIS SAME ACFT. AMM 32-61-00-5 PINNED GEAR & CYCLED GEAR HANDLE WITH HYD APPLIED. ALL INDICATIONS NORMAL IAW AMM, NO ODOR OF OZONE PRESENT. INSPECTED BEHIND CAPT & FOS INSTRUMENT PANEL TO INCLUDE MLG SELECTOR, NO ODORS OR DAMAGED WIRING NOTED. PERFORMED GVI OF AREAS: ALL C/BS & BEHIND ALL C/B PANELS IN FLT DECK, MAIN A/C BATTERY & CHARGER & ASSOCIATED WIRING, ALL PANELS IN E & E FOR OPEN BREAKERS & BEHIND PANELS FOR ANY PRESENCE OF OZONE OR DAMAGED WIRING. NO OPEN BREAKERS OR DAMAGED WIRING FOUND ON ACFT. NO ODOR OF OZONE PRESENT DURING INSPECTION PROCESS IAW CREW DEBRIEF THERE WERE NO ANOMALIES OF ANY SYS DURING EVENT. ACFT OK FOR SERVICE.

RT ENTRY DOOR SLIDE WILL NOT ARM. RELEASED FOR SERVICE PER MEL : 52-11-01-A. R1 DOOR OR SLIDE INOP. ADJUSTED R1 DOOR GIRT BAR REF AMM 25-66-10-2. OPS CHECKED GOOD.

EXISTING REPAIR ON MAIN DECK CROSSBEAM FR20,Y1959~Y2462 REQUIRES EVALUATION FOR CONFORMITY.

EXISTING REPAIR ON MAIN DECK SEAT TRACK FR40-FR45,Y1456 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK FR40-FR45, Y1456 WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG: A53832020(ISSUE: J00), NO RECORD FOUND. EO: 6-5100-7- 5000 D07 PART1 WAS COMPLETED. THE REPAIR IS CATEGORY "A" AND CLASSIFIED AS MAJOR PER GMM6-2-100. MAJOR REPAIR IAW FEDEX GMM6-2-100.

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1279, X= -47.5" FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1279, X = - 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICES BS 1249 TO 1311, X = - 47.5 IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100

LEFT WING OTBD L/E SLAT # 4 I/B LOWER SURFACE REAR EDGE HAS (2) GOUGES APPLIED PERMANENT REPAIR AT L/WING O/B L/E SLAT # 4 I/B LOWER SKIN IAW SRM 57-43-02- 2R, REP 1, TABLE 201, FIG 201, SHEET 6 AND SRM 51-70-10-2R, REP 4

CRACK L=2.500" ON UPPER SURFACE OF FLOOR PANEL 242SFF AT MDC. FLOOR PANEL 242SFF AT MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV. 94 DEC 15/2025

DURING RAMP TRAINING L1 DOOR GUST LOCK WOULD NOT RELEASE. AMM 52-11-08-8 INSTALLED SERVICEABLE SPLIT COLLAR IN REF TO AMM. CLEARED MEL.

DELAMINATION ON LWR SURFACE OF THE SPOILER 6 AT 12.5 INCH FROM OUTBD SIDE AND 16 INCH AFT EDGE, LH WING SPOILER 6 AT 12.5 INCH FROM OUTBD SIDE AND 16 INCH AFT EDGE LH WING WAS REPAIRED IAW B767 SRM 57-70-01-2R FIG 201 REP 1 SHEET 2 AND SRM 51-70-17-0G PAR 4 "A" FIG 10 SHEET 1 REV 94 DEC 15/2025

EXISTING REPAIR ON MAIN DECK CROSSBEAM FR38,Y0~Y953 REQUIRES EVALUATION FOR CONFORMITY.

EXISTING REPAIR ON MAIN DECK SEAT TRACK FR36-FR38.1,Y450 REQUIRES EVALUATION FOR CONFORMITY.

EXISTING REPAIR ON MAIN DECK SEAT TRACK FR18-FR21,-Y1959 REQUIRES EVALUATION FOR CONFORMITY.

PER CREW DEBRIEF, R1 DOOR SLIDE HANDLE HARD TO ARM/DISARM, DOOR OPENING/CLOSING AND LATCHING NOT AFFECTED, DOOR OPERATES NORMAL. RELEASED FOR SERVICE IAW MEL : 52-11-01-01, CREW ENTRY DOOR ESCAPE SLIDE R1 INOP. SLIDE REMAINS INSTALLED ON DOOR. AMM: 25-61-21-04-0 DURING GVI OF RT SLIDE FOUND SLIDER BOUND BY GIRT BAR FABRIC SLEEVE.RELEASED BINDING GIRT AND QUICK CHANGE BAR.DOOR SLIDE ARM/DISARM OPERATION CHECKS NORMAL.RETURNED RT DOOR TO OPERATION.

PUNCTURE ON UPPER SURFACE OF FLOOR PANEL 241ZFF AT MDC FLOOR PANEL 241ZFF AT MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94. DEC 12/2025.

TWO PUNCTURES ON UPPER SURFACE OF FLOOR PANEL 242VFF AT MDC FLOOR PANEL 242VFF AT MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94. DEC 15/2025

SEVEN CRACKS L=1.200" ON UPPER SURFACE OF FLOOR PANEL 241WFF AT MDC FLOOR PANEL 241WFF AT MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94. DEC 15/2025.

DENT ON UPPER SKIN WEDGE OF SLAT NR 8 OSS 457 SLAT NR 8 OSS 457 WAS REPAIRED IAW SRM 57-43-02-2R FIG 201 SHEET 1 AND SRM 51-70-10-2R PAR G FIG 209, SHEET 1, REV 94. DEC 15 /2025

GEAR DISAGREE MESSAGE. NLG INDICATION WAS NOT ILLUMINATED. NLG DID NOT EXTEND. COMPLETED QRH 14.1.12. AFTER CHKLST COMPLETION NLG EXTENSION SUCCESSFUL. EMERGENCY DECLARED. AFTER SHUTDOWN STATUS MESSAGE LDG GEAR MONITOR. EMERGENCY DECLARED. LANDING GEAR LOCKED DOWN. ADC VMO/MMO SWITCH SELECTED TO ALTN POSITION. PLACED ACFT TO NORMAL CONFIGURATION. CYCLED NLG MULITPLE TIMES ON JACK UNBLE TO GET NLG TO FAILED TOEXTEND. NOTICED EVERY OTHER CYCLE NLG & DOORS SLOW TO OPEN & EXTEND. SUSPECT NLG DOOR SEQUENCE VALVE, NLG DOOR ACTUATOR & NLG LOCK ACTUATOR. R & R NLG SEQUENCE VALVE, NLG DOOR ACTUATOR & NLG LOCK ACTUATOR. OPS & LEAK CHECK PASSED. CYCLED NLG MULTIPLE TIMES, ALL INDICATIONS NORMAL.

CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 979, X= -27.5 FOUND CROWN WORN. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 979, X = - 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1.CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 969 TO STATION 1029, X = - 27.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

LOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON SPLICE FITTING FOUND CRACK BETWEEN STATION 1801-1821 LONGERON 46 RIGHT. CRACKED LONGERON SPLICE FITTING AT LOWER CENTER CARGO COMPARTMENT BILGE AREA BETWEEN STATION 1801-1821, LONGERON - 46 RIGHT REMOVED AND REPLACED WITH FABRICATED LONGERON SPLICE FITTING PER MD11 SRM 51-33-01-0G. LONGERON SPLICE FITTING FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AFA 7225 REVISION J. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 755, X= -27.5" FOUND CROWN WORN. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 755, X = - 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT STATION 805 TO EXISTING SPLICE STATION 745, X = - 27.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

PUNCTURES AT FLOOR PANEL 221DFF OF MAIN DECK CARGO COMPARTMENT. THE FLOOR PANEL 221 DFF OF MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4-B FIG.201 SHEET 2 REV 94.

PUNCTURED FLOOR PANEL 242AFF. SEC 45 OF MDC. FLOOR PANEL 242AFF. SEC 45 OF MDC. WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4-B FIG. 201 SHEET 2. REV. 94 DEC 15,2025.

PUNCTURES AT FLOOR PANEL 231LFF OF MAIN DECK CARGO COMPARTMENT. FLOOR PANEL 231LFF OF MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00- 50-2R PAR 4-B FIG 201 SHEET 2 REV.94.

PUNCTURED FLOOR PANEL 232EFF.SEC 43 OF MDC. FLOOR PANEL 232EFF SEC 43 OF MDC. WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV. 94 DEC 15,2025.

PUNCTURES AT FLOOR PANEL 221CFF OF MAIN DECK CARGO COMPARTMENT. FLOOR PANEL 221CFF OF MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG.201 SHEET 2 REV 94.