N146FE

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 12,709 hrs · 5,837 cycles

MAIN DECK CARGO, 242VFF, FLOOR PANEL WITH EXPOSED FIBERS. MAIN DECK CARGO FLOOR PANEL 242VFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 12,709 hrs · 5,837 cycles

MAIN DECK CARGO, STA 1263, BTW RBL77 AND RBL88, FLOOR PANEL WITH DENTS. MAIN DECK CARGO FLOOR PANEL 252NFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 12,709 hrs · 5,837 cycles

MAIN DECK CARGO, BTW STA 1197 66 AND 1197 44, BTW RBL 11 AND LBL 11, FLOOR PANEL WITH BROKEN FIBERS MAIN DECK CARGO FLOOR PANEL 252EFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 12,709 hrs · 5,837 cycles

MAIN DECK CARGO, 241AGF WITH EXPOSED FIBERS MAIN DECK CARGO FLOOR PANEL 241AGF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 12,709 hrs · 5,837 cycles

MAIN DECK CARGO, STA 1263, BTW RBL77 AND RBL88, FLOOR PANEL WITH DENTS. MAIN DECK CARGO FLOOR PANEL 252NFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 12,709 hrs · 5,837 cycles

MAIN DECK FROM STA 911 TO 871.5, RBL 88 TO RBL 77, FLOOR PANEL WITH BROKEN FIBERS. MAIN DECK CARGO FLOOR PANEL 242HFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 12,709 hrs · 5,837 cycles

MAIN DECK CARGO, BTW STA 1197 66 AND 1197 44, BTW RBL 11 AND LBL 11, FLOOR PANEL WITH BROKEN FIBERS MAIN DECK CARGO FLOOR PANEL 252EFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 12,709 hrs · 5,837 cycles

MAIN DECK CARGO, STA 1263, BTW LBL 77 AND LBL 55, FLOOR PANEL WITH BROKEN FIBERS AND HONEYCOMB. MAIN DECK CARGO FLOOR PANEL 251NFA WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 12,709 hrs · 5,837 cycles

MAIN DECK CARGO, STA 1263, BTW LBL 33 AND LBL 55, FLOOR PANEL WITH BROKEN FIBERS. MAIN DECK CARGO FLOOR PANEL 251MFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 12,709 hrs · 5,837 cycles

MAIN DECK, FLOOR PANEL FROM STA 412 TO STA 522, FROM LBL 55 TO LBL 77, WITH DENTS AND BROKEN FIBERS. MAIN DECK CARGO FLOOR PANEL 231DFA WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 12,709 hrs · 5,837 cycles

MAIN DECK CARGO, BTW STA 1197 22 AND 1197, BTW RBL 11 AND LBL 11, BROKEN FLOOR PANEL MAIN DECK CARGO FLOOR PANEL 251LFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024

Part: SKIN — DENTED (ZONE 500) · airframe 12,709 hrs · 5,837 cycles

A DENT ON TRAILING EDGE WEDGE UPPER SKIN OF SLAT NO 2 AT 17" FROM INBOARD EDGE. LH WING SLAT NO 2 AT 17" FROM INBOARD EDGE UPPER SKIN WAS REPAIRED IAW B767 SRM 57- 43-02-2R REP 1 FIG 201 (SHEET 1) AND SRM 51-70-10-2R REP 4 FIG 201 (SHEET 1) REV 90 AUG 15/2024

Part: SKIN — CRACKED (ZONE 500) · airframe 12,709 hrs · 5,837 cycles

BREAK ON TRAILING EDGE WEDGE OF SLAT NO 4, LEFT WING AT 33.5" FROM INBOARD EDGE. LH WING, SLAT NO.4 TRAILING EDGE WEDGE WAS REPAIRED IAW B767 SRM 57-43-02-2R REP 1 SHEET 1 FIG 201 AND SRM 51-70-10-2R REP 4 FIG 202 SHEET 8 REV 90 AUG 15,2024

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 12,709 hrs · 5,837 cycles

MAIN DECK CARGO, BTW STA 1263 AND 1241, BTW RBL11 AND LBL 11, FLOOR PANEL WITH BROKEN FIBERS MAIN DECK CARGO FLOOR PANEL 251LFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 12,709 hrs · 5,837 cycles

MAIN DECK FROM STA 911 TO 871.5, LBL 88 TO LBL 77, FLOOR PANEL WITH BROKEN FIBERS. MAIN DECK CARGO FLOOR PANEL 241KFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 12,709 hrs · 5,837 cycles

MAIN DECK CARGO, BTW STA 1197 22 AND 1197, BTW RBL 11 AND LBL 11, BROKEN FLOOR PANEL MAIN DECK CARGO FLOOR PANEL 251LFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 12,709 hrs · 5,837 cycles

MAIN DECK FROM STA 654 22 TO STA676, LBL33 TO LBL11, FLOOR PANEL WITH SEVERAL DENTS. MAIN DECK CARGO FLOOR PANEL 231MFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 12,709 hrs · 5,837 cycles

MAIN DECK, FLOOR PANEL, FROM STA 287 TO STA 412, RBL 54.75 TO RBL 77.5 WITH SEVERAL DENTS. MAIN DECK CARGO FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 12,709 hrs · 5,837 cycles

MAIN DECK, FLOOR PANEL, FROM STA 287 TO STA 412, RBL 33.0 TO RBL 54.75 WITH SEVERAL DENTS. MAIN DECK CARGO FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 12,709 hrs · 5,837 cycles

MAIN DECK, FLOOR PANEL, FROM STA 287 TO STA 412, RBL 11.0 TO RBL 33.0 WITH SEVERAL DENTS. MAIN DECK CARGO FLOOR PANEL 222AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 12,709 hrs · 5,837 cycles

MAIN DECK, FLOOR PANEL, FROM STA 287 TO STA 412, LBL 33.0 TO LBL 11.0 WITH SEVERAL DENTS. MAIN DECK CARGO FLOOR PANEL 221DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024

Part: FORMER — CRACKED (LT WING LE) · airframe 9,265 hrs · 4,150 cycles

CRACKED LE FORMER AT LWS 499 LH WING. OLD PN 114T2511-13. REMOVED AND REPLACED DAMAGED LEFT WING LEADING EDGE FORMER P/N 114T2511-13 ANGLE 114T2511-11 WITH NEW FORMER B67-57-002-03,REF EA T-H5720-T0368934 P1 WRI 57204233 WORK CARD 000134

Part: FORMER — DAMAGED (LT WING LE) · airframe 9,265 hrs · 4,150 cycles

L WING LEADING EDGE HAS DAMAGED/LOOSE FASTENER HEADS IN 4 PLACES (MWT) REMOVED AND REPLACED DAMAGE LEFT WING LEADING EDGE FORMER P/N 114T2511-13 ANGLE 114T2511-11 WITH NEW FORMER AND ANGLE B67-57-003-03 REF T-H-5720-T0368934-P1 WRI 57204233 WORK CARD 134

Part: FORMER — CRACKED (NR 8 SLAT) · airframe 9,265 hrs · 4,150 cycles

RIGHT WING #8 SLAT OUTBOARD OF ENGINE PYLON UPPER WING SURFACE LEADING EDGE FLUSH RIVETS AND NOSE FORMER ANGLE HAS EVIDENCE OF DAMAGE AT APPROX WING STATION 441. (MWT) REPLACED CRACKED FORMER PER EA H-5720-T0368934 P1

Part: FORMER — CRACKED (NR 8 SLAT) · airframe 9,265 hrs · 4,150 cycles

RIGHT WING #8 SLAT, OUTBOARD OF ENGINE PYLON, UPPER WING SURFACE LEADING EDGE FLUSH RIVETS AND NOSE FORMER ANGLE HAS EVIDENCE OF DAMAGE AT APPROX WING STATION 499. (MWT) REPLACED FORMER PER EA H-5720-T0368934 P1

Part: SLAT — DELAMINATED (ZONE 500) · airframe 9,265 hrs · 4,150 cycles

#5 SLAT DAMAGED DUE TO LOOSE FASTENER HEADS REPAIRED SLAT IN REF. TO B767 SRM 51-70-10-2R AND B767 SRM 57-43-02-2R.

Part: FLOOR PANEL — GOUGED (CABIN) · airframe 6,212 hrs · 2,737 cycles

CABIN FLOOR PANEL 241JFF UPPER SIDE IS CRUSHED. FABRICATED NEW FLOOR PANEL, PER FED X DWG SRZ-25-005 REV R.

Part: BEAM — CRACKED (RT WING) · airframe 6,212 hrs · 2,737 cycles

RIGHT WING FIXED LEADING EDGE NOSE BEAM WEB AT OSS 679 IS CRACKED. INSTALLED REPAIR, PER B767 SRM 57-41-13-2R REPAIR 3.

Part: ANGLE — CRACKED (E/E BAY) · airframe 6,212 hrs · 2,737 cycles

E&E COMPARTMENT (OVERHEAD LT TUNNEL), MAIN CABIN FLOOR SUPPORT SUB-STRUCTURAL STIFFENER ANGLE IS CRACKED IN THE UPPER CORNER OF THE RADIUS AT STA 246 APPROXIMATELY LBL 50. FABRICATED NEW SUPPORT ANGLE, PER BAC DWG 141T5146 REV B. REMOVED AND REPLACED SUPPORT ANGLE, PER BAS DWG 141T5600 REV.

Part: FORMER — CRACKED (RT WING LE) · airframe 6,212 hrs · 2,737 cycles

RIGHT WING LEADING EDGE AT STA OSS 499 HAS A CRACKED NOSE FORMER. REMOVED AND REPLACED NOSE FORMER RT WING LEADING EDGE AT STA OSS 499, PER BAC DWG 114T2161 REV- AND B767 SRM 51-40-02-0G AND FEDEX EA H-5720-T0357934. P1, WINGS-SECONDARY WING STRC-RT WING, LEADING EDGE, ANGLE, OSS 499, ALTERNATE FASTENERS.

Part: STRAP — CRACKED (RT WING LE) · airframe 6,212 hrs · 2,737 cycles

RIGHT WING LEADING EDGE SPLICE STRAP IS CRACKED AT OSS 514. REMOVED AND REPLACED SPLICE STRAP RT WING LEADING EDGE, IAW B767 SRM 51-40-02.

Part: FORMER — CRACKED (RT WING LE) · airframe 6,212 hrs · 2,737 cycles

RIGHT WING LEADING EDGE NOSE FORMER AT STA 441 HAS A CRACKED NOSE FORMER. REMOVED AND REPLACED NOSE FORMER AND ANGLE, PER BAC DWG 114T2241 REV- AND FEDEX EA H-5720-T0357933. PT 1 TITLE WINGS-SECONDARY WING STRICTURE-RT WING, LEADING EDGE, ANGLE, OSS 441, ALTERNATE FASTENERS.

Part: FORMER — CRACKED (LT WING LE) · airframe 6,212 hrs · 2,737 cycles

LEFT WING LEADING EDGE NOSE FORMER CRACKED AT LES 436 OUTBOARD SIDE OF INBOARD AUX TRACK. REMOVED DAMAGED AND INSTALLED NEW FORMER LT WING, PER BAC DWG 114T2240 REV -. INSTALLED NEW ANGLE, PER FEDEX EA H-5720-T0357932 P1. TITLE WINGS-SECONDARY STRUCT-LT WING, LEADING EDGE, ANGLE OSS 437, ALTERNATE FASTENERS.

Part: FAIRING — CRACKED (LT WING) · airframe 6,212 hrs · 2,737 cycles

LEFT WING FLAP FAIRING 571DB FORWARD EDGE IS CRACKED. REPAIRED LEFT WING FLAP FAIRING 571DB FORWARD EDGE, IAW B767 SRM 57-53-70-2R FIGURE 201 AND 51-70-07-0G PARA 5 G.

Part: FORMER — CRACKED (RT WING) · airframe 6,212 hrs · 2,737 cycles

RIGHT WING LEADING EDGE NOSE FORMER IS CRACKED AT OSS 565. REMOVED DAMAGED FORMER AND INSTALLED NEW FORMER P/N 114T2512U14 PO NR 982576.1, IAW BAC DWG. 114T2162 REV AND FEDEX EA H-5720-T0357935 P1 AND B767 SRM 51-40-02.

Part: LANDING GEAR — INOPERATIVE (LEFT) · airframe 5,958 hrs · 2,608 cycles

A/C LANDED WITH L/H MLG RETRACTED AT LAX

Part: DOOR — DAMAGED (LT MLG) · airframe 5,958 hrs · 2,608 cycles

A/C LANDED WITH LT MLG RETRACTED AT LAX. FACT 13SEP20 21:35 LAX. FOUND NR 6 BRAKE LINK ROD ATTACH PIN MISSING. INSTALLED NEW BRAKE ROD ASSY AND ATTACH PIN, REF WRI 32-43/2755, 32-10/2839 AND 32-30/2756. ACCOMPLISHED INSPECTION EA H-0550-T0356026 PT 1/2/3, EA H-0550-T0356031 PT 1/2/3/4/5/6/7. DEFECTS FOUND, CORRECTED, REF EA H-5100-T0356095 PT 1/2/3/4/5/6. LT MLG DOOR REPLACED, REF WRI 32-10/2766. LT ENG REPLACED, REF WRI 72-00/2742. LT ENG LT & RT T/R REPLACED, REF WRI 78-30/2758 & 78-30/2759. LT ENG FAN COWLS REPLACED, REF WRI 71-10/2760, 71-10/2761. LT ENG CORE COWLS REPLACED, REF WRI 71-10/6762, 71-10/2763. ACCOMPLISHED MLG EXTENSION & RETRACTION TEST, REF AMM 32-35-00-5. ALL TESTS PASSED.

Part: SEAT — MALFUNCTIONED (COCKPIT) · airframe 5,716 hrs · 2,496 cycles

CREW NOTICED SPARKS AND ELECTRICAL BURNING SMELL COMING FROM UNDER THE FO SEAT. POWER ADJUSTMENT SYSTEMS - INOP." FOUND ELETCRIC FUNCTION OF THE FO SEAT TO BE VERY SLOW AND ALSO OPERATES IN REVERSE, WHEN SWITCH IS ACTIVATED AFT THE SEAT SLIGHTLY MOVES FWD AND THE SAME IS FOR FWD ACTIVATION, SEAT MOVES AFT. THE MOTOR IS VERY WEAK. INSPECTED ALL WIRES AND DID NOT NOTICE ANY PINCHED, CUT OR CHAFED WIRES AMM25-11-01-2-1 AMM 25-11-01-6 AMM 25-11-00-6 AND WSSM 25-11-02. REMOVED AND INSTALLED FIRST OFFICERS SEAT PER AMM 25-11-01-2-1, CHECKS OK. NO DAMAGE NOTED TO THE EITHER THE EFB POWER CORD OR THE HANDMIC CORD. A/C OK FOR SERVICE.

Part: TEST PANEL — FAILED (ZONE 200) · airframe 2,830 hrs · 1,188 cycles

DURING POSTFLIGHT CHECK, CARGO COMPT BOTTLE 2 SQUIB LIGHT DID NOT TEST WHEN SWITCH 1 OR 2 WAS DEPRESSED. R&R SQUIB TEST PANEL ASSEMBLY REF AMM 26-21-04-4. OPS CKS NORMAL

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 2,217 hrs · 939 cycles

ON PREFLIGHT-FIRST OFFICER MIC TEST ON 02 MASK NOT WORKING. REMOVED AND REPLACED F/O'S FULL FACE MASK PER M/M 35-11-51-2. OK FOR SERVICE.

Part: VALVE — STUCK (FUEL SYS)

NR 3 FUEL CROSSFEED VALVE W/N OPEN. *S/D* REMOVED AND REPLACED CROSSFEED VALVE ACTUATOR PER MM 28-22-011-4 PAR 4 A-D & PAR 9 A-P. VALVE OPS CK GOOD.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE)

A/C WILL NOT PRESSURIZE, EITHER PACK ANY BLEED SOURCE, MANUAL OR AUTO MODE. NO DOOR LIGHTS ILLUM ON 2ND OFF PNL. R&R LT & RT OUTFLOW VALVE & CABIN PRESSURE CONTROLLER PER 727 MM 21-30-051-4, 21-31-010-4 & 21-30-000-5.

Part: SPLICE — CORRODED (CENTER WING) · airframe 69,868 hrs · 59,464 cycles

DURING ROUTINE INSP, THE CENTER WING AFT UPPER SPAR SPLICE AT BS 870, RBL 70.5 FND CORRODED BEYOND ALLOWED LIMITS. R&R PER IAW SRM 51-30-2.

Part: BRACKET — SEPARATED (PAX DOOR) · airframe 69,868 hrs · 59,464 cycles

DURING A ROUTINE INSP, FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE LIGHT BRACKET WAS FND SEPARATED FROM LIGHT. REPAIRED BRACKET ASSY PER IAW SRM 51-30-2.

Part: SLIDE — TORN (PAX DOOR) · airframe 69,868 hrs · 59,464 cycles

N 45 DURING ROUTINE INSPECTION, FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE GIRT ASSY FOUND FRAYED & TORN. R&R GIRT ASSY IAW SRM 51-40-9.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,868 hrs · 59,464 cycles

DURING ROUTINE INSPECTION, CORROSION FOUND ON EXTERNAL FUSELAGE BETWEEN STR 7 RT TO 10 RT FROM BS 1173 - 1183. R&R SKIN BETWEEN STR 3 RT & 10 RT FROM BS 1080 - 1183 IAW BOEING DRAWING 65-18382 & SRM 51-30-2.

Part: SPOILER — CRACKED (NR 10) · airframe 69,868 hrs · 59,464 cycles

DURING ROUTINE INSPECTION NR 10 SPOILER SKIN FOUND CRACKED AT CENTER MOUNTING LUG. R&R IAW MM 27-61-001-4. RIGGED & OPS CHECKED SPOILER IAW MM 27-61-001-5.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,868 hrs · 59,464 cycles

DURING ROUTINE INSPECTION, FUSELAGE SKIN WAS FOUND CRACKED AT STR 1, BS 430. R&R PER IAW SRM 53-30-3 FIG 4.

Part: SPOILER — CRACKED (NR 11) · airframe 69,868 hrs · 59,464 cycles

DURING ROUTINE INSPECTION, NR 11 SPOILER PANEL WAS FOUND CRACKED. R&R IAW SRM 51-40-6. RIGGED & OPS CHECK SPOILER IAW MM 27-61-001-5.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,868 hrs · 59,464 cycles

N 165 DURING ROUTINE INSPECTION, FUSELAGE SKIN WAS FOUND BULGED BETWEEN STR 24 LT & 27 LT JUST AFT OF BS 1183. R&R IAW SRM 53-30-3.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,868 hrs · 59,464 cycles

N 349 DURING ROUTINE INSPECTION, BS 870 RT, TERMINAL FITTING FOUND CRACKED AT FWD UPPER FASTENER HOLE AT S-9 RT. R&R PER IAW FEDEX EA 7-5310-50105.

Part: SWITCH — STICKS (CARGO DOOR)

AFT CARGO DOOR LIGHT ILLUMINATED AFT T/O, LIGHT EXT ON APPROACH, AT APPROACH SPD. FOUND INNER DOOR SWITCH STUCK. LUBED SWITCH, OPS CK NORMAL.

Part: BATTERY — DISCHARGED (PAX DOOR)

FORWARD ENTRY DOOR ESCAPE SLIDE EMERGENCY LIGHT BATTERY IS DEAD. *S/D* REMOVED AND REPLACED FWD ENTRY DOOR ESCAPE SLIDE EMERGENCY LIGHT BATTERY AND FUNCTIONAL TESTED IAW FED-EX M/M 33-50-121.

Part: BRACKET — CORRODED (WS 425)

NR 0179 058 - R/W I/B AILERON, TURNAROUND CASTING CORRODED.

Part: FITTING — CORRODED (LT AILERON)

NR 0622 056 CORROSION (C57-581-01) L/W O/B AILERON LOCKOUT FILLING IS CORRODED, AREA MARK. REMOVED AND REPLACED AILERON LOCKOUT FITTING IAW FED-EX EA NR 7-5710-37352.

Part: SPAR CHORD — CORRODED (WS 638-648)

NR 0251 057 CORROSION (C57-581-04-01) L/W T/E UPPER CHORD ABOVE NR 1 FLAP TRANSMISSION. REPAIRED L/W T/E UPPER SPAR CHORD ABOVE NR 1 FLAP TRANSMISSION IAW FED-EX EA NR 7-5710-36849.

Part: STRINGER — CORRODED (BS 950-1183)

NR 0186 055 CORROSION (C53-224-01) ON STRINGER 2 LT, BS 950-1183. REPAIRED STR 2 LT, BS 950-1183 IAW FEDEX SRM 53-10-3.

Part: STRINGER — CORRODED (BS 970-990)

NR 0646 053 CORROSION (C53-224-01) ON STR 5 LT, BS 970 - 990. REPAIRED STR 5 LT, BS 950-998 IAW FED-EX SRM 53-10-3.

Part: SPAR — CORRODED (VERT STAB)

NR 0970 054 CORROSION ON VERTICAL STABILIZER INTER SPAR SKIN BS 1340 - 1344, LBL 18, WL 260.

Part: FITTING — CRACKED (BS 870)

WHILE WORKING NR0842, DISCOVERED CRACK IN FORWARD I/B RADIUS OF LT 870 TERMINAL FITTING, 2.8 INCHES ABOVE STR 10 TO 1.7 INCHES BELOW STR 10.

Part: SKIN — DENTED (BS 380)

NR 0939 050 WHILE WORKING NR0829 DISCOVERED DENT IN EXTERIOR SKIN BS 380, STR 21L. REMOVED DENTED AREA AT BS 380, STR 21L PER FED-EX SRM 53-20-3. FABRICATED PATCH AND INSTALLED PER FED-EX SRM 53-30-3, SRM FED-EX SRM 51-10-2.

Part: CLIPS — GOUGED (BS 1010/990/970)

NR 0648 051 DAMAGED STRINGER CLIPS BS 970, STR 7 LT, BS 990, STR 7, RT, BS 1010, STR 5 RT AND 5 LT. REPLACED STR CLIPS AT BS 970, STR 7L, BS 990, STR 7R, BS 1010, STR 5R AND BS 1010, STR 5L, IAW FEDEX SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 1130)

NR 0937 049 CORROSION (C53-224-01) ON FLOORBEAM BS 1130, RBL 16 - RBL 31, WL 208. REMOVED UPPER CHORD OF FLOORBEAM AT BS 1130, RBL 15 TO RBL 39, WL 208 AND REPAIRED IAW FED-EX EA NR 7-5310-37355 AND ER 97-2706.

Part: CHORD — CORRODED (BS 450-680)

CORROSION (C53-111-01, 2) UNDER NUT PLATES ON BL 0 CHORD BS 450 TO BS 680, WL 200. FWD CARGO BAY AS PER FEDEX DRAWING SR 27-53-009 AND FASTENER INSTALLATION AS PER FEDEX SRM 51-30-02. *S/D* REMOVED AND REPLACED BL 0 CHORD FROM BS 450 TO BS 740, WL 200 IN FWD CARGO BAY PER FED DWG SR 27-23-009 AND FASTENER INSTALLATION PER SRM 51-30-2.

Part: STRAP — CORRODED (BS 500-600)

CORROSION (C53-111-01, 2) ON I/B STRAP BS 500 TO 600, RBL 25, WL 156 FWD CARGO BAY. *S/D* REMOVED AND REPLACED I/B STRAP BS 500 TO 600, RBL 25, WL 156 FWD CARGO BAY PER FED SRM 51-30-02.

Part: SKIN — CORRODED (BS 710-660)

NR 0673 045 CORROSION (C53-224-01) ON INSIDE SKIN BETWEEN BS 710-660 AND STR 4 RT, 6 LT CROWN AREA (MARKED IN RED). CUT OUT DAMAGED AREAS AND REPAIRED SKIN BETWEEN BS 660-710, STR 4 RT, STR 6 LT IAW FED-EX SRM 53-30-3.

Part: FITTING — CORRODED (BS 360)

NR 0950 046 CORROSION (C53-224-01(2)) BARRIER NET CASTING BS 360, RBL 20. REMOVED AND REPLACED BARRIER NET CASTING BS 360, RBL 20 PER FED-EX SRM 51-30-2.

Part: FITTING — CRACKED (BS 870)

CRACK INDICATION NOTED IN RT BS 870 TERMINAL FITTING ROW 3, HOLE NR 2. *S/D* REPAIRED CRACKED FASTENER HOLE IN THE 870 RT TERMINAL FITTING ROW 3, HOLE NR 2 IAW FEDEX EA NR 7-5310-37308.

Part: BEAM — CORRODED (BS 950)

NR 0459 041 CORROSION (C53-224-01(2) BS 950 UPPER CHORD BL-O-LBL 24, RBL 45-62. UPPER SURFACE AND RBL 62-LBL 46 ON LOWER SURFACE AT NUTPLATES. ACCOMPLISHED REPAIR ON BS 950 BEAM IAW FED EA NR 7-5310-36830.

Part: FLOORBEAM — CORRODED (BS 1130)

CORROSION AFT BAY BS 1130 LOWER FLOORBEAM CHORD LOWER SURFACE LBL 21, WL 200 AT FASTENER HOLE. *S/D* REPAIRED AFT BAY BS 1130 LOWER BEAM CHORD, LOWER SURFACE, LBL 21, WL 200 PER ER 97-2664 AND EA 7-5310-36853.

Part: FITTING — CRACKED (BS 870)

NR 0842 044 CRACK INDICATION NOTED LT 870 TERMINAL FITTING ROW 3, HOLE NR 3. REPAIRED LT BS 870 TERMINAL FITTING AS PER FED-EX EA NR7-5310-37383.

Part: SPAR CHORD — CORRODED (BS 1342)

NR 0949 038 WHILE WORKING (FEDEX CARD NR 0652) FOUND LT REAR VERTICAL SPAR CORRODED AT BS 1342. REMOVED AND REPLACED SECTION OF THE LT VERTICAL SPAR CHORD BS 1342, FIN STA 0.00 TO FIN STA 99.0 IAW FED-EX EA NR 7-5530-37380.

Part: FLOORBEAM — CORRODED (BS 1148)

CORROSION (C53-111-01, 3) AFT BAY BS 1148, RBL 35 - BL 0, WL 208 AT FASTENER HOLES. *S/D* REPAIRED FLOORBEAM AT BS 1148 LOWER CHORD, RBL 35 TO BL 0, WL 208 IAW FED-EX SRM 53-10-8.

Part: SPAR — CORRODED (BS 1342)

NR 0948 037 WHILE WORKING (FEDEX CARD NR 0652) FOUND RT REAR VERTICAL SPAR CORRODED AT BS 1342. REPLACED RT REAR VERTICAL SPAR CHORD FROM BS 1342 TO FIN STA 55, RBL 18 IAW FED-EX EA NR 7-5510-37337.

Part: SPAR WEB — CORRODED (BS 1342-1344)

NR 0952 039 CORROSION (C53-395-11) ON VERTICAL STABILIZER INTER SPAR SKIN BS 1340 - 1344, RBL 18, WL 260. REPAIRED CORROSION ON RT INNER SPAR SKIN OF VERT STAB BS 1340-1344, RBL 18, WL 260 IAW FED-EX EA NR 75510-37338 AND FED-EX EA NR 7-5330-37334.

Part: STRINGER — CORRODED (BS 640-700)

CORROSION (C53-224-01) ON STRINGER 2 RT, BS 700 TO 640 (MARKED). *S/D* REMOVED CORROSION ON STR 2 RT, BS 700 TO 640. FOUND AREA 1.25 X .375 AT BS 697 TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. FABRICATED AND INSTALLED REPAIR IAW EA NR 7-5310-36831.

Part: SKIN — CORRODED (BS 870)

UPON REMOVAL OF LOWER CHORD (NR0145) FOUND INSIDE LOWER TANK SKIN TO BE CORRODED BS 870, RBL 60- LBL 60, WL 148. *S/D* REMOVED CORROSION ON INSIDE LOWER TANK SKIN BS 870, RBL 60 - LBL 60, WL 148 PER FED 53-10-1 AND EA 7-5710-36884 AND ER 97-2658.

Part: SKIN — CORRODED (BS 870)

UPON REMOVAL OF UPPER CHORD (NR0413) FOUND INSIDE UPPER TANK SKIN TO BE CORRODED, BS 870, RBL 60 - LBL 60, WL 178. *S/D* REMOVED CORROSION INSIDE UPPER TANK SKIN BS 870, RBL 60 - LBL 60, WL 178 PER FED EA 7-5710-36884 AND ER 97-3658.

Part: BULKHEAD STRAP — CORRODED (BS 870)

UPON REMOVAL OF 8.70 BULKHEAD WEB (NR0414) FOUND TENSION LOAD STRAP TO BE CORRODED RBL 50-LBL 50, WL 160. *S/D* REMOVED AND REPLACED TENSION LOAD STRAP RBL 65 - LBL 65, WL 160, BS 870 PER BOEING DWG 65-15978 AND ER NR 054. INSTALLED HILOCS PER FED SRM 51-30-2.

Part: CHORD — CORRODED (BS 760)

CORROSION (C53-224-01, 2) LONGITUDINAL BS 760 TO 848, WL 208, LBL 45 AT NUTCLIP LOCATIONS ON UNDERSIDE OF FLANGE BS 820 ON UPPER SURFACE AND SEAT TRACK FASTENER CUTOUT BS 760.

Part: CHORD — CORRODED (BS 760-848)

CORROSION (C53-224-01,2) LONGITUDINAL BS 760 TO 848, WL 208 UPPER AND LOWER FLANGE SURFACES AT NUTCLIP LOCATIONS. *S/D* REMOVED AND REPLACED LONGITUDINAL BS 760 TO 848, WL 208, RBL 24 UPPER CHORD IAW FED DWG 65-34144.

Part: CHORD — CORRODED (BS 760-848)

CORROSION (C53-224-01, 2) AND BORE METAL ON LONGITUDINAL BS 760 TO 848, WL 208, RBL 48 ON LOWER SURFACE OF INBOARD FLANGE AT NUTCLIP LOCATIONS.

Part: STRINGER — CRACKED (BS 1010)

CRACK IN STRINGER 24 RIGHT UNDER 1010 FRAME. *S/D* STOP DRILLED CRACK PER FED-EX SRM 51-10-1, FABRICATED J-CHANNEL PER FED-EX SRM 53-10-3. ALODINED AND PRIMED PER FED-EX SRM/ MM 51-10-2 AND 51-20-151. INSTALLED J-CHANNEL REPAIR PER FED-EX SRM 53-10-3.

Part: SKIN — CORRODED (BS 481)

CORROSION ON FORWARD SIDE OF BS 481 SPLICE PLATE BETWEEN STRINGER 5 RT AND 6 RT.

Part: STRINGER — CORRODED (BS 360-430)

CORROSION (C53-224-01) ON STRINGER 2 LT, BS 360 TO 430 (AREA MARKED IN RED). *S/D* REPAIRED STR 2 LT, BS 360 TO 430 IAW FED-EX SRM 53-10-3.

Part: STRINGER — CORRODED (BS 360-445)

CORROSION (C53-224-01) ON STRINGER 3 LT, BS 445 TO 360 IN AREAS (MARKED IN RED). *S/D* REPAIRED STR 3 LT, BS 377 TO 387, BS 417 TO 428 PER FED-EX EA 7-5310-36840.

Part: FITTING — CORRODED (BS 360)

CORROSION (C53-111-01-1) STR 26R FITTING BS 360. *S/D* REMOVED CORROSION ON SHEAR TIE FITTING BS 360, STR 26R PER FED SRM 53-10-1. INSTALLED NEW SHEAR TIE FITTING BS 360, STR 26R PER FED SRM 51-30-2 PG 2B.

Part: STRAP — CORRODED (BS 440-480)

CORROSION (C53-224-01, 1) EMANATING UNDER STRINGER ON MCD BARE STRAP FROM BS 460 TO 480 STRINGER 3 LT.

Part: STRAP — CORRODED (BS 475)

CORROSION BS 475 BETWEEN STRINGER 2 AND STRINGER 3 LT. *S/D* REPAIRED CORROSION AT BS 475 BETWEEN STR 2 AND STR 3 LT IAW FED EA NR 7-5330-37314.

Part: SKIN — CORRODED (BS 950-990)

NR 0645 022 CORROSION (C53-224-01) ON INTERNAL SKIN 950-990 STR 1 - STR 4 RT. REPAIRED SKIN BS 950-990, STR 1 - STR 4 RT IAW FED-EX SRM 53-30-3 FIG 3.

Part: FLOORBEAM — CORRODED (BS 264)

CORROSION (C53-221-01) ON UPPER SURFACE OF FLOOR SUPPORT AT BS 264, WL 208, LBL 2 THROUGH LBL 7. *S/D* REMOVED AND REPLACED UPPER CHORD OF FLOORBEAM (25G BEAM) DUE TO CORROSION BEING OUT OF LIMITS IAW FED SRM 53-10-1, 51-30-2, 51-30-2 AND BAC DRAWING 65-17588 AT BS 264, LBL 2 TO RBL 21, WL 208.

Part: SKIN — CORRODED (BS 1006)

CORROSION (C53-224-01) ON INSIDE SKIN BS 1006 BETWEEN STR 1 TO 2 RT. *S/D* REMOVED CORROSION ON INNER SKIN BS 1006 BETWEEN STR 1 TO 2 RT. REMOVED .043 FROM .063 ORIGINAL THICKNESS IN AREA OF 2 X 1. FOUND TO BE OUT OF LIMITS PER FED SRM 53-30-1. TRIMMED DAMAGED AREA PER FED SRM 53-30-3. FABRICATED DOUBLER PER FED SRM 53-30-3 AND INSTALLED DOUBLER PER FED SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 600)

CORROSION (C53-111-01, 2) UNDER NUT PLATES ON FLOORBEAM BS 600, RBL 25 LBL 25, WL 200 FWD CARGO BAY. *S/D* MECHANICALLY REMOVED CORROSION FROM UNDER NUT PLATES ON BS 600 FLOORBEAM, RBL 25 TO LBL 25, WL 200 FWD BAY. FOUND TO BE OUT OF LIMITS PER FED SRM 53-10-1. TRIMMED OUT OF LIMITS AREA PER ER 97-2639. FABRICATED, ALODINED, PRIMED AND PAINTED REPAIR PARTS PER ER 97-2639, FED SRM 51-10-2, FED SRM 51-20-151.

Part: SPAR — CRACKED (LT AILERON)

CRACK IN LT O/B AILERON REAR SPAR ON THE I/B SIDE, WBL 493. *S/D* CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND FILLER INSTALLED. ALL WORK DONE IAW FED-EX SRM 57-50-2 SRM 51-40-3 AND FED-EX M/M 27-10-41.

Part: DOUBLER — CORRODED (BS 219.8)

NR 0626 017 CORROSION (C53-221-01) ON AFT SIDE OF BS 219.8 FRAME LEFT HAND SIDE WL 234. REMOVED AND REPLACED DOUBLER AT BS 219, LT WL 228-239 PER FED SRM 51-30-2, BOEING DWG 65-16305.

Part: STRINGER — CORRODED (BS 580)

WHILE WORKING NR 0898, FOUND CORROSION UNDER NUT PLATE COMMON TO STRINGER 28 RT, BS 580. *S/D* MECHANICALLY REMOVED CORROSION, .032 IN A 1 X 2 AREA FROM ORIGINAL THICKNESS OF .067, FOUND TO BE OUT OF LIMITS PER FED SRM 53-10-1. FABRICATED, LOCATED, AND DRILLED REPLACEMENT STRINGER AND REPAIR SPLICE IAW FED SRM 53-10-3. INSTALLED REPLACEMENT STRINGER SEGMENT IAW FED SRM 53-10-3.

Part: STRINGER — CORRODED (BS 623)

WHILE WORKING NR 0696 UPON REMOVAL OF STRINGER FROM BS 610 TO 624, STR 28 LT TO ACCESS KEEL BEAM CORROSION FOUND CORROSION IN BETWEEN SURFACES OF KEEL BEAM AND STRINGER. *S/D* MECHANICALLY REMOVED CORROSION ON STR 28 LT, BS 623, FOUND TO BE OUT OF LIMITS PER FED SRM 53-10-1. REMOVED AND REPLACED STR 28 LT, BS 590 TO 625 PER FED SRM 53-10-3 FIG 1.

Part: SKIN — CORRODED (BS 456-463)

CORROSION (C53-224-01) ON INSIDE SKIN AT BS 458 BETWEEN STR 1 TO 2 LT. *S/D* REPAIRED CORROSION (C53-224-01) ON INSIDE SKIN AT BS 458 BETWEEN STR 1 TO 2 LT IAW PER FED EX NR 7-5330-37314.

Part: FLOORBEAM — CORRODED (BS 344)

CORROSION (C53-224-01) ON FLOORBEAM TOP FLANGE BS 344, RBL 20 LBL 55, WL 208. *S/D* REMOVED AND REPLACED UPPER CHORD FLOORBEAM BS 344 FROM RBL 63 TO LBL 63 IAW FEDEX SRM 53-10-8.

Part: BULKHEAD CHORD — CORRODED (BS 870)

NR 0415 011 - CORROSION (C53-132-02-1/2) ON BS 870 LOWER CHORD LBL 65 TO LBL 40.

Part: BULKHEAD WEB — CORRODED (BS 870)

NR 0414 010 - CORROSION (C53-132-02-1/2) ON BS 870 BULKHEAD WEB, LBL 45 TO RBL 45.

Part: CHORD — CORRODED (BS 870)

NR 0413 012 STA-PAE - CORROSION (C53-132-02-1/2) ON BS 870, UPPER CHORD LBL 65 TO LBL 40. REMOVED AND REPLACED BS 870 UPPER CHORD PER FED-EX EA NR 7-5710-36884.

Part: SKIN — CORRODED (BS 436-438)

CORROSION FWD OF CIRCUMFERENTIAL JOINT BS 440, STRINGER 3 LT ON SKIN. *S/D* REMOVED CORROSION FROM FWD OF CIRCUMFERENTIAL JOINT BS 440, STR 3 LT ON SKIN. DAMAGE OUT OF LIMITS. REPAIRED PER FED SRM 53-30-3.

Part: SKIN — CORRODED (BS 940-930)

BARE METAL ON INTERIOR SKIN BS 940 TO 930, BETWEEN STR 1 AND STR 2 L. *S/D* CLEANED UP CORROSION ON BARE METAL BS 940 TO 930, BETWEEN STR 1 AND STR 2L. FOUND TO BE OUT OF LIMITS, IAW 727 FED-EX SRM 53-30-1. REPAIRED AREA IAW 727 FED-EX SRM 53-30-3.

Part: STRINGER — CORRODED (BS 870-880)

NR 0686 - 007 - CORROSION (C53-224-01(2)) STR 6R, BS 870-880 (VARIOUS AREAS MARKED). REPAIRED STR 6R, BS 870-880 PER FED-EX SRM 53-10-3.

Part: FLOORBEAM — CORRODED (BS 600)

CORROSION (C53-111-01, 2) UNDER NUT PLATES ON FLOORBEAM BS 600, RBL 25 TO LBL 25, WL 200 FWD CARGO BAY.

Part: STRINGER — CORRODED (BS 950-1130)

NR 0188 005 CORROSION (C53-224-01) ON STRINGER 2 RT, BS 950-130. REPLACED STRINGER NR 2 RT, BS 950-1030 PER FEDEX SRM 53-10-3 AND 53-10-4. REMOVED CORROSION FROM STRINGER NR 2 RT BS 1030-1130 PER FEDEX SRM 51-10-6, WITHIN LIMITS PER FEDEX SRM 53-10-1.

Part: SKIN — CORRODED (RUDDER)

NR 0715 006 WHILE WORKING NR0363, FOUND AREA OF CORROSION UNDER DOUBLER ON EXTERNAL SKIN RT SIDE 12 INCHES DOWN AND 4 INCHES AFT OF RUDDER FRONT SPAR. REMOVED AND REPLACED UPPER RUDDER PER FED-EX M/M 27-20-1.

Part: KEEL BEAM — CORRODED (BS 624)

NR 0696 004 CORROSION (C53-111-01(02) ON KEEL BEAM BS 624, LBL 6, WL 148 FWD CARGO BAY. REMOVED AND REPLACED KEEL BEAM FROM BS 620 - 740, LBL 6, WL 148 AS PER FED-EX SRM 51-30-2, 51-40-2 AND PER BOEING DRAWING 65-18216.

Part: BULKHEAD WEB — CORRODED (BS 870)

NR 0414 002 CORROSION (C53-132-02 1/2) ON BS 870 BULKHEAD WEB LBL 45 TO RBL 45.

Part: CHORD — CORRODED (BS 870)

NR 0413 001 STA-PAE - CORROSION (C53-132-02-1/2) ON BS 870 UPPER CHORD LBL 65 TO LBL 40. REMOVED AND REPLACED BS 870 UPPER CHORD PER FED-EX EA NR 7-5710-36884.

Part: ANTI-ICE DUCT — BLOWN (NR 2 ENGINE)

LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED AFTER TAKEOFF AT TAKEOFF THRUST SETTING. RAN THROUGH RED TABS AND ISOLATED NR 2 ENGINE BLEED CAUSES LIGHT TO ILLUMINATE ABOVE 88 PERCENT AT 15,000 MSL. LIGHT REMAINED OUT AS LONG AS NR 2 WAS KEPT AT REDUCED THRUST. FOUND THE NR 2 ENG TOP ANTI-ICE DUCT BLOWN AND FIRE-WALL DAMAGE. INVESTIGATION REVEALED BLOWN NR 2 ENG PNEUMATIC DUCT AND LARGE HOLE IN FORWARD FIRE WALL WHICH ALLOWED BLEED AIR INTO AFT BODY AREA. FIRE WALL DAMAGE REPAIRED. BLEED AIR DUCT REPLACED. NR 2 ENG RUN TO POWER PER JET RUN-UP HANDBOOK AND THERE WAS NO REOCCURRENCE OF AFT BODY OVERHEAT.

Part: RETRACT MECH — LACK OF LUBE (NLG)

ON GEAR EXTENSION, RED NOSE GEAR LIGHT DID NOT ILLUMINATE NORM. GRN LIGHT CAME ON OK, IT THEN FLICKERED AND THE WARN HORN STARTED TO SOUND INTERMITTENTLY. GRN LIGHT THEN WENT OUT AND WOULD NOT TEST, THEN TESTED OK. THROTTLE RESTARTED AND UNSAFE INDICATION WARN GEAR RECYCLED TO NO AVAIL. COULD NOT SEE ALIGNMENT STRIPE. NOSE GEAR MANUALLY EXTENDED, GRN LIGHT CAME ON AND MAINS HYDRAULICALLY EXTENDED OK. ON FINAL NOSE GEAR GRN LIGHT STAYED ON BUT WARN HORN SOUNDED INTERMITTENTLY AGAIN. LUBED NOSE GEAR ASSY PER M/M 12-21-11 PG 202. CKD DOWNLOCK SWITCH, RETRACT AND EXTEND COMPONENTS, NO DEFECTS NOTED. JACKED NOSE AND RETRACTED SEVERAL TIMES, OPERATIONAL CKS GOOD PER M/M 32-33-11.

Part: DOWNLOCK SWITCH — DIRTY (NLG)

AFTER INITIAL EXTENSION OF LANDING GEAR, NOSE GEAR LIGHT DID NOT ILLUMINATE GREEN LIGHT TESTED OKAY. LANDING GEAR RETRACTED AND EXTENDED AGAIN WITH SAME RESULT OF UNSAFE NOSE GEAR INDICATION. ACCOMPLISHED CHECK LIST, RAISED AND LOWERED GEAR AGAIN. NOSE GEAR INDICATION GREEN ON THIRD ATTEMP AND ON ALL ATTEMPTS FELT NOSE GEAR EXTEND. CHECKED FOR WATER IN E AND E BAY AROUND LANDING GEAR MODULE, CHECKED ALL WIRING AND RIGGING ON NOSE GEAR DOWN LOCK SWITCH. CLEANED SWITCH WITH CONTACT CLEANER AND LUBED LINKAGE.