N273FE

Part: SKIN — CRACKED (ZONE 500) · airframe 6,107 hrs · 3,034 cycles

LEFT WING, SLAT NO 6, INBOARD STRUCTURE, (RIGHT SIDE) SKIN BROKEN. LH WING, SLAT 6, INBD RIB WAS REPAIRED IAW E.A. #: H-2780-T0380461

Part: SKIN — DELAMINATED (LT TE FLAP) · airframe 6,107 hrs · 3,034 cycles

LH WING, L/E OUTBD FLAP BETWEEN WS 543.00/ 597.00 WITH DELAMINATION LH WING, L/E OUTBD FLAP BETWEEN WS 543.00/ 597.00 WAS REPAIRED IAW B767 SRM 57-53-01-2R TABLE I AND 51-70-03-0G PAR 5.A FIG 5 REV 89 APR 15/2024

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 6,107 hrs · 3,034 cycles

MAIN DECK CARGO COMPARTMENT STA 1000 FLOOR PANEL 242UFF WITH PUNCTURE MAIN DECK CARGO COMPARTMENT STA 1000 FLOOR PANEL 242UFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 89 APR 15/2024

Part: SKIN — WORN (RT AILERON) · airframe 6,107 hrs · 3,034 cycles

RIGHT WING, INBOARD AILERON LOWER SURFACE, INBOARD FWD CORNER WITH WEAR. RIGHT WING, INBOARD AILERON LOWER SURFACE, INBOARD FWD CORNER WAS REPAIRED IAW B767 SRM 57-60-01-2R TABLE VII AND SRM 51-70-17-0G PAR 4.G FIG 15 REV 89 APR 15/2024

Part: LINKAGE — DAMAGED (RT TE FLAP) · airframe 5,082 hrs · 2,539 cycles

RH WING INBD TRALING EDGE FLAP LINKAGE (113T770-52G) FAIRNIG AT WS 671. HAS A HOLE PUNCTURE REPAIRED RH WING TRAILING EDGE FLAP LINKAGE FAIRING (PNL# 671FB) AT WS 671. IN REF. TO EA#: H-5750-T03773386 767 SRM 57-53-70-2R FIG. 201 SHEET 2, 767 SRM 51-70-03-0G PARA 4&5. C. , AND BOEING DRW# 113T1771.

Part: FORMER — CRACKED (UNKNOWN) · airframe 4,441 hrs · 2,225 cycles

THE NOSE FORMER ANGLE AT OSS 499 ON THE RIGHT WING FIXED LEADING EDGE IS CRACKED. REPLACED CRACKED FORMER ON RIGHT WING AT OSS 499 REF. FEDEX DWG SR67-57-002

Part: FORMER — CRACKED (UNKNOWN) · airframe 4,441 hrs · 2,225 cycles

FOUND THE NOSE FORMER ANGLE AT OSS 441, RIGHT SIDE WING FIXED LEADING EDGE, TO BE CRACKED. 0000392280 : BILLMAN, CRAIG B - 22-JUL-2023 05:08 REPLACED FORMER AT OSS 441 AS REQUIRED PER BOEING DRAWING SR67-57-002 REV A.

Part: FORMER — DAMAGED (UNKNOWN) · airframe 4,441 hrs · 2,225 cycles

FOUND THE NOSE FORMER ANGLE AT OSS 441, RIGHT SIDE WING FIXED LEADING EDGE, TO BE CRACKED. 0000392280 : BILLMAN, CRAIG B - 22-JUL-2023 05:08 REPLACED FORMER AT OSS 441 AS REQUIRED PER BOEING DRAWING SR67-57-002 REV A.

Part: FORMER — CRACKED (ZONE 600) · airframe 4,441 hrs · 2,225 cycles

FOUND NOSE FORMER ANGLE AT OSS 441 RIGHT SIDE WING FIXED LEADING EDGE TO BE CRACKED. REMOVED AND REPLACED FORMER AS REQUIRED PER DWD SR67-57-002.

Part: WEDGE — WORN (RT NR 8 SLAT) · airframe 3,131 hrs · 1,563 cycles

RH WING, SLAT # 8, WEDGE AREA, LOWER SKIN WITH WEAR. R.H. WING, SLAT #8, WEDGE AREA, LOWER SKIN WAS REPAIRED IAW B767 SRM 57-43-02-2R FIG. 201 PAGE 1-2 AND SRM 51-70-10-2R REPAIR 4 FIG. 202 PAGE 149-169 REV. 82 12-15-21

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 3,131 hrs · 1,563 cycles

RH WING, OUTBOARD FLAP, NEAR EXTERIOR EDGE, INNER SKIN WITH TWO DENTS. RH WING, OUTBOARD FLAP, LOWER SKIN, TWO DENTS WERE EVALUATED, ONE FOUND WITHIN LIMITS AND ONE WAS REPAIRED IAW SRM 57-53-01-1A TABLE I NOTE C, SRM 57-53-01-2R REP. 1 FIG. 201 SHEET 1 AND SRM 51-70-10-2R REPAIR 2 REV. 82 DEC15/2021

Part: FORMER — CRACKED (ZONE 600) · airframe 2,512 hrs · 1,236 cycles

NR 12 441 AT RS FLE OSS 441 CRACKED FORMER 114T2170-6 WITH ANGLE 114T2171-3, ALONG WITH LOOSE/DAMAGED FASTENERS AT THIS LOCATION. REPLACED WITH B67-57-002-02 FORMER & B67-57-003-02 ANGLE REFERENCE EA H-5720-T0368124 P1

Part: FORMER — CRACKED (ZONE 500) · airframe 2,512 hrs · 1,236 cycles

NR 8 AT LS FLE OSS 441 CRACKED FORMER 114T2170-5 WITH ANGLE 114T2171-4, ALONG WITH LOOSE/DAMAGED FASTENERS AT THIS LOCATION REPLACED WITH B67-57-002-01 FORMER & B67-57-003-01 ANGLE REFERENCE EA H-5720-T0368124 P1

Part: FORMER — CRACKED (N/A) · airframe 2,512 hrs · 1,236 cycles

AT RS FLE OSS 499 CRACKED FORMER 114T2511-14 WITH ANGLE 114T2511-12, ALONG WITH LOOSE/DAMAGED FASTENERS AT THIS LOCATION. REMOVED AND REPLACED CRACKED FORMER REF E.A H-5720-T0368124 P1

Part: FORMER — CRACKED (N/A) · airframe 2,512 hrs · 1,236 cycles

AT RS FLE OSS 565 CRACKED FORMER 114T2512-14 WITH ANGLE 114T2512-12, ALONG WITH LOOSE/DAMAGED FASTENERS AT THIS LOCATION. 0000553921 : DAVIES, ANDREW M - 22-APR-2022 10:11 REMOVED AND REPLACED CRACKED FORMER REF E.A. H-5720-T0368124 P1

Part: FORMER — CRACKED (N/A) · airframe 2,512 hrs · 1,236 cycles

AT LS FLE OSS 565 CRACKED FORMER 114T2512-13 WITH ANGLE 114T2512-11, ALONG WITH LOOSE/DAMAGED FASTENERS AT THIS LOCATION. REMOVED AND REPLACED CRACKED FORMER REF E.A. H-5720-T0368124 P1

Part: FORMER — CRACKED (N/A) · airframe 2,512 hrs · 1,236 cycles

AT LS FLE OSS 499 CRACKED FORMER 114T2511-13 WITH ANGLE 114T2511-11, ALONG WITH LOOSE/DAMAGED FASTENERS AT THIS LOCATION. REMOVED AND REPLACED CRACKED FORMER REF E.A, H-5720-T0368124 P1

Part: ENGINE — FAILED (NR 2) · airframe 43,477 hrs · 27,603 cycles

LOUD BANG/ ACFT SHUDDER DURING TAKEOFF, ACFT TAKEOFF REJECTED AT 115 KNOTS. GROUND PERSONNEL REPORTED HEARING 3 DISTINCT LOUD BANGS, NO APPARENT ENGINE MALFUNCTION NOTED PRIOR TO REJECT (ON GAUGE) WITH ALL INDICATIONS NORMAL AT IDLE. INSPECT ALL THE ACFT AIRFRAME EXTERIOR ALL ENGINE IN-LETS. INSP ON THE AIR FRAME IAW MM 5-51-181-2 AND FOUND NO DAMAGE ON THE AIRFRAME. R & R NR 2 ENGINE ASSY IAW WORK CARD 70T0002 AND TEST OK. ACFT OK FOR SERVICE.

Part: INLET — OBSTRUCTED (A/C PACK) · airframe 43,160 hrs · 27,345 cycles

LT AND RT PACK "TRIP OFF" LIGHTS W/ "DUCT OVER" LIGHT. ON POST FLIGHT, PACK COOLING DOOR FILLED WITH SNOW. INSPECTED PACK INTAKES AND FOUND SNOW PACKED INSIDE. MELTED SNOW FROM PACK INLET AREA. OPERATED PACKS IAW MM 21-61-000-5 AND 21-55-000-5. OPS CHECK GOOD OK FOR SERVICE.

Part: MOTOR — LEAKING (HYD SYSTEM) · airframe 42,952 hrs · 27,163 cycles

LOST SYS A HYD FLUID DURING CLIMBOUT DID QRH CHECKLIST. SECURED SYS A HYD PUMPS AND CLOSED FLUID SHUTOFF SWITCHES IAW QRH. REMOVED AND REPLACED BOTH FLAP MOTORS IAW 27-51-062-4, REMOVED AND REPLACED ENG NR 1 AND 2 CASE DRAIN FILTERS IAW 29-11-041-2, REMOVED SYS A HYD PRESSURE FILTERS IAW 29-11-062-3 NO METAL OR PARTICLES WERE FOUND. A SYS HYD OPS CHECKS NORMAL DURING ENGINE RUN. RAN FLAPS UP AND DOWN NO LEAKS NOTED AT ALL OF THE ASSOCIATED FILTERS THAT WERE CHANGED. SERVICED "A" SYS HYD IAW 12-12-000-2 TO FULL. ACFT OK FOR SERVICE.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,262 hrs · 26,602 cycles

LOWER FUSE WING BODY FILLET FRG SUPPORT FRAME U CHANNEL IS CORRODED BS 773, LBL 9 - RBL 9, WL 140. REMOVED U CHANNEL REF SRM 51-30-2. FABRICATED "U" CHANNEL ON SHOP SNRM NR N00692, DRILLED UP, TREATED, PRIMED AND PAINTED "U" CHANNEL REF DWR 65-58504, SRM 51-10-2. IDENTIFIED "U" CHANNEL REF GMM 7-0-1001. INSTALLED "U" REF SRM 51-30-2 APPLIED CIC TO NEW "U" CHANNEL REF SRM 51-10-2. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: INTERCOSTAL — CORRODED (BS 740) · corrosion level 2 · airframe 42,262 hrs · 26,602 cycles

DELTA BEAM AT STA 740 HAS CORROSION AROUND AND UNDER HEADS OF SEVERAL FASTENERS. CAN BE SEEN THRU ACCESS HOLE BELOW BEAM. REMOVED CORROSION. ORIGINAL "T" .107 LOSS AT LOWEST POINT IS .028 REMAINING "T" IS .079. OUT OF LIMITS REF SRM 53-10-1 FIG 101 DETAIL I. REMOVED FWD DELTA BOX INTERCOSTAL REF 51-30-2 PG 1-6 MANUFACTURED NEW INTERCOSTAL P/N 69-47111-2 REF DWG 69-47111. TREATED AND PRIMED REF SRM 51-10-2 PG 7. INSTALLED REF SRM 51-30-2 PG 1-6.

Part: BRACKET — CRACKED (NR 1 NACELLE) · airframe 42,262 hrs · 26,602 cycles

NR 1 ENG UPPER COWL, BRACKET CRACKED AT FWD O/B LOWER CORNER REMOVED AND REPLACED CRACKED SEGMENT, PAINTED AFFECTED AREA OF COWLING. REF SRM 51-30-2 PG 2, MM 51-20-151-7 PG1-5. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FAIRING — CRACKED (ZONE 100) · airframe 42,262 hrs · 26,602 cycles

RT BODY FAIRING PANEL NR 3349 CRACKED AT EDGE. REMOVED DAMAGED EDGE PLATE. VERIFIED MATERIAL FOR NEW EDGE PLATE, FABRICATED NEW EDGE PLATE, TREATED AND PRIMED AND INSTALLED. REF DWR 65-58505 AND SRM 51-10- 2 PG1, 51-30-2 PG1. THIS IS CLASSIFIED AS A MINOR REPAIR

Part: RETAINER — CORRODED (ZONE 600) · corrosion level 2 · airframe 42,262 hrs · 26,602 cycles

LEFT MLG W/W LOWER FWD WING PANEL HAS CORROSION ON SEAL RETAINER STRIP NEAR LOWER MLG SUPPORT BEAM, WSS 217. REMOVED AND REPLACED LEFT MLG W/W LOWER FWD WING PANEL SEAL RETAINER AT WSS 217 REF SRM 51-30-2 PG 2 AND DWR 65-21656. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,262 hrs · 26,602 cycles

UNDER FWD LAV STA 328 TO 344 FLOOR SUPPORT RBL 52 HAS CORROSION AROUND NUTPLATES REMOVED AND REPLACED SUPPORT FROM STA 326-344 RBL REF SRM 51-30-2 PG 2, FLOOR SUPPORT AT RBL 52 STA 328-344. FOUND TO BE WITHIN LIMITS OF SRM 53-10-06, TREATED AND PRIMED REF SRM 51-10-2.

Part: BULKHEAD — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,262 hrs · 26,602 cycles

CORROSION AT BS 1166 BULKHEAD RT SIDE "T" ANGLE (AT BOTTOM NUTPLATE AFT SIDE OF BULKHEAD). REPLACED T-CHORD AT AFT PIT BULKHEAD BS 1166 RBL 25 INCHES. REMOVED CORROSION AND FOUND NOT WITHIN ALLOWABLE LIMITS ORIG MATERIAL THICKNESS IS .063, MATERIAL LOSS IS .038, AND REMAINING MATERIAL IS .025, REF SRM 51-10-1 PG 5. FABRICATED NEW T-CHORD, REF BOEING DWR 65-67250-10 SHEET 2/3. TREATED AND PRIMED NEW T-CHORD REF 51-10-2 PG 1-7 AND 25. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: WEB — CRACKED (ZONE 600) · airframe 42,262 hrs · 26,602 cycles

RIGHT WING O.B. L.E. NR 5 SLAT BN 279, CRACKED LWR. AFT INTERNAL WEB ANGLE AT INBD. SIDE OF ACTUATOR RAM ATACH STRUCTURE REMOVED ACCESS PANEL, INSPECTED FOR CRACKS, VERIFIED MATERIAL, FABRICATED, LOCATED AND DRILLED REPAIR PART. INSTALLED REPAIR, INSTALLED ACESS PANEL. REF SRM 51-30-2 PG 1-10. REF NDT MAN PART 6. 51-00-00 FIG 23, REF SRM 51-40-3 PG 1, REF SRM 51-10- 2 PG 1-10, THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: CHANNEL — CRACKED (BS 423) · airframe 42,262 hrs · 26,602 cycles

E/E DOOR CUT-OUT FWD ANGLE CRACKED BY LATCH REPLACED CUT OUT FWD ANGLE AND RIGGED E/E DOOR REF BOEING DWR 65-16351, SRM 51-30-01 PG 1-10, SRM 51-30-5 PG 3, SRM 51-30-2 PG 2/3, AMM 51-20-151 PG 1-6, AMM 20-60-001 PG10, MM 52-40-011 PG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: PANEL — DELAMINATED (NR 3 SLAT) · airframe 42,262 hrs · 26,602 cycles

NR 3 SLAT UNDERWING PANEL NR 6224 HAS AREA OF DELAMINATION REPAIRED PANEL 6224 REF SRM 51-40-9 STEPS 3D, 4E, 4F PG3-7 AND AMM 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SKIN — CORRODED (BS 680-682) · corrosion level 2 · airframe 42,262 hrs · 26,602 cycles

C1 PIT BILGE AREA-STR 28R STA 680 LEVELING COMPOUND BULGING WITH CORROSION ON SKIN. REMOVED DAMAGED COMPOUND. FOUND CORROSION AT SKIN AND NDT FOR LIMITS ORIGINAL "T" .070 LOSS AT LOWEST POINT IS .034, REMAINING T IS .036 IS OUT OF LIMITS REF SRM 53-30-3. REMOVED DAMAGE AREA REF SRM 53-30-3 FIG 3A. FABRICATED AND VERIFIED REPAIR DOUBLER AS 2024-T3 .080 REF SRM 53-30-2 FIG 3A (A17124/PO NR 1038533). TREATED AND PRIMED REF SRM 51-30-2 PG 7. INSTALLED REF SRM 53-30-3 FIG 3A. RESTORED COMPOUND REF MM 51-40-00-0. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: PANEL — DELAMINATED (ZONE 300) · airframe 42,262 hrs · 26,602 cycles

UPPER TAIL PANEL NR 9607, INNER FOIL DISBONDED REPAIRED TEDLAR COVERING ON INNER SURFACE REF SRM 51-40-9 STEP 11 PG 18. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 305-312) · corrosion level 2 · airframe 42,262 hrs · 26,602 cycles

FWD LAV FLOOR SUPPORT STA 305-312 RBL 42 NUTPLATES RUSTED AND FLOORBEAM CORRODED. REMOVED CORROSION FROM FLOORBEAM, ORIGINAL THICKNESS .070, REMAINING .066. REMOVED .004, FOUND TO BE WITHIN LIMITS, REMOVED CORROSION FROM FLOOR SUPPORT, ORIG THICKNESS.070, REMAINING .035. REMOVED .035, FOUND TO BE OUT OF LIMITS REF SRM 53-10-1 PG 2. TOOL ID AAR 9800 CAL DUE DATE 06/24/09. REMOVED AND REPLACED FLOOR SUPPORT AND "T" CLIP, TREATED AND PRIMED "T" CLIP AND AFFECTED AREAS ON AIRCRAFT REF SRM 51-10-2 PG2. INSTALLED SUPPORT AND T CLIP, REF SRM 51-30-2 PG 2. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FLOOR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 50,447 hrs · 35,587 cycles

MAIN DECK LAV FLOOR WEB PANEL, UPPER LWR SURFACES ARE CORRODED BS 304 - 340, RBL 40 - 60, WL 208. REMOVED CORROSION, ORIGINAL MATERIAL THICKNESS .042 INCH, REMAINING .035', REMOVED .007. FOUND TO BE OUT OF LIMITS REF DRM 53-10-1 PG 2, TOOL ID AAR 9800 CAL DUE 6-28-09. CUT DRAIN OPENINGS IN NEW PANEL, TREATED AND PRIMED, REF SRMM 51-10-2 PG 2, FED EX GMM 7-0-1001 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FRAME — CORRODED (EMERGENCY HATCH) · airframe 42,262 hrs · 26,602 cycles

RT AFT EMERGENCY EXIT HATCH LOWER FRAME OUTER SURFACE HAS CORROSION. REMOVED CORROSION REF SRM 52-00-2 NDT THICKNESS ORIGINAL "T" .063, .005 LOSS, .058, DAMAGE WITHIN LIMITS REF SRM 53-10-1 FIG 1 SHEETS 1, 2, 3. TREATED PRIMED AND PAINTED REWORKED AREAS REF SRM 51-10-2 AND MM 51-20-151-7. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: DOOR — GOUGED (CARGO BAY) · airframe 42,262 hrs · 26,602 cycles

MAIN CARGO DOOR, AFT EDGE LOWER CORNER GOUGED LOWER AFT CORNER GOUGED BEYOND LIMIT. REMOVED DOUBLER FABRICATED NEW DOUBLER, TREATED AND PRIMED. INSTALLED NEW DOUBLER REF 727 P-FSRM 52-30-2 PG 1/2. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: PANEL — CRACKED (ZONE 200) · airframe 42,262 hrs · 26,602 cycles

PANEL 3617 BOTTOM AFT END CRACKED REPAIRED PANEL 3617 REF SRM 51-40-9 STEPS 3D, 4E, 4F, PGS 3-7 AND AMM 51-20-051 PG1, AMM 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,262 hrs · 26,602 cycles

FLOORBOARD, FWD LAV SUPPORT NUT PLATES RUSTED STA 305 - RBL 44. REMOVED FLOOR SUPORT ANGLE, REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. ORIG. MATERIAL THICKNESS .040 INCH. REMAINING .031 INCH REMOVED .009'. FABRICATED NEW ANGLE, PENATRANT INSP FOR CRACKS. NO DEFECTS, TREATED AND PRIMED AND INSTALLED NEW ANGLE REF SRM 51-10-2 PG 2, SRM 51-30-2, SRM 53-10-1 PG 2, TPPL ID AAR 9800 CAL DATED 6- 24-09, BOEING DWG 65-17593-153, THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FRAME — CORRODED (EMERGENCY HATCH) · airframe 42,262 hrs · 26,602 cycles

RIGHT FWD EMERGENCY HATCH FRAME LOWER OUTER SURFACE CORRODED BETWEEN SEAL RETAINER AND SKIN REMOVED CORROSION REF SRM 52-00-2. NDT THICKNESS ORIG "T" .063 LOSS .005 .058. REMAINING DAMAGE WITHIN LIMITS REF SRM 53-10-1 FIG 1 SHEETS 1, 2, 3. TREATED, PRIMED AND PAINTED REWORK REF SRM 51-10-2 AND MM 51-20-151-7. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 50,447 hrs · 35,587 cycles

LEFT WING INBD AFT FLAP, 3RD ATTACH FITTING OUTBD SKIN CRACKED FABRICATED REPAIR PARTS AT LEFT WING T/E AFT FLAP, THIRD ATTACH FITTING O/B SKIN, REF 27-50-4 FIG 11. TREATED, PRIMED AND INSTALLED, REF SRM 51-20-2 PG 1-7, 57-50-04 FIG 11, 51-30-2 PG 2-4. PAINTED REPAIR AREA REF MM 51-20-151-1, THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 305-320) · corrosion level 2 · airframe 42,262 hrs · 26,602 cycles

FLOORBOARD SUPPORT NUTPLATES RUSTED STA 305-312 RBL 55 FWD LAV. REMOVED FLOOR SUPPORT ANGLE, REMOVED CORROSION, FOUND TO BE OUT OF LIMITS ORIG MATERIAL THICKNESS .040, REMAINING .033, REMOVED .007. INSTALLED NEW ANGLE REF SRM 51-30-2 PG 2, SRM 53-10-1 PG 1, BOEING DWG 65-17593-151, TOOL ID AAR 9800 CAL DUE DATE 6/24/09. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,262 hrs · 26,602 cycles

BS 740 BULKHEAD LOWER SURFACE, "T" ANGLE AT RBL 5" WL 146.5 CONNECTION TO DELTA BEAM "T" FLANGE IS CORRODED NEW T ANGLE FABRICATED ON SHOP NON-ROUTINE N00670. REMOVAL AND INSTALLATION ACCOMPLISHED ON N00167. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: ANGLE — CORRODED (BULKHEAD) · corrosion level 2 · airframe 42,262 hrs · 26,602 cycles

BS 740 BULKHEAD LOWER FWD SURFACE, ANGLE LBL 4.5 TO RBL 4.5, WL 146.5 HAS CORROSION ON AFT SURFACE FABRICATED NEW ANGLE REF SRM 51-10-2 PG 2, DWR 65-23555. TREATED AND PRIMED REF 51-10-2 PG 2. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: SUPPORT BRACKET — CORRODED (NLG WW) · corrosion level 2 · airframe 42,262 hrs · 26,602 cycles

CORROSION AROUND BOLT HOLE AT STA 340 FITTING SUPPORT BRACKET JUST BEHIND NOSE WHEEL WELL LT SIDE. REMOVED FITTING SUPPORT AT STA 340 AFT OF NOSE WHEEL WELL LT SIDE. TREATED AND PRIMED NEW SUPPORT FITTING REF SRM 51-30-2 PG 1-20 AND MM 51-20-7. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,262 hrs · 26,602 cycles

LWR AFT CARGO PIT, CORROSION ON UPPER FLANGE OF FRAME AT STA 1090 STR 27L REMOVED CORROSION, ORIGINAL "T" .063, REMOVED .017, REMAINING .046 OUT OF LIMITS. FABRICATED REPAIR DOUBLER FROM 7075-0 .063, HEAT TREAT T6, APPLIED ALODINE, PRIMER AND INSTALLED REPAIR DOUBLER, TIE DOWN REMOVED AND REINSTALLED FOR ACCESS REF SRM 51-40-3 PG 1-6, 51-30-2 PG 8, DRW 65-1634516345-71. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 42,262 hrs · 26,602 cycles

NUMBER 3 CARGO DOOR LOWER FWD "T" CHORD CRACKED AT FASTENERS REPAIRED LOWER FWD "T" CHORD. REMOVED LWR INNER DOOR SKIN REF SRM 51-30-2. FABRICATED REPAIR ANGLES AND FILLER REF SRM 51-40-04 PG 14-16 FIG 3. TREATED AND PRIMED REPAIR PARTS REF SOPM 20-44-04 PG 3 AND 20-43-03 PG 6. INSTALLED REPAIR ANGLES AND FILLER SRM 51-40-04 PG 14-16. INSTALLED LWR INNER DOOR SKIN REF SRM 51-30-02 PG 2 AND 8. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: RETAINER — CORRODED (RT WING) · corrosion level 2 · airframe 42,262 hrs · 26,602 cycles

RT WING REAR SPAR LWR CHORD, APPROX 12" IB OF FWD MLG TRUNNION, SEAL RETAINER CORRODED AT OB END. REMOVED FAIRING AND SEAL RETAINER REF SRM PG 2 LOCATED AND DRILLED NEW SEAL RETAINER REF SRM 51-30-5 PG 1, INSTALLED SEAL RETAINER AND FAIRING REF SRM 51-30-2 PG 2. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SLAT — CRACKED (LT WING) · airframe 42,262 hrs · 26,602 cycles

LT WING NR 4 SLAT FENCE UPPER AFT END COMPOSITE IS CRACKED AND DELAMED. REPAIRED NR 4 SLAT FENCE REF SRM 51-40-9 STEP 7 PG 9 AND AMM 51-20-051-7 PG 1 AND 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: LINE — FAILED (HYD SYSTEM) · airframe 41,479 hrs · 25,981 cycles

AFTER TOUCHDOWN AMD SPOILER DEPLOYMENT, EXPERIENCED LOSS OF "A" HYDRAULIC SYSTEM QUANTITY AND PRESSURE. FOUND BLOWN FLEX LINE ON LT ELEVATOR PCU. PART IS IN STOCK AT SAV. REMOVED AND REPLACED I/B FLEX LINE PER MM27-30-081-4. SERVICED "A" HYD SYS TO FULL PER MM 12-12-000-2. REMOVED AND REPLACED NR 1 AND NR 2 CASE DRAIN FILTERS PER MM 29-11-041-2. REMOVED AND REPLACED "A" SYSTEM PRESSURE FILTERS PER MM 29-11-062-3. RAN NR 1 AND NR 2 ENGINES. NO METAL FOUND IN FILTERS. ALL SYSTEMS OPS AND LEAK CHECK GOOD.

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL FILTER) · airframe 40,588 hrs · 25,200 cycles

AT FL350, AND FUEL TEMPERATURE 5, NR 2 FUEL ICING LIGHT ILLUMINATED. PERFORMED RELEVANT EMERG CK-LIST. DECLARED EMERGENCY. RELEASED FOR SERVICE PER MEL/CDL: 73-04 CATEGORY: C "MEL 73-04. TWO FUEL FILTER DIFFERENTIAL PRESSURE WARNING SYSTEM INOP. REMOVED AND REPLACED NR 2 FUEL FILTER PRESSURE SWITCH PER 727-200 M/M 73-14-021-4. OPS AND LEAK CHECK NORMAL ON ENG RUN.

Part: REPAIR — UNKNOWN (FUSLAGE) · airframe 40,545 hrs · 25,160 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT FS 500 STR.30 WAS ACCOMPLISHED IAW SRM 53-30- 3, FIG. 24 BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION OF THE REPAIR, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE, THICKNESS, GENERAL WORKMANSHIP OF THE REPAIR INSTALLATION, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 40,545 hrs · 25,160 cycles

FOUND PREVIOUSLY INSTALLED REPAIR AT AFT INBD CORNER OF PNEUMATIC GROUND CONNECTION CUTOUT WAS DETERMINED TO BE IAW SR 27-53-024, BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED, EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBER, MATERIAL THICKNESS, TYPE, GENERAL WORKMANSHIP OF PREVIOUS INSTALLATION, REPAIR IS CLASSIFIED AS A MAJOR BASED ON FEDEX GMM 6-2-100.

Part: SWITCH — MALFUNCTIONED (TE FLAPS) · airframe 38,558 hrs · 23,623 cycles

ON FLAP RETRACTION FROM 5 DEG TO 2 DEG, LED NR 5 (RT SIDE) DID NOT FULLY RETRACT. AMBER LIGHT ILLUMINATED ON LED POSITION INDICATOR AFT BULKHEAD. COMPLIED WITH RED TABS, DID NOT CORRECT PROBLEM. REMOVED AND REPLACED NR 5 L/E FLAP POSITION SWITCH IAW MM 27-82-001-4. FLAP/SLAT INDICATION NORMAL WITH NUMEROUS EXTENSION AND RETRACTION.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,356 hrs · 23,455 cycles

FUSELAGE SKIN HAS A DENT, STRINGER 6L, BS 720C. REPAIR DENTED SKIN PER SRM 53-30-3 FIG 3.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,356 hrs · 23,455 cycles

CORROSION (C53-113-01, 2) BULGING SKIN ON STR 28L, BS 1055.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 37,870 hrs · 23,089 cycles

DURING FLAP RETRACTION FROM FLAPS 2 TO FLAPS UP. LED AMBER LIGHT REMAINED ILLUMINATED. POSITION TEST SELECTOR INDICATED NR 2 LED WAS STILL EXTENDED, NR 2 SLAT.

Part: SKIN — CRACKED (VERTICAL STAB)

CRACK IN SKIN, VERTICAL STAB, LEFT SIDE, STR 10, BOTTOM OF STAB. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 55-30-3 AND FEDEX EA 7-5510-56226.

Part: FRAME — DENTED (FUSELAGE)

FRAME IS DENTED AT BS 520, STRINGER 22 RT. *S/D* REMOVED, REPLACED AND FAB PER FEDEX SRM 51-40-3.

Part: DOUBLER — GOUGED (DOOR FRAME)

MAIN CARGO DOOR AFT FRAME BS 620 IS GOUGED AT PREVIOUS REPAIR. INGD RADIUS APPROX 21 INCHES UP FROM THE BOTTOM EDGE. *S/D* REMOVED, REPLACED AND FAB PER IAW FEDEX SRM 51-40-3. PREVIOUS REPAIR. INSTALL REPAIR DOUBLER PER IAW FEDEX SRM 51-30-2.

Part: STRINGER — CRACKED (FUSELAGE)

NR 420 CRACK AT STR 15 RT SIDE BS 720B+4 FWD OF EXT LIGHT. ** S/D ** COMING

Part: KEELBEAM — CORRODED (FUSELAGE)

CORROSION ON LT KEELBEAM AT BS 960 O/B FLANGE AROUND FASTENERS. ** S/D ** COMING

Part: STRINGER — CRACKED (FUSELAGE)

CRACK AT STR 15 LT SIDE BS 720C-4 AFT OF EXT LIGHT. ** S/D ** R&R PER IAW FEDEX SRM 53-10-3 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE)

NR 419 CRACK AT STR 15 LT SIDE BS 720D+4 FWD OF EXT LIGHT. ** S/D ** R&R PER IAW FEDEX SRM 53-10-3 FIG 1.

Part: STRINGER — DAMAGED (FUSELAGE)

NR 319 TEN OPEN FASTENER HOLES ON SIDE OF STRINGER 24 LT AT BS 480. ** S/D ** R&R & FAB PER FEDEX SRM 53-10-3, 53-10-3.

Part: SWITCH — OUT OF ADJ (RT MLG DOOR)

RT MG DOOR REMAIN ILLUM AFT GEAR RETRACTION GOES OUT IN UP POSITION. *S/D* ADJUSTED RT GEAR DOOR SWITCH PER 2 B (2) OF MM 32-62-11-4.

Part: BELLFRAME — DAMAGED (BS 1010)

NR 0546 - LOWER AFT CARGO COMP FS 1010 BELLFRAME BETWEEN STRINGERS 25L AND 26L CREASED. REMOVED DAMAGED AREA. FABRICATED DOUBLERS, TREATED, PRIMED AND INSTALLED DOUBLER AND FILLER PER SRM 53-10-4.

Part: STRINGER — CORROSION (BS 720)

CORROSION (C53-111-01-2), ON STR 28L BS 720 PLUS 4 WL 149. REMOVED, FABRICATED AND REPLACED STR 28L BS 720 PLUS 4 WL 149 IAW FEDEX SRM 53-10-2 AND 53-10-3.

Part: FLOORBEAM — CORROSION (BS 460)

CORROSION ON FLOORBEAM BS 460 RBL 10 AND 15 WL 208. REPAIRED FLOORBEAM AT BS 460 RBL 10 TO 15 WL 208. ALL WORK DONE IAW FEDEX EA 7-5310-26943.

Part: FLOORBEAM — CORROSION (BS 1130)

CORROSION (C53-11-01 AND -3), ON LOWER CHORD OF FLOORBEAM AT NUTPLATE HOLES BS 1130 FROM RBL 50 TO LBL 38 WL 200. REMOVED CORROSION, FABRICATED REPAIR ANGLE PER EA 7-5310-26949.

Part: SKIN — DAMAGED (BS 710)

BS 710 LBL 6 WL 149 FOUND DEEP GOUGE AT FASTENER HOLE ON EXTERIOR SKIN WHILE WORKING NR 0413. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-30-3.

Part: STRINGER — CRACKED (VERT FIN)

VERTICAL FIN STA 110, STR 8L IS CRACKED, BAY NR 6. REPAIRED CRACKED STRINGER PER SRM 55-30-4.

Part: SKIN — DENTED (BS 1050-1056)

FIVE DENTS IN SKIN 1050 TO 1056 STR 28 TO 29R. REPAIRED SKIN IAW FEDEX SRM 53-30-3.

Part: SKIN — DAMAGED (BS 1073)

BS 1073 STR 19 TO 20L THERE IS A SHARP CREASE IN SKIN. REMOVED DAMAGE AT BS 1073 STR 19 TO 20L IN SKIN. FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3.

Part: FRAME — DENTED (BS 700)

DENTS IN FRAME BS 700 RBL 34 TO 44 WL 160. REPAIRED DENTED FRAME AT BS 700 RBL 34 TO 44 WL 160 IAW FEDEX SRM 51-40-3.

Part: SKIN — DENTED (BS 1050-1056)

FIVE DENTS IN SKIN STA 1050 TO 1056, STR 28 TO 29R. REPAIRED SKIN IAW FEDEX SRM 53-30-3.

Part: SKIN — CREASED (BS 1030-1050)

BS 1030 TO 1050, STR 20 TO 21L SKIN IS CREASED. REMOVED DAMAGE AT BS 1030 TO 1050, STR 20 TO 21L IN SKIN. FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3.

Part: STRINGER — DAMAGED (BS 460)

GOUGE ON STRINGER AT BS 460 STR 3R. REMOVED DAMAGED SECTION STR 3R BS 460, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-3.

Part: STRINGER — DAMAGED (BS 620)

MECHANICAL DAMAGE IN HAT SECTION OF STRINGER, AT BS 620 STR 4R. REMOVED DAMAGED SECTION STRINGER 4R BS 620, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-3.

Part: SKIN — CREASED (BS 1073)

BS 1973 STR 19 TO 20L, THERE IS A SHARP CREASE IN SKIN. REMOVED DAMAGE AT BS 1073 STR 19 TO 20L IN SKIN. FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3.

Part: STRINGER — CORROSION (BS 720)

CORROSION (53-111-01-2), ON STR 28L BS 720 PLUS 4 WL 149. REMOVED, FABRICATED AND REPLACED STR 28L BS 720 PLUS 4 WL 149 IAW FEDEX SRM 53-10-2 AND 53-10-3.

Part: SEAT TRACK — CORRODED (BS 480)

CORROSION (C53-224-01), ON SEAT TRACK BS 480 RBL 25 WL 208. REMOVED SECTION OF TRACK, FABRICATED NEW SECTION AND INSTALLED PER SRM 53-10-5.

Part: SKIN — DELAMINATED (LT TE AFT FLAP)

LT WING O/B AFT FLAP DELAMINATED 14 INCHES FROM O/B END T/E. REPAIRED PER SRM 51-40-06.

Part: TE SKIN — DELAMINATED (LT TE FOREFLAP)

LT WING I/B FOREFLAP I/B TRAILING EDGE HAS DELAMINATED AREA, MARKED. REPAIRED PER SRM 51-40-6.

Part: FRAME — DENTED (BS 500)

DENT IN FRAME BS 500 LBL 34 TO 46 WL 160.

Part: SKIN — DISBONDED (RT TE FOREFLAP)

RT WING I/B FOREFLAP I/B END HAS DISBONDED RUBSTRIP UPPER SURFACE. REPAIRED PER SRM 51-40-06.

Part: SKIN — DAMAGED (BS 480-560)

AREA OF SKIN DAMAGE STA 480 TO 560 STR 26 LT AND RT LOWER SKIN PANEL INCLUDING 2 DENTS STA 498 AND 503 BETWEEN STR 26 TO 27R, MARKED. BLENDED AREA OF SKIN DAMAGE STA 480 TO 560 STR 26 LT AND RT LOWER SKIN PANEL. FOUND TO BE WITH LIMITS EXCLUDING TWO AREAS. ONE AT STA 500 RBL 14 AND ONE AT STA 490 RBL 22 PER FEDEX SRM 53-30-1. REPAIRED BOTH AREAS PER FEDEX SRM 53-30-3.

Part: FRAME — DENTED (BS 700)

DENTS IN FRAME BS 700 LBL 34 TO 44 WL 160. REMOVED DAMAGE AND FABRICATED REPAIR PARTS PER SRM 51-40-3.

Part: FRAME — DENTED (BS 500)

DENTS IN FRAME BS 500 RBL 34 TO 44 WL 160. CUT OUT DAMAGE REPAIRED FRAME BS 500 RBL 34 TO 44 WL 160 PER FEDEX SRM 51-40-3.

Part: BEAM — CORROSION (BS 268)

CORROSION (C53-221-01), ON 25G BEAM AT BS 268 LBL 7 WL 08.1. REMOVED AND REPLACED 25G BEAM PER SRM 53-10-01.

Part: FRAME — DENTED (BS 680)

DENTS IN FRAME BS 680 LBL 34 TO 45 WL 160. CUT OUT DAMAGE ON FRAME BS 680 LBL 34 TO 45 WL 160, FABRICATED AND INSTALLED REPAIR PER FEDEX SRM 51-40-3.

Part: TE WEDGE — DELAMINATED (RT AILERON)

RT WING O/B AILERON T/E WEDGE DELAMINATED AT O/B END. REPAIRED PER SRM 51-40-6.

Part: SKIN — DAMAGED (BS 1030-1050)

BS 1030 TO 1050 STR 20 TO 21L SKIN IS CREASED. REMOVED DAMAGE AT BS 1030 TO 1050 STR 20 TO 21L IN SKIN. FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3.

Part: FRAME — GOUGE (BS 360)

FOUND GOUGE IN FRAME STA 360 WL 156 LBL 40, BETWEEN STR 24 TO 25 LT, E-BAY. REMOVED DAMAGE AND FABRICATED PART. REPAIRED PER SRM 51-40-3 AND 53-10-2.

Part: SKIN — DAMAGED (BS 480-560)

AREA OF SKIN DAMAGE STA 480 TO 560 STR 26 LT TO RT LOWER SKIN PANEL INCLUDING 2 DENTS STA 496 AND 503 BETWEEN STR 26-27R, MARKED. BLENDED AREA OF SKIN DAMAGE STA 480 TO 560 STR 26 LT AND RT LOWER SKIN PANEL. FOUND TO BE WITHIN LIMITS EXCLUDING 2 AREAS. ONE AT STA 500 RBL 14 AND 1 AT STA 490 RBL 22 PER FEDEX SRM 53-30-1, REPAIRED BOTH AREAS PER FEDEX SRM 53-30-3.

Part: FRAME — DENTED (BS 580)

DENTS IN FRAME BS 580, LBL 37 - LBL 46, WL 160. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER AT BS 580, LB 37 - LB 46, WL 160 PER FEDEX SRM 51-40-3.

Part: FRAME — GOUGED (BS 720)

GOUGE IN FRAME AT BS 720B, LT BETWEEN STR 15 AND STR 14. GOUGE IN FRAME AT BS 720B, LT BETWEEN STR 15 AND STR 14 WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1 AND WAS REPAIRED PER FEDEX SRM 51-40-3.

Part: FRAME — DENTED (BS 500)

DENT IN FRAME BS 500 LBL 34 TO 46 WL 160. CUT OUT DENT, FABRICATED REPAIR DOUBLER, CLEANED, TREATED PART AND FRAME. INSTALLED REPAIR DOUBLER PER FEDEX SRM 51-40-3.

Part: FRAME — DENTED (BS 520)

DENTS IN FRAME BS 520 LBL 37 TO 46 WL 160. DENTS IN FRAME AT BS 520 LBL 37 TO 46 WL 160 WERE FOUND TO BE OUT OF LIMITS PER FEDEX SRM 51-10-1. REPAIRED FRAME PER FEDEX SRM 51-40-3.

Part: FRAME — DENTED (BS 700)

DENTS IN FRAME BS 700 RBL 34 TO 44 WL 160. REPAIRED DENTED FRAME AT BS 700 RBL 34 TO RBL 44 WL 160 IAW FEDEX SRM 51-40-3.

Part: FRAME — DENTED (BS 600)

DENTS IN FRAME BS 600 LBL 34 TO 46 WL 160. REPAIRED DENTS IN FRAME BS 600 LBL 34 TO 46 WL 160 PER FEDEX SRM 51-40-3.

Part: FRAME — GOUGE (BS 720)

GOUGE IN FRAME AT BS 720B LT BETWEEN STR NR 14 TO NR 15, WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 51-40-3. REMOVED AND REPLACED FABRICATED DOUBLER AND INSTALLED PER SRM 51-40-3.

Part: FRAME — DENTED (BS 660)

DENTS IN FRAME BS 660 LBL 34 TO 46 WL 160. REPAIRED DENTED FRAME BS 660 LBL 34 TO 46 WL 160 IAW FEDEX SRM 51-40-3.