N118FE

Part: STRUCTURE — NO DISCREPANCY (ZONE 200) · airframe 21,866 hrs · 7,729 cycles

WE HEARD A LOUD BANG IN FLIGHT AT THE TOP OF DESCENT. THE SAME NOISE OCCURRED SEVERAL MORE TIMES AT THE BEGINNING OF EACH DESCENT. UPON INSPECTION AFTER LANDING, THE DEMI CAN IN POSITION 7D WAS NOT PROPERLY SECURED AND IT WAS SLIDING BACK AND FORTH DURING FLIGHT. WE LANDED UNEVENTFULLY. IAW AMM: 25-57-00-1-2 AMM: 25-57-01-4 AMM: 25-52-00-6 VISUAL INSPECTION OF MAIN DECK CARGO COMPARTMENT AT POSITION 6D AND 7D. NO DAMAGE NOTED ON FLOOR TRACK AND CARGO HANDLING COMPONENTS. SIDEWALL LINERS ALSO HAS NO DAMAGE. OPS CHECK OF LOCKS FOUND SATIS. AFFECTED CONTAINER AND ADJACENT CONTAINERS HAVE NO DAMAGE. ACFT OK FOR SERVICE.

Part: VALVE — FAILED (HYD SYSTEM) · airframe 18,786 hrs · 6,460 cycles

WHILE WE WERE AWAITING TAKEOFF CLEARANCE WITH THE PARKING BRAKE SET, RECEIVED A MASTER CAUTION WITH A R HYD QTY EICAS MESSAGE FOLLOWED BY A R HYD PRIM PUMP EICAS MESSAGE. ACTIVATED THE STATUS PAGE AND WITNESSED THE RIGHT HYDRAULIC RESERVOIR QUANTITY DROP TO ZERO. ADVISED ATC AND CLEARED THE RUNWAY. COMPLIED WITH THE QRH, ADVISED GOC , RETURNED TO THE GATE. R & R SELF RESETING FUSE VALVE IAW AMM 32-42-02-4. RIGHT HYD SYS FILLED TO FULL IAW AMM 12-12-01-3 & PERFORMED HYD SYS PRESSURIZED ON ALL SYS IAW AMM 29-11-00-2 READ NORMAL WITH NO LEAK NOTED, PERFORMED RIGHT ENGINE RAN UP CHECK IAW JRH WITH ALL PARAMETER READ NORMAL IAW AMM 71-00-00-2-3. NO EICAS MESSAGE RELATED FOUND. ACFT OK FOR SERVICE.

Part: CIRCUIT CARD — INOPERATIVE (LANDING CONFIG) · airframe 18,293 hrs · 6,280 cycles

SPEED BRAKES SEGMENT LIGHT & SPREED BRAKES EXT EICAS MESSAGE ILLUMINATED AFTER TAKEOFF BELOW 1000FT. AFTER ARRIVAL, ACFT CAUTION MSG EICAS & SPEED BRAKES ANNUNCIATOR LIGHT ILLUM. R & R LANDING CONFIG WARNING CARD (M983) OPS TEST OK IAW AMM 31-51-04-4. CONFIRMED SPEED BRAKES ANNOUNCIATOR LIGHT NOT ILLUM & OPS TEST SPEED BRAKE LEVER W/ SPOILER PANEL POSITION IAW AMM 27-61-00-5. SPEEDBRAKE CAUTION IND SYS - INOP." MEL: 27-62-02. PEFORMED SPOILER CONTROL MODUE BITE PROCEDURE IAW FIM 27-09 FT 808. NO FAULTS. PERFORMED LANDING & TAKEOFF CONFIGURATIN WARNING CARD MODULE TEST IAW AMM 31-51-04-4. TEST PASSED. PERFORMED SPEEDBRAKE CONTROL SYS OPS TEST IAW AMM 27-61-00-5. TEST NORMAL. A/C OK FOR SERVICE.

Part: ACCESS DOOR — CRACKED (ZONE 800) · airframe 17,908 hrs · 6,173 cycles

LOWER HALF OF FUSELAGE, ACCESS DOOR 113AL WITH A BIRD STRIKE ON EXTERNAL SURFACE. THE DAMAGE AT EXTERNAL SURFACE IN ACCESS DOOR 113AL WAS REPAIRED. I.A.W. DRAWING 141T6401 REV.L I.A.W. SRM 51-40-02-0G REV.87 AUG 15,2023.

Part: SKIN — DAMAGED (ZONE 100) · airframe 17,908 hrs · 6,173 cycles

LOWER HALF OF FUSELAGE, BETWEEN STA 132.5 AND 143.5, AND BETWEEN STGR 30-L AND STGR 31-L, BIRD STRIKE. DAMAGE AT LOWER HALF OF FUSELAGE, BETWEEN STA 132.5 AND BETWEEN STGR 50-L AND STGR 31-L, WAS REPAIRED I.A.W. E.A.:# H-5330-T0377078 PART: 1(P1) RELEASE DATE: NOV 23, 2023

Part: SKIN — CRACKED (ZONE 200) · airframe 17,908 hrs · 6,173 cycles

UPPER HALF OF FUSELAGE, BETWEEN STA 132.5 AND STA 143.5, AND BETWEEN STGR 14-L AND STGR 18-L, BIRD STRIKE. DAMAGE AT UPPER HALF OF FUSELAGE, BETWEEN STA 132.5 AND STA 143.5, AND BETWEEN STGR 14-L AND STGR 18-L WAS REPAIRED. I.A.W. E.A.#: H-5330- T0377062 PART: 1 (P1) RELEASE DATE: NOV 23,2023.

Part: SKIN — DENTED (ZONE 100) · airframe 17,908 hrs · 6,173 cycles

LOWER HALF OF FUSELAGE, BETWEEN STA 135.5 AND STA 148.5, AND BETWEEN STGR 21R AND STGR 30R, BIRD STRIKE. DAMAGE AT LOWER HALF OF FUSELAGE, BETWEEN STA 135.5 AND STA 148.5, AND BETWEEN STGR 21R AND STGR 30R WAS REPAIRED. I.A.W. E.A.#: H-5330-T0377079 PART: 1 (P1) RELEASE DATE: NOV 23,2023.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 17,303 hrs · 5,978 cycles

ESCAPE ROPE FOR CREW ENTRY DOOR IS PARTIALLY OUT OF ITS POCKET JAMMING THE DOOR. REINSTALLED EMERGENCY ECSAPE ROPE AS REQUIRED IAW MM 25-61-04-2-1. OK FOR SERVICE

Part: FLAP — UNKNOWN (UNKNOWN) · airframe 16,573 hrs · 5,777 cycles

FOUND DENT ON RH INBOARD TRAILING EDGE FLAP TOPSIDE. REPAIRED RT WING- INBOARD FLAP UPPER SKIN TOP SURFACE TRAILING EDGE DENT AT LOCATION INBD FLAP TRAILING EDGE TOP SURFACE 39 INCHES FROM INB EDGE 9.5 INCHES WITH A 2 IN. CIRCLE REPAIR, IN REF. TO 767 SRM 57-53-01-2R AND 767 SRM 51-70-10-2R. SEE JPF FOR OTHER WORK ACOMPLISHED. (COMPLIED WITH EA# H-57-50-T0374025 P1) THIS IS CONSIDERED MAJOR REPAIR.

Part: SLAT — DENTED (ZONE 600) · airframe 14,926 hrs · 5,188 cycles

RH WING SLAT # 8 WITH 11 DENTS IN UPPER WEDGE AREA RH WING SLAT # 8 WITH 14 DENTS WERE EVALUATED AND FOUND WITHIN LIMITS IAW SRM MAXIMIM DIMENSION L= 1.600" W=0.600". DENT ON OSS 445.35 WAS REPAIRED IAW B767 SRM 57- 43-02-1A PAG. 1-6 FIG. 101 (SHEET 3) NOTE K REV. 82 DEC15/2021 AND B767 SRM 57-43-02-R1 PAG. 201-202 AND B767 SRM 51-70-10-2R PAG. 150 FIG. 201 REV. 82 DEC15/2021

Part: SLAT — DENTED (ZONE 500) · airframe 14,926 hrs · 5,188 cycles

LEFT WING SLAT NO 5 DENT IN UPPER WEDGE AREA WS. 433.1 LEFT WING SLAT NO 5 DENT IN UPPER WEDGE AREA WS 433.1 THAT WAS REPAIRED I.A.W. SRM 57- 43-02-2R FIG. 201 SHEET 1 AND SRM B767 51-70-10-2R PAGE 149, 157 FIG. 202 SHEET 3 REV. 82 DEC15/2021

Part: FLAP — DELAMINATED (ZONE 600) · airframe 14,926 hrs · 5,188 cycles

RIGHT WING OUTBOARD FLAP LEADING EDGE WITH DELAMINATION WBL: 414. RIGHT WING OUTBOARD FLAP LEADING EDGE WBL 414 WAS REPAIRED IAW B767 SRM 57-53-01-2R REP. 1 PAG. 1-9 FIG. 201 (SHEET 5) TABLE I AND B767 SRM 51-70-17-0G PAR. 4.A. FIG. 10 REV. 82 DEC15/2021

Part: FORMER — CRACKED (N/A) · airframe 14,605 hrs · 5,091 cycles

CRACKED FORMER ON LS PN: 114T2170-5/WITH ANGLE 114T 2171-4; LOOSE/DAMAGED FASTENERS LOCATED AT LS FLE OSS 441 ALSO. 0000452710 : ROSNER, DANIEL D - 17-APR-2022 03:18 REMOVED THE DAMAGED FORMER AND ANGLE LOCATED AT LH WING STATION OSS 441.596. AND INSTALLED NEW FORMER AND ANGLE. REFERENCED E.A TH-5720-T0368056P1.

Part: SLAT — GOUGED (ZONE 600) · airframe 11,381 hrs · 4,297 cycles

RIGHT WING #8 SLAT, UPPER TRAILING EDGE, LOWER FACE IS GOUGED AT OUTBOARD AUX TRACK. REPAIRED RIGHT WING #8 SLAT UPPER TRAILING EDGE LOWER FACE GOUGED AT OUTBOARD AUX TRACK IAW B767 SRM 57-43- 02-2R-1 DETAIL 1 AND SRM 51-70-10-2R REPAIR GENERAL

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 11,381 hrs · 4,297 cycles

MAIN DECK FLOOR PANEL 242SFF IS PUNCTURED & HAS EDGE DAMAGE REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2R

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 11,381 hrs · 4,297 cycles

MAIN DECK FLOOR PANEL 241KFF IS PUNCTURED REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2R

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 11,381 hrs · 4,297 cycles

MAIN DECK FLOOR PANEL 241FFF DENTED REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2R

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 11,381 hrs · 4,297 cycles

MAIN DECK FLOOR PANEL 242UFF IS DELAMINATED ON FWD END REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2R

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 11,381 hrs · 4,297 cycles

MAIN DECK FLOOR PANEL 241BFF HAS DAMAGED INSERT REMOVED & REPLACED INSERT IAW B767 SRM 53-00-50-2R & FEDEX DRAWING SRZ-25-005, REV R

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 11,381 hrs · 4,297 cycles

MAIN DECK FLOOR PANEL 241YFA IS PUNCTURED & HAS EDGE DAMAGE REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2R

Part: STRAP — CRACKED (LT WING LE) · airframe 11,381 hrs · 4,297 cycles

LEFT WING LEADING EDGE SPLIC STRAP IS CRACKED REMOVED & REPLACED STRAP IAW BAC DWG 114T2800 REV C

Part: SHEAR TIE — CRACKED (NR 2 NACELLE) · airframe 11,381 hrs · 4,297 cycles

#2 PYLON, INBD SHEAR TIE @ NAC STA 303 IS CRACKED REMOVED & REPLACED SHEAR TIE IAW BAC DWG 313T2310 REV -

Part: STRAP — CRACKED (RT WING LE) · airframe 11,381 hrs · 4,297 cycles

RH WING LEADING EDGE SPLICE STRAP IS CRACKED REMOVED & REPLACED STRAP IAW BAC DWG 114T2800 SHT 6 REV C

Part: HEAT SHIELD — CRACKED (APU BAY) · airframe 11,381 hrs · 4,297 cycles

TAIL SECTION , INTERNAL , APU BLEED AIR DUCT HEAT SHIELD IS CRACKED AT THE UPPER AFT ATTACH FASTENER HOLE IN THE L/H STABILIZER TORSION BOX AREA BELOW THE THS JUST AFT OF STA 1725.5 REPAIRED DAMAGE ON HEAT SHIELD IAW EA# H-3610-T0360506

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 11,381 hrs · 4,297 cycles

L/H NOSE TUNNEL MAIN CABIN FLOOR SUPPORT STRUCTURAL VERTICAL ANGLE IS CRACKED AT STA 246 APROX LBL50 REMOVED AND REPLACED ANGLE IAW BAC DRAWING 141T5146, REV B

Part: FLOOR SUPPORT — CRACKED (BS 1087) · airframe 11,381 hrs · 4,297 cycles

AFT PIT , FWD OF AFT COMP. STA 1087 RBL20 FLOOR SUPPORT STRUCTURE VERTICAL ATTACH CLIP UPPER SIDE IS CRACKED REMOVED AND REPLACED AFT PIT , FWD OF AFT COMPT. STA 1087 RBL20 FLOOR SUPPORT STRUCTURE VERTICAL ATTACH CLIP

Part: TUBE — CRACKED (DOOR COUNTER BAL) · airframe 11,381 hrs · 4,297 cycles

BULK DOOR COMPARTMENT DOOR COUNTER BALANCE SPRING TUBE IS CRACKED REMOVED AND REPLACED BULK DOOR COUNTER BALANCE SPRING TUBE PER B767 AMM 52-36- 02-5

Part: ATTACH ANGLE — CRACKED (BS 1087) · airframe 11,381 hrs · 4,297 cycles

AFT PIT, FWD OF PIT STA 1087 LBL20 FLOOR SUPPORT STRUCTURE VERTICAL ATTACH ANGLE UPPER SIDE IS CRACKED REMOVED AND REPLACED AFT PIT , FWD OF AFT PIT STA 1087 LBL20 FLOOR SUPPORT STRUCTURE VERTICAL ATTACH ANGLE

Part: SHEAR TIE — CRACKED (NR 1 NACELLE) · airframe 11,381 hrs · 4,297 cycles

NO.1 PYLON, INBD SIDE, NAC STA 303 HAS CRACKED SHEAR TIE REMOVED & REPLACED SHEAR TIE IAW BAC DWG 313T2310

Part: SHEAR TIE — CRACKED (NR 1 NACELLE) · airframe 11,381 hrs · 4,297 cycles

NO.1 PYLON, INBD SIDE, NAC STA 303 SHEAR TIE IS CRACKED REMOVED & REPLACED SHEAR TIE IAW BAC DWG 313T2310

Part: PANEL — CRACKED (LT WING FUEL) · airframe 11,381 hrs · 4,297 cycles

LEFT WING, LEADING EDGE , FUELING PANEL 521 QB , WEB IS CRACKED REPAIRED WEB BEHIND 521 QB IAW B767 SRM 57-41-13-2R , B767 SRM 51-20-01 AND B767 AMM 52-49- 04-4

Part: FORMER — CRACKED (LT WING) · airframe 11,381 hrs · 4,297 cycles

LEFT WING NOSE FORMER & ANGLE CRACKED @ OSS 441 REMOVED & REPLACED FORMER & ANGLE ASSY IAW BAC DWG 114T2241REV - & FEDEX EA H- 5720-T0360399-P1

Part: FORMER — CRACKED (LT WING LE) · airframe 11,381 hrs · 4,297 cycles

LH WING LEADING EDGE NOSE FORMER IS CRACKED @ OSS 499 REMOVED & REPLACED FORMER IAW BAC DWG 114T2161 REV - & FEDEX EA H-5720-T0360398-P1

Part: BRACKET — CRACKED (RT WING DOOR) · airframe 11,381 hrs · 4,297 cycles

RIGHT WING FUELING STATION DOOR LIGHT HOUSING BRACKET IS CRACKED REMOVED & REPLACED BRACKET IAW B767 AMM 52-49-04

Part: FRAME ANGLE — CRACKED (NR 1 NACELLE) · airframe 11,381 hrs · 4,297 cycles

#1 PYLON, NAC STA 377, OUTBD FRAME CLIP IS CRACKED REMOVED & REPLACED CLIP IAW BAC DWG 313T3380 REV F

Part: FRAME ANGLE — CRACKED (NR 2 NACELLE) · airframe 11,381 hrs · 4,297 cycles

#2 PYLON, NAC STA 377, OUTBD FRAME CLIP IS CRACKED REMOVED & REPLACED CLIP IAW BAC DWG 313T3380 REV F

Part: FRAME ANGLE — CRACKED (NR 2 NACELLE) · airframe 11,381 hrs · 4,297 cycles

#2 PYLON, NAC STA 377, INBD SIDE, FRAME CLIP CRACKED REMOVED & REPLACED CLIP IAW BAC DWG 313T3380 REV F

Part: FRAME ANGLE — CRACKED (NR 1 NACELLE) · airframe 11,381 hrs · 4,297 cycles

#1 PYLON, NAC STA 377, INBD FRAME CLIP IS CRACKED REMOVED & REPLACED CLIP IAW BAC DWG 313T3380 REV F

Part: BRACKET — CRACKED (RT WING) · airframe 11,381 hrs · 4,297 cycles

RH WING TORQUE TUBE GUIDE BRACKET CRACKED @ LES 285 REMOVED & REPLACED BRACKET IAW BAC DWG 114T1240 REV -

Part: BRACKET — CRACKED (LT WING) · airframe 11,381 hrs · 4,297 cycles

LH WING TORQUE TUBE GUIDE BRACKET CRACKED LES 285 REMOVED & REPLACED BRACK IAW BAC DWG 114T1240 REV -

Part: ROD — DAMAGED (NR 2 BRAKE) · airframe 10,304 hrs · 3,964 cycles

DURING ACCOMPLISHMENT OF FEA H-3243-F0356064, FOUND #2 MLG BRAKE ROD NEED TO BE DISASSEMBLE AND PROPERLY REASSEMBLE TO BRAKE ATTACHMENT JOINT DISASSEMBLED AND REASSEMBLED #2 MLG BRAKE ROD TO BRAKE ATTACHMENT JOINT REF AMM 32-11-20-4-4. A/C OK TO CONTINUE.

Part: ROD — DAMAGED (NR 5 BRAKE) · airframe 10,304 hrs · 3,964 cycles

DURING ACCOMPLISHMENT OF FEA H-3243-F0356064, FOUND #5 MLG BRAKE ROD NEED TO BE DISASSEMBLE AND PROPERLY REASSEMBLE TO BRAKE ATTACHMENT JOINT DISASSEMBLED AND REASSEMBLED #5 MLG BRAKE ROD TO BRAKE ATTACHMENT JOINT REF AMM 32-11-20-4-4. A/C OK TO CONTINUE.

Part: ROD — DAMAGED (NR 4 BRAKE) · airframe 10,304 hrs · 3,964 cycles

DURING ACCOMPLISHMENT OF FEA H-3243-F0356064, FOUND NR 4 MLG BRAKE ROD NEED TO BE DISASSEMBLE AND PROPERLY REASSEMBLE TO BRAKE ATTACHMENT JOINT. DISASSEMBLED AND REASSEMBLED THE NR 4 MLG BRAKE ROD TO BRAKE ATTACHMENT JOINT IAW AMM 32-11-20-4-4. ACFT OK TO CONTINUE.

Part: ROD — DAMAGED (NR 6 BRAKE) · airframe 10,304 hrs · 3,964 cycles

DURING ACCOMPLISHMENT OF FEA H-3243-F0356064, FOUND #6 MLG BRAKE ROD NEED TO BE DISASSEMBLE AND PROPERLY REASSEMBLE TO BRAKE ATTACHMENT JOINT DISASSEMBLED AND REASSEMBLED #6 MLG BRAKE ROD TO BRAKE ATTACHMENT JOINT REF AMM 32-11-20-4-4. A/C OK TO CONTINUE.

Part: PUMP — MALFUNCTIONED (LT FUEL BOOST) · airframe 9,260 hrs · 3,529 cycles

20 MINUTES INTO FLIGHT GOT FUEL CONFIG ALERT. RETURNED TO KMEM. FUEL NOT FEEDING FROM LEFT TANK. REMOVED AND REPLACED THE L/H AFT BOOST PUMP IN REF. TO B767 AMM. 28-22-032-4. OPS AND LEAK TEST NORMAL.

Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 9,260 hrs · 3,529 cycles

20 MINUTES INTO FLIGHT GOT FUEL CONFIG ALERT. RETURNED TO KMEM. FUEL NOT FEEDING FROM LEFT TANK. CHANGED LEFT AND RIGHT BOOST PUMPS MPN 5006003D. REMOVED AND REPLACE THE LT AFT BOOST PUMP, IN REF TO B767 AMM 28-22-032-4. OPS AND LEAK TEST NORMAL.

Part: SKIN — DAMAGED (BS 1109 S4L) · airframe 9,100 hrs · 3,471 cycles

FUSELAGE HAS IMPACT DAMAGE AT STA 1109 AT STR 4L REPAIRED FUSELAGE SKIN PER E.A. H-5330-T0351626 PART 1.

Part: PUMP — LEAKING (LT ENGINE) · airframe 8,577 hrs · 3,276 cycles

APPROX 2HRS INTO FLT, EICAS ALERT 'L HYD QTY', LT HYD QTY SLOWLY DECREASED FROM ABOVE 0.9 TO 0.01 WITH 'RF' INDICATED. EICAS ALERT 'HYD PRIM PUMP' DISPLAYED SHORTLY THEREAFTER QRH COMPLIED WITH AND LT ENG PRIMARY PUMP SELECTED 'OFF'. LT HYD PRESS STAYED IN NORMAL RANGE WITH LT QTY INDICATING 0.00 ALSO, CREW REPORTED THEY NEVER LOST LT HYD SYSTEM PRESS, IT KEPT CLOSE TO 3000PSI THE WHOLE FLIGHT, WITH 0.01 QTY SHOWN AFTER THEY SHUT DOWN EDP. NOTICED HYD LEAK FROM LT ENG ON ARRIVAL FOUND HYDRAULIC FLUID DRIPING FROM LEFT HAND ENGINE EDP CASE DRAIN PIPE AT ENGINE DRAIN MAST. REMOVED AND REPLACED EDP IAW AMM 29-11-05-4-4. FOUND DRIVE SHAFT SHEARD OFF INSIDE (SEE PICTURES). ALSO REPLACED BOTH CASE AND PRESSURE FILTERS IAW AMM 29-11-17-4-0. BOTH FILTERS INSPECTED, NO METALIC DEBRI OR PARTICULES FOUND. ALSO INSPECTED GEARBOX FOR EVIDENCE OF DAMAGE NO FINDINGS. CRANKED LEFT ENGINE, NO LEAK DETECTED. RAN LEFT ENGINE DISCOVERED LARGE LEAK DRAINING FROM RACEWAY BOX, OPENED RACEWAY BOX, CRANKED ENGINE FOUND LARGE LEAK AT FWD LINE LOWER PORTION, SLEEVE CRIMPED ON THE LINE CAME LOOSE. LINE SHOULD BE REPLACED BUT NIS CDG REMOVED AND REPLACED FWD TUBE LOWER PORTION IAW AMM 20-10-09-4. CRANKED LEFT ENGINE IAW JET RUN-UP HANBOOK, NO LEAK DETECTED. RAN LEFT ENGINE NO LEAK DETECTED.

Part: WEDGE — GOUGED (LT WING SLAT) · airframe 8,416 hrs · 3,227 cycles

LEFT WING #5 SLAT TRAILING EDGE WEDGE GOUGED REPAIRED DAMAGED IAW EA# H-2780-T0348663 - P1 FLIGHT CONTROL- L/E SLATS-#5 SLAT, TRAILING EDGE SKIN- GOUGE GOUGE-RSC SRM REPAIR TRACKING

Part: WEDGE — CHAFED (RT WING SLAT) · airframe 8,416 hrs · 3,227 cycles

RIGHT WING #8 SLAT TRAILING EDGE WEDGE CHAFFED REPAIRED DAMAGE IAW EA# H-2780-T0348645 FLIGHT CONTROLS - L/E SLATS & FLAPS - NO. 8 SLAT, RSC SRM REPAIR TRACKING.

Part: PROXIMITY SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 4,282 hrs · 1,687 cycles

EICAS ALERT FWD CARGO DOOR IN CRUISE AT FL330. OVERHEAD LIGHT FOR THE CARGO DOORS ALSO ILLUMINATED. DIVERTED. TROUBLESHOT IAW FIM 52-71, FIG 104, PSEU BITE CHECK, NO FAULTS APPEARED. LATCH, LOCK, AND LATCH HANDLE MECHANISM IN GOOD CONDITION AND NO ABNORMALITIES FOUND. ADJUSTED CLEARANCE OF THE S893 PROXIMITY SWITCH IAW AMM 52-71-00-5. OPS CHECKED GOOD.. ACFT OK FOR SERVICE.

Part: DOOR — UNSECURE (ESCAPE ROPE) · airframe 3,387 hrs · 1,343 cycles

FIRST OFFICER`S EMERGENCY ESCAPE ROPE COVER DOES NOT REMAIN CLOSED. REPAIRED THE ESCAPE ROPE IN THE ROPE CONTAINER IAW AMM 25-61-02-2. OPENED AND CLOSED THE ROPE CONTAINER DOOR SEVERAL TIMES, CHECKED THE DOOR IS SECURED CLOSED. ACFT OK FOR SERVICE.

Part: D-RING — MISSING (ESCAPE HARNESS) · airframe 3,177 hrs · 1,263 cycles

DURING PREFLIGHT CHECK, FOUND 4 EMERGENCY ESCAPE HARNESSES MISSING THE D LINK.

Part: SKIN — CHAFED (TE FLAP) · airframe 2,342 hrs · 919 cycles

LT WING INBD MAIN FLAP OTBD END UPPER SKIN EDGE APPROXIMATELY 26" AWAY FROM L/E HAS CHAFED. REPAIRED LT WING INBD FLAP, PN 113T2201-409G, SN 000198 IAW SRM 57-53-01 AND 51-70-03-0G. RSC TRACKING, LT INBD FLAP REPAIR TO THE OTBD END 26" AFT OF L/E. EA TH-5750-T0327258, P1, DATED: AUG. 04, 2016. MAJOR REPAIR IAW TRACKING EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,101 hrs · 48,916 cycles

AT BS 400 STR 1, 2R & 3L ARE CRACKED AT FASTENER COMMON TO STR AND FRAME. REMOVED AND REPLACED STRINGERS PER IAW FEDEX EA 7-5310-57956.

Part: VALVE — DAMAGED (NOSE STRUT)

RED GEAR DOOR LIGHT AND AMBER NOSE GEAR DOOR LIGHT REMAIN ON. ASSOCIATED AIR NOISE AND VIB FELT IN NOSE GEAR AREA. RED TAB PROC AND CYCLE GEAR. *S/D* REMOVED AND REPLACED NOSE STRUT CHARGING VALVE AND SERVICED WITH FLUID AND NITROGEN. PER GEAR RETRACTION CK. ALL IND OPS CK NORM REF 727-100 MM 32-33-000-5 & MM.

Part: VALVE — MALFUNCTIONED (NR 3 PYLON)

AFT T/O BRING RT PACK ON, TURNED NR 3 BLD ON AND RT PACK ON. AFT COMING ON A LOUD BOOMING NOISE HEARD AND MOMENTARY PRESS SPIKE IN CABIN. *S/D* REMOVED AND REPLACED NR 3 ENG BLEED AIR SHUTOFF VALVE. REMOVED AND REPLACED NR 3 ENG HIGH PRESS MODULATING AND SHUTOFF VALVE REF 72-727-100 MM 36-10-001 & 36-112-0414.

Part: CONTROL CABLE — OUT OF ADJ (NLG DOOR)

ON T/O, LANDING GEAR SELECTED UP, GEAR CAME UP WITH VIB AFT GREEN/RED GEAR IND WENT OUT WITH THE EXCEPTION OF THE RED DOOR LIGHT ON FWD PNL (NOSE). COMPLIED WITH RED TABS. A/C RELEASED FOR SERVICE PER MEL. *S/D* ADJUSTED NOSE GEAR DOORS PER MM 32-22-1. ADJUSTED TENSION ON DOOR RETRACTION CABLES PER MM 32-22-1. OPS CK NORM.

Part: CONNECTOR — DIRTY (LG DOOR LIGHT)

99-177 - LEFT LANDING GEAR DOOR LIGHT IND UNSAFE. AFT CYCLING GEAR, RED LIGHT EXTINGUISHED. CK LEFT DOOR SWITCH ADJUSTMENT PER MM 32-62-011-4. CLEANED AND SECURED CONNNECTOR. DOOR AND LIGHT CHECK NORMAL.

Part: SKIN — CRACKED (BS 1150)

LEFT SIDE OF FUSELAGE BS 1150 3 ABOVE STR S4L SHEAR FASTENER HEAD AND SKIN CRACK. REPAIRED PER SRM 53-30-3 FIG 13A.

Part: SKIN — CORRODED (BS 340-342)

NR 273 BULGING SKIN AT BS 340-342, RBL 18, WL 148. ** S/D ** REPAIRED SKIN AT BS 338, RBL 21, WL 148 IAW FEDEX SRM 53-30-03.

Part: CHORD — CORRODED (BS 351.2)

CORROSION (C-53-100-01,1) ON BS 351.2 FRAME BETWEEN STR 26 AND 27 LT. *S/D* REMOVED AND REPLACED BS 351.2 LOWER REINFORCEMENT CHORD PER FEDEX SRM 51-30-2.

Part: FRAME — CORRODED (E/E DOORWAY)

PAE - NR 0546 - CORROSION (C53-100-010) ON E/E DOOR FRAME AT BS 423, RBL 4 - LBL 4, WL 148. (X)

Part: FRAME — CORRODED (E & E DOORWAY)

NR 546 CORROSION (C53-100-010) ON E&E DOOR FRAME AT BS 423, RBL 4-LBL 4, WL 148. ** S/D ** R&R E & E DOOR FRAME AT BS 423, WL 148 PER FEDEX SRM 51-30-2 & FEDEX SRM 51-10-1.

Part: BEAM — CRACKED (CARGO DOOR)

NR 0072 AFT CARGO DOOR #4 TRANSVERSE BEAM HAS CRACK INDICATION AT OUTBOARD FLANGE. *** S/D *** R&R #4 TRANSVERSE BEAM IN AFT CARGO DOOR IAW FEDEX SRM 51-30-2.

Part: SKIN — CREASED (CARGO DOOR)

FWD CARGO DOOR OUTER SKIN IS DENTED 17 AFT OF FWD EDGE AND 27 UP FROM BOTTOM. *S/D* REPAIRED FWD CARGO DOOR 17 AFT OF FWD EDGE AND 27 UP FROM BOTTOM, PER FEDEX SRM 52-00-3.

Part: CHANNEL — CRACKED (CARGO DOOR)

NR0424 FWD CARGO DOOR #4 TRANSVERSE BEAM (FROM BOTTOM) IS CRACKED IN OUTBOARD RADIUS. *** S/D ***R&R FWD CARGO DOOR #4 TRANSVERSE BEAM IAW FEDEX DRAWING 65-18620.

Part: SHEAR WEB — CORRODED (BS 116-1174)

CORROSION (C53-224-08) ON SHEAR WEB BS 1166 TO 1174, LBL 37, WL 208. *S/D* REPAIRED SHEAR WEB AT BS 1166 TO 1174, LBL 37, WL 208 PER FED-EX SRM 51-40-2.

Part: SKIN — CORRODED (BS 440-680)

BS 440 TO 680, STR 1 TO STR 3 LT SHOWS SIGN OF CORROSION DUE TO SKIN PILLOWING AND DISHED RIVET HEADS. *S/D* REMOVED AND REPLACED CROWN SKIN AT STA 440 TO 740, STR 4 LT- STR 4 RT PER FED EX EA 7-5330-42276.

Part: LONGERON — CORRODED (BS 760 - 857)

STA-PAE: CORROSION ON LONGITUDINAL BS 836 AND 839, RBL 45, WL 208.1. *S/D* REMOVED DAMAGE LONG BEAM FROM BS 760-850, RBL 45, WL 208.1 AND REPLACED PER FEDEX DRAWING 65-34144.

Part: FITTING — CRACKED (BS 870)

NR0479 STA-PAE - CRACK INDICATION NOTED IN HOLE NR 1 OF ROW 3, BS 870 RIGHT TERMINAL FITTING. REPAIRED HOLE NR 1 OF ROW 3, BS 870 RIGHT TERMINAL FITTING PER FEDEX EA 7-5310-39911.

Part: FITTING — CRACKED (BS 870)

NR 0421 STA-PAE - MECHANICAL DAMAGE NOTED IN HOLES NR 1 THROUGH 5 OF ROW 3 BS 870 LEFT TERMINAL FITTING. REPAIRED MECH DAMAGED HOLES IN LEFT TERMINAL FITTING AT BS 870 HOLE NR 1 THROUGH NR 5 OF ROW 3 PER EA NR 7-5310-39910.

Part: SKIN — DELAMINATED (RT TE FOREFLAP)

NR 0455 005 STA-PAE: STEEL RUBSTRIP IS DISBONDED ON R/W I/B FOREFLAP I/B END. *** S/D *** REPAIRED R/W I/B FOREFLAP I/B END UPR & LWR SURFACES PER FEDEX SRM 51-40-6 & DRAWING 65-32738.

Part: FITTING — CRACKED (BS 870)

NR0420 STA-PAE - CRACKS NOTED BY NDI IN HOLE NR 1 AND NR 2 OF ROW 2 BS 870 LEFT TERMINAL FITTING. REPAIRED LEFT TERMINAL FITTING AT BS 870 HOLE NR 1 AND NR 2 OF ROW 2 PER EA NR 7-5310-39910.

Part: FITTING — CRACKED (BS 870)

NR 0478 STA-PAE - VISUAL DAMAGE, CRACK AND CORROSION INDICATION NOTED IN HOLES NR 1 THROUGH 5 OF ROW 2 BS 870 RIGHT TERMINAL FITTING. REPAIRED HOLES NR 1 - 5 OF ROW 2, BS 870 RIGHT TERMINAL FITTING PER FEDEX EA 7-5310-39911.

Part: RETRACT MECH — FAILED (NR 2 LE FLAP)

AFTER TAKEOFF, NR 2 LEADING EDGE FLAP WOULD NOT RETRACT WHEN HANDLE MOVED FROM 5 TO 2. RED TABS WHERE FOLLOWED BUT PROBLEM STILL EXIST RETURNED TO ATL. CLEANED AND RESEATED CANNON PLUG NR 2 LEADING EDGE FLAP, OPERATIONAL CHECK NORMAL.

Part: DOOR MECHANISM — NOT LATCHED (ENTRY DOOR)

AIRCRAFT WOULD NOT HOLD PRESSURE ABOVE 2,000 FT GROUND LEVEL. PRESSURIZATION WOULD RESPOND IN MANUAL BUT ONLY TO 10,000 CABIN PRESSURE. THEN EVEN IN FULL MANUAL INCREASE CABIN WOULD CLIMB AT 1,500 TO 1,800 FT PER MINIMUM RATE OF CLIMB. FORWARD ENTRY DOOR WAS VERY DIFFICULT TO CLOSE. UPON ARRIVAL FOUND L1 ENTRY DOOR IMPROPERLY SECURED. CYCLED DOOR SEVERAL TIMES AND PRESSURIZED AIRCRAFT ON GROUND.

Part: HYD LINE — LEAKING (A-HYD SYST)

HYDRAULIC SYSTEM-A FAILURE, QTY DROPPED TO ZERO, MANUALLY CRANKED GEAR DOWN. FLUID SHUTOFF VALVES OFF FOR 30 MINUTES PRIOR TO ENGINE SHUTDOWN. PARTS CATALOG 27-60-00 FIG 20 PG 1, FOUND HYD FLUID LEAKING FROM B-NUT TO T-FITTING NR 60 AND A SMALLER LEAK AT T-FITTING NR 65. REPLACED BOTH T-FITTINGS ALONG WITH HYD LINE NR 11A AND HYD LINE NR 3. REPLACED BOTH ENGINE DRIVEN PUMPS, REPLACED BOTH ASSOCIATED CASE DRAIN FILTERS, LEAK CHECKED HYD PUMPS AND ALL SPOILER RELATED LINES AND B-NUTS LEAK CHECKS GOOD. CYCLED ALL FLT CONTROLS FROM SYS-A AND SERVICED A-SYS HYD QTY.

Part: FORGING — CRACKED (BS 870)

HFEC IND A CRACK IN LT STA 870 FORGING AT INTEGRAL RIB, BELOW CABIN FLOOR WL 190 ON TOP SIDE AT LOWER AFT FASTENER CRACK. ALSO, RUNNING UNDER RIB EXTENDING AFT. REMOVED INTEGRAL RIB FLUSH WITH WEB, PER ESO 11782. HFEC CONFIRMED NO CRACKS AFTER DAMAGE REMOVAL. FABRICATED BATH TUBE FITTING PER ESO 11782 DATED 2-15-96 AND BOEING S/B 53-0116 DATED 10-31-91. INSTALLED REPAIR FITTING AND EXTERNAL STRAP PER ESO 11782 AND FEDEX EA 7-5310-27474A.

Part: FLOORBEAM — CORRODED (BS 950)

CABIN FLOORBEAM AT STA 950 IS CORRODED AROUND SCREW HOLES TOP AND BOTTOM OF BEAM FROM SEAT TRACK NR 3 TO NR 5. REMOVED CORROSION PER 51-10-06, OUT OF LIMITS. REPAIRED PER ESO 11782 AND FEDEX EA 7-5310-27477.

Part: BELLFRAME — PLUGGED HOLE (BS 990)

STR 27L BELLFRAME 990 PLUGGED HOLE TOP NEAR EXISTING FASTENER HOLE. INSTALLED DOUBLER PER SRM 51-40-3.

Part: WEB — CORRODED (CENTER TANK)

LOWER FUSE CENTER TANK REAR SPAR UPPER CHORD, 3 RIVETS HAD POPPED 2 RIVETS WORKING, SKIN WARP BULGE LBL 18 TO 30. INSTALLED DOUBLER AND TRIPLER TO CENTER TANK UPPER WEB PER ESO 11782 DATED 2-13-96, AWAITING FEDEX EA.

Part: STRINGER — CRACKED (BS 676)

UPPER LOBE MAIN CARGO INTERIOR STRUCTURE, STR 15L CRACKED AT FS 676. REMOVED DAMAGED SECTION OF STR 15L AND INSTALLED STR SPLICE REPAIR PER SRM 53-10-3 FIG 1 PG 3 TO 48.