N944FD

Part: ENGINE — FAILED (N/A) · airframe 62,825 hrs · 25,203 cycles

PDIS 944 79-01 0275 22FEB23 RSW OPEN U IN FLIGHT AT FL390 NOTICED R ENG OIL PRESS DISCREET LIGHT FLICKERING. ON EICAS NOTICED OIL QUANTITY 0, ALL OTHER ENGINE INDICATIONS APPEARED NORMAL. FOLLOWED QRH WHICH DIRECTED US TO REDUCE THROTTLE AND EVENTUALLY SHUT DOWN RIGHT ENGINE. DECLARED EMERGENCY, DIVERTED, LANDED IN RSW. ***EMERGENCY DECLARED*** ENG IS APPROVED FOR REMOVAL OPS CHECK GOOD, LEAK CHECK GOOD, OK FOR SERVICE

Part: PAN — GOUGED (R1 DOOR HANDLE) · airframe 62,659 hrs · 25,084 cycles

R1 DOOR EXTERIOR HANDLE PAN WORN REMOVED AND REPLACED R1 DOOR HANDLE PAN IAW DWG 141N6200 REV T AND AMM 52-11-13-02.

Part: WEDGE — DELAMINATED (NR 4 SLAT) · airframe 62,659 hrs · 25,084 cycles

#4 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 27-81-02-4

Part: WEDGE — DELAMINATED (NR 3 SLAT) · airframe 62,659 hrs · 25,084 cycles

#3 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 27-81-02-4

Part: WEDGE — DELAMINATED (NR 5 SLAT) · airframe 62,659 hrs · 25,084 cycles

#5 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 27-81-01-4

Part: WEDGE — DELAMINATED (NR 6 SLAT) · airframe 62,659 hrs · 25,084 cycles

#6 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 81-01-4

Part: FLOORBEAM — CORRODED (BS 1681) · airframe 62,659 hrs · 25,084 cycles

MAIN CABIN FLOOR BEAM STA 1681 IS CORRODED ON THE AFT FACE AND LOWER SURFACE OF THE UPPER CAP AT APPROX RBL 48 ACCOMPLISHED FEDEX EA # F-5310-T0371106 FUSELAGE - MAINFRAME - FLOOR BEAM, STA 1681, LBL 23, LBL 5, RBL 48, CORRODED DAMAGE. ORIG SUBMISSION DATE: 11/3/2022

Part: PANEL — CRACKED (NR 1 NACELLE) · airframe 62,659 hrs · 25,084 cycles

#1 PYLON PANEL 434DR HAS A CORNER CRACKED REPAIRED #1 PYLON PANEL 434DR CRACKED CORNER WITH 350 DEGREE REPAIR IAW B757 SRM 54-50-70-2R FIG 201 REPAIR 1 SHEET 3, 51-40-02,51-70-04,54-50-70-0IAND AMM 51-24-02-7, 51-21-00/701, B757NDTM PART 1 51-01-01.

Part: FLOORBEAM — CORRODED (BS 310) · corrosion level 2 · airframe 62,659 hrs · 25,084 cycles

MAIN CABIN FLOOR BEAM IS CORRODED AT FASTENER HOLE BS 310 LBL 20 ACCOMPLISHED FEDEX EA # F-5310-T0371036 FUSELAGE - MAINFRAME - FLOOR BEAM TEE CAP, STA 310, LBL 20, CORROSION REPAIR

Part: FITTING — CORRODED (BS 324-345) · corrosion level 2 · airframe 62,659 hrs · 25,084 cycles

MAIN CABIN - STA 324-345 RBL2 INTERCOSTAL IS CORRODED AT FLOOR PANEL HOLES REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL IAW B757 DWG 141N5160 REV CD AND 141N5161 REV -

Part: STRINGER — CRACKED (BS1680-1701 S29L) · airframe 62,659 hrs · 25,084 cycles

AFT CARGO COMPARTMENT STA 1680-1701 STR29R HAS CRACKED STINGER REMOVED CRACKED STINGER SECTION ON STA 1680 - 1701 STR29 R/H FABRICATED -1 HAT SECTION AND -2 FILLER INTALLED IAW B757 SRM 53-00-03-2R

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 62,659 hrs · 25,084 cycles

MAIN CABIN - ZONE 250 - STA 1681 FLOOR BEAM IS CORRODED ON LOWER SURFACE - LBL5 ACCOMPLISHED FEDEX EA #: F-5310-T0371106 FUSELAGE - MAINFRAME - FLOOR BEAM, STA 1681, LBL 23, LBL5, RBL48, CORROSION DAMAGE

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,659 hrs · 25,084 cycles

MAIN CABIN FLOOR SUPPORT PLATE IS CORRODED AFT OF CABLES BS 340, LBL 27 REMOVED, FABRICATED AND INSTALLED NEW FLOOR WEB IAW B757 DWG 141N5170 REV C

Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,659 hrs · 25,084 cycles

MAIN CABIN INTERCOSTAL IS CORRODED UPPER AND LOWER SIDE AT NUTPLATES HOLES BS 327 RBL 25 - RBL 39 REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW BAC DWG 141N5160 REV C. ORIG SUBMISSION DATE: 10/24/2022

Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,659 hrs · 25,084 cycles

MAIN CABIN INTERCOSTAL IS CORRODED UPPER AND LOWER SIDE AT NUTPLATES HOLES BS 327 RBL 4- RBL 23 REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW B757-2 DWG 141N5160. ORIG SUBMISSION DATE: 10/24/2022

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 62,659 hrs · 25,084 cycles

MAIN CABIN FLOOR SUPPORT BEAM IS CORRODED UPPER SIDE AT NUTPLATE HOLE BS 344 LBL20 - LBL22 REMOVED, FABRICATED AND REPLACED FLOOR SUPPORT BEAM ISW B757-2 DWG 141N5161 REV A AND 141N5170 REV C

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 62,659 hrs · 25,084 cycles

MAIN CABIN ZONE 240 - FLOOR PANEL 242MCF IS DELAMINATED REPAIRED FLOOR PANEL 242 MCF IAW B757 SRM 53-00-50-2R, REMOVED AND INSTALLED INSERTS IAW B757 SRM 53-00-50-2R

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 62,659 hrs · 25,084 cycles

MAIN CABIN FLOOR PANEL AT STA 480-500 LBL 45 IS DAMAGED REPAIRED FLOOR PANEL IAW B757SRM 53-00-50-2R REPAIR 1

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 62,659 hrs · 25,084 cycles

MAIN CABIN FLOOR BEAM IS CORRODED UPPER AND LOWER SIDE AT NUTPLATES HOLES AND FWD EDGE IS GOUGED AND CORRODED BS 344 LBL0-LBL20 REPAIRED FLOOR BEAM IAW B757-2 SRM 53-00-51-2R REPAIR #10

Part: WEDGE — DELAMINATED (RT NR 8 SLAT) · airframe 62,659 hrs · 25,084 cycles

#8 SLAT T/E WEDGE IS DISBONDED REPAIRED #8 SLAT T/E WEDGE DISBOND ON 3EA. AREA IAW FEDEX EA# F-5750-T0370952.

Part: SKIN — DAMAGED (RT NR 8 SLAT) · airframe 62,659 hrs · 25,084 cycles

RIGHT WING #8 SLAT UPPER TRAILING EDGE LOWER SURFACE HAS AREA OF BARE METAL REPAIRED #8 SLAT UPPER TRAILING EDGE LOWER SURFACE ARE OF BARE METAL IAW FEDEX EA# F-5750-T0370952

Part: PANEL — DAMAGED (VERTICAL STAB) · airframe 62,659 hrs · 25,084 cycles

LH VERTICAL PANEL 322CL DAMAGED REPAIRED L/H VERTICAL STAB PANEL 322CL SKIN IAW B757-200 SRM 55-30-01-2R FIG 201 REPAIR 4 SHEET1 AND SRM 51-70-07-0G.

Part: PANEL — CRACKED (RT WING LE) · airframe 62,659 hrs · 25,084 cycles

RW LEADING EDGE PANEL BEHIND #7 SLAT IS CRACKED AT OB SPLICE AREA. REPAIRED RW LEADING EDGE PANEL BEHIND #7 SLAT IAW B757-200 SRM 57-41-02-2RFIG 201 SHEET 8 AND 51-70-07

Part: DRAG FITTING — CORRODED (RT WING) · airframe 61,278 hrs · 24,069 cycles

THE RT WING OUTBOARD DRAG FITTING UPPER SURFACE HAS CORROSION ON NR 4 AND NR 13 HOLES. COMPLIED WITH FEDEX EA NR F-5740-T0343112 C P3. WINGS-ATTACH FITTINGS-RT WING DRAG FITTING TO WING UPPER SKIN SHIM MIGRATION REPAIR. REPLACED OUTBOARD FITTING.

Part: DRAG FITTING — CORRODED (RT WING) · airframe 61,278 hrs · 24,069 cycles

THE RT INBOARD DRAG FITTING UPPER SURFACE HAS CORROSION AT NR 3 AND NR 8 HOLES. COMPLIED WITH FEDEX EA NR F-5740-T0343112 C P3. REPLACED INBOARD FITTING.

Part: DRAG FITTING — CRACKED (RT WING) · airframe 61,278 hrs · 24,069 cycles

THE RT WING INBOARD DRAG FITTING HAS INDICATIONS ON THE NR 3, NR 8 HOLE AND THE 3RD HOLE FROM THE BOTTOM THAT ATTACHES TO THE SPAR. THE 2 HOLES THAT ATTACH TO THE SKIN HAVE MULTIPLE SIGNALS AND UNABLE TO CLOCK POSITION. THE 3RD HOLE FROM THE BOTTOM THAT ATTACHES TO THE FWD SPAR HAS "CRACK INDICATION" THAT IS VISUALLY CONFIMED AT THE 12 O`CLOCK POSITION. COMPLIED WITH FEDEX EA NR F-5740-T0343112 C P3. WINGS-ATTACH FITTINGS-RT WING DRAG FITTING TO WING UPPER SKIN SHIM MIGRATION REPAIR. REPLACED INBOARD FITTING.

Part: DRAG FITTING — CRACKED (RT WING SKIN) · airframe 61,278 hrs · 24,069 cycles

THE RT UPPER SKIN DRAG FITTING NR 3 AND NR 5 HOLES HAVE INDICATIONS OF DEFECTS NOTED. THE NR 3 HOLE HAS INDICATION AT THE 1 O`CLOCK LOOKING AFT. THE NR 5 HOLE HAS INDICATION AT THE 12 O`CLOCK LOOKING AFT. COMPLIED WITH FEDEX EA NR F-5740-T0343112 C P3. WINGS-ATTACH FITTINGS-RT WING DRAG FITTING TO WING UPPER SKIN SHIM MIGRATION REPAIR. REPLACED INBOARD FITTING.

Part: DRAG FITTING — CRACKED (RT WING) · airframe 61,278 hrs · 24,069 cycles

THE RT WING OUTBOARD DRAG FITTING HAS INDICATIONS OF DEFECTS ON THE NR 4 & NR 13 HOLE. THE NR 4 HOLE HAS INDICATION AT THE 3 O`CLOCK LOCKING AFT AND NR 13 HAS INDICATION ALSO AT THE 3 O`CLOCK LOOKING AFT. COMPLIED WITH FEDEX EA NR F-5740-T0343112 C P3. REPLACED OUTBOARD FITTING.

Part: SKIN — DENTED (LT NACELLE) · airframe 61,278 hrs · 24,069 cycles

LH ENGINE PYLON IB SIDE ABOUT MID SECTION ON LWR FACE HAS DENT. COMPLIED WITH FEDEX EA. F - 5430-T0358210 P1 NACELLS / PYLON - SKIN /PLATES/ PANELS - LH ENGINE PYLON INBOARD SIDE SKIN PANEL REPAIR NEAR PPS 136. PERFORMED SATIFACTORY LEAK CHECK IAW B757 AMM 36-11-00-5

Part: FRAME — CRACKED (BS 1640) · airframe 61,278 hrs · 24,069 cycles

THE LT 1640 FRAME BY STR 14L LOWER INBOARD OPEN HOLE HAS AN INDICATION OF DEFECT NOTED. INDICATION IS AT THE 9 O`CLOCK POSITION LOOKING AFT (GOING INBOARD). REPAIR AS REQUIRED, LAYERS NEED TO BE SEPARATED TO DETERMINE WHAT LAYER HAS DEFECT. ALL WORK ACCOMPLISHED, IAW FEDEX EA F-5310-T0357909. P1 FUSELAGE-MAINFRAME-CRACK INDICATION AT LT STA 1640 FUSELAGE FRAME WEB LOWER INBOARD HOLE LOCATION AT S-14L.

Part: FRAME — CRACKED (ZONE 200) · airframe 61,278 hrs · 24,069 cycles

THE RT 1640 FRAME BY STR 14R LOWER INBOARD OPEN HOLE HAS AN INDICATION OF DEFECT NOTED. INDICATION IS AT THE 9 O`CLOCK POSITION LOOKING AFT (GOING OUTBOARD). REPAIR AS REQUIRED, LAYERS NEED TO BE SEPARATED TO DETERMINE WHAT LAYER HAS DEFECT ALL WORK ACCOMPLISHED, IAW FEDEX EA F-5310-T0357915 P1. FUSELAGE-MAINFRAME-CRACK INDICATION AT RT STA 1640 FUSELAGE FRAME WEB LOWER INBOARD HOLE LOCATION AT S-14R.

Part: RESERVOIR — FAILED (R1 DOOR) · airframe 60,845 hrs · 23,769 cycles

R1 DOOR EMERGENCY POWER RESERVOIR HAS NO PRESSURE. REMOVED AND REPLACED EMERGENCY POWER RESERVOIR REF B757 AMM 52-11-30-4. OPS CHECK SATIS. A/C OK TO CONT SERVICE. RII BY

Part: COLLAR — INOPERATIVE (L1 DOOR) · airframe 60,642 hrs · 23,626 cycles

GUST LOCK ON L FWD ENTRY DOOR WILL NOT MOVE TO ALLOW DOOR TO CLOSE. REF MM 52-11-08-08, INSTALLED NEW HOLD OPEN LOCK COLLAR ON L1 DOOR. L1 DOOR HOLD OPEN LOCK COLLAR OPERATES NORMALLY. PART INSTALLED PN 10-N6008-1 / SN 20-024.

Part: BOTTLE — EMPTY (L1 DOOR ASSIST) · airframe 60,266 hrs · 23,343 cycles

FOUND POWER ASSIST RESIVOUR FOR L1 DOOR BLOWN. REMOVED AND REPLACED L1 DOOR ASSIST BOTTLE PER AMM 52-11-30-4-0 NOMENCLATURE-CYLINDER, EMERGENCY POWER RESERVOIR, /N 803300-35A, S/N 1394

Part: HOSE — DEFECTIVE (DOWNLOCK ACTUATO) · airframe 60,016 hrs · 23,158 cycles

L HYD SYS PRESS LIGHT ILLUMINATED ON FINAL AFTER LANDING GEAR DOWN AND LOCKED AND FLAPS AT FINAL CONFIGURATION. FOLLOWED BY L HYD SYS PRESS AND L YAW DAMPER. CLEARED RUNWAY AFTER LANDING- MAINT TOW TO GATE . REMOVED AND REPLACED DEFECTIVE FLEX HOSE ON LH MLG DOWNLOCK ACTUATOR LH MLG DOWNLOCK ACTUATOR OP'S CK'D GOOD. NO LEAKS NOTED. ACFT OK FOR FLT. FLEX HOSE MPN 271N6119-1 NO SERIAL NUMBER.

Part: SHIM — MIGRATED (RT PYLON) · airframe 59,797 hrs · 23,007 cycles

RT PYLON UPPER AFT DRAG LINK SPAR FITTING SHOWS SIGNS OF SHIM MIGRATION. COMPLIED WITH EA F-5740-T0343112 PART 1. RT WING DRAG FITTING TO WING UPPER SKIN SHIM MIGRATION REPAIR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,797 hrs · 23,007 cycles

CRACK LIKE INDICATION WAS NOTED AROUND AND BELOW FASTENER DURING NDT INSPECTION OF REPAIR AREA AT BS 1360 APPROX 4 INCHES ABOVE STR 5L. STRIP/REMOVED PAINT AT MARKED AREA FOR FURTHER NDT INSPECTIONS OF THE AREA. COMPLIED WITH EA F-5330-T0343048 P1. FUSELAGE SKIN REPAIR AT STA 1360 BETWEEN STRINGERS S-4L AND S-7L.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 59,797 hrs · 23,007 cycles

SUB BEAM AT STA 580 IS CRACKED. TRIMMED ENTIRE UPPER FLANGE OF THE BS 580 FLOOR BEAM SPLICE. FABRICATED REPAIR ANGLE AND RADIUS STRAP AND INSTALLED IAW EA F-5310-T0343027 P-1.

Part: SKIN — CORRODED (N/A) · corrosion level 2 · airframe 59,797 hrs · 23,007 cycles

CORROSION FOUND AFT LOWER SKIN, APPROX @ WSTA-681.50 RIGHT WING AFT OF FUEL VENT PANEL. ALL WORK ACCOMPLISHED IAW FEDEX EA F-5730-T0343147 P1 WINGS - PLATES AND SKINS - RH WING LOWER SKIN CORROSION AT TRAILING EDGE, WSTA 711.50 RH WING LOWER SKIN CORROSION AT TRAILING EDGE, WSTA 711.50 - 743.50, DOUBLER REPAIR

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 59,797 hrs · 23,007 cycles

CORROSION FOUND AFT LOWER SKIN, APPROX @ WSTA-681.50 RIGHT WING AFT OF FUEL VENT PANEL. ALL WORK ACCOMPLISHED IAW FEDEX EA F-5730-T0343147 P1 WINGS - PLATES AND SKINS - RH WING LOWER SKIN CORROSION AT TRAILING EDGE, WSTA 711.50 RH WING LOWER SKIN CORROSION AT TRAILING EDGE, WSTA 711.50 - 743.50, DOUBLER REPAIR

Part: ADC — MALFUNCTIONED (RIGHT) · airframe 58,842 hrs · 22,346 cycles

AFTER TAKEOFF, LOST MULTIPLE AVIONICS, PILOTS ALTITUDE, AIRSPEED, RADIO ALTIMETER, AUTOTHROTTLES. FIRST OFFICER`S FLT DISPLAY WAS SIMILAR BUT REGAINED AIRSPEED, ALTITUDE, BUT NO AUTOTHROTTLES. LAST FLIGHT FAULTED ADC SYS L WITH FAULT CODES 110401, AND 130401. ALSO A SECOND EVENT ON SAME FLIGHT LEG WITH FAULT ADC SYS L AND CODES 312251, 210401, AND 220401. TROUBLESHOT IAW FIM 22-02 FAULT TREE 829 AND REPLACED LEFT ADC IAW AMM 34-12-01-4, DUE TO TRIPPED FAULT BALL. ADC RTS CHECKED GOOD. FAULT WOULD APPEAR TO BE ISOLATED TO A LT ADC FAILURE IAW MTSI 34-16/5936, R & R THE RT ADC AS A PRECAUTION IAW AMM 34-12-01-4, AIR DATA COMPUTER OPS NORMAL. ALSO PERFORMED TEST 30 AND 40 IAW AMM 22-00-00-2, LOWER LANDINGS MINIMUM (LLM). MAINTENANCE PRACTICES. THERE WAS NO EVIDENCE OF WATER FOUND IN MOISTURE TRAPS.

Part: LANDING GEAR — MALFUNCTIONED · airframe 58,842 hrs · 22,346 cycles

AFTER TAKE OFF, PUT GEAR UP. GEAR RETRACTED. WHEN GEAR HANDLE WAS PUT TO OFF, GEAR CAME DOWN. PUT GEAR DOWN FOR LANDING AND RECEIVED GOOD DOWN INDICATION. PERFORMED A BITE OF THE PSEU AND FOUND NO FAULTS ON THE BOX IAW AMM 32-09-06, STEP 4. E. JACKED AIRCRAFT, CYCLED LANDING GEAR SEVERAL TIMES AND PUT GEAR HANDLE IN THE OFF NEUTRAL POSITION WITH HYDRAULICS ON AND OFF FOR 10 MIN EACH WITH NO DEFECTS NOTED, COULD NOT DUPLICATE ON GROUND. OPS CHECKED GOOD IAW AMM 07-11-01-2, & 32-32-00-0-0.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 58,296 hrs · 21,955 cycles

STUB FRAME BS 580 LBL 44-46 CRACKED. REMOVED AND REPLACED FLOORBEAM SECTION REINFORCEMENT STUB FRAME IAW DWG 657N4311 REV - AND SRM 51-40-05-0G, 51-40-02-0G. MAJOR REPAIR.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 56,775 hrs · 20,887 cycles

LEFT OTBD AFT FLAP UPSIDE OTBD END DELAMINATED. REPAIRED IAW EA F-5750-T0312494.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 56,678 hrs · 20,818 cycles

ON CLIMB OUT FIRST OFFICERS R1 WINDOW BEGAN TO ARC. COMPLIED WITH QRH & WINDOW CRACKED AFTER COMPLETING CHECKLIST. LANDED AT NEAREST SUITABLE AIRPORT. R&R FIRST OFFICERS WINDSHIELD. COMPLIED WITH WINDOW HEATING SYS CHECK & WINDOW WIPER OPERATIONAL CHECK. OPERATIONS CHECKED GOOD.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 55,368 hrs · 19,880 cycles

L1 DOOR ESCAPE SLIDE FELL OFF OF DOOR. REMOVED AND REPLACED L1 DOOR ESCAPE SLIDE IAW AMM 25-66-01-4. OPS CHECKED NORMAL. ACFT OK TO CONTINUE.

Part: CARRIAGE — GOUGED (FLAP TRACK) · airframe 55,203 hrs · 19,781 cycles

NR 3 FLAP TRACK CARRIAGE OTBD LOWER FITTING GOUGED. COMPLIED WITH EA F-2750-154109 WINGS-LT INBD FLAP CARRIAGE ASSY-GOUGE ON ROLLER SUPPORT ASSY.

Part: SENSOR — DIRTY (PAX DOOR) · airframe 55,114 hrs · 19,717 cycles

TAXIING INTO POSITION FOR TAKE OFF, RECEIVED LEFT FWD ENTRY DOOR EICAS MESSAGE CAME ON INTERMITTENTLY DURING TAXI BACK TO GATE. INSPECTED ENTRY DOOR, FOUND GREASE, DIRT AND DEBRIS ON PROXMITY SWITCH, CLEANED AREA , OPERATED DOOR IAW AMM 52-11-01-6 SYS CHECKED OK, OK TO CONTINUE.

Part: WIRE — BURNED (LIGHT PANEL) · airframe 54,986 hrs · 19,637 cycles

BURNING RUBBER ODOR HAPPENED AFTER LANDING. ODOR WAS STILL THERE AFTER SHUTDOWN. DURING WALKAROUND NOTICED RT TAXI LIGHT ON, WENT UP TO THE COCKPIT AND NOTICED THAT THE SWITCH WAS IN THE OFF POSITION. CYCLED SWITCH SEVERAL TIMES AND THE LIGHT REMAINED ON. PULLED CIRCUIT BREAKER AND LIGHT WENT OUT. REMOVED TAXI LIGHT SWITCH PANEL AND FOUND WIRES ATTATCHED TO RT RUNWAY TURNOFF SWITCH BURNED. ALSO NOTICED THAT THE WIRES NEXT TO SWITCH HAD MELTED. THESE WIRES GO TO THE LT OVERRIDE SWITCH. R & R LIGHT CORTROL PANEL IAW STANDARD MAINTENANCE PRACTICES. LIGHTS OPS CHECKED NORMAL IAW 33-42-00-5. GLARESHIELD AND AILE STAND LIGHTS OPS CHECKED NORMAL IAW MM 33-14-00-0. ACFT OK FOR SERVCIE.

Part: UNKNOWN — ODOR (CABIN) · airframe 54,921 hrs · 19,601 cycles

AFTER PUSH BACK-ENGINE START; PACKS ON A STRONG FUEL ODOR THROUGHOUT COCKPIT.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 54,807 hrs · 19,529 cycles

L1 DOOR ASSIST BOTTLE PRESSURE NOT IN SERVICEABLE BAND. R & R L 1 PASSENGER DOOR EMERGENCY POWER RESERVOIR REF AMM 52-11-30-4. OK FOR SERVICE.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 54,771 hrs · 19,508 cycles

LEFT DOOR SLIDE DEPLOYED ON DOOR OPENING . INSPECTING AND DISCONNECTING THE LT DOOR EMERGENCY EVACUATION SLIDE IAW MM 25-66-00-0. REMOVED SLIDE AND STOW BEHIND THE RCB. FOUND GIRT BAR SPRINGS WEAK, R & R GIRT BAR ASSY. COMPLETED AND VERIFIED INSTALLATION OF EMERGENCY ESCAPE SLIDE. VERIFIED OPERATION OF L1 DOOR. INSTALLED ESCAPE SLIDE COVER. REF AMM 25-66-01-4 AND 52-11-25-5. ACFT OK FOR SERVICE.

Part: RESERVOIR — EMPTY (DOOR ASSIST) · airframe 54,086 hrs · 19,097 cycles

ON ARRIVAL DURING L1 DOOR OPENING DOOR BOTTLE WAS DISCHARGED BUT SLIDE WAS NOT DEPLOYED. R & R L-1 DOOR EMERGENCY ASSIST POWER RESERVOIR IAW MM 52-11-30-4. OK FOR SERVICE.

Part: FITTING — MISALIGNED (FLAP TRACK) · airframe 53,491 hrs · 18,724 cycles

RT WING INBD FWD FLAP TRACK FAIRING BRACKET ATTACHMENT HOLES ON AFT LANDING GEAR TRUNNION HSG MISALIGNED. BRACKET FOR RT WING INBD FWD FLAP TRACK FAIRING REPAIRED IAW EA F-5740-142375. (WING ATTACH FITTINGS - 1 FASTENER HOLE MISALIGNED ON 113N1159-1 FITTING). REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — DENTED (ZONE 100) · airframe 53,491 hrs · 18,724 cycles

FUSELAGE EXTERIOR SKIN WITH DENT AT BS 1701 TO BS 1720, AT STR 20R. DENT REPAIRED IAW EA F-5330-142379. (FUSELAGE SKIN DENT AT S-20R LAP JOINT BETWEEN BS 1701 AND BS 1720). REPAIR IS CLASSIFIED AS MAJOR.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

FWD CARGO COMPT FLOOR DECK SPLICE STRAPS FOUND CORRODED AND BENT AT STA 550, STA 653.80 AND STA 749.40. CORRODED STRAPS IN FWD CARGO COMPARTMENT. R & R IAW AMM 25-50-04, REV 89. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

AFT CARGO COMPT FLOOR DECK SPLICE STRAPS FOUND CORRODED AND BENT AT STA 1330, STA 1470 AND STA 1510. CORRODED AFT CARGO COMPARTMENT FLOOR DECK SPLICE STRAPS R & R IAW AMM 25-50-04, REV 89. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

AFT CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS AT STA 1560, STA 1580, STA 1600 AND STA 1620 FOUND WITH CORROSION. CORRODED TIE-DOWN FITTINGS IN AFT CARGO COMPT REPAIRED IAW EA F-5340-142364. (AFT CARGO TIE DOWN FITTINGS CORROSION REPAIR) REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

FWD CARGO COMPT RT CARGO NET TIE-DOWN FITTINGS AT STA 660, STA 680, STA 700, STA 720 AND STA 740 FOUND WITH CORROSION. CORRODED FITTINGS IN FWD CARGO COMPT REPAIRED IAW EA F-5340-142360 (FWD CARGO TIE DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

FWD CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS AT STA 600, STA 620, STA 640 AND STA 660 FOUND WITH CORROSION. CORRODED FITTINGS REPAIRED IAW EA F-5340-142360 (FWD CARGO TIE-DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

FWD CARGO COMPT RH CARGO NET TIE-DOWN FITTINGS AT STA 520 AND STA 540 FOUND WITH CORROSION. CORRODED TIE-DOWN FITTINGS IN FWD CARGO COMPT REPAIRED IAW EA F-5340-142360. (FWD CARGO TIE DOWN FITTINGS CORROSION REPAIR) REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

AFT CARGO COMPT RH CARGO NET TIE-DOWN FITTINGS AT STA 1560, STA 1580, STA 1600 AND STA 1620 FOUND WITH CORROSION. REPAIR CARRIED OUT ON CORRODED FITTINGS IAW F-5340-142364 (AFT CARGO TIE-DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

FWD CARGO COMPT LT CARGO TIE-DOWN FITTINGS AT STA 760, STA 780, STA 800, STA 820 AND STA 840 FOUND WITH CORROSION. CORRODED TIE-DOWN FITTINGS IN FWD CARGO COMPT REPAIRED IAW EA F-5340-142360. FWD CARGO TIE DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

FWD CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS AT STA 680, STA 700, STA 720, STA 740, FOUND WITH CORROSION. CORRODED TIE-DOWN FITTINGS IN FWD CARGO COMPT REPAIRED IAW EA F-5340-142360 (FWD CARGO TIE DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

AFT CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS AT STA 1240, STA 1300, STA 1320 AND STA 1340 FOUND WITH CORROSION. REPAIR CARRIED OUT ON CORRODED FITTINGS AT STA 124, 1300, 1320 AND 1340 IAW F-5340-142364 (AFT CARGO TIE-DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

AFT CARGO COMPT RI CARGO NET TIE-DOWN FITTINGS AT STA 1360, STA 1377, STA 1383 AND STA 1400 FOUND WITH CORROSION. CORRODED TIE-DOWN FITTINGS AT STA 1360, 1377, 1383 AND STA 1400. R & R IAW SRM 51-40-02 REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: THRESHOLD — CRACKED (ZONE 100) · airframe 53,491 hrs · 18,724 cycles

AFT CARGO COMPT THRESHOLD PLATE FOUND WITH CRACKS AND DENTS. CRACKED THRESHOLD PLATE IN AFT CARGO COMPT. R & R IAW AMM 53-33-01, REV 89. REPAIR IS CLASSIFED AS MINOR IAW GMM 6-2-100.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 53,491 hrs · 18,724 cycles

AFT CARGO COMPT RH FLOOR DECK PLATE SUPPORT AT STA 1506 RBL 10.5 FOUND CRACKED. CRACKED SUPPORT AT STA 1506, RBL 10.5. R & R IAW SRM 51-40-02 REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: BRACKET — CRACKED (ZONE 400) · airframe 53,491 hrs · 18,724 cycles

NR 2 ENG INBD FAN COWL HAS 4EA UPPER HINGE COVER PLATES WITH CRACKS. CRACKED NR2 ENG INBD FAN COWL HINGE COVER PLATES REPAIRED IAW EA F-7110-142348 (NR1 AND NR2 ENG FAN COWLING SHIELD - HINGE BRACKET WELDING REPAIR). REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: BRACKET — CRACKED (ZONE 400) · airframe 53,491 hrs · 18,724 cycles

NR1 ENG OTBD FAN COWL UPPER HINGE HEAT SHIELD COVERS 4 EA FOUND WITH CRACKS. CRACKED NR1 ENGINE OTBD FAN COWL UPPER HINGE REPAIRED IAW EA F-7110-142348 (NR1 AND NR2 ENGINE FAN COWLING SHIELD HINGE BRACKET WELDING REPAIR). REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

RT WING TOP SKIN - AFTER REMOVAL OF OVERWING FILL PORT ADAPTOR, FOUND CORROSION ON SKIN CUTOUT. CORROSION REPAIR CARRIED OUT ON RT WING TOP SKIN IAW EA F-5730-137696 (RT WING TOP SKIN FUEL PORT CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

CABIN, EXISTING REPAIR AT STA 324, RBL 51 TO RBL 40, TO FLOORBEAM CAP. EVALUATE AND RECTIFY. CABIN STA 324 FLOORBEAM UPPER CAP PN 141N2932-23, R & R IAW SRM 51-40-02, REV 101. THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 53,491 hrs · 18,724 cycles

CABIN, INTERCOSTAL AT STN 324, RBL 0 HAS CRACKED TOP ANGLE. REMOVED AND REPLACED IAW SRM 51-40-02 REV 101. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — DAMAGED (ZONE 100) · airframe 53,491 hrs · 18,724 cycles

FUSELAGE EXTERIOR SKIN WITH EXISTING REPAIR DOUBLER AT BS 760 (BETWEEN BS 740 AND BS 780), STR 16L TO STR 18L. EXISTING REPAIR DOUBLER REPAIRED IAW EA F-5330-142367 (EXISTING FUSELAGE SKIN REPAIR AT BS 740 TO BS 760, BETWEEN S-16L AND S-18L- REPAIR ASSESSMENT). REPAIR IS CLASSIFIED AS MAJOR.

Part: INTERCOSTAL — CORRODED (BS 340) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

CABIN INTERCOSTAL AT BS 340, LBL 20 TO LBL 30 CORROSION AT FASTENER HOLE. CORRODED INTERCOSTAL AT BS 340 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 101. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SILL — CRACKED (ZONE 200) · airframe 53,491 hrs · 18,724 cycles

CABIN, DOOR L2 SILL PLATE FWD CORNER SECTION PULLED RIVETS. CRACK FOUND ON CORNER EDGE. CRACK REPAIR CARRIED OUT ON L2 DOOR SILL PLATE IAW EA F-5320-142350. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: STRAP — CRACKED (ZONE 200) · airframe 53,491 hrs · 18,724 cycles

CABIN, STABILIZATION STRAP CRACKED AT STN 345, LBL 24. REMOVED AND REPLACED IAW SRM 51-40-02 REV.101. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRAP — CRACKED (ZONE 200) · airframe 53,491 hrs · 18,724 cycles

CABIN, STABILIZATION STRAP CRACKED AT STN 345, LBL 0. CRACKED STABILISATION STRAP AT STA 345 REMOVED AND REPLACED IAW SRM 51-40-02 REV.101. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

DURING AFT CARGO DOOR SEAL REPLACEMENT FOUND CORROSION AT AFT LOWER CORNER. AFT CARGO DOOR CUTOUT LOWER CORNER CORROSION REPAIRED IAW EA F-5330-142370, PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: INTERCOSTAL — CRACKED (BS 1320-1342) · airframe 53,491 hrs · 18,724 cycles

CABIN, STN 1320 TO 1342 INTERCOSTAL CRACKED AT FWD END RBL 24.75. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 101. REPAIR IS CLASSIFIED AS MINOR.

Part: STRAP — TORN (ZONE 200) · airframe 53,491 hrs · 18,724 cycles

CABIN STN 1640 TO STN 1660, LB 45.5 LOWER STRAP BROKEN. REPAIR CARRIED OUT IAW EA F-5310-131701. REPAIR IS CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (BS 345) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

CABIN STN 345, RBL 25 TO LBL 25, FLOORBEAM SURFACE CORROSION ON BEAM CAP AROUND FLOOR PANEL ATTACHING HOLES. CORRODED FLOORBEAM AT STA 345 REMOVED AND REPLACED IAW SRM 51-40-02 REV.101. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT — CHAFED (RT WING TE FLAP) · airframe 53,491 hrs · 18,724 cycles

RT WING INBD FLAP OTBD CARRIAGE OTBD FWD ROLLER SUPPORT ASSY HAS A CHAFE MARK. RT WING INBD FLAP O/B CARRIAGE O/B FWD ROLLER SUPPORT ASSY REPAIRED AS PER E.A. F- 2750-142091. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 53,491 hrs · 18,724 cycles

CABIN, STN 1320 TO 1340, RBL 45 INTERCOSTAL CRACKED. CRACKED INTERCOSTAL BETWEEN STA 1320 AND STA 1340, RBL 45. R & R IAW SRM 51-40-02, REV. 101. REPAIR IS CLASSIFIED AS MINOR.

Part: SKIN — CRACKED (ZONE 400) · airframe 53,491 hrs · 18,724 cycles

NR1 ENG STRUT AFT FAIRING DRAIN TUBE EXIT COVER HAS VERY SMALL CRACK ON LWR EDGE. NR 1 ENGINE STRUT AFT FAIRING DRAIN TUBE EXIT COVER T/E SKIN. R & R IAW SRM 51-40-02, REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

AFT CARGO COMPT RT CARGO NET TIE-DOWN FITTINGS AT STA 1420, STA 1437, STA 1443 AND STA 1460 FOUND WITH CORROSION. REPAIR CARRIED OUT IAW EA F-5340-142364. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

AFT CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS AT STA 1360, STA 1377, STA 1383 AND STA 1400 FOUND WITH CORROSION. CORRODED LT TIE-DOWN FITTINGS REPAIRED IAW F-5340-142363 (AFT CARGO TIE-DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

FWD CARGO COMPT RT AND LT CARGO NET TIE-DOWN FITTINGS AT STA 623 FOUND WITH CORROSION. CORRODED TIE-DOWN FITTINGS R & R IAW SRM 51-40-02 REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

FWD CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS AT STA 520, STA 540, STA 560 AND STA 580 FOUND WITH CORROSION. REPAIR CARRIED OUT IAW EA F-5340-142360. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

FWD CARGO COMPT RT CARGO NET TIE-DOWN FITTINGS AT STA 760, STA 780, STA 800, STA 820 AND STA 840 FOUND WITH CORROSION. CORRODED RT TIE-DOWN RITINGS REPAIRED AS IAW ER F-5340-142360 (FWD CARGO TIE- DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

FWD CARGO COMPT RT CARGO NET FITTINGS AT STA 560, STA 580, STA 600, STA 620 AND STA 640 WITH CORROSION. FWD CARGO CORRODED RT FITTINGS REPAIRED IAW EA F-5340-142360 (FWD CARGO TIE-DOWN FITTINGS CORROSION REPAIR) . REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (BS 1420-1460) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

AFT CARGO BAY LEFT CARGO NET TIE-DOWN FITTINGS AT STA 1420, 1440 AND STA 1460 FOUND WITH CORROSION. LEFT TIE-DOWN FITTINGS CORROSION REPAIR CARRIED OUT IAW EA F-5340-142364. (AFT CARGO TIE-DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR.

Part: FRAME — DENTED (ZONE 100) · airframe 53,491 hrs · 18,724 cycles

FWD CARGO COMPT LT FRAME AT STA 780, S24L-25L FOUND DENTED. FWD CARGO COMPT DENTED LT FRAME REPAIRED IAW EA F-5310-142359, PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

AFT CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS AT STA 1480, STA 1500, STA 1520 AND STA 1540 FOUND WITH CORROSION. REPAIR CARRIED OUT IAW EA F-5340-142364. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

AFT CARGO COMPT RT CARGO NET TIE-DOWN FITTINGS AT STA 1480, STA 1500, STA 1520 AND STA 1540 FOUND WITH CORROSION. REPAIR CARRIED OUT IAW EA F-5340-142364. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

AFT CARGO COMPT RT CARGO NET TIE-DOWN FITTINGS AT STA 1280, STA 1300 AND STA 1340 FOUND WITH CORROSION. REPAIR CARRIED OUT IAW EA F-5340-142364. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAL — CRACKED (ZONE 400) · airframe 53,491 hrs · 18,724 cycles

NR2 ENGINE OTBD FAN COWL UPPER SPRING SEAL AFT EDGE HAS CRACK. CRACKED UPPER SPRING SEAL R & R IAW SRM 51-40-02, REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: PLATE — CRACKED (ZONE 100) · airframe 53,491 hrs · 18,724 cycles

FWD CARGO COMPT AFT BULKHEAD PANEL LT SUPPORT FRAME PLATE AT STA 845 S22L FOUND CRACKED. AFT BULKHEAD PANEL SUPPORT FRAME CRACKED PLATE. R & R IAW SRM 51-40-02, REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 400) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

NR 2 PYLON STRUT INTERNAL SKIN HAS CORROSION ON LT SIDE AROUND PANEL 443GL CUT OUT AREA PP STA 106.20 - 119.95. REPAIR CARRIED OUT IAW EA F-5450-142340 (NACELLES/PYLONS - PYLON STRUCTURE - NR 2 STRUT FWD OTBD AND INBD SKIN PANEL CORROSION REPAIR). REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 400) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

NR1 PYLON INTERNAL SKIN HAS CORROSION AROUND INBD FWD BLOW OUT PANEL 433GR CUTOUT AREA AT PP STA 106.20 - 119.95 REPAIR CARRIED OUT IAW EA F-5450-142339 ( NACELLES/PYLONS - PYLON STRUCTURE - NR 1 STRUT FWD INBD SKIN PANEL CORROSION REPAIR). REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 400) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

NR 2 PYLON/STRUT HAS CORROSION ON INTERNAL RT SKIN SURFACE INSIDE FWD BLOW OUT PANEL 443AR AT PP STA 106.20-119.95, PP WL 142.00. REPAIR CARRIED OUT IAW EA F-5450-142340 (NACELLES/PYLONS-PYLON STRUCTURE - NR 2 STRUT FWD OTBD & INBD SKIN PANEL CORROSION REPAIR). REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: ANGLE — CRACKED (ZONE 100) · airframe 53,491 hrs · 18,724 cycles

AFT CARGO COMPT SIDEWALL PANEL SUPPORT ANGLE CLIP AT STA 1260, S-23R FOUND CRACKED. CRACKED ANGLE CLIP AT STA 1260, STR S-23R. R & R IAW SRM 51-40-02, REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

AFT CARGO COMPT LT TRANSITION SIDE PANEL AT STA 1410- STA 1530 FOUND WITH CORROSION. CORRODED LT TRANSITION PANEL FROM STA 1410 TO STA 1530. R & R IAW SRM 51-40-02 REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 53,491 hrs · 18,724 cycles

WTB FAIRING STRUCTURE INTERCOSTAL ASSY LOWER CHORD AT STSA 820-STA 839 FOUND CRACKED. LOWER CHORD AT STA 820 TO STA 839, RBL 18. R & R IAW SRM 51-40-02, REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

AFT CARGO COMPT DOOR CUTOUT LOWER SILL PLATE AT STA 1380 - STA 1440 FOUND WITH CORROSION. CORRODED DOOR CUTOUT LOWER SILL PLATE FROM STA 1380 TO STA 1440 REMOVED AND REPLACED IAW SRM 51-40-02, REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

AFT CARGO COMPT RT TRANSITION SIDE PANEL AT STA 1310- STA 1380 FOUND WITH CORROSION. CORRODED RT TRANSITION PANEL FROM STA 1310 TO STA 1380. R & R IAW SRM 51-40-02 REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

CABIN, FLOORBEAM AT STA 377.7, LBL 5.3 TO LBL 7 HAS EXISTING CORROSION BLEND THAT REQUIRES FURTHER CORROSION BLENDING. REPAIR CARRIED OUT IAW EA F-5310-142343 - BS 377 FLOORBEAM CORROSION REPAIR AT LBL 6 TO LBL 52. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — DELAMINATED (ZONE 200) · airframe 53,491 hrs · 18,724 cycles

FUSELAGE INTERNAL STRUCTURE TEAR STRAP INSP FOUND WITH DISBOND BETWEEN FUSELAGE SKIN PANEL AND BONDED TEAR STRAP AT BS 1360 FROM STR 4L TO STR 7L. DISBOND BETWEEN SKIN PANEL AND TEAR STRAP AT BS 1360 FROM STR 4L TO STR 7L REPAIRED IAW SRM 53-00-01 FIG 201, REPAIR 12, REV 101, REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — DELAMINATED (ZONE 200) · airframe 53,491 hrs · 18,724 cycles

FUSELAGE INTERNAL STRUCTURE TEAR STRAP INSP FOUND WITH DISBOND BETWEEN FUSELAGE SKIN PANEL AND BONDED TEAR STRAP AT BS 1340 FROM STR 4L TO STR 7L. DISBOND BETWEEN FUSELAGE SKIN PANEL AND TEAR STRAP AT BS 1340, FROM STR 4L TO STR 7L REPAIRED IAW SRM 53-00-01 FIG 201, REPAIR 12, REV 101. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — DELAMINATED (ZONE 200) · airframe 53,491 hrs · 18,724 cycles

FUSELAGE INTERNAL STRUCTURE TEAR STRAP INSP FOUND WITH DISBOND BETWEEN FUSELAGE SKIN PANEL AND BONDED TEAR STRAP AT BS 1380 FROM STR 4L TO STR 8L. DISBONDED TEAR STRAP AT BS 1380, STR 4L TO STR 8L, REPAIRED IAW SRM 53-00-0- FIG 201, REPAIR 12, REV.101. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — DELAMINATED (ZONE 200) · airframe 53,491 hrs · 18,724 cycles

FUSELAGE INTERNAL STRUCTURE TEAR STRAP INSP FOUND WITH DISBOND BETWEEN FUSELAGE SKIN PANEL AND BONDED TEAR STRAP AT BS 1320 FROM STR 4L TO STR 7L. DISBONDED TEAR STRAP AT BS 1320 BETWEEN STR 4L AND STR 7L REPAIRED IAW SRM 53-00-01, FIG 201. REPAIR 12 REV 101. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — DELAMINATED (ZONE 200) · airframe 53,491 hrs · 18,724 cycles

FUSELAGE INTERNAL STRUCTURE TEAR STRAP INSP FOUND WITH DISBOND BETWEEN FUSELAGE SKIN PANEL AND BONDED TEAR STRAP AT BS 1400 FROM STR 4L TO STR 10L. DISBOND BETWEEN SKIN PANEL AND TEAR STRAP AT BS 1400 FROM STR 4L TO STR 10L REPAIRED IAW SRM 53-00-01, FIG. 201, REPAIR 12 REV 101. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — DENTED (ZONE 100) · airframe 53,491 hrs · 18,724 cycles

FWD CARGO COMPT LT FRAME AT STA 680 S24L FOUND DENTED. FWD CARGO COMPT DENTED FRAME AT STA 680, S24L REPAIRED IAW SRM 53-00-07, FIG 201. REPAIR 5, REV 101 CATEGORY B, REPAIR REQUIRES REPEAT INSP AT 12000 F/C INTERVAL AFTER FIRST INSP AT 37500 F/C. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: TRANSITION PANEL — CORRODED (BS 1310-1410) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

AFT CARGO COMPT LT TRANSITION SIDE PANEL AT STA 1310 - STA 1410 FOUND CORRODED. R & R IAW SRM 51-40-02 REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SUPPORT ANGLE — CRACKED (BS 560) · airframe 53,491 hrs · 18,724 cycles

FWD CARGO COMPT RT SIDEWALL PANEL UPPER SUPPORT ANGLE AT STA 560 CRACKED. SUPPORT ANGLE R & R IAW SRM 51-40-02 REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: INTERCOSTAL — CORRODED (BS 1440 S26R) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

AFT CARGO COMPT RT INTERCOSTAL LOWER CHORD AT STA 1440 S26R (AT E6 RACK) FOUND WITH CORROSION. LOWER CHORD (WEB) R & R IAW SRM 51-40-02, REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100

Part: INTERCOSTAL — CRACKED (BS 440-460) · airframe 53,491 hrs · 18,724 cycles

E/E COMPT INTERCOSTAL ASSY AT STA 440- STA 460 S24L FOUND CRACKED. CRACKED INTERCOSTAL FROM STA 440 TO STA 460, STR 24L R & R WORKCARD 118150066FL1R02 (SUPPORT INSTL - E1-E5 ELEX EQUIP CTR). ALTERATION IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: PLATE — CRACKED (ZONE 100) · airframe 53,491 hrs · 18,724 cycles

FWD CARGO COMPT AFT REVEAL PLATE FOUND BOTTOM CORNER CRACKED OFF. FWD CARGO COMPT AFT BOTTOM CORNER CRACKED REVEAL PLATE R & R IAW SRM 51-40-02 REV 100. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

CABIN, SEAT TRACK FROM BS 365.5 TO 640 RBL 45 CORRODED AT STN 365.5 TO 369 APPROX SEAT TRACK AT BS 365.5 TO 640 REPLACED IAW SRM 51-40-02 REV 100. REPAIR IS CLASSIFIED MINOR IAW GMM 6-2-100.

Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

WTB FAIRING STRUCTURE CHANNEL AT STA 1180 - STA 1200 RBL 6 FOUND WITH CORROSION. WTB FAIRING CHANNEL AT STA 1180 - STA 1200, RBL 6 REPLACED IAW SRM 51-40-02 REV 100. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100

Part: RETAINER — CORRODED (RT MLG) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

RT MLG CUTOUT SEAL RETAINER UNDER DOOR WARNING LIGHT AFTER REMOVING SEAL FOUND CORROSION. CORRODED SEAL RETAINER AT RT MLG CUTOUT REPLACED IAW SRM 51-40-02, REV 100. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 53,491 hrs · 18,724 cycles

CABIN INTERCOASTAL CRACKED AT STN 1320 TO 1340 LBL 454. R & R SRM 51-40-02 REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: RETAINER — CORRODED (RT MLG) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

RT MLG CUTOUT SEAL RETAINER UNDER DOOR WARNING LIGHT AFTER REMOVING SEAL FOUND CORROSION. CORRODED SEAL RETAINER AT RT MLG CUTOUT REPLACED IAW SRM 51-40-02, REV 100. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: ATTACH BRACKET — CRACKED (ZONE 200) · airframe 53,491 hrs · 18,724 cycles

CABIN DOOR 4R SILL PLATE ATTACH BRACKET FOUND CRACKED ON REINSTALLATION. CRACKED R4 DOOR SILL PLATE BRACKET REMOVED AND REPLACED IAW SRM 51-40-02 REV.100. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

NR 1 PYLON INTERNAL SKIN SURFACE OTBD SIDE HAS CORROSION BETWEEN PP STA 146.50-152.50 PP, WL 143.83. NR1 PYLON LT AFT SKIN PANEL R & R IAW SRM 51-40-02 REV.101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: PANEL — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

NR1 ENG PYLON STRUT INTERNAL LT SKIN HAS CORROSION INSIDE PANEL CUTOUT AREA 443AL AT PP STAS 106.00-119.00. R & R IAW SRM 51-40-02 REV. 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

NR1 ENG PYLON HAS CORROSION ON INBD INTERNAL SKIN SURFACE AT PP STA 153-168. NR1 ENGINE PYLON RT AFT SKIN PANEL R & R IAW SRM 51-40-02, REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 53,491 hrs · 18,724 cycles

NR 2 STRUT HAS CORROSION ON INTERNAL SKIN SURFACE LT BELOW PANEL CUTOUT 443J AT STA 154-171 PP WL 142.50. NR 2 PYLON LT AFT SKIN PANEL R & R IAW SRM 51-40-02, REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.