N936FD

Part: FRAME — UNKNOWN (ZONE 200) · airframe 92,964 hrs · 35,223 cycles

COMPLY WITH EA FOR FRAME REPAIR STA. 1640 RH COMPLIED WITH EA #T F-5310-138502E P9 EA TITLE FUSELAGE-MAINFRAME-EXISTING FRAME REPAIR OF BS 1640, WL 208.10 RIGHT HAND-FRAME SECTION REPLACEMENT, CATEGORY "B" REPAIR, MAJOR REPAIR.

Part: NONE — CRACKED (ZONE 200) · airframe 92,964 hrs · 35,223 cycles

CRACKED FLOOR BEAM @ STA. 580,LBL 45. REPAIRED FLOOR BEAM AT STA 580 LBL 45 PER E.A. # F-5310-T0364468 P1 AND SR DRAWING # 57-53-004 E.A. TITLE FUSELAGE-MAINFRAME-FLOOR BEAM AT STA. 580 AND LBL 45 CRACKED REPAIR PER DRAWING SR 57-53-004 WITH MINOR DEVIATION PER SR 57-53-004, CAT. "B" REPAIR, MAJOR REPAIR.

Part: SEAT TRACK — CRACKED (ZONE 20) · airframe 92,964 hrs · 35,223 cycles

SEAT TRACK AT STA 580, LBL 45, FLANGE HAS A CRACK. REPAIRED SEAT TRACK LBL45 AT STA 530 - 680 IAW EA# F-5321-T0364473, FUSELAGE - CARGO FLOOR - SECTION 43 - MCD SEAT TRACK FLANGE CRACK AT STA 580 LBL45. MAJOR REPAIR

Part: NONE — DAMAGED (ZONE 20) · airframe 92,964 hrs · 35,223 cycles

ZONE 220 FLOOR BOARD 222BF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222BF ON VT MAE TRAVELER T21/1575359 IAW DWG SRZ- 25-005 REVISION R MAJOR REPAIR

Part: NONE — DAMAGED (ZONE 20) · airframe 92,964 hrs · 35,223 cycles

ZONE 220 FLOOR BOARD 221AF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VT MAE TRAVELER T21/1575471 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIR

Part: NONE — DAMAGED (ZONE 20) · airframe 92,964 hrs · 35,223 cycles

ZONE 220 FLOOR BOARD 222MDF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MDF ON VT MAE TRAVELER T21/1575353 IAW DWG SRZ 25-005 REVISION R. MAJOR REPAIR

Part: NONE — DAMAGED (ZONE 20) · airframe 92,964 hrs · 35,223 cycles

ZONE 220 FLOOR BOARD 222MEF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MEF ON VT MAE TRAVELER T21/1575352 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR

Part: NONE — DAMAGED (ZONE 20) · airframe 92,964 hrs · 35,223 cycles

ZONE 220 FLOOR BOARD 221MBF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221MBF ON VT MAE TRAVELER T21/1575357 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR

Part: NONE — DAMAGED (ZONE 20) · airframe 92,964 hrs · 35,223 cycles

ZONE 220 FLOOR BOARD 222MAF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MAF ON VT MAE TRAVELER T21/1575476 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIR

Part: NONE — DAMAGED (ZONE 20) · airframe 92,964 hrs · 35,223 cycles

EDGE DAMAGE NOTED ON FLOOR PANEL 242MEF BOTTOM SIDE. FABRICATED FLOOR BOARD 242MEF ON VT MAE TRAVELER T21/1577548 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR

Part: INDICATOR — NO INDICATION (L1 DOOR ARMING) · airframe 92,487 hrs · 34,870 cycles

PRE-DEPARTURE UNABLE TO ARM L1 DOOR. NO SLIDE LIGHT. COMPLIED WITH INSPECTION & TEST OF GIRT BAR HANDING MECHANISM IAW MM 25-66-10-2. ALL CHECKED NORMAL . ARM LIGHT L1 DOOR TESTED NORMAL.. OK FOR SERVICE.

Part: TRANSMISSION — TRIPPED (RT WING TE FLAPS) · airframe 92,360 hrs · 34,788 cycles

TRAILING EDGE FLAP DISAGREE BETWEEN 20&25 W/FLAP HANDLE IN 25 DETENT. COMPLIED W/QRH EMERGENCY DECLARED. ACCOMPLISHED FIM 27-51-00-815-808 FIG 105. FOUND RT INBOARD FLAP TRANS OVERLOAD INDICATION POPPED. RESET AND ACCOMPLISHED LUBE OF TRANS, PER AMM 12-21-09/301. ACCOMPLISHED OPERATIONS CHECK OF THE TRAILING EDGE FLAPS, PER AMM 21-51-00. ALL CHECKS GOOD WITH NO DEFECTS NOTED.

Part: CUSP WEB — CORRODED (BS 1450) · airframe 91,441 hrs · 34,128 cycles

MAIN CARGO AREA STA 1450 RH CUSP WEB CORRODED. REMOVED,FABRICATED AND INSTALLED NEW CUSP WEB IAW DWG 146N5590.

Part: SKIN — DENTED (BS 408) · airframe 91,441 hrs · 34,128 cycles

EXTERIOR FUSELAGE SKIN DENTED AT STA 408 BETWEEN STRINGER 10L AND 11L REPAIRED PER EA# F-5310-T0349762-P1

Part: SKIN — DENTED (BS 1635) · airframe 91,441 hrs · 34,128 cycles

LOWER AFT CARGO FUSELAGE AT BS 1635 BETWEEN STR27R AND 28R HAS PITTING CORROSION ON INTERNAL SURFACE ACOMPLISHED WORK IAW EA F-5310-T0349844

Part: SLAT TRACK — CORRODED (LT WING) · airframe 91,441 hrs · 34,128 cycles

LEFT WING #3 SLAT INBD TRACK WORN AND PITTED. REMOVED AND REPLACED #3 SLAT IB MAINTRACK REF B757 AMM 27-81-12-4. ADJUSTMENT OF #3 TRACK IS ACCOMPLISHED ON NR N00107. OPS CHECK OF #3 SLAT MAIN TRACK IS ACCOMPLISHED ON NR N00107.

Part: ATTACH ANGLE — CORRODED (LT WING) · airframe 91,441 hrs · 34,128 cycles

LEFT WING L/E PANEL ATTACH ANGLE AT WS 478 HAD INTERGRANULAR CORROSION. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-40-02, AND DWG 114N2151.

Part: ATTACH ANGLE — CORRODED (LT WING) · airframe 91,441 hrs · 34,128 cycles

L/W L/E PNL ATTACH STRUCTURE AT STA 532 HAS INTERGRANULAR CORROSION REMOVED AND REPLACED ANGLE PER B757 SRM 51-40-02 AND DWG #114N2151

Part: GEAR — CORRODED (LT WING SLAT) · airframe 91,441 hrs · 34,128 cycles

LEFT WING NR 4 SLAT OTBD TRACK DRIVE MOTOR SPROCKET TEETH PITTED. REMOVED AND REPLACED NR 4 SLAT OTBD ROTARY ACTUATOR SPROCKET IAW AMM 27-81-18-4. OPS CHECKED GOOD IAW AMM 27-81-18-4.

Part: SLAT TRACK — CORRODED (LT WING) · airframe 91,441 hrs · 34,128 cycles

LEFT WING NR 4 SLAT INBD TRACK WORN AND PITTED. REMOVED AND REPLACED THE NR 4 SLAT INBOARD TRACK IAW AMM 27-81-12-4. ADJUSTMENT AND OPS CHECK ACCOMPLISHED ON SNRM N00108.

Part: SPROCKET — CORRODED (LT WING SLAT) · airframe 91,441 hrs · 34,128 cycles

LEFT WING NR 3 SLAT INBD TRACK DRIVE MOTOR SPROCKET TEETH PITTED. REMOVED AND REPLACED NR 3 SLAT INBD ROTARY ACTUATOR SPROCKET IAW AMM 27-81-18-4. OPS CHECK GOOD IAW AMM 27-81-18-4.

Part: STRIKER — DELAMINATED (LT MLG DOOR) · airframe 91,441 hrs · 34,128 cycles

LMLG DOOR AFT UPSTOP PAD IS WORN. REMOVED AND REPLACED STRIKER PLATE IAW SRM 51-10-02, DWG 149N6002, AND SRM 51-70-06-0G. REMOVED DAMAGED PLIES AND BONDED REPAIR IAW 5010, SRM 51-70-06-0G, AND SRM 52-80-02-2R. SEALED PLATE IAW SRM 51-20-05. RESTORED FINISH IAW SRM 51-70-06-0G, PAR 4H. ADJUSTMENT AND GAP CHECK GOOD IAW AMM 32-10-00-5.

Part: WEDGE — CORRODED (LT WING SLAT) · airframe 91,441 hrs · 34,128 cycles

LEFT WING NR 5 SLAT LOWER T/E WEDGE WAS DELAMINATED AT THE INBD AFT CORNER. REPLACED THE SLAT.

Part: ATTACH ANGLE — CORRODED (RT WING SLAT) · airframe 91,441 hrs · 34,128 cycles

RIGHT WING NR 9 SLAT LOWER T/E WEDGE ATTACH ANGLE IS CORRODED AND THE T/E WEDGE WAS BULGING WITH FASTENERS PULLING THROUGH AT THREE LOCATIONS. REPLACED THE SLAT.

Part: SPROCKET — CORRODED (LT WING SLAT) · airframe 91,441 hrs · 34,128 cycles

LEFT WING NR 4 SLAT INBD TRACK DRIVE MOTOR SPROCKET TEETH PITTED. REMOVED AND REPLACED THE NR 4 SLAT INBD ROTARY ACTUATOR SPROCKET IAW AMM 57-81-18-4. OPS CHECKED GOOD IAW AMM 27-81-18-4.

Part: SKIN — CORRODED (LT WING SLAT LE) · airframe 91,441 hrs · 34,128 cycles

LT WING NR 3 SLAT LEADING EDGE IS CORRODED APPROXIMATELY 32 IN OUTBOARD OF THE INBOARD EDGE IN THE UNPAINTED SURFACE. REPAIRED PER B757 SRM 57-43-01-2R.

Part: SPLICE — CORRODED (LT WING) · airframe 91,441 hrs · 34,128 cycles

LEFT WING T/E OTBD PANEL SPLICE STRIP, JUST AFT OF THE AILERON WAS CORRODED. REMOVED AND REPLACED THE SPLICE STRIP IAW SRM 51-40-02, AND DWG 113N1640, REV B.

Part: SKIN — CORRODED (LT WING SLAT) · airframe 91,441 hrs · 34,128 cycles

LEFT WING NR 3 SLAT L/E WAS CORRODED APPROX 32 INCHES OTBD OF THE INBD EDGE IN THE UNPAINTED SURFACE. REPAIRED THE SLAT IAW SRM 57-43-01-2R.

Part: SLAT TRACK — CORRODED (LT WING) · airframe 91,441 hrs · 34,128 cycles

LEFT WING NR 3 SLAT OTBD TRACK WORN AND PITTED. REMOVED AND REPLACED THE NR 3 SLAT OTBD TRACK IAW AMM 27-81-12-4. OPS CHECKED GOOD IAW AMM 57-81, 81-18-4.

Part: STRIKER — DELAMINATED (RT MLG DOOR) · airframe 91,441 hrs · 34,128 cycles

RIGHT MLG DOOR LOWER UPSTOP PAD HAD COMPOSITE MATERIAL DELAMINATION. REMOVED DAMAGE AND STRIKER PLATE, BONDED NEW POTTING AND REPAIR PLIES AND STRIKER PLATE IAW DWG 149N6002, DWG 149N6003, REV C, SRM 51-70-06-0G, AND SRM 52-80-02-2R. SEALED PLATE IAW SRM 51-20-05. RESTORED FINISH IAW SRM 51-70-06-0G, PAR 4H. R/H MLG DOOR GAP CHECK GOOD IAW AMM 21-12-00-5, FIG 501, AND 502.

Part: SKIN — DENTED (BS 1630) · airframe 91,441 hrs · 34,128 cycles

ETERIOR FUSELAGE SKIN IS DENTED AT APPROX BS 1630 ON STR17R. REMOVED EFECTED FASTENERS PREFORMED HFEC TO OPEN HOLES AND EFECTED AREA FOUND NO CRACKS. OVERSIZED OPEN HOLES AND INSTALLED NEW FASTENERS IAW EA F-5330-T0349901.

Part: SKIN — DENTED (APU DOOR) · airframe 91,441 hrs · 34,128 cycles

APU COMPARTMENT RT DOOR OUTER SURFACE IS CREASED. REPAIRED APU RT DOOR OUTER SKIN IAW EA F-5240-T0349703.

Part: SKIN — DENTED (APU DOOR) · airframe 91,441 hrs · 34,128 cycles

APU COMPARTMENT LT DOOR OUTER SURFACE IS BULGED. REPAIRED APU DOOR OUTER SURFACE IAW EA F-5240-T0349685.

Part: UNKNOWN — UNKNOWN · airframe 91,391 hrs · 34,092 cycles

MOD TYPE T MOD NO. F-5730-T0348437 REV NO. PS P2 WINGS - PLATES AND SKINS - LH WING T.E. SKIN PANEL W BL 235 TO 300 - CRACKS AND COMPLY WITH E..A. F-5730-T0348437 REV NO. POS.

Part: BATTERY — DISCHARGED (CABIN) · airframe 91,361 hrs · 34,075 cycles

DURING PRE-DEPARTURE CHECK, FOUND NUMEROUS EMERGENCY EXIT SIGNS AND R1 EXTERIOR LIGHT INOP. ATTEMPTED TO CHARGE EMERGENCY LIGHT BATTERIES USING SHIP'S POWER FOR 1 HOUR. NO HELP. REMOVED AND REPLACED #2 EMERGENCY LIGHT BATTERY ASSY IN REF TO AMM 33-51-07-2. OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 91,061 hrs · 33,869 cycles

TE FLAP DISAGREE EICAS MSG WHEN SELECTING FLAPS 25. COMPLIED WITH QRH AND LANDED WITH FLAPS 20. PERFORMED FSEU BITE CHECK IAW 757 FIM 27-51 FIG104B. NO EXISTING FAULTS AND BITE CHECK GOOD ON ALL 3 UNITS. CHECKED TRANSMISSIONS FOR TRIPED INDICATORS AND LEAKS. NO DEFECTS NOTED. PERFORMED OPS CHECK OF TE FLAPS NORMAL AND ALT DRIVE IAW AMM 27-51-00-5. NO DEFECTS NOTED OR EICAS MESSAGE. FLAP LEVER HAS NO BINDING IN EITHER DIRECTION. FLAPS RUN NORMAL AND SMOOTH. NO HISTORY. A/C OK FOR CONTINUED SERVICE AT THIS TIME.

Part: BOTTLE — EMPTY (DOOR ASSIST) · airframe 90,209 hrs · 33,335 cycles

AT BLOCK IN FOUND WHEN THE L1 DOOR WAS CRACKED OPEN. WHEN RAMP AGENT TRIED TO OPEN THE DOOR, THE GIRT BAR JAMMED IN OPENING. THE L1 DOOR WAS STUCK HALFWAY OPEN. INSPECTED THE DOOR IAW MM 52-11-00-6. THE GIRT BAR ENGAGES AND DISENGAGES NORMALLY. OPS CHECKED THE DOOR, CHECKED GOOD. FOUND THE DOOR ASSIST BOTTLE WAS EMPTY. R & R THE DOOR ASSIST BOTTLE IAW MM 52-11-30-4. ACFT OK FOR SERVICE.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 89,954 hrs · 33,152 cycles

DURING A POST FLIGHT, FOUND THE R1 DOOR SLIDE EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE POWER SUPPLY IAW AMM 33-51-07-2, PAR 5,6. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: FIREWALL — GOUGED (APU BAY) · airframe 89,854 hrs · 33,058 cycles

APU BAY RT SIDE FIREWALL HAS A GOUGE. ON EVALUATION FOUND THE APU FIREWALL TO BE 100% MATERIAL LOSS IAW IAW SRM 53-80-08-1A. REPAIRED THE FIREWALL IAW SRM 53-80-08-2R REPAIR 2.

Part: STRINGER — CORRODED (BS 1410) · corrosion level 2 · airframe 89,854 hrs · 33,058 cycles

AFT CARGO, CORROSION ON THE UPPER SECTION OF STRINGER 29R, BS 1410. FOUND OUT LIMIT IAW SRM 53-00-03-1A FIG.101 , REMOVED AND REPLACED THE STRINGER IAW SRM 53-00-03-1A, FIG 101 , 51-4040-02-OG AND DWG 146N3300 REV. F.

Part: BEAM — CRACKED (FUSELAGE) · airframe 89,854 hrs · 33,058 cycles

STUB BEAM AT BS 580 IS CRACKED. REMOVED AND REPLACED STUB BEAM IAW SRM 51-40-02-0G, AND DWG 657N4311, REV -.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,662 hrs · 32,940 cycles

ON CLIMBOUT FROM KLAX PASSING 5000 IAS DISAGREE EICAS. CONTINUE CLIMB AND ALT DISAGREE EICAS ILUMINATED. COMPLETED QRH AND DIVERTED TO KLAX . NOTE: WORSE CASE SPLITS WERE APROXX 500' LOW ON FO SIDE VERSUS CAPT AND APPROX 15 KNOTS SLOWER ON FO SIDE AT FL230. CHECKED WITH ATC AND VERIFIED CAPT'S REPLACED NR 2 ADC STATIC WATER DRAIN LINE P/N 50014A43-6-0150 AND PERFORM PITOT STATIC PRESSURE CHK UP TO 23000" 250 KNTS AND NO LEAK FOUND ON BOTH NR 1 AND NR 2 SYSTEM FOUND NO LEAKS IN REF TO AMM 34-11-00-2, AND AMM 34-12-00-5 A/C OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (BLEED AIR SYS) · airframe 88,976 hrs · 32,459 cycles

LOSS OF PRESSURIZATION AT FL 390 FOLLOWING LOSS OF RT ENG BLEED DECLARED EMERGENCY AND DECENDED TO 10,000. PERFORMED RUNUP AND TEST OF BLEED SYSTEMS ON BOTH ENGINES REF MM 36-11-00-5. BOTH BLEEDS PASSED TESTS. PRESSURES AND TEMPS WERE NORMAL DURING AN EXTENDED RUNUP.

Part: VALVE — FAILED (CABIN PRESSURE) · airframe 88,733 hrs · 32,277 cycles

TOTAL LOSS OF CABIN PRESSURE AT FL 390. PREVIOUS HISTORY OF CABIN PRESSURE PROBLEMS. RT ENGINE BLEED & ASSOC EICAS LIGHT ILLUMINATED. FOLLOWED APPROPRIATE QRH. PNEU DUCT PRESSURE, RT SIDE, SLOWLY BUT STEADILY DECREASED & THEN EICAS ILLUMINATED. THEN SUBSEQUENTLY THE LEFT ENGINE BLEED LIGHT ILLUMINATED WITH A CORRESPONDING PNEU DUCT DECREASE. USED FIM 36-10/811. FOUND NO DISCREPANCIES. DUE TO HISTORY GOING TO REPLACE BOTH ENGINE FAMV'S AT THIS TIME THE RIGHT VALVE HAS BEEN REMOVED AND REPLACED PER MM 36-11-16-4. OPS GOOD. REMOVED AND REPLACED LEFT FAMV PER MM 36-11-16-4. RAN BOTH ENGINES AND COULD FIND NO DISCREPANCIES. ACFT IS OK FOR SERVICE.

Part: BLEED AIR SYS — MALFUNCTIONED (LEFT) · airframe 88,724 hrs · 32,272 cycles

APPROXIMATELY 30 MINUTES AFTER LEVEL OFF, AT FL400 EICAS LT BLEED OFF. COMPLIED WITH QRH, CABIN ALTITUDE MAINTAINED APPROX 30 MINUTES LATER RT BLEED OFF. RAN QRH AFTER COMMENCED DESCENT FROM FL400 TO 10,000, GOT CABIN ALT EICAS, RAN QRH, O2 MASK ON. RESET RT ENG & LT ENG. BLEED VALVES, ESTABLISH PRESSURIZATION & CABIN ALTITUDE & LEVELED AT 15,000 FT & STATUS MSSY, CAB ALT AUTO 1. RAN ENGINES AS PER JRH AND ENGINE RUN FORM AND OPS CHECKED AND LEAKED CHECKED REVERSE FLOW CONTROLLER VALVE , OPS CHECKED NORMAL. OPS CHECKED THE COMPLETE PNUE . SYSTEM AS IAW AMM-36-11-00-5-0, EVERYTHING OPS CHECKDED NORMAL AS IAW AMM. ACFT OK TO CONTINUE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 884 hrs · 32,040 cycles

COURIER SEAT RBL 10, SEAT TRACK CORRODED. COMPLIED WITH EA F-5310-138503 P2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 884 hrs · 32,040 cycles

LIGHTNING STRIKE AT FACTORY SPLICE, BS 660, BETWEEN STRINGERS 28 - 29R. REPAIRED IAW EA F-5330-TO319956 P1.

Part: SKIN — DAMAGED (BS 514) · airframe 884 hrs · 32,040 cycles

LIGHTNING STRIKE LOCATED LOWER FUSELAGE STATION 514, STRINGER 28R. BLENDED LOWER FUSELAGE IAW SRM 53-00-01-2R, OUT OF LIMITS IAW SRM 53-00-01-1A. REPAIRED AREA IAW SRM 53-00-01-2R REPAIR 15.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 884 hrs · 32,040 cycles

LIGHTNING STRIKE LOWER SKIN BS 549, STRINGER 28R. COMPLIED WITH EA F-5330-T0319926 P1.

Part: FRAME — DENTED (BS 321) · airframe 884 hrs · 32,040 cycles

BS 321.25 FRAME DENTED AT BL 0, FWD E & E BAY DOOR CUT OUT. COMPLIED WITH EA F-5310-T0319779 P1.

Part: SERVO — MALFUNCTIONED (RUDDER) · airframe 881 hrs · 31,870 cycles

AFTER TAKEOFF RUDDER STARTED CYCLING LT TO RT. RUDDER CYCLE BECAME MORE VIOLENT THE FASTER WE WENT. SLOWED TO 220KTS & LEVELED OFF AT 15000'. STATUS MSG, RUDDER PCU. NO QRH TO LOOK AT, RETURNED TO LAND. REPLACED YAW DAMP MODULE & YAW DAMP SERVO.

Part: WINDOW — UNSECURE (COCKPIT) · airframe 881 hrs · 31,862 cycles

DURING TAKEOFF, LT WINDOW CAME OPEN AT 40 KTS, STOPPED & CLOSED WINDOW, TAXIED BACK FOR TAKEOFF. CAPTAIN CLOSED & LATCHED LT SLIDING WINDOW BEFORE TAKEOFF. VERIFIED THAT THE LT SLIDING WINDOW WAS CLOSED & LATCHED UPON ARRIVAL. NO HISTORY LAST 90 DAYS. OK FOR SERVICE.

Part: SEAL DEPRESSOR — DAMAGED (R1 DOOR) · airframe 87,408 hrs · 31,286 cycles

UNABLE TO ARM 1R DOOR, COULD NOT OPEN DOOR WITH HANDLE. FOUND IN THE UPPER FWD CORNER ABOUT A 3 INCH SECTION PEALING & JAMMING THE DOOR. REMOVED DAMAGED UPPER SEAL DEPRESSOR SEGMENT. FABRICATED NEW SEAL DEPRESSOR CORROSION PROTECTED REPAIR SEGMENT IAW SRM. CLEANED & SEALED UNDER REPAIR SEGMENT, INSTALLED REPAIR SEGMENT WITH 2 DOUBLE FLUSH AD6-4 RIVETS. CORROSION PROTECTED AREA IAW SRM EA F-5310-T0306094.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 87,071 hrs · 31,044 cycles

EMERGENCY EXIT UNARMED LIGHT HALF UNLIT. REPLACED BULBS AND CHECKED NORMAL.

Part: LIGHT — MISSING (ESCAPE SLIDE) · airframe 86,588 hrs · 30,689 cycles

LT SLIDE ILLUMINATION LIGHT IS MISSING (LIGHT IS 1" SQUARE) (ARMED LIGHT) ORIGINAL PLAN DATE WAS ENTERED. RELEASED FOR SERVICE IAW MEL: 25-66-05-A CATEGORY: C EXPIRATION: 18FEB13 "MEL 25-66-05-A: L1 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS- INOP VERIFY AND RECORD IN AML/EAML THAT ASSOCIATED SLIDE IS VISUALLY VERIFIED ENGAGED PRIOR TO EACH DEPARTURE." REPLACED L-1 DOOR INDICATOR (SLIDE LIGHT) L00403. LENS /CAP ASSY OPS CHECK GOOD REF WDM 25-66-11, SWPM 20-84. AMM 25-66-11-2 & 52-11-00-2. REMOVED INOP CNTRL STICKER, ACFT OK FOR SERVICE. RII:113925.

Part: UNKNOWN — UNKNOWN · airframe 86,435 hrs · 30,590 cycles

TWICE, A LOWER ALTITUDE WAS SELECTED AND ACFT FAILED TO DESCEND, OVER RODE WITH VERTICAL SPEED. COULD NOT CONFIRM ANY FAULTS LAST FLIGHT. NO PREVIOUS HISTORY PAST 30 DAYS. PERFORMED MCDP GROUND TESTS 30 & 40 IAW MM 22-00-02-2. NO DISCREPANCIES NOTED. OK FOR SERVICE. PERFORMED MCDP GROUND TESTS 30 & 40 IAW MM 22-00-02-2.

Part: ACTUATOR — INOPERATIVE (SLATS) · airframe 85,944 hrs · 30,288 cycles

L/E SLAT DISAGREE ON FLAP RETRACTION. RAN APPROPRIATE CHECKLISTS AND PROCEDURES. RETURNED FOR LANDING. CHECKED RT OUTBD SLAT FOR RIGGING AND OTBD SLAT ACTUATOR TRANSMITTER FOR PROPER RIGGING. REMOVED AND REPLACED SLAT ACTUATOR IAW AMM 27-81-18-4. PERFORMED RIG AND OPS CHECK OF LEADING EDGE SLAT DRIVE ROTARY DRIVE ACTUATOR AND TRANSMITTER IAW AMM 27-81-18-6, OPS CHECKED NORMAL.

Part: FSEU — MALFUNCTIONED (TE FLAPS) · airframe 84,425 hrs · 29,337 cycles

WHILE CONFIGURING FROM FLAPS 20 TO FLAPS 25, RECEIVED A T/E FLAP DISAGREE EICAS. EXECUTED GO-AROUND, RAN QRH AND LANDED UNEVENTFULLY. REMOVED AND REPLACED NR 1 FSEU REF 757 M/M 27-51-01-2. OPS TESTS WELL AT THIS TIME.

Part: PROXIMITY SENSOR — MALFUNCTIONED (THRUST REVERSER) · airframe 84,284 hrs · 29,252 cycles

LEFT REVERSER UNLOCKED DURING TAKEOFF AT 50 KNOTS. REJECTED TAKEOFF & AFTER SEVERAL MINUTES REVERSER LIGHT WENT OUT. RELEASED FOR SERVICE IAW MEL: 78-31-01-01 R& R LT ENGINE RT ACTUATOR PROXIMITY SENSOR S165 IAW AMM 78-36-01-4, REACTIVATED LT THRUST REVERSER & PERFORMED OPS CHECK OF LT THRUST REVERSER IAW AMM 78-31-00-5. ALL INDICATIONS NORMAL. R & R PROXIMITY SWITCH ELECTRONICS UNIT IAW AMM 32-09-04-4. OPS CHECKS GOOD. PERFORMED TAXI CHECK AND OPS CHECK OF LT THRUST REVERSER. DURING TAXI CHECK ALL INDICATION SATISFACTORY, NO AMBER REVERSER INDICATION. TOOK ENGINE TO POWER & NO AMBER REVERSER INDICATION. OPERATED THRUST REVERSER SEVERAL TIMES WITH NORMAL RESULTS.

Part: SKIN — DAMAGED (ZONE 200) · airframe 83,960 hrs · 29,058 cycles

CABIN : ELONGATED SCREW HOLE 02 EA ON FLOORBEAM LWR CHORD AT STA 580, RBL 26. FLOORBEAM LOWER CHORD AT STA 580, RBL 26, SCREW HOLE REPAIRED IAW EA NR F-5310-138510 (ELONGATED NUTPLATE HOLES ON FLOORBEAM LOWER CHORD ON BS 580). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — DAMAGED (ZONE 200) · airframe 83,960 hrs · 29,058 cycles

INTERIOR FRAME WITH DOUBLE HOLE AND CLOSE SPACED HOLES AT BS 418, BETWEEN STR 2L TO STR 2R. FRAME AT BS 418, STR 2L TO STR 2R, REPAIRED IAW STA EA 757-5312-08-E0612 (EXTRANEOUS FASTENER HOLES FOUND ON STA 395 AND STA 418 FRAMES, BETWEEN S-2L AND S-2R). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — DAMAGED (ZONE 200) · airframe 83,960 hrs · 29,058 cycles

INTERIOR FRAME WITH DOUBLE HOLE AND CLOSE SPACED HOLES AT BS 395, BETWEEN STR 2L TO STR 2R. FRAME AT STA 395, BETWEEN STR 2L AND 2R REPAIRED IAW EA 757-5312-08-E0612 (EXTRANEOUS FASTENER HOLES FOUND ON STA 395 AND 418 FRAMES, BETWEEN S-2L AND S-2R). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FUSELAGE EXTERIOR LOWER SKIN WITH SURFACE CORROSION AT LT BS 440 TO BS 660, BELOW STR 26L. CORROSION REPAIR CARRIED OUT ON EXTERIOR FUSELAGE SKIN FROM BS 440 TO BS 660, BELOW STR 26L, IAW STA ENGRG EA F-757-5331-08-E0571 (CORROSION ON EXISTING SKIN PANEL P/NR 143N3471-4 BETWEEN STA 440 TO STA 660, ALONG S-26L). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 83,960 hrs · 29,058 cycles

CABIN - ELONGATED SCREW HOLE 02 EA FLOORBEAM LWR CHORD AT STA 640 RBL 26. REPAIR CARRIED OUT ON FLOORBEAM LWR CHORD AT STA 640, RBL 26 IAW STA ENG EA F-757-5335-08-E0619 REV C (ELONGATED NUTPLATE HOLES FOUND ON STA 640 FLOORBEAM LOWER CHORD). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOORBEAM — NONE (ZONE 200) · airframe 83,960 hrs · 29,058 cycles

CABIN - EXISTING DOUBLER REPAIR FOUND ON FLOORBEAM UPPER CHORD AT STA 377 LBL 14. TO EVALUATE. REPAIR CARRIED OUT ON FLOORBEAM UPPER CHORD DOUBLER AT STA 277, FROM LBL 6.8 TO RBL 11.5 IAW EA F-5310-138503 (EXISTING FLOOR BEAM UPPER CHORD REPAIR AT BS 377.70). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — CRACKED (ZONE 100) · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT AT BS 508 BETWEEN STR 23L AND STR 24L FOUND CRACK ON FRAME WEB. FRAME WEB AT BS 508, BETWEEN STR 23L AND STR 24L REPAIRED IAW EA F-5310-138514. (FRAME WEB CRACK REPAIR AT BS 508, BETWEEN S-23L AND S-24L). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — UNKNOWN (ZONE 200) · airframe 83,960 hrs · 29,058 cycles

FUSELAGE R4 PASSENGER DOOR CUTOUT WITH EXISTING FRAME REPAIR AT DOOR GUSS LOCK CUTOUT LOWER INBD CORNER, AT BS 1640. TO EVALUATE R4 DOOR CUTOUT FRAME AT DOOR GUST LOCK CUTOUT LOWER INBD CORNER REPAIRED IAW EA NR F-5360-137439 (SECT. 46 RT NR 4 PASSENGER DOORWAY BS 1640 FRAME WEB REPAIR AT DOOR STOP NR 3 - REWORK EXISTING REPAIR NR MON/757/53-252/REP/3260). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 200) · airframe 83,960 hrs · 29,058 cycles

LT L4 PASSENGER DOOR WITH EXISTING FRAME REPAIR AT FWD EDGE HOLD OPEN LATCH CUTOUT AT BS 1640. TO EVALUATE, L4 PASSENGER DOOR CUTOUT FWD EDGE HOLD-OPEN LATCH CUTOUT REPAIRED IAW EA F-5360-137434, L4 PASSENGER DOORWAY BS 1640 FRAME WEB REPAIR AT DOOR STOP NR 3 DOOR -REWORK REPAIR REPAIR NR MON/757/53-251/REP/1131. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — UNKNOWN (CARGO DOOR) · airframe 83,960 hrs · 29,058 cycles

AFT CARGO NR 2 CARGO DOOR INNER SKIN BETWEEN BS 1383 TO BS 1388 FOUND WITH PREVIOUS REPAIR. REPAIR ON AFT CARGO DOOR INNER SKIN BETWEEN BS 1383 AND BS 1388 CARRIED OUT IAW EA F-5230-135817 (NR 2 CARGO DOOR INNER SKIN CRACK REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — DAMAGED (ZONE 100) · airframe 83,960 hrs · 29,058 cycles

AT BS 520 BETWEEN STR 25L AND STR 26L, 1 EA EXISTING FASENER HOLE FOUND ELONGATED (0.35") AT THE FLANGE OF FRAME. FRAME AT BS 520, FROM STR 25L TO STR 26L REPAIRED IAW STA ENG EA 757-5332-08-E0573 (INCOMING ELONGATED FASTENER HOLE AT STA 520 FRAME, BETWEEN 25L AND S-26L FOUND INTERFERING WITH DSS INTEGRATION). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: GUIDE — CHAFED (CARGO DOOR) · airframe 83,960 hrs · 29,058 cycles

FWD CARGO DOOR AFT CUTOUT LOWER ROLLER GUIDE FITTING FOUND WITH CHAFING MARK. DAMAGE ON FWD CARGO DOOR AFT CUTOUT LOWER ROLLER GUIDE FITTING REPAIRED IAW EA NR F-5230-135837 (NR 1 CARGO DOOR GUIDE FITTING PN 143N6635-5 NICK DAMAGE, REWORK). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOORBEAM — UNKNOWN (ZONE 200) · airframe 83,960 hrs · 29,058 cycles

CABIN FLOORBEAM LOWER CHORD AT STA 700, LBL 40 TO RBL 40 FOUND WITH PREVIOUS REPAIR. REPAIR CARRIED OUT ON CABIN FLOORBEAM LOWER CHORD AT STA 700, FROM LBL 40 TO RBL 40 IAW EA F-5310-138505 (EXISTING LOWER FLOORBEAM LOWER CHORD REPAIR AT BS 700). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SUPPORT BRACKET — DAMAGED (BS 620) · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT AT RT BS620, RBL 19 CEILING PANEL UPPER SUPPORT BRACKET FOUND WITH ELONGATED HOLE. SUPPORT BRACKET REPAIRED IAW EA F-5310-138512 (ELONGATED NUTPLATE HOLES ON FLOORBEAM LOWER CHORD ON BS 620).

Part: SKIN — CRACKED (ZONE 800) · airframe 83,960 hrs · 29,058 cycles

CABIN - L1 DOOR INNER SKIN CUT-OUT EDGE CRACKED AND CHIPPED AT ARM/DISARM LEVER, MOUNT BRACKET LOCATION. CRACKED INNER SKIN ON L1 DOOR REPAIRED IAW EA F-5210-137433 (L1 DOOR INNER SKIN CUT-OUT EDGE CRACK REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: BULKHEAD — CRACKED (NR 1 PYLON) · airframe 83,960 hrs · 29,058 cycles

NR 1 PYLON, 1 CRACK FOUND A AFT INBD HOLE OF MID BULKHEAD. REFER TO EO F-5450-7-5005 P1, PAGE 21, STEP 1.11 FOR DETAILS. CRACKED HOLE REPAIRED IAW EO F-5450-7-5005 PART 5 (PYLON STRUCTURE MID-BULKHEAD INSP). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1376 RT. CORRODED TIE DOWN FITTING AT STA 1376 RT R & R IAW SRM 51-40-02, REV. 99. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ACCESS PANEL — CRACKED (ZONE 100) · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT ACCESS COVER CRACKED AS MARKED, AFT OF P36 MISC ELECT EQUIP AREA. CRACKED COVER ON P36 EQUIPMENT AREA REPAIRED IAW EA F-5320-137447A. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA. 1260 RT. CORRODED TIE DOWN AT RT STA 1260 R & R IAW SRM 51-40-02 REV.99. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1300 LT. CORROSION REPAIR ON TIE DOWN FITTING AT STA 1300 LT CARRIED OUT IAW EA F-5340-137429 (AFT CARGO TIE-DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1320 RT. CORRODED TIE DOWN AT STA 1320 RT R & R IAW SRM 51-40-02 REV.99. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SUPPORT — BENT (ZONE 100) · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT, STA 740 SLOPE PANEL SUPPORT BENT AS MARKED LT SIDE. BENT SLOPE PANEL AT STAS 740 LT SIDE R & R IAW EA F-5320-135824 (BS 740 SIDEWALL SUPPORT CHANNEL FABRICATION) AND SRM 51-40-12 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA. 1480 LT. CORRODED TIE DOWN FITTING AT STA 1480 LT, R & R IAW SRM 51-40-02, REV/ 99. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STANCHION — CRACKED (ZONE 100) · airframe 83,960 hrs · 29,058 cycles

AFT CARGO RT STA 1500 SIDE WALL STANCHION FOUND CRACKED. CRACKED STANCHION AT RT STA 1500. R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: STANCHION — CRACKED (ZONE 100) · airframe 83,960 hrs · 29,058 cycles

AFT CARGO LT STA 1460 SIDE WALL STANCHION FOUND CRACKED. CRACKED STANCHION AT STA 1460 LT, R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: STANCHION — CRACKED (ZONE 100) · airframe 83,960 hrs · 29,058 cycles

AFT CARGO RT STA 1260 SIDE WALL STANCHION FOUND CRACKED. CRACKED STANCHION AT RT STA 1260. R & R IAW AMM 20-11-00 REV 5. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: STANCHION — CRACKED (ZONE 100) · airframe 83,960 hrs · 29,058 cycles

AFT CARGO RT STA 1600 SIDE WALL STANCHION FOUND CRACKED. CRACKED STANCHION AT STA 1600 RT SIDE WALL R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: INTERCOSTAL — CRACKED (BS 440-460) · airframe 83,960 hrs · 29,058 cycles

FWD CARGO LT STA 440 TO STA 460 STR 22L TO 23L, FOUND INTERCOSTAL WEB CRACKED. CRACKED INTERCOSTAL BETWEEN STA 440 AND STA 460 R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL RBL 19.00 TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 740. STA 740, RBL 19, TIEDOWN FITTING REPAIRED IAW EA NR F-5340-137430 (FWD CARGO TIEDOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL LBL 19.00 ATTACHED TIE DOWN FOUND WITH CORROSION AS MARKED AT STA 540. FITTING ON FLOOR SIDE PANEL AT LBL 19 REPAIRED IAW EA NR F-5340-137430. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR PANEL SUPPORT RBL 10.45 STA 1460 INTERCOSTAL TIE DOWN FOUND CORRODED AS MARKED. CORRODED TIE DOWN FITTING AT STA 1460, RBL10.45 REPLACED IAW SRM 51-40-02 AND EA F-5340-137429. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL LBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 720, STA 720, LBL 19. TIE DOWN FITTING CORROSION REPAIR CARRIED OUT IAW EA NR F-5340-134430 (FWD CARGO TIEDOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1580 LT. STA 1580, LT, TIE DOWN FITTING REPAIRED IAW EA F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1340 LT. STA 1340 LT TIE DOWN FITTING REPAIRED IAW EA NR F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL RBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 700. STA 700, RBL 19, TIE DOWN FITTING REPAIRED IAW EA F-5340-137430 (FWD CARGO TIE DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL LBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 740. STA 740, LBL 19. TIE DOWN FITTING CORROSION REPAIR CARRIED OUT IAW EA NR F-5340-137430 (FWD CARGO TIEDOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — DELAMINATED (ZONE 300) · airframe 83,960 hrs · 29,058 cycles

RT ELEVATOR T/E OTBD TIP HAS SIGN OF DELAM ON METAL DOUBLER. DELAMINATION ON RT ELEVATOR T/E OTBD TIP REPAIRED IAW EA NR F-5520-133349. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: ANGLE — CRACKED (PYLON FAIRING) · airframe 83,960 hrs · 29,058 cycles

LT PYLON AFT COMMON NOZZLE UPPER FAIRING LWR PANEL SUPPORT FWD ANGLES (BOTH) FOUND FWD CORNER CRACK. CRACKED SUPPORT ANGLES LT & RT REPLACED IAW EA F-7110-137437 (COMMON NOZZLE TO STRUT FAIRING - PARTS ANGLE FABRICATION FOR PN LJ34907 & LJ34909). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1360 RT. RT STA 1360 TIE DOWN FITTING REPAIRED IAW EA NR F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL LBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 820. STA 820, LBL 19 TIEDOWN FITTING CORROSION REPAIR CARRIED OUT IAW EA F-5340-137430 (FWD CARGO TIEDOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1620 RT. RT STA 1620 TIE DOWN FITTING REPAIRED IAW EA NR F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1520 LT. STA 1520, LT TIE DOWN FITTING REPAIRED IAW EA F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL RBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 720. STA 720, RBL 19 TIEDOWN FITTING CORROSION REPAIR CARRIED OUT IAW EA F-5340-137430 (FWD CARGO TIE DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL RBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 760. STA 760, RBL 19, TIE DOWN FITTING REPAIRED IAW EA NR F-5340-137430 (FWD CARGO TIE DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1300 RT. RT STA 1300 TIE DOWN FITTING REPAIRED IAW EA NR F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1460, LT. STA 1460, LT TIE DOWN FITTING REPAIRED IAW EA F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL LBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 839. STA 839, LBL 19 TIEDOWN FITTING CORROSION REPAIR CARRIED OUT IAW EA. NR F-5340-137430 (FWD CARGO TIEDOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ACCESS PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

LT WING FUEL TANK PANEL NR 543BB LOWER SURFACE SKIN HAS CORROSION. FUEL TANK PANEL NR 543BB LOWER SKIN REPAIRED IAW EA F-2810-135836 (FUEL TANK ACCESS COVER CORROSION DAMAGE REWORK). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1400, LT. STA 1400, LT TIE DOWN FITTING REPAIRED IAW EA EF-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN WITH SURFACE CORROSION AS MARKED, STA 1440, LT. STA 1440 LT, TIE DOWN FITTING REPAIRED IAW EA F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL RBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 800. STA 800, RBL 19, TIE DOWN FITTING REPAIRED IAW EA NR F-5340-137430 (FWD CARGO TIE DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1360, LT. STA 1360, LT, TIE DOWN FITTING REPAIRED IAW EA NR F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1600, RT. STA 1600, RT TIE DOWN FITTING REPAIRED IAW EA F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1240 LT. STA 1240 LT TIE DOWN FITTING REPAIRED IAW EA F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1280 LT. STA 1280, LT TIE DOWN FITTING REPAIRED IAW EA F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1580 RT STA 1580, RT TIE DOWN FITTING REPAIRED IAW EA 5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL LBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 580. TIE DOWN FITTING AT STA 580 REPAIRED IAW EA F-5340-137430. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL LBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 680. STA 680, LBL 19 TIEDOWN FITTING CORROSION REPAIR CARRIED OUT IAW EA NR F-5340-137430. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1260 LT. LT STA 1260 TIE DOWN FITTING REPAIRED IAW EA NR F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL LBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 600. TIE DOWN FITTING AT STA 600, LBL 19 REPAIRED IAW EA F-5340-137430. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL LBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 620. STA 620 TIE DOWN FITTING CORROSION REPAIR CARRIED OUT IAW EA F-5340-137430. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1540 RT STA 1450, RT TIE DOWN FITTING REPAIRED IAW EA F-5340-137429 [AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL RBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 640. STA 640, RBL 19 TIE DOWN FITTING REPAIRED IAW EA F-5340-137430 (FWD CARGO TIE DOWN FITTING CORROSION REPAIR) REPAIR IS CLASSIFED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL RBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 520. STA 520, RBL 19, TIEDOWN FITTING CORROSION REPAIR CARRIED OUT IAW EA F-5340-137430 (FWD CARGO TIEDOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL LBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 660. STA 660, LBL 19, TIEDOWN FITTING CORROSION REPAIR CARRIED OUT IAW EA NR F-5340-137430. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-1-200.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL LBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 520. FLOOR SIDE PANEL AT LBL 19.00 REPAIRED IAW EA F-5340-137430. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — DELAMINATED (LEFT ELEVATOR) · airframe 83,960 hrs · 29,058 cycles

LEFT ELEVATOR LOWER SURFACE OTBD TIP METAL DOUBLER SUSPECT DELAMINATED AT T/E 0.5" X 0.5". DELAMINATED LT ELEVATOR LOWER SURFACE OTBD TIP DOUBLER REPAIRED IAW EA NR F-5520-133348 (TITLE: LT ELEVATOR T/E OTBD TIP UPPER SURFACE DELAMINATION REPAIR). REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL RBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 780, STA 780, RBL 19, TIE DOWN FITTING REPAIRED IAW EA F-5340-137430 (FWD CARGO TIE DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STANCHION — CRACKED (ZONE 100) · airframe 83,960 hrs · 29,058 cycles

AFT CARGO RT BS 1220 SIDE WALL STANCHION FOUND CRACKED. AFT CARGO RT STA 1220 CRACKED STANCHION. R & R IAW SRM 51-40-02, REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL LBL 19.00 ATTACHED TIE DOWN FOUND WTIH SURFACE CORROSION AS MARKED AT STA 640. STA 640 TIE DOWN FITTING CORROSION REPAIR CARRIED OUT IAW EA NR F-5340-134430. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1220 LT STA 1220, LT TIE DOWN FITTING REPAIRED IAW EA F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED STA 1320, LT STA 1320 LT TIE DOWN FITTING REPAIRED IAW EA F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1220, RT. STA 1220 RT TIE DOWN FITTING REPAIRED IAW E A F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL RBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 540. STA 540, RBL 19, TIE DOWN FITTING REPLACED IAW EA F-5340-137430 (FWD CARGO TIE-DOWN FITINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL RBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 660. STA 660, RBL 19, TIE DOWN FITTING REPAIRED IAW EA F-5340-137430 (FWD CARGO TIE DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1500 LT. STA 1500, LT TIE DOWN FITTING REPAIRED IAW EA NR F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL LBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 780. STA 780, LBL 19 TIEDOWN FITTING CORROSION REPAIR CARRIED OUT IAW EA NR F-5340-137430. FWD CARGO TIEDOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL LBL 19.00 TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 760. STA 760, LBL 19 TIEDOWN FITTING CORROSION REPAIR CARRIED OUT IAW EA NR F-5340-137430. (FWD CARGO TIEDOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1560 LT STA 1560, LT TIE DOWN FITTING REPAIRED IAW EA F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (BS 1500) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1500 RT. RT STA 1500 TIE DOWN FITTING REPAIRED IAW EA NR F-5340-137429 [AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL LBL 19.00 TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 700. STA 700, LBL 19, TIE DOWN FITTING CORROSION REPAIR CARRIED OUT IAW EA NR F-5340-137430. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 1600 LT. STA 1600 LT TIE DOWN FITTING REPAIRED IAW EA F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL RBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 820. STA 820, RBL 19, TIE DOWN FITTING REPAIRED IAW EA F-5340-137430 (FWD CARGO TIE DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR PANEL SUPPORT RBL 10.45 STA 1480 INTERCOSTAL TIE DOWN FOUND CORRODED AS MARKED. CORRODED TIE DOWN FITTING AT STA 1480, RBL 10.45. R & R IAW EA F-5340-137429 (AFT CARGO TIE DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1620 LT. STA 1620, LT, TIE DOWN FITTING REPAIRED IAW EA F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL RBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 680. STA 680, RBL 19, TIE DOWN FITTING REPAIRED IAW EA NR F-5340-137430 (FWD CARGO TIE DOWN FITTINGS CORROSION REPAIR). REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1240, RT STA 1240, RT TIE DOWN FITTING REPAIRED IAW EA F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1540 LT. STA 1540 LT, TIE DOWN FITTING REPAIRED IAW EA F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1520, RT. STA 1520, RT, TIE DOWN FITTING REPAIRED IAW EA F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1380 LT. STA 1380, LT, TIE DOWN FITTING REPAIRED IAW EA F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL LBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 560. FLOOR SIDE PANEL AT STA 560, LBL 19 REPAIRED IAW EA F-5340-137430. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1560 RT. RT STA 1560 TIE DOWN FITTING REPAIRED IAW EA NR F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SUPPORT — CRACKED (PYLON FAIRING) · airframe 83,960 hrs · 29,058 cycles

RT PYLON AFT COMMON NOZZLE UPPER FAIRING LOWER PANEL SUPPORT FWD ANGLES (BOTH) FOUND FWD CORNER CRACK. CRACKED ANGLES ON RT PYLON AFT COMMON NOZZLE UPPER FAIRIING LOWER PANEL. R & R IAW EA F-7110-137437 (COMMON NOZZLE TO STRUT FAIRING -PARTS ANGLE FABRICATIION FOR PN LJ34907 & LJ34909). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL LBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 800. STA 800, LBL 19 TIEDOWN FITTING CORROSION REPAIR CARRIED OUT IAW EA NR F-5340-137430. (FWD CARGO TIEDOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1340, RT. RT STA 1340 TIE DOWN FITTING REPAIRED IAW EA NR F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1280 RT. RT STA 1280 TIE DOWN FITTING REPAIRED IAW EA NR F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL RBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 839. STA 839, RBL 19, TIE DOWN FITTING REPAIRED IAW EA F-5340-137430 (FWD CARGO TIE DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1420, LT. STA 1420, LT TIE DOWN FITTING REPAIRED IAW EA NR F-5340-137429 (AFT CARGO TIE DOWN FITTING CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — MISREPAIRED (ZONE 300) · airframe 83,960 hrs · 29,058 cycles

APU ACCESS DOOR RT WITH EXISTING REPAIR DOUBLER AT AFT LATCH ACCESS HOLE. APU RT ACCESS DOOR EXISTING DOUBLER AT AFT LATCH ACCESS HOLE REPLACED IAW SRM 51-70-13 FIG 1, REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SUPPORT — GOUGED (LT WING TE FLAP) · airframe 83,960 hrs · 29,058 cycles

LT WING T/E INBD FLAP OTBD CARRIAGE FOUND GOUGE ON OTBD EDGE OF THE ARM. GOUGED ARM OF LT INBD FLAP OTBD CARRIAGE REPAIRED IAW EA NR F-5750-135811 (LT INBD MAIN FLAP OTBD CARRIAGE FWD ROLLER SUPPORT GOUGE REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: PLATE — CORRODED (R2 DOOR CAM) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

R2 PAX DOOR LOWER DOOR HINGE CAMPLATE HAS SURFACE CORROSION. CORROSION REPAIR CARRIED OUT IAW E.A.F-5210-135809. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: PLATE — CORRODED (L2 DOOR CAM) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

L2 PAX DOOR LOWER HINGE UPPER AND LOWER CAMPLATES CORRODED. L2 PAX DOOR CAM PLATES REPAIRED IAW E.A. F-5210-135809. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

NOSE WHEEL WELL AREA WITH EVIDENT OF CORROSION AT SUPPER RT EDGE OF FLANGE BETWEEN RT BS 357 TO 365, RBL 20.50, WL 192.50. CORRODED ANGLE IN NOSE WHEEL WELL RH SIDE FROM BS 357 TO BS 365 REPLACED IAW SRM 51-40-02 REV. 99. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT — CRACKED (BS 1380) · airframe 83,960 hrs · 29,058 cycles

AFT CARGO RT STA 1380 CEILING PANEL SUPPORT FOUND CRACKED. CRACKED AFT CARGO CEILING SUPPORT AT STA 1380 REPAIRED IAW EA F-5310-137435 (FLOORBEAM STABILIZATION STRAP REPAIR BS 1360 TO BS 1380, RBL 44.25). REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SHIM — CRACKED (BS 1380) · airframe 83,960 hrs · 29,058 cycles

AFT CARGO DOOR CUTOUT STA 1380 DOOR LATCH SHIM FOUND CRACKED. CRACKED SHIM REPLACED ON AFT CARGO DOOR CUTOUT AT STA 1380. R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO FLOOR SUPPORT, LBL 2.90 STA 1445 TO STA 1498, FASTENERS HOLD AREA CORROSION AS MARKED. CORRODED FLOOR SUPPORT. R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO FLOOR SUPPORT, LBL 16.10 STA 1445 TO STA 1498 HOLE AREA CORROSION AS MARKED. CORRODED FLOOR SUPPORT FROM STA 1445 TO STA 1498, LBL 16.10, R & R IAW SRM 51-40-02 REV.99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT AT STA 620, DOOR CUTOUT SIDE WALL SUPPORT FOUND CORRODED AND CRACKED. CORRODED AND CRACKED SIDEWALL SUPPORT AT STA 620 DOOR CUTOUT R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 83,960 hrs · 29,058 cycles

AFT CARGO - DURING INSTALLATION LINING SUPPORT ANGLE AT BS 1440 RT SIDE FOUND CRACK. CRACKED LINING SUPPORT ANGLE AT BS 1440 RT SIDE R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO FLOOR SUPPORT, LBL 2.90 STA 1498 TO STA 1640, FASTENERS HOLE AREA CORROSION AS MARKED. CORRODED FLOOR SUPPORT FROM STA 1498 TO STA 1640, LBL 2.9, R & R IAW SRM 51-40-02 REV.99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO FLOOR SUPPORT, LBL 16.10, STA 1200 TO STA 1341, FASTENERS HOLE AREA CORROSION AS MARKED. CORRODED FLOOR SUPPORT FROM STA 1200 TO STA 1341, LBL 16, R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT, RBL 19.00 STA 530 UPPER SIDEWALL SUPPORT CRACKED AS MARKED. CRACKED SUPPORT AT STA 530, RBL 19, R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO COMPARTMENT FLOOR SIDE PANEL RBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 620. TIE-DOWN AT FWD CARGO STA 620, RBL 19 R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO FLOOR SUPPORT, RBL 7.55 STA 1200 TO STA 1341, FASTENER HOLE AREA CORROSION AS MARKED. CORRODED FLOOR SUPPORT FROM STA 1200 TO STA 1341, RBL 7.55, R & R IAW SRM 51-40-02 REV. 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO FLOOR SUPPORT, RBL 11.40 STA 1498 TO STA 1640, FASTENERS HOLE AREA CORROSION AS MARKED. CORRODED SUPPORT R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (FLOOR SUPPORT) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO STA 1375 STRINGER 23L SLOPE PANEL SUPPORT FITTING FOUND CORROSION. SUPPORT FITTING AT CARGO FOUND CORRODED THROUGH. FITTING REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: RETAINER — CORRODED (BS 560) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO DOOR CUTOUT LOWER SCUFF PLATE SUPPORT FITTING RETAINERS FOUND WITH SURFACE CORROSION AS MARKED, STA 560. CORRODED RETAINERS AT STA 560. R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: RETAINER — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO DOOR CUTOUT LOWER SCUFF PLATE SUPPORT FITTING RETAINERS FOUND WITH SURFACE CORROSION AS MARKED STA 600. R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 83,960 hrs · 29,058 cycles

EXISTING REPAIR DOUBLER ON EXTERIOR FUSELAGE SKIN AT BS 760 TO BS 780, STR 4R TO STR S5R. TO EVALUATE EXISTING REPAIR DOUBLER, REMOVED AND CARRIED OUT REPAIR IAW STA ENG EA NR 757-5331-08-E0641 REV A (SHORT EDGE MARGIN ON SKIN AT BETWEEN STA 700 AND STA 780, S-4R). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

FWD CARGO DOOR CUTOUT LOWER SCUFF PLATE SUPPORT FITTING RETAINERS FOUND WITH SURFACE CORROSION AS MARKED STA 615. CORRODED RETAINERS ON SCUFF PLATE FITTING AT STA 615 R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: PANEL — CORRODED (RUDDER) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

RUDDER EXTERIOR SURFACE LT BONDED CONDUCTIVITY FRAME WITH LIGHT SURFACE CORROSION BETWEEN RUDDER STA 381.269 TO STA 578.536. CORROSION REPAIR CARRIED OUT IAW EA NR F-5540-137419. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

CORROSION ON FLOOR SUPPORT AROUND 2 EA ANCHOR NUT HOLE AT STA 1020-1030 RBL 64. FLOOR SUPPORT REPAIRED IAW SRM 51-70-12 FIG 1 REV. 99. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — CORRODED (E/E DOOR) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

E & E DOOR ASSY SIDE FRAME AREA FOUND WITH CORROSION AS MARKED. R & R IAW SRM 51-40-02, REV. 99. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STANCHION — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT WITH LIGHT CORROSION AT RT STANCHION LOWER MOUNT AT BS 1440, RBL 19, ADJACENT TO STR 23R. STANCHION LOWER MOUNT AT AFT CARGO STA 1440, RBL 19 FOUND CORRODED THROUGH. STANCHION REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO FLOOR SUPPORT, RBL 2.90, STA 1445 TO STA 1498, FASTENERS HOLE AREA CORROSION AS MARKED. CORRODED FLOOR SUPPORT IN AFT CARGO FROM STA 1445 TO STA 1498, RBL 2.9, R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFED AS MINOR GMM 6-2-100 CRITERIA.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO FLOOR SUPPORT, RBL 7.55 STA 1445 TO STA 1498, FASTENERS HOLE AREA CORROSION AS MARKED. CORRODED AFT CARGO FLOOR SUPPORT FROM STA 1445 TO STA 1498, RBL 7.55. R & R IAW SRM 51-40-02 REV. 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-1-200 CRITERIA.

Part: HINGE — CRACKED (CARGO DOOR) · airframe 83,960 hrs · 29,058 cycles

AFT CARGO DOOR CUTOUT E6 RACK COVER LOWER HINGE FOUND CRACKED AT STA 1440. CRACKED HINGE AT AFT CARGO DOOR CUTOUT R & R IAW SRM 51-40-02, REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

CABIN: R4 PAX DOOR SILL "L" ANGLE IS CORRODED AT AFT DOOR FRAME. CORRODED L-ANGLE ON R4 PAX DOOR SILL REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: STIFFENER — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

CABIN: R4 PAX DOOR SILL BRACKETS CORRODED 12" AND 15.5" FROM FWD LOWER END OF DOOR FRAME. CORRODED BRACKETS ON R4 DOOR SILL REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 83,960 hrs · 29,058 cycles

AFT CARGO LT FRAME AT STA 1560 LOWER SIDEWALL SUPPORT FOUND CRACKED AT FASTENER HOLE AREA. CRACKED LT SIDEWALL SUPPORT AT STA 1560 R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRTIERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

CABIN FLOOR AFT RT INBD SEAT TRACK WITH LIGHT SURFACE CORROSION AT BS 1640, RBL 24. CORROSION ON SEAT TRACK AT BS 1640, RBL 24, FOUND OUT OF SRM LIMITS. SEAT TRACK R & R IAW SRM 51-40-02 REV.99. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: PANEL — CRACKED (LT PYLON) · airframe 83,960 hrs · 29,058 cycles

LT PYLON CRACK FOUND ON THE FWD LOWER CORNER OF PANEL NR 433 GR CUTOUT. REPAIRED IAW EA NR F-5450-135807. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

CABIN: 2L PAX DOOR SILL CHORD HAS EXFOLIATION CORROSION 7" FWD OF AFT DOOR FRAME. CORRODED SILL CHORD FWD OF L2 DOOR AFT DOOR FRAME REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FITTING — CRACKED (LT PYLON) · airframe 83,960 hrs · 29,058 cycles

LT ENG PYLON, 2 EACH CRACKS FOUND IN LT AFT INBD BOLT HOLE ON HORIZ FLANGE. (REF: EO F-5450-7-5006 P1 PG 13 STEP 2 FOR DETAILS). LT PYLON AFT BULKHEAD R & R IAW EA NR F-5450-135814. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CRACKED (RT NACELLE) · airframe 83,960 hrs · 29,058 cycles

RT ENGINE PYLON, 2 EACH CRACKS FOUND IN RT AFT INBD BOLT HOLE ON HORIZONTAL FLANGE. REF EO F-5450-7-5006 P2, PG 12 STEP 2. RT PYLON AFT BULKHEAD R & R IAW EA F-5450-135815 (AFT BULKHEAD FITTING REMOVAL AND INSTALLATION). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 400) · airframe 83,960 hrs · 29,058 cycles

NR 1 PYLON, ONE EACH CRACK FOUND AT FWD OTBD HOLE OF MID BULKHEAD. REFER EO F-5450-7-5005 P1 PG 19 STEP 1.8 FOR DETAILS. CRACKED FWD OTBD HOLE ON NR 1 PYLON MID BULKHEAD REPAIRED IAW EA NR F-5450-135810 (LT PYLON MID-BULKHEAD LOWER FLANGE INBD CRACK REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO AFT BULKHEAD STA 1720 AREA, RT ANGLE FOUND WITH CORROSION AS MARKED. CORRODED ANGLE AT BULKHEAD STA 1720 REMOVED AND REPLACED IAW SRM 51-40-02, REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1377 LT. CORRODED TIE-DOWN FITTING AT STA 1377 IN AFT CARGO COMPARTMENT REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

CORROSION ON DECK PLATE AT STA 1715, LBL 25. CORROSION REPAIR CARRIED OUT ON DECK PLATE AT STA 1715 IAW EA F-5320-135812 (BS 1715, LBL 25 AFT DECK PLATE CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SPLICE — CORRODED (FLOOR PANEL) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

AFT CARGO RT SIDE PANEL SPLICE AT STA 1530 FOUND CORROSION. CORRODED SPLICE AT AFT CARGO STA 1530, RT PANEL REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: PANEL — CRACKED (RT PYLON) · airframe 83,960 hrs · 29,058 cycles

RT WING PYLON PANEL 443GL CUTOUT FOUND CRACK AT PP STA 106.75 LWR FWD RADIUS OF PANEL CUTOUT AREA. CANNOT DETERMINE LENGTH. CRACK EXTENDS BEHIND INTERNAL STRUCTURE. REPAIRED IAW EA NR F-5450-135808. RT PYLON INBD STRUT SKIN PANEL REPAIR. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT NACELLE) · airframe 83,960 hrs · 29,058 cycles

RT WING PYLON PANEL 443AR (RT SIDE) CUTOUT FOUND CRACKED AT PP STA 106.75 LWR FORWARD RADIUS OF PANEL CUTOUT AREA. CANNOT DETERMINE LENGTH. CRACK EXTENDS BEHIND INTERNAL STRUCTURE. REPAIRED IAW EA F-5450-135806. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SUPPORT BRACKET — CRACKED (BS 843 S22L) · airframe 83,960 hrs · 29,058 cycles

FWD CARGO AT LT STA 843, STR 22L AREA FOUND SUPPORT BRACKET CRACKED. CRACKED BRACKET AT STA 843, STR 22L REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SKIN — CRACKED (LT PYLON) · airframe 83,960 hrs · 29,058 cycles

LT PYLON LWR PAN CRACK AT LT SIDE PP STN 277. CRACKED PAN ON LT PYLON AT PP STN 277. REMOVED AND REPLACED IAW SRM 51-40-02, REV.98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: ACCESS PANEL — CRACKED (ZONE 400) · airframe 83,960 hrs · 29,058 cycles

ENGINE NR 1 PYLON STRUT LT SKIN AT ACCESS PANEL CUTOUT (433AL), FLANGE LOWER FWD CORNER CRACK. REPAIRED IAW EA NR F-5450-135803. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SHIM — CRACKED (LT PYLON) · airframe 83,960 hrs · 29,058 cycles

LT PYLON UPPER PANEL 433DL FWD SUPPORT BRACKETS SHIMS CRACKED AND ANCHOR NUTS CORRODED. CRACKED SHIMS (BONDING STRIP) AND CORRODED ANCHOR NUTS ON LT PYLON UPPER PANEL 433DL REMOVED AND REPLACED IAW SRM 51-40-02 REV.98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: BRACKET — CRACKED (LT PYLON) · airframe 83,960 hrs · 29,058 cycles

LT PYLON UPPER AREA BRACKET FOUND CRACK AT PP STN 174 RT SIDE. CRACKED BRACKET AT PP STA 174 ON LT PYLON REMOVED AND REPLACED IAW SRM 51-40-02 REV 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SHIM — CRACKED (LT PYLON) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

LT PYLON UPPER PANEL 43ALL FWD SUPPORT BRACKETS SHIMS CRACKED AND ANCHOR NUTS CORRODED. LT PYLON UPPER PANEL 43ALL FWD SUPPORT BRACKET DOUBLER SHIMS AND ANCHOR NUTS REPLACED IAW SRM 51-40-02 REV.98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: BRACKET — CRACKED (ZONE 400) · airframe 83,960 hrs · 29,058 cycles

LT PYLON VERTICAL STIFFENER BRACKET CRACK AT PP STA 166 RT SIDE. REMOVED AND REPLACED IAW SRM 51-40-02 REV.98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: BRACKET — CRACKED (ZONE 400) · airframe 83,960 hrs · 29,058 cycles

LT PYLON AFT FAIRING UPPER SUPPORT LT BRACKET CRACK AT PP STA 208. CRACKED BRACKET ON LT PYLON AFT FAIRING UPPER SUPPORT REMOVED AND REPLACED IAW SRM 51-40-02 REV. 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

CABIN - 2L PAX DOOR SILL AFT "L" ANGLE HAS CORROSION. CORRODED L-ANGLE ON L2 PAX DOOR SILL R & R IAW SRM 51-40-02, REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT BRACKET — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

CORROSION ON L1 DOOR SCUFF PLATE FWD AND AFT EDGE SUPPORT BRACKET. REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 83,960 hrs · 29,058 cycles

CABIN - INTERCOSTAL AT FLOORBEAM STA 1320, RBL 45 FOUND CRACKED. CRACKED INTERCOSTAL REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 83,960 hrs · 29,058 cycles

CABIN - INTERCOSTAL AT FLOORBEAM STA 1320, LBL 25 FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-40-02, REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,960 hrs · 29,058 cycles

CABIN - CORROSION ON FLOORBEAM AT STA 300, RBL 26-30. CORRODED FLOOR PANEL SUPPORT AT STA 300, RBL 26 TO RBL 30, R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.