N940FD

Part: FRAME — CRACKED (ZONE 200) · airframe 69,402 hrs · 24,055 cycles

BS 1640 S-14R I/B BOTTOM HOLE HAS CRACK INDICATIONS AT 4 & 9 O'CLOCK LOOKING AFT // BS 1640 S-14R O/B BOTTOM HOLE HAS A CRACK INDICATION AT 5 O'CLOCK LOOKING AFT. ACCOMPLISHED FRAME REPAIR AT STA. 1640 BTW STR. 9 & STR 20 IAW EA # F-5310- T0366462 "FUSELAGE- MAINFRAME- FRAME, STA 1640, S-14R, EO F- 5310-EO344602 CRACK INDICATIONS REPAIR-PARTIAL FRAME REPLACEMENT." "MAJOR REPAIR"

Part: FRAME — CRACKED (ZONE 100) · airframe 69,402 hrs · 24,055 cycles

BS 1640 S-14L I/B BOTTOM HOLE HAS A CRACK INDICATION AT 8 O'CLOCK LOOKING AFT. COMPLIED WITH ALL STEPS TO COMPLETION 1-10 OF EA T F-5310-T0366488 P1 FUSELAGE - MAINFRAME - CRACK INDICATION AT STA 1640 FUSELAGE FRAME WEB, S-14L AT LOWER INBOARD HOLE LOCATION - FREEZE PLUG REPAIR. CAT 'B' REPAIR MAJOR REPAIR

Part: CLAMP — UNSECURE (LT ENG V BAND) · airframe 68,935 hrs · 23,715 cycles

ON CLIMB OUT PASSING 16000 EICAS MESSAGE L ENG OVHT. LEVELED AT 19000 TO COMPLY WITH QRH 8.1.20. L ENG THROTTLE WAS BROUGHT TO IDLE AND MESSAGE CLEARED AFTER APPROXIMATELY 30 SECONDS. CONTINUED CLIMB TO 350 AND CONTINUED TO DESTINATION WITH NO FURTHER ISSUES OR ABNORMAL INDICATIONS NOTED AT ANY TIME. EMERGENCY WAS DECLARED DUE TO NON NORMAL LANDING CONFIGURATION PER QRH. FOUND AFT V-BAND CLAMP NOT SECURED ON THE INTERMEDIATE PRESSURE CHECK VALVE. WAS LEAKING WITH APU AIR APPLIED. TIGHTENED V-BAND CLAMP, LEAK CHECKED AND FOUND NO AIR LEAKING. RAN ENGINE REF JRH, LEAK CHECKED WITH ENGINE RUNNING AT IDLE. NO LEAKS. REF MM 36-11-06, JRH.

Part: GIRT BAR — DETACHED (R1 DOOR) · airframe 68,855 hrs · 23,646 cycles

UPON OPENING R1 DOOR, NOTICED GIRT BAR SLIDER HAD FALLEN OFF. WHILE ATTEMPING TO SECURE SLIDER, R1 DOOR SLIDE LIBERATED FROM DOOR. ACCOMPLISHED ADJUSTMENT/TEST OF R1 DOOR GIRT BAR PER B757-200 AMM 52-11-25-5, FOUND LEAF SPRING ON FWD END OF GIRT BAR BENT AND NOT ALLOWING GIRT BAR SLIDER TO FULLY ENGAGED INTO GIRT BAR LIFTER ON DOOR WHEN DOOR IS OPENED. WILL REQUIRE NEW GIRT BAR, PART NOT STOCKED AT STATION. PART ON ORDER. R/R R1 DOOR GIRT BAR ASSY PER AMM 25-66-10-2. DOOR ARM/DISARM FUNCTIONS AS NORMAL NO FURTHER DEFECTS NOTED.

Part: FIRE WARNING — FALSE ACTIVATION (LT ENGINE) · airframe 68,799 hrs · 23,602 cycles

PDIS 940 26-10 7568 30MAR21 JAX FACT U AT CRUISE GOT INTERMITTENT L ENGINE FIRE WARNINGS. ALL ENGINE INDICATIONS AND AIRCRAFT PERFORMANCE NORMAL. AFTER APPROXIMATELY 3 MINUTES OF INTERMITTENT WARNINGS THEY STOPPED AND DID NOT OCCUR AGAIN DURING THE REMAINDER OF THE FLIGHT. FACT 30MAR21 10:33 JAX U REF B757 FIM 26-11-00 FT 802 FIG 103, PULLED AND REINSTALLED AFOLTS CARD REF B757 M.M. 26-10-01-4-0. FIRE SYSTEM TEST NORMAL AT THIS TIME. NOTE: MEL STILL IN PLACE FOR DEFERRED LOOP.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 68,796 hrs · 23,599 cycles

L1 DOOR EMERGENCY SLIDE PRESSURE INDICATING IN RED. REMOVED AND REPLACED L1 DOOR SLIDE/RAFT PER AMM 25-66-01-4.

Part: SENSOR — UNSECURE (R3 WINDOW) · airframe 68,237 hrs · 23,223 cycles

REJECTED T/O AT 50 KNOTS. ECIAS DISPLAYED RT SIDE WINDOW PERFORMED REJECTED T/O CHECK LIST IN QRH. FOUND THE R3 WINDOW SENSOR MOUNT LOOSE. SECURED THE SENSOR MOUNT. PERFORMED WINDOW HEAT ADJUSTMENT AND TEST IAW MM 30-41-01-03 AND CHECKED NORMAL. ACFT OK FOR SERVICE.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 67,947 hrs · 23,036 cycles

R/H HORIZONTAL STAB UPPER SKIN AUX SPAR PREVIUS REPAIR APROX.. 4" 3/4 CIRCUNFERENCE DELAM AT STA 78.00 REMOVED EXISTING REPAIR AND ACCOMPLISHED PERMENENT REPAIR ON R/H HORIZONTAL STAB UPPER SKIN AT STA 78 IAW B757 SRM 55-10-01-1A AND IAW B757 SRM 51-70-10-2R REP. 2

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,947 hrs · 23,036 cycles

AFT LOWER CARGO COMPARTMENT, CORROSION, SHEAR TIE STA 1480 BETWEEN STR 28R AND STR 29R. REMOVED CORROSION ON SHEAR TIE AT STA 1480 BETWEEN STR 28R-29R IAW SRM 51-10-02-0G. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A FIG 101 DET 2. REMOVED SHEAR TIE IAW SRM 51-40-02-0G. FABRICATED NEW SHEAR TIE, TREATED, PRIMED AND TOP COATED AND INSTALLED IAW SRM 51-40-05-0G, DWG 146N1015 REV C, SRM 51-20-01-0G, AMM 51-21-10-7 AND SRM 51-40-02-0G.

Part: BEAM — GOUGED (CARGO DOOR) · airframe 67,947 hrs · 23,036 cycles

3EA SMALL GOUGES - MAIN CARGO DOOR VERTICAL BEAM INBD CHORD INTERIOR SURFACE - APPROX STA 490,BETWEEN WATER LINE 210 - 215. REMOVED GOUGES ON MAIN CARGO DOOR VERTICAL BEAM I\B CHORD APPROX STA 490 BETWEEN WL 210-215 IAW B757 SRM 51-40-02. FOUND TO BE OUT OF LIMITS IAW B757 SRM 52- 30-02-1A FIG 101 DET IV. REMOVED DAMAGED FRAME, FABRICATED AND INSTALLED NEW FRAME IAW B757 SRM 51-40-02 AND BOEING DWG 65-25327 REV C AND U

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,947 hrs · 23,036 cycles

MAIN DECK STA 1055 BETWEEN BL0-RBL 24.75 FLOOR SUPPORT CORRODED. ACCOMPLISHED IAW EA F-5310-T0352036 P1 FUSELAGE - MAINFRAME -MAIN CARGO FLOOR SUPPORT STA 1055 CORRODED, NEW PART FABRICATION TEMPER ATERATION, REMOVED CORR IAW SRM 51-10-02-OG, FOUND TO BE OUT LIMITS IAW SRM 53-00-51-1A FIG 101 DETAIL VI. REMOVED, FABRICATED AND INSTALLED FLOOR SUPPORT IAW SRM 51-40-02-OG, 51-40-05-OG, 51-40-08-OG AND DWG 144N5005 REV - AND REV A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,947 hrs · 23,036 cycles

MAIN DECK SEAT TRACK FLANGE CORRODED BETWEEN STA 1180 - 1200 RBL 45.5. REMOVED CORROSION ON SEAT TRACK FLANGE AT STA 1180 TO 1200, RBL 45.5 IAW SRM 51-10-02-OG. EVALUATED DAMAGED AREA, ORIG MAT =.070', REM MAT = .040",MAT LOSS = .030" FOUND TO BE OUT LIMITS IAW SRM 53-00-52-1A, FIG 101, DETAL VIII. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AT STA 1180 TO 1280, RBL 45.5 IAW SRM 51-40-02-OG AND B DWG 146N5217, REV A AND M.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,947 hrs · 23,036 cycles

AFT CARGO COMPT SHEAR WEB STRUCTURE CLIP IS CRACKED AT O/B RBL 24.75" AND BS 1715. REMOVED, FABRICATED AND INSTALLED CLIP ON AFT CARGO COMP SHEAR WEB STRUCTURE AT O/B SIDE OF RBL 24.75, STA 1715 IAW SRM 51-40-02-OG AND B DWG 146N5329,REV - AND REV C.

Part: SHEAR TIE — CRACKED (EMERGENCY EXIT) · airframe 67,947 hrs · 23,036 cycles

FUSELAGE LT EMERGENCY EXIT INTERNAL STRUCTURE AT MID SECTION AFT STIFFENER CRACKED BETWEEN STR 13L TO STR 14L ON STA 1340. (SHEAR TIE) REMOVED AND REPLACED STIFFENER (SHEAR TIE) ON LT EMERGENCY EXIT DOOR AT INTERNAL STRUCTURE MID SECTION AFT SIDE IAW SRM 51-40-02-OG, FABRICATED NEW STIFFENER (SHEAR TIE) IAW DRAWING 146N6346 REV A AND REV -.

Part: HINGE — CRACKED (R2 DOOR) · airframe 67,947 hrs · 23,036 cycles

MAIN CABIN R2 DOOR ENTRY DOOR UPPER HINGE CUT OUT CRACKED. COMPLIED WITH FEDEX EA #: F-5210-T0351839 P1 TITLE : DOORS - PASSENGER / CREW - R-2 DOOR FOWARD FRAME UPPER HINGE CUT OUT SRM REPAIR - RSC TRACKING AND B 757 SRM 52-10-02-2R FIG 201 REP 1 DET III.

Part: SKIN — CRACKED (R2 DOOR) · airframe 67,947 hrs · 23,036 cycles

MAIN CABIN R2 DOOR ENTRY DOOR UPPER HINGE CUT OUT CRACKED. COMPLIED WITH EA #: F-5210-T0351839 P1 TITLE : DOORS - PASSENGER / CREW - R-2 DOOR FOWARD FRAME UPPER HINGE CUT OUT SRM REPAIR - RSC TRACKING AND B 757 SRM 52-10-02-2R FIG 201 REP 1 DET III.

Part: LINE — FAILED (HYD SYSTEM) · airframe 66,660 hrs · 22,116 cycles

GEAR DOORS EICAS MESSAGE DURING FINAL. REMOVED AND REPLACED THE FWD RETRACT HYD LINE ON THE RT MAIN LANDING GEAR DOOR ACTUATOR IAW AMM 20-10-10-4. PERFORMED AN OPS CHECK OF THE MAIN LANDING GEAR DOOR IAW AMM 32-32-12-4, PARA 3.G. OPS AND LEAK CHECKED GOOD. OK FOR SERVICE.

Part: GIRT BAR — BENT (L1 DOOR) · airframe 66,389 hrs · 21,938 cycles

LEFT L1 DOOR GIRT BAR TAB BENT. REMOVED AND REPLACED L1 DOOR GIRT BAR IN REF TO AMM 25-6601-4. OPS CHECK NORMAL. OK TO CONTINUE.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 65,781 hrs · 21,563 cycles

RH EMERGENCY EXIT LIGHTS NOT TESTING. REMOVED AND REPLACED THE M730 POWER SUPPLY BATTERY PACK IAW AMM 33-51-07-2, OPS CHECKED GOOD

Part: SIGN — MALFUNCTIONED (CABIN) · airframe 65,369 hrs · 21,285 cycles

CENTER CEILING EXIT SIGN AND R1 DOOR EXIT SIGN DO NOT ILLUMINATE DURING EMERGENCY LIGHT TEST. EMERGENCY LIGHTS OP CHECKS GOOD IAW MM 33-51-00-5. OK FOR SERVICE.

Part: LIGHT — MALFUNCTIONED (EXTERIOR) · airframe 65,369 hrs · 21,285 cycles

EXTERIOR EMERGENCY LIGHT BEHIND R1 DOOR NOT ILLUMINATED DURING EMERGENCY LIGHT TEST. EMERGENCY LIGHTS OP CHECKS GOOD. IAW MM 33-51-00-5. OK FOR SERVICE.

Part: GIRT BAR — OBSTRUCTED (ENTRY DOOR) · airframe 645 hrs · 20,756 cycles

RIGHT ENTRY DOOR DIFFICULT TO ARM. INSPECTED GIRT BAR ASSEMBLY IAW AMM 25-66-01-6. FOUND FOD IN DOOR SILL AREA NOT ALLOWING GIRT BAR TO REACH FLOOR LEVEL WHEN ARMED. REMOVED FOD & SLIDE NOW ARMS & DISARMS WITHOUT EFFORT. ACFT OK FOR SERVICE AT THIS TIME.

Part: RETAINER — OUT OF POSITION (NLG) · airframe 645 hrs · 20,716 cycles

WHEN RAISING GEAR ON TAKEOFF, HAD BIG VIBRATION FROM MAIN GEAR. AMBER DOOR & GEAR LIGHTS STAYED ILLUMINATED LONGER THAN USUAL, VERY NOISY. UPON INSPECTION FOUND RT NOSE WHEEL ASSEMBLY INBD BEARING RETAINER RING POPPED OUT & HANGING ON AXLE HOUSING. REPLACED NOSE TIRE ASSEMBLY.

Part: RESERVOIR — INOPERATIVE (R1 DOOR) · airframe 642 hrs · 20,515 cycles

ON BLOCK IN, FOUND R1 DOOR 1/2 OPEN WITH GRIT BAR STILL CONNECTED TO DOOR LOWER FRAME. REPLACED R1 DOOR EMER POWER RESERVOIR IAW MM 52-11-30-4. OPERATIONS NORMAL..

Part: LIGHT — INOPERATIVE (CABIN DOOR) · airframe 63,923 hrs · 20,260 cycles

LEFT MAIN CABIN DOOR WOULD NOT SHOW ARM SLIDE CORRECTLY. RELAMPED SLIDE ARMED WARNING LIGHT IAW SMP. LIGHT NOW FUNCTIONS WHEN DOOR IS ARMED.

Part: ACTUATOR — FAILED (SLAT SYSTEM) · airframe 63,445 hrs · 19,887 cycles

DURING DEPARTURE, WHEN FLAPS SELECTED TO UP THE LE SLAT DISAGREE EICAS CAME ON. THE LE DISCREET LIGHT ILLUMINATED. R & R NR 6 OTBD LE SLAT DRIVE ROTARY ACTUATOR IAW MM 27-81-18-4. OPS CHECKED GOOD.

Part: SHEAR TIE — CRACKED (BS 1300) · airframe 63,304 hrs · 19,785 cycles

FOUND SHEAR TIE CRACKED AT BS 1300 BETWEEN STRINGER 20 - 21L. REMOVED DAMAGED SHEAR TIE, FABRICATED NEW & INSTALLED IAW DWG 146N2002 REV EU & SRM 51-40-02.

Part: FSEU — INOPERATIVE (SLAT SYS) · airframe 63,234 hrs · 19,729 cycles

LEADING EDGE SLAT DISAGREE LIGHT ILLUMINATED DURING CONFIGURATION. FOLLOWED QRH, UNEVENTFUL LANDING. T/S PER FIM 27-81 FAULT TREE 803 FIG. 104 PG. 126 BLOCK 2, THE OVERLOAD INDICATOR WAS RESET. CHECKED ALL RIGHT WING ROTARY ACTUATORS PER MM 27-81-18 FIG 6, NON TRIPPED. RAN FLAPS/SLATS SEVERAL CYCLES AND PERFORMED BITE CHECK ON THE FSEU, NO FAULTS REOCCURRED. FLAPS/SLATS OPERATE NORMALLY AT THIS TIME, NO FAULTS NOTED. ACFT OK FOR FLIGHT.

Part: COVER — OUT OF POSITION (R1 DOOR) · airframe 62,582 hrs · 19,285 cycles

WHEN CLOSING AND ARMING, RT DOOR TAB POPS OUT TO INDICATE DOOR IS ARMED APPEARS TO BE BINDING AND DOES NOT POP OUT. FOUND TAB HANGING UP ON DOOR COVERING, TRIMMED COVERING AND PERFORMED OPS CHECK OF SLIDE ARM/DISARM FUNCTION IAW AMM 52-11-20-5. POP OUT TAB WORKS NORMALLY.

Part: COVER — LOOSE (L1 DOOR SLIDE) · airframe 62,347 hrs · 19,119 cycles

L1 DOOR SLIDE COVER LOOSE. SECURED & INSTALLED L1 DOOR SLIDE COVER IAW MM 25-66-01-4. OPS NORMAL.. OK FOR SERVICE.

Part: COVER — UNSECURE (ESCAPE SLIDE) · airframe 62,246 hrs · 19,016 cycles

BOTH ENTRY DOORS SLIDE COVERS NOT ATTACHED AT BOTTOM. SECURED BOTH ENTRY DOOR SLIDE COVER REF AMM 25-66-01-4.

Part: LAMP — INOPERATIVE (DOOR SLIDE) · airframe 61,718 hrs · 18,742 cycles

DOOR SLIDE ILLUMINATION LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.

Part: GIRT BAR — OUT OF POSITION (R1 DOOR) · airframe 61,706 hrs · 18,735 cycles

R1 DOOR ARMED LIGHT INOPERATIVE. REPOSITIONED GIRT BAR IAW AMM 25-66-10-2-0. OPS CHECKED GOOD.

Part: TARGET — MISSING (DOOR GIRT BAR) · airframe 61,680 hrs · 18,717 cycles

RT MAIN DOOR ARMING LIGHT WOULD NOT COME ON WHEN DOOR LATCHED SHUT AND GIRTH BAR FELL OUT OF STOWED POSITION. FOUND PROXIMITY SWITCH TARGET ON GIRT BAR NOT INSTALLED, REPOSITIONED TARGET ON GIRT AND INSTALLED GIRT BAR ON DOOR. ADJUSTEMENT CHECKED IAW MM 25-66-11-2-0, OPS CHECKED NORMAL.

Part: DOUBLER — MISSING (CARGO DOOR SKIN) · airframe 61,638 hrs · 18,696 cycles

FWD LWR CARGO NR1 DOOR INTERNAL SKIN SURFACE FOUND INTERNAL SKIN DOUBLER MISSING IN APPROX (5") AREA AT DOOR UPPER AFT CORNER. REPAIR CARRIED OUT IAW EA F-5230-154463, PART 1 (CARGO DOORS - EXISTING TRIM OUT FOUND ON NR 1 CARGO DOOR ASSY UPPER AFT CORNER OUTER SKIN). REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — LOOSE (NR 1 NACELLE) · airframe 61,638 hrs · 18,696 cycles

NR 1 NACELLE STRUT INBD BATHTUB FITTING MOUNTING BOLTS, FOUND LOOSE. BATHTUB FITTING R & R IAW EA F-5450-154642A.

Part: SKIN — DAMAGED (ZONE 500) · airframe 61,638 hrs · 18,696 cycles

LT WING NR 5 SLAT FOUND SMALL DRILLED HOLE AT 22" FROM INBD. REPAIRED IAW EA F-5750-157114. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE ROD — SHORT (ZONE 200) · airframe 61,638 hrs · 18,696 cycles

WHILE CARRYING OUT EO F-2530-7-5000, PT9, STEP 3, GALLEY 1A UPPER CENTER ATTACHING ROD WILL NOT FIT (TOO SHORT). EA F-2530-153492 COMPLIED WITH. THIS ALTERATION IS CLASSIFIED AS MINOR IAW GMM.

Part: WEB — TORN (PAX DOOR) · airframe 61,638 hrs · 18,696 cycles

R4 DOOR, FOUND A TEAR IN DOOR LIGHTNING HOLE BETWEEN 2ND AND 3RD FRAMES. COMPLIED WITH EA F-5210-153486, PART 1. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM.

Part: SKIN — DENTED (ZONE 200) · airframe 61,638 hrs · 18,696 cycles

DENT ON EXTERIOR SKIN AT BS 1690 AT STRINGER 16-17R. DENT REPAIR CARRIED OUT AS PER E.A. F-5330-154485. REPAIR IS CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 61,638 hrs · 18,696 cycles

FLOORBEAM AT BS 324, RBL 38 TO 40 HAS CORROSION ON UPPER TEE. CORROSION FOUND WITHIN SRM LIMITS. REMOVED & REPLACED IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: STRINGER FITTING — DAMAGED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

AFTER DOUBLER REMOVAL AT BS 1720, FOUND STRINGER END FITTING AT FORWARD SIDE OF BULKHEAD AT STRINGER 29 RT WAS DAMAGED. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: STRINGER FITTING — DAMAGED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

AFTER DOUBLER REMOVAL AT BS 1720, FOUND STRINGER END FITTING AT AFT SIDE OF BULKHEAD AT STRINGER 29 RT WAS DAMAGED. STRINGER FITTING R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: FRAME — CHAFED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO COMP, FRAME AT BS 1520 UPPER SURFACE CHAFED BETWEEN STRINGER 22 & 23R. REPAIR CARRIED OUT ON FRAME AT STA 1520 BETWEEN S-22R AND S-23R IAW EA F-5310-153485. REPAIR IS CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,638 hrs · 18,696 cycles

FLOORBEAM AT STA 377, BL 0 TO LBL 45 HAS CORROSION ON UPPER CHORD. CORRODED FLOORBEAM AT STA 377, R & R IAW SRM 51-40-02, REV 104, WITH EA F-5100-1544446 (ALTERNATE ANODIZING METHOD) COMPLIED. REPAIR IS CLASSIFIED AS MAJOR.

Part: STRINGER FITTING — DAMAGED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

AFTER DOUBLER REMOVAL AT BS 1720, FOUND STRINGER END FITTING AT AFT SIDE OF BULKHEAD AT STRINGER 29 LT WAS DAMAGED. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: FRAME — DAMAGED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO COMP, AFTER REMOVAL OF FASTENERS FOUND FRAME BS 1380 HAS ELONGATED HOLE BETWEEN STR 25 & 26R. REPAIR CARRIED OUT IAW EA F-5310-157117. REPAIR IS CLASSIFIED AS MAJOR.

Part: STRINGER FITTING — DAMAGED (BS 1720) · airframe 61,638 hrs · 18,696 cycles

FOUND BS 1720 STRINGER 29L END FITTING AT FORWARD SIDE OF BULKHEAD DAMAGED. END FITTING R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

FWD LWR CARGO COMP, LT TIE DOWN FITTING HAS CORROSION AT STA 800. REPAIR CARRIED OUT IAW EA F-5340-154469. REPAIR CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO COMP, RIGHT TIE DOWN FITTING HAS CORROSION AT BS 1220. REPAIR CARRIED OUT IAW EA F-5340-154470. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

FWD LWR CARGO COMP, RT TIE DOWN FITTING HAS CORROSION AT STA 540. REPAIR CARRIED OUT IAW EA F-5340-154469. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO COMP, LT TIE DOWN FITTING HAS CORROSION AT STA 1260. REPAIR CARRIED OUT IAW EA F-5340-154470. REPAIR CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO COMP, RIGHT TIE DOWN FITTING HAS CORROSION AT BS 1260. REPAIR CARRIED OUT IAW EA F-5340-154470. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO COMP, LT TIE DOWN FITTING HAS CORROSION AT STA 1280. REPAIR CARRIED OUT IAW EA F-5340-154470. REPAIR CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO COMP, LT TIE DOWN FITTING HAS CORROSION AT STA 1340. REPAIR CARRIED OUT IAW EA F-5340-154470. REPAIR CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

FWD LWR CARGO COMP, RT TIE DOWN FITTING HAS CORROSION AT STA 680. REPAIR CARRIED OUT IAW EA F-5340-154469. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO COMP, TIE DOWN FITTING HAS CORROSION AT BS 1560 LBL 2.90. REPAIR CARRIED OUT IAW EA F-5340-154470. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

FWD LWR CARGO COMP, LEFT TIE DOWN FITTING HAS CORROSION AT STA 820. REPAIR CARRIED OUT IAW EA F-5340-154469. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (BS 1480) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO COMP, LEFT TIE DOWN FITTING HAS CORROSION AT BS 1480. REPAIR CARRIED OUT ON LT TIE-DOWN FITTING IAW EA F-5340-154470. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 300) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO COMP LEFT TIE DOWN FITTING HAS CORROSION AT BS 1240. REPAIRED IAW EA F-5340-154470. REPAIR CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (BS 1400) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO, LT TIE DOWN FITTING HAS CORROSION AT BS 1400. REPAIRED IAW EA F-5340-154470. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO COMP, LEFT TIE DOWN TIE DOWN FITTING HAS CORROSION AT BS 1580. REPAIR CARRIED OUT ON LT TIE-DOWN FITTING IAW EA F-5340-154470. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (BS 1420) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO COMP, LT TIE DOWN FITTING HAS CORROSION AT BS 1420. REPAIR CARRIED OUT IAW EA. F-5340-154470. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO COMP, RIGHT TIE DOWN FITTING HAS CORROSION AT BS 1520. REPAIR CARRIED OUT IAW EA F-5340-154470. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO COMP, LT TIE DOWN FITTING HAS CORROSION AT STA 1300. REPAIR CARRIED OUT IAW EA F-5340-154470. REPAIR CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

FWD LWR CARGO COMP, LT TIE DOWN FITTING HAS CORROSION AT STA 839. REPAIR CARRIED OUT IAW EA F-5340-154469. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO COMP, RIGHT TIE DOWN FITTING HAS CORROSION AT BS 1300. REPAIR CARRIED OUT IAW EA F-5340-154470. REPAIR IS CLASSIFIED AS MAJOR.

Part: CREASE BEAM — MISREPAIRED (BS 1400) · airframe 61,638 hrs · 18,696 cycles

CREASE BEAM AT BS 1400 RT MISREPAIRED. REPAIRED IAW EAF-5310-157116.

Part: SKIN — CORRODED (RT WING TE FLAP) · airframe 61,638 hrs · 18,696 cycles

RT OTBD MAIN FLAP LOWER SURFACE PANEL INNER SKIN FOUND CORRODED AT FLAP FWD SPAR, 113" FROM WBL 302.0. REPAIR CARRIED OUT IAW EA F-5750-157102. REPAIR IS CLASSIFIED AS MAJOR.

Part: FLOORBEAM — UNKNOWN (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

FLOORBEAM AT BS 324 FROM RBL 58 TO RBL 64 THERE IS AN EXISTING REPAIR. REMOVED AND UPPER CHORD REPLACED IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: STRINGER — DAMAGED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO COMP, SCRATCH MARK ON STRINGER S25L BETWEEN BS 1360 - 1380. REPAIR CARRIED OUT IAW EA F-5310-157115. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — DAMAGED (BS 1700) · airframe 61,638 hrs · 18,696 cycles

CABIN, AFTER DECK PLATE REMOVAL, FLOORBEAM AT STA 1700, RBL 55 UPPER CHORD HAS 2 HOLES TOO CLOSE TOGETHER. REPAIR CARRIED OUT IAW EA F-5310-154452. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CRACKED (LT WING) · airframe 61,638 hrs · 18,696 cycles

WHILE PERFORMING E F-5450-7-5003 C2 PT3 STEP 41 PANEL 10, APPROX 0.010" CRACK STILL FOUND ON LT WING INBD HOLE FWD SIDE AFTER 2ND EDDY CURRENT INSPECTION. REPAIR CARRIED OUT IAW EA F-5450-157110 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 61,638 hrs · 18,696 cycles

RIGHT OTBD MAIN FLAP LOWER SURFACE PANEL INNER SKIN FOUND CORRODED AT FLAP FWD SPAR 83" FROM WBL 302.0. REPAIR CARRIED OUT ON RT OTBD FLAP OWER SURFACE PANEL SKIN IAW EA F-5750-157102. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — CORRODED (RT WING TE FLAP) · airframe 61,638 hrs · 18,696 cycles

RIGHT OTBD MAIN FLAP LOWER SURFACE PANEL INNER SKIN FOUND CORRODED AT FLAP FWD SPAR 1" FROM WBL 302.0. REPAIR CARRIED OUT IAW EA F-5750-157102. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (NR 5 SLAT) · airframe 61,638 hrs · 18,696 cycles

LEFT WING NR 5 SLAT, FOUND SMALL DRILLED HOLE AT 22" FROM INBD. REPAIRED IAW EA F-5750-157114. REPAIR IS CLASSIFIED AS MAJOR.

Part: FRAME — CHAFED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO COMP, FRAME UPPER SURFACE HAS CHAFE AREA. BS 1580, BETWEEN S25-26L. REPAIRED IAW EA F-5310-153470. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DENTED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

FUSELAGE DENTED BS 1578 STR 17L. DENT REPAIRED IAW EA F-5330-154474. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (BS 700) · airframe 61,638 hrs · 18,696 cycles

FWD LWR CARGO BAY LEFT TIE DOWN FITTING HAS CORROSION AT BS 700. REPAIR CARRIED OUT IAW EA F-5340-154469. REPAIR CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (BS 1580) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO BAY TIE DOWN FITTING HAS CORROSION AT BS 1580, LBL 2.90. REPAIRED IAW EA F-5340-154470. REPAIR CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (BS 1220) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO BAY, LEFT TIE DOWN FITTING HAS CORROSION AT BS 1220. REPAIR CARRIED OUT IAW EA F-5340-154470. REPAIR CLASSIFIED AS MAJOR.

Part: SHIM — MIGRATED (ZONE 400) · airframe 61,638 hrs · 18,696 cycles

NR1 PYLON MID BHEAD LOWER FLANGE OTBD AFT SIDE AT PPSTA 174.30, FOUND SHIM MIGRATED. R & R IAW SRM 54-50-90, REPAIR 7, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — CORRODED (ZONE 400) · airframe 61,638 hrs · 18,696 cycles

NR 2 PYLON NAC STRUT STRUCTURE INBD ACCESS HOLE FOR PANEL 443GL CUT-OUT INNER EDGES FOUND WITH CORROSION. REPAIRED IAW EA F-5450-157113. REPAIR IS CLASSIFIED AS MINOR.

Part: SHIM — MIGRATED (ZONE 400) · airframe 61,638 hrs · 18,696 cycles

NR 2 PYLON MID BULKHEAD LOWER FLANGE INBD FWD SIDE AT PPSTA 174.30 FOUND WITH SHIMS MIGRATION. SHIMS R & R IAW SRM 54-50-90, REPAIR 7, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: SHIM — MIGRATED (ZONE 400) · airframe 61,638 hrs · 18,696 cycles

NR 2 PYLON MID BULKHEAD LOWER FLANGE OTBD FWD SIDE AT PPSTA 174.30 FOUND WITH SHIMS MIGRATION. SHIMS R & R IAW SRM 54-50-90, REPAIR 7, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: SHIM — MIGRATED (ZONE 400) · airframe 61,638 hrs · 18,696 cycles

NR 1 PYLON NAC STRUCTURE BETWEEN MID BULKHEAD LOWER FLANGE AND STIFFENER AT PPSTA 174.3 FOUND OTBD SHIMS MIGRATED. R & R IAW SRM 54-50-90, REPAIR 7, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: SHIM — MIGRATED (ZONE 400) · airframe 61,638 hrs · 18,696 cycles

NR 1 PYLON NAC STRUCTURE BETWEEN MID BULKHEAD LOWER FLANGE AND STIFFENER AT PPSTA 174.3. FOUND INBD SHIMS MIGRATED. R & R IAW SRM 54-50-90 REPAIR 7, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: STRINGER — CHAFED (BS 1681-1701) · airframe 61,638 hrs · 18,696 cycles

AFT LOWER CARGO BAY, STRINGER 26R CHAFED BETWEEN BS 1681-1701. REPAIRED IAW SRM 53-00-03 FIG 201, REPAIR 2, DETAIL I, REV 104. REPAIR CLASSIFIED MAJOR.

Part: STRINGER — CHAFED (BS 1681-1701) · airframe 61,638 hrs · 18,696 cycles

AFT LOWER CARGO BAY, CHAFE ON STRINGER 27R UPPER SURFACE , BETWEEN BS 1681-1701. REPAIRED IAW SRM 53-00-03, FIG 201, REPAIR 2, DETAIL I REV 104. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — DAMAGED (ZONE 200) · airframe 61,638 hrs · 18,696 cycles

BS 377.7, S9-10R FRAME HAS A CUT MARK. DAMAGED FRAME REPAIRED IAW EA F-5310-157103. REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (ZONE 200) · airframe 61,638 hrs · 18,696 cycles

CABIN, AFTER REMOVAL OF CREASE BEAM AT 1720 TO 1640R, FOUND CREASE BEAM CORRODED TO 1720 BULKHEAD. R & R IAW SRM 51-40-02. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (NR 1 NACELLE) · airframe 61,638 hrs · 18,696 cycles

WHILE PERFORMING EA F-5450-154642A ON NR 1 PYLON STRUT, AFTER REMOVING BATHTUB AND MIDCHORD FITTINGS, FOUND BLENDOUT ON LT INNER SKIN. SKIN R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — DENTED (BS 1820) · airframe 61,638 hrs · 18,696 cycles

FUSELAGE SKIN DENTED AT BS 1820, STR 3L. REPAIRED IAW SRM 53-00-01, REPAIR 16, FIG 201, REV 104. REPAIR CLASSIFIED AS CATEGORY B, MAJOR.

Part: STRAP — CORRODED (ZONE 300) · corrosion level 2 · airframe 61,638 hrs · 18,696 cycles

EMPENNAGE SKIN STRAP BS 1790 THE FORWARD EDGE OF THE APU INLET CUTOUT HAS CORROSION. R & R IAW SRM 51-40-02, REV 104. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — DENTED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

FWD LWR CARGO COMP. FRAME UPPER SURFACE HAS DENT AT STA 820, BETWEEN STRINGERS S23L AND S24L. REPAIRED IAW EA F-5310-153483, PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — SCRATCHED (ZONE 200) · airframe 61,638 hrs · 18,696 cycles

FUSELAGE SKIN BS 780 STRINGER 4-10R SCRATCHED, WITH DEPTHS UP TO 0.0034" WITH OTHER AREAS UP TO 0.0029". REPAIRED IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,638 hrs · 18,696 cycles

CABIN, CREASE BEAM ANGLE AT BS 739 TO 746 STR 17R CORRODED. REPAIRED IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (BS 690-720) · corrosion level 2 · airframe 61,638 hrs · 18,696 cycles

CABIN. DOOR 2R CREASEBEAM HAS CORROSION, STA 690 TO STA 720. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: FRAME — DENTED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO COMP FRAME STA 1500 UPPER SURFACE HAS DENT ABOVE STRINGER S25R. REPAIRED IAW EA F-5310-153465. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 780 S4-10L) · airframe 61,638 hrs · 18,696 cycles

FUSELAGE EXTERIOR SKIN BS 780 FROM S4-10L SCRATCHED WITH DEPTHS UP TO 0.0021" WITH OTHER AREAS UP TO 0.0019". R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: FRAME — DENTED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

AFL LWR CARGO COMP FRAME UPPER SURFACE HAS DENT AT STA 1520, BETWEEN S25L & S26L. REPAIRED IAW EA F-5310-153466. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,638 hrs · 18,696 cycles

CABIN, FLOORBEAM AT STA 333.5 LBL 50 HAS CORROSION ON UPPER CHORD. R & R IAW SRM 51-40-02, REV 104. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — CHAFED (ZONE 200) · airframe 61,638 hrs · 18,696 cycles

CABIN FRAME AT BS STA 1280 BETWEEN STR 13L TO STR 14L FORWARD SURFACE CHAFED. REPAIRED IAW SRM 53-00-07. REPAIR 3, FIG 201, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,638 hrs · 18,696 cycles

CABIN, DOOR 2L CREASE BEAM HAS CORROSION STA 690 TO 720. R & R IAW SRM 51-40-02, REV 104. REPAIR CLASSIFIED AS MAJOR.

Part: SILL — CORRODED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

AFT LWR CARGO COMP. LOWER SILL UPPER CHORD SURFACE HAS CORROSION FROM BS 1380-1440. R & R IAW SRM 51-40-02, REV 104 AND EA F-51-00-154466. REPAIR IS CLASSIFIED AS MAJOR.

Part: CREASE BEAM — DAMAGED (BS 365-377) · airframe 61,638 hrs · 18,696 cycles

CREASE BEAM BS 365 TO 377, HAS AN ELONGATED HOLE. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,638 hrs · 18,696 cycles

BS 377 LBL 24 HAS CORROSION ON THE SEAT TRACK SUPPORT. REMOVED & REPLACED IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,638 hrs · 18,696 cycles

RIGHT CREASEBEAM WEB AT WL 208.1, CORRODED BETWEEN BS 1320 - 1340. REPAIRED IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,638 hrs · 18,696 cycles

AFTER REMOVAL OF DECK PLATE FITTING, FOUND CORROSION ON CREASE BEAM WEB AT BS 1718 RBL 62. REPAIRED IAW SRM 51-40-02 REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,638 hrs · 18,696 cycles

RIGHT CREASEBEAM WEB CORRODED AT WL 208.1 BETWEEN BS 1340 AND 1360. REPAIRED IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,638 hrs · 18,696 cycles

BS 377 LBL 45 HAS CORROSION ON THE SEAT TRACK SUPPORT. REMOVED & REPLACED IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,638 hrs · 18,696 cycles

CREASEBEAM BETWEEN BS 1320 TO 1360 AT STR 17R CORRODED. REPAIRED IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,638 hrs · 18,696 cycles

AFTER REMOVAL OF SEAT TRACK FROM BS 377 TO 418, RBL 24, FOUND SEAT TRACK SUPPORT CORRODED. REMOVED & REPLACED IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,638 hrs · 18,696 cycles

CABIN STA 310 TO STA 324 RT CREASEBEAM HAS CORROSION. R & R IAW SRM 51-40-02 REV 104. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — DAMAGED (ZONE 100) · airframe 61,638 hrs · 18,696 cycles

FLOORBEAM BS 640 DAMAGED. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — CORRODED (ZONE 500) · airframe 61,638 hrs · 18,696 cycles

LT WING UPPER SKIN FOUND CORRODED AT OVERWING FILL PORT AREA. CORROSION REPAIR ACCOMPLISHED IAW EA F-5730-154472, PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — BULGED (LT WING) · airframe 61,638 hrs · 18,696 cycles

LT WING FIXED T/E UPPER SKIN PANEL BULGED ABOVE REAR SPAR AT WBL 97.5 TO WBL 107.5. REPAIR CARRIED OUT IAW EA F-5730-153464. REPAIR CLASSIFIED AS MINOR.

Part: FLOOR SUPPORT — DAMAGED (ZONE 200) · airframe 61,638 hrs · 18,696 cycles

AFTER DECK PLATE REMOVAL FOUND FLOOR SUPPORT FITTING AT STA 1718, RBL 55 HAS EXISTING ELONGATED HOLE. DAMAGED FLOOR SUPPORT R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: FLOORBEAM — BENT (ZONE 200) · airframe 61,638 hrs · 18,696 cycles

BS 580 FLOORBEAM, FOUND BENT. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — GOUGED (ZONE 800) · airframe 61,638 hrs · 18,696 cycles

R1 DOOR FOUND GOUGED FROM EXTERNAL HANDLE ON DOOR EXTERIOR SURFACE. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: SUPPORT — DAMAGED (ZONE 200) · airframe 61,638 hrs · 18,696 cycles

CABIN, AFTER DECK PLATE REMOVAL, FOUND STA STA 1720 WL 208, AFT BULKHEAD SUPPORT HAS 14 EXISTING ELONGATED HOLES. R & R IAW SRM 51-40-02 REV 104. REPAIR CLASSIFIED AS MAJOR.

Part: FLOOR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,638 hrs · 18,696 cycles

CABIN, DECK PLATE CORRODED AT STA 1681 RBL 60, BS 1718 LBL 60 TO RBL 60, BS 1681 RBL 45-50, LBL 45-50. REMOVED AND REPLACED IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: FLOORBEAM — BENT (ZONE 200) · airframe 61,638 hrs · 18,696 cycles

FLOORBEAM AT BS 620 BENT. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: FLOORBEAM — BENT (ZONE 200) · airframe 61,638 hrs · 18,696 cycles

CABIN FLOORBEAM AT BS 600 BENT. R & R IAW SRM 51-40-02 REV 104. REPAIR IS CLASSIFIED AS MAJOR.