N933FD

Part: ACTUATOR — WORN (LE SLATS) · airframe 63,188 hrs · 37,181 cycles

AT FLAPS 1 SELECTION FLAPS MOVED TO 1 POSITION & GOT EICAS MESSAGE LE SLAT DISAGREE. RAN QRH PROCEDURES, AFTER MOVED THE ALTERNATE FLAP SELECTOR THE EICAS MESSAGE WENT AWAY. REF TSI 27-80 1381 WRI 27-80 1391, 27-80 1389, 27-80 1390 FOR TROUBLESHOOTING AND PARTS INFO. BASED ON TROUBLESHOOTING THREE LEADING EDGE SLAT ROTARY ACTUATORS WERE FOUND TO BE TRIPPED. THREE ACTUATORS IN POSITIONS #9 #12 AND#15 WERE REPLACED IAW AMM 27-81-18-4. OPS CHECK SATIS AND NO MESSAGES PRESENT DURING OPERATION OF LEADING EDGE SLATS. AIRCRAFT OK FOR SERVICE.

Part: SLAT SYSTEM — LACK OF LUBE · airframe 63,180 hrs · 37,174 cycles

LE SLAT DISAGREE BETWEEN UP AND 1 AT 225 KTS/3000 FEET. RAN QRH AND LANDED FLAPS 20 PER QRH. EMERGENCY DECLARED. LUBED LEFT AND RIGHT WING LEADING EDGE SLATS REF. B757 AMM 12-21-08-3. CHECKED BITE ON FSEU'S WITH NO FAULTS NOTED. RAN SLATS NUMEROUS TIMES WITH NO FAULTS.

Part: ATTACH ANGLE — CRACKED (RT WING TE FLAP) · airframe 62,643 hrs · 36,857 cycles

R/H WING I/B FLAP UPPER T/E PANEL ATTACK ANGLE IS CRACKED JUST ABOVE O/B END OF AFT FLAP. REMOVED AND REPLACED R/H WING I/B FLAP UPPER T/E PANEL ATTACH ANGLE IAW B 757 SRM 51-40-02-OG P/N - 113N2605-4 PO # FS2100720.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,643 hrs · 36,857 cycles

FWD WET AREA STA 333.45 BETWEEN RBL 2.5-RBL 4.5 FLOOR SUPPORT CORRODED. EVALUATED FLOOR SUPPORT AT FWD WET STA 333.45 BETWEEN RBL 2.5-4.5, FOUND TO BE WITH OUT LIMITS, IAW B 757 SRM 53-00-51-1A FIG 4 DETAIL III. REMOVED AND REPLACED FLOOR SUPPORT P/N 141N5161U40 PO FS2100324, IAW B 757 SRM 51-40-02-OG.

Part: FLOOR SUPPORT — PUNCTURED (MAIN DECK) · airframe 62,643 hrs · 36,857 cycles

MAIN DECK STA 1055 LBL 43 FLOOR SUPPORT HAS A PUNCTURE HOLES. EVALUATED FLOOR SUPPORT AT MAIN DECK STA 1055 LBL 43,FOUND DAMAGE ONLY ON CO COVER COVER PLATE IAW B 757 SRM 51-10-02-OG,FABRICATED AND INSTALLED NEW COVER PLATE IAW B 757 SRM 51-40-02-OG AND BOEING DWG # 144N5070 REV: B AND W.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,643 hrs · 36,857 cycles

FUSELAGE PLATE & SKIN STA 740 TO STA 760 STRINGER 26L REQUIRE REPLACE REPAIR DOUBLER. COMPLIED WITH EA # F-5330-131077 D P2 TITLE: FUSELAGE - PLATES AND SKIN - SKIN LAP, STA 740 TO STA 760,STRINGER S-26L - CORROSION REPAIR.

Part: SKIN — DAMAGED (ZONE 100) · airframe 62,643 hrs · 36,857 cycles

FUSELAGE & SKIN STA 660 - 700,STRINGER 26R LOWER SKIN LAP JOINT - DOUBLER REPAIR - REQUIRE REPLACE. COMPLIED WITH EA # F-5330-131060 B P2 TITLE: FUSELAGE - PLATES & SKIN - STA 660 - 700, S - 26R LOWER SKIN LAP JOINT - DOUBLER REPAIR

Part: LAMP — INOPERATIVE (MLG INDICATOR) · airframe 62,551 hrs · 36,802 cycles

LEFT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE WHEN EXTENDED PRIOR TO LANDING. FOUND BOTH LAMPS BURNED OUT IN LT GEAR POSITION LIGHT ASSEMBLY. RELAMPED WITH 2 EA GE 387 LAMPS, OPERATIONS CHECKS GOOD. A/C OK FOR SERVICE.

Part: COVER — DAMAGED (L1 DOOR SLIDE) · airframe 62,125 hrs · 36,551 cycles

THE L1 DOOR SLIDE COVER HAS ALL 4 FASTNERS PULLED THROUGH THE COMPOSITE THE FWD LATCH WILL NOT CONNECT TO THE DOOR. WILL NEED COMPOSITE SHOP. REMOVED AND PLACED IN CARGO NET IN THE MAIN CARGO. REPAIRED POTTED INSERT REF B757 AMM 25-00-00-8 REPAIR POTTED INSERTS K. SUBTASK 25-00-00-348-031 COMPLIED WITH E.A F-2560-T0354957 REINSTALLED L1 DOOR COVER IAW AMM 52-10-00. AC OK FOR SERVICE

Part: WARNING LIGHT — FALSE ACTIVATION (ACCESS DOOR) · airframe 61,349 hrs · 36,070 cycles

FWD ACCESS DOOR EICAS LIGHT ILLUMINATED WHEN AIRCRAFT ROTATED FOR TAKEOFF. OPS OK IAW FIM 52-71, FT 802 & AMM 52-70-00-5-0, GVI AND CHECKED FWD ACCESS DOOR TARGET, SENSOR AND DOOR STRIKER, ALL OK. PSEU BITE 1 HIT FOR SENSOR 085 SUBSEQUENT BITE OK, OPERATED DOOR MULTIPLE TIMES AND COULD NOT DUPLICATE. NO HISTORY, OK FOR SERVICE.

Part: GIRT BAR — FAILED (R1 DOOR SLIDE) · airframe 60,972 hrs · 35,800 cycles

R1 ENTRY DOOR GIRT BAR STAYED ENGAGED. R1 DOOR ASSIST BOTTLE BLEW. SLIDE PARTIALLY DEPLOYED. REMOVED AND REPLACED GIRT BAR IAW AMM 25-66-01-4. REPLACED SLIDE IAW AMM 25-66-01-4

Part: SKIN — GOUGED (CARGO DOOR) · airframe 60,912 hrs · 35,759 cycles

MAIN CARGO DOOR, UPPER SECTION SKIN, AT APPROXIMATE STATION 495, STRINGER S-6 LEFT, HAS GOUGE DAMAGE. REPAIRED PER SRM 52-30-01 FIG 201, REPAIR 4.

Part: PROXIMITY SWITCH — OUT OF ADJUST (LANDING GEAR) · airframe 60,861 hrs · 35,727 cycles

ON GEAR RETRACT RECEIVED EICAS "GEAR DISAGREE" MSG. AFTER 20 SEC MSG WENT AWAY. NOTE- GEAR SHOWED UP AMBER GEAR LIGHT WAS ILLUMINATED AND WENT AWAY AFTER 20 SEC. T/S REF. FIM 32-30 FT 815, CLEARANCE OUT OF LIMITS ON S10073 AND S10240, S10242, ADJUSTED ALL REF. AMM 32-61-02-2, REQUIRES GEAR SWING. REF FIM 32-30 FT 815, PERFORMED 5 SUCCESSFUL RETRACTS/EXTENSIONS OF GEAR WITH NO FAULTS USING EXTERNAL HYDRAULIC POWER REF AMM 29-11-00-2, OPS CHECK GOOD, NO FAULTS NOTED, A/C OK FOR SERVICE.

Part: FRAME — GOUGED (FUSELAGE) · airframe 60,850 hrs · 35,721 cycles

FWD ACCESS. COMPT. FRAME AT STA. 231.25 BL.0 HAS GOUGE ON EXISTING REPAIR ANGLE ON INSIDE OF FRAME REMOVED DAMAGED EXISTING REPAIR ANGLE, CUT OUT AREA OF FRAME, FABRICATED NEW REPAIR ANGLE, FILLER & LATCH SHEILD AND INSTALLED NEW REPAIR PARTS & LATCH SHEILD TO FRAME AT STA. 231.25 BL.0 INSUIDE FWD ACCESS. COMPT. IAW SRM 53-00-07-2R REPAIR 7.

Part: SLIDE — FAILED (L1 DOOR) · airframe 60,601 hrs · 35,550 cycles

ON ARRIVAL RAMP OPENED L1 DOOR AND SLIDE/RAFT MALFUNCTIONED AND DID NOT DISCONNECT FROM GIRT BAR ATTACHMENT POINTS. INSTALLED NEW L1 DOOR SLIDE IAW MM 25-66-01-4.

Part: GIRT BAR — OBSTRUCTED (L1 DOOR) · airframe 60,395 hrs · 35,437 cycles

L1 DOOR ARMING LEVER EXTREMELY DIFFICULT TO MOVE INTO THE ARMED POSITION. REQUIRED MULTIPLE L1 DOOR OPENING/CLOSING TO GET ARM LEVER TO ENGAGE. FOUND THE D-RING STRAP WRAPPED AROUND THE GIRT BAR. CLEARED THE STRAP FROM GIRT BAR, DOOR ARMS NORMALLY ON GROUND IAW AMM 52-11-25-5.

Part: GIRT BAR — MALFUNCTIONED (L1 DOOR SLIDE) · airframe 60,076 hrs · 35,229 cycles

L1 DOOR GIRT BAR FAILED TO DISCONNECT WHEN DOOR WAS MOVED TO DISARM. REMOVED AND REPLACE L1 DOOR EMERGENCY POWER RESERVOIR CYLINDER IAW MM 52-11-30-4.

Part: YOKE — DAMAGED (AILERONS) · airframe 59,396 hrs · 34,784 cycles

LATERAL PLAY IN YOKE FOR AILERON INPUT.

Part: ROLLER — DAMAGED (L1 DOOR) · airframe 59,083 hrs · 34,556 cycles

PRIOR TO PUSH BACK, AN EICAS LT FWD ENTRY DOOR EICAS ALERT. F/O OPENED AND SHUT DOOR AND EICAS WENT AWAY. SAME EICAS RETURNED AFTER ENGINE START. SAME PROCEDURE CLEARED EICAS MESSAGE. REMOVED AND REPLACED L1 UPPER AFT LATCH ROLLER AND DOOR LATCH FITTING IAW 52-11-00-5, AND 52-11-37-4. OPS CHECKED NORMAL.

Part: DEPRESSOR — DENTED (CARGO DOOR) · airframe 59,054 hrs · 34,537 cycles

CARGO DOOR LOWER AFT CORNER SEAL DEPRESSOR DENTED. REMOVED AND REPLACED IAW DWG 146N6603 REV. A. PERFORMED SATISFACTORY PRESSURIZATION LEAK CHECK, NO LEAKS NOTED IAW AMM 05-51-24-2. MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (BS 820) · corrosion level 2 · airframe 59,054 hrs · 34,537 cycles

FWD CARGO BAY BS 820 BL 0 HAS A SHEAR TIE CORRODED. REMOVED CORROSION IAW SRM 51-10-02 AND FOUND OUT OF LIMITS IAW SRM 53-00-53-1A DET. V. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-30-01, 51-04-05, DWG 141N1020 REV. F, AND SRM 51-40-02.

Part: SKIN — CORRODED (BS 720-740) · corrosion level 2 · airframe 59,054 hrs · 34,537 cycles

FWD CARGO BAY FUSELAGE SKIN AND VHF ANTENNA DOUBLER ARE CORRODED BETWEEN BS 720 - 740, BL 0 BETWEEN STRINGERS 28L AND 28R. REMOVED CORROSION, CUTOUT DAMAGED SECTION OF SKIN. FABRICATED & INSTALLED A REPAIR DOUBLER IAW EA TF-5330-T0330439 P1, COMPLIED WITH EA TF-5330-T03307439 P1.

Part: SKIN — DEBONDED (RT WING TE FLAP) · airframe 59,054 hrs · 34,537 cycles

DISBOND FOUND ON RIGHT INBOARD MAIN FLAP ON THE CORNER. ACCOMPLISHED PERMENENT REPAIR ON RIGHT INBD MAIN FLAP IAW 57-53-01-2R FIG. 201 AND SRM 51-70-10-2R REPAIR 2, TAP TESTED IAW SRM 51-70-10-2R PARAG 21.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 59,054 hrs · 34,537 cycles

LEFT HORIZONTAL STAB UPPER SKIN HAS A DENT AT HSS 107.604. REPAIRED IAW SRM 55-10-01-1A FIG 101 NOTE 1, AND SRM 51-70-10-2R REPAIR NR 4 TAP TESTED IAW SRM 51-70-10,2R PARAG 21.

Part: WARNING LIGHT — FALSE ACTIVATION (HYD PUMP) · airframe 58,757 hrs · 34,344 cycles

REJECTED T/O AT 60 KTS FOR AN EICAS R HYD ENG PUMP AND PRESSURE LIGHT ILLUMINATED FOR RT ENG HYD PUMP AND ON THE OVERHEAD PANEL. QRH RTO AND HYDRAULIC ENGINE PUMP PROCEDURES ACCOMPLISHED. RAN RT ENGINE, EDP WAS READING 3020 PSI WITH RT ACMP SELECTED OFF AND CHECK PRESSURE, CASE FILTERS CHECKED GOOD IAW MM 29-11-05-6-0 AND JRH CHECKLIST.

Part: BATTERY PACK — UNSECURE (CABIN) · airframe 58,699 hrs · 34,299 cycles

L1 DOOR OVERHEAD EMERGENCY EXIT LT AND EXT SLIDE LIGHT INOPERATIVE. FOUND BATTERY PACK AT M731 UNSECURED, NOT SURE HOW LONG IT HAS BEEN IN THIS CONDITION. R & R M731 EMERGENCY LIGHTS BATTERY PACK IAW MM 33-51-07-2, OPS CHECKS GOOD. RADIANT ILLUMINATION, BATTERY ASSY MPN 2013-1A, MSN 46241. ACFT OK FOR SERVICE.

Part: UNKNOWN — ODOR · airframe 58,661 hrs · 34,279 cycles

DURING DESCENT THRU 11,000' AND LEVELING OFF AT 10,000' AND POWERING UP, AIR CONDITIONING PACKS CYCLED AND A FUME EVENT OCCURRED. DIRTY SOCK ODOR UNTIL ENGINE SHUTDOWN. T/S BOTH PACKS IAW MM 21-00-00-2 & 21-00-01. NO FAULTS NOTED, COULD NOT DUPLICATE DISCREPANCIES. OK FOR SERVICE.

Part: SLIDE — UNWANTED DEPLOY (DOOR) · airframe 58,299 hrs · 33,994 cycles

SLIDE WAS UNARMED & WAS CRACKED OPEN WHEN RAMP FINISHED OPENING. DOOR SLIDE BAR WAS STILL ATTACHED & DOOR BLEW OPEN. SLIDE FELL ONTO AIRSTAIRS BEFORE LANYARD WAS PULLED PREVENTING FIRING PIN FROM BEING TRIGGERED. INSPECTED SLIDE & FOUND TO STILL BE IN SERVICEABLE CONDITION.

Part: LINE — OUT OF POSITION (ENTRY DOOR) · airframe 58,203 hrs · 33,941 cycles

RIGHT CREW ENTRY DOOR, SLIDE LIGHT DOES NOT ILLUMINATE WITH DOOR. FOUND GIRT BAR STATIC LINE OUT OF PLACE & NOT LETTING GIRT BAR LOCK GO FULL TRAVEL. REPOSITIONED STATIC LINE IAW MM 25-66-01-4. PERFORMED OPERATIONS CHECK IAW MM 25-66-00-5. OPERATIONS CHECK OK. ACFT OK FOR SERVICE.

Part: STOWAGE BOX — INOPERATIVE (COCKPIT) · airframe 577 hrs · 33,624 cycles

FOUND COURIER O2 MASK BOX PRESS TO TEST BUTTON BROKEN. R & R O2 MASK STOWAGE BOX IAW AMM 35-11-51-4-99. OK FOR SERVICE.

Part: FRAME — DENTED (BS 1420) · airframe 57,329 hrs · 33,361 cycles

AFT CARGO BAY LT SIDE FRAME DENTED AT BS 1420 BETWEEN STRINGERS 25 & 26L. REMOVED AND REPLACED THE FRAME SECTION IAW SRM 51-40-02 AND DRAWING 146N1012 REV C.

Part: FRAME — GOUGED (BS 231) · airframe 57,329 hrs · 33,361 cycles

FORWARD NOSE COMPARTMENT BILGE AREA BS 231 FRAME IS GOUGED AT BL 0. REPAIRED IAW EA F-5310-T0314177 P1.

Part: SKIN — DENTED (BS 523) · airframe 57,329 hrs · 33,361 cycles

SKIN DENTED AT BS 523 JUST BELOW STRINGER 26L. REPAIRED IAW EA F-5330-T0314272.

Part: SHEAR TIE — CRACKED (BS 350) · airframe 57,329 hrs · 33,361 cycles

SHEAR TIE HAS A CRACK AT BS 350 UPPER SIDE OF L1 DOOR FRAME. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, 51-40-05, 51-40-08 AND DRAWING 141N1318.

Part: SKIN — DENTED (BS 609) · airframe 57,329 hrs · 33,361 cycles

FUSELAGE HAS A DENT AT BS 609 BETWEEN STRINGERS 27 - 28L. REMOVED DAMAGE IAW SRM 53-00-01 FIG 201 REP 7. FABRICATED DOUBLER AND FILLER IAW SRM 53-00-01 FIG 201 REP 7. INSTALLED FILLER AND DOUBLER IAW SRM 53-00-01 FIG 201 REP 7.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,126 hrs · 33,197 cycles

L1 DOOR EXTERNAL EMER LIGHT INOPERATIVE. L1 DOOR EXTERNAL LIGHT FILAMENT REPLACED.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,613 hrs · 32,809 cycles

RIGHT SIDE OF FUSELAGE, STRINGER 26R LAP SEAM HAS FASTENERS PULLING THRU SKIN LAP SEAM AT BS 1670. EVIDENCE OF CORROSION. CUT OUT DAMAGE AT RT SIDE AT FUSELAGE, STRINGER 26R LAP SEAM BS 1670. FABRICATED DOUBLER & FILLER & INSTALLED IAW EA F-5330-T0 305495 REV NR PS P1.

Part: UNKNOWN — MALFUNCTIONED (LT ENGINE) · airframe 56,495 hrs · 32,732 cycles

PDIS 933 73-10 0004481 28NOV13 RSW CLOSE LOG PAGES 02099057. NORMAL START LT ENG. DURING RT ENG START, THE LT ENG FAILED. FUEL FLOW WAS ZERO, EICAS MESSAGE LT ENG FUEL VLV. FACT 28NOV13 04:00 RSW R PERFORMED TEST ON NR 1 ENG FUEL VLV SYS IAW MM 28-22-11-5. PULLED & RESET NR 1 ENG FIRE HANDLE. RAN NR 1 ENG IAW B757 JRH FOR 8 MINUTES, ALL ENG PARAMETERS INDICATED NORMAL, OK FOR SERVICE.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 56,424 hrs · 32,689 cycles

RIGHT ENTRY DOOR SLIDE FELL OUT WHEN OPENING DOOR. PILOT THOUGHT DOOR WAS DISARMED. FOUND DOOR OPEN AND SLIDE ON CREW STAIRS. R1 DOOR WAS IN ARMED POSITION. SLIDE HAD PINS PULLED ON YELLOW COVER BUT DID NOT INFLATE. DOOR ASSIST CYLINDER DEFLATED. INSTALLED R1 DOOR ESCAPE SLIDE IAW MM 25-66-01-4.

Part: SKIN — CHAFED (E/E BAY DOOR) · corrosion level 2 · airframe 55,725 hrs · 32,266 cycles

MAIN EQUIPMENT CENTER ACCESS DOOR EXTERIOR HANDLE CUTOUT IS DAMAGED REMOVED DOOR IAW MM 52-48-02-4. COMPLIED WITH EA F-5230-152474 "DOORS-E & E SERVICE DOOR GOUGE/NICK REWORK". REINSTALLED DOOR AND NEW HANDLE IAW SRM 51-40-02 AND MM 52-48-02-4.

Part: FRAME — CORRODED (BS 1600) · corrosion level 2 · airframe 55,725 hrs · 32,266 cycles

AFT PIT-CORROSION ON LOWER FLANGE OF FRAME AT BS 1600 (AFT SIDE) RBL 5 TO LBL 5. CUT OUT DAMAGED SECTION OF STA 1600 BOTTOM CHORD, FABRICATED AND INSTALLED. REPAIR PARTS IAW SRM 53-60-07, FIG 1 AND SRM 51-70-11, FIG 1.

Part: STRINGER SPLICE — CORRODED (BS 1180 S28R) · corrosion level 2 · airframe 55,725 hrs · 32,266 cycles

CORROSION ON STRINGER SPLICE, BS 1180, STRINGER 28R. REMOVED DAMAGED STRINGER SPLICE IAW SRM 51-40-02. FABRICATED NEW SPLICE IAW DWG 140N0103, REV P AND INSTALLED IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1200 S28-29L) · corrosion level 2 · airframe 55,725 hrs · 32,266 cycles

CORROSION ON SHEAR TIE, BS 1200 BETWEEN STR 28 AND 29L. REMOVED DAMAGED SHEAR TIE IAW SRM 51-40-02. FABRICATED NEW SHEAR TIE IAW DWG 140N2006, REV B AND SRM 51-40-05, INSTALLED NEW SHEAR TIE IAW SRM 51-40-02.

Part: STRINGER — CORRODED (BS 1180 S28R) · corrosion level 2 · airframe 55,725 hrs · 32,266 cycles

CORROSION ON STRINGER 28R AT BS 1180. CUT OUT DAMAGED SECT OF STRINGER BS 1180-1194, FABIRCATED, AND INSTALLED REPAIR PARTS IAW SRM 53-00-03 R2.

Part: GOVERNOR — MALFUNCTIONED (RT ENGINE) · airframe 55,691 hrs · 32,253 cycles

ON TAKEOFF ROLL, RT ENGINE WASN'T PROPER POWER, WOULD NOT MAINTAIN 1.59 EPR. ROLLED BACK TWICE. ABORTED T/O AT APROX 60 KTS, KNOB SPLIT BETWEEN LT AND RT THROTTLES WERE 2 KNOB WIDTHS. REMOVED AND REPLACED RIGHT HAND ENGINE FUEL FLOW GOVERNER IAW AMM 73-21-01-4-4 THRU STEP 3 H.

Part: ENGINE — ODOR (LEFT) · airframe 55,639 hrs · 32,219 cycles

AFTER TAKEOFF HAD A STRONG PACK ODOR. WENT AWAY AFTER A COUPLE MINUTES. R & R LT ENGINE.

Part: GIRT BAR — LACK OF LUBE (ESCAPE SLIDE) · airframe 55,607 hrs · 32,196 cycles

RT CREW ENTRY DOOR SLIDE LIGHT INOPERATIVE. FOUND RT DOOR GIRT BAR SLIDERS WITH ALMOST NO GREASE ON SLIDERS CAUSING TO DRAG. LUBERCATED BOTH RT DOOR GIRT BAR SLIDERS IAW 12-21-18-3. ARMED RT ENTRY DOOR SLIDE MULTIPLE TIMES, SLIDE LIGHT NOW OPS CHECKS SERVICEABLE. OK FOR SERVICE.

Part: OXYGEN MASK — FAILED (COCKPIT) · airframe 55,490 hrs · 32,129 cycles

CAPTAIN'S PRESS TO TEST AND RESET LEVER ON O2 BOX FAILS TO GIVE PROPER TEST NR O2 FLOW OR INTERMITTENT FLOW TO IRIS. SWAPPED CAPTAIN'S AND NR 2 COURIER O2 MASK BOX ASSY'S IAW MM 35-11-51-4-99. CAPTAINS O2 MASK TESTED GOOD. REMOVED AND REPLACED MASK AND BOX PER MM 35-11-51. SYSTEM OPS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,170 hrs · 31,906 cycles

L1 SLIDE ILLUMINATION LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.

Part: SLIDE — INOPERATIVE (PAX DOOR) · airframe 54,871 hrs · 31,694 cycles

PORT SIDE ENTRY DOOR SLIDE LT NOT ILLUMINATED UPON PARKING, MULTIPLE ATTEMPTS TO RE-ENGAGE FAILED. FOUND LT DOOR SLIDE ASSY PARTIALLY HANGING OUT. REINSTALLING. FOUND SPRING ON AFT OF GIRT BAR DAMAGED. NOT ALLOWING SLIDE LIGHT ARMING BLOCK TO BE IN PLACE. R & R L1 IAW AMM 25-66-01-4. OPS CHECK GOOD. SLIDE LIGHT NOW FUNCTIONS NORMAL. ACFT OK FOR SERVICE. PREMATURE REMOVAL/INSTALLATION OFF MFG D30654-122. FOUND SPRING ON AFT OF GIRT BAR DAMAGED. NOT ALLOWING SLIDE LIGHT ARMING BLOCK TO BE IN PLACE. R & R L1 IAW AMM 25-66-01-4. OPS CHECK GOOD. SLIDE LIGHT NOW FUNCTIONS NORMAL. ACFT OK FOR SERVICE.

Part: GIRT BAR — OUT OF POSITION (PAX DOOR SLIDE) · airframe 54,749 hrs · 31,623 cycles

LT DOOR SLIDE LIGHT NOT ILLUMINATED WITH DOOR CLOSED LOCKED AND ARMED. REPOSITIONED AND ATTACHED SLIDE GIRT BAR. OPS CHECKED NORMAL. OK FOR SERVICE.

Part: SKIN — CRACKED (LT WING) · airframe 54,543 hrs · 31,458 cycles

LT WING UPPER L/E HAS 5" CRACK IN COMPOSITE STRUCTURE WHERE OTBD SLAT 4 MEETS IN INBD SLAT 3. REPAIRED IAW SRM 57-41-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,501 hrs · 31,432 cycles

R1 EMERGENCY EXIT LIGHTS WILL NOT TEST. R & R R1 EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-51-07-2. OPS CHECK NORMAL.

Part: SKIN — GOUGED (BS 1445 S25R) · airframe 54,007 hrs · 31,144 cycles

SKIN GOUGED STA 1445, STRINGER 25R. REPAIRED AREA BY INSTALLING A DOUBLER IAW EA F-5330-123579.

Part: GIRT BAR — BINDING (L1 DOOR) · airframe 53,934 hrs · 31,103 cycles

LEFT FWD ENTRANCE DOOR (L1) SLIDE LIGHT - INOP. RELEASED FOR SERVICE IAW MEL: 52-11-01-A CATEGORY: B EXPIRATION: 27DEC10 "MEL 52-11-01-A: L1 DOOR SLIDE - INOP (INOP OR MISSING)." THE GIRT BAR IS NOT FULLY ENGAGING THE DOOR THRESHOLD BRACKET. IT APPEARS THAT THE DOOR IS RIGGED A LITTLE BIT HIGH, EVEN THOUGH IT IS CLOSING PROPERLY. DOOR OPERATES CORRECTLY IAW THE AMM 52-11-00-5. WHEN DOOR IS ARMED IT IS BINDING AT THE GIRT FLOOR FITTINGS. SLIDE COVER REMOVED FOR ACCESS. ADJUSTED THE GIRT BAR FLOOR FITTING IAW MM 52-11-25-5. TESTED DOOR WHEN CLOSED AND WITH DOOR SLIDE ARMED, THE SLIDE LIGHT OPERATES NORMALLY IAW MM 25-66-11-2-0. FINISHED REACTIVATING THE SLIDE ARMING SYS AND INSTALLED THE SLIDE COVER. LIGHT TEST GOOD.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 53,782 hrs · 31,032 cycles

L1 DOOR ESCAPE HAS DROPPED DOWN AND APPEARS TO BE UNATTACHED. RELEASED FOR SERVICE IAW MEL: 52-11-01-A. "MEL 52-11-01-A: L1 DOOR SLIDE- INOP (IDENTIFY INOP OR MISSING)." SAFELY PLACED SLIDE IN THE HSG. FOUND THAT BOTH UPPER STRAP CLASPS WOULD NOT TIGHTLY SECURE THE SLIDE AND IT WOULD SLIDE DOWN AGAIN. L1 DOOR UNUSEABLE. ORDERED STRAP ASSY AS REQUIRED. R & R L1 DOOR SLIDE HARNESS REF MM 25-66-00-2-0.

Part: FLOOR PANEL — DENTED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

AFT CARGO COMPARTMENT FLOOR PLATE AT BS 1330 TO BS 1470 FOUND CORRODED AND WITH NUMEROUS DENTS. EVALUATE AND RECTIFY. AT BS 1330 TO BS 1470 REMOVED IAW AMM 25-50-04 REV 4. FLOOR PLATE EVALUATED AND FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53 REV 97. FLOOR PLATE FABRICATED IAW DWG NR 453N1270 SHT 42 REV - AND PART MARKED AS FX 453N1805-168 IAW GMM 7-0-1001. REFER TO SNRM NR N0002 FOR INSTALLATION OF FLOOR PLATE. REPAIR IS CLASSIFIED AS MINOR REPAIR IAW GMM 6-2-100 CRITERIA.

Part: FLOOR PANEL — DENTED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

AFT CARGO COMPARTMENT FLOOR PLATE AT BS 1510 TO BS 1640 FOUND CORRODED AND WITH NUMEROUS DENTS. REMOVED IAW AMM 25-50-04 REV 4. FOUND OUT OF LIMIT IAW SRM 53- 00-53 REV 97. FLOOR PLATE FABRICATED IAW DWG NR 453N1270 SHT 42 REV -AND PART MARK IAW GMM 7-0-1001. REPAIR IS CLASSIFIED AS MINOR REPAIR IAW GMM 6-2-100 CRITERIA.

Part: PANEL — CORRODED (RT WING) · airframe 52,447 hrs · 30,243 cycles

RT WING UPPER SURFACE REAR SPAR FOUND WITH CORROSION AT AROUND WS 177.5. REPAIRED IAW EA F 5720-129619. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: PANEL — CORRODED (RT WING) · airframe 52,447 hrs · 30,243 cycles

RT WING UPPER SURFACE REAR SPAR FOUND WITH CORROSION AT AROUND WS 204.5. REPAIRED IAW EA F 5720-129619. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FWD CARGO COMPARTMENT FLOOR PLATE SPLICE AT BS 750 FOUND CORRODED. EVALUATE AND RECTIFY. BS 750 CORRODED FLOOR PLATE SPLICE STRAP REMOVED AND REPLACED IAW AMM 25-50-04 REV 4. SPLICE PLATE STRAP FABRICATED IAW DWG NR 453N1611 SHT 3 REV. B AND PART MARKED AS FX 453N1611-25 IAW, GMM 7-0-1001. REPAIR IS CLASSIFIED AS MINOR REPAIR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 840, RBL 26 TO LBL 26 UPPER BULKHEAD SUPPORT ANGLE CORRODED. EVALUATE AND REPAIR. BS 840, RBL 26 TO LBL 26 BULKHEAD SUPPORT ANGLE REPAIR CARRIED OUT IAW SRM 51-70-11 FIG. 1 REV. 97. REPAIR IS CLASSIFIED AS MINOR REPAIR IAW GMM 6-2-100 CRITERIA.

Part: SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FWD CARGO COMPARTMENT FLOOR PLATE SPLICE AT BS 654 FOUND CORRODED. EVALUATE AND RECTIFY. BS 654 CORRODED FLOOR PLATE SPLICE STRAP REMOVED AND REPLACED IAW AMM 25-50-04 REV. 4. SPLICE PLATE STRAP FABRICATED IAW DWG NR 453N1611 SHT 3 REV. B AND PART MARKED AS FX 453N1611-19 IAW GMM 7-0-1001 REV 107. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FLOOR PANEL — CORRODED (BS 1200-1330) · airframe 52,447 hrs · 30,243 cycles

AFT CARGO COMPARTMENT FLOOR PLATE AT BS 1200 TO BS 1330 FOUND CORRODED AND WITH NUMEROUS DENTS. REMOVED AND INSTALLED FABRICATED PLATE IAW EO E F-2550-7-5000 A1 PT3 : DEACTIVATION OFFWD AND AFT CARGO LOADING SYS. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: PANEL — CORRODED (RT WING) · airframe 52,447 hrs · 30,243 cycles

AFTER REMOVAL OF FASTENERS ON RT REAR SPAR UPPER INBD T/E PANEL, SUSPECT CORROSION SPREAD BEYOND WBL 130.50 TO UNDER ADJACENT PANEL 113N1612 UPPER CHORD. REPAIRED IAW EA F-5720-129619. REPAIR IS CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100.

Part: FLOOR PANEL — DENTED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

AFT CARGO COMPARTMENT FLOOR PLATE AT BS 1470 TO BS 1510 FOUND CORRODED AND WITH NUMEROUS DENTS. AT BS 1470 TO BS 1510 FLOOR PLATE REMOVED IAW AMM 25-50-04, REV 4. FLOOR PLATE EVALUATED AND FOUND OUT OF LIMIT IAW SRM 53-00-53 REV 97. FLOOR PLATE FABRICATED IAW DWG NR 453N1270 SHT 42 REV-AND PART MARK AS FX 453N1805-139 IAW GMM 7-0-1001. REFER TO SNRM NR N00002 FOR INSTALLATION OF FLOOR PLATE. REPAIR IS CLASSIFIED AS MINOR REPAIR IAW GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 750 TO BS 785, S-17L TO S-17R SKIN AROUND NUT PLATES CORRODED. BS 750 TO BS 785, S-17L TO S-17R SKIN AT NUTPLATES CORROSION REMOVED AND TREATED IAW SRM 51-10-02 AND 51-20-01, REV 97 AND FOUND EXCEEDED LIMIT AT BS 780, S-28L TO S-28R IAW SRM 53-00-01 FIG 101 REV 97 REPAIRED DOUBLER FABRICATED AND INSTALLED IAW SRM 53-00-01 REPAIR 3, FIG 201 REV 97. THIS REPAIR IS CLASSIFIED AS MAJOR IAW-GMM 6-2-100 CRITERIA. NOTE: REPETITIVE INSP REQUIRED IAW SRM 53-00-01 REPAIR 3 FIG 201, TABLE V REV 97 NEXT INSP IS 33,243 FC.

Part: FLOOR PANEL — CORRODED (BS 1470) · airframe 52,447 hrs · 30,243 cycles

AFT CARGO COMPARTMENT FLOOR PLATE SPLICE STRAP AT BS 1470 FOUND CORRODED. REMOVED AND REPLACED IAW AMM 25-50-04 REV. 4. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT ANGLE — MISSING (NR 1 PYLON) · airframe 52,447 hrs · 30,243 cycles

PYLON ANGLE NR 1 SUPPORT FOUND MISSING DURING REMOVAL. REPLACED. INSTALLED FABRICATED SUPPORT ANGLE ON PYLON NR 1 IAW EO F-2910-7-5002 A PT1 STEP 10. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SPLICE — CORRODED (FLOOR BOARD) · airframe 52,447 hrs · 30,243 cycles

AFT CARGO COMPARTMENT FLOOR PLATE SPLICE STRAP AT BS 1330 FOUND CORRODED. REMOVED AND REPLACED IAW AMM 25-50-04 REV 4. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: STRAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FWD CARGO COMPARTMENT FLOOR PLATE SPLICE AT BS 550 FOUND CORRODED. REMOVED AND REPLACED IAW SRM 25-50-04 REV 4. SPLICE STRAP FABRICATED IAW DWG NR 453N1611 SHT 3 REV B AND PART MARKED IAW GMM 7-0-1001 REV 107. REPAIR IS CLASSIFIED AS MINOR AS IAW GMM 6-2-100 CRITERIA.

Part: RETAINER — CRACKED (ZONE 800) · airframe 52,447 hrs · 30,243 cycles

R1 DOOR CUT OUT AFT UPPER CORNER SEAL RETAINER CRACKED. REPLACE SEAL RETAINER. R1 DOOR CUT OUT AFT UPPER CORNER SEAL RETAINER REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FLOOR PANEL — CORRODED (BS 1510) · airframe 52,447 hrs · 30,243 cycles

AFT CARGO COMPARTMENT FLOOR PLATE SPLICE STRAP AT BS 1510 FOUND CORRODED. REMOVED AND REPLACED IAW AMM 25-50-04 REV. 4. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — MISALIGNED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

INTERCOSTAL PN 146N8531-12 AT BS 1380, STR 20R, HOLES MISMATCHED TO NR 1 FWD STOP FITTING HOLES. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97 AND REPAIR IAW EA NR F-5360-132609, REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: TEE FITTING — CRACKED (L4 DOOR) · airframe 52,447 hrs · 30,243 cycles

CABIN L4 DOOR STOP NR 3 HAS TEE CLIP CRACKED. EVALUATE AND REPAIR. TEE CLIP FOUND CRACKED 2 INCH LENGTH. REPLACED IAW E.O. E F-5310-7-5000 PT 1. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FRAME — GOUGED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

RE-WORK BS 1480, STR 22L TO STR 27L FRAME DAMAGED DUE TO NON-COMPLIANCE OF EA NR F-5310-131075 STEP 1. REFER TO SNRM NR N00883. EA NR F-5310-131075 COMPLIED WITH. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: FRAME — GOUGED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

FRAME GOUGE BETWEEN STR 25L TO STR 27L AT BS 1480. FOUND OUT OF LIMIT IAW SRM 53-00-07 REV 97. REPAIR CARRIED OUT IAW SRM 53-00-07 FIG. 201 (SHT 4 OF 15) REPAIR 5. NOTE: INSP THRESHOLD AT 37,500 FC AFTER REPAIR INSTALLATION OR 50,000 AIRFRAME FC WHICHEVER COMES FIRST. REPEATITIVE HFEC AND DETAILED INSP AT AN INTERVAL OF 12,000FC. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

AT BS 1380 FWD OF NR 2 CARGO DOOR SIDE WALL SUPPORT DAMAGED. AT BS 1380 SIDE WALL SUPPORT FOUND WITH MULTIPLE CRACKS. SIDE WALL SUPPORT REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 620 TO 840 STR 26R TIE DOWN SUPPORT FITTINGS DAMAGED. CORRODED TIE DOWN FITTINGS (12 EA) REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

AFT CARGO COMPT FLOOR PANEL SUPPORT FOUND WITH .2500 INCH CRACK THROUGH NUTPLATE HOLE AT STA 1493 LBL 10.45. CRACKED SUPPORT ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FLOOR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FWD CARGO COMPT FLOOR PLATE FROM BS 653 TO BS 750 FOUND CORRODED AND WITH NUMEROUS DENTS. CORRODED FLOOR PLATES REMOVED AND REPLACED IAW EO F-2330-7-5000 A1 PT. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 780 TO 800 LBL 8 STR 28L CORRODED. CORRODED STRINGER (KEEL CHORD) REMOVED AND SECTIONAL REPAIR CARRIED OUT IAW EA F-5310-131064 (TITLE: KEEL CHORD , BS 700-800, STRINGER S-28L CORROSION REPAIR. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 840, STR 22R TO 26R SIDEWALL SUPPORT ANGLE CORRODED. CORRODED ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FLOOR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FWD CARGO COMPT FLOOR PLATE FROM BS 550 TO BS 653 FOUND CORRODED AND WITH NUMEROUS DENTS. CARGO FLOOR PANELS REPLACED IAW EA NRF-2550-132604 (TITLE : CARGO COMPARTMENT - FABRICATE NEW CARGO FLOOR PANELS). REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FWD CARGO COMPT RT SIDEWALL CAP STRIPS FROM BS 660 TO 880 FOUND CORRODED. SIDEWALL CAP STRIPS FOUND CORRODED BEYOND SRM LIMITS. CAP STRIPS REMOVED AND REPLACED IAW AMM 20-11-00 REV 4. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FLOOR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FWD CARGO COMPT FLOOR PLATE FROM BS 750 TO BS 843 FOUND CORRODED AND WITH NUMEROUS DENTS. CORRODED FLOOR PLATES REMOVED AND REPLACED IAW EO E F-2550-7-5000 A1-P1. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1360 STR 23R TO 26R FRAME CORRODED. CORRODED FRAME AT BS 1360 REPAIRED IAW SRM 53-00-07 REV 97. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 840, STR 22L TO 26L SIDEWALL SUPPORT ANGLE CORRODED. CORRODED SIDEWALL ANGLE AT BS 840 REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 508 TO 840 STR 26L TIEDOWN SUPPORT FITTINGS DAMAGED. CORRODED TIEDOWN FITTINGS (17 EA) REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FRAME — DENTED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

AT BS 1340 STR 26R FRAME DAMAGED. DENTED FUSELAGE FRAME FLANGE AT BS 1340 REPAIRED IAW SRM 53-00-07 REV 97. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 760 STR 22L SIDEWALL SUPPORT ANGLE CORRODED. CORRODED SIDEWALL SUPPORT ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 765 TO 840 LT SIDE TRANISTION PANEL CORRODED. CORRODED TRANSITION PANEL REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

DURING REMOVAL OF FRAME SHEAR TIE CLIP, FOUND CORROSION ON TEE CHORD AT STA 780, STR 28R LBL 8. TEE CHORD CORROSION REPAIR CARRIED OUT IAW EA F-5330-129624. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

PANEL 193AL DRAIN MAST PLATE WITH NUTPLATES ATTACHED CORRODED. CORRODED PANEL 193AL DRAIN MAST ADAPTER PLATE REMOVED AND REPLACED IAW CMM 38-31-01 REV 98 AND SRM 51-40-02 REV 96. REPAIR IS CLASSIFIED AS MINOR GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

ONE EXISTING REPAIR DOUBLER REQUIRES REMOVAL FROM STA 740-760 BETWEEN STR 25L-27L FOR S/M WORK ACCESS. EXISTING REPAIR DOUBLER REMOVED AND REPAIRED IAW EA F-5330-131077. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 765 TO 840 RT SIDE TRANSITION PANEL CORRODED. CORROSION ON TRANISTION PANEL FOUND EXCEEDED SRM DAMAGE LIMITS. TRANSITION PANEL REMOVED AND REPLACED IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

LAP JOINT AT STA 660 TO STA 760, S-26R, FOUND IN BETWEEN SKIN CORROSION AT SEVERAL PLACES. EVALUATE AND RECTIFY STA 660 TO STA 760, S-26R LAP JOINT SKIN CORROSION AREA REPAIR CARRIED OUT IAW EA F-5330-131060 PART 1, FUSELAGE-PLATES AND SKIN-FS 660- FS 760, STR S-26L TO S-26R LWR SKIN LAP JOINT (AD 2006-11-11-EO F-0524-7-5000; AD 2007-19-17, EO F-5330- 7-5000) DOUBLER REPAIR. REPAIR CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100 CRITERIA.

Part: SKIN PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT AIR CONDITIONING BAY UPPER SKIN HAS CORROSION AT STA 918, RBL 45.0 INCH. CORRODED SKIN REPAIRED IAW EA F-5730-126239. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FWD CARGO FLOORBEAM SPLICE ANGLE BELOW FOUND CORROSION AT STA 633 BL 3, 8, 12, 16 AND RBL 3,8, 12, 16. CORRODED SUPPORT SPLICE ANGLES REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 820 LBL 16 TRANSITION PANEL SUPPORT ANGLE CORRODED. CORRODED SUPPORT ANGLE ON TRANSITION PANEL AT BS 820 REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

TRANSITION PANEL BS 650 TO 765 RT SIDE CORRODED. CORROSION ON TRANSITION PANEL FOUND EXCEEDED SRM DAMAGE LIMITS. PANEL REMOVED AND REPLACED IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — DAMAGED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

AT BS 1200 STR 26R TO 26L BULKHEAD SUPPORT ANGLE HAS ELONGATED HOLES. BULKHEAD SUPPORT ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SKIN PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT WING UPPER SURFACE SKIN FOUND WITH CORROSION AT AROUND WBL 75.0 STRINGER 5. SKIN CORROSION REPAIR CARRIED OUT IAW EA F-5720-131081 (TITLE : RT WING UPPER SKIN, WBL 95, STR 5 SURFACE CORROSION REPAIR. REPAIR IS CLASSIFIED AS MAJOR GMM 6-2-100 CRITERIA.

Part: SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FWD CARGO COMPARTMENT TRANSITION PANEL SPLICES (02 EA) AT STA 645 AND STA 765, RBL 20 FOUND CORRODED. CORRODED TRANSITION PANEL SPLICES REMOVED AMD REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GIMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 740 RBL 8 FLOOR SUPPORT ANGLE CORRODED. CORRODED SUPPORT ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR GMM 6-2-100 CRITERIA.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FWD CARGO COMPARTMENT TRANSITION PANEL FOUND WITH CORROSION BETWEEN STA 645 AND STA 765 LBL 20. CORRODED TRANSITION PANEL REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 780 RBL12 FRAME SUPPORT ANGLE CORRODED. REMOVED AND REPLACED FRAME SUPPORT ANGLE IAW SRM 51-40-02 REV 97. REPAIR IS CLAISSIFIED AS MINOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT WING TANK OVERWING FILL PORT AREA UPPER WING SKIN WITH CORROSION AFTER ADAPTER REMOVAL. RT OVERWING FILL PORT CORROSION AREA REPAIRED IAW NR F-5720-129613. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

ONE EXTERNAL REPAIR DOUBLER REQUIRES REMOVAL FROM STA 888 TO STA 900 BUTT JOINT BETWEEN STR 25L AND STR 27L FOR SHEETMETAL ACCESS. EXISTING DOUBLERS REMOVED AND REPLACED IAW EA F-5330-131078. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 800, STR 28R CORRODED IN FWD CARGO PIT BESIDE FRAME SUPPORT ANGLE. CORRODED KEEL CHORD REPAIRED IAW EA F-5330-131083. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 720 TO 740 LBL 20 INTERCOSTAL CORRODED. INTERCOSTAL WEB FOUND CORRODED BEYOND SRM DAMAGE LIMITS. INTERCOSTAL WEB REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITIERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 680 LBL 20 TRANSITION PANEL SUPPORT ANGLE CORRODED. CORRODED SUPPORT ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FWD CARGO COMPARTMENT TRANSITION PANEL SPLICES ( 02 EA) AT STA 645 AND STA 765, LBL 20 FOUND CORRODED. CORRODED SPLICES REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FWD CARGO COMPARTMENT TRANSITION PANEL FOUND CORRODED BETWEEN STA 508 AND STA 645 LBL 20. CORRODED TRANSITION PANEL BETWEEN STA 508 AND STA 645 REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT WING UPPER SURFACE SKIN SEVERAL FASTENERS FOUND WITH CORROSION. EVALUATE AND RECTIFY. RT WING UPPER SKIN QTY 18 EACH CORRODED FASTENERS REPAIRED IAW EA F-5720-131067, WINGS-WING SECONDARY STRUCTURE-RT WING UPPER SKIN WS 285, WS 341, STR U1 AND STR U13 SURFACE CORROSION REPAIR-STATIC STRENGTH APPROVAL PENDING DTE. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 1400, RBL 22 FRAME SUPPORT ANGLE FOUND CORRODED. EVALUATE AND REPAIR. FRAME SUPPORT ANGLE REMOVED AT BS 1400, RBL 22 IAW SRM 51-40-02 REV 97. CORROSION FOUND EXCEED LIMIT IAW SRM 53-00-07, FIG 101 REV 97. SUPPORT ANGLE FABRICATED IAW DWG NR 140N2006, SHT 2, REV D. PART MARK AS FX 140N2006-210 IAW GMM 7-0-1001. SUPPORT ANGLE INSTALLED IAW SRM 51-40-02 REV. 97 REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FWD CARGO COMPARTMENT BS 660 TO BS 680, LBL 10 INTERCOSTAL WEB FOUND CORRODED. EVALUATE AND REPAIR. BS 660 TO BS 680, LBL 10 CORRODED INTERCOSTAL WEB REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. INTERCOSTAL WEB FABRICATED IAW NR 143N5355 SHT 5 REV. B. PART MARK AS FX 143N5355-35 IAW GMM 7-0-1001 REV 107. REPAIR CLASSIFIED AS MINOR REPAIR IAW GMM 6-2-100 CRITERIA.

Part: SKIN PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 840 TO 860 RBL 8 TO LBL 8 SKIN CORRODED. CORROSION ON SKIN BETWEEN BS 840 AND BS 860 FOUND EXCEEDED SRM DAMAGE LLIMITS. SKIN REPAIRED IAW EA F-5330-131068 (TITLE: BS 860, RBL0.0 FUSELAGE SKIN CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: BRACKET — DENTED (ZONE 300) · airframe 52,447 hrs · 30,243 cycles

AFT ACCESSORY COMPARTMENT, ON ELEVATOR AFT MECHANISM, A BRACKET PN 251N2299-3 HAVE A DENT. DENT ON ELEVATOR BRACKET PN 251N2299 REPAIRED IAW F-2730-129605. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

WHILE WORKING SNRM NR N00008 WITH EA F-5330-128607 FOUND EXISTING REPAIR AT LWR FUSELAGE SKIN BS 700 BETWEEN S-28L TO S-29R HAVING CORROSION ON EXTERNAL DOUBLER AND IS A TIME LIMITED REPAIR. REPAIR AS NECESSARY. STA 700, S-28L TO S-28R CORRODED EXTERNAL REPAIR DOUBLER REMOVED AND REPAIR CARRIED OUT IAW SRM 53-00-01 FIG 201 REV 97. REPAIR CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100. REPETITIVE INSP HFEC REQUIRED IAW SRM 53-00-01 FIG. 201, REPAIR 3 TABLE V REPAIR INSPECTION REQUIREMENTS REV 97. NEXT INSP IS 36,243 FLIGHT CYCLES.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AFTER EVALUATION WITH FASTENERS REMOVED, CORROSION FOUND ON RT UPPER SURFACE SKIN T/E MACHINE SKIN UNDER T/E FIXED PANEL. EVALUATE AND RECTIFY. RT WING UPPER SKIN T/E MACHINE SKIN UNDER T/E FIXED PANEL REPAIRED BETWEEN WBL 85 TO WBL 133 IAW EA F-5720-129619, WING SECONDARY STRUCTURE-AD 92-07-15 CORROSION ON RT WING REAR SPAR REPAIR. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

LAP JOINT AT STA 660 TO STA 760, S-26L, FOUND IN BETWEEN SKIN CORROSION AT SEVERAL PLACES. EVALUATE AND RECTIFY STA 660 TO STA 760, S-26L LAP JOINT SKIN CORROSION AREA REPAIR CARRIED OUT IAW EA NR F-5330-131060 PART 1, FUSELAGE-PLATES AND SKIN-FS 660-FS 760, STR S-26L TO S-26R LWR SKIN LAP JOINT (AD 2006-11-11-EO F-0524-7-5000; AD 2007-19-17, EO F-5330- 7-5000) DOUBLER REPAIR. REPAIR CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 879 TO BS 900 LBL 8 KEELBEAM CORRODED. KEEL BEAM CHORD AT BS 889 FOUND CORRODED BEYOND SRM DAMAGE LIMITS. KEEL BEAM CHORD REPAIRED IAW EA F-5330-131062 (TITLE: BS 889, STR S-28L KEEL BEAM CHORD CORROSION REPAIR. REPAIR IS CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100 CRITERIA.

Part: FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

NR 1 PYLON RT T/R AFT FITTING FOUND CORRODED. CORROSION ON RT T/R FITTING ON NR 1 PYLON FOUND EXCEEDED SRM DAMAGE LIMITS. FITTING REMOVED AND REPLACED IAW AMM 20-11-00 REV 4. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT AIR CONDITIONG UPPER BAY SURFACE HAS CORROSION AT STA 918, RBL 50.0 INCH TO RBL 54.0 INCH. CORRODED AREA REPAIRED IAW EA F-5710-131063 : REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 705 RBL 3-16 FLOORBEAM CORRODED AND DAMAGED. CORRODED AND DAMAGED FLOORBEAM BS 705 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

NR 2 PYLON LT AFT T/R FITTING FOUND CORRODED. FITTING REMOVED AND REPLACED IAW SOPM 20-50-01 REV 108. REPAIR IS CLASSIFIED IAW GMM 6-2-100 CRITERIA.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 686, STR 18L, STR SPLICE CORRODED. CORROSION ON STR SPLICE AT BS 686 FOUND EXCEEDED SRM DAMAGE LIMITS. SPLICE REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 660, STR 28L, STR SPLICE CORRODED. CORRODED STR SPLICE AT BS 660. REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 720 TO 740 RBL 8 INTERCOSTAL CORRODED. INTERCOSTAL FROM BS 720 TO BS 740 FOUND CORRODED THROUGH INTERCOSTAL. REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1300, STR 26L BELOW TRANSITION PANEL SUPPORT ANGLE CORRODED. CORROSION ON SUPPORT ANGLE AT BS 1300 FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. SUPPORT ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FWD CARGO FLOOR SUPPORT SPLICES (8 EACH) FOUND CORRODED AT STA 705 LBL 3, 8, 12, 16 AND RBL 3, 8, 12, 16. FLOOR SUPPORT SPLICES FOUND CORRODED BEYOND SRM ALLOWABLE DAMAGE LIMITS. SPLICES REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 705 TO 840 LBL 3, 8, 12 AND 16 FLOOR BEAMS CORRODED AND DAMAGED. FLOOR SUPPORT FOUND CORRODED THROUGH. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FROM STA 1360 TO STA 1380, BETWEEN STR 27L AND 28L, FOUND INTERCOSTAL CORRODED. CORROSION ON INTERCOSTAL BETWEEN STA 1360 AND STA 1380 FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. INTERCOSTAL REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 660, STR 27L STR SPLICE CORRODED. CORROSION ON STR AT BS 660 FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. STR REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: FITTING — LOOSE (ZONE 400) · airframe 52,447 hrs · 30,243 cycles

RT PYLON DIAGONAL BRACE FITTING SHIM TOTAL CUMULATIVE MOVEMENT APPROX 0.75 INCHES FOUND LOCATED AT RT TOP BETWEEN VERTICAL FLANGE AND BULKHEAD. REPAIR CARRIED OUT IAW EA F-5450-131090 : RT PYLON STRUT-TO-DIAGONAL BRACE FITTING SHIM MIGRATION REPAIR. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: BRACKET — CORRODED (BS 860-900) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AFTER REMOVAL OF INTERCOSTAL BTWEEN STA 860 AND 900, BRACKET FOUND CORRODED AT STA 900, LBL 7.0 WING-TO-BODY FAIRING. BRACKET BETWEEN STA 860 AND 900 FOUND CORRODED BEYOND SRM ALLOWABLE DAMAGE LIMITS. CLIP REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FLOOR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FWD CARGO COMPARTMENT FLOOR PLATE FROM BS508 TO BS 550 FOUND CORRODED AND WITH NUMEROUS DENTS. REMOVED AND REPLACED IAW EA NR F-2550-132604. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT WING-TO-BODY FAIRING INTERCOSTAL SUPPORT ANGLE TO FAIRING HAS CORROSION AT STA 900, RBL 19.0 INCH. CORROSION ON INTERCOSTAL CLIP FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. REMOVED AND REPLACED INTERCOSTAL CLIP IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: GATE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

R1 PAX DOOR LWR GATE HAS CORROSION. RI DOOR LWR GATE CORROSION FOUND EXCEEDED SRM ALLOWABLE LIMIT. DOOR GATE REMOVED AND REPLACED IAW AMM 52-11-38 REV 04. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (BS 839 S25-26R) · airframe 52,447 hrs · 30,243 cycles

BS 839 STRINGER S-25R TO S-26R FRAME SUPPORT ANGLE CORRODED. REMOVED AND FABRICATED IAW MFG DWG NR 143N1025 REV A AND INSTALLED IAW SRM 51-40-02 REV 97. PART MARKED IAW GMM 7-0-1001 REV 107. REPAIR IS CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100 CRITERIA.

Part: FITTING — GOUGED (ZONE 300) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

APU INTAKE DOOR SUPPORT TOP PORTION OF FITTING ENCOVERING THE TWO BUSHING HAS DEEP GOUGE MARK ON BOTH SIDES. REPAIR WAS CARRIED ON APU INTAKE DOOR SUPPORT TOP PORTION OF FITTING IAW E.A. F-4915-129231. REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 7-02-100 CRITERIA.

Part: GATE — CORRODED (L1 DOOR) · airframe 52,447 hrs · 30,243 cycles

L1 DOOR, LOWER DOOR GATE HAS CORROSION. REMOVED AND REPLACED IAW AMM 52-11-38 REV. 4. OPERATION CHECK CARRIED OUT IAW AMM 52-11-00 REV. 4, FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 CRITERIA.

Part: BELLCRANK — DAMAGED (ZONE 600) · airframe 52,447 hrs · 30,243 cycles

RT INBOARD TRAILING EDGE FLAP, MAIN FLAP O/B CARRIAGE AREA FAIRING BELLCRANK FORK END (LONGER SIDE) WITH ONE NICK. NICK ON RT INBD TRAILING EDGE FLAP OUTB CARRIAGE FAIRING BELLCRANK FORK END REPAIRED IAW E.A. F-5740-131082. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: STRINGER CLIP — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 839 STR 26R STRINGER CLIP CORRODED. STRINGER CLIP AT BS 839, STR-26R FOUND CORRODED BEYOND SRM REPAIR LIMITS. STRINGER CLIP REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 1640 BULKHEAD AFT CARGO ANGLE FOUND CORRODED. CORROSION ON ANGLE AT BS 1640 BULKHEAD FOUND EXCEEDED SRM REPAIR LIMITS. ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: RIB — CORRODED (ZONE 600) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RIGHT WING T/E OUTB RIB JUMPER BONDING SURFACE AT WS 817.27 FOUND WITH CORROSION. REPAIRED IAW E.A. F-5710-131074, REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

WING-TO-BODY FAIRING AT STA 800, LBL 5 TO RBL 5, SPLICE ANGLE HAS EXFOLIATION CORROSION. CORROSION ON SPLICE ANGLE FOUND EXCEEDED SRM DAMAGE LIMITS. ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (BS 840) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 840, STR 22R TO 22L, FLOOR SUPPORT BEAM CORRODED. FLOOR SUPPORT FOUND BADLY CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: ANGLE — CRACKED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

BS 840, STR 22R SUPPORT ANGLE CRACKED. SUPPORT ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 840, STR 22L, SIDEWALL-TO-SUPPORT ANGLES FOUND CORRODED. CORROSION ON SUPPORT ANGLES FOUND EXCEEDED SRM DAMAGE LIMITS. ANGLES REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AIR COND RAM AIR INLET FRAME SUPPORT STRUCTURE HAS CORROSION FROM STA 680 TO STA 900, RBL 19.0". CORROSION ON SUPPORT STRUCTURE FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. SUPPORT STRUCTURE REMOVED AND REPLACED IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CRACKED (ZONE 200) · airframe 52,447 hrs · 30,243 cycles

R2 PAX DOOR UPPER HINGE CUT-OUT HAS A CRACK. CRACKED CUT-OUT AREA REPAIRED IAW FEDEX E.A. F-5210-126216 (TITLE: R2 DOOR CRACK REPAIR). REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CRACKED (ZONE 200) · airframe 52,447 hrs · 30,243 cycles

L2 PAX DOOR UPPER HINGE CUT-OUT HAS A CRACK. CRACK ON L2 PAX DOOR UPPER HINGE CUTOUT FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. REPAIR CARRIED OUT IAW E.A. F-5210-12617. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: GATE — CORRODED (R2 DOOR) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

R2 PAX DOOR BOTTOM DOOR GATE HAS INTERGRANULAR CORROSION. CORROSION FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. R2 PAX DOOR BOTTOM GATE REMOVED AND REPLACED IAW B757-200 AMM 52-11-38 REV. 4. REPAIR IS CLASSIFIED AS MINOR PER GIMM 6-2-100 CRITIERIA.

Part: FRAME — DAMAGED (BS 1380) · airframe 52,447 hrs · 30,243 cycles

AFT CARGO FRAME FOUND WITH TOOLING DAMAGE AT BS 1380, BETWEEN STR 25R AND STR 26R. REPAIRED IAW EA F-5360-132602. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SKIN — DAMAGED (BS 1360-1375) · airframe 52,447 hrs · 30,243 cycles

TOOL DAMAGE FOUND ON AFT CARGO BAY FUSELAGE SKIN FROM BS 1360 TO 1375, BETWEEN STR 25R AND 26R. REPAIRED IAW EA NR F-5360-132602. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: HOUSING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RIGHT AIR COND RAM AIR INLET ASSY TORQUE TUBE SUPPORT HOUSING P/N. 213T3701-2 FOUND CORRODED. CORROSION ON SUPPORT HOUSING FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. SUPPORT HOUSING REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FRAME — CORRODED (BS 839) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 839 STR 25R TO 27R FRAME CORRODED. CORROSION ON FRAME SPLICE DOUBLER AT BS 839 FOUND EXCEEDED SRM LIMITS. REMOVED AND REPLACED SPLICE DOUBLER IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 839, BL 0 FRAME SUPPORT ANGLE CORRODED. CORROSION ON SUPPORT ANGLE AT BS 839 FRAME FOUND EXCEEDED SRM LIMITS. SUPPORT ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: GATE — CORRODED (L2 DOOR) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

L2 PAX DOOR BOTTOM DOOR GATE HAS INTERGRANULAR CORROSION. CORROSION ON L2 DOOR GATE EXCEEDED SRM ALLOWABLE DAMAGE LIMIT. DOOR GATE REMOVED AND REPLACED IAW AMM 52-11-38 REV 4. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1400 STR 24L TO 26L FRAME CORRODED AND DAMAGED. CORROSION ON FRAME FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. REPAIR CARRIED OUT IAW SRM 53-00-07 REV 97, FIG 201 DETAIL III. TO RE-INSPECT REPAIR AT 37,500 FC AND REPEAT AT 12,000 FC INTERVAL. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: FRAME — DAMAGED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

AT BS 1580 STR 23L FRAME DAMAGED. DAMAGED FRAME REPAIRED IAW SRM 53-00-07 REV 97 FIG 201 DETAIL III. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ACCESS DOOR) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

ELEVATOR CONTROL ACCESS DOOR (313AL) EDGE CORRODED. CORROSION ON ELEVATOR CONTROL DOOR SKIN FOUND EXCEED SRM DAMAGE LIMITS. DOOR SKIN REPLACED IAW SRM 52-40-01 REV 96. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: WEDGE — DENTED (NR 7 SLAT) · airframe 52,447 hrs · 30,243 cycles

MINOR DENT FOUND ON SLAT NR 7 UPPER SURFACE SKIN AT OSS 344.5 AS MARKED. RT WING NR 7 SLAT T/E WEDGE REPLACED. REFER TO REPAIR DIVISION FORM 8130-3 TRACKING NR NSF C187867 002. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

STA 1681, LBL 39.50 INCH FLOORBEAM UPPER CHORD BOTTOM CORRODED. CORROSION ON FLOORBEAM FOUND EXCEEDED SRM ALLOWABLE LIMITS. REPAIR CARRIED OUT IAW EA F-5310-126226, CORROSION ON FLOORBEAM 1681.80 AT MULTIPLE LOCATIONS - REPAIR. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 52,447 hrs · 30,243 cycles

TO COMPLY WITH EA F-5310-129611 REV A, REPAIR ELONGATED HOLES ON FLOORBEAM AT BS 780, LBL 51.0. REPAIR CARRIED OUT ON FLOORBEAM IAW EA F-5310-129611 REV A. REPAIR ELONGATED HOLES ON FLOORBEAM AT BS 780, LBL 51.0. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

STA 1681 LBL 32 IN FLOORBEAM UPPER CHORD BOTTOM CORRODED. CORROSION ON UPPER CHORD FOUND EXCEEDED SRM ACCEPTABLE LIMITS. REPAIR CARRIED OUT IAW EA F-5310-126226, CORROSION ON FLOORBEAM 1681.80 AT MULTIPLE LOCATIONS - REPAIR. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (NR 8 SLAT) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT WING SLAT NR 8 ANGLE FASTENER HOLES THRU ACCESS PANEL 623GB AT OSS 559.55 AND OSS 549.7 FOUND WITH MINOR CORROSION. SLAT NR 8 INTERIOR CORROSION AREA BETWEEN OSS 559.55 AND OSS 549.97 REPAIRED IAW SRM 51-10-02 REV 97. REFER TO FORM 8130-3 TRACKING NR FA 2009/0347. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

STA 1681, LBL 11.50 FLOORBEAM UPPER CHORD BOTTOM CORRODED. CORROSION ON FLOORBEAM UPPER CHORD FOUND EXCEEDED SRM LIMITS. REPAIR CARRIED OUT IAW EA F-5310-126226. CORROSION ON FLOORBEAM 1681.80 AT MULTIPLE LOCATIONS - REPAIR. REPAIR IS CLASSIFIED AS MAJOR, GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1680 LBL 53 BOTTOM OF TOP CHORD OF AFT PRESSURE DECK CORRODED. FLOORBEAM UPPER CHORD CORROSION FOUND EXCEEDED SRM REPAIR LIMITS. REPAIR CARRIED OUT IAW EA F-5310-126226. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: WEDGE — DENTED (NR 7 SLAT) · airframe 52,447 hrs · 30,243 cycles

MINOR DENT FOUND ON NR 7 SLAT UPPER SKIN AT OSS 333.3 AS MARKED. RT WING NR 7 SLAT T/E WEDGE REPLACED. REF TO FORM F8130-3 TRACKING NR SNF C187867 002. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (NR 7 SLAT) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT WING SLAT NR 7 T/E WEDGE TOP SKIN INTERNAL SURFACES FOUND WITH CORROSION AS MARKED. RT WING SLAT NR 7 REPAIRED IAW SRM 51-30-01 REV 97. REFER FORM 8130-3 TRACKING NR FA 2009/0327. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CITERIA.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

STA 1681, RBL 47.5 INCH FLOORBEAM UPPER CHORD BOTTOM CORRODED. CORROSION ON FLOORBEAM FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. REPAIR CARRIED OUT IAW EA F-5310-126226, CORROSION ON FLOORBEAM 1681.80, MULTIPLE LOCATIONS - REPAIR. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1620 STR 30 BL 0 CORRODED. CORROSION ON STRINGER FOUND EXCEEDED SRM DAMAGE LIMITS. STR 30 BETWEEN STA 1610 AND STA 1620 REPAIRED IAW SRM 53-00-53 REV. 97, REPAIR 2, FIG 207. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 1620, BL 0, STRINGER SPLICE PLATE CORRODED. CORROSION ON STR SPLICE PLATE FOUND EXCEEDED SRM REPAIRABLE LIMITS. SPLICE CHANNEL REMOVED AND REPLACED IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — DAMAGED (ZONE 200) · airframe 52,447 hrs · 30,243 cycles

LT FRAME STA 1280 FROM STR 10L TO STR 14L, SEVERAL NICKS AND GOUGE MARKS FOUND AT FWD SIDE OF FRAMES. DAMAGED FRAME REMOVED AND REPLACED IAW SRM 51-40-02 REV.97 REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ATTACH BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

WING-TO-BODY FAIRING SUPPORT FRAME HAS WIRE BUNDLE CLIPS CORRODED AT STA 900. CORRODED WIRE BUNDLE CLIPS ( 7 EA) AT STA 900 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 1661 RBL 55 TOP OF FLOORBEAM FOUND CORRODED. EVALUATE AND REPAIR. REPAIRED FLOORBEAM AT BS 1661 RBL 55 IAW PTF STA ENGRG EA NR 757- 5361-08-E0277 REV. -, CORROSION ON FLOORBEAM UPPER CHORD AT STA 1661 RBL 58.22 AFFECTING INSTALLATION OF STIFFENER AND SHEAR WEB. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA. RE-WORK REQUIRED DUE TO CORRECTIVE ACTION CROSS REFERENCE TO STA ENGRG. EA NR 757-5361-08-E0277. AN SNRM NR N05239 WAS GENERATED TO RE-WORK AND COMPLY IAW EA F-5360-131746 REV.- .

Part: STOP FITTING — GOUGED (ZONE 800) · airframe 52,447 hrs · 30,243 cycles

NR 1 CARGO DOOR AFT DOOR FRAME, 4TH DOOR STOP FROM TOP HAS A DEEP GOUGE. EVALUATE AND RECTIFY. NR 1 CARGO DOOR, 4TH DOOR STOP FITTING GOUGE AND CORROSION REMOVED AND FOUND TO BE OUT OF LIMIT IAW SRM 52-30-02 REV. 97. DOOR STOP FITTING REMOVED AND REPLACED IAW SRM 51-40-02, REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM ACCESS PANEL 149EL ATTACHED HOLD-OPEN ROD SUPPORT FITTING HAS SURFACE CORROSION. CORROSION ON SUPPORT FITTING FOUND EXCEEDED SRM DAMAGE LIMITS. REMOVED AND REPLACED SUPPORT FITTING IAW AMM 20-11-00 REV. 04. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

STA 1200 TO STA 1310 RT TRANSITION PANEL FOUND CORRODED. CORROSION ON TRANSITION PANEL FOUND EXCEEDED SRM DAMAGE LIMITS. REMOVED AND REPLACED TRANSITION PANEL IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: RETAINER — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

LT MLG DOOR SEAL RETAINERS AND HARDWARE ARE CORRODED FROM STA 1180 TO STA 1040, LBL 8 BELOW KEEL BEAM. CORROSION ON RETAINERS FOUND EXCEEDED ALLOWABLE SRM DAMAGE LIMITS. RETAINERS REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: BRACKET — DAMAGED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

RT AIR COND UPPER BAY SUPPORT BRACKET AT BS 918, RBL 10" FOUND BADLY DEFORMED. DEFORMED BRACKET REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1310 TO 1410 LT SIDE TRANSITION PANEL CORRODED. CORROSION ON TRANSITION PANEL FOUND EXCEEDED SRM REPAIRABLE LIMITS. PANEL REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

TEE CHORD ATTACHING SPLICE ANGLE AT STA 918, LBL 8 IN HAS CORROSION. CORROSION ON SPLICE ANGLE FOUND EXCEEDED ALLOWABLE SRM LIMITS. ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: TEE FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT STA 1240, STR 28L BELOW TRANSITION PANEL SUPPORT TEE CLIP FOUND CORRODED. CORROSION ON CLIP FOUND EXCEEDED SRM LIMITS. CLIP REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEELBEAM ACCESS PANEL 149CL ATTACHED HOLD-OPEN ROD SUPPORT PANEL FITTING FOUND CORRODED. CORROSION ON SUPPORT FITTING AT STA. 1085, LBL 8 FOUND EXCEEDED SRM LIMITS. SUPPORT FITTING REMOVED AND REPLACED IAW AMM 20-11-00 REV. 4. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: RETAINER — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT MLG DOOR SEAL RETAINERS AND HARDWARE HAVE CORROSION FROM STA 1180 TO STA 1040, RBL 8.0 INCHES BELOW BEAM. CORROSION ON SEAL RETAINERS FOUND EXCEEDED SRM LIMITS. SEAL RETAINERS REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

WING-TO-BODY FAIRING FRAME AT STA 800, BL0 TO RBL 11 HAS EXFOLIATION CORROSION. WING-TO-BODY FRAME AT STA 800 FOUND CORRODED BEYOND SRM DAMAGE LIMITS. FRAME REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: STRAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1560 RBL 26, CARGO CEILING SUPPORT STRAP CORRODED. CORROSION ON STRAP FOUND EXCEEDED SRM LIMITS. STRAP REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEELBEAM ACCESS DOOR HOLD-OPEN ROD SUPPORT FITTING AT STA 1087, LBL 8, FOUND CORRODED. CORRODED SUPPORT FITTING AT STA 1087 BLENDED AND FOUND EXCEEDED SRM REPAIRABLE LIMITS. SUPPORT FITTING REMOVED AND REPLACED IAW AMM 20-11-00, REV. 4. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

SUPPORT CHANNEL FOR TRANSITION PANEL ON AFT SIDE OF FRAME AT STA 1640 ABOVE STRINGER 27 RT, CORRODED. CORROSION ON SUPPORT CHANNEL FOUND EXCEEDED SRM LMITS. SUPPORT CHANNEL REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

STA 1320, RBL 24.75, WL 207.1, FLOORBEAM TOP FLANGE FOUND CORRODED. REPAIR CARRIED OUT IAW SRM 53-00-51, FIG 201. REV 96 AND EA F-5310-129614. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FROM STA 1540 TO STA 1560, STR 27L, INTERCOASTAL SUPPORT ANGLE CORRODED. CORROSION FOUND OUT OF SRM ALLOWABLE DAMAGE LIMITS. SUPPORT ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT STA 1540 TO STA 1560 STR 26R INTERCOSTAL SUPPORT ANGLE CORRODED. CORROSION ON SUPPORT ANGLE FOUND EXCEEDED SRM ALLOWABLE LIMITS. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-00 CRITERIA.

Part: STRINGER CLIP — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 900, STR 26 R STR SUPPORT ANGLE CORRODED. CORROSION ON SUPPORT ANGLE FOUND EXCEEDED SRM ALLOWABLE LIMITS. REPAIR CARRIED OUT IAW E.A. F-5310-131079 : BS 900, S-26R STRINGER SPLICE -REPAIR PART FABRICATION. REPAIR IS CLASSFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 881 STR 25 L STR CORRODED. CORROSION ON STRINGER AT BS 881, 25L FOUND EXCEEDED SRM ALLOWABLE LIMITS. STRINGER REPAIRED IAW SRM 53-00-03 FIG 201 REV 97. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: FRAME — CORRODED (FAIRING) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

LT CHORD ON FAIRING STRUCTURE FROM STA 1120 TO STA 1138, LBL 8.0" HAS CORROSION. CORROSION FOUND EXCEEDED SRM REPAIRABLE LIMITS ; LOWER CHORD REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA..

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FROM BS 1500 TO BS 1520, RBL 4, INTERCOSTAL CORRODED. CORROSION ON INTERCOSTA REMOVED AND FOUND OUT OF SRM LIMITS. INTERCOSTAL REMOVED AND REPLACED IAW B757-200 SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: MOUNT — CORRODED (A/C BAY DOORS) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

LT AIR CONDITIONG BAY : 4 DOOR MOUNTS HAVE CORROSION. CORROSION FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. REPAIR CARRIED OUT IAW E.A. F-5340-129618 : FORWARD KEEL BEAM FITTING REPAIR. REPAIR IS CLASSIFIED AS MINOR REPAIR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT AIR COND BAY UPPER BAY AT BS 917, RBL 10, FOUND SURFACE CORROSION. REPAIR CARRIED OUT IAW E.A. F-5720-131069. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FROM STA 1360 TO STA 1380, STR 27L, INTERCOASTAL SUPPORT ANGLE CORRODED. CORROSION FOUND EXCEEDED SRM REPAIRABLE LIMITS. SUPPORT ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1440 BETWEEN STR 29R AND 30R, FRAME SUPPORT PLATE CORRODED. CORROSION FOUND OUT OF SRM LIMITS. SUPPORT PLATE REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (NR 4 SLAT) · airframe 52,447 hrs · 30,243 cycles

LT WING L/E NR 4 SLAT PANEL NR 522HB T/E WEDGE TOP SKIN INTERNAL SURFACES WITH CORROSION. LT WING L/E NR 4 SLAT, T/E WEDGE REPLACED. REFER TO THE MFG REPAIR ORDER DISCREPANCY WORKSHEET AND FAA FORM 8130-3 WITH TRACKING NRS FA2009/0282 AND NSFC187868-002 , RESPECTIVELY.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 900 STR 24R STR SUPPORT ANGLE CORRODED. CORROSION ON SUPPORT ANGLE AT BS 900, S-24R, FOUND BEYOND SRM REPAIR LIMITS. ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 900 STR 27R STR SUPPORT ANGLE CORRODED. CORRODED SUPPORT ANGLE AT BS 900, STR 27R, FOUND BEYOND SRM REPAIR LIMIT. SUPPORT ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 900, STR 27L, STR SUPPORT ANGLE CORRODED. CORROSION ON SUPPORT ANGLE AT BS 900, S-27L, FOUND EXCEEDED SRM DAMAGE LIMITS. ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — DAMAGED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

AT BS 1340, STR 22R, SIDEWALL SUPPORT ANGLE DAMAGED. SIDEWALL ANGLE FOUND BADLY DEFORMED BEYOND SRM ALLOWABLE DAMAGE LIMITS. SUPPORT ANGLE REMOVED AND REPLACED IAW DWG 146N1008 SHT 4 REV- AND DWG 146N5405 SHT 1 REV A. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1420 RBL 4 INTERCOSTAL CORRODED. CORROSION FOUND EXCEEDED SRM REPAIR LIMITS. INTERCOSTAL AT BS 1420 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 860 BL0, 2 EACH FRAME SUPPORT ANGLES CORRODED. CORROSION ON SUPPORT ANGLES FOUND BEYOND SRM REPAIR LIMITS. ANGLES REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1380, STR 24L TO 28L FRAME CORRODED. CORROSION ON AFT CARGO FRAME AT BS 1380 FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. FRAME REPAIRED IAW SRM 53-00-07 REV. 97, REPAIR 5 FIG. 201. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ACCESS DOOR) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

ELEVATOR CONTROL ACCESS DOOR (313AL) EDGE CORRODED. CORROSION ON 3131L DOOR EDGE FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. DOOR SKIN REMOVED AND REPLACED IAW SRM 52-40-01 REV. 97. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1640, STR 22 TO 27R BULKHEAD TO SIDEWALL SUPPORT ANGLE CORRODED. CORROSION ON SUPPORT ANGLE AT BS 1640, STR 22R TO 27R FOUND BEYOND SRM ALLOWABLE DAMAGE LIMITS. SUPPORT ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: ATTACH FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CHANNEL CLIP HAS CORROSION AT STA 1651, WL 208.10. CORRODED CHANNEL CLIP REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 52,447 hrs · 30,243 cycles

AFTER INSTALLATION OF MLG WW SUPPORT CHANNEL P/N 149N7553-20, ADJACENT TEE FRAME FOUND CRACK. TEE SUPPORT REMOVED AND REPLACED AS PER SRM 51-40-02 REV. 97. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 CRITERIA.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RIGHT AIR CONDITIONING UPPER BAY HAS CONNECTING ROD FITTING CORRODED AT STA 950, RBL 43.0. RT AIR CONDITIONING UPPER BAY CONNECTING ROD FITTING AT STA 950, RBL 43 CORROSION BLENDED OUT AND FOUND EXCEEDED ALLOWABLE DAMAGED LIMITS IN ACCORDANCE WITH SRM 53-00-71 FIG. 101 DETAIL VII REV. 97. CORRODED CONNECTING ROD FITTING REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-40-02 REV. 97. FABRICATED REPLACEMENT FITTING AS PER DWG 213N1010 SHEET 1 REV. B. REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 CRITERIA.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FLOOR SUPPORT FOUND CORRODED AT STA 1451, RBL 64. STA 1451 TO STA 1461, RBL 64 FLOOR SUPPORT ANGLE REPAIR CARRIED OUT IN ACCORDANCE WITH EA F-5310-131065 AND SRM 51-70-12 REV. 97, FIG. 1, SHEET 5 DETAIL VI AND CARRIED OUT PART MARKED AS PER GMM 7-0-1001. REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: PRESSURE PANEL — DAMAGED (BS 1682) · airframe 52,447 hrs · 30,243 cycles

AT BS 1682, RBL 43, ELONGATED HOLE ON AFT PRESSURE DECK. REPAIR ON ELONGATED HOLES ON AFT PRESSURE DECK CARRIED OUT AS PER E. A. F-5300-128628. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: STAND OFF — CRACKED (BS 263) · airframe 52,447 hrs · 30,243 cycles

NLG WW : ELECTRICAL WIRE BUNDLE BRACKET IS GOUGED AND CRACKED AT STA 263, LBL 11.0 INCH BULKHEAD. DEFECTIVE BRACKET REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: ATTACH ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM CHORD ATTACHING SPLICE ANGLE HAS CORROSION AT STA 1003, LBL 8. EVALUATE AND RECTIFY. KEEL BEAM CHORD ATTACHING SPLICE ANGLE AT STA 1003, LBL 8 CORROSION BLENDED OUT AND FOUND EXCEEDED ALLOWABLE DAMAGE LIMITS IN ACCORDANCE WITH B757-200 SRM 53- 00-71 FIG. 101 DETAIL VIII REV. 97. CORRODED SPLICE ANGLE REMOVED AND REPLACED IN ACCORDANCE WITH B757-200 SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 CRITERIA.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

NR 2 CARGO DOOR THRESHOLD - CENTER SUPPORT BETWEEN NR 4 AND 5 SILL FITTING FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. NR 2 CARGO DOOR THRESHOLD CENTER SUPPORT REMOVED AND REPLACED IAW AMM 20-11-00 REV. 4. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: ATTACH ANGLE — CRACKED (ZONE 200) · airframe 52,447 hrs · 30,243 cycles

INTERCOSTAL FOUND CRACKED AT STA 1671, RBL 10. UPON INVESTIGATION FOUND ATTACH ANGLE CRACKED (CRACKED LENGTH 2 INCHES) CRACKED ATTACH ANGLE REMOVED IN ACCORDANCE WITH SRM 51-40-02 REV. 97. ATTACH ANGLE FABRICATED AS PER DWG 146N5191 SHT 1 REV. J. CLIP ANGLE INSTALLED IN ACCORDANCE WITH GMM 6-2-100 CRITERIA.

Part: SHIM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

WING-TO-BODY FAIRING AT STA 860, RBL 2.5 TO RBL 5.0 HAS ONE SHIM CORRODED AT LOWER FRAME. CORROSION ON SHIM FOUND EXCEEDED SRM LIMITS. SHIM REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: STRUCTURE — CORRODED (WING TO BODY) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

WING-TO-BODY FAIRING LOWER CHORD AT STA 900 HAS INTERGRANULAR CORROSION FROM RBL 33 TO LBL 22. CORROSION FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. REPLACED IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

NO.2 CARGO DOOR THRESHOLD MOST AFT NR 6 LOWER SILL FITTING P/N.69-45578-7 FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REFER SNRM N03199. NO.2 CARGO DOOR LOWER SILL NR 6 FITTING REMOVED AND REPLACED IAW AMM 20-11-00 REV. 04. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

NO.2 CARGO DOOR THRESHOLD NR 3 LOWER SILL SUPPORT FITTING FOUND EXCEED LIMIT AFTER CORROSION REMOVAL. REFER SNRM N03199. NR 2 CARGO DOOR LOWER SILL NR 3 SUPPORT FITING REMOVED AND REPLACED IAW AMM 20-11-00 REV. 04. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SUPPORT FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

NR 2 CARGO DOOR THRESHOLD, NR2 LOWER SILL SUPPORT FITTING FOUND EXCEED LIMIT AFTER CORROSION REMOVAL. REFER SNRM N03199. NR 2 CARGO DOOR LWR SILL NR 2 SUPPORT FITTING REMOVED AND REPLACED IAW AMM 20-11-00 REV 04. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

NO.2 CARGO DOOR THRESHOLD NR 4 LOWER SILL SUPPORT FITTING EXCEED LIMIT AFTER CORROSION REMOVAL. REFER SNRM N03199. NR 2 CARGO DOOR LOWER SILL NR 4 SUPPORT FITTING REMOVED AND REPLACED IAW AMM 20-11-00 REV.04. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SUPPORT FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

NO.2 CARGO DOOR THRESHOLD NR 5 LOWER SILL SUPPORT FITTING FOUND EXCEED LIMIT AFTER CORROSION REMOVAL. REFER SNRM N03199. NR 2 CARGO DOOR LOWER SILL NR 5 SUPPORT FITTING REMOVED AND REPLACED IAW AMM 20-11-00 REV. 04. REPAIR IS CLASSIFIED AS MNOR PER GMM 6-2-100 CRITERIA.

Part: SUPPORT FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

NO.2 CARGO DOOR THRESHOLD CENTER SUPPORT BETWEEN NR 2 AND 3 SILL FITTING FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. NO.2 CARGO DOOR THRESHOLD CENTER SUPPORT BETWEEN NR 2 AND 3 SILL FITTING REMOVED AND REPLACED IAW B757-200 AMM 20-11-00 REV.04. REPAIR IS CLASSIFIED AS MINOR PER GEMM 6-2-100 CRITERIA.

Part: SUPPORT FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

NR2 CARGO DOOR THRESHOLD NR3 LWR SILL SUPPORT FITTING FOUND EXCEED LIMIT AFTER CORROSION REMOVAL. REFER SNRM N03199. NR 2 CARGO DOOR LWR SILL NR 3 SUPPORT FITTING REMOVED AND REPLACED IAW AMM 20-11-00 REV.04. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1600, LBL 4 FLOORBEAM SUPPORT ANGLE CORRODED. FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. SUPPORT ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR GMM 6-2-100 CRITERIA.

Part: SUPPORT BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1400 STR 28R SUPPORT BEAM CORRODED. FOUND CORRODED BEYOND SRM ALLOWABLE DAMAGE LIMITS. REPAIR CARRIED OUT IAW EA F-5310-13076, REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 900, WL 208 FRAME BEHIND DOUBLER CORRODED ON RT SIDE OF FUSELAGE. REPAIR CARRIED OUT IAW R-5340-13106. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1400, LBL 4, INTERCOSTAL CORRODED. FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. INTERCOSTAL REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1520, STR 28R INTERCOSTAL CORRODED. CORROSION ON INTERCOSTAL FOUND EXCEEDED SRM REPAIRABLE LIMITS. INTERCOSTAL REMOVED AND REPLACED IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SKIN — DAMAGED (NR 1 SLAT) · airframe 52,447 hrs · 30,243 cycles

LT WING NR 1 SLAT INTERNAL SKIN AT OSS 809.46 AREA 3 RIVET HOLES CRACKED. REMOVED AND REPLACED BY FABRICATION AS PER DWG 114N40T5 SHEET 1 REV. A AND SRM 51-40-02 REV. 97. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 CRITERIA.

Part: SPAR — CORRODED (LT WING) · airframe 52,447 hrs · 30,243 cycles

EXFOLIATION CORROSION ON LT WING REAR SPAR WEB BETWEEN WS 150.5 TO WS 177.5 AT BOOST PUMP LWR MATING SURFACE. REPAIR CARRIED OUT ON LT WING REAR SPAR IAW EA F-5700-129607. REPAIR IS CLASSIFIED AS MINOR GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BULGING SKIN ON FUSELAGE SKIN BETWEEN STATION 1768 AND 1778, RBL 5 INCHES APPROX BULIGING SKIN BETWEEN STA 1768 AND 1778 FOUND EXFOLIATED. SKIN REPAIRED IAW EA F-5330-131073. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: MOUNT — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 199 WEATHER RADAR MOUNT AROUND MOUNT BOLTS CORRODED. CORROSION ON WEATHER RADAR MOUNT FOUND EXCEEDED SRM LIMITS. MOUNT REMOVED AND REPLACED IAW AMM 34-43-07 REV. 4. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RAM AIR - AIR CONDITIONING INLET LOWER SUPPORT STRUCTURE HS CORROSION AT STA 863, RBL 19.0". LWR SUPPORT FOUND CORRODED BEYOND SRM ALLOWABLE DAMAGE LIMITS. CHORD REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT — CORRODED (FAIRING) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

WING-TO-BODY FAIRING SUPPORT FRAME (ENTIRE FRAME) HAS CORROSION AT STA 900. CORROSION ON SUPPORT FRAME AT STA 900 FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. FRAME REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: WEB — CORRODED (FAIRING) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

WING-TO-BODY LOWER FAIRING; VERTICAL WEB AT STA 860, RBL 3.0 NR TO LBL 3.0 NR HAS INTERGRANULAR CORROSION. CORROSION ON VERTICAL WEB OF WING-TO-BODY LOWER FAIRING STRUCTURE AT STA 860 FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. WEB REMOVED AND REPLACED IAW SRM 51-40-02 REV 97.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

LT AIR COND - RAM AIR INLET ASSY LWR FWD WEDGE OTBD SUPPORT L ANGLE FOUND CORRODED. CORROSION ON L-ANGLE FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 760 STR 22L, SIDEWALL SUPPORT ANGLE CORRODED. REMOVED AND REPLACED IAW SRM51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 760 TO 840, LBL 24, CEILING SUPPORT CORRODED. CORROSION REMOVED AND FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. STRAP REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 560 TO 760, LBL 25 CEILING SUPPORT STRAP CORRODED. FOUND EXCEEDED SRM DAMAGE LIMITS. STRAP REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER G MM 6-2-100 CRTERIA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 700 STR 25R, SIDE WALL SUPPORT ANGLE CORRODED. SUPPORT ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 52,447 hrs · 30,243 cycles

FLOOR PANEL (PN 141N5369-12) FOUND DELAMINATED. REPLACE FLOOR PANEL. NEW FLOOR PANEL FABRICATED IAW PL 141N5369-12 (SHT 6, 15 & 28 OF 32) AND DWG (PG 28, 29.1, 46 & 49). FABRICATED FLOOR PANEL PART MARK AS FX-141N5369-12 IAW GMM 7-0-1001. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: RETAINER — CORRODED (RT WING) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT WING UPPER OTBD T/E UPPER PANEL SEAL RETAINER AT WS 652.5 TO WS 705.27 FOUND WITH CORROSION AS MARKED. EVALUATE AND RECTIFY. RT WING OTBD T/E UPPER PANEL SEAL RETAINER BETWEEN WS 652.5 TO WS 705.25 REMOVED AND REPLACED IAW SRM 51-10-02 REV. 96. SEAL RETAINER FABRICATED IAW DWG 113N1799 REV. B, PART MARKED AS FX 113N1799-30 IAW GMM 7-0-1001. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: RETAINER — CORRODED (RT WING) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT WING UPPER OTBD T/E UPPER PANEL SEAL RETAINER AT WS 775.45 TO WS 825.0 FOUND WITH CORROSION AS MARKED. EVALUATE AND RECTIFY. RT WING OTBD T/E UPPER PANEL SEAL RETAINER BETWEEN WS 775.45 TO WS 825.0. REMOVED AND REPLACED IAW SRM 51-10-02 REV. 96. SEAL RETAINER FABRICATED IAW DWG 113N1799, PART MARKED AS FX 113N1799-40 IAW GMM 7-0-1001. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 740 STR 22L TO 26L SIDEWALL SUPPORT ANGLE CORRODED. FOUND EXCEEDED SRM LIMITS. SUPPORT CHANNEL (ANGLE) REMOVED AND REPLACED IAW SRM51-40-02 REV/ 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: ATTACH ANGLE — CORRODED (KEELBEAM) · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM CHORD ATTACHING SPLICE ANGLE HAS A CORROSION AT STA 965, RBL 8. EVALUATE AND RECTIFY. KEEL BEAM CHORD ATTACHING SPLICE ANGLE AT STA 965, RBL 8 CORROSION BLENDED AND FOUND EXCEEDED ALLOWABLE DAMAGED LIMITS IAW SRM 53-00-71 FIG. 101 DETAIL VII REV. 97. CORRODED KEEL BEAM CHORD ATTACHING SPLICE ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: ATTACH ANGLE — CORRODED (KEELBEAM) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM CHORD ATTACHING SPLICE ANGLE HAS CORROSION AT STA 1003, RBL 8. EVALUATE AND RECTIFY. KEEL BEAM CHORD ATTACHING SPLICE ANGLE AT STA 1003, RBL 8 CORROSION BLENDED AND FOUND EXCEEDED ALLOWABLE DAMAGED LIMITS IAW SRM 53-00-71 FIG 101 DETAIL VII REV. 97. CORRODED KEEL BEAM ATTACHING SPLICE ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 680, STR 22R SIDEWALL SUPPORT ANGLE CORRODED. REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: ATTACH ANGLE — CORRODED (KEELBEAM) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM CHORD ATTACHING SPLICE ANGLE HAS A CORROSION AT STA 965, LBL 8 EVALUATE AND RECTIFY. KEEL BEAM CHORD ATTACHING SPLICE ANGLE AT STA 965, LBL 8 CORROSION BLENDED AND FOUND EXCEEDED ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-71, FIG. 101 DETAIL VII REV. 97. CORRODED KEEL BEAM CHORD ATTACHING SPLICE ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 760 TO BS 840, LBL 45, CEILING SUPPORT CORRODED. FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. SUPPORT REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FRAME — CORRODED (BS 310) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CORROSION FOUND ON FWD SIDE OF FRAME WEB STA 310.5 BETWEEN WL 206 AND 209 AT RBL 4 INCH AND BETWEEN LBL 16 INCH TO 19 INCH. REPAIRED IAW EA NR F-5310-131071 REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1460 RBL 22, CEILING SUPPORT STRAP SPLICE PLATE CORRODED. CORROSION ON STRAP SPLICE PLATE AT BS 1460, RB 22, FOUND OUT OF SRM ALLOWABLE DAMAGE LIMITS. SPLICE PLATE REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

STRAP AT STA 1885.2 FROM STR 25L TO STR 25R FOUND CORROSION DURING REMOVAL FOR ACCESS. EVALUATE AND RECTIFY. CORRODED STRAP AT STA 1885.20 FROM STR 25L TO STR 25R REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. NEW SKIN STRAP FABRICATED IAW DWG 148N6613, NEW STRAP PART MARKED AS FX 148N6613 IAW BAC 5307 REV. P AND GMM 7-0-1001. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT BRACKET — CORRODED (FAIRING) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

LT WING TOP WING TO BODY FAIRING SUPPORT BRACKET AT STA 940 WITH CORROSION. EVALUATE AND RECTIFY. RE-WORKS CORRODED AREA FOUND TO EXCEEDED ALLOWABLE LIMITS IAW SRM 51-00-71 REV. 97. MATERIALS REMOVED = 0.055 INCH, MATERIALS REMAINED = 0.025 INCH, MATERIALS THICKNESS = 0.080 INCH. NEW SUPPORT BRACKET FABRICATED IAW DWG 149N7210 SHT 1 REV. E. MATERIAL USING 7075-T0-0.080 INCH SUPPORT BRACKET HEAT TREATED TO T6 CONDITION IAW BAC 5602. PART MARK AS FX 149N721-57 IAW GMM 7-0-1001. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 740, STR 22R TO 26R, SIDEWALL SUPPORT ANGLE CORRODED. REMOVED AND REPLACED IAW SRM 51-40-02 REV/97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: RETAINER — CRACKED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

NR 2 CARGO DOOR CUTOUT LWR CTR SEAL RETAINER FOUND CRACKED AT RIVET HOLE. SEAL RETAINER REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: RETAINER — CORRODED (RT WING) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT WING UPPER OTBD T/E PANEL SEAL RETAINER AT WS 735.27 TO WS 775.45. FOUND WITH CORROSION AS MARKED. EVALUATE AND RECTIFY. RT WING OTBD T/E UPPER PANEL SEAL RETAINER BETWEEN WS 735.27 TO WS 775.45. REMOVED AND REPLACED IAW SRM 51-10-02 REV. 96. SEAL RETAINER FABRICATED IAW DWG 113N1799 REV. B, PART MARKED AS FX 113N1799-32 IAW GMM 7-0-1001. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 52,447 hrs · 30,243 cycles

FLOOR PANEL (PN 141N5369-15) FOUND DELAMINATED. REPLACED FLOOR PANEL. NEW FLOOR PANEL FABRICATED IAW PL 141N5369-15 (SHT 6, 7, 16 & 28 OF 32) AND DWG (SHT 3). FABRICATED FLOOR PANEL PART MARKED AS FX 141N5369-15 IAW GMM 7-0-1001. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 52,447 hrs · 30,243 cycles

FLOOR PANEL FOUND DELAMINATED. REPLACED FLOOR PANEL. FABRICATED IAW PL 141N5369-14 SHT 6, 15 & 28 OF 32 AND DRAWING (PG 32 & 33.1). REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2100 CRITERIA.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

STA 1180 TO STA 1200 LT AFT WING TO BODY FAIRING SUPPORT AT LBL 57.50 FOUND WITH CORROSION. EVALUATE AND RECTIFY. AFTER CORROSION REMOVAL IT WAS FOUND OUT THAT THE MATERIALS EXCEEDED THE ALLOWABLE LIMITS SET FORTH IAW SRM 53-00-71 REV. 97. MATERIAL REMOVED =0.040 INCH, MATERIAL REMAINED=0.023 INCH, MATERIAL THICKNESS=0.063 INCH. TYPICAL EXTRUDED SECTION REPAIR (FIGURE 1, SHEET 5 AND SHEET 6) CARRIED OUT IAW SRM 51-70-12 REV. 97, USING EXTRUSION PN (BAC1505-100403) 7075-T0-0.063 INCH, FABRICATED REPAIR PLATES (QTY 4 EACH) 7075-T0-00.040 INCH. EXTRUSION AND FABRICATED PLATES HEAT TREATED TO T6 CONDITION IAW BAC 5602. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM CHORD HAS INTERGRANULAR CORROSION AT STA 913, RBL 8.8 INCHES. EVALUATE AND RECTIFY. REPAIR CARRIED OUT IAW EA F-5430-126221 AND SRM 51-20-01 REV. 96. REMOVED CORROSION AND CLEANED IAW SRM 53-40-12 REV. 96, FIGURE 101 DETAIL IV AND SHOT PEEN THE RE-WORKED AREA IAW SRM 51-20-06. REV. 96.. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: FITTING — CORRODED (AC BAY) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT AIRCONDITIONING UPPER BAY SURFACE CONNECTING ROD FITTING HAS A CORROSION AT STA 959, RBL 42. EVALUATE AND RECTIFY. RT AIR CONDITIONING UPPER BAY CONNECTING ROD FITTING AT STA 959, RBL 42 CORROSION. BLENDED AND FOUND EXCEEDED ALLOWABLE DAMAGED LIMITS IAW SRM 53-00-71 FIG. 101 DETAIL VIII REV. 97. CORRODED CONNECTING ROD FITTING REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. FABRICATED REPLACEMENT FITTING IAW DWG 213N10010 SHEET 1 REV. B. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AFT ACCY COMPARTMENT DOOR CUTOUT FWD FRAME CORRODED BETWEEN LBL 10 TO RBL 10, STA 1883. EVALUATE AND RECTIFY. AFT ACCY COMPARTMENT DOOR CUTOUT FWD FRAME BETWEEN LBL 10 TO RBL 10, CORRODED FRAME REMOVED IAW SRM 51-40-02 REV. 97. NEW CHORD PN 148N3615-4 INSTALLED IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 52,447 hrs · 30,243 cycles

BRACKET FOUND CRACKED AT STA 1681, S-27L. EVALUATE AND REPAIR. BRACKET EVALUATED AND FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53 REV. 97. BRACKET FABRICATED IAW DWG 214N3058 SHT 1 REV. A. BRACKET IDENTIFIED AND MARK AS FX214N3058-4 IAW GMM 7-0-1001. REMOVED AND REPLACED BRACKET AT STA 1681, S-27L IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT KEEL BEAM CHORD HAS CORROSION FROM STA 1120 TO STA 1138, RBL 8.0" (FAIRING STRUCTURE) CORROSION ON KEEL BEAM CHORD FROM STA 1120 TO STA 1138, RBL 8, FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. KEEL BEAM CHORD REMOVED AND REPLACED IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 800 TO 820, RBL 4, INTERCOSTAL CORRODED. INTERCOSTAL ANGLE FOUND CORRODED THROUGH. ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 740 TO 760, LBL 16 INTERCOSTAL CORRODED. FABRICATED IAW DWG 143N5499, SHT 2, REV A. PART MARKED IAW GMM 7-0-1001 REV. 107. CORRODED INTERCOSTAL REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 740 TO 760, RBL 16 INTERCOSTAL CORRODED. AREA EVALUATED FOUND INTERCOSTAL WEB CORRODED. BS 740 TO BS 760, RBL 16 INTERCOSTAL WEB PN 143N5499-4 FABRICATED IAW DWG 143N5499 SHT 1, REV. INTERCOSTAL PART MARKED AS FX 143N5499-4 IAW GMM 7-0- 1001 REV 107. CORRODED INTERCOSTAL WEB REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,447 hrs · 30,243 cycles

BS 660 TO 680, RBL 20 INTERCOSTAL CRACKED. CRACKED INTERCOSTAL FROM BS 660 TO BS 680 REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 820 TO 839, RBL 12 INTERCOSTAL CORRODED. CORRODED INTERCOSTAL BETWEEN BS 820 AND BS 839 REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 680 TO 700, RBL 3, INTERCOSTAL CORRODED. INTERCOSTAL FROM BS 680 TO 700 FOUND CORRODED THROUGH. REMOVED AND REPLACED INTERCOSTAL IAW 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 640 TO 660, RBL 20 INTERCOSTAL CORRODED. FABRICATED IAW DWG 143N5367 SHT 3 REV A. PART MARKED IAW GMM 7-0-1001 REV 107. CORRODED INTERCOSTAL WEB REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 800 TO 820, LBL 8 INTERCOSTAL CORRODED. LWR ANGLE ON INTERCOSTAL FOUND CORRODED BEYOND SRM ALLOWABLE DAMAGE LIMITS. LWR ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 640 TO 660 RB 8, INTERCOSTAL CORRODED. REPAIRED INTERCOSTAL WEB. FABRICATED AS IAW DWG 143N5367 SHT 2 REV B. PART MARKED IAW GMM 7-0-1001 REV 107. CORRODED INTERCOSTAL WEB REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 670, RBL 20 DOUBLER ON INTERCOSTAL CORRODED. DOUBLER FOUND BADLY CORRODED. BS 670, RBL 20 DOUBLER ON INTERCOSTAL PN 143N5356-24 FABRICATED IAW DWG 143N5356 SHT 5 REV C. PART MARKED AS FX 143N5356-24 IAW GMM 7-0-1001. CORRODED DOUBLER REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. THIS REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 640 TO 660, LBL 8 INTERCOSTAL CORRODED. INTERCOSTAL FOUND BADLY CORRODED BEYOND SRM ALLOWABLE DAMAGE LIMITS. INTERCOSTAL REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 740 TO 760, RBL 12 INTERCOSTAL CORRODED. AREA EVALUATED FOUND INTERCOSTAL WEB AND CLIP CORRODED, BS 740 TO BS 760, RBL 12 INTERCOSTAL WEB PN 143N5498-4 AND CLIP PN 143N5496-2 FABRICATED IAW DWG 143N5498 SHT 2 REV D AND 143N5496 SHT 1 REV D, RESPECTIVELY. INTERCOSTAL WEB AND CLIP PART MARKED AS FX 143N5498-4 AND FX 143N5496-2 IAW GMM 7-0-1001 REV 107. CORRODED INTERCOSTAL WEB AND CLIP REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 720 TO 740, RBL 20 INTERCOSTAL CORRODED. INTERCOSTAL WEB FOUND BADLY CORRODED BEYOND SRM DAMAGE LIMITS. WEB BETWEEN BS 720 AND BS 740. REMOVED AND REPLACED IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 820 TO 839, LBL 20, INTERCOSTAL CORRODED. INTERCOSTAL WEB BETWEEN BS 820 AND BS 839 FOUND CORRODED BEYOND SRM REPAIR LIMITS. WEB REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 820 TO 839, LBL 16, INTERCOSTAL CORRODED. REPAIRED INTERCOSTAL. FABRICATED IAW DWG 143N5398 SHT 2 REV , 143N5345 SHT 1 REV C AND A43N5354 SHT 8 REV A. CORRODED INTERCOSTAL WEB, LWR ANGLE AND CLIP REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 800 TO 839, RBL 16, INTERCOSTAL CORRODED. INTERCOSTAL WEB BETWEEN BS 800 AND BS 839 FOUND BADLY CORRODED. WEB REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 680 TO 700, LBL 3, INTERCOSTAL CORRODED. INTERCOSTAL FROM BS 680 TO BS 700 FOUND CORRODED THROUGH. INTERCOSTAL REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 800 TO 820, RBL 8 INTERCOSTAL CORRODED. AREA EVALUATED FOUND INTERCOSTAL WEB, LWR CHORD AND CLIP CORRODED. BS 800 TO BS 820, RBL 8 INTERCOSTAL WEB CORROSION REMOVED AND TREATED IAW SRM 51-10-02 AND 51-20-01 REV 97. ORIGINAL THICKNESS 0.040 INCH, MATERIAL REMOVED 0.003 INCH, MATERIAL REMAINED 0.037 INCH FOUND WITHIN LIMIT IAW SRM 53-00-04 FIG 101, REV 97 LWR CHORD P/N 143N5345-16 AND CLIP PN 143N5354-72 FABRICATED IAW DWG 143N5345 SHT 1 REV C AND 143N4354 SHT 10 REV. PART MARKED AS FX 143N5345-16 AND FX 143N5354-72 IAW GMM 7-0-1001 REV 107. CORRODED LWR CHORD AND CLIP REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. THIS REPAIR IS CLASSIFIED AS MINOR AS IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 740 TO 760, LBL 12 INTERCOSTAL CORRODED. INTERCOSTA L WEB BETWEEN BS 740 AND BS 760 FOUND CORRODED BEYOND SRM DAMAGE LIMITS. WEB REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 640 TO 660, LBL 16, INTERCOSTAL CORRODED. CORROSION ON INTERCOSTAL FROM BS 640 TO BS 660 FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. INTERCOSTAL REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FAIRING — CRACKED (ZONE 500) · airframe 52,447 hrs · 30,243 cycles

LT INBD FLAP, OTBD TRACK FAIRING 572HB FWD FRAME FOUND CRACKED AS MARKED. LT, INBD FLAP, OTBD TRACK FAIRING 572HB CRACKED FWD FRAME REPAIRED IAW EA F- 5720--126231 TITLED: WING SECONDARY STRUCTURE - INBD FLAP FAIRING REPAIR. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FAIRING — CRACKED (TE FLAP) · airframe 52,447 hrs · 30,243 cycles

LT FLAP OPS MECHANISM FAIRING 571BB ANGLE STIFFENER FOUND CRACKED AS MARKED. CRACKED FAIRING NR 571BB STIFFENER REPAIRED IAW E.A. F-5710-126220 TITLED: LT MLG TRUNNION AFT FAIRING CRACK REPAIR IAW SB757-57-0029. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FITTING — CRACKED (NR 1 PYLON) · airframe 52,447 hrs · 30,243 cycles

INSIDE THE NR 1 PYLON RT SIDE HAS CRACKED ON THE TOP CORNER OF FITTING P/N 311N5220-56 AT PP STA 186. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96 AND DWG 311N5044 SHEET 5 REV. C. REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 CRITERIA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 52,447 hrs · 30,243 cycles

STA 1701, S-26L TO 27L BRACKET FOUND CRACKED. CRACKED BRACKET AT STA 1701, BETWEEN STR 26L AND 27L REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97.

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AFTER REMOVAL OF INTERCOSTAL BETWEEN STA 860 AND STA 900, BRACKET AT STA 860, FOUND WITH CORROSION LBL 7.0. CORROSION ON BRACKET FOUND EXCEEDED SRM DAMAGE LIMITS. INTERCOSTAL BRACKET AT STA 860 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: CHANNEL — CRACKED (ZONE 200) · airframe 52,447 hrs · 30,243 cycles

CABIN R2 DOOR SILL SUPPORT IS GOUGED (FIRST SUPPORT, FRONT TO BACK). R2 DOOR LOWER SILL CHANNEL FOUND GOUGED AND CRACKED. SILL SUPPORT CHANNEL REMOVED AND REPLACED IAW SRM 51-40-02 REV.96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1620, 27L TO 27R, FRAME CORRODED. CORROSION ON FRAME AT BS1620, 24L TO 24R FOUND EXCEEDED SRM DAMAGE LIMITS. FRAME REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: FITTING — CORRODED (AC BAY) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT AIR CONDITIONING UPPER BAY HAS CONNECTING ROD FITTING CORRODED AT STA 975, RBL 52.0". CORROSION ON FITTING FOUND EXCEEDED SRM LIMITS. CONNECTING ROD FITTING AT STA 975, RBL 52.0 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT BRACKET — DISLODGED (TE FLAP) · airframe 52,447 hrs · 30,243 cycles

RT INBD T/E FLAP, MAIN FLAP FAIRING PIN SUPPORT BRACKET AT MF STA 235 DISLODGED. REMOVED AND REPLACED AS PER SRM 51-40-02 REV. 97. CIC APPLICATION CARRIED OUT AS PER DWG B57-51-001. REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM INTERCOSTAL BETWEEN STA 860 AND STA 900 HAS INTERGRANULAR CORROSION AT LBL 7.0". CORROSION FOUND EXCEEDED SRM LIMITS. INTERCOSTAL WEB BETWEEN STA 680 AMD STA 900 AT LBL 7 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

STA 1715, LBL 39.50 INCH TO LBL 33.10 INCH, ANGLE CORRODED. ANGLE AT STA 1715, LBL 39.50 INCH TO LBL 33.10 INCH, REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: ANGLE — CRACKED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

AT STA 660 STR 26L FRAME INNER CHORD FASTENER HOLD CRACKED (ANGLE). REMOVED AND REPLACED CRACKED ANGLE IAW SRM 51-40-02 REV.96. REPAIR IS CLASSIFED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

NR 2 CARGO DOOR MOST FWD LOWER SILL FITTING FOUND CORROSION OUT OF LIMITS. NR 2 CARGO DOOR MOST FWD LOWER SILL FITTING REMOVED AND REPLACED IAW AMM 20-11-00 REV 4. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

PILOT SEAT TRACK (INBD FWD) HAS CORROSION UNDER THE BASE AND AROUND MOUNTING BOLT. PILOT INBD FWD SEAT TRACK REMOVED AND REPLACED IAW AMM 25-11-01 REV.4. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: WEB — CRACKED (ZONE 200) · airframe 52,447 hrs · 30,243 cycles

LOWER FLANGE ON MAIN CARGO DECK FLOOR WEB CRACKED AT STA 335, RBL 46 INCHES, AROUND IMPROPERLY BUCKED RIVET. CRACKED INTERCOSTAL AT STA 335, RBL 46 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

STA 1715, LBL 17 INCHES, ANGLE CORRODED. CORROSION FOUND OUT OF SRM DAMAGE LIMITS. ANGLE REPLACED IAW SRM 51-40-02 REV.96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: BRACKET — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

LINEAR ACCELEROMETER BRACKETS (QTY 02) CORRODED. CORROSION FOUND EXCEEDED SRM LIMITS. QTY 02 ACCELEROMETER BRACKETS REMOVED AND REPLACED IAW SRM 51-40-02 REV 96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CORRODED "L" ANGLE AT STA 1715, LBL 33.10 TO LBL 39.50, REMOVED AND REPLACED WITH A NEW "L" ANGLE IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR GMM 6-2-100 CRITERIA.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CORRODED "L" ANGLE FOUND AT STA 1715, LBL 9.2 TO LBL 15. EVALUATE AND REPAIR. CORRODED "L" ANGLE REMOVED AND REPLACED IAW SRM 51-40- 02 REV. 97. FABRICATE REPLACEMENT PART FOR 146N5240-20 IAW PL 146N5240 REV H AND DWG 146N5240 SH 1 REV. C. PART MARKED AS FX 146N5240-20 IAW GMM 7- 0-1001. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: BRACKET — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

WHILE WORKING ON SNRM N01290 FOUND LINEAR ACCELGROMETER BRACKETS CORRODED AT STA 1681, RBL 47.50, WL 208.10. EVALUATE AND REPAIR. ACCELGROMETER BRACKETS REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. REPLACEMENT BRACKETS FABRICATED FOR 284N1705-2 AND 284N1705-3 IAW PL 284N1705 AND DWG 284N1705 SHEET 01. PARTS IDENTIFIED IAW GMM 7-0-1001. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CORRODED "L" ANGLE FOUND AT STA 1715 TO 1720, RBL 51. EVALUATE AND REPAIR. CORRODED "L" ANGLE AT STA 1715 TO 1720, RBL 51 REMOVED AND REPLACED WITH NEW "L" ANGLE IAW SRM 51-40-02 REV. 97. FABRICATE REPLACEMENT PART FOR ANGLE 146N5300-22 IAW PL 146N5300 REV D AND DWG 146N5300 REV. A. PART MARKED IAW GMM 7-0-1-1001. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEELBEAM LWR CHORD FROM STA 1048 TO STA 1052, RBL 8 HAS CORROSION AROUND 5 RIVETS. EVALUATE AND RECTIFY. REPAIR CARRIED OUT IAW F-5350-129601, AND IAW SRM 51-00-06 AND 53-40-12 REV 96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: TEE FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEELBEAM LOWER TEE FITTING FOR FAIRING SUPPORT HAS CORROSION AT STA 955, BL0. CORROSION FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. REMOVED AND REPLACED KEELBEAM LOWER FITING IAW B757-200 SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

LT KEEL BEAM STIFFENER BRACKET FOUND CORRODED AT STA 967, LBL 8. EVALUATE AND REPAIR. CORRODED LT KEELBEAM STIFFENER BRACKET AT STA 967, LBL 8 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. STIFFENER BRACKET FABRICATED IAW PL 2171N6144 SHT. 2 OF 5 AND MFG DIMENSIONAL DWG SHT 1. PART MARKED IDENTIFIED AS FX 271N6144-2 IAW GMM 7-0-1001. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: BRACKET — DAMAGED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

RADOMED HOLDING ROD MOUNT LT SIDE ANGLE FOUND DAMAGED AT STA 199. EVALUATE AND REPAIR. DAMAGED RADOMED HOLDING ROD MOUNT LT SIDE ANGLE AT STA 199 REMOVED AND REPLACED IAW SRM 54-40-02 REV 97. ANGLE BRACKET FABRICATED IAW DWG 141N7835. PART IDENTIFIED AS FX 141N7835-2 IAW GMM 7-0-1001. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT MLG WHEEL WELL RT ACMP ASSY MOUNTING PLATE CORRODED AT SEVERAL PLACES. CORROSION FOUND EXCEEDED SRM DAMAGE LIMITS. REMOVED AND REPLACED RIGHT ACMP ASSY MOUNTING PLATE IAW AMM 20-11-00 REV.4. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: PANEL — CRACKED (ZONE 500) · airframe 52,447 hrs · 30,243 cycles

LT WING INBD T/E FIXED PANEL AT W STA 330, WIGGLE PLATE ASSY FOUND CRACKED. CRACKED PLATE REPLACED IAW SRM 51-40-02 REV 97 IAW DWG 113N1635. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SKIN — GOUGED (ZONE 200) · airframe 52,447 hrs · 30,243 cycles

CABIN INTERNAL FUSELAGE SKIN SURFACE AND INTERCOSTAL FLANGE SPLICE HAS A 1.5 INCHES GOUGE AT STA 393, BETWEEN STRINGERS S-13L AND S-14L. FUSELAGE SKIN SURFACE GOUGE MARK REMOVED IAW SRM 53- 00-01 AND FOUND WITHIN LIMIT. INTERCOSTAL FLANGE SPLICE AT STA 393, S-13L AND S-14L REMOVED AND REPLACED WITH NEW SHEAR TIE IAW DWG 141N1321 AND SRM 51-10-02 REV. 96. PART MARKED AS FX 141N1321-90 IAW GMM 7-0-1001. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: STRUCTURE — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 1664 L4 DOOR RAIN GUTTER CORRODED. CORROSION FOUND BEYOND SRM LIMITS. L4 DOOR RAIN GUTTER REPLACED IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT STA 780, LBL 51.0, WL 207.1, FOUND QTY 02 ELONGATED HOLES AND CORROSION ON FLOORBEAM UPPER FLANGE. ELONGATED HOLES AND CORROSION ON FLOORBEAM UPPER FLANGE AT STA 580, LBL 51.0, WL 207.1 REPAIRED IAW EA F-5310-129611. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: STRUCTURE — CORRODED (NR 2 PYLON) · airframe 52,447 hrs · 30,243 cycles

NR 2 PYLON PLATES AND RIVETS CORRODED ON LT AND RT SIDE OF THE PYLON FOR PANEL NR 441AL. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96 REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 CRITERIA.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1640, LBL 49, WL 208.10 CORROSION FOUND AROUND FASTENER HOLES UPPER FLOORBEAM CHORD LOWER SIDE. EVALUATE AND REPAIR. FLOORBEAM SUPPORT CHORD AT STA 1640, LBL 49, WL 208.10 REPAIRED IAW EA F5310-129615, FUSELAGE-MAIN FRAME CORROSION ON FLOORBEAM UPPER CHORD AT BS 1640, LBL44, REPAIR. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: CREASE BEAM — MISREPAIRED (ZONE 200) · airframe 52,447 hrs · 30,243 cycles

UNDOCUMENTED EXISTING REPAIR WAS FOUND ON CABIN RT CREASE BEAM FROM BS 780 TO BS 800, WL 208.10. FOUND NOT IAW STRUCTURAL REPAIR MANUAL. EA F-5300-128608, & EA F-5300-126218,

Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CORRODED COCKPIT ENTRY DOOR KICK PLATE AT STA 310, WL 208.10, LBL20 TO RBL 2. LH OUTBOARD ANCHOR NUT NOT INSTALLED. CORRODED KICKPLATE REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-40-02 REV. 96. KICK PLATE FABRICATED AS PER DWG 141N5810 SHT 15, REV. E AND PART MARK AS PER BAC 5307 AND GMM 7-0-1001. REPAIR IS CLASSIFED AS MINOR AS PER GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

LT KEELBEAM HAS CORROSION FROM STA 1100 TO STA 1120, LBL 8. KEELBEAMHAS NINE CORRODED NUT PLATES. EVALUATE AND RECTIFY. CORRODED LT KEELBEAM AT STA 1100 TO STA 1120, LBL 8 FOUND EXCEEDED. ALLOWABLE DAMAGE LIMITS. KEEL BEAM CHORD REMOVED AND REPLACED IAW DWG 144N8180 AND SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CORRODED KEEL BEAM CHORD AT STA 950, RBL 8 (FAIRING STRUCTURE). EVALUATE AND RECTIFY. CORRODED KEEL BEAM CHORD AT STA 950, RBL 8 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MINOR AS PE GMM 6-2-100 CRITERIA.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

NR 2 CARGO DOOR CUTOUT PRESSURE SEAL RETAINER FOUND CORROSION AT SEVERAL PLACES AS MARK. NUMBER 2 CARGO DOOR CUTOUT PRESSURE SEAL RETAINER AND ANGLE REMOVED AND REPLACED IN ACCORDANCE WITH DWG 146N6609 REV. J AND SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 CRITERIA.

Part: STRAP — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CORRODED AFT PRESSURE DECK STRAP FOUND AT BS 1680, BL0 TO RBL 15. EVALUATE AND REPAIR. CORRODED PRESSURE DECK STRAP AT BS 1680, BL0 TO RBL 15 REMOVED AND REPLACED IAW DWG 146N5184 AND SRM 51-40-02 REV. 96. PART MARK AS FX 146N5184-6 IAW GMM 7-0-1001. REPAIR CLASSIFIED AS MINOR GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CORRODED INTERCOSTAL AT STA 1610 TO STA 1620, LBL 4. INTERCOSTAL REMOVED AND REPLACED IAW DWG 146N5451-9 AND SRM 51-40-02 REV 96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CORRODED "L" ANGLE FOUND AT STA 1715, RBL 0 TO RBL 9.2. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. "L" ANGLE FABRICATED IAW DWG 146N5300 REV C AND PART MARKED IAW GMM 7-0-1001. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: TEE FITTING — CRACKED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

AFTER INSTALLATION OF LT MLG WW SUPPORT CHANNEL, ADJACENT TEE FITTING FOUND CRACKED. LT MLG WW TEE FITTING REMOVED AND REPLACED AS PER SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: TEE FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM TEE CHORD STRUCTURE HAS CORROSION AT STA 910, RBL 8. EVALUATE AND RECTIFY. KEEL BEAM TEE CHORD AT STA 910, RBL 8 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MINOR GMM 6-2-100 CRITERIA.

Part: ANGLE — CRACKED (ZONE 200) · airframe 52,447 hrs · 30,243 cycles

CRACKED WEB FOUND AT STA 1320 TO STA 1340, LBL 24.75, WL 207.10. TO REPLACE WEB ANGLE. REMOVED AND REPLACE WEB (P/N 140N2506-1) AND ANGLE (PN 140N2505-5) AT STA 1320 TO STA 1340, LBL 24.75, WL 207.10 IAW DWG 140N2506, DWG 140N2505, AND SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT BRACKET — CRACKED (ZONE 500) · airframe 52,447 hrs · 30,243 cycles

LT OTBD T/E MAIN FLAP PN 113N3003-13, SN CA-0206 OTBD CLOSURE RIB AREA AT WBL 561.0 AFT BRACKET WITH RIVET HOLE FOUND CRACKED. EVALUATE AND RECTIFY AS REQUIRED. LT OTBD T/E FLAP OTBD CLOSURE RIB AREA, WBL 561.0 AFT CRACK SUPPORT BRACKET REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. SUPPORT BRACKET FABRICATED IAW DWG 113N3370 REV. C AND PART MARKED AS FX 113N3370-9 IAW GMM 7-0-1001. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM FITTING HAS CORROSION AT STA 1037, BL 0, WL 133. EVALUATE AND RECTIFY. KEEL BEAM FITTING AT STA 1037, BL 0, WL 133 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CORRODED WEB ANGLE FOUND AT STA 1320 TO STA 1340, RBL 24.75, WL 207.10. TO REPLACE WEB ANGLE. REMOVED AND REPLACED WEB (P/N 140N2506-1) AND ANGLE (P/N 140N2505) AT STA 1320 TO STA 1340, RBL 24.75, WL 207.10 IAW DWG 140N2506, DWG 140N2505, AND SRM 51-40-02 REV 96. REPAIR IS CLASSIFIED AS MINOR GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1300 STR 21L TO 26L SIDEWALL SUPPORT ANGLE CORRODED. REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1460 STR 22L TO 26L SIDEWALL SUPPORT ANGLE CORRODED. FOUND CORRODED BEYOND SRM REPAIR LIMITS. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1560 STR 22L TO 27L SIDEWALL SUPPORT CORRODED. SIDEWALL SUPPORT CHANNEL AT BS 1560 FOUND BADLY CORRODED BEYOND SRM REPAIR LIMITS. SUPPORT CHANNEL REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 900 TO BS 1070, LBL 45, SEAT TRACK CORRODED. TRACK REMOVED AND REPAIRED IAW SRM 53-00-52 REV. 97. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 900 TO BS1070, LBL 24, SEAT TRACK CORRODED. FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. SEAT TRACK REMOVED AND REPLACED IAW SRM 53-00-52 REV.97. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1360 STR 22R TO 26R, SIDEWALL SUPPORT ANGLE CORRODED. REPLACEMENT PART FABRICATED IAW PL 453N1801 SHT 13 REV Y AND DWG NR 453N1801 SHT 2 REV. B. REPAIR IS CLASSIFIED AS MINOR AS IAW GMM G-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1300 STR 22L TO 26L, SIDEWALL SUPPORT ANGLE CORRODED. CORROSION ON SIDEWALL SUPPORT CHANNEL AT BS 1300 FOUND EXCEEDED SRM DAMAGE LIMITS. CHANNEL REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1300, STR 22R TO 26R SIDEWALL SUPPORT ANGLE CORRODED. REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1440 RBL 16, FLOOR SUPPORT ANGLE CORRODED. FOUND EXCEEDED SRM LIMITS. ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: HINGE — CORRODED (ZONE 800) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

PANEL 198 MR HAS 2 CORRODED BEARINGS FWD AND AFT CNT ON HINGES. CORROSION ON HINGE FITTING FOUND EXCEEDED LIMITS IN DWG 149N7723 REV. C. HINGE FITTING REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

WING-TO-BODY FAIRING SUPPORT FRAME AT STA 900, LBL0 TO LBL 22 HAS CORROSION IN SEVERAL PLACES. FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. SUPPORT FRAME REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

PANEL 149GL HAS CORROSION ON ATTACHED STIFFENER. CORROSION FOUND EXCEEDED SRM LIMITS. STIFFENER REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SKIN PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AROUND FUSELAGE DRAIN VALVE AT STATION 1663 BETWEEN STR 29L AND 29R HAS CORROSION AND HARDWARE CORRODED. CORRODED SKIN BLENDED, FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. REPAIR CARRIED OUT IAW EA F-5360-126233 (REPAIR DOUBLER AT BS 1661 TO BS 1681, S-29L TO S-29R. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM LOWER FITTING HAS CORROSION AT STA 1120, LBL 8.0 INCH TO RBL 8.0 INCH. CORROSION FOUND EXCEED SRM DAMAGE LIMITS. KEEL BEAM LOWER FITTING REPAIRED IAW E.A. F-5340-126238 AND B757 SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: BRACKET — CRACKED (W/B FAIRING) · airframe 52,447 hrs · 30,243 cycles

WING-TO-BODY FAIRING LOWER STRUCTURE AT STA 1060 RBL 10 INCHES ATTACHING BRACKET FOUND CRACKED AT FASTENER HOLE. CRACKED BRACKET REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT MLG WHEEL WELL RBL 8.0 MLG DOOR SEAL RETAINER SUPPORT AT STA 1064 CORRODED. FOUND EXCEEDED SRM LIMITS. DOOR SEAL RETAINER REMOVED AND REPLACED IAW AMM 20-11-00 REV.4. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM FITTING HAS CORROSION AT STA1037, LBL 7.0". CORROSION ON KEELBEAM FITTING FOUND EXCEEDED SRM DAMAGE LIMITS. FITING REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM FITTING AT STA 995 HAS INTERGRANULAR CORROSION AT BL 0 INCH. CORROSION FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. REMOVED AND REPLACED KEEL BEAM FITTING IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEELBEAM HAS CORROSION AT STA 1070, LBL 8.0 INCHES. FOUND EXCEEDED SRM DAMAGE LIMITS. SECTION REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

LT MLG WHEEL WELL LBL 8.0, MLG DOOR SEAL RETAINER SUPPORT AT STA 1120 CORRODED. FOUND EXCEEDED SRM REPAIRABLE LIMITS. SUPPORT REMOVED AND REPLACED IAW AMM 20-11-00 REV.04. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT MLG WHEEL WELL RBL 8.0 MLG DOOR SEAL RETAINER SUPPORT AT STA 1120 CORRODED. FOUND CORRODED BEYOND SRM ALLOWABLE DAMAGE LIMITS. SUPPORT REMOVED AND REPLACED IAW AMM 20-11-00 REV 4. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

LT MLG WHEEL WELL LBL 8.0, MLG DOOR SEAL RETAINER SUPPORT AT STA 1064 CORRODED. CORROSION ON DOOR SEAL RETAINER SUPPORT FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. SUPPORT REMOVED AND REPLACED IAW AMM 20-11-00 REV.04. REPAIR IS CLASSIFIED AS MINOR PERG GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CABIN : THREE FLOORBEAM INTERCOSTALS HAVE CORROSION FROM STA 680 TO STA 738, RBL 64.7. CORROSION ON 3 INTERCOSTALS REMOVED. FOUND ONE SUPPORT CORRODED BEYOND SRM REPAIRABLE LIMITS. SUPPORT REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (KEELBEAM) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM LOWER SUPPORT ANGLE FITTING HAS CORROSION AT STA 906, BL 0. FOUND EXCEEDED SRM DAMAGE LIMITS. SUPPORT ANGLE FITTING REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: CHANNEL — CRACKED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

RT MLG WHEEL WELL : UNDERWING FAIRING SUPPORT STRUCTURE CHANNEL HAS A 2.6250 INCH CRACK AT STA 1062.25, RBL 66.0". CRACK IS ABOVE FWD DOOR STOP FITTING. UNDERWING FAIRING SUPPORT CHANNEL REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96 AND IAW DWG 149N7553 REV.C. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

LT MLG WHEEL WELL LBL 8.0, MLG DOOR SEAL RETAINER SUPPORT AT STA 1100 CORRODED. FOUND EXCEEDED SRM DAMAGE LIMITS. SUPPORT REMOVED AND REPLACED IAW AMM 20-11-00 REV. 04. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT MLG WHEEL WELL RBL 8.0 MLG DOOR SEAL RETAINER SUPPORT AT STA 1140 CORRODED. FOUND EXCEEDED SRM DAMAGE LIMITS. SUPPORT REMOVED AND REPLACED IAW AMM 20-11-00 REV. 4. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

LT MLG WHEEL WELL LBL 8.0 MLG DOOR SEAL RETAINER SUPPORT AT STA 1140 CORRODED. FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. SUPPORT REMOVED AND REPLACED IAW AMM 20-11-00 REV.4. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEELBEAM ATTACHING SPLICE ANGLE HAS CORROSION AT STA 918, RBL 8 INCHES. CORROSION ON SPLICE ANGLE AT STA 918, RBL 8, FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. SPLICE ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR GMM 6-2-100 CRITERIA.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT MLG WHEEL WELL RBL 8.0 MLG DOOR SEAL RETAINER SUPPORT AT STA 1100 CORRODED. FOUND CORRODED BEYOND SRM ALLOWABLE DAMAGE LIMITS. DOOR RETAINER REMOVED AND REPLACED IAW AMM 20-11-00 REV.4. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT MLG WHEEL WELL LBL 8.0 MLG DOOR SEAL RETAINER SUPPORT AT STA 1073 CORRODED. FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. SUPPORT REMOVED AND REPLACED IAW 20-11-00 REV.4. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: CHANNEL — CRACKED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

LT MLG WHEEL WELL: UNDERWING FAIRING SUPPORT STRUCTURE CHANNEL HAS A ONE- INCH CRACK AT STA 1068.25, LBL 66.0". ABOVE FWD DOOR STOP FITTING. CRACKED CHANNEL REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

LT MLG WHEEL WELL LBL 8.0, MLG DOOR SEAL RETAINER SUPPORT AT STA 1073 CORRODED. FOUND EXCEEDED SRM DAMAGE LIMITS. SUPPORT REMOVED AND REPLACED IAW AMM 20-11-00 REV. 04. REPAIR IS CLASSIFIED AS MINOR PERG GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM CHORD HAS CORROSION AT STA 990, RBL 8 INCHES (FAIRING STRUCTURE) CORROSION FOUND EXCEEDED SRM DAMAGE LIMITS. REMOVED AND REPLACED KEEL BEAM CHORD IAW SRM 51-40-02 REV.97 REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: MOUNT — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT A/C BAY GROUND AIR CONNECTION LWR MOUNTING STRUCTURE HAS CORROSION AT STA 919, RBL 34.0 INCH TO RBL 43.0 INCH. CORRODED CHANNEL ON MOUNTING STRUCTURE AT STA 919 BLENDED OUT AND FOUND EXCEEDED SRM REPAIR LIMITS. CHANNEL REMOVED AND REPLACED IAW AMM 20-11- 00 REV. 4. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: TEE FITTING — CORRODED (BS 900-1040) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEELBEAM HAS INTERGRANULAR CORROSION FROM STA 900 TO STA 1040. FAIRING STRUCTURE. FOUND EXCEEDED SRM DAMAGE LIMITS. CHORD REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SUPPORT FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM ACCESS DOOR HOLD OPEN ROD SUPPORT FITTING AT BS1156, LBL 8 FOUND CORRODED. SUPPORT FITTING AT BS 1156 FOUND CORRODED BEYOND SRM REPAIRABLE LIMITS. SUPPORT FITTING REMOVED AND REPLACED IAW AMM 20-11-00 REV. 4. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

RT AIR CONDITIONG FWD BAY HAS 4 BRACE CORRODED BRACKETS AT STA 900, RBL 17 INCHES. CORROSION ON 2 BRACKETS FOUND EXCEEDED SRM LIMITS. REMOVED AND REPLACED BRACKETS IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

LT KEELBEAM LOWER FAIRING CORRODED FROM STA 1073 TO STA 1100, LBL 8.0 INCHES. CORROSION ON KEELBEAM LOWER CHORD FOUND EXCEEDED SRM DAMAGE LIMITS. CHORD REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CABIN FLOORBEAM INTERCOSTALS (3 EACH) HAVE CORROSION FROM STA 680 TO STA 738, LBL 64.7 INCHES. CORROSION FOUND EXCEEDED SRM DAMAGE LIMITS. REMOVED AND REPLACED INTERCOSTALS IAW SRM 51-10-02 REV.96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SKIN PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT AIRCON BAY UPPER SKIN SURFACE HAS CORROSION AT STA 918, RBL 36.0 INCHES. CORROSION AREA REPAIRED IAW EA F-5730-126239. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

AT BS 1560, STR 22R TO STR 27R, SIDEWALL SUPPORT ANGLE CORRODED. SUPPORT ANGLE FOUND BADLY DEFORMED AND CORRODED BEYOND SRM ALLOWABLE DAMAGE LIMITS. SUPPORT ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV.96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

STA 1715, RBL 17, L-ANGLE CORRODED. CORROSION ON L-ANGLE FOUND EXCEEDED SRM DAMAGE LIMITS. L-ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SKIN PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT AIRCON BAY UPPER SKIN SURFACE HAS CORROSION AT STA 918, RBL 36.0". REPAIRED IAW EA. NR F-5730-126239. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

MINOR CORROSION AT STA 879, WL 208.1, RBL 12.00 TO LBL 12.00 ON TOP SURFACE FLOORBEAM. REPAIR AT LBL 12 CARRIED OUT IAW SRM 53-00-51 REV 96 FIG 201 REPAIR 3. AT RBL 12, CORROSION REMOVED IAW SRM 51-10-02 REV 96, FOUND WITHIN LIMITS. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SUPPORT FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

WING-TO-BODY FAIRING LWR STRUCTURE SUPPORT FRAME HAS INTERGRANULAR CORROSION AT STA 839, RBL 28.0 INCHES. WING-TO-BODY FAIRING LWR STRUCTURE SUPPORT FRAME AT STA 839, RBL0 TO RBL 28.0 REPAIRED IAW SRM-200 SRM 51-70-11 FIG 1. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

LT AIRCOND BAY UPPER SKIN HAS CORROSION AT STA 967, LBL 10 INCH TO LBL 17.0 INCH CORROSION AREA REPAIRED IAW EA F-5710-126227. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: WEB — CORRODED (CARGO DOOR) · airframe 52,447 hrs · 30,243 cycles

CORROSION FOUND ON THE LOWER AFT DOOR WEB OF NUMBER 2 CARGO DOOR. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. WEB FABRICATED IAW DWG 146N6603 AND PART MARKED IAW GMM 7-0-1001. REPAIR IS CLASSIFIED MINOR IAW GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — DAMAGED (ZONE 100) · airframe 52,447 hrs · 30,243 cycles

ELONGATED HOLE FOUND ON FLOOR SUPPORT ANGLE AT BS 1279, LBL 65. EVALUATE AND REPAIR. FLOOR SUPPORT ANGLE REPAIR CARRIED OUT AT BS 1279, LBL 65 IN ACCORDANCE WITH B757-200 SRM 51-70-12 FIG 1 REV 96. PART MARKED ON REPAIR ANGLE AS FX 146N5590-58 IN ACCORDANCE WITH FEDEX GMM 7-0-1001. REPAIR CLASSIFIED AS MINOR PER FEDEX GMM 6-2-100 CRITERIA.

Part: ATTACH FITTING — CORRODED (ZONE 500) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

INTERGRANULAR CORROSION FOUND ON LT WING UPPER SURFACE AT AROUND LBBL 70.50, STRINGER U-14C. EVALUATE AND RECTIFY. REPAIR CARRIED OUT AS PER FEDEX EA F-5730-126219, TITLE: WINGS-PLATES AND SKINS, LEFT WING PLANK CORROSION AT WING ATTACH FITTING. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: ATTACH FITTING — CORRODED (ZONE 600) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

INTERGRANULAR CORROSION FOUND ON RT WING UPPER SURFACE SKIN AT AROUND RBBL 70.50, STRINGER U-23C. EVALUATE AND RECTIFY. REPAIR CARRIED OUT AS PER EA F-5730-126212, REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CORROSION FOUND AT FLOORBEAM TOP AND BOTTOM FLANGE, STA 1320, LBL 24.75, WL 207.10 AFTER SEAT TRACK HAS BEEN REMOVED. EVALUATE AND RECTIFY. EXISTING REPAIR OF FLOORBEAM UPPER TEE AT LBL 34 TO RBL 34, BS 1320 REMOVED AND REPAIRED IAW SRM 53-00-51 FIG. 201 REV. 96, FLOORBEAM UPPER TEE REPAIR AWAY FROM SEAT TRACK AND EA F-5310-129614 CARRIED OUT. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SKIN PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

LT AIR COND BAY UPPER SKIN HAS CORROSION AT STA 1000, LBL 10.0 INCHES TO LBL 24.0 INCHES. CORROSION AREA REPAIRED IAW EA F-5710-129608 (WINGS - BASIC WING STRUCTURE- CTR WING LT LWR SKIN PANEL, P/N. 111N4102, CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — DAMAGED (ZONE 200) · airframe 52,447 hrs · 30,243 cycles

DURING PTF MOD, FOUND FUSELAGE SKIN HAS DEEP SCRATCHES IN SEVERAL LOCATIONS AT BS 640 TO BS 900, STR 4R. REPAIRED IAW EA F-5300-128631A REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM LOWER CHORD HAS CORROSION FROM STA 1040 TO STA 1060, RBL 8.0 INCHES. CORROSION ON KEELBEAM LWR CHORD FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. CHORD REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM LOWER CHORD HAS CORROSION FROM STA 1040 TO STA 1060, LBL 8.0 INCHES. CORROSION ON KEEL BEAM CHORD FOUND EXCEED SRM ALLOWABLE DAMAGE LIMITS AFTER BLENDING. CHORD REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM6-2-100 CRITERIA.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM 90 DEGREE ANGLE HAS CORROSION AT STA 1140, LBL 8.0 INCH TO RBL 8.0 INCH. FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR GMM 6-2-100 CRITERIA.

Part: FAIRING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

WING-TO-BODY FAIRING LOWER STRUCTURE HAS CORROSION AT STA 1060, LBL 8.0 INCH TO RBL 8.0 INCH. CORROSION AREA BLENDED AND FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. REPAIR CARRIED OUT ON WING-TO-BODY FAIRING LOWER STRUCTURE IAW SRM 51-70-12 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT KEEL BEAM LOWER CHORD FROM STA 1073 TO STA 1100, RBL 8.0 INCH, HAS CORROSION. CORROSION ON RT KEELBEAM CHORD FROM STA 1073 TO STA 1100, RBL 8, FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS AFTER BLENDING. CHORD REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT KEEL BEAM CHORD HAS CORROSION FROM STA 1100 TO STA 1120, RBL 8.0 INCH. FOUND EXCEEDED SRM LIMITS. REMOVED AND REPLACED KEELBEAM IAW SRM 51-40-02 REV.96 AND DWG 144N8180. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT KEEL BEAM LOWER CHORD HAS CORROSION FROM STA 1060 TO STA 1073, RBL 8.0 INCH. CORROSION ON RT KEELBEAM LWR CHORD FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. CHORD REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (BS 1140-1168) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

RT KEELBEAM LOWER CHORD FROM STA 1140 TO STA 1168, RBL 8.0", HAS CORROSION. CORROSION ON RT KEELBEAM LOWER CHORD FROM STA 1140 TO STA 1168 FOUND EXCEEDED SRM LIMITS AFTER BLENDING. CHORD REMOVED AND REPLACED IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

LT KEEL BEAM STIFFENER HAS CORROSION AT STA 950, LBL 8.0 INCH. CORROSION ON KEELBEAM STIFFENER FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. STIFFENER REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

LT KEEL BEAM CHORD HAS CORROSION AT STA 1168, LBL 8.0 INCH. CORROSION ON LT KEELBEAM CHORD BLENDED AND FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. CHORD REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FAIRING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

WING-TO-BODY FAIRING LOWER STRUCTURE HAS CORROSION AT STA 1060, LBL 8.0 INCH TO RBL 8.0 INCH. REPAIR CARRIED OUT ON WING-TO-BODY FAIRING LWR STRUCTURE AT ST 1060 IAW SRM 51-70-12 FIG 1 DETAIL III REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM STIFFENER HAS INTERGRANULAR CORROSION AT STA 910, RBL 7.0 INCH. CORROSION ON KEEL BEAM STIFFENER AT STA 910, RBL7.0 FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. REMOVED AND REPLACED STIFFENER IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM STIFFENER HAS CORROSION AT STA 928, RBL 8.0 INCH. CORROSION ON KEELBEAM STIFFENER FOUND EXCEEDED SRM DAMAGE LIMITS. STIFFENER REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM6-2-100 CRITERIA.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEELBEAM STIFFENER HAS INTERGRANULAR CORROSION AT STA 918, RBL 7.0 INCH. CORROSION ON KEEL BEAM STIFFENER AT STA 918, RBL 7, FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. STIFFENER REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SKIN — DAMAGED (ZONE 200) · airframe 52,447 hrs · 30,243 cycles

DURING PTF MOD, FOUND FUSELAGE SKIN HAS DEEP SCRATCHES IN SEVERAL LOCATIONS AT STR 4L FROM BS 640 TO BS 900. FEDEX EA F-5330-126228, FUSELAGE PLATES AND SKINS, SCRATCH MARKS FOUND ON EXISTING SIDE SKIN BETWEEN STA 740 TO 780, S-4L, COMPLIED WITH. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

PILOT SEAT TRACK (INBD AFT) HAS CORROSION UNDER THE BASE AND AROUND THE MOUNTING BOLT. REPLACED INBD AFT PILOT SEAT TRACK IAW AMM AMM 25-11-01-02 REV.4 REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FIRST OFFICER SEAT TRACK (INBD AFT) HAS CORROSION UNDER THE BASE AND AROUND THE MOUNTING BOLT. FIRST OFFICER INBD AFT SEAT TRACK REPLACED IAW B757 AMM 25-11-01-2 REV.4. REPAIR IS CLASSIFIED MINOR PER GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (BS 780-879) · airframe 52,447 hrs · 30,243 cycles

SEAT TRACK FOUND CORRODED AT BS 780 TO BS 879, WL 208.10, LBL 24. REMOVED AND REPLACED WITH NEW SEAT TRACK IAW 143N5080 AND SRM 51-40-02 REV. 96 PART. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SHEAR TIE — CORRODED (BS 1200-1360) · airframe 52,447 hrs · 30,243 cycles

CEILING SHEAR STRAP FOUND CORRODED FROM BS 1200 TO BS 1360, RBL 24. REMOVED AND REPLACED IAW DWG 146N5180 AND SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SHEAR TIE — CORRODED (BS 1200-1360) · airframe 52,447 hrs · 30,243 cycles

CEILING SHEAR STRAP FOUND CORRODED FROM BS 1200 TO BS 1360, LBL 24. EVALUATE AND REPAIR. REMOVED AND REPLACED IAW DWG 143N5180 AND SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (BS 1180) · airframe 52,447 hrs · 30,243 cycles

SEAT TRACK HAS LIGHT SURFACE CORROSION SEVERAL PLACES AT STA 1180, WL 208.10, RBL 45.50. REMOVED AND REPLACED IAW DWG 144N5021 AND SRM 51-40-02 REV. 96. PART MARKED ON NEW SEAT TRACK AS 144N5021-2 IAW GMM 7-0-1001. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 780-879) · airframe 52,447 hrs · 30,243 cycles

SEAT TRACK FOUND CORRODED AT BS 780 TO BS 879, WL 208.10, LBL 45. EVALUATE AND REPAIR. SEAT TRACK REMOVED AND REPLACED IAW DWG 143N5080 AND SRM 51-40-02 REV. 96. PART MARKED ON NEW SEAT TRACK AS FX143N51061 IAW GMM 7-0-1001. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (BS 1080-1180) · airframe 52,447 hrs · 30,243 cycles

SEAT TRACK HAS LIGHT SURFACE CORROSION SEVERAL PLACES AT STA 1080 TO STA 1180, WL 208.10, LBL45.5. EVALUATE AND RECTIFY. SEAT TRACK REMOVED AND REPLACED IAW DWG 144N5021-2 AND SRM 51-40-02 REV. 96, PART MARKED ON NEW SEAT TRACK AS FX 144N5021-2 IAW GMM 7-0-1001. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (BS 1080-1180) · airframe 52,447 hrs · 30,243 cycles

SEAT TRACK HAS LIGHT SURFACE CORROSION SEVERAL PLACES AT STA 1080 TO STA 1180, WL 208.10, LBL 24.75, EVALUATE AND RECTIFY. SEAT TRACK REMOVED AND REPLACED IAW DWG 144N5021-2 AND SRM 51-40-02 REV. 96. PART MARKED ON NEW SEAT TRACK AS FX 144N5021-2 IAW GMM 7-0-1001. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (BS 1080-1180) · airframe 52,447 hrs · 30,243 cycles

SEAT TRACK HAS SEVERAL PLACES WITH LIGHT SURFACE CORROSION AT STA 1080 TO STA 1180, WL 208.10, RBL 24.75. EVALUATE AND RECTIFY. SEAT TRACK AT STA 1080 TO STA 1180, RBL 24.75, WL 208.10 REMOVED AND REPLACED IAW DWG 144N5021-2 AND SRM 51-40-02 REV. 96. PART MARKED ON NEW SEAT TRACK AS FX 144N5021-2 IAW GMM 7-0-1001. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: GATE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CABIN R4 PAX DOOR BOTTOM DOOR GATE HAS INTERGRANNULAR CORROSION. CORROSION FOUND EXCEEDED ALLOWABLE LIMITS IN SRM 51-10-02 FIG 101. REMOVED AND REPLACED DOOR GATE ASSY IAW AMM 52-11-38 REV 4. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: GATE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CABIN L4 PAX DOOR BOTTOM DOOR GATE HAS INTERGRANNULAR CORROSION. CABIN L4 PAX DOOR BOTTOM DOOR GATE CORROSION FOUND EXCEEDED ALLOWABLE DAMAGE LIMITS IAW SRM 52-10-02 FIG 101. GATE ASSY REMOVED AND REPLACED IAW 52-11-38 REV 4. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — FAILED (ZONE 200) · airframe 52,447 hrs · 30,243 cycles

EXISTING PATCH REPAIR FOUND ON CABIN FLOORBEAM UPPER TEE AT BS 324 BETWEEN RBL 13 AND RBL 70. EVALUATE AND REPAIR AS NECESSARY. EXISTING REPAIR EVALUATED IAW ATTACHMENT "B" OF EO F-5100-7-5001 PT.1 AND FOUND PREVIOUSLY ACCOMPLISHED BY NON-ROUTINE CARD SEQUENCE NR 589 IAW 53-00-51 REPAIR 3. REPAIR CARRIED OUT IAW EA F-5300-126222, REPAIR IS CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

BS 440 TO BS 640, RBL 24 SEAT TRACK CORRODED. FOUND OUT OF SRM LIMITS. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-10-02 REV/ 96. REPAIR IS CLASSIFIED AS MAJOR GMM 6-2-100 CRITERIA.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CORROSION FOUND ON FLOOR SUPPORT ANGLE FROM BS 1180 TO BS 1280, RBL 65. REMOVED AND REPLACED IAW DWG 143N5520 AND SRM 51-10-02 REV. 96. PART MARKED NEW SEAT TRACK IAW GMM 7-0-1001. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEELBEAM HAS CORROSION FROM STA 1033 TO STA 1036, RBL 8.0 INCH, LOWER FAIRING STRUCTURE. CORROSION ON KEELBEAM CHORD BLENDED AND FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. KEELBEAM CHORD REMOVED AND REPLACED IAW SRM 51-40-02, REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (BS 907) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM FITTING HAS CORROSION AT STA 907, RBL 4.0 INCH TO LBL 4.0 INCH FAIRING STRUCTURE. CORROSION ON KEEL BEAM FITTING AT STA 907, RBL 4.0 INCH TO LBL 4.0 INCH FOUND EXCEEDED SRM DAMAGE LIMITS. REMOVED AND REPLACED CHANNEL IAW SRM 51-40-02 REV.96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM CENTER CHORD HAS CORROSION AT STA 1020, BL 0 INCH. BLENDED AND FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. REPAIR CARRIED OUT IAW E.A. F-5350-126225. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM LOWER T FITTING FOR FAIRING SUPPORT HAS CORROSION AT STA 955, BL0. CORROSION ON TEE FITTING FOUND EXCEEDED SRM LIMITS. FITTING REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEELBEAM STIFFENER HAS INTERGRANNULAR CORROSION AT STA 950, RBL 8.0 INCH. BLENDED AND FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. STIFFENER REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEELBEAM LOWER LT CHORD HAS CORROSION AT STA 1003, LBL 8.0 INCH FAIRING STRUCTURE. FARING STRUCTURE LWR CHORD AT STA 1003, LBL 8 FOUND CORRODED BEYOND SRM REPAIRABLE LIMITS. CHORD REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FIRST OFFICER SEAT TRACK (OTBD FWD) HAS CORROSION UNDER THE BASE AND AROUND THE MOUNTING BOLT. FIRST OFFICER SEAT TRACK (OTBD FWD) REMOVED AND REPLACED IAW B757 AMM 25-11-01 REV 4. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM STIFFENER HAS INTERGRANNULAR CORROSION AT STA 910, LBL 8.0 INCH. CORROSION ON KEEL BEAM STIFFENER AT STA 910, LBL 8 INCH, BLENDED AND FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. STIFFENER REMOVED AND REPLACED SRM 51-40- 02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FIRST OFFICER SEAT TRACK (INBD FWD) HAS CORROSION UNDER THE BASE AND AROUND THE MOUNTING BOLT. FIRST OFFICER SEAT TRACK (INBD FWD) REMOVED AND REPLACED IAW AMM 25-11-01 REV 4. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FIRST OFFICER SEAT TRACK OUTBOARD AFT HAS CORROSION UNDER THE BASE AND AROUND THE MOUNTING BOLT. FIRST OFFICER SEAT TRACK REMOVED AND REPLACED IAW AMM 25-11-01 REV 4. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

PILOT SEAT TRACK (OUTBOARD FWD) HAS CORROSION UNDER THE BASE AND AROUND THE MOUNTING BOLT. PILOT SEAT TRACK (OUTBOARD FWD) REPLACED IAW AMM 25-11-01 REV 4. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

PILOT SEAT TRACK (OTBD AFT) HAS CORROSION UNDER THE BASE AND AROUND THE MOUNTING BOLT. PILOT SEAT TRACK (OTBD AFT) REMOVED AND REPLACED IAW AMM 25-11-01 REV 4. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

MAIN DECK CARGO HAS CORRODED SEAT TRACK AT STA 365 TO STA 377, WL 208.10, RBL 48 TO REPAIR AS REQUIRED, SEAT TRACK AT STA 365 TO STA 377, WL 208.10, RBL 48. REMOVED AND REPLACED IAW SRM 51-40-02 REV 96 AND DWG 141N5130. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

SKIN CORRODED AT STA 1677, LBL 1 INCH, BETWEEN STRINGERS 29L AND 29R. REPAIRED IAW SRM 53-00-01 REV. 96. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (NR 2 PYLON) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

NR 2 PYLON FORWARD SKIN LEFT SIDE CORRODED 3 INCH ABOVE LOWER EDGE OF PYLON PP STA 120 APPROX. FOUND EXCEEDED SRM LIMITS. REMOVED AND REPLACED INBD SKIN IAW SRM 51-10-02 AND SRM 51-40-02 REV.96. REPAIR IS CLASSIFIED AS MJOR IAW GMM 6-2-100 CRITERIA.

Part: SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

WING-TO-BODY FAIRING SPLICE SECTION HAS CORROSION AT STA 800 BL 0. CORROSION ON SPLICE SECTION AT STA 900 BL0, FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. SPLICE SECTION REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

STA 1640, AFT SIDE OF FRAME CORRODED BETWEEN STRINGER 26R AND 26L. CORROSION RUNNING INTO TRANSITION PANELS, U-CHANNELS AND VERTICAL SUPPORT STIFFENERS. REPLACED IAW SRM 51-40-02. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

FOUND STA 1661 FRAME CORRODED BETWEEN STRINGERS 28R AND 27L. CORROSION FOUND EXCEEDED SRM REPAIRABLE LIMITS. FRAME AT STA 1661 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CORROSION FOUND ON AFT PRESSURE DECK AREA FROM STA 1710 TO STA 1720, RBL 55 TO LBL 55. CORROSION ON PRESSURE DECK PLATE FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. DECK PLATE REPAIRED IAW EA F-5310-126215: FUSELAGE MAIN FRAME DECK PLATE REPAIR FROM BS 1681.8 TO 1720. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

KEEL BEAM HORIZONTAL WEB FITTING HAS INTERGRANULAR CORROSION FROM STA 900 TO STA 990, RBL 1.0 INCH. CORROSION BLENDED AND FOUND EXCEEDED SRM LIMITS. KEEL BEAM REPAIRED IAW SRM 53-40-12 REV. 96 AND EA F-5350-126232. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (NR 2 PYLON) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

NR 2 PYLON LT SIDE SKIN EXFOLIATED AROUND FASTENERS APPROX BETWEEN P/P STA 136 AND 140, AND 1 INCH ABOVE LWR SPAR. CORROSION ON NR 2 PYLON SKIN FOUND EXCEEDED ALLOWABLE DAMAGE LIMITS. PYLON SKIN REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MAJOR IAW 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CABIN ENTIRE SEAT TRACK HAS CORROSION, DAMAGE AND GOUGES FROM STA 1320 TO STA 1540, LBL 45.7. REMOVED AND INSTALLED NEW SEAT TRACK IAW 146N5219 AND SRM 51-40-02 REV. 96 AND IDENTIFIED AS FX 146N5219-1 IAW GMM 7-0-1001. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

SEAT TRACK HAS CORROSION DAMAGE AND GOUGES FROM STA 1180 TO STA 1280, LBL 24.5. CORROSION AND GOUGES ON SEAT TRACK FOUND EXCEEDED ALLOWABLE LIMITS IN SRM 53-00-52. SEAT TRACK REPLACED IAW SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

SEAT TRACK HAS CORROSION DAMAGE AND GOUGES FROM STA 1180 TO STA 1280, LBL45.7 INCH. FOUND EXCEEDED ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-52 FIG 101. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CABIN ENTIRE SEAT TRACK HAS CORROSION, DAMAGE AND GOUGES FROM STA 1320 TO STA 1540, RBL 45.7. REMOVED AND INSTALLED NEW SEAT TRACK IAW 146N5219 AND SRM 51-40-02 REV. 96 AND IDENTIFIED AS FX 146N5219-1 IAW GMM 7-0-1001. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CABIN ENTIRE SEAT TRACK HAS CORROSION DAMAGE AND GOUGES FROM STA 1180 TO STA 1280, RBL 45.7 INCH. CORROSION AND GOUGES ON SEAT TRACK FOUND EXCEEDED DAMAGE LIMITS IAW SRM 53-00-52 FIG.101. SEAT TRACK REPLACED IAW SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CABIN SEAT TRACK HAS CORROSION DAMAGE AND GOUGES BETWEEN STA 1320 AND STA 1540, RBL 24.5. SEAT TRACK CORROSION FOUND OUT OF SRM LIMITS. SEAT TRACK FROM STA 1320 TO STA 1540 REMOVED AND R EPLACED IAW SRM 51-10-02 REV.96. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CABIN SEAT TRACK HAS CORROSION DAMAGE AND GOUGES FROM STA 1180 TO STA 1280, RBL 24.5 INCH. CORROSION FOUND OUT OF SRM LIMITS. SEAT TRACK FROM STA 1180 TO STA 1280 REMOVED AND REPLACED IAW DWG 146N5218 AND SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SKIN PANEL — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

NR 1 PYLON HAS CORROSION AROUND VERTICAL FRAME ON INNER SKIN FWD AND AFT OF ACCESS HOLE PANEL 433HR. FOUND EXCEEDED SRM DAMAGE LIMITS. REMOVED AND REPLACED PYLON SKIN IAW SRM 51-40-02 REV 96. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SKIN PANEL — CORRODED (NR 2 PYLON) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

INSIDE PYLON NR 2 RT SIDE HAS CORROSION APPROX 8 INCHES FWD OF PANEL 443BR TO APPROX. 10 INCHES AFT OF PANEL 443BR. REPAIR AS REQUIRED. NR 2 PYLON OTBD SKIN REMOVED AND REPLACED IAW SRM 51-10-02 REV 96, SRM 51-40-02 REV 96, AND DWG 311N5002 SHT 13, REV E. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

STA 1661 FRAME CORRODED BETWEEN STRINGER 28R AND 27L.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CABIN, SEAT TRACK HAS CORROSION FROM STA 1540 TO STA 1640, RBL 45.50. CORROSION FOUND TO EXCEED DAMAGE LIMITS IAW SRM 53-00-52 FIG 101. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CABIN ENTIRE SEAT TRACK HAS CORROSION DAMAGE AND GOUGES BETWEEN STA 1320 AND STA 1540, LBL 24.5. CORROSION FOUND EXCEEDED SRM LIMITS. SEAT TRACK FROM STA 1320 TO STA 1540. REMOVED AND REPLACED IAW SRM 51-10-02 REV.96. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CABIN, SEAT TRACK HAS CORROSION FROM STA 1540 TO STA 1640, RBL 24.75. CORROSION ON SEAT TRACK FOUND EXCEEDED ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-52 FIG 101. SEAT TRACK REPLACED IAW SRM 51-40-02 REV.96. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CABIN, SEAT TRACK HAS CORROSION FROM STA 1540 TO STA 1640, LBL 45.50. CORROSION ON SEAT TRACK FOUND OUT OF SRM LIMITS. SEAT TRACK FROM STA 1540 TO STA 1640, LBL 45.50, WL 208.10, REMOVED AND REPLACED IAW DWN 146N530 AND B757-200 SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

CABIN, SEAT TRACK HAS CORROSION FROM STA 1540 TO STA 1640, LBL 24.75. CORROSION FOUND OUT OF LIMITS IAW SRM 53-00-52 FIG 101. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SKIN PANEL — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 52,447 hrs · 30,243 cycles

NR 1 PYLON HAS LIGHT CORROSION ON INNER SKIN FWD OF PANEL 433BL. REPAIR AS REQUIRED. NR 1 PYLON OTBD SKIN FROM PP STA 120.50 TO PP STA 209.50 REMOVED AND REPLACED IAW SRM 51-40-02 REV 96, AND DWG 311N5002 SHT 13, REV E. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,447 hrs · 30,243 cycles

FOUND CORRODED SEAT TRACK AT FS 365 TO FS 440, RBL 24. EVALUATE AND RECTIFY. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02 AND DWG 141N5130. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-02-100 CRITERIA.