N956FD

Part: LANYARD — OUT OF POSITION (L1 DOOR) · airframe 35,284 hrs · 21,416 cycles

DISARMING L1 DOOR. THE DOOR HANDLE REQUIRES EXTRA PRESSURE TO OPEN. OPENED L1 DOOR AND FOUND ESCAPE SLIDE STATIC LINE HANGING FROM BOTTOM OF DOOR AND INTERFERING WITH AND OBSTRUCTING DOOR SEAL CONTRIBUTING TO A PRESSURIZATION SQUEAL NOTED ON INBOUND PDIS AND INTERFERING WITH GIRT BAR ENGAGEMENT AND BOTTOM GATE OPERATION. PROPERLY STOWED ESCAPE SLIDE STATIC LINE PER AMM 25-66-01-4 AND INSPECTED L1 DOOR OPERATION PER AMM 52-11-00-6, OPS CHECKS GOOD. FORCE REQUIRED TO OPEN DOOR WELL WITHIN LIMITS PER AMM 52-11-00-6. OK FOR SERVICE.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 34,492 hrs · 20,829 cycles

MAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 333.45/362.25 AND RBL 17 DOT 09/47 REMOVED AND REPLACED SEAT TRACK BETWEEN STA. 333.45/362.25 RBL 17 IAW SRM 51-40-02, MAJOR REPAIR.

Part: LIMITER — TRIPPED (FLAP TRANSMISSIO) · airframe 34,121 hrs · 20,583 cycles

PDIS 956 27-50 6540 08OCT20 SAN FACT U. TRAILING EDGE FLAP DISAGREE ICAS ON APPROACH 170 KTS AIRSPEED ALTITUDE 2600 FEET. OCCURED WHEN MOVING FLAPS FROM 20 DEGREES TO 25 DEGREES. FLAP HANDLE AT 25 DEGREES FLAP INDICATOR MOVED FROM 20 DEGREES THEN STOPPED AT APPROX 21 DEGREES, IAW FIM 27-51-00-815-808. BITE CHECK ON FSCU 1 PRODUCED MESSAGE 305. INSPECTION FOUND RIGHT HAND OUTBOARD FLAP TRANSMISSION TORQUE LIMITER OVERLOAD INDICATOR POPPED. TRANSMISSION FLUID AND LUBE COMPLETE (INDICATOR RESET). RAN FLAPS UP AND DOWN 4 TIMES COMPLETE. TIMES COMPLETE TRANSITION FROM 20 DEGREES TO 25 DEGREES VERY SMOOTH, NEVER ANY FAULT LIGHT OR EICAS MESSAGES DURING CHECK. PER CONFERENCE CALL ALL MAINTENANCE ACTION ARE SUFFICIENT TO FACT THIS WRI, REF WRI 27-50-6542. OPENED ITEM PLACED ON OIL FOR CYCLED ROTATION INSPECTION.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,748 hrs · 20,296 cycles

EMERGENCY LIGHTS IN CTR COURER AREA, ABOVE R1 DOOR, AND R1DOOR EXTERIOR LIGHTS ARE INOP. AMM: 33-51-07-2 REMOVED AND REPLACED EMERGENCY PACK HOLDER ASSY REF B757 AMM 33-51-07-2. OPS CHECK GOOD.

Part: TRANSMISSION — CONTAMINATED (TE FLAP) · airframe 33,574 hrs · 20,175 cycles

TE FLAP DISAGREE ON APPCH WHEN LEVER MOVED TO FLAPS 1. COMPLIED WI/QRH AND LANDED FLAPS 20 USING APTN FLAPS. FLAP ISOLN VALVE STATUS MSG ON SHUTDOWN. NO RESTRICTION REF FIM 27-51-00-815-808. NR 5 FLAP TRANSMISSION OK TO CONTINUE PER EA F-2750-T0351488 COMPLIED WITH EA F-2750-T0351488 PART 1. TROUBLE SHOT REF FIM 27-51-00-815-808. FOUND NR 5 FLAP TRANSISSION OVERLOAD INDICATOR TRIPPED. FOUND WATER AT TORQUE LIMITER AND TORQUE TUBE AREA CONTAMINATED WITH WATER AND FROZEN. DISASSEMBLED AS REQUIRED AND CLEANED, LUBED AND SERVICED TRANSMISSION AND TORQUE LIMITER AS REQUIRED REF MM 27-51-06-4, SERVICED REF MM 12-21-09-3. OPS CHECKED SYSTEM AS REQUIRED REF MM 27-51-00-5. OPS CHECKED GOOD. VERIFIED AND INSPECTED ALL OTHER FLAP TRANSMISSIONS FOR PROPER SERVICING AND VERIFIED ALL OVERLOAD INDICATOR ARE NOT TRIPPED. REMOVED AND REPLACED NR 5 FLAP TRANSMISSION AND ATTACHING TORQUE TUBE IAW AMM 27-51-06-4. ASSEMBLY COMPLETE NEEDS OPS CK. ACCOMPLISHED OPS CK AND CHECKED ADJUSTMENT OF POSITION TRANSMITTER IAW AMM 27-51-06-4 AND 27-58-03. SYSTEM OPS CKS NORMAL.

Part: RELAY — MALFUNCTIONED (TE FLAPS SYS) · airframe 33,163 hrs · 19,893 cycles

DURING APPROCH, AT SELECTION OF FLAPS 1, RECEIVED TE FLAP DISAGREE EICAS MESSAGE AND TRAILING EDGE DISCREET LIGHT. RAN QRH PROCEDURE WITH NO IMPROVEMENT USING TRAILING EDGE ALTN FLAPS, LEADING TO TE FLAP ASYMETRY QRH. REMOVED AND REPLACED FLAP DEPRESSURIZATION RELAY IAW SWPM 20-15-46 THEN CYCLED FLAPS. NO DEFECTS NOTED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,628 hrs · 18,829 cycles

L1 DOOR EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACE THE NR 1 BATTERY PACK IAW MM 33-51-07-2. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,628 hrs · 18,829 cycles

L1 DOOR INTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK. OPS CHECKED GOOD.

Part: FLEX LINE — LEAKING (HYD SYSTEM) · airframe 31,420 hrs · 18,666 cycles

ON PUTTING THE GEAR DOWN, RECEIVED A GEAR DOORS MESSAGE. PERFORMED THE QRH AND LANDED. LEFT HYD SYSTEM LINE LEAKING.

Part: DOOR FRAME — CRACKED (R2) · airframe 31,288 hrs · 18,594 cycles

R2 DOOR FORWARD FRAME UPPER HINGE CUTOUT, EXISTING REPAIR ANGLE IS CRACKED IN 4 PLACES. VERIFIED BY HEFC INSPECTION. LOCATED AND DRILLED NEW REPAIR ANGLE IAW SRM 51-40-05-0G AND INSTALLED IAW SRM 52-10-02-2R.

Part: FLOORBEAM — CRACKED (BS 580) · airframe 31,288 hrs · 18,594 cycles

ON REMOVAL OF LOWER CARGO CEILING PANEL, FOUND THE FLOOR BEAM BS 580 LBL 45 CRACKED. LOCATED AND DRILLED A REPAIR IAW SRM 51-40-05, AND DWG 657N4311 REV -.

Part: DOOR — BINDING (L1) · airframe 30,765 hrs · 18,233 cycles

L1 DOOR WILL NOT CLOSE. RESET L1 DOOR & OPS CHECKED NORMAL IAW 757-200 & AMM 52-11-00-2.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 300 hrs · 17,747 cycles

R1 DOOR ESCAPE SLIDE ARMED LIGHT INOPERATIVE. R1 GIRT BAR ADJUSTED & ENGAGED IAW MM 25-66-01-4. ACFT OKAY TO CONTINUE.

Part: BOLT — LOOSE (R1 DOOR) · airframe 300 hrs · 17,746 cycles

ON WALK AROUND FOUND R1 DOOR SLIDE LIGHT NOT ILLUMINATED, WHEN DOOR IS PUT INTO THE ARM POSITION. DOOR SLIDES INOPERATIVE OR MISSING. NO JUMP SEATERS OR ACM'S ARE TO OCCUPY COURIER AREA IN FLIGHT. PERFORMED GIRT BAR & FLOOR FITTING INSPECTION IAW AMM 02-039. PERFORMED GIRT BAR MECHANISM ADJUSTMENT TEST IAW AMM 52-11-25 501. FOUND SEVERAL LOOSE BOLTS & A LOT OF FREE PLAY IN GIRT BAR LINKAGE. ALSO FLOOR PLATES WERE MISALIGNED. TIGHTENED LINKAGE & ADJUSTED FLOOR PLATES. OPERATES NORMAL IAW AMM 25-66-10. GOOD FOR SERVICE.

Part: LANYARD — UNSECURE (EVAC SLIDE) · airframe 299 hrs · 17,665 cycles

AFTER INBOUND FLIGHT, WHEN OPENING THE CAPTAIN SIDE CREW DOOR, NOTED A LANYARD & RING HANGING FROM THE BOTTOM OF THIS SLIDE COMPARTMENT. REMOVED LT DOOR SLIDE COVER, TO REINSTALL LANYARD & RING. FOUND NO DEFECT ON SLIDE & RE-INSTALLED LANYARD & RING & RE-INSTALLED SLIDE COVER IAW MM 25-66-01-4. ACFT OK TO CONTINUE.

Part: WINDOW — FAILED (COCKPIT) · airframe 297 hrs · 17,505 cycles

AT FL400, OBSERVED ARCING ON THE LT FWD WINDSHIELD & THEN IT SHATTERED. LT FWD WINDOW EICAS DISPLAYED & LT FWD WINDOW HEAT SHOWED INOPERATIVE. REMOVED NR 1 CAPTAIN`S WINDOW IAW MM 56-11-01-4. ALL OPS CHECKED NORMAL IAW MM 30-41-01-4. ACFT OK FOR SERVICE. WINDOW INSTALLATION COMPLETE IAW MM 56-11-01-4.

Part: SHEAR WEB — CORRODED (BS 395-440) · airframe 29,704 hrs · 17,477 cycles

MAIN CABIN SHEAR WEB IS CORRODED AT BS 395 - 440, LBL 24.75 TO LBL 45.5. REPAIRED IAW EA F-5310-T0315020 PT1.

Part: SHEAR WEB — CORRODED (BS 395-440) · corrosion level 2 · airframe 29,704 hrs · 17,477 cycles

MAIN CABIN SHEAR WEB IS CORRODED AT BS 395 - 440, BL 0 - LBL 24.75. REPAIRED IAW EA F-5310-T0315015 PT1.

Part: STRINGER — CRACKED (BS 1681) · airframe 297 hrs · 17,477 cycles

MAIN CABIN STRINGER 15L CRACKED AT BS 1681. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS, AND INSTALLED REPAIR PARTS ON STRINGER 15L AT B.S. 1681 IAW B757 SRM 53-00-02 REPAIR 2, 51-40-02 AND 51-20-01.

Part: ANGLE — CRACKED (R2 DOOR) · airframe 29,704 hrs · 17,477 cycles

R2 DOOR UPPER HINGE CUT OUT INNER ANGLE CRACKED. REPAIRED IAW EA F-5210-T0315194 PT1.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,689 hrs · 17,461 cycles

RIGHT EMER LIGHTING INOPERATIVE. R & R RT BATTERY PACK & OUTSIDE LIGHT BULB IAW AMM 33-51-07 33-51-00. OPERATIONS CHECKED GOOD.

Part: LATCH — LOOSE (EVAC SLIDE) · airframe 29,278 hrs · 17,169 cycles

LEFT FWD ENTRY DOOR VERY HARD TO CLOSE. LATCH ON SLIDE BROKEN. LATCH IS OK. FOUND ALL POTTED INSERTS PULLED OUT. REPOTTED INSERTS IAW CHAPTER 25 SMP. REACTIVATED L1 DOOR SLIDE & REINSTALLED SLIDE COVER IAW AMM. OPERATIONS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,240 hrs · 17,141 cycles

RIGHT ESCAPE SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW MM. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 29,045 hrs · 16,995 cycles

AT DEPARTURE CREW COULD NOT GET R1 DOOR SLIDE ARM LIGHT TO ILLUMINATE. RE LAMPED SLIDE ARM LIGHT IAW MM 33-51-06-2-1, OPERATIONS CHECKED NORMAL.

Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 29,027 hrs · 16,976 cycles

L1 DOOR WOULD NOT LATCH, SLIDE & WOULD NOT ARM. REMOVED ICE & DEBRIS FROM DOOR SILL & FOUND GIRT BAR WOULD NOT DISARM PROPERLY. DOOR NOW OPERATES CHECKED GOOD & SHOWS PROPER LOCKING & UNLOCKING INDICATION. CLEANED GIRT BAR, ATTACH POINT & LUBED. CYCLED DOOR CLOSED & ARMED SLIDE SEVERAL TIMES. NO DEFECTS NOTED, SLIDE ARMS & DISARMS NORMALLY.

Part: RESERVOIR — FAILED (R1 DOOR) · airframe 28,659 hrs · 16,711 cycles

R1 DOOR EMERGENCY POWER RESERVOIR DEFLATED WHILE OPENING DOOR AFTER IT GOT BOUND UP ATTEMPTING TO CLOSE IT. R & R R1 EMERGENCY POWER RESERVOIR CYLINDER IAW MM 52-11-33-4.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,368 hrs · 16,466 cycles

L1 DOOR SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP AND OPS TESTED GOOD IAW AMM 33-51-06-2-1.

Part: SEAL — LEAKING (WINDOW) · airframe 28,356 hrs · 16,455 cycles

R2 WINDOW LOWER RT CORNER HISSING SOUND (AIR LEAK) FROM 2.0 PSID-8.0. CHECKED F/O NR 2 WINDOW ADJUSTMENT. ALL WITHIN LIMITS. NO ADJUSTMENT NEEDED. REF MM 56-11-02-5. RESEALED AFT LOWER CORNER OF PRESSURE SEAL. REF MM 56-11-53-4. PRESSURIZED ACFT TO 5 PSID.

Part: KEELBEAM — GOUGED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE KEELBEAM EXTERNAL EXTENSION RT SIDE THE FASTENER HOLE AT BS1181 OTBD SIDE FOUND GOUGE MARK STA 1181 RT KEELBEAM EXTERNAL EXTENSION FASTENER HOLE WITH GOUGE MARK. REPLACED WITH NEW FABRICATED KEELBEAM EXTERNAL EXTENSION IAW DWG. NR 146N8838, SHT 1, REV A AND EA F-5310-155955, TITLE: FUSELAGE - KEELBEAM EXTENSION FABRICATION - MINOR ALTERATIONS FOR DEVIATION. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: KEELBEAM — GOUGED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE KEELBEAM EXTERNAL EXTENSION RT SIDE THE FASTENER HOLE AT BS 1182 OTBD SIDE FOUND GOUGED. STA 1182 RT KEELBEAM EXTERNAL EXTENSION FASTENER HOLE WITH GOUGE MARK. REPLACED WITH NEW FABRICATED KEELBEAM EXTERNAL EXTENSION IAW DWG NR 146N8838 SHT 1, REV A AND EA F-5310-155955,TITLE: FUSELAGE - KEELBEAM EXTENSION FABRICATION - MINOR ALTERATIONS FOR DEVIATION. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: KEELBEAM — DAMAGED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE KEELBEAM EXTERNAL EXTENSION RT SIDE THE HOLE AT BS 1182, INBD SIDE IS DAMAGED. STA 1182 RT KEELBEAM EXTERNAL EXTENSION FASTENER HOLE DAMAGED. REPLACED WITH NEW FABRICATED KEELBEAM EXTERNAL EXTENSION IAW DWG NR 146N8838, SHT 1, REV A WITH EA F-155955, TITLE: FUSELAGE - KEELBEAM EXTENSION FABRICATION - MINOR ALTERATIONS FOR DEVIATION. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: KEELBEAM — DAMAGED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE KEELBEAM EXTERNAL EXTENSION LT SIDE THE HOLE AT BS 1182 OTBD SIDE IS DAMAGED. STA 1182 LT KEELBEAM EXTERNAL EXTENSION FASTENER HOLE DAMAGED REPLACED WITH NEW FABRICATED KEELBEAM EXTERNAL EXTENSION IAW DWG NR 146N8838 SHT 1, REV A AND EA F-5310-155955, TITLE: FUSELAGE - KEELBEAM EXTENSION FABRICATION-MINOR ALTERATIONS FOR DEVIATION. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: KEELBEAM — GOUGED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE KEELBEAM EXTERNAL EXTENSION LT SIDE THE FASTENER HOLE AT BS 1200 INBD SIDE FOUND GOUGED. STA 1200 LT KEELBEAM EXTERNAL EXTENSION FASTENER HOLE WITH GOUGE MARK. REPLACED WITH NEW FABRICATED KEELBEAM EXTERNAL EXTENSION IAW DWG NR 146N8838 SHT 1, REV A AND EA F-5310-155955, TITLE: FUSELAGE - KEELBEAM EXTENSION FABRICATION - MINOR ALTERATIONS FOR DEVIATION. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: KEELBEAM — DAMAGED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE KEELBEAM EXTERNAL EXTENSION RT SIDE THE HOLE AT BS 1186 OTBD SIDE IS DAMAGED. STA 1186 RT KEELBEAM EXTERNAL EXTENSION FASTENER HOLE DAMAGED REPLACED WITH NEW FABRICATED KEELBEAM EXTERNAL EXTENSION IAW DWG NR 146N8838, SHT 1, REV A AND SEE EA F-5310-155955, TITLE: FUSELAGE - KEELBEAM EXTENSION FABRICATION - MINOR ALTERATIONS FOR DEVIATION. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: KEELBEAM — DAMAGED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE KEELBEAM EXTERNAL EXTENSION LT SIDE THE HOLE AT STA 1186 INBD SIDE IS DAMAGED. STA 1186 LT KEELBEAM EXTERNAL EXTENSION FASTENER HOLE DAMAGED REPLACED WITH NEW FABRICATED KEELBEAM EXTERNAL EXTENSION IAW DWG NR 146N8838, SHT 1, REV A AND EA F-5310-155955, TITLE: FUSELAGE - KEELBEAM EXTENSION FABRICARTION - MINOR ALTERATIONS FOR DEVIATION. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: KEELBEAM — GOUGED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE KEEL BEAM EXTERNAL EXTENSION LT SIDE THE FASTENER HOLE AT BS 1200 OTBD SIDE FOUND GOUGED. BS 1200 LT KEEL BEAM EXTERNAL EXTENSION FASTENER HOLE WITH GOUGE MARK. REPLACED WITH NEW FABRICATED KEEL BEAM EXTERNAL EXTENSION IAW DWG NR 146N8838, SHT 1, REV A AND EA F-5310-155955, TITLE: KEEL BEAM EXTENSION FABRICATIION - MINOR ALTERATIONS FOR DEVIATION. REPAIR CLASSIFIESD MAMJOR IAW GMM 6-2-100.

Part: KEELBEAM — DAMAGED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE KEELBEAM EXTERNAL EXTENSION LT SIDE THE HOLE AT BS 1181 OTBD SIDE IS DAMAGED. STA 1181 LT KEELBEAM EXTERNAL EXTENSION FASTENER HOLE DAMAGED REPLACED WITH NEW FABRICATED KEELBEAM EXTERNAL EXTENSION IAW DWG NR 146N8838 SHT 1, REV A AND EA F-5310-155955, TITLE: FUSELAGE - KEELBEAM EXTENSION FABRICATIOIN - MINOR ALTERATIONS FOR DEVIATION. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: KEELBEAM — GOUGED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE KEELBEAM EXTERNAL EXTENSION RT SIDE THE FASTENER HOLE AT BS 1200 OTBD SIDE FOUND GOUGED. STA 1220 RT KEELBEAM EXTERNAL EXTENSION FASTENER HOLE WITH GOUGE MARK. REPLACED WITH NEW FABRICATED KEELBEAM EXTERNAL EXTENSION IAW DWG NR 146N8838 SHT 1, REV A AND SEE EA F-5310-155955, TITLE: FUSELAGE - KEELBEAM EXTENSION FABRICATION - MINOR ALTERATIONS FOR DEVIATION. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: KEELBEAM — GOUGED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE KEELBEAM EXTERNAL EXTENSION RT SIDE THE FASTENER HOLE AT BS 1200 OTBD SIDE FOUND GOUGED. BS 1200 RT KEELBEAM EXTERNAL EXTENSION FASTENER HOLE WITH GOUGE MARK. REPLACED WITH NEW FABRICATED KEELBEAM EXTERNAL EXTENSION IAW DWG NR 146N8838, SHT 1, REV A AND EA F-5310-155955 , TITLE: FUSELAGE - KEELBEAM EXTENSION FABRICATION - MINOR ALTERATIONS FOR DEVIATION. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: KEELBEAM — DAMAGED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE KEELBEAM EXTERNAL EXTENSION LT SIDE THE HOLE AT BS 1182 INBD SIDE IS DAMAGED. STA 1182 LT KEELBEAM EXTERNAL EXTENSION FASTENER HOLE DAMAGED REPLACED WITH NEW FABRICATED KEELBEAM EXTERNAL EXTENSION IAW DWG NR 146N8838, SHT 1, REV A AND SEE EA F-5310-155955, TITLE: FUSELAGE-KEELBEAM EXTENSION FABRICATION - MINOR ALTERATIONS FOR DEVIATION. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: KEELBEAM — GOUGED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE KEELBEAM EXTERNAL EXTENSION RT SIDE THE FASTENER HOLE AT BS 1200 INBD SIDE FOUND GOUGED. STA 1200 RT KEELBEAM EXTERNAL EXTENSION FASTENER HOLE WITH GOUGE MARK. REPLACED WITH NEW FABRICATED KEELBEAM EXTERNAL EXTENSION IAW DWG NR 146N8838 SHT 1, REV A AND EA F-5310-155955, TITLE: FUSELAGE - KEELBEAM EXTENSION FABRICATION - MINOR ALTERATIONS FOR DEVIATION. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: KEELBEAM — GOUGED (BS 1181) · airframe 28,331 hrs · 16,449 cycles

KEELBEAM EXTERNAL EXTENSION LT SIDE THE FASTENER HOLE AT BS 1181 INBD SIDE FOUND GOUGED. R & R WITH NEW KEELBEAM EXTENSION. FABRICATED AND INSTALLED IAW DWG 146N8838, SHT 1, REV A, DWG 140N0841 AND EA F-5310-155955. REPAIR IS MAJOR.

Part: KEELBEAM — GOUGED (BS 1181) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE KEELBEAM EXTERNAL EXTENSION RT SIDE THE HOLE AT BS 1181 INBD SIDE FOUND GOUGED. KEELBEAM EXTERNAL EXTENSION R & R WITH NEW KEELBEAM FABRICATED AND INSTALLED IAW DWG 146N8838, SHT.1 REV A, DWG 140N0841 AND EA F-5310-155955. REPAIR IS MAJOR.

Part: SKIN — DAMAGED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE EXTERIOR SKIN LT SIDE THERE ARE NUMEROUS SCRATCHES ALONG THE PERIMETER OF THE WING TO BODY FAIRING PANEL AT BS 1320 -1340 FROM STR 24 -26L. SCRATCHES REMOVED FOUND WITHIN LIMITS IAW EA-5310-155959 PAGE 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,331 hrs · 16,449 cycles

FUSELAGE EXTERIOR SKIN LT SIDE THERE IS CORROSION AT BS 1380 - 1400 FROM STR 25 -26L. REPAIR CARRIED OUT EA F-5310-155959. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,331 hrs · 16,449 cycles

FUSELAGE EXTERIOR SKIN LT SIDE THERE IS CORROSION AT BS 1400-1420 FROM STR 25-26L. REPAIR CARRIED OUT IAW EA F-5310-155959. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,331 hrs · 16,449 cycles

FUSELAGE EXTERIOR SKIN LT SIDE THERE IS CORROSION AT BS 1360 - 1380 FROM STR 25 - 26L. REPAIR CARRIED OUT IAW EA F-5310-155959. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — SCRATCHED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE EXTERIOR SKIN THERE IS NUMEROUS SMALL SCRATCHES AND NICKS IN THE SKIN BETWEEN BS 1420 - 1440 AND STR 26L TO 26R. REPAIR CARRIED OUT IAW EA F-5310-155958. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,331 hrs · 16,449 cycles

FUSELAGE EXTERIOR SKIN LT SIDE THERE IS CORROSION AT BS 1340 -1360 FROM STR 25 - 26L. REPAIR CARRIED OUT IAW EA F-5310-155959. REPAIR CALSSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 780-783) · corrosion level 2 · airframe 28,331 hrs · 16,449 cycles

SEAT TRACK AT BS 780 TO 783, RBL 45.5 HAS CORROSION ON CROWN. REMOVED AND REPLACED WITH NEW SEAT TRACK FABRICATED AS PER DWG 143N5106 SHT.1 REV.A AND INSTALLED IAW DWG 143N5080 SHT.68 REV.A. REPAIR IS MAJOR.

Part: SKIN — DAMAGED (BS 1260-1280) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE EXTERIOR SKIN THERE IS NUMBEROUS SMALL SCRATCHES AND NICKS IN THE SKIN BETWEEN BS 1260 -1280 STR 26L- 26R. R & R WITH NEW SKIN IAW DWG 146N3300, SHT 15, REV A, SHT 16 REV -, SHT 17 REV B AND SHT 19 REV A. REPAIR CLASIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — DENTED (ZONE 200) · airframe 28,331 hrs · 16,449 cycles

CABIN BS 380 AREA INBD FLANGE ON STR 2 R OBSERVED WITH A DENT. REPAIRED IAW EA F-5310-155957. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 28,331 hrs · 16,449 cycles

HORIZONTAL STABILIZER RT SIDE THERE IS CORROSION ON THE EXTERIOR OF THE LOWER SKIN ALONG THE FUSELAGE FAIRING PANEL AT STAB STA 82. REMOVED AND REPAIR CARRIED OUT IAW EA F-5510-163817, PART 1. REPAIR IS CLASSIFIED MAJOR.

Part: SKIN — SCRATCHED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE EXTERIOR SKIN LT SIDE THERE ARE NUMBEROUS SCRATCHES ALONG THE PERIMETER OF THE WING TO BODY FARING PANEL AT BS 1320 -1300 FROM STR 26 - 27L. SCRATCHES ON EXTERIOR SKIN. R & R WITH NEW SKIN PN 146N3511-24, DWG 146N3300 SHT 15, REV A, SHT 16, REV -, SHT 17, REV B AND SHT 19, REV V, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE EXTERIOR SKIN THERE IS CORROSION ON THE SKIN AT BS 1240 BETWEEN STR 29L AND 29R. REMOVED AND REPLACED WITH NEW SKIN IAW DWG 146N3300 SHT 15, REV A, SHT 16 REV -AND SHT 17, REV B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE EXTERIOR SKIN THERE IS CORROSION ON THE SKIN AT BS 1260 BETWEEN STR 29L AND 29R. REMOVED AND REPLACED WITH NEW SKIN IAW DWG 146N3300 SHT 15, REV A, SHT 16 REV- AND SHT 17 REV B. REPAIR CLASSIFIED AS MAJOR IAW GMM6-2-100.

Part: FRAME — DENTED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

FWD CARGO COMP RT SIDE FRAME BS 660 HAS DENT ON TOP OF FRAME AT STRINGER 24R. REPAIRED IAW EA F-5310-155947, PART 1, REPAIR IS MAJOR.

Part: FRAME — CORRODED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

AFT CARGO BAY RIGHT SIDE FRAME BS 1360 HAS CORROSION BETWEEN STRINGERS 27 AND 25R. COMPLIED IAW EA F-5310-163135. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,331 hrs · 16,449 cycles

AFT CARGO BAY STRINGER 28R HAS CORROSION, BS 1438. R & R WITH NEW STRINGER FROM STA 1383 TO STA 1458 IAW DWG 146N3300, SHT 17 REV B. REPAIR IS MAJOR.

Part: FRAME — DENTED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

AFT CARGO BAY LT SIDE, FRAME BS 1400 HAS DENT ABOVE STRINGER 26L. COMPLIED IAW EA F-5310-155942, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — GOUGED (ZONE 300) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE SKIN GOUGED BETWEEN BS 199.09 - BS 205.59 AND WL 204.0. REPAIRED IAW STEPS B1 THROUGH C7 OF EA F-5330-163129.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,331 hrs · 16,449 cycles

AFT CARGO FRAME BS 1340 HAS CORROSION BETWEEN STRINGERS 27L AND 25L. REPAIRED IAW EA F-5310-163131 PART 1. REPAIR IS MINOR.

Part: SKIN — DAMAGED (ZONE 300) · airframe 28,331 hrs · 16,449 cycles

SKIN HAS NUMBEROUS SMALL SCRATCHES AND NICKS BETWEEN BS 1360 -1380 AND STR 26L -26R. SCRATCHES AND NICKS REMOVED IAW SRM 51-10-01, REV 107 AND FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL 11, REV 107. SKIN REMOVED AND REPLACED WITH NEW SKIN IAW DWG 146N3300, SHT 15, REV A, SHT 16 REV- AND SHT 17, REV B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — GOUGED (ZONE 300) · airframe 28,331 hrs · 16,449 cycles

SKIN GOUGED AT BS 199 -205 AT THE 10 O`CLOCK POSITION . REPAIRED IAW E.A.F-5330-163129 PART 1. REPAIR IS MAJOR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,331 hrs · 16,449 cycles

FLOOR SUPPORT AT BS 374 TO 380, LBL 60 HAS CORROSION. REMOVED AND REPLACED ANGLE FABRICATED AS PER DWG 141N8322 SHT.3 REV.G AND INSTALLED IAW DWG 141N8322 SHT.1 REV. K. REPAIR IS MAJOR.

Part: SKIN — DAMAGED (ZONE 300) · airframe 28,331 hrs · 16,449 cycles

THERE ARE NUMBEROUS SMALL SCRATCHES AND NICKS IN THE SKIN BETWEEN BS 1280 -1300 AND STR 26 L TO 26 R. NICKS AND SCRATCES REMOVED ON EXTERIOR SKIN IAW SRM 51-10-02, REV 107 AND FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL 11, REV 107, OUT OF LIMITS. SKIN REMOVED FROM STA 1180 -1401 STR 26L - 26R AND REPLACED WITH NEW SKIN PN 146N3511-24 IAW DWG 146N3300, SHT 15, REV A, SHT 16 REV -, SHT 17 REV B AND SHT 19 REV A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — DAMAGED (ZONE 300) · airframe 28,331 hrs · 16,449 cycles

SKIN HAS NUMEROUS SCRATCHES ALONG THE PERIMETER OF THE WING TO BODY FAIRING PANEL AT STA 1280 -1300 FROM STR 27-30R. REMOVED NUMEROUS SCRATCHES IAW SRM 51-10-02, REV 107 AND FOUND OUT LIMITS IAW SRM 53-00-01, FIG 101, DETAIL 11, REV 107. SKIN REMOVED AND REPLACED WITH NEW SKIN IAW DWG 146N3300 SHT 15, REV A, SHT 16, REV-, AND SHT 17, REV B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — CHAFED (ZONE 200) · airframe 28,331 hrs · 16,449 cycles

CABIN AT BS 1280 S10R, CHAFFED ON FRAME. REPAIRED IAW SRM 53-00-07 FIG.201 REPAIR 3 REV.106. REPAIR IS MAJOR.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,331 hrs · 16,449 cycles

CABIN CREASE BEAM HAS CORROSION AT BS 680 TO 740, LBL 60. REMOVED AND REPLACED IAW SRM 51-40-02 REV.106 AND DWG 143N832 SHT.5 REV.-. REPAIR IS MAJOR.

Part: STRINGER — MISREPAIRED (ZONE 200) · airframe 28,331 hrs · 16,449 cycles

STRINGER 16L AT BS 764 MISREPAIRED. REPAIRED IAW EA F-5310-163128, PART 1.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,331 hrs · 16,449 cycles

CABIN FLOORBEAM AT STA 270, LBL 60 TO LBL 43 HAS CORROSION ON UPPER TEE. FLOORBEAM REMOVED AND NEW FABRICATED IAW DWG 143N5504 SHT 3, REV A AND INSTALLED IAW DWG 143N5015, SHT 9, REV B. REPAIR IS MAJOR.

Part: FLOORBEAM — CORRODED (BS 720) · corrosion level 2 · airframe 28,331 hrs · 16,449 cycles

CABIN FLOORBEAM AT BS 720 HAS PREVIOUS CORROSION BLEND OUT WITH CORROSION INSIDE FASTENER HOLES AT LBL 40. R & R WITH NEW FLOORBEAM FABRICATED IAW DWG 143N5504 SHT 3 REV A AND INSTALLED IAW DWG 143N5015 SHT.9, REV B. REPAIR IS MAJOR.

Part: SKIN — SCRATCHED (ZONE 100) · airframe 28,331 hrs · 16,449 cycles

FUSELAGE SKIN HAS NUMEROUS SMALL SCRATCHES AND NICKS BETWEEN BS 1380 - 1400 AND STR 26 LEFT TO STR 26 RIGHT. SCRATCHES AND NICKS REMOVED IAW SRM 51-10-02, REV 107 AND FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL 11, REV 107. SKIN REMOVED AND REPLACED WITH NEW SKIN IAW DWG 146N3300, SHT 15 REV A, SHT 16 REV -, SHT 17 REV B AND SHT 19, REV A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRAP — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 28,331 hrs · 16,449 cycles

HORIZONTAL STABILIZER RT SIDE UPPER PIVOT STRAP HAS CORROSION. PIVOT STRAP REMOVED. NEW PIVOT STRAP FABRICATED IAW DWG 182N1607, SHT 1 REV A AND INSTALLED IAW DWG 182N1601 SHT 2 REV. REPAIR IS CLASSIFIED AS MAJOR.

Part: FRAME — CHAFED (ZONE 200) · airframe 28,331 hrs · 16,449 cycles

BS 1280, STR 11R, FRAME CHAFED. REPAIRED IAW SRM 53-00-07 FIG. 201 REPAIR 3 REV.106. REPAIR IS MAJOR.

Part: FRAME — CHAFED (BS 1280) · airframe 28,331 hrs · 16,449 cycles

BS 1280 FRAME CHAFED AT STR 14 L. REPAIRED IAW SRM 53-00-07 FIG.201 REPAIR 3 REV.106. REPAIR IS MAJOR.