N756AS

Part: FRAME — CRACKED (BS 360) · airframe 71,726 hrs · 41,569 cycles

RIGHT 360 FRAME IS CRACKED BETWEEN STR 13 AND 14 RT. ACFT GROUNDED. REPAIRED RT 360 FRAME BETWEEN STR 13 AND 14 RT IAW TASK CARD SB737-53A1399-400-4.

Part: SHEAR TIE — CRACKED (BS 360) · airframe 71,726 hrs · 41,569 cycles

SHEAR TIE AT BS 360 BETWEEN STR 13 AND 14R IS CRACKED. ACFT GROUNDED. NEW SHEAR TIE INSTALLED IAW SRM 51-40-05-0G-0, 51-40-02-0G-0 .

Part: FRAME — CRACKED (BS 360) · airframe 71,726 hrs · 41,569 cycles

RT 360, FRAME IS CRACKED BETWEEN STR 13 AND 14 RT. ACFT GROUNDED. REPAIRED RT 360 FRAME BETWEEN STR 13 AND 14 RT IAW TASK CARD SB737-53A1339-400-4. NOTE: RESUBMITTING 2/2/2016-AAR FOUND ERROR IN SB.

Part: BEAR STRAP — CRACKED (BS 949-969) · airframe 71,726 hrs · 41,569 cycles

L2 DOOR CUTOUT LOWER FWD CORNER CRACKED IN BEARSTRAP. ACFT GROUNDED. REPAIRED BEARSTRAP IAW SRM 53-00-01-2R-32, REPAIR 32.

Part: DOOR — LACK OF LUBE (L1) · airframe 70,818 hrs · 40,968 cycles

L1 DOOR VERY STIFF TO CLOSED. ACFT GROUNDED. PERFORMED OPS CHECK OF DOOR. FOUND NO DEFECT. LUBED PINS AND GUIDE AS PRECAUTIONARY. ACFT OK FOR SERVICE, REF AMM 52-11-00 AND AMM 52-11-11.

Part: DOOR — LACK OF LUBE (L1) · airframe 70,117 hrs · 40,526 cycles

FWD, PASSENGER DOOR, L-1, DIFFICULT TO CLOSE. ACFT GROUNDED. ACCOMPLISHED FWD ENTRY DOOR TEST. DOOR FAILED STEP 5, D. REQUIRED MORE THAN 600 IN.-LBS TO CLOSE. LUBRICATED LATCH ROLLERS, LATCH CAMS, GUIDE ARM HINGE AND CAM PLATE. PERFORMED DOOR CLOSING TORQUE TEST IAW AMM 52-11-00-755-051, STEP 5, D. TORQUE TEST GOOD AND WITHIN SERVICEABLE LIMITS. L-1 DOOR HAS NO HISTORY.

Part: SEAL DEPRESSOR — CRACKED (BS 956) · airframe 69,090 hrs · 39,928 cycles

THE R2 DOORWAY CUTOUT THE FWD SEAL DEPRESSOR FITTING ABOVE THE UPPER HINGE CUTOUT WAS FOUND CRACKED. ACFT GROUNDED. R & R THE K2 DOOR FWD UPPER HINGE DEPRESSOR FITTING IAW SRM 51-40-02-0G-0.

Part: SEAL DEPRESSOR — CRACKED (BS 956) · airframe 69,087 hrs · 39,927 cycles

L2 DOOR FWD LOWER HINGE SEAL DEPRESSOR IS CRACKED. ACFT GROUNDED. R & R THE DEPRESSOR IAW SRM 51-40-02-0G-0, PAR 4 A-D 7.

Part: SEAL DEPRESSOR — CRACKED (BS 296) · airframe 69,087 hrs · 39,927 cycles

R1 DOOR FWD FRAME UPPER HINGE SEAL DEPRESSOR IS CRACKED. ACFT GROUNDED. R & R THE SEAL DEPRESSOR IAW SRM 51-40-02-0G-0.

Part: ATTACH ANGLE — CRACKED (BS 348) · airframe 68,707 hrs · 39,705 cycles

FRAME BS 348.2 ATTACH ANGLE IS BROKE OFF AT LOWER ATTACH HOLE ABOVE STR 17L. ACFT GROUNDED. REPAIRED THE FRAME ATTACH ANGLE IAW T/C AD20120205, 400-53-2.

Part: FRAME — CRACKED (BS 348) · airframe 68,707 hrs · 39,705 cycles

FRAME BS 348.2 ANGLE IS BROKEN OFF AT LOWER ATTACH HOLE ABOVE STRINGER 17L. ACFT GROUNDED. REPAIRED FRAME ANGLE IAW T/C AD20120205.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 68,707 hrs · 39,705 cycles

RIGHT WING OTBD FOREFLAP INBD L/E IS CHAFED ON REPAIR. ACFT GROUNDED. REPAIRED RT WING OTBD FOREFLAP IAW SRM 57-3-01-2R-1, FIG 201.

Part: DOOR — LACK OF LUBE (L1) · airframe 68,049 hrs · 39,314 cycles

F/A & GATE AGENT REPORT FWD ENTRY DOOR DIFFICULT TO CLOSE WHILE MAKING GRINDING SOUND WHEN OPERATING. ACFT GROUNDED. DOOR OPERATION IS ROUGH AND VERY NOISY, HEAVY GRINDING NOISE COMING FROM UPPER HINGE AREA AND TORQUE TUBE PANEL. ACCOMPLISHED LUBRICATION OF GUIDE ARM ROLLER PIN AND HINGE GUIDE PLATES. REF MM TASK 12-25-21-603-001. ALSO ACCOMPLISHED FWD ENTRY DOOR TEST. OPS CHECKED GOOD IAW MM TASK 52-11-00-755-051. NO ADJUSTMENTS REQUIRED OR MADE.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 67,429 hrs · 38,960 cycles

FOUND A CRACK ON RT LOWER SKIN AT AFT SPAR AT SS 150.0. ACFT GROUNDED. REPAIR ACCOMPLISHED IAW EA 400-55EA-12482, REV NEW.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 67,429 hrs · 38,960 cycles

SKIN CRACKED AT LOWER SIDE OF RT STAB AT AFT SPAR AT APPROXIMATELY STABILIZER STA 129.0. ACFT GROUNDED. VERIFIED CRACK HFEC IAW BNDT 51-00.00 PART 6, FIG 23, 16050. REPAIR ACCOMPLISHED REF EA 400-55EA-12482, REV NEW.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 66,984 hrs · 38,718 cycles

EXIT SIGN LIGHT LENS FROM FWD ENTRANCE IS BROKEN. ACFT GROUNDED. REPLACED LENS. OPS NORMAL.

Part: DOOR — LACK OF LUBE (L1) · airframe 66,764 hrs · 38,569 cycles

F/A REPORTS L1 DOOR VERY DIFFCUT TO LATCH CLOSED. ACFT GROUNDED. LUBED L1 DOOR, REF 12-25-21. PERFORMED FORWARD ENTRY DOOR TEST AMM REF 25-11-00. GVI PERFORMED AND DOOR FOUND SERVICEABLE. DOOR TORQUE TEST PERFORMED AND CHECK GOOD. AMM REF 25-11-00, DOOR GOOD FOR CONTINUED SERVICE. NO HISTORY LAST 90 DAYS

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 66,470 hrs · 38,411 cycles

EMERGENCY EXIT SIGN OVER ROWS 16-17, ACFT RT, FELL OFF AND IS TAPED IN PLACE, APPEARS TO BE MISSING A SCREW. ACFT GROUNDED. RE-INSTALLED EMERG. EXIT SIGN COVER ACFT RT ROWS 16 & 17.

Part: LENS — DISLODGED (EMERGENCY LIGHTS) · airframe 66,379 hrs · 38,362 cycles

AIRCRAFT RT EXIT SIGN FELL OFF. AIRCRAFT GROUNDED. REINSTALLED SIGN RT OVERWING EMERGENCY EXIT.

Part: SIGN — UNSECURE (CABIN) · airframe 65,539 hrs · 37,833 cycles

EXIT SIGN NEXT TO L2 IS FALLING OFF. ACFT GROUNDED. INSTALLED L2 EXIT EXIT SIGN.

Part: ATTACH ANGLE — CRACKED (BS 338-344) · airframe 65,323 hrs · 37,698 cycles

FOUND L1 DOOR AFT SCUFF PLATE AFT ATTACHED ANGLE TO THE SKIN IS CRACKED. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SCUFF PLATE AFT ATTACHED ANGLE ON L1 DOOR IAW SRM 51-40-02-0G-0, FIG 8, SRM 51-40-05-0G AND 0 FIG 2, SHEET 1 AND SRM 51 40-02-0G-0, PAR 4 B.

Part: ATTACH ANGLE — CRACKED (BS 334-338) · airframe 65,323 hrs · 37,698 cycles

FOUND L1 DOOR AFT SCUFF PLATE AFT ATTACHED ANGLE TO THE SKIN IS CRACKED. ACFT GROUNDED. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SCUFF PLATE AFT ATTACHED ANGLE AT L1 DOOR IAW SRM 51-40-02-0G-0, FIG 8, SRM 51-40-05-0G-0, FIG 2, SHEET 1, AND SRM 51-40-02-0G-0, PARA 4(B).

Part: RETAINER — CRACKED (L1 DOOR) · airframe 65,323 hrs · 37,698 cycles

FORWARD L1 DOOR LOWER AFT CORNER OF LINER SUPPORT RETAINER IS CRACKED IN RADIUS. ACFT GROUNDED. R & R LINER SUPPORT IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 520) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

FWD CARGO COMPARTMENT SHEAR TIE CORRODED FS 520, S28L-28R. REMOVED, FABRICATED LOCATED, DRILLED AND INSTALLED SHEAR TIE IN FWD CARGO COMPARTMENT AT STA 520 BETWEEN STR 28L AND 28R IAW SRM 51-40-02-0G-0, FIG 8, SHEET 1, SRM 51-40-05-0G-0, FIG 2 AND SRM 51-40-02-0G-0 PARA 4.B.

Part: SKIN — DENTED (BS 320) · airframe 65,323 hrs · 37,698 cycles

SMALL DENT BELOW L1 DOOR. ACFT GROUNDED. REPAIRED SKIN IAW EA 400- 53EA-10542 REV NEW.

Part: SUPPORT ANGLE — CRACKED (RT NACELLE) · airframe 65,323 hrs · 37,698 cycles

RT PYLON OTBD SUPPORT ANGLE, STA 278 CRACKED. ACFT GROUNDED. FABRICATED NEW SUPPORT ANGLE.

Part: SHEAR TIE — CORRODED (BS 986) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

SHEAR TIE CORRODED AT BS 986 BETWEEN STR 27L AND 27R. ACFT GROUNDED. BLENDED CORRODED AREA, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A1, FIG 101, DETAIL II, R & R SHEAR TIE IAW SRM 51-40-02-0G 0.

Part: SHROUD — CHAFED (BS 1095) · airframe 65,323 hrs · 37,698 cycles

APU UPPER SHROUD INTERIOR CHAFED. ACFT GROUNDED. REPAIRED APU UPPER SHROUD INTERIOR SKIN IAW ASA EA 400-49EA-10647.

Part: FLOOR SUPPORT — DAMAGED (BS 312) · airframe 65,323 hrs · 37,698 cycles

INTERCOSTAL AT BL 0 AND BS 312 HAS A DAMAGED HOLE IN UPPER FLANGE (FOUND WHILE DOING 312 TEE CHORD REPAIR) ACFT GROUNDED. REMOVED DAMAGED UPPER TEE OF FLOOR SUPPORT. FABRICATED, TREATED, PRIMED, TOPCOATED AND INSTALLED NEW UPPER TEE FROM BS 294-312, BL 0 IAW SRM 51-40-02, 51-40-05, 51-20-01 AND SOPM 20-41-02.

Part: SKIN — CHAFED (APU DOOR) · airframe 65,323 hrs · 37,698 cycles

LOWER VENT ON APU ACCESS DOOR HAS CHAFED AREA. ACFT GROUNDED. WELDED PERMANENT REPAIR ON LOWER VENT ON APU ACCES DOOR IAW EA 400-52, EA-10581.

Part: STOP FITTING — CORRODED (BS 986) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

RT AFT GALLEY SERVICE DOOR MOP SILL AFT STOP FITTING HAS CORROSION. ACFT GROUNDED. R & R FITTING IAW SRM 51-40-02.

Part: ANGLE — BENT (BS 1005-1016) · airframe 65,323 hrs · 37,698 cycles

VERTICAL STAB LT FWD SKATE ANGLE BENT (SHORT ONE). REMOVED DAMAGED SKATE ANGLE, FABRICATED, ALODINED, PRIMED, TOPCOATED AND INSTALLED NEW SKAT ANGLE IAW DWG 65-54842, SRM 51-40-02, 51-40-05, AMM 51-21-21-307-014, 51-21-99-307-022.

Part: ACCESS PANEL — CHAFED (BS 1016-1032) · airframe 65,323 hrs · 37,698 cycles

RT VERTICAL ACCESS PANEL 9504 CHAFED IN 2 AREAS. ACFT GROUNDED. FABRICATED NEW PANEL IAW SRM 51-30-01. TREATED AND PRIMED IAW SRM 51-70-10, AND BONDED PANEL IAW SRM 51-70-10-2R-0.

Part: BEAM — CHAFED (RT MLG) · airframe 65,323 hrs · 37,698 cycles

RT MLG BEAM CHAFED ON LOWER SIDE. ACFT GROUNDED. C/W BLEND REPAIR OF RT MLG BEAM IAW EA 400-57EA-10584, REV NEW DATE ISSUED 6-26-13.

Part: CUSP WEB — CORRODED (BS 767-787) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

WHILE CLEANING AREA, FOUND CORRODED ON RT CUSP WEB FROM BS 767-787. ACFT GROUNDED. R & R RT CUSP WEB IAW SRM 51-40-02. FOUND TO BE OUT OF LIMITS IAW SRM 53- 60-13-1A-1.

Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 65,323 hrs · 37,698 cycles

LEFT WING NR 2 SLAT HAS DUCT CLOSE OUT DOOR ATTACH BRACKET CRACKED. FOUND AFTER REMOVAL FOR DUCT REPLACEMENT. ACFT GROUNDED. FABRICATED NEW BRACKET (CHANNEL) IAW SRM 51-40-05-0G-0 AND DWG 69-73541.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 65,323 hrs · 37,698 cycles

CABIN FLOORBOARD 2346Y HAS EDGE DAMAGE ON 1 SIDE, TRANS FROM MIG 85, ITEM NR 1 DUE TO RII. ACFT GROUNDED. REPAIRED FLOORBOARD IAW SRM 53-00-50, PAR 3C, PGS 1 AND 2.

Part: FLOOR PANEL — DENTED (PAX CABIN) · airframe 65,323 hrs · 37,698 cycles

PAX CABIN FLOOR PANEL 2450Y BOTTOM SIDE HAS NUMEROUS DENTS. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50 PAR 3C, PGS 1 AND 2.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PAX CABIN FLOOR PANEL 2378Y TOPSIDE HAS NUMEROUS DENTS AND DAMAGE TO FWD END. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50 PAR 3C, PGS 1 AND 2.

Part: FLOOR PANEL — DENTED (PAX CABIN) · airframe 65,323 hrs · 37,698 cycles

PAX CABIN FLOOR PANEL NR 2373Y TOPSIDE HAS NUMEROUS DENTS AND CRUSHED/MISSING HONEYCOMB CORE. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PGS 1 AND 2.

Part: FLOOR PANEL — SCRATCHED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PAX CABIN FLOOR PANEL 2469Y TOPSIDE HAS SCRATCHES. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PGS 1 AND 2.

Part: FLOOR PANEL — DAMAGED (PAX CABIN) · airframe 65,323 hrs · 37,698 cycles

PAX CABIN FLOOR PANEL, 2435Y FWD END HAS DAMAGED, CRUSHED HONEYCOMB CORE. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PGS 1 AND 2.

Part: FLOOR PANEL — DENTED (PAX CABIN) · airframe 65,323 hrs · 37,698 cycles

PAX CABIN RT OTBD CABIN FLOOR PANEL NR 2359Y TOPSIDE FWD AFT HAS NUMEROUS DENTS. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PGS 1 AND 2.

Part: FLOOR PANEL — DENTED (PAX CABIN) · airframe 65,323 hrs · 37,698 cycles

PAX CABIN FLOOR PANEL 2444Y TOPSIDE HAS NUMEROUS DENTS. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PGS 1 AND 2.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 65,323 hrs · 37,698 cycles

PAX CABIN FLOOR PANEL 2469Y AFT END HAS DELAMNATION AND DAMAGE TO EDGE/CORNERS. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PGS 1 AND 2.

Part: FLOOR PANEL — DENTED (PAX CABIN) · airframe 65,323 hrs · 37,698 cycles

PAX CABIN FLOOR PANEL 2466Y TOPSIDE/BOTTOM SIDE HAS NUMEROUS DENTS AND CRUSHED HONEYCOMB ON EDGES. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50 PAR 3C, PGS 1 AND 2.

Part: FLOOR PANEL — GOUGED (PAX CABIN) · airframe 65,323 hrs · 37,698 cycles

PAX CABIN RT INBD FLOOR PANEL 2348Y AFT END TOPSIDE HAS CRUSHED HONEYCOMB AND DEEP GOUGES. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PGS 1 AND 2.

Part: FLOOR PANEL — DENTED (PAX CABIN) · airframe 65,323 hrs · 37,698 cycles

PAX CABIN LT INBD CABIN FLOOR PANEL 2353Y TOPSIDE FWD/AFT HAS NUMEROUS DENTS. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PGS 1 AND 2.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 65,323 hrs · 37,698 cycles

PAX CABIN FLOOR PANEL 2455Y FWD END IS CRUSHED/DELAMINATION. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50 PAR 3C, PGS 1 AND 2.

Part: FLOOR PANEL — DENTED · airframe 65,323 hrs · 37,698 cycles

LT INBD CABIN FLOOR PANEL NR 2376 HAS SEVERAL DENTS. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PGS 1 AND 2.

Part: RETAINER — CORRODED (MLG WW) · airframe 65,323 hrs · 37,698 cycles

RT MLG WW NR 4 SEAL RETAINER CORRODED. ACFT GROUNDED. LOCATED AND DRILLED NEW RETAINER IAW SRM 51-40-05-06-0.

Part: RETAINER — CORRODED (FUSELAGE) · airframe 65,323 hrs · 37,698 cycles

RT MLG WW NR 3 LOWER SEAL RETAINER CORRODED. ACFT GROUNDED. LOCATED, AND DRILLED NEW RETAINER IAW SRM 51-40-05-06-0.

Part: RETAINER — CORRODED (BS 650-671) · airframe 65,323 hrs · 37,698 cycles

LT MLG WW NR 3 UPPER SEAL RETAINER CORRODED, LOCATED AND DRILLED NEW RETAINER IAW SRM 51-40-05-0G-0.

Part: RETAINER — CORRODED (BS 725-731) · airframe 65,323 hrs · 37,698 cycles

LEFT MLG WW NR 2 LWR SEAL RETAINER CORRODED. REPLACED SEAL RETAINER IAW SRM 51-40-05-0G-0.

Part: RETAINER — CORRODED (BS 725-731) · airframe 65,323 hrs · 37,698 cycles

RR MLG WW NR 2 LOWER SEAL RETAINER CORRODED. LOCATED AND DRILLED NEW SEAL RETAINER IAW SRM 51-40-05-0G-0.

Part: RETAINER — CORRODED (BS 718-720) · airframe 65,323 hrs · 37,698 cycles

RT MLG WW NR 1 UPPER SEAL RETAINER CORRODED. LOCATED AND DRILLED NEW SEAL RETAINER IAWSRM 51-40-05-0G 0.

Part: RETAINER — CORRODED (LT MLG DOOR) · airframe 65,323 hrs · 37,698 cycles

LT MLG WW NR 1 UPPER SEAL RETAINER CORRODED. ACFT GROUNDED. LOCATED AND DRILLED NEW SEAL RETAINER IAW SRM 51-40-05-06-0.

Part: FLOOR PANEL — DAMAGED (PAX CABIN) · airframe 65,323 hrs · 37,698 cycles

FLOOR PANEL 2440 HAS EDGE DAMAGE IN SEVERAL PLACES. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1.

Part: RETAINER — CORRODED (RT MLG WW) · airframe 65,323 hrs · 37,698 cycles

RT MLG W/W NR 4 LOWER SEAL RETAINER CORRODED. ACFT GROUNDED. ORDERED, LOCATED AND DRILLED NEW SEAL RETAINER IAW SRM 51-40-05-0G-0.

Part: RETAINER — CORRODED (FUSELAGE) · airframe 65,323 hrs · 37,698 cycles

RIGHT MLG W/W NR 2 UPPER SEAL RETAINER CORRODED. ACFT GROUNDED. LOCATED AND DRILLED NEW SEAL RETAINER IAW SRM 51-40-05-06-0.

Part: RETAINER — CORRODED (LT MLG WW) · airframe 65,323 hrs · 37,698 cycles

LT MLG W/W NR 4 UPPER SEAL RETAINER CORRODED. ACFT GROUNDED. LOCATED AND DRILLED NEW RETAINER IAW 51-40-05-06-0.

Part: RETAINER — CORRODED (LT MLG) · airframe 65,323 hrs · 37,698 cycles

LEFT MLG NR 1 LOWER SEAL RETAINER CORRODED. ACFT GROUNDED. LOCATED AND DRILLED PLACED ON PANEL RACK IAW SRM 51-40-05-0.

Part: RETAINER — CORRODED (BS 650-671) · airframe 65,323 hrs · 37,698 cycles

RT MLG W/W NR 3 UPPER SEAL RETAINER CORRODED. LOCATED AND DRILLED NEW RETAINER IAW SRM 51-40-05-0G-0.

Part: RETAINER — CORRODED (LT MLG WW) · airframe 65,323 hrs · 37,698 cycles

LT MLG W/W NR 4 LOWER SEAL RETAINER CORRODED. ACFT GROUNDED. LOCATED AND DRILLED NEW SEAL RETAINER IAW SRM 51-40-05-06-0.

Part: FLOOR PANEL — DENTED (PAX CABIN) · airframe 65,323 hrs · 37,698 cycles

PAX CABIN FLOOR PANEL NR 2465 TOPSIDE HAS NUMEROUS DENTS. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PGS 1 AND 2.

Part: RETAINER — CORRODED (LT MLG WW) · airframe 65,323 hrs · 37,698 cycles

LT MLG WW NR 2 UPPER SEAL RETAINER CORRODED. LOCATED AND DRILLED NEW SEAL RETAINER IAW SRM 51-40-05-0G-0.

Part: FLOOR PANEL — DENTED (BS 827-887) · airframe 65,323 hrs · 37,698 cycles

PAX CABIN FLOOR PANEL 2463Y, TOPSIDE HAS NUMEROUS DENTS, CRUSHED AND CRACKED HONEYCOMB CORE. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PGS 1 AND 2.

Part: RETAINER — CORRODED · airframe 65,323 hrs · 37,698 cycles

LT MLG WW NR 3 LOWER SEAL RETAINER CORRODED. ACFT GROUNDED. LOCATED AND DRILLED NEW RETAINER IAW SRM 51-40-05-06-0.

Part: FAIRING — CRACKED (LT PYLON) · airframe 65,323 hrs · 37,698 cycles

ON REMOVAL, FOUND LT PYLON AFT FIXED FAIRING TO BE CRACKED AT RIVET HOLE FOR TEFLON SUPPORT ON FWD MIDDLE EDGE. ACFT GROUNDED. DRILLED AND LOCATED NEW FAIRING IAW SRM 51-40-05.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PAX CABIN FLOOR PANEL 2439Y TOPSIDE HAS APPROX 9 LARGE DENTS AND NUMEROUS SMALLER DENTS. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PGS 1 AND 2.

Part: RETAINER — CORRODED (RT MLG WW) · airframe 65,323 hrs · 37,698 cycles

RT MLG WW NR 1 LOWER SEAL RETAINER CORRODED LOCATED AND DRILLED NEW SEAL RETAINER IAW SRM 51-40-05-0G-0.

Part: RETAINER — CORRODED (FUSELAGE) · airframe 65,323 hrs · 37,698 cycles

RT MLG WW NR 4 LOWER SEAL RETAINER CORRODED. LOCATED AND DRILLED RETAINER IAW SRM 51-40-05-0G-0.

Part: FLOORBOARD — DAMAGED (BS 500E-520) · airframe 65,323 hrs · 37,698 cycles

CABIN FLOORBOARD 2368Y HAS EDGE DAMAGE IN 4 AREAS. ACFT GROUNDED. REPAIRED FLOORBOARD IAW SRM 53-00-50, PAR 3C, PGS 1 & 2.

Part: WEB — GOUGED (BS 400-420) · airframe 65,323 hrs · 37,698 cycles

DURING GVI AFTER REMOVING SEAT TRACK, FOUND WEB AT BS 400-420, LBL 24 GOUGED. ACFT GROUNDED. REMOVED FABRICATED NEW AND INSTALLED NEW WEB IAW SRM 51-40-02-0G-0, PAR 7D.

Part: FAIRING — CORRODED (MLG) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

NR 5 LOWER MLG FAIRINGS CORRODED. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS, FOUND FAIRING OUT OF LIMITS IAW SRM 53-60-71-1A-1, FIG 101.

Part: STAND OFF — CORRODED (KEELBEAM) · airframe 65,323 hrs · 37,698 cycles

STANDOFF FOR AFT KEELBEAM DOOR RT SIDE IS CORRODED. FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-40-02-0G-0.

Part: WEB — CORRODED (BS 767-787) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

WHILE CLEANING AREA, FOUND CORROSION ON RT CUSP WEB FROM STA 767-787. ACFT GROUNDED. R & R RT CUSP WEB IAW SRM 51-40-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13-1A-1.

Part: FLOOR SUPPORT — CORRODED (GALLEY) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

AFT GALLEY FLOOR SUPPORT ANGLE AT BS 986 LBL 28 IS CORRODED. R & R ANGLE WITH NEW ANGLE IAW SRM 51-40-05 AND SRM 51-40-02.

Part: BRACKET — BROKEN (L1 DOOR GATE) · airframe 65,323 hrs · 37,698 cycles

L1 DOOR UPPER GATE FWD CORNER BRACKET IS BROKEN. ACFT GROUNDED. R & R BRACKET IAW SRM 51-40-02-0G 0.

Part: ANGLE — CHAFED (NR 1 NACELLE) · airframe 65,323 hrs · 37,698 cycles

NR 1 PYLON BEHIND FWD END OF PANEL 5752L ANGLE IS CHAFED. ACFT GROUNDED. REMOVED DAMAGED ANGLE AND INSTALLED NEW ANGLE IAW SRM 51-40-0G-0.

Part: STRINGER CLIP — CRACKED (BS 500E S7R) · airframe 65,323 hrs · 37,698 cycles

STINGER CLIP AT BS 500E, STR 7R IS CRACKED AT FASTENER HOLE. ACFT GROUNDED. REMOVED DAMAGED STRINGER CLIP. LOCATED AND DRILLED AND INSTALLED NEW STRINGER CLIP IAW SRM 51-40-05, FIG 3.

Part: LINK — DAMAGED (FUSELAGE) · airframe 65,323 hrs · 37,698 cycles

AFTER REMOVAL OF SEAT TRACK, BS 520-540, LBL 45 FOUND LINK HAS A EDGE DAMGE. ACFT GROUNDED. REPAIRED LINK IAW EA 400-53EA-10665.

Part: FLOOR PANEL — TORN (BS 380-420) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN RT OTBD FLOOR PANEL 2349Y END HAS FIBERGLASS FIBERS TORN. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR 3, PG 1.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

CABIN FLOOR PANEL DELAMINATED. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN FLOOR PANEL 2343Y TOPSIDE HAS NUMEROUS DENTS. ACFT GROUNDED. BONDED PANEL IAW SRM 53-00-50 PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN FLOOR PANEL 2469Y TOPSIDE AHS A PUNCHED HOLE AND DENTS. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — DENTED (MAI CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN FLOOR PANEL 2375Y TOPSIDE HAS NUMEROUS DENTS AND CRUSHED & MISSING HONEYCOMB ON EDGES. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR-3C, PGS 1 & 2.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN FLOOR PANEL 2374Y TOPSIDE/BOTTOM SIDE FORWARD CORNER HAS CRUSHED & MISSING HONEYCOMB. ACFT GROUNDED. BONDED FLOOR PANEL IAW 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — CRUSHED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

LT INBD CABIN FLOOR PANEL 2432 HAS HONEYCOMB SMASHED ON PERIMETER EDGE. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

LT INBD CABIN FLOOR PANEL 2437Y IS DELAMINATED. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

LT OTBD CABIN FLOOR PANEL 2442Y HAS NUMEROUS DENTS. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN FLOOR PANEL NR 2431Y TOPSIDE HAS NUMEROUS DENTS. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR-3C, PGS 1 & 2.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN FLOOR PANEL 2454Y TOPSIDE HAS NUMEROUS DENTS AND CRUSHED EDGES. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

LT INBD CABIN FLOOR PANEL 2458Y HAS NUMEROUS DENTS. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — CRUSHED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN FLOOR PANEL 2467Y TOPSIDE HAS CRUSHED, MISSING CORE AT CORNERS. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

LT INBD CABIN FLOOR PANEL 2437Y HAS SEVERAL DENTS. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN FLOOR PANEL 2443Y, TOPSIDE HAS DAMAGED MISSING HONEYCOMB AND DENTS. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN FLOOR PANEL 2478Y, TOPSIDE HAS DELAMINATION. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3G, PAGES 1 & 2.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

LT INBD CABIN FLOOR PANEL 2432Y HAS SEVERAL DENTS. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — DENTED (CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN FLOOR PANEL 2462Y, TOPSIDE HAS NUMEROUS DENTS. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PGS 1 AND 2.

Part: FLOOR PANEL — CRUSHED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

LEFT OTBD CABIN FLOOR PANEL 2457Y HONEYCOMB CRUSHED IN SEVERAL AREAS. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN FLOOR PANEL 2464Y, TOPSIDE HAS NUMEROUS DENTS AND DAMAGE, MISSING HONEYCOMB ON EDGES. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

LEFT INBD CABIN FLOOR PANEL 2432Y IS DELAMINATED. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — DEBONDED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN FLOOR PANEL 2472Y, TOPSIDE CORNER HAS LOOSE FIBERGLASS THREADS. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 AND 2.

Part: FLOOR PANEL — CRUSHED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

CENTER CABIN FLOOR PANEL 2475Y HAS HONEYCOMB SMASHED ON EDGES OF PANEL. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN FLOOR PANEL, NR 2471Y, ALL EDGES HAVE DAMAGE, MISSING HONEYCOMB. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PAX CABIN FLOOR PANEL 2452Y TOPSIDE HAS NUMEROUS DENTS AND CRUSHED/MISSING HONEYCOMB CORE. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PGS 1 AND 2.

Part: ANGLE — CRACKED (BS 294.5) · airframe 65,323 hrs · 37,698 cycles

SKIN TO INERCOSTAL ATTACHMENT ANGLE AT FS 294.5 NEAR STR 13R IS CRACKED. ACFT GROUNDED. REMOVED DAMAGED ANGLE. LOCATED AND DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-40-02 AND 51-40-05.

Part: SHEAR TIE — CRACKED (BS 277-291.5) · airframe 65,323 hrs · 37,698 cycles

SKIN TO INTERCOSTAL ATTACHMENT ANGLE AT FS 294.5 NEAR STR 9R IS CRACKED. ACFT GROUNDED. REMOVED DAMAGE, LOCATED AND DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-40-02 AND 561-40-05.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

CABIN FLOOR PANEL HAS SEVERAL DENTS. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 65,323 hrs · 37,698 cycles

PAX CABIN WET FLOOR PANEL 2476Y TOPSIDE/BOTTOM SIDE HAS NUMEROUS AREAS CORRODED, DELAMINATION AREAS, INCLUDING SUPPORT DOUBLER ON BOTTOM SIDE CORRODED. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PGS 1 AND 2 AND 5085 PAR 8.31. X PG 4.

Part: FLOOR PANEL — DENTED (CENTER CABIN) · airframe 65,323 hrs · 37,698 cycles

CENTER CABIN FLOOR PANEL 2448Y HAS NUMEROUS DENTS. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

LT INBD CABIN FLOOR PANEL HAS SEVERAL DENTS. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN FLOOR PANEL, 2433Y, TOPSIDE HAS NUMEROUS SCRATCHES AND GOUGES. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: STIFFENER — CRACKED (BS 294.5) · airframe 65,323 hrs · 37,698 cycles

SKIN TO INTERCOASTAL ATTACHMENT ANGLE AT FS 294.5 NEAR S12R IS CRACKED. ACFT GROUNDED. REMOVED CRACKED ANGLE LOCATED AND DRILLED TOPCOATED AND INSTALLED NEW ANGLE IAW SRM 51-40-02, 51-40-05 AND AMM 51-21-99-307-022.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN FLOOR PANEL 2460Y TOPSIDE HAS NUMEROUS DENTS. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PGS 1 & 2.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN FLOOR PANEL NR 2470Y, TOPSIDE, BOTTOM SIDE HAS NUMEROUS DENTS AND CRUSHED HONEYCOMB EDGES. ACFT GROUNDED. BONDED FLOOR PANEL NR 2470Y IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN FLOOR PANEL 2436Y TOPSIDE HAS NUMEROUS DENTS AND CRUSHED & MISSING HONEYCOMB CORE. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR-3C, PGS 1 & 2.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

LT OTBD CABIN FLOOR PANEL 2457Y HAS SEVERAL DENTS. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C 1 & 2.

Part: FLOOR PANEL — DENTED (PAX CABIN) · airframe 65,323 hrs · 37,698 cycles

PAX CABIN FLOOR PANEL 2452Y TOPSIDE HAS NUMEROUS DENTS AND CRUSHED MISSING HONEYCOMB CORE. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PGS 1 AND 2.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

CENTER CABIN FLOOR PANEL 2475 IS DENTED. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, 1 & 2.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

RT OTBD CABIN FLOOR PANEL 2456Z HAS SEVERAL DENTS. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3.C, PAGES 1 & 2.

Part: INTERCOSTAL — CRACKED (BS 277) · airframe 65,323 hrs · 37,698 cycles

INTERCOSTAL AT FS 277, NEAR STRINGER 14R IS CRACKED. ACFT GROUNDED. REMOVED CRACKED INTERCOSTAL IAW SRM 51-40-02-0G-0, 51-40-05 AND AMM 51-21-99-307-014.

Part: CUSP WEB — CORRODED (BS 807-827) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

CORROSION IN CUSP WEB AREA RT SIDE FROM BS 807 TO 827. REMOVED CORROSION FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-60-13-1A-1. R & R CUSP WEB IAW SRM 51-40-02-0G-0 AND DWG 65-47976. APPLIED PROTECTIVE FINISHES IAW AMM 51-21-21-307-014.

Part: CUSP WEB — CORRODED (BS 727F-727G) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

CORROSION IN CUSP AREA RT SIDE FROM BS 727F TO 727G. ACFT GROUNDED. REMOVED CORRODED ON CUSP WEB, FOUND OUT OF LIMITS. REMOVED, FABRICATED AND INSTALLED NEW CUSP WEB IAW SRM 51-40-02-0G-0, 51-30-01-0G-0, 53-60-13-1A-1, FIG 101, MM 51-21-21 307-014, 51-21-99-307-001.

Part: CUSP WEB — CORRODED (BS 727F-727G) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

CORROSION IN CUSP AREA RT SIDE FROM BS 727F TO 727G. ACFT GROUNDED. REMOVED CORROSION ON CUSP WEB AT 727F-727G RT SIDE OUT OF LIMITS REMOVED, FABRICATED AND INSTALLED NEW CUSP WEB IAW SRM 51-40-02-0G-0-51-30-01-0G 0-53-60-13-1A-1, FIG 101, MM 51-21-21 307-014, 51-21-99-307-001.

Part: CUSP WEB — CORRODED (BS 747-767) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

CORRODED IN CUSP WEB AREA RT SIDE FROM BS 747 - 767. ACFT GROUNDED. REMOVED WEB, FABRICATED AND INSTALLED NEW WEB IAW SRM 51-40-02 AND 51-30-02-0G-0, FIG 7.

Part: WEB — CORRODED (BS 727G-747) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

CORROSION IN CUSP AREA RT SIDE BETWEEN 727G TO 747. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13-1A-1. R & R WEB IAW SRM 51-40-02-0G-0 AND DWG 65C26402 APPLIED PROTECTIVE FINISHES IAW AMM 51-21-21-307-014.

Part: FLOOR PANEL — CRUSHED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN RT OTBD FLOOR PANEL 2364Y FWD EDGE HONEYCOMB CORE IS CRUSHED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR-2C, PGS 1 & 2.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CENTER FLOOR PANEL 2347Y EDGE OF HONEYCOMB CORE DAMAGED. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN FWD WET FLOOR PANEL 2344 AFT CORNER EDGE HONEYCOMB CORE IS DAMAGED. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: WEB — CORRODED (BS 800-840) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

AFT CARGO COMPARTMENT THRESHOLD WEB PANEL HAS SEVERAL AREAS OF CORROSION. GROUNDED. R & R AFT CARGO THRESHOLD WEB IAW SRM 51-40-02-06-0, STEP 6.

Part: STRUCTURE — CORRODED (BS 647-722) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

RT MLG WW UPPER STRUCTURE HAS CORROSION. REMOVED, FABRICATED NEW AND INSTALLED NEW STRUCTURE IAW SRM 51-40-02-0G-0, PAR 5.

Part: FLOOR PANEL — CRUSHED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN RT OUTBD FLOOR PANEL 2364Y AFT EDGE HONEYCOMB CORE IS CRUSHED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PGS 1 & 2.

Part: FLOOR PANEL — DENTED (MAIN CAIBN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN RT OTBD FLOOR PANEL, 2364Y AFT FWD TOPSIDE HAS NUMEROUS DENTS. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — CRUSHED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN FWD WET FLOOR PANEL NR 2339, EDGE HONEYCOMB CORE IS CRUSHED. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PAGES 1 & 2.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PASSENGER CABIN LT OTBD FLOOR PANEL 2369Y IS CRACKED ON AFT END AT INSERT. ACFT GROUNDED. BONDED FLOOR PANEL IAW SRM 53-00-50, PAR 3C. PAGES 1 & 2.

Part: FLOORBEAM — CORRODED (BS 807-809) · airframe 65,323 hrs · 37,698 cycles

AFT CARGO LBL 9 FLOORBEAM CORRODED AFT OF STA 807. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A-1. REPAIRED CARGO FLOORBEAM IAW SRM 53-00-53-2R-1.

Part: FRAME — DENTED (BS 727B) · airframe 65,323 hrs · 37,698 cycles

AFT CARGO FRAME AT BS 727B, DENTED FROM S24 - 25R, ACFT GROUNDED. REPAIRED FRAME IAW EA 400-53EA-10601, REV NEW ISSUED 06/27/2013.

Part: SUPPORT BRACKET — CORRODED (BS 727G) · airframe 65,323 hrs · 37,698 cycles

AFT CARGO LT SIDEWALL SUPPORT BRACKET CORRODED AT BS 727G. REMOVED CORROSION AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A1, FIG 101. R & R SUPPORT IAW SRM 51-40-02-0G-0, PAR 4.

Part: RIB — CRACKED (LT WING) · airframe 65,323 hrs · 37,698 cycles

LT WING STA 135.5, RIB CRACKED AT AFT STR. ACFT GROUNDED. REPAIRED LT WING, RIB IAW EA 400-57, EA-10604.

Part: SEAL DEPRESSOR — CHAFED (NR 1 NACELLE) · airframe 65,323 hrs · 37,698 cycles

NR 1 ENGINE PYLON METAL FIRE SEAL FLANGE CHAFED. ACFT GROUNDED. R & R SEAL DEPRESSOR ON NR 1 ENG PYLON IAW AMM 20-50-11-912-002, FIG 203, PAGE 8.

Part: CHANNEL — CORRODED (BS 787) · airframe 65,323 hrs · 37,698 cycles

AFT CARGO LT SIDEWALL MOUNT BRACKET AT BS 787 HAS CORRODED AND BARE METAL. ACFT GROUNDED. R & R LT SIDEWALL MOUNT BRACKET AT BS 787 IAW SRM 51-40-08 AND 51-40-05.

Part: INTERCOSTAL — CRACKED (BS 302) · airframe 65,323 hrs · 37,698 cycles

INTERCOSTAL CRACKED AT BS 302 AND S8L. ACFT GROUNDED. R & R INTERCOSTAL IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

AFT CARGO BS 947 LT BULKHEAD TO FLOOR SUPPORT CORRODED AND BARE METAL. ACFT GROUNDED. REMOVED & REPLACED AFT CARGO LT BULKHEAD AND FLOOR SUPPORT IAW SRM 51-40-02-0G0 AND SRM 51-40-05-0G0.

Part: SEAT TRACK — GOUGED (BS 344-480) · airframe 65,323 hrs · 37,698 cycles

LEFT SEAT TRACK BS 344-480, LBL 24 GOUGED. BLENDED GOUGE AND FOUND TO BE OUT OF LIMITS OF SRM 53-00-52-1A-1. R & R WITH A NEW SEAT TRACK IAW SRM 51-40-02-0G-0 AND EA 400 53EA 04953.

Part: SEAT TRACK — GOUGED (BS 480-520) · airframe 65,323 hrs · 37,698 cycles

RIGHT SEAT TRACK, BS 480-520, RBL 45 HAS GOUGES. BLENDED AFFECTED AREAS OF SEAT TRACK. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A1, FIG 101 DETAIL VI. REMOVED AND FABRICATED AND REPLACED SEAT TRACK IAW SRM 51-40-02-0G0, PARA D, SRM 51-40-05-0G0, FIG 2, DETAIL 1 AND ASA 400-53EA-04953.

Part: SEAT TRACK — GOUGED (BS 727B-927) · airframe 65,323 hrs · 37,698 cycles

LT SEAT TRACK BS 727B-927, LBL 45 HAS GOUGES. ACFT GROUNDED. REMOVED DAMAGE AND CHECKED LIMITS FOUND TRACK OUT OF LIMITS IAW SRM 53-00-52-1A1, FIG 101. REMOVED, FABRICATED NEW AND INSTALLED NEW TRACK IAW SRM 53-00-52-2R4 AND EA 400-53EA-04953, REV NEW.

Part: SKATE ANGLE — CHAFED (BS 1016-1125) · airframe 65,323 hrs · 37,698 cycles

VERTICAL STAB TO FUSELAGE RT SKATE ANGLE CHAFED BETWEEN FWD ATTACH LUGS AND RUDDER L/E. ACFT GROUNDED. REPAIRED VERTICAL STAB TO FUS. RT SKATE ANGLE IAW ASA EA 5530 01086. REPAIR 1.

Part: SKIN — DENTED (FUSELAGE) · airframe 65,323 hrs · 37,698 cycles

DENT IN EXTERIOR FUSELAGE, LT SIDE, BS 1088, AND 3 INCHES BELOW STRINGER 13L. ACFT GROUNDED. COMPLIED WITH EA 400, 53EA 10546 REV NEW.

Part: SEAT TRACK — GOUGED (BS 727B-927) · airframe 65,323 hrs · 37,698 cycles

LT SEAT TRACK BS 520-540, LBL 45 HAS GOUGES. REMOVED DAMAGE AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A-1. REMOVED, FABRICATED NEW AND INSTALLED NEW SEAT TRACK IAW AMM 20-50-11-912-002, FIG 202 AND EA 400 53EA 04953.

Part: FLOORBOARD — DAMAGED (BS 520-537.45) · airframe 65,323 hrs · 37,698 cycles

FLOORBOARD 2371Y HAS EDGE DAMAGE ON ALL SIDES. ACFT GROUNDED. REPAIRED FLOORBOARD IAW SRM 53-00-50, PAR 3C, PG 1 AND 2.

Part: SEAT TRACK — GOUGED (BS 727B-927) · airframe 65,323 hrs · 37,698 cycles

RT SEAT TRACK BS 727B-927, RBL 45 HAS GOUGES. ACFT GROUNDED. REMOVED GOUGES AND CHECKED LIMITS, FOUND TRACK OUT OF LIMITS SRM 53-00-52-1A-1, FIG 101, DETAIL VI. REMOVED, FABRICATED NEW AND INSTALLED NEW TRACK IAW SRM 53-00-52-2R4, FIG 201 AND EA 400 53EA 04953, REV NEW.

Part: SEAT TRACK — GOUGED (BS 480-520) · airframe 65,323 hrs · 37,698 cycles

RT SEAT TRACK BS 480-520, RBL 24 HAS GOUGES. ACFT GROUNDED. REMOVED DAMAGE AND CHECKED LIMITS FOUND TRACK OUT OF LIMITS IAW SRM 53-00-52-1A1, FIG 101. REMOVED, FABRICATED NEW AND INSTALLED NEW TRACK IAW SRM 51-40-02-0G 0 AND EA 400, 53EA 04953, REV NEW.

Part: SEAT TRACK — GOUGED (BS 540-727) · airframe 65,323 hrs · 37,698 cycles

LEFT SEAT TRACK BS 540-7276, LBL 24 GOUGED. REMOVED DAMAGE AND CKD LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A-1. REMOVED, FABRICATED NEW AND INSTALLED NEW TRACK IAW AMM 20-50-11-912-002, FIG 203 AND EA 400-53EA-04953.

Part: SEAT TRACK — GOUGED (BS 727B-927) · airframe 65,323 hrs · 37,698 cycles

RT SEAT TRACK BS 727B -927 RBL 24 HAS GOUGES, ACFT GROUNDED. REMOVED DAMAGE AND CHECKED LIMITS FOUND TRACK OUT OF LIMITS IAW SRM 53-00-52-1A1, FIG 101. REMOVED, FABRICATED NEW AND INSTALLED NEW TRACK IAW SRM 51-40-02-0G0 AND ASA EA 400-53EA-04953, REV NEW.

Part: WEB — CORRODED (BS 686-689.5) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

LT WHEEL WELL MANIFOLD ASSY CORRODED ON VERTICAL WEB AT 8:30 POSITION. ACFT GROUNDED. REPAIRED LT WHEEL WELL MANFIFOLD VERTICAL WEB AT 8:30 POSITION IAW AA EA 400, 53EA 10541.

Part: SEAT TRACK — GOUGED (BS 480-520) · airframe 65,323 hrs · 37,698 cycles

LT SEAT TRACK BS 480-520, LBL 45 HAS GOUGES. REMOVED DAMAGE AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A-1. REMOVED, FABRICATED NEW AND INSTALLED NEW SEAT TRACK IAW AMM 20-50-11-912-002, FIG 202 AND EA 400 53EA 04953.

Part: FLOOR SUPPORT — CORRODED (BS 986-1006) · airframe 65,323 hrs · 37,698 cycles

AFT GALLEY FLOOR SUPPORT WEB ANGLE RT BS 986 - 1006 IS CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 56-30-51, FIG 101. R & R SUPPORT ANGLE IAW SRM 51-40-02.

Part: SEAT TRACK — GOUGED (BS 480-520) · airframe 65,323 hrs · 37,698 cycles

LT SEAT RACK STA 480 -520, LBL 24 HAS GOUGES. ACFT GROUNDED. REMOVED GOUGES AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A1, FIG 101. REMOVED, FABRICATED NEW AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-02-0G0, PAR D AND EA 400-53EA- 04953, REV NEW ISSUED 09MAR11.

Part: SEAT TRACK — GOUGED (BS 540-727) · airframe 65,323 hrs · 37,698 cycles

RT SEAT TRACK BS 540-727, RBL 24 HAS GOUGES FABRICATED NEW SEAT TRACK IAW SRM 51-40-05 AND ASA EA 400-53EA-04953.

Part: SEAT TRACK — GOUGED (BS 540-727) · airframe 65,323 hrs · 37,698 cycles

RT SEAT TRACK, BS 540-727.6, RBL 45 HAS GOUGES REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-02-0G-0 AND EA 400-53EA-04953.

Part: SKATE ANGLE — CHAFED (BS 1016-1121) · airframe 65,323 hrs · 37,698 cycles

VERTICAL STABILIZER TO FUSELAGE LT SKATE ANGLE CHAFED FROM FWD ATTACH LUGS TO RUDDER L/E. ACFT GROUNDED. BLENDED CHAFE, CHECKED LIMITS, WAS OUT OF LIMITS IAW EA CM 5530-01086, ACCOMPLISHED REPAIR 2 IAW EA 5530 01086.

Part: SEAT TRACK — GOUGED (BS 520-540) · airframe 65,323 hrs · 37,698 cycles

LT SEAT TRACK STA 520-540, LBL 45 HAS GOUGES. REMOVED DAMAGE AND CHECKED LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A-1. REMOVED, FABRICATED NEW AND INSTALLED NEW SEAT TRACK IAW AMM 20-50-11-912-002, FIG 202 AND EA 400 53EA 04953.

Part: STRINGER CLIP — BROKEN (BS 500A) · airframe 65,323 hrs · 37,698 cycles

INTERIOR CABIN BS 500A, STRINGER 7R CLIP IS BROKEN. ACFT GROUNDED. REMOVED OLD STRINGER CLIP AND INSTALLED NEW STRINGER CLIP IAW SRM 51-40-02.

Part: STRINGER CLIP — BENT · airframe 65,323 hrs · 37,698 cycles

AFT CARGO STRINGER CLIP BENT AT S 25L AND STA 727B. R & R STRINGER CLIP (TIE) IAW SRM 51-40-02-0G-0, PAR 7D.

Part: FAIRING — CORRODED (BS 690-720) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

NR 4 LWR RT MLG FAIRING SHOWS CORROSION. ACFT GROUNDED. REMOVED CORROSION FROM FAIRING, OUT OF LIMITS IAW SRM 53-60-71-1A-1, FIG 101.

Part: FAIRING — GOUGED (BS 670-675) · airframe 65,323 hrs · 37,698 cycles

ONE LT MLG FAIRING HAS CHAFED AREA WITH BARE METAL PANEL RACK. ACFT GROUNDED. BLENDED CHAFE, OUT OF LIMITS IAW SRM 53-60-71-1A1, FIG 101.

Part: CUSP WEB — CORRODED (BS 727E-727F) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

CORRODED IN CUSP AREA, RT SIDE FROM 727E TO 727F CUSP WEB AT RT STA 727E TO 727F FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13-1A 1-FIG 101. REMOVED, FABRICATED AND INSTALLED NEW WEB IAW SRM 51-40-02 AND 51-30-01-0G-0.

Part: CUSP WEB — CORRODED (BS 747-767) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

SUSPECTED CORROSION AT STA 747 LT SIDE IN CUSP AREA. ACFT GROUNDED. REMOVED CORROSION ON LT CUSP WEB, FOUND OUT OF LIMITS. REMOVED CUSP WEB LOCATED DRILLED AND INSTALLED NEW CUSP WEB IAW SRM 53-60-13-1A1, FIG 101, 51-40-02 , 51-40-05.

Part: SKIN — CHAFED (NR 4 SLAT) · airframe 65,323 hrs · 37,698 cycles

RIGHT WING NR 4 SLAT LOWER SURFACE CHAFED ABOVE ACTUATOR. ACFT GROUNDED. REPAIRED CHAFE ON RT WING NR 4 SLAT IAW SRM 51-70-10 -2R0, REPAIR 4, PARA 20, PG 48.

Part: WEB — CORRODED (BS 986-1016) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

AFT GALLEY FLOOR SUPPORT WEB BETWEEN BS 986-1006 IS CORRODED NUMEROUS AREAS. ACFT GROUNDED. REMOVED AND REPLACED WEB IAW SRM 51-40-02 AND SRM 51-40-05.

Part: STIFFENER — CORRODED (BS 1121) · airframe 65,323 hrs · 37,698 cycles

APU BAY STIFFENER FOR AIR INTAKE AT APROX BS 1121 IS CORRODED. ACFT GROUNDED. REMOVED CORRODED AND CHECKED LIMITS, FOUND STIFFENER OUT OF LIMITS IAW SRM 53-80-13-1A-2. R & R STIFFENER IAW SRM 51-40-02-0G-0.

Part: FLOOR PANEL — GOUGED (AFT CARGO) · airframe 65,323 hrs · 37,698 cycles

AFT CARGO BAY NR 3 FLOOR PANEL HAS DEEP GOUGES FULL LENGTH OF PANEL. ACFT GROUNDED. FABRICATED NEW PANEL IAW SRM 51-40-05-06-0.

Part: INTERCOSTAL — CHAFED (BS 847-867) · airframe 65,323 hrs · 37,698 cycles

AFT CARGO BAY BS 847, S-25R TWO ATTACHMENTS ARE CHAFING INTO FORMED INTERCOSTAL CAUSING EXTENSIVE DAMAGES. ACFT GROUNDED. R & R WITH A NEW INTERCOSTAL AT BS 847 ABOVE S25R IAW SRM 51-40-02-0G 0.

Part: FLOORBEAM — GOUGED (BS 540) · airframe 65,323 hrs · 37,698 cycles

GOUGE IN FLOOR SUPPORT APPROX BS 540 RT SIDE INSTALLED NEW COVER PLATE ON CHANNEL IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 986) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

AFT GALLEY FLOOR SUPPORT WEB ANGLE RT, STA 986 IS CORRODED IN SERVERAL AREAS. REMOVED CORRODED FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51-1A1, FIG 101. R & R FLOOR SUPPORTS IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CORRODED (BS 9228) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

AFT ENTRY DOOR L2 LOWER MOP SILL SURROUND STA 928, S17L INBD SUPPORT ANGLE FOR SILL IS CORRODED. REMOVED OLD MOP SILL IAW SRM 51-40-02 DRILLED, COUNTERSANK NEW MOPS SILL IAW SRM 51-40-05 INSTALLED NEW MOP SEAL IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 989-993) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

AFT GALLEY BS 986, LT FWD FLOOR FITTING FOR THE GALLEY IS CORRODED 30. ACFT GROUNDED. R & R FITTING IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 360-390) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

CABIN BS 360 - 390, RBL 57, FLOOR SUPPORT HAS CORRODED SPOT ON TOP SIDE. REMOVED, FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND SRM 51-40-05.

Part: SUPPORT ANGLE — CRACKED (BS 847) · airframe 65,323 hrs · 37,698 cycles

AFT CARGO BAY BS 847, S25R SUPPORT CLIP FOR FORMED INTERCOSTAL HAS DAMAGES AND EVIDENCE OF A CRACK IN RADIUS. ACFT GROUNDED. R & R WITH A NEW SUPPORT CLIP FOR FORMED INTERCOSTAL AT STA 847, STR 25R IAW SRM 51-40-02-0G 0.

Part: SHIM — CORRODED (FLOOR SUPPORT) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

FWD CABIN STA 329-344 261-10 FLOOR SUPPORT HAS CORROSION. ACFT GROUNDED. REMOVED CORROSION FROM FLOOR SUPPORT SHIM, NO ALLOWABLE LIMITS APPLICABLE. R & R SHIM IAW SRM 51-40-02-0G0 AND 51-30-01-0G0.

Part: SKIN — DENTED (BS 505) · airframe 65,323 hrs · 37,698 cycles

RIGHT FUSELAGE AT BS 505 SKIN IS DENTED STRINGER 23R. REPAIRED SKIN IAW SRM 53-00-01-2R-31.

Part: FLOORBEAM — CORRODED (BS 344) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

FLOORBEAM, BS 344 CORROSION SPOT ON UPPER SIDE AT LBL 13. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 52-10-51-1A-1. REPAIRED FLOORBEAM TEE CAP IAW EA NR 400-53 EA-10605.

Part: DRAIN PAN — CORRODED (BS 294-360) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

FWD CABIN LT MOP SILL FROM BS 294.5 - 360 HAS SEVERAL CORROSION SPOTS. ACFT GROUNDED. REMOVED CORRODED FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-10-15-1A 1. R & R MOPSILL IAW SRM 51-40-02-0G 0 AND DWG 65-17688.

Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

CABIN FLOORBEAM BS 947 CORRODED. R & R FLOORBEAM IAW EA NR 400-53EA-10551.

Part: ANGLE — CORRODED (RT MLG WW) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

RT MLG WHEEL WELL MANIFOLD ASSY LOWER AFT ANGLE IS CORRODED WITH BARE METAL, OUT OF LIMITS. REMOVED ANGLE FORMED NEW ANGLE HEAT TREATED, LOCATED, DRILLED, ALODINED, PRIMED, TOPCOATED AND INSTALLED IAW SRM 51 40-02-0G-0, DETAIL I, 51-30-01-0G-0, 51-40-05-0G-0, DETAIL 1 AND AMM 51-21-21-307-014E AND F INSTALLED IAW SRM 51-40-02-0G-0, NR 4 BAA-C.

Part: FLOOR SUPPORT — CORRODED (BS 312-328) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

FWD CABIN BS 312-328, LBL10, FLOOR SUPPORT FRAME HAS CORRODED SPOT. ACFT GROUNDED. REMOVED CORROSION, FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 51-10-02-0G 0 AND 53-10 51-1A-1, FIG 101. R & R SUPPORT IAW SRM 51-40-02 -0G 0 AND DWG 65C33971.

Part: WEB — CORRODED (BS 986-1006) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

AFT GALLEY FLOOR SUPPORT WEB RT BETWEEN BS 986 - 1006 CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51, FIG 101. R & R RT SUPPORT WEB IAW SRM 51-40-02.

Part: SKIN — DENTED (BS 228) · airframe 65,323 hrs · 37,698 cycles

LEFT FUSELAGE AT BS 228, SKIN HAS A PROTRUSION BELOW 24L. ACFT GROUNDED. C/W EA 400-53EA-10505, REV NEW DATE ISSUED 6-13-13.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

CABIN FLOOR PANEL UNDER FWD LAV HAS DAMAGED AREA. ACFT GROUNDED. BONDED FLOOR PANEL IAW IAW SRM 53-00-50, PAR 30, PGS 1 & 2.

Part: CHANNEL — CORRODED (BS 294-344) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

CABIN FLOOR RT MOP SILL BS 294.5-344 HAS SEVERAL CORROSION SPOTS ON TOP SIDE. ACFT GROUNDED. R & R INNER CHORD IAW SRM 51-40-02, W 1", O .080", R .056", L 1", D .024".

Part: FLOOR SUPPORT — CORRODED (BS 1006-1016) · airframe 65,323 hrs · 37,698 cycles

CABIN FLOOR SUPPORT STRUCTURE, BS 1006, RT ANGLE SUPPORT IS CORRODED. ACFT GROUNDED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51, FIG 101. R & R FLOOR SUPPORT ANGLE STRAP IAW SRM 51-40-02.

Part: SILL — CORRODED (BS 947) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

AFT ENTRY DOOR L2 LOWER MOP SILL SURROUND AT CUTOUT BS 928 S17L FWD FITTING FOR DOOR IS CORRODED. R & R FITTING IAW SRM 51-40-02.

Part: CHANNEL — CORRODED (BS 294-377) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

CABIN FLOOR RT MOP SILL, STA 294.5 - 344 HAS SEVERAL CORROSION SPOTS ON TOP SIDE. ACFT GROUNDED. R & R INNER CHORD IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 312) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

CABIN FLOORBEAM, BS 312 HAS SEVERAL CORRODED AREAS ON TOP SIDE. ACFT GROUNDED. REMOVED CORROSION, FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 51-10-02-0G 0 AND 53-10 51-1A-1. REPAIRED FLOORBEAM TEE IAW SRM 53-10-51-2.

Part: FLOORBEAM — CORRODED (BS 344) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

FLOORBEAM BS 344 CORROSION SPOT ON UPPER SIDE AT LBL 13. ACFT GROUNDED. REMOVED CORROSSION, FOUND OUT OF LIMITS IAW SRM 52-10-51-1A-1. REPAIRED FLOORBEAM TEE CAP IAW EA NR 400-53EA-10605

Part: WEB — CORRODED (BS 986-1006) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

AFT GALLEY FLOOR WEB, LT BETWEEN STA 986-1006 IS CORRODED NUMEROUS AREAS. R & R WEB IAW SRM 51-40-02 AND SRM 51-40-05.

Part: FITTING — CORRODED (BS 947) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

RIGHT AFT R2 SERVICE DOOR, AT MOP SILL DOOR CUTOUT, HAS CORROSION. R & R FITTING IAW SRM 51-40-02.

Part: CREASE BEAM — CORRODED (BS 380) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

CABIN FLOOR RT CREASE BEAM HAS CORROSION SPOT AT BS 380. ACFT GROUNDED. INSTALLED REPAIR ANGLES IAW SRM 51-70-12-0G-0, FIG 1.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

BS 986 FLOORBEAM HAS AREAS OF CORROSION MAINLY AROUND CLIP NUT HOLES. ACFT GROUNDED. R & R FLOORBEAM UPPER TEE IAW EA 400-53EA-10598.

Part: SILL — CORRODED (BS 927-1006) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

RT AFT GALLEY SERVICE DOOR R2 MOP SILL SUPPORT ANGLE HAS CORRODED ON AFT INBD, OTBD END. ACFT GROUNDED. REMOVED CORRODED FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15, FIG 101. R & R RT R2 MOPSILL IAW SRM 51-40-02, W 4, O .071, R .027, L 7FT, D .044.

Part: SKIN — DENTED (NR 2 INLET) · airframe 65,323 hrs · 37,698 cycles

NR 2 ENGINE INLET COWL INNER SKIN DENTED AT 6:30 O`CLOCK POSITION 5 FROM AFT EDGE. ACFT GROUNDED. REPAIRED NR 2 ENGINE INLET COWL INNER SKIN IAW EA 400-71EA-10607, REV NEW ISSUED 6/28/13.

Part: SKIN — DENTED (BS 1000) · airframe 65,323 hrs · 37,698 cycles

LEFT FUSELAGE BS 1000, SKIN IS DENTED JUST ABOVE S14L. ACFT GROUNDED. REMOVED DAMAGED SKIN FROM BS 992-1016, S10-14L, LOCATED FABRICATED BONDED DRILLED AND INSTALLED NEW SKIN IAW SRM 51-40-05, 51-40-02, MM 51-21-307-014, 51-21-99-307-001, DWG 65-52988.

Part: STRUCTURE — CORRODED (BS 675-702) · airframe 65,323 hrs · 37,698 cycles

LT WHEEL WELL MANIFOLD ASSY UPPER CHORD HAS BARE METAL AND CORROSION. ACFT GROUNDED. REMOVED LT WHEEL WELL MANIFOLD UPPER CHORD FABRICATED NEW CHORD TREATED, PRIMED TOPCOATED AND INSTALLED IAW SRM 51-30-01-0G-0, 51-40-02-0G-0 AND AMM 51-21 21-307-014 AND 51-21-99-307-001.

Part: SKIN — DENTED (BS 193) · airframe 65,323 hrs · 37,698 cycles

RT FUSELAGE BS 193 SKIN IS DENTED LESS THAN 3 IN ABOVE 24R. ACFT GROUNDED. C/W EA-400-53EA, 10537 REV NEW.

Part: SKIN — CHAFED (RT WING) · airframe 65,323 hrs · 37,698 cycles

RT WING OTBD BOOST PUMP CUTOUT LAND HAS CHAFING. ACFT GROUNDED. REPAIRED CHAFING IAW SRM 57-20-01-2R 6.

Part: TRANSITION PANEL — CORRODED (BS 500E-500G) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

FWD CARGO LT TRANSITION PANEL CORRODED IN SEVERAL AREAS FROM BS 500E TO 500G. REMOVED CORRODED FROM THE TRANSITION PANEL AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-53-1A-1, FIG 101. REMOVED FABRICATED NEW AND REPLACED THE TRANSITION PANEL IAW SRM 53-30-53-2R-3.

Part: SKIN — DENTED (BS 240-251.5) · airframe 65,323 hrs · 37,698 cycles

RT FUSELAGE, BS 247 SKIN IS DENTED 2 INCHES ABOVE LAP SEAM. ACFT GROUNDED. REPAIRED SKIN IAW EA 400 53EA 10529 REV NEW.

Part: SUPPORT BEAM — CHAFED (NR 2 NACELLE) · airframe 65,323 hrs · 37,698 cycles

NR 2 PYLON OTBD FAN COWL SUPPORT BEAM CHORD CHAFED. ACFT GROUNDED. REPAIRED NR 2 PYLON OTBD FAN COWL SUPPORT BEAM CHORD IAW EA 400-54EA-10558.

Part: SILL — CORRODED (BS 928) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

AFT ENTRY DOOR L2 LOWER MOP SILL SURROUND AT CUTOUT STA 928 2A7L AFT FITTING FOR DOOR IS CORRODED. ACFT GROUNDED. R & R FITTING IAW SRM 51-40-02, W .5, O .300, R .190, L .5, D .112.

Part: WEB — CORRODED (BS 670-720) · airframe 65,323 hrs · 37,698 cycles

RT MLG WHEEL WELL WEB HAS CORRODED ON AFT OTBD SURFACE. R & R WEB IAW EA 400-53EA-10547.

Part: SKIN — DENTED (BS 413) · airframe 65,323 hrs · 37,698 cycles

RT FUSELAGE, BS 413 SKIN IS DENTED 2 INCHES ABOVE 27R. REPAIRED DENT IAW EA 400-53EA-10552, REV NEW.

Part: SUPPORT BEAM — CHAFED (NR 2 NACELLE) · airframe 65,323 hrs · 37,698 cycles

NR 2 PYLON INBD FAN COWL SUPPORT BEAM CHORD CHAFED. REPAIRED NR 2 PYLON INBD FAN COWL SUPPORT BEAM CHORD IAW EA 400-54EA-10558.

Part: TRANSITION PANEL — GOUGED (BS 500A-500B) · airframe 65,323 hrs · 37,698 cycles

FWD CARGO BAY LT TRANSITION PANEL BETWEEN BS 500A AND 500B GOUGED AT FASTENER HOLE. REMOVED, FABRICATED NEW AND REPLACED TRANSITION PANEL IAW SRM 53-30-53-2R3, FIG 201.

Part: SKIN — DENTED (BS 219) · airframe 65,323 hrs · 37,698 cycles

RT FUSELAGE SKIN IS DENTED 3 INCHES BELOW EXTERNAL POWER DOOR CUTOUT. ACFT GROUNDED. REPAIRED SKIN IAW EA 400-53EA-10536.

Part: SHEAR TIE — CORRODED (BS 500D) · airframe 65,323 hrs · 37,698 cycles

FWD CARGO BS 500D S26-27L FWD SIDE OF SHEAR TIE CORRODED. REPAIRED SHEAR TIE IAW SRM 53-00-07-2R-3. THIS IS A CAT B REPAIR.

Part: SKIN — CHAFED (RT WING) · airframe 65,323 hrs · 37,698 cycles

RIGHT WING INBD BOOST PUMP CUTOUT HAS MINOR CHAFING. ACFT GROUNDED. REPAIRED CHAFING IAW SRM 57-20-01-2R-6.

Part: TRANSITION PANEL — CORRODED (BS 500C-500G) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

FWD CARGO COMP RT TRANSITION PANEL CORRODED IN SEVERAL AREAS FROM STA 500C TO 500G. REMOVED CORROSION AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-53-1A-1, FIG 101. R & R TRANSITION PANEL IAW SRM 51-40-02-0G-0.

Part: SKIN — DENTED (BS 418) · airframe 65,323 hrs · 37,698 cycles

RIGHT FUSELAGE BS 418, SKIN HAS A PROTRUSION 2 INCHES ABOVE S27R. ACFT GROUNDED. REPAIRED DENT IAW EA 400-53EA-10552, REV NEW DATE ISSUED 6-21-13.

Part: TRANSITION PANEL — CORRODED (BS 380-420) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

FWD CARGO COMP RT TRANSITION PANEL CORRODED IN SEVERAL AREAS FROM BS 500C TO 500G. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-53-1A-1, FIG 101. R & R TRANSITION PANEL IAW SRM 51-40-02-0G-0, W 2. O .040, R .033, L 24, D .007.

Part: SKIN — DENTED (BS 202) · airframe 65,323 hrs · 37,698 cycles

RT FUSELAGE, BS 202, SKIN IS DENTED 9 INCHES FROM FWD ACCY BAY CUTOUT. ACFT GROUNDED. C/W EA 400-53EA-10508, REV NEW DATE ISSUED 6-13-13.

Part: FLOOR SUPPORT — GOUGED (BS 500B) · airframe 65,323 hrs · 37,698 cycles

FWD CARGO BAY JUST AFT BS 500B, ABOVE 28L, FLOOR SUPPORT GOUGED ON CORNER. REMOVED DAMAGE AND CHECKED LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 53-30-53-1A-1, FIG 101. REPAIRED CARGO FLOOR SUPPORT IAW SRM 53-00-53.

Part: SUPPORT BEAM — CHAFED (NR 1 NACELLE) · airframe 65,323 hrs · 37,698 cycles

NR 1 ENG PYLON FAN COWL SUPPORT BEAM INBD CHORD CHAFED. ACFT GROUNDED. REPAIRED NR 1 ENG PYLON INBD FAN COWL SUPPORT BEAM IAW ASA EA NR 400 54EA 10557.

Part: SKIN — CHAFED (THRUST REVERSER) · airframe 65,323 hrs · 37,698 cycles

NR 2 ENGINE INBD THRUST REVERSER FORWARD TORQUE BOX UPPER SKIN SECTION HAS A CHAFED AREA ON THE BACK SIDE. ACFT GROUNDED. REPAIRED UPPER TORQUE BOX SKIN IAW EA 400-78EA-10563, REV NEW ISSUE DATE 6-25-13.

Part: STRUCTURE — CHAFED (NR 4 SLAT) · airframe 65,323 hrs · 37,698 cycles

NR 4 SLAT INBD T/E EDGE IS CHAFED ON THE BOTTOM SIDE. ACFT GROUNDED. REPAIRED CHAFED ON NR 4 SLAT INDB T/E EDGE IAW SRM 51-70-10-2R 0. REPAIR 4, PARA 20, PG 48.

Part: ANGLE — CORRODED (BS 685-691) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

LT WHEEL WELL MANIFOLD ASSY LOWER AFT CHORD TO LOWER CENTER CHORD SPLICE PLATE CORRODED. ACFT GROUNDED. REMOVED LT WHEEL WELL MANIFOLD LOWER AFT CHORD SPLICE PLATE ANGLE FABRICATED NEW ANGLE TREATED, PRIMED, TOPCOATED AND INSTALLED IAW SRM 51-30-01-0G 0, FIG 7, 51-40-02 AND AMM 51-21-21-307-014 AND 51-21-99-307-001 .

Part: ANGLE — CORRODED (BS 687-702) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

LT WHEEL WELL MANIFOLD ASSY LOWER AFT ANGLE CORRODED ON VERTICAL AND HORIZ FLANGE. ACFT GROUNDED. REMOVED LT WHEEL WELL MANIFOLD LWR AFT CHORD FABRICATED NEW CHORD TREATED, PRIMED AND TOPCOATED AND INSTALLED IAW SRM 51-30-01-0G-0 FIG 7, 51-40-02-0G 0 AND AMM 20-50-11-912-002, FIG 201 USING T/W 515293, 51-21-21-307-014 AND 51-21-99-307-001.

Part: CLOSEOUT PANEL — CHAFED (RT WING) · airframe 65,323 hrs · 37,698 cycles

RIGHT T/E CLOSE OUT PANEL CHAFED ON OTBD NR 6 FAIRING. ACFT GROUNDED. REMOVED, FABRICATED AND INSTALLED NEW CLOSEOUT PANEL IAW SRM 51-40-02 AND DWG 65-69646 AND MM 20-50-11-912-002.

Part: SKIN — CHAFED (THRUST REVERSER) · airframe 65,323 hrs · 37,698 cycles

NR 1 ENGINE OTBD THRUST REVERSER FWD TORQUE BOX UPPER SKIN HAS AREAS CHAFED ON BACK SURFACE. ACFT GROUNDED. REPAIRED SKIN IAW EA 400-78EA-10569, REV NEW ISSUE DATE 6/25/13.

Part: SKIN — CHAFED (THRUST REVERSER) · airframe 65,323 hrs · 37,698 cycles

LEFT INBD THRUST REVERSER FWD TORQUE BOX SKIN UPPER SECTION HAS A CHAFE AREA ON BACK SIDE. REPAIRED NR1 ENGINE. INBD FWD TORQUE BOX SKIN IAW ASA EA400-78EA-10560.

Part: FAIRING — CHAFED (NR 6 FLAP) · airframe 65,323 hrs · 37,698 cycles

NR 6 FLAP FAIRING IF OT LANDING CHAFED. ACFT GROUNDED. REMOVED AND INSTALLED NEW STIFFENER AND DOUBLER IAW SRM 51-40-02-0G 0.

Part: FLANGE — CORRODED (BS 676-688) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

LT WHEEL WELL MANIFOLD ASSY LWR FWD CHORD HAS FRETTING CORROSION ON LOWER FLANGE. ACFT GROUNDED. REMOVED LT WHEEL WELL MANIFOLD LWR FWD CHORD FABRICATED NEW CHORD TREATED, PRIMED AND TOP COATED AND INSTALLED IAW SRM 51-30-01-0G-0, FIG 7, 51-40-02 0G-0 AND AMM 20-50-11-912-002, FIG 203 USING T/W 515293, 51-21-21-307-014 AND 51-21-99 307-001.

Part: SUPPORT BEAM — CORRODED (BS 311-344) · corrosion level 2 · airframe 65,323 hrs · 37,698 cycles

FWD ENTRY DOOR THESHOLD INNER SUPPORT CORRODED NEAR FWD AND AFT END. ACFT GROUNDED. REMOVED ENTRY DOOR THRESHOLD INNER SUPPORT AND REPLACED WITH NEW SUPPORT IAW SRM 51-40-02, FIG 8 AND 51-40-05, FIG 3, W .75, O .080, R .069, L 2.0, D .011.

Part: SUPPORT BRACKET — DAMAGED (NR 1 FLAP) · airframe 65,323 hrs · 37,698 cycles

NR 1 FLAP FAIRING SUPPORT BRACKET HAS BARE METAL AND PITTING. ACFT GROUNDED. REMOVED DAMAGED NR 1 FAIRING LOWER SUPPORT BRACKET, FABBED, INSTALLED NEW LWR SUPPORT BRACKET IAW SRM 51-40-02, 51-40-05.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 65,323 hrs · 37,698 cycles

LT OTBD AFT FLAP CHAFED NR 1 FLAP FAIRING LANDING. REPAIRED LT OTBD AFT FLAP CHAFED AT NR 1 FLAP FAIRING LANDING IAW SRM 51-70-10-2R-4, REPAIR 4. (PERMANENT REPAIR)

Part: REVEAL — CHAFED (BS 794) · airframe 65,323 hrs · 37,698 cycles

AFT CARGO BAY FWD REVEAL HAS EDGE DAMAGE, FABRICATED NEW REVEAL IAW SRM 51-40-05 AND DWG 65-56655.

Part: SKIN PANEL — CHAFED (BS 440-546) · airframe 65,323 hrs · 37,698 cycles

SKIN PANEL 6308 IS CHAFED. ACFT GROUNDED. BLENDED SKIN PANEL AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-70-1A-1, FIG 101. NEW PANEL, LOCATED AND DRILLED IAW DWG 65-79917.

Part: FLOOR PANEL — GOUGED · airframe 65,323 hrs · 37,698 cycles

AFT CARGO BAY FLOOR PANEL NR2 HAS A DEEP GOUGE. ACFT GROUNDED. FABRICATED NEW AFT CARGO BAY FLOOR PANEL NR2 IAW SRM 51-40-08-0G-0 AND RESTORED FINISH IAW SRM 51-20-01-0G-0.

Part: FLOOR PANEL — GOUGED (FWD CARGO) · airframe 65,323 hrs · 37,698 cycles

FWD CARGO BAY FLOOR PANEL NR 3 HAS DEEP GOUGE. ACFT GROUNDED. FABRICATED NEW FLOOR PANEL IAW SRM 51-40-05-0G-0.

Part: SKIN — DELAMINATED (SLAT) · airframe 65,323 hrs · 37,698 cycles

RT WING 5 SLAT OTBD T/E IS DELAMINATED. REPAIRED RT WING NR 5 SLAT OTBD T/E DELAMINATION IAW SRM 51-70-10-2R-4, REPAIR 4, PG 1.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 65,323 hrs · 37,698 cycles

AFT CARGO BAY FLOOR PANEL NR 4 IS DAMAGED AT EDGE. ACFT GROUNDED. FABRICATED NEW FLOOR PANEL IAW SRM 51-40-05-0G-0.

Part: SPINDLE — CORRODED (FLAP CARRIAGE) · corrosion level 2 · airframe 63,001 hrs · 36,355 cycles

CORROSION FOUND ON SPINDLE DURING INSPECTION, T/C, AD 20121307-400-57 ON THE NR 8 FLAP CARRIAGE SPINDLE, PN 65-46481-122, SN B5159. ACFT GROUNDED. REPLACED NR 8 FLAP CARRIAGE ASSY.

Part: HOUSING — GOUGED (AFT CARGO DOOR) · airframe 62,742 hrs · 36,194 cycles

AFT CARGO PIT BUMPER MISSING AND HOUSING GOUGED. HANDLE HOUSING GOUGE MEASURES GREATER THEN .060. REMOVED HANDLE ASSY FOR ACCESS TO HOUSING. REMOVED DAMAGE HOUSING AND INSTALLED NEW REF SRM 51-40-02. PRIMED AND PAINTED AREA REF AMM 51-21-99. INSTALLED INSIDE AND OUTSIDE DOOR HANDLE REF 52-31-14-004-054. OPS CK OK.

Part: BUMPER — OUT OF POSITION (L2 WINDOW) · airframe 61,670 hrs · 35,540 cycles

CAPT SLIDING WINDOW DIFFICULT TO OPEN AND CLOSE. FOUND CAPT SLIDING WINDOW INTERFERING WITH UPPER CRASH PAD REPOSITIONED UPPER CRASH PAD REF B737 400 AMM 20 50 11.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 61,669 hrs · 35,539 cycles

RIGHT OTBD AFT FLAP INBD TRAILING EDGE FOUND TO BE DELAMINATED. REPAIRED IAW SRM 51-70-10 REPAIR 2.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 38,476 hrs · 17,043 cycles

LONGITUDINAL FLOORBEAM AT RBL 45.5 STA 727B 20A CRACKS .375 LONG. REPAIRED LONGITUDINAL FLOORBEAM RBL 45.5 STA 727B IAW ALASKA AIRLINES EA AD20080506 400 57 108.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,669 hrs · 35,539 cycles

STA 500B LEFT SIDE WIRE PENETRATION HOLE CRACKED INBD SIDE FRONT AND AFT. REPAIRED FRAME STA 500B LEFT SIDE IAW B737 400 SRM 53 00 07 REPAIR 13.

Part: FRAME — CRACKED (BS 500F) · airframe 61,669 hrs · 35,539 cycles

BS 500F FRAME RIGHT STANDOFF TOOLING HOLE IS CRACKED I/B SIDE. REPAIRED FRAME IAW EA 400-53EA-07463.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,669 hrs · 35,539 cycles

STA 500E RIGHT SIDE WIRE PENETRATION HOLE CRACKED INBD SIDE FRONT AND AFT. REPAIRED FRAME AT 500E RT SIDE IAW B737 400 SRM 53 00 07 REPAIR 13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,669 hrs · 35,539 cycles

STA 500C LT SIDE WIRE PENETRATION HOLE IS CRACKED I/B AFT SIDE. REPAIRED FRAM STA 500C LT SIDE IAW B737 400 SRM 53 00 0 REPAIR 13.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,021 hrs · 35,123 cycles

POSSIBLE CRACK IN FUSELAGE CUTOUT AFT SIDE FOR EQUIPMENT COOLING EXHAUST. REMOVED CRACK DAMAGE ON FUSELAGE SKIN BS 360 BS 400 STR 27L 28R ANIC AD 2009 19 25. REPAIRED PER EA 400 53 EA 06525.

Part: DOOR — OUT OF ADJUST (L1) · airframe 34,547 hrs · 60,073 cycles

L1 DOOR VERY HARD TO OPEN & CLOSE. ADJUSTED L1 DOOR PER B737 400 AMM 52 11 00 705 007 STEPS E G(19). DOOR OPENING/CLOSING FORCES WITHIN LIMITS.

Part: SKIN — CRACKED (L2 DOOR) · airframe 58,759 hrs · 33,776 cycles

L2 DOOR UPPER HINGE CUTOUT IS CRACKED APPROX 1 INCH. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED REPAIR IAW B737 400 SRM 53 60 01 REPAIR 5.

Part: SLAT — DELAMINATED (WING) · airframe 58,491 hrs · 33,625 cycles

NR 2 SLAT INBOARD AFT UPPER CORNER PREVIOUS REPAIR DELAMINATED. REMOVED DAMAGED AREA. FABRICATED TREATED PRIMED AND BONDED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DAMAGED (E&E DOOR) · airframe 58,491 hrs · 33,625 cycles

E&E DOOR SKIN HAS DAMAGE ON RT SIDE. REPAIRED E&E DOOR SKIN.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,491 hrs · 33,625 cycles

STRINGER CLIP CRACKED AT STA 500D STRINGER 10L. REMOVED AND INSTALLED NEW STRINGER CLIP.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,491 hrs · 33,625 cycles

STRINGER CLIP CRACKED AT STA 500F STRINGER 10L. REMOVED AND INSTALLED NEW STRINGER CLIP.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 58,491 hrs · 33,625 cycles

LT MLG CENTER DOOR HAS CHAFE MARKS AT FWD AND AFT ENDS. REPAIRED DOOR.

Part: SKIN — CHAFED (FOREFLAP) · airframe 58,491 hrs · 33,625 cycles

RIGHT O/B FOREFLAP INBOARD LEADING EDGE CHAFED. REPAIRED FOREFLAP.

Part: SKIN — DENTED (FUSELAGE) · airframe 58,491 hrs · 33,625 cycles

DENT AT STA 1088 INBOARD OF TAIL JACK POINT FOUND TO BE WITHIN 3 INCHES OF SKIN SPLICE & WITHIN 3 INCHES OF CUTOUT (JACK POINT) & FOUND TO BE OVER STRUCTURE. ACCOMPLISHED SKIN REPAIR AT AFT JACK POINT IAW B737 400 SRM 53 80 01 FIG 201 REPAIR 4.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,393 hrs · 10,420 cycles

R2 DOOR LOWER CORNER OF FUSELAGE CRACKED. REMOVED CRACK INSTALLED REPAIR.

Part: SKIN — CRACKED (BS 964 S17R) · airframe 58,104 hrs · 33,393 cycles

R2 DOOR LOWER CORNER OF FUSELAGE CRACKED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,008 hrs · 32,729 cycles

CRACK ON FUSELAGE SKIN 2 INCHES AFT OF BS 727D BELOW STR 23L. REPAIRED CRACK 2 INCHES AFT OF BS 727D BELOW STR 23L.

Part: SKIN — DAMAGED (RUDDER) · airframe 55,882 hrs · 32,048 cycles

RUDDER COUNTERWEIGHT UPPER SURFACE SKIN DAMAGED. REPAIRED COUNTERWEIGHT UPPER SURFACE SKIN.

Part: WEDGE — CHAFED (LE SLAT) · airframe 55,743 hrs · 31,958 cycles

NR 4 SLAT T/E WEDGE LOWER SURFACE IS CHAFED. REPAIRED NR 4 SLAT T/E WEDGE PER SRM 57 43 02.

Part: SKIN — CHAFED (LE SLAT) · airframe 55,743 hrs · 31,958 cycles

NR 3 SLAT UPPER TRAILING EDGE LOWER SURFACE IS CHAFED FROM CONTACT WITH FIXED LEADING EDGE. REPAIRED NR 3 SLAT TRAILING EDGE PER SRM 57 43 02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,743 hrs · 31,958 cycles

INTERCOSTAL L-ANGLE CRACKED A FWD ENTRY DOOR WAY BS 300 STR 13L. REMOVED AND REPLACED ANGLE, ACCOMPLISED REPAIR PER ER 09 4345 ASA EA 400 53EA 02133.

Part: FORMER — CHAFED (RT WING) · airframe 55,743 hrs · 31,958 cycles

FAIRING FORMER AT RT WING UPPER TRAILING NO STEP PANEL ATTACH POINT IS CHAFED, LOCATED ABOVE NR 5 FLAP TRACK. REPLACED FORMER PER SRM 51 40 2.

Part: SUPPORT — DAMAGED (FUSELAGE) · airframe 55,743 hrs · 31,958 cycles

ELONGATED HOLE IN AFT FAIRING SUPPORT LEFT SIDE. REPLACED ATTACHED SUPPORT.

Part: SUPPORT ANGLE — DAMAGED (FUSELAGE) · airframe 55,743 hrs · 31,958 cycles

LEFT WING TO BODY STRUCTURE HAS ELONGATED HOLE COMMON TO LOWER SUPPORT ANGLE HOLE. REPAIRED PER EA.

Part: SUPPORT — CHAFED (NR 1 PYLON) · airframe 55,743 hrs · 31,958 cycles

LEFT WING AFT NR 1 PYLON LWR DRAIN INNER SUPPORT FOR DRAIN HAS FASTENERS CHAFED THROUGH INNER STRUCTURE. REPAIRED PER EA.

Part: CARGO TRACK — CORRODED (BS 940) · airframe 55,743 hrs · 31,958 cycles

CORROSION ON CARGO TRACK BS 940 LBL 17 WL 156. REMOVED CARGO TRACK FABRICATED NEW TRACK AND INSTALLED

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 55,743 hrs · 31,958 cycles

LEFT WING O/B FORE FLAP L/E SKIN O/B EDGE TO 1.75 AND 3 INCHES FROM LWR AFT EDGE OF BULLNOSE THERE IS A CHAFED AREA. REPAIRED LT WING O/B FORE FLAP L/E SKIN O/B EDGE TO 1.75 AND 3 INCHES FROM LWR AFT EDGE OF BULLNOSE.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 55,743 hrs · 31,958 cycles

LEFT WING O/B FORE FLAP L/E SKIN I/B EDGE TO 15 INCHES AND 7.5 INCHES FROM LWR AFT EDGE OF BULLNOSE THERE IS A CHAFED AREA. REPAIRED LT WING O/B FORE FLAP L/E SKIN O/B EDGE TO 15 INCHES AND 7.5 INCHES FROM LWR AFT EDGE OF BULLNOSE.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 55,743 hrs · 31,958 cycles

RIGHT WING O/B FORE FLAP L/E SKIN I/B EDGE TO 1.25 INCHES AND 7.5 INCHES FROM LWR AFT EDGE OF BULLNOSE THERE IS A CHAFED AREA. REPAIRED RIGHT WING OB FORE FLAP LE SKIN I/B EDGE TO 1.25 INCHES AND 7.5 INCHES FROM LWR AFT EDGE OF BULLNOSE.

Part: SUPPORT ANGLE — CRACKED (TE FLAP) · airframe 55,743 hrs · 31,958 cycles

SUPPORT ANGLE IS CRACKED T/E LEFT WING WBL 204. REPLACED SUPPORT ANGLE.

Part: PANEL — DENTED (RT WING TE FLAP) · airframe 55,743 hrs · 31,958 cycles

RIGHT WING I/B MAIN FLAP T/E PANEL HAS 2 DENTS THAT ARE OUT OF LIMITS ON THE LOWER SURFACE. REPAIRED DENTS.

Part: BEAR STRAP — CRACKED (BS 303) · airframe 55,743 hrs · 31,958 cycles

BEAR STRAP CRACKED AT FWD ENTRY DOOR LOWER HINGE CUTOUT. TRIMMED OUT CRACK, REPAIRED AREA PER ER 09-4345 & EA 400-53EA-02133.

Part: SKIN — DENTED (FUSELAGE) · airframe 55,743 hrs · 31,958 cycles

DENT IN FUSELAGE SKIN AT A PREVIOUS REPAIR. REMOVED PREVIOUS REPAIRS AND REPAIRED.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 55,743 hrs · 31,958 cycles

LEFT I/B FORE FLAP T/E WEDGE LOWER SKIN IS DENTED AND DELAMINATED 28 INCHES FROM O/B END, 9 INCHES FROM T/E. REPAIRED SKIN.

Part: SKIN PANEL — CHAFED (MIDFLAP) · airframe 55,743 hrs · 31,958 cycles

LEFT O/B MID FLAP LOWER AFT PANEL UPPER SURFACE ADJACENT TO THE O/B AFT FLAP TRACK IS CHAFED. REPAIRED PER SRM.

Part: SKIN — DENTED (FOREFLAP) · airframe 55,743 hrs · 31,958 cycles

LEFT O/B FORE FLAP LOWER SKIN 20 INCHES FROM I/B EDGE 2 INCHES FROM AFT EDGE IS DENTED. REPAIRED IAW SRM.

Part: SKIN — CHAFED (FOREFLAP) · airframe 55,743 hrs · 31,958 cycles

LEFT O/B FORE FLAP UPPER SKIN 9 INCHES, 2 INCHES FROM I/B. 4.5 INCHES FROM T/E IS CHAFED AT PREVIOUS REPAIR. REPAIRED FLAP SKIN.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 55,743 hrs · 31,958 cycles

LEFT O/B FORE FLAP LOWER SKIN 1.5 INCHES, 2 INCHES FROM TRAILING EDGE, 2 3 INCHES FROM I/B EDGE IS A DELAMINATED AREA. REPAIRED FLAP SKIN.

Part: WEDGE — DELAMINATED (NR 5 LE SLAT) · airframe 55,743 hrs · 31,958 cycles

NR 5 T/E WEDGE IS DELAMINATED 2 INCHES FROM I/B END UPPER SURFACE ON PREVIOUS REPAIR. REPAIRED NR 5 SLAT T/E WEDGE PER SRM 57-43-02.

Part: HINGE — LACK OF LUBE (L1 DOOR) · airframe 55,071 hrs · 31,554 cycles

F/A REPORTS MAIN CABIN ENTRY DOOR MAKES GROANING NOISE AND IS DIFFICULT FOR F/A TO OPEN AND CLOSE, CAPT CONCURS. LUBED DOOR HINGES, CHECKED DOOR OPS NORMAL REF MM 52 11 00 705 0650.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 54,367 hrs · 31,067 cycles

RUST ON NR 7 FLAP TRACK BEARING CONTACT SURFACES. REMOVED CORROSION AND TREATED IAW EA 400 57EA 00306.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 54,367 hrs · 31,067 cycles

RUST ON NR 2 FLAP TRACK BEARING CONTACT SURFACES. REMOVED CORROSION AND TREATED IAW EA 400 57EA 00306.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 54,367 hrs · 31,067 cycles

RUST ON NR 8 FLAP TRACK BEARING CONTACT SURFACES. REMOVED CORROSION AND TREATED IAW EA 400 57EA 00306.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 54,367 hrs · 31,067 cycles

RUST ON NR 1 FLAP TRACK BEARING CONTACT SURFACES. REMOVED CORROSION AND TREATED IAW EA 400 57EA 00306.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

DOUBLE DRILLED HOLE FOUND ON STRINGER FLANGE. REPAIRED PER SRM 53 00 01.

Part: SILL — DAMAGED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

AFT CARGO BAY DOOR LOWER SILL CHANNEL HAS TWO DRILL MARKS. REPLACED SILL PER SRM 51 40 05 AND 51 40 02.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

DOUBLE DRILLED HOLE ON STRINGER FLANGE. REPAIRED HOLE PER SRM 51 70 11.

Part: WEB — CRACKED (BS 986-1015) · airframe 52,370 hrs · 29,962 cycles

SHEAR WEB AT BS 986 TO BS 1015 RT IS CRACKED. SHEAR WEB REPLACED WITH FABRICATED PART IAW B737 400 SRM 52 60 51 SRM 51 40 05 AND 51 21 00.

Part: SEAT TRACK — WORN (CABIN) · airframe 52,370 hrs · 29,962 cycles

SEAT TRACK WORN. REPLACED TRACK PER SRM 53 00 52.

Part: PANEL — DENTED (NR 2 SPOILER) · airframe 52,370 hrs · 29,962 cycles

NR 2 SPOILER EVIDENCE OF DENT AT I/B LOWER AREA OF ACTUATOR LUG ATTACHMENT. NR 2 SPOILER PANEL REPLACED WITH NEW SERVICEABLE FLIGHT SPOILER PANEL IAW B737 400 AMM TASK 27 61 11 404 010 PARA F STEPS 1 16.

Part: BEAM — CRACKED (BS 616) · airframe 52,370 hrs · 29,962 cycles

RT SIDE BS 616 STUB BEAM CHORD CRACKED AT FASTENER HOLE. REPAIRED STUB BEAM CHORD IAW EO5310 02528 SECTION 6.

Part: FLOOR SUPPORT — CRACKED (BS 380-400) · airframe 52,370 hrs · 29,962 cycles

PASSENGER CABIN FLOOR STRUCTURE AT BS380 400 BL0 UPPER ANGLE IS CRACKED AT 3 FASTENER HOLES. REPLACED CABIN FLOOR UPPER ANGLE WITH NEW PART IAW B737 400 SRM 51 40 05 AND 51 40 02.

Part: BEAM — CRACKED (BS 616) · airframe 52,370 hrs · 29,962 cycles

LT SIDE BS616 STUB BEAM CHORD CRACKED AT FASTENER HOLE. REPAIRED IAW EO5310 02528 SECTION 5.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

STRINGER SHEAR TIE PREVIOUS REPAIR CORRODED. REPAIRED PER SRM 53 00 07.

Part: FRAME — DENTED (BS 727C S24-25R) · airframe 52,370 hrs · 29,962 cycles

AFT CARGO PIT BS 727C BETWEEN STR 24R AND 25R TOP FLANGE OF FRAME DENTED. FRAME REPAIRED WITH REPAIR PART IAW B737 400 SRM 51 70 11.

Part: FRAME — DENTED (BS 727E S22-23L) · airframe 52,370 hrs · 29,962 cycles

AFT CARGO PIT BS 727E BETWEEN STR 22L AND 23L TOP FLANGE OF FRAME DENTED. FRAME REPAIRED WITH REPAIR PART IAW B737 400 SRM 51 70 11.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

AFT CARGO PIT DOORWAY LWR AFT CORNER BS 847 MISDRILLED HOLE. AFT CARGO PIT DOORWAY LWR AFT CORNER BS 847 REPAIRED IAW RO 8463 AND ASA EA 5330 02356. ACCOMPLISHED INITIAL INSPECTION OF THE SUBJECT AREA AT 50 000 TOTAL FLIGHT CYCLES. CONTACT ENGINEERING FOR DEFINITION OF INSPECTION METHODS REPEAT INTERVAL.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 52,370 hrs · 29,962 cycles

NR 5 SPOILER LOWER SURFACE IS DENTED. REPAIRED PER SRM 51 70 10.

Part: SKIN — DENTED (BS 373-377) · airframe 52,370 hrs · 29,962 cycles

DENTS AT BS 374, 5 INCHES BELOW STR 32L AND BS 377.5 2 INCHES BELOW STR 24L. DENTS REPAIRED IAW B737 400 SRM 53 00 01 REPAIR 31 FIG 201 TR 53 27.

Part: SKIN — DENTED (BS 500) · airframe 52,370 hrs · 29,962 cycles

DENTS AT LT LOWER EXTERIOR AT BS 500 STR 26 TO 27L. REPAIRED WITH REPAIR PART.

Part: SPAR — CRACKED (CENTER WING) · airframe 52,370 hrs · 29,962 cycles

BS 663.75 WING CENTER SECTION REAR SPAR LOWER RIGHT WEB (COMPOSITE PANEL) CRACKED. WING CENTER SECTION REAR SPAR AT BS 663.75 LOWER RIGHT WEB CRACK REPAIRED PER SRM 51 70 04 REPAIR NR 10.

Part: NONE — NONE · airframe 52,370 hrs · 29,962 cycles

CARRY OUT PREVENT MOD ON BS 348.2 TO BS 360 STR 16 PER EM 5310 02389 STEP 4. CARRY OUT PREVENT MOD ON BS 348.2 TO BS 360 STR 16 PER EM 5310 02389 STEP 4.

Part: STRINGER CLIP — GOUGED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

STRINGER TIE CLIP GOUGED. REPLACED CLIP PER SRM 51 40 02 51 30 01 AND DWG 65 46569.

Part: SKIN — DENTED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

FUSELAGE SKIN DENT. REPAIRED PER SRM 53 00 01 AND EA 5330 02357.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

STRINGER TIE CLIP CRACKED. REPLACED CLIP PER SRM 51 40 02.

Part: SKIN — DENTED (BS 500A-500B) · airframe 52,370 hrs · 29,962 cycles

DENT OF LT LOWER FUSELAGE EXTERIOR BS 500A TO BS 500B STR25 TO STR26. DAMAGE REPAIRED IAW B737 400 SRM 53 00 01.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

STRINGER TIE CLIP CRACKED. REPLACED CLIP PER SRM 51 40 02.

Part: SKIN — DENTED (BS 480-500) · airframe 52,370 hrs · 29,962 cycles

DENTS AT BS 480 500 STR 25L 26L. REPAIRED WITH REPAIR PART.

Part: SKIN — DENTED (BS 500E-500F) · airframe 52,370 hrs · 29,962 cycles

LT LOWER FUSELAGE EXTERIOR DENTED AT STA 500E TO 500F STR 26 TO 27. REPAIRED DENT IAW B737 400 SRM TR53 27 REPAIR 31 FIG 201.

Part: SKIN — DENTED (BS 500-500A) · airframe 52,370 hrs · 29,962 cycles

DENT ON LT LOWER FUSEALGE AT BS 500 TO 500A STR 25 TO 26. REPAIR WORK ACCOMPLISHED IAW B737 400 SRM 53 00 01.

Part: INTERCOSTAL — CRACKED (BS 303 S4L) · airframe 52,370 hrs · 29,962 cycles

CRACKED INTERCOSTAL COMMON TO UPPER SILL BEAM STRAP STA 303 STR4L. REPAIRED WITH REPAIR PART.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,370 hrs · 29,962 cycles

APU COMPARTMENT TORQUE BOX STRINGER CORRODED. REPLACED STRINGER PER SRM 51 40 02.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

E&E COMPARTMENT BS 380 STR 22L TIE CLIP CRACKED. E&E COMPARTMENT BS 380 STR 22L TIE CLIP REPLACED IAW B737 400 SRM 51 40 02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,370 hrs · 29,962 cycles

FLOORBEAM UPPER FLANGE IS CORRODED. REPLACED BEAM PER EA 5310 02800.

Part: SUPPORT CHANNEL — CRACKED (BS 303-325 S17L) · corrosion level 1 · airframe 52,370 hrs · 29,962 cycles

L1 DOOR SILL INNER SUPPORT CORRODED ON SURFACE AND CRACKED. INSTALLED NEW CHANNEL IAW B737 400 SRM 51 40 02.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,370 hrs · 29,962 cycles

AFT CARGO PIT BS 767 BETWEEN 25R AND 26R LOWER FLANGE OF FRAME (AFT SIDE) HAS CORROSION. AFT CARGO PIT B767 BETWEEN STRINGER 25R 26R LOWER FLANGE REPAIRED IAW B737 400 SRM 51 70 11. REPAIRED WITH REPAIR PART.

Part: FRAME — CRACKED (BS 787) · airframe 52,370 hrs · 29,962 cycles

LT FRAME AT STA 787 CRACKED AT PSU RAIL BRACKET. FRAME REPAIRED IAW ASA EA5310 02797.

Part: CARGO TRACK — BROKEN (BS 450-500) · airframe 52,370 hrs · 29,962 cycles

FWD CARGO PIT TIE DOWN TRACK TIE DOWN POINT BROKEN OUT. TIE DOWN POINT REPAIRED IAW SRM 53 00 53 REPAIR 2 FIG 201.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

LEFT FRAME AT STA 867 CRACKED AT PSU RAIL BRACKET REPAIR PER EA 5310 02797.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

RT FRAME AT STA 907 CRACKED AT PSU RAIL BRACKET. FRAME REPAIRED IAW ASA EA5310 02797.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

RIGHT FRAME AT STATION 480 CRACKED AT PSU RAIL BRACKET. RIGHT FRAME AT STATION 480 AT PSU RAIL BRACKET REPAIRED IAW CASCADE ERO 8337 ASA EA 5310 02797.

Part: FRAME — CRACKED (BS 440 S8-9L) · airframe 52,370 hrs · 29,962 cycles

LT SIDE FRAME AT STA 440 CRACKED AT PSU RAIL BRACKET. REPAIRED FRAME IAW ASA EA5310 02797.

Part: FRAME — CRACKED (BS 827) · airframe 52,370 hrs · 29,962 cycles

RT FRAME AT STA827 CRACKED AT PSU RAIL BRACKET. FRAME REPAIRED IAW ASA EA5310 02797.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

RIGHT FRAME AT STA 867 CRACKED AT PSU RAIL BRACKET. REPAIRED PER EA 5310 02797.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

FRAME CRACKED AT PSU RAIL BRACKET. REPAIRED FRAME PER EA 5310 02797.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

LEFT FRAME AT STA 827 CRACKED AT PSU RAIL BRACKET. LEFT FRAME AT STA 827 AT PSU BRACKET REPAIRED IAW CASCADE ERO 8337 & ASA EA 5310 02797.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

RIGHT FRAME AT STATION 500A CRACKED AT PSU RAIL BRACKET. RIGHT FRAME AT STATION 500A AT PSU RAIL BRACKET REPAIRED IAW CASCADE ERO 8337 AND ASA EA 5310 02797.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

LT SIDE FRAME AT STA 727F CRACK AT PSU RAIL BRACKET. FRAME REPAIRED IAW ASA EA5310 02797.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

LEFT SIDE FRAME AT STA 747 CRACKED AT PSU RAIL BRACKET. LEFT SIDE FRAME AT STA 747 AT PSU RAIL BRACKET REPAIRED IAW ERO 8337 & ASA EA 5310 02797 REF CERT 11678.

Part: FRAME — CRACKED (BS 500A S8-9L) · airframe 52,370 hrs · 29,962 cycles

LT SIDE FRAME AT STA 500A CRACKED AT PSU RAIL BRACKET. FRAME REPAIRED IAW ASA EA5310 02797.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

RIGHT FRAME AT STA 787 CRACKED AT PSU RAIL BRACKET. REPAIRED PER EA 5310 02797.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

RIGHT FRAME AT PSU RAIL BRACKET CRACKED REPAIR PER EA 5310 02747.

Part: FRAME — CRACKED (BS 727D S8-9L) · airframe 52,370 hrs · 29,962 cycles

LT SIDE FRAME AT STA 727D CRACKED AT PSU RAIL BRACKET. FRAME REPAIRED IAW ASA EA5310 02797.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

RIGHT FRAME AT STA 440 CRACKED AT PSU RAIL BRACKET. REPAIRED PER EA 5310 02797.

Part: FRAME — CRACKED (BS 360) · airframe 52,370 hrs · 29,962 cycles

LT FRAME AT STA 360 CRACKED AT PSU RAIL BRACKET. REPAIRED IAW EA5310 02797.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

RIGHT FRAME AT STA 747 AT PSU RAIL BRACKET CRACKED. REPAIRED PER EA 5310 02797.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

RIGHT FRAME AT STA 727B CRACKED AT PSU RAIL BRACKET. RIGHT FRAME AT STA 727B AT PSU RAIL BRACKET REPAIRED IAW CASCADE ERO 8337 ASA EA 5310 02797.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

RIGHT FRAME AT STA 380 CRACKED AT PSU RAIL BRACKET. RIGHT FRAME AT STA 380 PSU RAIL BRACKET REPAIRED IAW CASCADE ERO 8337 AND ASA EA 5310 02797.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

FRAME CRACKED. REPAIRED FRAME PER EA 5310 02797.

Part: FRAME — CRACKED (BS 907) · airframe 52,370 hrs · 29,962 cycles

LT FRAME AT STA 907 CRACKED AT PSU RAIL BRACKET. FRAME REPAIRED IAW ASA EA5310 02797.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

AFT CARGO PIT BS 727C BW STR 24R 25R TOP FLANGE OF FRAME DENTED. AFT CARGO PIT FRAME BS 727C STR 24R 25R REPAIRED IAW B737 400 SRM 51 70 11.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,370 hrs · 29,962 cycles

FRAME TO SKIN ATTACH ANGLE CORRODED IN AFT BILGE AREA. REPAIRED PER SRM 53 00 07.

Part: BEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,370 hrs · 29,962 cycles

BEAR STRAP CORRODED IN AFT CARGO BAY AREA. REPAIR STRAP PER EA 5330 02357.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,370 hrs · 29,962 cycles

FORWARD CARGO BAY DOOR SILL PLATE CORRODED. REPLACED SILL PLATE PER SRM 51 40 05.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

AFT CARGO PIT BS 727E AT STR 24R FRAME DENTED ON TOP FLANGE. AFT CARGO PIT BS 727E AT STR 24R FRAME REPAIRED IAW B737 400 SRM 51 70 11.

Part: BEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,370 hrs · 29,962 cycles

AFT PIT BILGE STA 787 TO STA 793 RBL 23R BEAR STRAP HAS TWO AREAS OF CORROSION. REFER TO NIR 5097068 FOR REPAIR OF BEAR STRAP BS 787 TO BS 793 RBL 23.

Part: TIE CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,370 hrs · 29,962 cycles

TIE CLIP AT STA 787 RBL 15 HAS CORROSION. REPLACED TIE CLIP WITH REPAIR PART.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,370 hrs · 29,962 cycles

FLOORBEAM UPPER FLANGE IS CORRODED. REPAIRED PER EA 5310 02800.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

AFT CARGO PIT BS 727C AT STR 25L TOP FLANGE OF FRAME DENTED. REPAIRED WITH REPAIR PART IAW B737 400 SRM.

Part: SILL — CORRODED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

AFT CARGO PIT DOOR SILL PLATE STA 783 TO 847 CORROSION AROUND FASTENER HOLES TOP AND BOTTOM OF PLATE CORROSION ON AFT CARGO DOOR SILL PLATE AT BS 793 TO BS 847 WAS BLENDED OUT AND FOUND TO BE BEYOND ALLOWABLE LIMITS IAW 737 400 SRM 51 40 05 AND 51 40 02. REPAIR PERFORMED IAW B737 400 SRM.

Part: FRAME — CRACKED (BS 400) · airframe 52,370 hrs · 29,962 cycles

LT FRAME AT STA 400 CRACKED AT PSU RAIL BRACKET. REPAIRED IAW ASA EA5310 02797.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,370 hrs · 29,962 cycles

FLOORBEAM UPPER FLANGE CORRODED. REPLACED BEAM PER EA 5310 02800.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

AFT CARGO PIT BS 727E BETWEEN STRINGER 22L & 23L TOP FLANGE OF FRAME DENTED. AFT CARGO PIT FRAME REPAIRED AT BS 727E STRINGER 22L TO 23L IAW B737 400 SRM 51 70 11 FIG 1.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

STRINGER TIE CLIP CRACKED IN FORWARD CARGO BAY AREA. REPLACED CLIP PER SRM 51 40 02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

FORWARD CARGO BAY INTERCOSTAL ANGLE CRACKED. REPLACED INTERCOSTAL PER SRM 53 30 04 51 40 05 AND 51 40 02.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,370 hrs · 29,962 cycles

AFT CARGO COMPARTMENT FRAME AT BS 727G IS CORRODED BETWEEN STRINGER 25R AND 26R. REPAIRED WITH REPAIR PART IAW B737 400 SRM.

Part: INTERCOSTAL — CORRODED (BS 306-312) · corrosion level 2 · airframe 52,370 hrs · 29,962 cycles

CORROSION ON SUPPORT "T" AT RBL 12 WL 208 STA306. FLOOR SUPPORT "T" REPLACED WITH NEW PART IAW B737 400 SRM 51 40 02.

Part: SKIN — NICKED (FUSELAGE) · airframe 52,370 hrs · 29,962 cycles

FUSELAGE SKIN NICKED. REPAIRED PER SRM 53 00 01 AND EA 5300 01080.

Part: SKIN — DENTED (BS 374 S23-24L) · airframe 52,370 hrs · 29,962 cycles

DENT IN SKIN AT BS 374 5 INCHES BELOW STR 23L. DAMAGE REPAIRED ON MIG 5 NR 5097180 IAW B737 400 SRM 53 00 01.

Part: SKIN — DENTED (BS 373-377) · airframe 52,370 hrs · 29,962 cycles

4 DENTS IN SKIN 2 INCHES BELOW STR 24L FROM BS 373.5 TO BS 377.5. REPAIR WORK ACCOMPLISHED IAW B737 400 SRM 53 00 01.

Part: SLAT — DELAMINATED (NR 5) · airframe 52,370 hrs · 29,962 cycles

NR 5 SLAT INBOARD END FOUND DELAMINATION. NR 5 SLAT INBOARDD END REPAIRED IAW B737 400 SRM CH 51 70 10 REPAIR 4.

Part: SLAT — DELAMINATED (NR 4) · airframe 52,370 hrs · 29,962 cycles

NR 4 SLAT OUTBOARD END DELAMINATED. REPAIRED SLAT PER SRM 51 70 10.

Part: SLAT — DELAMINATED (NR 5) · airframe 52,370 hrs · 29,962 cycles

NR 5 SLAT OUTBOARD END DELAMINATED. REPLACED CORE AND INSTALLED DOUBLER PER SRM 51 70 10.

Part: SLAT — DELAMINATED (NR 2) · airframe 52,370 hrs · 29,962 cycles

NR 2 SLAT INBOARD END FOUND DELAMINATED. NR 2 SLAT REPAIRED PER SRM 51 70 10 REPAIR 4.

Part: BOLT — LOOSE (R1 DOOR) · airframe 50,412 hrs · 28,790 cycles

R 1 DOOR WILL NOT OPEN. UPON INSPECTION, FOUND BOLT TO ROD END NOT ATTACHED, NUT MISSING. REATTACHED ROD END INSIDE DOOR, TESTED PER AMM 52 41 00.

Part: STRINGER — CRACKED (BS 310-328) · airframe 49,454 hrs · 28,257 cycles

AIR START UNIT CONTACTED RIGHT SIDE OF AIRCRAFT BELOW DOOR R1. REPAIRED PER EA 5330 02206. NOTE ADDITIONAL P/N 65C36745 23.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,870 hrs · 27,915 cycles

R1 DOORWAY LOWER SILL CHORD ATTACHMENT ANGLE CORRODED. ATTACHMENT ANGLE REPLACED WITH NEW PART IAW SRM 51-40-02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,870 hrs · 27,915 cycles

R1 DOORWAY LOWER SILL CHORD CORRODED. REPLACED SILL WITH NEW PART IAW SRM 51-40-05 AND 51-40-02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 478,870 hrs · 27,915 cycles

L1 DOOR SILL CHORD CORRODED. REPLACED L1 DOOR SILL CHORD IAW SRM 51-40-02.

Part: SKIN — DEBONDED (T/E FLAP) · airframe 48,870 hrs · 27,915 cycles

LEFT O/B AFT FLAP END CAP DISBONDED. LEFT O/B AFT FLAP REPAIRED IAW CASCADE ERO 6540 AND ASA EA 57 50 02331.

Part: WEDGE — DENTED (L/E SLAT) · airframe 48,870 hrs · 27,915 cycles

NR 3 SLAT DENTED ON T/E WEDGE ASSY LOCATED 28 INCHES I/B OF O B E.D. NR 3 SLAT REPAIRED IAW SRM 51-70-10.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,870 hrs · 27,915 cycles

R1 DOORWAY LOWER SILL CHORD REINFORCEMENT STRAP EXFOILATED. REINFORCEMENT STRAPS REPLACED WITH NEW PART IAW SRM 51-40-05.

Part: WEB — GOUGED (FUSELAGE) · airframe 48,870 hrs · 27,915 cycles

R1 DOORWAY LOWER SILL WEB SCRATCHED. FLOOR WEB REPLACED WITH FABRICATED REPAIR PART IAW SRM 51-40-02 AND 51-40-05.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,870 hrs · 27,915 cycles

CABIN STA 312 FLOORBEAM UPPER CHORD CORRODED. FLOORBEAM UPPER CHORD REPAIR ACCOMPLISHED IAW SRM 53-10-51 REPAIR 5.

Part: SLIDE — TWISTED (R1 DOOR) · airframe 48,561 hrs · 27,754 cycles

DURING R1 DOOR SLIDE DEPLOY TEST THE SLIDE TWISTED UPON DEPLOYMENT. REPLACED R1 DOOR EVAC SLIDE.

Part: SLIDE — TWISTED (R1 DOOR) · airframe 48,506 hrs · 27,721 cycles

DURING R1 DOOR SLIDE DEPLOY TEST THE SLIDE TWISTED UPON DEPLOYMENT. REPLACED R1 DOOR EVAC SLIDE.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,474 hrs · 26,051 cycles

DENT IN FUSELAGE SKIN. REPAIRED PER SRM 53-80-01.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 45,474 hrs · 26,051 cycles

CORROSION AT BSTA 1016 PRESURE BULKHEAD LWR CTR CHANNEL JUST AFT OF BSTA 1016 FRAME CHORD. REPLACED LWR CTR CHANNELS PER EA 5310 02577.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 45,474 hrs · 26,051 cycles

CORROSION ON STRINGER. REPAIRED PER EA 5310 02576.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,474 hrs · 26,051 cycles

DENT IN FUSELAGE SKIN. REPAIRED PER SRM 53 80 01.

Part: SKIN — CORRODED (FUSELAGE) · airframe 45,474 hrs · 26,051 cycles

CORROSION ON SKIN. REPAIRED PER EA 5390 02045 AND EA 5330 02048.

Part: SKIN — DAMAGED (BS 317-319) · airframe 45,474 hrs · 26,051 cycles

DENT APPROX 42 INCHES AFT OF FWD LAV SERVICE DOOR FOUND TO BE CREASED. REPAIRED SKIN ON FUSELAGE PER SRM 53-00-01.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 45,474 hrs · 26,051 cycles

AFT CARGO DOOR CUTOUT FRAME CORRODED. REMOVED AND REPLACED AFT CARGO DOOR CUTOUT FRAME PER SRM 53-00-7.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 45,474 hrs · 26,051 cycles

FOUND CORROSION ON BOTTOM OF 986.5 FLOORBEAM UPPER FLANGE. REPAIRED PER EA 5310 02565.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 45,474 hrs · 26,051 cycles

FOUND CORROSION ON FLOORBEAM AT PREVIOUS REPAIR. REPAIRED FLOORBEAM PER EA 5310 02564.

Part: FRAME — CORRODED (BS 500A) · airframe 45,474 hrs · 26,051 cycles

FOUND CORROSION ON FRAME SHEAR TIE. REPAIRED PER SRM 53 00 07.

Part: SKIN — DENTED (BS 1069) · airframe 45,474 hrs · 26,051 cycles

DENT FOUND ON LE OF RT STAB APPROX 2 INCHES FROM WING ROOT. REPAIRED PER SRM 55 10 01.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,474 hrs · 26,051 cycles

CORROSION ON FRAME SHEAR TIE. REPAIRED PER SRM 53 00 07 REPAIR 3.

Part: SHEAR TIE — CORRODED (BS 727G) · airframe 45,474 hrs · 26,051 cycles

AFT CARGO COMPARTMENT CORROSION ON FRAME SHEAR TIE. REPAIRED PER SRM 53-00-07.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 45,474 hrs · 26,051 cycles

AFT CARGO COMPARTMENT, CORROSION ON STRINGER CLIP. REMOVED AND REPLACED STRINGER CLIP.

Part: FRAME — CRACKED (BS 794) · airframe 45,474 hrs · 26,051 cycles

FOUND DOUBLER ON FRAME CRACKED. REMOVED AND REPLACED DOUBLER PER SRM 51-40-05

Part: SILL — CORRODED (FUSELAGE) · airframe 45,474 hrs · 26,051 cycles

FOUND CORROSION ON AFT ENTRY DOOR MOPSILL. REMOVED AND REPLACED AFT ENTRY DOOR MOPSILL.

Part: SILL — CORRODED (FUSELAGE) · airframe 45,474 hrs · 26,051 cycles

FOUND CORROSION ON AFT GALLEY MOPSILL. REMOVED AND REPLACED MOPSILL CHORD ANGLE.

Part: WEB — CORRODED (CABIN) · airframe 45,474 hrs · 26,051 cycles

FOUND FLOOR WEB CORRODED. REMOVED AND REPLACED FLOOR WEB PER SRM 51-40-02.

Part: STRAP — CRACKED (FUSELAGE FRAME) · airframe 45,474 hrs · 26,051 cycles

FOUND FRAME STRAP CORRODED AND CRACKED. REMOVED AND REPLACED PER SRM 51-40-02 AND 51-40-05.

Part: SUPPORT — CORRODED (BULKHEAD) · airframe 45,474 hrs · 26,051 cycles

FOUND FLOOR TO AFT BULKHEAD SUPPORT CORRODED. REMOVED AND REPLACED FLOOR TO AFT BULKHEAD SUPPORT.

Part: FRAME — CORRODED (BS 847) · airframe 45,474 hrs · 26,051 cycles

FOUND CORROSION ON FRAME. REMOVED AND REPLACED FRAME PER SRM 51-40-02.

Part: SKIN — GOUGED (BS 1046-1049) · airframe 45,474 hrs · 26,051 cycles

FOUND EXTERNAL SKIN HAS GOUGES. REPAIRED EXTERNAL SKIN BY REMOVING DAMAGED AREA AND FABRICATING REPAIR DOUBLER AND INSTALLING PER SRM 53-80-01.

Part: WEB — CORRODED (BS 987) · airframe 45,474 hrs · 26,051 cycles

FOUND FLOOR WEB CORRODED. REMOVED AND REPLACED FLOOR WEB PER SRM 51-40-02.

Part: SILL — CORRODED (FUSELAGE) · airframe 45,474 hrs · 26,051 cycles

PAE- CORROSION ON AFT GALLEY MOPSILL. REMOVED AND REPLACED MOPSILL CHORD ANGLE PER B737-400 SRM 53-60-15 AND 51-40-02.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2

PAE: WHILE WORKING ON CARD NR 4989822, FOUND CORROSION ON FAIL SAFE ANGLE/ CHORD. REMOVED AND REPLACED FAIL SAFE CHORD IAW SRM. (K)

Part: SHEAR TIE — CORRODED (FS 986)

PAE - FOUND CORROSION ON SHEAR TIE AT BS 986.5 BETWEEN STRINGER 27L AND 27R. REMOVED AND REPLACED SHEAR TIE PER B737-400 SRM 51-40-02. (M)

Part: STRAP — CORRODED (FUSELAGE)

PAE: BSTA 847 FRAME INNER FLANGE STRAP CORROSION. REMOVED AND REPLACED IAW SRM. (K)

Part: CARGO TRACK — CORRODED (CARGO BAY)

PAE - AFT CARGO COMPARTMENT, CORROSION ON CARGO TIE DOWN TRACKS. FOUND OUT OF LIMITS, CARGO TIE DOWN TRACK REPLACED ON MIG-5 CARD NR 4989820 PER B737-400 SRM 53-60-53. (M)

Part: CARGO TRACK — CORRODED (FS 747)

PAE - FOUND AFT CARGO BAY, TIE DOWN FITTING CORRODED. FOUND OUT OF LIMITS, CARGO TIE DOWN TRACK REPLACED ON MIG-5 CARD PER B737-400 SRM 53-60-53. (M)

Part: CARGO TRACK — CORRODED (FS 793)

PAE - FOUND AFT CARGO BAY, TIE DOWN FITTING CORRODED. FOUND OUT OF LIMITS, CARGO TIE DOWN TRACK REPLACED ON MIG-5 CARD NR 4989820 PER B737-400 SRM 53-60-53. (M)

Part: FLOORBEAM — CORRODED (FS 967)

PAE - FOUND CORROSION ON FLOORBEAM AT BS 967, LBL 15-19, WL 208. REPAIRED PER B737-400 SRM 53-00-51 REPAIR 3. (M)

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR)

SEA - L1 DOOR IS DIFFICULT TO CLOSE. ADJUSTED GUIDE ARM. (M)

Part: NUT — MISSING (R1 DOOR)

PDX- FOUND R1 DOOR WOULD NOT OPEN. FOUND UPPER GEAR CONTROL ROD RETAINING NUT MISSING AND BOLT FELL OUT. SECURED UPPER CONTROL ROD BOLT AND RETAINING NUT. ALL RIG AND OPS CHECKS GOOD.

Part: FINGER DOUBLER — DAMAGED (FUSELAGE)

PAE - FINGER DOUBLER ON AFT EDGE OF AFT CARGO DOOR CUTOUT IS DAMAGED. REMOVED AND REPLACED FINGER DOUBLER ON AFT EDGE OF AFT CARGO DOOR CUTOUT. (K)

Part: RETAINER — DAMAGED (CARGO DOOR)

PAE - LOWER AFT SEAL RETAINER ON AFT CARGO BAY DOOR DAMAGED. REMOVED AND REPLACED LOWER AFT SEAL RETAINER ON AFT CARGO BAY DOOR. (K)

Part: SUPPORT — GOUGED (NR 2 PYLON)

GYR - DURING SI CHECK, FOUND NR 2 ENGINE PYLON OUTBOARD FAN COWL SUPPORT INBOARD AND OUTBOARD CHORD GOUGED. REPAIRED IAW EA. (M)

Part: SKIN — CHAFED (PYLONS)

GYR - DURING SI CHECK, FOUND NR 1 AND 2 PYLON INBOARD AND OUTBOARD STRUT SKINS CHAFING DAMAGE. REPAIRED IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE)

GYR - DURING SI CHECK, FOUND CORROSION ON NUTPLATE HOLE ON UPPER T-CAP STATION 344 FROM LBL 20 TO 50. REPAIRED IAW EA. (M)

Part: FRAME — CRACKED (FS 601)

GYR - DURING SI CHECK, FOUND CRACKED FRAME CHORD AFT SIDE AT STATION 601 RBL 65 WL 203. REPAIRED IAW EA. (M)

Part: DOOR FRAME — CRACKED (R1 DOOR)

GYR - DURING SI CHECK, FOUND CRACK AT R1 DOOR FRAME AT STATION 291.5. REPAIRED IAW EA. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

RNO - DURING MAINTENANCE CHECK, FOUND 2 EMERGENCY FLOOR TRACK SECTIONS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACKS OPERATIONAL CHECKED GOOD. (M)

Part: ATTACH FITTING — CRACKED (FUSELAGE)

PAE - DURING C-CHECK, FOUND AFT SUPPORT INBOARD ATTACH BRACKET CRACKED. REMOVED AND REPLACE IAW SRM. (M)

Part: RETAINER — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON RETAINER LEFT MAIN WHEEL WELL. REMOVED AND REPLACED IAW SRM. (M)

Part: STRAP — CRACKED (FUSELAGE)

PAE - DURING C-CHECK, FOUND STRAP IN E/E BAY IS CRACKED .68 INCH. REMOVED AND REPLACED IAW SRM. (M)

Part: WIRE — DISCONNECTED (LIGHTS)

SEA - DURING SERVICE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROWS 18-20. RECONNECTED WIRING AT ROW 18 OPS NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

JNU - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 13-17. REMOVED AND REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECKS NORMAL. (M)

Part: WIRE — DAMAGED (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 16. REPAIR WIRES, OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROWS 19-22 INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FOR ROW 10-22 TRACK LIGHTS, OPS CHECKED NORMAL. (M)

Part: WIRE — FAULTY (CABIN)

PSP - PRIOR TO FLIGHT - FOUND LAST FOUR EMERGENCY EXIT TRACK LIGHTS INOPERATIVE. REPAIRED FAULTY WIRE CONNECTION AS REQUIRED, OPS CHECK NORMAL. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, FOUND FIRST 5 FRONT EMERGENCY TRACK LIGHTS INOPERATIVE, DISCONNECTED. RECONNECTED MODULE WIRING ASSEMBLY, OPS CHECK NORMAL. (M)

Part: LIGHT — INOPERATIVE (MID CABIN)

SJC: PRIOR TO SCHEDULED FLIGHT FOUND EMERGENCY FLOOR TRACK EGRESS LIGHTS AT ROWS 16 & 17 INOP. REMOVED AND REPLACE EGRESS TRACK LIGHT BULBS AND REPLACED WIRES AT ROWS 16 & 17, OPS CHECKED NORMAL, RELEASED ACFT FOR SERVICE.

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 12 AND 13 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERABLE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

SNA - FLT 389 - BOTH FORWARD RED EMERGENCY EXI TFLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE FORWARD 3 AND AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED LIGHTS/WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK THE AFT EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING/LIGHTS AND LIGHT OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - PRIOR TO FLT 68, THE AFT 5 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: DISCHARGE LINE — CHAFED (NR 2 ENGINE)

OAK - DURING WALK AROUND, A HYDRAULIC LEAK WAS FOUND AT THE RT FLAP FAIRING. INSPECTED AND FOUND THE HYDRAULIC LINE FROM THE HEAT EXCHANGER CHAFING AGAINST THE FIRE PROTECTION DISCHARGE LINE. BOTH LINES CHAFED THROUGH. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC LINE AND THE FIRE PROTECTION DISCHARGE LINE. LEAK CHECKED GOOD. REFERENCE ASAA9740006.

Part: TUBE ASSY — CHAFED (NR 2 ENGINE)

OAK - DURING WALK AROUND, A HYDRAULIC LEAK WAS FOUND AT THE RT FLAP FAIRING. INSPECTED AND FOUND THE HYDRAULIC LINE FROM THE HEAT EXCHANGER CHAFING AGAINST THE FIRE PROTECTION DISCHARGE LINE. BOTH LINES CHAFED THROUGH. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC LINE AND THE FIRE PROTECTION DISCHARGE LINE. LEAK CHECKED GOOD. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED LOOSE TRACK WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - FLT 99 -AFT SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS INOP. RECONNECTED TRACK WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: SOCKET — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED SOCKET FOR WHITE LIGHT AND ALL LIGHTS OPERATED NORMALLY. (M)

Part: CIRCUIT BREAKER — POPPED (COCKPIT)

SEA - FLT 491 - AFTER TAKEOFF FROM SJC, THE GEAR HANDLE WOULD NOT MOVE UP PAST OFF. CREW COMPLETED CHECKLIST AND GEAR WAS RAISED. CREW NOTICED THAT THE LANDING GEAR LATCH AND PRESS WARNING CIRCUIT BREAKER WAS POPPED AND RESET SAME. AIRCRAFT LANDED IN SEA WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE PROBLEM ON GROUND, SUSPECT CIRCUIT BREAKER CAUSED THE ORIGINAL DISCREPANCY. CIRCUIT BREAKER REPLACED AS PRECAUTIONARY. AIRCRAFT RELEASED. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT 2 RED EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRES AND THE LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, FIVE MID CABIN EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AT ROW 15 AND LIGHTS OPERATED NORMALLY. (W)