N786AS

Part: SEAL DEPRESSOR — CRACKED (BS 951) · airframe 67,216 hrs · 37,180 cycles

L2 DOOR WAY CUT OUT FWD SEAL DEPRESSOR FITTING ABOVE THE UPPER HINGE CUT OUT WAS FOUND CRACKED. ACFT GROUNDED. REMOVED CRACKED SEAL DEPRESSER AND INSTALLED NEW SEAL DEPRESSOR IAW SRM 51-40-02-0G-10.

Part: SEAL DEPRESSOR — CORRODED (BS 956) · corrosion level 2 · airframe 67,216 hrs · 37,180 cycles

R2 DOORWAY CUTOUT FWD SEAL DEPRESSOR BELOW LOWER HINGE CUTOUT IS CORRODED. ACFT GROUNDED. REMOVED CORRODED IAW SRM 53-60-15-1A-1, FIG 101, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A1, FIG 101. R & R SEAL DEPRESSOR SRM 51-40-02-0G-0.

Part: FITTING — CRACKED (BS 298-305) · airframe 67,216 hrs · 37,180 cycles

THE R1 DOOR WAY CUT OUT THE FWD UPPER REVEAL CORNER FITTING WAS FOUND CRACKED. ACFT GROUNDED. R & R R1 DOOR FITTING IAW DWG 65-55878 AND SRM 51-40-02-0G-0.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 66,672 hrs · 36,865 cycles

FWD ENTRY AND SERVICE DOOR EXIT SIGN LENS MISSING CLEAR LENS PIECE. ACFT GROUNDED. R & R FWD GALLEY EMERGENCY EXIT OVERHEAD LIGHT LENS ASSY, VERIFIED ALL LIGHTS WORKED NORMAL.

Part: HINGE — LACK OF LUBE (L1 DOOR) · airframe 65,009 hrs · 35,828 cycles

L1 DOOR DIFFICULT TO CLOSE. ACFT GROUNDED. ACCOMPLISHED GVI, NO DEFECTS NOTED; LUBRICATED HINGE ARMS. OPS CHECK GOOD-LIGHT OP'S NORMAL.

Part: LIGHT — INOPERATIVE (L1 DOOR SLIDE) · airframe 64,961 hrs · 35,800 cycles

THREE INTEGRAL LIGHTS NOT ILLUMINATED AFTER SLIDE DEPLOYED. ACFT GROUNDED. R & R SLIDE ASSY.

Part: SKIN — CHAFED (HORIZONTAL STAB) · airframe 64,961 hrs · 35,800 cycles

LEFT HORIZONTAL STAB AFT/LOWER SLIDING SEAL CUTOUT HAS DEEP CHAFED AREA ON FWD SIDE. ACFT GROUNDED. R & R CUTOUT SKIN IAW SRM 51-40-02-0G-0.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 64,961 hrs · 35,800 cycles

MULTIPLE DENTS ON LOWER SKIN ON RT FLAP INBD. ACFT GROUNDED. REPAIRED MULTIPLE DENTS ON LOWER SKIN OF RT INBD FOREFLAP IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: ARM — OUT OF ADJUST (L-1 DOOR) · airframe 64,899 hrs · 35,771 cycles

UNABLE TO CLOSE L1 DOOR. ACFT GROUNDED. FOUND UPPER HINGE FLAP SEAL ASSY LOOSE AND HANGING DOWN ON L-1 DOOR FRAME CAUSING DOOR TO JAM. ADJUSTED THE GUIDE ARM AND 2 EA DOOR STOPS AND VERIFIED CORRECT ADJUSTMENT OF THE L1 DOOR MM 52-11-00-705-007. FWD ENTRY DOOR TEST GOOD AND HANDLE FORCES WITHIN LIMITS REF MM 52-11-00-755-051. REPLACED THE UPPER HINGE FLAP SEAL ASSY, WHICH HAD BEEN DAMAGED, REF SRM 51-40-02. MOVED THE ANNOUNCEMENT HOLDER, LIT. POCKET, TO ITS ALTERNATE POSITION REF. DWG A-2520014663 AND MOVED THE F/A HEADREST INBD. OPS CKS GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 64,618 hrs · 35,593 cycles

EMERGENCY EXIT SIDEWALL LIGHT ROW 17 BROKEN. ACFT GROUNDED. R & R EMERGENCY EXIT LIGHT ASSY IAW MM 33-51-01. OPS NORMAL.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 63,550 hrs · 34,953 cycles

L-1 DOOR EMERGENCY LT COVER OFF. ACFT GROUNDED. REPLACED LIGHT ASSY, REF MM 33-51-11. OPS CK GOOD.

Part: WINDOW FRAME — DAMAGED (BS 203) · airframe 62,745 hrs · 34,439 cycles

R1 WINDOW UPPER FASTENER ATTACH ROW, MOST OTBD FASTENER IS ELONGATED AT MIDDLE LAYER. ORIGINAL HOLE DIAMETER IS .256 DAMAGE IS .280-.2835, STEP REMEAD UPPER OTBD R-1 WINDOW FASTENER HOLE TO REMOVE DAMAGE. FINAL HOLE DAMAGE .328. DAMAGED CONFIRMED REMOVED. INSTALLED DOUBLER IAW SRM 53-10-01. REPAIR 10 STEP 10 & 11.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 61,676 hrs · 33,810 cycles

OVERWING EXIT LIGHT COVER FELL OFF. SECURED LENS COVER.

Part: DOOR — LACK OF LUBE (L1) · airframe 61,641 hrs · 33,785 cycles

DOOR L1 IS DIFFICULT TO CLOSE. STICKS IN MIDDLE. CLEANED AND LUBED L1 DOOR. OPS NORMAL OK. REF MM 52-11-00.

Part: WINDOW — DISLODGED (COCKPIT) · airframe 61,632 hrs · 33,781 cycles

R2 WINDOW FELL OFF TRACKS. REINSTALLED R2 WINDOW, PERFORMED OPS CHECK, REF MM 56-12-11-404-007 OPS CHECKED GOOD.

Part: LIGHT — BURNED OUT (CABIN) · airframe 61,580 hrs · 33,748 cycles

DOOR EMERGENCY LIGHTS BURNED OUT. OPEN

Part: SILL — CORRODED (BS 967-987) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

R2 DOOR MOP SILL HAS SEVERAL AREAS OF CORROSION. ACFT GROUNDED. R & R SILL IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 772) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

AFT PUT FLOOR SUPPORT, RBL 8 HAS CORROSION ON SPLICE ANGLE AT STA 772. REPAIRED FLOOR SUPPORT IAW EA 400-53EA-08977, REV NEW DATED.

Part: FLOOR SUPPORT — CORRODED (BS 727F) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

AFT PIT FLOOR SUPPORT RBL 3 HAS CORROSION ON SPLICE ANGLE AT STA 727F8. REPAIRED FLOOR SUPPORT IAW EA 400-53EA-08979, REV NEW.

Part: FLOOR SUPPORT — CORRODED (BS 727F) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

AFT PIT FLOOR SUPPORT, LBL 3 HAS CORROSION ON SPLICE ANGLE AT 727F8. REPAIRED FLOOR SUPPORT IAW EA 400-53EA-08979, REV NEW.

Part: FLOOR SUPPORT — CORRODED (BS 772) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

AFT PIT FLOOR SUPPORT LBL 12.5 HAS CORROSION ON SPLICE ANGLE AT STA 772. ACFT GROUNDED. REPAIRED FLOOR SUPPORT IAW EA 400-53, EA-08977, REV NEW.

Part: FLOOR SUPPORT — CORRODED (BS 772) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

AFT PIT FLOOR SUPPORT, RBL 8 HAS CORROSION ON SPLICE ANGLE AT BS 772. REPAIRED FLOOR SUPPORT IAW EA 400-53EA-08977, REV NEW.

Part: FLOOR SUPPORT — CORRODED (BS 727F) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

AFT PIT FLOOR SUPPORT, RBL 3 HAS CORROSION ON SPLACE ANGLE AT STA 727F8. ACFT GROUNDED. REPAIRED FLOOR SUPPORT IAW EA 400-53EA-08979, REV NEW.

Part: FLOOR SUPPORT — CORRODED (BS 727F) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

AFT PIT FLOOR SUPPORT LBL 12.5 HAS CORROSION ON SPLICE ANGLE AT STA 727F8. ACFT GROUNDED. REPAIRED FLOOR SUPPORT IAW EA 400-53EA-08979, REV NEW.

Part: FLOOR SUPPORT — CORRODED (BS 772) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

AFT PIT FLOOR SUPPORT, LBL 12.5 HAS CORROSION ON SPLICE ANGLE AT STA 772. REPAIRED FLOOR SUPPORT IAW EA 400-53EA-08977, REV NEW.

Part: FLOOR SUPPORT — CORRODED (BS 727F) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

AFT PIT FLOOR SUPPORT, LBL 3 HAS CORROSION ON SPLICE ANGLE AT 727F. REPAIRED FLOOR SUPPORT IAW EA 400-53EA-08979, REV NEW.

Part: FLOOR SUPPORT — CORRODED (BS 772) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

AFT PIT FLOOR SUPPORT LBL 3 HAS CORROSION ON SPLICE ANGLE AT STA 772. ACFT GROUNDED. REPAIR FLOOR SUPPORT IAW EA 400-53EA-08977, REV.

Part: FLOOR SUPPORT — CORRODED (BS 772) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

AFT PIT FLOOR SUPPORT, LBL 8 HAS CORROSION AT BS 772. REPAIRED FLOOR SUPPORT IAW EA 400 53EA 08977, REV NEW.

Part: FLOOR SUPPORT — CORRODED (BS 772) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

AFT PIT FLOOR SUPPORT, RBL 3 HAS CORROSION ON SPLICE ANGLE AT BS 772. REPAIRED FLOOR SUPPORT IAW EA 400-53, EA 08977, REV NEW.

Part: FLOOR SUPPORT — CORRODED (BS 772) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

AFT PIT FLOOR SUPPORT, LBL 8 HAS CORROSION AT STA 772. ACFT GROUNDED. REPAIRED FLOOR SUPPORT IAW EA 400-53EA-08977, REV NEW.

Part: FLOOR SUPPORT — CORRODED (BS 727F) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

AFT PIT FLOOR SUPPORT, LBL 12.5 HAS CORROSION ON SPLICE ANGLE AT BS 727F. REPAIRED FLOOR SUPPORT IAW EA 400-53EA-08979, REV NEW.

Part: FLOOR SUPPORT — CORRODED (BS 772) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

AFT PIT FLOOR SUPPORT, LBL 3 HAS CORROSION ON SPLICE ANGLE AT BS 772. REPAIRED FLOOR SUPPORT IAW EA 400-53EA-08977, REV NEW.

Part: FLOOR SUPPORT — CORRODED (BS 772) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

AFT PIT FLOOR SUPPORT, RBL 3 HAS CORROSION ON SPLICE ANGLE AT STA 772. REPAIRED FLOOR SUPPORT IAW EA 400-53EA-08977, REV NEW.

Part: SHEAR WEB — CORRODED (BS 982-986) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

RT SHEAR WEB R2 DOOR AFT WEB UNDER MOPSILL CORRODED ON LOWER SURFACE. ACFT GROUNDED. BLENDED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-60-15, FIG 101. R & R WEB IAW SRM 51 40 02.

Part: FRAME — CRACKED (BS 500C) · airframe 61,580 hrs · 33,748 cycles

FRAME AT BS 500C HAS A CRACK AT RAIL ATTACH BRACKET. REPAIRED IAW TASK CARD AD20062609-400-53-1-786, FIG 3.

Part: STRINGER CLIP — CRACKED (BS 1006) · airframe 61,580 hrs · 33,748 cycles

LT FUSELAGE STA 1006 S13L STRINGER CLIP IS CRACKED. R & R STRINGER CLIP IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 867) · airframe 61,580 hrs · 33,748 cycles

FRAME AT STA 867 R IS CRACKED AT AC RAIL ATTACH BRACKET. ACFT GROUNDED. REPAIRED FRAME IAW TASK CARD AD20062609-400-53-1-786, FIG 3.

Part: STRINGER CLIP — CRACKED (BS 1006) · airframe 61,580 hrs · 33,748 cycles

LT FUSELAGE BS 1006 STRINGER 9L STRINGER CLIP CRACKED. R & R STRINGER CLIP IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 500A) · airframe 61,580 hrs · 33,748 cycles

FRAME AT BS 500A, IS CRACKED AT RAIL ATTACH BRACKET. REPAIRED FRAME IAW T/C AD20062609-400-53-1-786, FIG 3.

Part: FRAME — CRACKED (BS 480) · airframe 61,580 hrs · 33,748 cycles

FRAME AT BS 480 RT IS CRACKED AT ACFT RAIL ATTACH BRACKET. REPAIRED IAW T/C AP20062609-400-53-1-786, FIG 3.

Part: ANGLE — CRACKED (BS 294) · airframe 61,580 hrs · 33,748 cycles

R1 DOOR CUTOUT, BS 294 ANGLE BELOW S9R IS CRACKED. R & R ANGLE IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 480) · airframe 61,580 hrs · 33,748 cycles

FRAME AT BS 480 LT IS CRACKED AT RAIL ATTACH BRACKET. REPAIRED FRAME IAW T/C AD20062609-400-53-1-786, FIG 3.

Part: STRINGER CLIP — CRACKED (BS 1006) · airframe 61,580 hrs · 33,748 cycles

FUSELAGE BS 1006 S12L STRINGER CLIP CRACKED. R & R STRINGER CLIP IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 440) · airframe 61,580 hrs · 33,748 cycles

FRAME AT BS 440 IS CRACKED AT RAIL ATTACH BRACKET. REPAIRED IAWAD 20062609-400-53-1-786, FIG 3.

Part: FRAME — CRACKED (BS 500A) · airframe 61,580 hrs · 33,748 cycles

FRAME AT STA 500A RT IS CRACKED AT ACFT RAIL ATTACH BRACKET. ACFT GROUNDED. REPAIRED IAW TASK CARD AS20062609-400-53-1-786.

Part: FRAME — CRACKED (BS 727D) · airframe 61,580 hrs · 33,748 cycles

FRAME AT BS 727D IS CRACKED AT RAIL ATTACH BRACKET. REPAIRED FRAME IAW T/C AD20062609, 400-53-1-786, FIG 3.

Part: FRAME — CRACKED (BS 500C) · airframe 61,580 hrs · 33,748 cycles

FRAME AT STA 500C LT IS CRACKED AT ACFT RAIL ATTACH BRACKET. ACFT GROUNDED. REPAIRED FRAME IAW TASK CARD AD20062609-400-53-1-786, FIG 3.

Part: RETAINER — CRACKED (VERTICAL STAB) · airframe 61,580 hrs · 33,748 cycles

RT VERTICAL STAB ACCESS PANEL 9502 HAS CRACKED RETAINER. R & R RETAINER IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 440) · airframe 61,580 hrs · 33,748 cycles

FRAME AT BS 440 IS CRACKED AT RAIL ATTACH BRACKET. REPAIRED FRAME IAW T/C AD20062609, 400-53-1-786, FIG 3.

Part: FRAME — CRACKED (BS 400) · airframe 61,580 hrs · 33,748 cycles

FRAME AT BS 400 R IS CRACKED AT ATTACH BRACKET. REPAIRED IAW TASK CARD AD20062609-400-53-1-786, FIG 3.

Part: FRAME — CRACKED (BS 787) · airframe 61,580 hrs · 33,748 cycles

FRAME AT BS 787, HAS A CRACK AT RAIL ATTACH BRACKET. REPAIRED FRAME IAW TASK CARD AD20062609-400-53-1-786, FIG 3.

Part: STRINGER CLIP — CRACKED (BS 1006) · airframe 61,580 hrs · 33,748 cycles

FUSELAGE BS 1006 S10L STRINGER CLIP IS CRACKED. R & R STRINGER CLIP IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 827) · airframe 61,580 hrs · 33,748 cycles

FRAME BS 827 RT IS CRACKED AT RAIL ATTACH BRACKET. REPAIRED FRAME IAW T/C AD20062609, 400-53-1-786, FIG 3.

Part: ANGLE — CRACKED (BS 294 S10-11R) · airframe 61,580 hrs · 33,748 cycles

R1 DOOR CUTOUT, BS 294 ANGLE BETWEEN S10 AND 11R IS CRACKED. R & R ANGLE IAW SRM 51 40 02.

Part: CHANNEL — CRACKED (BS 1080) · airframe 61,580 hrs · 33,748 cycles

APU AIR INLET FORWARD DUCT HAS A CRACKED CHANNEL. R & R CHANNEL IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 400) · airframe 61,580 hrs · 33,748 cycles

FRAME AT BS 400 IS CRACKED AT RAIL ATTACH BRACKET. REPAIRED IAW T/C AD20062609, 400-53-1-786, FIG 3.

Part: FRAME — CRACKED (BS 827) · airframe 61,580 hrs · 33,748 cycles

FRAME AT BS 827 IS CRACKED AT ACFT RAIL ATTACH BRACKET. REPAIRED FRAME IAW T/C AD20062609-400-53-1-786, FIG 3.

Part: FRAME — CRACKED (BS 727B) · airframe 61,580 hrs · 33,748 cycles

FRAME AT 727B LT IS CRACKED AT ACFT RAIL ATTACH BRACKET. REPAIRED IAW T/C AD20062609-400-53-1-786, FIG 3.

Part: ANGLE — CRACKED (BS 294) · airframe 61,580 hrs · 33,748 cycles

R1 DOOR CUTOUT, BS 294 ANGLE BELOW S12R IS CRACKED. R & R ANGLE IAW SRM 51 40 02.

Part: FRAME — CRACKED (BS +08) · airframe 61,580 hrs · 33,748 cycles

FRAME AT BS 907 IS CRACKED AT RAIL ATTACH BRACKET. REPAIRED IAW AD20062609-400-53-786, FIG 3.

Part: STRINGER CLIP — CRACKED (BS 1006) · airframe 61,580 hrs · 33,748 cycles

FUSELAGE BS 1006 S-11L STRINGER CLIP CRACKED. R & R STRINGER CLIP IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 747) · airframe 61,580 hrs · 33,748 cycles

FRAME AT BS 747 L IS CRACKED AT ATTACH BRACKET. REPAIRED IAW TASK CARD AD20062609-53-1-786, FIG 3.

Part: FRAME — CRACKED (BS 907) · airframe 61,580 hrs · 33,748 cycles

FRAME AT STA 907 RT IS CRACKED AT ACFT RAIL ATTACH BRACKET. REPAIRED FRAME IAW T/C AD20062609, 400-53-1-786, FIG 3.

Part: FRAME — CRACKED (BS 867) · airframe 61,580 hrs · 33,748 cycles

FRAME AT STA 867 LT HAS A CRACK AT ACFT RAIL ATTACH BRACKET. REPAIRED IAW AD20062609 400 53 1 786, FIG 3.

Part: FRAME — CRACKED (BS 380) · airframe 61,580 hrs · 33,748 cycles

FRAME AT BS 380 RT IS CRACKED AT ATTACH BRACKET. REPAIRED IAW TASK CARD AD20062609-400-52-1-786.

Part: SUPPORT ANGLE — CORRODED (BS 967-986) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

LT SUPPORT ANGLE B/T 986-967 UNDER MOB SILL HAS CORROSION ON LOWER SURFACE. ACFT GROUNDED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15, FIG 101. RECEIVED NEW ANGLE. LOCATED AND DRILLED IAW SRM 51-40-05.

Part: STIFFENER — CORRODED (BS 1126) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

RT TORQUE BOX APU INLET AFT STIFFENER CORRODED INSIDE CUTOUT AT BS 1126. R & R RT APU TORQUE BOX STIFFENER IAW SRM 51-40-02.

Part: SKIN — DEBONDED (NR 2 SLAT) · airframe 61,580 hrs · 33,748 cycles

LEFT WING NR 2 SLAT DISBONDED ON INBD UPPER T/E. REPAIRED NR 2 SLAT IAW SRM 51-70-10, REPAIR 4.

Part: SILL — CORRODED (BS 294-344) · corrosion level 2 · airframe 31,580 hrs · 33,748 cycles

UPON REMOVAL OF R1 DOOR LOWER SILL INNER CHORD FOUND SILL WEB AT STA 294-344 CORRODED. ACFT GROUNDED. R & R WEB IAW SRM 51 40 02.

Part: STIFFENER — CORRODED (BS 1112) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

APU TORQUE BOX AREA, CORROSION AT APU AIR PLENUM TO ACFT MATING SURFACE (INSIDE INNER TORQUE BOX). R & R RT APU TORQUE BOX FORWARD STIFFENER IAW SRM 51-40-02.

Part: WEB — CORRODED (BS 290-360) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

UPON REMOVAL OF R1 DOOR LOWER SILL INNER CORD FOUND SILL WEB AT STA 294-344 CORRODED. R & R WEB IAW SRM 51-40-02.

Part: WEB — CORRODED (BS 951-986) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

CENTER R1 DOOR SILL WEB CORRODED. REMOVED CORROSION, MATERIAL LOSS FOUND TO BE OUT OF LIMIT. FABRICATED AND REPLACED WEB IAW SRM 53-60-15, 51-40-05 AND 51-40-02.

Part: STRINGER CLIP — CRACKED (BS 500) · airframe 61,580 hrs · 33,748 cycles

BS 500, STRINGER 8R HAS CRACKED CLIP. ACFT GROUNDED. R & R STRINGER CLIP IAW EA 400 53EA 69052, REV NEW DATED 23OCT12.

Part: WEB — CORRODED (BS 951-989) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

CENTER R2 DOOR SILL WEB CORRODED. REMOVED CORROSION, MATERIAL LOSS FOUND TO BE OUT OF LIMITS. FABRICATED AND REPLACED WEB IAW SRM 53 60 15, 51 40 05 AND 51 40 02.

Part: STRINGER CLIP — CRACKED (BS 727E) · airframe 61,580 hrs · 33,748 cycles

BS 727E, STRINGER CLIP 4L CRACKED . R & R STRINGER CLIP IAW EA 400 53EA 09052, DATED 23OCT12 REV NEW.

Part: SHEAR TIE — CORRODED (BS 500B) · corrosion level 2 · airframe 61,580 hrs · 33,758 cycles

FRAME SHEAR TIE AT FS 500B BETWEEN S-28R AND S-28L CORRODED. REMOVED DAMAGED PORTION OF FRAME FS 500B BETWEEN S-28R AND S-28L. FABRICATED, LOCATED AND DRILLED SHEAR TIE IAW SRM 53-00-07, REPAIR 7.

Part: SILL — CORRODED (BS 294-360) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

L1 DOOR LOWER SILL INBD CHORD IS CORRODED, STA 312 TO 360. REMOVED CORRODED, FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-10-15, FIG 101. R & R MOPSILL IAW SRM 51-40-02; STEPS 9 AND 13, AND SRM 51-40-05, FIG 2.

Part: FRAME — CORRODED (BS 500) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

FRAME LOWER LEG AT FS 500 BETWEEN STR 28R AND 28L HAS CORROSION. REMOVED DAMAGED PORTION OF FRAME LEG FS 500 BETWEEN 5-28R AND S-28L. FABRICATED, LOCATED, AND DRILLED IAW 53-00-07, REPAIR 7.

Part: FRAME — CORRODED (BS 500D) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

FRAME LOWER LEG AT FS 500D BETWEEN S-28L AND S-27L CORRODED. REMOVED DAMAGED PORTION OF FRAME FS 500D BETWEEN S-28L AND S-27L. FABRICATED, LOCATED AND DRILLED IAW SRM 53-00-07, REPAIR 7.

Part: GUTTER — CORRODED (BS 296) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

R1 DOOR LOWER SILL CORRODED AT BS 296. ACFT GROUNDED. R & R MOP SILL IAW SRM 51-40-02.

Part: CHANNEL — CRACKED (BS 727D-727E) · airframe 61,580 hrs · 33,748 cycles

CHANNEL ON VHF 3 ANTENNA IS CRACKED ON THE LT SIDE VERTICAL PORTION OF THE HAT (AFT PIT). R & R VHF ANTENNA CHANNEL IAW SRM 51-40-05, DWG 99T074D22, SRM 51-40-02.

Part: SUPPORT ANGLE — CORRODED (BS 320-360) · corrosion level 2 · airframe 61,514 hrs · 33,718 cycles

R1 DOOR CUTOUT BOTTOM THRESHOLD SUPPORT FRAME HAS SURFACE CORROSION. ACFT GROUNDED. R & R SUPPORT FRAME IAW SRM 51-40-02.

Part: FRAME — CORRODED (BS 294-344) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

L1 DOOR CUT OUT BOTTOM THRESHOLD SUPPORT FRAME HAS SURFACE CORROSION. LOCATED AND DRILLED IAW SRM 51-40-05.

Part: SUPPORT ANGLE — CORRODED (BS 320-360) · airframe 61,580 hrs · 33,748 cycles

R1 DOOR CUTOUT BOTTOM THRESHOLD SUPPORT FRAME HAS SURFACE CORROSION. R & R SUPPORT FRAME IAW SRM 51-40-02.

Part: CARGO TRACK — CORRODED (BS 947) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

AFT CARGO TRACK AT RBL-13 CORRODED ON BOTTOM SIDE AT STA 947. R & R CARGO TRACK IAW SRM 53-00-53.

Part: ANGLE — CRACKED (BS 294) · airframe 61,580 hrs · 33,748 cycles

R1 DOOR CUTOUT, BS 294 ANGLE BELOW S11R IS CRACKED. R & R ANGLE IAW SRM 51 40 02.

Part: FITTING — CRACKED (BS 990) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

FITTING AT BS 990 EXFOLIATED. LOCATED AND DRILLED NEW FITTING IAW SRM 51-40-05.

Part: SILL — CRACKED (BS 967-986) · corrosion level 2 · airframe 61,580 hrs · 33,748 cycles

L2 DOOR MOPSILL HAS SEVERAL AREAS OF CORROSION. ACFT GROUNDED. R & R L2 MOPSILL IAW SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (BS 727A) · airframe 61,580 hrs · 33,748 cycles

BS 727A, S2R STRINGER CLIP CRACKED. R & R STRINGER CLIP IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (RT PYLON) · airframe 615,780 hrs · 33,748 cycles

RT PYLON AFT STRUT FAIR NAC STA 314.24 OTBD SUPPORT BRACKET LOWER END IS CRACKED. ACFT GROUNDED. R & R DAMAGED SUPPORT BRACKET IAW SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (BS 847) · airframe 61,580 hrs · 33,748 cycles

STRINGER CLIP S4L CRACKED. R & R STRINGER CLIP IAW SRM 51-40-02

Part: ANGLE — CRACKED (RT WING) · airframe 61,580 hrs · 33,748 cycles

RT WING T/E LOWER ANGLE OTBD OF PYLON IS CRACKED. R & R ANGLE IAW SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (BS 500G) · airframe 61,580 hrs · 33,748 cycles

BS 500G, S4L CRACKED STRINGER CLIP. R & R STRINGER CLIP IAW SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (BS 500F) · airframe 61,580 hrs · 33,748 cycles

BS 500F, S5L CRACKED STRINGER CLIP. R & R STRINGER CLIP IAW SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (BS 727D) · airframe 61,580 hrs · 33,748 cycles

BS 727D, STRINGER 6L HAS CRACKED STRINGER CLIP. R & R CRACKED STRINGER CLIP IAW SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (BS 706) · airframe 615,780 hrs · 33,748 cycles

BS 706, S2L CRACKED STRINGER CLIP. R & R STRINGER CLIP IAW SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (BS 727C) · airframe 61,580 hrs · 33,748 cycles

BS 727C, STRINGER 7L CLIP CRACKED. R & R STRINGER CLIP IAW SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (BS 380) · airframe 61,580 hrs · 33,748 cycles

BS 380, S7R CRACKED STRINGER CLIP. R & R STRINGER CLIP IAW SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (BS 500D) · airframe 61,580 hrs · 33,748 cycles

BS 500D, S3L CRACKED STRINGER CLIP. R & R STRINGER CLIP IAW SRM 51-40-02.

Part: ANGLE — CRACKED (LT WING) · airframe 61,580 hrs · 33,748 cycles

LT WING T/E LOWER ANGLE OTBD OF PYLON IS CRACKED. R & R ANGLE IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (RT PLYON) · airframe 61,580 hrs · 33,748 cycles

RT PYLON AFT FAIRING NAC 314 LOWER SUPPORT BRACKET IS CRACKED. R & R SUPPORT BRACKET IAW SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (BS 727A) · airframe 61,580 hrs · 33,748 cycles

STRINGER CLIP AT BS 727A, S5R IS CRACKED. R & R IAW 51-40-02 SRM.

Part: ROLLER — LACK OF LUBE (L1 DOOR) · airframe 61,355 hrs · 33,616 cycles

F/A REPORTED L1 DOOR IS HARD TO OPEN AND CLOSE. CLEANED & LUBED DOOR LATCH ROLLERS AND STRIKER PLATES. CHECKS GOOD IAW MM 52-11-00-755-051.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 61,150 hrs · 33,504 cycles

EMERGENCY LIGHT EXIT IDENTIFIER SIGN ADJACENT TO LEFT AFT OVERWING EXIT HAS DAMAGED LENS. R & R LENS AND TESTED IAW MM 33-51-81-962-011 - OPS NORMAL.

Part: SPRING — MISSING (L1 DOOR) · airframe 61,304 hrs · 33,590 cycles

L1 DOOR MADE CRACKING / BANGING NOISE FOR DURATION OF FLIGHT. DOOR WAS BULGING INWARD APPROX 1-2 FROM ABOUT HALFWAY UP AND FROM APPROX 6 FROM EITHER SIDE. GROUNDED. INSPECTED L1 DOOR REF AMM 52-11-00-206-001. FOUND LOWER FWD STOP PIN LOCK SPRING MISSING AND STOP PIN MIS-ADJUSTED. ADJUSTED STOP PIN AND INSTALLED LOCK SPRING REF AMM 52-11-00-705-007. ALSO FOUND UPPER DOOR LINER OUT OF POSITION. REMOVED AND CORRECTLY INSTALLED UPPER DOOR LINER REF AMM 52-11-31-404-009. DOOR OPS CKS GOOD REF AMM 52-11-00-755-051. PRESSURIZED ACFT AND DOOR OPS AND LEAK CKS GOOD REF AMM 05-51-91-702-001. NO NOISE HEARD FROM DOOR OR LINER.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 60,731 hrs · 33,277 cycles

EXIT SIGN ON L2 FELL OFF. ACFT GROUNDED. REPLACED EXIT LIGHT COVER, OPS NORMAL.

Part: LIGHT — LOOSE (CABIN) · airframe 59,516 hrs · 32,584 cycles

F/A REPORTS FLOOR TRACK LIGHTING AREAS ROWS 10, 11 AND 12 HAS COME LOOSE. SECURED TRACK LIGHTING.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 59,511 hrs · 32,581 cycles

LEFT WING UPPER FIXED T/E PANEL SUPPORT ANGLE COMMON TO SIDE OF LEFT FAIRING CRACKED. REPLACED CRACKED ANGLE WITH NEW PER SRM 51 40 02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,511 hrs · 32,581 cycles

BS 294 BS 303 STR 16L INTERCOSTAL WEB CRACKED. GROUNDED YES. REMOVED CRACKED INTERCOSTAL FABRICATED AND INSTALLED PER ASA E AD20091614 400 53 104.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 59,511 hrs · 32,581 cycles

RIGHT WING TRAILING EDGE AILERON AREA REAR SPAR/RIB AFT SUPPORT ANGLE IS CRACKED. REPLACED SUPPORT ANGLE.

Part: STRAP — CRACKED (FUSELAGE)

FLOORBEAM TENSION STRAP CRACKED. REPLACED FLOORBEAM TENSION STRAP AT BS 348 WL 200.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 59,511 hrs · 32,581 cycles

ANGLE CRACKED BS 294 303 STR 10L. REPAIR IN PROGRESS.

Part: SUPPORT — CRACKED (ENTRY DOOR) · airframe 59,511 hrs · 32,581 cycles

FORWARD ENTRY DOOR LINER SUPPORT CRACKED UPPER AFT CORNER. REPLACED WITH NEW SUPPORT BRACKET PER SRM 51 40 02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 59,511 hrs · 32,581 cycles

ANGLE CRACKED BS 294 303 STR 10L. REPLACED INTERCOSTAL WITH REPAIR KIT.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 59,511 hrs · 32,581 cycles

DISTRIBUTION DUCT FRAME MOUNT BRACKET CRACKED. REPLACED BRACKET.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 59,511 hrs · 32,581 cycles

PASSENGER CABIN UPPER PRESSURE DECK CRACKED. PERFORMED REPAIR IAW B737 400 SRM 53 60 51 REPAIR 4 DETAIL II AND III.

Part: OUTFLOW VALVE — OBSTRUCTED (CABIN PRESSURE) · airframe 59,157 hrs · 32,360 cycles

TEN MIN LVL AT 330 WHEN CABIN ALT WARN HORN SOUNDED. CABIN PRESS AT 10 100 WENT TO STBY NO CHANGE EXECUTED EMER DESCENT FOLLOWED QRH WENT MANUAL CABIN CONTINUED TO RISE. PASSING 18,000 OUTFLOW VALVE OPEN THEN CLOSE CABIN STOPPED AT 12,000 AND CNTRL REGAINED. F/A'S REPORTED LOUD SQUEAL FROM AFT GALLEY DOORS. A/C ARRIVED WITH AN INSULATION BLANKET STICKING OUT OF & MELTED TO AFT SURFACE OF OUTFLOW VALVE. MOVED BLANKET AND ACCOMPLISHED CABIN PRESSURE LEAK CHECK FAILED. LEAKAGE WAS 80 SECONDS FROM 4 2.5 PSI REF MM 05 51 91 702 001. BOTH AFT GLY DOORS SEALED NORMALLY. NO SQUEALS OR LEAKS NOTED DURING LEAK CHECK B. REPLACED AFT OUTFLOW VALVE PRECAUTIONARY REF MM 21 31 11.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

STR25R HAS ELONGATED HOLES BETWEEN STA 907 919. FABRICATED NEW STRINGER AND SPLICES AND REPLACED DAMAGED AREA IAW B737 400 SRM 53 00 03 FIG 201.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,719 hrs · 32,117 cycles

INTERCOSTAL AT STR 21R IS CORRODED BETWEEN STA 927 947. REMOVED DAMAGED INTERCOSTAL, FABRICATED NEW PARTS AND INSTALLED IAW B737 400 SRM 51 30 01 AND 51 40 05.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

INTERCOSTAL BETWEEN STA 847 867 BETWEEN STRINGER 21R AND 22R HAS ELONGATED HOLES. THIS DEFECT IS ASSOCIATED WITH AN EXISTING REPAIR. REMOVED DAMAGED AREA FABRICATED NEW INTERCOSTAL AND INSTALLED IAW B737 400 SRM 51 40 02 AND BAC DRAWING 65 47960.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

FLOOR SUPPORT AT LBL 6 STA 807 827 IS CORRODED AT PREVIOUS REPAIR. REMOVED DAMAGED AREA FABRICATED REPAIR ANGLES AND FILLER AND INSTALLED REPAIR IAW B737 400 SRM 53 00 53 FIGURE 201.

Part: STRINGER SPLICE — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

STRINGER 23R STA 907 STRINGER SPLICE HAS ELONGATED HOLES. REMOVED DAMAGED SPLICE FABRICATED AND INSTALLED NEW PARTS IAW B737 400 SRM 51 40 02.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

STR 20R HAS ELONGATED HOLES BETWEEN STA 907 919. REMOVED DAMAGED AREA. FABRICATED NEW STRINGER AND SPLICE PARTS AND INSTALLED IAW B737 400 SRM 53 00 03 FIG 201.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

STRINGER 22R FROM STA 847 907 HAS ELONGATED HOLES. REMOVED DAMAGED SECTION OF STRINGER FABRICATED AND INSTALLED NEW SECTION OF STR 22R IAW B737 400 SRM 51 40 05 AND 51 40 02.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

STRINGER 21R STA 907 SPLICE HAS SEVERAL ELONGATED HOLES.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 58,719 hrs · 32,117 cycles

AFT PIT CARGO RAIL/TIEDOWN TRACK HAS SEVERAL AREAS OF CORROSION. REMOVED CORRODED SECTION FABBED REPLACEMENT SECTION AND REPAIR PARTS AND INSTALLED THE NEW PARTS IAW ASA EA400 53EA 05916.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

STR 25R AT STA 907 HAS SEVERAL ELONGATED HOLES IN THE SPLICE. FABRICATED AND INSTALLED NEW SPLICE IAW B737 400 SRM 51 40 05 AND BAC DWG 65 51698.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

STR 22R HAS ELONGATED HOLES BETWEEN STA 907 919. FABRICATED NEW STRINGER AND SPLICES AND REPLACED DAMAGED AREA IAW B737 400 SRM 53 00 03 FIG 201.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

INTERCOSTAL BETWEEN STA 847 867 BETWEEN STRINGER 20R AND 21R HAS ELONGATED HOLES. THIS DEFECT IS ASSOCIATED WITH EXISTING REPAIR. FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02.

Part: STRINGER SPLICE — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

STRINGER 24R STA 907 STRINGER SPLICE HAS SEVERAL ELONGATED HOLES. FABRICATED AND INSTALLED REPLACEMENT SPLICE FOR STRINGER 24R AT STA 907 IAW DWG 65 51698 AND B737 SRM 51 40 05.

Part: STRINGER SPLICE — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

STRINGER 20R STA 907 STRINGER SPLICE HAS ELONGATED HOLES. REMOVED DAMAGED SPLICE FABRICATED AND INSTALLED NEW SPLICE IAW B737 400 SRM 51 40 02.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

STRINGER 21R FROM STA 907 919 HAS ELONGATED HOLES. REMOVED DAMAGED STRINGER FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 53 00 03.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

STRINGER 20R FROM STA 847 907 HAS ELONGATED HOLES. REMOVED DAMAGED SECTION OF STR 20R FABRICATED AND INSTALLED NEW SECTION OF STR 20R IAW B737 400 SRM 51 40 02 AND 51 40 05.

Part: STRINGER SPLICE — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

STR 22R STA 907 STR SPLICE HAS SEVERAL ELONGATED HOLES. RECEIVED NEW STR SPLICE LOCATED AND DRILLED NEW PART AND INSTALLED IAW B737 400 SRM 51 40 05.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

STR 23R HAS ELONGATED HOLES BETWEEN STA 907 919 IN PREVIOUS REPAIR AREA. REMOVED DAMAGED AREA FABRICATED NEW STRINGER AND REPAIR PARTS. INSTALLED REPLACEMENT PARTS IAW B737 400 SRM 51 40 02.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

STRINGER 24R FROM STA 907 919 HAS SEVERAL ELONGATED HOLES. REMOVED DAMAGED SECTION OF STRINGER. RECEIVED NEW PART LOCATED DRILLED AND INSTALLED NEW SECTION OF STR 24R IAW B737 400 SRM 51 40 02 AND 51 40 05.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

STRINGER 21R FROM STA 847 907 HAS ELONGATED HOLES. REMOVED DAMAGED SECTION OF STRINGER 21R. FABRICATED AND INSTALLED NEW STRINGER SECTION IAW B737 400 SRM 51 40 05 AND 51 40 02.

Part: SPLICE — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

STA 908 BUTT SPLICE BETWEEN STR 21R 26R HAS OVERSIZED HOLE FROM PREVIOUS REPAIR. FABRICATED NEW BUTT SPLICE IAW B737 400 SRM 51 40 05 PART TO BE INSTALLED ON NR 5327462.

Part: SKIN — DENTED (TE FLAP) · airframe 58,719 hrs · 32,117 cycles

RIGHT INBOARD AFT FLAP UPPR SURFACE HAS A DENT 33 INCHES FROM INBOARD END AND 6.5 INCHES FROM TRAILING EDGE. (WBL 103 TO WBL 109). REMOVED DAMAGED AREA FABRICATED REPAIR PARTS AND BONDED THE REPAIR IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: STRINGER CLIP — GOUGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

AFT PIT STRINGER TIE AT STA 867 STR 20R IS GOUGED ON THE AFT SIDE. REMOVED AND REPLACED STR TIE AT STA 867 STR 20R IAW B737 400 SRM 51 40 02 AND 51 40 05.

Part: AILERON — CRACKED (RIGHT) · airframe 58,719 hrs · 32,117 cycles

RT AILERON O/B LOWER LANDING FOR ACCESS PANEL IS CRACKED AT NUT PLATE HOLE. PREPPED DAMAGED AREA AND REPAIRED IAW B737 400 SRM 51 70 05 REPAIR 11.

Part: SPLICE — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

SCRIBE AT BS 727G BETWEEN STR 9R 10R. REMOVED DAMAGED BUTT SPLICE STRAP FABRICATED REPLACEMENT PARTS AND INSTALLED IAW B737 400 SRM 51 40 02 AND 51 40 05.

Part: SPLICE — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

SCRIBE AT BS 500C BETWEEN STR 6L AND 7L. REMOVED DAMAGED BUTT SPLICE FABRICATED REPLACEMENT PARTS AND INSTALLED REPLACEMENT SPLICE STRAP IAW B737 400 SRM 51 40 02 AND 51 40 05.

Part: SPLICE — DAMAGED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

SCRIBE AT BS 727G BETWEEN STR 10R 13R. REMOVED DAMAGED BUTT SPLICE STRAP FABRICATED REPLACEMENT STRAP AND INSTALLED REPAIR IAW B737 400 SRM 51 40 02 AND 51 40 05.

Part: SKIN — DENTED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

AT STA 922 STR 23L FOUND NEW DENT IN FUSELAGE SKIN COMMON TO STRUCTURE. FABRICATED REPAIR PARTS AND INSTALLED REPAIR IAW ASA EA 400 53EA 05830

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 58,719 hrs · 32,117 cycles

CARGO TRACK CORRODED AT STA 747 767 RBL 13. REMOVED DAMAGED SECTION. REPAIRED WITH FABRICATED SECTION PER B737 400 SRM 53 00 53.

Part: SKIN — DENTED (FUSELAGE) · airframe 58,719 hrs · 32,117 cycles

SKIN DENTED AT BODY STA 1019 STR 14L FOUND TO BE WITHIN 3 INCHES OF BUTT SPLICE. REMOVED DAMAGED AREA FABRICATED REPAIR PARTS AND INSTALLED IAW ASA EA 400 53EA 05858.

Part: DOOR — BINDING (CABIN) · airframe 58,587 hrs · 32,049 cycles

L1 DOOR WILL NOT CLOSE WITHOUT DOOR BEING PUSHED OR PULLED TO ENGAGE LATCH ROLLERS. ACCOMPLISHED L1 FWD ENTRY DOOR FLUSHNESS AND HANDLE TORQUE AMM DEVIATIONS PER ASA EA 400 52EA 05564.

Part: LATCH — OBSTRUCTED (L2 DOOR) · airframe 58,116 hrs · 31,754 cycles

F/A'S UNABLE TO ARM L2 (AFT ENTRY DOOR) CLEANED DEBRIS FROM LATCH. SLIDE ARMS NORMAL PER B737 400 AMM 25 61 35.

Part: TAB — DELAMINATED (AILERON) · airframe 56,557 hrs · 30,885 cycles

LT AILERON TAB TRAILING EDGE SEPARATING. REPAIRED DAMAGE.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,557 hrs · 30,885 cycles

DENT AT BS 1008.5 BETWEEN STRINGER 13L. REPLACED SKIN.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,204 hrs · 11,582 cycles

F5 578 STRINGER 5R CLIP IS CRACKED. REMOVED AND REPLACED STRINGER 5R CLIP F5 578.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,204 hrs · 11,582 cycles

UPPER FUSELAGE FRAME ATTACH CLIP AT STRINGER 10R IS CRACKED. REMOVED AND REPLACED STRINGER CLIP.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,204 hrs · 11,582 cycles

F5 500G STRINGER 5R CLIP IS CRACKED. REMOVED AND REPLACED STRINGER 5R CLIP AT F5 500G.

Part: SKIN — DELAMINATED (RT WING) · airframe 33,204 hrs · 11,582 cycles

RIGHT WING NR 5 O/B EDGE UPPER SURFACE HAS DELAMINATED AREA. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLERS AND BONDED REPAIR.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 33,204 hrs · 11,582 cycles

F5 500F STRINGER 5R CLIP IS DAMAGED. REMOVED AND REPLACED STRINGER 5R CLIP.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 33,204 hrs · 11,582 cycles

LEFT NR 1 SLAT AFT O/B UPPER CORNER DELAMINATED. REMOVED DAMAGED SKIN, FABRICATED REPAIR DOUBLER AND BONDED REPAIRS.

Part: BRACKET — CRACKED (CARGO BAY) · airframe 54,440 hrs · 29,644 cycles

AFT CARGO BAY SUB THRESHOLD SUPPORT ANGLE BRACKET CRACKED. REMOVED AND REPLACED SUPPORT ANGLE/BRACKET.

Part: SHEAR TIE — MISINSTALLED (FUSELAGE) · airframe 35,619 hrs · 15,960 cycles

SHEAR TIE STA 807 STR 27 L STR 27R IMPROPERLY INSTALLED. REPAIRED SHEAR TIE.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 54,440 hrs · 29,644 cycles

FLOOR TO SIDEWALL SUPPORT PLATE CRACKED. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 54,440 hrs · 29,644 cycles

STRINGER CLIP CORRODED. REMOVED STR CLIP REPLACED WITH NEW PER SRM

Part: DOOR — DEFECTIVE (L1) · airframe 53,461 hrs · 29,068 cycles

L1 DOOR HANDLE OPERATION HEAVY. INSIDE HANDLE FORCE MEASURED AT 80FT LBS OR 960 IN LBS. INITIATED MIG2C 238622 238626 250736 &250735.AGT22771. REMOVED AND REPLACED L1 DOOR PER MM 52 11 00. DOOR ADJUSTMENT & LEAK CHECK OK PER MM 52 11 00. SEE MIG2C 250733 250735 250736 240948 238626 &238622 FOR ALL WORK ACCOMPLISHED.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 53,459 hrs · 29,066 cycles

PRESSURIZATION IN AUTO CABIN RATE OF CLIMB FLUCTUATED + OR 50 FPM SWITCHED TO STANDBY AND FLUCTUATION INCREASED TO + OR 400 FPM. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER IAW MM 21 31 21 PERFORMED OP'S CHECK IAW MM 21 31 00 FAILED FOR MANUAL DC INDICATIONS SUSPECT OUTFLOW VALVE BAD PLACE ORDER . REMOVED AND REPLACED OUTFLOW VALVE AND OPS CHECKED GOOD IAW MM 21 31 11 STEPS 1 307 AND 3E DUE TO TIME CONSTRAINTS THE SEALANT HAS BEEN OMITTED AT THIS TIME AND HIGH SPEED TAPE INSTALLED IAW EA 2130 01057. SEALANT TO BE APPLIED WITHIN 50 FLT HRS.

Part: SKIN — PUNCTURED (ELEVATOR) · airframe 53,358 hrs · 32,175 cycles

RT ELEVATOR UPPER SURFACE PUNCTURED 45 INCHES FROM INBD END AND 19.6 FROM HINGE CENTERLINE AFT. REPAIRED PUNCTURE WITH GRAPHITE REPAIR PATCH.

Part: FLAP TRACK — CORRODED (TE FLAP) · corrosion level 2 · airframe 53,458 hrs · 29,064 cycles

NR 1 FLAP TRACK HAS SEVERAL AREAS OF PITTING CORROSION ON ROLLER SURFACE. REMOVED AND REPLACED NR 1 FLAP TRACK IAW MM 27 51 49.

Part: FLAP TRACK — CORRODED (TE FLAP) · corrosion level 2 · airframe 53,458 hrs · 29,064 cycles

NR 8 FLAP TRACK HAS SEVERAL AREAS OF PITTING CORROSION ON ROLLER SURFACE. REMOVED AND REPLACED NR 8 FLAP TRACK IAW MM 27 51 49.

Part: SUPPORT — CORRODED (CARGO BAY) · airframe 53,458 hrs · 29,064 cycles

CARGO BAY TIE DOWN TRACK SUPPORT CORRODED. REPLACED.

Part: SUPPORT CHANNEL — GOUGED (LT WING) · airframe 53,458 hrs · 29,064 cycles

LT WING SUPPORT CHANNEL AT RSS 500 GOUGED REPLACED CHANNEL.

Part: SUPPORT CHANNEL — GOUGED (RT WING) · airframe 53,458 hrs · 29,064 cycles

RT WING T/E SUPPORT CHANNEL AT RSS 500 GOUGED. REPLACED CHANNEL.

Part: TORQUE TUBE — GOUGED (CARGO DOOR) · airframe 53,458 hrs · 29,064 cycles

C1 TORQUE TUBE GOUGED. REPLACED TORQUE TUBE.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 53,458 hrs · 29,064 cycles

REINFORCEMENT STRAP BS 847 FRAME BETWEEN STR 23R AND 25 R HAS ELONGATED HOLES. REPLACED STRAP.

Part: CASTING — WORN (APU DOOR) · airframe 53,458 hrs · 29,064 cycles

APU DOOR DOUBLER AND CASTING WORN. REPLACED DOUBLER AND CASTING.

Part: TORQUE BOX — CRACKED (FUSELAGE) · airframe 53,458 hrs · 29,064 cycles

TORQUE BOX WEB CRACKED AT BS 699, RBL 61, WL 178. REPLACED WEB.

Part: FRAME — GOUGED (BS 847) · airframe 53,458 hrs · 29,064 cycles

GOUGE OUT OF LIMITS ON FRAME CLOSE OUT WEB. FABRICATED NEW WEB.

Part: PRESSURE PANEL — DAMAGED (NLG WW) · corrosion level 2 · airframe 53,458 hrs · 29,064 cycles

CORROSION ON NOSE WHEEL WELL UPPER LT PRESSURE PANEL NR 3107. REPLACED PANEL.

Part: WEB — GOUGED · airframe 53,458 hrs · 29,064 cycles

LW DOGHOUSE PANEL OTBD NR 1 PYLON GOUGED. REPLACED PANEL.

Part: STIFFENER — DAMAGED (BS 699) · airframe 53,458 hrs · 29,064 cycles

RT WHEEL WELL CUTOUT VERTICAL STIFFENER IS DAMAGED. REPLACED STIFFENER.

Part: DOOR FRAME — BROKEN (FUSELAGE) · airframe 53,458 hrs · 29,064 cycles

CLOSEOUT WEB BROKEN AT LOWER FASTENER IN AFT CARGO BAY FWD DOOR FRAME. REPLACED WEB.

Part: SUPPORT — CORRODED (BS 727-727H) · corrosion level 2 · airframe 53,458 hrs · 29,064 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED. REPAIRED.

Part: SKIN — DAMAGED (WING) · airframe 53,458 hrs · 29,064 cycles

FIXED L/E SKIN DAMAGED AT 31 SLAT I/B AUX TRACK CUTOUT. DAMAGE REPAIRED.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 53,358 hrs · 32,175 cycles

LEFT I/B FORE FLAP UPPER T/E SKIN IS DELAMINATED 34 INCHES FROM O/B END AND 8.5 INCHES FROM AFT END. REPAIRED LEFT I/B FORE FLAP UPPER T/E SKIN IS DELAMINATION. MATERIAL USED 2024 T3.

Part: SKIN — GOUGED (EXHAUST GATE) · airframe 53,358 hrs · 32,175 cycles

RIGHT I/B E GATE UPPER SKIN GOUGED BEYOND REPAIR. REMOVED AND REPLACED RIGHT I/B E GATE UPPER SKIN MATERIAL 2219 T62.

Part: FRAME — CRACKED (FLAP CARRIAGE) · airframe 53,458 hrs · 29,064 cycles

LEFT O/B MIDFLAP NR 2 CARRIAGE A FRAME IS CRACKED. REPLACED CRACKED A FRAME OF THE LEFT O/B MIDFLAP NR 2 CARRIAGE. CFE SERVICEABLE PART PO 311981 AND INSTALLED TO THE NR 2 CARRIAGE PER SOPM 20 50 01.

Part: SKIN — DEBONDED (LE SLAT) · airframe 53,458 hrs · 29,064 cycles

NR 5 O/B END CAP HAS COMPOSITE DAMAGE. REPAIRED NR 5 SLAT PER CMM 57 56 12.

Part: RIB — CRACKED (FOREFLAP) · airframe 53,458 hrs · 29,064 cycles

FOUND I/B FORE FLAP TRACK RIB INSTALLATION I/B RIB TO BE CRACKED AT LOWER FLANGE ON RIGHT O/B MID FLAP. THE I/B FOREFLAP TRACK I/B RIB WAS REMOVED AND REPLACED WITH NEW PER SRM 51 40 02.

Part: FRAME — CORRODED (BS 877) · airframe 53,458 hrs · 29,064 cycles

AFT CARGO FRAME REPLACEMENT. REPLACED FRAME.

Part: SKIN — DEBONDED (LE SLAT) · airframe 53,458 hrs · 29,064 cycles

NR 4 SLAT HAS DISBOND AT I/B END. REPAIRED DISBOND PER SRM 51 10 02.

Part: FILLER — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FWD ENTRY DOOR CUTOUT UPPER HINGE CUTOUT FILLER CRACKED IN TWO PLACES. REPLACED FILLER.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

L1 DOOR LOWER HINGE CUT OUT CRACK ON BEAR STRAP BS 304.5 WL 238. REPAIRED.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

L1 DOOR UPPER HINGE CUTOUT CRACK ON BEAR STRAP BS 304.5 WL 258.75. REPAIRED BEAR STRAP.

Part: SKIN — CHAFED (MIDFLAP) · airframe 53,358 hrs · 32,175 cycles

RIGHT O/B MIDFLAP L/E SKIN CHAFED 3 INCHES FOR I/B END. RIGHT O/B MIDFLAP L/E SKIN WAS REPAIRED PER SRM 57 53 01.

Part: SKIN — DENTED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

SKIN INDENTATIONS WILL REQUIRE PERMANENT REPAIR PER SRM 53-00-01. REPAIRED SKIN.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

L1 DOOR LOWER CUTOUT CRACK ON BEAR STRAP BS 304.5 WL 235. REPAIRED.

Part: SKIN — CHAFED (TE FLAP) · airframe 53,358 hrs · 32,175 cycles

RIGHT O/B MIDFLAP O/B AFT LOWER PANEL UPPER SURFACE IS CHAFED AT NR 3 AND NR 4 AFT FLAP TRACK. REPAIRED RIGHT O/B MIDFLAP O/B AFT LOWER PANEL UPPER SURFACE IS CHAFED AT NR 3 AND NR 4 AFT FLAP TRACK.

Part: SKIN PANEL — GOUGED (MIDFLAP) · airframe 53,358 hrs · 32,175 cycles

LEFT O/B MIDFLAP O/B AFT LOWER AFT PANEL UPPER SURFACE IS GOUGED AT NR 3 AND NR 4 AFT FLAP TRACK. REPAIRED CHAFING DAMAGE ON LEFT O/B MID FLAP O/B LWR AFT SKIN PANEL UPPER SURFACE.

Part: SKIN — CHAFED (MIDFLAP) · airframe 53,358 hrs · 32,175 cycles

LEFT O/B MIDFLAP L/E SKIN CHAFED 4 INCHES AT I/B END. REPAIRED LEFT O/B MIDFLAP L/E SKIN PER SRM 57 53 01.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

CORROSION AFT CARGO COMPARTMENT FOUND CORROSION ON THE RT SIDEWALL TO FLOOR SUPPORT BS 757-787. REPAIRED SIDEWALL/FLOOR SUPPORT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,729 hrs · 28,614 cycles

FUSELAGE SKIN HAS A 2" CRACK ON RT SIDE JUST AFT OF WING TO BODY FAIRING. INSTALL DOUBLER PER SRM 53 00 01.

Part: SEAT TRACK — DEFECTIVE (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

BS 500B RBL 24 SEAT TRACK INERFERES WITH SEAT INSTALLATION BS 500B TO BS 500D RBL 24. SEAT TRACK REPLACED IAW B737 400 SRM 53 00 52 REPAIR 1 FIG 201.

Part: STRINGER — DENTED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

STR 19L DENTED ON FREE FLANGE AT ST 477 STR 19L. FREE FLANGE AT STA 477 FOUND TO BE BEYOND ALLOWABLE LIMITS AND REPAIRED IAW B737 400 SRM 53 00 03 FIG 101 & FIG 201.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FUSELAGE STR 14R HAS DRILL BIT DAMAGES AT 3 LOCATIONS BETWEEN STA 500F+16 & 500 G + 4. REPAIRED WITH MADE REPAIR PARTS.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FWD CARGO PIT BS 400 TO 420 LBL 24 INTERCOSTAL CRACKED. CASCADE RESPONSIBILITY REPAIRED WITH REPAIR PARTS.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

BS 348.5 STR I5L & 16L 8 HOLES CRACKED. FRAME FOUND NOT TO BE CRACKED. ANGLE AT BS 348 STR 16 LT FOUND CRACKED AT FASTENER HOLES AND REPLACED WITH NEW PART IAW B737 400 SRM 51 40 02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FUSELAGE SKIN DAMAGE AT 500 E 3" BELOW STR 13R (CASCADE RESPONSIBILITY HUMAN FACTORS). REPAIRED WITH REPAIR PART.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FUSELAGE FRAME CRACKED AT BS 827 RT BETWEEN STR 13R AND 14R. FUSELAGE FRAME AT BS 827 RT BETWEEN STR 13R AND 14R REPAIRED IAW ASA DRAWING A 53100264247.

Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 50,105 hrs · 27,176 cycles

NR 5 SLAT HAS DELAM AT I/B AFT CORNER. REPAIRED NR 5 SLAT AT I/B END IAW B737 400 SRM CH 51 70 10 REPAIR 4.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

THREE CRACKS FOUND ON WINDOW FRAME AT BS 500G 500F RT. NEW WINDOW FRAME WAS TRIMMED AND INSTALLED IAW ASA EO 5330 02294.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

CORROSION FOUND ON FLOORBEAM AROUND SCREW HOLD AT BS 360 RBL 2. REPAIRED WITH MADE REPAIR PARTS.

Part: PANEL — CHAFED (L/E SLAT) · airframe 50,105 hrs · 27,176 cycles

NR 5 SLAT INBOARD END COVE PANEL INNER SURFACE AT END CAP LOCATION CHAFING DAMAGE. ON NR 5 SLAT INBOARD END COVE PANEL INNER SURFACE AT END CAP REPAIR IAW B737 400 SRM 57 43 01 FIG 201.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

SURFACE CORROSION UNDER FLOORBOARD 24794 ATTACH HOLES CORRODED. SUPPORT TEE UNDER FLOORBOARD REPLACED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FWD CARGO RBL 21 INTERCOSTAL CRACKED BS 500 F TO 500 G. INTERCOSTAL REPLACED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FWD CARGO RBL 21 INTERCOSTAL CRACKED AT BS 500 D TO 500 E. CASCADE RESPONSIBILITY INTERCOSTAL REPLACED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FWD CARGO RBL 21 FLOOR INTERCOSTAL CRACKED BS 500 C TO 500 D. CASCADE RESPONSIBILITY INTERCOSTAL REPLACED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FWD CARGO RBL 21 BS 500 E TO 500 F INTERCOSTAL CRACKED. CASCADE RESPONSIBILITY INTERCOSTAL REPLACED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FWD CARGO LBL 21 FLOOR INTERCOSTAL CRACKED BS 500 L TO 500 D. CASCADE RESPONSIBILITY INTERCOSTAL REPLACED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FWD CARGO LBL 21 INTERCOSTAL CRACKED AT BS 500A TO 500B. CASCADE RESPONSIBILITY INTERCOSTAL REPLACED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FWD CARGO LBL 21 FLOOR INTERCOSTAL CRACKED AT BS 500E TO 500F. CASCADE RESPONSIBILITY INTERCOSTAL REPLACED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FWD CARGO PIT LBL 21 FLOOR INTERCOSTAL CRACKED BS 500 B TO 500 C. CASCADE RESPONSIBILITY INTERCOSTAL REPLACED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FWD CARGO LBL 21 FLOOR INTERCOSTAL CRACKED AT BS 500D TO 500E. CASCADE RESPONSIBILITY INTERCOSTAL REPLACED.

Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 50,105 hrs · 27,176 cycles

NR 5 SLAT HAS DELAM AT O/B AFT END. REPAIRED NR 5 SLAT AT O/B AFT END IAW B737 400 SRM CH 51 70 10 REPAIR 4.

Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 50,105 hrs · 27,176 cycles

NR 1 SLAT HAS DELAM AT O/B AFT END. REPLACED NR 1 SLAT DELAMINATED AT O/B AFT END IAW B737 400 SRM CH 51 70 10 REPAIR 4.

Part: ANGLE — BROKEN (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FWD CABIN BS 345 LBL 64 WL 216 ANGLE BROKEN. BROKEN ANGLE AT BS 345 LBL 216 REPLACED WITH MADE REPAIR PART IAW B737 400 SRM 51 40 02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FWD GALLEY SERVICE DOOR WAY FLOOR ATTACH ANGLE FWD OF FWD STUB FRAME CRACKED AT AFT FASTENER HOLE ATTACHMENT TO LOWER SILL CHORD. REPAIRED WITH REPAIR PART.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FWD GALLEY SERVICE DOORWAY FWD STUB FRAME CRACKED AT BOTTOM FASTENER HOLE ATTACHING TO LOWER SILL CHORD. ONE CRACK FOUND AFTER SILL CHORD WAS REMOVED, REPAIRED WITH MADE REPAIR PART.

Part: SKIN — GOUGED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FUSELAGE GOUGE AT BS 500 G+1" 2" BELOW STR 13R (CASCADE RESPONSIBILITY HUMAN FACTORS). REPAIRED WITH REPAIR PART.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

BS 727 G FUSELAGE FRAME CRACKED AT FASTENER HOLE BETWEEN STR 13L 14L. REPAIRED WITH MADE REPAIR PART.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

AFT CABIN R2 DOOR SILL CHORD FOUND CORRODED AT BS 947+10 TO BS 988. SILL CHORD REPLACED WITH NEW PART.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

BS 500F FUSELAGE FRAME CRACKED AT FASTENER HOLE BETWEEN STR 13R AND 14R BS 500 F. FUSELAGE FRAME BETWEEN STR 13R AND STR 14R REPAIR IAW JA DRAWING A53100264248 AND EO 5310 02642.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

CORROSION ON FLOORBEAM MULTIPLE AREAS AT BS 324 RBL 10 TO RBL 30. REPAIRED WITH REPAIR PART.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

FLOORBEAM AT FS 328 BL 0 CORROSION AT SCREW HOLE. FLOORBEAM AT FS 328 BL 0 REPAIRED IAW B737 400 SRM 53 10 51 FIG 201.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

FWD GALLEY SERVICE DOOR SILL CHORD FROM STA 291.5 TO 330 IS CORRODED. SILL CHORD REPLACED WITH NEW PART.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

E & E COMP CORROSION FOUND ON FRAME SUPPORT ANGLE BS 328 AT STR 28R. E & E COMP FRAME SUPPORT ANGLE REPLACED WITH MADE REPAIR PART IAW B737 400 SRM 53 10 07 FIG 1.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

CORROSION ON VERTICAL STIFFENER AT BS 328 AND STR 28 RT. VERTICAL STIFFENER REPLACED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

BS 520 FUSELAGE FRAME CRACKED AT FASTENER HOLE BETWEEN STR 13L 14L. REPAIRED WITH MADE REPAIR PART.

Part: ATTACH BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT STRINGER TO INTERCOSTAL ATTACH BRACKET EXFOLIATED AT BS 767+6 RBL 20. AFT CARGO PIT ATTACHED STRINGER TO INTERCOSTAL AT BS 767+6 RBL 20 REPLACED WITH MADE REPAIR PART IAW B737 400 SRM 51 30 01 AND 51 40 02.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

CORROSION ON BS 328 FRAME AT STR 28R. CORROSION ON FRAME AT BS 328 STR 28R BLENDED BEYOND LIMITS IAW B737 400 SRM 53 10 07 FIG 1. REPAIR PART MADE FROM 0.0407 7075TG PDH 10978S AND 0.052" 7075TG PDH 11425 IAW B737 400 SRM 53 00 07. REPAIR 5 FIG 201. REPAIR PART INSTALLED IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

BS 727G FUSELAGE FRAME CRACKED AT FASTENER HOLD BETWEEN STR 13L 14L. CRACKED FRAME REPAIRED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

FLOORBEAM AT FS 294 BL L CORROSION AROUND SCREW HOLE. CORROSION BLENDED OUT AND FOUND TO BE BEYOND LIMITS. MATERIAL REMOVED 0.030" OUT OF 0.100" THE ORIGINAL THICKNESS. REPAIRED IAW B737 400 SRM CH 53 10 51 FIG 201.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

CORROSION ON BS 344 FRAME AT STR 28R CORROSION ON FRAME AT BS 344 STR L8R BLENDED OUT AND FOUND TO BE BEYOND LIMITS. REPAIR PARTS MADE FROM 0.040" 707ST6 PDH 109 785 AND 0.050" 7075T6 PDH109785 AND 0.050" 7075 T6 PDH 11425 IAW B737 400 SRM 53 00 07 REPAIRS FIG 201 AND INSTALLED IAW B737 400 SRM 53 00 07 REPAIR 5 FIG 201.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

FWD CARGO COMP FRAME REINFORCEMENT AT STA 500D RBL 28 IS CORRODED. REPAIRED WITH REPAIR PARTS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

BS 460 FUSELAGE FRAME CRACKED AT FASTENER HOLE BETWEEN STR 13L 14L. REPAIRED WITH MADE REPAIR PART.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT INTERCOSTAL AT BS 787 792 RBL 19 FOUND CORRODED. REPAIRED WITH REPAIR PART.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

FWD CARGO BILGE T/E FRAME AT FS 480 BL 2" L CORRODED SHEAR TIE. SHEER TIE REPAIRED WITH REPAIR PART.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

CORROSION ON VERTICAL STIFFENER AT BS 344 AND STR 28 RT. VERTICAL STIFFENER REPLACED.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

E+E COMP CORROSION FOUND ON FRAME SUPPORT ANGLE BS 344 AT STR 28R CORROSION ON FRAME ANGLE AT BS 344 STR 28R FOUND TO BE BEYOND LIMITS IAW B737 400 SRM 53 00 07 FIG 101. MADE REPAIR PART AND INSTALLED REPAIR PART IAW B737 400 SRM 51 30 01 51 40 05 AND 51 40 02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FWD CARGO PIT FLOOR SUPPORT INTERCOSTAL FOUND CORRODED AT BS 500F TO 500G LBL 24. INTERCOSTAL REPLACED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

FLOORBEAM AT FS 312 BL 2L TO BL 11R HAS CORROSION AROUND SCREW HOLES. FLOORBEAM REPAIRED WITH REPAIR PART.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

BS 500 E FUSELAGE FRAME CRACKED AT FASTENER HOLE BETWEEN STR 13L 14L BS 500 E. FRAME BETWEEN STA 13L AND 14L REPAIRED IAW ASA EO 5310 02642 AND ASA DRAWING A 53100264248.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT CORROSION ON BS 794 FRAME BETWEEN STR 25R AND 26R. REPAIRED WITH REPAIR PART.

Part: WEB — SCRATCHED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

E AND E COMPT DOOR CMT RT WEB SCRATCHES FOUND ABOUT LATCH FITTING. WEB REPLACED.

Part: CHANNEL — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

TRANSFERRED FROM NR 5116889 BEYOND LIMITS DAMAGE TO FLOOR CHANNEL BS 767+4 LBL 8 AFT CARGO PIT. REPAIRED WITH REPAIR PART.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

SEAT TRACK GOUGED BS 500 B+8 TO 500 L+12 RBL 25. REPAIRED WITH REPAIR PART.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

SEAT TRACK CORRODED BS 500 + 18 LBL 45. REPAIR WITH REPAIR PART.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

SEAT TRACK GOUGED BS 500D TO 500E RBL 45. REPLACED WITH MADE REPAIR PART.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

SEAT TRACK CORRODED BS 480 TO 500 RBL 45. SEAT TRACK REPLACED WITH REPAIR PART.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

SEAT TRACK GOUGED AT STA 727 B+4 LBL 45. SEAT TRACK REPAIR WITH NEW PART.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

SEAT TRACK GOUGED AT STA 536 LBL 25. SEAT TRACK REPLACED WITH NEW PART.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

SEAT TRACK AT BS 536 RBL 25 GOUGED. SEAT TRACK REPAIRED WITH NEW PART.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

SEAT TRACK GOUGED STA 727 B+4 "7" LBL 25. SEAT TRACK REPLACED.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

SEAT TRACK GOUGED STA 727 B+ (4" 7") LBL 25. REPAIRED WITH NEW PART.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

SEAT TRACK GOUGED AT STA 520 LBL 25. REPAIRED WITH NEW PART.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

SEAT TRACK AT STA 500 F+10" RBL 45 GOUGED. SEAT TRACK REPLACED WITH REPAIR PART.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

SEAT TRACK AT STA 536 RBL 45 GOUGED. REPAIRED WITH NEW PART.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

SEAT TRACK AT BS 536 RBL 45 GOUGED. SEAT TRACK REPLACED WITH NEW PART.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

SEAT TRACK GOUGED (2 PLACES) AT BS 536 LBL 45. REPLACED WITH NEW PART.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

SEAT TRACK AT STA 661 LBL 25 GOUGED SEAT TRACK AT STA 661 LBL 25. REPAIRED IAW B737 400 SRM 53 00 52 REPAIR 6.

Part: FRAME — CRACKED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT BS 787 BODY FRAME SKIN ATTACHMENT CRACKED AT STR 27R DUET. CORROSION REPAIR BODY FRAME TO SKIN ATTACHMENT ON AFT CARGO PIT. BS 787 STR 27R IAW B737 400 SRM 53 00 07 FIG 201.

Part: INTERCOSTAL — BENT (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FWD CARGO PIT INTERCOSTAL IS BENT BS 440 460 LBL 25. REPLACED WITH MADE REPAIR PART.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

STRINGER SPLICE CHANNEL CRACKED AT STR 15L AND BS 360. REPAIRED IAW ASA RA 5310 02 758.

Part: INTERCOSTAL — BENT (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FWD CARGO COMP INTERCOSTAL IS BENT AT BS 440 460 LBL 25. REPAIRED WITH REPAIR PART.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

CORROSION FOUND ON LOWER TEE STRINGER AT APU INLET TORQUE BOY RT SIDE. CORROSION ON LOWER TEE STRINGER WAS BLENDED OUT AND FOUND BEYOND ALLOWABLE IAW B737 400 SRM 53 80 13. REMOVED TEE STRINGER AND INSTALLED NEW PART IAW B737 400 SRM 51 40 02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT FAILSAFE ANGLE AT BS 907 STR 26R TO STR 27R FOUND CORRODED. REPAIRED WITH MADE REPAIR PART.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

TIE CLIP FOUND CRACKED AT STA 500G STR 7L. REPLACED WITH NEW PART.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT MAIN FRAME AT BS 727 G STR 24R 25R FOUND CORRODED. AFT CARGO PIT MAIN FRAME AT BS 727G REPAIRED IAW B737 400 SRM 51 70 11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

CORROSION FOUND ON FLOORBEAM AT BS 294 RBL 10 TO RBL 20. CORROSION BLENDED OUT FOUND TO BE BEYOND LIMITS. REPAIR & PART INSTALLED IAW B737 400 SRM CH 53 10 51 FIG 201.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

FWD CARGO COMP BILGE VHF NR 2 ANTENNA SUPPORT CHANNEL AND MOUNT PLATE AT STA 515 BL 0 HAS CORROSION. FWD CARGO VHF NR 2 ANTENNA SUPPORT REPLACED WITH MADE REPAIR PART IAW B737 400 SRM.

Part: INTERCOSTAL — CRACKED (FSUELAGE) · airframe 50,105 hrs · 27,176 cycles

FWD CARGO COMP INTERCOSTAL AT STA 500A RBL 27 IS CRACKED. INTERCOSTAL REPLACED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

CABIN FLOOR INTERCOSTAL STA 350 400 AT BL 0 IS CRACKED AT SCREW HOLES. REPAIRED WITH REPAIR PART.

Part: TIE CLIP — BROKEN (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

TIE CLIP BROKEN AT BS 294.5 S13L. REPAIRED IAW ASA EA 5310 02758.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT FLOOR CHANNEL FOUND CORRODED AT BS 767+6 LBL 8. REPAIRED WITH REPAIR PART.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT TIE DOWN TRACK LUG FOUND CORRODED AT BS 727 D LBL 17. TIE DOWN LUG REPLACED.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

FWD CARGO PIT 'Z' ANGLE FOUND CORRODED AT BS 500 A TO 500 G RBL 24. REPAIRED WITH REPAIR PART.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT LEFT TIE DOWN TRACK FOUND CORRODED ON LUG AT BS 847 LBL 17. REPAIRED WITH REPAIR PART.

Part: CARGO TRACK — GOUGED (CARGO BAY) · airframe 50,105 hrs · 27,176 cycles

FWD CARGO PIT RT TIE DOWN TRACK HAS GOUGED AT BS 460 + 2 RBL 14. FWD CARGO PIT RT TIE DOWN TRACK AT BS 460 REPAIRED IAW B737 400 SRM 53 00 53.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

FWD CARGO PIT FLOOR SUPPORT INTERCOSTAL CORRODED BS 500F TO 500G LBL 24. INTERCOSTAL REPLACED.

Part: SUPPORT FITTING — CHAFED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

R2 DOOR CUTOUT CHAFING DAMAGE ON DOOR SILL SUPPORT FITTING AT BS 966 STR 17R. REPAIRED WITH NEW PART.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

FWD CARGO PIT ZEE WEB BETWEEN BS 440 AND BS 420 STR 26 RT SIDE HAS DENT WITH CRACK. FWD CARGO PIT ZEE WEB REPLACED WITH MADE REPAIR PART IAW B737 400 SRM DWG 65 20725.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT FLOOR CHANNEL FOUND CORRODED AT BS 727F+8 LBL 11. REPAIRED WITH MADE REPAIR PARTS.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT FLOOR CHANNEL FOUND CORRODED AT BS 767+6 LBL 13. REPAIRED WITH REPAIR PART.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT FLOOR CHANNEL AT BS 790 TO 867 RBL 8 FOUND CORRODED. REPAIRED WITH REPAIR PART.

Part: CHANNEL — CRACKED (FSUELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT FLOOR CHANNEL FOUND CORRODED AT BS 767+6 RBL 8. REPAIRED WITH REPAIR PART.

Part: SKATE ANGLE — CHAFED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

CHAFING DAMAGE FOUND ON VERTICAL STAB TO FUSELAGE LT SKATE ANGLE. CHAFING DAMAGE FOUND ON VERTICAL STAB TO FUSELAGE AT LT SKATE ANGLE REPAIRED IAW ALASKA EA 5310 02769.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT FLOOR CHANNEL FOUND CORRODED AT BS 727 F + 8 RBL 3. AFT CARGO PIT FLOOR CHANNEL AT BS 727+8 RBL 3 REPAIRED IAW ASA EA 5310 02764.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT FLOOR CHANNEL FOUND CORRODED AT BS 767+6 TO BS 847+14 RBL 3. REPAIRED WITH REPAIR PART.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT FLOOR CHANNEL FOUND CORRODED AT BS 727 F +8 LBL 3. REPAIRED WITH REPAIR PART.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT FLOOR CHANNEL AT BS 847+14 867+14 LBL 3 FOUND CORRODED. REPAIRED WITH REPAIR PART.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT ATTACHED ANGLE INTERCOSTAL TO FRAME AT BS 847 RBL 19 FOUND CORRODED. INTERCOSTAL REPLACED DUE TO CRACK (CORROSION WITHIN SRM LIMITS).

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT LT TIE DOWN TRACK AT BS 947 LBL 17 FOUND CORRODED. REPAIRED WITH MADE REPAIR PART.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT FLOOR CHANNEL AT BS 847+14 TO 867 LBL 8 FOUND CORRODED. REPAIRED WITH REPAIR PART.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT RT TIE DOWN TRACK AT BS 767 TO 827 RBL 13 FOUND CORRODED. TIE DOWN TRACK REPLACED WITH NEW PART.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,105 hrs · 27,176 cycles

AFT CARGO PIT FLOOR CHANNEL FOUND CORRODED AT BS 767+6 LBL 3. REPAIRED WITH REPAIR PART.

Part: SKIN — DAMAGED (HORIZ STAB) · airframe 48,893 hrs · 26,517 cycles

LEFT HORIZONAL STABILIZER LEADING EDGE DAMAGED IN TWO LOCATIONS FROM FORKLIFT. INSTALLED TWO TEMPORARY EXTERNAL DOUBLERS THAT MUST BE INSPECTED EVERY A-CHECK. PERMANENT REPAIR TO BE INSTALLED AT NEXT HEAVY CHECK.

Part: SKIN — DENTED (HORIZ STAB) · airframe 48,844 hrs · 26,494 cycles

RIGHT HORIZONAL STAB DENT AT STA 212.3 TO 221.5. DENT IS 5" L X 2.2" W X .082 DEEP. RECHECKED DIMENSIONS. DENT IS NOW A ZONE 3 DENT. INSPECTED INTERNAL VISUAL INSPECTION OF DAMAGE AREA EVERY 400 FLT HRS OR LESS. IF CRACKS ARE FOUND OR DAMAGE BECOMES BIGGER REPAIR IMMEDIATELY. INSTALL A PERM REPAIR AFTER NO MORE THAN 5K FLT HRS OR 18 MONTHS WHICHEVER COMES FIRST.

Part: SKIN — DENTED (HORIZ STAB) · airframe 48,853 hrs · 26,498 cycles

RIGHT HORIZONAL STAB DENTED AT STA 212.3 TO STA 221.5. DENT IS 5" L X 2.2" W X .082 DEEP. RECHECKED DIMS. DENT IS NOW A ZONE 3 DENT. INSP INTERNAL VISUAL INSPECTION OF DAMAGE AREA EVERY 400 FLT HRS OR LESS. IF CRACKS ARE FOUND OR DAMAGE BECOMES BIGGER REPAIR IMMEDIATELY. INSTALL A REPAIR AFTER NO MORE THAN 5000 FLT HRS OR 18 MONTHS WHICHEVER COMES FIRST.

Part: SKIN — DENTED (BS 847-867) · airframe 46,881 hrs · 25,332 cycles

TWO DENTS COMMON TO THE FUSELAGE SKIN AT BS 847 - 867 STR 20. THE DAMAGE IS BEYOND SRM LIMITS DUE TO THE PROXMITY TO THE AFT CARGO DOOR CUTOUT AND EXITING REPAIR. REPAIRED SKIN IAW ASA EA 5330 02166.

Part: FLOORBEAM — CORRODED (BS 987) · airframe 46,881 hrs · 25,332 cycles

FLOORBEAM AT BS 987 HAS CORROSION BETWEEN LBL 35 AND RBL 35. REPAIRED BS 987 FLOORBEAM IAW ASA EA 5310 02685.

Part: FRAME — CRACKED (BS 492 S16-25R) · airframe 46,881 hrs · 25,332 cycles

FWD CARGO DOORWAY AFT FRAME NDT INDICATES CRACK BELOW FITTING AT STR 24R. REMOVED AND INSTALLED NEW CARGO FRAME IAW SRM 51-40-02 PG 6.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,881 hrs · 25,332 cycles

FLOORBEAM STA 967 IS CORRODED BETWEEN LBL 30 AND RBL 30 UPPER CHORD. REMOVED CORRODED SECTION OF FLOORBEAM UPPER CHORD. FABRICATED AND INSTALLED REPAIR CHORD ANGLES AND STRAPS IAW SRM 53-00-51 FIG 201 REPAIR 2.

Part: SILL — CORRODED (FUSELAGE) · airframe 46,881 hrs · 25,332 cycles

L2 DOOR MOPSILL IS CORRODED. REMOVED AND REPLACED L2 DOOR MOPSILL INNER IAW SRM.

Part: SKIN — DENTED (FUSELAGE) · airframe 46,881 hrs · 25,332 cycles

DENT IN FUSELAGE SKIN BETWEEN STR 27 28L AT STA 356. REMOVED DAMAGED AREAS OF SKIN FABRICATED AND INSTALLED REPAIR DOUBLER IAW ASA EA 5330 02163.

Part: SKIN — DENTED (FUSELAGE) · airframe 46,881 hrs · 25,332 cycles

DENT IN FUSELAGE SKIN BELOW LAST WINDOW ON ACFT RT SIDE AT STRINGER 17. REMOVED EXISTING REPAIR PIECES ABOVE DENT, REMOVED DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED REPAIR FILLERS DOUBLERS AND TRIPLER IAW ASA EA 5330 02164.

Part: REPAIR — CORRODED (FUSELAGE) · airframe 46,881 hrs · 25,332 cycles

BS 947 FLOORBEAM HAS CORROSION ON EXISTING REPAIR AT RBL 4 FASTENER HOLE. REMOVED EXISTING REPAIR. REMOVED UPPER CHORD FROM LBL 32.75 RBL 12. FABRICATED AND INSTALLED UPPER CHORD SPLICE ANGLES STRAPS AND FILLERS IAW ASA EA 5310 02684.

Part: WEB — CORRODED (BS 794-847) · airframe 46,881 hrs · 25,332 cycles

AFT PIT FLOOR WEB CORRODED JUST INSIDE CARGO DOOR. REMOVED CORRODED WEB INSTALLED NEW WEB IAW SRM 51 40 02.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 46,881 hrs · 25,332 cycles

LT OB FORE FLAP DELAMINATED AT IB EDGE. PREPPED AREA FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW SRM 51 70 10 PG 244.

Part: SKIN — DENTED (BS 869 S20L) · airframe 46,881 hrs · 25,332 cycles

FUSELAGE SKIN DENTED AT BS 869 JUST BELOW STR 20L. REMOVED DAMAGED AREA OF SKIN FABRICATED AND INSTALLED REPAIR FILLER DOUBLER AND TRIPLER IAW SRM 53 00 01 FIG 201 REPAIR 31.

Part: SKIN — DELAMINATED (AFT FLAP) · airframe 46,881 hrs · 25,332 cycles

LT OB AFT FLAP IB END IS DELAMINATED. PREPPED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW SRM 51 70 10 PG 249.

Part: STRINGER — DAMAGED (BS 900 S15R) · airframe 46,881 hrs · 25,332 cycles

STR 15R APPROX STA 900 HAS HOLE IN RADIUS. REMOVED DAMAGED SECTION OF STRINGER FABRICATED AND INSTALLED REPAIR STRINGER HEAT SPLICE AND FILLERS IAW SRM 53 00 03 FIG 201 REPAIR 1.

Part: REPAIR — TEMPORARY (FS 960)

YXX - TEMP REPAIR AT STRINGER 25 LEFT BS 837, AFT CARGO DOOR CUTOUT LOWER CORNER. REMOVED AND REPLACED REPAIR WITH PERM REPAIR PER B737-2000 SRM 53-00-01 FIG 201. (M)

Part: SKIN — DAMAGED (FUSELAGE)

OAK - FUSELAGE EXTERNAL STATION 540-1016 AT FS 837 BELOW AFT PIT DOOR REQUIRES REPLACEMENT PER EM 5330-01579, STEP 8. REMOVED EXTERNAL SKIN LAP JOINT REPAIR AT FS 837, STRINGER 25R BELOW AFT CARGO DOOR. ACCOMPLISH INTERIM REPAIR PER EA. PERM REPAIR TO BE ACCOMPLISHED WITHIN 6000 FLT CYCLES OR SEPT 2006 WHICH EVER OCCURS FIRST. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

OAK - FOUND AFT CARGO COMPARTMENT DOOR JAMB WEB IS CORRODED. REPLACED WEB. (M)

Part: SKIN — GOUGED (RT PYLON)

OAK - FOUND RIGHT PYLON SKIN GOUGED AT OUTBOARD NACELLE. BLENDED GOUGE AND INSTALLED WEAR STRIP. (M)

Part: SKIN — GOUGED (RT PYLON)

OAK - FOUND RIGHT PYLON SKIN GOUGED AT INBOARD NACELLE. INSTALLED WEAR STRIP. (M)

Part: PANEL — GOUGED (RT PYLON)

OAK - FOUND RIGHT PYLON PANEL NR 5829R HAS TWO GOUGES IN DOUBLER. INSTALLED REPAIR STRAP AND DOUBLER. (M)

Part: SKIN — DENTED (FORE FLAP)

OAK - FOUND RIGHT WING FORE FLAP DENTED ON LOWER SURFACE. CUT OUT DAMAGED AREA, INNER CORE REPLACEMENT AND BONDED EXTERNAL DOUBLER. (M)

Part: FRAME — DAMAGED (FUSELAGE)

OAK - FOUND LOWER FUSELAGE AFT CARGO COMPARTMENT LOWER LEG CIRCUMFERENTIAL FRAME BETWEEN CENTER FLOOR SUPPORTS 727B MATERIAL OUT OF LIMITS ON UT INSPECTION. REF SRM, ORIGINAL THICKNESS .063 INCH, REMAINING .055 INCH. INSTALLED DOUBLER REPAIR ON CIRCUMFERENTIAL FRAME BETWEEN CENTER FLOOR SUPPORTS AT STATION 727B PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FS)

OAK - FOUND AFT CARGO COMPARTMENT BILGE FLOOR SUPPORT CORRODED. REPLACED SECTION OF FLOOR SUPPORT. (M)

Part: ANGLE — CORRODED (FUSELAGE)

OAK - FOUND AFT CARGO COMPARTMENT ZEE ANGLE CORRODED. REPLACED ZEE ANGLE. (M)

Part: SKIN — GOUGED (LT PYLON)

OAK - FOUND LEFT PYLON SKIN GOUGES. INSTALLED WEAR STRAP PER EA 5430-01135. (M)

Part: SKIN — GOUGED (LT PYLON)

OAK - FOUND LEFT PYLON SKIN HAS GOUGES. INSTALLED WEAR STRAP PER EA 5430-01134. (M)

Part: ANGLE — CORRODED (FUSELAGE)

FOUND LOWER FUSELAGE AREA BELOW AFT CARGO COMPARTMENT BILGE LT ZEE ANGLE FROM 727-750 SPLICE IS CORRODED. REMOVED AND REPLACED ZEE ANGLE LT STATION 727-750 IN REF TO SRM 53-60-53 FIG 204 PGS 208-209. (M)

Part: ANGLE — CORRODED (FUSELAGE)

OAK - FOUND LOWER FUSELAGE AREA BELOW AFT CARGO COMPARTMENT BILGE LEFT ZEE ANGLE FROM STATION 750 TO 790 IS CORRODED. REMOVED AND REPLACED AFT CARGO COMPARTMENT ZEE ANGLE FROM STATION 750 TO 790. REF SRM 53-60-53 PGS 208-209 FIG 204. (M)

Part: LIGHT — INOPERATIVE (ROW 10-11)

SEA - FOUND ROW 10-11 EMERGENCY AISLE LIGHTING DO NOT ILLUMINATE. REPLACED BOTH LIGHT ASSEMBLYS, OPS CHECK NORMAL. (M)

Part: WIRE — BROKEN (EMERGENCY LIGHT)

WHILE CLEARING MEL FOR MISSING LENS FOR THE FLOOR TRACK LIGHTING AT ROW 10, FOUND TRACK LIGHTING INOPERATIVE, ROWS 13-16 AND ROWS 21-23. REPAIRED BROKEN WIRES. (M)

Part: SUPPORT — CORRODED (FLOORBOARD)

DURING C-CHECK, FOUND FLOORBOARD SUPPORT STRAP AT STA 767 CORRODED. REPAIRED IAW SRM. (M)

Part: ANGLE — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND CHINE ANGLE AT STATION 947 TO 992 CORRODED. REPAIRED IAW SRM. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND INTERCOSTAL CORRODED AT FS 947-967 CORRODED. REPAIRED IAW SRM. (M)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND SUPPORT ANGLE AT FS 767-807 CORRODED. REPAIRED IAW SRM. (M)

Part: ANGLE — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND CHINE ANGLE AT STATION 947 TO 992 CORRODED. REPAIRED IAW SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND FLOORBEAM AT STATION 947 CORRODED. REPAIRED IAW SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND UPPER FUSELAGE FLOOR SUPPORT TEE ANGLE CORRODED. REPAIRED IAW SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND SUPPORT ANGLE AT SERVICE DOORWAY CORRODED AT FS 328-295. REPAIRED IAW SRM. (M)

Part: FITTING — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND LAV ATTACH FITTING CORRODED ON FLOORBEAM AT STATION 947.5 AND WL 208. REPAIRED IAW SRM. (M)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND SIDE WALL SUPPORT ANGLE AT FS 328 TO 340 CORRODED. REPAIRED IAW SRM. (M)

Part: ANGLE — WORN (FUSELAGE)

OAK - DURING C-CHECK, FOUND SUPPORT FRAME ANGLES AT STATION 1016 HAVE WORN GROOVES FROM RUDDER CABLES. REPAIRED IAW EA. (M)

Part: FITTING — CORRODED (GIRT BAR)

OAK - DURING C-CHECK, FOUND CORROSION ON GIRT BAR FLOOR FITTING AT STATION 334 AND STRINGER 17. REPAIRED IAW SRM. (M)

Part: RIB — CRACKED (WING)

DURING CHECK FOUND RIB CRACKED AT WBL 135.5 AND BETWEEN STR 2 AND 3. REPAIRED IAW SRM AND EA.

Part: TERMINAL — DISCONNECTED (CABIN)

FAI - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTING AT ROWS 9, 10 AND 11 INOPERATIVE. RECONNECTED WIRE TERMINAL ENDS. LIGHTS THEN FUNCTIONED PROPERLY. (M)

Part: SKIN — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND SKIN BENEATH MARKER BEACON ANTENNA IS CORRODED AT BS 625, WL 148.5 AND BL 00. REPAIRED IAW EA. (M)

Part: SKIN — DENTED (CARGO DOOR)

PAE - DURING SI CHECK, FOUND FORWARD CARGO DOOR REQUIRED RESKIN DUE TO NUMEROUS OUT OF LIMIT DENTS. REMOVED AND REPLACED FORWARD CARGO DOOR EXTERNAL SKIN IAW SRM. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION ON AFT CARGO BAY FRAME AT BS 787 RBL 20 AND WL 160. REPAIRED IAW SRM. (M)

Part: DOOR FRAME — CHAFED (L1 DOOR)

PAE - DURING SI CHECK, FOUND L1 DOOR FORWARD FRAME CHAFED JUST ABOVE 4TH STOP PIN FROM THE TOP. REPAIRED IAW EA. (M)

Part: SKIN — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND SKIN BENEATH MARKER BEACON ANTENNA IS CORRODED AT BS 510, WL 148.5 AND BL 00. REPAIRED IAW EA. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND FRAME AT BS 794, RBL 20 WL 153 IS CORRODED. REMOVED AND REPLACED FRAME IAW SRM 53-00-07. (M)

Part: FAILSAFE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON FAIL/SAFE AT BS 946 RBL 18, AND WL 175. REMOVED AND REPLACED IAW SRM. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - BEFORE FLIGHT, FOUND EMERGENCY TRACK LIGHTS AT ROWS 4-6 DISCONNECTED. RECONNECTED WIRE, OPERATIONAL CHECK GOOD. (M)

Part: ANGLE — CORRODED (FUSELAGE)

SEA - DURING 92 INSPECTION, FOUND CORROSION ON L1 DOOR SKATE ANGLE UNDER AFT LEFT CORNER OF FORWARD LAVATORY FLOOR PANEL AT BS 301 TO 307 AND WATERLINE 208.1 AND BUTTOCK LINE 56.5. REPAIRED IAW EA 5310-01923. (M)

Part: SILL — CORRODED (FUSELAGE)

SEA - DURING 9C INSPECTION, FOUND CREASE BEAM CORROSION ON FORWARD ENTRY DOOR SILL AT BS 316 TO BS 343 AND FROM WATERLINE 208.1 LEFT TO BUTTOCK LINE 62 LEFT HAND. REPAIRED IAW ASA EA 5310-01922 AND SRM. (M)

Part: FITTING — CORRODED (FUSELAGE)

SEA - DURING 9C INSPECTION, FOUND AFT PIT TIE DOWN FITTING AT BS 947 AND WATERLINE 165 AND RBL 13.8 CORRODED AT FLOOR PANEL SCREW ATTACH HOLE. REPAIRED PER EA 5320-01451. (M)

Part: LIGHT — INOPERATIVE (ROW 17)

SEA DURING MAINTENANCE CHECK THE EMBERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 9-11 AND 13-17 WERE FORUND TO BE INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AT ROW 17 AND RECONNECTED THE WIRING AT ROW 9, ALL LIGHTS OPERATED NORMALLY.

Part: SEAL — LOOSE (PAX DOOR)

SEA - PRIOR TO FLIGHT 175, THE L1 DOOR WAS FUOND TO BE DIFFICULT TO CLOSE. RESECURED DOOR SEAL AND DOOR OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROW 13)

SEA - FLT 177 - CREW REPORTED EMERGENCY EXIT FLOOR TRACK LIGHT INOPERATIVE AT MID CABIN. RECONNECTED RED LIGHT AT ROWS 13 AND LIGHTS OPERATED NORMALLY. (M)

Part: CONNECTOR — DISCONNECTED (ROW 14)

GEG - PRIOR TO FLT 480 - THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 14-16. RECONNECTED WIRING/CONNECTION AT ROW 14, LIGHTS OPERATED NORMALLY. (M)

Part: SKIN — DAMAGED (NR 2 & 3 SLAT)

SEAT - DURING SCHEDULED C-CHECK, THE FIXED LEADING EDGE COMPOSITE SKIN BETWEEN NR 2 AND NR 3 SLAT WAS FOUND TO BE DAMAGED. REPAIRED PER EA 5740-01195. (M)

Part: SKIN — GOUGED (RT WING TE FLAP)

SEA - DURING SCHEDULED C-CHECK, THE RIGHT INBOARD FLAP WAS GOUGED AT THE INBOARD LOWER BOLT HOLE FOR ELEPHANT EAR ATTACHMENT. REPAIRED PER EA 5750-01376. (M)

Part: SKIN — GOUGED (RUDDER)

SEA - DURING SCHEDULED C-CHECK, THE RIGHT SIDE OF THE RUDDER LEADING EDGE SKIN WAS FOUND TO BE GOUGED. REPAIRED PER EA 5540-01041. (M)

Part: WIRE — DISCONNECTED (ROWS 18 - 19) · corrosion level 3 · airframe 24,837 hrs · 13,441 cycles

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 18-19 WERE FOUND INOPERATIVE. RECONNECTED LOOSE WIRING/CONNECTOR AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD SECTION OF THE EMERGENCY EXIT FLOOR TRACK LIGHT WIRING WAS FOUND DISCONNECTED. RE-CONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE AFT 4 EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING/LIGHTS AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE AFT 4 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS, LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PSP - PRIOR TO FLIGHT 585 - SEVERAL EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE IN FORWARD CABIN. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 17 AND THE AFT FOUR LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT TWO RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 15 AND 16 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD AND AFT EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD TWO AND AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE FORWARD THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SFO - FLT 377 - PRIOR TO FLGHT SEVERAL EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE TOWARDS THE AFT CABIN. RECONNECTED WIRING AND THE LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT GALLEY RT INBOARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FWD 2 RED EMERGENCY EXIT LIGHTS AND THE EMERGENCY EXIT LIGHTS FROM ROW 27 AFT WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AT BOTH LOCATIONS AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD 2 RED EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED SECOND LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE FROM ROW 26 AFT. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: SLIDE — OUT OF LIMITS (L2 DOOR)

PDX - DURING MAINTENANCE CHECK THE L2 DOOR EVAC SLIDE PRESSURE GAUGE WAS FOUND TO BE READING OUT OF LIMITS. MAINTENANCE REPLACED THE L2 DOOR EVAC SLIDE AND GAUGE INDICATED NORMAL. PART TOTAL CYCLES, 315. (X)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE ROW 26 AFT. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT FORWARD GALLEY, ROWS 14 THROUGH 16, AND ROW 27 AFT. RECONNECTED, REPAIRED, AND RESEATED TRACK LIGHT ASSEMBLIES WIRING AT THE AFFECTED ROWS AND LIGHTS OPERATED NORMALLY. (M)

Part: RIVETS — LOOSE (NR 1 NACELLE)

SEA - DURING STRUCTURAL INSPECTION, THE NR 1 ENGINE NACELLE AFT FAIRING END CAP WAS FOUND TO HAVE LOOSE RIVETS. REPAIRED PER EA 5750-01212 AND BOEING TELEX ASA-SEA-96-0203RR. TT: 16,604 HOURS. TC: 8,816. (X)

Part: FIRE WALL — DAMAGED (NR 2 PYLON)

SEA - DURING STRUCTURAL INSPECTION, THE NR 2 ENGINE PYLON, VERTICAL FIRE WALL, AFT SIDE OF FORWARD ENGINE MOUNT WAS FOUND DAMAGED/TORN BY DUCT CLAMP. REPAIRED PER EA 5410-01020 AND BOEING TELEX PAL-MNL-97-0071RR. TT: 16,604 HOURS. TC: 8,816. (X)

Part: WEDGE — DAMAGED (LT TE FOREFLAP)

SEA - DURING STRUCTURAL INSPECTION, THE LT OUTBOARD FOREFLAP T/E WEDGE WAS FOUND TO HAVE A HOLE IN THE LOWER SURFACE AT WBL 386. REPAIRED PER EA 5750-01249 AND BOEING TELEX ASA-SEA-97-0253TR. TT: 16,604 HOURS. TC: 8,816. (X)

Part: FLAP CARRIAGE — CORRODED (RT TE MIDFLAP)

SEA - DURING STRUCTURAL INSPECTION, THE RT INBOARD MID-FLAP INBOARD CARRIAGE OUTBOARD TRACK MOUNT BOLT WAS FOUND CORRODED. REPAIRED PER EA 5753-01005 AND BOEING TELEX ASA-SEA-97-0364RR. TT: 16,604. TC: 8,816. (X)

Part: FIRE WALL — TORN (NR 1 PYLON)

SEA - DURING STRUCTURAL INSPECTION, FOUND THE NR 1 ENGINE PYLON VERTICAL FIRE WALL AFT OF FORWARD ENGINE MOUNT IS TORN AND BENT. REPAIRED PER EA 5410-01020 AND BOEING TELEX PAL-MNL-97-0071RR. TT: 16,604 HOURS. TC: 8,816. (X)

Part: TRUNNION — CORRODED (BS 277)

SEA - DURING STRUCTURAL INSPECTION, THE LEFT NLG TRUNNION BEARING SUPPORT BORE WAS FOUND CORRODED AND PITTED. REPAIRED PER EA 5310-01545 AND BOEING TELEX ASA-SEA-97-0343RR. TT: 16,604 HOURS. TC: 8,816. (X)

Part: SKIN — CHAFED (RT TE MIDFLAP)

SEA - DURING STRUCTURAL INSPECTION, THE RT OUTBOARD T/E MID-FLAP INBOARD FORWARD CORNER WAS FOUND CHAFED. REPAIRED PER EA5750-01166 AND BOEING TELEX ASA-SEA-94-0483TR AND ASA-SEA-94-0559RR. TT: 16,604 HOURS. TC: 8,816. (X)

Part: FLOOR BEAM — CORRODED (BS 947)

SEA - DURING STRUCTURAL INSPECTION, THE FLOOR BEAM UPPER FLANGE AT BS 947 BETWEEN RBL 4 AND LBL 4 WAS FOUND CORRODED. REPAIRED PER EA 5310-01551. TT: 16,604 HOURS. TC: 8,816. (X)

Part: FLAP CARRIAGE — CORRODED (LT TE MIDFLAP)

SEA - DURING STRUCTURAL INSPECTION, THE LT INBOARD MID-FLAP CARRIAGE INBOARD AND OUTBOARD ATTACH BOLT HOLES WERE FOUND PITTED. REPAIRED PER EA 5753-01006 AND BOEING TELEX ASA-SEA-97-0364RR. TT: 16,604 HOURS. TC: 8,816. (X)

Part: BULKHEAD SEAL — TORN (BS 1016)

SEA - DURING STRUCTURAL INSPECTION THE PRESSURE BULKHEAD AT STA 1016, LOWER WEATHER SEAL WAS FOUND TORN. REPAIRED PER EA 5320-01318. TT: 16,604 HOURS. TC: 8,816. (X)

Part: FLOOR PAN — CORRODED (BS 277)

SEA - DURING STRUCTURAL INSPECTION, THE FORWARD LAVATORY FLOOR PAN WAS FOUND DAMAGED/CORRODED AT THE LOWER AFT WALL TO THE FLOOR JOINT AND ALONG DOOR OPENING. REPAIRED PER EA 2540-01026. TT: 16,604 HOURS. TC: 8,816. (X)

Part: BATTERY CHARGER — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT IDENTIFIER LIGHTS AT THE L2 AND R2 DOORS, R2 EXTERIOR LIGHT, AND ROW 24 RIGHT BULLNOSE CAME ON BRIGHT AND FADED TO OFF WITHIN 30 SECONDS. REPLACED THE BATTERIES AND THE BATTERY PACK/CHARGERS AT THE L2 AND R2 DOORS AND THE LIGHTS OPERATED NORMALLY. REFERENCE ASAA970031.

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT IDENTIFIER LIGHTS AT THE L2 AND R2 DOORS, R2 EXTERIOR LIGHT, AND ROW 24 RIGHT BULLNOSE CAME ON BRIGHT AND FADED TO OFF WITHIN 30 SECONDS. REPLACED THE BATTERIES ADN THE BATTERY PACK/CHARGERS AT THE L2 ADN R2 DOORS AND THE LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE L-1 DOOR EMERGENCY EXIT IDENTIFIER AND THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 4 THROUGH 9 WERE FOUND INOPERATIVE. REPLACED BATTERY PACK/CHARGER, LIGHTS OPERATED NORMALLY. (M)

Part: LAMP — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT SIX EMERGENCY EXIT TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED THREE TRACK LIGHT MODULES AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 5-12. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - FLT 417 - PRIOR TO DEPARTURE, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 13. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 14-17. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 14. RECONNECTED WIRING TO LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANE CHECK, THE EMERGNECY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE IN THE MID CABIN AND THE AFT TWO RED LIGHTS WERE FOUND INOPERATIVE. REPAIRED BROKEN WIRING AT ROW 15 SIDEWALL AND AT THE AFT SECTION OF TRACK. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENACNE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 15 THROUGH 17. RECONNECTED WIRING AT ROW 17 AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CEHCK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT THE FORWARD OVERWING AREA. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 14. RECONNECTED LOOSE WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - FLT 467 - PRIOR TO FLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 15. RECONNECTED/REPAIRED WIRING AT LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 13 AND 14 WERE FOUND TO BE INOPERATIVE. SECURED LOOSE WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLY AT ROW 15 AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 9-13. REPAIRED BROKEN WIRE AT FLOOR FEED AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, ALL FOUR RED AND ONE WHITE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT OVERWING EXITS. RECONNECTED TRACK LIGHT WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, SIX EMERGENCY EXIT FLOOR TRACK LIGHTS IN MID CABIN WERE FOUND INOPERATIVE. RECONNECTED LIGHTS AND SECURED TRACK, LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT FLOOR TRACKS LIGHTS WERE FOUND INOPERATIVE. REPLACED AFT FLOOR LIGHT ASSEMBLIES AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUR EMERGENCY EXIT FLOOR TRACK LIGHTS IN MID-CABIN AND THREE AFT EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED LOOSE WIRING AND ALL LIGHTS OPERATED NORMALLY. (X)

Part: LENSES — MISSING (CABIN)

SEA - FLT 315 - TWO LENS COVERS FOR EMERGENCY EXIT FLOOR TRACK LIGHTING MISSING AT ROW 17. RELAMPED AND INSTALLED MISSING LENSES; LIGHTS OPERATED NORMALLY. REFERENCE: OPERATOR CONTROL NR ASAA9640050.

Part: LAMPS — FAILED (CABIN)

SEA - FLT 315 - TWO LENS COVERS FOR EMERGENCY EXIT FLOOR TRACK LIGHTING MISSING AT ROW 17. RELAMPED AND INSTALLED MISSING LENSES; LIGHTS OPERATED NORMALLY. REFERENCE: OPERATOR CONTROL NR 96ZZZX3979. (X)