N724SW

Part: PANEL — ELONGATED (FUSELAGE) · airframe 76,696 hrs · 45,425 cycles

PANEL#193D HAS NUMEROUS WORKING COUNTERSINKS AND ELONGATED HOLES. ; / [01] REMOVED AND REPLACED PANEL PER AMM 53-51-21.

Part: PANEL — ELONGATED (FUSELAGE) · airframe 76,696 hrs · 45,425 cycles

PANEL#194E HAS WORKING COUNTERSINKS AND ELONGATED HOLES. ; PANEL#194E HAS NUMEROUS WORKING COUNTERSINKS AND ELONGATED HOLES. / [01] REMOVED AND REPLACED PER AMM 53-51-21.

Part: FLOOR PANEL — CORRODED (LAVATORY) · airframe 76,251 hrs · 45,160 cycles

WHILE WORKING DISCREPANCY FROM LP 1735036; AFT LAV DOOR IS BROKEN; FOUND CORROSION IN FLOOR BELOW DOOR STRIKE PANEL IN AFT LAVATORY. AFT LAVATORY 'B' WAS REPLACED ON TASK CARDS TTG8Q005ZB06 AND TTG8Q005ZB06.

Part: SLAT — FAULTY (LT WING) · airframe 75,476 hrs · 44,716 cycles

LE FLAPS TRANSIT LIGHT STAYED ILLUMINATED FLAPS 1-5. PERFORMED QRH PROCEDUE & DID A FLAPS 15 LNDG.. GREEN LE FLAPS EXT LIGHT ILLUMINATED UPON SELECTING FLAPS 15. / R&R #1 SLAT PER MM 27-81-21 INDICATION OPS CHECK GOOD PER MM 27-88-21 SLAT POSITION PN # ON 114A5010-3 SN # ON 000454 PN # OFF 114A5010-3 SN # OFF 000208 RAR # 96481

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 75,337 hrs · 44,638 cycles

PANEL 193B HAS DELAMINATED CORNER AND SEVERAL OVERSIZED HOLES / R&R PANEL I.A.W. A.M.M. 53-51-21 AND S.R.M. 51-40-02; 51-40-05; 51-40-08.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 74,270 hrs · 44,021 cycles

LT OVER WING EXIT DOOR FWD EMERGENCY EXIT SIGN LENS IS CRACKED. REMOVED AND REPLACED LT OVER WING EXIT DOOR FWD EMERGENCY EXIT SIGN LENS, PER AMM 33-51-01-960-801 STEP 2B(1) 4 AND STEP 2B(4).

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,270 hrs · 44,021 cycles

BATTERY CHARGER M1669 TEST BUTTON IS INOPERABLE. REMOVED AND REPLACED BATTERY CHARGER M1669 AND PERFORMED GOOD INSTALLATION TEST, PER AMM 33-51-06-960-806. 81136U 07OCT20.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,270 hrs · 44,021 cycles

EMERGENCY EXIT LIGHTS COMMON TO BATTERY PACK M1669 ARE INOPERABLE. REMOVED & REPLACED BATTERY PACK M1669, PER AMM 33-51-06-960-805 AND AMM 33-51-00-710-801. 59924C 06OCT20 PERFORMED GOOD OPERATIONAL TEST.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,270 hrs · 44,021 cycles

EMERGENCY EXIT LIGHTS COMMON TO BATTERY PACK M1672 ARE INOPERABLE. REMOVED & REPLACED AND OF BATTERY PACK M1672, PER AMM 33-51-06-960-805 AND AMM 33-51-00-710-801 59924C 06OCT20. PERFORMED GOOD OPERATIONAL TEST.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,270 hrs · 44,021 cycles

LEFT OVERWING EXTERIOR EXIT LIGHT IS OUT. RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF LT OVERWING EXIT EXTERIOR LIGHT, PER AMM 33-51-04-960-801. LENS ASSEMBLY WILL BE REINSTALLED ON NRC U220200.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,270 hrs · 44,021 cycles

LEFT OVER WING EXIT IDENTIFIER FWD SIDE HAS LAMPS OUT. RELAMPED AND PERFORMED GOOD FUNCTIONAL TEST OF LEFT OVERWING EXIT IDENTIFIER FWD SIDE, PER AMM 33-51-01-960-801.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 74,270 hrs · 44,021 cycles

RIGHT OVER WING EXIT LIGHT ABOVE HAS BURNED OUT LAMPS. RELAMPED AND PERFORMED GOOD FUNCTIONAL TEST OF RIGHT OVERWING EXIT LIGHT ABOVE, PER AMM 33-51-01-960-801.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,270 hrs · 44,021 cycles

RIGHT OVER WING EXIT IDENTIFIER FWD SIDE HAS LAMPS OUT. RELAMPED AND PERFORMED GOOD FUNCTIONAL TEST OF RIGHT OVERWING EXIT IDENTIFIER FWD SIDE, PER AMM 33-51-01-960-801.

Part: SHIELD — CORRODED (FWD CARGO) · airframe 74,270 hrs · 44,021 cycles

SHIELD AFT OF FWD CARGO DOOR HAS CORROSION AROUND NUT PLATE HOLES BS500 TO BS500A RBL23 WL156 / EVALUATED CORROSION ON SHIELD AFT OF FWD CARGO DOOR FOUND TO BE OUT OF LIMITS DUE TO NO SRM LIMITS; REPLACEMENT REQUIRED IAW SRM 51-10-02-0G-0 PARA 9. REMOVED AND REPLACED SHIELD AFT OF FWD CARGO DOOR BS500 TO BS500A; RBL23; WL156 IAW SRM 51-40-02-0G-0 PARA 4(B) AND DWG 143A0080

Part: STRINGER — CORRODED (BS 536 S25R) · airframe 74,270 hrs · 44,021 cycles

CORROSION COMMON TO END OF STR25R IN SNAKE PIT BS536 WL154 / REPAIRED STR 25 R/H IN FCB SNAKE PIT BS 536 WL154 PER ER 20-03337 REV IR AND EA 20-153-01958 REV IR

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 74,270 hrs · 44,021 cycles

AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS CORROSION AROUND NUT PLATE HOLES BETWEEN BS747 AND BS767 RBL21 WL156 / EVALUATED CORROSION ON ACB RH FLOOR TO SIDEWALL SUPPORT; REMOVED; .015' FROM ORIG .040'; FOUND TO BE OUT OF LIMITS; IAW SRM 53-00-53-1A-2. LOCATED AND DRILLED; AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT; BS727-767 R/H; IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 146A7500.

Part: WEB — CORRODED (BS 767-787) · airframe 74,270 hrs · 44,021 cycles

AFT CARGO BAY VERTICAL WEB BETWEEN BS767 AND BS787 RBL6 WL151 HAS CORROSION AROUND FASTENERS / VERTICAL WEB BS 767 - 787 RBL 6 WL 151; FOUND TO BE OUT OF LIMITS DUE TO NO SRM LIMITS. REMOVED AND REPLACED VERTICAL WEB PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 146A8130.

Part: SEAT TRACK — DAMAGED (BS 519-520) · airframe 74,270 hrs · 44,021 cycles

MECHANICAL DAMAGE ON SEAT TRACK ON CROWN BS 519-520; LBL 45; WL 208, MARKED. REMOVED DAMAGE ON SEAT TRACK CROWN BS 519-520; LBL 45; WL 208. MAX MATERIAL REMOVED WAS 0.030' 1' X 1' ON TOP, PER SRM 51-10-02-0G-0. DAMAGE FOUND TO BE OUT OF LIMITS, PER SRM 53-00-52-1A-1. REMOVED AND REPLACED SEAT TRACK BS 480-520; LBL 45; WL 208, PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; AND BOEING DWG 143A5300.

Part: STRINGER — CRACKED (BS 536) · airframe 74,270 hrs · 44,021 cycles

STR 26L IS CRACKED COMMON TO END OF STRINGER IN SNAKE PIT BS 536 WL 152. REMOVED DAMAGED SECTION OF STR 26-L AND INSTALLED REPAIR PARTS AT S-26L BS500D+4'-540, IAW SRM 53-00-03-2R-1 AND DWG 143A3230; 143A1215.

Part: SEAT TRACK — CORRODED (BS 480-520) · airframe 74,270 hrs · 44,021 cycles

***CORROSION*** CORROSION IN VARIOUS LOCATIONS ON SEAT TRACK IN WELL; BS 480-520; LBL 45; WL 208. MARKED. / SEAT TRACK TO BE REPLACED ON U129849.

Part: SKIN — CRACKED (BS 767) · airframe 74,243 hrs · 44,007 cycles

1 EACH CRACK FOUND FUSELAGE CROWN SKIN FS 767 2 RIGHT OF STRINGER 1R AND 11' AFT FS 767 AND CRACK IS 0.75' LONG. REPAIRED PER EA 20-153-01667 INTERIM REPAIR SEE 943.

Part: STRINGER — CRACKED (BS 767) · airframe 74,243 hrs · 44,007 cycles

DURING INSPECTION IN SI 12095 FOUND 0.75' CRACK 2' R OF STRINGER 1 AND 11' AFT OF BS 767 ON FUSELAGE CROWN SKIN. TRANSFERRED TO LP 1450217.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 74,111 hrs · 43,925 cycles

FWD CARGO FLOOR PANEL 120CF DAMAGED / REMOVED AND REPLACED FWD CARGO FLOOR PANEL 120CF IAW AMM 25-52-01

Part: COVER — OUT OF POSITION (R2 DOOR) · airframe 74,111 hrs · 43,925 cycles

AFT SERVICE DOOR EMERGENCY SLIDE; PULL HANDLE COVER IS NOT IN PLACE. REPOSITIONED AFT SERVICE DOOR EMERGENCY SLIDE; PULL HANDLE COVER PER MT 725-61-06.

Part: BATTERY — FAILED (CABIN) · airframe 72,655 hrs · 42,999 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1674. / R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 72,655 hrs · 42,999 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. / R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 72,655 hrs · 42,999 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. / R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 72,655 hrs · 42,999 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. / R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 72,655 hrs · 42,999 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1668. / R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 72,655 hrs · 42,999 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. / R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 72,655 hrs · 42,999 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1671. / R&R BATTERY PER AMM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 70,216 hrs · 41,388 cycles

AFT SERVICE DOOR FO SIDE LOWER EXIT LIGHT COVER MISSING REPLACED COVER AS REQUIRED REF SIP & AMM 33-51-01

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,860 hrs · 41,159 cycles

INTERCOSTAL CRACKED BETWEEN BS 270 TO BS 294.5, RBL 1. R&R INTERCOSTAL IAW DWG & SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,860 hrs · 41,159 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 45. R&R INTERCOSTAL IAW SRM & DWG.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 69,860 hrs · 41,159 cycles

PASSENGER CABIN, FLOORBOARD 222CF DAMAGED AT EDGE AND INSERTS. REPAIRED FLOORBOARD IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,860 hrs · 41,159 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 45. R&R INTERCOSTAL IAW SRM & DWG.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 69,860 hrs · 41,159 cycles

PASSENGER CABIN, FLOORBOARD 222BF DAMAGED INSERTS. REPAIRED FLOORBOARD IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,860 hrs · 41,159 cycles

FLOORBEAM CRACKED AT BS 328 RBL 20 NEAR FLOOR BOARD SCREW HOLE. REPAIRED FLOORBEAM PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,860 hrs · 41,159 cycles

FORWARD GALLEY AREA INTERCOSTAL CRACKED BETWEEN BS 294.5 TO BS 312, RBL 15. R&R INTERCOSTAL PER SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,860 hrs · 41,159 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 30. R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FWD GALLEY) · airframe 69,855 hrs · 41,158 cycles

FOUND INTERCOSTAL CRACKED IN FWD. GALLEY AREA AT LOCATION 15 RBL BETWEEN STA 294.5 AND STA 312 / DEFECT TRANSFERRED TO NON ROUTINE CARD # T918557

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,855 hrs · 41,158 cycles

INTERCOSTAL BETWEEN STA 312 AND STA328 30' RBL IS CCRACKED. / TRANSFERRED TO LOG PAGE 0927735

Part: INTERCOSTAL — CRACKED (FWD GALLEY) · airframe 69,855 hrs · 41,158 cycles

FOUND INTERCOSTAL CRACKED IN FWD GALLEY AREA AT LOCATION 15 RBL BETWEEN STATION 294.5 AND 312. / TRANSFERRED TO LOG PAGE 0927736

Part: MODULE — FAULTY (COCKPIT) · airframe 69,771 hrs · 41,100 cycles

ON APPROACHED WITH GEAR HANDLE DOWN RECEIVED 3-RED & 3 -GREEN GEAR INDICATIONS. RECYCLED GEAR HANDLE GEAR EXTENDED NORMALLY WITH 3-GREEN INDICATIONS. R&R LANDING GEAR CONTROL LEVER MODULE PER AMM.

Part: LENS — UNSECURE (CABIN) · airframe 69,596 hrs · 40,990 cycles

R2 DOOR ABOVE EMERGENCY EXIT LIGHT LENS UNSECURE. R&R LIGHT ASSEMBLY IAW AMM.

Part: PANEL — CRACKED (RIGHT WING) · airframe 69,596 hrs · 40,990 cycles

RIGHT WING LOWER LEADING EDGE PANEL 621NB AFT INBOARD CORNER SEPARATING/CRACKED. / REPAIRED R/H WING LOWER L/E PANEL 621NB AFT IB CORNER IAW B737-700 SRM 57-41-01-2R-1 REPAIR 1 REV 66.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

AFT CARGO FLOOR SUPPORT RAIL CORRODED AT BS 767+6, LBL 8. R&R RAIL IAW EA.

Part: GUARD — DAMAGED (CABIN) · airframe 69,596 hrs · 40,990 cycles

COCKPIT P5 PANEL EMERGENCY EXIT LIGHT SWITCH GUARD DAMAGED. R&R SWITCH GUARD IAW MM.

Part: STANCHION — CORRODED (AFT CARGO BAY) · airframe 69,596 hrs · 40,990 cycles

AFT PIT SIDE WALL EXTRUSION REMOVED FOR WASTE TANK REMOVAL HAS CORROSION AROUND BOLT HOLE / REMOVED DAMAGE ON AFT PIT SIDE WALL EXTRUSION FOR WASTE TANK SIDEWALL EVALUATED DAMAGE REMOVED AND FOUND TO BE 100% MATERIAL LOSS. OUT OF LIMITS. LOCATED AND DRILLED NEW STANCHION AND PLACED ON PARTS RACK. INSTALLATION ACCOMPLISHED ON WORKORDER 38662/1600/0019. J753-260-00-01Y IAW SRM 51-40-02-0G-0; 51-10-02-0G-0; AIPC 53-42-51-03; AND DWG 149A8113 SH AND 15 REV A

Part: SUPPORT — CRACKED (LWR FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

L/H MLG WW LOWER WING TO BODY PANEL SUPPORT BS 663; LBL 25 TO 70 IS CRACKED AT INBOARD END / L/H MLG W/W LOWER WING TO BODY PANEL SUPPORT BS 663 - LBL 25-70; REPAIRED AT INBD. REPAIRED; PANEL SUPPORT IAW EA 180724IR AND SWA 1-753-33826 IR.

Part: VAPOR BARRIER — CRACKED (RT WHEEL WELL) · airframe 69,596 hrs · 40,990 cycles

THIRD TIER- FOUND STIFFNER AT STA 663 R/H VAPOR WEB RBL31-RBL6.15 CRACKED AT I/B END / RECIEVED MATERIAL NEW STIFFENER AT STA 663 R/H VAPOR WEB RBL 31- RBL 6.15 LOCATED AND DRILLED NEW STIFFENER IAW BOEING DWG 111A1301 REV F AND SRM 51-40-05 STIFFENER INSTALLATION W/O 38663/1000/0037 X857180 WN6289

Part: SUPPORT — CRACKED (LT MLG WW) · airframe 69,596 hrs · 40,990 cycles

VAPOR WEB SUPPORT CRACKED AT BS 663, LBL 24. R&R WEB SUPPORT IAW SRM AND DWG.

Part: ACCESS PANEL — DELAMINATED (RT WING) · airframe 69,596 hrs · 40,990 cycles

#2 ENG PYLON ACCESS PANEL 441DL HAS EDGE DELAMINATION AT TOP EDGE 4 INCHES FROM AFT END / REMOVED; REPAIRED; PAINTED; AND REINSTALLED #2 ENG PYLON ACCESS PANEL 441DL IAW SRM 51-70-04-2R-2; AMM 51-21-99-300-802; SRM 51-40-02-0G-0 SEC 9B. (A35994) (A44704)

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

FLIGHT DECK FLOOR WEB ATTACH ANGLE CRACKED AT BS 178.5, LBL 19. R&R ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

AFT CABIN FLOORBEAM CORRODED AT BS 986.5, AROUND DOME NUT FOR AFT GIRT BAR FITTING AFT HOLE. R&R DOME NUT IAW SRM AND EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

AFT CARGO STRINGER SPLICE CORRODED BETWEEN BS 887, STR 20R. R&R STRINGER SPLICE IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

STRINGER ATTACH ANGLE CRACKED AT BS 294, STR 13L. R&R ANGLE IAW SRM AND DWG.

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 69,596 hrs · 40,990 cycles

PRIORITY 3: FWD CARGO FWD CORNER SCUFF PLATE CRACKED / REPAIRED FWD CARGO FWD SCUFF PLATE IAW: SWA EA 1-A53-2076 REV 11.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

STRINGER CLIP CRACKED AT BS 277, STR 10R. R&R CLIP IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FLIGHT DECK) · airframe 69,596 hrs · 40,990 cycles

FO'S FWD OUTBD SEAT TRACK CORRODED ON BOTTOM OF TRACK / REMOVED + REPLACED FO'S FWD OUTBD SEAT TRACK IAW AMM 25-11-400-801 ATAG# WN7440

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

NOSE LANDING GEAR WHEEL WELL EVIDENCE OF CORRODED AROUND MULTIPLE NUTPLATE HOLES FOR RT CEILING PANEL 114AC. REPAIRED SKIN IAW EA.

Part: SEAT TRACK — CORRODED (FLIGHT DECK) · airframe 69,596 hrs · 40,990 cycles

FO'S AFT INBD SEAT TRACK CORRODED ON BOTTOM OF TRACK / REMOVED + REPLACED FO'S INBD AFT SEAT TRACK IAW AMM 25-11-11-400-801 ATAG# WN1881

Part: SEAT TRACK — CORRODED (FLIGHT DECK) · airframe 69,596 hrs · 40,990 cycles

FO'S FWD INBD SEAT TRACK CORRODED AT FASTENER HOLES AND BOTTOM OF TRACK / REMOVED + REPLACED F'OS FWD INBD SEAT TRACK IAW AMM 25-11-11-400-801 ATAG# WN3810

Part: SEAT TRACK — CORRODED (FLIGHT DECK) · airframe 69,596 hrs · 40,990 cycles

FO'S AFT OUTBD SEAT TRACK CORRODED AT FASTENER HOLES AND GOUGED AT CORNER / REMOVED AND REPLACED FO'S OUTBD SEAT TRACK IAW AMM 25-11-11-400-801 ATAG# WN6879

Part: SEAT TRACK — CORRODED (FLIGHT DECK) · airframe 69,596 hrs · 40,990 cycles

CAPTAINS FWD OUTBD SEAT TRACK CORRODED AT FASTENER HOLES AND BOTTOM OF TRACK / REMOVED + REPLACED CAPT FWD OUTB SEAT TRACK IAW AMM 25-11-11-400-801 ATAG# 6667

Part: WEB — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

E&E COMPARTMENT WEB CORRODED AT BS 302, STR 23L. R&R WEB IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FLIGHT DECK) · airframe 69,596 hrs · 40,990 cycles

CAPTAINS FWD INBD SEAT TRACK CORRODED AT FASTENER HOLED / REMOVED & REPLACED CAPT FWIL INBD SEAT TRACK IAW AMM 25-11-11-400-801 ATAG # 6914

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

E&E COMPARTMENT LOWER FUSELAGE STRINGER END FITTING CORRODED AT BS 358, LBL 8. R&R STRINGER IAW SRM & DWG.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

RT HORSESHOE DOUBLER FOR A/C EXHAUST CRACKED AT BS 663. R&R DOUBLER IAW DWG AND SRM.

Part: VAPOR BARRIER — CRACKED (LT LT MLG WW) · airframe 69,596 hrs · 40,990 cycles

LT WHEEL WELL VAPOR BARRIER CRACKED AT BS 663, LBL 28. REPAIRED BARRIER IAW SRM.

Part: NONE — ELONGATED (VERTICAL STAB) · airframe 69,596 hrs · 40,990 cycles

PRIORITY 3 : VERTICAL STAB LEADING EDGE UPPER ATTACH FASTENERS 5 EA HAVE ELONGATED HOLES . / REPAIRED VERTICAL STAB LEADING EDGE UPPER ATTACH FASTENER HOLES IAW EA 190012 IR AND EA 1-755-4299 REV IR.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

FLIGHT COMPARTMENT FLOOR STRUCTURE CUTOUT CORRODED BETWEEN BS 270 TO BS 260, BETWEEN RBL 10.5 TO LBL 10.5. REPAIRED CUTOUT IAW EA.

Part: BRACKET — BROKEN (MAIN CABIN) · airframe 69,596 hrs · 40,990 cycles

PRIORITY 1; CABIN; STA 867 BETWEEN STR 2R AND 3R BRACKET BROKEN / REMOVED AND REPLACED BROKEN BRACKET AT CABIN STA 867 BETWEEN STR 2 AND STR 3R; P/N. 287A4015Y9 IAW B737 SRM 51-40-02-0G-0 AND BAC DWG: 146A7901; REV A. ATAG: ML0400.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

FLOOR SUPPORT RAIL CORRODED AT BS 767+6, LBL 3. R&R RAIL IAW SRM AND EA.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 69,596 hrs · 40,990 cycles

PRIORITY 2: AFT CARGO STA 887; FLOOR PANEL PPLICE STRAP HAS CORROSION ON UPPER AND LOWER SURFACE. / REMOVED AND REPLACED AFT CARGO STA 887 FLOOR PANEL SPLICE IAW SRM 51-40-02-0G-0 AND IPC 53-42-11-30

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

SIDEWALL BULKHEAD SUPPORT CORRODED AT BS 947, BETWEEN RBL 18 TO RBL 23. R&R SUPPORT IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

FLOOR SUPPORT RAIL CORRODED AT BS 767+6, RBL 3. R&R RAIL IAW SRM AND EA.

Part: FAIRING — CRACKED (LWR FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

PRIORITY 3 : WING TO BODY FAIRING SPLICE PLATE CRACKED AT MOST INBD LEADING EDGE BS 500 D JUST OTBD OF FUSELAGE. / REMOVED AND REPLACED WING-TO-BODY SPLICE PLATE L/H INBD LEADING EDGE BS 500D IAW: SRM 51-40-02-0G-0. REMOVED AND REINSTALLED L/H UPPER FWD WING -TO-BODY FAIRING PNL 195AL IAW: SRM 51-40-02-0G-0.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

STRINGER SPLICE CORRODED AT BS 887, STR 22R. R&R SPLICE IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

FLOOR SUPPORT RAIL CORRODED AT BS 727C+7, RBL 3. REPAIRED FLOOR RAIL IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

AFT CARGO RT Z-ANGLE CORRODED BETWEEN BS 727 TO BS 767 ON UPPER AND LOWER SURFACE. R&R Z ANGLE IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

FLOOR SUPPORT RAIL CORRODED AT BS 767+6, RBL 8. R&R RAIL IAW SRM & EA.

Part: SUPPORT ANGLE — CORRODED (AFT CARGO BAY) · airframe 69,596 hrs · 40,990 cycles

PRIORITY 2: AFT CARGO STA 847 TO 867; LBL 16; LAVE ACCESS BULKHEAD SUPPORT ANGLE HAS CORROSION ON UPPER SURFACE / REMOVED CORROSION FROM AFT CARGO STA 847 TO STA 867; LBL 16 LOWER LAVE ACCESS BULKHEAD SUPPORT ANGLE IAW 737-700 SRM 51-10-02-0G-0 FOUND NO PUBLISHED LIMITS ON SUPPORT ANGLE REMOVED AND REPLACED LOWER LAVE ACCESS BULKHEAD SUPPORT AND ANGLE IAW BOEING DWG 149A8102 REV A 737-700 SRM 51-40-02-0G-0; 737-700 SRM 51-40-05-0G-0 APPLIED C.I.C TO NEW SUPPORT BRACKET ANGLE IAW 737 AMM 51-21-91-620-802

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

STRINGER SPLICE CORRODED BETWEEN BS 887-3 TO BS 887+1, STR 19R. R&R STRINGER SPLICE IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

BAFFLE CLIP CRACKED AT BS 400, RBL 25. R&R CLIP IAW SRM AND DWG.

Part: TRACK — CORRODED (AFT CARGO BAY) · airframe 69,596 hrs · 40,990 cycles

PRIORITY 2: AFT CARGO STA 727D+6; RBL 8.1; FLOOR SUPPORT RAIL HAS CORROSION ON UPPER AND LOWER SURFACE / REMOVED CORROSION ON FLOOR SUPORT RAIL IN AFT CARGO STA 727D+6' RBL 8.1 AND FOUND MATERIAL LOSS OUT OF LIMITS .ORIG T= .063' MAT LOSS= .008' REV.T= .055' REPAIRED DAMAGE IAW SWA EA #1-A53-4982 ATAG WN9436

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

INTERCOSTAL CORRODED BETWEEN BS 927 TO BS 927+17, RBL 13. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

AFT CARGO FLOOR SUPPORT RAIL CORRODED AT BS 727D+6, LBL 3, ON UPPER AND LOWER SURFACE. R&R SUPPORT IAW EA AND SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

STRINGER CORRODED AT BS 887, STR 19R. R&R STRINGER IAW DWG AND EA.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 69,596 hrs · 40,990 cycles

PRIORITY 2: AFT CARGO LH Z-ANGLE HAS CORROSION FROM STA 727B+10 TO 787+6 / BLENDED OUT CORROSION ON AFT CARGO L/H Z ANGLE FROM STA 727B+10' TO 736+6' IAW B737 SRM 51-10-02-0G-0. ORIGINAL THICKNESS 0.040' MATERIAL LOSS .009; MAT REMAINING 0.031' THE AREA FOUND TO BE OUT OF LIMIT IAW B737 SRM 53-00-53-1A-2; THE NEW REPAIR Z ANGLE WAS INSTALLED ON X857611.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

FLOOR SUPPORT RAIL CORRODED AT BS 727D+6, RBL 3. R&R RAIL IAW SRM AND EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

STRINGER SPLICE CORRODED AT BS 887, STR 27R. R&R STRINGER SPLICE IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

AFT CARGO LT Z-ANGLE CORRODED AROUND NUTPLATE HOLES BETWEEN BS 727 TO BS 727B+6. R&R Z ANGLE IAW SRM.

Part: ATTACH ANGLE — CRACKED (AFT CARGO BAY) · airframe 69,596 hrs · 40,990 cycles

PRIORITY 2: AFT CARGO STA 867 LBL 11; ATTACH ANGLE CRACKED FOR LAV BULKHEAD SUPPORT ANGLES. / INSTALLED NEW ATTACH ANGLE P/N 149A8109-114; ATAG A56918 AT AFT CARGO STA 867 LBL 11 IAW SRM 51-40-02-0G-0 AND BOEING DWG 149A8102 REV A

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

AUX SILL WEB CORRODED AT BS 827+18, STR 27R. R&R WEB IAW SRM AND DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

ATTACH CLIP CRACKED AT BS 420, RBL 25. R&R CLIP IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,596 hrs · 40,990 cycles

RT HORIZONTAL STABILIZER LEADING EDGE CRACKED RIB LEADING EDGE STA 151.75. REPAIRED RIB IAW SRM & DWG.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 69,596 hrs · 40,990 cycles

AFT GIRT BAR FITTING FLOOR MOUNT AREA AT L2 DOOR AFT FLOORBOARD PASS THROUGH AND NUT CORRODED. R&R INSERTS IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,596 hrs · 40,990 cycles

RT HORIZONTAL STABILIZER STAB STA 120.3 RIB CRACKED AT 3RD VERTICAL STIFFENER FROM FORWARD END. R&R RIB IAW SRM AND DWG.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 69,596 hrs · 40,990 cycles

FLOORBOARD AT L2 DOOR JUST INBOARD OF AFT GIRT BAR MOUNT CORRODED FLOORBOARD SCREW AND RECEPTACLE. R&R INSERTS IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

INTERCOSTAL WEB CORRODED AT BS 847, STR 27R. REPAIRED WEB IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

AFT CARGO INTERCOSTAL WEB CORRODED BETWEEN BS 787 TO BS 787+6, STR 27R. R&R WEB IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

STRINGER CLIP CORRODED AT BS 807, STR 26R. R&R CLIP IAW SRM AND DWG.

Part: WEB — CORRODED (AFT CARGO) · airframe 69,596 hrs · 40,990 cycles

P2: AFT CARGO INTERCOSTAL WEB AT STA 767+3 RBL 20 HAS CORROSION AROUND NUT PLATE HOLE / REMOVED CORROSION FROM AFT CARGO INTERCOSTAL WEB AT STA 767+ 3 RBL 20 IAW SRM 51-10-02. ORIG. 'T' IS .050' WITH A LOSS OF .015' REMAINING 'T' OF .035' IS OUT OF LIMITS IAW SRM 53-60-0155-1A-1. REMOVED INTERCOSTAL WEB IAW SRM 51-40-02. INSTALLED NEW WEB; 146A8123-19; IAW SRM 51-40-02 AND DWG# 146A8123 REV. C.

Part: STRAP — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

AFT CARGO LOWER LONGITUDINAL STRAP BELOW DOOR SILL INTERCOSTAL WEB CORRODED BETWEEN BS 787 TO BS 787+8, RBL 20. R&R STRAP IAW SRM & DWG.

Part: PLATE — CORRODED (AFT CARGO COMPT) · airframe 69,596 hrs · 40,990 cycles

P3: AFT CARGO; STA 787+5; STR 22L; CARGO NET TIE DOWN PLATE HAS CORROSION / REMOVED & REPLACED AFT CARGO TIE DOWN PLATE STA 787+5 STR 22L IAW SRM 51-40-02-0G-0 7 DWG 146A9403 REV:- SRM GIVE NO ALLOWABLE LIMIT.

Part: STRAP — CORRODED (AFT CARGO) · airframe 69,596 hrs · 40,990 cycles

P2: AFT CARGO; LONGITUDINAL STRAP ON UPPER SIDE OF DOOR SILL INTERCOSTAL WEB HAS CORROSION AT RBL 20; STA 767+18 TO 787+6; / REMOVED CORROSION I/A/W B737 SRM 51-10-02-0G-0; EVALUATED DAMAGE; ORIGINAL MATERIAL .100'; LOSS .030'; REMAINING .070 FOUND TO BE OUT OF LIMITS I/A/W B737 SRM 53-60-15-1A-1. REMOVED AND INSTALLED A NEW AFT CARGO LONGITUDINAL STRAP ON UPPER SIDE OF DOOR SILL INTERCOSTAL I/A/W BOEING DRAWING 146A8120 REV E

Part: SHIELD — CORRODED (AFT CARGO COMPT) · airframe 69,596 hrs · 40,990 cycles

P2: AFT CARGO; RH SPLASH SHIELD FROM STA 767 TO 787 RBL 22 HAS CORROSION ON UPPER AND LOWER SURFACE AT NUT PLATE HOLES. / REMOVED CORROSION AT AFT CARGO R/H SPLASH SHIELD STA 767 TO 787 RBL 22 I/A/W B737 SRM 51-40-02-0G-0 . EVALUATED DAMAGE. ORIGINAL .050'; LOSS .012' REMAINING .038' FOUND TO BE OUT OF LIMITS I/A/W B737 SRM 53-60-15-1A-1. REMOVED AND INSTALLED A NEW SPLASH SHIELD I/A/W SRM 51-40-02-0G-0 AND BOEING DRAWING 141A0081 REV B

Part: PLATE — CORRODED (AFT CARGO COMPT) · airframe 69,596 hrs · 40,990 cycles

P3: AFT CARGO; STA 787+5; STR 24L; CARGO NET TIE DOWN PLATE HAS CORROSION / REMOVED AFT CARGO TIE DOWN PLATE STA 787+5 STR 24L AND REPLACED; REMOVED CORROSION ON SRM PROVIDES NO ALLOWABLE LIMITS IAW SRM 51-40-02-0G-0 & DWG 146A9405 REV:-

Part: ANGLE — CORRODED (FWD CARGO RH) · airframe 69,596 hrs · 40,990 cycles

P2 FWD CARGO COMPARTMENT RH STA 400 TO 420 HAS SPOTS OF CORROSION ON Z-ANGLE / REMOVED CORROSION ON THE 'Z' ANGLE FOUND OUT OF LIMITS AND INSTALLED NEW Z ANGLE P/N BAC 1496-444 7075-T62 AND RESTORED FINISH IAW B737-700 SRM 51-40-05-0G-0; SRM 51-40-05-0G; AMM 51-21-41-370-803 AND DWG# 143A7500 REV:A. STA 400 TO 420 R/H FWD CARGO COMPARTMENT .RBL 25'

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

STRINGER CLIP GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW DWG AND SRM.

Part: CAP — CORRODED (AFT CARGO) · airframe 69,596 hrs · 40,990 cycles

P3: AFT CARGO FLOOR PANEL 140CF CAP STRIPS HAVE CORROSION ON UPPER AND LOWER SURFACE / REMOVED AND REPLACED 2 EA CAP STRIPS ON AFT CARGO FLOOR PANEL 140CF; P/N: 453A2611-6 AND P/N: 453A2611-7 IAW B737 AMM: 25-52-10-400-801 AND IPC: 25-52-10-02. ATAG: ML0461 AND ML0467

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 69,596 hrs · 40,990 cycles

P3: AFT CARGO FLOOR PANEL 140CF; UPPER AND LOWER SURFACE HAS CORROSION; MARKED IN RED. / REPLACED AFT CARGO FLOOR PANEL 140CF WITH NEW AFT CARGO FLOOR PANEL DUE TO CORROSION BEING OVER 3. IN LENGTH AND OUT OF LIMITS SRM 53-00-53-1A-1 P/N 453A2610-2; ATAG WN9877 TO BE INSTALLED ON CARD NO JPANEL-141-CLOSE

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 69,596 hrs · 40,990 cycles

P3: AFT CARGO; CAP STRIP SPLICE STRAPS ARE CORRODED / AFT CARGO CAP STRIP SPLICE STRAPS 3 EACH CORRODED WITH NO LIMITS. NEW CAP STRIP SPLICE STRAPS VERIFIED AS P/N 453A2611-13 IAW AIPC 25-52-10-02. NEW PARTS ON AFT CARGO PARTS RACK.

Part: STRIP — CORRODED (FWD CARGO LH) · airframe 69,596 hrs · 40,990 cycles

P2: FORWARD CARGO COMPARTMENT L/H SIDE SIDEWALL TO FLOOR CAPSTRIPS ARE CORRODED / VERIFIED NO PUBLISHED LIMITS ON ALLOWABLE CORROSION ON FWD CARGO LH SIDEWALL CAP STRIPS VERIFIED RECORDED NON CAPSTRIPS P/N 453A1611-6; 453A1611-0; 453A1611-11 ATAG WN8710 AND WN5481 IAW B737-700 AIPC 25-52-10-01 PG 4 AND 33

Part: STRIP — CORRODED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

SUPPLEMENTAL INFORMATION: FORWARD CARGO COMPARTMENT R/H AFT CAPSTRIP IS CORRODED / ORDERED FWD CARGO PIT R/H SIDE AFT CAP STRIP NEW P/N: 453A1G11-12 AS PER B-737-700 IPC 25-52-10-01 REF ONLY CAPSTRIP INSTALLATION WILL 6E ACCOMPLISHED ON PANEL BOOK W/O: 388785 (SEE ATTACH COPY) ISSUE TAG: WN6134

Part: FLOOR PANEL — MISSING (CABIN) · airframe 69,596 hrs · 40,990 cycles

P3: PASS CABIN FLOOR PANEL 231XF; UPPER FACE SHEET HAS MISSING FIBERS AT O/B EDGE. / REPAIRED P3 PASS CABIN FLOOR PANEL 231XF OF MISSING FIBERS ON UPPER FACE SHEET IAW B737 SRM 53-00-50-2R-0 REV 66 AND B737 SRM 53-00-50-2R-1 REV 66.

Part: PLATE — CORRODED (AFT CARGO COMPT) · airframe 69,596 hrs · 40,990 cycles

P3: AFT CARGO FWD AND AFT NET TIE DOWN PLATES ARE CORRODED ON LOWER SURFACE / REPLACED AFT CARGO FWD AND AFT NET TIP DOWN PLATES WITH NEW AFT CARGO FWD AND AFT NET TIE DOWN PLATES; P/N 453A2611-1 ATAG A63133; P/N 453A2611-2 ATAG A47062 IAW IPC 25-52-10-02

Part: PLATE — CORRODED (FWD CARGO COMPT) · airframe 69,596 hrs · 40,990 cycles

P2 FORWARD CARGO COMPARTMENT AFT FLOOR TIE DOWN PLATE IS CORRODED / VERIFIED RECEIVED NEW FWD CARGO AFT FLOOR TIE DOWN P/N 453A1611-26 A TAG A63157. IAW B737-700 AIPC 25-52-10-01 PG 3 VERIFIED NO PUBLISHED LIMITS FOR ALLOWABLE CORROSION ON TIE DOWN.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 69,596 hrs · 40,990 cycles

LT HORIZONTAL PRESSURE DECK WEB CRACKED BETWEEN BS 663 TO BS 675, LBL 34. REPAIRED WEB IAW EA.

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 69,596 hrs · 40,990 cycles

P3: AFT CARGO; SIDEWALL CAP STRIP JUST AFT OF CARGO DOOR HAS CORROSION / REPLACED AFT CARGO; SIDEWALL CAP STRIP JUST AFT OF CARGO DOOR WITH NEW AFT CARGO SIDEWALL CAP STRIP; P/N 453A2411-3 ATAG A69533 IAW IPC 25-52-06-03

Part: WEB — CORRODED (AFT CARGO THRESH) · airframe 69,596 hrs · 40,990 cycles

P1: AFT CARGO DOOR CUTOUT LOWER THRESHOLD WEB HAS CORROSION / BLENDED OUT CORROSION I/A/W B737 SRM 51-10-02-0G-0; ORIGINAL MATERIAL .045'; LOSS .006'; REMAINING .039' FOUND TO BE OUT OF LIMITS I/A/W B737 SRM 53-60-15-01-1. REMOVED AND INSTALLED A NEW AFT CARGO DOOR CUTOUT LOWER THRESHOLD WEB I/A/W B737 SRM 51-40-02-0G-0 AND BOEING DRAWING 146A8340 REV A ATAG: WN9627

Part: CAP — CORRODED (AFT CARGO) · airframe 69,596 hrs · 40,990 cycles

P3: AFT CARGO FLOOR PANEL 140DF CAP STRIP HAS CORROSION ON UPPER AND LOWER SURFACE / AFT CARGO FLOOR PANEL 140DF CAP STRIP REPLACED WITH NEW AFT CARGO FLOOR PANEL CAP STRIP P/N 453A2611-5 ATAG ML0387 IAW IPC 25-52-10-02; TO BE INSTALLEF ON JPANEL-141- CLOSE 38662 1000 0022

Part: CAP — CORRODED (AFT CARGO) · airframe 69,596 hrs · 40,990 cycles

P3: AFT CARGO SIDEWALL TO FLOOR PANEL CAP STRIPS HAVE CORROSION / REPLACED 6 EA AFT CARGO SIDEWALL TO FLOOR PANEL CAP STROPS; P/N 453A2611-4 ATAG WN1903; P/N 453A2611-10 ATAG A62807; P/N 453A2611-3 ATAG WN5005; IAW IPC 25-52-10-02; TO BE INSTALLED ON JPANEL-141-CLOSE CARD; W/O 38662 1600 0022

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 69,596 hrs · 40,990 cycles

AFT CARGO DOOR CUTOUT AFT SCUFF PLATE CRACKED IN RADIUS. REPAIRED SCUFF PLATE IAW EA.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 69,596 hrs · 40,990 cycles

P2 FORWARD CARGO COMPARTMENT SCUFF PLATE AFT CORNER IS CRACKED / REPAIRED FWD CARGO AFT SCUFF PLATE IAW SWA EA 1-A53-2076 REV. 11

Part: STRIP — CORRODED (FWD CARGO COMPT) · airframe 69,596 hrs · 40,990 cycles

P2: FORWARD CARGO SIDEWALL TO FLOOR CAPSTRIP AT PANEL 122AW IS CORRODED / VERIFIED RECEIVED NEW FWD CARGO SIDEWALL TO FLOOR CAP STRIP AT PANEL 122AW P/N 453A1611-5 A TAG #A6280 IAW B737-700 AIPC 25-52-40-1 PG 3 AND 33. VERIFIED NO PUBLISHED LIMITS FOR ALLOWABLE CORROSION ON CAP STRIP.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,596 hrs · 40,990 cycles

LT WING NR 2 SLAT LOWER SURFACE OF THE SLAT NOSE SKIN CRACKED ADJACENT TO ACTUATOR ATTACH FITTING. REPAIRED NR 2 SLAT SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,596 hrs · 40,990 cycles

LT WING NR 3 SLAT LOWER SURFACE OF THE SLAT NOSE SKIN CRACKED ADJACENT TO ACTUATOR ATTACH FITTING. REPAIRED SKIN IAW SRM.

Part: SLAT — CRACKED (RT WING) · airframe 69,596 hrs · 40,990 cycles

RT WING LEADING EDGE NR 8 SLAT CRACKED FORMING FROM FASTENER HOLE. REPAIRED NR 8 SLAT IAW SRM.

Part: LENS — CRACKED (CABIN) · airframe 69,596 hrs · 40,990 cycles

RT STOWBINS EMERGENCY LIGHT LENSES CRACKED BETWEEN ROW 6 TO ROW 22. R&R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 69,596 hrs · 40,990 cycles

LT STOWBINS EMERGENCY LIGHT LENSES CRACKED BETWEEN ROW 1 TO ROW 17. R&R LENS IAW AMM.

Part: STIFFENER — CRACKED (CABIN) · airframe 69,056 hrs · 40,647 cycles

FLOOR PANEL STIFFENER AT STA. 540 BETWEEN CENTER FLOOR BEAM LBL 0.07 AND RBL 24.82 HAS A 3' CRACK IN THE FORWARD LEFT RADIUS. / R&R STIFFENER PER SRM 51-40-02

Part: LATCH — BROKEN (FLASHLIGHT DOOR) · airframe 67,266 hrs · 39,511 cycles

AFT GALLEY FLASHLIGHT DOOR LATCH BROKEN. R & R THE LATCH IAW AMM.

Part: COVER — OUT OF POSITION (R2 DOOR SLIDE) · airframe 66,895 hrs · 39,284 cycles

R2 DOOR SLIDE COVER OUT OF POSITION. REPOSITIONED THE COVER IAW MT.

Part: CONTROL LEVER — DIRTY (COCKPIT) · airframe 66,806 hrs · 39,229 cycles

DECLARED EMERGENCY, WHEN LANDING GEAR SELECTED DOWN, RED GEAR LIGHTS REMAINED ILLUMINATED. ON SUBSEQUENT APPROACH, PROPER INDICATIONS OF THREE GREEN DOWN AND LOCKED LIGHTS ILLUMINATED. CLEANED LANDING GEAR LEVER OF DUST AND GUNK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 66,776 hrs · 39,214 cycles

FORWARD LT EMERGENCY LIGHT BATTERY PACK FAILED DEEP CYCLE CHECK. R&R BATTERY PACK PER AMM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 66,728 hrs · 39,184 cycles

LT WHEEL WELL LOWER VAPOR BARRIER CRACKED AT LBL 32. REPAIRED BARRIER IAW SRM.

Part: PANEL — DELAMINATED (LH PYLON) · airframe 66,728 hrs · 39,184 cycles

LH ENGINE PYLON AFT FAIRING PANEL 431ER IS CHARRED / DELAMINATED ALONG LWR FWD INSIDE CORNER EDGE. / REPAIRED PANEL 431ER IAW B737 SRM 51-70-04-2R-6.

Part: FITTING — OUT OF ADJUST (R1 DOOR) · airframe 66,001 hrs · 38,714 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET OUT OF ADJUST. ADJUSTED CLIP PER SIP.

Part: LIGHT — LOOSE (CABIN) · airframe 65,867 hrs · 38,626 cycles

MID CABIN CEILING EMERGENCY EXIT LIGHT LOOSE. R&R LIGHT ASSEMBLY IAW AMM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 65,219 hrs · 38,217 cycles

R1 DOOR EMERGENCY SLIDE PRESSURE LOW. R & R THE SLIDE ASSEMBLY IAW MT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,732 hrs · 37,309 cycles

EMERGENCY EXIT LIGHT INOPERATIVE ABOVE ROW 4 ABC. REPLACED THE LAMPS IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,732 hrs · 37,309 cycles

EMERGENCY EXIT AISLE LIGHT INOPERATIVE AT ROW 4 ABC. REPLACED THE LAMPS IAW MM.

Part: ANGLE — CRACKED (RT WING) · airframe 62,996 hrs · 36,879 cycles

RT WING ANGLE CRACKED ON REAR SPAR STRUCTURE, WBL 71.24. R&R ANGLE IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

TIE CLIP CRACKED BS 986.5, STR 18L. R&R TIE CLIP IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

WEB CORRODED BETWEEN BS 986.5 TO BS 1016. R&R WEB IAW SRM AND DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

AFT CARGO COMPARTMENT CHANNEL CRACKED AT BS 767, STR 26R. R&R CHANNEL IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

WEB INTERCOSTAL CORRODED BETWEEN BS 767 TO BS 787, STR 25R. R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

AFT CARGO COMPARTMENT WEB INTERCOSTAL CORRODED BETWEEN BS 767 TO BS 787, STR 25R. R&R INTERCOSTAL IAW SRM AND DWG.

Part: LENS — BROKEN (CABIN) · airframe 62,996 hrs · 36,879 cycles

FORWARD GALLEY AREA EMERGENCY EXIT LIGHT LENS BROKEN. R&R LENS IAW AMM.

Part: PLATE — CRACKED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

FORWARD CARGO COMPARTMENT CHANNEL SIDE PLATE CRACKED BETWEEN BS 440+9.5 TO BS 500D, LBL 21.8. R&R SIDE PLATE IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

AFT CARGO COMPARTMENT ZEE CHANNEL CORRODED BETWEEN BS 727C TO BS 787, STR 25L. REPAIRED ZEE CHANNEL IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

FORWARD CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 500 TO BS 500A, BETWEEN STR 28L TO STR 28R. R&R CHANNEL IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

AFT GALLEY AREA FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, LBL 43. REPAIRED CHORD IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

FORWARD GALLEY AREA FLOOR STRUCTURE WEB CRACKED BETWEEN BS 344 TO BS 328, LBL 47. R&R WEB IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500D, STR 19R. R&R GUSSET IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

AFT GALLEY AREA FLOOR BEAM UPPER CHORD CORRODED AT BS 986.5, BETWEEN RBL 17 TO RBL 44. REPAIRED CHORD IAW EA.

Part: PLATE — CRACKED (LT HORIZ STAB) · airframe 62,996 hrs · 36,879 cycles

LT HORIZONTAL STABILIZER UPPER SEAL PLATE CRACKED AT LEVEL OF STAB BL 0. R&R PLATE IAW AMM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

R2 DOOR Z ANGLE CHORD CORRODED. R&R CHORD IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500D, STR 22L. R&R GUSSET IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

R1 DOOR Z ANGLE CHORD CRACKED. R&R CHORD IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

L1 DOOR Z ANGLE CHORD CRACKED AT BS 303.9, STR 17L. R&R CHORD IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500, STR 21L. R&R GUSSET IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

WEB INTERCOSTAL CRACKED AT BS 500D, STR 26R. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

FORWARD CARGO COMPARTMENT ANGLE CLIP CRACKED AT BS 500C, STR 26R. R&R CLIP IAW SRM AND DWG.

Part: FAIRING — CRACKED (TE FLAP) · airframe 62,996 hrs · 36,879 cycles

LT WING FLAP TRACK FAIRING 543BB INTERNAL CAVITY CRACKED. REPAIRED FAIRING IAW SRM AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,996 hrs · 36,879 cycles

AFT CARGO COMPARTMENT LOWER RT FRAME WEB CRACKED AT BS 727, WL 200. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 61,365 hrs · 35,906 cycles

AFT CARGO DOOR SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,254 hrs · 35,842 cycles

LEFT FWD LOWER OVERWING EXIT DOOR EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 60,834 hrs · 35,579 cycles

LEFT WING OTBD AFT FLAP INBD UPPER & LOWER DELAMINATED. R & R AFT FLAP IAW AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 60,834 hrs · 35,579 cycles

RIGHT WING OTBD AFT FLAP DELAMINATED, INBD END OF UPPER SURFACE. R & R AFT FLAP IAW AMM.

Part: ACTUATOR — LOOSE (LT SPOILER) · airframe 60,834 hrs · 35,579 cycles

LEFT WING NR 4 SPOILER ACTUATOR HOUSING PIVOT LOOSE & LEAKING HYD FLUID. R & R NR 4 SPOILER ACTUATOR IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 60,834 hrs · 35,579 cycles

M01674 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: ISOLATOR — DELAMINATED (LT WING) · airframe 60,834 hrs · 35,579 cycles

LEFT WING NR 3 FLAP TRANSMISSION FWD FAIRING ATTACH BRACKET ISOLATOR DELAMINATED. R & R ISOLATOR IAW SRM.

Part: SIGN — MISSING (CABIN) · airframe 59,746 hrs · 34,965 cycles

LEFT EMER EXIT FLOOR SIGN MISSING. INSTALLED SIGN IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,820 hrs · 34,409 cycles

EMERGENCY LIGHTS BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01672. R & R BATTERY PACK IAW AMM & DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,820 hrs · 34,409 cycles

EMERGENCY LIGHTS BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01673. R & R BATTERY PACK IAW AMM & DWG.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 58,820 hrs · 34,409 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,820 hrs · 34,409 cycles

EMERGENCY LIGHTS BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01668. R & R BATTERY PACK IAW AMM & DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 58,282 hrs · 34,105 cycles

LEFT HORIZONTAL STABILIZER STATION 92.70 RIB CRACKED AT AFT STIFFENER. R & R RIB IAW SRM.

Part: HYDRAULIC LINE — FAULTY (HYDRAULIC SYS) · airframe 57,959 hrs · 33,916 cycles

DIVERSION, DECLARED EMER, SYS B HYD SYS FAILURE. SYS B QTY & PRESS WENT TO 0. R & R HYD LINE IAW MM.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 57,336 hrs · 33,544 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR HANDLE ON SLIDE CONTAINER LOOSE. SECURED GIRT BAR ASSEMBLY IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,221 hrs · 33,475 cycles

LEFT OVERWING EMER LIGHT INOPERATIVE. R & R BULB IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

FRAME CRACKED AT BS 867, BETWEEN STRINGER 8L TO 9L. REPAIRED FRAME IAW EA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

FRAME SUPPORT BRACKET CRACKED AT BS 827, BETWEEN STRINGER 8L - 9L. REPAIRED BRACKET IAW EA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

FRAME SUPPORT BRACKET CRACKED AT BS 500C, BETWEEN STRINGER 8L - 9L. REPAIRED BRACKET IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

FRAME CRACKED AT BS 907, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

FRAME SUPPORT BRACKET CRACKED AT BS 360, STRINGER 8R. REPAIRED BRACKET IAW EA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

FRAME SUPPORT BRACKET CRACKED AT BS 400, STRINGER 8R. REPAIRED BRACKET IAW EA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

FRAME SUPPORT BRACKET CRACKED AT BS 480, STRINGER 8R. REPAIRED BRACKET IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

FRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

FRAME SUPPORT BRACKET CRACKED AT BS 440, BETWEEN STRINGER 8L - 9L. REPAIRED BRACKET IAW EA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

FRAME SUPPORT BRACKET CRACKED AT BS 380, BETWEEN STRINGER 8L - 9L. REPAIRED BRACKET IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

RIGHT NR 3 FLIGHT DECK WINDOW FRAME CRACKED. REPAIRED FRAME IAW ACO.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

FRAME SUPPORT BRACKET CRACKED AT BS 717, BETWEEN STRINGER 8R - 9R. REPAIRED BRACKET IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

FRAME CRACKED AT BS 520, BETWEEN STRINGER 8L TO 9L. REPAIRED FRAME IAW EA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

FRAME SUPPORT BRACKET CRACKED AT BS 787, BETWEEN STRINGER 8R - 9R. REPAIRED BRACKET IAW EA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

FRAME SUPPORT BRACKET CRACKED AT BS 727D, BETWEEN STRINGER 8L - 9L. REPAIRED BRACKET IAW EA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

FRAME SUPPORT BRACKET CRACKED AT BS 727D, BETWEEN STRINGER 8R - 9R. REPAIRED BRACKET IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,221 hrs · 33,475 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT STATION 92.70, AT 2ND VERTICAL STIFFENER LOWER END. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,221 hrs · 33,475 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STATION 92.70, AT LOWER ENDS OF VERTICAL STIFFENERS. REPAIRED RIB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

SKIN CRACKED AT BS 540, STRINGER 22R ORIGINATING FROM FASTENER HOLE SECOND FROM THE TOP, FWD. REPAIRED SKIN IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

SPLICE STRAP CRACKED AT BS 727B, RBL 45.5. REPAIRED SPLICE STRAP IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

SPLICE STRAP CRACKED AT BS 727B, LBL 45.5. REPAIRED SPLICE STRAP IAW EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

FUSELAGE SKIN CORRODED AROUND FASTENER HOLES OF THE AFT PIT DOOR CUT OUT SCUFF PLATE. REPAIRED SKIN IAW SRM & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 45.5. R & R SEAT TRACK IAW SRM & DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,221 hrs · 33,475 cycles

LEFT WING NR 1 SLAT SKIN LOWER SURFACE AT ACTUATOR CRACKED. REPAIRED NR 1 SLAT IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

STUB BEAM FITTING CRACKED AT BS 616. REPAIRED FITTING IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,221 hrs · 33,475 cycles

RIGHT WING NR 7 SLAT LOWER SKIN SURFACE AT ACTUATOR CRACKED. REPAIRED NR 7 SLAT IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

SPLICE STRAP CRACKED AT BS 727B, LBL 24.75. REPAIRED SPLICE STRAP IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,221 hrs · 33,475 cycles

SPLICE STRAP CRACKED AT BS 727B, RBL 24.75. REPAIRED SPLICE STRAP IAW EA

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,711 hrs · 32,571 cycles

FORWARD RT OVERWING EXIT LINER LIGHT INOPERATIVE BULB. R & R BULB IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,122 hrs · 32,211 cycles

LEFT EMER EXIT LIGHTS INOPERATIVE BETWEEN ROW 9 TO ROW 10. R & R BATTERY PACK IAW AMM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 54,969 hrs · 32,114 cycles

RIGHT WW BEADED WEB CRACKED AT BS 665, RBL 36. REPAIRED IAW EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 54,752 hrs · 31,986 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 138.70 & 25 INCHES AFT OF FWD SPAR. REPAIRED SKIN IAW SRM.

Part: SIGN — DAMAGED (CABIN) · airframe 54,204 hrs · 31,684 cycles

OVERWING CEILING EMERGENCY EXIT SIGN DAMAGED. R & R SIGN IAW AMM.

Part: LIGHT — LOOSE (EXIT SIGN) · airframe 53,578 hrs · 31,320 cycles

AFT GALLEY OVERHEAD EMERGENCY EXIT SIGN LIGHT ASSEMBLY LOOSE. SECURED LIGHT IAW MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,514 hrs · 30,660 cycles

FLOOR PANEL SUPPORT CRACKED AT STATION 540 LBL 2.0. R&R FLOOR BEAM IAW AMM.

Part: FRAME — PUNCTURED (FUSELAGE) · airframe 50,377 hrs · 29,416 cycles

PUNCTURED FRAME WEB AT BS.259, BETWEEN STR 12L TO STR 13L. REPAIRED WEB IAW ER.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 50,377 hrs · 29,416 cycles

CAPT'S NR 3 WINDOW FRAME CRACKED AT FWD EDGE 2ND FASTENER UP FROM BOTTOM. REMOVED AND REPLACED NR 3 CAPT'S WINDOW FRAME PER SRM 51-40-02, DWG 141A8800, DWG 141A0720, AND SRM 51-20-01.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 50,377 hrs · 29,416 cycles

LEFT WING UPPER TRAILING EDGE PANEL SUPPORT ANGLE IS CRACKED AT ORSS 271. REMOVED AND REPLACED LEFT WING UPPER T/E PANEL SUPPORT ANGLE AT RSS 271 IAW SRM 51-40-02.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 50,377 hrs · 29,416 cycles

LEFT MLG W/W BULKHEAD VERTICAL PRESSURE WEB CRACKED AT BS 540, LBL 42.83, 2.5". REPAIRED WEB IAW SRM.

Part: WEB — PUNCTURED (E&E DOOR) · airframe 50,377 hrs · 29,416 cycles

MAIN E&E DOOR, FWD WEB HAS A 14" PUNCTURE 3" ABOVE FWD DOOR LATCH FITTING. REPAIRED MAIN E & E DOOR, FWD WEB 3" ABOVE FWD DOOR LATCH FITTING IAW EA 1-753-21320 AND ATS ER 12-03756.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 50,377 hrs · 29,416 cycles

RIGHT MLG W/W BULKHEAD VERTICAL PRESSURE WEB CRACKED AT BS 540, RBL 32.83. REPAIRED WEB IAW SRM.

Part: COVER — LOOSE (CABIN) · airframe 50,103 hrs · 29,246 cycles

EMERGENCY EXIT COVER NOT SECURE ON CAPTAINS SIDE OF AIRCRAFT. APPLIED FEMALE SIDE VELCRO PER MM.

Part: LENS — LOOSE (L1 DOOR) · airframe 49,792 hrs · 29,041 cycles

L1 DOOR LOWER EMERGENCY EXIT LENS LOOSE. REPAIRED LENS PER EA.

Part: COVER — LOOSE (CABIN) · airframe 49,416 hrs · 28,794 cycles

FORWARD RIGHT GALLEY EMERGENCY EXIT LIGHT COVER LOOSE. SECURED LIGHT ASSY PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 47,754 hrs · 27,846 cycles

LEFT WING O/B AFT FLAP TRAILING EDGE WEDGE EXTERNAL SKIN DELAMINATED ON UPPER AND LOWER SURFACE. REPAIRED SKIN IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 47,754 hrs · 27,846 cycles

LEFT WING O/B AFT FLAP DELAMINATED AT LOWER I/B SIDE. REMOVED AND REPLACED AFT FLAP IAW SRM & AMM.

Part: SPLICE — DISCONNECTED (CABIN) · airframe 47,308 hrs · 27,587 cycles

DURING SCHEDULED SPV CHECK, FOUND RT EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 15. RECONNECTED SPLICE AT LIGHT. REPAIRED LIGHT ASSY PER WDM AND MM.

Part: VALVE — DEFECTIVE (AC BAY) · airframe 47,051 hrs · 27,439 cycles

DIVERSION/DECLARED EMERGENCY. PRESSURIZATION BECAME UNCONTROLLABLE APPROX 30 MINUTES INTO FLIGHT AT FL 330. HORN SOUNDED, WITH CABIN ALTITUDE INDICATING 10K, IMMEDIATELY DESCENDED, QRH COMPLETED. REMOVED AND REPLACED LEFT 35 DEGREE VALVE, FUSELAGE DRAIN, AND LT AND RT WATER SEPARATOR BAGS PER MM.

Part: LIGHT — ACTIVATED (CABIN) · airframe 45,433 hrs · 26,488 cycles

LT EMERGENCY EXIT LIGHT DIM. RELAMPED PER MM.

Part: ACTUATOR — FAULTY (NLG) · airframe 45,305 hrs · 26,412 cycles

NOSE DID NOT COME DOWN ON GEAR DEPLOYMENT, PLACED HANDLE OFF, RAISED AND LOWERED GEAR AGAIN. REMOVED AND REPLACED NLG RETRACT AND LOCK ACTUATOR PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT FLIGHT DECK AFT O/B SEAT TRACK WORN. REMOVED AND REPLACED SEAT TRACK PER MM.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT FLIGHT DECK AFT O/B SEAT TRACK WORN. REMOVED AND REPLACED SEAT TRACK PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT FLIGHT DECK SEAT TRACK CORRODED. REPAIRED SEAT TRACK ASSY PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD GALLEY AFT WALL EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD LAV, AFT WALL O/B AREA EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: SIGN — MISSING (CABIN) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT GALLEY EMERGENCY EXIT SIGN NEAR R2 DOOR MISSING. INSTALLED SIGN PER MM.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT FLIGHT DECK SEAT TRACK CORRODED. REPAIRED SEAT TRACK ASSY PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 24 TO LBL 45. REPAIRED BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR CREASE BEAM CORRODED. REMOVED AND REPLACED BEAM PER BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 54.6. REMOVED AND REPLACED SHEAR FITTING PER SRM.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING I/B AFT FLAP LOWER SURFACE PUNCTURED. REPAIRED AFT FLAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, BBL 0. REPAIRED BEAM PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER BAC DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT Z-ANGLE CORRODED BETWEEN BS 747 TO BS 767. REPAIRED Z-ANGLE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT AFT CREASE BEAM CORRODED BETWEEN BS 951 TO BS 986. REMOVED AND REPLACED BEAM PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT AFT CREASE BEAM CORRODED BETWEEN BS 967 TO BS 986. REMOVED AND REPLACED BEAM PER SRM AND BAC DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,724 hrs · 25,476 cycles

DURING SCHEDULED12Y CHECK, FOUND FWD CARGO COMPARTMENT RT Z-ANGLE CORRODED AT ABS 492. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 42,958 hrs · 25,036 cycles

DURING SCHEDULED CV CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER ASSY PER MM.

Part: COVER — BROKEN (CABIN) · airframe 42,808 hrs · 24,950 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT EMERGENCY EXIT LIGHT SWITCH COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 42,276 hrs · 24,632 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CASE. RE-ATTACHED SLIDE PER MT.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 40,087 hrs · 23,294 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LENS — MISSING (CABIN) · airframe 39,839 hrs · 24,634 cycles

R1 DOOR LOWER EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: COVER — MISSING (CABIN) · airframe 39,845 hrs · 23,143 cycles

RT OVERWING LOWER EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 39,285 hrs · 22,794 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 11. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,230 hrs · 22,752 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 37,709 hrs · 21,836 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOLDER LOOSE. SECURED BRACKET PER MM.

Part: COVER — DELAMINATED (CABIN) · airframe 37,429 hrs · 21,673 cycles

RT EEPLS STRIP COVER DELAMINATED BETWEEN ROW 14 TO ROW 16. REMOVED AND REPLACED EEPLS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,277 hrs · 21,576 cycles

DURING SCHEDULED HC1 CHECK, FOUND AFT RT BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 37,277 hrs · 21,576 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER SKIN CRACKED AT BS 129, FWD OF AFT SPAR. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,277 hrs · 21,576 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD RT BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FITTING — CRACKED (CENTER WING) · airframe 37,257 hrs · 21,564 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING CENTER BOX SHEAR FITTING CRACKED AT BS 540, LBL 15. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 37,257 hrs · 21,564 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING CENTER BOX SHEAR FITTING CRACKED AT BS 540, RBL 15. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 37,257 hrs · 21,564 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING CENTER BOX SHEAR FITTING CRACKED AT BS 540, RBL 32. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 37,257 hrs · 21,564 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING CENTER BOX SHEAR FITTING CRACKED AT BS 540, LBL 6. REMOVED AND REPLACED FITTING PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,257 hrs · 21,564 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 6. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 35,681 hrs · 20,631 cycles

DURING SCHEDULED MV3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,181 hrs · 20,335 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EVAC SLIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,567 hrs · 19,947 cycles

DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,579 hrs · 19,956 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — BROKEN (L1 DOOR) · airframe 31,263 hrs · 18,027 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 29,564 hrs · 17,046 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 26 TO RBL 42. REPAIRED FLOORBEAM PER SWA EA.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,094 hrs · 15,637 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,552 hrs · 16,331 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT 9 ABC. REMOVED AND REPLACED LIGHT PER MM.

Part: PUMP — FAULTY (A-HYD SYSTEM) · airframe 26,117 hrs · 15,090 cycles

DIVERSION/DECLARED EMERGENCY. ENGINE DRIVEN "A" SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. "A" SYSTEM QUANTITY INDICATED ZERO. REMOVED AND REPLACED NR 1 ENGINE DRIVEN "A" SYSTEM HYDRAULIC PUMP PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 24,746 hrs · 14,337 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 24,456 hrs · 14,181 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR STRAP OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 24,017 hrs · 13,931 cycles

L1 COCKPIT WINDOW ARCED & CRACKED. REMOVED AND REPLACED L1 COCKPIT WINDOW PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 22,758 hrs · 13,222 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — READS LOW (L1 DOOR) · airframe 22,689 hrs · 13,184 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM.

Part: COFFEEMAKER — FAULTY (AFT GALLEY) · airframe 20,143 hrs · 11,713 cycles

ELECTRICAL ODOR IN AFT GALLEY REPORTED. REMOVED AND REPLACED BOTH AFT COFFEEMAKERS PER MM.

Part: WEDGE — DELAMINATED (T/E FLAP) · airframe 18,740 hrs · 10,947 cycles

DURING SCHEDULED 5Y CHECK, FOUND LT WING OUTBOARD AFT FLAP T/E WEDGE DELAMINATED. REPAIRED T/E WEDGE PER SRM.

Part: LENS — DAMAGED (AFT SVC DOOR) · airframe 15,014 hrs · 8,811 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE SIDE LIGHT LENS DAMAGED. REMOVED AND REPLACED LENS PER MM.

Part: BUSHING — WORN (RT ELEV) · airframe 13,935 hrs · 8,205 cycles

DURING SCHEDULED PM CHECK, SI-11038-55, RT ELEVATOR TAB FAILED FREEPLAY CHECK. REMOVED AND REPLACED RT ELEV TAB NR 1 HINGE BOLT AND BUSHING PER MM.

Part: COVER — LOOSE (CABIN) · airframe 13,619 hrs · 8,034 cycles

EEPLS COVER LOOSE AT FWD CABIN. SECURED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 13,493 hrs · 7,951 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSYS OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: COVER — CRACKED (CABIN) · airframe 12,361 hrs · 7,299 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED AT ROW'S 11 AND 21. REMOVED AND REPLACED COVERS PER MM.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 12,361 hrs · 7,299 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 11,072 hrs · 6,555 cycles

DIVERSION, AT CRUISE ALTITUDE GOT A WHEEL WELL FIRE WARNING. REMOVED AND REPLACED P8-1 ENG AND APU FIRE CONTROL PANEL. FUNCTIONAL AND OPS CK GOOD PER MM.

Part: COVER — BROKEN (CABIN) · airframe 10,619 hrs · 6,307 cycles

DURING SCHEDULED A1 CHECK, FOUND EEPLS COVERS BROKEN AT ROWS 1, 2, 8, 9, 22 AND 23. REMOVED AND REPLACED COVERS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 10,026 hrs · 5,939 cycles

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT MID CABIN LT SIDE. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 9,770 hrs · 5,798 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP, ROW 6 TO ROW 10. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DAMAGED (CABIN) · airframe 9,695 hrs · 5,758 cycles

DURING SCHEDULED RON, FOUND FWD CABIN EEPLS BATTERY PIN CONNECTOR BENT. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 9,695 hrs · 5,758 cycles

DURING SCHEDULED RON, FOUND EEPLS INOP AT MID CABIN. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 7,522 hrs · 4,566 cycles

DURING SCHEDULED RON, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 9,547 hrs · 5,679 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT MID CABIN. REMOVED AND REPLACED BATTERY PER MM.

Part: BUSHING — WORN (RH ELEVATOR) · airframe 9,508 hrs · 5,656 cycles

DURING SCHEDULED SERVICE CHECK, RH ELEVATOR TAB FAILED FREE PLAY CHECK. R&R BUSHINGS AT HINGES # 2, # 3 & # 4 PER MM.

Part: VALVE — FAILED (BRAKE SYS) · airframe 8,050 hrs · 4,809 cycles

DURING TAXI INTO POSITION FOR TAKEOFF, BRAKES LOCKED UP & RTO LIGHT ILLUMINATED. AIRCRAFT WOULD NOT MOVE. TOWED AIRCRAFT BACK TO GATE. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT AND PARKING BRAKE VALVE PER MM. C/W BITE CHECK AND SPEED BRAKE RTO TEST PER MM, OPS CHECK GOOD.

Part: COVER — CRACKED (CABIN) · airframe 6,843 hrs · 4,109 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER CRACKED AR ROW 11. R&R COVER PER MM.

Part: GCU — INOPERATIVE (NR 1) · airframe 6,079 hrs · 3,654 cycles

AIR TURNBACK, ON CLIMBOUT NR 1 ENG T/R FAILED, LT FWD RT AFT BOOST PUMPS FAILED, BOTH CDU''S, ELEC HYD PUMPS, YAW DAMP, AUTO FAIL PRESS, MOST CAPT INST, NO C/B''S TRIPPED. REMOVED AND REPLACED NR 1 GCU PER MM.

Part: PCU — INOPERATIVE (COCKPIT) · airframe 6,055 hrs · 3,641 cycles

AIR TURNBACK,ON CLIMBOUT T/R/I FAILED, BOOST PUMPS, BOTH CDV''S, LEFT WINDOW HEAT, NR 2 ELEC HYD PUMP, YAW DAMP AUTO FAIL, PRESS, MOST CAPT''S INST, ANTI SKID INOP. REMOVED AND REPLACED STANDBY PCU PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 4,838 hrs · 2,895 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH ENTRY DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. REPOSITIONED BOTH SLIDES PER MM.