N716SW

Part: ACTUATOR — INOPERATIVE (LH RAM AIR DOOR) · airframe 77,207 hrs · 45,706 cycles

LEFT RAM AIR DOOR CLOSED ON THE GROUND / CLOSING DMA #0515442 R&R L/H RAM AIR INLET ACTUATOR PER AMM 21-51-21. OPS CHECK GOOD RAR 95461 C/N 76618 P/N OFF/ON: 541674-4 S/N OFF: 10-4825 S/N ON: 19-7836

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 76,675 hrs · 45,410 cycles

CRACK INDICATION AFT OF FASTENER ON ROW 44 DOUBLER OUTER ROW AT STATION 727D +7 INCH, 3 INCHES BELOW STR 3R. ACCOMPLISHED EA 21-153-00216.

Part: ENGINE — SURGES (LEFT) · airframe 76,499 hrs · 45,307 cycles

CLIMBING THROUGH 21K SLIGHT SOUND/BUMP ON LEFT SIDE. EGT ON NR 1 WENT TO 900 DEGREES, BUT WAS PULLED BACK BEFORE REF LIMITATION. CRUISED AT 260 WITH EGT APPROXIMATELY 100 DEGREES HIGHER ON NR 1 (COMPARED TO NR 2) WITH THROTTLE ALIGNED. NO OTHER MAJOR INDICATIONS. NR 1 NEG REMOVED AND REPLACED, PER MT 771-00-01 REFERENCE SAM 65A J11593774 AS WELL POS: NR 1 P/N ON/OFF: 0720332 S/N OFF: 893861 S/N: 804732.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,158 hrs · 45,105 cycles

FWD SERVICE DOOR BOTTOM EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED CHARGER ASSEMBLY PACK AND BATTERY PACK, PER AMM 33-51-06. OPERATIONS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,158 hrs · 45,105 cycles

FWD SERVICE DOOR BOTTOM EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED CHARGER ASSEMBLY PACK AND BATTERY PACK, PER AMM 33-51-06. OPERATIONS CHECK GOOD.

Part: HANDLE — LOOSE (L1 DOOR) · airframe 75,857 hrs · 44,927 cycles

FWD ENTRY DOOR AFT ASSIST HANDLE IS LOOSE. / TIGHTENED FWD ENTRY DOOR AFT ASSIST HANDLE I.A.W. AMM 25-21-31-420-802 3.B.(B)

Part: FLOOR SUPPORT — CRACKED (BS 328-348) · airframe 75,857 hrs · 44,927 cycles

FLOOR INTERCOSTAL IS CRACKED BETWEEN STA 328 TO 348; WL208; LBL 46. (E AND E BAY) / REMOVED AND REPLACED FLOOR INTERCOSTAL BETWEEN STA 328-348 WL208; LBL46 IAW SRM 51-40-02-0G-0 AND DWG 141A5400

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 75,857 hrs · 44,927 cycles

EMERGENCY LIGHTS IN LH OVERWING EXIT DOOR INOP / RE-TERMINATED W3142-0263-16 INTO D12452P AND PERFORMED GOOD FUNCTIONAL TEST OF L/H OWE EMERGENCY EXIT LIGHTS (L751; ABOVE OWE) IAW SWPM 20-61-28; WDM 33-51-13; AND AMM 33-51-01-960-801 STEP 2.B.(2).

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 75,857 hrs · 44,927 cycles

RH OVERWING EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE / PERFORMED GOOD EMERGENCY LIGHTS - OPERATIONAL TEST IAW AMM 33-51-00-710-801.

Part: LIGHT — INOPERATIVE (ROW 9) · airframe 75,857 hrs · 44,927 cycles

ROW 9 LH ISLE ILLUMINATION EMERGENCY LIGHT DOES NOT ILLUMINATE / RELAMPED & PERFORMED A GOOD INSTALLATION TEST OF ROW 9 LH ISLE ILLUMINATION EMERGENCY LIGHT PER AMM 33-51-03-960-801

Part: LIGHT — INOPERATIVE (ROW 22) · airframe 75,857 hrs · 44,927 cycles

ROW 22 RH ISLE ILLUMINATION EMERGENCY LIGHT DOES NOT ILLUMINATE / RELAMPED AND PERFORMED GOOD FUNCTIONAL CHECK OF ROW 22 RH ISLE ILLUMINATION EMERGENCY LIGHT PER AMM 33-51-03-960-801 57736U 20AUG20

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,857 hrs · 44,927 cycles

COCKPIT DOME EMERGENCY LIGHT DOES NOT ILLUMINATE / RELAMPED COCKPIT DOME EMERGENCY LIGHT (L273) AND PERFORMED GOOD FUNCTIONAL TEST IAW AMM 33-51-03-960-801.

Part: CRADLE — DAMAGED (FWD FLASHLIGHT) · airframe 75,857 hrs · 44,927 cycles

FWD L/H WINDSCREEN LWR FLASHLIGHT HOLDER IS DAMAGED / REMOVED AND REPLACED FWD L/H WINDSCREEN LWD FLASH LIGHT HOLDER PER SOPM 20-50-01

Part: SIGN — DAMAGED (EMERGENCY LIGHT) · airframe 75,857 hrs · 44,927 cycles

EXIT SIGN DAMAGED ON AFT WALL OF LAV A. / REMOVED AND REPLACED EXIT SIGN ON AFT WALL OF LAV A PER AMM 33-51-01-960-802; OPS CHECK GOOD.

Part: STRIP — DAMAGED (AFT CARGO) · airframe 75,857 hrs · 44,927 cycles

AFT CARGO BAY FORWARD BULKHEAD CAP STRIP (453A2511-1) IS DAMAGED / RECEIVED NEW ACB FWD BLK HD CAP STRIP (453A2511-1) ON PO# 800158. NEW CAP STRIP TO BE INSTALLED ON CUST CARD # JPANEL-141-CLOSE

Part: WEB — CORRODED (BS 259) · airframe 75,857 hrs · 44,927 cycles

CORROSION AT BS 259 VERTICAL WEB LBL3 - LBL 7 WL 207 / DAMAGE REPAIRED PER EA 20-153-01504 REV IR (ATS ER 20-03024 REV IR). REFER TO NRC U196065 FOR TRACKING.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 75,857 hrs · 44,927 cycles

PAX CABIN FLOOR PANEL 221BF HAS NUMEROUS DAMAGED AREAS. / PAX CABIN FLOOR PANEL 221BF NUMEROUS DAMAGED AREAS WERE REPAIRED IAW SRM 53-00-50-2R-0. 56144U. 08/04/2020 3622C 04AUG20

Part: STRAP — CORRODED (BS 633-639) · airframe 75,857 hrs · 44,927 cycles

***CORROSION*** ON R/H OVERWING EXIT CUTOUT LOWER SILL STRAP STA 633-639; RBL 67; WL 220. / REPLACED RH OWE CUTOUT LOWER SILL STRAP AT STA 663-639 RBL 67 WL220 DUE TO NO PUBLISHED LIMITS FOR MATERIAL LOSS. IAW SRM 51-40-02-0G-0 AND BOEING DWG 144A8201 REV 4 STRAP FABRICATED ON CUSTOMER RO# 799265-SWA.

Part: STRAP — CORRODED (BS 887) · airframe 75,857 hrs · 44,927 cycles

AFT CARGO BAY BS887 CARGO FLOOR SPLICE STRAP HAS CORROSION AROUND NUT PLATE HOLES RBL10 TO LBL10 WL156 / REMOVED & REPLACED ACB BS 887 CARGO FLOOR SPLICE STRAP RBL 10 TO LBL 10; WL 156 IAW SRM 51-40-02; SRM 51-40-05; AIPC 53-42-11-30.

Part: STRINGER — CORRODED (BS 536) · airframe 75,857 hrs · 44,927 cycles

CORROSION ON END OF STRINGER 25R AT BS536 WL156 IN SNAKE PIT / CORROSION END OF STRINGER 25R AND B.S 536 WL 156 WAS REPAIRED PER ATS ER 20-02998 REV IR AND SWA EA 20-153-01495 REV IR

Part: SKIN — CORRODED (BS 677-700 S1-2R) · airframe 75,857 hrs · 44,927 cycles

CORROSION ON FUSELAGE SKIN AROUND 12 EACH #1 ADF ANTENNA MOUNT HOLES BS 677 TO 700; BETWEEN STR 1 AND STR 2R / CORROSION WAS REMOVED FROM AROUND 12 EACH #1 ADF ANTENNA MOUNT HOLES BS 677 TO 700; BETWEEN STR 1 & STR 2R AREAS OF DAMAGE REMOVAL WAS REWORKED AS PER EA 20-153-01445 REV IR & ATS ER 20-03027 REV IR

Part: SHIELD — CORRODED (FWD CARGO) · airframe 75,857 hrs · 44,927 cycles

FWD CARGO BAY SHIELD AFT OF CARGO DOOR BS492 TO BS500A HAS CORROSION AROUND NUT PLATES RBL23 WL156 / CORROSION ON FWD CARGO BAY SHIELD; BS 492-500A RBL 23; WL 156 FOUND TO BE OUT OF LIMITS DUE TO NO SRM LIMITS. REMOVED AND REPLACED SHIELD PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 143A0080.

Part: SHIELD — CORRODED (FWD CARGO) · airframe 75,857 hrs · 44,927 cycles

AFT CARGO BAY SHIELD FWD OF CARGO DOOR HAS CORROSION AROUND NUT PLATE HOLES BS767 TO BS794 RBL23 WL156 / CORROSION ON AFT CARGO BAY SHIELD BS 767-794 RBL 23; WL 156 FOUND TO BE OUT OF LIMITS DUE TO NO SRM LIMITS; REMOVED AND REPLACED SHIELD PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 146A0081.

Part: SUPPORT — CORRODED (BS 727-847) · airframe 75,857 hrs · 44,927 cycles

AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE HAS CORROSION AROUND NUT PLATE HOLES BS727 TO BS847 LBL25 WL156 / EVALUATED CORROSION ON ACB L/H FLOOR TO SIDEWALL SUPPORT; BS 727-847; REMOVED .015' FROM ORIG .040'; FOUND TO BE OUT OF LIMITS; IAW SRM 53-00-53-1A-2; REMOVED DAMAGED SECTION; LOCATED; DRILLED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT; BS 727-847 L/H. IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 146A7500.

Part: SUPPORT PLATE — CORRODED (AFT CARGO) · airframe 75,857 hrs · 44,927 cycles

AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS CORROSION AROUND NUT PLATE HOLES BS727 TO BS767 RBL25 WL156 / REMOVED & REPLACED ACB R/H FLOOR TO SIDEWALL SUPPORT PLATE BS 727-767; RBL 25; WL 156 IAW SRM 51-40-02; SRM 51-40-05; DWG # 146A7500.

Part: FLOORBEAM — CORRODED (BS 259.5) · airframe 75,857 hrs · 44,927 cycles

CORROSION ON UPPER FWD CHORD OF BS 259.5 FLOOR BEAM FROM LBL 3 TO LBL 7; WL 207.5 / REMOVED AND REPLACED BS259 FWD CHORD I.A.W BOEING DWG 141A7430; 141A0631 (CORROSION OUT OF LIMITS DUE TO NO SRM LIMITS

Part: ATTACH ANGLE — CRACKED (BS 694) · airframe 75,857 hrs · 44,927 cycles

CRACKED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL; STA 694; LBL 1; WL 207. / REMOVED AND REPLACED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL AT B.S 694; LBL1 WL 207 IAW SRM 51-40-02-0G-0 AND DWG 237A9112

Part: ATTACH ANGLE — CORRODED (BS 663) · airframe 75,857 hrs · 44,927 cycles

***CORROSION*** ON CREASEBEAM WEB ATTACH ANGLE STA 663; LBL 67; WL 208 ON UPPER SURFACE. / REMOVED CORROSION ON CREASEBEAM ATTACH ANGLE; STA 663; LBL 67; WL 208 ON UPPER SURFACE. MAX MATERIAL REMOVED .010' .5' X .6' FROM .056'. OUT OF LIMITS PER SRM 53-40-13-1A-1; SRM 51-10-02-0G-0. FABRICATED; TREATED & PRIMED NEW ATTACH ANGLE 7075T6 CLAD .056' LOT#1331117-2; PER SRM 51-40-05-0G-0; 51-40-02-0G-0; DWG# 144A5930; REV R; DWG# 144A5930; SRM 51-20-01-0G-0; SOPM 20-43-03. INSTALLED PER SRM 51-40-02-G-0; DWG# 144A5900; DWG# 144A5920.

Part: FLOORBEAM — CORRODED (BS 259.5) · airframe 75,857 hrs · 44,927 cycles

CORROSION ON UPPER AFT CHORD OF BS 259.5 FLOOR BEAM FROM LBL 2 TO LBL 9; WL 207.5 / REPAIRED DAMAGE ON AFT CHORD OF BS 259.5 FLOOR BEAM FROM LBL 2 TO LBL 9; WL 207.5 PER ER #20-03024 REV IR AND EA #20-153-01504 REV IR.

Part: ATTACH ANGLE — CRACKED (BS 694) · airframe 75,857 hrs · 44,927 cycles

CRACKED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL; STA 694; RBL 1; WL 207. / REMOVED AND REPLACED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL AT B.S 694; RBL 1 WL 207 IAW SRM 51-40-02-0G-0 AND DWG 237A9110

Part: ATTACH ANGLE — CRACKED (BS 694) · airframe 75,857 hrs · 44,927 cycles

CRACKED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL; STA 694; RBL 25; WL 204. / REMOVED AND REPLACED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL AT B.S 694; RBL 25; WL 204 IAW SRM 51-40-02-0G-0 AND DWG 237A9112

Part: BULKHEAD — CRACKED (BS 663) · airframe 75,855 hrs · 44,926 cycles

B.S. 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT R.B.L. 48; W.L. 154. REMOVED AND REPLACED CRACKED BS663 LOWER COMPOSITE BULKHEAD RBL48 WL154 PER SRM 51-40-02-0G-0 & SRM 51-40-05-0G-0; DWG 111A1000; SOPM 20-50-19.

Part: FLOOR SKIN — DENTED (COCKPIT) · airframe 75,857 hrs · 44,927 cycles

FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. / DAMAGE REPAIRED PER EA 1-A53-33179 REV 1.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 75,857 hrs · 44,927 cycles

FWD ENTRY DOOR SLIDE COVER FWD GIRT BAR RETAINER FASTENERS ARE LOOSE. INSTALLED FOUR EACH FASTENERS FWD ENTRY DOOR SLIDE COVER FWD GIRT BAR IAW SRM 51-40-02-0G-0 AND PER DWG 416A2204 REV:B 92421U 08-08-20

Part: VAPOR BARRIER — CRACKED (R/H MLG W/W) · airframe 74,930 hrs · 44,334 cycles

TRANSFERRED FROM D303679. FOUND CRACK IN PANEL BEHIND MULE HOOK UP APPROXIMATELY 16' LONG. CRACK LOCATED IN WHEEL WELL VAPOR BARRIER ON RH SIDE BETWEEN RBL 45.64 AND RBL 54.21. / APPLIED INTERIM REPAIR IWA SRM 57-10-10-1A-2; PARA 2.C.(4)(A)

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 74,063 hrs · 43,764 cycles

L/H HORIZONTAL STAB. UPPER FWD SLIDING SEAL CRACKED. / R&R L/H HORIZONTAL STAB. UPPER FWD SLIDING SEAL REF AMM 53-31-31.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 73,781 hrs · 43,576 cycles

EMERGENCY LIGHT LENS COVER FELL OFF. INSTALLED COVER PER AMM.

Part: STRAP — INOPERATIVE (FLASHLIGHT) · airframe 73,572 hrs · 43,444 cycles

FORWARD LOWER FLIGHT ATTENDANT JUMPSEAT STRAP FOR FLASHLIGHT INOP. R&R STRAP IAW SIP.

Part: COVER — DETACHED (R2 DOOR) · airframe 73,559 hrs · 43,437 cycles

R2 DOOR ESCAPE SLIDE FLAP DETACHED. REAPPLIED HOOK AND LOOP COVER OVER SLIDE FLAP PER "SIP".

Part: FASTENER — LOOSE (EMERGENCY EXIT) · airframe 73,009 hrs · 43,081 cycles

RT EMERGENCY EXIT DOOR LOWER HANDLE MOLDING LOOSE. INSTALLED FASTENER PER SIP.

Part: COVER — CRACKED (R1 DOOR) · airframe 73,000 hrs · 43,074 cycles

R1 DOOR EXIT DOOR LIGHT CRACKED. R&R COVER IAW SIP.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 72,027 hrs · 42,448 cycles

FORWARD INBOARD EMERGENCY FLASHLIGHT INOP. R&R BATTERIES IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 72,027 hrs · 42,448 cycles

FORWARD OUTBOARD EMERGENCY FLASHLIGHT INOP. R&R BATTERIES IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 72,018 hrs · 42,443 cycles

FORWARD LOWER FLASHLIGHT INOP. R&R BATTERY PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 71,901 hrs · 42,365 cycles

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

Part: GIRT BAR — OUT OF POSITION (R1 DOOR) · airframe 71,282 hrs · 41,963 cycles

R1 DOOR SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED GIRT BAR PER MM.

Part: WINGLET — DELAMINATED (RIGHT WING) · airframe 70,646 hrs · 41,563 cycles

MULTIPLE DELAMANATIONS ON RIGHT WINGLET AROUND OPENING 627 AB MOD / REMOVED AND REPLACED R/H WINGLET PER AMM 57-21-21. LIGHTS OPS CHECK GOOD. TAG #555500 R/H PN OFF/ON: 737-0010-345 SN OFF/ON: N0403 / N0345

Part: BATTERY PACK — FAILED (CABIN) · airframe 69,682 hrs · 40,938 cycles

LT EMERGENCY LIGHTING BATTERY PACK FAILED OPS CHECK AT ROW 17. R&R BATTERY PACK IAW AMM.

Part: CHARGER — FAILED (CABIN) · airframe 69,682 hrs · 40,938 cycles

LT EMERGENCY LIGHTING BATTERY PACK FAILED OPS CHECK AT ROW 17. R&R CHARGER IAW AMM.

Part: SEAT TRACK — CRACKED (FLIGHT DECK) · airframe 69,682 hrs · 40,938 cycles

FLIGHT DECK CAPTAINS SEAT; INBOARD FORWARD SEAT TRACK; IS CRACKED ON THE FORWARD END. / REPLACED FLIGHT DECK; CAPTAIN'S SEAT; INBOARD FWD SEAT TRACK IAW B737NG AMM 25-11-11-400-801 STEP D. WN1189.

Part: STIFFENER — CRACKED (RT WING) · airframe 69,682 hrs · 40,938 cycles

RT WING TRAILING EDGE FORWARD CURVED STIFFENER ANGLE CRACKED. R&R STIFFENER IAW SRM AND DWG.

Part: RAIL — CORRODED (FWD CARGO RH) · airframe 69,682 hrs · 40,938 cycles

FWD CARGO PIT FLOOR PANEL ATTACH RAIL AT STA 500D HAS CORROSION ON AFT SIDE R/H SIDE / REMOVED CORROSION AT FWD CARGO FLOOR PANEL ATTACH RAIL STA 500D IAW SRM 51-10-02-0G-0 STEP 15 (100% MATERIAL LOSS). REMOVED / REPLACED FLOOR PANEL ATTACH RAIL AT FWD CARGO STA 500D FROM LBL 21 TO RBL 21. IAW SRM 51-40-02-0G-0 (BOEING DWG# 143A94581 REV A. TAG# WN0997

Part: SEAT TRACK — CRACKED (COCKPIT FLOOR) · airframe 69,682 hrs · 40,938 cycles

FIRST OFFICER`S AFT SEAT TRACK CRACKED. R & R THE SEAT TRACK IAW SRM AND MM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 69,682 hrs · 40,938 cycles

R1 DOOR FORWARD UPPER CORNER BEAR STRAP CRACKED AT BS 294. REPAIRED DOUBLER IAW EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,682 hrs · 40,938 cycles

R1 DOORWAY, UPPER COVE PANEL STUB FRAME CRACKED AT BS 294.1. R&R STUB FRAME IAW DWG.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 69,682 hrs · 40,938 cycles

MAIN CABIN SEAT TRACK LBL 45 STA 639 TO STA 663 HAS CORROSION ON LOWER LOBE. / BLENDED AND REMOVED CORROSION ON SEAT TRACK BETWEEN STA 639 TO STA 663 LBL 45 MAX MATERIAL LOSS OF .045' MAX ALLOWED .040' OUT OF LIMITS I/A/W SRM 53-00-52-1A-1. SEAT TRACK REPLACED FROM STA 639 +10' TO SAT 727B ON N/R X736971

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,682 hrs · 40,938 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 663 TO BS 706, LBL 45. R&R SEAT TRACK IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 69,682 hrs · 40,938 cycles

AFT CARGO PIT ON TOP OF FRAME CORNER ATTACH FITTING CRACKED AT BS 947, LBL 11. R&R FITTING IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (LT WHEEL WELL) · airframe 69,682 hrs · 40,938 cycles

WHILE ACCESSING L/H STA 663 VAPOR BARRIER FOUND P/N 111A1301-5 CRACKED ON INBD END / REPLACED ANGLE SUPPORT P/N: 111A1301-5 AT L/H STA 663 VAPOR BARRIER. REMOVED AND INSTALLED W/O 37281/1000/0004 IAW B737-700 SRM 51-40-05-0G-0 DWG: 111A1001 REV: F TAG:

Part: GUSSET — CRACKED (BS 500D) · airframe 69,682 hrs · 40,938 cycles

FUSELAGE GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R THE GUSSET IAW SRM.

Part: GUSSET — CRACKED (BS 500D) · airframe 69,682 hrs · 40,938 cycles

FUSELAGE GUSSET CRACKED AT BS 500D, STRINGER 19L. R & R THE GUSSET IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,682 hrs · 40,938 cycles

LT WING LOWER SURFACE NR 3 SLAT SKIN AT FASTENERS HOLE CRACKED. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (BS 787) · airframe 69,682 hrs · 40,938 cycles

FRAME CRACKED AT BS 787, BETWEEN STRINGERS 8L TO 9L. REPAIRED THE FRAME IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,682 hrs · 40,938 cycles

RT SIDE ANGLE STIFFENER CRACKED AT BS 663 BOTH LOWER INBOARD AND OUTBOARD FASTENER HOLES. R&R ANGLE IAW SRM & DWG.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 69,682 hrs · 40,938 cycles

AFT CARGO COMPARTMENT; STA 947.5; LBL-20; FLLOR SUPPORT STRAP; ON LWR SIDE HAS MULTIPLE AREAS OF BARE METAL / REMOVED FLOOR SUPPORT STRAP AT AFT CARGO STA 947.5 IAW SRM 51-40-02-0G-00 EVALUATE FLOOR SUPPORT STRAP NO LIMITS ALLOWABLE FOUND OUT OF LIMITS I.A.W SRM 51-10-02 DRILLED NEW FLOOR SUPPORT I.A.W SRM 51-40-0G-00 AND BOEING DWG 149A117. INSTALLED NEW FLOOR SUPPORT STRIP IAW SRM 51-40-02-0G-00 AND BOEING DWG 149A8117

Part: INTERCOSTAL — CRACKED (AFT CARGO COMPT) · airframe 69,682 hrs · 40,938 cycles

AFT CARGO COMPARTMENT; STA 937.5; RBL-10; FLOOR SUPPORT HAS CRACK AT FASTENER HOLE / REMOVED CRACKED LULER COSTAL AFT CARGO STA 947.5 RBL10 AND INSTALLED NEW INTERCOSTAL ALL IAW SRM 51-40-02-0G-0 AND DWG # 147A7500 REV-. ATAG#A44404

Part: STIFFENER — CRACKED (WHEEL WELL RH) · airframe 69,682 hrs · 40,938 cycles

STA. 663 RBL5 VERTICLE STIFFENER CRACKED BETWEEN TWO FASTERS. / REPLACED STA: 663 RBL 5 VERTICAL STIFFENER IAW B737-700 SRM 51-40-02-0G-0 DWG: 144A 7100 REV: B TAG: WN3325

Part: HOUSING — BROKEN (EMERGENCY LIGHT) · airframe 69,682 hrs · 40,938 cycles

MID CABIN OVERHEAD EXIT LIGHT HOUSING BROKEN. R & R THE LIGHT HOUSING IAW MM.

Part: FLOOR PANEL — CORRODED (FLIGHT DECK) · airframe 69,682 hrs · 40,938 cycles

FLT DECK PANEL 211 AF IS CORRODED / REPLACED CORRODED PANEL 211AF WITH NEW PANEL MPN 141A5133-15 IAW DWG 141A5133 REV C. APPLIED COLOR TOPCOAT IAW B737-700 AMM 51-21-73-370-803. ATAG A38180

Part: PANEL — ELONGATED (LH PYLON) · airframe 69,682 hrs · 40,938 cycles

#1 PYLON STRUT PANEL 431ER HAS OBLONG HOLE ON FORWARD EDGE / EVALUATED; PREPPED; CLEANED AND REPAIRED ELONGATED/OVERSIZED FASTENER HOLE ON FWD EDGE LOWER SURFACE ON PANEL 431ER IAW B737 SRM 51-70-04-2R-9; PARA (A-P) REV 64.

Part: SUPPORT — CRACKED (BS 500D) · airframe 69,682 hrs · 40,938 cycles

LEFT EXTERNAL FUSELAGE WING TO BODY PANEL SUPPORT SPLICE CRACKED AT BS 500D, BETWEEN STRINGERS 18L TO 19L. R & R THE THE SUPPORT IAW DWG AND SRM.

Part: SUPPORT — CRACKED (BS 500D) · airframe 69,682 hrs · 40,938 cycles

RIGHT EXTERNAL FUSELAGE WING TO BODY PANEL SUPPORT SPLICE CRACKED AT BS 500D, BETWEEN STRINGER 18R TO 19R. R & R THE SUPPORT SPLICE IAW DWG AND SRM.

Part: ANGLE — CRACKED (LT WING LE) · airframe 69,682 hrs · 40,938 cycles

LEFT WING LOWER LEADING EDGE AT WING STA 200 SPLICE ANGLE CRACKED. R & R THE ANGLE IAW SRM AND DWG.

Part: BRACKET — CRACKED (RT WING) · airframe 69,682 hrs · 40,938 cycles

RT WING LEADING EDGE CAVITY UNDER AND AFT OF OUTBOARD KRUEGER FLAP LEADING EDGE SUPPORT STRUCTURE BRACKET FOR LOWER ACCESS PANEL CRACKED. R&R BRACKET IAW DWG AND EA.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 69,682 hrs · 40,938 cycles

AFT CARGO PIT FWD CORNER SCUFF PLATE CRACKED / REPAIRED AFT CARGO FWD CORNER SCUFF PLATE WITH WELD REPAIR IAW EA 1-A53-2076 REV 11

Part: FAIRING — CRACKED (RT FLAP TRACK) · airframe 69,682 hrs · 40,938 cycles

RIGHT WING NR 6 FLAP TRACK FAIRING 642BB BOTTOM INTERNAL SURFACE CRACKED 46 INCHES FROM FORWARD EDGE. REPAIRED FAIRING IAW SRM AND AMM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 69,682 hrs · 40,938 cycles

HORIZONTAL PRESSURE DECK WEB CRACKED AT BS 663+2, LBL 30. REPAIRED WEB IAW EA.

Part: PRESSURE DECK — CRACKED (BS 663) · airframe 69,682 hrs · 40,938 cycles

HORIZONTAL PRESSURE DECK CRACKED AT BS. 663+2, BETWEEN RBL 38 TO RBL 40. / REPAIRED WEB IAW EA.

Part: FLAP — DELAMINATED (RH OUTBD AFT FLA) · airframe 69,682 hrs · 40,938 cycles

R/H WING OUTBD AFT FLAP INBD CORNER DELAMED. / REPAIRED R/ WING OUTBD AFT FLAP INBD CORNER LOWER SURFACE I/A/W SRM 51-70-10-2R-0 GENERAL REV 64; SRM 51-70-10-2R-4 REV 64; PER SRM 57-53-01-2R-4 REV 64.

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 69,682 hrs · 40,938 cycles

AFT CARGO COMPARTMENT; STA. 727D+15.5' OFF BL0; FLOOR SUPPORT HAS CORROSION. MARKED WITH A DOT. / NOT ALLOWABLE LIMITS PUBLISHED PER SRM REMOVED/REPLACED AFT CARGO CENTER SECTION FLOOR SUPPORT STA 727D + 15.5' IAW SRM 51-40-02-0G-0 TAG # A37182

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,682 hrs · 40,938 cycles

FORWARD CARGO COMPARTMENT "Z" ANGLE CORRODED BETWEEN BS 500C TO BS 500D, RT. R&R Z-ANGLE IAW SRM AND DWG.

Part: WEB — CORRODED (FWD CARGO THRESH) · airframe 69,682 hrs · 40,938 cycles

FWD CARGO DOOR SURROUND; STA 460 DOOR SILL WEB CORRODED. / BEGAN BLENDING CORROSION %100 MATERIAL LOSS OUT OF LIMITS; IAW SRM. 51-10-02-0G-0. AND 53-30-15-1A-1. ORIG 'T' .045' LOSS .045'; REMAINING .000'; REMOVED AND REPLACED DOOR SILL WEB. PN 654A0003-58 IAW; BOEING DWG 143A8120 REV- O ATAG A62528

Part: FLOORBEAM — CORRODED (BS 727E) · airframe 69,682 hrs · 40,938 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 727E+3, LBL 3. R & R THE FLOORBEAM IAW SRM AND DWG.

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 69,682 hrs · 40,938 cycles

AFT CARGO COMPARTMENT CENTER SECTION; STA. 767 LBL2.5; THERE IS CORROSION AROUND A SCREW HOLE ON THE FLOOR PANEL SUPPORT. / NOT ALLOWABLE LIMITS PUBLISHED PER SRM. REMOVED/REPLACED AFT CARGO CENTER SECTION AT STA 767 IAW SRM 51-40-02-0G-0 ATG # WN0692

Part: SKIN — CRACKED (RT WING SLAT) · airframe 69,682 hrs · 40,938 cycles

RIGHT WING NR 8 SLAT, LOWER SKIN CRACKED. REPAIRED THE SLAT SKIN IAW SRM.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 69,682 hrs · 40,938 cycles

FWD CARGO PIT CENTER SCUFF PLATE CRACKED / FWD CARGO PIT CENTER SCUFF PLATE WELDED ON S/W EA 1-A53-2076 REV 11

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 69,682 hrs · 40,938 cycles

FWD CARGO PIT FWD CORNER SCUFF PLATE CRACKED / FWD CARGO PIT FWD CORNER SCUFF PLATE WELDED ON S/W EA 1-A53-2076 REV 11

Part: FLAP — LOOSE (LT WING) · airframe 69,170 hrs · 40,627 cycles

LT WING OUTBOARD TRAILING EDGE FLAP LOOSE. R&R AFT FLAP PER MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 68,368 hrs · 40,090 cycles

R1 DOOR EXIT SIGN FORWARD ESCAPE SLIDE LIGHT FAILED TO TEST. R & R THE BATTERY IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 68,368 hrs · 40,090 cycles

OVERWING EXIT LOCATOR SIGN FAILED TEST. R&R BATTERY IAW MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 68,368 hrs · 40,090 cycles

LEFT AISLE LIGHTS FAILED TO TEST BETWEEN ROWS 1 AND 2. R & R THE BATTERY IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 68,368 hrs · 40,090 cycles

FORWARD EXIT LOCATOR SIGN FAILED TEST. R&R BATTERY IAW MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 68,368 hrs · 40,090 cycles

OVERWING ESCAPE AISLE LIGHT ASSEMBLY FAILED TO TEST. R & R THE BATTERY IAW MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 68,368 hrs · 40,090 cycles

LEFT OVERWING ESCAPE HATCH LIGHT ASSEMBLY FAILED TO TEST. R & R THE BATTERY IAW MM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,754 hrs · 39,718 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE SUPPORT FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 67,754 hrs · 39,718 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE SUPPORT FITTING CORRODED. REPAIRED FITTING PER EA.

Part: LIGHT — BROKEN (CABIN) · airframe 66,214 hrs · 38,814 cycles

LEFT OVERWING EXIT LIGHT BROKEN. R & R THE LIGHT ASSY IAW MM.

Part: CONTROL VALVE — FAULTY (PRECOOLER) · airframe 65,780 hrs · 38,549 cycles

RIGHT BLEED TRIPPED, WOULD NOT RESET. RETURNED TO DEPARTURE. R & R THE PRECOOLER CONTROL VALVE IAW MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 65,619 hrs · 38,459 cycles

EXIT LIGHT LENS MISSING AT ROW 6 ABC. INSTALLED A NEW LENS IAW MM.

Part: CONNECTOR — BROKEN (CABIN) · airframe 63,648 hrs · 37,285 cycles

R2 DOOR EMER EXIT LIGHT CONNECTOR BROKEN. R & R CONNECTOR IAW AMM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

FLOOR RAIL SPLICE STRAP CORRODED AT BS 767+5, LBL 3. R & R SPLICE IAW EA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

L2 INNER LOWER CHORD CORRODED. R & R CHORD IAW DWG & SRM.

Part: STRUCTURE — CORRODED (R2 DOOR) · airframe 63,648 hrs · 37,285 cycles

R2 DOOR LOWER INNER CHORD CORRODED. R & R CHORD IAW SRM & DWG.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 63,648 hrs · 37,285 cycles

WHEEL WELL SPAR VERTICAL PRESS WEB CRACKED AT BS 663, RBL 40. REPAIRED WEB IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 50 TO LBL 50. R & R FLOORBEAM IAW SRM & EA.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 63,648 hrs · 37,285 cycles

LEFT WING CTR SUPPORT BRACKET FOR UPPER TE WING PANEL CRACKED, AT LOWER MOUNT BOLT HOLE, RSS 270. R & R BRACKET IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 63,648 hrs · 37,285 cycles

RIGHT WING UPPER TE PANEL SUPPORT CLIP CRACKED INBD SIDE OF DEFLECTION ROLLER RIB, RSS 280, 15" AFT OF REAR SPAR. R & R CLIP IAW SRM.

Part: SUPPORT — CRACKED (RT WING) · airframe 63,648 hrs · 37,285 cycles

RIGHT WING UPPER TE PANEL, SEAL RETAINER SUPPORT CRACKED AT RSS 273, 18" AFT OF REAR SPAR. R & R SUPPORT IAW DWG.

Part: PRESSURE DECK — CORRODED (LT MLG WW) · airframe 63,648 hrs · 37,285 cycles

LEFT PRESS DECK ABOVE MLG WW INNER CREASE BEAM CHORD CORRODED, BETWEEN BS 710 - 714, LBL 64. REPAIRED CHORD IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

CREASE BEAM CHORD CORRODED, BETWEEN BS 720 - 725, BETWEEN LBL 63 - 65. R & R CHORD IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

CREASE BEAM INNER CHORD CORRODED AT BS 694, RBL 63. R & R CHORD IAW SRM & DWG.

Part: NUT PLATE — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

AFT CARGO DOOR FRAME NUTPLATE STRIP CORRODED AT BS 793, STRINGER 25R, FWD LOWER CORNER. R & R STRIP IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

FORWARD CARGO SUB THRESHOLD WEB CORRODED, BETWEEN BS 440 - 493, BETWEEN RBL 24 - 28. R & R WEB IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

INTERCOSTAL CORRODED AT BS 300, RBL 10. R & R INTERCOSTAL IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

AFT PAX COMPARTMENT FLOOR SUPPORT CORRODED AT BS 99.5, RBL 7. R & R SUPPORT IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

AFT PAX COMPARTMENT FLOOR STRUCTURE ANGLE CORRODED AT BS 945.5, LBL 0. R & R ANGLE IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

AFT PAX COMPARTMENT, FLOOR STRUCTURE FLOOR SUPPORT, UPPER SURFACE CORRODED AT BS 970.5, RBL 14. R & R STRUCTURE IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

AFT PAX COMPARTMENT FLOOR SUPPORT CORRODED AT BS 958.5, RBL 14. R & R SUPPORT IAW SRM & DWG.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

FLOOR STRUCTURE SHEAR WEB CORRODED, BETWEEN BS 986.5 - 1016, BETWEEN RBL 37 - 47. R & R SHEAR WEB IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

AFT PAX COMPARTMENT, FLOOR STRUCTURE CORRODED AT BS 966.5, RBL 24. REPAIRED FLOORBEAM IAW SRM & EA.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

AFT PAX COMPARTMENT, FLOOR STRUCTURE SHEAR WEB CORRODED AT BS 1014, LBL 40. R & R SHEAR WEB IAW DWG & SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

AFT PAX COMPARTMENT, FLOOR STRUCTURE CORRODED AT BS 949.5, RBL 44. R & R STRUCTURE IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

FLOORBEAM CORRODED AT BS 328, RBL 39, UPPER SURFACE. REPAIRED FLOORBEAM IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

AFT PAX COMPARTMENT FLOOR SUPPORT CORRODED AT BS 961.5, RBL 17. R & R SUPPORT IAW SRM & DWG.

Part: STRIP — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

AFT CARGO BAY FWD SCUFF PLATE TO FLOOR CAP CORRODED AT BS 787, RBL 20. R & R CAP STRIP IAW SRM & DWG.

Part: FAIRING — CRACKED (LT WING) · airframe 63,648 hrs · 37,285 cycles

LEFT WING TO BODY FAIRING 195BL TOP ROW OF SCREW HOLES CRACKED. REPAIRED FAIRING IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

FLOOR SIDEWALL SUPPORT CORRODED AT BS 865, LBL 12. R & R SUPPORT IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

INTERCOSTAL CORRODED BETWEEN BS 847 - 852, RBL 6. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

INTERCOSTAL CORRODED BETWEEN BS 767 - 771, RBL 6. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

INTERCOSTAL BETWEEN FLOORBEAMS CRACKED, BETWEEN BS 277 - 294, BL 0. R & R INTERCOSTAL IAW SRM & DWG.

Part: FAIRING — CRACKED (LT WING) · airframe 63,648 hrs · 37,285 cycles

LEFT WING TO BODY FAIRING 195CL AFT LOWER CORNER PATCH CRACKED. REPAIRED FAIRING IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

FLOORBEAM INTERCOSTAL CRACKED BETWEEN BS 308 - 328, LBL 47. R & R INTERCOSTAL IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

FORWARD ENTRY DOOR CREASE BEAM CORRODED. R & R CREASE BEAM IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

INTERCOSTAL CORRODED BETWEEN BS 344 - 328, LBL 12. R & R INTERCOSTAL IAW SRM & DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

SUB THRESHOLD WEB CORRODED, BETWEEN BS 802 - 835, RBL 25. R & R THRESHOLD IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

INTERCOSTAL CORRODED, BETWEEN BS 727A - 727A+2, RBL 3. R & R INTERCOSTAL IAW DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 727D - 767, RBL 20. R & R SUPPORT IAW SRM & DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

KEEL BEAM CLIP CORRODED AT BS 727D, STRINGER 27L. R & R CLIP IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

FLOOR RAIL BEAM CORRODED AT BS 727D+5, RBL 8. REPAIRED FLOORBEAM IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

FLOOR TRACK CRACKED AT BS 767, RBL 14. R & R FLOOR TRACK IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

INTERCOSTAL CORRODED BETWEEN BS 784 - 800, RBL 6. R & R INTERCOSTAL IAW DWG & SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

INTERCOSTAL CORRODED, BETWEEN BS 727A - 727A+6, LBL 3. R & R INTERCOSTAL IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

FLOOR RAIL BEAM CORRODED AT BS 727D+5, LBL 8. R & R FLOORBEAM IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

FRAME CORRODED AT BS 947, LBL 9. REPAIRED FRAME IAW DWG & SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

FLOOR TRACK CORRODED, BETWEEN BS 787 - 867, RBL 14. R & R TRACK IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

FRAME CORRODED AT BS 787, BETWEEN LBL 24 - 28. R & R FRAME IAW ER & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

FLOOR RAIL BEAM CORRODED AT BS 727D+5, LBL 12. R & R FLOORBEAM IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

FLOOR TRACK CORRODED AT BS 727D+5, LBL 17. R & R TRACK IAW DWG & SRM.

Part: LIGHT — DAMAGED (CABIN) · airframe 63,648 hrs · 37,285 cycles

G4 AFT GALLEY EMER EXIT LIGHT DAMAGED. R & R LIGHT IAW AMM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

R2 DOOR AT AFT END SHEAR WEB CORRODED AT BS 986, RBL 46. R & R WEB IAW SRM & DWG.

Part: LIGHT — DAMAGED (CABIN) · airframe 63,648 hrs · 37,285 cycles

AFT LAVATORY EMER EXIT & SALIDA LIGHT DAMAGED. R & R LIGHT IAW AMM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

INTERCOSTAL CORRODED BETWEEN BS 847 - 855, LBL 7. R & R INTERCOSTAL IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

FLOOR RAIL BEAM CORRODED AT BS 727D+5, LBL 3. REPAIRED FLOORBEAM IAW EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

FLOOR TRACK CORRODED BETWEEN BS 927 - 934, LBL 3. R & R FLOOR TRACK IAW SRM & DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

BULKHEAD SUPPORT CRACKED AT BS 727, RBL 4. R & R SUPPORT IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,648 hrs · 37,285 cycles

FLOOR RAIL BEAM CORRODED AT BS 727D+5, RBL. R & R FLOORBEAM IAW SRM & DWG.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,829 hrs · 36,825 cycles

LEFT GND EMER EXIT LIGHT INOPERATIVE. R & R BATTERY PACK ASSEMBLY IAW AMM.

Part: BRACKET — LOOSE (R2 DOOR) · airframe 61,406 hrs · 35,991 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET IAW SIP.

Part: COVER — LOOSE (EXIT SIGN) · airframe 61,336 hrs · 35,943 cycles

RIGHT OVERWING EXIT DOOR SIGN COVER LOOSE. SECURED SIGN IAW EA.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 60,754 hrs · 35,621 cycles

OVERWING EXIT SIGN COVER FELL OFF. REINSTALLED COVER IAW AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 60,665 hrs · 35,576 cycles

R1 DOOR SLIDE OUT OF ADJUSTMENT. REPOSITIONED SLIDE IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,207 hrs · 35,320 cycles

RIGHT OVERWING EMER HATCH LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 59,388 hrs · 34,862 cycles

EMERGENCY LIGHTING BATTERY PACK M1669 FAILED TEST. R & R BATTERY PACK IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 57,699 hrs · 33,883 cycles

R1 DOOR EXIT LIGHT BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 57,622 hrs · 33,847 cycles

RIGHT MID CABIN SERVICE DOOR SLIDE EMER LIGHT SIGN INOPERATIVE. R & R BATTERY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,622 hrs · 33,847 cycles

RIGHT BULLNOSE EMER LIGHT INOPERATIVE AT ROW 18. R & R LIGHT ASSEMBLY IAW MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 57,258 hrs · 33,645 cycles

L2 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE ASSEMBLY IAW MT.

Part: CONNECTOR — LOOSE (CABIN) · airframe 57,241 hrs · 33,637 cycles

RIGHT OVERWING EMER EXIT LOCATOR SIGN CONNECTOR LOOSE. RECONNECTED SIGN IAW WDM & MM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 57,241 hrs · 33,637 cycles

RIGHT LOWER FUSELAGE SUPPORT ANGLE CRACKED AT OTBD OF RT RAM AIR EXHAUST DUCT. R & R ANGLE IAW SRM & DWG.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 57,241 hrs · 33,637 cycles

COCKPIT RT NR 1 WINDOW FRAME CRACKED AT UPPER OTBD CORNER. REPAIRED FRAME IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,241 hrs · 33,637 cycles

MAIN CABIN SEAT TRACK FLANGE CRACKED AT BS 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 57,241 hrs · 33,637 cycles

RIGHT HORIZONTAL STABILIZER LOWER AFT PANEL 343AB INBD AFT SEAL CRACKED. R & R SEAL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,241 hrs · 33,637 cycles

FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,241 hrs · 33,637 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,241 hrs · 33,637 cycles

FRAME CRACKED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,241 hrs · 33,637 cycles

FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,241 hrs · 33,637 cycles

FRAME CRACKED AT BS 827, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,241 hrs · 33,637 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,241 hrs · 33,637 cycles

FRAME CRACKED AT BS 500C, STRINGER 8R. REPAIRED FRAME IAW SRM & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,241 hrs · 33,637 cycles

FRAME CRACKED AT BS 500C, STRINGER 8L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,241 hrs · 33,637 cycles

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

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 57,241 hrs · 33,637 cycles

RIGHT KEEL BEAM CRACKED AT BS 663, BETWEEN RBL 8 TO RBL16. REPAIRED KEEL BEAM IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 57,241 hrs · 33,637 cycles

RIGHT CHORD CRACKED AT BS 540, BETWEEN STRINGER 22R TO STRINGER 23R. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,241 hrs · 33,637 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 364 TO BS 371, BETWEEN STRINGER 17L TO STRINGER 17R. REPAIRED SKIN IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,241 hrs · 33,637 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 890 TO BS 900, BETWEEN STRINGER 17L TO STRINGER 17R. REPAIRED SKIN IAW AMM.

Part: SKIN — CORRODED (CARGO DOOR) · airframe 57,241 hrs · 33,637 cycles

AFT CARGO DOOR INNER SKIN CORRODED AT FWD LOWER. REPAIRED SKIN IAW SRM & EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,241 hrs · 33,637 cycles

E & E COMPARTMENT FLOORBEAM INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 11. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,241 hrs · 33,637 cycles

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

Part: PANEL — CRACKED (LT MLG WW) · airframe 57,241 hrs · 33,637 cycles

LEFT WW BEHIND HYD PTU VLV WEB PANEL CRACKED ALONG FASTENERS ROW. REPAIRED PANEL IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 57,241 hrs · 33,637 cycles

LEFT CHORD CRACKED AT BS 540, BETWEEN STRINGER 22L TO STRINGER 23L. REPAIRED CHORD IAW EA.

Part: FLAP — DAMAGED (LT WING) · airframe 57,241 hrs · 33,637 cycles

LEFT WING NR 1 KRUEGER FLAP DAMAGED AT INBD CORNER. R & R KRUEGER FLAP ASSEMBLY IAW AMM.

Part: PANEL — CRACKED (RT WING) · airframe 56,806 hrs · 33,396 cycles

RIGHT WING LE COVE PANEL CRACKED. R & R PANEL IAW DWG & SRM.

Part: PANEL — CRACKED (RT WING) · airframe 56,804 hrs · 33,394 cycles

RIGHT LE PANEL CRACKED. R & R PANEL IAW DWG & SRM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 55,727 hrs · 32,751 cycles

RT OVERWING AFT EMERGENCY EXIT SIGN INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,727 hrs · 32,751 cycles

RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,727 hrs · 32,751 cycles

LT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: PLATE — CRACKED (LT WING) · airframe 55,179 hrs · 32,416 cycles

LT WING LOWER FIXED TE PANEL AFT OF ENGINE CRACKED WIGGLE PLATE. R & R PLATE SRM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 53,781 hrs · 31,578 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 53,781 hrs · 31,578 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MM.

Part: SLIDE — CRACKED (LT HORIZ STAB) · airframe 52,927 hrs · 31,101 cycles

LEFT HORIZONTAL STAB FWD LOWER SLIDE CRACK. REMOVED AND REPLACED PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,927 hrs · 31,101 cycles

LEFT OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED PER AMM BATTERY PACK M1668.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,927 hrs · 31,101 cycles

RIGHT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED PER AMM BATTERY PACK M1669.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,927 hrs · 31,101 cycles

FWD LEFT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED PER AMM BATTERY PACK M1674.

Part: SLIDE — CRACKED (RT HORIZ STAB) · airframe 52,927 hrs · 31,101 cycles

RIGHT HORIZONTAL STAB FWD LOWER SLIDE CRACK. REMOVED AND REPLACED PER AMM.

Part: ESCAPE ROPE — PULLED (CABIN) · airframe 52,590 hrs · 30,917 cycles

LEFT OVERWING EMERGENCY EXIT ROPE PULLED. INSTALLED LIFELINE (ROPE) PER AMM.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 52,257 hrs · 30,715 cycles

IN FLT SHUT DOWN/DIVERSION/EMERGENCY DECLARED NR 2 ENG OIL FILTER BYPASS LIGHT IND AND VIBRATION INDICATION HIGH. REMOVED AND REPLACED NR 2 ENG PER MT.

Part: COVER — BROKEN (CABIN) · airframe 51,238 hrs · 30,071 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 50,406 hrs · 29,589 cycles

CAPTAINS NR 1 WINDOW EXTERNAL FRAME O/B POST CRACKED AT THE UPPER CORNER. REMOVED AND REPLACED FRAME PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 49,781 hrs · 29,239 cycles

RT EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,384 hrs · 29,014 cycles

DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 48,836 hrs · 28,706 cycles

DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY EXIT LIGHT FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 48,836 hrs · 28,706 cycles

DURING SCHEDULED HC1 CHECK, CENTER CABIN EMERGENCY EXIT LIGHT FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 48,836 hrs · 28,706 cycles

DURING SCHEDULED HC1 CHECK, FWD CABIN EMERGENCY EXIT LIGHT FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,794 hrs · 28,068 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT AT ROW 18. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,664 hrs · 27,986 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT AFT EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LENS — BROKEN (CABIN) · airframe 46,188 hrs · 27,135 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 45,227 hrs · 26,565 cycles

L2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW AND CONTROLLER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,155 hrs · 25,909 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 43,738 hrs · 25,660 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,738 hrs · 25,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 420, BETWEEN STR 14L TO STR 15L. REPAIRED FRAME PER AAR EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,738 hrs · 25,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT INOP AT L1 DOOR. RELAMPED PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,738 hrs · 25,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT SIDE LANDING GEAR FUSELAGE SUPPORT FRAME CORRODED AT BS 695. REPAIRED FRAME PER AAR EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,738 hrs · 25,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT SIDE LANDING GEAR FUSELAGE SUPPORT FRAME CORRODED AT BS 695. REPAIRED FRAME PER AAR EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 43,738 hrs · 25,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING NR 2 SLAT LOWER SKIN CRACKED. REPAIRED SLAT PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,738 hrs · 25,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,738 hrs · 25,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,738 hrs · 25,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR LOWER CREASE BEAM CORRODED BETWEEN BS 291 TO BS 332. REMOVED AND REPLACED BEAM PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 43,738 hrs · 25,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,738 hrs · 25,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,738 hrs · 25,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER EA.

Part: LENS — LOOSE (CABIN) · airframe 43,250 hrs · 25,370 cycles

DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT PER MM.

Part: CABLE — OUT OF POSITION (L1 DOOR) · airframe 41,259 hrs · 24,181 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER CABLE OUT OF POSITION. REPOSITIONED CABLE PER MT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,367 hrs · 21,798 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. R&R LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,366 hrs · 21,798 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,209 hrs · 21,707 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,209 hrs · 21,707 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,322 hrs · 20,560 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 35,322 hrs · 20,560 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.7. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,322 hrs · 20,560 cycles

DURING SCHEDULED HC1 CHECK, RT OVERWING EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,322 hrs · 20,560 cycles

DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 35,322 hrs · 20,560 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,006 hrs · 18,667 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 6 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 30,561 hrs · 17,859 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORR0DED AT BS 986, RBL 44. REPAIRED FLOORBEAM PER SWA EA.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,021 hrs · 17,558 cycles

DURING SCHEDULED 8Y CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLOORBEAM — CORRODED (BS 771) · airframe 30,021 hrs · 17,558 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 771, RBL 13 TO LBL 13. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 30,021 hrs · 17,558 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 44. REPAIRED FLOORBEAM PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 28,085 hrs · 16,478 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 28,085 hrs · 16,478 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 27,422 hrs · 16,095 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BRAKE ASSY — SEIZED (MLG W/W) · airframe 27,178 hrs · 15,958 cycles

AIRCRAFT DIFFICULT TO PUSH BACK, AFTER TUG DISCONNECT- AIRCRAFT WOULD NOT MOVE WITH NORMAL BREAKAWAY THRUST. FOUND NR 4 MAIN BRAKE SEIZED & DAMAGED. REMOVED AND REPLACED NR 4 MAIN BRAKE ASSY AND NR 4 MAIN TIRE/WHEEL ASSY PER MM.

Part: BATTERY PACK — INOPERATIVE (MID CABIN) · airframe 26,673 hrs · 15,669 cycles

DURING SCHEDULED RON CHECK, FOUND LT MID CABIN EMERGENCY BULLNOSE LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 25,377 hrs · 14,973 cycles

AIR TURNBACK, CABIN WOULD NOT PRESSURIZE. FOUND L1 DOOR GUIDE ARM OUT OF ADJUSTMENT. ADJUSTED GUIDE ARM PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,707 hrs · 14,016 cycles

DURING SCHEDULED MV3 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 9 ABC INOP. RELAMPED PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,811 hrs · 12,436 cycles

DURING SCHEDULED SPV, FOUND L1 DOOR AND RT BULLNOSE AT ROW 1 TO ROW 4, EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 19,834 hrs · 11,871 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 19,321 hrs · 11,591 cycles

DURING SCHEDULED PM CHECK, FOUND AFT CABIN EEPLS EXTINGUISHED AFTER SEVERAL SECONDS. REMOVED AND REPLACED AFT CABIN EEPLS BATTERY PER MM.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 17,991 hrs · 10,895 cycles

DIVERSION, HYDRAULIC A-SYS FLUID QTY LOSS NR HYD A-SYS MODULE AND ACOUSTIC FILTER. REMOVED AND REPLACED HYD LINE PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 16,672 hrs · 10,158 cycles

DURING SCHEDULED 5Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 16,299 hrs · 9,959 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 15,319 hrs · 9,448 cycles

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

Part: TAB — WORN (RT ELEVATOR) · airframe 15,195 hrs · 9,381 cycles

DURING SCHEDULED C3 CHECK, SWA SI 11075-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHINGS ON RT TAB MAST ROD ENDS AND REMOVED AND REPLACED HARDWARE AND BUSHINGS IN NR 1 TAB HINGE ATTACH FITTING PER MM.

Part: TAB — WORN (RT ELEVATOR) · airframe 13,077 hrs · 8,218 cycles

DURING SCHEDULED RON, SWA SI 11052-55, FOUND RT ELEVATOR TAB BOLT AND BUSHINGS WORN ON CONTROL ROD FITTINGS. REMOVED AND REPLACEDELEVATOR TAB PER MM.

Part: COVER — CRACKED (CABIN) · airframe 13,012 hrs · 8,175 cycles

DURING SCHEDULED CHECK, FOUND EEPLS COVERS CRACKED AT ROWS 2, 3, 17, 7, 16, 18, 20, 21, 22 AND 13. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: LIGHT — LOOSE (AFT CABIN) · airframe 12,904 hrs · 8,118 cycles

AFT GALLEY EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT ASSY PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 11,146 hrs · 7,086 cycles

OVERHEAD EMERGENCY EXIT SIGN NOT SECURE AT AFT CABIN. SECURED EXIT SIGN PER MM.

Part: COVER — LOOSE (CABIN) · airframe 10,403 hrs · 6,657 cycles

EEPLS TRACK COVER LOOSE AT FWD SECTION. R&R TRACK COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 10,392 hrs · 6,652 cycles

EEPLS LOOSE AT FWD SECTION. SECURED EEPLS PER MM.

Part: REGULATOR — INOPERATIVE (NR 1 ENGINE) · airframe 9,855 hrs · 6,345 cycles

AIR TURNBACK. AFTER TAKEOFF, NR 1 ENG PNEUMATIC BLEED C/B TRIPPED. WOULD NOT RESET ON FIRST ATTEMPT AND BLEED AIR PRESS NOT STABLE. REMOVED AND REPLACED NR 1 PNEUMATIC HIGH STAGE REGULATOR PER MM.

Part: COVER — CRACKED (CABIN FLOOR) · airframe 9,519 hrs · 6,124 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT ROWS 1 & 8. REMOVED AND REPLACED TRACK COVERS PER MM.

Part: RETAINER — LOOSE (GIRT BAR) · airframe 9,519 hrs · 6,124 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT RETAINER HOOKS HAVE LOOSE RIVETS. SECURED GIRT RETAINER PER MM.

Part: CONNECTOR — LOOSE (VHF CONTL PANEL)

EN ROUTE LOST ALL TRANSMIT FUNCTIONS FROM THE CAPT AUDIO PANEL, IE NR 1 AND NR 2 COMM, SERVICE AND FLT INTERPHONE AND O2 MASK. AUDIO ON CAPT AND F/O PANEL WOULD CUT OUT OR FADE OUT. AIRCRAFT DIVERTED TO ABQ AND MADE AN UNEVENTFUL LANDING. SWAPPED VHF CONTROL PANELS CAPT AND F/O. VERIFIED CANNON PLUG CONNECTIONS. OPS CHECK OK PER BOEING M/M.

Part: LAVATORY — CLOGGED (CABIN)

ABOUT 40 TO 50 MINUTES INTO FLIGHT, F/A NOTED AFT LAV WAS NOT FLUSHING AND BOWL WAS FILLING UP. FWD LAVATORY WAS ALREADY DEFERRED AND ON MEL. AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING. FOUND AFT LAV CLOGGED. REMOVED DEBRIS AND SERVICED PER BOEING M/M. FWD LAV STILL ON MEL.