N313AW

Part: NUT PLATE — STRIPPED (ENTRY DOOR)

ONT - MAINTENANCE FOUND THE FORWARD ENTRY DOOR ESCAPE SLIDE ASSEMBLY FORWARD UPPER BOLT NOT ENGAGING. ESCAPE SLIDE IS NOT SECURE TO THE DOOR FRAME. MAINTENANCE REMOVED AND REPLACED THE NUT PLATE IN ASSOCIATION WITH SRM 51-40-02 AND INSTALLED BOLT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - CRACK ON FUSELAGE FRAME AT BS 344, S7R ABOVE L-1 DOOR CUTOUT. REPAIRED FUSELAGE FRAME AT BS 344, S7R ABOVE L-1 DOOR CUTOUT IAW B737 SRM 53-00-07.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - FUSELAGE FRAME CRACKED AT BS787, S9L. REPAIRED FUSELAGE FRAME AT BS787, S9L IAW JOB CARD M1C53002.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - CRACKED STRINGER CLIP AT BS 887, S9L. REPLACED STRINGER CLIP AT BS 887, S9L IAW B737 SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - CRACKED STRINGER CLIP AT BS 787, S9L. REPLACED STRINGER CLIP AT BS787, S9L IAW B737 SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - CRACKS ON FUSELAGE SKIN BETWEEN BS 698 TO BS 700, S4R. REPAIRED FUSELAGE SKIN BETWEEN BS 698 TO BS 700, S4R IAW B737 SRM 53-00-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - CRACK ON FUSELAGE FRAME AT BS847, S9L. REPAIRED CRACK ON FUSELAGE FRAME AT BS 847, S9L IAW JOB CARD M1C53002.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - FUSELAGE FRAME CRACKED AT BS 867, S9R. REPAIRED FUSELAGE FRAME AT BS 867, S9R IAW JOB CARD M1C53002.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - CRACKED TIE CLIP AT BS 727D, S4L. REPLACED TIE CLIP AT BS 727D, S4L IAW B737 SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - FUSELAGE FRAME CRACKED AT BS 440, S9L. REPAIRED FUSELAGE FRAME AT BS 440, S9L IAW JOB CARD M1C53002.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - CRACK ON FUSELAGE FRAME AT BS 867, S9L. REPAIRED FUSELAGE FRAME AT BS 867, S9L IAW JOB CARD M1C53002.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - FUSELAGE FRAME CRACKED AT BS 887, S9R. REPAIRED FUSELAGE FRAME AT BS 887, S9R IAW JOB CARD M1C53002.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - FUSELAGE FRAME CRACKED AT BS 807, S9L. REPAIRED FUSELAGE FRAME AT BS 807, S9L IAW JOB CARD M1C53002.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - CABIN FUSELAGE FRAME CRACKED AT BS 480, S9L. REPAIRED FUSELAGE FRAME AT BS 480, S9L IAW JOB CARD M1C53002.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - FUSELAGE FRAME CRACKED AT BS 400, S9L. REPAIRED FUSELAGE FRAME AT BS 400, S9L IAW JOB CARD M1C53002.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - FUSELAGE FRAME CRACKED AT BS 827, S9L. REPAIRED FUSELAGE FRAME AT BS 827, S9L IAW JOB CARD M1C53002.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - FUSELAGE FRAME CRACKED AT BS 480, S9R. REPAIRED FUSELAGE FRAME AT BS 480, S9R IAW JOB CARD M1C53002.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - FUSELAGE FRAME CRACKED AT BS 787, S9R. REPAIRED FUSELAGE FRAME AT BS 787, S9R IAW JOB CARD M1C53002.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - FUSELAGE FRAME CRACKED AT BS 727A, S9L. REPAIRED FUSELAGE FRAME CRACKED AT BS 727A, S9L IAW JOB CARD M1C53002.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - CRACKED TIE CLIP AT BS 727D, S6L. REPLACED TIE CLIP AT BS 727D, S6L IAW B737 SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - FUSELAGE FRAME CRACKED AT BS 727E, S9L. REPAIRED FUSELAGE FRAME AT BS 727E, S9L IAW JOB CARD M1C53002.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - FUSELAGE FRAME CRACKED AT BS 887, S9L. REPAIRED FUSELAGE FRAME CRACKED AT BS 887, S9L IAW JOB CARD M1C53002.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - CORROSION ON SHEAR WEB AT BS 380, LBL 65. REPAIRED SHEAR WEB AT BS 380, LBL 65 IAW B737 SRM 51-70-13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - CRACKS ON FUSELAGE FRAME AT BS 847 BETWEEN S15R TO S27R. REPLACED FUSELAGE FRAME AT BS 847 BETWEEN S15R TO S27R IAW B737 SRM 51-40-02.

Part: SKIN — CORRODED (NACELLE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - THREE BULGES IN LEFT UPPER PYLON SKIN ALONG CENTER SEAM AT NAC STA 204 TO NAC STA 248 & BETWEEN BL2R TO BL2L. REPAIRED LEFT UPPER PYLON SKIN ALONG CENTER SEAM AT NAC STA204 TO NAC STA 248 & BETWEEN BL2R TO BL2L IAW EA 130422.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - CRACK IN FUSELAGE FRAME WEB AT BS 303.9, BETWEEN S15L TO S17L FWD LT DOOR. REPAIRED FUSELAGE FRAME WEB AT BS 303.9, BETWEEN S15L TO S17L IAW ENGINEERING JOB CARD M1L53001.

Part: SKIN — CORRODED (NACELLE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - THREE BULGES IN LEFT UPPER PYLON SKIN ALONG CENTER SEAM AT NAC STA 204 TO NAC STA 248 & BETWEEN BL2R TO BL2L. REPAIRED LEFT UPPER PYLON SKIN ALONG CENTER SEAM AT NAC STA 204 TO NAC STA 248 & BETWEEN BL2R TO BL2L IAW EA 130422.

Part: SKIN — CRACKED (LE SLAT) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - CRACK ALONG BOTTOM OF NR 6 SLAT LOWER SURFACE BETWEEN SLAT STA 314.03 TO 317.03. REPAIRED NR 6 SLAT LOWER SURFACE BETWEEN SLAT STA 314.03 TO 317.03 IAW B737 SRM 57-43-01.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 71,454 hrs · 44,243 cycles

MCN - C22 - MAJOR REPAIR - CRACK ON FUSELAGE SKIN PANEL AT BS 303.9 BETWEEN S6L TO S15L. REPAIRED FUSELAGE SKIN PANEL AT BS 303.9 BETWEEN S6L TO S15L IAW EA 130418.

Part: LIGHT — MALFUNCTIONED (CABIN)

DFW - PILOT REPORTED THAT EN ROUTE FROM LAS TO DFW, PILOT REPORTED ALL THE INTERIOR EMERGENCY EXIT LIGHTS FAILED. CIRCUIT BREAKER WAS CHECKED AND FOUND NOT POPPED. MAINTENANCE PERFORMED EMERGENCY LIGHTS FUNCTIONAL TEST PER MM 31-51-03. CHECKS GOOD.

Part: SKIN — DEBONDED (FOREFLAP) · airframe 33,504 hrs · 20,476 cycles

PHX - MAJOR REPAIR - B CHECK - LEFT WING INBOARD FOREFLAP UPPER SURFACE DISBONDED AT WBL 117. REPLACED THE LEFT WING INBOARD FORE FLAP IAW TASK CARD R3M27008.

Part: SKIN — CRACKED (ZONE 100) · airframe 70,530 hrs · 43,684 cycles

MAJOR REPAIR - FUSELAGE SKIN CRACKED AT BS 880, S24R & BS883, S23R. REPAIRED FUSELAGE SKIN AT BS 880, S24R & BS 883, S23R IAW SRM 53-00-01 REPAIR 31.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 70,530 hrs · 43,684 cycles

PHX - MAJOR REPAIR - RON - CORROSION ON STRINGER SPLICE AT BS 908, S25R. REPLACED STRINGER SPLICE AT BS 908, S25R IAW B737 SRM 51-30-02.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - NR 6202181 - CRACK ON WEB BETWEEN BS294.5 TO BS312, S4L. REPLACED WEB BETWEEN BS294.5 TO BS312, S4L IAW B737 SRM 51-10-02 & BOEING DRAWING 50-8261.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - NR 6201060 - GALVANIC CORROSION ON FLOORBEAM BETWEEN BS986 TO BS1006, LBL16. REPLACED FLOORBEAM BETWEEN BS986 TO BS1006, LBL16 IAW B737 SRM 51-10-02.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - NR 6202161 - DELAMINATION NR 5 SLAT SKIN UPPER SURFACE BETWEEN SLAT STA 170.40 TO STA172.40. REPAIRED NR 5 SLAT SKIN UPPER SURFACE BETWEEN SLAT STA 170.40 TO STA172.40 IAW B737 SRM 51-70-10.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - CORROSION ON PRESSURE BULKHEAD DOME WEB INTERNAL SKIN BETWEEN BS 1016 TO BS 1028 & BETWEEN S27L TO S27R. REPAIRED PRESSURE BULKHEAD DOME WEB INTERNAL SKIN BETWEEN BS 1016 TO BS 1028 & BETWEEN S27L TO S27R IAW US AIRWAYS EA 132443.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - NR 6201352 - CRACK ON FLOOR WEB BETWEEN BS312 TO BS328, RBL31. REPAIRED FLOOR WEB BETWEEN BS312 TO BS328, RBL31 IAW B737 SRM 51-70-11.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,436 hrs · 23,712 cycles

SAL - C21 - MAJOR REPAIR - NR 6201732 - TIE CLIP CRACKED AT BS663.75, S9L. REPLACED TIE CLIP AT BS663.75, S9L IAW B737 SRM 51-10-02.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,436 hrs · 23,712 cycles

SAL - C21 - MAJOR REPAIR - NR 6201734 - TIE CLIP CRACKED AT BS597, S9R. REPLACED TIE CLIP AT BS597, S9R IAW B737 SRM 51-10-02.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - NR 6201746 - CRACK ON SUPPORT ANGLE AT BS952.5, S7L. REPLACED SUPPORT ANGLE AT BS952.5, S7L IAW B737 SRM 51-10-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - NR 6201747 - GALVANIC CORROSION ON FLOOR BEAM AT BS986.5, RBL39. REPAIRED FLOORBEAM AT BS986.5, RBL39 IAW B737 SRM 53-00-51.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - NR 6201726 - CRACK ON STRINGER TIE CLIP AT BS706, S10L. REPLACED STRINGER TIE CLIP AT BS706, S10L IAW B737 SRM 51-10-02.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - CRACK ON TIE CLIP AT BS 616, S3R. REPLACED TIE CLIP AT BS 616, S3R IAW B737 SRM 51-10-02-0G.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - CRACK ON TIE CLIP AT BS 639, S2L. REPLACED TIE CLIP AT BS 639, S2L IAW B737 SRM 51-10-02-0G.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - NR 6201742 - CRACK ON STRINGER BETWEEN BS489 TO BS500D, S16L. REPAIRED STRINGER BETWEEN BS489 TO BS500D, S16L IAW B737 SRM 53-00-03.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - CRACK ON TIE CLIP AT BS 639, S1R. REPLACED TIE CLIP AT BS 639, S1R IAW B737 SRM 51-10-02-0G.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,436 hrs · 23,712 cycles

SAL - C21 - MAJOR REPAIR - NR 6201733 - TIE CLIP CRACKED AT BS706, S9L. REPLACED TIE CLIP AT BS706, S9L IAW B737 SRM 51-10-02.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,436 hrs · 23,712 cycles

SAL - C21 - MAJOR REPAIR - CRACK ON TIE CLIP AT BS 639, S3R. REPLACED TIE CLIP AT BS 639, S3R IAW B737 SRM 51-10-02-0G.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - GALVANIC CORROSION ON STIFFENER CHANNEL ON BS 1016 PRESSURE BULKHEAD AT S27L. REPLACED STIFFENER CHANNEL ON BS 1016 PRESSURE BULKHEAD AT S27L IAW B737 SRM 51-10-02.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,436 hrs · 23,712 cycles

SAL - C21 - MAJOR REPAIR - NR 6201735 - TIE CLIP CRACKED AT BS727B, S7R. REPLACED TIE CLIP AT BS727B, S7R IAW B737 SRM 51-10-02.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,436 hrs · 23,712 cycles

SAL - C21 - MAJOR REPAIR - NR 6201739 - TIE CLIP CRACKED AT BS597, S7L. REPLACED TIE CLIP AT BS597, S7L IAW B737 SRM 51-10-02.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,436 hrs · 23,712 cycles

SAL - C21 - MAJOR REPAIR - NR 6201727 - TIE CLIP CRACKED AT BS578, S9R. REPLACED TIE CLIP AT BS578, S9R IAW B737 SRM 51-10-02.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - NR 6201731 - CRACK ON TIE CLIP AT BS616, S5L. REPLACED TIE CLIP AT BS616, S5L IAW B737 SRM 51-10-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - NR 6200880 - CORROSION ON SEAT TRACK AT BS 445, RBL 24.75. REPAIRED SEAT TRACK AT BS 445, RBL 24.75 IAW B737 SRM 53-00-52.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - NR 6201854 - CORROSION ON TIE CLIP AT BS847, S25R. REPLACED TIE CLIP AT BS847, S25R IAW B737 SRM 51-10-02 & BOEING DRAWING 65-46554.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - NR 6201068 - GALVANIC CORROSION ON INNER CHORD OF R-2 DOOR SUPPORT ANGLE LOWER SILL AREA BETWEEN BS947 TO BS990, S17R. REPLACED R-2 DOOR SUPPORT ANGLE LOWER SILL AREA BETWEEN BS947 TO BS990, S17R IAW B737 SRM 51-10-02.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - NR 6201832 - CRACK ON AFT PRESSURE BULKHEAD WEB AT BS1016 BETWEEN S5R TO S7R. REPAIRED AFT PRESSURE BULKHEAD WEB AT BS1016 BETWEEN S5R TO S7R IAW B737 SRM 53-80-08.

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - NR 6201083 - GALVANIC CORROSION ON AFT FACE OF FUSELAGE FRAME AT BS727C BETWEEN S26L TO S27L. REPAIRED AFT FACE OF FUSELAGE FRAME AT BS727C BETWEEN S26L TO S27L IAW B737 SRM 53-00-07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - NR 6201066 - GALVANIC CORROSION ON SEAT TRACK BETWEEN BS1006 TO BS1016, RBL38. REPLACED SEAT TRACK BETWEEN BS1006 TO BS1016, RBL38 IAW B737 SRM 51-10-02.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - NR 6201057 - GALVANIC CORROSION ON INNER CHORD OF L2 DOOR SUPPORT ANGLE LOWER SILL AREA BETWEEN BS947 TO BS1006, LBL52. REPLACED L2 DOOR SUPPORT ANGLE LOWER SILL AREA BETWEEN BS947 TO BS1006, LBL52 IAW B737 SRM 51-10-02.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - GALVANIC CORROSION ON SHEAR WEB BETWEEN BS 1016 TO BS 1030. REPLACED SHEAR WEB BETWEEN BS 1016 TO BS 1030 IAW B737 SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - GALVANIC CORROSION ON STRINGER BETWEEN BS 967 TO BS 972, S27R. REPLACED STRINGER BETWEEN BS 967 TO BS 972, S27R IAW B737 SRM 53-00-03.

Part: WEB — CORRODED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - NR 6201100 - CORROSION ON WEB UPPER FLANGE BETWEEN BS767 TO BS793.5 ABOVE S25R. REPLACED WEB BETWEEN BS767 TO BS793.5 ABOVE S25R IAW B737 SRM 51-10-02.

Part: STRAP — CORRODED (FUSELAGE) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - NR 6201062 & 6201065 - CORROSION ON STRAP BETWEEN BS 1006 TO BS 1029, RBL 4 & AT LBL 4. REPLACED STRAP BETWEEN BS 1006 TO BS 1029, RBL 4 & AT LBL 4 IAW B737 SRM 51-10-02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 59,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - GALVANIC CORROSION ON UPPER FLANGE OF FUSELAGE FRAME AT BS 793.5 BETWEEN S25R TO S26R. REPLACED FUSELAGE FRAME AT BS 793.5 BETWEEN S16R TO S27R IAW B737 SRM 51-10-02.

Part: FLAP — DELAMINATED (LT WING) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - NR 6202093 - DELAMINATION ON LEFT HAND WING OUTBOARD AFT FLAP INBOARD EDGE LOWER CORNER. REPAIRED LEFT HAND WING OUTBOARD AFT FLAP INBOARD EDGE LOWER CORNER IAW B737 SRM 51-70-10.

Part: SKIN — DELAMINATED (SPOILER) · airframe 69,436 hrs · 43,048 cycles

SAL - C21 - MAJOR REPAIR - NR 6176058 - DELAMINATION NR 9 SPOILER UPPER SURFACE, 43 INCHES FROM INBOARD END & 16.5 INCHES FROM AFT EDGE. REPAIRED NR 9 SPOILER UPPER SURFACE IAW B737 SRM 51-70-10.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,194 hrs · 42,349 cycles

PHX RON MAJOR REPAIR LOG NR 4458497 FUSELAGE SKIN CRACK AT BS727D, S23L AT AFT EDGE OF EXISTING REPAIR. REPAIRED FUSELAGE SKIN AT BS727D, S23L IAW B737 SRM 53-00-01-2R-31.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

F/A REPORTED THE EMERGENCY FLASHLIGHT CHARGING INDICATOR INOPERATIVE. MAINT REMOVED AND REPLACED THE BATTERY. OPS CHECK NORMAL. (K)

Part: SPOILER — DELAMINATED (NR 7) · airframe 67,889 hrs · 42,163 cycles

PHX - MAJOR REPAIR, NR 7 SPOILER IS DELAMINATED IN 2 SPOTS. REPLACED NR 7 SPOILER IAW B737 MM 27-61-11.

Part: SKIN — CRACKED (ZONE 100) · airframe 67,666 hrs · 42,021 cycles

PHX- DAILY -MAJOR REPAIR- FUSELAGE SKIN CRACKED AT BS 747, S23L. REPAIRED FUSELAGE SKIN AT BS747 S23L IAW B737 SRM TEMPORARY REVISION 53-33 REPAIR 31. (S)

Part: SKIN — CRACKED (ZONE 100) · airframe 67,666 hrs · 42,021 cycles

PHX- DAILY -MAJOR REPAIR- FUSELAGE SKIN CRACKED AT BS 727E S22R. REPAIRED FUSELAGE SKIN AT BS 727E S22R IAW B737 SRM TEMPORARY REVISION 53-33 REPAIR 31. (S)

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 67,274 hrs · 41,787 cycles

FLT 282 - CREW REPORTED FWD F/A FLASHLIGHT INOP. MX REPLACED FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD. (S)

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 66,639 hrs · 41,380 cycles

FLT 586 - PHX - CREW REPORTED FWD FLASHLIGHT INOP. MX REPLACED THE FWD FLASHLIGHT. OPERATIONAL CHECK WAS GOOD.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - VERTICAL STABILIZER LEADING EDGE RIB IS CRACKED, STABILIZER STATION 86.12. REPAIRED VERTICAL STABILIZER LEADING EDGE RIB, STABILIZER STATION 86.12 IAW USAIRWAYS EA 100232.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - CRACKED FUSELAGE SKIN, BS 312, S10L - S11L. REPAIRED FUSELAGE SKIN, BS 312, S10L - S11L CRACKED FUSELAGE SKIN, BS 312, S10L - S11L.

Part: WEB — CRACKED (L1 DOOR) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - CRACKED L1 DOOR INNER WEB SKIN PREVIOUS REPAIR, BS 319, S9L - S10L. REPAIRED L1 DOOR INNER WEB SKIN, BS 319, S9L - S10L IAW B737 SRM 51-70-13.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - NR 6033495, RIGHT ELEVATOR UPPER SURFACE HAS AREA OF DELAMINATION, ELEVATOR STATION 84.9 - 93.9. REPAIRED RIGHT ELEVATOR UPPER SURFACE, ELEVATOR STATION 84.9 - 93.9 IAW B737 SRM 51-70-04.

Part: SKIN — DELAMINATED (NR 7 SPOILER) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - NR 6033563, RIGHT WING NR 7 SPOILER HAS 2 AREAS OF DELAMINATION, WBL 356 - WBL 358 AND WBL 378 - WBL 387. REPAIRED RIGHT WING NR 7 SPOILER IAW B737 SRM 51-70-10-2R3.

Part: RIB — CRACKED (HORIZ STAB) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - LEFT HORIZONTAL STABILIZER LEADING EDGE RIB WEB CRACKED, STABILIZER STATION 83. REPAIRED LEFT HORIZONTAL STABILIZER LEADING EDGE RIB WEB, STABILIZER STATION 83 - 86.66 IAW USAIRWAYS EA 100234.

Part: WEDGE — DEBONDED (L/E SLAT) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - RIGHT WING NR 5 SLAT TRAILING EDGE WEDGE HAS AREA OF DISBOND, SS 126.9. REPAIRED RIGHT WING NR 5 SLAT TRAILING EDGE WEDGE, SS 124.90 - SS 128.40 IAW B737 SRM 51-70-10-2R.

Part: SKIN — DELAMINATED (RUDDER) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK NR 6038691, DELAMINATION ON THE RIGHT SIDE OF RUDDER, RS 220 - RS 232. REPAIRED RIGHT SIDE OF RUDDER, RS 220 - RS 232 IAW B737 SRM 51-70-07.

Part: SUPPORT ANGLE — CRACKED (BS 335 S17-18L) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - CRACKED SUPPORT ANGLE, BS 335.5, S17L - S18L. REPLACED SUPPORT ANGLE, BS 335.5, S17L - S18L IAW B737 SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - CRACKED FUSELAGE SKIN, BS 894, S25R. REPAIRED FUSELAGE SKIN, BS 894, S25R IAW B737 SRM 53-00-01-2R 31.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - NR 6060828, RIGHT WING OUTBOARD MIDFLAP RIB CRACKED, WBL 387.06. REPLACED RIGHT WING OUTBOARD MIDFLAP RIB IAW B737 SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 663,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - CRACKED FUSELAGE SKIN, BS 390, BL 0, WL 390. REPAIRED FUSELAGE SKIN, BS 390, BL 0, WL 390 IAW USAIRWAYS EA 100191.

Part: SKIN — DEBONDED (TE FLAPS) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - NR 6033450, LEFT WING INBOARD FORE FLAP, UPPER SURFACE HAS AREA OF DEBOND, WBL 117.5 - WBL 119.5. REPAIRED LEFT WING INBOARD FORE FLAP, UPPER SURFACE IAW B737 SRM 51-70-10-2R REPAIR 3.

Part: SKIN — DELAMINATED (NR 4 SLAT) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - NR 6033405, DISBOND ON THE LEFT WING NR 4 SLAT WEDGE LOWER SURFACE, SS 91. REPAIRED LEFT WING NR 4 SLAT WEDGE LOWER SURFACE, SS 91 IAW B737 SRM 51-70-10-2R4.

Part: KEELBEAM — CORRODED (BS 500D S28L) · corrosion level 2 · airframe 66,311 hrs · 41,173 cycles

CLT - MAJOR REPAIR - C2 CHECK - NR 6033578, LEVEL 2 CORROSION ON KEEL BEAM LOWER CHORD, BS 500D, S28L. REPAIRED KEEL BEAM LOWER CHORD, BS 500D, S28L IAW B737 SRM 53-30-12.

Part: SKIN — DELAMINATED (NR 7 SPOILER) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - RIGHT WING NR 7 SPOILER UPPER SURFACE HAS DELAMINATION. REPAIRED RIGHT WING NR 7 SPOILER UPPER SURFACE IAW B737 SRM 51-70-10-2R REPAIR 4.

Part: STRINGER — CORRODED (BS 1120-1126) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - NR 6034177, CORROSION ON APU CUT OUT TORQUE BOX STRINGER, BS 1120 - BS 1126, S18R. REPLACED APU CUT OUT TORQUE BOX STRINGER, BS 1120 - BS 1126, S18R IAW B737 SRM 51-40-02.

Part: STIFFENER — CORRODED (TORQUE BOX) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - NR 6028278, CORROSION ON APU CUT OUT TORQUE BOX STIFFENER, BS 1116, S18R. REPLACED APU CUT OUT TORQUE BOX STIFFENER, BS 1116, S18R IAW B737 SRM 51-40-02.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - CRACKED FORWARD CARGO DOOR SURROUND LOWER AFT CORNER BEAR STRAP, BS 492, S25R. REPAIRED FORWARD CARGO DOOR SURROUND LOWER AFT CORNER BEAR STRAP, BS 492, S25R IAW B737 SRM 53-00-01-2R32.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - CRACKED SKIN, BS 454, BL 0 - LBL 2, WL 148. REPAIRED SKIN, BS 454, BL 0 - LBL 2, WL 148 IAW USAIRWAYS TASK CARD M2A53002.

Part: FITTING — CRACKED (LT WING) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - LEFT WING LANDING GEAR SUPPORT FITTING CRACKED, RSS 224.14. REPLACED LEFT WING LANDING GEAR FITTING, RSS 224.14 IAW USAIRWAYS EA 100196.

Part: SKIN — CRACKED (BS 727E S25R) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - NR 6040935, CRACKED FUSELAGE SKIN, BS 727E, S25R. REPAIRED FUSELAGE SKIN, BS 727E, S25R IAW B737 SRM 53-00-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - CRACKED SKIN, BS 500D - BS 520, S12R. REPAIRED SKIN, BS 500D - BS 520, S12R IAW USAIRWAYS EO 100228.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - CRACKED NR 2 PYLON SKIN PANEL, PYLON STATION 261. REPAIRED NR 2 PYLON SKIN PANEL, PYLON STATION 261 IAW USAIRWAYS EA 100219.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,795 hrs · 40,853 cycles

PHX - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 757, S23R. REPAIRED FUSELAGE SKIN CRACK, BS 757, S23R IAW B737 SRM 53-00-01.

Part: ACTUATOR — FAILED (RT MLG) · airframe 64,966 hrs · 40,298 cycles

MKE - PHX - EL - LOG# 7746754 - CREW SELECTED GEAR DOWN, RIGHT MAIN RED LANDING GEAR LIGHT REMAINED ILLUMINATED, GREEN LIGHT ON NOSE AND LEFT MAIN. TOWER CONFIRMED RIGHT GEAR WAS UP. THE CREW DECLARED AN EMERGENCY AND PERFORMED GEAR LIGHT DISAGREEMENT CHECKLIST. CREW PERFORMED MANUAL GEAR EXTENSION, 3 GREEN LIGHTS. THE CABIN WAS PREPARED FOR AN EMERGENCY LANDING. THE LANDING WAS UNEVENTFUL. THE A/C TAXIED TO THE GATE. MX PERFORMED GEAR SWING OF RIGHT MLG. MX FOUND GEAR WOULD NOT DROP WHEN SELECTING GEAR HANDLE FROM OFF TO DOWN. OPS NORMAL WHEN GEAR HANDLE MOVED FROM UP DIRECTLY TO DOWN. MX REMOVED AND REPLACED RT MLG UP LOCK ACTUATOR, RT TRANSFER CYLINDER AND RT MLG MODULAR PACKAGE IAW REF R4M32010, M

Part: SKIN — CRACKED (ZONE 100) · airframe 64,910 hrs · 40,266 cycles

CRACKED FUSELAGE SKIN, BS 727D, S23R. REPAIRED FUSELAGE SKIN, BS 727D, S23R IAW USAIRWAYS EA 120072.

Part: WIRE — BROKEN (DOOR SENSOR) · airframe 64,838 hrs · 40,216 cycles

PHX - DFW - EL - CREW REPORTED DURING CLIMB, WERE NOT ABLE TO PRESSURIZE THE A/C. CREW DECLARED AN EMERGENCY AND RETURNED TO PHX. MX FOUND BROKEN WIRE ON E/E DOOR SENSOR SWITCH S197. MX REPAIRED WIRE IAW MM CH 20. EQUIPMENT DOOR LIGHT AND WARNING OPERATIONAL CHECKS WERE GOOD. THE A/C WAS RETURNED TO SERVICE.

Part: UPLOCK SENSOR — FAILED (RT MLG) · airframe 64,813 hrs · 40,197 cycles

PHX - PVR - EL - CREW REPORTED AFTER T/O, GEAR HANDLE RAISED UP. ALL GEAR LIGHTS EXTINGUISHED EXCEPT RIGHT GEAR LIGHT. RT GEAR RED LT REMAINED ILLUMINATE. ACCOMPLISHED GEAR LIGHT DISAGREEMENT CHECKLIST GOT 3 GREEN, NO RED LIGHTS. CREW DECLARED AN EMERGENCY AND RETURNED TO PHX. THE LANDING WAS UNEVENTFUL. THE CREW TAXIED TO THE GATE. MX REPLACED UPLOCK SENSOR S74 IAW M/M 32-61-21-4 AND CK'D SENSOR CLEARANCE PER 32-61-21-5. (.189 INCH). MX PERFORMED L/GEAR POSITION INDICATING AND WARNING SYSTEM TEST IAW 32-61-00-5. OPS CHECK WAS GOOD. THE A/C WAS RETURNED TO SERVICE.

Part: ACTUATOR — FAILED (RT MLG) · airframe 64,727 hrs · 40,137 cycles

PHX- RETF - CREW REPORTED DURING CLIMB, RAISING THE GEAR CREW RECEIVED A RIGHT GEAR UNSAFE INDICATION CREW DECLARED AN EMERGENCY, BURNED OFF FUEL AND RETURNED TO PHX. THE LANDING WAS UNEVENTFUL. FUP 9809870 WAS ISSUED TO REPLACE CARD M986. MX REPLACED CARD M986. OPERATIONAL CHECK WAS GOOD. WITH THE LANDING GEAR LEVER IN THE "OFF" POSITION THE RIGHT MAIN LANDING GEAR RED AND GREEN LIGHTS ILLUMINATED. DUE TO HISTORY, ENGINEERING REQUESTED MX REPLACE THE RIGHT MLG UPLOCK ACTUATOR AND THE RIGHT MLG MODULE VALVE ASSEMBLY. MX REPLACED THE COMPONENTS. CREW PERFORMED A FUNCTIONAL CHECK FLIGHT. OPERATIONAL CHECK WAS GOOD. THE A/C WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (BS 727D S23R) · airframe 63,113 hrs · 39,159 cycles

MCN - MAJOR REPAIR - FUSELAGE SKIN CRACKED, BS 727D + 3", S23L. REPAIRED FUSELAGE SKIN, BS 727D + 3", S23L IAW AWA ER 03-5300-06297-SS2.

Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 63,113 hrs · 39,159 cycles

C-19 CHECK - NR 5928339, STRINGER TIE CLIP CRACKED, BS 727D, S22L. REPLACED STRINGER TIE CLIP, BS 727D, S22L IAW SRM 51-40-02, FIGURES 8 AND 12.

Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 63,113 hrs · 39,159 cycles

C-19 CHECK - NR 5928341, STRINGER TIE CLIP CRACKED, BS 727D, S24L. REPLACED STRINGER TIE CLIP, BS 727D, S24L IAW SRM 51-40-02, FIGURES 8 AND 12.

Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 63,113 hrs · 39,159 cycles

C-19 CHECK - NR 5928340, STRINGER TIE CLIP CRACKED, BS 727D, S23L. REPLACED STRINGER TIE CLIP, BS 727D, S23L IAW SRM 51-40-02, FIGURES 8 AND 12.

Part: CONNECTOR — BROKEN (EMERGENCY LGIHTS) · airframe 63,113 hrs · 39,159 cycles

MCN - EEL - EMERGENCY ESCAPE PATH LEFT HARNESS HAS NUMEROUS CONNECTORS DAMAGED AND MISSING PINS. REPLACED CONNECTORS AND INSTALLED PINS ON THE LEFT EMERGENCY ESCAPE PATH HARNESS IAW BSWPM 20-42-01, 20-30-12 AND 20-90-14.

Part: FLOORBEAM — CRACKED (BS 663-677) · airframe 63,113 hrs · 39,159 cycles

MCN - MAJOR REPAIR - MAIN CABIN LONGITUDINAL FLOORBEAM UPPER TEE CRACKED, BS 663, BS 666.5, BS 670.5 AND BS 677, LBL 24.5, WL 208.1. REPAIRED MAIN CABIN LONGITUDINAL FLOORBEAM UPPER TEE, BS 663, BS 666.5, BS 670.5 AND BS 677, LBL 24.5, WL 208.1 IAW AWA ER 03-5702-06291-SS1.

Part: SKIN — CRACKED (NR 4 SLAT) · airframe 63,113 hrs · 39,159 cycles

MCM - THREE CRACKS, BOTTOM NR 4 SLAT SKIN, SLAT STA 71.4 TO 74. REPAIRED BOTTOM OF NR 4 SLAT SKIN STA 71.4 TO 74 IAW B737-300 SRM 57-43-01-2R6 FIG 201.

Part: ANGLE — CRACKED (BS 500D-520) · airframe 63,113 hrs · 39,159 cycles

CRACKED FLOOR STABILIZER UPPER ATTACH ANGLE, BS 500D- BS 520, BL 0. REPLACED FLOOR STABILIZER UPPER ATTACH ANGLE, BS 500D - BS 520, BL 0 IAW SRM 51-40-02-0G FIG 8 AND 51-40-02, FIGS 12 AND 14.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,113 hrs · 39,159 cycles

CRACK AT LT CREASE BEAM SHEAR WEB, BS 617.5, LBL 64.53, WL 208.1. REPLACED LT CREASE BEAM SHEAR WEB, BS 617.5, LBL 64.53, WL 208.1 IAW SRM 51-40-02-0G PAR 4 PG 1 AND 2 FIGURES 3, 6, 7 AND 8 AND DWG 65-47973 SHEETS 6 AND 57.

Part: CREASE BEAM — CRACKED (BS 617) · airframe 63,113 hrs · 39,159 cycles

MCN - MAJOR REPAIR - LEFT CREASE BEAM CRACKED, BS 617.5, LBL 64.53, WL 208.1. REPAIRED LEFT CREASEBEAM, BS 617.5, LBL 64.53, WL 208.1 IAW AWA ER 03-5361-06297-SS1.

Part: FLOORBEAM — CRACKED (BS 683) · airframe 63,113 hrs · 39,159 cycles

MCN - MAJOR REPAIR - C-19 CHECK - FOUND CLIP CRACKED, OUTBOARD SIDE OF FLOORBEAM, BS 683.25, LBL 0.07, WL 208.1. REPLACED CLIP, OUTBOARD SIDE OF FLOORBEAM, BS 683.25, LBL 0.07, WL 208.1 IAW AWA ER 03-5360-06296-SS2.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,113 hrs · 39,159 cycles

CORROSION ON AFT CARGO COMPARTMENT FRAME, BS 827 BETWEEN LBL 3.00 AND RBL 3.00. REPAIRED AFT CARGO COMPARTMENT FRAME, BS 827 BETWEEN LBL 3.00 AND RBL 3.00 IAW SRM 53-00-07-2R 5 FIG 201.

Part: FRAME — CRACKED (BS 492 S24R) · airframe 63,113 hrs · 39,159 cycles

MCN - MAJOR REPAIR - FORWARD CARGO COMPARTMENT DOOR OPENING AFT FRAME WEB CRACKED, BS 492.3, S24R. REPAIRED FORWARD CARGO COMPARTMENT DOOR OPENING AFT FRAME WEB, BS 492.3, S24R IAW AWA ER 03-5332-06293-ES3.

Part: SKIN — DEBONDED (STABILIZER) · airframe 63,113 hrs · 39,159 cycles

MCN - MAJOR REPAIR - LEFT HORIZONTAL STABILIZER O/B TRAILING EDGE DISBONDED FROM TIP FAIRING TO O/B END OF ELEVATOR, STAB STATION 295.10 - 149.12. REPAIRED LEFT HORIZONTAL STABILIZER O/B TRAILING EDGE DISBONDED FROM TIP FAIRING TO O/B END OF ELEVATOR, STAB STATION 295.10 - 149.12 IAW BOEING DRAWING 65C25162.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 63,113 hrs · 39,159 cycles

MCN - MAJOR REPAIR - C-19 CHECK - RIGHT ELEVATOR UPPER SURFACE DELAMINATED, 32 INCHES FROM OUTBOARD END, ELEVATOR STA 181. REPAIRED RIGHT ELEVATOR UPPER SURFACE 32 INCHES FROM OUTBOARD END IAW 737-300 SRM 51-70-04-0G REPAIR 1 FIGURE 10.

Part: SKIN — DEBONDED (ZONE 500 SPOILER) · airframe 63,113 hrs · 39,159 cycles

NR 4 SPOILER UPPER SURFACE HAS A DISBONDED AREA 55 INCHES FROM OB END. REPAIRED NR 4 SPOILER UPPER SURFACE IAW SRM 51-70-10-2R4, REPAIR 4, FIGURE 201.

Part: SKIN PANEL — CRACKED (BS 792 S25R) · airframe 63,113 hrs · 39,159 cycles

MCN - MAJOR REPAIR - FUSELAGE SKIN CRACKED, BS 792, S25R. REPAIRED FUSELAGE SKIN, BS 792, S25R IAW AWA ER 03-5361-06293-ES1.

Part: FRAME — CRACKED (BS 440 S24L) · airframe 63,113 hrs · 39,159 cycles

MCN - MAJOR REPAIR - FORWARD CARGO COMPARTMENT DOOR OPENING FORWARD FRAME WEB CRACKED, BS 440, S24R. REPAIRED FORWARD CARGO COMPARTMENT DOOR OPENING FORWARD FRAME WEB, BS 440, S24R IAW AWA ER 03-5332-06293-ES4.

Part: STRINGER — CRACKED (BS 727 S18AL) · airframe 63,113 hrs · 39,159 cycles

MCN - FOUND LEFT STRINGER 18A CRACKED, BS 727. REPAIRED LEFT STRINGER 18A CRACKED, BS 727 IAW ER 03-5300-06290-SS2.

Part: STRINGER — CRACKED (ZONE 100) · airframe 63,113 hrs · 39,159 cycles

C-19 CHECK - NR 5931682, RT STRINGER 18A CRACKED, BS 727 AT IB FASTENER. REPAIRED RT STRINGER 18A, BS 727 IAW AWA ER 03-5314-06287-ES1.

Part: SKIN — DEBONDED (STABILIZER) · airframe 63,113 hrs · 39,159 cycles

MCN - MAJOR REPAIR - RIGHT HORIZONTAL STABILIZER O/B TRAILING EDGE DISBONDED FROM TIP FAIRING TO O/B END OF ELEVATOR, STAB STATION 295.10 - 149.12. REPAIRED RIGHT HORIZONTAL STABILIZER O/B TRAILING EDGE DISBONDED FROM TIP FAIRING TO O/B END OF ELEVATOR, STAB STATION 295.10 - 149.12 IAW BOEING DRAWING 65C25162.

Part: SKIN — CRACKED (L1 DOOR) · airframe 63,113 hrs · 39,159 cycles

MCN - L1 DOOR INNER SKIN CRACKED AFT SIDE AT NR 6 FROM TOP STOP PIN CUTOUT. REPAIRED L1 DOOR INNER SKIN, AFT SIDE AT NR 6 FROM STOP PIN CUTOUT, IAW B737-300 SRM 51-70-13-0G, FIG 1.

Part: SENSOR — FAULTY (AIR FLOW) · airframe 62,190 hrs · 38,581 cycles

CREW REPORTED THAT DURING CRUISE EQUIPMENT COOLING EXHAUST OFF LIGHT ILLUMINATED. CREW PERFORMED QRH AND THE ALTERNATE COOLING OFF LIGHT ILLUMINATED. CREW RETURNED TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE M00100 AIR FLOW DETECT SENSOR. OPERATIONAL CHECKS WERE GOOD. NO FAULTS WERE NOTED.

Part: CONNECTOR — DISCONNECTED (MLG) · airframe 61,655 hrs · 38,271 cycles

FLT 626 - CREW DECLARED EMERGENCY INOP PHX DUE TO GEAR DOWN AND GEAR WARNING LIGHTS BEING INOPERATIVE. REPORTED THAT THE AURAL GEAR WARNING OPERATED NORMALLY. MAINTENANCE TROUBLESHOT AND FOUND CONNECTOR D4262P DISCONNECTED AT THE LANDING GEAR PANEL. MAINTENANCE RECONNECTED THE CONNECTOR, D4262P. PERFORMED MASTER WARNING AND CAUTION LIGHT TEST. OPERATIONAL WAS NORMAL IAW BOEING 737-300 MM 33-15-00-5. AURAL WARNING WAS ALSO NOTED TO OPERATE NORMALLY.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,311 hrs · 41,173 cycles

MCN - MAJOR REPAIR - C20 CHECK - CRACKED FUSELAGE SKIN, BS 870, S24R. REPAIRED FUSELAGE SKIN, BS 870, S24R IAW B737 SRM 53-00-01-2R 31.

Part: ODOR — DETECTED (CABIN) · airframe 60,712 hrs · 37,699 cycles

PHX - BURNING ODOR - FLIGHT ATTENDANTS REPORTED A RUBBER/BURNING SMELL COMING FROM ROW 10-15 AREA. MAINTENANCE INSPECTED CABIN AND FOUND NO RESIDUAL SMELLS OR ODORS.

Part: ACTUATOR — MALFUNCTIONED (RT MLG) · airframe 60,097 hrs · 37,330 cycles

AFTER TAKEOFF, DURING CLIMB, THE RT MLG WOULD NOT STOW PROPERLY. DECLARED EMERGENCY, RETURNED TO ELP & LANDED WITHOUT FURTHER INCIDENT. ACFT FERRIED BACK TO PHX WITH MLG DOWN. MX TROUBLESHOT & FOUND UPLOCK ACTUATOR NOT ENGAGING. REPLACED THE RT MLG UPLOCK ACTUATOR IAW AMWEST TASK CARD R4M32010. LEAK CHECK & OPS CHECKS GOOD. VENDOR TEAR DOWN REPORT SHOWS THAT THE UNIT DID NOT HAVE ANY INCOMING TESTS PERFORMED ON IT. VENDOR FOUND WORN HARDWARE, SCRAPER, SEALS, BACK UP RINGS, AND PACKINGS. UNIT WAS OVERHAULED IAW BOEING OHM 32-30-21 REV. 13.

Part: FRAME — CRACKED · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK, FOUND FUSELAGE FRAME CRACKED, .50 INCHES IN LENGTH, AT BS 616, BL 65R BELOW STRINGER 17, CABIN AREA. MAINTENANCE REMOVED CRACK FROM INNER CHORD FRAME AT BS 616, BL 65R BELOW STRINGER 17, CABIN AREA IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5311-01143-DD1. FABRICATED STIFFENING ANGLE AND FILLER IAW AWA ER 03-5311-01143-DD1. INSTALLED FABRICATED REPAIR PARTS IAW AWA ER 03-5311-01143-DD1.

Part: POWER UNIT — INOPERATIVE · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED AFT FLIGHT ATTENDANT SEAT FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT SEAT FLASHLIGHT POWER UNIT AS REQUIRED. OPERATIONAL CHECKS WERE GOOD.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 59,620 hrs · 37,014 cycles

MCN - DURING C18 CHECK, DISCOVERED INNER CHORD CRACKED, 1 INCH, IN CABIN AREA, BS 616, WL 208, BL 60R. MAINTENANCE CUT OUT DAMAGED SECTION OF INNER CHORD AT BS 616, WL 208, BL 60R IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ER) NUMBER 03-5361-0522-RC1. FABRICATED SPLICE CHANNEL, SPLICE STRAP AND INNER CHORD IAW AWA ER 03-5361-05221-RC1. INSTALLED FABRICATED REPAIR PARTS AT BS 616, WL 208, BL 60R IAW AWA ER 03-5361-5221-RC1.

Part: WEB — CRACKED · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED WEB CRACKED, 2.3 INCHES IN LENGTH, IN THE CABIN AREA AT BS 616, BL 60R, WL 208. MAINTENANCE REMOVED CRACKED WEB AT BS 616, BL 60R, WL 208 IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. RECEIVED NEW WEB AND PREPARED FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-02-0 FIG 1. INSTALLED REPAIR PARTS AT BS 616, BL 60R, WL 208 IAW BOEING 737-300 SRM 51-40-02-0 FIGS 8 AND 12.

Part: FITTING — CORRODED (ZONE 500 - LEFT) · corrosion level 2 · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED CORROSION ON THE LT MLG STABILIZER BEAM, AFT ATTACH FITTING. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 57-20-30-1. MAINTENANCE REMOVED AND REPLACED THE AFT ATTACH FITTING ON THE LT MLG STABILIZER BEAM IAW BOEING 737-300 AMM 57-15-00-4.

Part: FITTING — CORRODED (ZONE 600 - RIGHT) · corrosion level 2 · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED CORROSION ON THE RT MLG STABILIZER BEAM, AFT ATTACH FITTING. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 57-20-30-1. MAINTENANCE REMOVED AND REPLACED THE AFT ATTACH FITTING ON THE RT MLG STABILIZER BEAM IAW BOEING 737-300 AMM 57-15-00-4.

Part: FITTING — CORRODED (ZONE 600 - RIGHT) · corrosion level 2 · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED CORROSION ON THE RT MLG STABILIZER BEAM, FORWARD ATTACH FITTING. CORROSION WAS REMOVED IAW BOEING 737-300 SRM 51-10-02 AND FOUND TO BE OUT OF LIMITS IAW BOEING 7 37-300 SRM 57-20-90-1 FIG 102. MAINTENANCE REMOVED THE RT MLG STABILIZER BEAM, FORWARD ATTACH FITTING IAW BOEING 737-300 AMM 57-15-00-4. PREPARED NEW ATTACH FITTING FOR INSTALLATION IAW BOEING 737-300 51-40-05. INSTALLED NEW RT MLG STABILIZER BEAM, FORWARD ATTACH FITTING IAW BOEING 737-300 AMM 57-15-00-4 IAW BOEING 737-300 AMM 57-15-00-4.

Part: STRINGER — CRACKED · airframe 59,620 hrs · 38,997 cycles

DURING C18 CHECK DISCOVERED STRINGER 8L CRACKED, 1.125 INCHES IN LENGTH, AT BS 380. MAINTENANCE CUT OUT CRACK ON STRINGER 8L, BS 380, IAW BOEING 737-300 SRM 53-00-03-2 FIG 203. FABRICATED TWO ZEE ANGLES AND FILLER IAW BOEING 737-300 SRM 53-00-03-2 FIG 203. INSTALLED FABRICATED REPAIR PARTS AT STRINGER 8L, BS 380 IAW BOEING 737-300 SRM 53-00-03-2 FIG 203.

Part: BOLT — CORRODED (ZONE 500 - LEFT) · corrosion level 2 · airframe 59,620 hrs · 37,014 cycles

MCN - DURING C18 CHECK DISCOVERED CORROSION ON RETAINING BOLTS FOR THE LT INBOARD MID FLAP GIMBAL SUPPORT. NO CORROSION REMOVAL LIMITS AVAILABLE FOR RETAINING BOLTS FOR THE LT INBOARD MID FLAP GIMBAL SUPPORT. MAINTENANCE REMOVED AND REPLACED BOLTS ON THE LT INBOARD MID FLAP INBOARD GIMBAL SUPPORT IAW AMERICA WEST AIRLINES TASK CARD I3L57057. ADDITIONAL BOLT WAS FOUND WITH CORROSIN THAT SHOULD HAVE BEEN INCLUDED IN THE ORIGINAL SDR. ADDED INFORMATION TO SDR.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED STRINGER TIE CRACKED, .200 INCHES IN LENGTH, AT BS 312, STR 28R. MAINTENANCE REMOVED STRINGER TIE AT BS 312, STR 28R, IAW BOEING 737-300 SRM 51-40-02. INSTALLED NEW STRINGER TIE AT BS 312, STR 28R IAW BOEING 737-300 SRM 51-40-02-0.

Part: WEB — CRACKED (L1 DOOR) · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED L1 DOOR CUTOUT WEB CRACKED, .5 INCHES IN LENGTH, AT THE FORWARD INBOARD SIDE AT BS 294.5, STRINGER 12L. MAINTENANCE REMOVED THE L1 DOOR CUTOUT AT BS 294.5, STRINGER 12L WEB IAW BOEING 737-300 SRM 51-40-02-0. FABRICATED NEW INTERCOSTAL WEB IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5312-05215-SS2. INSTALLED FABRICATED REPAIR PARTS AT BS 294.5, STRINGER 12L IAW AWA ER 03-5312-05215-SS2.

Part: ANGLE — CORRODED · corrosion level 2 · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED CORROSION ON FLOOR WEB ANGLE AT BS 270, FROM BL8L TO BL8R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-1 FIG 101. MAINTENANCE REMOVED DAMAGED SECTION ON ANGLE AT BS 270, BL8L TO BL8R IAW BOEING 737-300 SRM 51-70-11-0. FABRICATED REPLACEMENT ANGLE, REPAIR ANGLE AND FILLER IAW BOEING 737-300 SRM 53-10-51-0 FIG 1, 51-70-11-0 FIG 1, AND BOEING DWG 65-45833. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 51-70-11-0 FIG 1.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 59,620 hrs · 37,014 cycles

MCN - MAJOR REPAIR - DISCOVERED, DURING C16 CHECK, L1 DOOR CUTOUT SIDEWALL LINER SUPPORT ANGLE CRACKED AT BS 344, ST 14L. MAINTENANCE REMOVED THE DAMAGED AREA ON THE SUPPORT ANGLE FOR THE L1 DOOR CUTOUT SIDEWALL LINER IAW BOEING 737-300 SRM 51-70-11-0 FIG. 1. FABRICATED REPAIR ANGLE AND FILLER FOR L1 SIDEWALL LINER IAW BOEING 737-300 SRM 51-70-11-0. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 51-70-11-0 FIG 1.

Part: BEAM — CORRODED · corrosion level 2 · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED CORROSION ON BS 312 BEAM FROM BL 0 TO BL 21R, WL 208. PREVIOUS BLEND OUT PRESENT, MATERIAL LOSS GREATER THAN ALLOWED, IAW BOEING 737-300 SRM 53-10-51-1. MX CUT OUT DAMAGED SECTION OF BEAM IAW BOEING 737-300 SRM, 53-10-51-2 FIG 205. FABRICATED TWO ANGLES IAW BOEING 737-300 SRM 53-10-51. RECEIVED AND PREPARED CHORD AND SHIMS FOR INSTALLATION IAW BOEING 737-300 SRM 53-10-51-2. INSTALLED FABRICATED REPAIR PARTS AT BS 312 BEAM FROM BL 0 TO BL 21R, WL 208 IAW BOEING 737-300 SRM 53-10-51-2 FIG 205.

Part: STIFFENER — CORRODED (BS 297-308) · airframe 59,620 hrs · 37,014 cycles

MCN - DURING C18 CHECK DISCOVERED CORROSION ON THE BOTTOM OF FLOOR SUPPORT STIFFENER AT RBL 11, WL 208, BS 297 TO BS 308. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-1 FIG 101. REMOVED STIFFENER AND PREPARED NEW STIFFENER FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0. INSTALLED FABRICATED REPAIR PARTS AT RBL 11, WL 208, BS 297 TO BS 308 IAW BOEING 737-300 SRM 51-40-02-0.

Part: ANGLE — CORRODED · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED CORROSION ON THE R1 INNER CHORD, UPPER ANGLE AT BS 305 TO BS 324, BL 58R, WL 209. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-13-1 FIG 101. MAINTENANCE REMOVED ANGLE AT BS 305 TO BS 324, BL 58R, WL 209 IAW BEING 737-300 SRM 51-30-01. PREPARED NEW ANGLE FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-02-0. INSTALLED REPAIR PARTS AT BS 305 TO BS 324, BL 58R, WL 209 IAW BOEING 737-300 SRM 51-40-02-0 FIG 3.

Part: SPOILER — DEBONDED (ZONE 500 - LEFT) · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK FOUND A DISBOND AREA ON THE UPPER SURFACE OF THE NR 4 SPOILER, 36" FROM INBOARD END FROM WBL 123.75 TO WBL 135.75. MAINTENANCE REMOVED DISBOND AREA FROM THE UPPER SURFACE OF THE NR 4 SPOILER, 36" FROM INBOARD END IAW BOEING 737-300 SRM. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 81-70-10-0. BONDED AND SEALED REPAIR PARTS TO THE UPPER SURFACE OF THE NR 4 SPOILER FROM WBL 123.75 TO WBL 135.75 IAW BOEING 737-300 SRM 51-70-10-0 FIG 31.

Part: FRAME — CRACKED · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED FRAME CRACKED, .17 INCHES IN LENGTH, UNDER DOOR ASSIST HANDLE AT THE R2 DOOR, BS 954, STR14R. MAINTENANCE TRIMMED OUT CRACK AT DOOR ASSIST HANDLE AT THE R2 DOOR, BS 954, STR 14R IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ER) 03-5362-05224-DF2. FABRICATED FILLER, STRAP, AND FRAME SPLICE STRAP IAW AWA ER 03-5362-05224-DF2. INSTALLED FABRICATED REPAIR PARTS UNDER DOOR ASSIST HANDLE AT THE R2 DOOR, BS 954, STR14R IAW AWA ER 03-5362-5224-DF2.

Part: CLIP — CRACKED · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK FOUND SEVERAL CLIPS CRACKED LOCATED AT BS 380, STRINGER 1 (1.5" LONG), STRINGER 2R (1.5" LONG) AND STRINGER 8L (.26" LONG). MAINTENANCE REMOVED CRACKED CLIPS AT BS 380, STRINGER 1, STRINGER 2R AND STRINGER 8L IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. RECEIVED NEW CLIPS AND PREPARED FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0. INSTALLED REPAIR PARTS AT BS 380, STRINGER 1, STRINGER 2R AND STRINGER 8L IAW BOEING 737-300 SRM 51-40-02-0 FIGS 3, 8 AND 12.

Part: SKIN — DEBONDED (ZONE 500 - LEFT) · airframe 59,620 hrs · 37,014 cycles

MCN - DURING C18 CHECK, DISCOVERED DISBOND AREA ON TOP SURFACE OF THE NR 3 SLAT AT THE INBOARD END. MAINTENANCE REMOVED DISBOND SKIN AND CORE ON THE NR 3 SLAT IAW BOEING 737-300 SRM 51-70-10-0 FIG 16. FABRICATED REPAIR DOUBLER AND CORE IAW BOEING 737-300 SRM 51-70-10-0 FIG 16. BONDED AND SEALED REPAIR PARTS TO THE NR 3 SLAT INBOARD END OF WEDGE IAW BOEING 737-300 SRM 51-70-10-0 FIG 16.

Part: SKIN — CRACKED (ZONE 500) · airframe 59,620 hrs · 37,014 cycles

MCN - DURING C18 CHECK, DISCOVERED FOUR CRACKS IN THE NR 1 SLAT, .250 INCHES IN LENGTH, LOCATED AT THE LOWER SKIN AT OUTBOARD END SS 385. MAINTENANCE REMOVED AND REPLACED THE NR 1 SLAT IAW BOEING 737-300 AMM 27-81-21-004-001 AND 27-81-21-404-002. OPERATIONAL CHECKS WERE GOOD IAW BOEING 737-300 AMM 27-81-00-825-018.

Part: CLIP — CRACKED · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED ATTACH CLIP AT BS 500A, STRINGER 16R CRACKED .275 INCHES IN LENGTH. MAINTENANCE REMOVED CRACKED CLIP AT BS 500A, STRINGER 16R. RECEIVED AND PREPARED NEW STRINGER CLIP FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0 FIG 2 & 3. INSTALLED NEW STRINGER CLIP IAW BOEING 737-300 SRM 51-40-02-0 FIG 8 & 12.

Part: CLIP — CRACKED (FUSELAGE) · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED CLIP CRACKED, .375 INCHES IN LENGTH, AT BS 336 STRINGER 6R. MAINTENANCE REMOVED CRACKED CLIP AT BS 336 STRINGER 6R IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. FABRICATED NEW CLIP IAW BOEING 737-300 DWG 65-45874 AND BOEING 51-30-01-0 FIG 3, 7, 8. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 51-40-02-0 FIG 5, 8 , 12 AND BAC DWG 65-45874.

Part: SKIN — CRACKED (NR 2 SLAT) · airframe 59,620 hrs · 37,014 cycles

MCN - DURING C18 CHECK DISCOVERED, 4 CRACKS IN THE NR 2 SLAT SKIN BELOW THE INBOARD AUXILIARY TRACK, FROM SS 90 TO SS 164. MAINTENANCE REMOVED DAMAGED AREA OF NR 2 SLAT SKIN BELOW THE INBOARD AUXILIARY TRACK, FROM SS 90 TO SS 164 IAW BOEING 737-300 SRM 57-43-01-2. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 52-43-01-2 FIG 206. INSTALLED FABRICATED REPAIR PARTS ON THE NR 2 SLAT SKIN BELOW THE INBOARD AUXILIARY TRACK FROM SS 90 TO SS 164 IAW BOEING 737-300 SRM 57-43-01-2 FIG 206.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED FUSELAGE SKIN CRACK, 1.43 INCHES IN LENGTH, AT BS 727E+4 INCHES, STRINGER 24R. MAINTENANCE CUT OUT DAMAGED AREA OF SKIN AT BS 727E+4 INCHES, STRINGER 24R IAW BOEING 737-300 SRM 53-00-01-3 FIG 229. FABRICATED DOUBLER, TRIPLER AND FILLER IAW BOEING 737-300 SRM 53-00-01-3 FIG 229. INSTALLED AND SEALED FABRICATED REPAIR PARTS AT BS 727E+4 INCHES, STRINGER 24R IAW BOEING 737-300 SRM 53-00-01-3 FIG 229.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED STINGER CLIP CRACKED, .200 INCHES IN LENGTH, AT BS 277, STRINGER 10R. MAINTENANCE REMOVED STRINGER CLIP AT BS 277, 10RT IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. FABRICATED NEW STRINGER CLIP IAW BOEING DWG 65-45805. MAINTENANCE INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 51-40-02.

Part: FRAME — CRACKED · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED ANGLE CRACKED, .375 INCHES IN LENGTH, AT FORWARD UPPER CORNER OF THE R1 DOOR, CUTOUT. MAINTENANCE CUT OUT CRACKED AREA OF FRAME ANGLE IAW BOEING 737-300 SRM 51-70-11-0. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-11-0. INSTALLED FABRICATED REPAIR PARTS AT FORWARD UPPER CORNER OF THE R1 DOOR, CUTOUT, IAW BOEING 737-300 SRM 51-70-11-0 FIG. 1.

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED, THE NR 3 SLAT SKIN AT OUTBOARD END, SS 124, CRACKED .375 INCHES IN LENGTH. MAINTENANCE REMOVED DAMAGED AREA OF THE NR 3 SLAT SKIN IAW BOEING 737-300 SRM 57-43-01-2. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 52-43-01-2 FIG 206. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 57-43-01-2 FIG 206.

Part: TAB — DELAMINATED (ZONE 300 - STABI) · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED, THE LT HORIZONTAL ELEVATOR TAB DELAMINATED, AT OUTBOARD END, TOP SURFACE FROM ES 127L TO ES 129L. MAINTENANCE CUT OUT DELAMINATED AREA ON THE LT HORIZONTAL ELEVATOR TAB IAW BOEING 737-300 SRM 51-70-17-0 FIG 11. SANDED AND CLEANED AREA ON THE LT HORIZONTAL ELEVATOR TAB IAW BOEING 737-300 SRM 51-70-17-0. OBTAINED REPAIR PLIES AND BONDED TO SURFACE OF THE LT HORIZONTAL ELEVATOR, OUTBOARD END, TOP SURFACE, FROM ES 127L TO ES 129L IAW BOEING 737-300 SRM 51-70-17-0 FIG 11. NO WEIGHT WAS ADDED TO THE ELEVATOR IAW BOEING 737-300 SRM 51-60-06-0.

Part: STRAP — CRACKED · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED STABILIZER STRAP CRACKED, .65 INCHES IN LENGTH, ON CABIN FLOOR AT BS 330, BL 15L, WL 204. MX STOP DRILLED CRACK IN STABILIZER STRAP AT BS 330, BL 15L, WL 204 IAW BOEING 737-300 SRM 53-10-51-2. FABRICATED REPAIR PLATE IAW BOEING 737-300 SRM 53-10-51-2 FIG 204. INSTALLED REPAIR PLATE ON STABILIZER STRAP AT BS 330, BL 15L, WL 204 IAW BOEING 737-300 SRM 51-40-02-0.

Part: FRAME — CRACKED · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED R1 DOOR FORWARD STOP CUTOUT, FOURTH FROM TOP, CRACKED, .60 INCHES IN LENGTH. MAINTENANCE TRIMMED OUT CRACK AREA AT R1 DOOR FORWARD STOP CUTOUT, FOURTH FROM TOP IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5200-5214-SS1. FABRICATED DOUBLER IAW AWA ER 03-5200-5214-SS1. INSTALLED FABRICATED REPAIR PARTS AT R1 DOOR FORWARD STOP CUTOUT, FOURTH FROM TOP IAW BOEING 737-300 SRM 51-40-02-0 FIG 3 AND AWA ER 03-5200-5214-SS1.

Part: WEDGE — DELAMINATED (ZONE 500 - LEFT) · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED LT INBOARD FORE FLAP LOWER SURFACE DELAMINATED, AT THE INBOARD TRACK ATTACHMENT. MAINTENANCE REMOVED DAMAGED AREA ON THE LT INBOARD FORE FLAP LOWER SURFACE AND CLEANED AREA IAW BOEING 737-300 SRM 51-70-10. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-0 FIG 30. INSTALLED, BONDED AND SEALED FABRICATED REPAIR PARTS TO THE LT INBOARD FORE FLAP LOWER SURFACE IAW BOEING 737-300 SRM 51-70-10-0 FIG 30.

Part: WEDGE — DELAMINATED (FLAP) · airframe 59,620 hrs · 37,014 cycles

MCN - DURING C18 CHECK, DISCOVERED THE LT OUTBOARD AFT FLAP DELAMINATED AT THE INBOARD END OF THE UPPER AND LOWER SURFACES AT WBL 23.68 TO WBL 235.68. MAINTENANCE REMOVED DAMAGED AREA ON THE LT OUTBOARD AFT FLAP AND PREPARED FOR REPAIR IAW BOEING 737-300 SRM 51-70-10-0 FIG 16. FABRICATED REPAIR DOUBLERS AND FILLER IAW BOEING 737-300 SRM 51-70-10-0 FIG 16. INSTALLED, BONDED AND SEALED REPAIR PARTS TO THE LT OUTBOARD AFT FLAP, THE INBOARD END OF THE UPPER AND LOWER SURFACES AT WBL 23.68 TO WBL 235.68 IAW BOEING 737-300 SRM 51-70-10-0 FIG 16.

Part: STRUCTURE — CRACKED · airframe 59,620 hrs · 37,014 cycles

DURING C18 CHECK DISCOVERED SEVERAL SUBSTRUCTURES CRACKED AT THE L1 FWD ENTRY DOOR CUTOUT FROM STR 15L TO STR 16L, BS 348.20. MX REMOVED ALL DAMAGED PARTS, (1) CLIP CRACKED .5", (2) CLIP CRACKED .5", (3) CLIP CRACKED .5", (4) CLIP CRACKED .5" IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5312-05215-SS2. FAB`D REPAIR CLIPS IAW AWA ER 03-5312-05215-SS2. MX INSTALLED FABRICATED REPAIR PARTS AT THE L1 FWD ENTRY DOOR CUTOUT FROM STRINGER 15L TO STRINGER 16L, BS 348.20 IAW AMERICA WEST AIRLINES ER 03-5312-05215-SS2. (1)CLIP, PN 69-16970-501; NSN; BOEING; CRACKED (2)CLIP, PN 69-26555-2; NSN; BOEING; CRACKED (3)CLIP, PN 69-26555-3; NSN; BOEING; CRACKED(4)CLIP, PN 65-16509-6; NSN; BOEING; CRACKED.

Part: WIRE — BACKED OUT (CABIN) · airframe 58,794 hrs · 36,542 cycles

PHX - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 2 LT INOPERATIVE. MAINTENANCE FOUND WIRE PULLED OUT OF RECEPTACLE WITH EVIDENCE OF ARCHING. REPLACED EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS AT SEAT ROW 2 LT, OPERATIONAL WAS GOOD.

Part: PACKING — TORN (LT WING) · airframe 58,025 hrs · 36,109 cycles

LAS - DIVERSION - FLT 0765 - APPROXIMATELY 20 MINUTES OUT OF PHX EN ROUTE TO SMF NOTICED HYDRAULIC FLUID LEAKING FROM THE TOP OF LEFT WING, ALSO OBSERVED B-SYSTEM HYDRAULIC QUANTITY DECREASING, FLUID LEVEL STABILIZED AT 1/2 QUANTITY ON INDICATOR, DIVERTED INTO LAS FOR REPAIR. MAINTENANCE FOUND LEAK COMING FROM FITTING AT NR 3 SPOILER, REPLACED 2 EACH O-RING SEALS ON FITTING FOR NR 3 SPOILER, LEAK CHECK WAS GOOD.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 55,862 hrs · 34,921 cycles

MCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND IN SUPPORT ANGLE (CLIP) OF AFT CARGO COMPARTMENT DOOR SILL BS 807, RBL 30. MAINTENANCE REMOVED CRACKED SUPPORT ANGLE (CLIP) AT AFT CARGO COMPARTMENT DOOR SILL BS 807, RBL 30; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE (CLIP) PER DWG 69-42949; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 4B.

Part: WEB — CORRODED (DOOR SILL) · corrosion level 2 · airframe 55,862 hrs · 34,921 cycles

MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL WEB IN SEVERAL LOCATIONS BETWEEN BS 794.3 AND BS 847, RBL 20. MAINTENANCE REMOVED CORRODED SECTION OF AFT CARGO COMPARTMENT DOOR SILL WEB FROM BS 794.3 TO BS 847, AT RBL 20; FABRICATED A NEW REPLACEMENT SECTION OF WEB AND A REPAIR SPLICE; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11, FIG. 1.

Part: STRAP — CORRODED (DOOR SILL) · corrosion level 2 · airframe 55,862 hrs · 34,921 cycles

DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL WEB (STRAP) BS 794.3, RBL 20. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR SILL STRAP AT BS 794.3, RBL 20; FABRICATED A NEW REPLACEMENT STRAP PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 4B.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,862 hrs · 34,921 cycles

MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL SUPPORT ANGLE AT BS 794.3, RBL 20. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL SUPPORT ANGLE, BS 794.3, RBL 20; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 2-3, 8, & 12.

Part: REVEAL — CORRODED (FUSELAGE) · airframe 55,862 hrs · 34,921 cycles

MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON R-1 DOOR CUTOUT UPPER AFT REVEAL AT FASTENER HOLE BS 336, STR 10 RT. MAINTENANCE REMOVED CORRODED R-1 DOOR UPPER AFT REVEAL AT BS 336, STR 10 RT; FABRICATED A NEW REPLACEMENT REVEAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 3-4, & 6-8.

Part: PANEL — CRACKED (L/E SLAT) · airframe 55,862 hrs · 34,921 cycles

MCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND IN NR 5 SLAT OUTBOARD COVE PANEL SKIN AT STAB STA 255.7. MAINTENANCE REMOVED CRACKED NR 5 SLAT OUTBOARD COVE PANEL AT SS 255.7; FABRICATED A NEW REPLACEMENT PANEL PER DWG 65C26602; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-04 FIG 1.

Part: WEB — CORRODED (DOOR SILL) · corrosion level 2 · airframe 55,862 hrs · 34,921 cycles

MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND UNDER FORWARD INBOARD CORNER OF AFT CARGO COMPARTMENT DOOR SILL WEB BS 794, RBL 30. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR SILL WEB AT BS 794, RBL 30; FABRICATED A NEW REPLACEMENT STRAP PER DWG 65-47688; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 9.

Part: WEB — CRACKED (DOOR SILL) · airframe 55,862 hrs · 34,921 cycles

MCN - MAJOR REPAIR - DURING C-17 CHECK A 1/2 INCH CRACK WAS FOUND IN L-1 DOOR SILL WEB, BS 328, LBL 60. MAINTENANCE REMOVED CRACKED L-1 DOOR SILL WEB AT BS 328, LBL 60; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-17688; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 12.

Part: BOLT — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 55,862 hrs · 34,921 cycles

MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON THE LT VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT BS 1016, STR 2 LT. MAINTENANCE REMOVED AND REPLACED L/H VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT IAW T/C I6B55002.

Part: BOLT — CORRODED (VETICAL STAB) · corrosion level 2 · airframe 55,862 hrs · 34,921 cycles

MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON RT VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT BS 1016, STR 2 RT. MAINTENANCE REMOVED AND REPLACED RT VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT IAW T/C I6B5502.

Part: BOLT — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 55,862 hrs · 34,921 cycles

MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON RT AFT INBOARD VERTICAL STABILIZER ATTACH BOLT BS 1085, STR 2 RT. MAINTENANCE REMOVED AND REPLACED RT AFT INBOARD VERTICAL STABILIZER ATTACH BOLT IAW T/C I6B55002.

Part: VERTICAL BEAM — CRACKED (BULKHEAD) · airframe 55,862 hrs · 34,921 cycles

MCN - MAJOR REPAIR - DURING C-17 CHECK A 1/2 INCH CRACK WAS FOUND IN BS 178 BULKHEAD VERTICAL WEB BEAM AT LBL 5.7, WL 176. MAINTENANCE CUTOUT DAMAGED SECTION OF BS 178 BULKHEAD VERTICAL WEB; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH TAPERED SHIMS, A REPAIR WEB & FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, FIG. 212.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,862 hrs · 34,921 cycles

MCN - MAJOR REPAIR - DURING C-17 CHECK A 1" CRACK WAS FOUND IN UPPER ANGLE OF INTERCOSTAL BETWEEN BS 927 AND BS 947, BL "0". MAINTENANCE REMOVED CRACKED UPPER ANGLE ON INTERCOSTAL FROM BS 927 TO BS 947, BL "0"; FABRICATED A NEW REPLACEMENT UPPER INTERCOSTAL ANGLE PER DWG 69-36656 AND INSTALLED REPAIR PART.

Part: BOLT — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 55,862 hrs · 34,921 cycles

DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON THE RT HORIZONTAL STABILIZER FORWARD LOWER ATTACH BOLT BS 1088, WL 258. MAINTENANCE REMOVED AND REPLACED R/H HORIZONTAL STABILIZER FORWARD LOWER ATTACH BOLT IAW T/C I6C55038.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,862 hrs · 34,921 cycles

MCN - MAJOR REPAIR, DURING C-17 CHECK A .2500 CRACK WAS FOUND AT FASTENER HOLE IN FUSELAGE SKIN AT LOWER FORWARD CORNER OF R-2 DOOR CUTOUT BS 981.8 TO BS 984.8, WL 198. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED AN INNER, MIDDLE, AND OUTER DOUBLERS; INSTALLED FREEZE PLUG IN STOP DRILL HOLE, INSTALLED DOUBLERS IAW SRM 53-60-01, FIG. 203, AND E.R. 03-5300-04128-HFIA.

Part: SKIN — BULGED (FUSELAGE) · airframe 55,862 hrs · 34,921 cycles

MCN - MAJOR REPAIR - DURING C-17 CHECK THE SKIN WAS FOUND BULGING BETWEEN FASTENERS INSIDE THE FORWARD CARGO COMPARTMENT AT A PREVIOUSLY INSTALLED REPAIR DOUBLER BS 370 TO BS 390, RBL 36. MAINTENANCE REMOVED REPAIR DOUBLER BS 370 TO BS 390, RBL 36 AND FOUND EVIDENCE OF WATER ENTRAPMENT, NO CORROSION. CLEANED AND TREATED SURROUNDING SKIN AREA; FABRICATED A DOUBLER, TRIPLER, AND FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01 FIG 229.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,862 hrs · 34,921 cycles

MCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND IN FORWARD CABIN FLOOR SUPPORT ANGLE BETWEEN BS 380 AND BS 400, AT BL "0". MAINTENANCE REMOVED CRACKED FLOOR SUPPORT ANGLE FROM BS 380 TO BS 400, AT BL "0"; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT ANGLE PER DWG 69-35365; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 3.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,862 hrs · 34,921 cycles

DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 27 LT AT BS 967. MAINTENANCE CUTOUT DAMAGED SECTION OF STRINGER 27 L/H AT BS 967; FABRICATED A 4 EACH ANGLES & SHIMS, 2 EACH CHANNELS, AND A HAT SECTION; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03, FIG. 201.

Part: SKIN — DELAMINATED (SLAT) · airframe 55,862 hrs · 34,921 cycles

DURING C-17 CHECK FOUND THE UPPER NO. 5 SLAT WEDGE DELAMINATED AT SS 147.5. MAINTENANCE REMOVED PREVIOUSLY INSTALLED REPAIR DOUBLERS ON NO. 5 SLAT WEDGE AT SS 147.5; FABRICATED NEW REPLACEMENT DOUBLERS; BONDED REPAIR PARTS TO SLAT IAW B737-300 SRM 51-70-10, FIG. 31.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,862 hrs · 34,921 cycles

MCN - MAJOR REPAIR, DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON L-1 DOOR SILL IB STIFFENER ANGLES AT SCREW HOLES BS 328, LBL 60. MAINTENANCE REMOVED 2 EACH CORRODED STIFFENER ANGLES AT BS 328, LBL 60; FABRICATED 2 EACH NEW REPLACEMENT ANGLES IAW DWG 65-17688; INSTALLED REPAIR PARTS IAW SRM 51-40-02, FIG. 12.

Part: PANEL — CRACKED (RT WING SPOILER) · airframe 55,862 hrs · 34,921 cycles

DURING C-17 CHECK 2 EACH CRACKS WERE FOUND ON NR 6 SPOILER PANEL ABOVE ACTUATOR AT WBL 245 RT. MAINTENANCE REMOVED AND REPLACED NR 5 SPOILER PANEL IAW AMM 27-62-11, FIG. 401, PG. 1-5.

Part: PANEL — CORRODED (RT WING SPOILER) · corrosion level 2 · airframe 55,862 hrs · 34,921 cycles

MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON NO. 5 SPOILER PANEL ALONG LEADING EDGE OF LOWER SEAL BETWEEN WBL 71.24 AND WBL 191 R/H. MAINTENANCE REMOVED AND REPLACED NO. 5 SPOILER PANEL IAW AMM 27-62-12, FIG. 401, PG. 1-5.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 55,862 hrs · 34,921 cycles

DURING C-17 CHECK THE UPPER SURFACE OF LT OUTBOARD FORE FLAP WAS FOUND DELAMINATED 89.5 INCHES FROM INBOARD END WS 378 TO WS 386. MAINTENANCE REMOVED DELAMINATED PREVIOUS REPAIR ON LT OUTBOARD FORE FLAP FROM WS 378 TO WS 386; FABRICATED A REPAIR DOUBLER; BONDED REPAIR PART TO FORE FLAP IAW B737-300 SRM 51-70-10, FIG. 17.

Part: SEAT TRACK — CRACKED (FUSELAGE) · corrosion level 2 · airframe 55,862 hrs · 34,921 cycles

DURING C-17 CHECK EXFOLIATION CORROSION AND A 1 INCH CRACK WAS FOUND ON SEAT TRACK BS 420 TO BS 425, RBL 45. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK FROM BS 380 TO BS 480, RBL 45; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK PER DWG 65-46813; INSTALLED REPAIR PART IAW B737-300 SRM 53-30-52, FIG. 1.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 55,862 hrs · 34,921 cycles

MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND THE L/H OUTBOARD AFT FLAP SEPARATING AT THE AFT INBOARD CORNER WS 230.68. MAINTENANCE PERFORMED A BOND REPAIR IAW B737-300 SRM 51-70-10, FIG. 10.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 55,862 hrs · 34,921 cycles

DURING C-17 CHECK THE UPPER SURFACE OF LT INBOARD MID FLAP TRAILING EDGE WEDGE WAS FOUND DELAMINATED 9 INCHES FROM INBOARD END. MAINTENANCE CUTOUT DAMAGED UPPER SKIN AND CORE ON LT INBOARD MID FLAP TRAILING EDGE AT WS 82 LT; FABRICATED A NEW REPLACEMENT CORE AND A REPAIR DOUBLER; BONDED REPAIR PARTS TO MID FLAP IAW B737-300 SRM 51-70-10, FIG. 16.

Part: FLASHLIGHT — INOPERATIVE (ZONE 900 - LAVAT) · airframe 54,074 hrs · 33,856 cycles

FLIGHT CREW REPORTED THE FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 53,472 hrs · 33,504 cycles

EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD CABIN EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,119 hrs · 32,712 cycles

DURING C-16 CHECK, A .5000 INCH CRACK WAS FOUND ON LOWER FLOORBEAM TIE STRAP AT BS 340, STR 45 LT, JUST ABOVE AIR STAIR RAIL OUTBOARD END. MAINTENANCE STOP DRILLED END CRACK ON LOWER FLOORBEAM TIE STRAP AT BS 340; FABRICATED A REPAIR PLATE; REMOVED VERTICAL STIFFENER FOR ACCESS; INSTALLED REPAIR PART AND REINSTALLED VERTICAL STIFFENER IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,119 hrs · 32,712 cycles

DURING C-16 CHECK, A .5000 INCH CRACK WAS FOUND ON LOWER FLOORBEAM TIE STRAP AT BS 340 JUST ABOVE AIR STAIR RAIL RBL 24.75. MAINTENANCE STOP DRILLED HOLE ON LOWER FLOORBEAM TIE STRAP AT BS 340; FABRICATED A REPAIR PLATE; AND INSTALLED REPAIR PART IAW SRM.

Part: TIE CLIP — CRACKED · corrosion level 0 · airframe 52,119 hrs · 32,712 cycles

YVR - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 616, STR 2 L/H. MAINTENANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 616, STR 2 L/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 12.

Part: TIE CLIP — CRACKED · corrosion level 0 · airframe 52,119 hrs · 32,712 cycles

YVR - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 616, STR 2 R/H. MAINTENANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 616, STR 2 R/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 12.

Part: TIE CLIP — CRACKED · corrosion level 0 · airframe 52,119 hrs · 32,712 cycles

YVR - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 663, STR 10 R/H. MAINTENANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 663, STR 10 R/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 12.

Part: TIE CLIP — CRACKED · corrosion level 0 · airframe 52,119 hrs · 32,712 cycles

YVR - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 616, STR 1. MAINTENANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 616, STR 1; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 12.

Part: TIE CLIP — CRACKED · corrosion level 0 · airframe 52,119 hrs · 32,712 cycles

YVR - MAJOR REPAIR - DURING C-16 CHECK A 3/8" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 663, STR 10 L/H. MAINTENANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 663, STR 10 L/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 12.

Part: SLAT — DELAMINATED · corrosion level 0 · airframe 52,117 hrs · 32,112 cycles

YVR - MAJOR REPAIR - DURING C-16 CHECK THE #5 SLAT WAS FOUND DELAMINATED AT THE OUTBOARD UPPER TRAILING EDGE SURFACE. MAINTENANCE REMOVED THE #5 SLAT AND REPAIRED DAMAGE IAW B737-300 SRM 51-70-10 REPAIR 22 & 23. REINSTALLED #5 SLAT IAW BMM 27-81-21, PG. 401-419.

Part: SKIN — CRACKED · corrosion level 0 · airframe 52,117 hrs · 32,712 cycles

YVR - MAJOR REPAIR - DURING C-16 CHECK A 1/2" CRACK WAS FOUND ON FUSELAGE SKIN AT THE UPPER HINGE CUTOUT OF THE L-2 DOOR, BS 951, STR 10 L/H. MAINTENANCE CUTOUT CRACKED AREA OF SKIN AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; AND INSTALLED REPAIR PART IAW B737-300 SRM 53-60-01, FIG 205, PG. 211.

Part: SKIN — CRACKED (FUSELAGE) · corrosion level 2 · airframe 52,119 hrs · 32,712 cycles

DURING C-16 CHECK, CORROSION AND 3 EACH .2500 INCH CRACKS WERE FOUND ON LOWER EXTERIOR FUSELAGE SKIN (LT AND RT KEELBEAM) AT BS 727+5 - BS 727+10, STR 27 LT - STR 27 RT. MAINTENANCE CUT SKIN FOR ACCESS TO KEEL BEAM; TRIMMED OUT DAMAGED AREAS OF OUTBOARD LOWER FLANGE ON KEELBEAM BS 727+5 - BS 727+10, STR 27 LT - STR 27 RT; BLENDED OUT AND TREATED CORROSION; PERFORMED HFEC INSPECTION OF CUTOUTS TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER, TRIPLER, FILLER & REPAIR ANGLE FOR LT KEELBEAM, AND FILLER & REPAIR ANGLE FOR RT KEELBEAM; INSTALLED REPAIR PARTS IAW AWA ER.

Part: CONTROL CABLE — BROKEN (TE FLAPS) · airframe 52,117 hrs · 32,712 cycles

DURING C-16 CHECK, FLAP FOLLOW UP CABLES WFFA, WFFB WERE FOUND TO HAVE LOW TENSION IAW TABLE 4, W/C 12B27001. WHILE APPLYING TENSION TO CABLES, CABLE WFFA BROKE .1250 INCH INSIDE THE TERMINAL DUE TO NUMEROUS BROKEN WIRE STRANDS. MAINTENANCE REMOVED AND REPLACED FLAP FOLLOW UP CABLE WFFA IAW BMM. MAINTENANCE ALSO DISCOVERED BROKEN WIRE STRANDS ON FLAP FOLLOW UP CABLE WFFB, AND REPLACED CABLE WFFB IAW BMM.

Part: SLAT — DELAMINATED · corrosion level 0 · airframe 52,119 hrs · 32,712 cycles

YVR - MAJOR REPAIR - DURING C-16 CHECK THE #4 SLAT WAS FOUND DELAMINATED AT THE INBOARD UPPER TRAILING EDGE SURFACE. MAINTENANCE REMOVED THE #4 SLAT AND REPAIRED DAMAGE IAW B737-300 SRM 51-70-10 REPAIR 22 & 23. REINSTALLED #4 SLAT IAW BMM 27-81-21, PG. 401-419.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,221 hrs · 32,148 cycles

PHX - EEL - FLIGHT ATTENDANT REPORTED THAT EMERGENCY EXIT LIGHT IN FIRST CLASS WAS INOPERATIVE. REPLACED BULLNOSE LIGHT ASSEMBLY PER BMM 33-51-21-201, OPERATIONAL CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 49,754 hrs · 31,139 cycles

GEG - DIVERSION - FLT 592 - O - EN ROUTE FROM GEG TO PHX AT FL 330 CABIN PRESSURE DIFFERENTIAL OF 7.8 PSI CAPTAINS WINDSHIELD OUTER PANE SHATTERED. EMERGENCY WAS DECLARED AND AIRCRAFT DIVERTED SAFELY TO BOI. MAINTENANCE ARRIVED AT BOI FROM PHX AND REPLACED THE CAPTAINS WINDSHIELD IAW T/C R1B56001. AS A PRECAUTION THE CAPTAINS NR 1 WINDOW HEAT CONTROL UNIT WAS ALSO REPLACED. WINDOW HEAT CONTROL UNIT, PACIFIC ELECTRO, P/N: 83000-05602, S/N: 2421.

Part: WIRE — DETACHED (SEAT ROW 17) · airframe 49,511 hrs · 30,965 cycles

YVR - EEL - "C" - DURING C-15 CHECK DISCOVERED BLACK WIRE PULLED OUT OF SPLICE IN FLOOR CONDUIT ON L/H SEAT MOUNTED ESCAPE PATH LIGHTING SEAT ROW 17. MAINTENANCE RE-SPLICED WIRE PER STANDARD WIRING PRACTICES MANUAL 20-30-12, PG. 3.

Part: RECEIVER — MALFUNCTIONED (EE BAY) · airframe 46,976 hrs · 29,296 cycles

LAS - AIR TURNBACK 1/7/01 - ON APPROACH IN SLC THE CAPT''''''''S GLIDE SLOPE INDICATION WENT FULL DEFLECTION AND THE 1ST OFFICER''''''''S FULL DEFLECTION DOWN. TWO APPROACHES TRIED WITH THE SAME RESULT. THE AIRCRAFT RETURNED TO LAS AND BOTH GLIDE SLOPE INDICATORS INDICATED NORMAL. AWA DISPATCH CONTACTED SLC AND FOUND OTHER AIRCRAFT HAD SIMILAR PROBLEMS WITH VOR/ILS. ON 1/8/01, THE NR 1 VOR/ILS RECIEVER WAS CHANGED AS A PRECAUTION.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION ON FLOORBEAM AT STA 328 LBL 49 AND GOUGES IN FLOORBEAM UPPER CHORD AT RBL 22 AND 35; FOUND DURING CPCP INSPECTION EVALUATED AT LEVEL 1 CORROSION. CORROSION REMOVAL IAW SRM BEYOND LIMITS, GOUGES CLEANED UP IAW SRM 53-10-51 BEYOND LIMITS; REPAIRED FLOORBEAM IAW 51-70-12 PG 4

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION ON FLOORBEAM AT STA 294 LBL 3 FOUND DURING CPCP INSPECTION EVALUATED AS LEVEL 1. CORROSION REMOVAL IAW SRM BEYOND LIMITS; REPAIRED FLOORBEAM IAW SRM 53-10-51 PG 220-222 FIG 205 SHT.3-4; PREPPED AND PAINTED IAW MM51-21-00

Part: SEAT TRACK — CRACKED (FUSELAGE)

SEAT TRACK ATTACH FRAME AT STA 727A TO 727B WL 207 RBL 45 CRACKED. REPAIRED IAW AWA ER 03-5310-00335-JS2

Part: SKIN — DAMAGED (FUSELAGE) · airframe 46,831 hrs · 29,202 cycles

FUSELAGE SKIN FOUND DAMAGD STA 500A STR 3L. FABED AND INSTALLED REPAIR PARTS IAW SRM 53-00-01 FIG 202

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,831 hrs · 29,202 cycles

D: SEVERAL CRACKS FOUND BS 178 WL 185, 195, AND 207 AT AND BETWEEN LEFT AND RIGHT BL 5.6 AND 24.00 IN SIDE CHORDS, WEB AND FLOOR PANEL STRUCTUREC: REPAIRED ALL IAW EO 53-12-07

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,831 hrs · 29,202 cycles

SEVERAL CRACKS FOUND BS 178 WL 185, 195, 207 AT AND BETWEEN LEFT AND RIGHT BL 5.6 AND 24.00 IN SIDE CHORDS, WEB AND FLOOR PANEL STRUCTURE. REPAIRED ALL IAW EO 53-12-07.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 46,831 hrs · 29,202 cycles

D; FUSELAGE SKIN FOUND DAMAGD STA 500A STR 31C: FABED AND INSTALLED REPAIR IAW SRM 53-00-01 FIG 202

Part: SEAT TRACK — CORRODED (BS 500B - 500D)

C-CHECK, CORROSION ON SEAT TRACK AT RIGHT OUTBD FS 500B-500D OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK PER SRM 51-40-02, FABRICATED SEAT TRACK FROM BAC 1520-792/7178T6 PER SRM 53-30-52 R659935, TREATED AND PRIMED PER SRM 51-20-01 AND INSTALLED PER SRM 51-40-02.

Part: BULKHEAD — CRACKED (BS 644)

C-CHECK, CABIN STA 663.75 LBL 32, WHEEL WELL PRESSURE DECK HAD 1 .4375 CRACK. HFEC VERIFIED CRACK. REMOVED DAMAGED AREA, FABRICATED DOUBLER, TREATED, PRIMED, AND INSTALLED PARTS PER ER 03-5310-99288-EY1. FABRICATED REPAIR DOUBLER FROM 2024T3 X .050 R700212, FILLER FROM 2024T3 X .050 R700212, ANGLE FROM 7075T6 X .063 R699452.

Part: SKIN — CREASED (BS 380)

C-CHECK, TWO SMALL DENTS 5 FEET FWD OF FWD CARGO DOOR, FS 380 STR 24R. CREASE IN BOTTOM OF DENTS OUT OF LIMITS. REMOVED DAMAGE, NDT REVEALED NO CRACKS. FABRICATED REPAIR PARTS FROM 2024T3 X.063 R699111 2024T3 X.050 R697963. INSTALLED CONICAL WASHERS, ALODINED AND PRIMED IAW SRM 51-40-02, 51-20 -02 AND 53-00-01.

Part: SKIN — GOUGED (TE FLAP)

C-CHECK, RIGHT O/B MID FLAP AT I/B TRACK IS GOUGED ON LWR L/E SURFACE. REMOVED DAMAGED AREA, FABRICATED REPLACEMENT DOUBLER FROM .032301 CRES 1/2 HARD MATERIAL, IAW SRM 57-53-01. TREATED AND PRIMED IAW SRM 51-20-01. INSTALLED DOUBLER IAW SRM 57-53-01.

Part: SKIN — CRACKED (FUSELAGE)

C-CHECK, CRACK IN FUSLAGE SKIN AT LWR AFT CORNER OF R1 DOOR HAD CRACKS EXTENDING FROM 2 FASTENER HOLES. REMOVED FASTENERS AND REAMED HOLES TO .25 IAW SRM 53-10-01, HFEC REVEALED INTERIOR CRACKS, EXTERIOR CRACKS ARE CONTAINED AT FASTENER HOLES. INSTALLED FLUSH WASHERS AND FABRICATED DOUBLERS FROM 2024 .063 R681615, FABRICATED SHIMS FROM 7075T .100R707582. TREATED, PRIMED AND INSTALLED WET PER SRM 53-10-1.

Part: INTERCOSTAL — CORRODED (BS 787 - 793)

C-CHECK, AFT PIT STA 787-793, STR 25R INTERCOSTAL HAD CORROSION ON UPPER FLANGE AT NUT PLATE ATTACH AREAS. REMOVED CORRODED INTERCOSTAL, FABRICATED, TREATED, AND PRIMED REPAIR PART AND INSTALLED PER SRM 53-60-15, 51-40-12 AND 51-10-1.

Part: FAN — FAILED (AFT GALLEY)

DURING DESCENT, FA REPORTED ELECTRICAL SMELL IN AFT GALLEY, CYCLING RECIRC FAN MADE DIFFERENCE INSTANTLY. REPLACED RECIRC FAN PER MM 21-21-22 PG 401. NONE RELATED RECOMMENDATION.

Part: PANEL — LEAKING (RT WING)

EMERGENCY LANDING, INFLIGHT RIGHT WING FUEL LEAK. NON REV PILOT REPORTED FLUID LEAK ON RT WING UNDETERMINED QTY, TYPE, AND SOURCE. CAPTAIN INITIATED AN EMERGENCY LANDING. REMOVED AND REPLACED UPPER PANEL ON WING JUST AFT OF PYLON, LEAK CK GOOD, NO LEAKS.

Part: COMPRESSOR — FAILED (NR 2 ENGINE)

AIR TURNBACK FOR SMOKE IN CABIN AND AFT LT LAV SMOKE DETECTOR SOUNDING. FOUND OIL IN HIGH PRESSURE COMPRESSOR OF NR 2 ENGINE. REMOVED AND REPLACED ENGINE. REPLACED SMOKE DETECTOR AS NO SMOKE WAS NOTED IN CABIN ONLY OIL SMELL.

Part: AIR DISTRIBUTION — ODOR (FLIGHT DECK)

BURNED SMELL NOTED BY CABIN AND FLIGHT DECK CREW. RECIRCULATION FAN TURNED OFF AND SMELL DIMINISHED. RAN RECIRCULATION FAN AT GATE DURING TURN. NO BURN SMELL, OPS CHECK NORMAL.

Part: CHECK VALVE — INOPERATIVE (NR 1)

AIR TURNBACK, AFTER ROTATION, SMELLED A HOT ELECTRIC SMELL. SHUT DOWN RECIRCULATION FAN AND SMELL WENT AWAY. APPROXIMATELY 15 MIN INTO FLIGHT, COOLING EXHAUST LIGHT ILLUMINATED. SWITCHED TO ALTERNATE FAN AND RESET CIRCUIT BREAKERS WITH NOT EFFECT. REMOVED AND REPLACED NORMAL EQUIPMENT COOLING EXHAUST CHECK VALVE. REMOVED AND REPLACED ALTERNATE EQUIPMENT COOLING EXHAUST BLOWER ALTERNATE EQUIPMENT COOLING EXHAUST BLOWER 6577-1 9012 MALFUNCTIONED, A/EPART TOTAL TIME = 13572, PART TOTAL CYCLES = 7937, PART TIME SINCE OVERHAUL/REPAIRED = 344.

Part: CONTROL CABLE — MISRIGGED (MLG)

LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. FOLLOWED QRH PROCEDURES AND RETRACTED GEAR. FOUND TELEFLEX CABLE AND AIR SAFETY SENSOR NOT RIGGED PER MM. CORRECTED PER MM 32-09-01.

Part: CARRIAGE ASSY — WORN (LT TE FLAP)

CREW REPORTED DURING FLAP SELECT 15 TO 40 DEGREES, THE A/C ROLLED TO THE LEFT WHICH REQUIRED 7 UNITS OF RT RUDDER TRIM TO LEVEL. LANDING WAS MADE WITHOUT INCIDENT. UNITED MAINTENANCE COULD FIND NO OBVIOUS DEFECTS, MADE REQUIRED LOGBOOK ENTRY FOR MAINTENANCE FERRY FLIGHT. INSPECTED ALL FLIGHT CONTROLS, NO DEFECTS NOTED. FUNCTION CHECK FLAPS, SLATS AND SPOILERS, FUNCTION CHECK GOOD. FOUND AILERON, TRIM L-WING DOWN, NO OTHER FAULTS. CHECKED FLAP TRACKS, TOGGLERS AND ROLLERS, NO DEFECTS NOTED. CHECKED LE ACTUATORS AND SUPPORTS, NO DEFECTS NOTED. REMOVED AND REPLACED SPINDLE BEARING AND HOUSING.

Part: DRAG BRACE — DAMAGED (NLG)

DRAG BRACE SENT FOR REPAIR. BEARING MIGRATED FROM LOCATION CAUSING DAMAGE TO BRACE DURING GEAR ACTUATION. BEARING INSTALLED AND TESTED PER BAC OHM 32-01-03. CAUSE OF MIGRATION IS UNKNOWN.

Part: SKIN — CRACKED (NR 1 LE FLAP)

DURING ROUTINE SCHEDULED C-10 MAINTENANCE CHECK, FOUND SEVERAL SMALL CRACKS IN OUTER SKIN COMING FROM RIVETS AT CENTER INBOARD STOP MOUNT ON NR 1 SLAT. REPAIRED PER DWG 65C30133PT2. (M)

Part: FLOOR BEAM — CORRODED (BS 344)

DURING ROUTINE SCHEDULED C-10 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 344, LBL 28 TO LBL 56 IN NUMEROUS PLACES. REMOVED UPPER CHORD, FABRICATED AND INSTALLED REPLACEMENT AT BS 344, IAW SRM 53-10-51. (M)

Part: MOPSILL — CORRODED (BS 304-328)

PAE - FLT 7818 - DURING ROUTINE SCHEDULED C-10 MAINTENANCE CHECK, FOUND CORROSION ON FORWARD ENTRY DOOR MOPSILL, STATION 304-328, LBL 42. REMOVED AND REPLACED FORWARD MOPSILL, STATION 304-328, LBL 42 PER SRM 51-10-02. (M)

Part: FLOOR BEAM — CORRODED (BS 328)

PAE - FLT 7818 - DURING ROUTINE SCHEDULED C-10 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 328 - LBL 28. REPAIRED FLOOR BEAM AT BS 328, LBL 28 TO 65 PER SRM 53-10-51. (M)

Part: ACTUATOR — FAILED (NR 5 LE FLAP)

LAS/SNA - FLT 0806 - AIR TURNBACK. ON TAKEOFF FROM LAS AT 200 FEET, HAD A STICK SHAKER FOR 25 SECONDS AT 170 KIAS. LEADING EDGE FLAP ANNUNCIATOR LIGHTS FLASHING BETWEEN TRANSIT EXT. AND L/E DEVICES OVERHEAD ANNUNCIATOR PANEL SHOWED NR 5 SLAT GOING BETWEEN EXT. GREEN AND TRANS AMBER. VISUALLY, F/O SAW NR 5 SLAT MOVING ABOUT 2 INCHES FROM EVEN WITH NR 6 TO 2 INCHES EXTENDED. REMOVED AND REPLACED NR 5 SLAT ACTUATOR PER CARD R3M27020. OPS CHECKS NORMAL. PART TOTAL CYCLES, 19,667. (X)

Part: WINDOW — CRACKED (LT COCKPIT)

LAS - FLT 192 - AIR TURN BACK, CLIMBING THROUGH 18000 MSL, CAPTAINS WINDSHIELD BEGAN ARCING BADLY. THEN HEARD A DISTINCT POP AND IMMEDIATELY NOTICED A LARGE CRACK. REMOVED AND REPLACED LEFT WINDOW PER T/C R1B56001. REPLACED LEFT WINDOW CONTROLLER PER GPP. (M)

Part: CONTROLLER — MALFUNCTIONED (LT COCKPIT)

LAS - FLT 192 - AIR TURN BACK, CLIMBING THROUGH 18000 MSL, CAPTAINS WINDSHIELD BEGAN ARCING BADLY. THEN HEARD A DISTINCT POP AND IMMEDIATELY NOTICED A LARGE CRACK. REMOVED AND REPLACED LEFT WINDOW PER T/C R1B56001. REPLACED LEFT WINDOW CONTROLLER PER GPP. REFERENCE AWXA960113.

Part: WIRE — BROKEN (CABIN)

PHX - FLT 0226 - DURING ROUTINE MAINTENANCE CHECK, FOUND INTERIOR EMERGENCY LIGHTING FOR AFT DOOR EXIT PATHWAYS INOPERATIVE. REPAIRED AND REPINNED WIRE AT PIN 2. SYSTEM OPS CHECKED GOOD. (X)

Part: HOSE — FAILED (B-HYD SYSTEM)

PHX - FLT 460 - DURING FINAL APPROACH TO PHX, THE B-SYSTEM HYDRAULIC QUANTITY STARTED DECREASING. B-SYSTEM WAS SHUT DOWN AND AIRCRAFT CONTINUED TO PHX, LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED HYDRAULIC PRESSURE LINE FROM PUMP TO HYDRALIC PRESSURE MODULE. LEAK CHECK COMPLIED WITH. NO LEAKS NOTED. (M)

Part: SKIN — DAMAGED (BS 364)

PHX - DURING SCHEDULED C9 INSPECTION, FOUND LIGHTNING STRIKE DAMAGE TO SKIN THAT EXCEEDED SRM LIMITS AT STATION 364 STRINGER 6L. CLEANED AREA AND REPAIRED PER SRM 53-00-01, FIGURE 201. (M)

Part: EEL ASSY — INOPERATIVE (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE IN AFT OF AIRCRAFT. REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD. (M)

Part: EGT — HIGH (NR 2 ENGINE)

CMH - FLT 843 - THE NR 2 ENGINE HIGH EGT OCCURRED DURING TAKEOFF AND CLIMB, TEMP REACHED 936 DEGREES FOR 11 SECONDS. CREW RETURNED AC TO CMH AND LANDED UNEVENTFULLY. MX PERFORMED ENGINE PERFORMANCE GROUND RUN AND AVIONICS PERFORMED TEST OF EGT HARNESS, NO FAULTS WERE NOTED ON EITHER TEST. MX ELECTED TO DERATE BOTH ENGINES TO B1 POWER. AC RELEASED FOR FURTHER SERVICE. (W)

Part: EEL ASSEMBLY — LOOSE (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR TRACK EMERGENCY EXIT LIGHTS INOPERATIVE ROWS 11 THROUGH 15. RECONNECTED LIGHT ASSEMBLY, OPS CHECK GOOD. (X)

Part: EEL WIRE — BROKEN (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PATH EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 7 THROUGH ROW 13. REPAIRED WIRE AT ROW 7, OPS CHECK GOOD. (X)

Part: EEL ASSY — DISCONNECTED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS ROW 7 THROUGH ROW 9 INOPERATIVE. RECONNECTED LIGHTS, OPS CHECK GOOD. (M)

Part: CONNECTOR — DIRTY (COOLING FAN)

ABQ-PHX - FLT 475 - CREW REPORTED THE EQUIPMENT COOLING WAS INOPERATIVE AND ELECTED TO RETURN TO ABQ. CONTRACT MAINTENANCE FOUND EQUIPMENT COOLING NORMAL, THE SUPPLY FAN FAILED. AN UNMANNED STATION RELEASE WAS GIVEN AND THE AIRCRAFT RETURNED TO PHX. UPON ARRIVAL IN PHX, MAINTENANCE CLEANED THE CONNECTOR FOR EQUIPMENT COOLING NORMAL FAN. NO FURTHER DISCREPANCY NOTED. UNMANNED STATION RELEASE REMOVED AND AIRCRAFT RETURNED TO SERVICE. (M)

Part: POSITION — MALFUNCTIONED (TE FLAPS)

LAS-PHX - FLT 1229 - ON CLIMB-OUT, UNABLE TO RAISE FLAPS PAST FLAPS 1. AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND FLAP POSITION INDICATOR BAD. REMOVED AND REPLACED FLAP POSITION INDICATOR. FLAPS WERE CYCLED NUMEROUS TIMES AND NO MALFUNCTIONS NOTED, PER MM 27-51-00. SYSTEM OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: EEL WIRE — BROKEN (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE ROWS 9 THROUGH 11 AND FIRST CLASS. REPAIRED LIGHTS AT ROWS 9 THROUGH 11, AND RECONNECTED WIRES IN FIRST CLASS SECTION. OPS CHECK GOOD. (Z)

Part: EEL BATT PACK — DISCHARGED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHCEK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE ROWS 7 THROUGH 13. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECK GOOD. (Z)

Part: HEAT CONTROLLER — FAILED (LT WINDSHIELD)

PHX-SFO - FLT 604 - AIR TURNBACK DUE TO CAPTAIN'S WINDSHIELD OUTER PANE SHATTERED IN FLIGHT. MX REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER PER AWA TASK CARD R1B56001, OPS CHECK GOOD. ACFT RETURNED TO SERVICE. REF AWXA9500021.

Part: WINDSHIELD — BROKEN (LT COCKPIT)

PHX-SFO - FLT 604 - AIR TURNBACK DUE TO CAPTAIN'S WINDSHIELD OUTER PANE SHATTERED IN FLIGHT. MX REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER PER AWA TASK CARD R1B56001, OPS CHECK GOOD. ACFT RETURNED TO SERVICE. REF 95ZZZW