N425US

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,532 hrs · 42,403 cycles

OVERNIGHT CHECK - ALL EMERGENCY LAMPS WORKING OFF CHARGER ASSEMBLY M1137 ARE INOP. REPLACED BATTERY ASSEMBLY, CHECKS OK IAW B373 AMM 33-51-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,908 hrs · 41,981 cycles

C6 CHECK - CRACK IN FUSELAGE SKIN AT BS 882 APPROX 1 INCH ABOVE S25R. REMOVED DAMAGE, FABRICATED AND INSTALLED TEAR STRAP, FILLERS AND DOUBLER IAW B737 SRM 53-00-01-2R-31, DETAIL XIX.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 62,751 hrs · 41,880 cycles

MAINTENANCE REPORTED THE OVERWING EMERGENCY LIGHT INOPERATIVE - LEFT SIDE. MAINTENANCE REPLACED CHARGER ASSEMBLY (INCLUDING BATTERY PACK) PER AMM 33-51-51-962. OPS CHECKS OK.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 62,341 hrs · 41,630 cycles

RON - AFT GALLEY LOWER FLASHLIGHT WON'T CHARGE. REPLACED AFT GALLEY LOWER FLASHLIGHT PER B737-400 AMM 25-60-00, OPERATIONAL CHECKED GOOD.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 62,318 hrs · 41,613 cycles

CREW REPORTED DOOR 1L SLIDE PACK FALLING DOWN. MAINTENANCE REPOSITIONED 1L SLIDE PACK. CHECKS GOOD.

Part: FUSE — BLOWN (CABIN) · airframe 61,675 hrs · 41,204 cycles

MAINTENANCE REPORTED SEAT ROWS 6 THRU 9 EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED PICO FUSE IN EMERGENCY LIGHT POWER SUPPLY. OPS CHECKS OK.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 61,458 hrs · 41,071 cycles

FLIGHT ATTENDANT REPORTED A STRONG ODOR ON APPROACH. ODOR WAS STRONG AT FORWARD FLIGHT ATTENDANT JUMPSEAT AREA, COCKPIT NORMAL. MAINTENANCE FOUND APU OVERSERVICED. CLEANED AREA AND SERVICED APU. ACCOMPLISHED CABIN ODOR TROUBLESHOOTING J/C 03L00021001. OK FOR SERVICE.

Part: SEAT TRACK — LACK OF LUBE (COCKPIT) · airframe 60,686 hrs · 40,589 cycles

CREW REPORTED THE FIRST OFFICER'S SEAT IS HARD TO SLIDE FORE AND AFT. MAINTENANCE LUBED AS REQUIRED. OPS CHECK GOOD PER AMM 25-11-00.

Part: SEAT TRACK — DIRTY (COCKPIT) · airframe 60,373 hrs · 40,394 cycles

CREW REPORTED THE FIRST OFFICER'S SEAT VERY DIFFICULT TO ADJUST FORE AND AFT. MAINTENANCE CLEANED SEAT TRACK FOR FIRST OFFICER'S SEAT AND REMOVED FOOD ITEMS. SEAT OPERATES OK. AIRCRAFT OK FOR SERVICE.

Part: SEAT TRACK — DIRTY (COCKPIT) · airframe 60,278 hrs · 40,334 cycles

CREW REPORTED THE CAPTAIN'S SEAT IS VERY DIFFICULT TO ADJUST FORE AND AFT. MAINTENANCE CLEANED AND LUBED THE SEAT TRACKS. OPS CHECK NORMAL. OK FOR SERVICE.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - CRACK IN VERTICAL STIFFENER AT BS 328, RBL 32. REPLACED VERTICAL STIFFENER AT BS 328, RBL 32 IAW BOEING DRAWING 65-45812 & B737 SRM 51-10-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - CRACK ON FLOOR SUPPORT AT BS 330, LBL 46. REPLACED FLOOR SUPPORT AT BS 330, LBL 46 IAW B737 SRM 51-20-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FRAME SHEAR TIE AT BS 747, RBL 5. REPAIRED FRAME SHEAR TIE AT BS 747, RBL 5 IAW B737 SRM 53-00-02R-4 REPAIR 4.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - CRACK IN FORWARD LEFT ENTRANCE DOOR FORWARD CUTOUT FRAME WEB AT BS 303.9, S16L. REPLACED FORWARD CUTOUT FRAME WEB AT BS 303.9, S16L IAW EO 5311-01025.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FRAME AT BS 727G, BETWEEN S27L TO S27R, BL 0. REPAIRED FRAME AT BS 727G, BETWEEN S27L TO S27R, BL 0 IAW B737-400 SRM 53-00-07 REPAIR 4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 GALVANIC CORROSION ON AFT CARGO FLOOR TRACK/BEAM BS 747, RBL 14. REPAIRED AFT CARGO FLOOR TRACK/BEAM IAW BOEING DRAWING 65-53844 & B737 SRM 51-10-02 & 53-00-53 REPAIR 2.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FRAME AT BS 747, BETWEEN S26L TO S27L, LBL 8. REPAIRED FRAME AT BS 747, BETWEEN S26L TO S27L, LBL 8 IAW B737-400 SRM 53-00-07-2R-4 REPAIR 2.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON STRINGER TIE CLIP AT BS847, S25R. REPLACED STRINGER TIE CLIP AT BS847, S25R IAW B737 SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE AT BS 787 BETWEEN BL 0 TO LBL 4. REPLACED SHEAR TIE AT BS 787 BETWEEN BL 0 TO LBL 4 IAW B737 SRM 51-00-07 REPAIR 4.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON STRINGER AT BS 927, S21R. REPAIRED STRINGER BETWEEN BS 907 TO BS 935, S21R IAW B737 SRM 53-00-03, FIG 201, REPAIR 1.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE AT BS 907 BETWEEN S27L TO S27R. REPLACED SHEAR TIE AT BS 907 BETWEEN S27L TO S27R IAW B737 SRM 51-00-07 REPAIR 3.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON INTERCOSTAL WEB BETWEEN BS 767 TO BS 787, RBL 6. REPLACED INTERCOSTAL WEB BETWEEN BS 767 TO BS 787, RBL6 IAW B737 SRM 51-40-02.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON AFT FRAME AT AFT CARGO DOOR CUTOUT AT BS 847, RBL 22. REPLACED AFT FRAME AT AFT CARGO DOOR CUTOUT AT BS 847, RBL 22 IAW B737-400 SRM 51-10-02.

Part: STRAP — CORRODED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - CORROSION ON FUSELAGE SKIN STRAP BETWEEN BS 907 TO BS 927 & BETWEEN S26L TO S26R. REPLACED FUSELAGE SKIN STRAP BETWEEN BS 907 TO BS 927 & BETWEEN S26L TO S26R IAW B737 SRM 53-00-01 REPAIR 31, DETAIL XXI.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - CRACK ON VERTICAL STIFFENER AT BS 328, LBL 47. REPLACED VERTICAL STIFFENER AT BS 328, LBL 47 IAW SRM 51-10-02 & BOEING DRAWING 65-45812.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 GALVANIC CORROSION ON DOUBLER FOR PHONE ANTENNA AT BS 786 + 6 INCHES. DOUBLER FOR PHONE ANTENNA AT BS 786 + 6 INCHES IAW B737 SRM 53-00-01 FIG 101.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - CRACK ON STRINGER AT BS 1011, S7L. REPLACED STRINGER AT BS 1011, S7L IAW BOEING DRAWING 65-52988 & SRM 51-10-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON AFT CARGO FLOORBEAM/TRACK CHANNEL AT BS 727F + 6 INCHES, LBL 3. REPAIRED AFT CARGO FLOORBEAM/TRACK CHANNEL IAW EA 103284.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - .50 INCH CRACK ON FRAME AT BS 500E, BETWEEN S20L TO S21L, WL 182.5. REPAIRED FRAME AT BS 500E, BETWEEN S20L TO S21L, WL 182.5 IAW SRM 53-00-07, REPAIR 13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - .75 INCH CRACK ON FRAME AT BS 500F, BETWEEN S20L TO S21L, WL 182. REPAIRED FRAME AT BS 500F, BETWEEN S20L TO S21L, WL 182 IAW SRM 53-00-07.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - 0.5 INCH CRACK ON FRAME AT BS 500C, BETWEEN S20R TO S21R, WL 182.5. REPAIRED FRAME AT BS 500C, BETWEEN S20R TO S21R, WL 182.5 IAW SRM 53-00-07, REPAIR 13.

Part: FLAP — DELAMINATED (LT WING) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - DELAMINATION ON LEFT OUTBOARD MID FLAP AT LOWER TRAILING EDGE 18 INCHES FROM EDGE OF AFT FLAP & 13 INCHES FROM LEADING EDGE. REPLACED LEFT OUTBOARD MID FLAP IAW JOB CARD 03C30727030.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 GALVANIC CORROSION ON STIFFNER AT BOTH LOWER CORNERS OF APU INLET CUTOUT AT INBOARD SIDE BETWEEN BS 1116 TO BS 1126, S17R. REPLACED STIFFENER AT BOTH LOWER CORNERS OF APU INLET CUT-OUT IAW BOEING DRAWING 65-46579.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - CRACK ON FUSELAGE SKIN AT AFT ENTRY UPPER DOOR HINGE CUTOUT AT BS 948, S20L. REPAIRED FUSELAGE SKIN AT AFT ENTRY UPPER DOOR HINGE CUTOUT IAW B737 SRM 53-60-01.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SHEAR TIE AT BS 947 BETWEEN S19L TO S20L, LBL 49. REPLACED SHEAR TIE AT BS 947 BETWEEN S19L TO S20L, LBL49 IAW B737 SRM 51-20-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - 2 CRACKS ON FUSELAGE SKIN AT MAIN ENTRY LOWER DOOR HINGE CUTOUT AT BS 303.9 BELOW S9L. REPAIRED FUSELAGE SKIN AT MAIN ENTRY LOWER DOOR HINGE CUTOUT IAW TEMPORARY REVISION SRM 53-30 & B737-400 SRM 53-10-01 REPAIR 14.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - CRACK ON FUSELAGE SKIN AT FORWARD SERVICE DOOR LOWER HINGE CUTOUT AT BS 291.5. REPAIRED FUSELAGE SKIN AT FORWARD SERVICE DOOR LOWER HINGE CUTOUT IAW EA 103271.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - CORROSION ON FLOOR SUPPORT INTERCOSTAL BETWEEN BS 328 TO BS 344, RBL 11. REPLACED FLOOR SUPPORT INTERCOSTAL BETWEEN BS 328 TO BS 344, RBL 11 IAW B737 SRM 53-10-51 & SRM 51-10-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN BS 335 TO BS 339, RBL 23. REPLACED FLOORBEAM BETWEEN BS 335 TO BS 339, RBL 23 IAW B737 SRM 53-00-52.

Part: TRIM TAB — DELAMINATED (AILERON) · airframe 60,229 hrs · 40,304 cycles

Q5 CHECK - RIGHT AILERON TAB AFT CORNER DELAMINATED. REPLACED RIGHT AILERON TAB IAW B737 AMM 27-11-11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - CRACK ON FRAME AT BS 500F BETWEEN S20R TO S21R, WL 182.5. REPAIRED FRAME AT BS 500F, BETWEEN S20R TO S21R, WL 182.5 IAW B737-400 SRM 53-00-07 REPAIR 13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - CRACK ON FRAME AT BS 500E, BETWEEN S20R TO S21R, WL 182.5. REPAIRED FRAME AT BS 500E, BETWEEN S20R TO S21R, WL 182.5 IAW B737-400 SRM 53-00-07 REPAIR 13.

Part: SKIN — DELAMINATED (RUDDER) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - DELAMINATION ON RIGHT SIDE OF RUDDER EXTERIOR SKIN 38 INCHES FROM BOTTOM & 4 INCHES AFT OF FORWARD SPAR. REPAIRED RIGHT SIDE OF RUDDER EXTERIOR SKIN IAW EA 103256B & B737 SRM 51-70-17.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - CORROSION ON VERTICAL STIFFENER AT AFT SIDE OF APU INLET AT BS 1147, RBL 15. REPLACED VERTICAL STIFFENER AT AFT SIDE OF APU INLET IAW B737 SRM 51-10-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - 0.5 INCH CRACK ON FRAME AT BS 520, BETWEEN S20L TO S21L, WL 182.5. REPAIRED FRAME AT BS 520, BETWEEN S20L TO S21L, WL 182.5 IAW SRM 53-00-07, REPAIR 13.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON STRINGER AT BS 847, S22R. REPLACED STRINGER BETWEEN BS 847 TO BS 905, S22R IAW B737 SRM 53-60-03, FIG 1, DETAIL II & SRM 51-10-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - CRACK ON STUB BEAM / FRAME INNER CHORD AT BS 616, WL 208, LBL 70.85. REPAIRED STUB BEAM / FRAME INNER CHORD AT BS 616, WL 208, LBL 70.85 IAW TYPICAL REPAIR TR 737-5362-10-0023.

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON LEFT STABILIZER SKIN UPPER SURFACE TRAILING EDGE BEAM COVER AT STAB STA 176.64. REPAIRED LEFT STABILIZER SKIN UPPER SURFACE TRAILING EDGE BEAM COVER IAW B737 SRM 55-10-13.

Part: SKIN — CRACKED (LE SLAT) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - MULTIPLE CRACKS ON NR 6 SLAT LOWER LEADING EDGE SKIN SURFACE JUST FORWARD OF INBOARD AUX TRACK. REPAIRED NR 6 SLAT LOWER LEADING EDGE SKIN IAW B737 SRM 57-43-0, REPAIR 6.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - .050 INCH CRACK ON FRAME AT BS 380, BETWEEN S8R TO S9R. REPAIRED FRAME AT BS 380, BETWEEN S8R TO S9R IAW EA 103250.

Part: SKIN — CRACKED (LE SLAT) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - MULTIPLE CRACKS ON NR 5 SLAT LOWER LEADING EDGE SKIN SURFACE JUST FORWARD OF INBOARD AUX TRACK. REPAIRED NR 5 SLAT LOWER LEADING EDGE SKIN IAW B737 SRM 57-43-0, REPAIR 6.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - 2 CRACKS IN FUSELAGE SKIN AT BS 278.5 BETWEEN S28L & S28R AT EQUIPMENT COOLING EXHAUST PORT CUTOUT. REPAIRED FUSELAGE SKIN AT EQUIPMENT COOLING EXHAUST PORT CUTOUT IAW EA 103255.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - CRACK ON FUSELAGE FRAME AT BS 500A BETWEEN S8L TO S9L. REPAIRED FUSELAGE FRAME AT BS 500A BETWEEN S8L TO S9L IAW EA 103250.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - .25 INCH CRACK ON FRAME AT BS 727B, BETWEEN S8L TO S9L. REPAIRED FRAME AT BS 727B, BETWEEN S8L TO S9L IAW EA 103250.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - .25 INCH CRACK IN FRAME AT BS 727B, BETWEEN S8R TO S9R. REPAIRED FRAME AT BS 727B, BETWEEN S8R TO S9R IAW EA 103250.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE AT BS 927 BETWEEN S27L TO S27R. REPLACED SHEAR TIE AT BS 927 BETWEEN S27L TO S27R IAW B737 SRM 51-00-07 REPAIR 4.

Part: SKIN — CRACKED (ENTRY DOOR) · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - 3 CRACKS ON MAIN ENTRY DOOR ON INNER SKIN AT NR 5, 6, & 7 STOPS BS 1147, RBL 15. REPAIRED MAIN ENTRY DOOR ON INNER SKIN IAW EA 103251.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON STRINGER AT BS410, S23R. REPAIRED STRINGER AT BS410, S23R IAW B737 SRM 53-00-03 REPAIR 1.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FRAME AT BS 747, BETWEEN S27L TO S27R, RBL 4. REPAIRED FRAME AT BS 747, BETWEEN S27L TO S27R, RBL4 IAW B737-400 SRM 53-00-07-2R-4-REPAIR 2.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON WEB BETWEEN BS 927 TO BS 947, S21L. REPLACED WEB BETWEEN BS 927 TO BS 947, S21L IAW B737-400 SRM 53-00-03 BOEING DRAWING 65-45856.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON Z-ANGLE BETWEEN BS 312 TO BS 370, S17L. REPLACED Z-ANGLE BETWEEN BS 312 TO BS 370, S17L IAW SRM 51-10-02 & 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM UPPER T-CAP AT BS 344 & BETWEEN RBL 67 TO LBL 67. REPAIRED FLOORBEAM UPPER T-CAP AT BS 344 & BETWEEN RBL 67 TO LBL 67 IAW B737 SRM 53-10-51, REPAIR 5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 INTERGRANULAR & EXFOLIATION CORROSION IN MULTIPLE AREAS OF FLOORBEAM UPPER CHORD AT BS 270, WL 208 BETWEEN LBL 18.750 TO RBL 18.50. REPAIRED FLOORBEAM UPPER CHORD AT BS 270, WL 208 BETWEEN LBL 18.750 TO RBL 18.50 IAW EA 103283.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON Z-ANGLE BETWEEN BS 290 TO BS 350, S17R, RBL 62. REPLACED Z-ANGLE BETWEEN BS 290 TO BS 350, S17R, RBL 62 IAW SRM 51-10-02 & 51-40-03.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON Z-ANGLE BETWEEN BS 976 TO BS 986, LBL 43. REPLACED Z-ANGLE BETWEEN BS 976 TO BS 986, LBL 43 IAW B737 SRM 51-10-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM UPPER T-CAP AT BS 986.5 & BETWEEN RBL 51 TO LBL 51. REPAIRED FLOORBEAM UPPER T-CAP AT BS 986.5 & BETWEEN RBL 51 TO LBL 51 IAW B737 SRM 53-00-51, REPAIR 2.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,222 hrs · 40,296 cycles

Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON INTERCOSTAL AT BS 947+10.5 INCHES, LBL 49. REPLACED INTERCOSTAL AT BS 947+10.5 INCHES, LBL 49 IAW B737 SRM 53-60-51.

Part: CSD — LEAKING (NR 1 ENGINE)

CLT - CREW REPORTED A STRANGE ODOR (DIRTY SOCK SMELL) IN COCKPIT AND CABIN DURING LAST 30 MINUTES OF FLIGHT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED BOROSCOPE OF BOTH ENGINES AND TROUBLESHOOTING TASK CARD 03L00021001 CABIN ODOR CHECKLIST. FOUND NR 1 ENGINE CSD WITH OIL LEAK. REMOVED AND REPLACED CSD PER MM 24-11-11. OPERATIONAL CHECK AND LEAK CHECK GOOD. ALSO, REMOVED AND REPLACED HEPA FILTERS AS PRECAUTIONARY. AIRCRAFT OK FOR SERVICE.

Part: EXTRACTOR — SATURATED (AC BAY)

CLT - EN ROUTE BDL TO CLT, CREW REPORTED THAT DURING TAKEOFF AND LANDING, A VERY STRONG SMELL OF DIRTY SOCKS WAS PRESENT IN THE COCKPIT. SMELL WAS NOT AS NOTICEABLE DURING CRUISE. FLIGHT LANDED WITHOUT INCIDENT IN CLT. MAINTENANCE COMPLIED WITH JOB CARD 03L00021001. FOUND RESIDUAL WATER RETAINED IN EXTRACTOR. REPOSITIONED VALVE. REMOVED WATER. REPLACED FILTERS. OPERATIONAL CHECK GOOD.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 59,020 hrs · 39,567 cycles

PIT - MAJOR REPAIR - FWD PRESSURE BULKHEAD INSP - CRACKED WEB AT BS 179.75, LBL 17, WL 230. REPAIRED WEB AT BS 179.75, LBL 17, WL 230 IAW B737 SRM 53-10-08.

Part: FITTING — CRACKED (FUSELAGE) · airframe 59,020 hrs · 39,567 cycles

PIT - MAJOR REPAIR - FWD PRESSURE BULKHEAD INSP - CRACKED SKIN CLIP AT BS 294.5, S11L. REPLACED SKIN CLIP AT BS 294.5, S11L IAW B737 SRM 53-10-15.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 59,020 hrs · 39,567 cycles

PIT - MAJOR REPAIR - FWD PRESSURE BULKHEAD INSPECTION - 03-0553-8-0349, CRACKED BULKHEAD WEB AT BS 178, LBL 11.5, WL 234. REPAIRED BULKHEAD WEB AT BS 178, LBL 11.5, WL 234 IAW B737 SRM 53-10-08.

Part: SKIN — CORRODED (FUSELAGE) · airframe 58,091 hrs · 38,991 cycles

CLT - RON - MAJOR REPAIR - CRACK ON FUSELAGE SKIN AT BS 727F, S23R. REPAIRED FUSELAGE SKIN AT BS 727F, S23R IAW B737 SRM 53-00-01 REPAIR 31.

Part: SKIN — CORRODED (FUSELAGE) · airframe 58,091 hrs · 38,991 cycles

CLT - RON - MAJOR REPAIR - CRACK ON FUSELAGE SKIN AT BS 727E, S24R. REPAIRED FUSELAGE SKIN AT BS 727E, S24R IAW B737 SRM 53-00-01 REPAIR 31.

Part: BULKHEAD — CORRODED (FUSELAGE)

MIA - C20 - MAJOR REPAIR - AFT PRESSURE BULKHEAD LOWER FORWARD WEB HAS CORROSION FROM BL 0 ANGLE STIFFENER TO LBL 6, AT BS 1016, WL 196. REPAIRED AFT PRESSURE BULKHEAD LOWER FORWARD WEB AT BS 1016 BETWEEN BL 0 TO LBL 6, WL 196 IAW TYPICAL REPAIR 53-83-01.

Part: WIRE — BROKEN (CABIN)

DCA - MAINTENANCE REPORTED THE OVERHEAD EMERGENCY LIGHT HAS A BROKEN WIRE BY SEAT ROW 5. MAINTENANCE REPAIRED WIRE AT EMERGENCY LIGHT ASSEMBLY REF: WDM 20-10-13.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

BDL - MAINTENANCE REPORTED SEVERAL EMERGENCY LIGHTS IN THE AFT SECTION OF THE CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY ALONG WITH THE BATTERY PACK. OPERATIONAL CHECK GOOD. REF: MM 33-51-51.

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - MAINTENANCE REPORTED THE AFT SECTION OF THE CABIN HAS SEVERAL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK BAD. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

PIT - DURING WEEKLY CHECK, MAINTENANCE REPORTED THE EMERGENCY PATH LIGHTS AT SEAT ROWS 20, 21, 22 AND 23 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,020 hrs · 39,567 cycles

PIT - MAJOR REPAIR - FWD PRESSURE BULKHEAD INSP - CRACKED INTERCOSTAL AT BS 294.5, S12L. REPLACED INTERCOSTAL AT BS 294.5, S12L IAW B737 SRM 53-10-15.

Part: BATTERY PACK — DISCHARGED (CABIN)

BDL - MAINTENANCE REPORTED THE EMERGENCY LIGHTS ON SEATS 20 THRU 23 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT BATTERY PACK M1197. OPERATIONAL CHECK NORMAL PER MM 33-51-51.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,823 hrs · 37,573 cycles

PIT - SEAT MOD - MAJOR REPAIR - CRACK ON FUSELAGE FRAME AT BS 440, S24R. REPAIRED FUSELAGE FRAME AT BS 440, S24R IAW EA 113834.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,823 hrs · 23,992 cycles

PIT - MAJOR REPAIR - SEAT MODIFICATION - CRACKED FRAME AT BS 440, S24R. REPAIRED FRAME AT BS 440, S24R IAW EA 113834.

Part: CONNECTOR — DISCONNECTED (CABIN)

DFW - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 12 AND 16, LEFT SIDE, INOPERATIVE. MAINTENANCE FOUND THE CONNECTOR DISCONNECTED AT SEAT 16. RECONNECTED CONNECTOR AT SEAT 12. MAINTENANCE FOUND THE WIRE DISCONNECTED. RECONNECTED WIRE/BUTT SPLICE PER SWP CHAPTER 20. OPERATIONAL CHECK OF LIGHTS GOOD.

Part: ANGLE — CRACKED (RT WING) · airframe 50,034 hrs · 50,034 cycles

ON RIGHT WING, LOWER -T- CRACKED AT WBL 135.5. REMOVED & REPLACED WING LOWER ANGLE PER EA 98794, DEFECT SIZE: .75 INCH.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHTS)

CLT - MAINTENANCE REPORTED THE L1 DOOR OVERHEAD INTERIOR EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPAIRED WIRING TO REFLECT 737 WDM 33-51-12. OPERATIONAL CHECK GOOD.

Part: FUSE — BLOWN (EMERGENCY LIGHTS)

CLT - MAINTENANCE REPORTED THE R2 DOOR EXTERIOR ESCAPE SLIDE EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY FUSE. OPERATIONAL CHECK GOOD.

Part: WIRE — SHORTED (EMERGENCY LIGHTS)

CLT - MAINTENANCE REPORTED THE AFT CABIN EMERGENCY LIGHTS AT SEAT ROWS 24 AND 25 INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLIES ON SEAT ROWS 24 AND 25 DUE TO SHORTED WIRING. REPAIRED WIRING. ALSO, REPLACED FUSE IN POWER SUPPLY. OPERATIONAL CHECK GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

BS 907 FRAME AT A/C RAIL ATTACH POINT BETWEEN STRINGERS 8L & 9L CRACKED. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER TR 53-10-20E, DEFECT SIZE: .5 INCH.

Part: BUSHING — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 50,034 hrs · 50,034 cycles

BUSHING, VERT STAB LEFT AFT O/B ATTACH FITTING FWD FACE LUG L-5 HAS CORROSION. REMOVED CORROSION, INSTALLED NEW BUSHINGS PER EA 98801; CORR LEVEL 2; TASK C55-706-11, DEFECT SIZE: .25 INCH.

Part: LUG — GOUGED (VERTICAL STAB) · airframe 50,034 hrs · 50,034 cycles

AFT FACE OF L-8 LUG OF VERTICAL FIN GOUGED. REMOVED DAMAGED BUSHING, PITTING & REPLACED BUSHING PER EA 98801. CORROSION RESULT OF GOUGE. DEFECT SIZE: .250 INCH.

Part: BUSHING — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 50,034 hrs · 50,034 cycles

R5 O/B AFT ATTACH FITTING FWD FACE OF BUSHING PITTED, R5 LUG HAS CORROSION. REMOVED BUSHING, CORROSION & INSTALLED NEW BUSHING PER EA 98801; CORR TSK C55-706-11, DEFECT SIZE: .250 X .250 INCH.

Part: LUG — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 50,034 hrs · 50,034 cycles

PITTED & CORRODED VERT FWD FACE OF L4 LUG ON FUSELAGE. REMOVED BUSHING & BLENDED LUG TO REMOVE CORROSION, TREATED & REPLACED PER EA 98800; CORR TASK C55-70, DEFECT SIZE: .25 INCH.

Part: LUG — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 50,034 hrs · 50,034 cycles

PITTING ON FWD FACE OF L6 LUG ON FUSELAGE CORRODED. REMOVED BUSHING, CLEANED CORROSION & RE-INSTALLED PER EA 98800; CORR TSK C55-706-11, DEFECT SIZE: .25 INCH.

Part: BUSHING — CORRODED (ELEVATOR) · corrosion level 2 · airframe 50,034 hrs · 50,034 cycles

RIGHT AFT I/B ATTACH FITTING FUW FACE OF BUSHING PITTED & CORRODED, R-8 LUG. REMOVED BUSHING, LUG BORE, FACES CLEANED, INSTALLED NEW BUSHING PER EA 98801; CORR TASK C55-706-11, DEFECT SIZE: .250 X .250 INCH.

Part: BUSHING — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 50,034 hrs · 50,034 cycles

RIGHT HORIZ STAB INTERSPAR BOX STAB STA 0, R7 LUG BORE HAS CORROSION. FAB'D BUSHING INSTALLED INTO BORE PER SRM 55-10-10; CORR TASK C53-701-02, DEFECT SIZE: .25 INCH.

Part: BRACKET — CORRODED (LT LAVATORY) · corrosion level 2 · airframe 50,034 hrs · 50,034 cycles

LEFT LAV TIE DOWN BRACKET STA 947 LBL 51 CORRODED AROUND MOUNT HOLES. REMOVED & REPLACED TIE DOWN BRACKET; CORR TASK C53-107-01; LEVEL 2, DEFECT SIZE: .250 INCH.

Part: LUG — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 50,034 hrs · 50,034 cycles

FWD FACE OF L8 LUG ON VERT FIN CORRODED & LITE GOUGE. FAB'D BUSHING PER EA 98801; CORR TASK C55-706-11, DEFECT SIZE: .25 X .25 INCH.

Part: BUSHING — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 50,034 hrs · 50,034 cycles

LEFT STAB INTERSPAR BOX STAB STA 0, NR 7 LEFT LUG HAS CORROSION. FAB'D BUSHING INTO REWORKED BORE PER SRM 55-10-10, SB 737-55-1058, CORR LEVEL 2; TASK C53-701-02, DEFECT SIZE: .25 INCH.

Part: DOOR FRAME — CRACKED (DOOR) · airframe 50,034 hrs · 50,034 cycles

CUTOUTS FOR THE 3RD & 4TH STOPS DOWN FROM TOP, AFT SIDE OF DOOR CRACKED. FAB'D & INSTALLED REPAIR DOUBLERS PER TR52-10-11, DEFECT SIZE: .025 INCH.

Part: LUG — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 50,034 hrs · 50,034 cycles

AFT FACE OF L6 LUG ON FUSELAGE VERT STAB LUG CORRODED. REMOVED LUG BUSHING, CORROSION, TREATED & REPLACED PER EA 98800; CORR TASK C55-706-11, DEFECT SIZE: .25 INCH.

Part: BUSHING — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 50,034 hrs · 50,034 cycles

LEFT STAB INTERSPAR BOX TAB STA 0, BUSHING/BORE NR 9 LEFT LUG HAS CORROSION. FAB'D BUSHING, INSTALLED INTO REWORKED BORE PER SRM 55-10-10, SB 737-55-1058; CORR LEVEL 2, DEFECT SIZE: .25 INCH.

Part: BUSHING — DAMAGED (VERTICAL STAB) · corrosion level 2 · airframe 50,034 hrs · 50,034 cycles

AFT FACE OF BUSHING, FWD FACE OF R8 LUG ON VERT FIN PITTED. REMOVED PITTING & INSTALLED NEW BUSHING PER EA 98801; CORR TASK C55-706-11, DEFECT SIZE: .250 X .250 INCH.

Part: LUG — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 50,034 hrs · 50,034 cycles

RIGHT AFT I/B ATTACH FITTINGG FUW FACE OF BUSHING R8 LUG ON VERT FIN HAS CORROSION. FAB'D BUSHING & INSTALLED PER SOMP 20-50-03 BOEING DWG 65-52274; EA 98801; CORR TASK C55-706-01, DEFECT SIZE: .250 X .250 INCH.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,034 hrs · 50,034 cycles

NUT PLATE HOLE, RBL 12, STA 987 CORRODED. REMOVED & REPAIRED T-CAP AREA PER SRM 53-00-01; CORR TASK C53-107-01, DEFECT SIZE: 2 X INCHES.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,034 hrs · 50,034 cycles

STA 950 LBL 51, INTERCOSTAL HAS CORROSION. REMOVED & REPLACED INTERCOSTAL; CORR TASK C53-107-01; LEVEL 2, DEFECT SIZE: 3 INCHES.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

RIGHT SIDE OF 178 BULKHEAD, JUST TO LEFT OF BOTTOM RIGHT INSPECTION HOLE OIL CANNING. FAB'D NEW DOUBLER & FILLERS PER SRM 53-10-08 FIG 201, DEFECT SIZE: 18 X 12 INCHES.

Part: LUG — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 50,034 hrs · 50,034 cycles

VERT FWD FACE OF LUG R4 ON FUSELAGE AT 4:00 POSITION HAS CORROSION. REMOVED CORROSION REAMED BORE, CHAMFERED EDGES, INSTALLED NEW BUSHING PER EA 98800; CORR TASK C55-70, DEFECT SIZE: .25 INCH.

Part: BUSHING — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 50,034 hrs · 50,034 cycles

BUSHING & FLANGE, VERT AFT FACE OF R5 LUG ON FUSELAGE AT 5:00-9:00 POSITION HAS CORROSION. REPLACE FLANGE BUSHING, BLENDED FLANGE TO REMOVE DAMAGE TREATED PER EA 98800; CORR TASK C55-706-01, DEFECT SIZE: .25 INCH.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

STA 400 STR 4L HAS CRACK. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-10-02, DEFECT SIZE: 1 INCH.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

BS 685 S-4R HAS CRACK. REPLACED STRINGER TIE CLIP PER SRM 51-40-02, DEFECT SIZE: .250 INCH.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

RIGHT SIDE OF 178 BULKHEAD, LEFT OF BOTTOM RIGHT INSPECTION HOLE HAS OIL CANNING. FAB'D NEW DOUBLERS, FILLERS & INSTALLED PER SRM 53-10-08 FIG 201 REPAIR 9, DEFECT SIZE: 18 X 12 INCHES.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,034 hrs · 50,034 cycles

LEFT Z-ANGLE AT AFT ENTRY DOOR BETWEEN STA 947 & 986 CORRODED. REPLACED Z-ANGLE PER SRM 51-20-01, 51-40-03; CORR TASK C53-701-01; LEVEL 2, DEFECT SIZE: 3 X 36 INCHES.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

RIGHT STA 727A, STR 6, STRINGER TIE CLIP CRACKED. REMOVED & REPLACED CLIP PER SRM 51-40-02, DEFECT SIZE: 1 INCH.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

BS 420, S-4L, CRACKS AT STRINGER TO TIE CLIP ATTACH FASTENER HOLES. INSTALLED REPAIR FILLER, ANGLES & NEW TIE CLIP, DEFECT SIZE: .5 & .25 INCH.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

STA 907 STR 4L, STRINGER SPLICE CRACKED. INSTALLED REPAIR PARTS PER SRM 51-10-02, DEFECT SIZE: .5 INCH.

Part: WEB — CRACKED (AFT CARGO DOOR) · airframe 50,034 hrs · 50,034 cycles

AFT CARGO DOOR, FWD FRAME, LOWER CLOSEOUT WEB CRACKED. FAB'D NEW WEB PER BOEING DWG 65-53583, SRM 51-19-02, DEFECT SIZE: 1 INCH.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

STA 706 RBL 24 CRACKED. INSTALLED FABRICATED REPAIR PART PER SRM 51-40-02, DEFECT SIZE: 1 INCH.

Part: STOP FITTING — CRACKED (SERVICE DOOR) · airframe 50,034 hrs · 50,034 cycles

CUTOUTS OF THE 3RD & 4TH STOPS DOWN FROM THE TOP, AFT SIDE OF FWD SERVICE DOOR CRACKED. INSTALLED REPAIR DOUBLERS PER TR 52-10-11, DEFECT SIZE: .025 INCH.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 50,034 hrs · 50,034 cycles

PYLON NR 1 ENGINE UNER PANEL 5727 HAS CRACK. STOP DRILLED & INSTALLED DOUBLER PER TR 54-30-07, DEFECT SIZE: 1 INCH.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

STA 277 STR 15R HAS CRACK. FAB'D & REPLACED STRINGER CLIP PER BOEING DWG 69-37272, SRM 51-20-01, DEFECT SIZE: 1 INCH.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

STA 303, STR 7R - 8R FWD UPPER CORNER OF DOOR CUTOUT ON AIRFRAME CORNER FITTING CRACKED. REMOVED & REPLACED CORNER FITTING, DEFECT SIZE: .5 INCH.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

TIE CLIP AT STA 706 STR 10-L CRACKED. REMOVED & REPLACED TIE CLIP PER SRM 51-10-02, DEFECT SIZE: 1 INCH.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

TIE CLIP, STR 25L AT BS 807 CRACKED. REMOVED & REPLACED TIE CLIP PER SRM 51-20-01, DEFECT SIZE: 1 INCH.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

BACKSIDE OF 178 BULKHEAD AT DEAD CENTER OF BULKHEAD FLOORLINE LEVEL, SUPPORT ANGLE CRACKED. FAB'D NEW ANGLE & INSTALLED PER BOEING DWG 3-94762, DEFECT SIZE: .25 INCH.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

INTERCOSTAL, STA 294.5, STR 11L CRACKED. INSTALLED FABRICATED REPAIR PARTS PER SRM 51-20-01, DEFECT SIZE: 3 INCHES.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

STA 907 BETWEEN STR 8L & 9L AT A/C RAIL ATTACH POINT CRACKED. REMOVED & INSTALLED REPAIR PARTS PER TR 53-10-20E, DEFECT SIZE: .25 INCH.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

BS 685 S-4R HAS CRACK. REPLACED STRINGER TIE CLIP PER SRM 51-40-02, DEFECT SIZE: .250 INCH.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

BS 827 FRAME CRACKED BETWEEN STR 8L & 9L. ALL WORK REPAIRED IAW TR 53-10-20E, DEFECT SIZE: .25 INCH.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

BS 328 & LBL 45 CRACKED. REMOVED & REPLACED INTERCOSTAL PER SRM 51-70-11, DEFECT SIZE: 1 INCH.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 50,034 hrs · 50,034 cycles

NR 2 PYLON AFT I/B ANGLE CRACKED. INSTALLED FABRICATED REPAIR PART PER SRM 51-10-02; 51-20-01, BOEING DWG 65-26300-29, DEFECT SIZE: 2 INCHES.

Part: FLOOR SKIN — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

STA 663, LBL 32 FLOOR SKIN AT AILERON QUADRANT CRACKED. INSTALLED REPAIR DOUBLER & SHIMS PER TR 53-60-04, DEFECT SIZE: .5 INCH.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

BS 328 FLOORBEAM AT LBL 45, VERTICAL STIFFENER / INTERCOSTAL ATTACH ANGLE CRACKED. FAB'D NEW STIFFENER & INSTALLED PER DWG 65-45812, SRM 51-10-02, DEFECT SIZE: 1 INCH.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

STA 500G BL 0, SHEAR WEB TOP FLOOR ANGLE CRACKED. REMOVED CRACKED METAL MADE REPAIR, TREATED & PRIMED PER SRM 51-70-13, DEFECT SIZE: 1 INCH.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

BS 178 WL 216 LBBL 12, 178 BULKHEAD WEB CRACK. INSTALLED DOUBLER & FILLER PER SRM 53-10-08, FIG 201 REPAIR 9, DEFECT SIZE: 5 INCHES.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,034 hrs · 50,034 cycles

STA 400 STR 4R CRACKED. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-10-02, DEFECT SIZE: 1 INCH.

Part: BUSHING — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 50,034 hrs · 50,034 cycles

RIGHT HORIZ STAB INTERSPAR BOX STAB STA 0, BUSHING, R9 LUG BORE CORRODED. FABRICATED BUSHING, INSTALLED INTO BORE PER SRM 55-10-10; CORR TASK C53-701-02; LEVEL 2, DEFECT SIZE: .25 INCH.

Part: CIRCUIT BREAKER — FAULTY (COCKPIT)

CLT FLT1053 JUST AFTER TAKEOFF FROM CLT, EN ROUTE TO NAS, CREW COULD NOT RAISE THE LANDING GEAR HANDLE. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND THEN RAISED THE GEAR. FOUND THE -LANDING GEAR LATCH & PRESSURE WARNING- CIRCUIT BREAKER POPPED. CONSULTED WITH DISPATCH AND MAINTENANCE AND RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE -LANDING GEAR LATCH & PRESSURE WARNING- CIRCUIT BREAKER C00129. ACCOMPLISHED MAIN AND NOSE LANDING GEAR EXTENSION AND RETRACTION CHECKS PER MM 32-32-00-715 AND MM 32-33-00-735. OPERATIONAL CHECK GOOD.

Part: FAN — FAILED (AVIONICS BAY)

CLT - FLT945 - EN ROUTE FROM ROC TO CLT, CREW REPORTED EXHAUST FUMES IN CABIN AND FLIGHT DECK. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT RECIRCULATION FAN INOPERATIVE DURING OPERATIONAL CHECK. REPLACED THE LEFT RECIRCULATION FAN AND VENTILATION FILTERS. SYSTEM CHECKS GOOD. RAN AIR FOR EXTENDED TIME. NO ODORS NOTED.

Part: WIRE — SHORTED (FWD LAVATORY)

CLT - FLT1831 EN ROUTE FROM ALB TO CLT, CREW REPORTED NUMEROUS CIRCUIT BREAKERS ASSOCIATED WITH THE FORWARD LAVATORY POPPED IN FLIGHT. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT CLT. MAINTENANCE FOUND THE FORWARD LAVATORY FLUSH MOTOR WIRING SHORTED BEHIND TRASH CABINET RESULTING IN COLLATERAL DAMAGE TO LAV SPEAKER, LAV CALL AND FLUORESCENT LIGHT BALLAST WIRING. REPAIRED ALL AFFECTED WIRING IAW WEBER CMM 25-47-91 AND SWPM 20-10-13. ALL BUNDLES PROTECTED AND SECURED. ALL FORWARD LAVATORY SYSTEMS OPERATE NORMALLY INCLUDING OPERATIONAL CHECK OF FLUSH MOTOR. ACCOMPLISHED SATISFACTORY PA SYSTEM OPERATIONAL TEST PER MM 23-31-00. AIRCRAFT OK FOR SERVICE.

Part: SHUTOFF VALVE — FAULTY (MLG)

ON LANDING IN MIA, CREW REPORTED BOTH LEFT MAIN LANDING GEAR TIRES BLEW. THE LT MAIN LANDING GEAR CAUGHT FIRE, WHEREAS, TRUCKS WERE DISPATCHED AND THE FIRE WAS EXTINGUISHED. PASSENGERS WERE EVACUATED VIA THE EMERGENCY ESCAPE SLIDES, AND TRANSPORTED TO THE TERMINAL. NO INJURIES WERE REPORTED. MAINTENANCE ACCOMPLISHED LEFT MLG TIRE BURST FERRY FLIGHT PREPARATION. AIRCRAFT WAS THEN MAINTENANCE FERRIED GEAR DOWN TO CLT. MAINTENANCE IN CLT TROUBLESHOT SYSTEM AND FOUND A FAULTY PARKING BRAKE SHUTOFF VALVE. THE VALVE HAD NO GROUND AT D1040, PIN 15. REPLACED SHUTOFF VALVE AND PERFORMED SATISFACTORY ADJUSTMENT TEST PER MM 32-42-00. OPERATIONAL CHECK GOOD. IN ADDITION, REPLACED DAMAGED LEFT MLG TIRE/WHEEL ASSEMBLIES

Part: SKIN — CRACKED (L/E SLAT) · airframe 47,800 hrs · 47,800 cycles

FOUND CRACK NR 1 SLAT SKIN 43" INBOARD FROM INBOARD END ON LOWER SURFACE. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-43-01, DEFECT SIZE: .25".

Part: SKIN — CHAFED (MID FLAP) · airframe 47,800 hrs · 47,800 cycles

FOUND CHAFED AREA RIGHT OUTBOARD MID FLAP AT INBOARD END OF LEADING EDGE. FABRICATED AND INSTALLED DOUBLER IAW SRM 57-53-01 REPAIR 8 DEFECT SIZE: 4" BY .4" BY .025".

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 47,653 hrs · 47,653 cycles

FOUND CRACK RT HORIZ STAB LOWER SKIN STAB STA 160. INSTALLED DOUBLER IAW TR 55-10-07, DEFECT SIZE: 1.75".

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 47,653 hrs · 47,653 cycles

FOUND FRAME CRACKED BS 492.4 S-24R AT DOORSTOP FOOTPRINT. CUT OUT DAMAGE, FABRICATED REPAIR DOUBLERS IAW EA 97947, DEFECT SIZE: .6".

Part: ENGINE — FAILED (RIGHT)

PHL - FLT1447 - ON CLIMB-OUT FROM PHL, AT 12,000 FT, THE NR 2 ENGINE LOST THRUST AND WENT TO IDLE. PARTIAL THRUST CAME BACK BUT DECREASED AGAIN ON APPROACH. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT PHL. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE ON IT'S OWN POWER. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE ASSEMBLY. OPERATIONAL CHECK AND LEAK CHECK GOOD.

Part: SKIN — DENTED (FUSELAGE)

CLT - Q - SKIN, 2 INCH X 3 INCH DENT, BS328 AND S23R. REPAIR DOUBLER IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

CLT - MAINTENANCE REPORTED THE MAIN ENTRY DOOR OVERHEAD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD LEFT EMERGENCY LIGHT BATTERY PACK FOR THE MAIN ENTRY DOOR OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT)

BDL - MAINTENANCE REPORTED THE AFT RIGHT EXERIOR OVERWING EMERGENCY LIGHT BECAME INOPERATIVE WHEN RESTORING WIRING TO PROPER CONFIGURATION FROM A PREVIOUS EMERGENCY LIGHT PROBLEM AT SEAT ROW 11ABC. MAINTENANCE REPLACED SECTION OF DAMAGED WIRE W1150-029-020 IN ASSOCIATION WITH BOEING WIRING SPM, CHAPTER 20. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD. (M)

Part: LIGHT — INOPERATIVE (ROW 11)

BWI - MAINTENANCE FOUND THE EMERGENCY EXIT IDENTIFIER LIGHT AT SEAT ROW 11, LEFT SIDE, INOPERATIVE. MAINTENANCE ACTION PENDING. (M)

Part: CHARGER — FAILED (EMERGENCY LIGHT)

MAINTENANCE REPORTED NUMEROUS EMERGENCY LIGHTS, THROUGHOUT THE INTERIOR CABIN, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY PACK. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

PHL - MAINTENANCE REPORTED THE EMERGENCY EXIT SIGN AT SEAT ROW 11C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

CLT - MAINTENANCE REPORTED THE INTERIOR EMERGENCY EXIT MARKER LIGHT AT SEAT ROW 11 ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD. (M)

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT)

BDL - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHTS, AT SEAT ROWS 10 AND 11ABC, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER FUSE, AT STATION 598, ABOVE SEAT ROW 11 DEF. ALSO, REPLACED BATTERY PACK ASSEMBLY, P/N 2013-1A. OPS CHECK GOOD. (M)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

BDL - MAINTENANCE REPORTED THE EMERGENCY ROW IDENTIFIER LIGHTS AT SEAT ROWS 10 AND 11, LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 BATTERY CHARGER ASSEMBLY AT STATION 598. OPS TEST OF EMERGENCY LIGHTS GOOD. (M)

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT)

MAINTENANCE REPORTED THE AFT RIGHT EMERGENCY ESCAPE LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TEH 5 AMP FUSE IN POWER SUPPLY M1479. OPS CHECK GOOD. (M)

Part: WIRE — DAMAGED (EMERGENCY LIGHT)

MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEATS 10ABC AND 11ABC INOPERATIVE. MAINTENANCE REPAIRED WIRE AT LIGHT ON SEAT 11ABC. OPS CHECK GOOD. (M)

Part: FRAME — CRACKED (FUSELAGE)

FOUND FRAME CRACKED .75 INCH, STATION 360 1 INCH BELOW STRINGER 14R CLIP. REPAIRED PER SRM 53-00-07. (M)

Part: ANGLE — CORRODED (FUSELAGE)

FOUND Z-ANGLE CORRODED IN SEVERAL AREAS 1 INCH AREA OF CORROSION, L26L BS 787 TO BS 898. CORRODED LEVEL 1, TASK NR C53-202-01. REPLACED Z-ANGLE FROM BS 727D TO BS 898 PER SRM 53-60-03. (M)

Part: CHARGER — FAILED (EMERGENCY LIGHT)

MAINTENANCE REPORTED THE LEFT MID-CABIN CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY PER MM 33-51-51. OPS CHECKS GOOD. (M)

Part: SKIN — CRACKED (FUSELAGE)

CLT - FOUND SKIN CRACKED 2.2 INCH, BELOW S23R AT STATION 727D. INSTALLED DOUBLER PER T/R 53-60-03. (M)

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS)

ALB - FLT 1057 - ON APPROACH INTO ALB, FROM CLT, CREW RECEIVED A TWO DEGREE FLAP ASYMMETRY INDICATION. CREW DECLARED AN EMERGENCY AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. ON TAXI TO THE GATE, THE FLAP PROBLEM CORRECTED ITSELF. MAINTENANCE OPERATED FLAPS THROUGH ENTIRE RANGE. INSPECTED JACKSCREW ASSEMBLIES, TRACK ASSEMBLIES AND ATTACHMENT POINTS. NO DISCREPANCIES NOTED. SYSTEM OPERATES NORMAL. (M)

Part: CHARGER — INOPERATIVE (CABIN)

CLT - PILOT REPORTED THAT THE EMERGENCY EXIT LIGHTS FLASH OFF AND ON DURING FLIGHT. LIGHTS STOP FLASHING WHEN CYCLED ON, OFF AND BACK TO ARMED POSITION. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT BATTERY CHARGER ASSEMBLY AND BATTERY PACK. SYSTEM OPERATIONALLY CHECKS GOOD PER MM 33-51-02. (M)

Part: CHARGER — FAILED (CABIN)

PHL - MAINTENANCE REPORTED THE AFT RIGHT SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT EMERGENCY LIGHT BATTERY PACK AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

DCA - MAINTENANCE REPORTED THE RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1479 BATTERY SUPPLY PACK AT STATION 598R. OPERATIONAL CHECK GOOD. (M)

Part: FCU — MALFUNCTIONED (APU)

BNA - FLT 1577 - EN ROUTE CLT TO MCI, CAPTAIN ADVISED CLIMBING FROM FL 310 TO FL 350 WHEN APU GEN DROPPED OFF-LINE AT FL 330. WITH LT GEN ALREADY ON MEL, CAPTAIN DESCENDED FLIGHT BACK DOWN TO FL 310, VOLTS INDICATED OK BUT FREQUENCIES INDICATING ZERO. DESCENDED FLT DOWN TO FL 280, NO CHANGE. RESETTING C/B'S HAD NO EFFECT. FLT DIVERTED BNA, LANDED WITHOUT INCIDENT. NO EMERG DECLARED. MAINT REMOVED, REPLACED APU FCU PER MM 49-31-11 DUE LOW FREQ. APU, APU GEN OPER CHK GOOD. FOUND NR 1 ENG GEN BREAKER C801 FAULTY. REMOVED, REPLACED NR 1 ENG GEN BREAKER (PN 941D335-4) PER MM 24-21-41, CLEARED MEL. REMOVED, REPLACED NR 1, NR 2 ENG GEN CONTROL UNITS (PN 915F212-5) PER MM 24-21-81. OPER CHKS NORMAL. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA - MAINTENANCE FOUND SEVERAL LOW LEVEL EMERGENCY EXIT LIGHTS IN THE CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK ON THE M1645 BATTERY MODULE. OPERATIONAL CHECK GOOD. (M)

Part: CHARGER — FAILED (CABIN)

CLT - MAINTENANCE FOUND THE MID-CABIN CEILING EMERGENCY EXIT SIGN, LEFT HAND SIDE, WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (X)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

CLT - FOUND ATTACH ANGLE CRACKED .75 INCH, STATION 290, WL 241 RIGHT SHEAR WEB OUTBOARD. REPAIRED PER SRM 51-40-02. (M)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

CLT - FOUND ATTACH ANGLE CRACKED .75 INCH, STATION 290, WL 249 RIGHT SHEAR WEB OUTBOARD. REPAIRED PER SRM 51-40-02. (M)

Part: FRAME — CRACKED (FUSELAGE)

CLT - FOUND FRAME CRACKED .75 INCH, BS 601, BELOW STRINGER 17L, LBL 66. INSTALLED FILLER AND DOUBLER PER TR 53-62-01 AND EA 66517. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

CLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 11 INCHES, STATION 947 FROM RBL 6 - LBL 5 FLOOR LEVEL. INSTALLED NEW T-CAP AND ANGLE PER SRM 53-00-51. (M)

Part: ANGLE — CRACKED (FUSELAGE)

CLT - FOUND ANGLE CRACKED .75 INCH, STATION 290, WL 259, RIGHT SIDE SHEAR WEB OUTBOARD ANGLE. REPAIRED PER SRM 51-40-02. (M)

Part: FRAME — CRACKED (FUSELAGE)

CLT - FOUND FRAME CRACKED .5 INCH BETWEEN STRINGER 8R AND 9R BS 867. INSTALLED DOUBLER PER TR 53-10-14. (M)

Part: FRAME — CRACKED (FUSELAGE)

CLT - FOUND FRAME CRACKED .5 INCH, BS 727F BETWEEN STRINGER 8R AND 9R. INSTALLED FILLER AND ODUBLER PER TR 53-10-14. (M)

Part: BULKHEAD — CRACKED (FUSELAGE)

CLT - FOUND BULKHEAD WEB CRACKED 1 INCH, STATION 178 RBL 5 BETWEEN WL 202 AND 203. INSTALLED DOUBLER PER TR 53-10-07. (M)

Part: FRAME — CRACKED (FUSELAGE)

CLT - FOUND FRAME BS 907 CRACKED .5 INCH, BETWEEN STRINGER 8R AND 9R. INSTALLED FILLER AND DOUBLER PER TR 53-10-14. (M)

Part: FRAME — CRACKED (FUSELAGE)

CLT - FOUND FRAME CRACKED .5 INCH, BS 867 BETWEEN STRINGER 8L AND 9L. INSTALLED FILLER AND DOUBLER. (M)

Part: FRAME — CRACKED (FUSELAGE)

CLT - FOUND FRAME CRACKED, BS 787 BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER SRM 53-10-14. (M)

Part: FRAME — CRACKED (BS 727)

CLT - FOUND FRAME CRACKED .5 INCH, BS 727F BETWEEN STRINGER 8L AND 9L. INSTALLED FILLER AND DOUBLER PER TR 53-10-14. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .75 INCH, STATION 947, STRINGER 27L. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02 PAGE 18. (M)

Part: BULKHEAD — CRACKED (FUSELAGE)

CLT - FOUND BULKHEAD WEB CRACKED 1.5 INCHES, STATION 178 RBL 5 BETWEEN WL 197.5 AND 199. INSTALLED DOUBLER PER TR 53-10-07. (M)

Part: BULKHEAD — CRACKED (FUSELAGE)

CLT - FOUND BULKHEAD WEB CRACKED .5 INCH, STATION RBL .5, WL 188. INSTALLED BULKHEAD WEB PER SRM 53-10-08. (M)

Part: FRAME — CRACKED (FUSELAGE)

CLT - FOUND FRAME CRACKED .5 INCH, BS 827 BETWEEN 8R AND 9R. INSTALLED FILLER AND DOUBLER PER TR 53-10-14. (M)

Part: FRAME — CRACKED (FUSELAGE)

CLT - FOUND FRAME CRACKED .5 INCH, BS 747 BETWEEN STRINGER 8R AND 9R. INSTALLED FILLER AND DOUBLER PER TR 53-10-14. (M)

Part: FRAME — CRACKED (FUSELAGE)

CLT - FOUND FRAME CRACKED .5 INCH, BS 727D BETWEEN STRINGER 8R AND 9R. INSTALLED FILLER AND DOUBLER PER TR 53-10-14. (M)

Part: PLATE — CORRODED (FUSELAGE)

CLT - FOUND CORROSION ON SILL PLATE 1 INCH BY 24 INCHES, BS 959 TO 983 FLOOR LEVEL. REPAIRED PER 51-10-02. CORROSION LEVEL 1. (M)

Part: FRAME — CRACKED (FUSELAGE)

CLT - FOUND FRAME CRACKED .5 INCH, BS 500A BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)

Part: ANGLE — CORRODED (FUSELAGE)

CLT - FOUND Z-ANGLE CORRODED 2 INCHES BY 24 INCHES, BS 951 TO 975. REPAIRED PER 51-10-01. (M)

Part: FRAME — CRACKED (FUSELAGE)

CLT - FOUND FRAME CRACKED .5 INCHES, BS 400 BETWEEN STRINGER 8R AND 9R. INSTALLED FILLER AND DOUBLER PER TR 53-10-14. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CLT - FOUND FLOOR SUPPORT CORRODED 2 INCHES BY 2 INCHES, BS 951 AND 953 LBL 24. REPAIRED PER 51-10-02. CORROSION LEVEL 1. (M)

Part: FRAME — CRACKED (FUSELAGE)

CLT - FOUND FRAME CRACKED .5 INCH, BS 400 BETWEEN STRINGER 8L AND 9L. INSTALLED FILLER AND DOUBLER PER TR 53-10-14. (M)

Part: FRAME — CRACKED (FUSELAGE)

CLT - FOUND FRAME CRACKED .5 INCH, BS 440 BETWEEN STRINGER 8L AND 9L. INSTALLED DOULBER PER TR 53-10-14. (M)

Part: FRAME — CRACKED (FUSELAGE)

CLT - FOUND FRAME CRACKED .5 INCH, BS 727D, BETWEEN STRINGER 8L AND 9L. INSTALLED FILLER AND DOUBLER PER TR 53-10-14. (M)

Part: ANGLE — CORRODED (FUSELAGE)

CLT - FOUND CORROSION ON Z-ANGLE 2 INCHES BY 45 INCHES, BS 951 TO 996. REPAIRED PER 51-10-02. (M)

Part: BATTERY — DISCHARGED (CABIN)

ALB - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOP AT THE FORWARD FIRST CLASS SEATS (ROWS 1 AND 2) AND ABOVE THE FORWARD SERVICE DOOR. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AND BATTERY CHARGER. OPERATIONAL CHECK GOOD. (M)

Part: CHARGER — FAILED (CABIN)

ALB - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOP AT THE FORWARD FIRST CLASS SEATS (ROWS 1 AND 2) AND ABOVE THE FORWARD SERVICE DOOR. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AND BATTERY CHARGER. OPERATIONAL CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

CLE - MAINTENANCE FOUND THE AFT LEFT EMERGENCY EXIT LIGHT BATTERY PACK INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK NORMAL. (X)

Part: BATT CHARGER — FAILED (CABIN)

PHL - MAINTENANCE FOUND THE OVERWING MID AISLE EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY PACK, CHECKS OK. (M)

Part: FLOOR BEAM — CORRODED (BS 947)

INT - DURING 'Q-1' CHECK VISUAL INSPECTION, FOUND 4 AREAS 1 INCH BY 1 INCH CORRODED AREAS FLOOR BEAM BS 947, LBL 4 - RBL 11. INSTALLED T-CAP AND REPAIR ANGLES. REPAIRED PER SRM 53-00-051 AND EA 40947. (X)

Part: FLOOR BEAM — CORROSION (BS 344)

INT - DURING 'Q-1' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA BS 344 FLOOR BEAM LBL 9 INCH AND LBL 21 INCH. INSTALLED T-CAP FROM RBL 17 TO LBL 36, REPAIRED PER T.R. 53-10-03. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. (X)

Part: FLOOR BEAM — CORROSION (BS 328)

INT - DURING 'Q-1 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 2 INCH CORRODED AREAS BS 328 FLOOR BEAM, RBL 14 INCH TO RBL 56 INCH. SPLICED SECTION AND REPAIRED PER SRM 53-10-01. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)

Part: FLOOR BEAM — CORRODED (BS 312)

INT - DURING 'Q-1' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA, BS 312, FLOOR BEAM BL ZERO. CUT OUT CORRODED SECTION OF UPPER CHORD FROM LBL 38 TO RBL 25 AND SPLICED IN NEW CHORD SECTION. REPAIRED PER T.R. 53-10-03. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)

Part: FLOOR BEAM — CORRODED (BS 986.5)

INT - DURING 'Q-1' CHECK, VISUAL INSPECTION FOUND 10 AREAS 1 - 2 INCH SQUARES OF CORROSION FLOOR BEAM (FLOOR BOARD HOLES) BS 986.5, RBL 46 - LBL 46. CUT OUT CORRODED UPPER T-CAP AND REPLACED T-CAP, PLACING A SPLICE AT LBL 7, REPAIRED PER EA 40946. (X)

Part: FLOOR BEAM — CORRODED (BS 967)

INT - DURING 'Q-1' CHECK VISUAL INSPECTION, FOUND .75 INCH CORROSION FLOOR BEAM BS 967, RBL 42. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED REPAIR ANGLES AND FILLER. REPAIRED PER SRM 53-60-51, FIGURE 203. (X)