N418US

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 70,954 hrs · 46,264 cycles

DISCREPANCY: L-2 DOOR EMERGANCY BATTERY DOSE NOT HOLD CHARGE. CORRECTIVE ACTION: REMOVE AND REPLACED BATTERY PACK IAW B737-AMM 33-51-51 TEST OKAY IAW AMM 33-51-51.

Part: WIRE — BROKEN (CABIN) · airframe 70,461 hrs · 46,025 cycles

EMERGENCY EXIT LIGHTS ON SEAT ROWS 14-22 INOP. TROUBLESHOT IAW WDM 33-57-42, FOUND BROKEN WIRE AT CONNECTOR D3686. REPAIRED BROKEN WIRE IAW SWPM 20-30-02, TEST GOOD IAW AMM 33-37-02.

Part: POWER SUPPLY — INOPERATIVE (ZONE 100) · airframe 68,370 hrs · 45,036 cycles

LEFT FUSELAGE AFT LOWER EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY AT BS 753, OPERATIONAL CHECKED GOOD, IAW AMM 33-51-51

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 67,871 hrs · 44,814 cycles

SEAT MOUNTED AISLE LOCATOR LIGHTS INOPERATIVE ON RT SEAT ROWS 11 THROUGH 21. REPLACED THE BATTERY PACK.

Part: SEAL — LOOSE (CABIN PRESSURE) · airframe 67,693 hrs · 44,735 cycles

CABIN ALTITUDE WARNING AT 36,000 FEET. AIRCRAFT CABIN ALTITUDE WAS SHOWING 13,000 FEET.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 66,401 hrs · 44,031 cycles

DURING EMERGENCY LIGHT TEST, ROW 6-10 FAILED TO ILLUMINATE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,351 hrs · 42,989 cycles

EMERGENCY EXIT LIGHTS AT R2 DOOR INOPERATIVE. REPLACED POWER SUPPLY 2012-1, OFF SN 3980 ON SN 40617. OPS CHECKED GOOD UPON REPLACEMENT.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 64,004 hrs · 42,822 cycles

L1 DOOR SLIDE WAS IN ADVERTENTENLY DEPLOYED. SLIDE WAS REPLACED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,383 hrs · 42,393 cycles

C3 CHECK - BULKHEAD INTERCOSTAL CORRODED AT BS 227.8 AND BL 0. REMOVED AND REPLACED INTERCOSTAL IAW B737 DRAWINGS 69-38740 & 6545801-512 AND B737 SRM 53-10.

Part: SPAR — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 63,383 hrs · 42,393 cycles

C3 CHECK - VERTICAL STABILIZER REAR SPAR CORRODED FROM FIN STATION 219.5 TO FIN STATION 228. REMOVED CORROSION IAW EA 502578.

Part: CONNECTOR — LOOSE (CABIN) · airframe 63,383 hrs · 42,393 cycles

R2 DOOR EMERGENCY LIGHT'S ARE INOP. SECURED CONNECTOR ON R2 DOOR EMERGENCY LIGHT IAW B737 AMM 33-51-02.

Part: CONNECTOR — LOOSE (CABIN) · airframe 63,383 hrs · 42,393 cycles

EPL SEAT 25, 24, 21 AND 2 EMERGENCY LIGHT'S INOP. SECURED CONNECTOR ON SEAT 25, 24 ,21, 2 OF EPL IAW B737 AMM 33-51-02.

Part: CONNECTOR — LOOSE (CABIN) · airframe 63,383 hrs · 42,393 cycles

C3 CHECK - RIGHT OVERWING AFT EMERGENCY LIGHT INOP. SECURED CONNECTOR ON RIGHT OVERWING AFT EMERGENCY LIGHT IAW B737 AMM 33-51-02.

Part: POWER SUPPLY — DEFECTIVE (CABIN) · airframe 63,384 hrs · 42,393 cycles

C3 CHECK, EMERGENCY LIGHT POWER SUPPLIES M1197 AND M1479 UNABLE TO SECURE BATTERIES. REMOVED AND REPLACED POWER SUPPLIES IAW B737 AMM 33-51-51-962-016. POWER SUPPLIES TESTED GOOD IAW WITH B737 AMM 33-51-51.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,001 hrs · 42,154 cycles

C2 CHECK - FUSELAGE SKIN CRACED AT BS 727G + 5 IN, S24L. REPAIRED SKIN IAW EA 202937.

Part: SKIN — CRACKED (FUSELAGE) · airframe 627 hrs · 42,008 cycles

RON VISIT - CRACK IN FUSELAGE SKIN AT BS 727F, S25R. REPAIRED FUSELAGE SKIN AT BS 727F, S25R IAW B737 SRM 53-00-01-2R-31 DETAIL XIX.

Part: COVER — INTERFERENCE (COCKPIT) · airframe 62,756 hrs · 42,008 cycles

CREW REPORTED THE FAIRING ON LEFT SIDE CO-PILOT RUDDER PEDAL ADJUSTMENT PEDESTAL INTERFERES WITH RUDDER PEDAL MOVEMENT. MAINTENANCE REMOVED AND RE-INSTALLED FIRST OFFICERS RUDDER PEDAL COVER PER AMM 27-21-31-084-040. NO RUBBING OR BINDING NOTED. OK FOR SERVICE.

Part: TIRE — BLOWN (RT MLG) · airframe 62,740 hrs · 41,996 cycles

FLIGHT RETURNED TO FIELD DUE TO NR 3 RIGHT INBOARD TIRE BLOWN ON TAKEOFF. CREW DECLARED AN EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 3 WHEEL/TIRE ASSEMBLY WITH NEW. REFERENCE AMM 32-45-11-004-001 & 32-45-11-4004-014 AND AMM 05-51-54-212-023. ALSO, REPLACED NR 4 WHEEL/TIRE ASSEMBLY AND NR 3 AND NR 4 BRAKE ASSEMBLIES. REPLACED DAMAGED RIGHT WING I/B T/E AFT FLAP AND MID FLAP SEAL PLATE DUE TO NR 3 TIRE DEBRIS. AIRCRAFT OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 62,516 hrs · 41,851 cycles

CREW REPORTED AN ODOR IN THE AFT GALLEY DURING FLIGHT CAUSING FLIGHT ATTENDANT TO BECOME ILL. APU NOT RUNNING. RECIRC FANS TURNED OFF. SMELL PROGRESSED TO SEAT ROW 22 AND STOPPED. MAINTENANCE ACCOMPLISHED CABIN ODOR JOB CARD 03L00021001. NO DEFECTS FOUND. REPLACED HEPA FILTERS PER AMM 21-21-23. ALSO ACCOMPLISHED TASK 21-00-01-102-001 FOR OIL CONTAMINATION REMOVAL. OPS CHECK OK. NO ODOR NOTED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 62,382 hrs · 41,764 cycles

MAINTENANCE REPORTED SEAT 4A EMERGENCY LIGHT LENS MISSING. MAINTENANCE INSTALLED LENS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,214 hrs · 41,672 cycles

RON VISIT - 3 INCH CRACK IN FUSELAGE SKIN AT BS 727E+4 INCHES, S23L. REPAIRED FUSELAGE SKIN AT BS 727E+4 INCHES, S23L IAW B737 SRM 53-00-01 REPAIR 31 DETAIL XI.

Part: COVER — CRACKED (EXIT SIGN) · airframe 62,087 hrs · 41,586 cycles

CREW REPORTED THE LENS COVER FOR EXIT SIGN AT ROW 12 WAS BROKEN. MAINTENANCE REPLACED CRACKED COVER. CHECKS OK AT ROW 12 LEFT SIDE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,211 hrs · 41,055 cycles

MAINTENANCE REPORTED THE EMERGENCY LIGHT INOPERATIVE AT SEAT ROW 25ABC. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 25ABC. OPS CHECK GOOD.

Part: LENS — DETACHED (CABIN) · airframe 61,080 hrs · 40,968 cycles

CREW REPORTED THE EMERGENCY EXIT SIGN AT SEAT ROW 12, AIRCRAFT LEFT, WAS DETACHED. MAINTENANCE RE-INSTALLED EMERGENCY EXIT SIGN LENS AT SEAT ROW 12, AIRCRAFT LEFT.

Part: SIGN — OUT OF POSITION (CABIN) · airframe 60,738 hrs · 40,751 cycles

CREW REPORTED THE EMERGENCY EXIT SIGN FROM SEAT ROW 12 ABC FELL OFF. MAINTENANCE REINSTALLED EMERGENCY EXIT SIGN ON SEAT ROW 12ABC.

Part: APU — FAILED (APU BAY) · airframe 60,646 hrs · 40,697 cycles

CREW REPORTED THE APU FIRE LITE ILLUMINATED CLIMBING THROUGH 25,000 TO 26,000 FEET. CREW ACCOMPLISHED QRH PROCEDURE. EGT WAS IN THE RANGE ON A RUNNING APU BUT SWITCH TO APU WAS IN THE OFF POSITION FOR OVER 15 TO 20 MINUTES. APU FIRE LIGHT BEGAN TO GO OUT AND EGT DECREASED AFTER FIRE HANDLE WAS PULLED AND FIRED. FLIGHT RETURNED TO FIELD AT DCA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TESTED APU FIRE DETECTION SYSTEM. TESTED GOOD PER AMM 26-15-00, DID IT'S JOB AND DETECTED TAIL FIRE. FOUND APU EGT HARNESS CHARED. REPLACED APU PER J/C 03L70349004. OPS AND LEAK CHECK GOOD. ALSO, REPLACED APU FIRE EXTINGUISHER BOTTLE PER AMM 26-22-11. AIRCRAFT OK FOR SERVICE.

Part: UNKNOWN — FUMES (CABIN) · airframe 60,616 hrs · 40,677 cycles

CAPTAIN ADVISED DISPATCH THAT THEY WERE DECLARING AN EMERGENCY INBOUND TO PIT AFTER A FLIGHT ATTENDANT REPORTED THAT THERE WERE FUMES OF SOME TYPE IN THE CABIN. THE FLIGHT LANDED WITHOUT INCIDENT. FLIGHT ATTENDANTS WENT TO THE HOSPITAL AS A PRECAUTION. MAINTENANCE ACCOMPLISHED CABIN ODOR J/C 03L00021001. NO ABNORMAL ODORS FOUND IN FORWARD, MID, AFT CABIN OR GALLEYS. ACCOMPLISHED HIGH POWER ENGINE RUN WITH ALL BLEEDS AND AIR PACKS. ALL CHECK OK INCLUDING PRESSURIZATION. PERFORMED TEST FLIGHT. TEST FLIGHT PASSED.

Part: LENS — BROKEN (EXIT SIGN) · airframe 60,611 hrs · 40,673 cycles

CLT - SEAT 12C EXIT SIGN BROKEN. INSTALLED LENS FOR EMERGENCY EXIT SIGN AT SEAT 12C. OK FOR CONTINUED SERVICE.

Part: WEDGE — DEBONDED (TE FLAP) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - DISBONDING ON RIGHT INBOARD AFT FLAP LOWER TRAILING EDGE WEDGE IN 2 PLACES. REPLACED RIGHT INBOARD AFT FLAP IAW JOB CARDS 03C40927012 & 03C40927009.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - CRACK ON STRINGER CLIP AT BS 380, S22L. REPLACED STRINGER CLIP AT BS 380, S22L IAW B737 SRM 51-10-02.

Part: SPOILER — DELAMINATED (LT WING) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - DELAMINATION ON LEFT WING NR 1 SPOILER AT UPPER AFT CORNER AT WS 425. REPLACED LEFT WING NR 1 SPOILER IAW B737 AMM 27-62-91.

Part: SPAR — DAMAGED (HORIZ STAB) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - ELONGATED FASTENER HOLES ON LEFT HORIZONTAL STABILIZER FORWARD UPPER SPAR CHORD AT BS 1104, HHS175.5. REPAIRED FASTENER HOLES ON LEFT HORIZONTAL STABILIZER FORWARD UPPER SPAR CHORD AT BS 1104, HHS175.5 IAW EA 103156.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - PREVIOUSLY BLENDED AREA OF FUSELAGE SKIN IS OUT OF LIMITS AT BS312, S24R. REPAIRED FUSELAGE SKIN IAW B737 SRM 53-00-01 REP 31, FIG 201 DETAIL XII.

Part: TRIM TAB — CORRODED (ELEVATOR) · corrosion level 2 · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON RIGHT ELEVATOR TRIM TAB MAST FITTING. REPLACED RIGHT ELEVATOR TRIM TAB IAW JOB CARD 03C71227004.

Part: TRIM TAB — CRACKED (ELEVATOR) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - 4 CRACKS ON LEFT ELEVATOR TRIM TAB 3 & 4 HINGE CUTOUTS. REPLACED LEFT ELEVATOR TRIM TAB IAW JOB CARD 03C71127007.

Part: SKIN — DELAMINATED (ELEVATOR) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - DELAMINATION ON LEFT ELEVATOR LOWER SKIN AT TAB CONTROL ROD CUTOUT. REPLACED LEFT ELEVATOR IAW JOB CARD 03C71127007.

Part: TORQUE SHAFT — CORRODED (MIDFLAP) · corrosion level 2 · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON RIGHT INBOARD MID FLAP INBOARD TORQUE SHAFT. REPLACED RIGHT INBOARD MID FLAP IAW JOB CARD 03C40927012 & 03C40927009.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - CRACK ON SKIN DOUBLER AT AIR CONDITIONING HOOK-UP CUTOUT AT BS 520 BETWEEN S28L TO S28R, BL 0. REPAIRED SKIN DOUBLER AT AIR CONDITIONING HOOK-UP CUT-OUT IAW EA 103155.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON VERTICAL STIFFENER AT BS 1124 BETWEEN S13L TO S17L AT APU INLET CUTOUT (INSIDE TORQUE BOX). REPLACED VERTICAL STIFFENER IAW B737 SRM 51-40-02, 51-10-02 & BOEING DRAWING 65-46579.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - CRACK ON STUB FRAME INNER CHORD AT BS 616 BETWEEN S17R TO S18R. REPAIRED STUB FRAME INNER CHORD AT BS 616 BETWEEN S17R TO S18R IAW EA 103107 & TYPICAL REPAIR 737-5362-10-0023.

Part: SKIN — CRACKED (ENTRY DOOR) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - CRACK IN FORWARD ENTRY DOOR SKIN AT AFT TRACE BEAM UNDER NR 6 STOP FITTING. REPAIRED FORWARD ENTRY DOOR SKIN AT AFT TRACE BEAM UNDER NR 6 STOP FITTING IAW EA 103142A.

Part: BEAM — CRACKED (ENTRY DOOR) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - CRACK IN FORWARD ENTRY DOOR AT AFT TRACE BEAM AT NR 11 & NR 12 STOP FITTING ACCESS HOLES. REPAIRED FORWARD ENTRY DOOR AT AFT TRACE BEAM AT NR 11 & NR 12 STOP FITTING ACCESS HOLES IAW EA 103142A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - CRACKS ON FUSELAGE FRAME AT BS 380, BETWEEN S20L TO S23L. REPAIRED FUSELAGE FRAME AT BS 380, BETWEEN S20L TO S23L IAW EA 103130.

Part: SKIN PANEL — WORN (FUSELAGE) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - WORN SKIN PANEL AT RIGHT STABILIZER HINGE JOINT AT BS 1142, STR 12R+ 6 INCHES. REPLACED SKIN PANEL AT RIGHT STABILIZER HINGE JOINT AT BS 1142, STR 12R+ 6 INCHES IAW B737 SRM 51-40-05, B737 SRM 51-40-08, BOEING DRAWING 65-48240.

Part: FASTENER — LOOSE (TE FLAP) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - APPROX 50 LOOSE & WORKING FASTENERS IN LEADING EDGE OF RIGHT OUTBOARD FORE FLAP SKIN. REPLACED RIGHT OUTBOARD FORE FLAP IAW JOB CARDS 03C40727020 & 03C40727016.

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON LEFT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM COVER AT STAB STA 200. REPAIRED LEFT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM COVER AT STAB STA 200 IAW B737 SRM 55-10-13 REPAIR 3.

Part: STRAP — CRACKED (FUSELAGE) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - CRACK ON STRAP BELOW LEFT HORIZONTAL STABILIZER AT BS 1183.6, RBBL 40. REPAIRED STRAP BELOW LEFT HORIZONTAL STABILIZER AT BS 1183.6, RBBL 40 IAW B737 SRM 53-00-01 FIG 201 REPAIR 22.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - CRACK IN FORWARD LEFT ENTRY DOOR FRAME WEB DOUBLER AT LOWER DOOR STOP FITTING AT BS 303.9, S16L. REPLACED FORWARD LEFT ENTRY DOOR FRAME WEB IAW EO 5311-01025.

Part: FASTENER — LOOSE (FOERFLAP) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - LOOSE FASTENERS ON LEFT OUTBOARD FOREFLAP BETWEEN WBL 202.60 TO WBL 414.40. REPLACED LEFT OUTBOARD FOREFLAP BETWEEN WBL 202.60 TO WBL 414.40 IAW JOB CARDS 03C30727030 AND 03C30727026.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - DELAMINATION ON NR 5 SLAT SKIN AT LOWER TRAILING EDGE 5 INCHES FROM OUTBOARD END. REPAIRED NR 5 SLAT SKIN AT LOWER TRAILING EDGE 5 INCHES FROM OUTBOARD END IAW EA 103090.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - CRACK ON FRAME AT BS 500E, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME AT BS 500E, BETWEEN STR 20R TO STR 21R IAW B737 SRM 53-00-07 REPAIR 13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,443 hrs · 40,460 cycles

Q3 CHECK - CRACKS ON FRAME AT BS 500B, STR 20L. REPAIRED FRAME AT BS 500B, STR 20L IAW B737 SRM 53-00-07R13.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON Z-ANGLE AT BS 970, RBL 50. REPLACED Z-ANGLE AT BS 970, RBL 50 IAW B737 SRM 51-10-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,443 hrs · 40,460 cycles

CLT - Q4 CHECK, CRACK ON AFT PRESSURE BULKHEAD SKIN AT BS 1016, STR 6R. REPAIRED AFT PRESSURE BULKHEAD SKIN AT BS 1016, STR 6R IAW B737-400 SRM 53-80-08 REPAIR 7.

Part: HINGE FITTING — WORN (ELEVATOR) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - WORN HINGE FITTING ON ELEVATOR HINGE LINE AT STABILIZER STATION 258. REPLACED HINGE FITTING ON ELEVATOR HINGE LINE AT STABILIZER STATION 258 IAW B737 SRM 51-40-02, BAC DRAWING 65C25144.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,443 hrs · 40,460 cycles

CLT - Q4 CHECK - CRACK ON FRAME AT BS 500B, BETWEEN STR 19R TO STR 22R. REPAIRED FRAME AT BS 500B, BETWEEN STR 19R TO STR 22R IAW B737-400 SRM 53-00-07, REPAIR 13.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON APU INLET TORQUE BOX ANGLE BETWEEN BS 1114 TO BS 1120. REPAIRED APU INLET TORQUE BOX ANGLE BETWEEN BS 1114 TO BS 1120 IAW EA 103102.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON AFT CARGO LOWER SILL THRESHOLD WEB BETWEEN BS 807 TO BS 827+10 INCHES, RBL 27.5. REPLACED AFT CARGO LOWER SILL THRESHOLD WEB IAW B737 SRM 53-60-15 FIG 101 DETAIL L VIIL.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON IFPC ANTENNA DOUBLER AT BS 754, BL 0. REPLACED IFPC ANTENNA DOUBLER AT BS 754, BL 0 IAW EA 103188.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON AFT CARGO FLOOR TRACK BEAM AT BS 727F, RBL 13.8. REPLACED AFT CARGO FLOOR TRACK BEAM AT BS 727F, RBL 13.8 IAW B737 SRM 53-00-53 REPAIR 2.

Part: TIE CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,443 hrs · 40,460 cycles

CLT - Q4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON STRINGER TIE CLIP AT BS 323, STR 28R. REPAIRED STRINGER TIE CLIP AT BS 323, STR 28R IAW B737-400 SRM 53-00-03 REPAIR 1.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON ZEE ANGLE BETWEEN BS 767 TO BS 794, RBL 22. REPLACED ZEE ANGLE BETWEEN BS 767 TO BS 794, RBL 22 IAW B737 SRM 51-10-02.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - EXFOLIATION CORROSION ON PREVIOUSLY BLENDED UPPER CHORD TCAP AT BS 334, WL 208, BETWEEN LBL 33 TO RBL 68. REPLACED UPPER CHORD TCAP AT BS 334, WL 208, BETWEEN LBL 33 TO RBL 68 IAW B737 SRM 53-10-51, FIG 201, REPAIR 5.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - EXFOLIATION CORROSION ON FORWARD FLOOR GIRT BAR BRACKETS BETWEEN BS 312 TO BS 340, LBL 56. REPLACED FORWARD FLOOR GIRT BAR BRACKETS BETWEEN BS 312 TO BS 340, LBL 56 IAW B737 SRM 51-10-02.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - EXFOLIATION CORROSION ON AFT FLOOR GIRT BAR BRACKETS BETWEEN BS 312 TO BS 340, LBL 56. REPLACED AFT FLOOR GIRT BAR BRACKETS BETWEEN BS 312 TO BS 340, LBL 56 IAW B737 SRM 51-10-02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - WIDESPREAD EXFOLIATION CORROSION ON Z ANGLE BETWEEN BS 294.5 TO BS 390, LBL 56. REPLACED Z ANGLE BETWEEN BS 294.5 TO BS 390, LBL 56.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE AT BS 947, BETWEEN STR 19L TO STR 20L. REPLACED SHEAR TIE AT BS 947, BETWEEN STR 19L TO STR 20L IAW B737 SRM 51-10-02 AND BOEING DRAWING 65-46560.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE ATTACH ANGLE AT BS947 BETWEEN S26L TO S27L. REPAIRED SHEAR TIE ATTACH ANGLE IAW B737 SRM 53-00-07 REPAIR 5 & BOEING DRAWING 65-46560.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,443 hrs · 40,460 cycles

CLT - Q4 CHECK - CORROSION ON FLOORBEAM AT BS 967, RBL 18. REPAIRED FLOORBEAM AT BS 967, RBL 18 IAW B737-400 SRM 53-60-51 FIG 201.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - LEVEL 2 FILIFORM CORROSION ON SHEAR TIE BETWEEN BS 1026 TO BS 1031, RBL 7. REPAIRED SHEAR TIE BETWEEN BS 1026 TO BS 1031, RBL 7 IAW SRM 51-70-13-04.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,443 hrs · 40,460 cycles

Q4 CHECK - EXFOLIATION CORROSION ON PREVIOUSLY BLENDED FLOORBEAM T-CAP AT BS 986, BL-9. REPLACED FLOORBEAM T-CAP AT BS 986, BL-9 IAW B737 SRM 51-10-02, BOEING DRAWING 69C5346117.

Part: DOOR — LACK OF LUBE (MAIN ENTRY)

CLT - FLIGHT ATTENDANT REPORTED THE FORWARD MAIN ENTRY DOOR WAS HARD TO OPEN. MAINTENANCE LUBRICATED THE FORWARD MAIN ENTRY DOOR, INCLUDING THE GUIDE ARM. DOOR OPERATES GOOD IN ASSOCIATION WITH MM 52-11 AND 52-11-21-4.

Part: FUSE PIN — CORRODED (NACELLE) · corrosion level 2 · airframe 58,716 hrs · 39,483 cycles

CLT - RON - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON RIGHT OUTBOARD MID SPAR FUSE PIN. REPLACED RIGHT OUTBOARD MID SPAR FUSE PIN IAW B737 AMM 54-10-01.

Part: FUSE PIN — CORRODED (NACELLE) · corrosion level 2 · airframe 58,716 hrs · 39,483 cycles

CLT - RON - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON NR 1 ENGINE OUTBOARD FUSE PIN AT NAC STA 278, NAC WL 132. REPLACED NR 1 ENGINE OUTBOARD FUSE PIN AT NAC STA 278, NAC WL 132 IAW ENGINEERING CARD E5M54001 REV 2.

Part: FLASHLIGHT — FAULTY (GALLEY)

PHL - PILOT REPORTED THAT ONE OF THE AFT BREAKAWAY FLASHLIGHTS WAS NOT CHARGING. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT LOWER BREAKAWAY FLASHLIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,128 hrs · 38,477 cycles

CLT - MAJOR REPAIR - RON - EXTERIOR FUSELAGE SKIN CRACKED AT THE R1 DOOR CUTOUT LOWER AFT CORNER, BS 332.10 AND S17R. REPAIRED EXTERIOR FUSELAGE SKIN AT THE R1 DOOR CUTOUT LOWER AFT CORNER, BS 332.10 AND S17R IAW EA 101707.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,813 hrs · 38,284 cycles

RON - BOS - EEL - EMERGENCY ESCAPE PATH LIGHTS SEATS ROWS 20-23ABC INOPERATIVE. REPLACED LEFT AFT EMERGENCY BATTERY PACK IAW B737-400 AMM 33-51-12.

Part: BATTERY PACK — DISCHARGED (CABIN)

FLL - MAINTENANCE REPORTED THE SEAT EMERGENCY LIGHTS IN AFT CABIN ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IN THE AFT GALLEY. OPERATIONAL CHECK OF LIGHTS OK.

Part: LIGHT — BROKEN (CABIN) · airframe 56,622 hrs · 38,166 cycles

FLT 1831 - CLT TO MIA - EEL - LEFT EMERGENCY EXIT LIGHT BROKEN OFF. REPLACED LEFT EMERGENCY EXIT LIGHT ASSEMBLY.

Part: WIRE — DAMAGED (RT WING)

CLT - INBOUND INTO CLT WITH AUTOPILOTS ENGAGED, AT 13,000 FEET AND 315 KNOTS, THE AIRCRAFT SUDDENLY ROLLED LEFT 25 - 30 DEGREES THEN ROLLED QUICKLY BACK 25 - 30 DEGREES. CREW DISCONNECTED AUTOPILOTS, SLOWED AND STRAIGHTENED AIRCRAFT AND THEN MADE A NORMAL APPROACH AND LANDING. MAINTENANCE FOUND MULTIPLE SHIELDED WIRES BAD ON D229 RIGHT WING FLAP TRANSMITTER. REPAIRED WIRES PER WDM 22-11-21. PERFORMED CHECKOUT PER JOB CARD 03210122001. OPS CHECK GOOD. ALSO, REPLACED AUTOPILOT AILERON ACTUATOR ASSEMBLY AND PERFORMED CAT TEST PER JOB CARD 03T10134001. OPS CHECK GOOD. ALSO, REPLACED MISSING BUSHING ON AILERON ACTUATOR A.

Part: HINGE PIN — CORRODED (HORIZ STAB) · airframe 55,585 hrs · 37,549 cycles

CLT - C5 - MAJOR REPAIR - CORROSION ON RIGHT HORIZONTAL STABILIZER HINGE INNER PIN. REPLACED RIGHT HORIZONTAL STABILIZER HINGE PINS (INNER & OUTER) IAW US AIRWAYS TASK CARD 03T71027002.

Part: HINGE PIN — CORRODED (HORIZ STAB) · airframe 55,585 hrs · 37,549 cycles

CLT - C5 - MAJOR REPAIR - CORROSION ON LEFT HORIZONTAL STABILIZER HINGE INNER PIN. REPLACED LEFT HORIZONTAL STABILIZER HINGE PINS (INNER & OUTER) IAW US AIRWAYS TASK CARD 03T70927002.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,586 hrs · 37,550 cycles

CLT - C5 - MAJOR REPAIR - CRACK IN FUSELAGE SKIN AT BS 767, S24L. REPAIRED FUSELAGE SKIN AT BS 767, S24L IAW B737 SRM 53-00-01 REPAIR 31.

Part: FLANGE — CRACKED (NR 1 PYLON) · airframe 55,585 hrs · 37,549 cycles

CLT - C5 - MAJOR REPAIR - FLANGE CRACKED ON NR 1 ENGINE PYLON PANEL 5727L CUTOUT. REPAIRED CRACKED FLANGE ON NR 1 ENGINE PYLON PANEL 5727L CUTOUT IAW US AIRWAYS TYPICAL REPAIR 54-30-07.

Part: SKIN — CRACKED (LE SLAT) · airframe 55,585 hrs · 37,549 cycles

PIT - C7 - MAJOR REPAIR - CRACK IN NR 6 SLAT SKIN AT TRAILING EDGE, SLAT STATION 288.9. REPAIRED NR 6 SLAT SKIN AT TRAILING EDGE, SLAT STATION 288.9 IAW B737 SRM 57-43-04 REPAIR 6.

Part: ACTUATOR — INOPERATIVE (LT RAM AIR DOOR)

ON DESCENT, CREW REPORTED A FOUL ODOR OF DIRTY SOCKS COMING FROM THE PACKS. MAINTENANCE REMOVED AND REPLACED THE LT PACK RAM AIR DOOR ACTUATOR. OPERATIONAL CHECK GOOD.

Part: UNKNOWN — ODOR (COCKPIT)

ON DESCENT, AT APPROXIMATELY 15,000 FT, CREW NOTICED A STRONG ODOR IN THE COCKPIT. SMELLED LIKE SOMETHING OVERHEATED OR WAS BURNING. CABIN CREW VERIFIED ODOR BUT DID NOT NOTICE ANY SMOKE. GALLEY OVENS AND COFFEEMAKERS WERE NOT IN USE AND NO CIRCUIT BREAKERS WERE POPPED. ODOR BECAME STRONGER AND LASTED APPROXIMATELY FIVE MINUTES. CREW DECLARED AN EMERGENCY. FLIGHT LANDED AT RSW WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. ODOR DISSIPATED ONCE AIRCRAFT ARRIVED. MAINTENANCE ACCOMPLISHED MM TASK 21-00-01, PAGE 1, FAULT ISOLATION. INSPECTED FORWARD AND MID E & E COMPARTMENTS, BOTH CARGO BAYS, CABIN, COCKPIT, GALLEYS, PACK BAYS, WHEEL WELLS, LAVATORIES AND ENGINES. NO ODORS NOTED.

Part: POWER SUPPLY — FAULTY (CABIN)

MAINTENANCE REPORTED THE AFT EMERGENCY LIGHTS REMAINING ON AT RIGHT HAND OVERHEAD AND EXTERIOR. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY IN AFT CEILING IAW MM 33-51-51. OPERATIONAL TEST GOOD AS LIGHTS ARE NOW EXTINGUISHED. (K)

Part: WIRE — SPARKS (LAVATORY)

MCO FLT 1458 DURING CRUISE, EN ROUTE FROM FLL TO PHL, CREW REPORTED TO DISPATCH VIA ACAR'S THAT A PASSENGER AND A FLIGHT ATTENDANT SAW SPARKS COMING FROM BENEATH THE PAPER TOWEL RACK IN THE AFT LEFT LAVATORY. THE FIRST OFFICER ALSO CONFIRMED SPARKS FROM THAT AREA. CREW DECLARED AN EMERGENCY AND DIVERTED TO MCO. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. MAINTENANCE DISABLED AFFECTED WIRE BUNDLE, BLOCKED THE LAV AND PLACED IT ON MEL. MAINTENANCE REPAIRED BROKEN WIRE BEHIND TOWEL RACK AND RECONNECTED HARNESS. REMOVED MEL.

Part: LIGHT — INOPERATIVE (CABIN)

CLT - MAINTENANCE REPORTED AN AFT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.

Part: SKIN — CRACKED (BS 752-755) · airframe 51,207 hrs · 34,832 cycles

CLT - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 752.5 - BS 755, S25L. REPAIRED FUSELAGE SKIN, BS 752.5 - BS 755, S25L IAW B737 SRM 53-00-01 REPAIR 31.

Part: DOOR FRAME — CRACKED · airframe 50,460 hrs · 50,460 cycles

FWD SERVICE DOOR FRAME AFT SIDE AT APEX OF OPENING FOR DOOR STOPS. REMOVED DAMAGED AREAS & INTALLED REPAIR DOUBLERS PER EA 98738, DEFECT SIZE: .125 INCH.

Part: STOP FITTING — CORRODED (BS 440 S24R) · corrosion level 2 · airframe 50,460 hrs · 50,460 cycles

FOUND PITTING STA 440 S24R DOOR STOP ON FWD DOOR FRAME, LOWEST STOP. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER STANDARD PRACTICE MANUAL; CORROSION TASK C53-100-01, DEFECT SIZE: 1/16" BY 1/16".

Part: FLOORBEAM — CORRODED (BS 344) · corrosion level 2 · airframe 50,460 hrs · 50,460 cycles

FOUND BS 344, RBL 10 - LBL 50, CORROSION AND CLIP NUT WEAR MARKS ON TOP UPPER CHORD. REMOVED DAMAGE AND INSTALLED REPAIR ANGLES PER SRM 53-10-51; CORROSION TASK C53-107-01; LEVEL 2, DEFECT SIZE: 1".

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 50,460 hrs · 50,460 cycles

FOUND CRACK AT 2 PYLON PANEL NR 5828R BENEATH LONGERON. STOP DRILLED END OF CRACK AND INSTALLED REPAIR DOUBLER PER TR 54-30-07, DEFECT SIZE: .250".

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,460 hrs · 50,460 cycles

BS 312 AT LBL 7 TO RBL 8, TOP CHORD OF FLOORBEAM HAS CORROSION. REMOVED DAMAGED T-CAP & REPLACED WITH NEW PART PER SRM 53-51-51, 51-20-01; CORR TASK C53-107-02; DEFECT SIZE: 15 INCHES.

Part: FLOOR SUPPORT — CORRODED (BS 328-344) · corrosion level 2 · airframe 50,460 hrs · 50,460 cycles

FOUND CORROSION BETWEEN BS 328 AND 344, LBL 11 FLOOR SUPPORT. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-02; CORROSION TASK C53-107-01; LEVEL 2 DEFECT SIZE: 16".

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,460 hrs · 50,460 cycles

BS 500A & 500B, BETWEEN STR 27R & 28R HAS CORROSION. REMOVED & INSTALLED NEW DOUBLER PER T/R 20-00-02; CORR TASK C53-208-01, DEFECT SIZE: 4 X 6 INCHES.

Part: ANGLE — CORRODED (BS 965-986) · corrosion level 2 · airframe 50,460 hrs · 50,460 cycles

FOUND CORROSION Z ANGLE AFT ENTRY DOOR BS 965-986 LBL49. REMOVED Z ANGLE AND REPLACLED WITH NEW PER SRM 51-40-02, 51-20-01; CORR TASK C53-107-01, DEFECT SIZE: 24" BY 3.5".

Part: INTERCOSTAL — CORRODED (BS 947-967) · corrosion level 2 · airframe 50,460 hrs · 50,460 cycles

FOUND RBL 17, BETWEEN BS 947 AND 967, MULTIPLE AREAS OF FLOORBOARD ATTACH CLIPNUT. REMOVED AND REPLACED WITH IDENTICAL PART PER SRM 51-10-02; CORROSION TASK C53-107-02, DEFECT SIZE: 1.250" BY 1.250".

Part: SUPPORT ANGLE — CORRODED · corrosion level 2 · airframe 50,460 hrs · 50,460 cycles

TWO NUTS CORRODED ON FASTENERS THRU SKIN SUPPORT ANGLE DOOR CABLE TENSIONER. REMOVED AND REPLACED FASTENERS, NUTS AND WASHERS PER STANDARD PRACTICE; CORROSION TASK C53-202-01; LEVEL 2, DEFECT SIZE: .250" BY .175".

Part: FRAME — CORRODED (BS 794 S24R) · airframe 50,460 hrs · 50,460 cycles

FOUND CORROSION FWD FRAME AFT CARGO DOOR BS 794 1" BELOW STR 24R. INSTALLING STRUCTURE REMOVED FOR DOOR FRAME CHANGE, REF DWG 65-47959, DEFECT SIZE: 1/4".

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,460 hrs · 50,460 cycles

BS 500A - 500B, BETWEEN S27R & 28R HAS CORROSION. REMOVED, FABRICATED & INSTALLED NEW DOUBLER PER T/R 20-00-02; CORR TASK C53-208-01.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,460 hrs · 50,460 cycles

BETWEEN BS 500 & BS 400, STR 28L & 28R UNDER CHANNEL HAS CORROSION. REPAIRED PER BOEING DWG 65-45783, SRM 51-10-02; CORR TASK C53-208-01, DEFECT SIZE: 4 X 6 INCHES.

Part: FLOORBEAM — CORRODED (BS 328) · corrosion level 2 · airframe 50,460 hrs · 50,460 cycles

FOUND CORROSION BS 328 FLOORBEAM FROM BL0 TO LBL 58. CUT OUT DAMAGE AND INSTALLED DOUBLER AND FILLER PER SRM 53-10-51; CORROSION TASK C53-107-01; LEVEL 2, DEFECT SIZE: 36" BY .750".

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,460 hrs · 50,460 cycles

STA 967 LBL 10 TO LBL 37, FLOORBEAM HAS CORROSION. REMOVED DAMAGE & INSTALLED REPAIR PER SRM 53-00-51 FIG 201; CORR TASK C53-107-01, DEFECT SIZE: 27 INCHES.

Part: STOP — CORRODED (BS 492) · corrosion level 2 · airframe 50,460 hrs · 50,460 cycles

FOUND DOOR STOP PITTED, STA 492.4 AT 522R, AFT DOOR FRAME (FUSELAGE) 3RD FROM BOTTOM. REPLACED WITH IDENTICAL PART PER STANDARD PRACTICE MANUAL; CORROSION TASK C53-100-01; LEVEL 2, DEFECT SIZE: 1" BY .5".

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 50,460 hrs · 50,460 cycles

FOUND CRACK AT 2 PYLON AT PANEL NR 5827R. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER TR 54-30-07, DEFECT SIZE: .200".

Part: FLOOR SUPPORT — CORRODED (BS 294-312) · corrosion level 2 · airframe 50,460 hrs · 50,460 cycles

FOUND FLOOR SUPPORT CORRODED, BS 294.5 - BS 312. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-02; CORR TASK C53-107-02; LEVEL 2, DEFECT SIZE: 16".

Part: FLOOR SUPPORT — CORRODED (BS 312-328) · corrosion level 2 · airframe 50,460 hrs · 50,460 cycles

FOUND FLOOR SUPPORT CORRODED, STA 312-328 LBL-11. REMOVED AND REINSTALLED NEW FLOOR SUPPORT PER SRM 51-10-02; CORROSION TASK C53-107-01; LEVEL 2 DEFECT SIZE: 12".

Part: SKIN — DELAMINATED (NR 5 LE SLAT) · airframe 50,460 hrs · 50,460 cycles

FOUND DELAMINATION NR 5 L/E SLAT ON O/B AND T/E WEDGE. ADDED DOUBLER REPAIR PER T/R 57-42-04, DEFECT SIZE: 2" BY 6".

Part: SKIN — CRACKED (FWD CARGO DOOR) · airframe 50,460 hrs · 50,460 cycles

FOUND FWD CARGO DOOR SKIN AT UPPER AFT CORNER OF DOOR HANDLE CUTOUT. CUT OUT DAMAGE AND INSTALLED DOUBLERS PER EA 98744, DEFECT SIZE: 3/8".

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 50,460 hrs · 50,460 cycles

FOUND CORROSION TOP OF FLOORBEAM AT STA 986, LBL 37 - RBL 25. REMOVED AND REPLACED T CAP PER T/R 53-60-01; CORR TASK 53C-107-01; CORR LEVEL 2, DEFECT SIZE: 12".

Part: INTERCOSTAL — CRACKED (BS 294 S11L) · airframe 50,460 hrs · 50,460 cycles

FOUND CRACK STA 294.5 STRINGER 11L. REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL PER BOEING DWG 66-14208 AND JOB CARD, DEFECT SIZE: 3".

Part: ANGLE — CRACKED (BS 294 S11L) · airframe 50,460 hrs · 50,460 cycles

FOUND CRACK BS 294.5, S-11L. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-40-03, BOEING DWG 65-17684, DEFECT SIZE: 1".

Part: FRAME — CRACKED (BS 500C S8-9L) · airframe 50,460 hrs · 50,460 cycles

FOUND CRACK STA 500C BETWEEN STR 8L AND 9L. INSTALLED DOUBLER PER T/R 53-10-20E, DEFECT SIZE: 1".

Part: STRINGER CLIP — CRACKED (BS 344 S11R) · airframe 50,460 hrs · 50,460 cycles

FOUND STA 344 STRINGER 11R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02, DEFECT SIZE: 1/2".

Part: STRINGER SPLICE — CRACKED (BS 360 S15L) · airframe 50,460 hrs · 50,460 cycles

FOUND CRACK BS 360 S-15L. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-10-02, DEFECT SIZE: .250".

Part: FRAME — CRACKED (BS 867 S9R) · airframe 50,460 hrs · 50,460 cycles

FOUND CRACK STA 867; S-9R. FABRICATED FRAME REPAIR PER TR 53-10-20E, DEFECT SIZE: .250".

Part: ATTACH ANGLE — CRACKED (BS 294 S12L) · airframe 50,460 hrs · 50,460 cycles

FOUND CRACK STA 294.5 AT STRINGER 12L. REMOVED, FABRICATED AND INSTALLED NEW ATTACH ANGLE PR BOEING DWG 65-17684, DEFECT SIZE: .250.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 50,460 hrs · 50,460 cycles

FOUND BS 328 AND BS 344 AT LBL 45. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-02, DEFECT SIZE: 1/2".

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,460 hrs · 50,460 cycles

FOUND STA 500C ACTION: INSTALLED DOUBLER PER INSTALLED DOUBLER PER T/R 53-10-20E, DEFECT SIZE: 1".

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 50,460 hrs · 50,460 cycles

FOUND BS 328 FLOORBEAM AT LBL 27, VERTICAL STIFFENER. REPLACED STIFFENER PER SRM 52-10-01, DEFECT SIZE: 1".

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 50,460 hrs · 50,460 cycles

VERT STIFFENER/ATTACH ANGLE FWD SIDE BS 328 FLOORBEAM LBL 45. REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-10-02, DEFECT SIZE: .050.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 50,460 hrs · 50,460 cycles

FOUND CRACK BS 360 S-14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM 51-20-01, DEFECT SIZE: .500.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,460 hrs · 50,460 cycles

FOUND CRACKED STA 747 BETWEEN STRINGERS 8R AND 9R. INSTALLED DOUBLER PER T/R 53-10-20E, DEFECT SIZE: 2".

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,460 hrs · 50,460 cycles

INBD FASTENER HOLE FOR A/C RAIL ATTACH BRACKET, BS 400 STR 8R AND 9R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLERS PER 53-10-20E, DEFECT SIZE: 1/8".

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 50,460 hrs · 50,460 cycles

VERT STIFFENER ATTACH ANGLE, AFT SIDE OF BS 328 FLOORBEAM AT LBL 45. REMOVED CRACKED ANGLE AND REPLACED WITH NEW PART PER SRM 51-10-02 DEFECT SIZE: 1/8".

Part: FRAME — CRACKED (BS 492) · airframe 50,460 hrs · 50,460 cycles

BS 492 FWD CARGO DOOR AFT FRAME S-24R WL 163 HAS CRACK. REMOVED & REPLACED FWD CARGO AFT FRAME PER SRM 51-10-02, DWG 65-20723, DEFECT SIZE: .500 INCH.

Part: SHEAR TIE — CRACKED (BS 1040) · airframe 50,460 hrs · 50,460 cycles

STA 1040 BETWEEN S2L AND S3L HAS CRACK. FABRICATED SHEAR TIE, HEAT TREATED & INSTALLED PER SRM 51-40-02, 51-20-01, DEFECT SIZE: .5 INCH.

Part: FRAME — CRACKED (BS 440) · airframe 50,460 hrs · 50,460 cycles

BS 440 FWD CARGO DOOR FWD FRAME WL 180 HAS CRACK. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER SRM 51-10-02 & DWG 65-20722, DEFECT SIZE: .125 INCH.

Part: FRAME — CRACKED (BS 787) · airframe 50,460 hrs · 50,460 cycles

FUSELAGE FRAME STA 787 BETWEEN STR 8L & 9L AT A/C PSU RAIL ATTACH BRACKET HAS CRACK. CUT OUT DAMAGE & INSTALLED REPAIR DOUBLERS PER TR 53-10-20E, DEFECT SIZE: .0625 INCH.

Part: INTERCOSTAL — CRACKED (BS 312) · airframe 50,460 hrs · 50,460 cycles

BL 0 FASTENER HOLE AT ATTACH POINT TO BS 312 FLOORBEAM UPPER CHORD HAS CRACK. FAB'D & INSTALLED NEW REPAIR ANGLE PER SRM 51-70-13, DEFECT SIZE: .500 INCH.

Part: FRAME — CRACKED (BS 867) · airframe 50,460 hrs · 50,460 cycles

AROUND INBOARD LOCK FASTENER HEAD AT STA 867 BETWEEN S81 & S91 HAS CRACK. CUT OUT DAMAGE & INSTALLED DOUBLER PER TR 53-10-20E, DEFECT SIZE: .0625 INCH.

Part: STRINGER — CRACKED (BS 295 S10L) · airframe 50,460 hrs · 50,460 cycles

BS 295 S-10L HAS CRACK. FABRICATED STRINGER REPAIR PER SRM 51-70-11, DEFECT SIZE: .250 INCH.

Part: RIB — CRACKED (LEFT WING) · airframe 50,460 hrs · 50,460 cycles

LEFT WING RIB STA 135.5 AFT END JUST BEFORE REAR SPAR HAS CRACK. REMOVED DAMAGE & INSTALLED REPAIR PER EA 98713, DEFECT SIZE: .625 INCH.

Part: STIFFENER — CRACKED (BS 328 RBL 31) · airframe 50,460 hrs · 50,460 cycles

STA 328, RBL 31.5 HAS CRACK. REMOVED, FAB'D & INSTALLED NEW VERTICAL STIFFENER PER SRM 51-10-02, DEFECT SIZE: .500 INCH.

Part: BATTERY PACK — DISCHARGED (CABIN)

MAINTENANCE REPORTED THE OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE OVERWING EMERGENCY EXIT LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD.

Part: SKIN — CRACKED (BS 944 S24L) · airframe 47,742 hrs · 47,742 cycles

FOUND SKIN CRACKED, BS 944 JUST ABOVE S-24L. INSTALLED DOUBLER, TRIPLER AND FILLER IAW SRM 53-00-01 REP 31, DEFECT SIZE: 2.250".

Part: WIRE — BROKEN (SEAT 24ABC)

MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT AT SEAT 24ABC INOPERATIVE. MAINTENANCE FOUND THE WIRE BROKEN AT PIN FROM WIRING COMING UP TO SEAT AT MUX BOX. CRIMPED NEW PIN ON BROKEN WIRE AND INSTALLED IN PLUG. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (SEAT 11C)

PIT - PILOT REPORTED THE EMERGENCY EXIT LIGHT AT SEAT 11C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.

Part: SKIN — WORN (BS 980-990) · airframe 46,616 hrs · 31,761 cycles

SKIN WEAR .036 INCH DEEP, 10 INCH LONG AT STA 980-990 BETWEEN S2R AND S3R (UNDER DORSAL FIN). INSTALLED DOUBLER, TRIPLER AND FILLERS IAW SRM 53-60-01 (REPAIR 9) AND EA 97162.

Part: SKIN — WORN (BS 887) · airframe 46,616 hrs · 31,761 cycles

.013 INCH SKIN WEAR, 12 INCH LONG AT STA 887 AND S2R-L (UNDER DORSAL FIN). INSTALLED DOUBLER IAW SRM AND EA 97151.

Part: SKIN — WORN (BS 860-887) · airframe 46,616 hrs · 31,761 cycles

APPROX 9 INCH WEAR AREA AT OUTER FUSELAGE SKIN UNDER DORSAL FIN STA 860-887. FABRICATED DOUBLER AND INSTALLED PER EA 97151.

Part: FRAME — CRACKED (BS 312) · airframe 46,112 hrs · 46,112 cycles

FOUND CRACK AFT E/E FRAME 312. FABRICATED AND INSTALLED NEW STRAPS IAW SRM 53-10-51, DEFECT SIZE: 1" LONG CRACKS.

Part: SKIN — CORRODED (WING)

CLT - FOUND WING UPPER SURFACE WITH CORROSION 2 INCH BY 3 INCH, 2 INCH BY 4 INCH, 2 INCH BY 2 INCH, 4 INCH BY 6 INCH, 1 INCH BY 3 INCH, BETWEEN WBL 117 AND WBL 133 AFT OF FWR SPAR, STRINGER 10 STRINGER 15. REMOVED CORROSION IAW SRM 57-20-01. (M)

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

MCO - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT THE LAST TWO SEAT ROWS ON LEFT SIDE OF CABIN WERE INOPERATIVE. MAINTENANCE REPAIRED WIRING AT THE EMERGENCY LIGHTS ON SEAT ROWS 24 AND 25, LEFT SIDE. ALSO, REPLACED M1479 AND M1137 BATTERY PACKS, P/N 2013-1A. OPS CHECK GOOD. (M)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

PIT - MAINTENANCE REPORTED THE INTERIOR EMERGENCY LIGHTS INOPERATIVE. S/D - MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPS CHECK GOOD. (M)

Part: DOUBLER — CRACKED (FUSELAGE SKIN)

FOUND FUSELAGE SKIN DOUBLER CRACKED 3.5 INCH, AFT FUSELAGE BS 1138 STRINGER 12 LT. INSTALLED DOUBLER .63 CRES 301 1/2 HARD PER 53-00-01 PAGE 262 BOEING DWG 65-46585. (M)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT AT SEAT ROW 11DEF INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY AT STATION 634L. OPERATIONAL CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PIT - MAINTENANCE REPORTED THE FORWARD GALLEY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)

Part: FITTING — CORRODED (HORIZ STAB) · corrosion level 2

TPA - FOUND FITTING CORRODED .5 INCH AREA, FORWARD FACE, FORWARD UPPER JOINT CLEVIS, LT SIDE HORIZ STAB. CORROSION LEVEL 2. REMOVED CORROSION, TREATED, PRIMED, INSTALLED FILLER PER SRM 55-10-10 AND EA 94300. (M)

Part: ODOR — DETECTED (CABIN)

CLT - FLT 222 - EN ROUTE FROM MCO TO CLT,PASSENGERS AND FLIGHT ATTENDANTS NOTED A STRONG SMELL OF FUEL NEAR ROW 6. MAINTENANCE RAN THE PACKS WITH THE APU AND THE ENGINES AND COULD NOT DUPLICATE THE SMELL. A GENERAL INSPECTION WAS PERFORMED WITH NO DISCREPANCIES FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

TPA - FOUND FUSELAGE SKIN CRACKED .75 INCH, BS 294, MED LOWER HINGE CUTOUT BETWEEN S13L AND 14L. REPAIR DOUBLER INSTALLED PER SRM 53-10-01, FIG 205. (M)

Part: SKIN — CRACKED

CLT - FOUND AFT CARGO DOOR SKIN CRACKED .5 INCH, HANDLE CUTOUT, AFT UPPER CORNER. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER SRM 52-30-03. (M)

Part: SKIN — CRACKED (BS 294.5)

CLT - FOUND FUSELAGE SKIN CRACKED .75 INCH, BS 294.5, MED LOWER HINGE CUTOUT. INSTALLED REPAIR DOUBLER PER SRM 53-10-01, FIG 205. (M)

Part: FLOORBEAM — CORRODED (BS 1016)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION AT BS 1016, RBL 31 FLOORBEAM. CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. REPAIRED PER EA 65407. (M)

Part: FRAME — CRACKED (BS 480)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 480R BETWEEN STRINGER 8/9 FRAME. INSTALLED DOUBLER PER SRM 53-00-07. (M)

Part: FRAME — CRACKED (BS 440)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 440L BETWEEN STRINGER 8/9 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)

Part: FLOORBEAM — CORRODED (BS 947)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AT NUTPLATE HOLES ON UPPER T-CAP OF FLOORBEAM AT BS 947, LBL 14 TO RBL 14, WL 208. CORROSION LEVEL 1. SPLICED NEW UPPER CHORD/DOUBLERS PER SRM 53-00-51 AND TR 53-60-02. (M)

Part: FRAME — CRACKED (BS 440)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 440R BETWEEN STRINGER 8 AND 9 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)

Part: ANGLE — CORRODED (FUSELAGE)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A AREA OF CORROSION TOP Z-ANGLE FORWARD ENTRY. CORROSION LEVEL 1. REPAIRED PER SRM 51-10-02. (M)

Part: SKIN — CRACKED (BS 727)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2.5 INCH CRACK FUSELAGE SKIN STATION 727D PLUS 10, CORROSION LEVEL 1. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202 AND EA 65488. (M)

Part: INTERCOSTAL — CORRODED (BS 328-344)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH STATION 328-344 RBL 10.5 INTERCOSTAL. CORROSION LEVEL 1. REPAIRED PER SRM 53-10-02. (M)

Part: FRAME — CRACKED (BS 480)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 480L BETWEEN STRINGER 8/9 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)

Part: UNKNOWN

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION FLOORBEAM 321 UPPR CHORD AT LBL 12.5 T-CAP. CORROSION LEVEL 1. REMOVED AND REPLACED FLOORBEAM UPPER CHORD PER SRM 53-10-51. (M)

Part: ANGLE — CRACKED (BS 601)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 601, WL 203 LEFT SIDE CHORD ANGLE. REPAIRED STIFFENER ANGLE PER EA 65335 ADN TR 53-10-23. (M)

Part: ANGLE — CRACKED (BS 616)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FASTENER HOLE INNER CHORD ANGLE BS 616 FUSELAGE FRAME WL 200 LEFT SIDE. INSTALLED DOUBLER PER EA 65335. (M)

Part: SKIN — CRACKED (HORIZ STAB)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK RT HORIZONTAL STAB TORQUE BOX LOWER SKIN ACCESS. INSTALLED REPAIR DOUBLER ACCESS PANEL PER EA 65418. (M)

Part: ANGLE — CORRODED (FUSELAGE)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A AREA OF CORROSION TOP ANGLE FORWARD SERV, CORROSION LEVEL 1. REPAIRED PER SRM 51-10-02. (M)

Part: FRAME — CORRODED (SERVICE DOORWAY)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH CORRODED AREA FORWARD SERVICE DOOR CUTOUT FRAME FWD INBOARD CHORD AT BOTTOM END JUST ABOVE CREASE BEAM INNER CHORD ANGLE, CORROSION LEVEL 1. REMOVED MINOR CORROSION PER SRM 51-10-02. (M)

Part: SKIN — CRACKED (BS 128)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT RT HORIZONTAL STABILIZER STAB AFT SPAR STAB STATION 128 LOWER SKIN. REPAIRED PER SRM 55-10-01 FIG 206 AND TR 55-10-07 REV A. (M)

Part: ANGLE — CRACKED (BS 601)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FAST HOLE INNER CHORD ANGLE BS 601 FUSELAGE FRAME, WL 203 LEFT SIDE. INSTALLED DOUBLER PER EA 65335 AND TR 53-10-23. (M)

Part: FRAME — CRACKED (BS 827)

C.T - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 827L, STRINGER 8/9 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)

Part: FRAME — CRACKED (BS 400)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 400L BETWEEN STRINGER 8/9 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)

Part: FRAME — CRACKED (BS 380)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 380L BETWEEN STRINGER 8/9 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)

Part: INTERCOSTAL — CORRODED (BS 312-328)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION AT STATION 312-328, RBL 30 UPPER CHORD INTERCOSTAL. CORROSION LEVEL 1. REPAIRED PER SRM 51-40-02. (M)

Part: FLOORBEAM — CORRODED (BS 328)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AT NUT PLATE HOLES ON T-CAP FLOORBEAM STATION 328, LBL 28, AND LBL 11. CORROSION LEVEL 1. REPLACED T-CAP. INSTALLED PER SRM 53-10-51 FIG 205. (M)

Part: FRAME — CRACKED (SERVICE DOORWAY)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK LOWER OUTBOARD CORNER OF FORWARD SERVICE DOOR UPPER FORWARD STOP PAN FITTING FRAME. REPLACED DEFECTIVE PART PER DRAWING 65-45807. (M)

Part: ANGLE — CRACKED (BS 601)

CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FAST HOLE INNER CHORD ANGLE BS 601, FUSELAGE FRAME, WL 203 RT SIDE. INSTALLED REPAIR DOUBLER AND HI-LOCKS PER TR 53-10-23, EA 65335 AND SRM 53-60-07. (M)

Part: SENSOR — FAILED (LT MLG)

CLT - AFTER TAKEOFF AND LANDING GEAR RETRACTION, THE LEFT MAIN LANDING GEAR UNSAFE ILLUMINATED AND REMAINED ON WITH GEAR RETRACTED. CREW RECYCLED THE GEAR WITH NO HELP. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK SENSOR PER MM 32-61-21. SYSTEM OPERATIONAL CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

CLT - MAINTENANCE FOUND THE FORWARD LEFT EMERGENCY EGRESS LIGHTS INOP. MAINTENANCE REPLACED FUSES IN BATTERY CHARGER AND INSTALLED REPLACEMENT BATTERY PACK. OPERATIONAL CHECK GOOD. (M)

Part: SWITCH — OUT OF ADJUST (CARGO DOOR)

SDF - FLT 1732 - DURING CLIMB-OUT, THE FORWARD CARGO DOOR WARNING LIGHT ILLUMINATED. CAPTAIN DECIDED TO RETURN TO FIELD AT SDF TO VERIFY SECURITY OF THE CARGO DOOR. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. CAPTAIN NOTED THAT ON LANDING, THE CARGO LIGHT EXTINGUISHED. MAINTENANCE CHECKED THE FORWARD CARGO DOOR SWITCH, MOUNTING AND WIRING. ADJUSTED PLUNGER ONE TURN. OPERATED DOOR SEVERAL TIMES. OPERATIONAL CHECK OF DOOR WARNING SYSTEM GOOD. (X)

Part: SEAL — FAILED (CARGO DOOR)

CLT - FLT 2310 - CLIMBING THROUGH 8,000 FEET, THE FIRST OFFICER NOTICED THE CAIBN WAS CLIMBING. CREW WENT THROUGH PROCEDURES WITH NO HELP. AT 11,000 FEET, THE CREW DECIDED TO RETURN TO FIELD AT CLT BECAUSE OF THE INABILITY TO PRESSURIZE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. AFTER LANDING, THE CAPTAIN PERFORMED A WALK-AROUND INSPECTION OF THE AIRCRAFT AND FOUND THE AFT CARGO DOOR SEAL HANGING OUTSIDE THE AIRCRAFT. MAINTENANCE FOUND THE THE AFT CARGO DOOR SEAL SEPARATED FROM THE TRACK. REINSTALLED DOOR SEAL IN TRACK. OK FOR CONTINUED SERVICE. (M)

Part: PRESSURIZATION — MALFUNCTIONED (CABIN)

BOS - FLT 157 - DURING CLIMB-OUT FROM BOS EN ROUTE TO PIT, CAPTAIN NOTICED AIRCRAFT WAS NOT PRESSURIZING. THE CABIN PRESSURE WAS NOT HOLDING. FLIGHT WAS AT 8,000 FEET AND CAPTAIN DECIDED TO RETURN TO FIELD AT BOS. ON DESCENT AND APPROACH, CABIN PRESSURE WAS ERRATIC. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CHECKED ALL DUCTING AND PRESSURIZED AIRCRAFT WITH BOTH ENGINES AND APU. ALL SYSTEMS OPERATE NORMAL. (M)

Part: SKIN — DENTED (BS 288)

CLT - DURING A Q6-CHECK INSPECTION, VISUALLY FOUND A SKIN DENT 3.5 INCHES BY 3.5 INCHES BY .180 INCH DEEP IN THE LAV SERVICE DOOR STATION 288 AT STRINGER 20R AND 21R. INSTALLED SKIN. (M)

Part: SKIN — DENTED (BS 921)

CLT - DURING A Q6-CHECK INSPECTION, VISUALLY FOUND A DENT 2.5 INCHES BY 5 INCHES BY .060 DEEP AT STATION 921 BETWEEN STRINGER 17R AND 18R. INSTALLED DOUBLER. (M)

Part: FLOOR BEAM — CORROSION (BS 312)

CLT - DURING A Q6-CHECK INSPECTION, VISUALLY INSPECTED A 2 INCH CORRODED AREA LOCATED AT THE FLOOR BEAM STATION 312 RBL 6. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. INSTALLED T-CAP. (M)

Part: FLOOR BEAM — CORROSION (BS 986.5)

CLT - DURING A MQ6-CHECK INSPECTION, VISUALLY FOUND CORROSION AT FLOOR BOARD ATTACH HOLES AND AT TOP HORIZONTAL EDGE 10 INCHES LOCATED ON FLOOR BEAM AT STATION 986.5 ATTACH HOLES ALONG SPAN OF BEAM AND LEADING EDGE BL 33R TO BL 44R. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. INSTALLED T-CAP. (M)

Part: DOOR FRAME — CORROSION (AFT CARGO BIN)

CLT - DURING A Q6-CHECK INSPECTION, VISUALLY FOUND A 1 INCH BY 4 INCH CORRODED AREA AFT CARGO BIN DOOR FRAME AT LOWER FORWARD CORNER. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. DOUBLER INSTALLED ON FRAME. (M)

Part: FLOOR BEAM — CORROSION (BS 344)

CLT - DURING A MQ6-CHECK INSPECTION, VISUALLY FOUND CORRODED AREAS AROUND FLOOR BOARD ATTACH HOLES (40 INCHES) AT STATION 344 RBL 8 TO LBL 45.5, ON FLOOR BEAM. CORROSION TASK NR C53-127-02, CORROSION LEVEL 2. REMOVED AND REPLACED T-CAP. (M)

Part: FLOOR BEAM — CORROSION (BS 328)

CLT - DURING A MQ6-CHECK INSPECTION, VISUALLY FOUND CORRODED AREAS AROUND FLOOR BOARD ATTACH HOLES 30 INCHES AT STATION 328 FROM LBL TO RBL 55, ON FLOOR BEAM. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. INSTALLED T-CAP (UPPER) PER TYPICAL REPAIR 53-10-03. (M)

Part: TRACK — CRACKED (BS 520)

CLT - DURING A Q-6 CHECK INSPECTION, FOUND BY EDDY CURRENT A 1.9 INCH CRACKED TRACK LOCATED AT STATION 520 EXTENDING 1.1 INCH INBOARD AND .8 INCH OUTBOARD OF RBL 24.75. INSTALLED DOUBLERS AND TUB FITTINGS. (M)

Part: TRACK ASSY — CRACKED (BS 520)

CLT - DURING A Q6-CHECK INSPECTION, FOUND BY EDDY CURRENT A 1.8 INCH CRACK LOCATED AT STATION 520, CENTERED AT LBL 45.5. INSTALLED TUB FITTING AND TRACK ASSY KIT 65C3468827. (M)

Part: SEAT TRACK — CRACKED (BS 520)

CLT - DURING A Q6-CHECK, INSPECTION FOUND BY EDDY CURRENT A 2.2 INCH CRACKED TRACK LOCATED AT STATION 520 A CENTERED RBL 45.5. INSTALLED DOUBLERS, TRIMMED FITTINGS, TRACKS AS REQUIRED. (M)

Part: ROLLERS — LOOSE (TE FOREFLAP)

FLL - FLT 44 - DURING CLIMB AT APPROX 1,000 FEET FLAPS SET, ACFT EXPERIENCED VIBRATION WHICH INCREASED WITH AIRSPEED. FLIGHT RETURNED TO FLL WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE FERRIED ACFT TO CLT. TIGHTENED ROLLERS ON BOTH I/B ENDS AND ON BOTH I/B FOREFLAP TOGGLES. CYCLED FLAPS, NO FURTHER DEFECTS NOTED ON TEST. (W)