N506AU

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 66,119 hrs · 41,492 cycles

CLT - C5 - MAJOR REPAIR - CRACK ON STRINGER TIE CLIPS AT BS 986 & BS 1006, S27L. REPLACED STRINGER TIE CLIPS AT BS 986 & BS 1006, S27L IAW BOEING DWG 65-46567.

Part: STRINGER — CORRODED (BS 978-1016) · airframe 66,119 hrs · 41,492 cycles

CLT - C6 - MAJOR REPAIR - CORROSION ON STRINGER BETWEEN BS 978 TO BS 1016, S27L. REPLACED STRINGER BETWEEN BS 978 TO BS 1016, S27L IAW B737 SRM 53-00-03.

Part: SKIN — CORRODED (BS 953-1016) · airframe 66,119 hrs · 41,492 cycles

CLT - C6 - MAJOR REPAIR - CORROSION ON FUSELAGE SKIN BETWEEN BS 1016 TO BS 953 & BETWEEN S25L TO S25R. REPAIRED FUSELAGE SKIN BETWEEN BS 1016 TO BS 953 & BETWEEN S25L TO S25R IAW EA 101415.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,554 hrs · 40,492 cycles

CLT - LINE - MAJOR REPAIR - A 3 INCH CRACK IN FUSELAGE SKIN AT AFT LOWER CORNER OF R1 DOOR, BS 328, WL 208, S17R. REPAIRED FUSELAGE SKIN AT AFT LOWER CORNER OF R1 DOOR, BS 328, WL 208, S17R IAW B737 SRM 53-10-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,817 hrs · 39,992 cycles

CLT - C5 - MAJOR REPAIR, CRACK ON FUSELAGE SKIN AT BS 727E BELOW S23L. REPAIRED FUSELAGE SKIN AT BS 727E BELOW S23L IAW B737 SRM 53-00-01 REPAIR NR 31 TEMPORARY REVISION NR 53-33.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 63,448 hrs · 39,716 cycles

FLT 1640 (CLT-EWR) - EMERG EQUIP - EMERGENCY FLASHLIGHT IN AFT GALLEY LIGHT NOT BLINKING. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE AFT GALLEY FLASHLIGHT. OPERATIONAL CHECK WAS GOOD. (A)

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,596 hrs · 39,063 cycles

CLT - MAJOR REPAIR - RON - CORROSION ON STRINGER, BS 1006 - BS 1016, S26R. REPAIRED STRINGER, BS 1006 - BS 1016, S26R IAW B737 SRM 53-60-03.

Part: SKIN — CRACKED (ZONE 200) · airframe 61,964 hrs · 38,586 cycles

CLT - MAJOR REPAIR - A CRACK FOUND ON FUSELAGE SKIN AT BS 520 S10L. INSTALLED REPAIR ON FUSELAGE SKIN AT BS 520, S10L.

Part: SKIN — CRACKED (ZONE 100) · airframe 61,496 hrs · 38,133 cycles

CLT - MAJOR REPAIR - C-4 CHECK, CRACKED FUSELAGE SKIN, BS 767, S21R. REPAIRED FUSELAGE SKIN, BS 767, S21R IAW B737-300 SRM 53-00-01.

Part: WEB — CRACKED (ZONE 100) · airframe 61,496 hrs · 38,183 cycles

CLT - MAJOR REPAIR -C-4 CHECK, CRACKED WEB, BS 727, S18A RIGHT. REPLACED WEB, BS 727, S18A RIGHT IAW B737-300 SRM 51-10-02 AND 51-40-00.

Part: STRINGER — CRACKED (ZONE 100) · airframe 61,496 hrs · 38,183 cycles

CLT - MAJOR REPAIR - C-4 CHECK, CRACKED STRINGER WEB, BS 727, S18A LEFT. REPAIRED STRINGER WEB, BS 727, S18A LEFT IAW USAIRWAYS EA 98912.

Part: STRAP — CRACKED (ZONE 200) · airframe 61,496 hrs · 38,183 cycles

CLT - MAJOR REPAIR - C-4 CHECK, CRACKED FRAME STRAP, BS 312, S13L. REPLACED FRAME STRAP, BS 312, S13L IAW BOEING DRAWING 65-17684.

Part: SKIN — CRACKED (ZONE 100) · airframe 61,496 hrs · 38,183 cycles

CLT - MAJOR REPAIR - C-4 CHECK, CRACKED FUSELAGE SKIN, BS 727E - BS 747, S25R. REPAIRED FUSELAGE SKIN, BS 727E - BS 747, S25R IAW B737-300 SRM 53-00-01 REPAIR 31.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,255 hrs · 61,255 cycles

STA 727D + 17" TO +19", .5 INCH ABOVE STR 22L CENTER LINE HAS CRACK. DOUBLER REPAIR FROM .050 2024-TS INSTALLED PER SRM 53-00-01, REP 31, DEFECT SIZE: 2 INCHES.

Part: SOLENOID — FAULTY (COCKPIT)

CLT - AFTER TAKEOFF FROM CLT, DURING GEAR RETRACTION FROM UP TO OFF, CREW RECEIVED TWO MAIN LANDING GEAR RED LIGHTS AND A LEFT MAIN LANDING GEAR GREEN LIGHT. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR LEVER LATCH SOLENOID. ALSO, REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK ACTUATOR PER MM 32-32-41-4. PERFORMED RETRACTION TEST PER MM 32-32-00-501. OPERATIONAL TEST GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

DCA - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. MAINTENANCE REPAIRED THE LIGHT ASSEMBLY AT SEAT 22C. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

BOS - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE AFT RIGHT REAR GALLEY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT BATTERY PACK. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AFT OF SEAT ROW 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK FOR AFT SECTION OF SEAT MOUNTED EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD.

Part: PANEL — CRACKED (BS 685) · airframe 59,500 hrs · 59,500 cycles

STA 685 AT KEELBEAM PANEL CRACKED. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED IAW BOEING DWG 65-45866, DEFECT SIZE: 2 INCHES.

Part: TEE FITTING — CRACKED (LWS 135) · airframe 59,500 hrs · 59,500 cycles

LEFT WING STA 135 INTERNAL CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW EA 98206, DEFECT SIZE: 2 INCHES.

Part: SPAR — CRACKED (LEFT WING) · airframe 59,500 hrs · 59,500 cycles

LEFT WING REAR SPAR STA 223 CRACKED. REMOVED AND REPLACED IMG BEAM SUPPORT FITTING PER EA 98203, DEFECT SIZE: .125 INCH.

Part: ANGLE — CRACKED (RT WING) · airframe 59,500 hrs · 59,500 cycles

LOWER TEE ANGLE INSIDE OF RIGHT WING FUEL TANK AT WS 135 CRACKED. REMOVED DAMAGE, FABRICATED REPAIR TEE, FILLER AND DOUBLER AND INSTALLED IAW EA 98207, DEFECT SIZE: 2.0 INCH.

Part: DOOR FRAME — CRACKED (FWD SERVICE DOOR) · airframe 59,500 hrs · 59,500 cycles

FWD SERVICE DOOR FWD STUB FRAME CRACKED. REMOVED DAMAGED FRAME AND FABRICATED REPAIR PARTS AND INSTALLED NEW FRAME IAW SRM 51-20-01, DEFECT SIZE: .125 INCH.

Part: INTERCOSTAL — CRACKED (BS 344 S3R) · airframe 59,500 hrs · 59,500 cycles

BS 344 STR 3R CRACKED. REMOVED DAMAGED INTERCOSTAL AND FABRICATED INTERCOSTAL/WEB IAW EA 98233, DEFECT SIZE: .25 INCH.

Part: ANGLE — CORRODED (BS 312-360) · corrosion level 1 · airframe 59,500 hrs · 59,500 cycles

STA 312 360 AT ENTRY DOOR HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM 51-10-02 LEVEL 1 C53-107-02, DEFECT SIZE: 48 INCHES.

Part: SUPPORT ANGLE — CRACKED (BS 291) · airframe 59,500 hrs · 59,500 cycles

BETWEEN STA 291.5 AND LOWER STUB FRAME FOR RIGHT SERVICE DOOR CUTOUT. FABRICATED REPAIR ANGLE AND INSTALLED IAW SRM 51-10-02, DEFECT SIZE: 1 INCH.

Part: SPAR — CRACKED (LT MLG REAR SPAR) · airframe 59,500 hrs · 59,500 cycles

LEFT LG REAR SPAR UPPER CHORD CRACKED. REAMED AND REWORKED FASTENER HOLE IAW EO 5702V054, DEFECT SIZE: .25 INCH.

Part: ANGLE — CRACKED (BS 360 S15L) · airframe 59,500 hrs · 59,500 cycles

STA 360 STR 15L ANGLE CRACKED. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM 51-10-02, DEFECT SIZE: 1 INCH.

Part: FRAME — CRACKED (BS 291 S10-11R) · airframe 59,500 hrs · 59,500 cycles

BS 291.5 BETWEEN STR 11R AND 10R CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW DWG 65-45807, DEFECT SIZE: 2 INCHES.

Part: SPAR — CRACKED (LT MLG) · airframe 59,500 hrs · 59,500 cycles

LEFT LG REAR SPAR UPPER CHORD CRACKED. REAMED AND REWORKED FASTENER HOLE IAW EO 5702V054, DEFECT SIZE: .25 INCH.

Part: STRUCTURE — CRACKED (LWS 135) · airframe 59,500 hrs · 59,500 cycles

LEFT WING STA 135 INTERNAL CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW EA 98206, DEFECT SIZE: 2.5 INCHES.

Part: ANGLE — CORRODED (BS 747-767) · corrosion level 1 · airframe 59,500 hrs · 59,500 cycles

AFT CARGO RT SIDE FROM STA 747-767 HAS CORROSION. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW SRM 53-30-53 LEVEL 2 C53-202-01, DEFECT SIZE: 20 INCHES.

Part: ANGLE — CORRODED (BS 312-360) · corrosion level 1 · airframe 59,500 hrs · 59,500 cycles

STA 312 TO 360 AT ENTRY DOOR HAS CORROSION. REMOVE AND REPLACE IAW SRM 51-10-02 LEVEL 1 C53-107-02, DEFECT SIZE: 48 INCHES.

Part: SKIN — DELAMINATED (TE FLAPS) · airframe 59,500 hrs · 59,500 cycles

LEFT I/B AFT FLAP O/B END LWR SIDE DELAMINATED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: 5.250 X 11 INCHES.

Part: INTERCOSTAL — CRACKED (BS 294 S7L) · airframe 59,500 hrs · 59,500 cycles

BS 294.5 AND STR 7L CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-02, DEFECT SIZE: 1 INCH.

Part: SKIN — CRACKED (GALLEY DOOR) · airframe 59,500 hrs · 59,500 cycles

FWD GALLEY DOOR INNER SKIN CRACKED. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW TR 52-10-16, DEFECT SIZE: 1 INCH.

Part: SKIN — CRACKED (FWD GALLEY DOOR) · airframe 59,500 hrs · 59,500 cycles

FWD GALLEY DOOR INNER SKIN CRACKED. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW TR 52-10-16, DEFECT SIZE: 1 INCH.

Part: INTERCOSTAL — CRACKED (BS 277-294) · airframe 59,500 hrs · 59,500 cycles

STR 14 BETWEEN STA 277 AND STA 294.5 CRACKED. REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW PART IAW DWG 65-45807, DEFECT SIZE: .250 INCH.

Part: FLOORBEAM — CORRODED (BS 344) · corrosion level 1 · airframe 59,500 hrs · 59,500 cycles

STA 344 24 INCHES FROM LEFT OF BUTT LINE -0- HAS CORROSION. INSTALLED NEW T-CAP SECTION, IAW SRM 53-10-51 FIG 201 LEVEL 1 C53-107-02, DEFECT SIZE: 1 X 1 INCH.

Part: SKIN — DELAMINATED (LT TE FLAP) · airframe 59,500 hrs · 59,500 cycles

LEFT I/B AFT FLAP O/B END LWR SIDE DELAMINATED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: 5.250 X 11 INCHES.

Part: FLOOR SUPPORT — CORRODED (BS 747-767) · corrosion level 2 · airframe 59,500 hrs · 59,500 cycles

AFT CARGO RT SIDE FROM STA 747 TO 767 CORROSION. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS LEVEL 2 C53-202-01, DEFECT SIZE: 20 INCHES.

Part: ANGLE — CRACKED (RT WING) · airframe 59,500 hrs · 59,500 cycles

LOWER TEE ANGLE INSIDE OF RIGHT WING FUEL TANK AT WS 135. REMOVED DAMAGE, FABRICATED REPAIR TEE, FILLER AND DOUBLER INSTALLED IAW EA 98207, DEFECT SIZE: 2.0 INCHES.

Part: KEELBEAM — CRACKED (BS 685) · airframe 59,500 hrs · 59,500 cycles

STA 685 AT KEEL BEAM CRACKED. REMOVED AND REPLACED DAMAGE, DEFECT SIZE: 2 INCHES.

Part: FLOORBEAM — CORRODED (BS 312) · corrosion level 2 · airframe 59,500 hrs · 59,500 cycles

STA 312 BUTT LINE 0 CORROSION. REMOVED DAMAGED SECTION OF TEE CAP AND INSTALLED REPAIR PARTS IAW SRM 53-10-51 LEVEL 2 C53-107-02, DEFECT SIZE: .25 INCH.

Part: DOOR FRAME — CRACKED (BS 440) · airframe 59,500 hrs · 59,500 cycles

FWD CARGO DOOR FRAME AT STA 440 STR 24R LOWER O/B HOLE CRACKED. REMOVED DAMAGE FRAME AND INSTALLED NEW FRAME IAW DWG 6-15224, DEFECT SIZE: 1 INCH.

Part: ANGLE — CORRODED (BS 917-1006) · corrosion level 1 · airframe 59,500 hrs · 59,500 cycles

AFT RIGHT DOOR ZEE ANGLE BETWEEN STA 917.5 TO STA 1006 CORROSION. REMOVED DAMAGED ZEE ANGLE AND REPLACED WITH NEW ANGLE IAW SRM 51-40-02 C53-107-02 LEVEL 1, DEFECT SIZE: 12 X 3 INCHES.

Part: ANGLE — CORRODED (DOOR SILL) · corrosion level 1 · airframe 59,500 hrs · 59,500 cycles

FOUND Z-ANGLES CORRODED, MAIN ENTRY DOOR SILL SUPPORT STRUCTURE. INSTALLED BLENDED MINOR SURFACE CORROSION IAW SRM 51-10-02 LEVEL 1 C53-107-01, DEFECT SIZE: 10" BY .50".

Part: INTERCOSTAL — CORRODED (BS 320) · corrosion level 1 · airframe 59,500 hrs · 59,500 cycles

FOUND INTERCOSTAL CORRODED STA 320 12" LEFT OF BUTT LINE 0. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-02 LEVEL 1 C53-107-02, DEFECT SIZE: .2".

Part: STRINGER — CORRODED (BS 323-1177 S28R) · corrosion level 2 · airframe 59,500 hrs · 59,500 cycles

FOUND CORROSION STRINGER 28R AT BS 323 TO BS 1177. REMOVED DAMAGED AREAS OF STRINGER AND REPAIRED IAW SRM 51-10-02 LEVEL 2 C53-107-02, DEFECT SIZE: 2" BY 1".

Part: ANGLE — CRACKED (RWS 135) · airframe 59,500 hrs · 59,500 cycles

FOUND CRACK LOWER T CHORD ANGLE INSIDE OF RT WING FUEL TANK AT WS 135. REMOVED DAMAGED, FABRICATED REPAIR TEE, FILLER AND DOUBLER IAW EA 98207, DEFECT SIZE: 2".

Part: ANGLE — CORRODED (DOOR SILL) · airframe 59,500 hrs · 59,500 cycles

FOUND CORROSION AFT ENTRY DOOR SILL. REMOVED AND REPLACED ZEE ANGLE WITH NEW PART IAW SRM 51-40-03 C53-107-02, DEFECT SIZE: 20".

Part: FRAME — CRACKED (BS 492) · airframe 59,500 hrs · 59,500 cycles

FOUND CRACK, BS 492.4 FWD DOOR FRAME. REMOVED CRACKED FRAME AND INSTALLED NEW FRAME IAW SRM 51-40-02, DEFECT SIZE: .25".

Part: CHANNEL — CORRODED (BS 986) · corrosion level 1 · airframe 59,500 hrs · 59,500 cycles

STA 986 LBL 14 CORROSION. BLENDED MINOR SURFACE CORROSION AND TREATED IAW SRM 51-10-02 LEVEL 1 C53-107-02, DEFECT SIZE: 2 INCHES.

Part: STRINGER — CORRODED (BS 323-1177 S28R) · corrosion level 1 · airframe 59,500 hrs · 59,500 cycles

S28R, BS 323 TO BS 1177 CORROSION. REMOVED DAMAGE AREAS OF STRINGER AND REPAIRED IAW SRM 51-10-02 LEVEL 1 C53-107-02, DEFECT SIZE: 1 INCH.

Part: STRINGER SPLICE — CRACKED (BS 908 S41) · airframe 59,500 hrs · 59,500 cycles

STA 908 S41 CRACK. REMOVED AND REPLACED STRINGER SPLICE IAW SRM 51-10-02, DEFECT SIZE: .125 INCH.

Part: STIFFENER — CRACKED (BS 320) · airframe 59,500 hrs · 59,500 cycles

STA 320 CRACK. REMOVED AND REPLACED WITH PARTS IAW SRM 51-10-02, DEFECT SIZE: .375 INCH.

Part: STRINGER CLIP — CRACKED (BS 907 S2R) · airframe 59,500 hrs · 59,500 cycles

FOUND TIE CLIP CRACKED, S2R, STA 907. REMOVED AND REPLACED TIE CLIP IAW SRM 51-10-02, DEFECT SIZE: .125".

Part: STRINGER CLIP — CRACKED (BS 500A S16R) · airframe 59,500 hrs · 59,500 cycles

BS 500A STR 16R CRACKED. REMOVED AND REPLACED TIE CLIP IAW SRM 51-10-02, DEFECT SIZE: 1 INCH.

Part: SKIN — WORN (LE FLAP) · airframe 57,676 hrs · 57,676 cycles

LEADING EDGE SKIN OF MIDFLAP AT INBOARD END WORN. FABRICATED AND INSTALLED DOUBLER IAW SRM 57-53-01 REPAIR 8, DEFECT SIZE: 8 X 4 INCHES.

Part: SKIN — WORN (TE FLAP) · airframe 57,676 hrs · 57,676 cycles

LEADING EDGE SKIN OF MID FLAP 13 TO 20 INCHES FROM OUTBOARD END WORN. FABRICATED AND INSTALLED DOUBLER IAW SRM 57-53-01 REPAIR 8, DEFECT SIZE: 7 X 4 INCHES.

Part: SKIN — CRACKED (SLAT) · airframe 57,676 hrs · 57,676 cycles

OUTBOARD END OF NR 6 SLAT, LOWER, TRAILING EDGE SKIN CRACKED. REMOVED DAMAGED, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-43-01, DEFECT SIZE: 1.5 INCH.

Part: CHARGER — FAILED (EMERGENCY LIGHT)

PHL - MAINTENANCE REPORTED THE RIGHT-HAND CENTER EMERGENCY EXIT SIGN AND THE LEFT-HAND OVERWING EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY POWER SUPPLY AND BATTERY M1160. OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — FAULTY (FWD CABIN)

PILOT REPORTED THE EMERGENCY EXIT LIGHTS FLASH ON AND OFF INDEPENDENT OF SWITCH POSITION. MAINTENANCE REMOVED AND REPLACED THE M1136 POWER SUPPLY AND BATTERY PACK IAW MM. OPERATIONAL CHECK GOOD.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

PIT - MAINTENANCE REPORTED THE FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT CONNECTOR BEHIND LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

BDL - FOUND EMERGENCY EXIT SIGN OVER AFT LEFT DOOR INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND CHARGER. (M)

Part: SKIN — CHAFED (FUSELAGE)

PIT- FOUND SKIN WITH CHAF MARKS THROUGH WEAR STRIPS, STATION 880-887 STRINGER 1L-1R. BLEND DAMAGED AREA, INSTALL DOUBLER, TRIPLER, COUNTER BORE, INTERNAL DOUBLER (WEB PLATE) PER EA 76023. (M)

Part: SKIN — CRACKED (FUSELAGE)

PIT - FOUND SKIN PANEL CRACKED TWO PLACES 1.25 INCH AND .750 INCH, STATION 685 BL 0 AT KEELBEAM. STOP DRILLED CRACKS, INSTALLED EXTERNAL DOUBLER PER EA 53683E. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

IND - MAINTENANCE FOUND THE EMERGENCY LIGHTS FROM SEAT ROWS 17 LEFT THROUGH 22 LEFT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND RELAMPED THE LIGHTS. OPERATIONAL CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (MID CABIN)

LGA - MAINTENANCE REPORTED THE EMERGENCY PATH LIGHTING INOPERATIVE AT SEAT ROW 12 LEFT AND SEAT ROWS 10, 16, 18 AND 20 RIGHT. ALSO, THE OVERWING EMERGENCY LIGHTS ARE DIM AND EXTINGUISH WITHIN 30 SECONDS OF OPERATION. MAINTENANCE REMOVED AND REPLACED THE M1136 BATTERY PACK. OPERATIONAL CHECK GOOD. (M)

Part: SKIN — CRACKED (FUSELAGE)

CLT - FOUND FUSELAGE SKIN CRACKED 1 INCH, AFT END OF E/E COOLING DUCT OUTLET. INSTALLED EXTERNAL DOUBLER PER TR 53-30-07. (M)

Part: CONTROLLER — FAILED (EE BAY)

CLT - FLT 1187 - EN ROUTE FROM IAH TO CLT, CRUISING AT FL330, THE CABIN ALTITUDE CLIMBED TO 10 WITH WARNING HORN SOUNDING. CREW DESCENDED THE FLIGHT TO FL110, WHEREAS UPON DESCENDING THROUGH FL160, THE WARNING HORN SILENCED. FLIGHT CONTINUED ON TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER. TESTED GOOD PER MM 21-31-00. ALSO, FOUND THE AFT CARGO DOOR SEAL TORN AND HANGING OUT. REMOVED AND REPLACED THE AFT CARGO DOOR SEAL (P/N 10-60821-4) PER MM 52-09-12. PRESSURIZED AIRCRAFT. LEAK CHECKED GOOD. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

PHL - FLT 1797 - ON CLIMB-OUT FROM PHL, EN ROUTE TO MCO, THE OUTER PANE ON THE CAPTAINS WINDSHIELD CRACKED. CAPTAIN REPORTED THAT THE LOWER LEFT CORNER ARCED AND GLOWED BEFORE CRACKING. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD. OPERATIONAL CHECK OF WINDOW HEAT SYSTEM GOOD. (M)

Part: WINDSHIELD — LEAKING (COCKPIT)

PIT - FLT 338 - DURING CLIMB-OUT FROM PIT, THE FIRST OFFICERS WINDSHIELD SEAL AND SEALANT HAD RUPTURED ON THE UPPER RIGHT CORNER. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. THE FIRST OFFICERS WINDSHIELD HAD BEEN REPLACED LAST NIGHT. MAINTENANCE CLEANED AND REMOVED EXCESSIVE SEALANT AND RETAPED WINDOW. PROGRAMMED FOR RESEAL OF WINDSHIELD AT THE NEXT MAINTENANCE RON. UNFORTUNATELY, TAPE REPAIR BLEW OFF EN ROUTE TO CLT AND AN AIR LEAK WAS NOTED AT 4 PSI WHICH CEASED AT 5 PSI. MAINTENANCE ENDED UP REMOVING AND REPLACING THE FIRST OFFICERS WINDSHIELD PER MM 56-11-11. PRESSURIZED AIRCRAFT. NO LEAKS NOTED. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

PIT - FLT 1195 - EN ROUTE FROM DCA TO IND, AT FL350, THE FIRST OFFICERS WINDSHIELD OUTER PANE SHATTERED AND CONTINUED TO CRACK INTERMITTENTLY. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD PER JOB CARD J356-11-01. ALSO, REPLACED THE F/O''S WINDSHIELD HEAT CONTROL UNIT (P/N 231-2) AS PRECAUTIONARY. OPS CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ALB - DURING OVERNIGHT MAINTENANCE CHECK, MAINTENANCE FOUND THE FORWARD CABIN EMERGENCY LIGHTS DIM DURING OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY WITH NO HELP. FOUND MAIN ENTRY DOOR EMERGENCY EXIT IDENTIFIER LIGHT DAMAGED CAUSING A SHORT. REMOVED AND REPLACED IDENTIFIER LIGHT. OPERATIONAL CHECK GOOD. (M)

Part: PANEL — CRACKED (KEELBEAM)

PIT - FOUND PANEL CRACKED .375 INCH PAST EXISTING STOP DRILL, KEEL BEAM PANEL BETWEEN WHEEL WELLS. INSTALLED TEMP REPAIR DOUBLER INCORPORATING BOTH CRACKED AREAS PER SRM 53-60-12 FIG 202/EA 53683D. (M)

Part: FLOORBEAM — CRACKED (BS 520)

CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK STATION 520, LBL 45, WL 207 FLOORBEAM. INSTALLED DOUBLER PER EA 63061. (M)

Part: FLOORBEAM — CRACKED (BS 520)

CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A 1.625 INCH CRACK STATION 520, RBL 45, WL 207 FLOORBEAM. INSTALLED DOUBLER PER EA 63061. (M)

Part: FLOORBEAM — CRACKED (BS 520)

CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A 1.4 INCH CRACK STATION 520, RBL 25, WL 207 FLOORBEAM. INSTALLED DOUBLER PER EA 63061. (M)

Part: WEB — CRACKED (BS 294)

CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK STATION 294 WL 209 RBL 56 WEB. INSTALLED DOUBLER PER BOEING 737-300 SRM 51-70-11. (M)

Part: ANGLE — CRACKED (BS 520)

CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK STATION 520 STRINGER 7L FUSELAGE ANGLE EXTERIOR. INSTALLED DOUBLER PER TR 53-50-03. (M)

Part: FUEL TANK — CRACKED (BS 280-350)

CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND FOUR 1 INCH CRACKS AUX FUEL TANK SHROUD AFT WALL LOWER CORNER SKIN. INSTALLED DOUBLER PER EA 63089. (M)

Part: FLOORBEAM — CRACKED (BS 520)

CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A 1.75 INCH CRACK STATION 520, LBL 24.75, WL 207 FLOORBEAM. INSTALLED DOUBLER PER EA 63061. (M)

Part: ANGLE — CRACKED (BS 520)

CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK STATION 520 STRINGER 7R FUSELAGE ANGLE EXTERIOR. INSTALLED DOUBLER PER TR 53-50-03. (M)

Part: WEB — CORRODED (BS 790-847)

CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION SURROUNDING NUTPLATE HOLES 1 INCH BY 57 INCH FROM BS 790 TO 847 RBL 20 WEB. CORROSION TASK NR 53-202-01. INSTALLED NEW WEB AND FILLER PER SRM 51-30-01. (M)

Part: SILL — CORRODED (BS 280-350)

CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 70 INCH ALONG FORWARD SERVICE DOOR 'Z' ANGLE LOWER SILL INBOARD CHORD ANGLE AT BS 280-350 RBL 35. CORROSION TASK NR C53-107-01. REPLACED PART PER BOEING 737-300 SRM 51-40-02 AND 51-20-05. (M)

Part: SKIN — CRACKED (PASSENGER DOOR)

CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK FORWARD ENTRY DOOR INNER SKIN. INSTALLED DOUBLER PER EA 63053. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - DURING OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM, MAINTENANCE FOUND THE FORWARD ENTRY AND SERVICE DOOR SLIDE LIGHTS INOP AFTER ABOUT THREE SECONDS OF OPERATION. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)

Part: WIRE — FAILED (CABIN)

CLT - RED FLOOR TRACK EMERGENCY LIGHT INOP, LAST ONE ON RIGHT SIDE AT OVERWING EXIT. WIRING NEEDS REPAIRED. THE WIRING WAS REPAIRED. SYSTEM OPERATIONALLY CHECKED OK. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

CLE - DURING OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM, MAINTENANCE FOUND FOUR OVERHEAD EMERGENCY LIGHTS IN THE AFT CABIN ON OVERHEAD BIN BULLNOSE INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY IN THE AFT CABIN. OPERATIONAL CHECK GOOD. (M)

Part: FIRE LOOP — MALFUNCTIONED (NR 1 ENGINE)

BWI - FLT 378 - AT CRUISE, CAPTAIN RECEIVED AN ENGINE OVERHEAT/FIRE INDICATION ON THE NR 1 ENGINE. WITH POWER REDUCED TO ENGINE IDLE, THE INDICATION REMAINED. FLIGHT DIVERTED TO BWI. NO EMERGENCY WAS DECLARED AND THE NR 1 ENGINE WAS NOT SHUT DOWN. FLIGHT LANDED WITH NO FURTHER INCIDENT. MX REPLACED THE NR 1 ENGINE FIRE DETECTOR LOOP ASSEMBLY, THE FIRE/OVERHEAT CONTROL MODULE AND THE ENGINE/APU FIRE CONTROL PANEL. SYSTEM OPERATIONAL CHECKS AND TESTS NORMAL. RAN ENGINE, 'A' LOOP CHECKS NORMAL. FIRE DET LOOP ASSY P/N 6678, FIRE/OVERHEAT CONT MODULE P/N 6594-01, ENGINE/APU FIRE CONTROL PANEL P/N 69-37307-145. (M)

Part: HAT CHANNEL — CORRODED (BS 308)

INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 5 INCH CORRODED AREA ON FLOOR HAT CHANNEL, BS 308 (AFT BULKHEAD FOR FORWARD LAVATORY). REPAIRED PER SRM 51-10-1 FIG 1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)

Part: ANGLE — CORRODED (BS 727D-945)

INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 137 INCH CORRODED AREA BS 727 D TO BS 945 AT RBL 14 INCHES. REPAIRED PER SRM 53-00-53. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)

Part: STRAP — CORRODED (BS 787-847)

INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 40 INCH CORRODED AREA AFT CARGO STRAP BS 787-847. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (W)

Part: INTERCOSTAL — CORRODED (BS 947-967)

INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 3 INCH CORRODED AREA BS 947-967 48 INCHES LBL AT AFT ENTRY DOOR. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W)

Part: FLOORBEAM — CORRODED (BS 967)

INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA BS 967 LBL 40. REPAIRED PER SRM 53-00-51. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)

Part: HAT CHANNEL — CORRODED (AFT CABIN)

INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORRODED AREA INBOARD END RT LAVATORY FORWARD WALL HAT CHANNEL AFT CABIN. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)

Part: SUPPORT ANGLE — CORRODED (BS 957)

INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 7 INCH AREA CORRODED BS 957 RBL 25 TO RBL 50. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)

Part: ANGLE — CORROSION (BS 294.5 -312)

INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH AREA CORROSION FLOORBOARD SUPPORT ANGLE 294.5 TO 312 LBL 12. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)

Part: CHANNEL — CORROSION (BS 305)

INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCH AREA OF CORROSION BS 305 AT LBL 36. REPAIRED PER 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)

Part: INTERCOSTAL — CORRODED (BS 312-328)

INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 3 INCH LONG BY 2 INCH WIDE CORROSION TOP OF INTERCOSTAL BS 312 TO BS 328 RBL 12 INCHES. REPAIRED PER SRM 53-10-01. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W)