N302DQ

Part: BULKHEAD WEB — CRACKED · airframe 34,502 hrs · 14,976 cycles

(LOG 1377182) DURING INSPECTION FOUND CRACK IN CENTER WING REAR SPAR VAPOR WEB ON RBL 40.00. REPAIRED CRACK REF B737 SRM 57-10-10 REPAIR 4.

Part: LENS — DAMAGED (CABIN) · airframe 34,418 hrs · 14,936 cycles

(LOG 1345765) DURING INSPECTION FOUND THRESHOLD LIGHT LENS / COVER DAMAGED. REPLACED LENS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,246 hrs · 14,386 cycles

DURING INSPECTION, FOUND LEFT OVERWING EXIT DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY M1168 PER B737 AMM 33-51. OP CKS GOOD.

Part: TERMINAL — SHORTED (EMERGENCY LIGHT) · airframe 32,363 hrs · 13,875 cycles

DURING EMERGENCY LIGHT CHECK FOUND GALLEY FLOOD EMERGENCY LIGHT OUT. T/S TO EMERGENCY CEILING LIGHT L1417 TERMINAL SHORTING TO GND. REPOSITION TERMINAL AND RESECURED. OPS CHECKS GOOD.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 32,301 hrs · 13,849 cycles

DURING INSPECTION FOUND 1/2 CRACK ON GROUND SVC PANEL FUSELAGE SKIN. INSTALLED CATEGORY "A" PERMANENT REPAIR PER SRM 53-10-15 REPAIR 4.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 31,329 hrs · 13,435 cycles

(LOG 5181344) DURING INSPECTION FOUND FUNCTIONAL CHECK EMERGENCY LIGHTING, SEAT MOUNTED LIGHT FAILED TEST POWERED BY M1669. M1670 & M1672 POWER PACK. R/R POWER SUPPLY M1669, M1670 & M1672 BATTERY PACK PER AMM 33-51-06. OPS CKD OK.

Part: ATTACH FITTING — CORRODED (RT MLG TRUNNION) · airframe 29,430 hrs · 12,318 cycles

RIGHT MLG FWD TRUNNION ATTACH FITTING, OTBD UPPER POINT HAS CORROSION COMING FROM BETWEEN THE LUG AND BUSHING, ON THE OTBD FACE. REPAIRED IAW SRM 57-20-90, REPAIR 2.

Part: ATTACH FITTING — CORRODED (RT MLG TRUNNION) · airframe 29,430 hrs · 12,318 cycles

RIGHT MLG FWD TRUNION ATTACH FITTING, INBD LOWER POINT HAS CORROSION COMING FROM BETWEEN THE LUG AND BUSHING ON THE INBB FACE. REPAIRED IAW SRM 57-20-90, REPAIR 2.

Part: ATTACH FITTING — CORRODED (RT MLG TRUNNION) · airframe 29,430 hrs · 12,318 cycles

RIGHT MLG FWD TRUNNION ATTACH FITTING, INBD UPPER POINT HAS CORROSION COMING FROM BETWEEN THE LUG, AND BUSHING, ON THE INBD FACE. REPAIRED IAW SRM 57-20-90, REPAIR 2.

Part: ATTACH FITTING — CORRODED (RT MLG TRUNNION) · airframe 29,430 hrs · 12,318 cycles

RIGHT MLG FWD TRUNNION ATTACH FITTING INBD UPPER POINT HAS EVIDENCE OF CORROSION COMING FROM BETWEEN THE LUG, AND BUSHING ON THE OTBD FACE. REPAIRED IAW SRM 57-20-90, REPAIR 2.

Part: ATTACH FITTING — CORRODED (RT MLG TRUNNION) · airframe 29,430 hrs · 12,318 cycles

RIGHT MLG FWD TRUNNION ATTACH FITTING OTBD LOWER POINT HAS CORROSION COMING FROM BETWEEN THE LUG AND BUSHING, ON THE INBD AND OTBD FACES. REPAIRED IAW SRM 57-20-90, REPAIR 2.

Part: FLOORBEAM — CORRODED (BS 986.5) · airframe 26,658 hrs · 10,806 cycles

DURING INSPECTION, FOUND CABIN FLOORBEAM CORRODED AT BS 986.5 LBL 44. MAINTENANCE REPAIRED THE FLOORBEAM IAW SRM 53-70-51 REPAIR 4.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 26,658 hrs · 10,806 cycles

DURING INSPECTION FOUND CABIN FLOORBOARD SUPPORT STIFFENER CORRODED AT BS947.5 + 3" LBL 53. MAINTENANCE LOCATED AND DRILLED PART & IAW SRM 51-40-05 AND INSTALLED NEW PART AT STATION 947.5 + 3 LBL 53 IAW SRM 51-40-02.

Part: SHIELD — CORRODED (CARGO DOOR) · airframe 26,658 hrs · 10,806 cycles

DURING INSPECTION FOUND AFT CARGO COMPARTMENT CARGO DOOR AFT SHIELD AT STATION 847 TO STATION 867, STRINGER 25R HAS CORROSION. MAINTENANCE REMOVED AND REPLACED DAMAGED SHIELD IAW SRM 51-40-02, 51-40-05 & DWG 146A0081.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,658 hrs · 10,806 cycles

DURING INSPECTION FOUND AFT CARGO COMPARTMENT LT SIDE Z ANGLE FROM STATION 787 TO STATION 827 STRINGER 25L HAS MULTIPLE AREAS OF CORROSION. MAINTENANCE REPAIRED LT SIDE Z ANGLE FROM STATION 787 TO 827 STRINGER 25L IAW SRM 53-00-53 REPAIR 5.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,658 hrs · 10,806 cycles

DURING INSPECTION FOUND AFT CARGO COMPARTMENT LEFT SIDE Z ANGLE FROM STATION 727B TO STATION 727D STRINGER 25L HAS MULTIPLE AREAS OF CORROSION. MAINTENANCE REPAIRED LT Z ANGLE FROM STATION 727B TO 727 D STRINGER 25L IAW SRM 53-00-53 REPAIR 5.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,658 hrs · 10,806 cycles

DURING INSPECTION FOUND AFT CARGO COMPARTMENT LT SIDE Z ANGLE FROM STATION 747 TO 787 STRINGER 25L HAS MULTIPLE AREAS OF CORROSION. MAINTENANCE REPAIRED LT SIDE Z ANGLE FROM STATION 747 TO 787 STRINGER 25L IAW SRM 53-00-53 REPAIR 5.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,658 hrs · 10,806 cycles

DURING INSPECTION FOUND AFT CARGO COMPARTMENT LT SIDE Z ANGLE FROM STATION 727D TO STATION 747 STR 25L HAS MULTIPLE AREAS OF CORROSION. MAINTENANCE REPAIRED LT SIDE Z ANGLE STATION 727 TO 747 STRINGER 25L IAW SRM 53-00-53 REPAIR 5.

Part: ANGLE — CORRODED (BS 727D-767) · airframe 26,658 hrs · 10,806 cycles

DURING INSPECTION, FOUND AFT CARGO BAY RT ANGLE FROM BS 727D TO 767, STRINGER 25R HAS MULTIPLE AREAS OF CORROSION. MAINTENANCE REPAIRED THE ANGLE IAW SRM 53-00-53 REPAIR 5.

Part: ANGLE — CORRODED (BS 727-727B) · airframe 26,658 hrs · 10,806 cycles

DURING INSPECTION, FOUND AFT CARGO BAY ANGLE FROM BS 727 TO 727B, STRINGER 25R HAS MULTIPLE AREAS OF CORROSION. MAINTENANCE REPAIRED THE ANGLE IAW SRM 53-00-53 REPAIR 5.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 26,658 hrs · 10,806 cycles

DURING INSPECTION FOUND AFT CARGO COMPARTMENT FLOOR PANEL 140DF HAS MULTIPLE AREAS OF CORROSION ALONG EDGE OF PANEL. MAINTENANCE FABRICATED FLOOR PANEL 140DF FOR AFT CARGO COMPARTMENT IAW DWG 453A2610 REV K.

Part: ANGLE — CORRODED (BS 727B-727D) · airframe 26,658 hrs · 10,806 cycles

DURING INSPECTION, FOUND AFT CARGO BAY ANGLE FROM BS 727B TO 727D, STRINGER 25R HAS MULTIPLE AREAS OF CORROSION. MAINTENANCE REPAIRED THE ANGLE IAW SRM 53-00-53 REPAIR 5.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 26,658 hrs · 10,806 cycles

DURING INSPECTION, FOUND AFT CARGO BAY FLOOR PANEL 140BF HAS MULTIPLE AREAS OF CORROSION ALONG EDGES OF PANEL. MAINTENANCE FABRICATED A NEW FLOOR PANEL IAW DWG 453A2610 REV K, SRM 53-00-53, SRM 51-40-05, AMM 51-21-41, AND AMM 51-21-72.

Part: FLOOR PANEL — CORRODED (FWD CARGO BAY) · airframe 26,658 hrs · 10,806 cycles

DURING INSPECTION, FOUND FORWARD CARGO BAY FLOOR PANEL 120AF CORRODED SEVERAL AREAS ALONG FORWARD EDGE. MAINTENANCE CUT AND DRILLED A NEW FLOOR PANEL IAW SRM 51-40-05 & 53-60-53, AND DWG 453A1610 REV F.

Part: DOUBLER — CRACKED · airframe 24,375 hrs · 9,550 cycles

DURING INSPECTION FOUND AREA OF THE GROUND POWER RECEPTACLE SURROUND DOUBLER WAS CRACKED JUST BELOW THE LOWER HIGE LOCATION. MAINTENANCE REPAIRED IAW 534599-14.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 23,461 hrs · 9,075 cycles

DURING INSPECTION FOUND SEAT EMERGENCY LIGHT AT 12D INOPERATIVE. MAINTENANCE FOUND LOOSE CONNECTOR. SECURED CONNECTOR, OPS NORMAL.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 18,757 hrs · 6,796 cycles

DURING INSPECTION, FOUND FUSELAGE CABIN SEAT TRACK BS 727B SPLICE STRAP AT LBL 45.5 HAS CRACK DAMAGE. MAINTENANCE C/W ERA 523330-14AD, REV ORIG SECTION L, PERMANENT REPAIR ON NRC 135.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 11,865 hrs · 3,997 cycles

WORKING ERA 484067-14 REV B HAD TO REMOVE DOUBLERS FROM PREVIOUS REPAIR INSTALLED ON SAME ERA WHICH FAILED DTA. REMOVED DOUBLES AND FOLLOWED INSTRUCTION REF AS PRI 484067-14 REV C. INSTALL AND SIGNED OFF A FOLLOWED INSTRUCTIONS AS OUTLINED IN ERA 484067-14 REC C. (DALA1212063602)(MMR 121206)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 6,827 hrs · 2,149 cycles

BAGGAGE LOADER HIT SIDE OF A/C AT STA 440 AT STR AT 24R (DL73W101923).