N62883

Part: BATTERY — DISCHARGED (ZONE 200) · airframe 30,991 hrs · 11,380 cycles

FWD IB FA FLASHLIGHT BATTERY LOW. RED LIGHT SHOWING REPLACED FLASHLIGHT BATTERY AT FWD FA INB FLASHLIGHT. OPS CHECK GOOD REF AMM 25-64-00

Part: COFFEEMAKER — FAULTY (ZONE 900) · airframe 30,033 hrs · 11,007 cycles

DOOR 1L GIRT BAR IS JAMMED IN THE DISARM BRACKET REPOSITIONED GIRT BAR TO CORRECT POSITION. NO FURTHER DEFECTS NOTED.PARTS USED: 29-2599-9-0001, QTY :1

Part: SKIN — DAMAGED (BS 390 S19L) · airframe 27,868 hrs · 10,116 cycles

PERFORM A PERMANENT REPAIR AT LH FUS EXTERNAL SKIN AT STA 390, STRG 19L PER LP#4324692.(REF: AAR NR 100008644) SFR #1036381 1036524). PERFORMED A PERMANENT REPAIR AT L/H FUSELAGE EXTERNAL SKIN STA 390, STR 19L & INSTALLED IAW SRM 53-00-01-2R-1, IS A CATEGORY B REPAIR AND REQUIRED INSPECTION INTERVALS IAW B737-900ER SRM 53-00-01-2R-1, PAR:5, TABLE 203, FIG 202 (SDR # ADD EMP:N078352 PERFORMED A PERMANENT REPAIR AT L/H FUSELAGE EXTERNAL SKIN STA 3. 90, S19L & INSTALLED IAW B737-900 SRM 53-00-01-2R-1, THIS IS A CATEGORY B REPAIR AND REQUIRED INSPECTION INTERVALS IAW SRM 53-00-01-2R-1, PAR 5, TABLE 203, FIG 202.

Part: FLOORBEAM — CORRODED (BS 948 RBL 52) · airframe 27,868 hrs · 10,116 cycles

AFT WET AREA POSSIBLE CORROSION AT FLOOR BEAM STA 947.5 AND RBL 52.

Part: SKIN — BUCKLED (TAIL) · airframe 27,865 hrs · 10,115 cycles

RAMP REPORTS DAMAGE TO THE TAIL STAND AREA

Part: NONE — NONE (INSIDE NOSE COWL) · airframe 23,722 hrs · 8,526 cycles

FOUND PANEL 412AR UNLATCHED AND OPEN ON #1 ENG NOSE COWL ON ARRIVAL -- SEE PHOTO LOTS IF HISTORY UNDER ATA 71; 72 AND 54 PHOTO ADDED -- SUSPECT AIR LEAK FROM SEAL MISSING AROUND DUCT -- PHOTO -- CMM 71-11-22 FIG 1 SHEET 4 SHOWING REQUIRED SEAL ASSLY NOTE : THIS A PRESSURE RELIEF DOOR 412AR SEE NOTES ON PHOTO -- THE #2 ENGINE DOES NOT HAVE ANY GAPS AT ITEMS 190; 195; 200; 187; 185; 180.. ALL AND THE SEAL IS VISIBLE --- REMOVED AND REPLACED LH ENGINE INLET COWL ASSY AND OPS/LEAK CHECK GOOD

Part: PANEL — MISSING (RT WING) · airframe 19,729 hrs · 7,079 cycles

INSP PANEL MISSING ON TOP OF RIGHT WING IN FRONT OF AILERON. FOUND TWO INSPECTION PANELS OPEN. ONE WAS STILL ATTACHED BY FASTENER. THE LARGER ONE FASTENERS STILL IN PLACE,PANEL MISSING. 115A4523-904. DIMENTION IS 4"X4" FOUND PART NUMBER OF MISSING PANEL. PANEL 671 AT. P/N MANUFACTURED PANEL PER BOEING DRAWING PL 115A4523. CHAMFERED LEADING EDGE . MATERIAL USED 2024 T3 .075 THICKNESS. NEED TO ACP PART 2 AND PART 3 PER ECRA 5751-01396 PART 2 - INSPECTION REQUIREMENTS: 1. PERFORM A DETAILED VISUAL INSPECTION OF THE INTERIM REPAIR PANELS. ENSURE THAT THEY REMAIN PROPERLY INSTALLED. CORRECT AS/IF REQUIRED. MUST ACCOMPLISH PART 2 DAILY INSPECTION. INTERIM REPAIR PER PART 1 FOR PANEL 671AT ECRA 5751-01396, ORIGINAL 671BT INSTALLED, ACCOMPLISH DAILY INSPECTION PER PART 2 OF ECRA AND PERFORM A PERMANENT REPAIR PER PART 3 WITHIN 7 DAYS TOMC-APPROVAL FROM SC1ELBYC COMMENT REVIEWED RECORDS UPDATE QC REVIEWED RIR: DAILY, NO M&E REQ''D (TOMC "D" METERED) T/A: W/IN 7 DAYS....NC/U342507 CLAD SHEET. .040" THICKNESS. NEED QC MATERIAL VERIFICATION PER ECRA 5751-01396 REV. A 2024-T3 PERFORMED MATERIAL VERIFICATION REF 5751-01396 REV. A 2024-T3 CLAD SHEET. .040" PO 8415431 LOT 514269. OK TO CONTINUE. TOMCQC REV PERFORMED COMPLETED FABRICATION, PREP AND INSTALLATION OF R/H OVERWING PANELS 671AT AND 671BT IAW ECRA 5751-01396 REV A PART 3. PREVIOUS ENTRY INSPECTION REQUIREMENT ENTERED IN ERROR. COMPLETED INSPECTION REQUIREMENTS REF ECRA5751-01396 REV A PART 3 STEP 1.A FOR MATERIAL VER

Part: PULLEY — MISSING (RT WING SPOILER) · airframe 19,463 hrs · 6,982 cycles

PDA 2 R/H WING REAR SPAR HAS SPOILER PULLEY AND SUPPORT BRACKET MISSING BELOW #8 SPOILER BEHIND #2 ENGINE PYLON. CLASSIFIED AS CATEGORY 2 PDA PER GMM 02-30-95. COMPLIED WITH GMM 02-30-95 FOR MISSING PULLEY BRACKET ON R/H WING TRILING EDGE BEHIND #2 ENGINE PYLON.REF. AAR N/R: 9485440 " INSTALLED NEW PULLEYAND SUPPORT BRACKET AT R/W FIXED T/E REAR SPAR SPOILER CABLE . REF. B737-900 AMM 20-10-09-400-801 AND SRM 51-40-82-06-0.ADJUSTMENT AND OP''S CHECK OF CONTROL CABLES OK, ADD EMP:V914420 INSPETCED BY: V891406 WOK ACCOMPLISHED BY V914420 STATION 287." REF. B737-900 AMM 27-61-00-820-801 AND SRM 51-40-02-06-0,WING

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 17,739 hrs · 6,358 cycles

EMERGENCY LIGHTS IN UPPER CABIN AT ROW 29 & 34 INOP. REPLACED BATTERY PACK LOCATED ON CEILING PANEL AT 31 DEF, AS PER AMM 33-51-06-960-805. LIGHTS CHECK GOOD. LOG CLEARED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 17,739 hrs · 6,358 cycles

EMERGENCY EXIT LIGHTS AT RIGHT OVERWING EXIT DOOR INOP. REPLACE BATTERY PACK AT M 1695, PER AMM 33-51-06-960-805. OPS CHECKS GOOD.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 9,286 hrs · 3,283 cycles

EMERGENCY LIGHT COVER ON LEFT BOTTOM SIDE OF FIRST CLASS CLOSET IS BROKEN INSTALLED NEW LENS FOR EMERGENCY LIGHT LEFT SIDE FIRST CLASS CLOSET

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 8,256 hrs · 2,901 cycles

1ST CLOSET EMERGENCY LIGHT COVER MISSING. REPLACED LENS COVER.

Part: OVEN — SPARKS (GALLEY) · airframe 7,477 hrs · 2,634 cycles

OVEN SMOKING OR SPARKING 204 OVEN 204 IN 1ST CLASS GALLEY SMOKES WHEN YOU TURN IT ON. REMOVED AND REPLACED OVEN 204 IAW 25-34-00, NO SPARKS OR SMOKE