N27722

Part: GUARD — DAMAGED (ZONE 200) · airframe 83,131 hrs · 30,479 cycles

AFT F/A PANEL EMERG LIGHTS PB SWITCH FLIP GUARD SPRING DAMAGED. INSTALLED NEW FLIP GUARD TO AFT PANEL EMERGENCY LIGHT PUSH BUTTON IAW BSWPM 20-84-00. OPS CHECK GOOD.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 83,131 hrs · 30,479 cycles

EMERGENCY LIGHT BATTERY PACK M1674 FAILED CAPACITY CHECK. REMOVED AND REPLACED M1674 BATTERY PACK IAW AMM 33-51-06-960-805. OP CHECKED GOOD.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 83,131 hrs · 30,479 cycles

EMERGENCY LIGHT BATTERY PACK M1675 FAILED CAPACITY CHECK. REMOVED AND REPLACED M1675 BATTERY PACK IAW AMM 33-51-06-960-805. OPS CHECK GOOD.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 83,131 hrs · 30,479 cycles

EMERGENCY LIGHT BATTERY PACK M1670 FAILED CAPACITY CHECK. REPLACED M1670 BATTERY PACK IAW AMM 33-51-06-960-806.

Part: OVEN — ODOR (ZONE 900) · airframe 82,864 hrs · 30,356 cycles

AFT GALLEY OVEN 3 POSITI ON 425 HAS STRONG ELECTRICAL SMELL WHE N HEATING OPS CHECKED G4 GALLEY OVEN #3. OPS CHECKED GOOD. NO ELECTRICAL SMELL.SMELL ASSOCIATED WITH OVEN TRAYS BEING HEATED. REF AMM TASK 25-34-00-400-801-C4

Part: SLIDE — OUT OF ADJUST (ZONE 800) · airframe 82,790 hrs · 30,315 cycles

SLIDE AT 2R IS HANGING TO LOW READJUSTED THE SLIDE GIRT BAR ON 2R DOOR IAW AMM 25-66-01-200-802, OPS CHECK GOOD, OKAY TO CONTINUE.

Part: BUMPER — DAMAGED (ZONE 200) · airframe 82,503 hrs · 30,175 cycles

SEAT 21C EMERGY LIGHT HOUSING HANGING DOWN SEAT 19C. REPLACED ARM SHROUD REF CMM 25-22-59 NO OTHER FAULTS FOUND.

Part: LIGHT — NO DISCREPANCY (ZONE 200) · airframe 82,150 hrs · 29,979 cycles

CAPTAIN REPORTS EMERGENCY LIGHT BROKEN AT SEAT ROW 20. INSPECTED ROW 20 AISLE PATH LIGHTS, NO DEFECTS.

Part: HOUSING — FAULTY (ZONE 200) · airframe 82,164 hrs · 29,986 cycles

26C AISLE PATH SEAT MOUNTED EMERGENCY ESCAPE PATH MARKING SYSTEM, LIGHT ASSY BROKEN. REMOVED AND REPLACED SEAT MOUNTED FLOOR PROXIMITY LIGHT HOUSING IAW CMM 25-22-59.

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 82,106 hrs · 29,960 cycles

EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK. RT AFT LWR EXTERIOR EMEGENCY LIGHT INOP. REPLACED M1670 BATTERY PACK POWER SUPPLY REF AMM 33-51-06. OPS CHECK GOOD AT THIS TIME.

Part: DOOR — OUT OF ADJUST (ZONE 800) · airframe 82,077 hrs · 29,943 cycles

FWD ENTRY LGT ILLUM AIRB ORNE. FLT ATT RESECURED HANDLE LGT EXTINGUISHED DEBRIEFED CREW THEY STATED THAT THEY HAD A PROBLEM CLOSING THE DOOR TO PUT THE WARNING LIGHT OUT DURING TAKE OFF ROLE THE DOOR HANDLE POPPED UP AND THE WARNING LIGHT CAME ON PERFORMED PSEU BITE CHECK PER FIM TASK 52-10 TASK 815 NO FAULTS WERE LOGGED CREW STATED HANDLE MOVEMENT OCCURRED ON THE GROUND DURING TAKEOFF ROLL. T/S BY SOFT UNLATCHING PROCEDURE AMM REF 52-11-00-820-802.ADJUSTED AS REQUIRED UPPER LATCH TORQUE TUBE . DOOR OPERATION IS NOW NORMAL AND DOOR INDICATION SENSOR OPS CHECKS GOOD. OK TO CONTINUE. COMPLIED WITH RII REQUIREMENTS IN THE ADJUSTMENT OF L1 DOOR ASSY UPPER LATCH TORQUE TUBE PER AMM 52-11-820-802. OK TO CONTINUE.

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 81,912 hrs · 29,870 cycles

EMERGENCY EXIT SIGN DOES NOT TURN OFF DOOR 2L DEBRIEFED FA, R & R BATTERY PACK M1673. EMERGENCY LIGHTS OPERATE NORMAL AND OPS CHK OK. REF AMM 33-51-06-960-805.

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 800) · airframe 81,808 hrs · 29,817 cycles

FWD ENTRY DOOR ANNUNCIATOR ON. PLACED ON MEL 5203E VERIFIED DOOR IS CLOSED AND LOCKED. TO ASSIST T/S ADJUSTED ENTRY DOOR SENSOR GAP IAW AMM 52-71-11-820-801. OPS CHECK GOOD. PLACARD REMOVED.

Part: WARNING LIGHT — ILLUMINATED (MAIN DOOR) · airframe 80,757 hrs · 29,330 cycles

FWD ENTRY DOOR LIGHT ILLUMINATED UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC METER INITIATED FOR WITH VENDOR ID MAC RELATED WORK ORDER 000000003127505 AND PRTR DOOR CONFIRMED CLOSED - PLACING ON DEFERRAL IN REF WITH MEL 5203EDOOR CONFIRMED CLOSED - PLACING ON DEFERRAL IN REF WITH MEL 5203E VERIFIED FORWARD L ONE DOOR CLOSED AND SECURED.

Part: TOILET — FAULTED (ZONE 900) · airframe 80,653 hrs · 29,275 cycles

TOILET FLUSH SYSTEM DOES NOT FLUSH AFT LH LAV D FOUND PORTABLE WATER TANK DRAIN VALVE NO FULLY CLOSED, FULLY SECURED VALVE CLOSED. SINGLED OUT PORTABLE WATER TANK AIR SUPPLY (APU AND COMPRESSOR). EACH SUPPLIED NECESSARY PRESSURE TO OPERATE LAV A TOILET FLUSH WITH WATER. OK FOR CONTIUNED SERVICE.

Part: WINDSHIELD — SMOKE (ZONE 200) · airframe 79,534 hrs · 28,740 cycles

LARGE SPARKS AND SMOKE IN THE CAPTAINS FRONT WINDOW WIPER INSTALLATION. A/C WILL REQUIRE A CAT III. PARTS USED: 1528616,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1528616 SN OFF 7041 REMOVED COCKPIT GLARESHIELD TO FOM. REF AMM 56-11-11 FLAGGING SDR REF GMM 04-20-16 REMOVED WINDSHIELD REF AMM 56-11-11. STARTED TO INSTALL NEW WINDSHIELD UP TO STEP H.8. REF AMM 56-11-11. INSTALLED WIRES TO POWER AND SENSOR TERMINALS AND INSTALLED BONDING JUMPERS REF AMM 56-11-11. WINDSHIELD STILL REQUIRES SEALANT, GLARESHIELD, AMD WINDSHIELD, B73 OFF 99-5610-9-9001 7041 ON 99-5610-9-9001 7411 MAN HOUR UPDATE CONTINUED THE L1 FRONT WINDSHIELD INSTALLATION AT STEP H9. CABIN PRESURE LEAK CHECK GOOD. APPLIED SEALANT, INSTALLED GLARESHIELD AND WIPER REF AMM 56-11-11. WINDSHIELD HEAT OPS CHECK GOOD. AND WIPER OPS CHECK GOOD. ADD EMP:U349255

Part: WINDSHIELD — SPARKS (ZONE 200) · airframe 79,507 hrs · 28,728 cycles

LARGE SPARKS AND SMOKE IN THE CAPTAINS FRONT WINDOW REMOVED COCKPIT GLARESHIELD TO FOM. REF AMM 56-11-11 FLAGGING SDR REF GMM 04-20-16 REMOVED WINDSHIELD REF AMM 56-11 11. STARTED TO INSTALL NEW WINDSHIELD UP TO STEP H.8. REF AMM 56-11-11. INSTALLED WIRES TO POWER AND SENSOR TERMINALS AND INSTALLED BONDING JUMPERS REF AMM 56-11-11. WINDSHIELD STILL REQUIRES SEALANT, WIPER INSTALLATION. A/C WILL REQUIRE A CAT III.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 78,896 hrs · 28,440 cycles

(SUPPORT TASK) EMERGENCY LIGHTS ON ROW 3 TO 11 INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT ROW 10DEF IAW B737 AMM 33-51-06-960-805. SYSTEM CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 78,896 hrs · 28,440 cycles

PRIOR TO REMOVAL OF LAVATORIES OR GALLEYS, PERFORM LOCKOUT PROCEDURE FOR EMERGENCY EXIT LIGHTS PER APPLICABLE AMM.

Part: FLOORBEAM — CORRODED (BS 986, RBL8) · airframe 78,896 hrs · 28,440 cycles

CORROSION ON MAIN DECK FLOORBEAM STA 986, BL 8 RBL 43 ON TOP CHORD UPPER & LOWER SURFACE

Part: CREASE BEAM — CORRODED (R2 DOOR) · airframe 78,896 hrs · 28,440 cycles

CORROSION ON R/H CREASEBEAM ON MAIN DECK BY R2 DOOR AT STA 945-986. REMOVED CREASEBEAM R/H DAMAGE AND INSTALLED NEW CREASEBEAM. P/N 147A854008 ON MAIN DECK BY R2 DOOR AT STA 945-986 IAW SRM 51-40-02-0G-0 PAR 9, 13.

Part: FLOOR SUPPORT — CORRODED (STA 967-986) · airframe 78,896 hrs · 28,440 cycles

(B737-06-3-0049) CORROSION ON TOP SURFACE OF MAIN DECK FLOOR SUPPORT AT LBL 16 STA 967-986.

Part: FLOORBEAM — CORRODED (BS 951 RBL27-49) · airframe 78,896 hrs · 28,440 cycles

(B737-05-3-0049) CORROSION ON MAIN DECK FLOOR SUPPORT ON EDGES AT STA 951, RBL 27-49. FLOOR SUPPORT DAMAGED WAS REMOVED AND INSTLLED NEW ONE P/N:147A5 676U6 PER B737-700 SRM 51-40-02-0G-0 PAR 7.

Part: FLOORBEAM — CORRODED (BS 947 RBL37-54) · airframe 78,896 hrs · 28,440 cycles

CORROSION ON MAIN DECK FLOOR BEAM STA 947, RBL 37-54. UPPER CHORD UPPER SURFACE AND LOWER SURFACE. PERFORMED REPAIR ON MAIN DECK FLOOR BEAM STA 947 60 RBL - 60 LBL IAW B737-700 SRM 53-70-51-2R REPAIR 5 SECTION 47 PAR 4.

Part: FLOOR SUPPORT — CORRODED (STA 959, RBL 49) · airframe 78,896 hrs · 28,440 cycles

CORROSION ON MAIN DECK FLOOR SUPPORT ON TOP SURFACE AT STA 959, RBL 49. REMOVED INTERCOSTAL FLOOR SUPPORT DAMAGE AND INSTALLED NEW P/N: 147A5660U22 AT STA 959 RBL 49 IAW B737-700 SRM 51-40-02-0G-0 PAR 9,B.

Part: FLOOR SUPPORT — CORRODED (BS 974-984 RBL17) · airframe 78,896 hrs · 28,440 cycles

(B737-06-3-0049) CORROSION ON MAIN DECK FLOOR SUPPORT STA 974-984 RBL 17. REMOVED FLOOR SUPPORT DAMAGE AND INSTALLED NEW FLOOR SUPPORT P/N :140A987204 IAW B737-700 SRM 51-40-02-0G-0 PAR 9,B.

Part: CREASE BEAM — CORRODED (BS 294-328 RBL58) · airframe 78,896 hrs · 28,440 cycles

CORROSION ON R/H CREASEBEAM BY R1 DOOR ON MAIN DECK STA 294-328 RBL 58. RH CREASEBEAM ON R1 DOOR (CHORD ASSY) P/N: 654A0004-106 REPLACED PER BOEING SRM 51-40-02-0G-0 PAR 4.B,C AND PAR 7D.

Part: FLOORBEAM — CORRODED (BS 328 RBL 11) · corrosion level 2 · airframe 78,896 hrs · 28,440 cycles

(B737-06-3-0288) SEVERAL SPOTS OF CORROSION ON MAIN DECK FLOORBEAM AT RBL 11 STA 328

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 78,896 hrs · 28,440 cycles

(B737-33-3-0235) EMERGENCY LIGHTS INOP AFTER 10 MINUTES AT AFT GALLEY L/H REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW B737 AMM 33-51-06-760-805. OPS CHECK TO BE PERFORMED ON TASK CARD 4136/ 4017 SEQ 1547 PAGE 8 STEP 9.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 78,896 hrs · 28,440 cycles

(B737-33-3-0235) EMERGENCY LIGHTS INOP AFTER 10 MINUTES AT AFT GALLEY R/H REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW B737 AMM 33-51-06-760-805. OPS CHECK TO BE PERFORMED ON TASK CARD 4136/ 4017 SEQ 1547 PAGE 8 STEP 9.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 78,896 hrs · 28,440 cycles

(B737-33-3-0233) EMERGENCY LIGHTS INOP AFTER 9 MINUTES FROM ROW 22 TO LAST ROWS REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW B737 AMM 33-51-06-760-805. OPS CHECK TO BE PERFORMED ON TASK CARD 4136/ 4017 SEQ 1547 PAGE 8 STEP 9.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 78,896 hrs · 28,440 cycles

(B737-33-3-0235) EMERGENCY LIGHTS INOP AFTER 11 MINUTES AT R1 DOOR. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW B737 AMM 33-51-06-760-805. OPS CHECK TO BE PERFORMED ON TASK CARD 4136/ 4017 SEQ 1547 PAGE 8 STEP 9.

Part: SELECTOR PANEL — DAMAGED (AUDIO) · airframe 78,474 hrs · 28,239 cycles

CAPT SIDE WINDOW LEAKED WATER ONTO COMM BOX CAPT LOST ALL COMM FUNCTIONS THROUGH PARTS INFO UPDATE ONLY. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1885852 SN OFF 4488 PANEL, AUDIO SE OFF 29-2351-9-0003 4488 ON 29-2351-9-0003 4212 PANEL, AUDIO SE OFF 29-2351-9-0003 4488 ON 0000 REPLACED CAPT''S ACP REF. TO AMM 23-51-02, TESTED GOOD. PARTS USED: 29-2351-9-0003,QTY :1 ADD EMP:U146084

Part: BLEED VALVE — OUT OF LIMITS (ENG#1) · airframe 77,759 hrs · 27,959 cycles

NO LFT BLEED PRESSURE 0 PERFORMED PNEUMATIC HEALTH CHECK REF AMM 36-11-00-710-802/803. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1812315 SN OFF 6380 FOUND BLEED AIR REGULATOR AT UPPER LIMIT. REMOVED AND REPLACED BLEED AIR REGULATOR REF AMM 36-11-03-000-801/400-801. RAN NUMBER 1 ENGINE TO 70% N1. 45 PSI INDICATED OPERATIONAL CHECKS GOOD. ADD EMP:364728 REGULATOR, BLEE OFF 29-3611-9-0005 6380 ON 29-3611-9-0005 5248

Part: BATTERY PACK — FAILED (M1676) · airframe 77,227 hrs · 27,683 cycles

EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - EMERGENCY LIGHTS FROM ROW 3AB TO 11 ABC WONT STAY ON. REMOVED AND REPLACED EMERGENCY BATTERY PACK AND CHARGER ASSY M1676 PER AMM 33-51-06. OPS CHECK GOOD.

Part: LIGHT — DAMAGED (ROW 15ABC) · airframe 72,162 hrs · 25,594 cycles

ROW 15ABC UPPER SEAT MOUNTED EMERGENCY LIGHT DAMAGED. REMOVED AND REPLACED RED EMERGENCY LIGHT REF MM 33-51-11 AND CONFIG DRAWING 3350DD12295A01. OPS CK OK. VERIFIED OPERATION OF EMERGENCY LIGHTIN.

Part: VORTEX GEN — DAMAGED (HORIZONTAL STAB) · airframe 71,240 hrs · 25,246 cycles

PDA 2 ONE AFT BODY VORTEX GENERATOR MISSING ABOVE LEFT HORIZONTAL STABILIZER -- SEE PHOTO PHOTO ADDED CDL CARD 553010 FIGURE 102 CDL DEFERRAL ONLY 1 MISSING ON LEFT SIDE -- ALL OTHERS ARE PRESENT -- REQUEST APPROVED CDL APPLIED -- PARTS ADDED PER IPC 53-31-21-01 ITEM 60

Part: INTERCOSTAL — WORN (FWD E&E DOOR) · airframe 70,366 hrs · 24,910 cycles

FWD E&E DOOR R/H CUTOUT CENTER SECTION LATCH FITTING SUPPORT DOUBLER HAS WEAR MARKS. MKD 126-014. REF. AAR N/R: 9186435 GENERATED BY : V898275 ACCOMPLISHED REPAIR AT FWD E/E COMPARTMENT DOOR RT CUTOUT CENTER SECTION LATCH FITTING SUPPORT AT DOOR SURROUND RT INTERCOSTAL WEB REPAIR PER ECRA 5310-07872 AND RES WI 2017289-2.REF. AAR N/R:9186435 WORK ACCOMPLISHED BY: V900829. INSPECTED BY:V915555 ADD EMP:V095628

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,682 hrs · 24,638 cycles

SHEAR FITTING AT STA 540 RBL 6.14 IS CRACKED. 5866404-SPT REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 6.14, IAW B737-700 SRM 51-40-02 AND UNITED ECRA 5714-01177 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U355204 12/14/20 INSPECTION COMPLETE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,682 hrs · 24,638 cycles

SHEAR FITTINGS AT STA 540 LBL 54 60 IS CRACKED. 5866403-SPT REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 54.60, IAW B737 -700 SRM 51-40-02 AND UNITED ECRA 57147-01176 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U355204, 12/14/ 20 INSPECTION COMPLETE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,682 hrs · 24,638 cycles

SHEAR FITTING AT STA 540 LBL 6 14 IS CRACKED. 5866363-SPT REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 6.14, IAW B737 -700 SRM 51-40-02 AND UNITED ECRA 5714-01172 REV ORIGINAL. DATA WAS TRANSCRIBED FROM 5866363, WORK ACCOMPLISHED BY V905004, INSPECTED BY V912634 INSPECTION COMPLETE.

Part: FITTING — CRACKED (BS 540) · airframe 69,682 hrs · 24,638 cycles

SHEAR FITTING AT STA 540 LBL 40.87 IS CRACKED. 5866402-SPT REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 40.87, IAW B737 -700. SRM 51-40-02 AND UNITED ECRA 5714-01175 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U355204, 12/14/ 20 INSPECTION COMPLETE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,682 hrs · 24,638 cycles

SHEAR FITTING AT STA 540 LBL 32 40 IS CRACKED. 5866365-SPT REMOVED AND REPLACE SHEAR FITTING AT STA 540 LBL 32.40 AND SUPPORT BRACKET, IAW B737-700 SRM 51-40-02 AND UNITED ECRA 5714-01174 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTI ON U355204 INSPECTION COMPLETE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,682 hrs · 24,638 cycles

SHEAR FITTING AT STA 540 LBL 15.04 IS CRACKED. 5866364-SPT REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 15.04, IAW B737 -700 SRM 51-40-02 AND UNITED ECRA 5714-01173 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U355204 INSPECTION COMPLETE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,682 hrs · 24,638 cycles

SHEAR FITTING AT STA 540 RBL 54.60 IS CRACKED. SPT- 5866407 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 54.60, IAW B737 -700 SRM 51-40-02 AND UNITED ECRA 5714-01180 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BU UAL INSPECTION U355204 12/14/20 ACCOMPLISHED INSPECTION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,682 hrs · 24,638 cycles

SHEAR FITTING AT STA 540 RBL 15.04 IS CRACKED. 5866405-SPT REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 15.04, IAW B737 -700 SRM 51-40-02 AND UNITED ECRA 5714-01178 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UNITED INSPECTION U355204, 12/1 4/20 INSPECTION COMPLETE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,682 hrs · 24,638 cycles

SHEAR FITTING AT STA 540 RBL 32 40 IS CRACKED. 5866406-SPT REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 32.40, IAW B737 -700 SRM 51-40-02 AND UNITED ECRA 5714-01179 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U355204, 12/14/2 0 INSPECTION COMPLETE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,682 hrs · 24,638 cycles

SHEAR FITTINGS AT STA 540 LBL 54 60 IS CRACKED 5866403-SPT, MORE DETAILS AWAITED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,682 hrs · 24,638 cycles

SHEAR FITTING AT STA 540 LBL 40.87 IS CRACKED. 5866402- SPT, MORE DETAILS AWAITED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,682 hrs · 24,638 cycles

SHEAR FITTING AT STA 540 LBL 15.04 IS CRACKED. 5866364- SPT, MORE DETAILS AWAITED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,682 hrs · 24,638 cycles

SHEAR FITTING AT STA 540 RBL 15.04 IS CRACKED. 5866405- SPT, MORE DETAILS AWAITED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,682 hrs · 24,638 cycles

SHEAR FITTING AT STA 540 RBL 6.14 IS CRACKED. 5866404- SPT, MORE DETAILS AWAITED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,682 hrs · 24,638 cycles

SHEAR FITTING AT STA 540 RBL 32 40 IS CRACKED. 5866406- SPT, MORE DETAILS AWAITED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,682 hrs · 24,638 cycles

SHEAR FITTING AT STA 540 LBL 32 40 IS CRACKED. 5866365- SPT, MORE DETAILS AWAITED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,682 hrs · 24,638 cycles

SHEAR FITTING AT STA 540 RBL 54.60 IS CRACKED. SPT-5866407, MORE DETAILS AWAITED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,682 hrs · 24,638 cycles

SHEAR FITTING AT STA 540 LBL 6 14 IS CRACKED. 5866363- SPT. MORE DETAILS AWAITED.

Part: BALLAST — OVERHEATED (CABIN LIGHTS) · airframe 66,069 hrs · 23,210 cycles

SMOKE BEGAN TO FILL THE BACK OF THE CABIN. A/C DEPLANED AS QUICK AS POSSIBLE. FOUND SMOKE SOURCE, CEILING LIGHT AND BALLAST ASSEMBLY OVERHEATED ABOVE SEATS 29-30 DEF. REPLACED LIGHT ASSEMBLY OPERATED NORMAL.

Part: WINDOW FRAME — CRACKED (L1) · airframe 62,416 hrs · 21,652 cycles

L1 WINDOW FRAME UPPER EDGE FOUND CRACKED. A REPAIR WAS PERFORMED IAW ECRA 5311-01913.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 56,343 hrs · 19,202 cycles

SUPPORT TASK EEPL LIGHTS INOPERATIVE FROM ROWS 22 - 28 LT. R & R EMER POWER SUPPLY & TESTED GOOD IAW AMM 33-51-060 POSITON M1670. MFG PAGE STATION 7 27C+13, WL 212, BL L068 SN 12161 & PN D717-02-030.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,343 hrs · 19,202 cycles

SUPPORT UPON FURTHER INVESTIGATION OF NR'S 6453318 & 6453375, DENTS FOUND TO EXCEED LIMITS IAW SRM 53-00-01 PAGE 106 TABLE 102. PERFORMED SKIN REPAIR, BETWEEN STRINGER 13L & 17L AFT FS 1016 IAW SRM 53-80-01 REPAIR 2 & ECRA 5330-05656 REV ORIGINAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,343 hrs · 19,202 cycles

SUPPORT TASK RT FWD OVERWING EXIT ON UPPER PART OF DOOR IS INOPERATIVE, INBD. RELAMPED RT FWD OVERWING EXIT ON UPPER PART OF DOOR & OPERATIONAL CHECKED GOOD IAW AMM 33-51-01-960-801. LOCATION L 00751, STATION 628, WL 270 & RBL 6.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,343 hrs · 19,202 cycles

THE FOLLOWING 1ST CLASS EEPL LIGHTS ARE INOPERATIVE, INBOUND. RT FWD 2 BULLNOSE LIGHTS, CTR FWD EXIT SIGN ON LIFE RAFT 1, & CEILING EXIT LIGHT. REMOVED EMER LIGHTING BATTERY PACK SN 83769, & REPLACED WITH SN 173943 FROM THE 1ST CLASS RT FWD 2 BULLNOSE IAW AMM 33-51-06-900-805. OPERATIONS CHECKED GOOD IAW AMM 33-51-06-960-805.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,851 hrs · 18,600 cycles

LBL 24.75 LOCATION NR 1 SHOWS A CRACK INDICATION. REPAIRED INBD & OTBD SEAT TRACK FLANGES AT STATION 727B, LBL 24.75 IAW ECRA 5320-02581. SEE ALL SUB TASKS & WIPS FOR PARTIAL WORK ACCOMPLISHED.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,851 hrs · 18,600 cycles

SEAT TRACK FLANGES AT STATION 727B, RBL 45.5 IAW EA 5320-02076, ALL FOUR HOLES CRACKED. REPAIRED INBD & OTBD SEAT TRACK FLANGES IAW ECRA 5320-02581. SEE ALL SUB TASKS & WIPS FOR PARTIAL WORK ACCOMPLISHED.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,851 hrs · 18,600 cycles

LBL 45.50 LOCATION NR 1, SHOWS CRACK INDICATION. REPAIRED INBD & OTBD SEAT TRACK FLANGES AT STATION 727B, LBL 45.50 IAW ECRA 5320-02581. SEE ALL SUB TASKS & WIPS FOR PARTIAL WORK ACCOMPLISHED.

Part: TRANSMITTER — UNSERVICEABLE (TE FLAP) · airframe 54,122 hrs · 18,307 cycles

ON APPROACH AT 188 KTS CALLED FOR FLAPS 15 FLAPS, DID NOT MOVE. SHOWED SPLIT AT FLAPS 5. DURING GO AROUND FLAPS UNSPLIT & BOTH NEEDLES SHOWED ON TOP OF EACH OTHER AT FLAPS 5 LT FLAPS THERE. R & R RT FLAP TRANSMITTER IAW AMM 27-58 -01-400-801. PERFORMED ALL TESTS NO FAULTS NOTED. PERFORMED BITE ON FSEU NO FAULTS EXIST. PERFORMED LAND VERIFY IAW AMM 22-11-00. ALL TESTS PASSED. ACFT TO REMAIN NO AUTO LAND DUE TO NR 2 RADIO ALT ON PLACARD.

Part: DOOR FRAME — CRACKED (R1 DOORWAY) · airframe 47,538 hrs · 15,871 cycles

R1 DOOR STUB FRAME CRACKED AT BOTTOM TWO HOLES BS 291.50, WL 210.00 INTERIM REPAIR IAW ECRA 5311-01611,

Part: FRAME — CRACKED (BS 867) · airframe 47,538 hrs · 15,871 cycles

CABIN RT FUSELAGE FRAME HAS CRACK INDICATION AT STRINGER 8-9R BS 867 RT CABIN, REPAIRED IAW EC/RA 5310-05772.

Part: FLOORBEAM — CORRODED (BS 260) · airframe 47,538 hrs · 15,871 cycles

CABIN FLOOR STRUCTURE BS 260, RBL 10 - LBL 10 HAS SURFACE CORROSION ON UPPER SURFACE. CABIN FLOOR STRUCTURE REPAIRED IAW EC/RA 5321-01855.

Part: FRAME — CRACKED (BS 747 S8-9L) · airframe 47,538 hrs · 15,871 cycles

FRAME BETWEEN STRINGERS 8 AND 9L, BS 747, INBD FASTENERS HAS A CRACKED. FRAME REPAIRED IAW EC/RA 5310-05772.

Part: FRAME — CRACKED (BS 400) · airframe 47,538 hrs · 15,871 cycles

FRAME HAS CRACK INDICATION AT STRINGERS 8-9R, BS 400. FRAME REPAIRED IAW EC/RA 5310-05772.

Part: STRUCTURE — CORRODED (R1 DOOR) · airframe 47,538 hrs · 15,871 cycles

R1 DOOR STRUCTURE HAS CORROSION. INSTALLED R1 IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 727D) · airframe 47,538 hrs · 15,871 cycles

LEFT FRAME BETWEEN STRINGERS 8 AND 9 BS 727D BOTH FASTENERS HAS A CRACK. LT FRAME BETWEEN STRINGERS 8 AND 9 STA HAS BEEN REPAIRED IAW EA 5310-04716, REV E.

Part: FRAME — CRACKED (BS 500C) · airframe 47,538 hrs · 15,871 cycles

CABIN RT FUSELAGE FRAME HAS CRACK INDICATION AT STRINGER 8-9R BS 500C. REPAIRED EA 5310-04716, REV E, FIG 3.

Part: FRAME — CRACKED (BS 500A) · airframe 47,538 hrs · 15,871 cycles

FRAME BETWEEN STRINGERS 8 - 9L, BS 500A INBD FASTENER HAS A CRACK. REPAIRED IAW EA 5310-04716, REV E FIG 3.

Part: FRAME — CRACKED (BS 500C) · airframe 47,538 hrs · 15,871 cycles

FRAME BETWEEN STRINGERS 8 AND 9L BS 500C INBD FASTENER HAS A CRACKED. REPAIRED IAW EA 5310-04716, REV E, FIG 3.

Part: FRAME — CRACKED (BS 727B) · airframe 47,538 hrs · 15,871 cycles

RT FUSELAGE FRAME HAS A CRACK INDICATION, STRINGER 8-9R, BS 727B. FRAME REPAIRED IAW EA 5310-04716, REV E.

Part: FRAME — CRACKED (BS 787) · airframe 47,538 hrs · 15,871 cycles

FRAME BETWEEN STRINGERS 8 AND 9L, BS 787 INBD FASTENERS HAS A CRACK. REPAIRED EA 5310-04716, OP1, REV E.

Part: FRAME — CRACKED (BS 827) · airframe 47,538 hrs · 15,871 cycles

FRAME BETWEEN STRINGERS 8 - 9L, BS 827 BOTH FASTENERS HAS A CRACK. REPAIRED FRAME IAW EA 5310 -04716, REV E, OP1.

Part: PRESSURE BLKHD — CRACKED (BS 663) · airframe 46,998 hrs · 15,685 cycles

LT MLG WW VERTICAL PRESSURE WEB CRACKED BS 663 LBL 35. INSTALLED REPAIR REF SRM 57-10-10, REP.3.

Part: PRESSURE BLKHD — CRACKED (RT MLG WW) · airframe 46,998 hrs · 15,685 cycles

RT MLG WW AT FLOOR LEVEL RBL 31 TO 40, CRACKED IN PRESSURE BULKHEAD, APPROX 6 INCHES IN LENGTH. INSTALLED REPAIR IAW SRM 57-10-10 REP.3.

Part: FLAP SYSTEM — INOPERATIVE (TE FLAPS) · airframe 44,847 hrs · 14,935 cycles

FLAPS WOULD NOT COME DOWN. RAN QRH AND WAS ABLE TO GET LEADING EDGE DEVICES OUT. NO T/E FLAPS. FLAP ASSYM ALSO. PERFORMED FSEU BITE, FOUND FAULT 27-53280 R28 VAC EXC INV. FOUND CIRCUIT BREAKER T/E FLAP POS, SKEW SENSOR INDICATOR OUT. RESET CIRCUIT BREAKER, PERFORMED FLAPS/SLATS. OPS CHECKED IAW AMM 27-51-00. OPS CHECKED GOOD. OK TO CONTINUE.

Part: ELEMENT — FAILED (NR 1 ENGINE) · airframe 43,865 hrs · 14,608 cycles

ON CLIMBOUT ENG FIRE FAULT LIGHT ILLUMINATED INTERMITTENTLY TO STEADY, BECAME MORE STEADY AS FLT CONTINUED ON AIR RETURN TO EWR. REMOIVED AND REPLACED "UPPER FIRE DETECTOR ELEMENT "A". PER AMM 26-11-01 OPS CHECK GOOD. NO FAULTS NOTED AT THIS TIME. ALL INDICATIONS NORMAL. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1526285 SN OFF 07754 IPC REFERENCE.

Part: BULKHEAD — CANNING (BS 304) · airframe 32,344 hrs · 10,367 cycles

PER EA 5310-04639 REV A STEP 3.1, AFT PRESURE BULKHEAD HAS ONE OIL CAN SPOT STATION 1016 BETWEEN STR 0L AND 2L AT WATER LINE STATION 304. FABRICATED AND INSTALLED REPAIR PER ECRA 5311-01420. DIP WRITEN TO ACCOMPLISH A PERMANENT REPAIR WITHIN 12 MONTHS FROM SEPTEMBER 4, 2008. PLANNING SHOULD CONTACT ENGINEERING AFTER JULY 4, 2009 BUT BEFORE AUGUST 4, 2009 FOR PERMANENT REPAIR.

Part: INTERCOSTAL — CORRODED (BS 303-312) · airframe 32,344 hrs · 10,367 cycles

INTERCOSTAL CORRODED BETWEEN BS 303 AND 312 IN E AND E COMPARTMENT ON LEFT SIDE OF TUNNEL. REMOVED AND REPLACED INTERCOSTAL BETWEEN STATION 303 AND 312 IN E AND E COMPARTMENT ON LEFT SIDE OF TUNNEL PER SRM 51-40-02.

Part: FRAME — CRACKED (BS 440 S8-9R) · airframe 32,344 hrs · 10,367 cycles

CABIN STA 440 FRAME CRACKED BETWEEN S8-9R. INSTALLED REPAIR PER EC/RA 5310-04824 REV A.

Part: FRAME — CRACKED (BS 400 S8-9L) · airframe 32,344 hrs · 10,367 cycles

CABIN STA 400 FRAME CRACKED BETWEEN S8-9L. INSTALLED REPAIR PER EC/RA 5310-04824 REV A.

Part: STRUCTURE — CORRODED (BS 303-312) · airframe 32,344 hrs · 10,367 cycles

E AND E COMPARTMENT FRAME BETWEEN STATION 303.9 TO 312 AND STRINGER S23L AREA CORRODED. REPAIRED FRAME BETWEEN STATION 303.9 AND 312 AND STRINGER 23L PER SRM 51-70-12 REPAIR 2.

Part: FRAME — CRACKED (BS 827 S8-9R) · airframe 32,344 hrs · 10,367 cycles

CRACK IN BELT FRAME AT STA 827, BETWEEN S8-9R AT FASTENER FOR OVERHEAD BIN MOUNT. INSTALLED REPAIR PER EC/RA 5310-04824 REV A.

Part: FRAME — CRACKED (BS 440 S8-9L) · airframe 32,344 hrs · 10,367 cycles

CABIN STA 440 FRAME CRACKED BETWEEN S8-9L. INSTALLED REPAIR PER EC/RA 5310-04824 REV A.

Part: FRAME — CRACKED (BS 480 S8-9R) · airframe 32,344 hrs · 10,367 cycles

CABIN STA 480 FRAME CRACKED BETWEEN S8-9R. INSTALLED REPAIR PER EC/RA 5310-04824 REV A.

Part: FRAME — CRACKED (BS 787 S8-9R) · airframe 32,344 hrs · 10,367 cycles

CRACK IN BELT FRAME BS 787 S8-9R AT FASTENER FOR OVERHEAD BIN MOUNT. INSTALLED REPAIR PER EC/RA 5310-04824 REV A.

Part: FLOORBEAM — CORRODED (BS 773) · airframe 32,344 hrs · 10,367 cycles

AFT CARGO STATION 773 RBL 13.84 FLOOR SUPPORT HAS MILD CORROSION. FABRICATED AND INSTALLED REPAIR PER ECRA 5321-01562.

Part: FRAME — CRACKED (BS 480 S8-9L) · airframe 32,344 hrs · 10,367 cycles

CABIN STATION 480 FRAME CRACKED BETWEEN S8 LT AND S9 LT. REPAIRED CRACKED FRAME BODY STATION 480 STR 8 AND STR 9 LEFT REF EC/RA 5310-04824 REV A.

Part: FRAME — CRACKED (BS 867 S8-9L) · airframe 32,344 hrs · 10,367 cycles

CRACK IN BELT FRAME STATION 867 BETWEEN STR 8 AND 9 LEFT AT FASTENER FOR OVERHEAD BIN MOUNT. REPAIRED CRACKED FRAME BODY STATION 867 STR 8 AND 9 LEFT REF EC/RA 5310-04824 REV A.

Part: FRAME — CRACKED (BS 380 S8-9L) · airframe 32,344 hrs · 10,367 cycles

CABIN STA 380 FRAME CRACKED BETWEEN S8-9L. INSTALLED REPAIR PER EC/RA 5310-04824 REV A.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,591 hrs · 10,110 cycles

EMERGENCY LIGHTS ON BULLNOSE IN 1ST CLASS AND ABOVE R-1 DOOR ARE INOPERATIVE. INSTALLED NEW BATTERY CHARGER AND BATTERY PACK, OPERATIONAL CHECK OK PER AMM 33-51-00 AND 33-51-06.

Part: INTERCOSTAL — CORRODED (BS 947-967) · airframe 25,655 hrs · 8,150 cycles

INSPECTION FOUND INTERCOSTAL CORRODED AT STA 947.5 TO 967, RBL 51. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 25,655 hrs · 8,150 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, RBL 43. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01394.

Part: FLOORBEAM — CORRODED (BS 951) · airframe 25,655 hrs · 8,150 cycles

INSPECTION FOUND FLOOR SUPPORT BEAM CORRODED AT STA 951, RBL 24.75-41. THE FLOOR SUPPORT BEAM WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 25,659 hrs · 8,150 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 947.5, LBL 50. REPAIRED IAW ECRA 5321-01395.

Part: INTERCOSTAL — CORRODED (BS 947-967) · airframe 25,655 hrs · 8,150 cycles

INSPECTION FOUND INTERCOSTAL CORRODED BETWEEN STA 947.5 AND 967, LBL 48. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: ENGINE — VIBRATION (NR 1) · airframe 19,430 hrs · 6,143 cycles

THE NR 1 ENGINE BEGAN TO VIBRATE AND THE EGT ROSE TO GREATER THAN 710 DEGREES WHILE ON FINAL APPROACH. HE VIBRATION AND EGT RISE WERE ACCOMPANIED BY ENGINE POWER LOSS. THE ENGINE WAS NOT SHUTDOWN, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. ENGINEERING CONCLUDED THAT THE PRIMARY CAUSE OF ENGINE VIBRATION AND EGT RISE WAS DUE TO FAILURE OF THE NR 4 BEARING.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 4,606 hrs · 1,536 cycles

INSPECTION FOUND RT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. THE EMERGENCY POWER SUPPLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-51-00.