N33264

Part: A/C PACK — FAULTED (ZONE 100) · airframe 75,741 hrs · 26,826 cycles

AIR RETURN PGUM - PGUM UPDATE FROM CREW: BURNING OIL SMELL IN CABIN, VERY DISTINCT OIL SMELL CLIMBING THROUGH 22K GOT WORSE ON DECENT. ALL INDICATIONS WERE NORMAL. FLIGHT CREW REPORTS STRONG SMELL OF BURNING OIL AT FLIGHT LEVEL 220 AND SMELL INCREASED ON DESCENT ENGINE RUN PERFORMED FOR FLUSHING THE LUBE, SUMPS, AND BLEED SYSTEMS PER AMM 72-00-00-100-803-F00 (4)(H)(2). OPERATED ENGINE AT IDLE WITH NO FUMES OR ODOR DETECTED IN THE COCKPIT OR CABIN. PERFORMED INSPECTION PER AMM 05-51-26-800-801-C1 COMPLETED UP TO ITEM L. NO FAULTS OR EVIDENCE OF ANY FUILD IN PNEUMATIC DUCT SYSTEM OR SMOKE FROM ELECTRICAL COMPONENTS FOUND DURING COMPLETED INSPECTION. UPDATED WORK PERFORM PER AMM 05-51-26-800-801-C1 PERFORMED WORK UP TO DETAILED INSPECTION PARAGRAPH D ITEM (1) STEP (K) NEED TO CONTUINE AT STEP (L) CONT'D W/ MM 05-51-26, ITEM (1) TO DETERMINE SOURCE OF SMOKE/ODORS C/W. C/W ITEM (2) DETAILED OPERATION CHECKS W/ NO FINDINGS. RAN NR 1 & 2 AT HIGH POWER W/ ENG BLEEDS ON, APU BLEED OFF, PACKS ON & ISOLATION VALVE CLOSED W/ NO EVIDENCE OF SMOKE OR UNUSUAL ODOR IN COCKPIT OR CABIN, REF MM 71-00-00, NEED DISPOSITION FROM TOMC AS PER ITEM D.(3) OF MM 05-51-26. CONFIRMED W/ TOMC OK TO CLEAR THIS LOG PAGE W/ NO ADDITIONAL MAINTENANCE REQUIRED, OK TO CONTINUE.

Part: ACM — FAULTED (RIGHT) · airframe 75,655 hrs · 26,793 cycles

PACK TRIP OFF LIGHT LIGHT ON ON GROUND, LIGHT COMES ON AGAIN AFT ER RESET RIGHT PEFERRED RH PACK PER MEL 2101B. PERFORMED PZTC BITE, FOUND TCV FAULT. FURTHER T/S FOUND ACM IN-OP. RIGHT PACK TRIP. RESET RH PACK. PLACARD INSTALLED. MEL 2101B REJECTED FOR MEL CHANGE DEFERRED RH PACK TEMP CONTROL VALVE PER MEL 2133B. PERFORMED PZTC BITE, FOUND RT TCV FAULT. CAP AND STOWED RT TCV ELECTRICAL PLUG.VERIFIED STAND-BY TCV OPERATES NORMAL. PLACARD INSTALLED. TOMC APPROVED ITEM DEFERRED. RECONNECTED RH TCV ELECTRICAL CONNECTOR. MEL CHANGED TO 2133E, REF LOG PAGE 6857948 RIGHT PACK PLACED ON MEL. PERFORMED RH PACK TEMP CONTROL VALVE RESTORATION PER AMM 21-00-00-440-812. RECONNECTOR AND PLACED MANUAL OVERRIDE VALVE BETWEEN OPEN AND CLOSED POSITION. WITH PACK COOLED, PERFORMED #2 ZONE TEMP CNTL BITE TEST, BITE TEST PASSED. OPS CHK'D RT PACK AND NOTICED PACK DISCHARGE TEMP RISING CAUSING PACK TO TRIP WITH TCV AND STBY TCV FULLY CLOSED. REMOVED HPWS MIX MUFF PER AMM 21-51-04 AND TRIED TO MANUALLY TURN ACM, FOUND ACM SEIZED. R/H PACK REQ'S ACM REPLACEMENT. M&L LISTING UPDATED. REF L/P: 6857948 - REMOVED AND REPLACED RH ACM PER AMM 21-51-04. PERFORMED PZTC BITE NO FAULTS NOTED. OPS CHECK NORMAL. LEAK CHECK NONE. OKAY FOR SERVICE. PLACARD REMOVED. MEL CLEARED.

Part: CHAIN — EXPOSED (ZONE 800) · airframe 75,368 hrs · 26,693 cycles

2R GIRT BAR INFLATION CHAIN EXPOSED PERFORMED CHECK ON 2R GIRT BAR, INFLATION CHAIN IS PROPERLY SECURED AND NOT VISIBLE/EXPOSED. REF AMM 25-66-01

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 75,310 hrs · 26,672 cycles

INOPERATIVE EMERGENCY LIGHT FWD. REPLACED BATTERY FOR FWD RIGHT SIDE OPS CHECK GOOD PER AMM 33-51-06.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 75,212 hrs · 26,636 cycles

AFT CARGO COMPARTMENT UNDER FLOOR CORROSION PREVENTION & CONTROL PROGRAM (CPCP) INSPECTION. AFT CARGO BAY LT STRINGER 25 AT BS 847 HAS HEAVILY CORRODED BUILD UP FORWAD OF BULKHEAD. CLEANED & INSPECTED S25L, BS 807-847. REMOVED FASTENERS FROM SHEAR TIES AT BS 827-847 BETWEEN S24L - S25L. REMOVED CORRODED STRINGER S25L IAW SRM 53-00-03. REMOVED SHEAR TIE BS 867, S24 - 25L. ACCOMPLISHED HFEC INSP. NO DEFECTS NOTED. DURING STEPS 5 THRU 7 HFEC INSP. FOUND HEAVY CORROSION AT BS 792 S25L AND BULGING ON EXTERNAL SKIN AT SAME LOCATION. REMOVED CORRODED STRINGER FROM BS 776 - 816. REMOVED SHEAR TIE S24 & 25L. PERFORMED HFEC AT TRIMMED AREA. NO DEFECTS NOTED NTM PART 6 51-00-00 PROCEDURE 23. FABRICATED REPAIR SPLICE

Part: LAMP — NO TEST (ZONE 200) · airframe 75,158 hrs · 26,615 cycles

EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - L/H OVERHEAD BINS #22, #24 AND #27 AREA LIGHT ARE INOP. RELAMPED L/H OVERHEAD BINS #22, #24, AND #27 AREA LIGHTS REF AMM TASK 33-51-03-960-801. OPS CHECK WAS GOOD REF AMM 33-51-03. OK FOR SERVICE.

Part: PRECOOLER — FAULTED (NR 1 ENGINE) · airframe 73,389 hrs · 25,955 cycles

BLEED TRIP OFF LIGHT COMES ON DURING CRUISE LIGHT NO. 1 RAN QRH LIGHT CAME BACK ON. PERFORMED NO.1 ENGINE BLEED AIR SYSTEM HEALTH CHECK, RESULT NO DEFECT FOUND IAW AMM TASK 36-11-00-700-801. REMOVED AND REPLACED #1 ENG PRECOOLER CONTROL VALVE IAW AMM 36-12-02 AND #1 ENG PRECOOLER CONTROL VALVE SENSOR IAW AMM 36-12-03. INSTALLATION AND LEAK TESTS GOOD. OPERATED BOTH ENGINE PER MM 36-00-00-860-804, OPS CHKS GOOD. NO BLEED TRIP OR DUCT SPLIT NOTED. OK FOR SERVICE. ADD EMP:U274351

Part: SKIN — DENTED (ZONE 800) · airframe 73,294 hrs · 25,914 cycles

DENT WITH PULLED FASTENERS IN DOOR SURROUND SKIN AT AFT EDGE OF FWD CARGO BAY DOOR BETWEEN STRINGERS S20R AND S21R DENT MEASURES 6.3X 1.2, WITH A MAX DEPTH OF 0.043" ADDING PICRURE INSPECTION TASK, PERFORMED HFEC ON CUTOUT REF NTM PART 6 51-00-00 PROCEDURE 23. NO INDICATIONS NOTED. REQUIRES HOLE PROBE INSPECTION. DENT FOUND TO BE BEYOND LIMITS FOUND IN SRM 53-00-01. REQUIRES TRIMMED DAMAGED AREA AT AFT EDGE OF FWD CARGO DOOR SURROUND PER REMOVED EXISTING FASTENERS FROM REPAIR AREA. OPEN FASRENER HOLES OPEN HOLES REQUIRE HFEC INSPECTION REPAIR SR, 53-00-01-2R-25. CUT EDGE REQUIRES HFEC INSPECTION REQUIRE HFEC INSPECTION PER SRM 53-00-01-2R-25 CW HFEC ON REMOVED FASTENER HOLES PER NTM PART 6 51-00-00, NO RII TASK, VERIFIED REPAIR MATERIAL (DOUBLER & FILLER) PO#''S. DEFECTS NOTED. OK TO CONTINUE. FABRICATED INNER DOUBLER AND DOUBLER FROM 0.080 2024 T3 CLAD DRAFT MEASUREMENT FOR REPAIR PARTS AND DRILLED NEW HOLES, PICK SHEET PO 3807116330, OUTER DOUBLER FROM 0.160 2024 T3 CLAD UP EXISTING HOLES ON REPAIR PARTS. PER SRM 53-00-01-2R-25 SHEET, PO 267415330, AND FILLER FROM TWO LAYERS OF 0.100 2024 T3 CLAD SHEET PO 4569336 PER SRM 53-00-01-2R-25 GRIPPED FASTENERS LENGHT, STARTED TO RIMMED HOLES FINAL SIZE. REF SRM 51-40-02; SRM 53-00-01-2R-25. REQUEST TO DIP FOR RECURRENT INSPECTION OF REPAIR AND BEARSTRAP PER SRM 53-00-01-2R-25, STEP T-1-A DIP 53-DIP REFERENCE TO LOG 3606561 FOR SRM 53-00-01-2R-25 DIP INSPECTION LIMITS. RII TASK, C/W INSPECTION OF REPAIR AND MATERIALS REF SRM.

Part: TRANSMITTER — FAULTY (HYD SYSTEM) · airframe 72,539 hrs · 25,635 cycles

HYD SYS A SHOWED CONSISTANT INDICATION OF QTY LOSS IN CRZ FLIGH T PER TOMC'S REQUEST R&R HYD 'A' SYS QTY TRANSMITTER IAW AMM REF 29-33-12-400-801. OPERATION & INDICATIONS CHECKED NORMAL. NO LEAKS NOTED AT THIS TIME. HYD SYS 'A' FLT DECK QTY INDICATION READS 95% WHILE RESERVOIR READS FULL. FOR REFERENCE, WITH THE INDICATORS ON THE RESERVOIR TRANSMITTERS [1] SERVICED TO THE F (FULL) POSITION, MAKE SURE THAT THE QUANTITY INDICATION SHOWN ON THE SYSTEM DISPLAY IN THE FLIGHT DECK SHOWS 1006%/-9%. SUBTASK 29-33-12-210-005 PARTS USED: 29-2909-9-9001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1527188 SN OFF 1815 TRANSMITTER, HY OFF 29-2909-9-9001 1815 ON 29-2909-9-9001 2009 SDR GENERATED

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,384 hrs · 25,215 cycles

FOUND EMERGENCY BATTERIES FOR M1670 AND M1672 INOPERATIVE (REF A AR NR 100011180)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 71,384 hrs · 25,215 cycles

PASSENGER CABIN EMERGENCY LIGHT, BATTERY PACK M1670 FAILS OP CHE CK (REF. AAR NR 100007647).

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 71,384 hrs · 25,215 cycles

RH HORIZONTAL STAB LWR SKIN - TWO CRACKS WERE FOUND AT STA 129.50 LOCATED AT 12" & 21" FORWARD FROM REAR SPAR. MARKED ON SKIN. (REF: AAR NR 100007979)

Part: WINDOW FRAME — CRACKED (R1 WINDOW) · airframe 71,384 hrs · 25,215 cycles

AFTER NDT INSPECTION PER EA5310-04554 REV C, OP 004 , AT RH 1 WI NDOW FRAME FOUND TO BE CRACKED. (REF AAR NR 100007984) WORK PERFORMED ON ROUTINE CARD 3502117-2000-0221, CUST W/C: 7384383, EA 5310-04554 REV. C. OP 004.

Part: SKIN — UNKNOWN (CARGO DOOR) · airframe 71,384 hrs · 25,215 cycles

PER CUST-REQ REMOVE AND REPLACE AFT CARGO DOOR EXTERNAL SKIN LOG 4683070. (REF AAR NR 100007731) REMOVED AND REPLACED AFT CARGO DOOR EXTERNAL SKIN IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, SRM 51-40-08-0G-0, SRM 51-20-01-0G-0, AMM 51-21-72-370-803, SRM 52-30-01-2R-3, AMM 51-21-99-300 AND DRW 146A6110

Part: SKIN — UNKNOWN (CARGO DOOR) · airframe 71,384 hrs · 25,215 cycles

PER CUST -REQ REMOVE AND REPLACE FWD CARGO DOOR EXTERNAL SKIN . REMOVED AND REPLACED FWD CARGO DOOR EXTERNAL SKIN IAW SRM 52-30-01-2R-3,51-40-02-0G-0,51-40-05-0G-0,51-40-08-0G-0,AMM 51-21-41-370-803,51-21-72-370-804,51-31-00-390-804,51-21-99-300- 801,51-21-99-300-801 & BOEING DWG 143A6110 REMOVED AND REPLACED FWD CARGO DOOR EXTERNAL SKIN IAW SRM 52-30-01-2R-3,51-40-02-0G-0,51-40-05-0G-0,51-40-08-0G-0,AMM 51-21-41-370-803,51-21-72-370-804,51-31-00-390-804,51-21-99-300- 801,51-21-99-300-801 & BOEING DWG:143A6110.

Part: FITTING — CRACKED (STA540 LBL15.04) · airframe 70,095 hrs · 24,617 cycles

B737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 15.04 IS CRACKED SUPPORT TASK NSA EMX NR 00072

Part: FITTING — CRACKED (STA540,RBL15.04) · airframe 70,095 hrs · 24,617 cycles

B737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRACKED SUPPORT TASK NSA EMX NR 00071

Part: PUMP — SEIZED (HYD SYS) · airframe 70,055 hrs · 24,599 cycles

ENG 2 LOW PRESSURE LIGHT LIGHT ON REMOVED #2 ENG EDP PER MM 29-11-11-000-801-001. REMOVED AND REPLACED SEALOIL SEAL PER 72-60-00. OUTER O RING WAS WARPED. PERFORMD INSPECTIONS PER STEP F.11 TO END. FOUND PUMP SIEZED AND CASE DRAIN FILTER DAMAGED. ALL OTHER REQUIRED INSPECTIONS OK. INSTALLED NEW EDP PER MM 29-11-11-400-801-001 UP TO AND INCLUDING STEP H.12 REF L/P 5886659 FOR HYD SYSTEM FLUSH PARTS USED: 29-2910-9-0003,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1535728 SN OFF 9955 PUMP, HYD ENG D OFF 29-2910-9-0003 9955 ON 29-2910-9-0003 8979 PUMP, HYD ENG D OFF 29-2910-9-0003 9955 ON 0000 REF L /P 5886647 FOR ENGINE OIL FLUSH. CONTINUED WITH AMM 29-11-11-400-801-001 FROM STEP I. TO COMPLETION. OPS AND LEAK CHECK GOOD. OK TO CONTINUE.

Part: PROBE — FAILED (RT FUEL TANK) · airframe 67,044 hrs · 23,231 cycles

RIGHT TANK FUEL DECREASD 1000LBS FOR UNKNOWN REASON. REMOVED AND REPLACED NR 1 FQIS TANK UNITS F15L, F1L, F2L, F3L, AND NR 2 FQIS TANK UNITS F15R, F1R, F2R, F3R, F4R, F5R, F6R, F7R, F8R, F9R, F10R, F12R IAW AMM 28-41-21-000/400-801. . FQIS TEST PASS REF AMM 28-41-00-730-801. A/C FQIS BACK NORMAL. OK TO RETURN TO SERVICE.

Part: AOA — DAMAGED (CAPTAINS) · airframe 61,989 hrs · 21,205 cycles

CAPT`S PITCH LIMIT INDICATOR CAME DOWN 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 RELATED WORK ORDER 000000003001138 AND PRTR CAPT AOA REPLACED, REF AMM 34-21-05-400-801. PERFORMED AOA SYSTEM TEST AND DFCS BITE 34-21-05-730-801 & 22-11-00-810-801. ALL CHECK NORMAL, OK TO CONTINUE. MAC METER INITIATED WITH VENDOR ID CAPT AOA REPLACED, REF AMM 34-21-05-400-801. PERFORMED AOA SYSTEM TEST AND DFCS BITE 34-21-05-730-801 & 22-11-00-810-801. ALL CHECK NORMAL, OK TO CONTINUE. UPDATED DATED ROTABLE PARTS CHANGE. ROTABLE PARTS CHANGE WAS INDICATED-TT NR 1040350 SN OFF 6527 SENSOR, ANGLE O OFF 29-3412-9-0001 6527 ON 29-3412-9-0001 4422.

Part: ANTENNA — DAMAGED (VHF) · airframe 60,224 hrs · 20,533 cycles

RAMP REPORTS POSSIBLE DAMAGE TO VERTICLE ANTENNA ON TOP OF FUSELAGE MID SECTION OF AC

Part: CHARGER — INOPERATIVE (CABIN) · airframe 53,757 hrs · 18,063 cycles

DOOR 2L EMERGENCY EXIT INDICATOR LIGHT INOP. .REPLACED BATTERY CHARGER OP CHECK NORMAL REF AMM 33-51-06.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 49,126 hrs · 16,199 cycles

R1 DOOR STUB FRAME ASSEMBLY CRACKED AT APPROX STATION 296, WL 210. R & R R1 DOOR STUB FRAME IAW SRM 51-40-02, PN 141A8371U8.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 49,126 hrs · 16,199 cycles

ONE INCH CRACK FOUND IN WEB OF RT WW FWD BULKHEAD LOCATED BETWEEN RBL 31.83 & RBL 40.00 & WL 200.6 - 192.0. INSTALLED CATEGORY B REPAIR AT RT VERTICAL PRESS DECK IAW SRM 57-10-10 REPAIR 3 ALT 1 PARA 4 FIG 203.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,126 hrs · 16,199 cycles

FORWARD ENTRY FLOORBEAM HAS CORROSION ON TOP SURFACE LOCATED AT STATION 344 & BL 0. INSTALLED UPPER FLOORBEAM CHORD REPAIR IAW ECRA 5321-01929.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,126 hrs · 16,199 cycles

FORWARD ENTRY FLOORBEAM HAS CORROSION ON TOP SURFACE LOCATED AT BS 328 & RBL 0 - RBL 55, LOCATION IS APPROX. REMOVED DAMAGED SECTION OF UPPER FLOORBEAM CHORD. FABRICATED & INSTALLED UPPER T CHORD REPAIR IAW ECRA 5321-01930.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 49,126 hrs · 16,199 cycles

2" CRACK FOUND IN WEB OF LT WW FWD BULKHEAD, LOCATED BETWEEN LBL 40.00 - 45.64 & WL 200.6 - 192.0. INSTALLED CATEGORY B REPAIR AT WING CTR SECTION REAR SPAR VERTICAL PRESS DECK LT SIDE IAW SRM 57-10-10 REPAIR 3 ALTERNATIVE 2 PARAGRAPH 5 FIGURE 204.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,851 hrs · 15,398 cycles

R2 EXTERIOR EMER LIGHT WILL NOT ILLUMINATE. TROUBLE SHOT & FOUND LAMP INOPERATIVE AT R2 EMER LIGHT IAW WDM 33-51-14. REPLACED LAMP & PERFORMED FUNCTIONAL CHECK OF EMER LIGHT IAW AMM 33-54-04. FOUND OK.

Part: BRAKE — DAMAGED (MLG) · airframe 43,943 hrs · 14,331 cycles

NUMBER 1 MLG BRAKE DAMAGED. REPLACED NR 1 MLG BRAKE IAW AMM 32-41-41-000-801 & 32-41-41-400-8 0. ROTABLE PARTS CHANGE WAS INDICATED TT 1528254 SN OFF 07754 BRAKE, MLG, STE OFF 58-3241-9-0001 7754 ON 58-3241-9-0001 1080.

Part: CONTROL ROD — OUT OF ADJUST (R2 DOOR) · airframe 40,545 hrs · 13,124 cycles

AFTER TAKEOFF ADVISED BY F/A R2 DOOR HAD A LOUD NOISE, AND FRONT OF DOOR NOT SEALED SHUT. WE DID NOT HAVE A WARNING LIGHT IN COCKPIT. AIR RETURN. FOUND FWD LATCH ROLLER HITTING LATCH RECEIVERS. ADJUSTED HORIZONTAL CONTROL ROD IAW AMM 52-13-00-820-801. STEP O. OPS CHECK GOOD.

Part: DOOR — LOOSE (R2) · airframe 39,198 hrs · 12,658 cycles

AFTER TAKEOFF, ACFT FAILED TO PRESSURIZE, F/A IN AFT CALLED AND SAID AFT DOOR R2 CLOSED, HANDLE SET CLOSED BUT HE COULD SEE A SPACE BETWEEN DOOR AND ACFT. RETURNED TO DEPARTURE. NO DOOR LIGHT ON OVERHEAD. FOUND FWD EDGE OF R2 DOOR NOT FAIRED. CLOSED DOOR PROPERLY AND FOUND DOOR FAIRED. LUBRICATED DOOR GUIDE ARM AND TIGHTENED ALL HARDWARE. DOOR OPERATES NORMAL. DOOR LIGHT OPERATES NORMAL AND FWD EDGE OF DOOR ALWAYS GRABS THE CATCH AND CLOSES NORMAL.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 37,777 hrs · 12,165 cycles

ON TAXI OUT, F/A COMPLAINED OF MIST IN AFT CABIN, ODOR OF SULFER, AND THROAT IRRITATION. ACCOMPLISHED FIM TASK 05-51-26-0800-801C. FOUND ODOR EMINATING FROM AFT OVENS. REMOVED FOOD SCRAPS FROM SAME. NO ODOR NOTED ON ENGINE RUN. O/B CREW SUPPLIED WITH FORM 46-6020, SMOKE-ODOR IN ACFT. ACFT OK FOR SERVICE.

Part: DOOR — UNSECURE (R2) · airframe 37,425 hrs · 12,032 cycles

AIRCRAFT FAILED TO PRESSURIZE AFTER TAKEOFF. F/A REPORTED AIR RUSHING OUT SOUND AT R2 DOOR. ON ARIVAL, FOUND R2 DOOR INCORRECTALLY CLOSED. VERIFIED DOOR OPERATION, ALL CHECKED NORMAL. ACFT OK TO CONTINUE.

Part: DOOR — NOT CLOSED (CABIN) · airframe 35,552 hrs · 11,337 cycles

A/C DID NOT PRESSURIZE AFTER TAKEOFF. F/A REPORTED DOOR L2 NOT PROPERLY CLOSED. NO DOOR ANNUNCIATOR DOOR LIGHT ILLUMINATED FOUND R-2 DOOR NOT CLOSED PROPERLY. L2 CHECKS OK. CYCLED R-2 DOOR. DOOR CLOSED NORMALLY. PER FLT CREW NO OVERWEIGHT CONDITION ON LANDING OCCURRED.

Part: WIRE — DAMAGED (COCKPIT) · airframe 33,955 hrs · 10,769 cycles

DURING CLIMB THE NR 2 OVERHEAT AND ENG 2 CUT OFF LIGHT COME ON AND OFF 4 TIMES. THEY WERE ON FOR 1 SEC AND THEN WENT OFF. RETURNED TO EWR. T/S PER FIM 26-10-00-810-805. FOUND WIRES DAMAGED ON STUDS FOR M1757. REMOVED AND REPLACED MW0316 PER WDM 26-11-11 PAGE 1 AND REPLACED M279 DUE TO DAMAGE ON ONE OF RETENTION BAR. OPS CHECK GOOD. RUN ENGINE NR 2 FOR SAFETY FACTOR. OK FOR SERVICE. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1442321, S/N OFF 01395 PANEL, CONTROL OFF 29-2615-9-0001 1395, ON 29-2615-9-0001 1359.

Part: PRESSURE BLKHD — CANNING (FUSELAGE) · airframe 33,934 hrs · 10,760 cycles

APB SHOWS SIGN OF OIL CANNING AT S7L TO BL 0 OUTER PERIMETER. SEE PAGE 30 OF EA5310-04639 FOR LOCATION OF DAMAGE. REPAIRED PER ECRA5310-05379. SEE FORM 44.0008 ATTACHED 3 PAGES FOR PARTIAL WORK. ISSUE A DIP TO ACCOMPLISH A PERMANENT REPAIR PRIOR TO 46760 TOTAL FLIGHT CYCLES. PLANNING TO CONTACT ENG AFTE 39760 BUT BEFORE 40760 TOTAL FLIGHT CYCLES FOR A PERMANENT REPAIR. FOUND OIL CAN DAMAGE ON APB. PER ECRA 5310-05379 COMPLETED INTERIM REPAIR. C/W PERMANENT REPAIR PRIOR TO 46,760 TOTAL FLT CYCS. PLANNING TO CONTACT ESC AFTER 39,760 TOTAL FLT CYCS NOT TO EXCEED 40,760 TOTAL FLT CYCS FOR PERMANENT REPAIR. 1) INIT: AFTER 39760 BUT BEFORE 40760 TOTAL A/C F/C (PLG/ENG) & 2) T/A: W/I 46760 TOTAL A/C F/C-ODEE

Part: SUPPORT BRACKET — CRACKED (BS 440) · airframe 33,934 hrs · 10,760 cycles

SUPPORT TASK RT BODY STA 440R SHOW CRACK AT I/B FASTENER FOR SUPPORT BRACKET MFEC EA 5310-04716 REV C. REPAIRED PER EA 5310-04716 REV C .

Part: SKIN — CRACKED (HORIZ STAB) · airframe 33,934 hrs · 10,760 cycles

RT HORIZ STAB LOWER SKIN SHOWS CRACK INDICATION AT STAB STA 147.90 I/B SIDE OF RIB 8, 17 .5 INCH FWD IF AFT EDGE IF AFT SPAR. REF STEP 5 OF EA 5510-01843 OP 1. RT HORIZ STAB LOWER SKIN REPAIRED PER EC/RA 5510-02171.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 33,934 hrs · 10,760 cycles

RT HORIZ STAB LOWER SKIN SHOWS CRACK INDICATION AT STAB STA 147.90 I/B SIDE OF RIB 8, 9 .5 INCH FWD OF AFT EDGE OF AFT SPAR. REF STEP 5 OF EA 5510-01843 OP 1. RT HORIZ STAB LOWER SKIN REPAIRED PER EC/RA 5510-02171.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,934 hrs · 10,760 cycles

SUPPORT TASK: RT BODY STA 380 R SHOW CRACK BOTH FASTENER FOR SUPPORT BRACKET EA 5310-04716. (MFEC) REPAIRED FRAME RT STA 380 R AT BRACKET IN REF TO EA 5310-04716 REV C.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,934 hrs · 10,760 cycles

SUPPORT TASK RT BODY STA 500C SHOW CRACK AT I/B FASTENER FOR SUPPORT BRACKET (MFEC) EA 5310-04716 REV C. INSTALLED REPAIR ON RT BODY STA 500C FOR SUPPORT BRACKET IAW EA 5310-04716 REV C.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,868 hrs · 8,917 cycles

AFT LEFT OVERHEAD EMERGENCY LIGHT NOT ILLUMINATING. REMOVED AND REPLACED BATTERY PACK AFT LEFT OVERHEAD. OPERATIONAL CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,868 hrs · 8,917 cycles

OVERHEAD EMERGENCY LIGHT IN AFT GALLEY NOT ILLUMINATING. REMOVED AND REPLACED BATTERY PACK OVER AFT GALLEY. OPERATIONAL CHECKS GOOD.

Part: SLIDING WINDOW — CRACKED (COCKPIT) · airframe 28,489 hrs · 8,780 cycles

L-2 WINDOW CRACKED. REPLACED L-2 WINDOW PER AMM TASK 56-12-11-400-801. CHECKS NORMAL ROTABLE PARTS CHANGE WAS INDICATED S/N OFF 05264.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,319 hrs · 8,101 cycles

CABIN FLOORBEAM AT STATION 328 REQUIRES A SINGLE FLANGE REPAIR, AFT SIDE FROM RBL 28 TO RBL 38 DUE TO CORROSION. REPAIRED AFT FLOORBEAM FLANGE IAW B737 SRM 53-00-51 AND MODIFIED INTERCOSTAL AT RBL 24 IAW ECRA-5321-01590.

Part: CONTROL LEVER — DIRTY (COCKPIT) · airframe 9,445 hrs · 2,708 cycles

WHEN GEAR WAS EXTENDED FOR LANDING INTO EWR, THREE GREEN AND THREE RED LIGHTS WERE RECEIVED ON THE MAIN PANEL AND THERE WERE THREE GREENS ON THE OVERHEAD. THE GEAR WAS CYCLED DURING A GO-AROUND AND THE GEAR EXTENDED NORMALLY WITH PROPER INDICATIONS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LANDING GEAR CONTROL LEVER DIRTY. THE CONTROL LEVER WAS CLEANED AND LUBRICATED. OPERATIONAL CHECKS WERE NORMAL.