N72405

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 67,187 hrs · 28,170 cycles

THIRD LOWER HOLE ON L3 WINDOW SHOWS A CRACK INDICATION AFTER PRE-COLD REAM. 0.297" REPAIR ACCOMPLISHED ON NR - 003009272. THE L3 WINDOW POST E-F,

Part: POTABLE WATER — CONTAMINATED (ZONE 100) · airframe 67,140 hrs · 28,145 cycles

WATER HAS STRONG CHEMICAL SMELL AND TASTE REF FIM 38-10 TASK 810 DUMPED AND FLUSHED POTABLE WATER. SMELL IS NO LONGER. ACFT OK FOR SERVICE

Part: LAVATORY — ODOR · airframe 66,796 hrs · 27,975 cycles

FWD LAV RANCID SMELL POSSIBLY FROM DRAINS. FLUSHED TOILET AND SINK DRAINS WITH SANI/CLEANER FLUIDS. NO LEAKS OR SPILLAGE AROUND DRAINS/FLOOR. OK TO CONTINUE SERVICE.

Part: SLIDE — NO DISCREPANCY (ZONE 800) · airframe 65,768 hrs · 27,516 cycles

FA REPORTS 1R DOOR SLIDE LOOKS ABNORMAL IN ARMED POSITION R1 DOOR IS WITHIN LIMITS PER AMM TASK 25-66-01-200-802.

Part: COMPUTER — FAULTED (ELEVATOR FEEL) · airframe 65,101 hrs · 27,218 cycles

ELEVATOR EXCESS FORCE REQDEBRIEFED CREW-- STATED EXCESSIVE FORCE REQUIRED FOR ELEVATOR MOVEMENT, EMPHASIZED FELT HEAVY/OUT OF TRIM. OCCURRED ON CLIMB OUT TO 16K AND ON FLARE FOR LANDING, SPEED OF 162 KNOTS, LEVELED OFF AT 16K. -- NO LIGHTS OR FAULTS DURING EVENT, WHEN INITIALLY ENGAGING AUTOPILOT, INITIALLY PITCHED DOWN, DISENGAGED AUTOPILOT. SUSPECT OUT OF RIG. CREW REPORTED OVERWEIGHT LANDING--SMOOTH REMOVED ELEVATOR FEEL COMPUTER IAW AMM TASK 27-31-37-000-801 INSTALLED ELEVATOR FEEL COMPUTER IRW AMM TASK 27-31-37-400-801, UP TO, AND INCLUDING, STEP (G)(7). NEED QC VERIFICATION FOR RIG PIN REMOVAL. VERIFIED RIG PIN REMOVED AND STOWED REF AMM 27-31-37-400-801 STEP G(7). IDT REQ C/W. PERFORMED ELEVATOR FEEL COMPUTER LEAK TEST REF 27-31-17-790-801 , 27-31-37-400-801 NO LEAK DECTECTED. CONTINUED INSTALLATION TO STEP (H)(1). PITOT PROBE TOOLING IS STILL ATTACHED FOR FURTHER T/S. OBSERVED EXCESS STIFFNESS IN ELEVATOR CONTROLS WHEN SIMULATING AIRSPEEDS OF 2.46 PSIG (300 KNOTS), BUT NORMAL RESISTANCE WHEN SIMULATED PRESSURE IS RELEASED. FEEL FORCE SYSTEM TEST PASSED AT THIS TIME. COMPLETED STEPS UP TO AND INCLUDING G. (2). PECOMPLETED REF AMM AMM. 27-31-00-700-812 FROM G(3) TO COMPLETION

Part: LAMP — NO TEST (ZONE 200) · airframe 64,953 hrs · 27,155 cycles

EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK. FOUND ROW 15ABC RED EPL INOP REPLACED RED EPL LIGHT BULBS REF AMM TASK 33-51-11-960-801. EPL OPS CHECKS OKAY.

Part: SEAL — LEAKING (ZONE 800) · airframe 64,846 hrs · 27,110 cycles

PRESSURIZATION SQUEAL REPORTED AT 21A FROM CABIN CREW...NO SYSTEM ABNORMALITIES NOTED. PRESSURIZED AIRCRAFT AND IDENTIFIED A SIGNIFICANT LEAK FROM EMERGENCY EXIT DOOR AT 21A. REMOVED AND REPLACED THE BLADE SEAL REF AMM 52-09-11-400-801. LEAK CHECK GOOD. NO SQUEALING NOISE FROM INSIDE THE AIRCRAFT AT 4 PSID.

Part: CONTACT — BROKEN (ZONE 200) · airframe 64,721 hrs · 27,054 cycles

DURING REINSTALLATION OF SEAT ROW 23ABC, FOUND BLACK EMERGENCY LIGHT WIRE BROKEN OFF FROM CONNECTOR.RE-TERMINATED WIRE WITH NEW CONTACT TO BLACK EEPL IAW SWPM 20-42-01. OPS CHECK GOOD IAW AMM 33-51-00. SUPPORT TASK NSA EMX N/R 00115.

Part: BRACKET — CRACKED (ZONE 100) · airframe 64,721 hrs · 27,054 cycles

STA 663 LH WHEEL WELL FORWARD SIDE,CRACK FOUND IN BRACKET. SUPPORT TASK NSA EMX N/R 00063.

Part: PIN — INSTALLED (NLG) · airframe 63,593 hrs · 26,527 cycles

TOOK OFF. WAS UNABLE TO RETRACT NOSE GEAR. WE RAN CHECKLIST. CY CLED GEAR....DECLARED EMERGEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED. PERFORMED NOSE LANDING GEAR INSPECTION UPON ARRIVAL IN REF WITH AMM 32-21-00-200-801 AND FIM 32-30- TASK 812 - FOUND NOSE LANDING GEAR DOWN LOCK PIN REMAINED IN THE NOSE LANDING GEAR ASSEMBLY. REMOVED PIN. INSPECTION FOUND NO DAMAGE. READ, PERFORMED NOSE LANDING GEAR INSPECTION UPON ARRIVAL IN REF WITH (V912844) AMM 32-21-00-200-801 AND FIM 32-30- TASK 812 - FOUND NOSE LANDING GEAR DOWN LOCK PIN REMAINED IN THE NOSE LANDING GEAR ASSEMBLY. REMOVED PIN. INSPECTION FOUND NO DAMAGE.

Part: TIRE — BLOWN (MLG) · airframe 61,617 hrs · 25,575 cycles

POSSIBLE TIRE BLOW OUT ON TAXI IN TO GATE # 1 AND # 2 TIRE BLOW OUT ON TAXI IN TO GATE. REMOVED AND REPLACED # 1 MAIN TIRE FOR TOWING AIRCRAFT FROM TAXI WAY,REF AMM 32-45-11 WITH WHEEL ASSY S/N OFF 4340 AND WHEEL ASSY S/ N ON 2601. PARTS USED: 60-3249-9-0002,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1787614 SN OFF 4340 WHEEL, TIRE, AS OFF 60-3249-9-0002 4340 ON 60-3249-9-0002 2601 REF L/P 5318233 FOR CONDITIONAL INSPECTIONAL. PERFORMED CONDITIONAL INSPECTION PER MM 05-51-54-210-801. NO DEFECTS FOUND. REF LOG PAGES 5318188 AND 5318832 FOR #1 AND #2 BRAKE CHANGES. ALSO PEFORMED VISUAL AXEL INSPECTION WHILE BRAKES WERE OFF. NO DEFECTS NOTED. REMOVED AND REPLACED BRAKE #2 INSPECTED WHEEL AXLE FOR HEAT DAMAGE AND NONE FOUND. PARTS USED: 60-3241-9-0001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1690899 SN OFF 2779. REMOVED AND REPLACED BRAKE PER MM 32-41-41. NO LEAKS NOTED. ALSO DID VISUAL INSPECTION OF AXLE FOR HEAT DAMAGED. NO DEFECTS NOTED PARTS USED: 1690865,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1690865 SN OFF 7713.

Part: BRACKET — BROKEN (RT PACK EXH DIFF) · airframe 58,627 hrs · 24,077 cycles

RT PACK, EXAUST DUCT AFT HANGER BRACKET BROKEN IPC REF , 21-51-03-06 ITEM 30 IPC 21-51-03-06A. ITEM 5. REMOVED RIGHT PACK PRIMARY HEAT EXCHANGER AND PLENUM REF AMM 21-51-03. INSTALLED THE RIGHT PRIMARY HEAT EXCHANGER AND PLENUM /DIFFUSER ASSEMBLY,REF AMM-TASK-21-51-03-400-804-002 UP TO STEP(J). WILL REQ OPS CK. HEAT EXCHANGER OPS/LEAK CHECK GOOD REF AMM 21-51-03

Part: SKIN PANEL — DENTED (STA 480 AT S5L) · airframe 56,911 hrs · 23,302 cycles

DENTS INFUSELAGE SKIN PANEL 143A3131-77 STA 480 AT S5L. REPAIRED FUSELAGE SKIN PANEL 143A3131-77 AT STA 480 AND S5L REF ECRA 5331-02794 SEE F/C NR 9794173 FOR WORK ACCOMPLISHED.ISSUED DTA DIP L/P 7539934 FOR PERMANENT REPAIR. VERIFIED WORK PERFORMED REF EC/RA 5331-02794

Part: SKIN PANEL — DENTED (STA 500A AT S5L) · airframe 56,911 hrs · 23,302 cycles

DENTS IN FUSELAGE SKIN PANEL 143A3131-77 STA 500A AT S5L.DENTS #9,#10,#11. REPAIRED FUSELAGE SKIN PANEL 143A3131-77 AT STA 500A AND S5L REF ECRA 5331-02794 SEE F/C NR 9794174 FOR WORK ACCOMPLISHED.ISSUED DTA DIP L/P 7539934 FOR PERMANENT REPAIR. VERIFIED WORK ACCOMPLISHED REF EC/RA 5331-02794

Part: SKIN — NONE (STA 500F-500H) · airframe 56,894 hrs · 23,294 cycles

REF FLEET CYCLE LOG PAGE 9790017. INITIATE A DIP TO STATE "ACCOMPLISH INITIAL INSPECTION OF FUSELAGE REINFORCED AREA AT STA 500F TO STA 500H AND S2R TO S-3L ON OR BEFORE THE AIRCRAFT REACHING 50,000 TOTAL FLIGHT CYCLES" PER EC/RA 5331-02792 STEP E.1. EC/RA #5331-02792 STEP E.1. INITIATED A DTA DIP " ACCOMPLISH INITIAL INSPECTION OF FUSELAGE REINFORCED AREA AT STA 500F TO STA 500H AND S2R TO S-3L ON OR BEFORE THE AIRCRAFT REACHING 50,000 TOTAL FLIGHT CYCLES" . PER INITIATED A DTA DIP " ACCOMPLISH INITIAL INSPECTION OF FUSELAGE TOMC-APPROVAL FROM SC1ELBYC COMMENT REINFORCED AREA AT STA 500F TO STA 500H AND S2R TO S-3L ON OR BEFORE THE AIRCRAFT REACHING 50,000 TOTAL FLIGHT CYCLES" . PER EC/RA #5331-02792 STEP E.1.. NO INSPECTION BUYBACK REQUIRED. NOT AN RII ITEM QC QC REVIEWED. T/A: 50,000 TAFC...SP/U366013 RECORDS UPDATE...SP

Part: SKIN — DENTED (STA500A) · airframe 56,894 hrs · 23,294 cycles

DENT IN SKIN PANEL 143A3111-29 NEAR STA 500A AND S-2R...REQUIRES A REPAIR DOUBLER TO BE INSTALLED REFORMED DENT, PERFORMED ALL REQUIRED INSPECTIONS, FAB''D REPAIR PARTS, TREATED, PRIMED, INSTALLED AND PAINTED IN REF TO ECRA#5331-02790 CONFIRMED COMPLIANCE WITH ALL EC/RA 5331-02790 STEPS. GENERATED DTA DIP ELB L/P# 7538923 AND ENTERED INTO ESFR

Part: SKIN — DENTED (STA480) · airframe 56,894 hrs · 23,294 cycles

DENTS INFUSELAGE SKIN PANEL 143A3131-77 STA 480 AT S5L. REPAIRED FUSELAGE SKIN PANEL 143A3131-77 AT STA 480 AND S5L REF ECRA 5331-02794 SEE F/C NR 9794173 FOR WORK ACCOMPLISHED.ISSUED DTA DIP L/P 7539934 FOR PERMANENT REPAIR. VERIFIED WORK PERFORMED REF EC/RA 5331-02794

Part: SKIN — DENTED (STA500A) · airframe 56,894 hrs · 23,294 cycles

DENTS IN FUSELAGE SKIN PANEL 143A3131-77 STA 500A AT S5L.DENTS #9,#10,#11. REPAIRED FUSELAGE SKIN PANEL 143A3131-77 AT STA 500A AND S5L REF ECRA 5331-02794 SEE F/C NR 9794174 FOR WORK ACCOMPLISHED.ISSUED DTA DIP L/P 7539934 FOR PERMANENT REPAIR. VERIFIED WORK ACCOMPLISHED REF EC/RA 5331-02794

Part: SKIN — DENTED (STA787) · airframe 56,894 hrs · 23,294 cycles

DENTS IN SKIN PANEL 146A3101-35 NEAR STA 787 AND S2L REQUIRE DOUBLER /TRIPLER INSTALLATION REF ECRA 5331-02800. MAJOR REPAIR UPGRADED TO RII REPAIRED FUSELAGE SKIN PANEL 146A3101-35 NEAR STA 787 AND S2L.REF ECRA 5331-02800.SEE F/C L/P 9794510 FOR WORK ACCOMPLISHED.ISSUED DTA DIP L/P 7531692 FOR INITIAL INSPECTION OF REPAIR AREA. VERIFIED ALL WORK ACCOMPLISHED PER F/C L/P 9794510.

Part: SKIN — CRACKED (STA 138.7) · airframe 56,894 hrs · 23,294 cycles

RH HORIZ STAB LOWER INSPAR SKIN CRACKED AT STA 138.7 DIRECTLY AC ROSS FROM DRAIN HOLE.CRACK IS APPROX .500 IN LENGTH(ENDS OF CRAC K VERIFIED WITH EDDY CURRENT AND MARKED) REPEAT INSPECTIONS-DVI 9000 FLIGHT CYCLES AND EXTERNAL LFEC 9000 FLIGHT CYCLES REF 737NDT PART 6,51-00-26 FIG 1. REPAIRED STAB INSPAR SKIN STA 138.7 REF SRM 55-10-01-2R-11.SEE F /C L/P 9786939 FOR WORK PERFORMED.ISSUED DIP FOR INSP REQUIREMEN TS AS FOLLOWS(INSPECTION THRESHOLD 56000 TOTAL FLIGHT CYCLES. VERIFIED REPAIRED STAB INSPAR SKIN STA 138.7 REF SRM 55-10-01-2R-11.SEE F /C L/P 9786939 FOR WORK PERFORMED.ISSUED DIP FOR INSP REQUIREMEN TS AS FOLLOWS(INSPECTION THRESHOLD 56000 TOTAL FLIGHT CYCLES.

Part: SKIN — NONE (L2 DOOR) · airframe 56,894 hrs · 23,294 cycles

CATERING TRUCK HIT AIRCRAFT REAR LEFT DOOR FOUND DENT ON L2 DOOR 6 IN VELOW HANDLE, 8 IN FWD AFT EDGE OF DO OR. DENT DIMS L: 2.00 IN ; W: 1.500 IN; Y: 0.150 IN. INSPECTED P ER SRM 52-10-01. OK TO DIP FOR REINSPECTION EVERY 1500 F/HRS. FOUND DENT ON L2 DOOR 6 IN BELOW HANDLE, 8 IN FWD AFT EDGE OF DO TOMC-APPROVAL FROM SC1ELBYC COMMENT OR. DENT DIMS L: 2.00 IN ; W: 1.500 IN; Y: 0.150 IN. INSPECTED P ER SRM 52-10-01. OK TO DIP FOR REINSPECTION EVERY 1500 F/HRS. LINMITS ENTERED INCORRECTLY. SHOULD BE A DEAD LIMIT OF 5 FLT THIS ITEM IS TO BE REINSPECTED AT OR BEFORE EVERY 1500 FLT QC REVIEWED CYCLES HOURS QC REVIEWED RIR: 1500 FH...MB/V740009 SEE LOG PAGE 7102365 FOR ALL WORK ACCOMPLISHED. REOPEN IAH U305497 13JUN18 FOR: PREMATURE CLOSING ITEM DID NOT MEET MINIMUM FLIGHT REQUIREMENTS BEFORE CLOSING. TOMCQC REV PERFORMED PER SRM 52-10-01 ALLOWABLE DAMAGE 3 PAGE 104, THE REINSPECTION I RECORDS UPDATE...MB/V740009 S TO OCCURE EVERY 1500 FLT HRS. WHQLM LINK REINSPECTED DENT NO PROGRESSION NOTED, DIP REMAINS. ADD EMP:U190230 REINSPECTED DENT NO PROGRESSION NOTED, DIP REMAINS. REINSPECTED DENT. NO FURTHER DAMAGE NOTED. DIP REMAINS. REINSPECTED DENT NO PROGRESSION NOTED, DIP REMAINS. INSTALLED REPAIR DOUBLER PER SRM#52-00-01-2R-3. SEE FLEET CYCLE LP#9786677 FOR REPAIR DETAIL. TOMCQC REV PERFORMED VERIFIED ALL WORK ACCOMPLISHED ON NON ROUTINE 9786677 CLEARED LOG PAGE, REINSPECTION NO LONGER REQUIRED AS CATEGORY A REPAIR WAS INSTALLED PER SRM 52-00-01-2R-3 REPAIR 3, PARA 2.A. P ER PREVIOU

Part: SPAR — CRACKED (STA663) · airframe 56,894 hrs · 23,294 cycles

LEFT MAIN GEAR WHEEL WELL, CENTER WING BOX REAR SPA VERTICAL WEB, STA 663 LBL 34.83, AND APPROX. 4" FROM CEILING, HAVE A CRACK INDICATION REF FLEET CYCLE LP# 9786603. THIS LP IS FOR DIP AND ESFR ONLY. REPAIR DISCREPANCY REF SRM 57-10-10 2R-3 ALT 2. SEE LP# 9786603 FOR ALL WORK ACCOMPLISHED. THIS LP FOR DIP AND ESFR ONLY. TOMC APPROVED FOR DIP TO PERFORM INSPECTIONS AS GIVEN IN SRM TOMC-APPROVAL FROM SC1ELBYC COMMENT 57-10-10-2R-3 TABLE 205/REPAIR 3 AND FIGURE 208/REPAIR 3 AT 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION AND REPEAT INSPECTIONS AT 36,000 FLIGHT CYCLE INTERVALS HANGE TO NONE INSP INITIATED DIP TO PERFORM INSPECTIONS AS GIVEN IN TABLE Q/C REVIEWED. 205/REPAIR 3 AND FIGURE 208/REPAIR 3 AT 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION AND REPEAT INPECTIONS AT 36,000 FLIGHT CYCLE INTERVALS. INSPECTION METHODS WILL BE HFEC AND LFEC. Q/C REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: BULKHEAD — CRACKED (RH WHEEL WELL) · airframe 56,894 hrs · 23,294 cycles

RIGHT MAIN GEAR WHEEL WELL, CENTER WING BOX REAR SPAR VERTICAL WEB AT STA 663, RBL 42 , APROX 5" FROM CEILING, HAVE A CRACK INDICATION REF FLEETCYCLE LOG PAGE 9786602 INITIATED DIP TO PERFORM INSPECTIONS AS GIVEN IN TABLE FLIGHT CYCLE INTERVALS. INSPECTION METHOD WILL BE HFEC AND LFEC. 205/REPAIR 3 AND FIGURE 208/REPAIR 3 AT 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION AND REPEAT INSPECTIONS AT 36,000 TRIMMED OUT DAMAGE SECTION OF WEB, FABRICATED AND INSTALLED REPAIR PER SRM 57-10-10-2R-3 ALT 2. SEE FLEETCYCLE LP 9786602 FOR DETAILS OF WORK ACCOMPLISHED. THIS LP FOR DIP AND ESFR ONLY! TOMC APPROVED FOR DIP TO PERFORM INSPECTIONS AS GIVEN IN SRM TOMC-APPROVAL FROM SC1ELBYC COMMENT 57-10-10-2R-3 TABLE 205/REPAIR 3 AND FIGURE 208/REPAIR 3 AT 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION AND REPEAT INSPECTIONS AT 36,000 FLIGHT CYCLE INTERVALS Q/C REVIEWED. Q/C REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,892 hrs · 23,293 cycles

EMERGENCY BATTERY PACK INOP MOUNTED ON THE CEILING PANEL JUST TO THE RIGHT OF THE FDR ACESS PANEL REMOVE AND REPLACE EMERGENCY BATTERY PACK MOUNTED ON THE CEILING PANEL JUST TO THE RIGHT OF THE FDR ACCESS PANEL REF. 737-900 AMM 33-51-06 REV 75

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,892 hrs · 23,293 cycles

EMERGENCY BATTERY PACK INOP LOCATED ON ROW 27CBA BEHIND DADO PANEL REMOVE AND REPLACE EMERGENCY BATTERY PACK LOCATED ON ROW 27CBA BEHIND DADO PANEL REF. 737-900 AMM 33-51-06 REV 75

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,892 hrs · 23,293 cycles

EMERGENCY BATTERY PACK INOP MOUNTED ON THE CEILING PANEL JUST TO THE LEFT OF THE FDR ACCESS PANEL REMOVE AND REPLACE EMERGENCY BATTERY PACK MOUNTED ON THE CEILING PANEL JUST TO THE LEFT OF THE FDR ACCESS PANEL REF. 737-900 AMM 33-51-06 REV 75

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,892 hrs · 23,293 cycles

EMERGENCY BATTERY PACK INOP MOUNTED JUST TO THE RIGHT OF THE FWD ENTRY LIGHT PANEL REMOVE AND REPLACE EMERGENCY BATTERY PACK MOUNTED JUST TO THE RIGHT OF THE FORWARD ENTRY LIGHT PANEL REF. 737-900 AMM 33-51-06 REV 75

Part: CABLE — DISCONNECTED (EMERGENCY LIGHT) · airframe 55,292 hrs · 22,552 cycles

SEAT MOUNTED EMERGENCY EXIT PATH LIGHT IS INOP AT SEAT 11, RELAMPED, NO HELP. FOUND SEAT TO SEAT CABLE DISCONNECTED, RE CONNECTED, OP CHECKED GOOD. REF AMM SUBTASK 33-51-11-710-001.

Part: PANEL — MISSING (WIND TO BODY) · airframe 55,002 hrs · 22,435 cycles

PDA 1 PANEL 193 CR MISSING FROM AIRCRAFT. INSTALLED SERVICABLE PANEL 193CR.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,340 hrs · 22,159 cycles

RED EMERGENCY LIGHTS ON PAX SEATS INOP. REMOVED AND REPLACED CHARGER ASSY AND BATERY PACK IAW AMM 33-51-06-960-805. TEST OK. RED EMERGENCY LIGHTS WORKING GOOD.

Part: CABLE — DISCONNECTED (SPLR INTERLOCK) · airframe 53,492 hrs · 21,775 cycles

GEAR HANDLE WOULD NOT COME UP ON T/O... RED T/O WARNING LIGHT AF TER FLAP RETRACTION. FOUND GRND SPOILER INTERLOCK CABLES DISCONNECTED, RECONNECTED AN D SAFETIED AS PER AMM 27-62-51-400-801 ACCOMPLISHED GROUND SPOILER INTERLOCK VALVE FUNCTIONAL TEST AND FOUND NORMAL PER AMM 27-62-61. ACCOMPLISHED MAIN LANDING GEAR OPERATIONAL TEST PER AMM 32-32-09-710-801 AND FOUND NORMAL. OK TO CONTINUE IN SERVICE. WITNESSED GROUND SPOILER FUNCTIONAL TEST AND MAIN LANDING GEAR O PERATIONAL TEST. ALL TESTS PASSED. OK FOR FURTHER SERVICE.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 50,280 hrs · 20,322 cycles

R2 DOOR EXIT SIGN LENS WILL NOT STAY ON. REPLACED EMERGENCY LIGHT ASSY AND OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,076 hrs · 19,787 cycles

EMERGENCY LIGHTS OUT AT ROWS 32 & 33F. REMOVED AND REPLACED BATTERY PACK AT ROW 32F PER AMM 33-51-06-201-960-805.

Part: FUSE — FAULTY (CABIN) · airframe 49,076 hrs · 19,787 cycles

EMERGENCY LIGHTS OUT AT ROWS 19,20 AND 21CBA. REMOVED AND REPLACED FUSES AT POWER AT ROW 20CBA PER AMM 33-51-06-960-804. OPS CHECK GOOD.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 48,014 hrs · 19,329 cycles

CRACK FOUND ON LEFT HORIZONTAL STAB LOWER SKIN AT HSS 184. 7 AND 11 INCHES FROM FRONT SPAR, VERIFIED NDT 737 PART 6,51-00-00-23. CUT OUT DAMAGE AND INSTALLED A REPAIR IAW SRM 55-10-01,REPAIR 11.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 47,045 hrs · 18,934 cycles

RT AFT OVERWING EMERGENCY EXIT LIGHT INOP RELAMPED LIGHT IAW AMM 33-51-04. OPS CHECK GOOD.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 40,754 hrs · 16,485 cycles

CRACK INDICATION FOUND AT FASTENER HOLES COMMON TO SEAT TRACK OTBD & INBD FLANGES LOCATED AT FWD OF STATION 727B AT RBL 24.75. TRIMMED CRACKED AREAS, FABRICATED REPAIR SPLICE, MATERIAL USED 7075T6 0.125 INCHES, REPAIR FILLER NR 1 MATERIAL USED 7075T6 0.090 INCHES, REPAIR FILLER NR 2, MATERIAL USED 7075T6 0.16 0 INCHES. TREATED, PRIMED & INSTALLED IAW RES NR 2007446-16.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 40,754 hrs · 16,485 cycles

FOUND CRACK AT MAIN CABIN SEAT TRACK FASTENER HOLE LOCATED AT FRAME 727B LBL 24.75 OTBD FLANGE. TRIMMED CRACKED AREAS, FABRICATED & INSTALLED REPAIR PARTS IAW AAR-MIA RES NR 200744 6-12. THIS ECRA 5320-02328 PROVIDES APPROVED PERMANENT REPAIR INSTRUCTIONS FOR THE DAMAGED CHORDS.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 40,754 hrs · 16,485 cycles

CRACK INDICATION FOUND AT FASTENER HOLES COMMON TO SEAT TRACK OTBD & INBD FLANGES LOCATED AT FWD STATION 727B RBL 45.50. TRIMMED CRACKED AREAS, FABRICATED REPAIR SPLICE, MATERIAL USED 7075T6 0.125 INCHES, REPAIR FILLER NR 1 MATERIAL 7075T6 0.090 INCHES, REPAIR FILLER NR 2 MATERIAL USED 7075T6 0.160 INCHES. TREATED, PRIMED & INSTALLED IAW RES NR 2007476-17.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 40,754 hrs · 16,485 cycles

FOUND CRACK AT MAIN CABIN SEAT TRACK FASTENER HOLES LOCATED AT FRAME 727B LBL 45.50 OTBD & INBD FLANGES. DISCREPANCY TRIMMED CRACKED AREAS, FABRICATED & INSTALLED REPAIR PARTS IAW AAR-MIA RES NR 200744 6-13. THIS ECRA 5320-02328 PROVIDES APPROVED PERMANENT REPAIR INSTRUCTIONS FOR THE DAMAGED CHORDS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,754 hrs · 16,485 cycles

CRACK FOUND BETWEEN STRINGER 8R & 9R STATION 400 AT THE OUTLET EXTRUSION SUPPORT BRACKET INBD ATTACHMENT RIVET. SDR FORM ATTACHED. REPAIR CRACKED AREA AT STATION 400 FRAME BETWEEN STRINGER 8R TO 9R IAW EA 5310-04716 REV G.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,754 hrs · 16,485 cycles

CRACK FOUND BETWEEN STRINGER 8L & 9L, FRAME STATION 727B AT THE ACFT OUTLET EXTRUSION SUPPORT BRACKET INBD ATTACHMENT RIVET. REPAIRED CRACKED ANGLE IAW EA 5310-0476 REV G.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,754 hrs · 16,485 cycles

CRACK FOUND BETWEEN STRINGER 8L & 9L, FRAME STATION 500L AT THE OUTLET EXTRUSION SUPPORT BRACKET INBD ATTACHMENT RIVET. REPAIRED CRACKED AREA IAW EA 5310-04716 REV G.

Part: INTERCOSTAL — CORRODED (BS 328-344) · airframe 40,754 hrs · 16,485 cycles

CABIN AREA INTERCOSTAL BETWEEN STATION 328 - 344 LBL 11 SHOWS AREAS OF CORROSION. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS, LOCATED & DRILL IAW SRM 51-10-02 PG 10. INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02 & 53-10-5 PG 101.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,754 hrs · 16,485 cycles

CRACK FOUND BETWEEN STRINGER 8R, FRAME STATION 500A AT THE ACFT OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT RIVET. REPAIRED CRACKED AREA IAW EA 5310-04716 REV G.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,754 hrs · 16,485 cycles

CRACK FOUND BETWEEN STRINGER 8L & 9L, FRAME STATION 867 AT THE ACFT OUTLET EXTRUSION SUPPORT BRACKET INBD ATTACHMENT RIVET. SDR FORM ATTACHED. REPAIRED CRACKED AREA IAW EA 5310 -04176 REV G OP 3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,754 hrs · 16,485 cycles

FOUND BETWEEN STRINGER 8L, FRAME STATION 500H AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET INBD ATTACHMENT RIVET. REPAIRED CRACKED AREA AT FRAME STATION 500H BETWEEN STRINGER 8R TO 9R IAW EA 5310-04716 REV G.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,754 hrs · 16,485 cycles

CRACK FOUND BETWEEN STRINGER 8R & 9R FRAME STATION 727B AT THE ACFT OUTLET EXTRUSION SUPPORT BRACKET INBD ATTACHED RIVET. REPAIRED CRACKED AREA IAW EA 5310-0476 REV G OP3 REV G.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,754 hrs · 16,485 cycles

CRACK FOUND BETWEEN STRINGER 8L & 9L, FRAME STATION 787 AT THE ACFT OUTLET EXTRUSION SUPPORT BRACKET INBD ATTACHMENT RIVET. SDR FORM ATTACHED. REPAIRED CRACKED ANGLE IAW EA 5310-04716 REV G OP 03 REV G.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,754 hrs · 16,485 cycles

FOUND BETWEEN STRINGER 8R & 9R, FRAME STATION 440 AT THE ACFT OUTLET EXTRUSION SUPPORT BRACKET INBD ATTACHMENT RIVET. SDR FORMS ATTACHED. REPAIRED CRACKED AREA IAW EA5310-04716 REV G.

Part: FLOOR SUPPORT — CORRODED (BS 947-986) · airframe 40,754 hrs · 16,485 cycles

CABIN AREA FLOOR SUPPORT BS 947.5 - 986.5 CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS SRM 53-70-15. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,754 hrs · 16,485 cycles

CABIN AREA FLOOR SUPPORT ANGLE STA992-1009 RBL 32 SHOW AREA OF CORROSION. REMOVED AND REPLACED FLOOR SUPPORT ANGLE AT MAIN CABIN STA 992 TO 1009 RBL 32 IRW B737-900 SRM 51-40-02.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 37,374 hrs · 15,188 cycles

FIRST CLASS SECTION EMERGENCY LIGHT HAS A LOW CHARGE, VERY DIM. REPLACED BATTERY CHARGER AND BATTERY PACK. OPS CHECKED NORMAL. OK FOR SERVICE.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 33,074 hrs · 13,504 cycles

LT HORIZONTAL STABILIZER LOWER SKIN HAS A .750 IN. CRACK AT STA B STA 138.25 IN. FROM THE SKIN L/E. TREATED, PRIMED, FILLER AND DOUBLER. EXISTING DOUBLER WAS REMOVED AND INCORPORATED WITH THIS LOG PAGE AND LOG PAGE# 9965766. INSTALLED REPAIR REF SRM 55-10-01 DETAIL D.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 33,074 hrs · 13,504 cycles

LEFT HORIZONTAL STAB LOWER SKIN CRACK INDICATION AT STAB STATION 147.90 16.5 INCHES AFT OF FRONT SPAR TREATED AND PRIMED FILLER AND DOUBLER, EXISTING DOUBLER WAS REMOVED, AND INCORPORATED WITH THIS LOG PAGE AND LOG PAGE NUMBER 9 965678, INSTALLED REPAIR REFERENCE SRM 551001 DETAIL D.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,945 hrs · 13,460 cycles

F/A REPORTED "BURNT PEANUT" FUMES IN FWD COACH CABIN, WITH RECIRC FANS OFF, THE ODOR WENT AWAY. ANOTHER F/A REFERRED TO SMELL AS BURNT RUBBER. F/A IN AFT GALLEY REPORTED NO FUMES. PERFORMED TASK 05-51-26-800-801C1 WITH ENG RUNS AND RECIRC FAN TEST NO DEFECTS. FOUND CEILING LIGHT ASSY AT ROW 8ABC INOP RE- PLACED P/N 4041-12. OPS CKS NORMAL. REPLACED RECIRC FILTERS AS PRECAUTIONARY.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 32,281 hrs · 13,213 cycles

FAULT LIGHT AND APU DET INOP LIGHT ILLUMINATED ENGINE AND APU FIRE DETECTION SYSTEM WILL NOT TEST. WHEEL WELL FIRE DETECTION SYSTEM TEST OK. T/S PER FIM TASK 26-10-00-810-801 FOUND ALL LIGHTS ILLUMINATED ON FRONT OF ENG/ APU FIRE DETECTION CONTROL MODULE M 279. REMOVED AND REPLACED MODULE REF AMM 26-10-01-400-801, OPS CHECK NORMAL. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1470582 SN OFF 03249 PANEL, CONTROL, OFF 29-2615-9-0001 3249 ON 29-2615-9-0001 0470.

Part: DUCT — SEPARATED (BLEED AIR SYS) · airframe 32,157 hrs · 13,163 cycles

RT DUCT PRESS & LT; 10 PSI AT CLIMB PWR ON GROUND 0 PSI. T/S FOUND ECS CONTROL LINE P/N 332A2350-14 SEPARATED. REPOSITIONED PRECOOLER CONTROL VALVE AND REPLACED LINE AS REQ`D PERFORMED ENGINE RUNS, PNEUMATIC PRESSURES NORMAL.

Part: FRAME — PUNCTURED (FUSELAGE) · airframe 27,585 hrs · 11,411 cycles

AFT PIT FRAME AT STATION 947.5, AT STRINGER 25R, HAS A PUNCTURE ON INNER CHORD FROM ELONGATED SCREW. PERFORMED INTERIM REPAIR PER ECRA5311-01498,PT.1. ACCOMPLISH PERMANENT REPAIR WITHIN 24 MONTHS FROM 18-JUN-10. PLANNING TO CONTACT ENGINEERING AFTER 22 MOS, BUT BEFORE 23 MOS, FOR PERM REPAIR. NOTE TO PLANNING: THIS ECRA BEING EVAL'D FOR DMG TOLERANCE UNDER 14CFR 25.571 + WILL LIKELY BECOME PERM WITH REPEAT INSPECTIONS. QC INTERIM REPAIR ACCOMPLISHED PER ECRA 5311-01498, PART 1. ACCOMPLISH A PERMANENT REPAIR WITHIN 24 MONTHS FROM 18-JUN-10. PLANNING TO CONTACT ENGINEERING AFTER 22 MONTHS BUT BEFORE 23 MONTHS FOR A PERMANENT REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 23,358 hrs · 9,813 cycles

FLOORBEAM 986.5 HAS CORROSION LBL 5 TO RBL 44. INSTALLED ONE FLANGE REPAIR REF SRM 53-00-51 REPAIR 1 AND ECRA 5310-04886.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 23,358 hrs · 9,813 cycles

LEFT HORIZONTAL STABILIZER CRACKED AT STATION 147.90 APPROXIMATELY 10 INCHES AFT OF FRONT SPAR. FABRICATED AND INSTALLED FILLER AND DOUBLER PER ECRA 5510-01961. DIP GENERATED ON LOG PAGE 9703646.

Part: SKIN — CORRODED (FUSELAGE) · airframe 23,358 hrs · 9,813 cycles

BOTTOM ATC ANTENNA AIRCRAFT SURFACE CORRODED. CLEANED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-01. FABRICATED AND INSTALLED DOUBLER PER ECRA 5330-03875.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 23,358 hrs · 9,813 cycles

FLOOR SUPPORT CRACKED AT STA 344 TO 360, BL 0. REMOVED AND INSTALLED FLOOR SUPPORT IAW SRM 51-40-02.

Part: SKIN — DENTED (AFT CARGO DOOR) · airframe 23,358 hrs · 9,813 cycles

DENT ON AFT CARGO DOOR IS OUT OF LIMITS, 15 INCHES FROM FWD EDGE 32 INCHES FROM BOTTOM EDGE. INSTALLED REPAIR DOUBLER AND PAINTED REPAIR AREA IAW SRM 52-00-01, REPAIR 3.

Part: BATTERY — DISCHARGED (CABIN) · airframe 19,049 hrs · 8,033 cycles

THE EMERGENCY LIGHT BATTERY ABOVE AFT GALLEY A/C RIGHT WOULD ONLY HOLD CHARGE FOR 1 MINUTE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY. CHECKS GOOD IAW AMM 33-51-06-960-805.

Part: BATTERY — DISCHARGED (CABIN) · airframe 19,049 hrs · 8,033 cycles

THE EMERGENCY LIGHT BATTERY AT 21 DEF WOULD ONLY HOLD 4 MIN CHARGE. THE BATTERY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW AMM 33-51-06-960-805.