N73259

Part: A/C PACK — ODOR (ZONE 100) · airframe 70,706 hrs · 26,058 cycles

DANK SMELL COMING FROM PACKS AT LOW ALTITUDES W/ RAM DOORS OPEN RAN THE PACKS FOR DURATION OF 20MIN, SMELL WENT AWAY. REF FIM 21-00 TASK 806.

Part: GIRT BAR — OUT OF LIMITS (ZONE 800) · airframe 70,305 hrs · 25,856 cycles

EXCESS SLIDE MATERIAL ABOVE GIRT BAR DOOR 1R. RETUCKED GIRT Z-FOLD TO PROPER GIRT PAYOUT DIMENSION PER AMM 25-66-01-400-801 D (2)(C)(D).

Part: POTABLE WATER — ODIFEROUS (ZONE 100) · airframe 69,182 hrs · 25,371 cycles

WATER SUPPLY IN LAVATORY POOR QUALITY AFT RH LAV E DRAINED AND SERVICEDTHE PORTABLE WATER SYSTEM A COUPLE OF TIMES AND RAN THE WATER FAUCETS AT ALL LAVATORIES. NO BAD SMELLS OR SINGS OF WATER CONTAMINATION WERE FOUND. REF AMM 38-10 TASK 810

Part: LIGHT — DETACHED (ZONE 200) · airframe 68,750 hrs · 25,189 cycles

LAV D AFT LOWER EMERGENCY LIGHT BROKE OFF UPON REMOVAL REMOVED AND REPLACED LAV D EMERGANCY LIGHT. IAW B737 AMM 33-51-14 OPS TEST GOOD NO DEFECTS NOTED.

Part: ELEC CONNECTOR — DAMAGED (ZONE 200) · airframe 68,349 hrs · 25,009 cycles

SEAT ROW 14ABC EPL HAS EXPOSED WIRE AND ALSO MISSING LOCKING MECHANISM ON THE CONNECTOR. SUPPORT TASK NSA EMX N/R 00120.SECURED SEAT ROW 14ABC EEPL SHIPSIDE WIRING IAW B737-800 SWPM 20-10-11. REMOVED SEAT ROW 14ABC SEAT SIDE EE[PL CONNECTOR IAW B737-800 SWPM 20-42-01 AND WDM 33-51-21. INSTALLED SERVICEAB LE AT ROW 14ABC SEAT SIDE EEPL CONNECTOR(PN:17023) IAW B737-800 SWPM 20-42-01 AND WDM 33-51-21. PERFORMED OPS CHECK FOR SEAT ROW 14ABC EEPL LIGHT IAW B737-800AMM 33-51-00-710-801. AND 33-51-00-720-801. OPS CHECK GOOD. IAW B737-800 AMM 33-51-00-710- 801 AND 33-51-00-720-801.

Part: ANGLE — CRACKED (ZONE 100) · airframe 68,349 hrs · 25,009 cycles

STA 663 LEFT WHEEL WELL FORWARD BULKHEAD VAPOR BARRIER ANGLE IS CRACKED.

Part: FITTING — CRACKED (STA540) · airframe 68,349 hrs · 25,009 cycles

SUPPORT TASK - SHEAR FITTING AT STA 540 AND RBL 6.14 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 6.14 I IAW SRM 51-40-02-0G AND BAC DWG 111A2000 REV ORIGINAL FO 06.

Part: FITTING — CRACKED (ZONE 200) · airframe 68,349 hrs · 25,009 cycles

SHEAR FITTING AT STA 540 AND LBL 15.04 IS CRACKED. SUPPORT TASK NSA EMX N/R 00075. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 15.04 IAW B737-800 SRM 51-40-02-0G AND BAC DWG 111A2000 REV ORIGINAL F 04.

Part: FITTING — CRACKED (STA540) · airframe 68,349 hrs · 25,009 cycles

SHEAR FITTING AT STA 540 AND LBL 6.14 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 6.14 I AW B737-800 SRM 51-40-02-OG AND BAC DWG 111A2000 REV ORIGINAL FO 05.

Part: FITTING — CRACKED (ZONE 200) · airframe 68,349 hrs · 25,009 cycles

SHEAR FITTING AT STA 540 AND RBL 15.04 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 15.04 IAW B737-800 SRM 51-40-02-0G AND BAC DWG 111A2000 REV ORIGINAL F 7.

Part: HOSE — LEAKING (WATER SEPARATOR) · airframe 67,239 hrs · 24,479 cycles

RIGHT PACK LIGHT ILLUMINATED DDP COMPLIED WITH, DEACTIVATED RT PACK FCV PER MEL 2101B DDP COMPLIED WITH. PLACARDED RT PACK SWITCH INOP. OK TO PLACARDED FLT DECK RT PACK SWITCH. OK TO CONTINUE. CONTINUE. APPROVED CONTROLLERS IN REF WITH AMM-21-62 TASK 801. NO FAULTS NOTED AT HISTORY. WILL NEED FURTHER TROUBLESHOOTING DUE TO FAULT BEING EDURE F. STEP (1-7) VERIFY STCV IS FULL CLOSED WITH PACK RUNNING, DEACTIVATED RT PACK. MEL REMAINS DUE TO PREVIOUS INTERMITTENT. CHECK STCV SENSE LINES TO CONDENSER FOR DEFECTS. NOTE FAULTS. RECONNECTED RT PACK, RAN PACKS AT FULL LOAD FOR 20 MINS COULD POTENTIAL CHRONIC: REF. FIM 21-53TASK820. BITE BOTH TEMP CONTROL CHECKED SENSE LINES ON RT PACK, NO DEFECTS NOTED. NOT DUPLICATE RT PACK FAULT. PERFORMED BITE CHECK ON BOTH LERS NOTE FAULTS THEN DO APPLICABLE FIM. DO FAULT ISOLATION PRO NEED SINGLE OR DUAL CHANNEL FAULTS TO START REPLACING COMPONETS DUE TO ALL OPS CHECKS PASSING DURING TROUBLESHOOTING. RII INSPECTION NOT REQUIRED REF GMM 09-25-05 ENSURED STCV FULL CLOSED WITH PACK RUNNING. ACCOMPLISHED OPS FOUND HOSE INBOARD OF RT PACK WATER EXTRACTOR TO BE LEAKING, REPLACED LEAKING HOSE, NO LEAKS WITH PACK RUNNING, RAN PACK WITH UNABLE TO CLEAR DUE TO MAJOR REPAIR, RADA SYSTEM REF MM 21-51-00-730-802. OPS CHECK GOOD EXCESSIVLY.

Part: A/C PACK — NONE (RIGHT) · airframe 67,255 hrs · 24,488 cycles

PREVIOUS UPDATES SUGGESTED THIS ITEM CAN BE CLEARED. CONFIRMED THE RH PACK IS OPERATIONAL AND THE MEL CAN BE CLEARED RAN AND OPS CHECKED REF AMM 21-51-00-730-802. RH PACK HAS BEEN RE-ACTIVATED AND OK FOR SERVICE. THIS ITEM WAS FLAGGED BY TECH FLAGGED MAJOR REPAIR, SFR, AND SDR IN ERROR. NONE OF THESE MEET THE REQUIREMENT FOR THIS LOG PAGE AND CONDITION.

Part: ARM — LOOSE (AUTOPILOT) · airframe 66,968 hrs · 24,359 cycles

A SYSTEM AUTO PILOT ARM IS LOOSE. SECURED A SYSTEM AUTO PILOT ARM REF AMM 22-11-25-400-801 CYCLED MANY TIMES AND FOUND BINDING.

Part: PITOT TUBE — LOOSE (FUSELAGE) · airframe 66,970 hrs · 24,360 cycles

A SYSTEM AUTO PILOT ARM IS LOOSE. SECURED A SYSTEM AUTO PILOT ARM REF AMM 22-11-25-400-801 CYCLED MANY TIMES AND FOUND BINDING.

Part: SKIN — DAMAGED (AFT CARGO DOOR) · airframe 66,873 hrs · 24,309 cycles

PER S.R, RE-SKIN AFT CARGO DOOR (REF: AAR NR 100008122) REPLAVED AFT CARGO DOOR SKIN IAW B737 800 AMM 51-21-99,51-31-00, 51-21-72,51-21-41, SRM 52-30-01-2R-3, 51-40-08-0G-0,51-40-05-0G- 0,51-40-02-0G-0 AND BOEING DWG:146A6110 REV.C.

Part: FORGING — CRACKED (L1 WINDOW) · airframe 66,873 hrs · 24,309 cycles

AFTER NDT INSPECTION PER EA5310-04554 REV C, OP-003, AT LH #1 WINDOW FRAME FOUND TO BE CRACKED. REMOVED DAMAGE (CRACK) ON #1 LH WINDOW FRAME IAW EA 5310-04554 OP 003, REV C, CONFIG B.

Part: WARNING LIGHT — ILLUMINATED · airframe 66,817 hrs · 24,281 cycles

AUTO FAIL LIGHT LIGHT ON, ALTN LIGHT NOT ON ALTN LIGHT CAME ON INITIALLY BUT WENT OUT AFTER A FEW SECONDS C URRENTLY ALT IS CONTROL CPC BITE SHOWS OFV LRU FAIL MESSAGE. REF FIM 21-31 801 AND 802 ACCOMPLISHED SUCCESSFUL SYSTEM TESTS OF CPC 1&2. NO FAULTS SHOWN. INTERMITTENT FAULT, OFV OPS CK GOOD.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 66,714 hrs · 24,236 cycles

PDA 1 REF L/P 7625580 #8 SPOILER FOUND DELAMINATED BY PASSENGER DURING FINAL APPROACH. PASSENGER HAD PICTURES PRIOR TO PANEL DELAMINATING. TOP SECTION OF PANEL DELAMINATED AS WELL AS LESS THAN 25% OF THE HONEYCOMB.DELAMINATED PANEL ON RIGHT WING INBOARD SPOILER UPON ARRIVAL AT GATE VERIFIED #8 SPOILER DAMAGE. INCLUDE PICTURES. REMOVED #8 SPOILER REF AMM 27-61-11-000-810 INSP INSTALL OF #8 SPOILER FROM STEP 3.F(2)(H), 3F(K)4 INTO 3G(6). AMM 27-61-11-400-801. ACP FLIGHT SPOILER ADJUSTMENT IAW AMM 27-61-00-820-803 UP TO & INCLUDING STEPS 5.F(3)M. VERIFIED NO.8 SPOILER EFFECTIVITY IN IPC. CHECKED FOR PROPER INSTALLATION OF NO.8 SPOILER THROUGH STEPS 3.F.(2)(K)(2) AND 3.F.(2)(I)(2) EXCEPT STEP 3.F.(2)(J). REF AMM 27-61-11-400-801 AND GMM 09-25-05. DURING RE-PERFORMING STEP 3.F(2)(H), TO VERIFY I/B HINGE ATTACHMENT HARDWARE ASSY BUSHING [55] AND FOUND MISSING. REMOVED & REINSTALLED INBD & OUTBD HINGE ATTACH HARDWARE ON #8 SPOILER IAW AMM 27-61-11-400-801 (STEPS 3.F(2)(H), 3.F(2)(I). CONNECTED SPOILER ACT. ROD END TO #8 SPOILER IAW AMM 27-61-11-400-801 STEP 3.F(1)(E). CONTINUED INSTALL OF #8 SPOILER FROM STEP 3F(K)4 INTO 3G(6). AMM 27-61-11-400-801. ACOMPLISHED FLIGHT SPOILER ADJUSTMENT IAW AMM 27-61-00-820-803 UP TO & INCLUDING STEPS 5.F(3)M. NEED TO CONTINUE 5.F(4) OF SPOILER ADJUSTMENT. THEN CONTINUE BACK TO AMM INFO CORRECTION OF STEP. CONNECTED SPOILER ACT. ROD END TO #8 SPOILER IAW AMM 27-61-11-400-801 STEP 3.F(2)(J). DISREGARD STEP 3.F(1)(E). REF 7638446 FOR P

Part: STRINGER — CORRODED (STA847) · airframe 65,999 hrs · 23,919 cycles

EVIDENCE OF CORRISION ON STRINGER 25L AT STA 847 IMAGES AT STA 847 ON S-25L REMOVED RIVETS FROM STA 847 TO STA 827 COMMON TO S-25L REF SRM REMOVED HI-LOCKS ON S-25L FROM STATION 847 TO STAION 867 REF. 51-40-02. SRM. 51-40-02 CUT DAMAGED STRINGER MINIMUM AMOUNT TO INSPECT FUSELAGE SKIN FOR CORROSION UNDER NEATH APPROX 9.75" REF SRM 51-40-02 C/W HFEC REF PARA. 4.B. OF SRM 53-00-03-2R-1. NO DEFECTS NOTED. VERIFIED STRINGER CUTS TO BE AT STA. 827 + 7" AND STA. 847 + 7". C/W HFEC REF PARA. 4.B. OF SRM 53-00-03-2R-1. NO DEFECTS NOTED. CUT AND REMOVED DAMAGED SECTION OF STRINGER 25L FROM STA. 827 TO MEET MINIMUM FASTENER REQUIREMENTS FOR INTIAL STRINGER +8" TO STA. 847 +8" REF PARA. 4.B. OF SRM 53-00-03-2R-1. REQUEST THICKNESS OF 0.056"; EXTENDED REMOVED STRINGER SECTION TO STA. INSPECTION TO ACCOMPLISH HFEC INSPECTION TO MAKE SURE ALL DAMAGE 827 +7" AND STA. 847 +7" REF SRM 53-00-03-2R-1. REQUEST HAS BEEN REMOVED. INSPECTION TO ACCOMPLISH HFEC. VERIFIED 2 EA J ANGLES SECTIONS AS 7075-0 .071" THICK. REF SRM VERIFIED MATERIAL FOR STRINGER P/N 146A3233Y44, HAT SECTION P/N 53-00-03-2R-1 REPAIR 1 PARAGRAPH 4, TABLE 202 ITEM 3 FOR HEAT 69-78188-17 AND C SECTION P/N BAC1493-715 PER SRM 53-00-03-2R-1

Part: ANTI-ICE VALVE — FAULTY (ENG#2) · airframe 65,978 hrs · 23,910 cycles

COWL VALVE OPEN LIGHT STAYS ON BRIGHT WHEN THE ENG ANTI-ICE SWIT CH IS MOVED TO ON ENG-2 VALVE, ANTI-ICE OFF 29-3021-9-0002 8336 ON 0000 VALVE, ANTI-ICE OFF 29-3021-9-0002 8336 ON 29-3021-9-0002 0750 REMOVED AND REPLACED #2 ENG ANTI ICE VALVE REF FIM /FAULT ISOLATION REFERENCE: 30-21 TASK 805OPS NORMAL.

Part: LINE — LEAKING (LH MLG) · airframe 65,871 hrs · 23,858 cycles

AIRCRAFT LANDING BEHIND US NOTICED MORE THAN NORMAL SMOKE FROM L EFT MAIN ON LANDING INBD HYDRAULIC BRAKE DISCONNECT LINE ON #2 BRAKE WAS REPLACED REMOVED AND REPLACED BRAKE DISCONNECT LINE PER AMM 32-41-00. LEAK CHECK AND OPS CHECK GOOD AT THIS TIME. A/C BIS.

Part: RIB — CRACKED (STA101RIB) · airframe 61,499 hrs · 21,912 cycles

LEFT HORIZONTAL STABILIZER STA.101.90 RIB HAS 3/4" CRACK ON LOWER HORIZONTAL FLANGE AT VERTICAL STIFFENER # 2. (REF AAR NR 9641753) TO T7075 T6 .063", REF BHC 5602 AND OP 84, REINSTALLED REPAIR AT STA 101.90, VERTICAL STIFFNER IN REF B737-800 SRM 55-10-09-2R-5 FIG 204. REMOVED RIB L/H AT STA 101.90. REMOVED T SECTION REPAIR EXTRUSION FOR HEAT TREAT NO.1 AND REMOVED ANGLE REPAIR NO.2 FOR HEAT TREAT, HEAT TREATED T SECTION FROM 7075-T6511 TO 7025-T73511 AND HEAT TREATED ANGLE REPAIR FROM 7075 0.063" ADD EMP:V913194 PERMANENT REPAIR WAS PREVIOUSLY REPORTED, PLEASE REFER TO LAST UPDATE.

Part: RIB — CRACKED (STA 101.90) · airframe 61,499 hrs · 21,912 cycles

L/H HORIZONTAL STAB STA 101.90 RIB CRACKED AT LOWER FWD FLANGE REF AAR N/R 9642208 INSTALLED REPAIR ANGLE AT LT HORIZONTAL STAB STA 101.90 AT LOWER FWD FLANGE OF RIB REF B737 SRM 55-10-09-2R-5 FIG 205 WORK ACCOMPLISHED BY V920314

Part: NONE — CORRODED (STA 986.5) · airframe 61,499 hrs · 21,912 cycles

MAIN CABIN AFT WET AREA STA 986.5 FLOOR BEAM L/H JUST I/B OF L2 CREASE BEAM UPPER SURFACE CORROSION. (REF AAR NR 9641534) CABIN AFT WET AREA STA 986.5 AS PER B737-800 SRM 53-70-51-2R-4 AND EC/RA 5320-02466. REMOVED EXISTING REPAIR AT MAIN CABIN AFT WET AREA STA 986.5 FLOOR BEAM AS PER B737-800 SRM 51-40-02 AND 53-70-51-2R-4. FABRICATED NEW T-CHORD USING EXTRUSION BAC 1505-10474, 70757 AS PER B737-800 SRM 53-70-51-2R-4. INSTALLED NEW T-CHORD AT MAIN ADD EMP:V936291

Part: SKIN — DENTED (STA190) · airframe 61,499 hrs · 21,912 cycles

REF ELB LP 8128621 ITEM REPETITIVE INSP PER AMM FOUND BIRD STRIKE DENT ON LT SIDE OF FUSLAGE STA 190 WL 184 3.75IN DIA AND .160 DEEP REF AAR N/R 9641251 CONTACT ENGINEERING FOR THE INSPECTION REQUIREMENTS FOR PART 2 OF THE LATEST REVISION OF ECRA 5331-02855 REMVOED DAMAGED AREA AND ACCOMPLISHED INTERIM REPAIR AT FUSELAGE SKIN STA 188 - 203.8 STR 17L - 25L PER ECRA 5331-02855 ANDAS PER ECRA 5331-02855 STEP 17 DIP TO READ UPON THE ACCUMULATION OF 48,000 TOTAL FLIGHT CYCLES PLANNING TO REF ELB LP 8162475 FOR INSP REQUIREMENTS FOR PLANNING TO CONTACT ENGINEERING

Part: SKIN — DENTED (FWD CARGO DOOR) · airframe 61,499 hrs · 21,912 cycles

REFERENCE LOG PAGE 5529746 (CLOSED).FWD CARGO DOOR CUTOUT TOP R/H AREA HAS DENT REWORKED DAMAGE IAW B SRM 53-00-01-2R-21. INSPECTION THRESHOLD OF 50000 FLIGHT CYCLES. EXTERNAL LFEC AT 3500 FLIGHT CYCLES, INTERNAL HFEC AT 3500 FLIGHT CYCLES AND EXTERNAL DV AT 3500 FLIGHT CYCLES. SB 737-21-1149 HAS NOT BEEN INCORPORATED ON THIS AIRCRAFT. INSPECTION THRESHOLD OF 50000 FLIGHT CYCLES. EXTERNAL LFEC AT EXTERNAL DV AT 3500 FLIGHT CYCLES. SB 737-21-1149 HAS NOT BEEN 3500 FLIGHT CYCLES, INTERNAL HFEC AT 3500 FLIGHT CYCLES AND INCORPORATED ON THIS AIRCRAFT. REFERENCE LOG PAGE 5529746 (CLOSED).FWD CARGO DOOR CUTOUT TOP R/H AREA HAS DENTREWORKED DAMAGE IAW B SRM 53-00-01-2R-21. INSP C/W

Part: RIB — CRACKED (STA82.7) · airframe 61,499 hrs · 21,912 cycles

R/H HORIZONTAL STAB RIB NO.1 AT STA 82.70 CRACKED AT NO.3 VERTICAL STIFFNER LOWER AREA REF AAR N/R 9642159 REMOVED NO.1 RIB AT STA 92.70 REMOVED T-SCETIOC REPAIR EXTRUSION REPAIR AT RIB NO.1 AND REINSTALLED RIB AT FR STA 92.70 REF B737 FOR HEAT TREAT AND REMOVED ANGLE REPAIR NO.2 FOR HEAT TREAT HEAT SRM 51-40-02-0G-0 AND SRM 55-10-09-2R-5 FIG 204 TREATED T-SECTION FROM 7075T6511 TO 7075-T3511 AND HEAT TREATED WORK ACCOMPLISHED BY V900829 7075 0.063 TO 7075.T6.063 REF B-5602 AND OP84 REINSTALLED REPAIR 7075T6 0.063. REF:BAC-5602 AND OP-84 , REINSTALLED REPAIR AT RIB #1 AND REINSTALLED RIB AT FR STA 92.70, REF. B737-800 SRM 51-40-02-OG-0 AND SRM 55-10-09-2R-5 FIG 204 REF. AAR NR:9642159 REMOVED NO.1 RIB AT STA 92.70 REMOVED T-SECTION REPAIR EXTRUSION FOR HEAT TREAT AND REMOVED ANGLE REPAIR NO.2 FOR HEAT TREAT REPAIR NO.2 FOR HEAT TREAT. HEAT TREATED T-SECTION FROM 7075T6511 TO 7075-T73511 AND HEAT TREATED 7075 0.063 TO ADD EMP:V900829

Part: BEAM — CORRODED (STA 986.5) · airframe 61,499 hrs · 21,912 cycles

MAIN CABIN AFT WET AREA STA 986.5 RBL 4" FLOOR BEAM UPPER SURFACE CORROSION (REF AAR NR 9641538) REMOVED EXISTING REPAIR AT MAIN CABIN AFT WET AREA STA 986.5 FLOOR BEAM AS PER B737-800 SRM 51-40-02 AND EC/RA #5320-02466. INSTALLED NEW T-CHORD AT MAIN CABIN AFT WET AREA STA 986.5 AS PER B737-800 SRM 53-70-51-2R-4 AND EC/RA 5320-02466 ADD

Part: BEAM — CORRODED (STA 986.5) · airframe 61,499 hrs · 21,912 cycles

MAIN CABIN AFT WET AREA STA 986.5 RBL 4" FLOOR BEAM UPPER SURFACE CORROSION (REF AAR NR 9641538) REMOVED EXISTING REPAIR AT MAIN CABIN AFT WET AREA STA 986.5 FLOOR BEAM AS PER B737-800 SRM 51-40-02 AND EC/RA #5320-02466. INSTALLED NEW T-CHORD AT MAIN CABIN AFT WET AREA STA 986.5 AS PER B737-800 SRM 53-70-51-2R-4 AND EC/RA 5320-02466 ADD

Part: SKIN — DENTED (STA370) · airframe 61,499 hrs · 21,912 cycles

AS PER ECRA 5331-02856 STEP 20 INITIATE A 2ND DIP LOGPAGE WHICH REFERENCES DIP LOGPAGE 9732475 REF AAR N/R 9641301 ENGINEERING FOR THE INPSECTION REQUIREMENTS FOR PART 2 OF THE LATEST REVISION OF ECRA 5331-02856. REFERENCE LP 9732475, PER ECRA 5331-02856 UPON THE ACCUMULATON OF 48,000 TOTAL AIRCRAFT FLIGHT CYCLES, PLANNING TO CONTACT DIP TO READ AS FOLLOWS AS PER ECRA 5331-02856 UPON THE ACCUMULATION OF 48,000 TOTAL AIRCRAFT FLIGHT CYCLES PLANNING TO CONTACT ENGINEERING FOR THE INSPECTION REQUIREMENTS FOR PART 2 OF THE LATEST REVISION OF ECRA 5331-02856

Part: SKIN — DENTED (STA190WL184) · airframe 61,499 hrs · 21,912 cycles

REF ELB LP 8128621 ITEM REPETITIVE INSP PER AMM FOUND BIRD STRIKE DENT ON LT SIDE OF FUSLAGE STA 190 WL 184 3.75IN DIA AND .160 DEEP REF AAR N/R 9641251 CONTACT ENGINEERING FOR THE INSPECTION REQUIREMENTS FOR PART 2 OF THE LATEST REVISION OF ECRA 5331-02855 REMVOED DAMAGED AREA AND ACCOMPLISHED INTERIM REPAIR AT FUSELAGE SKIN STA 188 - 203.8 STR 17L - 25L PER ECRA 5331-02855 ANDAS PER ECRA 5331-02855 STEP 17 DIP TO READ UPON THE ACCUMULATION OF 48,000 TOTAL FLIGHT CYCLES PLANNING TO

Part: SKIN — NONE (NA) · airframe 61,499 hrs · 21,912 cycles

AS PER ECRA 5331-02856 STEP 20 INITIATE A 2ND DIP LOGPAGE WHICH REFERENCES DIP LOGPAGE 9732475 REF AAR N/R 9641301 ENGINEERING FOR THE INPSECTION REQUIREMENTS FOR PART 2 OF THE LATEST REVISION OF ECRA 5331-02856. REFERENCE LP 9732475, PER ECRA 5331-02856 UPON THE ACCUMULATON OF 48,000 TOTAL AIRCRAFT FLIGHT CYCLES, PLANNING TO CONTACT DIP TO READ AS FOLLOWS AS PER ECRA 5331-02856 UPON THE ACCUMULATION OF 48,000 TOTAL AIRCRAFT FLIGHT CYCLES PLANNING TO CONTACT ENGINEERING FOR THE INSPECTION REQUIREMENTS FOR PART 2 OF THE LATEST REVISION OF ECRA 5331-02856

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 54,365 hrs · 19,137 cycles

EMERGENCY LIGHTS AT SEAT ROWS 22 - 37 AND AT THE R2 DOOR INOPERATIVE. FOUND THE BATTERY PACK AND CHARGER BAD. REPLACED BOTH. OPS CHECKED OK.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 53,340 hrs · 18,744 cycles

EMERGENCY LIGHTS AT SEAT 7ABC TO 14ABC DO NOT ILLUMINATE WHEN TESTED. FOUND THE M1676 POWER SUPPLY AT FAULT. REMOVED AND REPLACED THE POWER SUPPLY IAW MM 33-51-06-960-806, AND THE BATTERY PACK IAW MM 33-51-06-960-805. OPS CHECKED GOOD.

Part: ALTIMETER — OUT OF TOLERANCE (STANDBY) · airframe 53,304 hrs · 18,729 cycles

STANDBY ALTIMETER IS 1100 FT LOW AT FL380 AND CATCH T LOW AT FL380 AND HANGS UP. REPLACED STANDBY ALTIMETER & AIRSPEED INDICATOR IAW MM 34-13-01, OPS CHECKED GOOD.

Part: OVEN — SMOKE (GALLEY) · airframe 53,244 hrs · 18,700 cycles

SMOKEY ODOR REPORTED NEAR THE AFT LAVATORY, NO SIGN OF SMOKE OR FIRE. REMOVED AND REPLACED THE OVEN. OPS CHECKED NORMAL IAW AMM 25-34-00.

Part: GIRT BAR — LOOSE (L1 DOOR SLIDE) · airframe 52,947 hrs · 18,574 cycles

L1 DOOR SLIDE GIRT BAR BRACKET LOOSE. ADJUSTED THE GIRT BAR HOLDING CLAMPS, OK TO CONTINUE.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 52,502 hrs · 18,406 cycles

AFT EMERGENCY EXIT COVER FELL OFF. SECURED LIGHT COVER ,LIGHT CKD OK

Part: POSITION SENSOR — FAULTY (LE SLAT) · airframe 45,990 hrs · 15,951 cycles

LE SLAT IN TRANSIT LIGHT UPON REACHING CRUISE ALTITUDE, DIVERTED. LIGHT SUBSEQUENTLY EXTINGUISHED, LE SLAT NR 7. REPEAT WRITE UP, CHRONIC PROBLEM. REPLACED INBD NR 7 LE SLAT POSITION SENSOR IAW AMM 27-88-11-4 01. FSEU NO FAULTS.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 45,314 hrs · 15,697 cycles

FORWARD CARGO DOOR OUTER SKIN FOUND OUT OF SRM LIMITS, SEE LOG PAGE 973522. R & R FWD CARGO DOOR OUTER SKIN. SEE NR 9735227 FOR FWD DOOR SKIN R & R & SUB STEPS. NR 9 737909 FOR FWD DOOR OUTER SKIN REPAINT & PLACARD MARKINGS & NR 9737158 FOR SUB STEPS WORK FOR FWD DOOR SKIN REPLACEMENT REF SRM 52-30-01.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 45,314 hrs · 15,697 cycles

LOWER RT HORIZONTAL STAB SKIN HAS A 1/2" CRACK, LOCATED INBD SIDE OF RIB STATION 147.90 & 24" AFT OF FWD SPAR. CRACK ENDS MARKED IN BLACK MARKER FOUND USING HFEC C-SCAN NTM-UAL PART 6 SECTION 55-10-01. ACCOMPLISHED REPAIR IAW ECRA 5510-02514.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,314 hrs · 15,697 cycles

CABIN FRAME BRACKET AT STATION 500A RT, BETWEEN STATION 8R & 9R. INSTALLED DOUBLER REPAIR & PRESERVED WITH CORROSION INHIBITING COMPOUND IAW EA 5310-04716 REV I FIG 3 STEPS 8, 9 & 13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,314 hrs · 15,697 cycles

FRAME CRACKED AT INBD FASTENER, PSU RAIL STATION 727B, BETWEEN STRINGER 8R & 9R. SEE WIP STEPS FOR WORK PERFORMED. REPAIRED FRAME AT STATION 727B BETWEEN STRINGER 8R - 9R IAW EA 5310-04716 REV I FIGURE 3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,314 hrs · 15,697 cycles

FRAME CRACKED AT INBD FASTENER PSU RAIL STATION 727B BETWEEN STRINGER 8L & 9L. SEE ALL WIPS PERFORMED BY MECH FOR REPAIRED FRAME IAW 5310-04716 REV I FIGURE 3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,314 hrs · 15,697 cycles

FRAME CRACKED AT INBD FASTENER, PSU RAIL STATION 867, BETWEEN STRINGER 8R & 9R. INSTALLED DOUBLER REPAIR, SUPPORT BRACKET & APPLIED CORROSION INHIBITING COMPOUND IAW EA 5310-04716 REV I REPAIR 3 FIG 3, 8, 9, 12 & 13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,314 hrs · 15,697 cycles

FRAME CRACKED AT INBD FASTENER, PSU RAIL, STATION 480 BETWEEN STRINGER 8L & 9L. INSTALLED REPAIR ANGLES A & B AT STATION 480L BETWEEN STRINGER 8L & 9L IAW EA 5310-04716 P2.

Part: SUPPORT BEAM — WORN (FUSELAGE) · airframe 44,218 hrs · 15,312 cycles

SUPPORT CTR WING BEAM AT RBL 41.0 & STATION 549 HAS WORN AREA FROM LATCH ON PN 192DR. REMOVED RT LOWER CHORD IAW SRM 51-40-02. LOCATED & DRILLED LOWER CHORD IAW DWG 111A7001 REV A. INSTALLED LOWER CHORD RT IAW DWG 111A7001 REV A & SRM 51-4 0-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,394 hrs · 14,666 cycles

EMERGENCY EXIT LIGHT IN BULLNOSE AT SEAT ROW 28DEF INOPERATIVE. PLACED ON MEL.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 37,259 hrs · 12,917 cycles

LEFT HORIZONTAL STAB DENTED AT L/E STA 216 IS OUT OF LIMITS IAW SRM 55-10-01, ALLOWABLE DAMAGE 1, PG 105, STEP (2) GENERAL CONDITION. REPAIRED LT HORIZONTAL L/E AT STA 216 REF SRM 55-10-01, REPAIR 1.

Part: WIRE HARNESS — DAMAGED (FIRE LOOPS) · airframe 36,611 hrs · 12,705 cycles

ON PUSH BACK AND START ENG NR 2 OVERHEAT LIGHT ILLUMINATED AND WENT OUT. AFTER TEST, ALL CHECKED GOOD AND CONTINUED AFTER TAKEOFF. 8000FT LIGHT ILLUMINATED, RAN QRH LIGHT WENT OUT. RETURNED TO DEPARTURE, INSPECTED NR 2 ENG FOR PNEUMATIC LEAKS, NONE FOUND, CHECKED FIRE LOOPS RESISTANCE REF 26-11-00-730-801. TESTED SYS REF MM 26-11-00-730-802. CHECKED NORMAL. FOUND HARNESS D30420 DAMAGED, REMOVED AMP A & B LOOPS HARNESSES REF MM 26-11-02-401.

Part: SHUTOFF VALVE — LEAKING (BLEED SYSTEM) · airframe 36,215 hrs · 12,563 cycles

ON START NR 2 ENGINE OVERHEAT ILLUMINATED. CHECKED ENG WIRING/FIRE DETECTOR REF FIM 26-10 TASK 805. ALL VALUES OK. PERFORMED ENGINE BLEED AIR LEAK CHECK IAW MM 36-11-00. FOUND PRSOV LEAKING. R & R PRSOV REF MM 36-11-04. R & R FIRE CONTROL PANEL IAW MM 26-00-01. RAN ENGINE IAW MM 71-00-00, TEST 5. ALL TESTED NORMAL. NO FAULTS FOUND.

Part: CLAMP — LOOSE (OVERHEAT SYS) · airframe 32,763 hrs · 11,337 cycles

ENGINE 2 OVERHEAT LIGHT CAME ON ONE MINITE AFTER TAKE OFF. WENT WITH POWER REDUCTION PER CHECK LIST. INSPECTED NR 2 ENGINE OVERHEAT SYSTEM PER THE AMM 26-10-00-710- 801. FOUND 2 EA LOOSE CLAMPS ON DUCTS. SECURED BOTH CLAMPS INSPECTED ALL WIRES TO OVERHEAT SYSTEM. FOUND NO DAMAGE, RAN NR 2 FOR 5 MIN TO TAKEOFF POWER, NR 2 ENGINE OVERHEAT DID NOT COME ON. AIRCRAFT BACK IN SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,804 hrs · 10,628 cycles

CABIN INTERIOR LT SIDE STA 400 FRAME CRACKED AT PSU RAIL ATTACH POINT BETWEEN STRINGER 8 AND 9. INSTALLED REPAIR DOUBLERS IN INTERIOR CABIN LT SIDE AT STA 400 FRAME BETWEEN STRINGER 8 AND 9 REFECRA 5310-05296.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,804 hrs · 10,628 cycles

CABIN INTERIOR RT SIDE STA 480 FRAME CRACKED AT PB737-53-3-0739-CABIN INTERIOR RT SIDE STA 480 FRAME CRACKED AT PUS RAIL ATTACH POINT BETWEEN STRINGER 8 AND 9. INSTALLED REPAIR DOUBLER IN INTERIOR CABIN RT SIDE AT STA 480 FRAME BETWEEN STRINGER 8 AND 9 REF ECRA 5310-05296.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 30,804 hrs · 10,628 cycles

RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STAB STA 101.90. REPAIRED RT HORIZONTAL LOWER SKIN IAW EC/RA 5510-02129.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 30,804 hrs · 10,628 cycles

SUPPORT TASK: RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STA 129.50. LENGTH OF CRACK IS 2.8 INCHES. REPAIRED RT HORZ STAB LOWER SKIN AT STAB STA129.50 PER ECRA 5510-02128. INITIATED DIP C/N 07694 TO ACCOMPLISH A PERMANENT REPAIR WITHIN 12 MONTHS FROM DATE 10/29/2010. REF: ECRA 5510-02128 PART 1 STEP 20. "Q/C" ACCOMPLISH A PERMANENT REPAIR WITHIN 12 MONTHS FROM DATE 10/29/2010. NOTE TO PLANNING: THIS REPAIR IS BEING ANALYZED FOR DMG TOLERANCE AND WILL LIKELY BECOME A PERMANENT REPAIR WITH REPEAT INSP CONTACT ESC AFTER 10 MONTHS AND BEFORE 11 MONTHS FOR THE PERMANENT REPAIR. DIP C/N 07694 ISSUED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,804 hrs · 10,628 cycles

CABIN INTERIOR RT SIDE STA 400 FRAME CRACKED AT PSU RAIL ATTACH POINT BETWEEN STRINGER 8 AND 9. INSTALLED REPAIR DOUBLERS IN INTERIOR CABIN RT SIDE AT STA 400 FRAME BETWEEN STRINGER 8 AND REF ECRA 5310-05296.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,804 hrs · 10,628 cycles

CABIN INTERIOR RT SIDE STA 380 FRAME CRACKED AT PSU RAIL ATTACH POINT BETWEEN STRINGER 8 AND 9 (MARKED). INSTALLED REPAIR DOUBLERS IN MAIN CABIN AT STA 380 BETWEEN STR 8 & 9 RT SIDE REF.EC/RA 5310-05295. INITIATED DIP TO READ AS FOLLOWS: ACCOMPLISH INSPECTION PRIOR TO 50,000 TOTAL A/C FLT CYCLES PER EC/RA 5310-05295, PART 2. PLANNING IS TO CONTACT ENG AFTER 44,000 FLT CYCLES BUT BEFORE45000 FLT CYCLES FOR A PERM REPAIR FOUND FRAME CRACKED, STA 380, STR 8RT.PER ECRA 5310-05295 COMPLETED INTERIM REPAIR.INSPECT REPAIR PER PART 2 OF ECRA PRIOR TO 50,000 TOTAL FLT CYC`S. PLANNING TO CONTACT ESC AFTER 44,000 FLT CYC`S NOT TO EXCEED 45,000 TOTAL FLT CYC`S.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,804 hrs · 10,628 cycles

CABIN INTERIOR LT SIDE STA 440 FRAME CRACKED AT PSU RAIL ATTACH POINT BETWEEN STRINGER 8 AND 9. INSTALLED REPAIR DOUBLERS IN INTERIOR CABIN RT SIDE AT STA 440 FRAME BETWEEN STRIGER 8 AND 9 REF ECRA 5310-05296.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,804 hrs · 10,628 cycles

CABIN INTERIOR RT SIDE STA 440 FRAME CRACKED AT PSU RAIL ATTACH POINT BETWEEN STRINGER 8 AND 9. INSTALLED REPAIR DOUBLER IN INTERIOR CABIN RT SIDE AT STA 440 BETWEEN STRINGER 8 AND 9 REF ECRA 5310-05296.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,565 hrs · 10,542 cycles

SUPPORT TASK; EMERGENCY BATTERY PACK M1671 AT STA 727C +13 RIGHT INOP. REMOVED & REPLACED EMERGENCY LIGHTING BATTERY PACK AND CHARGER ASSY M1671 AND OPS CHECKED GOOD IAW B737-789AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,565 hrs · 10,542 cycles

SUPPOR TASK; EMERGENCY BATTERY PACK M1694 STA 565 LEFT INOP REMOVED & REPLACED EMERGENCY LIGHTING BATTERY PACK & CHARGER ASSY M1694 AND OPS CHECKED GOOD IAW B737-789AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,565 hrs · 10,542 cycles

SUPPORT TASK; EMERGENCY BATTERY PACK M1670 INOP AT STA 727C +13 LEFT. REMOVED & REPLACED BATTERY PACK & CHARGER ASSY M1670 AND OPS CHECKED GOOD IAW B737-789AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,487 hrs · 9,409 cycles

EMERGENCY LIGHTS ARE INOPERATIVE AT SEATS 5ABC THROUGH SEATS 10ABC. REMOVED AND REPLACED EMERGENCY POWER BATTERY PACK RIGHT SIDEWALL BY FLOOR AT STATION 500 PER AMM 33-51-06 PAGE BLOCK 201. NO FAULTS NOTED. EMERGENCY LIGHTS AT SEATS 5ABC THROUGH SEATS 10ABC OPS CHECKS GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 27,231 hrs · 9,320 cycles

SEAT 26 ABC EMERGENCY EVACUATION LIGHT WIRES BROKEN. REPINNED WIRE AT SEAT 26ABC, WIRE WB144-02-60-20, LOCATED AT STA 875 WL 208 IAW SWPM-20-10-13, WDM 33-51-22. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 24,691 hrs · 8,460 cycles

SHEAR WEB AT STATION 986.5 LBL 48 CRACKED. FABRICATED REPAIR PER ECRA 5321-01585 AND INSTALLED PER SRM 51-40-02 FOR SHEAR WEB AT STATION 986.5 LBL 48.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 24,691 hrs · 8,460 cycles

SHEAR WEB AT STATION 986.5 RBL 48 CRACKED. FABRICATED REPAIR PER ECRA 5321-01585 AND INSTALLED PER SRM 51-40-02 FOR SHEAR WEB AT STATION 986.5 RBL 48.

Part: WEB — CRACKED (FUSELAGE) · airframe 24,691 hrs · 8,460 cycles

WEB AT STATION 1016 RBL 36 CRACKED. REMOVED DAMAGE AND PERFORMED TYPICAL WEB REPAIR PER SRM 51-70-13.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 24,691 hrs · 8,460 cycles

CABIN FLOORBEAM AT STATION 986.5 THE ENTIRE WIDTH HAS AREAS OF CORROSION LBL 50 - RBL 50 FLOORBEAM 986.5 CAP. REPLACED CORRODED FLOORBEAM PER ECRA 5321-01584 AND SRM TR 53-02 / 53-70-51 FOR ASSEMBLY INSTALLATIONS.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 24,691 hrs · 8,460 cycles

FLOORBEAM VERTICAL FLANGE AT STATION 986.5 HAS CRACK FROM CUT-LINE TO FASTENER HOLE AT LBL 50. LBL 50 VERTICAL FLANGE OF FLOORBEAM 986.5. REPAIRED PER ECRA 5321-01584 AND REASSEMBLED PER SRM 53-70-51.

Part: VAPOR BARRIER — CRACKED (MLG W/W) · airframe 20,122 hrs · 6,993 cycles

INSPECTION FOUND MLG WHEEL WELL LEFT FORWARD BULKHEAD HAD A CRACK ON VAPOR BARRIER, REAR SPAR CENTER SECTION, LT SIDE THAT HAD MIGRATED BEYOND A STOP DRILL. THE CRACK WAS NOW 18 INCHES LONG. A TEMPORARY REPAIR HAD BEEN PERFORMED PREVIOUSLY A FEW MONTHS PRIOR. A PERMANENT REPAIR WAS PERFORMED IAW SRM 57-10-10 TO BAYS 5, 7 AND 8.

Part: LIFE RAFT — DISCHARGED (AFT CABIN) · airframe 4,336 hrs · 1,548 cycles

INSPECTION FOUND AFT MOST RAFT IN CEILING STOWAGE BOX HAD LOW PRESSURE. THE RAFT WAS REPLACED IAW MM 25-64-00.