N33292

Part: SLIDE — MISCONFIGURED (ZONE 800) · airframe 61,742 hrs · 22,761 cycles

1R DOOR SLIDE NOT STOWED PROPERLY. TUCKED IN EXCESS GIRT MATERIAL PER ECRA 2560-01987, DOOR OPERATES NORMALLY.

Part: WARNING MESSAGE — MULTIPLE FAIL · airframe 61,200 hrs · 22,496 cycles

AFTER T/O CA SIDE SPD LI M FLAG ILLUM. LOSS OF ST ALL SPD TAPE. LOST CA FD PITCH. INT SHAKER INFO FROM FLIGHT CREW: AFTER T/O CA SPD LIM FLAG APPEARED. LOST STALL SPEED TAPE. INTERMITTENT LOSS OF CA FD PITCH INDICATOR. INTERMITTENT STICK SHAKER ABOVE 18,000. SPD LIM FLAG GONE AFTER TOUCHDOWN ACCOMPLISHED DFCS BITE PER FIM 22-11 TASK 801 CH A MSG 22-11397 ACCOMPLISHED LRU REPLACEMENT TEST , PASSES. CH B MSG 22-11323 AND 22-11006 ACCOMPLISHED LRU REPLACEMENT TESTS , PASSES. ACCOMPLISHED SMYD 1 BITE TEST PER FIM 27-32 TASK 801, MSG 27-31004 NOT LATCHED, ACCOMPLISHED FIM TASK 27-32 TASK 809, NO CURRENT FAULTS INTERMITTENT, AOA MOVES FREELY. MSG 27-31026 , INT FAULT, ACMPL FIM TASK 27-32 TASK 838 NO CURRENT FAULTS. ACCOMPLISHED FIM 27-32 TASK 831, NO EXISTING FAULTS ON SMYD, ACCOMPLISHED DEU SELF.

Part: SMOKE DETECTOR — FALSE ACTIVATION (ZONE 100) · airframe 61,024 hrs · 22,420 cycles

AFT CARGO FIRE WARNING ILLUMINATED 3 TIMES BOTTLE WAS DISCHARGE DPER CAPTAIN, DURING CLIMB OUT AGT CARGO PIT SMOKE DET LITE ILLUMINATED TWICE. HE BLEW THE BOTTLE AND THE LITE CAME ON AGAIN. CABIN CREW DID NOT SMELL SMOKE. REMOVED FIRE BOTTLE 1 REF AMM 26-23-01-000-801-001. REMOVED AND REPLACED CARGO FIRE EXTINGUISING FILTER/DRIER DUE TO BOTTLE BEING DISCHARGED. REF AMM 26-23-04-400-801. ALL FIRE DETECTION/ SUPPRESSION CIRCUIT BREAKERS PULLED AND RESET REF SDS 26-23-00-007. COMPLETED INSTALLATION OF LEFT BOTTLE CARGO REF AMM 26-23-01-400-802-001 CONTINUING FROM STEP H SUBTASK D. TEST OPS CHECK GOOD REF AMM 26-23-01.

Part: NONE — NONE (NONE) · airframe 60,920 hrs · 22,377 cycles

REF. LP 5268054. PER SRM 53-00-01-2R-12 SEC. 5(B), AFTER 50,000 TOTAL AIRPLANE CYCLES, PERFORM INTERNAL HFEC INSPECTIONS AT 15,0 00 FLIGHT CYCLE INTERVALS AROUND RIVET HEADS OF THE TWO OUTER RI VET ROWS OF THE INNER SKIN AND THE OUTER ROW OF THE OUTER SKIN. REFER TO 737 NDT PART 6, 53-30-00, PROCEDURE 7. CONCURRENTLY, PE RFORM EXTERNAL DETAILED VISUAL (DET) INSPECTIONS OF THE ENTIRE R EPAIR DOUBLER FOR CRACKS, LOOSE OR MISSING FASTENERS.AFTER 50,000 TOTAL AIRPLANE CYCLES, PERFORM INTERNAL HFEC INSPEC TIONS AT 15,000 FLIGHT CYCLE INTERVALS AROUND RIVET HEADS OF THE TWO OUTER RIVET ROWS OF THE INNER SKIN AND THE OUTER ROW OF THE OUTER SKIN. REFER TO 737 NDT PART 6, 53-30-00, PROCEDURE 7. CON CURRENTLY, PERFORM EXTERNAL DETAILED VISUAL (DET) INSPECTIONS OF THE ENTIRE REPAIR DOUBLER FOR CRACKS, LOOSE OR MISSING FASTENER S. TOMC APPROVED TO PERFORM AN INSPECTION AT AN INITIAL THRESHOLD O F 50,000 TOTAL AC FLT CYCS. PERFORM THE FOLLOWING INSPECTIONS AT THE SPECIFIED REPEAT INTERVALS: EXTERNAL DETAILED VISUAL (DET) INSPS AT 4,000 FLT CYC INTERVALS, INTERNAL DETAILED VISUAL (DET ) INSPS AND INTERNAL HIGH FREQUENCY EDDY CURRENT (HFEC) IN AT 15 ,000 FLT CYC INTERVALS IN REF WITH SRM 53-00-01-2R-12.

Part: SKIN — DAMAGED (ZONE 100) · airframe 60,920 hrs · 22,377 cycles

PER SRM 53-00-01-2R-12 SEC. 5(B), AFTER 50,000 TOTAL AIRPLANE CYCLES, PERFORM EXTERNAL DETAILED VISUAL (DET) IN SPECTIONS AT 4,000 FLIGHT CYCLE INTERVALS OF THE REPAIR AREA FOR SKIN CRACKS AT THE OUTER PERIMETER ROW OF FASTENERS COMMON TO T HE REPAIR DOUBLER AND FILLER. CONCURRENTLY, PERFORM EXTERNAL DET AILED VISUAL (DET) INSPECTIONS OF THE ENTIRE REPAIR DOUBLER FOR CRACKS, LOOSE OR MISSING FASTENERS.AFTER 50,000 TOTAL AIRPLANE CYCLES, PERFORM EXTERNAL DETAILED VISUAL (DET) INSPECTIONS AT 4,000 FLIGHT CYCLE INTERVALS OF THE REPAIR AREA FOR SKIN CRACKS AT THE OUTER PERIMETER ROW OF FASTENERS COMMON TO THE REPAIR DOUBLER AND FILLER.

Part: NONE — NONE (NONE) · airframe 60,920 hrs · 22,377 cycles

PER SRM 53-00-01-2R-12 SEC. 5(B), AFTER 50,000 TOTAL AIRPLANE CYCLES, PERFORM INTERNAL DETAILED VISUAL (DET) IN SPECTIONS AT 15,000 FLIGHT CYCLE INTERVALS OF THE REPAIR AREA FO R SKIN CRACKS AT THE OUTER PERIMETER ROW OF FASTENERS COMMON TO THE REPAIR DOUBLER AND FILLER. CONCURRENTLY, PERFORM EXTERNAL DE TAILED VISUAL (DET) INSPECTIONS OF THE ENTIRE REPAIR DOUBLER FOR CRACKS, LOOSE OR MISSING FASTENERS.AFTER 50,000 TOTAL AIRPLANE CYCLES, PERFORM INTERNAL DETAILED VISUAL (DET) INSPECTIONS AT 15,000 FLIGHT CYCLE INTERVALS OF THE REPAIR AREA FOR SKIN CRACKS AT THE OUTER PERIMETER ROW OF FASTENERS COMMON TO THE REPAIR DOUBLER AND FILLER. CONCURRENTLY, PERFORM EXTERNAL DETAILED VISUAL (DET) INSPECTIONS OF THE ENTIRE REPAIR DOUBLER FOR CRACKS, LOOSE OR MISSING FASTENERS. TOMC APPROVED TO PERFORM AN INSPECTION AT AN INITIAL THRESHOLD OF 50,000 TOTAL AC FLT CYCS AND CONCURRENT INSPECTIONS AT 15,000 FLT CYCS OF AN EXTERNAL DETAILED VISUAL (DET) INSPECTIONS OF THE ENTIRE REPAIR DOUBLER FOR CRACKS, LOOSE OR MISSING FASTENERS CONCURRENTLY WITH THE REQUIRED DET INSPECTIONS FOLLOWING THE THRESHOLD.

Part: WINDOW FRAME — NOT REPORTED (ZONE 200) · airframe 60,920 hrs · 22,377 cycles

ACCOMPLISH INSPECTION REQUIREMENTS OF THE LH #3 FLIGHTDECK WINDOW FRAME E-F POST, PER PART 2 OF EC/RA 5311-03372 ON OR BEFORE THEAIRCRAFT REACHING 50,000 TOTAL FLIGHT CYCLES.

Part: SKIN — DENTED (ZONE 100) · airframe 60,920 hrs · 22,377 cycles

DENT IN FUSELAGE SKIN FS500B PLUS 12" STRINGER 27RC/W REPAIR PER SRM 53-00-01-2R-3. REF NR 2723023 FOR WORK ACCOMPLISHED. ESFR INFORMATION ENTERED. REFERENCE NON-ROUTINE 002723023 FOR WORK DETAILS ACCOMPLISHED. DIP INITIATED TO ACCOMPLISH INSPECTIONS PER SRM 53-00-01-2R-3, P T. 5,D., TABLE 205. AFTER AN INSPECTION THRESHOLD OF 50000 TOTAL FLT CYCLES, DO THE FOLLOWING REPEAT INSPECTIONS: EXT. LFEC INSP ECT EVERY 7000 FLT CYCLS (ARROW 8) , INT. HFEC INSPECT (ARROW 9) EVERY 36000 FLT CYCLS, EXT. LFEC INSPECT (ARROW 10) EVERY 36000 FLT CYCLS, EXT. DETAILED VISUAL (ARROW 5) EVERY 4000 FLT CYCLS, AND INT. DETAILED VISUAL (ARROW 7), EVERY 36000 FLT CYCLES ITEM IS NOT RII, NON-ROUTINE IS DOWNGRADED TO NONE. T

Part: SLIDE — NO DISCREPANCY (ZONE 800) · airframe 60,603 hrs · 22,213 cycles

DOOR 1L SLIDE STILL ARMED WHEN OPENED PARTIA LY. SLIDE PACK NOT SECURE. PINNED L1 DOOR SLIDE. RESECURED L1 DOOR SLIDE. OPS CHECK GOOD REF AMM25-66-01 VERIFIED THAT THE L1 DOOR SLIDE WASE PINNED AND RESECURED L1 DOOR SLIDE (NOTE: SAFETY PINNED WAS REMOVED AND STOWED AS PART OF THE INSTALLATION). OPS CHECK GOOD REF AMM25-66-01

Part: CONNECTOR — DAMAGED (ZONE 200) · airframe 60,084 hrs · 21,995 cycles

DURING REINSTALLATION OF R/H FWD OVERWING EXIT DOOR LINER FOUND CONNECTOR D12458P DAMAGED. SUPPORT TASK NSA EMX N/R 00190 REMOVED AND REPLACED R/H FWD OVERWING EXIT LINER DOOR CONNECTOR D12458. OPS CHECK GOOD IAW B737-800 AMM 33-51-04-420-002 AND B73 7-800 SWPM 20-60-06.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 60,084 hrs · 21,995 cycles

MID CABIN EMERGENCY EXIT LIGHTS INOP.SUPPORT TASK NSA EMX N/R 00024.MID CABIN EMERGENCY EXIT LIGHTS INOP.SUPPORT TASK NSA EMX N/R 00024. 37-800 AMM 33-51-06-960-805. OPS CHECK GOOD I.A.W B737-800 AMM 33-51-06-960-805. DATA WAS TRANSCRIBED FROM NSA EMX N/R 00024. REMOVED SEAT ROW 10DEF AIR GRILLE I.A.W B737-800 AMM 21-23-03-00 0-801. REMOVED SEAT ROW 10D-EF BATTERY PACK M1676 (P/N#AD-717-0 1-100, S/N#260191)I.A.W B737-800 AMM 33-51-06-960-805.INSTALLED SEAT ROW 10DEF BATTERY PACK M1676 (P/N#AD-717-01-100, S/N280778) I.A.W B737-800 AIPC 33-51-06-02 AND AMM 33-51-06-960-805. CLOSED AIR GRILLE AT SEAT ROW 10DEF IAW B737-800 AMM 21-23-03-400-802. PERFORMED OPS CHECK FOR SEAT ROW 10DEF BATTERY PACK M1676 EEPL AND FLOOR PROXIMITY LIGHTS FROM SEAT 7ABC TO SEAT 14ABC.

Part: BULB — INOPERATIVE (ZONE 200) · airframe 59,906 hrs · 21,907 cycles

RT SIDE EXIT 2ND ROW LIGHT IS INOP OVERWING EXIT DOOR WINDOW LT INOP AT ROW 21DEF. QUICT TURN, NO TIME TO T/S. REQUESTING TO DEFER. TOMC APPROVED RT SIDE EXIT 2ND ROW LIGHT IS INOP COMPLIED WITH MEL, ITEM PLACED ON DEFERRAL. REMOVE AND REPLACE LIGHT BULB AT RT SIDE EXIT ROW AT 21DEF OPS CHECKS GOOD OK FOR SERVICE.

Part: AOA — BROKEN (ZONE 100) · airframe 59,856 hrs · 21,888 cycles

INTERMIT SPD LIM IND ON CA AIRSPEED INTMT SLOW SPD TAPE INTM CA STICK SHAKERFLAGGED AS SDR CAPT STCK SHAKER AND SPD LIM FLAG STARTED ON CLIMB OUT AND CAPT SPEED TAPE FLUXING ABOUT 10000 FT WOULD GO IN AND OUT REMAINDER OF FLIGHT RETURN TO FIELD. AIR SPEED IND ALL NORMAL BOTH SIDES. PICS FROM #1 SMYDS. AOA PROBE ON AOG AND GASKETS AND SCREWS ON ODER TO HANGER. AMM 34-21-05. CAPT AOA PROBE CDS FAULT WAS NOT ANNUCIATED ON EITHER CAPTAIN OR FIRST OFFICERS OUTBOARD DU PERFORMED CDS BITE IN REFERENCE TO B737 FIM 31-62 TASK 801 BITH DEUS SHOWED NO FAULTS PERFORMED STALL MANAGEMENT YAW DAMPER BITE PROCEDURE IN REFERENCE TO B737 FIM 27-32 TASK 801 SMYD 1 SHOWED MESSAGE "AOA SIG ERROR" 27-31004 FOLLOWED B737 FIM 27-32 TASK 809 CHECKED FOR GOOD 28VDC AT LEFT AOA VANE CONNECTOR D365 PIN 1 HAD GOOD 28VDC PRESENT CHECKED WIRING BETWEEN LEFT AOA VANE CONNECTOR D365 PINS 3, 4 AND5 TO SMYD 1 BENCH PLUG D3683B PINS 72, 71 AND 58 HAD GOID CONTINUITY 1.9 OHMS NO SHORTS TO GROUND OR WIRE TO WIRE SHORTS PRESENT VERFIED PINS 2, 10 AND 12 ON CONNECTOR D365 WERE GOOD GROUND 0.3 OHMS REFERENCE B737 WDM 27-32-11-4.1 SINCE WIRING CHECKS ARE GOOD SUGGEST WE REPLACE LEFT ANGLE OF ATTACK VANE T433 REFERENCE B737 FIM 27-32 TASK 809 REPLACED THE LEFT ANGLE OF ATTACK SENSOR T433 IN REFERENCE TO B737 AMM 34-21-05-400-801 PERFO00-0583-3-7855 .

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 59,677 hrs · 21,810 cycles

SEAT MOUNTED EMERGENCY LIGHTS INOP AT SEAT 7-15ABC REMOVED AND REPLACED POWER SUPPLY AND BATTERY IAW AMM 33-51-06-960-806, OPS CHECK GOOD

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 58,020 hrs · 21,017 cycles

RH HORIZONTAL STAB LWR SKIN - TWO CRACKS FOUND ON STA. 157.10 LOCATED AT 16" & 23" FORWARD FROM AFT SPAR.

Part: SKIN — DENTED (CARGO DOOR) · airframe 58,020 hrs · 21,017 cycles

REMOVE AND REPLACE THE AFT CARGO DOOR EXTERNAL SKIN , LP 4994929 (REF AAR NR 100006124) REMOVED AND REPLACED AFT CARGO DOOR EXTERNAL SKIN IAW B737-800, SRM 52-30-01-2R-3.

Part: SKIN — DENTED (CARGO DOOR) · airframe 58,020 hrs · 21,017 cycles

REMOVE AND REPLACE THE FWD CARGO DOOR EXTERNAL SKIN . REF TO LP 9898412 (REF AAR NR 100006123) REMOVED AND REPLACED FWD CARGO DOOR EXTERNAL SKIN IAW B737-800; SRM 52-30-01-2R-3.

Part: VALVE — LEAKING (NOT REPORTED) · airframe 54,415 hrs · 19,451 cycles

REMOVED AND REPLACE BALL VALVE REF AMM 38-32-03-400-801 OPS LEAK CHKS OK. DUE TO NATURE OF LEAK, RECOMMEND IN DEPTH CLEAN UP OF AFT CARGO PIT AREA IN REF TO ECRA 2011-01000 ITEM 2 B. ACCOMPLISHED IN-DEPTH CLEANUP PROCEDURE.

Part: HANDLE — MISALIGNED (2L DOOR) · airframe 51,204 hrs · 18,102 cycles

AFT DOOR 2L HANDLE CAME UP ON CLB OUT W/SQUEL DOOR LIGHT ON AT F L170 TECH SPT UPDT, THIS ITEM CHRONIC SUGGEST PERFORMING AMM 52-13-00 -820-802 SOFT LATCHING CHECKS. ADJUST AS NEEDED THANKS

Part: NONE — NONE · airframe 51,176 hrs · 18,088 cycles

DURING REPLACEMENT OF NUPLATES ON LH LEADING EDGE, MISDRILLED (1 2) NUTPLATE FASTENER HOLES FROM STA. 184.7-249.1 (REF AAR NR 999 17492). K ACCOMPLISHED BY V931568 AND V936245). REMOVED, REPAIRED AND INSTALL NUTPLATE ON L/H HORIZONTAL STABILI ZER LEADING EDGE. ALL WORK DONE IAW B737-800 SRM 51-40-02, SRM 5 1-40-05, SRM 51-20-01, AMM 51-21-72, SRM 51-10-01, AMM 55-10-00, AMM 27-41-21, EC-RA# 5510-03093 AND EA# 210256 REVISION P3 (WOR INITIATE DTA DIP TO PERFORM INSP UPON THE ACCUMULATION OF 54000 TTL FLT CYC PER PART 2 OF THE LATEST REV OF ECRA 5510-03093. DIP 55-DIP REJECTED INCORRECT DIP LIMIT ENTERED, SEE ELB LP 7777908 FOR REPAIR AND DIP INFORMATION.

Part: BATTERY PACK — NONE (M7694) · airframe 51,176 hrs · 18,088 cycles

LH FWD & AFT OVWG EXIT SIGNS EXTINGUISH PRIOR TO 15 MINUTE MINIM UM REQUIRED FOR CAPACITY CHECK (REF. AAR NR 99916671). REMOVED AND REPLACED BATTERY PACK FOR L/H OVERWING EXIT SIGN FWD AND AFT, AND PERFORMED OPS TEST GOOD IAW B737 AMM 33-51-06-960-8 05 (WORK ACCOMPLISHED BY V936248 AND AAR QC V936245).

Part: BATTERY PACK — NONE (M1670) · airframe 51,176 hrs · 18,088 cycles

LH EMERGENCY EXIT AISLE LIGHTS FROM SEAT ROWS 7ABC-12ABC & 32ABC EXTINGUISH PRIOR TO 15 MINUTE MINIMUM REQUIRED FOR CAPACITY CHE CK (REF. AAR NR 99916676). REMOVED AND REPLACED BATTERY PACK POS M1670 AND PERFORMED OPS TE ST GOOD IAW B737 AMM 33-51-06-960-805 FOR SEAT ROWS 7ABC-12ABC A ND 32ABC (WORK ACCOMPLISHED BY V936248 AND AAR QC V936245).

Part: BATTERY PACK — NONE · airframe 51,176 hrs · 18,088 cycles

LH SEATS 7-21 EPL EXTINGUISHES PRIOR TO 15 MINUTE MINIMUM REQUIR ED FOR CAPACITY CHECK (REF. AAR NR 99916669). REMOVED & REPLACED POWER SUPPLY BATTERY PACK M1676 IAW 737 AMM 3 3-51-06-960-805 & WDM 33-51-21; OPS CR NEEDED AFTER INTERIOR LIG HT INSTALLED AND OPS TEST GOOD IAW B737 AMM 33-51-06-960-805 FOR LH SEATS 7-21 (WORK ACCOMPLISHED BY V934915 & AAR QC V936245).

Part: DOOR SILL — CORRODED (STA285.62-360.0) · airframe 51,176 hrs · 18,088 cycles

B737-53-0711 CORROSION ON R1 DOOR SILL UNDER AND SCUFF PLATE BET WEEN STA 285.62 AND 360.00. AAR RFD NR 99917236 REMOVED AND REPLACED INNER CHORD AND FRAME ASSY ON R1 DOOR SILL UNDER BETWEEN STA 285.62 AND 360.00 ALL WORK ACCOMPLISHED SRM 51 -40-02-0G-0. WORK ACCOMPLISHED BY AAR TECH V934562 AND AAR QC A- 13 V918050 RII INECTION C/W

Part: BATTERY PACK — DISCHARGED (M1671) · airframe 51,176 hrs · 18,088 cycles

LH & RH FWD OVWG EXTERNAL EMERGENCY LIGHTS ECTINGUISH PRIOR TO 1 5 MINUTE MINIMUM REQUIRED FOR CAPACITY CHECK (REF AAR NR 9991667 5). REMOVED AND REPLACED BATTERY PACK POSM1671 IAW B737 AMM 35-51-00 -960-805. TEST OF BATTERY PACK GOOD IAW AMM 35-51-06-960-805. (A CCOMPLISHED BY V931618 AND V935579).

Part: PLATE — GOUGED (STA727J-767) · airframe 51,176 hrs · 18,088 cycles

GOUGE BETWEEN STA727J & STA767, STR22L TO STR25L. ON OR BEFORE MAY 24, 2023, PERFORM AN INSPECTION PER PART 2 OF THE LATEST REVISION OF ECRA 5331-02816. TOMC APPROVED TO PLACE ON DIP FOR ON OR BEFORE MAY 24, 2023, TOMC-APPROVAL FROM SC1ELBYC COMMENT PERFORM AN INSPECTION PER PART 2 OF THE LATEST REVISION OF ECRA 5331-02816. REPAIRED IAW ECRA 5331-02816 PART 1 STEP 1, BY AAR TECH QC V916729 & AAR INSP A-70. QC REVIEWED. T/A: INSPECT ON/BEFORE 24MAY23...KJB RECORDS UPDATE...KJB

Part: SKIN — NONE (NA) · airframe 51,176 hrs · 18,088 cycles

UPON THE ACCUMULATION 50,000 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM AN INSPECTION PER PART 2 OF THE LATEST REVISION OF ECRA 5331- 02817. AAR RFD NR 99916884 SEE ELB LP 7678871 FOR REPAIR AND DIP INFORMATION.

Part: FUSE — BLOWN (M1695) · airframe 51,176 hrs · 18,088 cycles

BATTERY PACK M1695 FAILED EMERGENCY LIGHT OPC (REF AAR NR 999226 64). PERFORMED TROUBLESHOOTING IAW B737 FIM 33-50-00-810-801 STEP J(3 V932628 AND V918069). ) AND REPLACED FUSE ON BATTERY PACK (M1695) IAW B737 AMM 33-51-0 0-960-804 AND PERFORMED TEST ON BATTERY PACK (M1695) IAW B737 AM M 33-51-06-960-804. STEP 3D(5). TEST GOOD. (ACCOMPLISHED BY

Part: FLOOR SUPPORT — CORRODED (STA967-986.5) · airframe 51,176 hrs · 18,088 cycles

CORROSION ON THE SURFACE OF FLOOR SUPPORT TRACK AT STA 967 THRU STA 986.5 AT APPROXIMATELY RBL15 IN AFT CABIN (REF. AAR NR 99917 115). REMOVED AND REPLACED (1EA) FLOOR SUPPORT ON BS 967 TO 986.5 RBL1 5 IAW B737-800 SRM 51-40-02 (WORK ACCOMPLISHED BY V916729 AND AA R QC V895387).

Part: NONE — CORRODED (STA987-1006) · airframe 51,176 hrs · 18,088 cycles

AFT FLOOR STRUCTURE WEB LEFT AND RIGHT SIDES STA 987 TO 1006 HAV E CORROSION (REF. AAR NR 99917088). REMOVED AND REPLACED (2EA) FLOOR WEB R/2 L/2 ON BS 987 TO 1006 I AW B737-800 SRM 51-40-02 (WORK ACCOMPLISHED BY V916729 AND AAR Q C V895387).

Part: NONE — CORRODED (STA1016) · airframe 51,176 hrs · 18,088 cycles

CORROSION ON 3 EA FLOOR STRAPS STARTS FROM MID THRU LEFT SIDE OF THE FLOOR AT STA 1016 (REF. AAR NR 99917104). REMOVED DAMAGE 3 EA STRAP,FABRICATED NEW 3 EA STRAPS, & REPLACED 3 EA STRAPS ON BS 1016 TO 1030 LBL15 TO LBL30 IAW B737-800 SRM 51-40-02 & DWG PL 147A5714 REV LTRC (WORK ACCOMPLISHED BY V91672 9 AND AAR QC V935579).

Part: BEAM — CORRODED (STA 986.5) · airframe 51,176 hrs · 18,088 cycles

CORROSION ON SEVERAL AREAS ON FLOOR BEAM STA 986.5 STARTS FROM L EFT THRU RIGHT SIDE IN AFT CABIN (REF. AAR NR 9917112). REPAIRED FLOOR BEAM BS 986.5 IAW B737-800 SRM 53-70-51-2R REP 4 SEC 47. (WORK ACCOMPLISHED BY V916729 AND AAR QC V895387).

Part: NONE — CORRODED (STA990) · airframe 51,176 hrs · 18,088 cycles

CORROSION ON SEVERAL AREAS ON FLOOR SUPPORT (CUSP ANGLE) AT REF STA 990 IN AFT CABIN (REF. AAR NR 99917111). REMOVED AND REPLACED INNER CHORD 907 1016 LBL60 IAW B737-800 SRM 51-40-02 (WORK ACCOMPLISHED BY V916729 AND AAR QC V895387).

Part: NONE — CORRODED (STA947-990) · airframe 51,176 hrs · 18,088 cycles

CORROSION ON FLOOR SUPPORT AT STA 947 THRU STA 990 ON OUTBOARD S IDE IN AFT CABIN (REF. AAR NR 99917113). REMOVED AND REPLACED INNER CHORD ON BS 907 TO 1016 RBL60 IAW B73 7-800 SRM 51-40-02 (WORK ACCOMPLISHED BY V916729 AND AAR QC V935 579).

Part: SKIN — CRACKED (LH HOR STAB) · airframe 51,176 hrs · 18,088 cycles

HALF INCH CRACK AT LH HORIZONTAL STABILIZER LOWER SKIN AT STATIO N 129.5 APPROX. 1'' FROM LEADING EDGE (REF. AAR NR 99916788). REMOVED DAMAGE CRACK & REPAIRED AREA ON L/H HORZ LOWER SKIN AT S TA 129.5 APPROX. 1'' FORM LEADING EDGE IAW B737-800 SRM 55-10-01- 2R-11 THIS REPAIR IS A CATEGORY B & REQUIRED REPEAT INSPECTION G IVEN AT B737-800 SRM 55-10-01-2R-11-STEP 5 TABLE 204 (WORK ACCOM PLISHED BY V931931 & AAR QC V935163). INITIATE DIP FOR REINSPECTION THRESHOLD REF SRM 55-10-01-2R-11 STEP 5 TABLE 204 @ 56000 TOTAL CYC, DVI & LFEC @ 9000 CYC INTERVALS.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 50,044 hrs · 17,665 cycles

MIDDLE LH EXTERIOR OVERWING EMERGENCY EXIT LIGHT IS INOP RELAMPED L6, NO HELP, ALL OTHER LIGHTS FROM BATTERY PACK M1670 CHECK GOOD, NO FUSES IN STOCK AT LAS NO TIME TO TS FURTHER. DISPATCH DESK: 92 NAME: - APPROVED NO PARTS IN LAS SUSPECT FUSE. FOUND FUSE, REPLACED FUSE REF AMM TASK 33-51-06-960-804, OP CHECKS GOOD

Part: WASTE TANK — LEAKING (LAVATORY) · airframe 48,412 hrs · 17,046 cycles

LAV WASTE BLOWN ALL OVER COMPARTMENT AND INSULATION BLANKETS PERFORMED IMMEDIATE CLEANUP IN AFT CARGO COMPARTMENT. NEED TO INITIATE DIP TO PERFORM IN-DEPTH CLEANUP WITHIN 7 DAYS PER ECRA 2011-01000 REV AA IN AFT CARGO COMPARTMENT. AFFECTED AREA IS FROM STA 951 TO APPROX. 1006 AND FROM LBL 15 TO APPROX LBL 50 AND WILL INCLUDE SOILED INSULATION BLANKETS. PERFORMED IMMEDIATE CLEANUP IN AFT CARGO COMPARTMENT. NEED TO INITIATE DIP TO PERFORM IN-DEPTH CLEANUP WITHIN 7 DAYS PER ECRA 2011-01000 REV AA IN AFT CARGO COMPARTMENT. AFFECTED AREA IS CONTROL #: N/A SOURCE DOCUMENT: ECRA 2011-01000 REV AA FROM STA 951 TO APPROX. 1006 AND FROM LBL 15 TO APPROX LBL 50 AND WILL INCLUDE SOILED INSULATION BLANKETS. TOMC-APPROVAL FROM SC1ELBYC COMMENT REVISE STATION NUMBERS OF AFFECTED AREA TO READ FROM STA 849 TO STA 947. QC RECORDS UPDATE TOMC APPROVED QC REVIEWED DIP LIMIT Y PER ECRA2011-01213, W/IN 8 DAYS FROM27MAY19,ACCOMP ECRA2011-0100 0 LAVATORY SPILL, SECTION2B,INDEPTH CLEAN UP IN THE APPROX AREA FROM STA951-1006& FROM LBL15TO LBL50&INCLUDE INSULATION BLANKETS RECORDS UPDATE PER ECRA2011-01213, W/IN 8 DAYS FROM27MAY19,ACCOMP ECRA2011-0100 0 LAVATORY SPILL, SECTION2B,INDEPTH CLEAN UP IN THE APPROX AREA FROM STA951-1006& FROM LBL15TO LBL50&INCLUDE INSULATION BLANKETS PER MRB DIP REV DATED 01JUN19; LIMITS CHANGE AS FOLLOWS:T/A:8 DAYS...DB U359554 C/W THE IN DEPTH CLEAN-UP PORTION OF ECRA 2011-01000. REPLACED BLANKETS AS NEEDED PER ECRA 2500-01704. THIS CLOSED DIP. WORK COMPLET

Part: COVER — LOOSE (DOOR HANDLE) · airframe 42,619 hrs · 14,824 cycles

RIGHT BOTTOM OF EMERGENCY EXIT WINDOW HANDLE CAME OFF. SECURED EXIT WINDOW COVER

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,772 hrs · 14,515 cycles

RT FWD OVERWING EXIT DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED RT FWD OVERWING EXIT EXTERIOR EMERGENCY LIGHT PER AMM 33-51-04-960-801. OPS CKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,979 hrs · 13,833 cycles

EPL LIGHTS INOP FROM ROW 22 TO 31. REMOVED BATTERY PACK S/N 68504 AND INSTALLED BATTERY PACK S/N 300708 AND OPS CHECK GOOD IAW AMM 33-51-06.

Part: BATTERY — WEAK (CABIN) · airframe 39,979 hrs · 13,833 cycles

LT AFT EMERGENCY BATTERY PACK WEAK M01673. REMOVED BATTERY PACK S/N 96150 AND INSTALLED BATTERY PACK AND OPS CHECK GOOD IAW AMM 33-51-06.

Part: SLIDE — PARTIAL DEPLOY (L1 DOOR) · airframe 38,708 hrs · 13,373 cycles

FORWARD DOOR 1L PARTIAL SLIDE DEPLOYMENT. R & R ESCAPE SLIDE AT DOOR 1 LT IAW AMM 25-66 -01-400-803 & 25-66-01-400-801.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,172 hrs · 11,727 cycles

SUPPORT TASK ELONGATED HOLE LOCATED AT 727D THRU STRINGER 3R RT & SKIN. THIS NON-ROUTINE ADDRESSES THE DAMAGE TO THE SKIN. ALL WORK ACCOMPLISHED IAW ECRA 5330-05010 REV ORIGINAL. INITIATED DIP TO READ AS FOLLOWS, ON OR BEFORE 1/7/2016 ACCOMPLISH A PERMANENT REPAIR. PLANNING TO CONTACT ENGINEERING AFTER 11/7/2015 BUT BEFORE 12/7/2015 FOR THE PERMANENT REPAIR. INITIATED DIP CONTROL 031721, 44-0008 ATTACHED. IAW ECRA 5330-05010 NOTE THIS REPAIR UNDER DTA. LIMIT.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 34,172 hrs · 11,727 cycles

SUPPORT TASK ELONGATED HOLE AT STRINGER 3 RT AT STATION 727D. THIS NON-ROUTINE FOR SDR TRACKING PURPOSES ONLY. ALL WORK ACCOMPLISHED REACHED. INITIATED DIP CONTROL 031722. ACCOMPLISHED ON NON-ROUTINE 6415610. STRINGER SPLICE REPAIR ACCOMPLISHED AT STRINGER 3R, STATION 727+0 TO 727E+12 IAW SRM 53-00-03 REPAIR 3 CATEGORY B. REPAIR THRESHOLD FOR START OF SUPPLEMENTAL INSPECTION IS 61727 CYCLES & EVERY 2350 FLIGHT CYCLES AFTER THRESHOLD. ACCOMPLISH INSPECTION AT THRESHOLD OF 50,000 FLIGHT CYCLES AFTER THE REPAIR & INTERVALS OF EVERY 2350 FLIGHT CYCLES THERE AFTER IAW SRM 53-00-03 REPAIR 3 PARA 5 A 2.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 33,779 hrs · 11,596 cycles

RIGHT MLG FWD TRUNNION SUPPORT FITTING LOWER INBD ATTACH POINT CORRODED ON FACE. R & R RT MLG FWD TRUNNION SUPPORT FITTING IAW DWG 115A5002 REV N. PREFORMED FUEL LEAK CHECK IAW MM 28-11-00-400-801. NO LEAKS NOTED.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 33,779 hrs · 11,595 cycles

RIGHT STAB INSPAR RIB NR 2 VERTICAL STIFFENER IS CRACKED STAB STATION 92.70. TRIMMED DAMAGED AREA & INSTALLED REPAIR IAW REPAIR INSTRUCTIONS STEPS 4 A - 4 N OF SRM 55-10-09 REPAIR 4.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 33,779 hrs · 11,595 cycles

RIGHT STAB INSPAR RIB NR 3 VERTICAL STIFFENER IS CRACKED STAB STATION 92. TRIMMED DAMAGED AREA & INSTALLED REPAIR IAW REPAIR INSTRUCTIONS STEPS 4 A - 4 N OF SRM 55-10-09 REPAIR 4.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 33,779 hrs · 11,595 cycles

RIGHT HORIZONTAL STAB LOWER SKIN HAS A CRACK AT STAB STATION 128.5 26 INCHES AFT OF THE FWD SPAR. INSTALLED REPAIR DOUBLER AT STAB STATION 128.5 26 INCHES AFT OF FWD SPAR. INSPECTION REQUIREMENT AFTER REPAIR INSTALLATION AT 56000 FLIGHT CYCLES & 9000 FLIGHT CYCLES THEREAFTER IAW SRM 55-10-10-01 REPAIR 11 PART 5 TABLE 204.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,779 hrs · 11,595 cycles

FUSELAGE FRAME STATION 440R HAS A CRACK IN THE WEB BETWEEN STRINGER 8RT & 9RT. REPAIRED FUSELAGE FRAME RT SIDE STATION 440 BETWEEN STRINGER 8R - 9R IAW EA 5310-04716 REV H OP 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,779 hrs · 11,595 cycles

CABIN FRAME CRACKED STATION 400 BETWEEN STRINGER 8L & 9L. TRIMMED OUT CRACKED AREA & REPAIRED IAW EA 5310-04716 REV H FIG 3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,779 hrs · 11,595 cycles

FUSELAGE FRAME STATION 440L HAS A CRACK IN THE WEB BETWEEN STRINGER S 8LT & 9LT. FABRICATED & INSTALLED REPAIR ANGLES IAW EA 5310-047160 REV H OPT 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,778 hrs · 11,595 cycles

FUSELAGE FRAME STATION 380RT HAS A CRACK IN THE WEB BETWEEN STRINGER 8RT & 9RT. REPAIRED CRACK IN FRAME IAW EA 5310-04716 REV H OP 2.

Part: RECEPTACLE — FAULTY (EXTERNAL POWER) · airframe 31,519 hrs · 10,824 cycles

ELEC SPARKING IN COCKPIT WHEN WE TRY TO CONNECT GND POWER, ALSO ELEC BURN SMELL. INSPECTED AIRCRAFT IAW 05-51-26-800-801C1. FOUND EXTERNAL POWER RECEPTACLE AT FAULT. SEE ATTACHED 44.0008 & NR,S 4618644 THRU 4618659 FOR WORK ACCOMPLISHED TO REPAIR DAMAGE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,428 hrs · 10,420 cycles

FRAME CRACKED STATION 500A BETWEEN S8L & S9L. TRIMMED OUT CRACKS, FABRICATED REPAIR ANGLES & INSTALLED REPAIR IAW EA 5310-04716 REV F.

Part: LATCH — FAILED (COCKPIT DOOR) · airframe 29,113 hrs · 9,961 cycles

FLIGHT DECK DOOR WILL NOT LOCK WHEN DOOR IS CLOSED. HAVE TO TURN AND PLAY WITH DOOR KNOB TO LOCK. VERY UNSAFE AND PRONE TO DOOR BEING PULLED OPEN BY PERSON ON OUTSIDE OF DOOR. REPLACED LATCH ASSY AND OPS CHECKED REF AMM 52-52-02-800-801 C18/ CMM 52-51-02. OPS CHECK NORMAL.

Part: SIGN — MISSING (ROW 25) · airframe 26,865 hrs · 9,184 cycles

MID CABIN OVERHEAD EXIT SIGN MISSING. AT ROW 25. REINSTALLED SIGN ON FWD SIDE, SIGN TESTED OK.

Part: FEEDER CABLE — LOOSE (NR 2 GENERATOR) · airframe 25,994 hrs · 8,873 cycles

NR 2 ENGINE GENERATOR SOURCE OFF LIGHT INFLT, UNABLE TO BRING NR 2 GENERATOR ONLINE. UNABLE TO START APU INFLIGHT. OPS CHECKED APU REF AMM 49-00-00. OPS CHECKED GOOD. FOUND MAIN FEEDER HARNESS LOOSE AT FIREWALL, ECURED, RAN ENGINE, GENERATOR OPS AND LEAK CHECKED GOOD.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 17,549 hrs · 5,845 cycles

737-53-3-0714 FWD CARGO COMPARTMENT RT SIDE PLATE - CHANNEL OR SUPPORT ZEE HAS CORROSION FROM STA 495 - 500I. REMOVED, FABRICATED NEW PART P/N 143A8126-30, AND RE-INSTALLED REF SRM 53-00-53 AND SRM 51-40-02.