N36280

Part: CONTROL SWITCH — FAULTED (THRUST REVERSER) · airframe 62,746 hrs · 23,144 cycles

ENG 2 REV THRUST STICKY ON LANDING. PERFORM THE BITE TEST ON 2 ENGINE REV THE EAU FOUND ONLY ONE FAULT T/R DELOY FAULT DID THE NORMAL OPS TEST SYSTEM WORK UNTIL NOTICE AFTER YOU DELOYED THE HANDLE TO FULL DELOY THE T/R DOES NOT DELOY AND YOU GET THE REV LIGHT BUT WHEN YOU GO BACK A FEW INCHES SHORT OF FULL DELOY T/R DELOYED AND STOWED WITHOUT A PROBLEM SUSPECT THE SWITCHPACK SWITCH IS BAD I NEED MORE TROUBLESHOOTING REF AMM 78-31-00-700-801-F00 AND FIM 78-34 TASK 810 . PERFORM SYNC LOCK OPERATION TEST AND THE TEST PASS REF AMM 78-31-00-700-803-F00. CYCLED ENG 2 T/R. FIRST CYCLE IT DEPLOYED APPROX 3-5 INCHES THEN STOWED IMMEDIATELY W/O MOVING LEVER TO STOW. EVERY CYCLE AFTER T/R FULLY DEPLOYED AND STOWED CORRECTLY. PERFORMED EAU BITE, PICTURES ATTACHED. REF FIM 78-32 TASK 806 FAULT ISOLATION, PERFORMED SPRING FREE ANGLE CHECK. SPRING IS OUT OF LIMITS. GAINED ACCESS TO CONTROL SWITCH IN ENG 2 THRUST LEVER REF AMM 78-34-04. SUSPECT SWITCH WAS INSTALLED OR WIRED BACKWARDS. ACTUATOR BUTTON WAS AFT, AMM/AIPC SHOWS ACTUATOR BUTTON FWD. WIRING COMPLETED INSTALL OF ENG 2 TR CONTROL SWITCH REF AMM 78-34-04 THROUGH END OF TASK. OPS CHECK GOOD NO FAULTS NOTED AT THIS TIME. OPERATED ENG 2 TR WITH ENGINE RUNNING NO FAULTS NOTED REF LP 5723511 FOR TRA FLUCTUATIONS.

Part: GIRT BAR — LOOSE (ZONE 800) · airframe 62,152 hrs · 22,863 cycles

1L GIRT BAR NEEDS INSPECTION.FA REPORTS END IS LOOSE L1 DOOR SLIDE GIRT BAR RELEASE STOP COLLAR HALVES SPLIT. INSTALLED NEW GIRT BAR RELEASE STOP ASSEMBLY IAW AMM 25-66-01-400-803.

Part: SMOKE DETECTOR — FALSE ACTIVATION (ZONE 900) · airframe 61,114 hrs · 22,408 cycles

LAV E SMOKE ALARM WENT OFF INTERMITANTLY 3 TIME S WITH NO EVIDEN CE OF SM OKE OR FUMES NO FAULTS NOTED UPON ARRIVAL. PERFORMED BITE OF LAV E SMOKE DET PER AMM26-14-00-710-802. OPS CHECK GOOD. NO HISTORY

Part: WIRE — LOOSE (ZONE 200) · airframe 61,051 hrs · 22,379 cycles

EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - ROWS 2ABC,3ABC,4ABC EMERGENCY LIGHTS INOP. FOUND LOOSE WIRES BELOW SEAT TRACK COVER IN WIRE BUNDLE TRACK. ADJ/SECURED WIRES. OPS CHK GOOD. EMERG. LIGHTS WORKING AS DESIGNED. AMM REF 33-51-00

Part: WARNING LIGHT — ILLUMINATED (AIR SPEED) · airframe 60,289 hrs · 21,980 cycles

IAS DISAGREE LIGHT 80KTS CA...95KTS FO PERFORMED FIM 31-62 TASK 876. UPON PERFORMING FLUSHING, AMM TASK 34-11-00-170-802.RETRACTED DEBRIS FROM CAPTAIN'S PITOT LINE.PERFORMED PITOT LEAK CHECK PER AMM TASK 34-11-00-790-810.OPS CHECK GOOD. VERIFIED PITOT TUBES WERE CLOSED AND SECURE.

Part: SKIN — DAMAGED (BS 727E S3L) · airframe 59,384 hrs · 21,566 cycles

FOUND DAMAGE ON EXTERNAL SURFACE OF SKIN JUST AFT OF LIVE TV DOUBLER LOCATED AT 727E S-3L. DAMAGED AREA IS APPROXIMATELY 2 1/ 2 INCHED LONG. SEE BAM N/R 001867632 FOR REPAIR OF AREA. READ "ACCOMPLISH INSPECTION REQUIREMENTS OF THE CROWN SKIN EC/RA 5331-03088 ON OR BEFORE 7 MARCH 2025." 2ND DIP ISSUED ON E BETWEEN BS 727E AND 727F UNDER LIVE TV RADOME PER PART 2 OF LB 7818000. REF EC/RA 5331-03088 PART 1- INTERIN REPAIR ACCOMPLISHED EC/RA 5331-03088 PART 1 INTERIM RERPAIR SEE BAM N/R 001867632 FOR ALL WORK ACCOMPLISHED. ISSUED 1ST DIP TO TOMC APPROVED, PLACED ON DIP ?ACCOMPLISH INSPECTION REQUIREMENTS TOMC-APPROVAL FROM SC1ELBYC COMMENT OF THE CROWN SKIN BETWEEN BS 727E AND 727F UNDER LIVETV RADOME PER PART 2 OF EC/RA 5331-03088 ON OR BEFORE 7 / MARCH 2025.? REF ECRA 5331-03088 QC QC REVIEW INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: SKIN — DENTED (BS 727C S2-3L) · airframe 59,384 hrs · 21,566 cycles

LIVE TV DOUBLER LOCATED ON EXTERNAL SURFACE AT 727C BETWEEN S-2L AND S-3L IS DIFFERENT THAN WHAT IS SHOWN OF T-CARD T29-4430-1-0057. ALL 3 END FASTENERS AT FWD END ARE UNDER THE DOUBLER SO THE TWO FWD FASTENERS SHOWN ON THE ILLUSTRATION CAN NOT BE HFEC INSPECTED DUE TO A PREVIUS DENT APPROVED BY ECRA 5330-04712 AND LIVE TV EA 1944. NOWTHE DENT WILL INTERFERE WITH THE CURRENT KA MODIFICATION . TV RADOME PER PART 2 OF EC/RA 5330-05083 REV. A ON OR BEFORE SEPTEMBER 1ST. 2024. INITIATE A DIP TO STATE ACCOMPLISH INSPECTION REQUIREMENTS OF THE FUSELAGE CROWN SKIN DOUBLER AT STA. 727C AND S-2L UNDER LIVE TOMC APPROVED, PLACED ON DIP. ?ACCOMPLISH INSPECTION TOMC-APPROVAL FROM SC1ELBYC COMMENT REQUIREMENTS OF THE FUSELAGE CROWN SKIN DOUBLER AT STA727C AND S-2L.

Part: STRINGER — CORRODED · airframe 59,384 hrs · 21,566 cycles

L/H WING UPPER STRINGER 12A HAS CORROSION AT WSTA 685.

Part: SKIN — CORRODED (L/H WING UP SKN) · airframe 59,384 hrs · 21,566 cycles

L/H WING UPPER SKIN INTERNAL SKIN CORROSION AT WSTA 685 BETWEEN STRINGER 12A-10B WAS REPAIRED ON BAM N/R 001906676 REF EC/RA 5721-01492 AND REQUIRES A SIGNIFICANT FINDINGS REPORT TO NE ISSU ED. CREATED SFR #1035938

Part: FRAME — MECHANIC ERROR (BS 520) · airframe 59,384 hrs · 21,566 cycles

BS 520 FRAME INNER CORD AT L/H WL 210 HAD A MISDRILLED FASTENER. INNER CHORD AT S-17L, ACCOMPLISH INSPECTION REQUIREMENTS PER 50,000 TOTAL FLIGHT CYCLES." REF EC/RA 5310-08292 REV A PART 1 001876045 FOR ALL WORK ACCOMPLSHED. PART 2 OF EC/RA 5310-08292 ON OR BEFORE THE AIRCRAFT REACHING INTERM REPAIR. SEE ELB 7709300 FOR 2ND DIP AND BAM N/R ACCOMPLISHED PART 1 INTERM REPAIR SEE BAM N/R 001876045 FOR ALL WORK ACCOMPLISHED AND ISSUED DIP TP READ "AT THE BS 520 FRAME DIP 53-DIP THIS DIP LOG PAGE NEEDS TO BE INITIATED AS *DTA* PER ECRA 5310-08292 REV A PART 1 ITEM 8.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 59,384 hrs · 21,566 cycles

LEFT HAND SIDE LOWER HORIZONTAL SKIN CRACKED AT STATION 157.10 APROX. 10 INCHES AND 20 INCHES FROM AFT SPAR. EACH CRACK IS ONE INCH IN LENGTH AND MARKED. REF BAM NON-ROUTINE 001864997 FOR COMPLETION OF REPAIR. A DIP IS REQUIRED TO BE ISSUED IAW SRM 55-10-01-2R-11 REPAIR 11 STEP 5 TABLE 204. TERNAL PART OF DOUBLER AND THE SPAR CHORD UNDER THE EXTERNAL PAR -11 REPAIR 11. ISSUED DIP TO READ " INSPECTION THRESHOLD 56,000 EXTERNAL PART OF THE DOUBLER AND PERFORM A LFEC INSPECTION OF TH UNDER THE EXTERNAL PART OF THE DOUBLER. REPEAT INSPECTIONS EVERY REPAIR 11 STEP 5 TABLE 204. T OF THE DOUBLER. REPEAT INSPECTIONS EVERY 9,000 FC THEREAFTER. TOTAL FLIGHT CYCLES PERFORM A DETAILED VISUAL INSPECTION OF THE E SKIN UNDER THE EXTERNAL PART OF THE DOUBLER AND THE SPAR CHORD 9,000 FLIGHT CYCLES THEREAFTER." REF SRM 55-10-01-2R-11 REF SRM 55-10-01-2R-11 REPAIR 11 STEP 5 TABLE 204. INSTALLED REPAIR DOUBLER AT STAB STA 157.10 SEE BAM NR 1864997 TASKS AND UPDATES FOR ALL WORK ACCOMPLISHED. REF SRM 55-10-01-2R TOMC APPROVED FOR DIP INSP THRESHOLD 56,000 TOTAL FLT CYCLES TOMC-APPROVAL FROM SC1ELBYC COMMENT PERFORM A DETAILED VISUAL INSPECTION OF THE EXTERNAL PART OF THE DOUBLER AND PERFORM A LFEC INSPECTION OF TH E SKIN UNDER THE EXTERNAL PART OF THE DOUBLER AND THE SPAR CHORD UNDER THE EXTERNAL PART OF THE DOUBLER. REPEAT INSPECTIONS EVERY 9,000 FLT CYCLES THEREAFTER." REF SRM 55-10-01-2R-11 VERIFIED ESFR #1035775 AND DIP BY QC VERIFIED DIP. INSTALLED REPAIR DOUBLER AT STAB STA 147.90 SEE BAM N

Part: SKIN — CRACKED (RH HORIZ STAB) · airframe 59,384 hrs · 21,566 cycles

RIGHT HORIZONTAL STAB LOWER SKIN IS CRACKED AT STAB STA 147.90 LOCATED 9 INCHES FWD OF AFT SPAR. CRACK IS MARKED AND MEASURES 1 INCH LONG. REF BAM NON-ROUTINE 001865013 FOR COMPLETION OF RE PAIR. A DIP IS REQUIRED TO BE ISSUED IAW SRM 55-10-01-2R-11 REPA IR 11 STEP 5 PAGE 7 TABLE 204. ISSUED DIP TO READ " INSPECTION THRESHOLD 56,000 TOTAL FLIGHT PART OF THE DOUBLER AND PERFORM A LFEC INSPECTION OF THE SKIN THE EXTERNAL PART OF THE DOUBLER. REPEAT INSPECTIONS EVERY STEP 5 PAGE 7 TABLE 204. CYCLES PERFORM A DETAILED VISUAL INSPECTION OF THE EXTERNAL UNDER THE EXTERNAL PART OF DOUBLER AND THE SPAR CHORD UNDER 9,000 FLIGHT CYCLES THEREAFTER. REF SRM 55-10-01-2R-11 REPAIR 11 INSTALLED REPAIR DOUBLER AT STAB STA 147.90 SEE BAM NR 1865013 FOR ALL WORK ACCOMPLISHED. REF SRM 55-10-01-2R-11 REPAIR 11.

Part: SKIN — CRACKED (RH HORIZ STAB) · airframe 59,384 hrs · 21,566 cycles

R/H HORIZONTAL STAB LOWER SKIN HAS 2 CRACKS AT STAB STA 101.90 O NE 10" FWD OF AFT SPAR AND ONE 20" FWD OF AFT SPAR. REF BAM NR 1 865008 AND NR 1865012. 12 ARE COMBINDED INTO ONE REPAIR DOUBLER ON BAM NR 1865008. INSTALLED REPAIR DOUBLER AT STAB STA 101.90 SEE BAM NRS 1865008 AND 1865012 FOR ALL WORK ACCOMPLISHED. BAM NR 1865008 AND 18650.

Part: STRUCTURE — CORRODED (R2 DOOR) · airframe 59,384 hrs · 21,566 cycles

R2 DOOR CHORD HAS CORROSION ON BOTTOM (MARKED). FROM BAM N/R 001885605. FOR ESFR REPORTING. REF. BAM N/R 001885605 FOR ALL WORK PERFORMED.. REMOVED AND REPLACED R2 CHORD PER SRM 51-10-02 AND SRM 51-40-02. FOR ESFR REPORTING. VERIFIED ESFR C/W.

Part: UNKNOWN — UNKNOWN (FLIGHT DECK) · airframe 58,578 hrs · 21,253 cycles

INTERMITENT ELECTRICAL SMELL CAPT SIDE WHILE ENROUTE.CAPT LEFT AND OR BEHIND AREA SUSPECT. DEBRIEFED CREW, F/O DID NOT SMELL ODOR, ONLY CAPTAIN. PERFORMED ELECTRICAL ARCING IN FLIGHT DECK NOR CABIN. CONDITIONAL INSPECTION, SMOKE/ODOR IN FLIGHT DECK/CABIN IAW AMM 05-51-26-800-801-C1 WITH APU RUNNING AND PACKS ON. NO FAULTS FOUND. NO OPEN BREAKERS, NO EVIDENCE OF ANY BURNING OR ADD EMP:U231339

Part: LATCH — BINDING (DOOR SLIDE) · airframe 58,458 hrs · 21,202 cycles

L1 DOOR SLIDE DROPPED FROM SHROUD. SLIDE DID NOT DEPLOY. FOUND DOOR SLIDE LATCH ASSY STIFF. REPLACED CHECK OK. END

Part: PITOT HEAD — NONE (REL) · airframe 54,252 hrs · 19,548 cycles

FEEL DIFF PRESS LITE ON ROTATE CLIMB OUT FOUND BUILDUP AT INLET OF RT ELEV PITOT PROBE. CLEANED AND FLUSHED ELEV FEEL PITOT PROBES PER AMM 27-31-17. PERFORMED PRESSURIZATION CHK PER SAME. PRESS READS SAME AND INDICATIONS NORMAL. OK TO CONTINUE.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 53,936 hrs · 19,410 cycles

SUPPORT TASK - EA 5510-01843 REV H OP 001 - L/H HORIZONTAL STABI LIZER LOWER SKIN PANEL AT STA 129.5 FOUND 1EA CRACK APPROX 0.875 " IN LENGTH REF NR LP 9130720 LH HORI STAB LOWER SKIN REPAIRED AS PER SRM 55-10-01-2R-11 REPAI R 11 FIG 204 TABLE 201 AND TABLE 203 CATEGORY B REPAIR AND REPEA T INSPECTION REQUIRMENT PER SRM 55-10-01-2R-11 REPAIR 11 TABLE 2 04 AND FIG 206 AT STA 129.5 APPROX 34" FROM LWR SKIN FWD EDGE. REPEAT INSPECTION REQUIRMENT REFER LP 6565132

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 53,936 hrs · 19,410 cycles

SUPPORT TASK - EA 5510-01843 REV H OP 001 - L/H HORIZONTAL STABI LIZER LOWER SKIN PANEL AT STA 101.9 FOUND 1EA CRACK APPROX 1" IN LENGTH REF NR LP 9130721 LH HORI STAB LOWER SKIN REPAIRED AS PER SRM 55-10-01-2R-11 REPAI R 11 FIG 204 TABLE 201 AND TABLE 203 CATEGORY B REPAIR AND REPEA T INSPECTION REQUIRMENT PER SRM 55-10-01-2R-11 REPAIR 11 TALBE 2 04 AND FIG 206 AT STA 101.9. REPAIR LOCATION AT STA 101.9 APPROX 38" FROM LWR SKIN FWD EDGE. REPEAT INSPECTION REQUIRMENT REFER ADD EMP:V896888 L/P 6565231 INSPECTED BY HX 182816

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 53,936 hrs · 19,410 cycles

SUPPORT TASK - EA 5510-01843 REV H OP 001 - RH HORIZONTAL STABIL IZER LOWER SKIN PANEL AT STA 175.5 FOUND 1EA CRACK APPROX 1.750" IN LENGTH REF NR LP 9130719 RH HORIZONTAL STABILIZER LOWER SKIN REPAIRED AS PER SRM 55-10-01 -2R-11 REPAIR 11 FIG 204 TABLE 202 AND TABLE 203 CATEGORY B REPA IR AND REPEAT INSPECTION REQUIRMENT PER SRM 55-10-01-2R-11 REPAI R 11 TABLE 204 AND FIG 206 AT STA 129.5 APPROX 17" FROM LWR SKIN FWD EDGE. REPEAT INSPECTION REQUIRMENT REFER LP 6565255 ADD EMP:V896888 INSPECTED BY HX182816

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 53,936 hrs · 19,410 cycles

SUPPORT TASK - EA 5510-01843 REV H OP 001 - RH HORIZONTAL STABIL IZER LOWER SKIN PANEL AT STA 129.5 FOUND 1EA CRACK APPROX 0.875" IN LENGTH REF NR LP 9130718 RH HORI STAB LOWER SKIN REPAIRED AS PER SRM 55-1-01-2R-11 REPAIR 11 FIG 204 TABLE 201 AND TABLE 203 CATEGORY B REPAIR AND REPEAT INSPECTION REQUIRMENT PER SRM 55-10-01-2R-11 REPAIR 11 TABLE 20 4 AND FIG 206 AT STA 129.5 APPROX 17" FROM LWR SKIN FWD EDGE. REPEAT INSPECTION REQUIRMENT REFER LP 6565449

Part: RESTRICTOR VALVE — OBSTRUCTED (LT ELEVATOR) · airframe 53,607 hrs · 19,268 cycles

FEEL DIFF PRESS LIGHT, PER FLIGHT CREW FEEL DIFF LIGHT EXTINGUISHED AFTER LANDING. PERFORMED FIM TASK 27-31-00-810-815 STEP E(7). CLEANED DEBRIS FROM LT ELEVATOR RESTRICTOR VALVE. UNABLE TO COMPLETE ISLOLATION PROCEDURE "C" LIFT EQUIP UNAVAILABLE 1-00-700-811. NOTE ALL FAULTS FOUND. 0-730-801 AND FEEL DIFFERENTIAL PRESSURE LIGHT TEST, PER AMM 27-3 -31-17-170-801 AND VERIFY PITOT HEATER OPERATION, PER AMM 30-31-0 TECH SUPPORT REQUEST: ALSO DO ELEV PITOT SYSTEM FLUSH, PER AMM 27 UPDATE: TEMPERATURE CHECK ON BOTH PITOT AND LEFT SIDE READS LITTLE LOWER THAN RIGHT 10 FEET AWAY. RIGHT SIDE READS. 137 DEGREE AND LEFT 128 DEGREE. JUST INFORMATION. PERFORMED ELEVATOR PITOT SYSTEM FLUSHING, PER AMM 27-31-17-170-801. CLEARED DEBRIS OUT OF LEFT ELEVATOR PITOT, OPERATIONS AND LEAK CHECKS GOOD. PERFORMED ELEVATOR PITOT HEATER TEST, PER AMM 30-31-00-730-801, CHECKS NORMAL. PERFORMED FEEL DIFFERENTIAL PRESSURE LIGHT TEST, PER AMM 27-31-00-700-811 SYSTEM OPERATES CORRECTLY W/NO FAULTS NOTED. OK FOR SERVICE.

Part: SWITCH — OPEN · airframe 53,169 hrs · 19,103 cycles

AIR RETURN FLIGHT 2859 MNL. ALL LANDING GEAR WOULD NOT RETRACT. ALL GREEN LIGHTS (6) AND ALL RED LIGHTS (3) ON WHEN GEAR HANDLE WAS SELECTED UP, VERBAL FROM CREW. CYCLED HANDLE DOWN AND LANDED NORMAL. PERFORMED BITE OF PSEU NO FAULTS, NO FAILURES. FIM 32-09-00-810-801. PERFORMED CHECK OF EMERGENCY GEAR SYSTEM DOOR AND SWITCH. CYCLED SWITCH. AMM 32-34-00-820-802. PERFORMED FIM 32-30-00-810-813 LANDING GEAR CONTROL LEVER LOCK. OPS NORMAL. PERFORMED GROUND LANDING GEAR CHECK WITH GEAR PINS AND TOMC MANAGER CONCUR WITH ACTION. INSTALLED. ALL OPERATING NORMAL. OK FOR SERVICE.

Part: PIN — WORN (R2 WINDOW) · airframe 53,126 hrs · 19,077 cycles

UNABLE TO ACCESS COCKPIT USING EXTERNAL FIRST OFFICERS WINDOW EMERGENCY RELEASE HANDLE. NO AMOUNT OF PULLING RELEASES WINDOW. AFTER FURTHER EVALUATION FOUND CAMSHAFT PIN WORN. R & R CAM PIN ASSEMBLY & AMP. PERFORMED EMERGENCY EXIT RELEASE ADJUSTMENT IAW AMM REF 56-12-11, CMM REF 56-10-01 & IPC REF 56-22-51. OPERATIONS CHECK NORMAL AT THIS TIME.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 53,104 hrs · 19,059 cycles

SEAT ROW 30 AND 34 ABC AND L2 DOOR EMERGENCY LIGHT INOP REMOVE AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK (M1673) AT LEFT AFT CABIN CEILING STA 952 WL 290 LBL 14 PER AMM 33-51-06

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 49,959 hrs · 17,678 cycles

AFTER T/O GEAR LEVER UP ALL 3 GEAR INDICATONS SHOWED RED AND GREEN LIGHTS. GEAR NOT RTRCTD PERFORMED FIM TASK 32-30-00-810-805. OPS CK SEVERAL TIMES, NO FAULTS NOTED. A/C OK FOR SVC -END- RII INSPECTION C/W PER GMM 09-25-05.

Part: FITTING — CORRODED (R1 DOOR) · airframe 48,611 hrs · 17,084 cycles

R1 DOOR STOP PIN FITING THIRD FROM TOP HAS CORROSION. REMOVED AND REPLACED FITTING PER SRM 51-40-02 AND DWG 141 A6516.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 48,611 hrs · 17,084 cycles

LT HORIZ STAB LWR SKIN HAS 1.5" CRACK AT STAB STA 129.50, 27" FROM STAB FRONT SPAR. REPAIRED LOWER STAB SKIN AS REF SRM 55-10-01 REPAIR 11.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 48,611 hrs · 17,084 cycles

RT HORZ STAB LWR SKIN HAS 2 EA CRACK AT STAB SKIN STA 129.50 THE FIRST CRACK IS 1.25 LONG 27 INCHES FROM STAB FRONT SPAR AND THE SECOND CRACK IS 1.25 LONG 35 INCHES FROM FRONT SPAR. REPARED STAB SKIN REF SRM 55-10-01 REF FLEETCYCLE L/P 9614041 FOR WORK PERFORMED. REINSPECT AFTER 56000 FLIGHT CYCLES DV INSPECT ON DOUBLER AND LFEC ON SKIN UNDER DOUBLER EVER 9000 CYCLES. PERFORMED REPAIR IAW SRM 55-10-01 REPAIR 11 TABLE 201 AND TABLE 203, INSPECTION THRESHOLD OF 56,000 TOTAL FLIGHT CYCLES WITH INTERVAL EVERY 9000 FLIGHT CYCLES FOR DVI AND LFEC TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTED QC REVIEWED. QC REVIEWED. RECORDS UPDATE...MB/V740009 INIT: 56K TAFC (WILL ITO TO RIR -2209) RIR: 9K FC...MB/V740009.

Part: FITTING — LOOSE (L2 DOOR) · airframe 45,857 hrs · 16,042 cycles

GIRT BAR CLIP ON SLIDE PACK HOUSING LOOSE AT DOOR 2L. ADJUSTED GIRT BAR CLIP. NO DEFECTS NOTED,.

Part: CIRCUIT BREAKER — OPEN · airframe 45,481 hrs · 15,886 cycles

REVERSE THRUST LEVER HAS LOST MOTION, NO THRUST REVERSER OPERATION FOR NR 2 ENGINE, FOUND CIRCUIT BREAKERS OUT AT GATE. NR 2 ENGINE SYNC LOCK, INTLK , CONT, AND IND. RESET. NR 2 THRUST REVERSER OPS CHECKED OK, NO FAULTS NOTED.

Part: BEZEL — BURNED (WORK LIGHT) · airframe 45,434 hrs · 15,869 cycles

FLT ATTENDANT REPORTED A BRIEF MOMENT OF SMOKE, BOTH VISUALLY AND BY SMELL FROM FORWARD GALLEY, SPOKE WITH FLIGHT CREW, FO COULD DETECT THE SMOKE AND FLT ATTENDANT ALSO AROUND FIRST CLASS GALLEY, WHITE SMOKE WAS NOTED AT TOP END OF GALLEY FOR A SHORT TIME. NO INDICATIONS OF LIGHTING OR ANY COCKPIT PROBLEMS BY CREW NOTED. P6 PANEL BACKS UP TO GALLEY. ACCOMPLISHED SMOKE/ODER INSPECTION IAW MM 5-51-26-800-801C. FOUND GALLEY G2 WORK LIGHT WITH THREE BURNED OUT LAMPS, REPLACED THE LAMPS, OPS CHECKED GOOD. ALSO FOUND THE L1 DOOR. FLIGHT ATTENTANT WORK LIGHT WITH BURNED BEZEL ASSY, REPLACED THE BEZEL AND LAMP, OPS CHECKED GOOD. INSPECTED BEHIND P5 AND P6 PANELS, GALLEY G1 AND G2 CIRCUIT BREAKER PANELS, GALLEY G1 AND G2 WORK AND AREA LIGHT ASSEBLIES. L1 DOOR ENTRY LIGHT ASSY. BEHIND OVERHEAD CEILING PANEL AT ROW 1. OPS CHECKED GALLEY OVENS AND COFFEE MAKERS FOR SEVERAL HOURS, NO DEFECT NOTED. RAN APU AND PACKS FOR 1/2 HOUR NO DEFECTS NOTED .

Part: LENS — LOOSE (EXIT SIGN) · airframe 43,509 hrs · 15,118 cycles

EMERGENCY EXIT SIGN DOES NOT TURN OFF. OVERWING EXIT SIGN FALLING OFF ACTUAL PROBLEM IS AISLE CENTER EMERG EXIT SIGN LENS LOOSE. REATTACHED AND SECURED LENS.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 43,007 hrs · 14,923 cycles

AFT GALLEY EMERG FLASHLIGHT INDICATOR NOT FLASHING. REPLACED THE BATTERY.

Part: FLAP — MALFUNCTIONED (WING) · airframe 37,741 hrs · 12,961 cycles

ON FINAL APPROACH, WIND GUST EXCEEDED FLAPS 30 SPD & THEY RETRACTED TO 25, ON MISSED APPROACH THEY WERE LOCKED OUT AT ABOUT 27 COULD NOT RETRACT, FLAP STAYED AT 27 UNTIL LANDING & RETURNED TO 25 AFTER TOUCHDOWN. MAX SPEED ON MISS WAS 195 WITH GUSTS & FLAP AT 27 DEGREES. INSPECTED FLAPS & SLATS WINGS, NO DEFECTS NOTED. PERFORMED FSEU BITE IAW FIM 27-51-00 810-801. PERFORMED TE FLAP LOAD RELIEF GND TEST ALL PASSED IAW FIM 27-51-00. ALSO PERFORMED PHASE 1 FLAP & SLAT OVER SPEED CONDITION IAW MM 05-51-08-201, ALL GOOD. OK FOR SERVICE AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,243 hrs · 12,778 cycles

EMERGENCY BATTERY PACK FOR LT WING EMER LIGHTS INOPERATIVE. SEE WORK ACCOMPLISHED ON NR 6174406. R & R EMER EXIT LIGHT BATTERY PACK M1694 IAW AMM 33-51. OPERATIONS CHECKED GOOD IAW AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,243 hrs · 12,778 cycles

SUPPORT TASK EMER LIGHT OUTSIDE L1 ENTRY DOOR INOPERATIVE, STATION 322. R & R EMER LIGHT BATTERY PACK. OPERATIONAL CHECKED GOOD IAW AMM 33-51-06. PN AD-D717-01-100.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,243 hrs · 12,778 cycles

SUPPORT TASK EMER LIGHTS ABOVE RT WING INOPERATIVE, STATION 565, WL 213 & RBL 68. REMOVED EMER EXIT LIGHT BATTERY PACK M1695 FOR RT OVERWING & INSTALLED NEW EMER BATTERY PACK IAW AMM 33-51-06. OPERATIONS CHECKED GOOD. MANUFACTURER PN ADD717-01-100 BN 156305, STATION 565, WL 213 & RBL 68.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,243 hrs · 12,778 cycles

SUPPORT TASK FWD LT EMER PATH LIGHT INOPERATIVE AT STATION 322, WL 291 & RBL 7. R & R BATTERY PACK M1674 IAW MM 33-51-06. OPERATIONAL CHECKED GOOD PN AD-D 717-01-100.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 37,243 hrs · 12,778 cycles

SUPPORT TASK GEN N/ TO CAPTURE ADDITIONAL WORK FROM ORIGINATING NR 6167014. REMOVED DAMAGED SKIN, FABRICATED & INSTALLED FILLER & DOUBLER IAW ECRA 5330-05083 REV.

Part: SKIN — GOUGED (FUSELAGE) · airframe 32,375 hrs · 11,101 cycles

UPPER CROWN, LIVE TV ANTENNA MOUNT AREA, JUST OTBD OF LT DOUBLER, 2 INCHES FWD OF STATION 727E AT STRINGER 3L SKIN GOUGED. ACCOMPLISHED EC/RA 5330-04711 PART 1 INTERIM REPAIR INSTALLED DOUBLER FROM STATION 727D-727E & STRINGER 2L-3L.

Part: SKIN — GOUGED (FUSELAGE) · airframe 32,375 hrs · 11,101 cycles

UPPER CROWN, LIVE TV ANTENNA MOUNT AREA, JUST OTBD OF LT DOUBLER, STATION 727E AT STRINGER 3L SKIN GOUGED. ACCOMPLISHED EC/RA 5330-04711 PART 1 INTERIM REPAIR INSTALLED DOUBLER FROM STATION 727D-727E & STRINGER 2L-3L.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,375 hrs · 11,101 cycles

IAW AD 2009-01-02 EA 5310-04716 REV E FRAME AT STATION 480L BETWEEN STRINGERS 8 & AMP 9 INBD RIVET HOLE HAS A CRACK INDICATION. REPAIRED IAW ECRA 5310-05855.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,375 hrs · 11,101 cycles

IAW AD 2009-01-02 EA 5310-04716 REV E FRAME AT STATION 727D R BETWEEN STRINGERS 8 & AMP 9 INBD RIVET HOLE HAS CRACK INDICATION REPAIRED IAW ECRA 5310-05855.

Part: SKIN — GOUGED (FUSELAGE) · airframe 32,375 hrs · 11,101 cycles

UPPER CROWN, LIVE TV ANTENNA MOUNT AREA, FWD OF AFT LT DOUBLER, BETWEEN STATION 727D & AMP STATION 727E 3 INCHES TO THE LT OF STRINGER 2L SKIN GOUGED. ACCOMPLISHED EC/RA 5330-04711 PART 1 INTERIM REPAIR INSTALLED DOUBLER FROM STATION 727D-727E & STRINGER 2L-3L.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,375 hrs · 11,101 cycles

REF AD 2009-01-02, EA 5310-04716 REV E FRAME AT BS 400R, BETWEEN STRINGERS 8 & AMP; 9, INBOARD RIVET HOLE HAS A CRACK INDICATION. REPAIRED BS 400R FRAME BETWEEN STRINGERS 8 & AMP; 9 IAW EA 5310-04716 REV E.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,375 hrs · 11,101 cycles

REF AD 2009-01-02, EA 5310-04716 REV E FRAME AT BS 727D L, BETWEEN STRINGERS 8 & AMP; 9, INBOARD RIVET HOLE HAS A CRACK INDICATION. REPAIRED BS 727D L/H FRAME IAW EA 5310-04716 REV E.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,375 hrs · 11,101 cycles

IAW AD2009-01-02, EA5310-04716 REV E. FRAME AT STATION 440L, BETWEEN STRINGER 8 & AMP; 9 INBD RIVET HOLE HAS A CRACK INDICATION. REPAIRED FRAME AT STATION 440L BETWEEN STRINGER 8 & AMP; 9 IAW EA5310-04716 R EV E. SEE WIPS & TASKS FOR ALL WORK PERFORMED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,375 hrs · 11,101 cycles

REF AD 2009-01-02, EA 5310-04716 REV E FRAME AT STA 400L, BETWEEN STRINGERS 8 & 9, INBOARD RIVET HOLE HAS A CRACK INDICATION. REPAIRED STA 400L FRAME BETWEEN S-8 & S-9 IN ACCORDANCE WITH EA 5310-04716 REV E.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,375 hrs · 11,101 cycles

REF AD 2009-01-02, EA 5310-04716 REV E FRAME AT BS 500A R, BETWEEN STRINGERS 8 & AMP; 9. INBOARD RIVET HOLE HAS A CRACK INDICATION. REPAIRED FRAME AT BS 500A R/H BETWEEN STRINGERS 8 & AMP; 9 IN IAW EA 5310-04716 REV E.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,375 hrs · 11,101 cycles

IAW AD 2009-01-02, EA 5310-04716 REV E. FRAME AT BS 440R, BETWEEN STRINGER 8 & AMP; 9 INBOARD RIVET HOLE HAS A CRACK INDICATION. REPAIRED FRAME AT BS 440R BETWEEN STRINGER 8 & AMP; 9 PER EA 5310-04716 REV E. SEE WIPS & AMP; TASKS FOR ALL WORK PERFORMED

Part: BLADES — DAMAGED (NR 2 ENGINE) · airframe 27,822 hrs · 9,495 cycles

TAKE OFF ROLL NR 2 ENGINE BIRD STRIKE & VIBRATION 4.5 IN CLIMB. NR 2 ENGINE BSI, FAN BLADES & ACOUSTIC PANELS R & R IAW AMM 72-21-02-000-801.

Part: LIGHT — FAILED (GALLEY) · airframe 25,453 hrs · 8,643 cycles

FWD GALLEY LIGHT INOP BURNING SMELL NOTED AND THEN LIGHT BURNED OUT. REMOVED AND REPLACED FWD AREA GALLEY LIGHT ASSY. OPS GOOD.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 24,593 hrs · 8,326 cycles

SUPPORT TASK RT STAB LOWER SKIN AREA FOUND CRACK AT STA 138, 70 AND 17 INCHES FROM FRONT SPAR (L/E). CRACK MEASURES 1/2 INCH LONG. REF EA 5510-01843,OP 1. REPAIRED CRACK PER EC/RA 5510--2163 INSTALLED EXTERNAL DOUBLER REPAIRED CRACK PER EC/RA 5510-02163 INSTALLED EXTERNAL DOUBLER WITH SOLID RIVET. ISSUED DIP PER EC/RA 5510 44.0008 FOR PARTIAL WORK ACCOMPLISHED. ISSUED DIP PER EC/RA -02163 PART 2, SRM 55-10-01 REPAIR 2 PAGE 216 STEP 5 TABLE 204. 5510-02163 PART 2, SRM 55-10-01 REPAIR 2 PAGE 216 STEP 5 TABLE 204. PERFORM A DV INSP OF THE RT HORZ STAB LWR SKIN REPAIR AT APPROX SS 138.70 USING THE EXT LOW FREQ EDDY CURRENT (LFEC) METHOD AT THE 56,000 FLT CYC THRESHOLD AND 9,000 FLT CYC INTERV- AL THERE AFTER FROM DATE 3/28/11 PER B737 NDT PART 6 FIG 5. REF B737-800 SRM 55-10-01 REP 11 AND ECRA 5510-02163. DIP C/N 09993.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 24,593 hrs · 8,326 cycles

SUPPORT TASK LT HORIZONTAL STAB LOWER SKIN HAS A CRACK AT STAB STATION 138.70" 16.400" FROM AFT SPAR I/B .70" FROM CENTER OF RIB AND 1.300" IN LENGTH. INSTALLED DOUBLER REPAIR AT LT HORIZONTAL STAB LOWER SKIN AT STATION 138.70" 16.400" FROM AFT SPAR I/B .700 FROM CENTER OF RIB AND 1.300" IN LENGTH IAW EC/RA 5510-02162. SEE NR 5748202 FOR DIP REQUIREMENTS PER EC/RA 5510-02162 PART 2.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 24,593 hrs · 8,326 cycles

SUPPORT TASK LT STAB LOWER SKIN HAS A 1" LONG CRACK LOCATED AT STAB STA 138.70, 9.5" FWD OF AFT EDGE OF PANEL AND 32" AFT OF L/E OF PANEL APPROX. 7" I/B OF RIB. INSTALLED DOUBLER REPAIR AT LT STAB LOWER SKIN STA 138.70, 9.5 "FWD OF AFT EDGE OF PANEL & 32" AFT OF L/E PANEL APPROX .7" I/B OF RIB IAW ECRA 5510-02162 WORK ACCOMLISHED BY M5128FS SEE ATTACHED FORM 44.0008 FOR PARTIAL WORK ACCOMPLISHED ISSUED DIP PER ECRA5510-02162 PART2 SRM 55-10-01 PG 216 STEP 5 REPAIR 11 TABLE 204 ACCOMPLISH AN INITIAL INSPECTION WITHIN 56,000 FLT CYCLES AND REPEAT EVERY 9,000 CYCLES THEREAFTER, REF EC/RA 5510-02162 REV A NOTE. DETAILED VISUAL AND LFEC INSPECTION REQUIRED. DIP CNTL #09992.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,358 hrs · 7,870 cycles

L1 DOOR EMERGENCY LIGHT INOP. R & R L1 DOOR EMERGENCY POWER BATTERY PACK PER MM 33-51-06- 960-805.

Part: LIFE RAFT — UNSERVICEABLE (CABIN) · airframe 21,712 hrs · 7,268 cycles

FORWARD CABIN CEILING LIFE RAFT INFLATION PRESSURE GAUGE AT 2000 PSI, P/N 64356-101 S/N 0196 NSU DEN IPC 25-64-00-45. PLACARD FORWARD CABIN CEILING LIFE RAFT INOP, EXTENDED OVER WATER FLIGHT IS PROHIBITED AND OPERATIONS TO/FROM ALASKA ARE NOT CONDUCTED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 20,735 hrs · 6,923 cycles

FWD ATTENDANT BOX LT EMERGENCY FLASHLIGHT IS DISCHARGED. REMOVED AND REPLACED FWD ATTENDANT BOX LT EMERGENCY FLASHLIGHT REF B737AMM 25-64-00.