N36272

Part: UNKNOWN — ODOR (CABIN) · airframe 74,908 hrs · 26,863 cycles

ON TAKE OFF ROLL ABOVE 100KT, SMELLED STRONG OIL ODOR WITH HYD LEVELS WELL BLOW 100% AFT FLAP UP PERFORMED SMOKE/ODOR INSPECTION IAW AMM TASK 05-51-26-800-801-C1 UP TO STEP C SUBSTEPS (2)(E)(4) WITH APU RUNNING. NO ODOR NOTED. CONTINUED AMM TASK 05-51-26-800-801-C1, PERFORMED IDLE RUN OF LT ENG IAW AMM 71-00-00 WITH LT BLEED AND LT PACK, NO ODOR DETECTED. PERFORMED GVI OF LT ENG, NO LEAKS OR DEFECTS NOTED. PERFORMED ENG POWER RUNS IAW AMM 71-00-00. PERFORMED WITH LT & RT ENGINES. LT & RT PACKS SEPARATELY AND THROUGH ALL POWER SETTINGS. NO ODORS NOTED IN COCKPIT OR CABIN.

Part: REGULATOR — FAULTED (NR 2 ENGINE) · airframe 74,868 hrs · 26,839 cycles

CHIME QAR ALERTING RIGHT *DUCT PRESSURE < 29*. RT SIDE HAS BEEN RUNNING 10+ PSI LOWER THAN LT SIDE DURING HIGH N1 (5TH STAGE) OPS FOR A FEW LEGS NOW. PERFORMED ENG BLEED AIR SYS HEALTH CHK ON ENG NR 2 IAW AMM TASK 36-11-00-700-801, & FOUND PC LESS THAN 20 PSIG FROM BAR. PERFORMED REMOVAL & INSTALLATION OF BLEED AIR REGULATOR IAW AMM TASK 36-11-03. OPS TEST REQUIRED. PERFORMED ENG BLEED AIR SYS HEALTH CHK ON ENG NR 1 IAW AMM TASK 36-11-00-700-801. NO FAULTS FOUND. PERFORMED ENG BLEED AIR CROSSOVER OPS TEST ON BOTH ENGS IAW AMM 36-11-00-710-801. BOTH ENG IN PARAMETERS OF OPS TEST.

Part: SKIN — CRACKED (ZONE 100) · airframe 73,252 hrs · 26,105 cycles

EXTERNAL POWER RECEPTACLE SHOW SMALL CRACK AROUND A RIVET ON THE AFT DOUBLER OF THE PERIMETER ABOUT HALF WAY DOWN. ACCOMPLISHED ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER REPAIR IN REF TO EC/RA 5310-08556.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 73,252 hrs · 26,105 cycles

REF EA 5310-08195 REV B OP 004 STEP 26 - CRACK FOUND ON 3RD LOWER FASTENER HOLE AT RT WINDOW FRAME #3 AFTER REAM UP TO PRE COLD WORK DIMENSION (0.300"). ACCOMPLISHED CATEGORY B REPAIR AT RH SIDE NR 3 WINDOW FRAME E-F POST AS PER EC/RA 5310-08554 PART 1. PERFORM REPETITIVE INSPECTION REQUIREMENTS (RIR) AS STATED IN PART 2, AND THERE IS NO TERMINATING ACTION FOR THESE REPETITIVE INSPECTION REQUIREMENTS AS STATED ON PART 3 OF AFOREMENTIONED EC/RA. INITIATE NEW DIP LOG PAGES TO READ SAME AS EC/RA PART 1 PARAGRAPH 2 AND PART 1 PARGRAPH 3.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 73,251 hrs · 26,104 cycles

FOR SDR TRACKING PURPOSES. REF EA 5310-08195 OP 003 LH SIDE NO. 3 WINDOW FRAME POST PERMANENT REPAIR. (REF AAR N/R 9960183) REFERENCE EA 5310-08195 REV B OP 003 SEQ#1205. PERMANENT REPAIR ACCOMPLISHED AS PER ROUTINE CARD SEQ NO. 1205 (EA 5310-08195 REV B - OPERATION 003 - 737NG -LH SIDE NUMBER 3 WINDOW FRAME POST - PERMANENT REPAIR.

Part: SKIN — CRACKED (ZONE 300) · airframe 73,251 hrs · 26,104 cycles

CRACK FOUND AT LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB. STA 157.10, 32" FROM FRONT SPAR , I/B ROW.CRACK LENGTH : 0.406". INSTALLED, INSPECTED, AND SUBMITTED SSFR. NO CRACK NOTED DURING C-SCAN INSPECTION. REMOVED AND REPLACED PER SRM 55-10-01-2R-11 REPAIR ESFR.

Part: COVER — BROKEN (ZONE 200) · airframe 72,529 hrs · 25,770 cycles

EXIT ROW COVER MISSING AT 21DEF NEEDS RETAINER AND HARDWARE FOR COVER STUD. REF IPC 52-22-51-28 NEW COVER IS LOCATED ON SEAT BOTTOM OF SEAT 21F. EXIT HANDLE AND OUTER COVER HAS BEEN DISASSEMBLED TO GAIN ACCESS FLAGGED AS SDR ITEM 430 (00-0593-3-1637). TO INNER COVER RETAINERS. ALL PARTS ARE BAGGED INLUDING NEW INNER COVER AND LOCATED ON SEAT BOTTOM OF SEAT 21A.

Part: RETAINER — DAMAGED (ZONE 200) · airframe 72,529 hrs · 25,770 cycles

EXIT ROW COVER LOOSE AT 21ABC NEEDS COVER ASSY RETAINER HARDWARE REF IPC 52-22-51-28 DETAIL N FLAGGED AS SDR. ON SHEET 7 ITEM (-430) PLUS HARDWARE.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 72,452 hrs · 25,731 cycles

EMERGENCY LIGHTS ON SEAT ROWS 7-14 ABC DO NOT COME ON. SUPPORT TASK NSA EMX NR 00158 REMOVED THE BATTERY FROM BATTERY CHARGER AND INSTALLED SERVICEABLE BATTERY PACK IAW B737 AMM 33-51-06-360-805. OPERATION CHECK GOOD IAW B737-800 AMM 33-51-00-720-801. DATA WAS TRANSCRIBED FROM NSA EMX NR 00158, WORK ACCOMPLISHED BY V936328

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 72,452 hrs · 25,731 cycles

VARIOUS EMERGENCY LIGHTS OUT (NOT ON) THROUGHOUT THE CABIN SUPPORT TASK NSA EMX NR 00157 EMERGENCY LIGHT BATTERY M02267 FAILED TO CHARGE/BATTERY PACK REPLACED

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 72,452 hrs · 25,731 cycles

-F.S. 540 L/H I/B SEAT TRACK HAS WEAR DAMAGE MARKED W/TAPE. SUPPORT TASK NSA EMX N/R 00101

Part: FITTING — CRACKED (STA540 LBL15.04) · airframe 69,603 hrs · 24,424 cycles

B737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRACKED SUPPORT TASK NSA EMX N/R 00071 REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 15.04 N/R 5429168, , AND INSPECTED IAW SRM 51-40-02 AND BACDWG 111A2000 REV ORIGINAL.

Part: FITTING — CRACKED (STA540 LBL6.14) · airframe 69,603 hrs · 24,424 cycles

B737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRACKED SUPPORT TASK NSA EMX NR 00070 REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 6.14 INSPECTED IAW SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL

Part: FITTING — CRACKED (STA540 LBL32.40) · airframe 69,603 hrs · 24,424 cycles

B737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 32.40 IS CRACKED SUPPORT TASK NSA EMX N/R 00072 REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 32.40 N/R 5429202, AND INSPECTED IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL.

Part: FITTING — CRACKED (STA540 LBL6.14) · airframe 69,603 hrs · 24,424 cycles

B737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 6.14 IS CRACKED SUPPORT TASK NSA EMX NR 00069 REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 6.14 N/R 5429161, IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIG.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 69,400 hrs · 24,324 cycles

BLEED TRIP OFF LIGHT COMES ON DURING TAKEOFF LIGHT NO. 1 BLEED TRIP OFF DURING T/O. HAPPENED TWICE AT HIGH N1 ABOVE 90 PERCENT. CREW REPORTS BOTH ENGINE BLEEDS WERE CLOSED FOR HOT TAKEOFF -APU BLEED WAS ON ONLY. #1 ENGINE BLEED PRSOV LOCKED CLOSED IN REFERENCE TO MEL 3605A. FOUND PRSOV REF PRESSURE FLEX LINE FROM VALVE TO REGULATOR LEAKING, REF AMM 36-11-00-700-803. ACP HIGH POWER RUN ON ENGINES, BLEED PRESSURES WITHIN LIMITS AND NO BLEED TRIPS.

Part: AOA — OUT OF RANGE (CAPTAIN'S) · airframe 68,928 hrs · 24,109 cycles

PER CREW CAPTAINS SPD LIMIT FLAG AFTER ROTATION, CA AND FO SPEEDS MATCHED ENTIRE FLIGHT SEE IMAGES. FOUND CAPT AOA SENSOR OUT OF RANGE. REPLACED CAPT AOA. OPS TEST GOOD USING ALTERNATE METHOD. REF AMM 34-21-08 AND 34-21-05-730-801. PARTS USED: 29-3412-9-0001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1749122 SN OFF 5545 SENSOR, ANGLE O OFF 29-3412-9-0001 5545 ON 29-3412-9-0001 8772

Part: AOA — OUT OF RANGE (CAPTAIN'S) · airframe 68,928 hrs · 24,109 cycles

PER CREW CAPTAINS SPD LIMIT FLAG AFTER ROTATION, CA AND FO SPEEDS MATCHED ENTIRE FLIGHT SEE IMAGES. FOUND CAPT AOA SENSOR OUT OF RANGE. REPLACED CAPT AOA. OPS TEST GOOD USING ALTERNATE METHOD. REF AMM 34-21-08 AND 34-21-05-730-801. PARTS USED: 29-3412-9-0001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1749122 SN OFF 5545 SENSOR, ANGLE O OFF 29-3412-9-0001 5545 ON 29-3412-9-0001 8772

Part: LEVER — WARNING LIGHT (GEAR) · airframe 68,915 hrs · 24,103 cycles

UNSAFE GEAR INDICATION DURING GEAR EXTENSION FOLLOWED GEAR DISAG REE QRH. ISSUE RESOLVED NO FAULTS ON PSEU BITE, GEAR LEVER FORCE WITHIN LIMITS PER TASK 32-30 TASK 816. CLEANED GEAR LEVER PRECAUTIONARY. CAN NOT DUPLICATE. ADD FAULT:32

Part: SENSOR — NONE (LE FLAP) · airframe 67,927 hrs · 23,655 cycles

LE FLAP TRANSIT LIGHT ILLUMINATED OVERHEAD SLAT 1 LIGHT OFF REQUEST MEL 2704K.#1 SLAT INDICATION PROBLEM. LEADING EDGE FLAP INDICATIONS NORMAL, APPLYING MEL 2704K FOR #1 TRUE. WOULD BITE CHECK FSEU TO CONFIRM FULL EXTEND/RETRACT COMPARE RESISTANCE VALUES WITH #8 SLAT S1009. REPLACE FAULTY SLAT TRANSIT LIGHT INDICATION INOP.DDP C/W. SENSOR S994 #1 L.E. SLAT FAULT. ALSO REF WDM 27-81-12/22 AND SENSOR. THANKS DISPATCH APPROVED TECH SUPPORT UPDATE, THIS EVENT DID LOG A "DFD 271" REPORT SHOWED FULL EXTEND SENSOR TO BE "FALSE" WHEN SHOULD HAVE BEEN PC# 9107292 REF AMM 27-81-00-480-801 LEADING EDGE FLAP AND SLAT LOCKS NEED LOCKOUT TOOL TO PERFORM MAINTENANCE. REF AMM FSEU BITE FAULT HISTORY LEG 0 FAULT CODES 27-81200 AND 27-81223 INSTALLATION PC# 9107292 27-81-00-480-801 LEADING EDGE FLAP AND SLAT LOCKS INSTALLATION COLLARED CCB PER MEL 2704K OK TO CONTINUE STATION DOES NOT HAVE TOOLING.. NEED LOCKOUT TOOL TO PERFORM MAINTENANCE. REF AMM 27-81-00-480-801 LEADING EDGE FLAP AND SLAT LOCKS INSTALLATION. PERFORMED T/S IAW FIM 27-88 TASK 811 &AMP; AWD 27-81-12, FOUND LE SL EL, P2. PUSHED (CLOSE) THE STALL WARNING ASYMMETRY MODE CIRCUIT AT 1 INBOARD SENSOR S995 DEFECTIVE, REMOVED AND REPLACED SENSOR BREAKER ON THE P18-2 PANEL. REF. MEL 2704K. OPS CHECK NORMAL. PL S995 REF. AMM 27-81-11, REINSTALLED THE BULBS AT THE ASSOCIATED ACARDS REMOVED. FORWARD POSITION INDICATOR LIGHT(S) ON THE CENTER INSTRUMENT PAN

Part: SKIN — DAMAGED (STR 15R-18R) · airframe 66,411 hrs · 22,972 cycles

NO DOCUMENTS FOUND DURING THE AAI RECORD REVIEW AND INSPECTION FOR THE FUSELAGE EXTERNAL REPAIR DOUBLER AT APROX STATION 1060, STR 15R-18R, CUSTOMER REQUEST (UAL QC) (REF AAR NR 99940419) COMPLIED WITH EA NO. 22195, REV P2 AND EC/RA 5331-C2929 (WORK AC COMPLISHED BY V935492 AND V918069)

Part: DOUBLER — NONE (STATION 1060) · airframe 66,411 hrs · 22,972 cycles

NO DOCUMENTS FOUND DURING THE AAI RECORD REVIEW AND INSPECTION FOR THE FUSELAGE EXTERNAL REPAIR DOUBLER AT APROX STATION 1060, S TR 15R-18R, CUSTOMER REQUEST (UAL QC) (REF AAR NR 99940419) COMPLIED WITH EA NO. 22195, REV P2 AND EC/RA 5331-C2929 (WORK AC COMPLISHED BY V935492 AND V918069)

Part: BATTERY PACK — INOPERATIVE (M1694/M1695/M167) · airframe 66,411 hrs · 22,972 cycles

BATTERY PACKS M1673, M1694 AND M1695 INOP (REF. AAR NR 99937908) .

Part: PRESSURE WEB — CRACKED (CENTER WING FWD) · airframe 66,411 hrs · 22,972 cycles

CENTER WING FWD L/H SIDE VERTICAL PRESSURE WEB CRACK. (REF AAR RFD NR 99938172). BY AAR RFD TECH V920656 AND AAR QC A-69 V895387. REPAIRED CRACK ON L/H CENTER WING VERTICAL PRESSURE WEB IAW B737 SRM 57-10-10-2R-3 ALT 2 THIS IS A CATAGORY B REPAIR, REINSPECT REQUIREMENT THRESHOLD 56,000 FLIGHT CYCLES AFTER REPAIR INSTALL REPEAT INSPECTION AT 36,000 FLIGHT CYCLES. WORK ACCOMPLISHED REQUIREMENT INITIAL THRESHOLD PER TABLE 205 IS 56,000 FLIGHT CYCLES. WORK ACCOMPLISHED BY AAR RFD TECH V920656 AND INSPECTOT CYCLES AFTER REPAIR INSTALL. REPEAT INSPECTION AT 36,000 FLIGHT V895387 ON NR 99938172. REPAIRED CRACK ON L/H CENTER WING VERTICAL PRESSURE WEB IAW B737 SRM 57-10-10-2R-3 ALT 2 THIS IS A CATAGORY B REPAIR, REINSPECT ADD EMP:V920656 V895387 TOMC APPROVED TO PERFORM AN HFEC AND LFEC INSPECTION WITH AN TOMC-APPROVAL FROM SC1ELBYC COMMENT THRESHOLD OF 56,000 AFTER REPAIR INSTALLATION AND REPEAT INSPECTION AT INTERVALS OF 36000 FLIGHT CYCLES IN REF WITH SRM 57-10-10-2R-3 ALTERNATE 2 CATEGORY B REPAIR FIGURE 205 Q/C REVIEWED. QC REVIEWED RECORDS UPDATE QC REVIEWED INIT: 56,000 FC HFEC AND LFECAFTER REPAIR INSTALL INIT(-5357) WILL AUTO ITO TO RIR(-5358) RIR: INTERVALS OF 36,000 FC......LN/U253409

Part: SPAR — CRACKED (RH WING) · airframe 66,411 hrs · 22,972 cycles

REF LPS 3909955, 3910260, AND 3906367, 3 TEMPORARY REPAIRS ON THE WCS REAR SPAR ASSEMBLY VERTICAL PRESSURE WEB REQUIRE REPLACEMENT BETWEEN RBL 27 AND RBL 43. PERMANENT REPAIR IAW SRM 57-10-10-2R-3 ALTERNATIVE 3. THIS IS A LFEC INSPECTION PER TABLE 206 DUE IN 56000 CYCLES, WITH A REPEAT CAT B REPAIR THAT REQUIRES INSPECTIONS WITH THE INITIAL HFEC AND INSPECTION INTERVAL OF 36000 CYCLES. REF AAR NR 99940354, REMOVED 3 TEMPORARY CRACK REPAIRS ON RH WING CENTER SECTION VERTICAL PRESSURE WEB AND REPLACED WITH A ADD EMP:V918170 AND V 895387 CATAGORY B ALT 3 REPAIR MADE TO WING CENTER SECTION REAR SPAR TOMC-APPROVAL FROM SC1ELBYC COMMENT VERTICAL PRESSURE DECK WEB RBL 27 AND RBL 43 PER SRM 57-10-10-2R-3. PERFORM ALT 3 HFEC AND LFEC INSPECTIONS PER TABLE 206 INITIAL THRESHOLD 56000 FLIGHT CYCLES AFTER REPAIR INSTALLATION AND REEAT HFEC AND LFEC INSPECTION INTERVALS OF 36000 FLIGHT CYCLES. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT &AMP; UPDATE. QC QC REVIEWED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,214 hrs · 20,037 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RE-LAMPED LIGHT REF MM 33-54-01. OPS CK OK.

Part: PUMP — LOW PRESSURE (NR 2 ENGINE) · airframe 57,349 hrs · 19,317 cycles

ENG 2 LOW PRESSURE LIGHT LIGHT ON NUMBER 2 ENGINE HYD LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT REMOVED NR 2 ENGINE DRIVEN PUMP IAW AMM29-11-11-000-801-001 UP TO STEP 10 INSTALLED EDP PER AMM 29-11-11-400-801-001 STEPS A1 THRU F7 ACCP EDP INST TEST FROM STEP G, REF AMM 29-11-11-801-001,EDP LEA K AND OPS CK GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT 1936048 SN OFF 3123 PUMP, HYD ENG D OFF 29-2910-9-0003 3123 ON 29-2910-9-0003 3780.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 53,467 hrs · 17,776 cycles

SMALL EMERGENCY SIGN AT ROW 21A MISSING. INSTALLED A NEW LENS.

Part: LENS — BROKEN (CABIN) · airframe 51,949 hrs · 17,153 cycles

ROW 28ABC EMERGENCY EXIT PATH LIGHT LENS BROKEN. REPLACED LENS COVER

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,943 hrs · 17,150 cycles

EMERGENCY EXIT LIGHT INOPERATIVE. OVERHEAD BIN BULLNOSE BETWEEN ROWS 3EF AND 4EF. REPLACED THE LAMPS. OPS CHECKED GOOD.

Part: HEATER — UNSERVICEABLE (CABIN) · airframe 47,758 hrs · 15,557 cycles

FLIGHT ATTENDANT REPORTED BURNING RUBBER SMELL & HOT FLOOR IN AFT CABIN. COFFEE POTS WERE HOT. PERFORMED TASK 05-51-26-800-801C1 STEP 1 C D THROUGH H & STEP 2A & B. CHECKED AFT DOOR AREA HEATER OPERATIONS CHECKED IAW TASK 21-45-00700- 802, NO HEAT. FOUND HEATER CLOGGED & MISSING INSULATION ON WIRING. REPLACED IAW TASK 21-45-01-400-801. OPERATIONS CHECKED GOOD.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 47,670 hrs · 15,522 cycles

ON TAXI OUT PRESSURIZATION AUTO FAIL LIGHT & ALT LIGHT ILLUMINATED, GATE RETURN. TROUBLE SHOT & FOUND CONTROLLER INOPERATIVE. R & R CONTROLLER IAW MM 21-31-01-401. OPERATIONS CHECKED GOOD AT THIS TIME. WIRING CHECKS DONE ON NR 4922229.

Part: PUMP — LEAKING (NR 2 ENGINE) · airframe 47,476 hrs · 15,444 cycles

EXTEND FLAPS ON APPROACH, FLAPS STOPPED AT HALFWAY TO POSITION 1 & WOULD NOT MOVE UP OR DOWN. LE TRANSIT LIGHT ON, ALTERNATE EXTEND TO POSITION 15, NORMAL NO ASYMMETRY ENCOUNTERED. TROUBLE SHOT E FLAPS IAW FIM 27-51-00-810-836, FOUND B HYD EDP LEAKING & QTY AT REFILL. REPLACED NR 2 ENG EDP ON 4910058, BITE CHECK OF FSEU MSG 27-53280. ON INSPECTION OF XMISSION FOUND NR 1 & 8 TRIPPED, RESET TRIP INDICATOR & FLAP SYS ALL CHECKED NORMAL OPERATION IAW FIM 27-51- 00-810-849 & 27-51-00-710-801.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,612 hrs · 14,786 cycles

SUPPORT TASK G7 FWD PATH LIGHT INOPERATIVE. R & R FWD PATH LIGHT ASSEMBLY IAW AMM 33-51-0 0. OPERATIONS CHECKED GOOD. PN S479W230-7, STATION 365.55, SN NONE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,612 hrs · 14,786 cycles

SUPPORT TASK FWD ENTRY EMER LIGHTS INOPERATIVE. R & R FWD ENTRY EMER BATTERY PACK IAW AMM 33-51-00. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,612 hrs · 14,786 cycles

AFT CABIN AFT LT EMER LIGHTS INOPERATIVE. R & R AFT CABIN EMER EXIT LIGHT BATTERY PACK AT STATION 952, PN AD-D717-01-100 IAW AMM 33-51-06. OPERATIONS CHECKED GOOD IAW AMM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,612 hrs · 14,786 cycles

SUPPORT TASK G7 AFT PATH LIGHT INOPERATIVE. R & R AFT PATH LIGHT ASSEMBLY IAW AMM 33-51-0 0. OPERATIONS CHECKED GOOD. PN S479W230-7 STATION 365.5 5 SN NONE.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 45,612 hrs · 14,786 cycles

DEFECT NOTED WHILE PERFORMING HFEC INSPECTION OF FASTENER HOLE AT STATION 727B, RBL 45.50 OTBD FLANGE AFT HOLE. RECEIVED ECRA 5320-02418 REV ORIGINAL FOR REPAIR OF FASTENER HOLE AT 727B, RBL45.50 OTBD FLANGE AFT HOLE. ALL WORK ACCOMPLISHED IAW ECRA 5320-02418 REV ORIGINAL STEPS 1 - 13.

Part: TRANSMITTER — FAILED (TE FLAP) · airframe 44,328 hrs · 14,340 cycles

ON FINAL FLAPS STOPPED WORKING 0+1 DEGREE FLAPS. ACCOMPLISHED CHECKLIST. R & R FLAT POSITION TRANSMITTER RT IAW AMM 27-5 8-01-000-801 & 27-58-01-400-801. PERFORMED LAND VERIFY AMM 22-11- 00-700-801. ALL TESTS PASSED. IAW 7729885 FOR AUTO THROTTLES NO AUTO LAND. ROTABLE PARTS CHANGE WAS INDICATED TT 1642728 SN OFF 01972 TRANSMITTER, FL OFF 29-2759-9-0001 1972 ON 29-2759-9-0001 1727.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 41,219 hrs · 13,246 cycles

LT HORIZONTAL STAB LOWER SKIN AREA STATION 138.70 & ABOUT 10 INCHES FROM REAR SPAR, CRACK INDICATION NOTED WITH C SCAN. CRACK SIZE IS ABOUT 1/2 INCH LONG IAW EA 5510-01843 REV C OP 1 LT HORIZONTAL STAB LOWER SKIN AT STATION 138.70 HAS BEEN REPAIRED IAW SRM 55-10-01 REPAIR 11.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 33,805 hrs · 10,598 cycles

PER EA 5510-01843, PERFORMED C-SCAN INSPECTION ON LT HORIZONTAL STAB, FOUND CRACK INDICATION AT STA 129.5 17" AFT OF FRONT SPAR 1.0" LONG. CORRECTED TO READ AIRCRAFT 272 REPAIRED LT LOUVER HORIZONTAL STAB PER ECRA 5510-02181.

Part: FAN — FAILED (CABIN) · airframe 33,649 hrs · 10,541 cycles

FA'S REPORTED STRONG SMELL OF ELECTRICAL SMOKE ENTIRE AIRCRAFT AND SLIGHT FOG BY DIVIDER. TURNED ON STERIL LIGHT, BUSS TRANSFE R OFF GALLEY SWITCH OFF AND RECIRC FAN OFF. SMOKE AND FUMES DISSIPATED. T/S AS PER AMM 21-00-00-810-806 AND 05-21-26-200-801C2. FOUND RT RECIRC FAN BEARING FAILURE REF N/R 4271579. CHECKED WIRING IN COCKPIT AND CABIN, CHECKED GOOD. R&AMP;R OVERHEAD PANELS AND LAV SHROUDS. ALL CHECKED GOOD. AIRCRAFT IS OK TO CONTINUE.

Part: POWER SUPPLY — INOPERATIVE (EMERENCY LIGHTS) · airframe 30,010 hrs · 9,298 cycles

FOUND BOTH FWD AND AFT OVERWING HATCH EMERGENCY EXIT LIGHTS ON RIGHT SIDE INOP. REMOVED AND REPLACED POWER SUPPLY FOR RT OVERWING HATCHES EMERGENCY LIGHTS IAW AMM 33-51-06. ALSO REPLACED BATTERY PACK FOR POWER SUPPLY. OPS CHECK GOOD, OK TO CONTINUE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,521 hrs · 8,720 cycles

ROW 25 ABC OVERHEAD EMERGENCY PATH LIGHT INOPERATIVE. RELAMPED, ALL OPS NORMAL AT THIS TIME.

Part: SKIN — CORRODED (FUSELAGE) · airframe 27,003 hrs · 8,178 cycles

CORROSION AT BS 355 BL 0 REF ECRA 5331-01451 PART 2 INTERIM REPAIR REQ'S INSPECTION ON ANTENNA DOUBLER ISSUED DIP TO ACCOMPLISH AN INITIAL INSP PRIOR TO 50,000 TOTAL A/C CYCLES AND THEN REPEAT INSP'S AT INTERVALS NOT TO EXCEED 4,000 CYCLES PER PART 2 OF ECRA 5331-01451PART 1 INTERIM C/W PER ECRA 5331-01451 ORIG, PART 1 STEP 12, ACCOMPLISH AN INITIAL INSPECTION PRIOR TO 50,000 TOTAL AIRCRAFT CYCLES AND THEN REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 4,000 CYCLES PER PART 2 OF ECRA 5331-01451. 1) INIT: W/I 50000 TOTAL A/C F/C. INIT WILL AUTO-ITO TO 2) RIR: EVERY 4000 F/C THEREAFTER (M&AMP;E 58-9953-8-1471)-ODEE.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 22,936 hrs · 6,916 cycles

AFT MEGAPHONE SIREN INOP. REMOVED AND REPLACED AFT MEGAPHONE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,874 hrs · 5,649 cycles

EMERGENCY PATH LIGHTING INOP AT SEAT 8C. REPAIRED IAW AMM 33-51-01.

Part: FAN — ODOR (CABIN) · airframe 10,459 hrs · 2,982 cycles

HEAVY BURNING SMELL IN AFT CABIN AREA. STARTED QRH FOR AIR CONDITIONING/ SMOKE FUMES. SMELL DISSIPATED. REPLACED RT RECIRCULATION FAN PER AMM 21-25-02.