N69824

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 37,411 hrs · 13,713 cycles

FOUND EMERGENCY PATHWAY LIGHTS INOPERATIVE, ROWS 14 & 26. REMOVED AND REPLACED EMERGENCY PATHWAY LIGHTS AT SEAT 26 AND 14 IAW CMM 25-23-55, OPS CHECKED GOOD.

Part: STRUCTURE — DAMAGED (RT NR 7 SLAT) · airframe 37,411 hrs · 13,713 cycles

BIRD STRIKE ON RIGHT SIDE OF AIRCRAFT ALT-1000. 190KTS. PERFORMED BIRD STRIKE INSPECTION IAW AMM 05-51-18, FOUND DAMAGE TO NR 7 LEADING EDGE SLAT. INSPECTED ALL ATTACHMENT POINTS AND HARDWARE FOR SLAT NR 7, NO DEFECTS NOTED. INSTALLED NR 7 LEADING EDGE SLAT IAW AMM 27-81-21-400-801. COMPLETED UP TO AND INCLUDING STEP 3 H(9)(F). CONTINUE FROM STEP 3 H(10) TO COMPLETION.

Part: UNKNOWN — ODOR (CABIN) · airframe 36,836 hrs · 13,465 cycles

SMOKE IN CABIN DURING TAKEOFF. REJECTED TO. SMOKE CEASED AND DIS SI PATED. REJECT AT 50 KTS CAPT STATED APU WAS OFF, RT AND LT PACK TURNED OFF PER A CHECKLIST. LT PACK WAS THEN TURNED BACK ON AND A SMALL AMOUNT OF SMOKE WAS EMITTED. LT PACK TURN OFF. F/O STATED HE THOUGHT IT WAS A SMOKE SMELL AND CAPT STATED A SLIGHT HINT OF ELECTRICAL IN HIS OPINION. PERFORMED 10 MINUTE HIGH POWER RUN WITH ENGINE BLEEDS ON AND BOTH PACKS ON HIGH IAW AMM 72-00-00-100-803-F00 AND 05-51-26 NO SMOKE OR ELECTRICAL SMELL THROUGHOUT THE AIRCRACT . NOTICED FOG COMING FROM VENTS ( THIS IS NORMAL WHEN COLD AIR IS MIXED WITH A WARM AIRCRAFT)

Part: SIGN — BROKEN (ZONE 200) · airframe 36,015 hrs · 13,138 cycles

FOR TRACKING PURPOSES, REF NR002685856 "G4 /2LH DOOR AREA EMERGENCY EXIT SIGN BROKEN" REMOVED AND REPLACED LOWER EMERGENCY EXIT SIGN ASSY AT G4/2LH DOOR, REF AMM 33-51-01/201. OPS CHECK NORMAL.

Part: LAVATORY — ODOR (ZONE 900) · airframe 35,663 hrs · 13,011 cycles

FLIGHT ATTDT SAYS FWD LAV SMELLS HORRID. PLZ SERVICE AND DEODERIZE. LAV CLEANED.

Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 35,601 hrs · 12,985 cycles

REF FIM 21-00 TASK 806 MONITOR THE NEXT FEW FLIGHTS FOR ANY RE-OCCURING FLIGHT DECK-CABIN ODORS. SUSPECT PREVIOUS SMELL WAS FROM #1 ENG WATER WASH IN MCO BEFORE THE FLIGHT. CARRIED BY ELB PERFORMED.SMOKE OR FUMES IN THE CABIN, SOURCE UNKNOWN - FAULT ISOLATIONEFERENCE: FIM 21-00 TASK 806. NO RE-OCCURING FLIGHTDECK-CABIN ODORS DETECTED

Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 35,601 hrs · 12,985 cycles

FUME/ODOR IN FLIGHTDECK/ CABIN BELOW 10000 ENGINE BLEED SOURCE ADDING SMOKE/ ODOR FORM. CONFIRMED WITH PLANNING DEPARTMENT THAT ENGINE 1 HAD AN ENGINE W AS AT MCO THE NIGHT BEFORE AND PER FIM 21-00-00-806 A.4 (ODORS I N THE CABIN AFTER AN ENGINE HAS BEEN OVERHAULED OR THE COMPRESSOR HAS BEEN WASHED ARE NOT UNCOMMON AND NOT CONSIDERED A FAULT)AS A PRECAUTION, RAN ENGINE 1 AND 2 SEPARATELY, OPERATED PACKS I NDIVIDUALLY AND TOGETHER. UNABLE TO DUPLICATE FAULT AND NO DISCR EPANCIES NOTED.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 35,286 hrs · 12,866 cycles

SEAT 31C ROW EMERGENCY LIGHT INOP DEFERRING SEAT MOUNTED EMERGENCY LIGHT AT 31C TOMC APPROVED SEAT 31C EMERGENCY EXIT SEAT MOUNTED LIGHT DEFERRED DDP C/W REMOVED AND REPLACED LIGHT ASSY PER CMM 25-23-55. OPS CHECH GOOD.PARTS USED: 29-3326-3-0013, QTY :1

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 35,153 hrs · 12,806 cycles

SEAT 31 ABC EMERGENCY LIGHTS NOT WORKING REMOVED AND REPLACED SEAT 31 ABC LIGHT ASSEMBLY REF AMM 33-51-11 OPS CK PARTS USED: 29-3326-3-0013,QTY :1

Part: STRINGER — DAMAGED (STA 1060 L/H) · airframe 30,470 hrs · 10,963 cycles

(SUPPORT TASK) STR #27 L/H AT STA 1060 L/H HAS DAMAGE IN TAIL CO MPT. (APU COMPT)

Part: STRINGER — DAMAGED (STA 1060 L/H) · airframe 30,470 hrs · 10,963 cycles

(SUPPORT TASK) STR #26 L/H AT STA 1060 L/H HAS DAMAGE IN THE APU TAIL COMPT.

Part: INTERCOSTAL — CRACKED (BS 344 -360) · airframe 30,470 hrs · 10,963 cycles

(B737-53-3-0736) MAIN CABIN FLOOR HAS CRACKED INTERCOSTAL BS 344 -360, LBL 12"

Part: INTERCOSTAL — CRACKED (BS 344 -360) · airframe 30,470 hrs · 10,963 cycles

MAIN CABIN FLOOR HAS CRACKED INTERCOSTAL BS 344 -360, LBL 12" REMOVED AND REPLACED INTERCOSTAL P/N 141A5410U148 ON MAIN CABIN FLOOR AT BS 344-360, LBL 12" PER BOEING SRM 51-40-02-0G-0 PAR 7. DATA WAS TRANSCRIBED FROM PAPER DOC AERSALE WO 3953 NR 33327.

Part: FLOOR SUPPORT — CRACKED (BS 540 BL0) · airframe 30,470 hrs · 10,963 cycles

(B737-53-3-0710) MAIN CABIN FLOOR SUPPORT BS 540 BL0 IS CRACKED

Part: INTERCOSTAL — CRACKED (BS31 2-325) · airframe 30,470 hrs · 10,963 cycles

B737-53-3-0736 MAIN CABIN FLOOR HAS CRACKED INTERCOSTAL AT BS 31 2-325 RBL 32 REMOVED AND INSTALLED INTERCOSTAL FLOOR MAIN CABIN BS 312-328 RB L 32 IAW B737-900 ER SRM 51-40-02-06-0. DATA WAS TRANSCRIBED FRO M PAPER DOC AERSALE 3953 OPS 33275 WORK ACP BY MECH V942859 INSP BY AQC004

Part: FITTING — CORRODED (LAV E) · airframe 30,470 hrs · 10,963 cycles

B737-06-3-0049 CORROSION BY INBOARD LAV E FITTING ON MAIN DECK S TRUCTURE BY BS 947 REPLACED FITTING ON MAIN DECK STRUCTURE AT STA 947 IAW SRM 51-40 -02-0G-0 PARA 7. DATA WAS TRANSRIBED FROM PAPER DOC AERSALE WO 003953 NR 33008 WORK ACP BY MECH V937322 INSP BY AQC004

Part: INTERCOSTAL — CRACKED (BS 31 2-325 RBL) · airframe 30,470 hrs · 10,963 cycles

B737-53-3-0736 MAIN CABIN FLOOR HAS CRACKED INTERCOSTAL AT BS 31 2-325 RBL 32 REMOVED AND INSTALLED INTERCOSTAL FLOOR MAIN CABIN BS 312-328 RB L 32 IAW B737-900 ER SRM 51-40-02-06-0. DATA WAS TRANSCRIBED FRO M PAPER DOC AERSALE 3953 OPS 33275 WORK ACP BY MECH V942859 INSP BY AQC004

Part: FLOOR SUPPORT — CORRODED (LAV D NS 949) · airframe 30,470 hrs · 10,963 cycles

B737-06-3-0049 CORROSION ON MAIN DECK FLOOR STRUCTURE BY INBOARD LAV D FITTING NS 949 REMOVED AND REPLACED NEW FLOOR SUPPORT ON MAIN DECK FLOOR STRUCTURE BY IB LAVATORY D BS 947 IAW B737-900 ER SRM 51-40-02-OG-0 PA RA 7. DATA WAS TRANSCRIBED FROM PAPER DOC AERSALE WO 3953 OPS 3 3012 WORK ACP BY MECH V940623 INSP BY AQC004

Part: FLOOR SUPPORT — CRACKED (CABIN FLOOR) · airframe 30,470 hrs · 10,963 cycles

B737-53-3-0736 MAIN CABIN FLOOR HAS CRACKED INTERCOSTAL BS 344-3 60 BL0 REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN FLOOR AT BS344-36 0 BL0 WITH PN 141A5410U147 PO 10228378 IAW B737-900ER SRM 51-40- 02 PAR 7. DATA WAS TRANSCRIBED FROM AERSALE WO 003953 OPS 33328 WORK ACP BY MECH V922869 INSP BY AQC044

Part: INTERCOSTAL — WORN (STA 336, LBL 46) · airframe 30,470 hrs · 10,963 cycles

(B737-06-3-0288) SURFACE WEAR ON MAIN DECK INTERCOSTAL BS 336, L BL 46 REMOVED AND REPLACED INTERCOSTAL P/N 141A54100142 ON MAIN DECK STA 336, LBL 46 PER BOEING SRM 51-40-02-0G-0 PAR 7. DATA WAS TRAN SCRIBED FROM PAPER DOC AERALE WO 3953 NR 33025 WORK ACP BY MECH V940458 INSP BY AQC044

Part: INTERCOSTAL — CRACKED (BS 312 TO 328) · airframe 30,470 hrs · 10,963 cycles

(B737-06-3-0288) CRACKED INTERCOSTAL AT FASTENER HOLE ON MAIN DECK AT BS 321, LBL 45 INSTALLED NEW INTERCOSTAL SUPPORT ON FLOOR STRUCTURE IN MAIN DECK CABIN BETWEEN BS 312 TO 328, LBL 45 IAW B737-900ER SRM 51-40-0 2-0G-0 PAR 7 C. DATA WAS TRANSCRIBED FROM PAPER DOC AERSALE WO 3 953 NR 33026 WORK ACP BY MECH V940623 INSP BY AQC044

Part: SEAT TRACK — CORRODED (BS500B-500E) · airframe 30,470 hrs · 10,963 cycles

(B737-06-3-0288) SEAT TRACK AT LBL44 CORROSIOIN DAMAGE FROM BS 500B-500E REMOVED AND REPLACED NEW SEAT TRACK ON BS 480 TO 520 IAW B737-90 0ER SRM 51-40-02-0G-0 PAR 4.B. AND PAR 7.A. DATA WAS TRANSCRIBED FROM PAPER DOC AERSALE WO 3953 NR 33036 WORK ACP BY MECH V94062 3 INSP BY AQC003

Part: INTERCOSTAL — CORRODED (MAIN DECK FLOOR) · airframe 30,470 hrs · 10,963 cycles

(B737-06-3-0049) CORROSION ON MAIN DECK FLOOR STRUCTURE TOP SURF ACE RBL 48, BS 958 REMOVED AND INSTALLED NEW INTERCOSTAL FLOOR STRUCTURE RBL48 BS 9 58 IAW B737-700ER SRM 51-40-02-0G-0 7.A. DATA WAS TRANSCRIBED FR OM PAPER DOC AERSALE WO 3953 NR 33007 WORK ACP BY MECH V934896 I NSP BY AQC056

Part: BEAM — CORRODED (BS 986, LBL 44) · airframe 30,470 hrs · 10,963 cycles

(B737-53-3-0711) CORROSION ON MAIN DECK FLOOR BEAM UPPER CHORD A ROUND FASTENER HOLE BS 986, LBL 44

Part: CONTROL PANEL — SMOKE (COCKPIT) · airframe 22,605 hrs · 8,118 cycles

DROPPED IPAD ON CTR CONSOLE NEAR TRANSPONDER BRIEF SMOKE FROM PANEL SEVERAL LIGHTS NOW INOPERABLE. REMOVED AND REPLACED ATC CONTROL PANEL, REF M/M 34-45-00. OPERATIONS CHECKED AND ALL LIGHTS NORMAL ROTABLE PARTS CHANGE WAS INDICATED-TT NR 1011949 S/N OFF 5940 PANEL, ATC CONT OFF 29-3445-9-0004 5940 ON 29-3445-9-0004 1480.

Part: CHECK VALVE — FAILED (CABIN PRESSURE) · airframe 22,048 hrs · 7,918 cycles

A/C WILL NOT PRESSURIZE IN AUTO/MANUAL. REMOVED CHECK VALVE, REF MM 21-21-01-000-804-002, PARTS AND HARWARE IN AREA. ADD EMP:U353062 PARTS RECEIVED. TETR 1930. REPLACED CHECK VALVE, PER AMM 21-21-01-000-804-002-2. OPS CHECKS GOOD WITH NO LEAKS NOTED.

Part: VORTEX GEN — MISSING (VERTICAL STAB) · airframe 20,795 hrs · 7,440 cycles

PDA 2 1EA AFT BODY VORTEX GENERATOR MISSING ON RIGHT SIDE OF VERTICAL STAB. ONLY 1 MISSING ON RIGHT SIDE - ALL OTHERS ARE PRESENT - REQUEST CDL TOMC APPROVES CDL 55J CDL APPLIED. REF IPC 53-31-21-01 AND AMM 53-21-21

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 19,483 hrs · 6,933 cycles

EMERGENCY FLOOR PROXIMITY LIGHTS ON ALL FIRST CLASS SEATS DO NOT COME ON DURING TEST. REPLACED BATTERY AND CHARGER AND FUSES. NO HELP. NEED MORE TROUBLESHOOTING. REF SSM 33-51-12. REPAIRED SHORT FOUND IN TRAY TABLE AREA OF SEAT 5B, REF ESPM 20-52-22. OPERATIONAL CHECK OF EE LIGHT TEST PASSED. OPS CHECKS NORMAL AFTER REPAIR AT 5B.

Part: WIRE — CHAFED (LIGHT PANEL) · airframe 19,360 hrs · 6,889 cycles

FOUND WIRES RUBBING ON MO 1675 EMERGENCY POWER SUPPLY IN CEILING ABOVE LIGHT PANEL BETWEEN DOOR L1 AND R1. MARKED WITH BLUE TYE WRAP. W4142-0042-20 WIRE REPAIRED BY REPLACING SPLICE SM1 REF WDM 33-51-11 AND SWPM 20-10-13. EMERGENCY LIGHTS TESTS NORMAL REF AMM 33-51-06.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 12,678 hrs · 4,452 cycles

LENS MISSING OUTSIDE OF DOOR TO LAV D. REPLACED EMERGENCY LIGHT LENS IAW IFM 25-40-03. OPS CHECKED GOOD.

Part: LATCH — BINDING (R1 DOOR GIRT BAR) · airframe 12,638 hrs · 4,438 cycles

GIRT BAR ON DOOR 1R HARD TO ARM REMOVED DEBRIS FROM FLOOR MOUNTED ESCAPE SLIDE BRACKETS OPS CHK NORMALLY REF AMM 25-66-02.

Part: LENS — BROKEN (CABIN) · airframe 11,351 hrs · 3,984 cycles

EMERGENCY AISLE LIGHT BROKEN AT SEAT 8-C. PUSHED INTO HOUSING. REPLACED LENS AT SEAT 8C, OPS CHECKS GOOD REF AMM33-51-14.

Part: SLIDE — LOOSE (1L DOOR) · airframe 9,350 hrs · 3,262 cycles

FWD ENTRY DOOR DIFFICULT TO PLACE IN ARM POSITION. REMOVED & REPACKED L-1 DOOR ESCAPE SLIDE PACK REF AMM 25-66-01.