N87531

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 46,293 hrs · 16,616 cycles

SEAT ROWS 15ABC THROUGH 21ABC SEAT MOUNTED EMERGENCY LIGHTS INOP SUPPORT TASK NSA EMX NR 00276. SEAT ROWS 15ABC THROUGH 21ABC SEAT MOUNTED EMERGENCY LIGHTS INOP. REMOVED BATTERY PACK IAW AMM 33-51-06. INSTALLED AND OPS CHECKED SERVICABLE BATTERY PACK IAW AMM 33-51-06. OPS

Part: PUMP — LOW PRESSURE (HYD SYS) · airframe 46,270 hrs · 16,608 cycles

HYDRAULIC PUMP A. ENG DRIVEN LOW PRESSURE. REPLACED NR 1 ENGINE DRIVEN PUMP IAW AMM 29-11-11.

Part: LENS — LOOSE (PRESSURE GAUGE) · airframe 46,086 hrs · 16,522 cycles

L1 PRESSURE GAUGE COVER LOOSE. RAFT RESECURED PRESSURE GAUGE LENS COVER.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 45,877 hrs · 16,423 cycles

ROW 26 AISLE SEAT EMERGENCY EXIT LIGHTING INOP. - EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - FOUND HARNESS UNPLUGGED FROM FLOOR TO CHAIR. RECONNECTED HARNESS AND EMERGENCY LIGHTS OPS CHECK GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (ZONE 900) · airframe 45,877 hrs · 16,423 cycles

AFT LAV SMOKE ALARM WENT OFF. 321 LAV. NO SIGNS OF FIRE OR SMOK E PERFORMED AFT LAV SMOKE DETECTOR SELF TEST REF AMM 26-14-00. TEST GOOD AT THIS TIME. NO SIGNS OF SMOKE OR BURNING SMELLS NOTED AT THIS TIME.

Part: LAMP — NO TEST (ZONE 200) · airframe 45,341 hrs · 16,184 cycles

EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - SEAT 12ABC EMERGENCY FLOOR PROXIMITY LIGHTS INOP R/R LAMPS IAW AMM 33-51-11. OPS CK GOOD

Part: SENSOR — FAULTY (FLAP SYS) · airframe 44,908 hrs · 15,994 cycles

REJECTED TAKEOFF SPLIT FLAPS AFTER TAKEOFF ROLL. PERF BITE ON FSEU AND SHOWS FAULT MSG 27-53254. PERF FIM TASK 27-59 TASK 814. TS AND FOUND SKEW SENSOR NO 6 AT FAULT. R/R #6 SKEW SENSOR REFF AMM 27-59-01-000-804 & 400-804. PERF SYS FUNCTIONAL TEST AND OPS CHKS OK. REFF 27-59-00-730-801.

Part: NONE — NONE (NONE) · airframe 42,848 hrs · 15,064 cycles

MULTIPLE BIRD STRIKE ON TAKEOFF APPROX 500FT RIGHT WING AND FUSELAGE 2. ACP BIRDSTRIKE INSPECTION, FOUND BIRD STRIKES ON RH AND LH OB WING LE AND SCIMITAR, NOSE RADOME AND ONE ABOVE FLIGHT DECK WINDOWS, CLEANED SURFACES, NO DAMAGE TO AIRCRAFT STRUCTURE WAS FOUND. OPENED RADOME AND ACP VISUAL INSP OF INTERIOR SURFACE, NO DAMAGE FOUND, CLOSED AND SECURED RADOME. ACP REF TO AMM'S TASK 53-52-00-400-801, AND TASK 05-51-18-210-801.

Part: THRUST REVERSER — UNKNOWN (NR 1) · airframe 42,609 hrs · 14,959 cycles

OPENED THE #1 ENG COWLING AND T/R''S. PERFORMED ASSOSIATED LOTO AMM 78-31-00-440-803-F00. CLOSED ENG #1 COWLING AND T/R''S REF AMM 78-31-00-010-804-F00 AND CORRECTION: UP TO AND INCLUDING STEP 17. C. (7) AMM 71-11-02-410-801-F00. REMOVED LOTO AND ACCOMPLISHED T/R ACTIVATION AFTER GND MAINTENANCE UP TO AND INCLUDING STEP 17. C.(8)THRUST REVERSER NORMAL OPERATION TEST STILL REQUIRED REF ACCOMPLISHED THRUST REVERSER OPERATIONAL CHECK PER AMM78-31-00-700-801-F00. OPS CHKS NORMAL

Part: SKIN — UNKNOWN (STA92/ RIB 4) · airframe 39,408 hrs · 13,629 cycles

(SUPPORT TASK) PREVIOUS REPAIR ON RH HORIZONTAL STABILIZER LOWER SKIN AT STA 92 REMOVED FOR ACCESS TO RIB NO. 4 REPAIRS REF NR 2 9842 5 LBS DOUBLER THICKNESS.090". REMOVED FOR ACCESS TO RIB #4 REPAI AERSALE DOC# 29868 ACCOMPLISED BY TECH # V940623. INITIAL INSP RM 55-10-01-2R-11 TABLE 204 RS IAW B737-800 SRM 55-10-01-2R-11 PAR. 4. DATA TRANSCRIBED FROM AT 56,000 FLT CYC, DVI & LFEC AT 9,000 FLT CYC THEREAFTER PER S REMOVED EXISTENT REPAIR AND ACCOMPLISHED NEW CAT B REPAIR ON R/H HORZ STABILIZER LWR SKIN AT STA 92 TO STA 115 DOUBLER WEIGHT 1.

Part: STIFFENER — CRACKED (STA92.70 #3 RIB) · airframe 39,408 hrs · 13,629 cycles

RH HORIZ STAB HAS A CRACK AT RIB STIFFENER STA 92.70 NO. 3 RIB. REMOVED DAMAGE AND PERFORMED REPAIR ON RH HORIZ STAB AT RIB STIF FENER STA 92.70 # 3 RIB IAW B737-800 SRM 55-10-09-2R-4 PAR 4.

Part: STIFFENER — CRACKED (STA92.70) · airframe 39,408 hrs · 13,629 cycles

RH HORIZ STAB HAS A CRACK AT RIB STIFFENER STA 92.70 # 2 RIB. REMOVED DAMAGE AND PERFORMED REPAIR ON RH HORIZ STAB AT RIB STIF FERNER STA 92.70 # 2 RIB IAW B737-800 SRM 55-10-09-2R-4 PAR 4. D

Part: SKIN — CRACKED (L HORIZ STAB) · airframe 39,408 hrs · 13,629 cycles

SUPPORT TASK - L/H HORIZONTAL STAB LWR SURFACE "C SCAN INSP" REV EALED CRACK INDICATION RIB 147.90 ACCOMPLISHED REPAIR ON L/H HORIZONTAL STAB LOWER SURFACE AT RIB 147.90 IAW BOEING SRM 55-10-01-2R-11 REPAIR 11 PAR 4 FIGURE 204. DATA WAS TRANSCRIBED FROM PAPER DOC AERSALE WO 3875 NR 26435 WO RK ACP BY MECH V940458 INSP BY AQC004

Part: STIFFENER — CRACKED (STA92.70 #4 RIB) · airframe 39,408 hrs · 13,629 cycles

RT STAB HAS A CRACK AT RIB VERT STIFFENER STA 92.70 #4 STIFFENER APPROX 2" FROM BOTTOM. REPAIRED RIB VERT STIFFENER STA 92.70 IAW B737-800 SRM 55-10-09- 2R-4.

Part: RIB — CRACKED (RIB #10) · airframe 39,408 hrs · 13,629 cycles

(SUPPORT TASK) AFTER REMOVAL OF EXISTING REPAIR ON L/H LOWER HOR IZONTAL STABILIZER SKIN, FOUND CRACK ON LOWER CHORD OF RIB #10, 24 INCHES AFT OF L/E AND "2" .098 PILOT HOLES DRILLED THROUGH LO WER CHORD 31.5 INCHES FROM L/E

Part: CREASE BEAM — CORRODED (STA 986) · airframe 39,408 hrs · 13,629 cycles

B737-53-3-0711 MAIN CABIN FLOOR LT CREASE BEAM HAS CORROSION 986 INNER CHORD P/N 147A8540U7 WAS REPLACED ON L/H MAIN CABIN FLOOR STA 986 IAW B737 SRM 51-40-02-0G-0 PARA 4.B.(1) AND 7.A.(1). DAT A WAS TRANSCRIBED FROM PAPER DOC AERSALE WO 3875 NR 29569 WORK A CP BY MECH V940624 INSP BY AQC008

Part: FLOORBEAM — CORRODED (BS 947) · airframe 39,408 hrs · 13,629 cycles

MAIN CABIN FLOORBEAM UPPER SURFACE HAS CORROSION STA 947 LBL 51 PERFORMED REPAIR IN MAIN CABIN FLOORBEAM BS 947 LBL 51 IAW B737-80 0 SRM 53-70-51-2R-5.

Part: CREASE BEAM — CORRODED (STA963-992) · airframe 39,408 hrs · 13,629 cycles

B737-53-3-0711 MAIN CABIN FLOOR RT CREASE BEAM HAS CORROSION STA 963-992 INNER CHORD P/N 147A954OU8 WAS REPLACED ON R/H MAIN CABIN FLOOR STA 963-992 IAW B737 SRM 57-40-02-0G-0 PAR 4.B (1) AND 7.A.(1). DATA WAS TRANSCRIBED FROM PAPER DOC AERSALE WO 3875 NR 29572 WOR K ACP BY MECH V940628 INSP BY AQC009

Part: FLOOR SUPPORT — CORRODED (STA951) · airframe 39,408 hrs · 13,629 cycles

B737-06-3-0049 MAIN CABIN FLOOR UPPER SURFACE HAS CORROSION STA 951 RBL 35 REMOVED AND REPLACED FLOOR SUPPORT AT MAIN CABIN STA 951 RBL 35 P/N 147A5676U6 IAW B737-800 SRM 51-40-02 PAR 7. DATA WAS TRANSCR IBED FROM PAPER DOC AERSALE WO 3875 NR 29633 WORK ACP BY MECH V9 22809 INSP BY AQC004

Part: INTERCOSTAL — DAMAGED (LBL 45) · airframe 39,408 hrs · 13,629 cycles

(B737-06-3-0040) DAMAGED INTERCOSTAL IN MAIN DECK AROUND A NUTPLATE BS 320, LBL 45 REMOVED AND REPLACED INTERCOSTAL IN MAIN DECK BS 320 LBL 45 IAW B737-800 SRM 51-40-02-0G-0 PARA 7D. DATA WAS TRANSCRIBED FROM PA PER DOC AERSALE WO 3875 NR 29620 WORK ACP BY MECH V937321 INSP B Y AQC009

Part: BEAM — CORRODED (STA 986LBL34&43) · airframe 39,408 hrs · 13,629 cycles

B737-53-3-0711 MAIN CABIN FLOOR BEAM UPPER SURFACE HAS CORROSION STA 986 LBL 34 & LBL 43 REPAIRED FLOOR BEAM STA 986 IAW SRM 53-70-51-2R-6 SEE PARTIAL WO RK FOR WORK ACCOMPLISHED. DATA WAS TRANSCRIBED FROM PAPER DOC AE RSALE WO 3875 NR 29571 WORK ACP BY MECH V937322 INSP BY AQC009

Part: PROXIMITY SENSOR — DIRTY (MLG & NLG) · airframe 37,948 hrs · 13,064 cycles

LANDING GEAR, MAIN AND NOSE DOES NOT RETRACT WHEN LANDING GEAR L EVER MOVED TO UP POSITION GEAR HANDLE MOVED FREELY ALL RED AND GREEN LIGHTS ON IN UP AND OFF POSITIONS. CLEANED PROXIMITY SENSORS AND CYCLED GEARS 10 TIMES REF AMM MOMENT. 32-32-00-710-801 NO DEFECTS FOUND, CLEANED AND CHECKED ADJUSTMENT OF MANUAL EXTENSION SYSTEM DOOR SWITCH REF 32-34-00-820-802, OPS CHECK GOOD NO DEFECTS FOUND AT THIS ADD EMP:U355299,U355141,U346475

Part: POWER SUPPLY — INOPERATIVE (M2816) · airframe 37,320 hrs · 12,841 cycles

ALL OF FIRST CLASS SEATS EMERGENCY LIGHT INOP.

Part: SEAL — MISSING (RT WING TE FLAP) · airframe 34,108 hrs · 11,726 cycles

PDA 3 AERODYNAMIC SEAL MISSING ON O/B RIGHT AFT FLAP SEE PHOTO. ADDED PHOTO. ADDED PHOTO. THIS HAS BEEN ADDRESS. SEE L/P 6823743 FOR CORRECTION.

Part: SEAL — MISSING (RH WING TE FLAP) · airframe 33,798 hrs · 11,615 cycles

PDA 3 RIGHT WING OUTBD AFT T/EDGE FLAP AERODYNAMIC SEAL ON LEADING EDGE MISSING/BROKEN JUST OUTBOARD OF #7 FLAP FAIRING -- SEE PHOTO PHOTO ADDED ONLY 1 MISSING -- REQUEST CDL DEFERRAL 57BZ DISPATCH DESK: 83 NAME: PAM DATE: 09-AUG-21- NEEDS SEAL CDL APPLIED EVALUATED RIGHT WING OUTBD AFT T/EDGE FLAP SEAL, NEEDS TO REMOVE FLAP LEADING EDGE PANEL TO FACILITATE REMOVAL AND INSTALLATION OF SEAL. FLAP AND ACCOMPLISH REPAIR. SEE PHOTO. RIVETED ON, WILL NEED MULTIPLE SHIFTS TO REMOVE OUTBOARD AFT RIGHT WING OUTBOARD AFT TRAILING EDGE FLAP AERODYNAMIC SEAL IS

Part: SHUTOFF VALVE — CHAFED (NR 2 ENGINE) · airframe 32,541 hrs · 11,214 cycles

ENG 2 FAILED TO START AFTER 2 ATTEMPTS. FOUND SPAR VALVE CB POPP ED FOUND #2 ENG FUEL SHUTOFF WIRE W1034-1001-20, BETWEEN DISCONNECTS D40034 TO D970, NAC STA 285, WD 28-21-11 DAMAGED DUE TO CHAFFING ON STRUCTURE. PERFORMED SHIELDED WIRE REPAIR PER SWPM 20-10-13 AND ADJUSTED WIRE FOR PROPER SEPERATION FROM STRUCTURE AND SLACK FOR HIGH VIBRATION AREAS PER SPWM 20-10-11, NO FURTHER FAULTS, RETURNED TO SERVICE. SPLICE REPAIR. PERFORMED ENGINE SPAR VALVE TEST REF 28-22-00, WIRE AT NEXT HEAVY MAINT VISIT AND LOG 5933217 FOR ACHIVE OF REF EA2820-02207 REV ORIG. SEE LOG 5933003 FOR DIP TO REPLACE

Part: PANEL — DETACHED (CABIN OVERHEAD) · airframe 31,983 hrs · 11,052 cycles

OVERHEAD PANEL IN 1ST CLASS PARTIALLY CAME DOWN IN FLIGHT. OVERHEAD PANEL IN 1ST CLASS WAS INSTALLED CORRECTLY. OPERATIONS CHECK GOOD.

Part: SKIN — DAMAGED (TE FLAP) · airframe 26,391 hrs · 9,135 cycles

ON WALK AROUND SVC CK. FOUND LT IB FLAP IB OF CANOE DAMAGE TO BOTTOM OF FLAP. SHEETMETAL TO INSP DAMAGE. ACCOMPLISH HFEC INSPECTION OF SKIN DENT PRIOR TO REWORK TO VERIFY NO CRACKS ARE PRESENT REF AVO ESC181014-0531-1 STEP 1. TRIMMED OUT PUNCTURE DAMAGE REF AVO ESC181014-0531-1 STEP 2. PERFORMED HFEC OF DENTED AREA PER AVO ESC181014-0531-1 STEP 1. NO CRACKS NOTED. ALSO VERIFIED CUTOUT OF PUNCTURE PER STEP 2. PERFORMED HFEC OF DENTED AREA PER AVO ESC181014-0531-1 STEP 1. NO CRACKS NOTED. ALSO VERIFIED CUTOUT OF PUNCTURE PER STEP 2. C/W IN MAINT ACTION REF AVO 181014-0531-1 STEP 3 REFORMED DENT TO AERO DYNAMIC CONTOUR. READY FOR STEP 4 HFEC 51-00-00 PROC. 23. FOUND, REF AVO ESC181014-0531-1, STEP 4 AND NDT PART 6 PERFORMED HFEC INSPECTION OF THE SKIN AFTER REWORK, NO CRACKS COMPLIED W STEP 5 OF AVO ESC181014-0531-1 PROVIDED DETAILS AND FINAL DIMENSIONS OF TRIM OUT TO ESC DEPT NS SENT TO ESC. VERIFIED COMPLETION OF STEP 5 OF AVO ESC181014-0531-1. DIMENSION NEED TO VERIFY REPAIR DOUBLER MATERIAL AS 0.090" 2024-T3 CLAD SHEET PER PART 2 STEP 1 OF AVO ESC181014-0531-1A PO 6747496 2 STEP 1 OF AVO ESC181014-0531-1A. PO 6747496. VERIFIED DOUBLER MATERIAL AS 0.090" 2024-T3 CLAD SHEET PER PART FABRICATED REPAIR DOUBLER IAW AVO ESC181014-0531-1A PART2 STEPS 2-4. ALODINED AND PRIMED NEED OK TO INSTALL 1A PART 2. OK TO INSTALL REPAIR DOUBLER. VERIFIED COMPLETION OF STEPS 1 THROUGH 4 OF AVO ESC181014-0531- PERFORMED STEPS 5

Part: LIGHT — INOPERATIVE (ROWS 20-25) · airframe 23,272 hrs · 7,985 cycles

SEAT MOUNTED EMERGENCY LIGHTS INOP FROM ROW 20 TO 25 INOP. REPLACED DAMAGED LIGHT AT SEAT 20. OP-CHECKED OK. AMM 33-51-11-9 60.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,049 hrs · 7,914 cycles

LEFT AFT OVERWING EMERGENCY EXIT EXTERIOR DOOR LIGHT INOPERATIVE. REMOVED AND REPLACE THE LAMP IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: STRINGER — DENTED (BS 445) · airframe 20,933 hrs · 7,120 cycles

STRINGER 2L DENTED AT BS 445. ACCOMPLISHED A REPAIR IAW EC/RA 5310-07109.

Part: SKIN — DENTED (BS 445) · airframe 20,932 hrs · 7,119 cycles

DENTED CROWN SKIN AT BS 445, STRINGER 2L. INSTALLED A SKIN REPAIR IAW SRM 53-00-01, REPAIR 35, AND EC/RA 5310- 07109.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 20,932 hrs · 7,119 cycles

CRACK INDICATED ON LEFT HORIZONAL STAB STA HSS 101.9, 10 INCHES FROM T/E. VERIFI ED THE CRACK WITH EDDY CURRENT. CUT OUT DAMAGED AREA AND INSTALLED A DOUBLER IAW SRM 55-10-01, REPAIR 11.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 20,932 hrs · 7,119 cycles

LEFT HORIZONTAL STAB BEAM CRACKED AT THIRD STIFFENER FROM FWD SPAR LOCATED 33 INCHES FROM FUSELAGE. CUT OUT DAMAGE AND REPAIRED IAW ECRA 5510-02736.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 20,932 hrs · 7,119 cycles

CRACK INDICATED WHILE PERFORMING C-SCAN ON LT HORIZONTAL STAB LOWER I NSPAR SKIN AT 184.70, 10 INCHES FROM T/E. VERIFIED WITH EDDY CURRENT. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR IAW SRM 55-10-0 1 REPAIR 11.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 20,932 hrs · 7,119 cycles

TWO CRACKS INDICATED WHILE PERFORMING C-SCAN ON THE LT HORIZONAL STAB HSS 129.5 APPROXIMATELY 8 AND 14 INCHES FROM THE T/E. VERIFIED THE CRACKS WITH EDDY CURRENT. CUT OUT THE DAMAGED AREAS AND INSTALLED REPAIRS IAW SRM 55-10-0 1 REPAIR 11.

Part: WIRE — SHORTED (CABIN) · airframe 14,368 hrs · 4,869 cycles

ON TAKEOFF ROLL FLIGHT CREW REPORTED STRONG SMELL OF RUBBER IN COCKPIT & CABIN. FLIGHT ATTENDANTS REPORTED A STRONG ELECT SMELL, WOULD COME & GO DURING ALL PHASES OF FLIGHT, BECAME STRONG AGAIN ON DECENT AT 4K THROUGHOUT ACFT. NO SMOKE REPORTED. TRACKED ODOR TO SEAT ROWS 12LT & 20RT. IT APPEARS THAT BOTH LED TRACK LIGHT ARE SHORTED. FOUND LIGHT TRACK AT 12LT WITH 2 BROKEN WIRES. AMM CONDITIONAL INSPECTION PERFORMED. LIGHTS & FILTERS REPLACED.