N16617

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,484 hrs · 22,426 cycles

CRACKED FRAME AT STA 360 BETWEEN STR 8 LT AND 9 LT REPAIRED FRAME PER ECRA 5311-01481 NEED TO REINSPECT BEFORE THE ACCUMULATION OF 82426 TOTAL A/C FLT CYCLES AND AT INTERVALS NOT TO EXCEED 3000 FLIGHT CYCLES THEREAFTER PER PART 2 OF ECRA 5311-01481 INSPECT BEFORE THE ACCUMULATION OF 82426 TOTAL A/C FLIGHT CYCLES AND AT INTERVALS NOT TO EXCEED 3000 FLT CYCLES THEREAFTER PER PART 2 OF ECRA 5311-01481. 1) INIT: W/I 82426 TOTAL A/C F/C INIT WILL AUTO-ITO TO 2) RIR: EVERY 3000 F/C THEREAFTER (M&E 24-9953-8-1447).

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 42,484 hrs · 22,426 cycles

SUPPORT TASK - FWD CARGO DOOR CUTOUT AFT FRAME WEB IS CRACKED AT DOOR LOWER STOP PAD, UPPER I/B CORNER, MARKED. REMOVED & REPLACED FRAME WEB, REF SRM 51-40-02, BOEING DOC 65-20723.

Part: TRANS PANEL — CORRODED (CARGO BAY) · airframe 42,484 hrs · 22,426 cycles

FWD CARGO COMPARTMENT RT TRANSITION PANEL BETWEEN STA 460-520 HAS SURFACE CORROSION. REMOVED CORROSION WITHIN LIMIT FROM STA 460 TO 480, TREATED AND PRIMED REF SRM 53-30-53. REMOVED AND REPLACED TRANSITION PNL FROM STA 460 TO STA 520 REF SRM 51-40-02.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 42,484 hrs · 22,426 cycles

BELTFRAME STA 867 BETWEEN STRINGER S8R-S9R HAS CRACKED AT FASTENER AREA. REPAIRED FRAME PER EA 5310-04498 OP2.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 42,484 hrs · 22,426 cycles

SUPPORT TASK - BELT FRAME STA 827 BETWEEN STRINGERS S8R-S9R HAS CRACKED INDICATION AT I/B FASTENER OF SUPPORT BRACKET OF AIR CONDITIONING OUTLET ASSY USING MFEC (STEP 4.0 OF EA 5310-04498 OP 02-AIR COND FRAME BRACKET INS/REPAIR). A/C NUMBER ENTERED IN ERROR. REPAIRED FRAME AT STA 827 RT PER-ECRA 5311-1480. ATTACHED FORM- 44.0008, PAGE 1 TO 3, ITEM 1 TO 13 AND INITIATED DIP #53-DIP, CNT- 03730 PER ECRA 5311-014800, STEP 7. FOR ONE TIME INSPECTION LT & AMP; RT FRAME STATION 827 BETWEEN 18,000 TO 24,000 AIRCRAFT FLIGHT CYCLES AFTER REPAIR INSTALLATION. DIP HAS BEEN TRANSFERRED TO LOG PAGE 9714627 FOR THE 1 TIME INSPECTION PER ECRA 5311-01480.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,484 hrs · 22,426 cycles

CRACKED FRAME AT STA 400 BETWEEN STRINGERS 8LT AN D 9LT INSTALLED FRAME REPAIR PER EA5310-04498, SEE ATTACHED HEAT TREAT FORMS AND 44.0008 FORMS FOR C/W.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,484 hrs · 22,426 cycles

CRACKED FRAME AT STA 380 BETWEEN STRINGERS 8RT AND 9RT. INSTALLED FRAME REPAIR PER EA 5310-04498. HEAT TREAT FORMS & 44.0008 FORMS FOR C/W JOB.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 42,484 hrs · 22,426 cycles

SUPPORT TASK - BELTFRAME STA 827 BETWEEN STRINGERS S8L-S9L HAS CRACKED INDICATION AT THE I/B FASTENER OF SUPPORT BRACKET OF AIR CONDITIONING OUTLET ASSY. USING MFEC (STEP 4.0 OF EA 5310-04498 OP 02-AIR COND FRAME BRACKET INS/REPAIR.) REPAIRED FRAME AT STA 827 BETWEEN STRINGERS 8L-9L PER ECRA 5311-01480, ATT 44.0008 PAGE 1 TO PG 3, ITEM 1 TO 13.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,484 hrs · 22,426 cycles

LEFT O/B SEAT TRACK IS CORRODED STA 887-912. LEFT O/B SEAT TRACK FROM STA 877 TO 927 REF SRM 53-00-52 FIG 201, INSTALLED SPLICE REPAIR 4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,484 hrs · 22,426 cycles

FRAME CRACKED AT STA 727B BETWEEN S-8 & S-9 LT SIDE. REPAIRED FRAME AT STA 727B BETWEEN S8&S9. REF EA 5310-04498.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 42,484 hrs · 22,426 cycles

B737-53-4-0012 BELT FRAME STA 787 BETWEEN STRINGER S8R - S9R HAS CRACK AT FASTENER AREA. REPAIRED FRAME PER EA 5310-04498 OP 02.

Part: CABLE — DAMAGED (R2 DOOR) · airframe 40,670 hrs · 21,458 cycles

R-2 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR LATCH CABLE HAS BROKEN STRANDS. B737-25-4-0002 REMOVED AND REPLACED LATCH CABLE REF AMM 25-61-35.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,825 hrs · 15,877 cycles

CABIN FLOOR CORROSION AT STA 986.5, APPROXIMATELY 48 INCHES. REPLACED BEAM PER SRM 53-00-51 FIG 203.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,825 hrs · 15,877 cycles

INSPECTION FOUND MAIN CABIN FLOORBEAM BEAM CORRODED AROUND SCREW HOLES AT STA 947.5, LBL 17 TO RBL 17. A REPAIR WAS INSTALLED IAW ECRA 5310-04049.

Part: SENSOR — OUT OF ADJUST (RT MLG) · airframe 26,119 hrs · 13,924 cycles

THE CREW WAS UNABLE TO RAISE THE GEAR AFTER TAKEOFF. THE GEAR HANDLE WAS IN THE OFF POSITION WITH THREE GREEN AND THREE RED INDICATION LIGHTS. THE AIRCRAFT WAS RETURNED TO EWR. TROUBLESHOOTING FOUND THE RIGHT MAIN GEAR SAFETY SENSOR OUT OF ADJUSTMENT. THE SENSOR GAP AND TELEFLEX CABLE WERE ADJUSTED IAW MM 32-09-01. A GEAR SWING WAS PERFORMED AND ALL OPERATION CHECKED GOOD.

Part: FITTING — WORN (R/H ELEVATOR) · airframe 25,176 hrs · 13,430 cycles

INSPECTION FOUND THE R/H ELEVATOR O/B HINGE FITTING WORN. THE HINGE FITTING WAS REMOVED AND REPLACED IAW SRM 51-51-02 AND 51-40-02.

Part: SKIN — DENTED (STA 400) · airframe 25,176 hrs · 13,430 cycles

INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 400 BELOW STRINGER 17L. A REPAIR WAS INSTALLED IAW SRM 53-00-01.

Part: SKIN — DENTED (STA 380) · airframe 25,176 hrs · 13,430 cycles

INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 380, STRINGER 17L. INSTALLED REPAIR IAW SRM 53-00-01.

Part: FIRE LOOP — MALFUNCTIONED (MLG WW) · airframe 24,252 hrs · 12,945 cycles

THE WHEEL WELL FIRE LIGHT ILLUMINATED AND THE FIRE WARNING BELL SOUNDED SHORTLY AFTER THE LANDING GEAR WAS RETRACTED ON TAKEOFF FROM IAH. THE WARNING WAS INTERMITTENT AT FIRST AND EVENTUALLY BECAME STEADY. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANED WITHOUT INCIDENT. THERE WAS NO EVIDENCE OF FIRE. A CHECK OF THE WHEEL WELL FIRE LOOP FOUND IT FAULTY. THE NR 3 BRAKE WAS ALSO FOUND TO BE VERY HOT. THE WHEEL WELL FIRELOOP WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE NR 3 BRAKE WAS ALSO REMOVED AND REPLACED.

Part: HORIZ STAB — DENTED (RIGHT)

IAH - INSPECTION FOUND THE HORIZONTAL STABILIZER RIB CORD AND SKIN DENTED ON INBOARD RT SIDE CAUSED BY A BIRD STRIKE. (X)