N62631

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,298 hrs · 23,435 cycles

AISLE EMERGENCY LIGHTS INOP SEATS 1B, 2B, 7C, 8C, 10C. FOUND SEAT 2B AFT LT SHORTED, REPLACED FUSE ON BATT PACK M1674 REF WDM 33-51-12 PG 3 AND AMM 33-51-51. REPLACED LT ASSY, OPS CHECK GOOD.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,815 hrs · 22,654 cycles

CORROSION ON SKIN CLIP OF STA 727A O/B OF S26R AFT CARGO COMPT. REMOVED CORRODED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE REF EC/RA 5311-01524.

Part: FRAME — CHAFED (FUSELAGE) · airframe 42,815 hrs · 22,654 cycles

APU BLEED AIR DUCT RUBBING FRAME STA 1040 (TAIL COMP). REPAIRED FRAME AT STA 1040 PER AVO HOU032311-01 REV A AND ECRA 5311-01523 WEIGHT CHANGE IS LESS THAN FIVE POUNDS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,815 hrs · 22,654 cycles

SUPPORT TASK - FUSELAGE FRAME WEB HAS A 1 IN CRACK AT STR 16L STA 303.9. REPAIRED CRACKED FRAME REF EA 5310-04659 REV A OP 2.

Part: HINGE FITTING — CRACKED (L1 DOOR) · airframe 42,815 hrs · 22,654 cycles

SUPPORT TASK - L1 DOOR JAMB UPPER HINGE FITTING IS CRACKED. REMOVED AND REPLACED L1 DOOR UPPER HINGE FITTING REF SRM 51-40- 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,815 hrs · 22,654 cycles

SUPPORT TASK EA 5310-05331 MAIN FRAME CRACKED STA 616 RT SIDE JUST BELOW MAIN DECK FLOOR. REPAIRED CRACK FRAME AT STA 616 RT REF EA5310-05331 STEPS 25. 0 TP 25.14 AND NON-ROUTINE 9726968 SEQ N00288.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 42,815 hrs · 22,654 cycles

RT WING NR 7 FLAP TRACK AFT ATTACH EMITTING RUST. REPLACED FLAP TRACK REF MM 27-51-49-004-001 AND MM 27-51-49-404 -006. ROTABLE PARTS CHANGE WAS INDICATED - TT 1429471 S/N OFF 01631 TRACK, FLAP, O/B OFF 24-5753-9-9001 1631, ON 24-5753-9-9001 2569.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,086 hrs · 19,617 cycles

FRAME CORRODED AT STATION 767 FROM S-27L TO S-26R. CUT OUT DAMAGED AREA AND INSTALLED SHEAR TIE REPAIR PER SRM 53-00-07, REPAIR 10.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 37,086 hrs · 19,617 cycles

VERTICAL STABILIZER LEADING EDGE RIB AT STATION 235.90 IS CRACKED ON RIGHT SIDE. INSTALLED REPAIR PER SRM 51-40-02 AND SRM 51-70-11.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 37,086 hrs · 19,617 cycles

VERTICAL STABILIZER LEADING EDGE RIB AT STATION 292.07 IS CRACKED ON RIGHT SIDE. INSTALLED REPAIR PER SRM 51-40-02 AND SRM 51-70-11.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 37,086 hrs · 19,617 cycles

VERTICAL STABILIZER LEADING EDGE RIB AT STATION 273.35 IS CRACKED ON RIGHT SIDE. INSTALLED REPAIR PER SRM 51-40-02 AND SRM 51-70-11.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,086 hrs · 19,617 cycles

FRAME CORRODED STATION 907 AT S-27R. ROUTED OUT CORROSION FROM S-27R TO BL 0 STA 907 AND INSTALLED REPAIR PER SRM 53-00-07 FIG 201, REPAIR 10.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 37,086 hrs · 19,617 cycles

VERTICAL STABILIZER LEADING EDGE RIB AT STATION 189.09 IS CRACKED ON RIGHT SIDE. REMOVED AND REPLACED CRACKED RIB AT STATION 189.09 PER SRM 51-40-02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,086 hrs · 19,617 cycles

FRAME CORRODED AT STATION 807, S-25L TO S-27R. REMOVED AND REPLACED BOTTOM FRAME AT STATION 807 FROM STR 25 RT TO STR 23 LEFT PER SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,086 hrs · 19,617 cycles

FRAME CRACKED AT STATION 907 ABOVE S-9R. REPAIRED FRAME PER EA.5310-04498, OP 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,086 hrs · 19,617 cycles

FRAME CRACKED AT STATION 360 ABOVE S-9L. REPAIRED FRAME PER EC/RA 5311-01430.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,086 hrs · 19,617 cycles

FRAME CRACKED AT STATION 440 ABOVE S-9L. REPAIRED FRAME PER EA 5310-04498, OP 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,086 hrs · 19,617 cycles

FRAME CRACKED AT STATION 867 ABOVE S-9R. REPAIRED FRAME PER EA 5310-04498, OP 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,086 hrs · 19,617 cycles

FRAME CRACKED AT STATION 747 ABOVE S-9L. REPAIRED PER EA 5310-04498 OP 2, INSTALLED REPAIR ANGLES ON FRAME STATION 747, S-9L.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,086 hrs · 19,617 cycles

FRAME CRACKED AT STATION 907 S-9L. REPAIRED FRAME PER EA 5310-04498, OP2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,086 hrs · 19,617 cycles

FRAME CRACKED AT STATION 827 ABOVE S-9R. REPAIRED FRAME PER EC/RA 5311-01431 AND EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,086 hrs · 19,617 cycles

FRAME CRACKED AT STATION 380 ABOVE S-9R. REPAIRED FRAME PER EA 5310-04498, OP 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,086 hrs · 19,617 cycles

FRAME CRACKED AT STATION 827 ABOVE S-9L. REPAIRED FRAME PER EC/RA 5311-01431.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,086 hrs · 19,617 cycles

FRAME CRACKED AT STATION 787 ABOVE S-9L. INSTALLED REPAIR ANGLE AT STATION 787, S-9L PER EA 5310-04498 OP 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,086 hrs · 19,617 cycles

FRAME CRACKED AT STATION 440 ABOVE S-9R. REPAIRED FRAME PER EA 5310-04498, OP2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,086 hrs · 19,617 cycles

FRAME CRACKED AT STATION 867 ABOVE S-9L. INSTALLED REPAIR ANGLE AT STATION 867, S-9L PER EA 5310-04498 OP 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,086 hrs · 19,617 cycles

FRAME CRACKED AT STATION 400 ABOVE S-9R. REPAIRED FRAME PER EA 5310-04498, OP 2.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 37,086 hrs · 19,617 cycles

BULKHEAD VERTICAL WEB AT RBL 17.1 CRACKED AT FASTENER HOLE APPROXIMATELY AT WL 226. REPLACED CRACKED WEB AS REQUIRED PER SRM 51-10-2.

Part: TIRE — FAILED (MLG) · airframe 36,070 hrs · 19,087 cycles

LEFT INBOARD TIRE BLEW ON LANDING. REMOVED AND REPLACED NR 1 AND NR 2 MAIN TIRES PER MM 32-45-11. NR 1 MAIN S/N ON 9069, S/N OFF 3490, NR 2 MAIN S/N ON 9253 S/N OFF 3114.Â

Part: FUSE — BLOWN (BATTERY PACK) · airframe 35,767 hrs · 18,929 cycles

AISLE PATH LIGHTING INOP, BETWEEN OVERWING HATCH AND STA 727C. FOR SDR REPORTING. FUSE IN POSITION 3 ON LEFT HAND POWER SUPPLY AT ROW 19 BAD. REMOVED AND REPLACED FUSE IAW B737-500MM CHAPTER 33-51-51, OPS CHECK NORMAL.

Part: SHEAR TIE — CRACKED (BS 1040) · airframe 30,831 hrs · 16,255 cycles

INSPECTION FOUND A .5 INCH CRACK IN THE AFT TAIL COMPARTMENT SHEAR TIE AT STA 1040 BETWEEN S2R AND S3R. A NEW SHEAR TIE WAS INSTALLED IAW SRM 51-10-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,831 hrs · 16,255 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 23-31. THE CORRODED SECTIONS OF FLOORBEAM WERE CUTOUT AND A REPAIR WAS INSTALLED IAW SRM 53-60-51 FIGURE 201.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,831 hrs · 16,255 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, RBL 31. THE CORROSION WAS REMOVED AND NEW REPAIR PARTS WERE INSTALLED IAW SRM 53-60-51.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,831 hrs · 16,255 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, RBL 4. A REPAIR STRAP WAS INSTALLED ON FORWARD FLANGE OF FLOORBEAM IAW SRM 53-00-51 FIGURE 201.

Part: SKIN — DENTED (FUSLEAGE) · airframe 24,860 hrs · 13,150 cycles

INSPECTION FOUND A DENT IN FUSELAGE SKIN AT BS 420 BELOW S17L. THE SKIN WAS REPAIRED IAW ECRA 5331-01133.

Part: FAIRING — DAMAGED (RT WING) · airframe 24,632 hrs · 13,032 cycles

THE RT RED GEAR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION ON TAKEOFF. THE GEAR WAS CYCLED, BUT THE LIGHT REMAINED ILLUMINATED. THE AIRCRAFT WAS DIVERTED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT I/B FLAP FAIRING HANGING BY FORWARD END ATTACH HARDWARE WHICH OBSTRUCTED GEAR ON RETRACTION. IT APPARENTLY WAS DISLODGED BY DAMAGED ELEPHANT EAR AT FLAP RETRACTION. THE FAIRING WAS REPLACED IAW MM 27-51-32. A GEAR SWING WAS PERFORMED AND OPERATIONAL CHECKS WERE GOOD.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 24,198 hrs · 12,796 cycles

INSPECTION FOUND THE OVERHEAD EMERGENCY LIGHT ABOVE FIRST/COACH DIVIDER INOPERATIVE. REPLACED PICO FUSES IN POWER SUPPLY FOR LIGHT.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 24,198 hrs · 12,796 cycles

INSPECTION FOUND EMERGENCY LIGHT ABOVE LT OVERWING EXIT INOPERATIVE. MAINTENANCE FOUND DISCONNECT ON LT OVERWING EXIT LIGHT ASSEMBLY L-7 AND L-751 WITH LOOSE CONNECTOR D2976 AND LOOSE GROUND GD 1912-DC. RECONNECTED AND OPERATION CHECKED GOOD.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 24,198 hrs · 12,796 cycles

INSPECTION FOUND EMERGENCY LIGHTING ON FIRST CLASS SEATS INOPERATIVE. REPLACED PICOFUSES IN POWER SUPPLY FOR LIGHT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 18,830 hrs · 9,834 cycles

INSPECTION FOUND CABIN FLOORBEAM CORRODED AT SEVERAL FASTENER HOLES, STA 986, LONGERON 29R AND 27L. STRAP REPAIRS WERE INSTALLED IAW SRM 53-00-51.