N16648

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,946 hrs · 16,889 cycles

SUPPORT TASK - EA 5330-03736 LOWER HINGE CUTOUT FOR L-1 DOOR HAS A CRACK INDICATION AT LWR HOLE IN INSP AREAS. REPAIRED PER ECRA 5330-03997. GENERATED DIP TO READ "FOR L-1 DOOR LWR HINGE CUTOUT ACCOMP AN INSP OF REPAIR BEFORE ACCUM OF 71889 TOT AC FLT CYC PER PT 2 OF ECRA5330-03997. PLAN TO CONT ENG AFTER ACCUM OF 66000 TOT FLT CYC BUT BEFORE 670 00 TOT FLT CYCL FOR INSP DETAILS. QC ACCOMPLISH AN INSPECTION OF THE REPAIR BEFORE THE ACCUMULATION OF 71,889 TOTAL ACFT FLT CYCLES PER PART 2 OF ECRA 5330-03997. PLANNING TO CONTACT ENGINEERING AFTER ACCUMULATION OF 66,000 TOTAL FLT CYCLES BUT BEFORE 67,000 TOTAL FLT CYCLES FOR INSPECTION DETAILS. 1) INIT: AFTER 66000 BUT BEFORE 67000 TOTAL ACFT F/C & 2) T/A: W/I 71889 TOTAL A/C F/C-ODEE

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,002 hrs · 16,380 cycles

FOUND R-1 DOOR AND LEFT SIDE OVERWING HATCH, EMERGENCY LIGHTS OUT. TROUBLESHOT AND FOUND BULBS BURNT, ALSO SYSTEM LOW ON CHARGE. REMOVED AND REPLACED BULBS. CHARGED EMERGENCY LIGHT SYSTEM PER 33-51-51-/201, OPS CHECK GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,049 hrs · 15,375 cycles

BS 360 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR 8L AND STR 9L. ACCOMPLISHED EA 5310-04498 ON BS 360 LEFT FRAME AT STR 8L AND STR 9L. ACCOMPLISHED EC/RA 5310-04867 ON CLIP REPLACEMENT AT BS 360 AT STR 8L.

Part: SKIN PANEL — SCRATCHED (RUDDER) · airframe 29,049 hrs · 15,375 cycles

RUDDER BETWEEN ATTACH POINT 4 AND 5 SCRATCH ON RIGHT SIDE CLOSE TO TRAILING EDGE. ACCOMPLISHED REPAIR OF RT RUDDER SKIN PANEL PER CO EC/RA 5540-01257.

Part: DRAG ANGLE — CORRODED (VERTICAL STAB) · airframe 29,049 hrs · 15,375 cycles

VERTICAL STABILIZER AFT LEFT ATTACH LUG AREA, FWD DRAG ANGLE FITTING HAS CORROSION INSIDE O/B HOLE. REMOVED LT VERTICAL STABILIZER AFT I/B AND O/B ATTACH BOLTS, REMOVED AND REPLACED LT DRAG ANGLE PER B737 SRM 51-40-02. REINSTALLED LT VERTICAL STABILIZER AFT I/B AND O/B ATTACH BOLTS PER B737 SRM 55-30-00 AND CO WORK CARD 24-55-30-1-2600 SEQ 342.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,049 hrs · 15,375 cycles

BODY STATION 727B LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR 8L AND STR 9L. REPAIRED BODY STATION 727B FRAME AT AC RAIL BRACKET BETWEEN STR 8L AND STR 9L PER EA5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,049 hrs · 15,375 cycles

BODY STATION 747 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR 8L AND STR 9L. REPAIRED FRAME BODY STATION 747 AT AC RAIL BRACKET BETWEEN STR 8L AND STR 9L PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,049 hrs · 15,375 cycles

BODY STATION 907 FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR 8R AND STR 9R. BODY STATION 907 FRAME REPAIRED BETWEEN STR 8R AND STR 9R PER CO EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,049 hrs · 15,375 cycles

BODY STATION 867 FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR 8L AND STR 9L. REPAIRED BODY STATION 867 AT AC RAIL BRACKET BETWEEN STR 8L AND STR 9L PER CO EA5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,049 hrs · 15,375 cycles

BODY STATION 867 FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR 8R AND STR 9R. BODY STATION 867 FRAME REPAIRED BETWEEN STR 8R AND STR 9R PER CO EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,049 hrs · 15,375 cycles

BODY STATION 827 FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR-8L AND STR-9L. REPAIRED FRAME BODY STATION 827 AT AC RAIL BRACKET BETWEEN STR 8L AND STR 9L PER EA 5310-04498.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 29,049 hrs · 15,375 cycles

BODY STATION 328 - 344 LBL 12 INTERCOSTAL HAS CORROSION ON TOP SURFACE. REMOVED AND REPLACED DAMAGED INTERCOSTAL AT BODY STATION 328 - 344 LBL 12 PER B737 SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,049 hrs · 15,375 cycles

FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR 8L AND STR 9L. REPAIRED FRAME BODY STATION 787 AT STR 8L AND STR 9L AT AC RAIL BRACKET PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,049 hrs · 15,375 cycles

BODY STATION 400 FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR-8R AND STR-9R. REPAIRED CRACK BETWEEN S-8R AND S-9R AT BODY STATION 400 FRAME PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,049 hrs · 15,375 cycles

BODY STATION 440 FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR-8R AND STR-9R. REPAIRED BODY STATION 440 FRAME CRACK BETWEEN S-8R AND S-9R PER EA 5310-04498.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 29,049 hrs · 15,375 cycles

BODY STATION 312 - 328 RBL 12 INTERCOSTAL HAS CORROSION ON TOP SURFACE. REMOVED AND REPLACED DAMAGED INTERCOSTAL AT BODY STATION 312 - 328 RBL 12 PER B737 SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,049 hrs · 15,375 cycles

BODY STATION 440 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR 8L AND STR 9L. REPAIRED BODY STATION 440 LEFT HAND SIDE FRAME BETWEEN S-8L AND S-9L PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,049 hrs · 15,375 cycles

BODY STATON 400 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR-8L AND STR-9L. REPAIRED BODY STATION 400 LEFT SIDE FRAME AT (AC) RAIL BRACKET BETWEEN S-8L AND S-9L PER EA 5310-04498.

Part: SKIN — CRACKED (RT WING) · airframe 29,049 hrs · 15,375 cycles

RIGHT WING NUMBER 4 SLAT LEADING EDGE SKIN AT ACTUATOR CUTOUT APPEARS TO BE CRACKED. REMOVED ACTUATOR DOOR SEAL ASSEMBLY IAW B737 SRM 57-41-01, STOP DRILLED CRACK IAW B737 SRM 57-41-01. MATERIAL ID 301 1/2 HARD, .040", IC 0649022 IAW B737 SRM 57-41-01, FABRICATED REPAIR DOUBLER IAW B737 SRM 57-41-01. PRIMED REPAIR DOUBLER IAW B737 SRM 51-20-01, INSTALLED REPAIR DOUBLER IAW B737 SRM 52-41-01. REINSTALL ACTUATOR DOOR SEAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,049 hrs · 15,375 cycles

BODY STATION 787 FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR 8R AND STR 9R. ACCOMPLISHED EA5310-04498 ON BODY STATION 787 FRAME AT STR 8R - STR 9R.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,049 hrs · 15,375 cycles

BODY STATION 747 FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR 8R AND STR 9R. ACCOMPLISHED EA 5310-04498 ON BODY STATION 747 FRAME AT STR-8R AND STR-9R.

Part: SKIN — DELAMINATED (SLAT) · airframe 29,049 hrs · 15,375 cycles

RIGHT WING NUMBER 5 SLAT OUTBOARD EDGE ON TRAILING EDGE WEDGE SEALANT MISSING, CHECK FOR DELAMINATION. REPAIRED DAMAGE AT OUTBOARD TRAILING EDGE WEDGE NUMBER 5 SLAT PER B737-500 SRM 51-70-10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,049 hrs · 15,375 cycles

BODY STATION 380 FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR-8R AND STR-9R. REPAIRED BODY STATION 380 FRAME CRACK BETWEEN S-8R AND S-9R PER EA 5310-04498.

Part: SKIN — CRACKED (L/E SLAT) · airframe 22,482 hrs · 11,929 cycles

INSPECTION FOUND A .5 INCH CRACK IN THE LT WING NR 1 SLAT LOWER SKIN AT FASTENER AREA O/B OF I/B AUX TRACK. THE CRACKED AREA WAS REMOVED AND FILLER AND A SPLICE PLATE WERE INSTALLED IAW SRM 57-43-01, FIGURE 201.

Part: INTERCOSTAL — BROKEN (BS 344-360) · airframe 20,840 hrs · 11,097 cycles

INTERCOSTAL AT STA 344-360, LBL 0 IS BROKEN. REPLACED INTERCOSTAL PER SRM 51-10-02.

Part: INTERCOSTAL — CRACKED (BS 340-360) · airframe 20,840 hrs · 11,097 cycles

TOP OF INTERCOSTAL AT STA 340-360, LBL 11 IS CRACKED. INSTALLED ANGLE PER SRM 51-10-02 AND ECRA 5310-03585.

Part: ANGLE — CRACKED (RT WING) · airframe 16,406 hrs · 8,827 cycles

RT WING 90 DEGREE GREEN ANGLE CRACKED AT FORWARD SIDE OF RT MLG INBOARD DOOR OPENING WBL 71 UNDER STRUT DOOR. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-10-02.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 16,406 hrs · 8,827 cycles

INSPECTION FOUND LT Z-ANGLE CORRODED AT L-2 DOOR SILL, STA 977. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 16,406 hrs · 8,827 cycles

INSPECTION FOUND VERTICAL STABILIZER RT REAR SPAR FORWARD DRAG ANGLE FITTING CORRODED AT OB MOUNTING BOLT AREA. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02.