N58606

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,076 hrs · 22,409 cycles

BS 303.9 FRAME CRACKED AT STR 16L FORWARD SIDE AROUND OVAL HOLE. INSTALLED REPAIR PER ECRA 5311-01515. GENERATED DIP TO REINSPECT BEFORE THE ACCUMULATION OF 66000 TOTAL A/C FLY CYCLES PER PART 2 OF ECRA 5311-01515 REF DIP 08205 FRAME CRACKED STA 303.9 PER ECRA 5311-01515 COMPLETED REPAIR. INSPECT REPAIR AT 66,000 TOTAL FLT CYC`S. PLANNING TO CONTACT ESC AFTER 60,000 TOTAL FLT CYC`S NOT TO EXCEED 61,000 TOTAL FLT CYC`S FOR PERMANENT REPAIR. QC UPDATE: PLANNING TO CONTACT ESC AFTER 60,000 TOTAL FLT CYC`S BUT BEFORE 61,000 TOTAL FLT CYC`S FOR CORRECTIVE ACTION LIMIT: INSPECT REPAIR AT 66,000 TOTAL FLT CYC`S. PLANNING TO CONTACT ESC AFTER 60,000 TOTAL FLT CYC`S NOT TO EXCEED 61,000 TOTAL FLT CYC`S FOR PERMANENT REPAIR.

Part: SKIN — CRACKED (L1 DOOR HINGE) · airframe 43,076 hrs · 22,409 cycles

CRACK INDICATION FOUND AT FWD ENTRY DOOR UPPER HINGE CUTOUT AFT FASTENER HOLE 4TH FROM TOP, REF EA 5330-03736 REV B, STEP 14, INSTALLED REPAIR IAW ECRA 5330-04091.

Part: SKIN — WORN (RT OB MIDFLAP) · airframe 43,076 hrs · 22,409 cycles

SUPPORT TASK - RT OTBD MIDFLAP, INBD L/E WORN. MARKED, TRIMMED OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER IAW E CRA 5752-01496.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 43,076 hrs · 22,409 cycles

SUPPORT TASK BELTFRAME STA 706 HAS CRACK INDICATION BETWEEN STRINGERS S8R AND S9R AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT (RIVET BUCKED TAIL) AREA PER MID-FREQ EDDY CURRENT INSPECTION (MFEC). REPAIRED FRAME STA 706-R, PER EC/RA 5311-01514 AND EA 5310-04498. DIP CTL # 07974 LP 9723422 SEQ # N00760.

Part: SUPPORT FITTING — CORRODED (TE FLAP) · airframe 43,076 hrs · 22,409 cycles

SUPPORT TASK LT WING NR 2 FLAP TRACK MOUNT HOLES SPOT FACE HAS SURFACE CORROSION UPPER SIDE. REMOVED AND REPLACED FLAP TRACK SUPPORT FITTING REF BOEING DWG 65C80736, SOPM 20-50-19, AND SRM 51-40-02.

Part: SKIN — DENTED (CARGO DOOR) · airframe 43,076 hrs · 22,409 cycles

SUPPORT TASK: WHEN PERFORMED DMG LOG 9593545 INSP ON A/B/B DOOR FOUND DENT AT 15 INCHES FROM TOP AND 14 INCHES FROM FWD EDGE OUT OF LIMITS PER SRM 52-00-01. A=1.6 Y=.063 A/Y=25 LESS THAN MIN LIMIT 30 CUT OUT SECTION OF DAMAGE AND INSTALLED DOUBLER REF SRM 52-00-0 1, REPAIR 3. ALODINED AND PRIMED AND PAINTED REF SRM 51-20-01.

Part: HINGE FITTING — CRACKED (L1 DOOR) · airframe 43,076 hrs · 22,409 cycles

L-1 DOOR UPPER HINGE FITTING CRACK INDICATION. INSTALLED NEW UPPER HINGE FITTING / SRM 51-40-02, AFTER DISCOVERY UPPER HINGE FITTING WAS CRACKED.

Part: HINGE FITTING — CRACKED (L1 DOOR) · airframe 43,076 hrs · 22,409 cycles

L-1 DOOR LOWER HINGE FITTING CRACK INDICATION. INSTALLED NEW LOWER HINGE FITTING SRM 51-40-02, AFTER DISCOVERY LOWER HINGE FITTING WAS CRACKED.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 43,076 hrs · 22,409 cycles

SUPPORT TASK - BELFRAME STA 827 HAS CRACK AT FASTENER HOLE BETWEEN STRINGERS S8L AND S9L AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT AREA. REPAIRED FRAME-REF-EC/RA 5311-01512,DIP PER EA-5310-04498 STEP 35 TO PERFORM A ONE TIME INSPECTION.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 43,076 hrs · 22,409 cycles

SUPPORT TASK - BS 360L STR 11L, CRACK ON ATTACH CLIP. REMOVED CLIP, INSPECTED HOLES IN AREA AND INSTALLED NEW CLIP PER ECRA 5311-01513.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 43,076 hrs · 22,409 cycles

SHEAR TIE CRACKED STA 967 AT S4L CABIN CTN 53-304-108. REMOVED AND REPLACED SHEAR TIE REF SRM 51-40-02 AND BOEING DWG 65-46563.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,076 hrs · 22,409 cycles

SUPPORT TASK - RIVET HOLE STA 420 BETWEEN S-17 AND S-17 SHOWS CRACK INDICATION ON HFEC HOLE PROBE INSP REF NDT PT 6 51-00-00 FIG 16. REMOVED RIVET, REPAIRED SKIN PER SRM 53-00-01 FIG 201 SECTION 2 REPAIR 19, REMOVED AND REPLACED SHEAR TIE.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 43,076 hrs · 22,409 cycles

RT WING NR 7 FLAP TRACK AFT ATTACH POINT EMITTING RUST. CORRECTED 11/10/2010 HOU 66274 INSTALLED NEW SERVICEABLE NR 7 FLAP TRACK; REF AMM 27-51-49-404-006. ROTABLE PARTS CHANGE WAS INDICATED - TT 1441858 S/N OFF 01606 TRACK, FLAP, O/B OFF 24-5753-9-9001 1606 ON 24-5753-9-9001 3585.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,076 hrs · 22,409 cycles

MAIN FRAME CRACKED STA 616 RT JUST BELOW MAIN DECK FLOOR. COMPLETED REPAIR FRAME STA 616R REF EC/RA 5311-01158.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,076 hrs · 22,409 cycles

MAIN FRAME CRACKED AT STA 616 JUST BELOW FLOOR DECK LT SIDE. COMPLETED REPAIR OF STA 616 FRAME REF EC/RA 5311-01158.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 43,076 hrs · 22,409 cycles

SUPPORT TASK - BELTFRAME STA. 747 HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8L AND S9L AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT AREA. INSTALLED REPAIR ANGLES A & B REF EA 5310-04498.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 43,076 hrs · 22,409 cycles

SUPPORT TASK - BELTFRAME STA 360, CRACKED AT FASTENERS HOLE BETWEEN STR 8L & 9L AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT AREA. INSTALLED REPAIR ANGLE A & B AND INSTALLED NEW CLIP PER EC/RA 5311-01511.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 43,076 hrs · 22,409 cycles

SUPPORT TASK - BELTFRAME AT STA 727B HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8L AND S9L AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT AREA. REPAIRED FRAME AT STA727B BETWEEN STRINGERS 8L AND 9L PER EA 5310-04498 OP2.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 43,076 hrs · 22,409 cycles

SUPPORT TASK - BELTFRAME STA 400 CRACKED AT FASTENER HOLE BETWEEN STR 8L & 9L AT A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT AREA. INSTALLED REPAIR ANGLE A & B REF EA 5310-04498 OP.02.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 43,076 hrs · 22,409 cycles

SUPPORT TASK. BELTFRAME STA 400 CRACK INDICATION BETWEEN STR 8R AND 9R AT A/C OULET EXTRUSION SUPPORT BRACKET ATTACHMENT (RIVET BUCKED TAIL) AREA PER MID-FREQ EDDY CURRENT INSPECTION (MFEC). INSTALLED REPAIR ANGLE A & B REF EA 5310-04498 OP2.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 43,076 hrs · 22,409 cycles

SUPPORT TASK - BELTFRAME STA 440 HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8L AND S9L AT THE A/C OUTLET SUPPORT BRACKET ATTACHMENT AREA (ALL WORK ACCOMPLISHED ON FORMS 44.008 AND 43.0150). REMOVED DAMAGED FRAME SECTION INSTALLED REPAIR DOUBLERS REF EA 5310-04498 OP2.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 43,076 hrs · 22,409 cycles

SUPPORT TASK - BELTFRAME STA 867 HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8L AND S9L AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT AREA. REPAIRED BELTFRAME STA 867 STRINGERS 8L-9L REF EA 5310-04498.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 43,076 hrs · 22,409 cycles

SUPPORT TASK BELTFRAME STA 867 HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8R AND S9R AT A/C OUTLET EXTRUSION BRACKET DAMAGED AREA REMOVED FROM FRAME AT STA 867 B/W STR S8R AND S9R. AREA REPAIRED PER EA 5310-04498 OP2.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 43,076 hrs · 22,409 cycles

SUPPORT TASK BELTFRAME STA 380 HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8R AND S9R AT THE A/C OUTLET SUPPORT BRACKET DAMAGED AREA REMOVED FROM FRAME AT STA 380 B/W STR S8R AND S9R. AREA REPAIRED PER EA 5310-04498 OP2.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 43,076 hrs · 22,409 cycles

SUPPORT TASK BELTFRAME STA440 HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8R AND S9R AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET DAMAGED AREA REMOVED FROM FRAME AT STA 440 B/W STR S8R AND S9R. AREA REPAIRED PER EA 5310-04498 OP2.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,076 hrs · 22,409 cycles

FWD ENTRY BETWEEN STA 344 - 360 BL-0 INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL, ALL HOLES DRILLED AS NEEDED REF SRM 51-40-02 & 51-40-05.

Part: FRAME — CRACKED (BS 400 S17-28R) · airframe 37,081 hrs · 19,306 cycles

INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR CUTOUT FORWARD FRAME AT LOWER STOP PAD, STA 400, S17R TO S28R. A NEW FRAME WAS INSTALLED IAW SRM 51-10-02 AND 51-40-00.

Part: SLIDE — LOW (L-2 DOOR) · airframe 33,393 hrs · 17,365 cycles

THE L-2 DOOR SLIDE WAS FOUND WITH LOW PRESSURE. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-35.

Part: FIRE DETECTOR — INOPERATIVE (APU) · airframe 27,992 hrs · 14,627 cycles

THE APU FIRE DETECTION LIGHT ILLUMINATED WHILE ENROUTE FROM PHL TO IAH. THE APU FIRE BOTTLE WAS DISCHARGED, BUT THE WARNING LIGHT REMAINED ILLUMINATED. THE AIRCRAFT WAS DIVERTED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE APU FIRE DETECTION ELEMENT M334 WAS FOUND AT FAULT. THE FIRE DETECTION ELEMENT WAS REMOVED AND REPLACED. THE FIRE DETECTION SYSTEM PASSED ALL FUNCTIONAL TESTS. THE APU FIRE BOTTLE WAS REMOVED AND REPLACED IAW MM 26-22-00.

Part: ENGINE — LEAKING (NR 1) · airframe 19,085 hrs · 9,801 cycles

ON TAKE-OFF AND LANDING WITH THROTTLES ADVANCED COCKPIT AND CABIN HAS STRONG UNPLEASANT ODOR. REMOVED AND REPLACED ENGINE DUE TO OIL LEAK PER MM 71-00-00.

Part: ACCESS DOOR — WORN (LT WING) · airframe 18,929 hrs · 9,710 cycles

INSPECTION FOUND LEFT WING TANK NR 1 FUEL BOOST PUMP ACCESS PANEL UNSECURABLE DUE TO WORN SPOTS ON LOWER WING SKIN AT WBL 146. REPAIRED AREA IAW ECRA 5720-01793.

Part: SKIN — DENTED (FUSELAGE) · airframe 18,929 hrs · 9,710 cycles

INSPECTION FOUND SKIN LAP DENTED AT STA 967, STRINGER 26L. REPAIRED IAW ECRA 5360-01039.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 18,929 hrs · 9,710 cycles

INSPECTION FOUND CABIN FLOOR R-1 DOOR THRESHOLD Z-ANGLE ATTACH CHORD CORRODED AT STA 294 - 298. THE ATTACH CHORD STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: SKIN — DENTED (BS 295)

INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 295,S23L. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5330-02924.

Part: SENSOR TARGET — OUT OF ADJUST (NLG)

EWR - FLT 1535 - THE NLG RED LIGHT REMAINED ILLUMINATED WHEN GEAR WAS EXTENDED FOR LANIDNG AT IAH. THE GEAR WAS CYCLED WITH NO CHANGE. EMERGENCY PROCEDURES WERE FOLLOWED AND A TOWER FLY-BY CONFIRMED THE GEAR WAS EXTENDED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE NOSE GEAR SENSOR TARGET IAW MM 32-33-00. THE NOSE GEAR WAS SWUNG WITH ALL OPERATION AND INDICATIONS CHECKING GOOD. (X)

Part: EGT INDICATOR — INOPERATIVE (NR 1 ENGINE)

FLT NR 1646 - DFW - THE NR 1 ENGINE OVERHEATED ACCOMPANIED BY ILLUMINATION OF RED LIGHT WHILE AT CRUISE. THE THROTTLE WAS REDUCED TO IDLE AND THE ENGINE SHUTDOWN MOMENTS LATER. THE AIRCRAFT WAS RETURNED TO DFW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE BOROSCOPED THE NR 1 ENGINE AND INSPECTED THE EGT HARNESS WITH NO EVIDENCE OF HEAT OR OTHER DEFECTS FOUND. THE FUEL FILTER AND CHIP DETECTORS WERE FOUND CLEAN. THE NR 1 ENGINE EGT INDICATOR WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. BOTH ENGINES WERE RUN AT IDLE, PART, AND TAKEOFF POWER WITH EGT'S INDICATING WITHIN 15 DEGREES OF EACH OTHER. (M)