N842AL

Part: SKIN — CORRODED (ZONE 100) · corrosion level 3 · airframe 68,422 hrs · 68,390 cycles

FUSELAGE SKIN AT BS 1121, AT STRINGER 20R HAS FASTENERS PULLING THROUGH SKIN LOCATED ABOVE APU ACCESS DOOR CUT OUT. AFTER REMOVAL OF FASTENERS IT WAS DETERMINED THAT WHITE POWDER AND CORRODED METAL CAME OUT OF THE FASTENER HOLES. AFTER A CUT OUT OF THE CORRODED ACFT SKIN REVEALED EXTENSIVE CORROSION TO INTERNAL FRAMES COMMMON TO THE SKIN CORROSION. DUE TO THE LEVEL OF CORROSION THE REPAIR WAS OUTSIDE OF THE SRM, CONTACTED ENGINEERING FIRM FLIGHT VEHICLES CONSULTING (FVC), WHO DEVELOPED A REPAIR AND PROVIDED REPAIR ON DWG 53-13023-1, REVISION "NEW" DATED 01/16/2013. R & R VERTICAL STIFFENERS AT BS 1096, 1104,1156 IAW SRM 51-30-2 & DWG 65-46579 "REV V". R & R RT TORQUE BOX LOWER CORD AT BS 1088 THU 1156 IAW SRM 51-30-2 & DWG 65-46579 "REV V". FRAME REPAIR STR TIE CLIP AT 1121 IAW SRM 51-30-02. STRINGER 17R SPLICE REPAIR IAW SRM 53-10-3. AFTER INTERNAL REPAIRS WERE CONCLUDED THE EXTERNAL SKIN REPAIR WAS PERFORMED IAW FVC DWG 53-13023-1, REV "NEW". 8110-3 APPROVAL WAS PROVIDED. ALL RELATED COMPONENTS THAT WERE REMOVED TO ACCESS THIS REPAIR WAS RE-INSTALLED IAW PERTAINANT MM REF.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,422 hrs · 68,390 cycles

CORROSION IN AFT CARGO BS 767 STRINGER 27L TO 27R AT AFT FRAME, SHEAR TIES. REMOVED FASTENERS FOR ACCESS TO CORROSION IAW SRM 51-30-2. CORROSION AT SHEAR TIE IS FOUND TO BE OUT OF LIMITS. CUT OUT AND REMOVED CORRODED SHEAR TIE ANGLE IAW SRM 53-10-4. FABRICATED NEW SHEAR TIE ANGLE IAW SRM 51-20-01. INSTALLED REPAIR PARTS (SHEAR TIE ANGLE) IAW SRM 51-30-02.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,422 hrs · 68,390 cycles

EXTERIOR FUSELAGE BELLY, SKIN BULGE AROUND FASTENERS BETWEEN STRINGER 27L AND 27R. REMOVED FASTENERS AT EXTERIOR FUSELAGE SKIN AT BS 747 BETWEEN STRINGER 27L & 27R IAW SRM 51-30-02. FRAME HAS CORROSION DAMAGE BEYOND LIMITS IAW SRM 53-10-1. FABRICATED REPAIR PARTS (SHEAR TIE ANGLE) IAW SRM 53-10-4. INSTALLED REPAIR PARTS IAW SRM 51-30-02

Part: ATTACH ANGLE — CRACKED (ZONE 200) · airframe 68,422 hrs · 68,390 cycles

MAIN CABIN, LT LOWER AFT BULKHEAD SIDE WALL ATTACH ANGLE CRACKED IN 4 PLACES. FABRICATED REPAIR ANGLE FROM MATERIAL 2024 T3 IAW SRM 51-20-1.

Part: FLOORBOARD — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,415 hrs · 68,386 cycles

FORWARD PIT FLOORBOARD SPLICE BETWEEN NR 1 AND NR 2 FLOORBOARD IS CORRODED AND MISSING NUT PLATES. FORWARD PIT FLOORBOARD SPLICE FOUND TO BE OUT OF LIMITS. FABRICATED FLOORBOARD SPLICE IAW SRM 51-30-5. TREATED AND PRIMED SPLICE IAW SRM 51-10-2. INSTALLED 21 NUT PLATES IAW SRM 51-30-2.

Part: RIB — WORN (RT NACELLE) · airframe 68,422 hrs · 68,390 cycles

RT ENGINE COWL HAS AREA OF DAMAGE, AREA NR 7 RIB. REMOVED DAMAGE RIB ANGLE IAW SRM 51-40-3. FABRICATED NEW REPAIR ANGLE IAW SRM 51-40-3. INSTALLED NEW REPAIR ANGLE TO NR 7 RIB IAW SRM 51-40-3.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,442 hrs · 68,390 cycles

FORWARD PIT STATION 385 AT RBL 14 CARGO FLOOR SUPPORT IS CORRODED. REMOVED CORROSION ON FLOOR SUPPORT IAW SRM 51-10-1. CORROSION WAS FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS IAW SRM 53-10-5. INSTALLED REPAIR PARTS IAW 51-30-2 AND 53-10-5.

Part: SKIN — WORN (ZONE 400) · airframe 68,422 hrs · 68,390 cycles

RT ENGINE COWL WORN. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW REPAIR DOUBLER ON THE RT ENGINE COWL IAW SRM 51-40-3.

Part: STRAP — WORN (ZONE 400) · airframe 68,422 hrs · 68,390 cycles

NR 2 ENGINE UPPER FIXED COWL HAS A CHAFED STRAP. RUB STRAP DOUBLER FOUND TO BE WORN BEYOUD LIMITS IAW SRM 54-10-1. FABRICATED REPAIR PARTS IAW SRM 51-20-1. INSTALLED STRAP DOUBLER IAW SRM 51-30-2.

Part: RIB — WORN (RT NACELLE) · airframe 68,422 hrs · 68,390 cycles

RT ENGINE COWL HAS AN AREA OF DAMAGE AT NR 11 RIB. AREA OF DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 54-10-1. REMOVED DAMAGE AND WORN PARTS (ANGLE) IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW REPAIR ANGLE IAW 200 51-40-3.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,422 hrs · 68,390 cycles

LOWER FUESLAGE E/E BAY CORROSION ON SHEAR TIE ANGLE AT BS 312 AT STRINGER 27L, FORWARD OF ACCESS DOOR. REMOVED CORRODED SHEAR TIE ATTACH ANGLE IAW SRM 51-30-2. FABRICATED NEW ATTACH ANGLE IAW SRM 51-20-1. INSTALLED NEW SHEAR TIE ATTACH ANGLE IAW SRM 51-30-2.

Part: SHIM — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,422 hrs · 68,390 cycles

EXTERIOR FUSELAGE, EXTERNAL POWER RECEPTACLE ACCESS DOOR HAS CORRODED SHIMS BENEATH LATCHES ALONG WITH CORRODED HARDWARE. REMOVED CORRODED SHIMS AND HARDWARE, FOUND TO BE OUT OF LIMITS. FABRICATED REPLACEMENT SHIMS IAW SRM 51-20-1. INSTALLED REPLACEMENT SHIMS WITH NEW HARDWARE IAW SRM 51-30-2.

Part: RIB — WORN (RT NACELLE) · airframe 68,422 hrs · 68,390 cycles

RT ENGINE COWL HAS AN AREA OF DAMAGE AT NR 10 RIB. AREA OF DAMAGE IS FOUND TO BE OUT OF LIMITS IAW SRM 54-10-1. REMOVED DAMAGED PARTS (ANGLES). FABRICATED NEW REPAIR ANGLES IAW SRM 51-40-3. INSTALLED REPAIR ANGLES IAW SRM 51-40-3.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,442 hrs · 68,390 cycles

EXTERIOR FUSELAGE BELLY SKIN, BULGE AROUND FASTENERS AT BS 727B BETWEEN STRINGER 27L AND 27R. REMOVED FASTENERS AT EXT FUSELAGE AT BS 727B, DICOVERED FRAME BETWEEN STR 27L & 27R HAS CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED UNSERVICEABLE PARTS 53-10-4. FABRICATED REPAIR PARTS IAW SRM 53-10-4. INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,422 hrs · 68,390 cycles

CORROSION ON INTERCOSTAL AT BS 727A AND 727B AT STRINGER 27L AND 27R. REMOVED INTERCOSTALS AT STRINGER 27L & 27R SRM 51-30-02, UPON FURTHER EVALUATION BOTH INTERCOSTALS WERE FOUND TO HAVE EXTENSIVE CORROSION. IN ADDITION TO THE INTERCOSTALS A WEB AND 2 ANGLES REQUIRE TO BE REPACED. FABRICATED ALL REPAIR PARTS IAW SRM 51-20-01. INSTALLED INTERCOSTALS WEB AND ANGLES IAW SRM 51-30-2.

Part: SKIN — DENTED (ZONE 300) · airframe 66,394 hrs · 64,103 cycles

A DENT WAS FOUND ON THE RT HORIZ STABILIZER LOWER SURFACE BETWEEN STABILIZER STA 120.0 AND 129.0 JUST FORWARD OF THE REAR SPAR. A/Y RATIO DETERMINED THE DENT WAS OUT OF LIMITS. THIS AREA WAS THEN REPAIRED IAW SRM REF 55-10-3, FIG 8. NO OTHER DAMAGE WAS NOTED AT THIS LOCATION.

Part: STRINGER — CORRODED (BS 344) · airframe 66,394 hrs · 64,103 cycles

DURING A C-CHECK, A VISUAL INSP REVEALED CORROSION ON STR 22 LT AT FUSELAGE BODY STA 344. A 20 IN SECTION OF STR WAS REPLACED IAW SRM REF 53-10-3. NO OTHER DAMAGE WAS NOTED AT THIS LOCATION.

Part: STRINGER — CORRODED (ZONE 100) · airframe 66,394 hrs · 64,103 cycles

DURING C-CHECK, A VISUAL INSP REVEALED CORROSION ON STR 19 LT AT BODY STA 294.5. A 16 IN SECTION OF STRINGER WAS REPLACED IAW SRM REF 53-10-3. NO OTHER DAMAGE WAS NOTED AT THIS LOCATION.

Part: STRINGER — CORRODED (BS 294.5 S19L) · airframe 66,394 hrs · 64,103 cycles

DURING A C-CHECK, A VISUAL INSP REVEALED CORROSION ON STR 19 LT AT FUSELAGE BODY STA 294.5. A 16 INCH SECTION OF STRINGER WAS REPLACED IAW SRM REF 53-10-3. NO OTHER DAMAGE WAS NOTED AT THIS LOCATION.

Part: STRINGER — CORRODED (BS 344 S22L) · airframe 66,394 hrs · 64,103 cycles

DURING A C-CHECK, A VISUAL INSP REVEALED CORROSION ON STR 22 LT AT FUSELAGE BODY STA 344. A 20 INCH SECTION OF STRINGER WAS REPLACED IAW SRM REF 53-10-3. NO OTHER DAMAGE WAS NOTED AT THIS LOCATION.

Part: WARNING HORN — ACTIVATED · airframe 65,641 hrs · 62,472 cycles

NON-ETOPS CARGO FLIGHT. TAKEOFF WARNING HORN SOUNDED AT THROTTLE UP FOR TAKEOFF. CREW ABORTED TAKEOFF AT 10 KTS. CREW FOUND THE SPEED BRAKE LEVER WAS NOT COMPLETELY IN THE STOWED POSITION. CREW STOWED THE SPEED BRAKE LEVER AND CONTINUED THE FLIGHT WITHOUT FURTHER INCIDENT. NO MX ACTION WAS TAKEN.

Part: BULKHEAD — CRACKED (BS 1016 S17L) · airframe 65,617 hrs · 62,424 cycles

A SCHEDULED INSPECTION REVEALED A CRACK AT THE 1ST RIVET AT BS 1016 AFT PRESSURE BULKHEAD AT THE WEB DOME SECTION ALONG STIFFENER/ STR-17L. TRIMMED DOME WEBS ONE FASTENER ROW BELOW EXISTING REPAIR. REMOVED CIRCUMFERENTIAL TEAR STRAP AND DAMAGED WEB DOME SECTION. VISUALLY INSPECTED UNDERLYING STRUCTURE AREAS NO DISCREPANCIES NOTED. PERFORMED HFEC ROTARY PROBE INSPECTION OF FASTENER HOLES COMMON TO THE REPAIR IAW NDT MANUAL PT. 6, 51-00-00, FIG. 16. FABRICATED AND INSTALLED REPAIR DOUBLER P/N 65C37292-8 GORE WEB AND APPLIED CORROSION INHIBITOR. RECEIVED FORM 8100-9. REPAIR COMPLIED WITH IAW SRM 53-10-11, FIG. 13 AND ECO 3811.

Part: TRANSMITTER — INOPERATIVE (NR1 ENG EPR) · airframe 65,304 hrs · 61,753 cycles

ABORTED TAKEOFF, WHEN ADVANCING POWER FOR TAKEOFF NR 1 EPR MOVED SLOWLY AND ONLY WENT TO 1.50. ON TAXI BACK NR 1 EPR WOULD NOT MOVE. R & R NR1 ENGINE EPR TRANSMITTER IAW MM 77-11-21. GROUND RUN UP OPS & LEAK CK OK. ACFT RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (SMOKE DETECTOR) · airframe 65,275 hrs · 61,692 cycles

DURING APPROACH AFT CARGO COMPARTMENT SMOKE LIGHT ILLUMINATED. R & R AFT CARGO SMOKE DETECTOR BULB ASSY. OPS CK OK IAW AMM 26-16-00.

Part: CONTROL PANEL — FAILED (FIRE DETECTION) · airframe 65,056 hrs · 61,216 cycles

NON-ETOPS CARGO FLIGHT. AFTER TAKEOFF PWR WAS SELECTED, OVERHEAT/FIRE ANNUNCIATOR LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AND THE CREW RETURNED THE ACFT TO FREIGHT RAMP WITHOUT FURTHER INCIDENT. MX FOUND THAT THE CARGO FIRE DETECTION AND SUPPRESSION PANEL MODULE CAUSED A FALSE WARNING. THE MODULE WAS REMOVED AND REPLACED AND TESTED IAW AMM 26-20-13. THE ACFT WAS RETURNED TO SERVICE.

Part: DUCT — FAILED (ANTI ICE SYS) · airframe 65,047 hrs · 61,195 cycles

NON-ETOPS CARGO FLIGHT, DURING CLIMB, THE CREW NOTED THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATE. NR1 ENGINE EGT REMAINED WITHIN LIMITS. THE NR 1 THROTTLE WAS RETARDED TO IDLE AND THE OVERHEAT LIGHT EXTINGUISHED. ENGINE WAS KEPT AT IDLE AND THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX FOUND AN AIR LEAK IN THE ENG NOSE COWLING THERMAL ANTI-ICE DUCT. THE DUCT WAS REMOVED AND REPLACED AND OPERATIONALLY CHECKED IAW AMM 75-11-61. THE ACFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 64,559 hrs · 60,157 cycles

UPPER FUSELAGE, CARGO CABIN AT BS 660 RBL 50 FLOOR SUPPORT CORRODED.

Part: STRINGER — CRACKED (ZONE 200) · airframe 64,559 hrs · 60,157 cycles

FUSELAGE TAIL CONE BETWEEN BS 1138 AND BS 1142 STR 5A LT, CRACKED.

Part: STRINGER CLIP — CRACKED (BS 685 S6L) · airframe 64,559 hrs · 60,157 cycles

UPPER FUSELAGE,CARGO CABIN AT BS 685 STR 6L, STRINGER CLIP CRACKED.

Part: STRINGER — CRACKED (ZONE 200) · airframe 64,559 hrs · 60,157 cycles

UPPER FUSELAGE CARGO CABIN AT BS 503, STR 8L, CRACKED.

Part: STRINGER — CRACKED (ZONE 200) · airframe 64,559 hrs · 60,157 cycles

UPPER FUSELAGE CARGO CABIN, LAVATORY AREA BS 303 STR 14L, CRACKED.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 64,559 hrs · 60,157 cycles

UPPER FUSELAGE CARGO CABIN AT BS 747 STR 5R CLIP CRACKED.

Part: FRAME — DAMAGED (ZONE 100) · airframe 64,559 hrs · 60,157 cycles

LOWER FUSELAGE AT BS 219.8, RBL 17.5 FRAME OTBD CHORD DRILLED.

Part: SKIN — SCRATCHED (BS 227) · airframe 64,559 hrs · 60,157 cycles

LWR FUSELAGE AT BS 227.8, RBL 17.5, SKIN SCRATCHED.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 64,559 hrs · 60,157 cycles

UPPER FUSELAGE CARGO CABIN AT BS 663 STR 10L CLIP CRACKED.

Part: ANGLE — CRACKED (ZONE 100) · airframe 64,559 hrs · 60,157 cycles

LOWER FUSELAGE BS 1040 STR 21 ANGLE CRACKED.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,559 hrs · 60,157 cycles

LOWER FUSELAGE ST BS 500 BETWEEN STR 27R AND 28R,SKIN CORRODED

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,559 hrs · 60,157 cycles

LOWER FUSELAGE AT STA 1016 STR 24L END FITTING CORRODED.

Part: STRINGER — DAMAGED (ZONE 100) · airframe 64,559 hrs · 60,157 cycles

LOWER FUSELAGE E&E COMPARTMENT,BETWEEN BS 355 AND BS 365,STR 19R WITH DOUBLE HOLE.

Part: SKIN — SCRATCHED (BS 875) · airframe 64,559 hrs · 60,157 cycles

LOWER FUSELAGE AT BS 875.5 STR 17R SKIN WITH SCRATCH.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 64,559 hrs · 60,157 cycles

UPPER FUSELAGE CARGO CABIN FROM BS 540 TO BS 685, RBL 25 TRANSVERSAL BEAM UPPER FLANGE CORRODED.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 64,559 hrs · 60,157 cycles

LOWER FUSELAGE FWD CARGO COMPARTMENT BS 380 BETWEEN STR 19 AND MAIN CARGO DOOR CUTOUT, SHEAR TIE CRACKED.

Part: WEB — CRACKED (ZONE 100) · airframe 64,559 hrs · 60,157 cycles

LOWER FUSELAGE, NOSE WHEEL WELL AT BS 250, RBL 2" UPPER WEB CRACKED.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 64,559 hrs · 60,157 cycles

LOWER FUSELAGE E AND E AT BS 360 BETWEEN STR18R AND 19R, SHEAR TIE CRACKED.

Part: STRINGER — CRACKED (ZONE 200) · airframe 64,559 hrs · 60,157 cycles

UPPER FUSELAGE, CARGO CABIN AT BS 503 STR 8L CRACKED.

Part: SKIN — PUNCTURED (ZONE 100) · airframe 64,559 hrs · 60,157 cycles

LOWER FUSELAGE SKIN WITH PUNCTURES AT BS 355, BETWEEN STR 18R AND 19R.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,559 hrs · 60,157 cycles

LOWER FUSELAGE E AND E COMPARTMENT STR 20R FROM BS 365 TO BS 380 CORRODED.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 64,559 hrs · 60,157 cycles

UPPER FUSELAGE, CARGO CABIN AT BS 747 STR 6L, CLIP CRACKED.

Part: SKIN — SCRATCHED (ZONE 100) · airframe 64,559 hrs · 60,157 cycles

LOWER FUSELAGE ST BS 871 BETWEEN S23-24L SKIN SCRATCHED.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 64,559 hrs · 60,157 cycles

LOWER FUSELAGE, FWD CARGO COMPARTMENT BS 495 FRAME SHEAR TIE CRACKED, BETWEEN 19L AND MAIN CARGO DOOR CUTOUT LOWER SILL BEAM.

Part: STRINGER SPLICE — CRACKED (ZONE 100) · airframe 64,559 hrs · 60,157 cycles

LOWER FUSELAGE E & E COMPARTMENT STRINGER 19L SPLICE CRACKED AT BS 360.

Part: SKIN — CANNING (ZONE 100) · airframe 64,559 hrs · 60,157 cycles

LOWER FUSELAGE AT BS 973, BETWEEN STR 21L AND 22L, SKIN OIL CANNING.

Part: SKIN PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,559 hrs · 60,157 cycles

LOWER FUSELAGE AT BS 889, BETWEEN STR 22L AND 23L, SKIN CORRODED.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,559 hrs · 60,157 cycles

UPPER FUSELAGE CARGO CABIN FROM BS 540 TO BS 663, BL 0 TRANSVERSAL BEAM UPPER FLANGE CORRODED.

Part: SKIN — DENTED (ZONE 100) · airframe 64,559 hrs · 60,157 cycles

LOWER FUSELAGE AT BS 950 BETWEEN STR 21L AND 22L, SKIN DENTED.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 64,559 hrs · 60,157 cycles

UPPER FUSELAGE CARGO CABIN AT BS 727B STR 5L, CLIP CRACKED.

Part: SKIN — CANNING (ZONE 100) · airframe 64,559 hrs · 60,157 cycles

LOWER FUSELAGE AT BS 963 BETWEEN STR 21L AND 22L, SKIN OIL CANNING.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 64,559 hrs · 60,157 cycles

UPPER FUSELAGE CARGO CABIN FLOOR SUPPORT CORRODED AT BS 980,RBL18.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 64,559 hrs · 60,157 cycles

UPPER FUSELAGE, CARGO CABIN AT BS 685 STR 5R CLIP CRACKED.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 64,559 hrs · 60,157 cycles

UPPER FUSELAGE CARGO CABIN AT BS 747 STR 6R, CLIP CRACKED.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 64,559 hrs · 60,157 cycles

UPPER FUSELAGE CARGO CABIN AT BS 660 LBL 50, FLOOR SUPPORT CORRODED.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 64,559 hrs · 60,157 cycles

UPPER FUSELAGE CARGO CABIN AT BS 747 STR 5L, STRINGER CLIP CRACKED.

Part: STRINGER SPLICE — DENTED (ZONE 100) · airframe 64,559 hrs · 60,157 cycles

E AND E COMPARTMENT AT BS 360 STR 24R SPLICE DENTED.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,559 hrs · 60,157 cycles

UPPER FUSELAGE PAX CABIN AT BS 660 LBL 50 FLOOR SUPPORT CORRODED.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 64,559 hrs · 60,157 cycles

CARGO CABIN AT BS 616 BETWEEN LBL 25 AND LBL 45 FLOORBEAM CORRODED.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 64,559 hrs · 60,157 cycles

CARGO CABIN AT BS 616 RBL 45, FLOOR SUPPORT CRACKED.

Part: WEB — CRACKED (ZONE 100) · airframe 64,559 hrs · 60,157 cycles

LOWER FUSELAGE BS 727 STR 18A, WEB CRACKED.

Part: SKIN — CRACKED (ZONE 200) · airframe 64,559 hrs · 60,157 cycles

UPPER FUSELAGE FWD SERVICE DOOR CUTOUT UPPER HINGE LOWER SKIN CRACKED.

Part: SKIN — SCRATCHED (ZONE 100) · airframe 64,559 hrs · 60,157 cycles

FUSELAGE SKIN BETWEEN BS 292 TO BS 390 AND BETWEEN S14-20L SCRATCHED, SKIN REPAIRED.

Part: FRAME — CRACKED (ZONE 100) · airframe 65,559 hrs · 60,157 cycles

SECTION 43 FWD CARGO COMPARTMENT BS 492.4 AFT DOOR WAY FRAME WEB CRACKED.

Part: FRAME — DAMAGED (ZONE 200) · airframe 64,559 hrs · 60,157 cycles

BS 303.9 FRAME FLANGE WITH DOUBLE HOLES BETWEEN S-7L AND 16L.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 64,441 hrs · 59,924 cycles

DURING ACCOMPLISHMENT OF ECO 3512 (AD 2005-17-19) FOUND THREE CRACKS AT FORWARD CARGO DOOR, LOWER FORWARD CORNER APPROX 0.5, LOWER AFT CORNER APPROX 0.5 AND AT RIVET BELOW LOWER AFT CORNER APPROX STRINGER 25. FWD CARGO DOOR, LOWER FORWARD CORNER - REPAIRED IAW SRM 53-30-3, FIG. 46, DETAIL VI. FWD CARGO DOOR, LOWER AFT CORNER REPAIR COMPLIED PER SRM 53-30-3, FIG. 46, DETAIL V. CRACK AT RIVET BELOW LOWER AFT CORNER OF FWD CARGO DOOR APPROX. STRINGER 45: HFEC COMPLETED, NO CRACK NOTED.

Part: CABLE — UNSECURE (DOOR WARNING) · airframe 63,506 hrs · 57,868 cycles

FLT 956: AFT CARGO DOOR LIGHT ILLUMINATED AFTER TAKEOFF. RETURNED TO BASE. RE-SECURED DOOR CABLE AND TARGET. OPS CHECK ON GROUND OK. (S)

Part: SKIN — DENTED (BS 444 S14R) · airframe 62,932 hrs · 56,539 cycles

DENT IN SKIN AT STR 14 +6 BS 444. REPAIRED BY ECO 3720 FINAL REPAIR SIZE APPROX 12IN X 16IN.

Part: SKIN — DENTED (BS 486 S14R) · airframe 62,932 hrs · 56,539 cycles

DENT IN SKIN AT STR 14 + 6 BS 486. REPAIRED BY ECO 3720 FINAL REPAIR SIZE APPROX 13IN X 19IN.