N705UP

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A CENTER LIGHT UNDER GLARESHIELD FOR EMERGENCY LIGHT ARM INOP. ACCOMPLISHED OPERATIONAL TEST, NO DISCREPANCY NOTED IAW MM 33-50-01.

Part: GAUGE — OUT OF POSITION (ESCAPE SLIDE)

FOUND ESCAPE SLIDE PRESSURE GAUGE NOT IN VIEW. REPOSITIONED SLIDE PACK. OK FOR SERVICE.

Part: COALESCER BAG — DIRTY (A/C BAY)

INSPECTION TYPE:N/A STRONG BURNING ODOR WHEN LEFT PACK OPERATED WITH MIX VALVE IN FULL COLD POSITION. REMOVED AND CLEANED LT PACK COALESCER BAG IAW MM 21-55-03-2. RAN PACK WITH NO ODOR NOTED. A/C OK TO CONTINUE.

Part: SMOKE GOGGLES — SCRATCHED (COCKPIT)

F/O SMOKE GOGGLES SCRATCHED. REPLACED F/O SMOKE GOGGLES. OPS NORMAL.

Part: SKIN — CORRODED (FUSELAGE)

FUSELAGE HAS A BULGED AREA 25" FWD OF PIT 31 LWR FWD CORNER MARKED AND ADVISED BY MX. GAINED ACCESS TO THE BACKSIDE OF AREA NO CORROSION OR DEFECTS FOUND AT THIS TIME AS PER SRM 51-1-0. OK FOR SERVICE, AREA FOUND TO BE FREE AND SMOOTH.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 65,650 hrs · 26,243 cycles

INSPECTION TYPE:C-2, INTERCOSTAL AT STA 980 HAS CORROSION. CORROSION OUT OF LIMITS PER SRM 53-2-0. FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-1-21, AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 65,650 hrs · 26,243 cycles

INSPECTION TYPE:C-2, LONGERON 24L CRACKED ON O/B FLANGE. REMOVED AND REPLACED LONGERON 24L IAW SRM 51-3-2, 51-1-8, AND 51-1-20D.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 65,650 hrs · 26,243 cycles

C2 SEAT TRACK HEAVILY CORRODED AT STA 420 LBL 25. REMOVED AND REPLACED SEAT TRACK AT STA 360-560 LBL 25 IAW SRM 51-3-0, 51-3-2, 53B-003-501.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 65,650 hrs · 26,243 cycles

MAIN CABIN SEAT TRACK HAS HEAVY CORROSION, STA 1480 RBL 50. REMOVED AND REPLACED SEAT TRACK SECTION FROM STA 1460-1580 RBL 50 IAW SRM 51-3-0.

Part: FRAME — CORRODED (CARGO BAY) · airframe 65,650 hrs · 26,243 cycles

INSPECTION TYPE:C-2. MAIN CARGO STA 1700 RBL 24 SEVERE CORROSION AT TOP OF FRAME ON UNDERSIDE AND CONTINUES OUTBD TO RBL48. CUT OUT DAMAGED AREA PER SRM 51-2-1 FIG 1, SHEET 7. FABRICATED REPAIR REPAIR DOUBLER AND REPAIR ANGLES IAW SRM 51-1-21 FIG 1, AND INSTALLED IAW SRM 51-2-1 FIG 7, SHEET 7.

Part: FITTING — CORRODED (CARGO BAY) · airframe 65,650 hrs · 26,243 cycles

INSPECTION TYPE:C-2. A-PIT AT STA 320 L33R, BATH TUB FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED BATH TUB FITTING AT A-PIT STA 320 L33R IAW SRM 53-2-0 FIG 1F, 51-1-20D, AND 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,650 hrs · 26,243 cycles

INSPECTION TYPE:C-2. BANANA FITTING CRACKED AT STA 340 L33R. REMOVED AND REPLACED BANANA FITTING AT STA 340 L33R IAW SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (STA375 RBL59) · airframe 65,650 hrs · 26,243 cycles

INSPECTION TYPE:C-2. HEAVY CORROSION IN SEAT TRACK ALONG RBL 59 STA 375-420. REMOVED AND FABRICATED SEAT TRACK PER DWG S2400463. INSTALLED FABBED SEAT TRACK AT STA 375-420 PER SRM 53-2-3.

Part: FLOOR SUPPORT — CRACKED (MAIN CABIN) · airframe 65,650 hrs · 26,243 cycles

INSPECTION TYPE:C-2. MAIN CABIN STA 759 LBL24 UNDER SEAT TRACK. SEAT TRACK FLOOR SUPPORT FITTING CRACKED. REMOVED AND REPLACED SUPPORT FITTING AT STA 759 LBL24 IAW 51-1-20D, AND 51-3-0.

Part: FITTING — CRACKED (FUSLEAGE) · airframe 65,650 hrs · 26,243 cycles

INSPECTION TYPE: C2, B-PIT BETWEEN STA 460-440 L28R SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING IN B-PIT AT STA 460-440, L28R IAW SRM 51-1-21D AND SRM 51-1-21

Part: SKIN — DAMAGED (RUDDER) · airframe 65,650 hrs · 26,243 cycles

INSPECTION TYPE:C-2. UPPER PORTION OF RUDDER ON RT SIDE JUST ABOVE LOGO, OIL CANNING OF SKIN. REMOVED AND REPLACED SKIN ON RT SIDE OF RUDDER JUST ABOVE LOGO IAW DC8 DWG 5655077 AND SRM 51-1-8, AND 51-1-21A. NO WEIGHT AND BALANCE DUE TO 1FOR 1 SKIN CHANGE.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 65,650 hrs · 26,243 cycles

LT HORIZ STAB L/E 2ND INBD LWR RIB REPAIR HAS DOUBLER AND TRIPLER CRACKED. REMOVED, FABRICATED, AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW SRM 55-2-0, 51-1-21, AND SRM 55-2-0 FIG 2.

Part: FITTING — CORRODED (RT WW) · airframe 65,650 hrs · 26,243 cycles

INSPECTION TYPE C-2, CORNER FITTING CRACKED AND HEAVILY CORRODED, RT W/W STA 980 CEILING O/B CORNER NEXT TO L24R. REMOVED FITTING IAW SRM 51-1-20D. FABRICATED DOUBLER, REPAIR ANGLE AND FILLERS IAW SRM 53-02-00-0, INSTALLED DOUBLER REPAIR ANGLE AND FILLERS IAW SRM51-1-20D, AND 51-1-15.

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 65,650 hrs · 26,243 cycles

INSPECTION TYPE:C-2. LT ELEVATOR CONTROL TAB SKIN AND DOUBLER CRACKED AT INBD EYEBOLT ACCESS HOLE LWR SKIN. REMOVED AND REPLACED LT ELEVATOR CONTROL TAB ASSY PER TASK CARD 3016 STEP 13.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 65,650 hrs · 26,243 cycles

INSPECTION TYPE C-2, CORROSION BETWEEN TOP OF L24L AND REPAIR DOUBLER STACK IN LT W/W NEAR STA 906. REMOVED CORROSION OUT OF LIMITS IAW SRM 51-1-8 AND 53-2-0 FIG 1F. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 53-02-02 FIG 005 SHEET 8.

Part: STRAP — CORRODED (FUSELAGE)

CORROSION ON SKIN SPLICE STRAP STA 450 LONG 30R. ENGINEERING SUBMITTED PROPOSAL TO BOEING FOR REPAIR. REMOVED ALL FASTENERS IN AREA OF CORROSION WS 05577521. REMOVED CORROSION AS NEEDED FOR REPAIR REF N/R 680150.

Part: BATTERY PACK — WILL NOT TEST (EMERGENCY LIGHT)

EMERGENCY LIGHTING WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK, GROUND OPS CHECK NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS FADED DURING EMERGENCY LIGHTS TEST. REMOVED AND INSTALLED A SERVICEABLE LIGHTING BATTERY AND RELAY UNIT REF DC8 MM 30-50-01-2. TEST GOOD.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE ON PREFLIGHT TEST. REMOVED AND REPLACED BATTERY PACK, OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOPERATIVE. ROBBED EMERGENCY LIGHT BATTERY PACK FROM A/C 708 SN D69 P/N 5708454-503. OPS CKS GOOD

Part: LONGERON — CORRODED (FUSELAGE) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, STA. 1690 AFT SIDE LONG. 30L END FITTING AND LONGERON SECTION IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING,FABRICATED AND REPLACED LONGERON SECTION IAW DWG. 5649329 AND SRM.53-2-2 FIG. 10 AND 51-1-21,51-1-20D.

Part: FITTING — CRACKED (RIGHT WING) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, STRINGER END FITTING IS CRACKED INBOARD SIDE OF XRS 74 AT STRINGER 51 AFT SIDE IN NR 3 MAIN TANK. REMOVED AND REPLACED FITTING IAW DWG. 3704841 AND SRM. 51-1-20D

Part: FRAME — DAMAGED (FUSELAGE) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, MAIN CABIN L-2 DOOR TORQUE BOX WEB HAS A RIVNUT INSTALLED NEXT TO HI -LOCK WITH NO EDGE DISTANCE STA. 1660 LONG. 10L. REMOVED WEB AND REMOVED DAMAGE FROM FRAME,FABRICATED AND INSTALLED DOUBLER ON FRAME AND WEB AT STA. 1660 LONG.10L IAW SRM. 53-2-0 FIG. 23.

Part: FITTING — CRACKED (AFT CABIN) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, STATION 1690 LONG 28L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641324 AND SRM 51-1-20D.

Part: ATTACH FITTING — CRACKED (FRAME) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STATION 1220 AT LONG 20R. REMOVED AND REPLACED FITTING IAW DWG 4750418 AND SRM 51-1-20D.

Part: FITTING — CRACKED (AFT FUSELAGE) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, STA 1781 LONG 17L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FRAME) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE:C1 INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA 1160 LONG 18R. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D.

Part: FITTING — CRACKED (SUBFLOOR) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, LT SIDE STA 800 ON SUBFLOOR AFT OF FLOORBEAM AT LBL 60 THERE IS A CRACKED SUPPORT FITTING. REMOVED AND REPLACED FITTING IAW DWG 3643112 AND SRM 51-1-20D.

Part: ATTACH FITTING — CRACKED (AFT CABIN) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED STA 1152 LONG 20R. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA 1152 LONG 19R. REMOVED AND REPLACED FITTING IAW DWG 4750418 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, LT STA 980 FITTING IS CRACKED NEXT TO FUSELAGE ON WING BOX. REMOVED AND REPLACED FITTING IAW DWG 4647365 AND SRM 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,807 hrs · 25,387 cycles

INSPECTION TYPE: C1, RADIOGRAPHIC (X-RAY)INSPECTION DETECTED 4 CRACKS ON THE R-2 DOOR UPPER AFT CORNER AT STA. 1660 LONG. 11R CUTOUT DAMAGE AND REMOVED DAMAGE AT LONG. 11R,NDT VERIFIED NO CRACKS AT CUTOUT AND DAMAGE REMOVAL, FABRICATED AND INSTALLED DOUBLER, TRIPLER,FILLER AND STRAP I.A.W. E.O. SAA SK 705-086 AND SRM. 53-2-0 FIG. 16

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA 1220 LONG 19R. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D.

Part: FITTING — CORRODED (A/C BAY) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE:C1 A/C BAY STA 70 LONG FRAME FITTING 34L IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 4611159 AND SRM 51-1-20D.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, C-PIT STA. 1120 BELOW LONG. 21R SHEARTIE IS CRACKED REMOVED, FABRICATED AND REPLACED SHEARTIE I.A.W. UPS ENGINEERING FILE NUMBER ,SAA SK 705-061 AND SRM. 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT LONG 1180 LONG 18R. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, STATION 1781 LONG. 17R AND END FITTING ARE CRACKED, REMOVED LONGERON AND ENDFITTING, FABRICATED LONGERON AND REPLACED END FITTING IAW DWG. 4772397 AND 5649327,AND SRM. 51-1-21,51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE:C1 INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA 1200 LONG 20R. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D.

Part: ANGLE — CRACKED (R-1 DOOR) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, 1 INCH CRACK ON ANGLE DOUBLER INNER FRAME OF R-1 DOOR AT STA 160 LONG 15R-17R ON DOOR. REMOVED, FABRICATED AND INSTALLED ANGLE DOUBLER IAW DWG 5615762, AND SRM 51-1-21, 51-1-21A, 51-3-0.

Part: FITTING — CRACKED (LONGERON) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE:C1 MAIN CABIN LONGERON END FITTING IS CRACKED BETWEEN STA 660-680 LONG 11L. REMOVED AND REPLACED FITTING IAW DWG 5750540 AND SRM 51-1-20D.

Part: RIB — CRACKED (LEFT WING LE) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, LEFT WING LE. UPPER RIB IS CRACKED AT XFS 697.5 STOPDRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK,FABRICATED AND INSTALLED STACK ANGLE REPAIR IAW SRM. 57-2-0 FIG. 2

Part: WEB — CRACKED (R-1 DOOR) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, 1.25 INCH CRACK UPPER LEFT INNER WEB R-1 DOOR AT STA 156 LONG 12R TO 13R ON DOOR. STOP DRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 52-2-0 FIG 1B.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, AT STATION 1730 CANTED FRAME LONGERON 14L IS CRACKED. REMOVED LONGERON SECTION STATION 1710-1760, FABRICATED AND INSTALLED LONGERON SECTION IAW SRM 53-2-2 FIG 10.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, STATION 1730 LONG 14R IS CRACKED. REMOVED LONGERON STA 1720 TO 1760, FABRICATED AND INSTALLED LONGERON SECTION IAW DWG 5649327 SRM 53-2-2 FIG 10.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, L-1 UPPER AFT CORNER DOUBLER,TRIPLER DOES NOT CONFORM TO SRM 53-2-0 FIG 15, STA 60 AT LONG 10L. REMOVED EXISTING DOUBLER AND TRIPLER, FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW SRM 53-2-0 FIG 15.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, R-1 LOWER AFT CORNER DOUBLER AND TRIPLER DOES NOT CONFORM TO SRM. 53-2-0 FIG. 14 STA. 418 AT LONG. 21R. REMOVED EXISTING REPAIR,CUTOUT DAMAGE,NDT VERIFIED NO CRACKS AT CUTOUT,FABRICATED AND INSTALLED DOUBLER,TRIPLER AND FILLER IAW SRM. 53-2-0 FIG. 14

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,807 hrs · 25,587 cycles

INSPECTION TYPE: C1, REMOVE DOUBLER FROM L-1 DOOR UPPER FWD CORNER, DOUBLER DOES NOT CONFORM TO SRM. REPAIR PER SRM 53-2-0 FIG 15 ST STA 60 LONG 10L. REMOVED EXISTING REPAIR, CUTOUT CRACK DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW SRM 53-2-0 FIG 15.

Part: COMPRESSOR — STALLED (NR 3 ENGINE)

NR 3 ENGINE COMPRESSOR STALL IFSD AT FL350 WHEN POWER WAS REDUCED FROM 85 TO 77 N & CONTINUED TO STALL IN DESCENT WHEN POWER WAS REDUCED BELOW 72N NR 3 ENG SHUTDOWN IN FLIGHT DUE TO CONTINUED COMPRESSOR STALLS IN LEVEL FLIGHT WITHOUT MOVING THROTTLE. REMOVED AND REPLACED NR 3 ENG IAW MAINT TC 9071 6 STEP 1-4(82586) RIGGED VSV & VBV PER TC 9071 7(09326) BAD FROM STOCK MEC PARTS ON ORDER (99610) BOROSCOPED NR 3 HPT AND LPT BOTH LOW AND HIGH PER MM 72-00-00, CKS OK ON ALL STAGES.

Part: CONTROL CABLE — OUT OF RIG (LT MLG)

INSPECTION TYPE:N/A AFTER GEAR RETRACTION WITH GEAR HANDLE IN THE "UP" POSITION THE DOORS NOT LATCHED LIGHT IS ILLUMINATED. THE LT MLG DOOR ALTERNATE AMBER LIGHT IS ILLUMINATED. GEAR HAD TO BE CYCLED SEVERAL TIMES TO GET THE DOORS NOT LATCHED LIGHT. RIGGED LT MLG FOLLOWUP GEAR DOOR CABLES PER MM 32-31-05 RIG & OPS CHECKED GOOD, CHECKED UPLOCK ROLLER CLEARANCE & PULL CHECK OPS CHECKED NORMAL. CYCLED GEAR, FREE FULL & LIGHT INDICATIONS CHECKED NORMAL PER MM 32-31-05, 32-31-04.

Part: LINK — OUT OF ADJUST (RT MLG DOOR)

INSPECTION TYPE: AS, DOOR NOT LATCHED LT REMAINED ON FOLLOWING GEAR RETRACTION. RT ALT MAIN GEAR DOOR LIGHT WAS ALSO ON. BOTH LTS EXTINGUISHED WHEN THE GEAR HA NDLE WAS MOVED TO THE UPLATCH CK POS. A/C ARRIVED ON PARKING SPOT WITH RH GEAR DR HANGING DOWN APPROX 2 INCHES. ADJUSTED RT MAIN LANDING GEAR DR ADJUSTABLE LINK PER M/M 32-31-05. GROUND & OPS CK GOOD.

Part: HYDRAULIC LINE — FAILED (HYD SYSTEM)

INSPECTION TYPE:N/A, HYD FAILURE IN FLIGHT. EMERGENCY DECLARED. ON CLIMBOUT LOSS OF HYDRAULIC FLUID DOWN TO AUX QUANTITY POSITION. R&R MS ON AILERON RETURN LINE I/B RT WING BEHIND O/B FALSE PANEL. RAN NR 2 & 3 ENG, ALL SYS RAN AND NO LEAKS NOTED. REMOVED AND REPLACED NR 2 ENG HYD PUMP, REMOVED AND REPLACED HYD FILTER PUMP CASE DRAIN. BLEED AIR FROM SYSTEM PUMP PRESS CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHT DIM. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK IAW MM 33-50-01.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:IN EMERGENCY LIGHTS WILL NOT TEST ON PREFLIGHT CHECK. REMOVED, REPLACED BATTERY PACK AND RELAY UNIT PER DC8 MM 33-50-01. OPS CHECK GOOD.

Part: SHEAR TIE — CRACKED (FUSELAGE)

INSPECTION TYPE:IN AFT PRESS BULKHEAD CANTED WEB 2 SHEAR TIES CRACKED RT SIDE BETWEEN L10 & L11 45 ANGLE BRACKET ATTACHED TO CONTROL BULKHEAD CRACKED AS MARKED. REMOVED EXISTING FASTENER FOR REPAIR. FABRICATED REPAIR DOUBLER. INSTALLED DOUBLER.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:IN EMERGENCY EXIT LIGHTS BATTERY LOW VOLTAGE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-01. OPS CHECKS GOOD.

Part: REGULATOR — FAILED (COCKPIT)

INSPECTION TYPE:N/A DEPARTURE-F/O'S OXY REG EMER SELECTOR FAILED. R&R F/O'S OXY REG

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERG LIGHTS INOP. REMOVED AND REPLACED EMERG LIGHT BATTERY PACK. OPS CHECKS GOOD.

Part: SLIDING WINDOW — LEAKING (COCKPIT)

INSPECTION TYPE:IN FOUND F/O'S SLIDING WINDOW LEAKING AIR AT TOP APPROX MID POSITION OF SEAL. APPROX 1/2 PSID. REMOVED & REPLACED RT SLIDING WINDOW IAW MM 56-10-03.

Part: SKIN PANEL — CORRODED (RUDDER) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2 RIGHT RUDDER PANEL IS CORRODED BEYOND LIMITS AT ZR 253. REMOVED, FABRICATED, AND REPLACED SKIN IAW DWG 5655077 AND EO M-5100-11491-B.

Part: RIB — CRACKED (LT WING) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2,3 LEFT WING O/B RIB IS CRACKED AT XFS 653. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2,3 LEFT WING OUTBOARD L/E RIBS ARE CRACKED AT XFS 722.5, XFS 728.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2,3 LEFT WING OUTBOARD L/E RIBS ARE CRACKED AT XFS 791.25, XFS 755.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: INTERCOSTAL — CRACKED (RT WING) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2,3 RIGHT WING CENTER L/E INTERCOSTAL IS CRACKED AT XS 454.976. REMOVED AND REPLACED INTERCOSTAL IAW DWG 5769857 AND SRM 57-1-0, 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (HORIZ STAB) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2,3 RIGHT HORIZONTAL STAB T-FITTING AT I/B LOWER SECTION FWD OF FRONT SPAR IS CRACKED AT APPROX 47.5. REMOVED AND REPLACED FITTING IAW DWG 3701427 AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2 STA 1228 LONG 31R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754916 AND SRM 53-1-0, 51-1-20D.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2 STA 1260 - 1280 LONG 35L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3759258 AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2 STA 1150 AT LONG 33R BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755847 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2 STA 1260-1280 LONG 34R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3759222 AND SRM 51-1-20D.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2,3 STA 1040 - 1060 LONG 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 53-1-0, 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2 STA 1340 FRAME IS CORRODED BEYOND LIMITS AT LONG 36. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2 STA 1400 FRAME IS CORRODED BEYOND LIMITS AT LONG 35R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2,3 STA 1040 - 1060 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 53-1-0, 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C23 STA 1160 LONG 35L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3755845 AND SRM 53-2-0 FIG 2D.

Part: SKIN PANEL — CORRODED (RUDDER) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2 RUDDER TRAILING EDGE IS CORRODED BEYOND LIMITS AT APPROX ZR 168 P/N 5655077-80, JUST ABOVE RUDDER TAB. REMOVED, FABRICATED AND REPLACED RUDDER SKIN PANEL IAW DWG 5655077 AND SRM 51-1-21.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2 STA 1360 FRAME IS CORRODED BEYOND LIMITS AT LONG 36. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2,3 STA 380 - 400 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754473 AND SRM 53-1-0, 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2,3 RIGHT WING OUTBOARD L/E HAS CRACKED UPPER RIB AT XFS 572.5, AND LOWER RIB AT XFS 566.25. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (RT WING) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2,3 RIGHT WING OUTBOARD L/E UPPER INTERNAL DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600, AND SRM 57-1-0, 51-1-20D, 51-1-21.

Part: DOUBLER — BROKEN (RT WING) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2,3 RIGHT WING OUTBOARD L/E STUB WING LOWER INTERNAL DOUBLER IS BROKEN AT XOLDO 67.5. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5802736 AND SRM 57-2-1 FIG 14A.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2 STA -60 AT LBL 53 SUBFLOOR FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5612298 AND SRM 51-1-20D, 51-1-21.

Part: SKIN — CORRODED (RT WING) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2,3 RIGHT WING INBOARD L/E LOWER SKIN HAS INTERGRANULAR CORROSION AT XFS193. REPAIRED SKIN IAW EO DC8-5720-7767-A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2 STA 1190 LONG 21R RT CUSP TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754918 AND SRM 51-1-20D, 51-3-0.

Part: RIB — DAMAGED (RT WING) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2,3 RIGHT WING OUTBOARD L/E RIB WEB IS TORN AT XW 761. REMOVED, FABRICATED, AND REPLACED WEB IAW DWG 5769467 AND SRM 57-1-0, 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2 STA 804 RIGHT KEEL BEAM FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750727 SRM 51-1-20D, 51-1-21, 51-3-0.

Part: SKIN — CRACKED (RT WING) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XW 0. REPAIRED SKIN IAW SRM 57-2-1 FIG 20.

Part: SKIN — CRACKED (RT WING) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2,3 RIGHT WING UPPER SKIN IS CRACKED AT STA XW 402 AT STRINGER 10. REPAIRED SKIN IAW SRM 57-2-1 FIG 21.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2 MAIN CABIN SEAT TRACK HAS BROKEN SCALLOPS AND PLUG GOUGED BETWEEN STA 765-781 LBL 24. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2 MAIN CABIN SEAT TRACK SCALLOPS ARE BROKEN AT STA 1600 RBL 48. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A.

Part: SKIN — CRACKED (LT WING) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2,3 LEFT WING UPPER SKIN IS CRACKED AT XRS 74 AT STRINGER 10. REPAIRED SKIN IAW SRM 57-2-1 FIG 10.

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2 STA 61-63 INNER SKIN IS CORRODED BEYOND LIMITS, BETWEEN LONG 36 AND LONG 35R. REPAIRED SKIN IAW 8110-3 APPROVED DH SK 705-086.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2 MAIN CABIN SEAT TRACK IS CORRODED BEYOND LIMITS AT STA 610 LBL 59. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A.

Part: SKIN — CRACKED (LT WING) · airframe 63,712 hrs · 24,823 cycles

INSPECTION TYPE:C2,3 TRANSFERRED FROM LOG PAGE 9645247, REF DMI D-188382 CRACK ON LEFT WING L/E OUTBOARD OF NR 2 PYLON AT XW 257. REPAIRED SKIN IAW DC8-5720-4087 APPX C.

Part: ENGINE — FLAMED OUT (NR 4 ENGINE)

INSPECTION TYPE:N/A NR 4 ENGINE FLAME-OUT IN FLT. REMOVED AND REPLACED NR 4 ENG FUEL FILTER. INSPECTED INTAKE AND EXHAUST FOR FOD. NONE FOUND. MANUALLY ROTATED FAN. ROTATES FREELY. INSPECTED CHIP DETECTORS. NO DEFECTS FOUND SUMPED NR 3 AND NR 4 AND NR 4 AUX FUEL TANKS (PER MM 71-00-00).

Part: SLIDE — OUT OF POSITION (CABIN)

INSPECTION TYPE:IN, ESCAPE SLIDE NEEDS TO BE PUT BACK IN SLIDE CASE. RE-SECURED ESCAPE SLIDE IN CASE.

Part: INDICATOR — FAILED (ELEVATOR)

INSPECTION TYPE:N/A, DURING BEFORE T/O CHECKLIST ON ELEVATOR CHECK FAILED. RETURN TO BLOCKS FOR MAINTENANCE INSPECTION. ELEVATOR FELT AS IF IT DID NOT MOVE AFTER SEVERAL ATTEMPTS. EPI SHOWED NO MOVEMENT. PERFORMED ELEVATOR POSITION INDICATION SYSTEM ADJ/TEST PER MM 27-31- 00. OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:P/F, EMERGENCY LIGHTING INOP. FOUND SOCKET NR 11 CONNECTOR P1-1345 BAD. REPLACED PER WDM 33-50-01 PG 1. REPLACED BATTERY PACK DUE TO LOW VOLTAGE. SYSTEM OPS CHECKS NORMAL PER MM 33-50-01.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS, OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS DISARM CHECK FAILED. REPLACED DEAD BATTERY AND RELAY ASSY IAW MM 35-50-01, REPAIRED OPEN IN WIRE HVL9812R22 IN CHARGING CIRCUIT. REPAIRES OPEN AT SWITCH S1-3 27 A1 WIRE L9608A24. SYSTEM OPS NORMAL REF WDM 33-50-01.

Part: FLOORBEAM — CORRODED (BS 980)

INSPECTION TYPE:C1, STA 980 AT LBL 9.5, THE FLOORBEAM FLANGE FWD SIDE HAS HEAVY CORROSION. REPAIRED AREA IAW DH SK 705-484.

Part: FRAME — CORRODED (BS 1120)

INSPECTION TYPE:C1, FRAME CAP AT STA 1120 STR 31L-31R IS CORRODED AND CRACKED. REMOVED AND REPLACED CAP IAW DWG 5764343 AND SRM 51-1-21.

Part: RIB — CRACKED (WS 422.185)

INSPECTION TYPE:C1, LT CENTER L/E UPPER RIB IS CRACKED AT STA XS 422.185. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 467.323)

INSPECTION TYPE:C1, LT CENTER L/E UPPER RIB IS CRACKED AT THE AFT END, STA XS467.323. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 360.25)

INSPECTION TYPE:C1, LT CENTER L/E UPPER RIB IS CRACKED AT STA XFS 360.250. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: ANGLE — CRACKED (WS 520)

INSPECTION TYPE:C1, LT CENTER LEADING EDGE O/B VERTICAL ATTACH ANGLE AT I/B SIDE OF NR 1 STUB WING AT STA XS 520.00 IS CRACKED. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753297.

Part: RIB — CRACKED (WS 354)

INSPECTION TYPE:C1, LT CENTER L/E UPPER RIB IS CRACKED AT STA XFS 354.000. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FRAME — CORRODED (BS 1734)

INSPECTION TYPE:C1, STA 1734 AT STR 25R HAS HEAVY CORROSION (FRAME). REPAIRED AREA IAW SRM 53-2-0 FIG 2 AND 53-5-1.

Part: SKIN — CORRODED (WS 710)

INSPECTION TYPE:C1, RT WING O/B LEADING EDGE HAS HEAVY CORROSION AT STA XFS 710.000. REPAIRED AREA IAW SRM 57-2-1 FIG 2H.

Part: SEAT TRACK — CORRODED (BS 1520)

INSPECTION TYPE:C1, STA 1520 AT RBL 59, THE SEAT TRACK MOUNTING FLANGE HAS HEAVY CORROSION. REPAIRED AREA IAW DH SK 705-154.

Part: SKIN — CORRODED (BS 630-640)

INSPECTION TYPE:C1, STA 630-640 BETWEEN STR 34L-35R, THE EXTERNAL SKIN HAS HEAVY CORROSION. REPAIRED AREA IAW DH SK 705-552.

Part: FITTING — CRACKED (BS 840)

INSPECTION TYPE:C1, LONGERON 19L INTERCOSTAL ATTACH FITTING IS CRACKED AT STA 840. REMOVED AND REPLACED FITTING IAW DWG 3777874 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 759)

INSPECTION TYPE:C1, FRAME 759 ATTACH FITTING IS CRACKED AT STR 13L. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3779874.

Part: FITTING — CRACKED (BS 440-460)

INSPECTION TYPE:C1, STA 440-460, STR 29L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4646163 AND SRM 51-1-20D.

Part: SKIN — CRACKED (WS 74)

INSPECTION TYPE:C1, RT WING SKIN IS CRACKED AT STA XRS 74.0 AND STR 12. REPAIRED AREA IAW SRM 57-2-1-FIG 10.

Part: FITTING — CORRODED (BS 580)

INSPECTION TYPE:C1, FLOORBEAM ATTACH FITTING AT STA 580 AND STR 21R HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3773479 AND SRM 51-1-20D.

Part: FRAME — CORRODED (BS 480)

INSPECTION TYPE:C1, STA 480 AT STR 36 THE FRAME HAS HEAVY CORROSION. REPAIRED AREA IAW SRM 53-2-0 FIG 2.

Part: CLIP — BROKEN (PAX DOOR SLIDE)

INSPECTION TYPE-N/A, MAIN ENTRY DOOR SLIDE PACK RETAINER CLIP BROKEN. REMOVED AND REPLACED SLIDE COVER RETAINER CLIP.

Part: FRAME — CORRODED (BS 1300)

INSPECTION TYPE-C/CK, FRAME CORRODED AT STATION 1300, BETWEEN LONGERONS 36 AND 35L, MARKED. BLENDED OUT CORROSION IAW DC8 SRM 51-1-8, FABBED REPAIR DOUBLER IAW3 REO 04060 AND DC8 SRM 53-2-0 FIG 2, HEAT TREATED REPAIR DOUBLER IAW TPS 1003, ALODINED AND PRIMED FRAME AND DOUBLER IAW DC8 SRM 51-1-8, INSTALLED REPAIR DOUBLER WITH HI-LOKS IAW DC8 SRM 51-1-8.

Part: SEAL — GOUGED (PAX DOORWAY)

INSPECTION TYPE-C, FWD PAX DOOR OPENING, TOP AFT CORNER, METALIC SEAL GOUGED WITH ROUGH, JAGGED EDGES. REMOVED DAMAGED AREA UPPER AFT CORNER L-1 DOOR. REMOVED FASTENERS FABRICATED DOUBLER AND TRIPLER AND INSTALLED IAW DC8 SRM 53-2-0, 51-1- 11, 51-1-8 Z9 ALODINED AND PRIMED TIMCO REO- 04O52.

Part: SKIN — CORRODED (BS 1050-1350)

INSPECTION TYPE-C/CK, CORROSION WAS FOUND ON INTERIOR DOUBLER, L35L TO L35R STA 1177 TO 1260. REMOVED AND REPLACED BELLY SKIN AND DOUBLER CADIUM PLATED STEEL LONGERONS ALODINED AND PRIMED BARE METAL, SEALED STRUCTURE AND INSTALLED SKIN AND DOUBLER IAW DC8 SRM 51-1-20D ABD 51-1-21, 51-1-8, 51-1-11, 51-1-24 AND UPS EO DC8-5330-9319-A4.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS DIM ON PRE-DEPARTURE CHECK. REPLACED EMERGENCY LIGHT BATTERY PACK, CKS OK.

Part: SKIN — CRACKED (LT WING)

INSPECTION TYPE-N/A, ON WALK-AROUND NOTICED 3.25 INCH CRACK O/B OF NR 1 ALT FILL VALVE ACCESS PANEL JUST O/B OF NR 1 PYLON. STOP DRILLED CRACK PER 75838 WWP QC 68458, INSTALLED REPAIR DOUBLER AS PER SRM 57-2-0.

Part: MOUNTING FLANGE — CRACKED (RT ELEVATOR)

INSPECTION TYPE CS2, RT ELEVATOR TOADSTOOL UPPER ACCESS PANEL MOUNTING FLANGE IS CRACKED. REPAIRED PER UPS EO.

Part: SPAR — CORROSION (WS 64.76)

INSPECTION TYPE CS2, HEAVY CORROSION ON HOLE CENTER WING UPPER INBOARD FRONT SPAR AT STA XFS64.76 RIB. REPAIRED PER UPS EO.

Part: LONGERON — CRACKED (BS 879-902)

INSPECTION TYPE CS2, HEAVY CORROSION AND CRACKED LONGERON 24R FITTING BETWEEN FS 879 TO 902. REPAIRED PER UPS EO.

Part: SKIN — CRACKED (BS 161)

INSPECTION TYPE CS2, FUSELAGE SKIN CRACKED AT LT RADOME HINGE CUTOUT STA 161. REPAIRED PER UPS EO.

Part: PAN — CRACKED (X-SLIDE DOOR)

INSPECTION TYPE CS2, A X-SLIDE DOOR FWD LOWER PAN CRACKED. REPLACED PAN ASSY PER DOUGLAS DRAWING 575384.

Part: FRAME — CORROSION (BS 640)

INSPECTION TYPE CS2, HEAVY CORROSION ON BELTFRAME FS 640, LONGERONS 34L AND 34R. REPLACED FRAME SECTION PER SRM 51-1-20D AND SRM 51-1-21.

Part: SHEAR TIE — CRACKED (FS 1600)

INSPECTION TYPE: CS2. FS 1600 BETWEEN LONGERONS 32L-33L, SHEAR TIE CRACKED. REPLACED SHEAR TIE PER SRM 53-2-0.

Part: FINGER DOUBLER — CORROSION (SUBFLOOR)

INSPECTION TYPE CS2, HEAVY CORROSION ON FINGER DOUBLER PANEL SUBFLOOR FS 131 TO 135 RBL 15 TO 25. REPAIRED PER UPS EO.

Part: BULKHEAD FITTING — CRACKED (FS 980-1000)

INSPECTION TYPE CS2, FS 980 TO 1000, LONGERON 30R, BULKHEAD FITTING HAS CORROSION CRACK. REPLACED FITTING PER SRM 51-1-20D.

Part: SKIN — CRACKED (RUDDER)

INSPECTION TYPE: CS2. RUDDER RT SIDE AT LEADING EDGE SKIN CRACKED AT SECOND HINGE POINT CUTOUT LOWER SKIN. REPLACED RUDDER ASSY PER T/C S55-682-44.

Part: BELTFRAME — CRACKED (BS 70)

INSPECTION TYPE CS2, CORROSION CRACK ON BELTFRAME, FS 70 FWD SIDE, LONGERON 30R. REPAIRED FRAME PER SRM 53-2-5.

Part: SKIN — CRACKED (HORIZ STAB)

INSPECTION TYPE CS2, RT HORIZONTAL STAB LEADING EDGE SKIN CRACKED AT DOUBLER STA XFS21 6. REPAIRED PER UPS EO.

Part: END FITTING — CORROSION (FS 70)

INSPECTION TYPE CS2, HEAVY CORROSION ON END FITTING, LONGERON 31R FS 70, FWD END. REPLACED FITTING PER SRM 51-1-20D AND SRM 51-1-21.

Part: SKIN — CRACKED (RUDDER)

INSPECTION TYPE: CS2. RUDDER LEADING EDGE LT SIDE CRACKED AT SECOND HINGE POINT CUTOUT LOWER SKIN. REPLACED RUDDER ASSY PER T/C S55-682-44.

Part: END FITTING — CORROSION (FS 70)

INSPECTION TYPE CS2, MODERATE CORROSION ON END FITTING, LONGERON 33R, FS 70 FWD END. REPLACED FITTING PER SRM 51-1-21 AND 51-1-20D.

Part: T FITTING — CRACKED (KEEL BEAM)

INSPECTION TYPE: C. KEEL BEAM LOWER SURFACE 3 EA T-FITTINGS CRACKED AT FS 900, FS 940 AND FS 950. REPLACED FITTINGS PER SRM 51-1-20D.

Part: FLOOR BEAM — CORROSION (BS 1280)

INSPECTION TYPE CS2, HEAVY CORROSION ON FLOOR BEAM FS 1280, LEFT TUNNEL AREA LBL 57. REPAIRED PER UPS EO.

Part: ANGLE — CORROSION (BS 1625)

INSPECTION TYPE CS2, MAIN CABIN HEAVY INTERGRANULAR CORROSION ON LONG 21R, FS 1625 ON ANGLE. REPLACED ANGLE PER SRM 51-1-20D.

Part: BELTFRAME — CORROSION (BS 1400)

INSPECTION TYPE CS2, HEAVY CORROSION ON BELTFRAME AT FS 1400 ABOVE LONGERON 35R. REPAIRED FRAME PER SRM 53-2-0.

Part: RIB — CRACKED (LT HOR STAB LE)

INSPECTION TYPE: CS2. LT HORIZONTAL STABILIZER LEADING EDGE INBOARD UPPER RIB IS CRACKED. REPAIRED RIB PER SRM 55-2-0.

Part: DOUBLER — CORROSION (BS 1644)

INSPECTION TYPE CS2, HEAVY CORROSION ON FUSELAGE SKIN STA 1644 BETWEEN LONGERONS 29R AND 30R ON INNER DOUBLER. REPLACED INNER DOUBLER PER SRM 51-1-21.

Part: SKIN — CORROSION (RUDDER)

INSPECTION TYPE CS2, RUDDER LT SIDE HEAVY CORROSION JUST ABOVE THE TAB. REPLACED RUDDER ASSY ON N/R TASK NR 463759 AND ROUTINE T/C NR S55- 682-44.

Part: RIB — CRACKED (RT WING)

INSPECTION TYPE: CS2. RT WING LEADING EDGE 5 EA UPPER RIBS CRACKED AT STA XFS635, XFS641, XFS654, XFS660 AND XFS672. REPAIRED RIBS PER MM 57-00-00, PG 801.

Part: RIB — CRACKED (RT WING)

INSPECTION TYPE: CS2. RT WING LEADING EDGE 3 EA LOWER RIBS CRACKED AT STA XFS672, XFS804 AND XFS822. REPAIRED PER MM 57-00-00, PG 801.

Part: RIB — CRACKED (RT WING)

INSPECTION TYPE: CS2. RT WING LEADING EDGE 6 EA UPPER RIBS CRACKED AT STA XFS728, XFS766, XFS772, XFS804, XFS810, XFS816. REPAIRED PER MM 57-00-00, PG 801.

Part: DOUBLER — CRACKED (AFT FUSELAGE)

INSPECTION TYPE: CS2. DOUBLER CRACKED AT FUSELAGE SKIN MAIN CARGO DOOR AFT JAMB 20 FROM AFT UPPER CORNER. REPLACED DOUBLER PER SRM 51-1-21A.

Part: SKIN — DELAMINATED (NR 4 SPOILER)

INSPECTION TYPE CS2, RT WING NR 4 SPOILER DELAMINATED ON LOWER INBD AFT CORNER. REPLACED SPOILER ASSY PER MM 27-61-01.

Part: BATTERY PACK — DISCHARGED (CREW ENTRY)

MAINTENANCE REPORTED, EMERGENCY EXIT LIGHTS DO NOT TEST PROPERLY DURING PRE/FLT. REPLACED BATTERY AND RELAY UNIT WITH REF TO MM 33-50-01, GROUND CKS GOOD.

Part: FITTING — CRACKED (LT TE FLAP)

MAINTENANCE REPORTED, FLAP FITTING CRACKED ON O/B FLAP I/B FITTING. REMOVED AND REPLACED FITTING.

Part: EEL CONNECTOR — BROKEN (CABIN)

MAINTENANCE REPORTED EMERGENCY EXIT LIGHT INTERMITTENT. REPLACED CONNECTOR AT TERMINAL BLOCK, CHECKS OK.

Part: EEL WIRE — BROKEN (CABIN)

MAINTENANCE REPORTED CABIN DOOR EMERGENCY LIGHT INOP. REPAIRED BROKEN WIRE AT BATTERY TERMINAL BLOCK. OPS CK OK.