N701UP

Part: CONTROL VALVE — LEAKING (HYDRAULIC SYS)

INSPECTION TYPE:N/A DURING DESCENT INTO SDF THE CREW RECEIVED AN AILERON LIGHT MESSAGE & BEGAN LOSING HYDRAULIC FLUID. THE CREW LATER DECLARED AN EMERGENCY. REMOVED AND REPLACED WING SLOT CONTROL VALVE WHILE RIGHT MANIFOLD WAS REMOVED IN REF TO AMM 27-80-04-2.

Part: GIRT BAR — UNKNOWN (ESCAPE SLIDE)

INSPECTION TYPE:N/A CAN'T STOW GIRT BAR ON ESCAPE SLIDE. STOWED GIRT BAR ON SLIDE.

Part: SLIDE — OUT OF POSITION (COCKPIT)

INSPECTION TYPE:N/A ESCAPE SLIDE PRESSURE UNREADABLE. REPOSITION SLIDE INSIDE OF COVER.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS)

INSPECTION TYPE:N/A EMERGENCY LIGHTS WON'T TEST. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT PER MM 33-50-01-2.

Part: ENGINE — FLAMED OUT (NR 3)

INSPECTION TYPE:AS-E AT FLIGHT LEVEL 360 NR 3 ENGINE FLAMED OUT. RAN FLAME OUT CHECKLIST & RESTART IN FLIGHT CHECKLIST WHILE DESCENDING TO FLIGHT LEVEL 240 RESTART SUCCESSFUL OPERATED NORMALLY REMAINDER OF FLIGHT. PERFORMED ENGINE FLAME-OUT T/S REF MM 71-00-00-1 FIG 139. NO SIGNIFICANT FINDINGS. PERFORMED HI POWER RUN W/BOOST & FEED PUMP OFF. EDP OPERATES NORMALLY. OK FOR SERVICE.

Part: WEB — CRACKED (NR 2 MAIN TANK) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 NR 2 MAIN TANK THRU PNL 506C WEB IS CRACKED FWD OF CTR/SPAR XRS -6. STOP DRILLED CRACK AT NR 2 MAIN TANK WEB AT STA XRS -6 IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT NR 2 MAIN TANK WEB AT STA XRS -6 IAW SRM 57-02-00 FIG 002A, AND SRM 51-1-20D.

Part: SKIN — CRACKED (FS1600) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 HFEC & VISUAL INSPECTION DETECTED A CRACK ON THE R-2 DOOR FWD UPPER CORNER APPROX .50 INCH IN LENGTH. CUT OUT DAMAGED AREA OF THE R-2 DOOR FWD UPPER CORNER IAW SRM 53-02-00 FIG 16, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-02-00 FIG 16 AND SRM TR 53-197.

Part: ATTACH FITTING — CRACKED (NR 4 PYLON) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 1ST CLIP FROM FWD C/S IS CRACKED NR 4 PYLON O/B SKATE ANGLE. REMOVED, FABRICATED AND INSTALLED CLIP IAW SRM 51-1-20D, DWG 5804007.

Part: FLOORBEAM — CORRODED (FS 1260 LBL 59) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 HEAVY CORROSION & EXFOLIATION ON AFT SIDE OF FLOORBEAM, C-PIT TUNNEL LT SIDE STA 1260 LBL 59. REPAIRED FLOORBEAM AT STA 1260 LBL 59 IAW SAA EA 008-5310-01-A0693 UPS RAA DC8-53-20612, AND FAA FORM 8100-9.

Part: FLOORBEAM — CORRODED (FS 1580) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 HEAVY CORROSION ON TOP OF FLOORBEAM AFT ACCY COMPT STA 1580 RBL 50-60, FWD SIDE. CUT OUT CORRODED AREA ON FLOORBEAM AT STA 1580 RBL 50-60 IAW SRM TR 51-2-1. FABRICATED AND INSTALLED REPAIR FILLER, REPAIR ANGLES AND SPLICE ANGLES IAW SRM TR 51-2-1.

Part: FRAME — CORRODED (FS1040 L35-35L/R) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 C-PIT STA 1040 FRAME FROM L35L-L35R HAS EXFOLIATION CORROSION. REMOVED DAMAGED AREA OF FRAME CAP AT STA 1040 IAW SRM 51-1-21, AND DWG 53A-011-A. FABRICATED AND INSTALLED REPAIR ANGLE AND STRAP AT STA 1040 FROM L35L-L35R IAW DWG 2537716, DWG DC8-53A-011 AND SRM 51-1-4, 51-1-20D.

Part: FLOORBEAM — CRACKED (FS 280 RBL 48) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 CRACKED END FITTING ON FLOORBEAM AT STA 280, RBL 48 A-PIT DOORWAY UPPER FWD CORNER REMOVED FLOORBEAM END FITTING AT STA 280, RBL 48 A-PIT DOORWAY UPPER FWD CORNER IAW SRM 51-1-20D. FABRICATED AND INSTALLED FLOORBEAM END FITTING AT STA 280 RBL 48 IAW DWG 974022 AND SRM 51-3-2 AND SRM 51-1-20D.

Part: SUPPORT ANGLE — MISSING (FS 740 L22R) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 MAIN CABIN CENTER WING BOX SUB FLOOR FRAME FITTING SUPPORT ANGLE MISSING AT STA 740 L22R. FABRICATED AND INSTALLED SUPPORT ANGLE IAW SRM 51-3-2, 51-1-20D AND DWG 2892086.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 SUPPORT CHANNEL CRACKED AT STA 1730 RBL 20. REMOVED SUPPORT CHANNEL AT STA 1730 RBL 20 IAW SRM 51-01-21. FABRICATED AND INSTALLED SUPPORT CHANNEL AT STA 1730 RBL 20 IAW SRM 51-3-0, AND DWG 5755032.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 CABIN STA 3.0 RBL 45 SUBFLOOR WEB IS CRACKED. STOP DRILLED CRACK ON WEB AT STA 3.0 RBL 45 IAW SRM 53-2-00 FIG 001B. FABRICATED AND INSTALLED REPAIR DOUBLER AT SUBFLOOR STA 3.0 RBL 45 IAW SRM 53-02-00-0 FIG 001D, AND SRM 51-1-20D.

Part: BEAM — CRACKED (FUSELAGE) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 CRACK IN RADIUS OF NR 3 J-BEAM, 60 COMPT RBL 2. STOP DRILLED CRACK IN RADIUS OF NR 3 J-BEAM IN THE 60 COMPT IAW SRM 53-02-05. FABRICATED AND INSTALLED REPAIR DOUBLER, AND ANGLE IN RADIUS OF THE NR 3 J-BEAM IN THE 60 COMPT IAW SRM 53-02-05-0 AND SRM 51-01-20D.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 CABIN SUBFLOOR STA 25-48 RBL 10 FLOOR SUPPORT ANGLE IS BROKEN. REMOVED FLOOR SUPPORT ANGLE AT CABIN SUBFLOOR AT STA 25-48 RBL 10, REPAIRED FLOOR SUPPORT ANGLE AT STA 25-48 RBL10 IAW SRM 51-01-19, AND SRM 51-3-2.

Part: BOSS — CORRODED (SHOCK STRUT) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 LEFT MLG RETRACT PIN BOSS HAS PITTING AND TOOLING MARKS. REMOVED AND REPLACED LEFT MLG SHOCK STRUT ASSY IAW 32-11-00, RETRACT AND EXTENSION CHECKS GOOD IAW 32-11-00.

Part: RIB — CRACKED (LT WING) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 LT WING CENTER LEADING EDGE UPPER RIB CRACKED AT XFS 366. STOP DRILLED CRACK AT LEFT WING L/E AT STA XFS 366 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER ON LEFT CENTER L/E AT STA XFS 366 IAW SRM 57-02-00 AND SRM 51-01-20D.

Part: FRAME — CRACKED (RWS 252) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 CRACK IN DRILL START IN FRAME ON OUTBOARD LWR SIDE OF NR 3 ENG STUB WING. STOP DRILLED CRACK IN FRAME AT RIGHT STUB WING STA 252.351 IAW SRM 54-2-0, AND SRM TR 54-38. FABRICATED AND INSTALLED REPAIR ANGLE AND DOUBLER AT RIGHT STUB WING STA 252.351 IAW DWG 97532964, AND SRM 54-2-0 FIG 3 AND SRM TR 54-40.

Part: BRACKET — CRACKED (FUEL DUMP CHUTE) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 LEFT WING FLAP WELL FUEL DUMP CHUTE HORSE SHOE BRACKET CRACKED. REMOVED CRACKED HORSE SHOE BRACKET FROM LEFT WING DUMP CHUTE IAW SRM 51-1-20D. FABRICATED AND INSTALLED HORSE SHOE BRACKET AT LEFT WING FUEL DUMP CHUTE IAW DWG 5649654, AND SRM 51-1-4, 51-3-2, AND SRM 51-1-21A.

Part: DOUBLER — CRACKED (LT WING) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 LEFT WING CENTER L/E UPPER INNER DOUBLER CRACKED AT STA XOLDI 6.2246. REMOVED CRACKED DOUBLER AT LEFT WING CENTER L/E STA XOLDI 6.2246 IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT DOUBLER AT LEFT WING CENTER UPPER L/E STA XOLDI 6.2246 IAW SRM 57-03-01, 51-1-8, AND SRM 51-2-20D.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD CRACKED AT STA 1766 LBL 24 L10L AREA. CUT OUT DAMAGED AREA AT AFT PRESSURE BULKHEAD STA 1766 LBL 24 L10L IAW SRM 53-2-5 FIG 14A. FABRICATED AND INSTALLED FINGER DOUBLER, FILLER AND REPAIR DOUBLER AT AFT PRESSURE BULKHEAD STA 1766 LBL 24 L10L IAW SRM 53-2-5 FIG 14A, AND SRM TR 53-194.

Part: SKIN — CRACKED (XFS 107) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 LEFT WING UPPER SKIN 1 INCH CRACK AT XRS 107.000 UPPER FRONT SPAR SKIN. REPAIRED UPPER WING SKIN AT XRS 107.000 FRONT SPAR IAW SAA EA 008-5710-01-A0685 AND UPS RAA DC8-57-20211.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 CORROSION UNDER SPLICE FITTING AND LONGERON 33L IN AFT ACCESSORY COMPT AT STA 1550. REMOVED SPLICE FITTING AND CUT OUT CORRODED SECTION OF L33L FROM STA 1530-1550 IAW SRM 51-1-21. LOCATED, DRILLED UP, AND INSTALLED NEW SPLICE FITTING AND LONGERON 33L SECTION FROM STA 1530-1550 IAW SRM 53-04-01-0, AND SRM 53-02-02-0 FIG 11.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 HEAVILY CORRODED LONGERON IN AFT ACC COMPT STA 1570 L34L. REMOVED CORRODED LONGERON SECTION L34L STA 1560-1570 IAW SRM 51-01- 20D, AND SRM 51-01-21-0. FABRICATED AND INSTALLED LONGERON SPLICE SECTION AND NEW END FITTING AT STA 1560-1570 L34L IAW SRM 53-04-01-0, AND SRM 51-1-20D.

Part: SKIN — DENTED (RUDDER) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 RUDDER RT SIDE LEADING EDGE STA ZR 140 SKIN HAS DENT. FOUND DENT OUT OF LIMITS AT RUDDER STA ZR 140 IAW SRM 55-02-00-0 FIG 001. REMOVED AND REPLACED SKIN AT RUDDER BAY NR 2 STA ZR 140 IAW SRM 51-3-0, 51-1-21, AND SRM 55-06-01-0. NO WEIGHT AND BALANCE REQUIRED ONE FOR ONE SKIN CHANGE IAW SRM 55-06-01-0.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,075 hrs · 27,839 cycles

INSPECTION TYPE:C3 LEFT FUSELAGE STA 1580 BETWEEN L24L & L25L EXT SKIN HAS DENT WITH GOUGE 6 INCHES LONG 1.5 INCH WIDE AND APPROX. .100 INCH DEEP. CUT OUT DAMAGED AREA AT STA 1580 BETWEEN L24L & L25L EXTERIOR SKIN IAW SRM 53-2-1 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER, AND FINGER DOUBLER AT STA 1580 BETWEEN L24L & L25L IAW SRM 53-2-1 FIG 7.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A ON PRE-DEPARTURE, EMERGENCY ARM/DISARM LIGHT WILL NOT GO OUT WHEN SWITCH IS POSITION TO ARM. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK GOOD PER MM 33-50-01-2.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS NO TEST ON PREFLIGHT. REPLACED EMERGENCY LIGHTING BATTERY PACK. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS WOULD NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-50-01-2. OPS CHK GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,167 hrs · 27,140 cycles

FRAME AND SPLICE CORRODED BEYOND LIMITS AT STA 1420 L34R-L36. REMOVED SPLICE FTG AND CUT OUT CORRODED FRAME SECTION BETWEEN L36 AND L34R. FAB REPLACMENT SPLICE FROM SHT 7075-0-.063 HEAT TREAT TO T6. FAB FRAME SECTION FROM EXTR 2641520. INSTALLED PARTS REF SRM 51-1-20D, 53-4-1 FIG 51, 51-3-2, 51-1-8, DWGS 2616545, S2537716, DPS7.00-1.

Part: FITTING — CRACKED (CARGO BAY) · airframe 66,167 hrs · 27,140 cycles

INSPECTION TYPE:C1 INTERCOSTAL-TO-FRAME ATTACH FITTING CRACKED AT STA 1140 LONGERON 35R. REMOVED AND REPLACED FITTING REF SRM 51-1-20D, 51-1-8, 51-1-15.

Part: FITTING — CORRODED (RT WING) · airframe 66,167 hrs · 27,140 cycles

INSPECTION TYPE:C3 RT WING STA XW97 CANOE SUPPORT FITTING ATTACH BOLT HOLES CORRODED & GOUGED. REMOVED AND REPLACED FITTING REF SRM 51-3-2, 51-1-20D, 51-3-0, MM 20-16-00, 27-51-12.

Part: FITTING — CRACKED (LT WING) · airframe 66,167 hrs · 27,140 cycles

INSPECTION TYPE:C3, CLIP CRACKED IN NR 1 ALT TANK AT NR 1 PYLON SKATE ANGLE BETWEEN STR 62 & 63 XRS508.997 LT WING INT. FAB REPLACEMENT CLIP PER DWG5804007 FROM BAR7075T6. DYE-PEN INSP PER DPS 4.707; NO CRACKS NOTED. REMOVED AND REPLACED FITTING REF SRM 51-1-20D, 51-1-15 , 51-1-8. LEAK CHECK C/W ON TC8000.

Part: SUPPORT FITTING — CORRODED (FLAP TRACK) · airframe 66,167 hrs · 27,140 cycles

RT STA 98 FLAP SUPPORT FITTING (CANOE) HAS CORROSION UNDER FLAP TRACK AREA, O/B SURFACE .025 DEEP I/B SURFACE IS .006 DEEP. UNDERCUT AND REMOVED CORROSION .050 AND FABRICATED AND INSTALLED REPAIR FILLERS PER SB 27-164 PAGE 8.

Part: FITTING — CRACKED · airframe 66,167 hrs · 27,140 cycles

INSPECTION TYPE:C1, TAIL CONE ATTACH FITTING CRACKED ON L36, STA 1875. REMOVED AND REPLACED FITTING IAW SRM 51-1-21, 51-1-20D, 51-1-8, 51-3-0.

Part: WEB — CRACKED (R1 DOOR FRAME) · airframe 66,167 hrs · 27,140 cycles

INSPECTION TYPE:C1, R1 DOOR JAMB TORQUE WEB CRACKED ABOVE UPPER DOOR HINGE ARM STA 150- 155, NEXT TO L14R. CUT OUT DAMAGE, NDT VERIFIED REF NDT/SPM06-10-01.001. FAB DOUBLER FROM SHT2024T3-.050, TREAT, PRIME & INSTALLED SAME REF SRM 53-2-0 FIG 1F, 51-1-8, 51-1-21, 51-1-20D, DWG 5615700.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 66,167 hrs · 27,140 cycles

MAIN CABIN AT STA 702 LBL (LONGERON 13LH) FRAME ATTACH FITTING CRACKED. REMOVED, FABRICATED AND REPLACED FRAME ATTACH FITTING AT F/S 702 L13L IAW 51-1-20-D, DWG3779978 AND SAA TRAVELER 0035.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 66,167 hrs · 27,140 cycles

MAIN CABIN STA 835.5 L18L, FRAME ATTACH FITTING CRACKED. REMOVED AND REPLACED FRAME ATTACH FITTING AT STA 853.5 L18L, IAW SRM 51-1-20D.

Part: LONGERON — CRACKED (L36) · airframe 66,167 hrs · 27,140 cycles

LONGERON 36 HAS 1 INCH CRACK ON RT UPPER FLANGE IN RADIUS BETWEEN F/S 1260-1280. REMOVED AND REPLACED DAMAGED LONGERON SECTION IAW DWG 5750322 AND SRM 51-1-20D FROM F/S 1260-1360 L36.

Part: FITTING — CRACKED (MAIN CABIN) · airframe 66,167 hrs · 27,140 cycles

INSPECTION TYPE:C1, LONGERON 8R END FITTING CRACKED AT STA 676. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D, 51-1-8.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 66,167 hrs · 27,140 cycles

MAIN CABIN LONGERON CRACKED AT STA 1760 L15L. REMOVED DAMAGED SECTION OF LONGERON AND FABRICATED SPLICE AND LONGERON SECTION INSTALLED IAW SRM'S 53-2-2 FIG10, 51-1-21, 53-2-0,51-1-20D AND DC8-53B-OO9-39.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,167 hrs · 27,140 cycles

A-PIT FRAME CORRODED AND MISDRILLED AT STA 280 L32R. CUT OUT DAMAGE, NDT VERIFIED ALL DAMAGE REMOVED PER NDTSPM 06-10-01.001. FAB REPAIR ANGLE FROM SHT 7075-0-.080 HEAT TREAT TO T6 PER DPS7.00-1. FAB FILLERS FROM SHT 7075T6-.080. INSTALLED ALL PARTS REF'S DC8-53A-011, SRM 53-4-1 FIG 40 SHT 9, 51-1-8, 51-1-20D.

Part: WEB — CRACKED (L1 DOOR FRAME) · airframe 66,167 hrs · 27,140 cycles

INSPECTION TYPE:C1, L1 DOOR FWD TORQUE WEB CRACKED BELOW SWITCH PANEL, NEAR L16L STA 25. STOP DRILLED CRACK AND NDT VERIFIED PER 53-2-0, NDT/SPM06-10-01.001. FAB REPAIR ANGLE FROM SHT7075T6-.063, TREAT, PRIME AND INSTALL SAME REF SRM 53-2-0, 51-1-8, 51-1-21, 51-1-20D, DWG5597646.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,167 hrs · 27,140 cycles

LWR CARGO PIT STA 1140 L34R UPPER FWD FITTING CRACKED ON THE FRAME. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: PRESSURE BLKHD — CRACKED (FUSELAGE) · airframe 66,167 hrs · 27,140 cycles

MAIN CABIN, AFT PRESSURE BULKHEAD CRACKED, RBL 50 UPPER SIDE. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER, FILLERS AND FINGER DOUBLER IAW SRM'S 53-2-5 FIG 14A, 51-1-21, 51-1-20D AND DWG SRO8530007.

Part: FITTING — CRACKED (THRUST REVERSER) · airframe 66,167 hrs · 27,140 cycles

NR 4 ENG OTBD T/R COWL HAS CRACK (0.625) IN UPPER CORNER FITTING, JUST AFT OF UPPER BLOCKER DOOR. (TRANSLATING COWL) STOP DRILLED CRACK AND INSTALLED TWO STIFFENERS IAW CFM-7830-5209-A AND SRM 51-1-20D.

Part: FITTING — CRACKED (THRUST REVERSER) · airframe 66,167 hrs · 27,140 cycles

INSPECTION TYPE:C1 FITTING CRACKED AT LOWER CORNER OF NR 1 OUTBOARD T/R BLOCKER DOOR POCKET. STOP DRILLED CRACK. FABBED STIFFENER AND REPAIR ANGLE AND INSTALLED IAW EO CFM-7830-5209 APPROX B.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

EMERGENCY EXIT LIGHTS DO NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK UNIT; SYSTEM OPS CHECK NORMAL IAW MM33-50-01-2.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK. OPS CHECK GOOD IAW MM 33-50.

Part: LINE — RUPTURED (RT MLG)

AFTER LANDING LOST ALL HYDRAULIC PRESSURE AND QUANTITY. AIR BRAKE USED TO STOP AIRCRAFT. FOUND RT MLG BOGIE TRIM CYLINDER PRESSURE LINE RUPTURED, REPLACED SAME. SERVICED RESERVOIR, BLED HYDRAULIC PUMPS, OPERATED ALL HYDRAULIC POWERED SYTEMS TO REMOVE AIR FROM SYSTEM. CHECKED CASE DRAIN FILTERS AS A PRECAUTION. NO METAL FOUND.

Part: SWITCH — INOPERATIVE (COCKPIT)

EMERGENCY EXIT LIGHT SWITCH ANNUNCIATOR LIGHT INOP. RELAMPED EMERGENCY EXIT ANNUNCIATOR, OPS CHECK OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK IAW MM 33-50-01.

Part: INTERCOSTAL — CORRODED (LOWER CARGO) · airframe 65,356 hrs · 26,471 cycles

INSPECTION TYPE: C2, STA 1400 INTERCOSTAL IS CORRODED BEYOND LIMITS AT RBL 49. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-2-0 FIG 23.

Part: FITTING — CRACKED (RT WING) · airframe 65,356 hrs · 26,471 cycles

INSPECTION TYPE: C2, RT WING STRINGER END FITTING IS CRACKED I/B OF XRS 74 AT STRINGER 51. REMOVED AND REPLACED FITTING IAW DWG 3704841, AND SRM 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,356 hrs · 26,471 cycles

INSPECTION TYPE: C2, RADIOGRAPHIC (X-RAY) INSPECTION DETECTED 4 CRACKS ON THE R-2 DOOR UPPER AFT CORNER APPROX .406, 1.11, 1.64, 1.74 INCHES IN LENGTH, AT STA 1660 LONG 10R APPROX. CUT OUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 16.

Part: FITTING — CRACKED (HORIZONTAL STAB) · airframe 65,356 hrs · 26,471 cycles

INSPECTION TYPE: C2, RT HORIZONTAL STAB L/E LOWER T-ANGLE IS CRACKED AT XFS 47. REMOVED AND REPLACED FITTING IAW DWG SE08550009, AND SRM 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,356 hrs · 26,471 cycles

INSPECTION TYPE:C2 RADIOGRAPHIC (X-RAY) INSPECTION DETECTED A CRACK ON THE R-1 DOOR LOWER AFT CORNER APPROX .700 INCHES IN LENGTH, STA190 APPROX AT LONG 20R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW SRM 53-2-0 FIG 14.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,356 hrs · 26,471 cycles

INSPECTION TYPE: C2, FLOORBEAM TO VERTICAL STIFFENER ATTACH ANGLE IS CRACKED AT STA 680 AT RBL 48. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5773275, AND SRM 51-1-20.

Part: WEB — CRACKED (TORQUE BOX) · airframe 65,356 hrs · 26,471 cycles

INSPECTION TYPE: C2, D-PIT DOOR AFT TORQUE BOX WEB IS CRACKED AND TORN AT HOLES AT STA 1440 LONG 33R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUTS. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 23.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,356 hrs · 26,471 cycles

INSPECTION TYPE:C2 REMOVE STEEL DOUBLER FROM L-2 DOOR LOWER FWD CORNER AND REPAIR PER SRM 53-2-0 FIG 18. REMOVED EXISTING REPAIR, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AROUND CUTOUT. FABRICATED AND INSTALLED DOUBLERS AND FILLER IAW SRM 53-2-0 FIG 18.

Part: SKIN — CRACKED (LEFT WING LE) · airframe 65,356 hrs · 26,471 cycles

INSPECTION TYPE:C2 LEFT WING L/E LOWER SKIN REPAIR DOUBLER SCREW HOLES HAVE COUNTERSUNK TOO DEEP AT STA XFS 307, AND IS CRACKED. REMOVED DOUBLER, STOPDRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-4087-B.

Part: AILERON — CRACKED (LT WING) · airframe 65,356 hrs · 26,471 cycles

INSPECTION TYPE: C2, LT WING OUTBOARD AILERON L/E UPPER SKIN IS CRACKED AT XA 684. REMOVED, FABRICATED AND REPLACED SKIN SECTION IAW SRM 57-8-0 FIG 4.

Part: RIB — CRACKED (RT WING L/E) · airframe 65,356 hrs · 26,471 cycles

INSPECTION TYPE: C2, RT LEADING EDGE RIB REPAIR DOUBLER IS CRACKED AT XFS 385.25. REMOVED DOUBLER, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 57-2-0 FIG 2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 65,356 hrs · 26,471 cycles

INSPECTION TYPE: C2, STA 70 LONGERON 30R IS CRACKED AT END FITTING. TRIMMED OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER AND REPAIR ANGLE IAW SAA SK 701-098.

Part: SKIN — CRACKED (LT WING)

LT WING DOUBLER SKIN CRACKED, FERRIED TO VENDOR AQUAMISED, NR 2 MAIN TANK 5788, INSTALLED DOUBLER & TRIPLER PER EO DC8-2810-6720I. H FEC INSPECTION PER NDT SPM 06-10-01.00 OF THE LT WING REAR SPAR LOWER ROOT DID NOT DETECT ANY CRACKS. VISUALLY INSPECTED ALL STRIPPED AREAS TO VERIFY NO STRUCTURAL DISCREPANCIES EXIST PER SAME EO. NO DESCREPANCIE S FOUND. APPLIED SEALANT TO AQUAMISED AREA. PERFORMED 12 HR FUEL SOA K CHECK PER DC8 MM 28-10-01. NO LEAKS NOTED.

Part: CONTROL UNIT — MALFUNCTIONED (FIRE DETECTION)

INSPECTION TYPE:N/A DIV TO SBN. EN ROUTE TO ORD AFT CARGO COMPARTMENT FIRE WARNING LIGHT ON IN FLIGHT. CREW DECLARED EMERGENCY. R&R CENTRAL CONTROL UNIT. OPS CHECK GOOD PER MM26-18-01.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A LIGHT BULBS VERY DIM WHEN EMERGENCY LIGHT SWITCH SELECTED TO ARM. SUSPECT LOW BATTERY. REMOVED AND REPLACED EMERGENCY BATTERY PACK MM 33-50-01, OPS CHECK NORMAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 65,356 hrs · 26,471 cycles

INSPECTION TYPE: C2, STA 950 INTERCOSTAL IS CRACKED BETWEEN MAIN LANDING GEAR DOORS AT RBL 4. REMOVED AND REPLACED INTERCOSTAL IAW DWG 5616306, AND SRM 51-1-20D.

Part: ENGINE — FLAMED OUT (NR 2)

INSPECTION TYPE:N/A EXPERIENCED IN FLIGHT FLAME-OUT NR 2 ENG DURING CRUISE. FLAME-OUT OCCURRED APPROX 1 MINUTE AFTER NR 2 X-FEED LEVER PLACED DOWN/OPEN. ALL MAIN BOOST PUMPS ON 1, 3 AND 4 FILL VALVES OPEN. NR 2 TANK 1000 LBS HEAVIER THAN 1, 3 + 4. PERFORMED AIR START IAW CHECKLIST. RESTART NORMAL, RETURNED TO OPS NORMAL. T/S, CHECKED FUEL QTY SYS, AND BOOST PUMPS CKS OK. SUMPED NR 2 TANK. INSPECTED, REMOVED AND REPLACED FUEL FILTER CKS GOOD. INSPECTED CDP AND CIT TUBES & LINES CKS GOOD. CHECKED MAG CHIP DETECTORS, OK. CHECKED MECH FUEL SHUTOFF LEVER, CHECKS OK. PERFORMED MAX PWR ASSUR RUN CKS GOOD PER MM.

Part: WINDOW — LEAKING (COCKPIT)

INSPECTION TYPE:IN LOUD SQUEAL FROM CAPTAIN`S CLEAR VIEW WINDOW TOP. CHECKED CAPTS CLEAR VIEW WINDOW SEAL FOUND NO EVIDENCE OF SEAL TORN. CLEANED WINDOW SEAL AND FRAME. PRESSURIZED AND NO NOTICE OF LOUD SQUEAL.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. R&R BATTERY PACK. OPS CHECKS GOOD PER DC8 MM 33-50-00.

Part: SLIDE — UNSECURE (DOOR)

INSPECTION TYPE:PFLT, DOOR SLIDE NEEDS TO BE RESECURED. REINSTALLED SLIDE.

Part: LANDING GEAR — FAILED (MLG)

INSPECTION TYPE:N/A, AFTER TAKEOFF MLG FAILED TO RETRACT. MAINTAINED AIRSPEED BELOW 230 KTS AND CLIMBED TO 15000 FT. PERFORMED GEAR HANDLE JAMMED CHECKLIST ON DESCENT TO PHL BELOW 10000 FT NOSE GEAR POSITION APPEARED. AIRCRAFT FERRY PERMIT DMI CONTROL NR D210467 COMPLIED WITH AIRCRAFT IN SAFE CONDITION FOR FERRY A/C ARRIVED SAFELY 8:30 PM THIS CLEARS D-210467 ITEM.

Part: FITTING — CRACKED (CABIN) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1, 3 STA 742 LONG 18L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751640, AND SRM 51-1-20D.

Part: WEB — CRACKED (CABIN) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1,3 STA 1300 AND 1350 LT CUSP MEMBRANE IS CRACKED. REPAIRED CUSP MEMBRANE IAW EO DC8-5330-2159.

Part: RIB — CRACKED (LT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, LEFT WING L/E LOWER RIB IS CRACKED AT XFS 360. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 728.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 741.250. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 760. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (CABIN) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1, 3 STA 1325 LONG 21L T-1 DOOR FITTING IS CRACKED AT CUSP. REMOVED AND REPLACED FITTING IAW DWG 5888714, AND SRM 51-1-20D.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, LEFT WING CENTER L/E VERTICAL ATTACH ANGLE IS CRACKED AT XS 520. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753297, AND SRM 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, LEFT WING CENTER L/E UPPER RIB IS CRACKED AT XOLDI 6.225. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (LT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, LEFT WING CENTER L/E INTERNAL DOUBLER IS CRACKED AT XFS 297.5. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-20D, 51-1-21.

Part: RIB — CRACKED (LT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, LEFT WING L/E UPPER RIBS ARE CRACKED AT XOLDI 6.225, XS 435.78, XS 442.185, XS 448.581, XS 466.651. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 835, XFS 828.75, XFS 822.5, XFS 816.25, XFS 803.75, XFS 797.5, XFS 785, XFS 766.25. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, LEFT WING L/E LOWER RIBS ARE CRACKED AT XFS 616.25, XFS 641.25, XFS 653.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, LEFT WING CENTER L/E UPPER RIBS ARE CRACKED AT XFS 347.75, XFS 354, XFS 372.75, XFS 379. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, LEFT WING L/E LOWER RIB IS CRACKED AT XFS 828.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (LT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 597.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600, AND SRM 51-1-20D, 51-1-21.

Part: RIB — CRACKED (LT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, LEFT NR 2 STUBWING HAS UPPER RIB CRACKED AT XILD .7095. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (LT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769600, AND SRM 51-1-20D, 51-1-21, AND REPAIRED CRACKED SKIN IAW EO DC8-5720-7767A.

Part: DOUBLER — BROKEN (LT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, LEFT WING L/E LOWER INTERNAL DOUBLER HAS A CORNER BROKEN OFF AT XS 520. REMOVED AND REPLACED DOUBLER AND SKIN IAW DWG 5769759, AND SRM 51-1-20D, 51-1-21.

Part: ANGLE — CRACKED (RT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, RIGHT WING CENTER L/E VERTICAL ATTACH ANGLE AT XS 520 IS CRACKED. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753297, AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (RT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, RIGHT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 597.5. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769600, AND SRM 51-1-20D, 51-1-21.

Part: DOUBLER — CRACKED (RT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1,3, RIGHT WING NR 4 STUB WING L/E LOWER DOUBLER IS CRACKED AT XW485. REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM 57-2-1A.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1,3, STA 134 AND 140 HAS CRACKED SHEAR TIES BETWEEN LONG 5L AND 6L. REMOVED, FABRICATED, AND REPLACED SHEAR TIES IAW DWG 5772785, AND SRM 51-1-20D, 51-1-21.

Part: DOUBLER — CRACKED (RT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, RIGHT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769600, AND SRM 51-1-20D, 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, RIGHT WING L/E UPPER RIBS ARE CRACKED AT XFS 616.25, XFS 622.250. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, RIGHT WING L/E UPPER RIBS ARE CRACKED AT FASTENER END AT XFS 297.5, XFS 354. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (CARGO BAY) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1, 3 STA 290 LONG 33R FWD LOWER LATCH BACKUP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754023, AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, STA 440 - 460 LONG 34R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750330, AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (RT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, RIGHT WING CENTER L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 335. 250. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (CARGO BAY) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, STA 600 - 620 LONG 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 51-1-20D.

Part: DOUBLER — CORRODED (CARGO BAY) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1, 3 STA 600 - 620 FINGER DOUBLER IS CORRODED BEYOND LIMITS BETWEEN LONG 31L-31R. REMOVED, FABRICATED, AND REPLACED FINGER DOUBLER IAW DWG 5779913, AND SRM 51-1-20D, 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1,3 RIGHT WING L/E UPPER RIBS ARE CRACKED AT FASTENER END AT XS442.185, XS448.581, XS467.323, XS478.897. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: LONGERON — CORRODED (CARGO BAY) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1,3 STA 600 - 620 LONG 36 SPLICE AND LONGERON ARE CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING AND REPAIRED LONGERON IAW DWG 3750330, AND SRM 53-2-2 FIG 10, 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1, 3, STA 350 RT LOWER CUSP FITTING IS CRACKED AT LONG 21R. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3754047 AND SRM 51-1-20D.

Part: RIB — CRACKED (TE FLAPS) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, RIGHT INBOARD FLAP RIB IS CRACKED AT AFT SPAR MOST I/B RIB AT XCW 64. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (CARGO BAY) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, STA 440 - 460 LONG 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 51-1-20D.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, STA 680 LBL 48 VERTICAL FLOORBEAM SUPPORT ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5773275, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, STA 680 BL 0 FLOORBEAM VERTICAL SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5773275, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, STA 742 LBL 24 FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755222, AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, STA 717 LBL 24 FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3773906, AND SRM 51-1-20D.

Part: SEAT TRACK — BROKEN (CABIN) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1,3 STA 250 BL 0 MAIN CABIN SEAT TRACK HAS A BROKEN TANG. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 6D.

Part: FITTING — CRACKED (CABIN) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, STA 822 RBL 63 INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 4753360, AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, STA 1740 LONG 15R IS CRACKED. REMOVED, FABRICATED, AND REPLACED LONGERON SECTION IAW DWG 5649327, AND SRM 53-2-2 FIG 10.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, STA 720 LBL 63 FLOORBEAM VERTICAL SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3616948, AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, STA 822 LBL 24 FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755222 AND SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1, 3 STA 590 RBL 24 SEAT TRACK CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A.

Part: FITTING — CORRODED (CABIN) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1, 3 STA 940 FRAME FITTING AT RBL 60 IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED FRAME FITTING IAW 8110-3 APPROVED 8110-3 DH SK 701-332, AND SRM 51-1-20D, 51-1-21, 53-1-0.

Part: FITTING — CRACKED (CABIN) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, STA 781 LBL 24 FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3773906, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1,3 STA 340 LONG 33R O/B BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755847, AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, STA 781.5 FLOORBEAM ATTACH FITTING IS CRACKED AT RBL 24. REMOVED AND REPLACED FITTING IAW DWG 3755222 AND SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, STA 1670 - 1705 SEAT TRACK IS CORRODED BEYOND LIMITS AT RBL 24. REPAIRED SEAT TRACK SECTION IAW SRM 53-2-3 FIG 14.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, STA 1717 TO 1725 LBL 10 FLOOR SUPPORT IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED SUPPORT IAW DWG 5755032 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1,3 STA 857 LONG 7R END FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3779659, AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, STA 759 LONG 18L INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751640, AND SRM 51-1-20D.

Part: FITTING — CRACKED (MAIN CABIN) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1,3 STA 834 - 857 LONG 1 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750521, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, STA 675 LONG 4L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762, AND SRM 51-1-20D, 51-1-21, 51-1-23.

Part: FITTING — CRACKED (CABIN) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, STA 680 LONG 11L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751625, AND SRM 51-1-20D.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1, 3 STA 1766 RBL 10 - 18 FLOOR SUPPORT IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED SUPPORT IAW DWG 5753522, AND SRM 51-1-20D, 51-1-21A.

Part: CLIP — CORRODED (CABIN) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, STA 1766 LONG 6L INTERCOSTAL TO BULKHEAD ATTACH CLIP IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED CLIP IAW DWG 5773844, AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1&3, STA 717 LONG 18L INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 4751640, AND SRM 51-1-20D.

Part: FITTING — CRACKED (A/C BAY) · airframe 64,392 hrs · 25,744 cycles

INSPECTION TYPE:C1,3 STA 67 LONG 24R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4611067, AND SRM 51-1-20D, 51-1-21.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:P/F, EMERGENCY LIGHT WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK.

Part: LIGHT — SMOKE (CABIN)

INSPECTION TYPE:N/A, SMOKE IN COCKPIT WITH FUMES BEING SMELLED. SMOKE CAME FROM CO -PILOTS SIDE TO RIGHT OF SEAT AND BELOW WINDOW. ALSO, NOTICE BY F/E''S WORK TABLE LIGHT. CB POPPED IN BACK, DIVERTED TO MSP IMMEDIATLELY. REMOVED ALL ACCESS PNLS FROM F/O''S KICK PANEL AFT TO C/B PANELS AND COCKPIT OVERHEAD LIGHTING PANEL. INSPECTED ALL WIRES, BUNDLES AND COMPONENTS, NO DEFECTS NOTED. ALSO, RAN BOTH PACKS WITH NO DEFECTS, AS NOTED BY CREW AND VERIFIED BY MX 5AMP F/E FLOOD WAS POPPED. DEFERRED COCKPIT OVERHEAD LIGHTING. C/BS COLLARED AND PLACARD INSTALLED.

Part: CONTROL VALVE — FAILED (MLG WW)

AFTER RETRACTING THE GEAR, GEAR UNLATCHED LIGHT ILLUMINATED. RECYCLED THE GEAR AND NOTED LEFT GEAR DOWN GREEN LIGHT ILLUMINATED IMMEDIATELY, THE RIGHT ALTERNATE DOORS LIGHT ILLUMINATED THEN WENT OUT. HOWEVER, THE LEFT ALT DOOR LIGHT NEVER ILLUMINATED. ALSO, THE SPOILER PRESSURE REMAINED AT 3000 PSI THE WHOLE TIME. REMOVED AND REPLACED MLG CONTROL VALVE PER MM 32-31-00 PG 203, SAFTIED AND ADJUSTED.

Part: WIRE — SHORTED (COCKPIT)

EMERGENCY EXIT LIGHTS INOP. T/S AND FOUND WIRE LG19DW22 SHORTED TO GROUND AT COCKPIT DOME LIGHT ASSY. REPAIRED WIRE LIGHT, OP CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATT PACK, OPS CHECK GOOD.

Part: ACTUATOR — FAILED (NLG)

INSPECTION TYPE-N/A, UPON LOWERING LANDING GEAR HANDLE ON APPROACH, A VERY LOUD VIOLENT NOISE WAS HEARD FROM WHAT SEEMED LIKE THE AREA OF THE NOSE GEAR. THE RT AND NOSE GEAR INDICATED DOWN AND LOCKED, THERE WAS NO GREEN GEAR DOWN LIGHT FOR THE LEFT GEAR. AT THE SAME TIME HYD SYS PRESS INDICATED ZERO AND THE HYD QTY WAS MOVING QUICKLY TOWARDS EMERGENCY HYD PUMPS SELECT BYPASS. ACCOMPLISHED LOSS OF ALL HYD CHECKLIST, LANDED SAFELY.

Part: SEAT TRACK — CORRODED (BS 1540)

INSPECTION TYPE-C, SEAT TRACK CORRODED AT FS 1540 LBL 45. REPAIRED IAW SRM ADDN DC8-5320-5167-C.

Part: WEB — CRACKED (WS 23)

INSPECTION TYPE:C NR 2 MAIN TANK VERT WEB PREVIOUS REPAIRED CRACK HAS EXTENDED BEYOND DOUBLER AT STA XRS 23 STR 13. REPAIRED IAW DH SK 701-152 AND DH SK 701-453.

Part: SEAT TRACK — CORRODED (BS 1520)

INSPECTION TYPE-C, SEAT TRACK CORRODED AT FS 1520, LBL 50. REMOVED DAMAGED SEAT TRACK FROM FS 1530 TO 1580, FABRICATED AND REPLACED SEAT TRACK IAW SRM EO DC8-5320-5167-C AND SRM 51-3-0.

Part: SEAT TRACK — CORRODED (BS 1470-1480)

INSPECTION TYPE-C, SEAT TRACK CORRODED AT FS 1470 TO 1480 UNDER FLOORBEAM FLANGE LBL 60 VIEWED FROM D PIT FLOOR LOOKING UP. REPAIRED IAW SRM 53-2-3.

Part: SEAT TRACK — CORRODED (BS 1490-1500)

INSPECTION TYPE-C, SEAT TRACK CORRODED AT 1500 TO 1490, RBL 60. REMOVED DAMAGED SEAT TRACK FROM FS 1490 TO 1550, FABRICATED AND REPLACED SEAT TRACK IAW EO DC8-5320-5167-C, SRM 51-3-0.

Part: STIFFENER — CORRODED (BS 855)

INSPECTION TYPE-C, VERTICAL STIFFENER AT FS 855, LBL 55 IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED STIFFENER IAW DWG 5646674 AND SRM 51-1-21 AND 51-3-0.

Part: SHEAR TIE — CRACKED (BS 1480)

INSPECTION TYPE-C, SHEAR TIE CRACKED AT FS 1480, BETWEEN LONG 34L AND 35L. CUT OUT DAMAGED SHEAR TIE AND REPAIRED IAW SRM 53-2-0 FIG 2A.

Part: SPACER — CORRODED (BS 780)

INSPECTION TYPE-C, AIRCRAFT STRUCTURE UNDER VERTICAL FITTING AT FS 780 AND RBL 55 IS BADLY CORRODED. REMOVED AND REPLACED SHIM PLATE IAW SRM 51-3-0.

Part: FLOORBEAM — CORRODED (BS 879)

INSPECTION TYPE-C, UPPER TANG OF FLOORBEAM AT FS 879, RBL 68 IS CORRODED. REPAIRED FLOORBEAM IAW DHC SK701-677.

Part: FLOORBEAM — CORRODED (BS 879)

INSPECTION TYPE-C, FS 879 FLOORBEAM AT LBL 60 IS CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM IAW DH SK701-681.

Part: LONGERON — CRACKED (BS 85-95)

INSPECTION TYPE-C, LONG 35R FS 85 TO 95 IS CRACKED UNDER THE SPLICE. REMOVED, FABRICATED AND REPLACED LONGERON IAW SRM 53-2-2 AND 51-1-2OD.

Part: CLIP — CORRODED (BS 855)

INSPECTION TYPE-C, FS 855 REAR SPAR IS CORRODED BEYOND LIMITS AT LBL 28. REMOVED AND REPLACED DAMAGED CLIP IAW SRM 51-1-20D AND 51-3-0.

Part: LONGERON — MISDRILLED (BS 220-240)

INSPECTION TYPE:C LONGERON 35R AT FS 220-240 HAS A ROW OF FASTENERS WITH NO OR SHORT ED. REPAIRED LONGERON 35R IAW DH SK 701-833.

Part: FRAME — CRACKED (BS 1480)

INSPECTION TYPE-C, FUSELAGE FRAME CRACKED AT FS 1480, LONG 33L. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53-2-0 FIG 2.

Part: FITTING — CRACKED (BS 920)

INSPECTION TYPE-C, AFT TEE FITTING IN KEEL BEAM LT FS 920 HAS A 8.75 CRACK. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLES IAW DWG 5754125, SB-53-68, AND SRM 51-1-20D.

Part: SKIN — CRACKED (WS 364)

INSPECTION TYPE-C, RT WING UPPER SKIN AT STA 364 AND STR 10 IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 21A.

Part: FRAME — CRACKED (BS 55)

INSPECTION TYPE-C, FS 55 FRAME IS CRACKED AT LONG 24R. CUT OUT DAMAGED SECTION AND REPAIRED FRAME IAW SR DWG 0853008 AND SRM 53-2-0.

Part: SEAT TRACK — CORRODED (BS 1370)

INSPECTION TYPE:C SEAT TRACK AT FS 1370, AT BL 0 HAS CORROSION OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK FROM FS 1370 TO 1530 AT BL 0 AND SPLICED IN A NEW SECTION OF TRACK IAW SRM 53-2-3.

Part: SEAT TRACK — CORRODED (BS 920-940)

INSPECTION TYPE-C, SEAT TRACK BETWEEN FS 920 AND 940, RBL 60 IS CORRODED OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK BETWEEN FS 720 AND 950, SPLICED IN A NEW SECTION IAW EO DC8-5320-5167-C.

Part: FITTING — CRACKED (BS 1150)

INSPECTION TYPE:C INTERCOSTAL FITTING AT FS 1150 AND LONGERON 35R IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FLOORBEAM — CRACKED (BS 340)

INSPECTION TYPE-C, A PIT FLOORBEAM CRACKED AT FS 340 AND RBL 52. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-1-20D AND 51-1-21.

Part: SEAT TRACK — CORRODED (BS 1500)

INSPECTION TYPE-C, SEAT TRACK BLOWN AT FS 1500 AT RBL 50. REMOVED DAMAGED SEAT TRACK BETWEEN FS 1470 TO 1550, FABRICATED AND REPLACED SEAT TRACK IAW SRM 53-2-3 FIG 6A, 51-3-0.

Part: FITTING — CRACKED (BS 270)

INSPECTION TYPE-C, BATHTUB FITTING CRACKED AT FS 270 AND LONG 30L. REMOVED AND REPLACED FITTING IAW 51-1-20D AND 53-2-0 FIG 2D.

Part: SEAT TRACK — CORRODED (BS 1060-1080)

INSPECTION TYPE:C SEAT TRACK AT FS 1060-1080 AT RBL 60 HAS HEAVY CORROSION. REMOVED AND REPLACED SEAT TRACK FROM FS 1030 TO 1110, RBL 60 IAW SRM 53-2-3.

Part: SEAT TRACK — CORRODED (BS 1500)

INSPECTION TYPE:C SEAT TRACK AT FS 1500 AT LBL 50 HAS HEAVY CORROSION. CUT OUT DAMAGED SEAT TRACK FROM FS 1270 TO 1520, LBL 50 AND SPLICED IN A NEW SECTION IAW SRM 53-2-3.

Part: FITTING — CORRODED (BS 1180)

INSPECTION TYPE:C FS 1180, LONGERON 29L BATHTUB FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-1-20D.

Part: FITTING — CRACKED (BS 1240)

INSPECTION TYPE:C INTERCOSTAL END FITTING CRACKED FS 1240 AT LONGERON 33R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SEAT TRACK — SPLIT (BS 1060)

INSPECTION TYPE:C SEAT TRACK SPLIT AND CORRODED AT FS 1060, LBL 60. REMOVED DAMAGED SEAT TRACK FROM FS 1000-1300, LBL 60 IAW SRM 53-2-3.

Part: FRAME — CORRODED (BS 1080)

INSPECTION TYPE-C, HEAVY CORROSION AND BULGING FRAME FS 1080 FROM L33R TO 31R. REPAIRED IAW SRM 53-2-0.

Part: FITTING — CRACKED (BS 1050)

INSPECTION TYPE-C, LONG 31R SPLICE IS CRACKED AT FS 1050. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 90)

INSPECTION TYPE-C, HEAVY CORROSION ON LONG 35R SPLICE FITTING AT FS 90. REMOVED AND REPLACED SPLICE FITTING IAW SRM 53-2-2 FIG 10.

Part: SEAT TRACK — CORRODED (BS 1060)

INSPECTION TYPE-C, SEAT TRACK BLOWN AT FS 1060, RBL 50. REMOVED DAMAGED SEAT TRACK BETWEEN FS 1010 TO 1106, FABRICATED AND REPLACED SEAT TRACK IAW SRM 53-7-1, 51-1-21 AND 51-3-0.

Part: FITTING — CORRODED (BS 960-980)

INSPECTION TYPE-C, HORIZONTAL FITTING HAS EXFOLIATION CORROSION THAT IS OUT OF LIMITS AT FS 960 TO 980, RBL 48. REMOVED AND REPLACED FITTING IAW SRM 51-1-21, 51-3-0.

Part: FITTING — CRACKED (BS 1050)

INSPECTION TYPE:C LONGERON 27R SPLICE FITTING AT FS 1050 IS CRACKED. REMOVED AND REPLACED LONGERON SPLICE FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 960)

INSPECTION TYPE-C, CUSP TO FRAME END FITTING, RT SIDE AT 960, HAS EXFOLIATION CORROSION. REMOVED, FABRICATED AND REPLACED FITTING IAW DHC SK701-669 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 815)

INSPECTION TYPE-C, FITTING AT FS 815 AND LBL 24 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-1-21.

Part: FITTING — CRACKED (BS 776)

INSPECTION TYPE-C, FITTING AT FS 776 AT RBL 24 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-1-21.

Part: FITTING — CORRODED (BS 780)

INSPECTION TYPE:C FLOORBEAM TO CENTER TANK ATTACH ANGLE AT FS 780, LBL 55 HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 385.25)

INSPECTION TYPE-C, RT WING L/E RIB AT XFS 385.25 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 780)

INSPECTION TYPE-C, VERTICAL FITTING COMPLETELY BROKEN AT RBL 55 AT FS 780. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-3-0.

Part: FITTING — CRACKED (BS 940)

INSPECTION TYPE-C, UNDERSIDE OF W/W CENTER KEEL BEAM ATTACH FITTING IS CRACKED AT FS 940. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (BS 703)

INSPECTION TYPE-C, INTERCOSTAL FITTING CRACKED AT FS 703 AND LONG 19R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SKIN — CRACKED (RT AILERON)

INSPECTION TYPE:C RT INBD AILERON UPPER L/E SKIN AT THE MANUAL REVERSION MECH IS CRACKED. CUT OUT DAMAGED SKIN AND SPLICED IN NEW SECTION IAW SRM 57-2-0.

Part: ANGLE — CRACKED (WS 250.089)

INSPECTION TYPE-C, RT WING L/E INBOARD SIDE OF THE XS 250.089 RIB, THE VERTICAL ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753293 AND SRM 51-1-20D.

Part: FITTING — CORRODED (BS 879)

INSPECTION TYPE-C, FS 879 FITTING ABOVE LONG 24R HAS MODERATE CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 8.

Part: SEAT TRACK — CORRODED (BS 770)

INSPECTION TYPE:C HEAVY CORROSION ON SEAT TRACK LOR FLANGE AT FS 770 AT LBL 25. REMOVED DAMAGED SECTION OF SEAT TRACK, FS 650-875 LBL 25, PER SRM 53-2-3.

Part: WEB — CORRODED (BS 960-980)

INSPECTION TYPE-C, HORIZONTAL FITTING HAS CORROSION EXTENDING UNDER FITTING AND POPPED FASTENER BETWEEN FS 980 AND 960 RBL 48. REPAIRED IAW DH SK701-670.

Part: SKIN — CRACKED (WS 74)

INSPECTION TYPE:C LT WING UPPER SKIN AT XRS 74 AT STR 8 IS CRACKED AT A FASTENER HOLE. CUT OUT DAMAGED AREA AND REPAIRED SKIN IAW SRM 57-2-1 FIG 10.

Part: RIB — CRACKED (WS 660)

INSPECTION TYPE:C LT WING L/E UPPER RIB CRACKED AT XFS660. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 630)

INSPECTION TYPE-C, LT WING L/E RIB AT XFS 630 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (WS 597.5)

INSPECTION TYPE-C, RT WING L/E LWR SKIN AT XFS 597.5 IS CRACKED AT THE DRAIN HOLE. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-4087-B.

Part: DOUBLER — CORRODED (RT WING)

INSPECTION TYPE-C, RT WING L/E AT ACCESS PANEL 519B, THE INTERNAL DOUBLER HAS MODERATE EXFOLIATION CORROSION. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 3641256 AND SRM 51-1-20D AND 51-1-21.

Part: SKIN — CORRODED (WS 399)

INSPECTION TYPE-C, RT WING UPPER SKIN AT STR 8 AND STA XW 399 HAS INTERGRANULAR CORROSION AND IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 32.

Part: SKIN — CRACKED (WS 358)

INSPECTION TYPE-C, LT WING UPPER SKIN AT XRS 358 AT THE REAR SPAR IS CRACKED AT THE AFT FASTENER. REPAIRED SKIN IAW DHC SK701-230.

Part: SKIN — CRACKED (WS 360.25)

INSPECTION TYPE-C, RT WING L/E UPPER SKIN AT XFS 360.25 IS CRACKED AT A FASTENER HOLE 2 INCHES FWD OF THE SPAR. REPAIRED IAW SRM 57-3-2.

Part: SKIN — CRACKED (RT WING LE)

INSPECTION TYPE-C, RT WING L/E UPPER SKIN AT XFS 597.5 IS CRACKED 2 INCHES FWD OF THE SPAR. CUT OUT DAMAGED AREA AND REPAIRED IAW DHC SK 701-160 AND SRM 57-2-1 FIG 38.

Part: LIGHT — MALFUNCTIONED (CABIN)

EEL ARM DISARM INOP. EEL OPS NORMAL PER MM33-50-01. NO DEFECTS NOTED.

Part: FLOORBEAM — CORRODED (BS 902)

INSPECTION TYPE-C, STA 902 RBL 34 TO 55.5 THE FLOORBEAM HAS CORROSION THAT IS OUT OF LIMITS. REPAIRED FLOORBEAM IAW DHC SK 701-673 REV B.

Part: SLIDE — DAMAGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY ESCAPE SLIDE GIRT BAR HAS BEEN PULLED OUT TO FAR FROM STORAGE AREA AND NEEDS TO BE REPLACED. EMERGENCY SLIDE DEFERRED PER MMOC CONTR NR D-140201. SLIDE REMOVED AND STOWED IN THE BELLY COMPARTMENT 32. COURIER SEATS TAPED REF EO DC8-2560-7565. REMOVED AND REPLACED EMERGENCY SLIDE PER 25-60-01. THIS CLEARS D-140201 (P/N 5156100-4DG-DME) (S/N 91) ON, (S/N 1G1) OFF, LOG PAGE 859813.

Part: ANGLE — CORRODED (BS 970)

INSPECTION TYPE:C, KEEL BEAM ATTACH ANGLE AT F/S 970 CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-3-0, 51-1-20D, 51-1-21, AND DWG 5614943.

Part: FITTING — CRACKED (BS 920)

INSPECTION TYPE-C, FS 920 RBL 65, SUB FLOOR FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-3-0, 51-1-20D, AND DHC SK-701-042.

Part: SKIN — CORRODED (BS 1691)

INSPECTION TYPE:C, AFT FUSELAGE SKIN F/S 1691 AT LONG 30R TO 28R CORRODED BEYOND LIMITS. REPAIRED IAW SRM 51-1-20D, 51-1-21, AND 53-2-1.

Part: FLOORBEAM — CRACKED (BS 1680)

INSPECTION TYPE-C, FLOORBEAM UPPER FLANGE CRACKED FS 1680 LBL 48. REPAIRED IAW DHC SK 701-043.

Part: DOUBLER — CORRODED (BS 1615)

INSPECTION TYPE:C, AFT ACCY COMPARTMENT HEAVY INTERGRANULAR CORROSION ON SKIN DOUBLER F/S 1615 L-26L TO 27L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, 51-1-20D, AND DWG 5779934.

Part: FLOORBEAM — CORRODED (BS 1660)

INSPECTION TYPE-C, MODERATE CORROSION ON FLOORBEAM FS 1660 LBL 48. REPAIRED IAW DHC SK 701-044.

Part: MEMBRANE — CRACKED (BS 1615)

INSPECTION TYPE:C, AFT ACCY COMPARTMENT SUB FLOOR MEMBRANE CRACKED F/S 1615 JUST INBD OF L-21R. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 AND 53-4-1 PG 55 AND 56.

Part: DOUBLER — CORRODED (BS 920-940)

INSPECTION TYPE:C, F/S 920-940 RBL 59-65 - SUB FLOOR FINGER DOUBLER IS BULDING AND HAS NUMEROUS SHEARED RIVETS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, 53-7-3 FIG 4, AND DWG 5645332.

Part: DOUBLER — CORRODED (BS 940-960)

INSPECTION TYPE:C, F/S 940-960 RBL 59-65 - SUB FLOOR FINGER DOUBLER IS BULDGING AND HAS NUMEROUS SHEARED RIVETS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-7-3 FIG 4, 51-1-21, 51-1-14, AND DWG 5645332.

Part: SEAT TRACK — CORRODED (BS 1306-1310)

INSPECTION TYPE:C, MAIN CABIN F/S 1306-1310 LBL 24, SEAT TRACK HAS HEAVY CORROSION, LOCK TANGS ARE SEPARATING. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-2-3, 51-3-0, AND 51-1-11.

Part: FITTING — CORRODED (BS 900)

INSPECTION TYPE:C, FRAME 900 FWD SIDE BELOW PRESSURE FLOOR JOGGLED PLATE FITTING EXFOLIATED, RT W/W. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D, 51-1-21, 51-3-0, AND DWG 2646348.

Part: DOUBLER — CORRODED (BS 960-980)

INSPECTION TYPE:C, F/S 960-980 RBL 59-65 - FINGER DOUBLER IS BULGING AND HAS SEVERAL SHEARED RIVETS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, 53-7-3, AND DWG 5645332.

Part: DOUBLER — CORRODED (BS 880-900)

INSPECTION TYPE:C, F/S 880-900 RBL 59-65 - SUBFLOOR FINGER DOUBLER IS CORRODED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-7-3, 51-1-21, AND DWG 5645332.

Part: SEAT TRACK — CORRODED (BS 942)

INSPECTION TYPE:C, F/S 942 LBL 24, SEAT TRACK HAS HEAVY CORROSION. REPAIRED TRACK IAW SRM 53-2-3, 53-1-0.

Part: SEAT TRACK — CORRODED (BS 563-586)

INSPECTION TYPE:C, F/S 563 AND 586 LBL 59, SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-2-3, 51-1-11, 51-1-20.

Part: RIB — CRACKED (WS 821)

INSPECTION TYPE:C, RT WING L/E AT STA XFS 821.00 - THE L/E RIB IS CRACKED AT THE AFT UPPER END. REPAIRED L/E RIB IAW SRM 57-3-1 FIG 7 AND 51-1-20D.

Part: SEAT TRACK — CORRODED (BS 680)

INSPECTION TYPE:C, F/S 680, 635-642 RBL 59, SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK FROM F/S 610-730 IAW SRM 51-3-0, 51-1-11, 53-2-3, 51-1-21, AND 51-1-20.

Part: FITTING — CRACKED (BS 980)

INSPECTION TYPE:C, F/S 980 RBL 65 ON SUB FLOOR, TIE FITTING IS CRACKED IN HALF. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D, AND DWG 4647365.

Part: SEAT TRACK — CORRODED (BS 586)

INSPECTION TYPE:C, F/S 586 LBL 44 SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 51-1-21, 53-2-3, AND 53-3-0.

Part: FRAME — CRACKED (BS 940)

INSPECTION TYPE-C, FS 940 LBL 65 FRAME HAS 3.5 IN RADIUS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DHC SK-701-894.

Part: RIB — CRACKED (WS 636)

INSPECTION TYPE:C, RT WING L/E AT STA XFS 636.00 - THE UPPER L/E RIB IS CRACKED AT THE AFT END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-20D.

Part: RIB — CRACKED (WS 478.897)

INSPECTION TYPE:C, LT WING CENTER L/E RIB AT STA XS478.897 IS CRACKED AT THE AFT UPPER END. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.

Part: SUPPORT — CRACKED (BS 1220)

INSPECTION TYPE:C, FLOORBEAM SUPPORT LWR SUPPORT FITTING CRACKED AT F/S 1220 RT SIDE. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-3-0 51-1-20D, AND DWG 3754025.

Part: RIB — CRACKED (WS 322.75)

INSPECTION TYPE:C, LT WING CENTER L/E RIB AT XFS 322.75 IS CRACKED AT THE AFT UPPER END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-20D, AND 51-1-21.

Part: FRAME — CRACKED (BS 55)

INSPECTION TYPE:C, F/S 55 FRAME AT STR 24L HAS 2 CRACK IN RADIUS. REPAIRED IAW SRM 53-2-0.

Part: FLOORBEAM — CORRODED (BS 59)

INSPECTION TYPE-C, FS 59 FLOORBEAM TOP FLANGE LWR SURFACE HAS SEVERE CORROSION AT RBL 36. REPAIRED IAW DHC SK 701-539.

Part: TRANSFORMER — FAILED (COCKPIT)

INSPECTION TYPE:N/A, CREW SMELLED SMOKE FUMES BEFORE DESCENT. REPLACED OVERHEAD GLARESHIELD POWER TRANSFORMER.

Part: CONTROL VALVE — BY PASSING (RT MLG ANTI-SKID)

INSPECTION TYPE-N/A, ON BEGINNING OF TAKEOFF ROLL, AIRCRAFT PULLED RIGHT AND OTHER AIRCRAFT REPORTED FIRE ON RT BRAKE. ABORTED TAKEOFF. FOUND THAT THE NR 3 BRAKE WAS NOT GETTING PROPER HYD PRESS AND THE RT OUTBD ANTI-SKID CONT VLV HARNESS WAS CRUSHED. REMOVED AND REPLACED RT INBD ANTI-SKID CONT VLV PER M/M 32-43-03 AND REMOVED AND REPLACED RT OUTBD ANTI-SKID CONT VLV HARNESS AND CONNECTOR P1-1807 PER WDM 32-40-01.

Part: FITTING — CRACKED (BS 793)

INSPECTION TYPE: BCK. KEEL CAP BATHTUB FITTING AT FS 793 RT HAS VERTICAL CRACK, NEED AOG TO REMOVE 4 BOLTS IN KEEL BEAM FOR REMOVAL AND REPLACEMENT OF FITTING. NOTE: BOLTS ARE IN FUEL TANK. REMOVED AND REPLACED 4 BOLTS IN KEEL BEAM FITTING AT FS 793 RT. CLEANED AND SEALED IAW 28-10-01. MM LEAK CHECK DUE, LEAK CHECK GOOD.

Part: FITTING — CRACKED (FS 1152)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, FITTING ON LONGERON 31R CRACKED FS 1152. REPLACED FITTING PER SRM 51-1-20D.

Part: LONGERONS — CRACKED (FS 250-310)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, LONGERONS CRACKED TOP O/B FLANGE, F.S 260. REPLACED LONGERON, SECTION F.S. 250-310, PER SRM 51-1-20D.

Part: LONGERON — CRACKED (FS 340-348)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, 4 CRACKS IN O/B LOWER FLANGE OF LONGERON 35L 340 TO 348. REPLACED LONGERON SECTION FS 190 TO 390 PER SRM 51-1-20D.

Part: LONGERON — CRACKED (FS 260)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LONGERON 35L CRACKED FS 260. REPLACED LONGERON SECTION PER SRM 51-1-20D.

Part: SKIN — CORRODED (FS 190-450)

WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION AT FUSE. SKIN FS 190-450. REPLACED SKIN PER DAC DRAWING NR 5755271.

Part: DOUBLER — CORRODED (FS 220-260)

WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION INNER DOUBLER FS 220-260 LONGERON 35L-31R. REPLACED DOUBLER PER SRM 51-1-20D AND SRM 51-1-21.

Part: RIBS — CRACKED (WS 138/328)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT WING L/E 2 EACH RIBS CRACKED AT STA XFS138, XFS 328. REPAIRED RIBS PER MM 27-00-00, FIG. 801.

Part: FITTING — CRACKED (FS 1230)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, B/T FITTING CRACKED AT F.S. 1230, BETWEEN LONGERONS 33R-34R. REPLACED FITTING PER SRM 51-1-20D.

Part: LONGERONS — CRACKED (FS 1230)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, B/T FITTING CRACKED F.S. 1230, BETWEEN LONGERONS 33R-34R. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CRACKED (FS 1200)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CRACKED FITTING F.S. 1200, BETWEEN LONGERONS 33R AND 34R. REPLACED FITTING PER SRM 53-1-0.

Part: RIBS — CRACKED (LT WING LE)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, LT WING L/E, 3 EACH, RIBS CRACKED AT STA. XFS 767, 846, 679. REPAIRED RIBS PER MM 57-00-00, FIG. 801.

Part: WEB — CRACKED (RT WING LE)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT WING L/E LOWER SURFACE CRACKED IN WEB BETWEEN STA. XFS 608-614. REPAIRED WEB PER SRM 57-2-0.

Part: FITTING — CRACKED (FS 70)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, FS 70 LONGERON 21R END FITTING CRACKED. REPLACED FITTING PER SRM 51-1-20D.

Part: KEEL BEAM — CRACKED (FS 940)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, KEEL BEAM SPLICED RT SIDE CRACKED AT F.S. 940. REPLACED SPLICE PER SRM 51-3-0.

Part: FITTING — CRACKED (LT HORIZ STAB)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT HORIZ STAB CRACKED ON T-FITTING LOWER FWD I/B. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTINGS — CRACKED (FS 940/960)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, T-FITTINGS, 2 EACH, CRACKED AT KEEL BEAM, CRACKED F.S. 940 AND 960. REPLACED FITTINGS PER SRM 51-1-21.

Part: BELT FRAME — CRACKED (FS 1440)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, BELT FRAME CRACKED ON FORWARD SIDE F.S. 1440, LONGERON 23R. REPAIRED PER SRM 53-2-0.

Part: RIBS — CRACKED (RT WING LE)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT WING L/E ASSY, 8 EACH, RIBS CRACKED AT STA. XFS 608, 596, 871, 827, 803, 785, 779, AND 749. REPAIRED RIBS PER MM 57-00-00, FIG. 801.

Part: RIBS — CRACKED (RT WING LE)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT WING L/E ASSY, 8 EACH, RIBS CRACKED AT STA XFS 841, 836, 817, 797, 771, 652, 620, AND 626. REPAIRED RIBS PER MM 57-00-00, FIG. 801.

Part: CANOE FITTING — CRACKED (WS 428)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT WING NR 5 FLAP SUPPORT CANOE FITTING CRACKED UPPER FORWARD FASTENER HOLE, STA 428. REPLACED FITTING PER MM 27-51-12.

Part: LONGERONS — CRACKED (FS 260-270)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, LONGERONS CRACKED 35L, F.S. 260-270. REPLACED LONGERON SECTION F.S. 250-310 PER SRM 51-1-20D.

Part: SKIN — CRACKED (FS 160)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, 2 CRACKS ON SKIN FS 160 FWD UPPER CORNER OF FWD SERVICE DOOR. REPAIRED SKIN PER SRM 53-0 FIG 14.

Part: DOUBLER — CORROSION (FS 72)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, F.S. 72 JACK PAD DOUBLER HAS CORROSION. REPLACED DOUBLER PER SRM 51-1-20D.

Part: ANGLE — CORROSION (FS 1040)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, HEAVY CORROSION ON VERT. SUPPORT ANGLE FORWARD SIDE, F.S. 1040 LONGERON 27R. REPLACED ANGLE PER SRM 51-1-20D.

Part: WEB — CORRODED (FS 70)

WHILE IN FOR C CHECK, MAINTENANCE REPORTED MODERATE CORROSION LWR. SIDE WEB FS 70 LONGERON 21R. REPAIRED WEB PER SRM 53-2-0.

Part: DOUBLER — CORRODED (FS 620)

WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON INNER DOUBLER, FS 620 LONGERON 35R. REPAIRED PER UPS E.O.

Part: CUSP FITTING — CORRODED (FS 1580)

WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON CUSP FITTING FS 1580 LONGERON 21R. REPLACED FITTING PER SRM 51-3-0.

Part: BELT FRAME — CORRODED (FS 200)

WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON BELT FRAME LWR. LIP. LONGERON 36, FS 200. REPAIRED FRAME PER SRM 53-2-0 AND 51-1-20D.

Part: DOUBLER — CORRODED (FS 1050-1350)

WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON INNER DOUBLER FS 1050-1350 LONGERON 31L-31R. REPLACED DOUBLER PER SRM 50-2-0 AND 51-1-20D AND UPS E.O.

Part: SKIN — CORRODED (FS 1060/1070)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, HEAVY CORROSION AT FUSELAGE EXTERNAL SKIN PANEL FS 1060 AND FS 1070 UNDER KEEL PLATE. REPAIRED SKIN PER UPS EO.

Part: FITTING — CORRODED (FS 70)

WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON END FITTING FS 70 LONGERON 30L. REPLACED END FITTING PER SRM 51-1-20D.

Part: FITTING — CORRODED (FS 1220/1175)

WHILE IN FOR C CHECK, MAINTENANCE REPORTED 2 EACH FITTINGS HAVE HEAVY CORROSION AT FS 1220 LONGERON 35R, AND FS 1175 LONGERON 33R. REPLACED FITTINGS PER SRM 51-1-20D.

Part: BOLT FRAME — CORRODED (FS 1120)

WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION UPPER FLANGE BOLT FRAME, FS 1120 LONGERON 36. REPAIRED PER SRM 53-2-0.

Part: FRAME — CORRODED (FS 1140)

WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION UPPER FLANGE OF FRAME FS 1140 LONGERON 34L-35L. REPAIRED PER UPS E.O.

Part: SHEAR TIE — CORRODED (FS 1060)

WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON SHEAR TIE, FS 1060 LONGERON 35R - 36R. REPLACED SHEAR TIE PER SRM 51-1-20D.

Part: FITTING — CORROSION (FS 1220/1260)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, 2 EACH FITTINGS CRACKED AT FORWARD END, F.S. 1220, LONGERON 17R, AND F.S. 1260, LONGERON 18R. REPLACED FITTINGS PER SRM 51-1-20D.

Part: FITTING — CRACKED (FS 1150)

WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION AND CRACKED FITTINGS, FS 1150 LONGERON 34R-33R. REPLACED FITTINGS PER SRM 51-1-20D AND 51-1-8.

Part: BLKHD CAP — CORRODED (FS 980)

WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON BULKHEAD CAP FS 980 LONGERON 34R-35R. REPAIRED PER UPS E.O.

Part: FLOOR BEAM — CORRODED (FS 55)

WHILE IN FOR C CHECK, MAINTENANCE REPORTED EXFOLIATION CORROSION ON UPPER FLANGE OF FLOOR BEAM, FS 55 RBL 45. REPAIRED PER UPS E.O.

Part: LONGERON — CORRODED (FS 1018)

WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION LONGERON 35R, FS 1018. REPLACED SECTION PER SRM 51-1-20D.

Part: FRAME — CORRODED (FS 1280)

WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON BELT FRAME FS 1280 LONGERON 22R. REPAIRED FRAME PER SRM 53-2-0, FIG. 2

Part: FITTING — CRACKED (CARGO DOOR)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, 2ND DR. LATCH FITTING FROM FORWARD LOWER SIDE OF A B/B DR. HAS CORROSION AND CRACKS. REPLACED FITTING PER SRM 50-1-20.

Part: FITTING — CORRODED (FS 1580)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, CORROSION IN FRAME FITTING F.S. 1580, LONGERON 21R. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CORRODED (FS 1560)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION, CRACK AT FRAME FITTING F.S. 1560, LONGERON 21R. REPLACED FITTING PER SRM 51-1-20D.

Part: TRAP FITTING — CRACKED (FS 879)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT TRAPEZODIAL FITTING CRACKED PAST STOP DRILL. REPLACED FITTING PER UPS E.O.

Part: DNLOCK CYLINDER — MALFUNCTIONED (LT MLG)

CREW REPORTED, LT LANDING GEAR DID NOT INDICATE DOWN AND LOCKED UPON INITIAL GEAR EXTENSION AND 2ND GEAR CYCLE OK. REPLACED DOWNLOCK BUNGEE CYLINDER.

Part: GEAR LIGHT — MALFUNCTIONED (LT MLG)

CREW REPORTED UPON SELECTING LANDING GEAR TO DOWN, NO GREEN LIGHT SHOWED ON LEFT GEAR. RECYCLED LDG GEAR WHEN GEAR HANDLE WAS SELECTED DOWN. LT MLG GREEN LIGHT ILLUMINATED BRIEFLY THEN REMAINED OUT. FLY-BY TOWER CONFIRMED ALL GEAR DOWN. APPROPRIATE EMERGENCY CHECKLISTS WERE COMPLETED. NORMAL LANDING WAS MADE, ACFT WAS STOPPED ON RUNWAY TO ALLOW MX TO INSTALL GEAR PINS PRIOR TO TAXI TO RAMP. MRR FILED OPEN.

Part: RETRACT MECH — LACK OF LUBE (MAIN GEAR)

CREW REPORTED ON UPLATCH CHECK, GEAR NOT LATCHED LIGHT ON. RECYCLED, NO HELP, DOORS DID HOLD GEAR UP. CHECKED OPERATION OF ALL MLG AND MLG DOOR SWITCHES, ALL CHECKED GOOD. LUBED MAIN GEAR AND DOOR MECHANISMS, CHECKED UPLATCHES, ALL CHECKED OK. NO DEFECTS NOTED, OK FOR SERVICE.

Part: SKIN — CRACKED (FUSELAGE)

WHILE ON GROUND, MAINTENANCE FOUND NR 4 PIT FWD UPPER RADIUS HAS .75 INCH CRACK. FABRICATED DOUBLER AS PER SRM 53-2-1, INSTALLED DOUBLER.