N772UP

Part: SKIN — CRACKED (RT ELEVATOR)

INSPECTION TYPE:N/A RIGHT ELEVATOR UPPER SKIN HAS A CRACK 3.75 INCH LONG, JUST AFT OF I/B ELEVATOR HINGE. ACCOMPLISHED INTERIM REPAIR AS SPECIFIED IN PARAGRAPH 6A. LOG PAGE 812958. PERMANENT REPAIR IS REQUIRED AT OR BEFORE NEXT C CHECK (11/08)

Part: SLIDE — DISLODGED

INSPECTION TYPE:N/A SLIDE FELL OUT OF CASE ON DOOR OPENING. DEFERRED PER MEL 52-7-4. PLACARD INSTALLED. SLIDE IS REMOVED. REINSTALLED FORWARD ENTRANCE DOOR ESCAPE SLIDE PER MM 25-60-01-2. OPS CHECKS NORMAL.

Part: SLIDE — LOOSE (COCKPIT)

INSPECTION TYPE:N/A ESCAPE SLIDE IS LOOSE. REINSTALLED ESCAPE SLIDE.

Part: SLIDE — OUT OF POSITION (EMERGENCY EXIT)

INSPECTION TYPE:N/A ESCAPE SLIDE FELL OUT WHEN DOOR WAS OPENED. RESECURED SLIDE. OK FOR SERVICE.

Part: SLIDE — TORN (COCKPIT)

INSPECTION TYPE:N/A GIRT BAR HARD TO FASTEN ON ESCAPE SLIDE. FOUND ESCAPE SLIDE TORN NEAR GIRT BAR. REMOVED AND REPLACED ESCAPE SLIDE PER AMM 25-60-01-2, OPS CHECK OK.

Part: SLIDE — OUT OF POSITION (COCKPIT)

INSPECTION TYPE:N/A ESCAPE SLIDE OUT OF ITS ENCLOSURE. DEFERRED IAW MEL 52-7-1 M355759. RE-INSTALLED ESCAPE SLIDE.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS WILL NOT COME ON DURING BATTERY CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY IAW MM 33-50-01-2.

Part: SLIDE — UNSECURE (FWD ENTRY DOOR)

INSPECTION TYPE:N/A THE FWD ENTRY DOOR EMERGENCY SLIDE IS SLIPPING OUT OF ITS CONTAINER. FWD ENTRY DOOR SLIDE RESECURED IAW DC8 AMM 25-60-01-2.

Part: GIRT BAR — MALFUNCTIONED (ESCAPE SLIDE)

INSPECTION TYPE:N/A GIRT BAR WILL NOT LATCH IN PLACE TO ARM THE SLIDE CHUTE WHEN DOOR IS CLOSED. REPOSITIONED SLIDE ON DOOR PER MM 25-60-00. OPS CHECK OK.

Part: GIRT BAR — DAMAGED (PAX DOOR SLIDE)

GIRT BAR DIFFICULT TO ARM, NOT ENOUGH MATERIAL TO PULL BAR INTO PLACE. ADJ EVAC SLIDE IN CONTAINER. GIRT BAR OPERATIONAL NORMAL, REF MM 25-60-01-2.

Part: SLIDE — LOOSE (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY ESCAPE SLIDE & GIRT BAR LOOSE AND CANISTER OPENED. REPLACED DAMAGED & MISSING ATTACHMENT HARDWARE, RESEALED CANISTER AND SECURED GIRT BAR.

Part: RADAR — MALFUNCTIONED (RADOME) · airframe 69,351 hrs · 46,126 cycles

INSPECTION TYPE:C1 ATB - WX RADAR TAKES 3 DEGREES PITCH UP RADAR AND 3 DEGREES PITCH UP ON A/C TO GET RID OF GROUND CLUTTER. REMOVED AND REPLACED WX RADAR AND PEDESTAL IAW MM 34-41-01. OPS CHECK GOOD, ALL WORK ACCOMPLISHED BY CAT 2 QUALIFIED TECH.

Part: HOOK — OUT OF ADJUST (COCKPIT WINDOW) · airframe 69,351 hrs · 46,126 cycles

INSPECTION TYPE:C1 F/O'S SLIDING WINDOW WILL NOT OPEN. ADJUSTED F/O'S CLEARVIEW WINDOW LWR AFT HOOK PER MM 56-10-0-03-5, OPS CHECK GOOD.

Part: SKIN — GOUGED · airframe 69,351 hrs · 46,126 cycles

INSPECTION TYPE:C1 3" GOUGE IN AC SKIN AFT OF CAPTAIN'S CLEAR VIEW WINDOW FWD OF L1 DOOR. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7.

Part: SKIN — CRACKED (FS 1748 L14-17L) · airframe 69,351 hrs · 46,126 cycles

INSPECTION TYPE:C1 FUSELAGE SKIN CRACKED UNDER EXISTING DOUBLER AT FS 1748 BETWEEN L14L-L17L. REPAIRED FUSELAGE SKIN AT STA 1748 BETWEEN L14L-17L IAW SAA EA NR 008-5320-01-A0471 REV A, UPS EO DC8-5330-25332-B, BAC SERV MSG NR 1-234702180, AND FAA FORM 8100-9.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 69,351 hrs · 46,126 cycles

INSPECTION TYPE:C1 FINGER DOUBLER UNDER FWD LT CORNER OF EPC RACK HAS 4 POPPED RIVETS AND CORROSION AT STA FS -5 LBL 60. REMOVED CORROSION AND FINGER DOUBLER AT STA -5 LBL60 IAW SRM 51-1-21. FABRICATED AND INSTALLED FINGER DOUBLER AT STA -5 LBL 60 IAW SRM 53-02-00-0, 53-02-01-0.

Part: BOSS — OUT OF LIMITS (MLG) · airframe 69,351 hrs · 46,126 cycles

INSPECTION TYPE:C1 L/MLG RETRACT PIN BOSS REQUIRES BUSHING, MAX OD IS 1.800" ACTUAL MEASUREMENT IS 1.831". FABRICATED AND INSTALLED REPAIR BUSHING TO L/MLG RETRACT PIN BOSS BORE IAW SAA EA NR 008-3230-01-A0469 REV.A, UPS EO DC8-3230-25374-A, SB DC8-32-102, AD 71-25-09, AND FAA FORM 8100-9.

Part: STRINGER — CRACKED (WS 428-463) · airframe 69,351 hrs · 46,126 cycles

INSPECTION TYPE:C1 STRINGER 64 IS CRACKED BET XRS428 AND XRS463 NR 4 ALT REMOVED STRINGER 64 AND CLIP AT STA 428 IN NR 4 ALT TANK IAW SRM 51-01-20D. FABRICATED AND INSTALLED STRINGER IAW DWG 3644045, AND SRM 51-03-02, 51-1-20D AT STA XRS 428 AND XRS 463.

Part: FITTING — CRACKED (WING STRINGER) · airframe 69,351 hrs · 46,126 cycles

INSPECTION TYPE:C1 STRINGER END FITTINGS FOR STRINGER 51 ARE CRACKED AT XRS 74 NR 3 MAIN TANK. REMOVED AND REPLACED 2 STRINGER END FITTINGS AT STA XRS 74 NR 3 MAIN TANK IAW SRM 51-1-20D, 51-03-02.

Part: FITTING — CRACKED (FS 340 L21R) · airframe 69,351 hrs · 46,126 cycles

INSPECTION TYPE:C1 CRACK BETWEEN UPPER VERTICAL BOLTS IN CUSP/FLOORBEAM FITTING A-PIT STA 340, L21R. REMOVED FITTING AT CUSP/FLOORBEAM IN A-PIT STA 340 L21R IAW SRM 51-3-0, AND SRM 51-1-21. FABRICATED AND INSTALLED FITTING, T-ANGLE AND INTERCOSTAL AT STA 340 L21R IAW DWG 9754022, SRM 51-01-15-0 AND SRM 51-01-2OD-0.

Part: LONGERON SPLICE — CRACKED (FS 1746 L16L) · airframe 69,351 hrs · 46,126 cycles

INSPECTION TYPE:C1 CRACKED LONGERON STA 1746 L16L. REMOVED AND REPLACED LONGERON SPLICE AT STA 1766-1738 L16L IAW SRM 51-01-21-0, AND SRM 53-02-02-0 FIG 10.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 69,351 hrs · 46,126 cycles

INSPECTION TYPE:C1 MISSING RIVETS, SKIN CRACKED ON RT ELEVATOR UPPER SKIN STA XE 84.96. REMOVED AND REPLACED SKIN ON RT ELEVATOR UPPER STA XE 84.96 IAW SRM 55-2-1, AND SRM 55-2-1 FIG 8.

Part: LONGERON SPLICE — CRACKED (FS 1734 L15R) · airframe 69,351 hrs · 46,126 cycles

INSPECTION TYPE:C1 CRACKED LONGERON STA 1734 L15R. REMOVED AND REPLACED LONGERON SPLICE AT STA 1734 L15R IAW SRM 51-1-21, AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FS 1742 L15L) · airframe 69,351 hrs · 46,126 cycles

INSPECTION TYPE:C1 CRACKED LONGERON STA 1748 L15L BEHIND CANTED FRAME REMOVED AND REPLACED LONGERON SPLICE SECTION AT STA 1766-1742 L15L IAW SRM 53-02-02-0 FIG 10, AND SRM 53-05-02-0.

Part: FITTING — CRACKED (FS 857 L6R) · airframe 69,351 hrs · 46,126 cycles

INSPECTION TYPE:C1 CRACKED LONGERON END FITTING STA 857 L6R. REMOVED AND REPLACED LONGERON END FITTING AT STA 857 L6R IAW SRM 51-1-21, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FS 902 L5R) · airframe 69,351 hrs · 46,126 cycles

INSPECTION TYPE:C1 CRACKED LONGERON END FITTING STA 902 L5R. REMOVED AND REPLACED LONGERON END FITTING AT STA 902 L5R IAW SRM 51-03-02-0, AND SRM 51-01-23-0.

Part: LONGERON — CRACKED (FS1754 L14L) · airframe 69,351 hrs · 46,126 cycles

INSPECTION TYPE:C1 CRACKED LONGERON STA 1754 L14L BEHIND CANTED FRAME. REMOVED LONGERON SECTION FROM STA 1766-1746 L14L IAW SRM 51-01-21-0. FABRICATED AND INSTALLED LONGERON AND REPAIR SPLICES IAW SRM 53-05-02-0, AND SRM 53-02-02.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS DID NOT ILLUMINATE IN TEST. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK AND PERFORMED, OPS CK IAW AMM 33-50 -01-2. OPS CK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS DID NOT ILLUMINATE IN TEST. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK AND PERFORMED OPS CK IAW AMM 33-50- 01-2. OPS CK GOOD.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

FOUND EMERGENCY BATTERY PACK (EMERGENCY LIGHT) WILL NOT STAY CHARGED. EMERGENCY LIGHTING BATTERY PACK REPLACED IAW MM 33-50-01-2 AND SYSTEM CHECKS SERVICEABLE.

Part: WINDSHIELD — CORRODED (COCKPIT)

F/O RIGHT SIDE WINDSHIELD FRAME & PAN HAS SEVERE CORROSION & RUST FLAKING & PITTED. PREVIOUSLY REPORTED ON CNTL UPS06847280, HOWEVER A/C FERRIED TO SAT FOR FINAL REPAIR. THIS CLOSES FERRY DEFERRAL - D328628. C/W ULT THICKNESS CK AFTER BLENDING UP TO 35% OF MAT'L REMOVED IN BLENDED AREAS. C/W HFEC OF BLENDED AREAS, NO CRACKS DETECTED.

Part: WINDOW POST — CORRODED (FUSELAGE)

FOUND CORROSION ON F/O'S WINDSHIELD FRAME. UPS ENGINEERING REQUESTS METAL REMOVAL VERIFICATION AND CRACK DETECTION AFTER BLEND OUT. C/W ULT THICKNESS CK AFTER BLENDING UP TO 35 PERCENT OF MAT'L REMOVED IN BLENDED AREAS. C/W HFEC OF BLENDED AREAS, NO CRACKS DETECTED.

Part: WINDSHIELD — DELAMINATED (COCKPIT)

INSPECTION TYPE:N/A, F/O FWD RIGHT SIDE WINDSHIELD DELAMINATED & WILL NOT DEFOG. REMOVED F/O'S RT SIDE WINDSHIELD. REPLACED F/O'S RIGHT SIDE WINDSHEILD PER MM 56-10-02-2. INSTALLED TAPE INSTEAD OF SEALER FOR ONE TIME FERRY FLT TO SAT FOR CNTL UPS06847280.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

EMERGENCY LIGHTING INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND RELAY UNIT PER M/M 33-50-01-2.

Part: LIGHT — WEAK (EMERGENCY EXIT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS ARE DIM. REPLACED EMERGENCY LIGHTS BATTERY PACK. OPS CHECK NORMAL IAW MM 33-50-01.

Part: LIGHT — INOPERATIVE (CABIN)

FOUND COCKPIT EMERGENCY EXIT LIGHT OVER ENGINEER SEAT INOP. PERFORMED OPS CK OF EMERGENCY LIGHT SYS PER M/M 33-50-02-2, SYS OPS NML.

Part: SHEAR TIE — CORRODED (BS 55 L34L-L34R) · airframe 68,891 hrs · 45,788 cycles

INSPECTION TYPE:SP AT STA 55 IN BETWEEN L34L AND L34R HAS CORROSION BEYOND LIMIT ON SHEER TIE. REMOVED, FABRICATED AND INSTALLED SHEER TIE IAW SRM 53-03-01, 51-3-2, 51-1-21 AND 51-1-20D.

Part: SHEAR TIE — CORRODED (BS 35 L34R-L34L) · airframe 68,891 hrs · 45,788 cycles

INSPECTION TYPE:SP, AT STA 35 IN BETWEEN L34L AND L34R HAS CORROSION BEYOND LIMITS ON SHEAR TIE. REMOVED, FABRICATED AND INSTALLED SHEER TIE IAW SRM 53-03-01 FIG 003, 51-3-2, 51-1-21 AND 51-1-21.

Part: SKIN — CORRODED (FS 21.92-70) · airframe 68,891 hrs · 45,788 cycles

INSPECTION TYPE:SP REMOVE AND REPLACE LOWER FWD SKIN STA -21.92 TO STA 70 L31L- L31R. REMOVED AND REPLACED LWR FWD SKIN STA -21.92 TO STA 70 L31L-L31R IAW EO DC8-5330-8942-D.

Part: SKIN — CRACKED (FUSELAGE)

SKIN BULGE AND CRACK. ASSIGNED FERRY PERMIT NR 9148 TO SAA. PER NRC 788843 REPAIRED ON NRC 788844. PERFORMED LOW FREQ EDDY CURRENT INSP IN AREA OF SKIN BULGE AT FS 35 PER NDT SPM 06-10-2.002. MAT LOS S DETECTED AT FS 35 IN AREA BTWN L36 & L34R APPX 8". SKIN REPLACED.

Part: WARNING LIGHT — ILLUMINATED (NR 4 ENGINE)

INSPECTION TYPE:N/A ATB - NR 4 ENG OIL PRESS LIGHT CAME ON IN FLT. OIL PRESS AT CLIMB THRUST WAS 60 & OPS AFTER SHUTDOWN (WINDMILLING). NR 4 ENG LOW OIL PRESSURE LIGHT DEFERRED PER MEL 79-6 OIL PRESSURE & OIL QTY WERE NORMAL PER FLT CREW, PLACARD INSTALLED M296095.

Part: PUMP — LEAKING (STBY RUDDER)

INSPECTION TYPE:N/A ON CLIMBOUT HYD FLUID QTY LOSS. FOLLOWED EMERGENCY PROCEDURE CHECK LIST. ON LANDING REMOVED AND REPLACED EMERGENCY STBY RUDDER PUMP. SERVICED & RAN AND OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP OVER COURIER SEAT & IN COCKPIT CEILING. RELAMPED PER MM 33-50-02-2, CK'S OK.

Part: DOUBLER — CRACKED (STUB WING) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE:C3, UPON REMOVAL OF STUB WING NR 4 FOUND AT TRAILING EDGE OF STUB WING INTERNAL DOUBLER CRACKED AT STA XW406 RIGHT WING. REPAIRED NR 4 STUB WING INTERNAL DOUBLER IAW DC-8 SRM 57-2-0 FIG 2.

Part: FRAME — CORRODED · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE: C3, FS 1360 FRAME LWR FLANGE AT LONGERON 36 HAS EXFOLIATION CORROSION. REMOVED CORROSION & FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. FABRICATED TWO REPAIR ANGLES & INSTALLED IAW DC-8 SRM 53-2-0, 51-1-21 AND 51-1-20D.

Part: BEAM — CRACKED (PRESS BULKHEAD) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD AFT SIDE 3RD J-BEAM UP FROM BOTTOM CRACKED AT BO BOTH UPPER & LOWER EXISTING DOUBLERS AT CENTERLINE WITH UPPER FLANGE HANS SHEARED & LOOSE FASTENERS. NDT VERIFIED CRACK IN BOTH UPPER & LOWER J-BEAM DOUBLERS IS 2 INCHES IN LENGTH. REMOVED EXISTING REPAIR DOUBLERS. NDT VERIFIED CRACK IN J-BEAM IS TERMINATED AT EXISTING STOPDRILLS. FABRICATED AND INSTALLED TWO REPAIR DOUBLERS IAW EO DC8-5310-6598-C.

Part: FITTING — CORRODED (FUSELAGE) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE: C3, BS 1220.00 & L34R BATHTUB FITTING HAS CORROSION. REMOVED AND REPLACED FITTING IAW DC-8 SRM 53-2-0 FIG 2G.

Part: BEAM — CRACKED (PRESS BULKHEAD) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE:C3 AFT SIDE OF AFT PRESSURE BULKHEAD 4TH J-BEAM UP FROM BOTTOM HAS LOWER EXISTING DOUBLER CRACKED AT CENTERLINE. NDT VERIFIED CRACK IN LOWER EXISTING DOUBLER IS 2 INCHES IN LENGTH. REMOVED EXISTING REPAIR DOUBLERS. NDT VERIFIED 2 INCH CRACK IN J-BEAM TERMINATES AT FASTENER HOLE AND STOPDRILL. FABRICATED AND INSTALLED TWO REPAIR DOUBLERS IAW EO DC8-5310-6598-C.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE: C3, LONGERON 14L CRACKED AT CANTED FRAME STA 1740. CUT OUT DAMAGED AREA. NDT VERIFIED NO CRACKS NOTED AT CUT OUT. FABRICATED REPAIR ANGLE & FILLER AND INSTALLED IAW DC-8 SRM 53-2-2 FIG 11.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE-C3 SHEARED FASTENERS AND CORROSION UNDER FINGER DOUBLER STA 880-900 BL 0. CUT OUT DAMAGE TO WEB AND FINGER DOUBLER. FABRICATED FILLER, FINGER DO DOUBLER, AND DOUBLER IAW SRO DWG 5645332. INSTALLED ALL REPAIR PARTS IAW SAA SK772-069.

Part: FITTING — CORRODED (CARGO DOOR) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE: C3, LOWER CARGO COMPARTMENT C-PIT DOOR (JAMB) FRAME AT APPROX STA 1165 LW LOWER LATCH BACK-UP FITTING HAS SEVER CORROSION ON FITTING & FASTENERS. REMOVED AND REPLACED FITTING IAW DC-8 SRM 53-2-0 FIG 2D.

Part: PAN — CRACKED (PAX DOOR) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE: C3, RADIOGRAPHIC (X-RAY) INSP DETECTED A CRACK ON THE FWD LEFT EMERGENCY OV OVERWING EXIT ON THE UPPER AFT JAMB CORNER APPROX .562 INCH IN LENGTH. NDT VERIFIED CRACK EXISTS IN INTERNAL DOOR PAN. TRIMMED EDGE OF INTERNAL DOOR PAN TO REMOVE CRACK. NDT VERIFIED NO CRACKS NOTED AT TRIM OUT. TRIM OUT FOUND WITHIN LIMITS IAW DC-8 SRM 53-2-0 FIG 6.

Part: RIB — CRACKED (LT WING) · airframe 68,469 hrs · 45,463 cycles

C3 LT WING L/E AT STA. XFS 716.250 RIB IS CRACKED. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE AND INSTALLED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 68,469 hrs · 45,463 cycles

C3 WING LT L/E RIB IS CRACKED AT STA XFS 816.250. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE AND SHIM AND INSTALLED IAW SRM 57-2-0 FIG 2

Part: RIB — CRACKED (LT WING) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE: C3, WING LT LEADING EDGE AT STA XFS 672.500 RIB IS CRACKED. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED SHIM & REPAIR ANGLE AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE:C3 WING LEFT L/E RIB IS CRACKED AT STA 785. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING LE) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE:C3, WING LT OUTBOARD LEADING EDGE AT STA 778.250 APROX RIB CRACKED. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (NR 4 STUB WING) · airframe 68,469 hrs · 45,463 cycles

C3 RT WING NR 4 STUB WING HAS TWO RIBS CRACKED ABOVE NR 4 PYLON FOOT STOOL. STOP DRILLED ONE CRACK AND CUT OUT ONE CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK AND NO CRACKS NOTED AT CUT OUT. FABRICATED REPAIR ANGLES AND INSTALLED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 68,469 hrs · 45,463 cycles

C3 WING LT L/E AT STA. XFS 591.250 RIB IS CRACKED. REPAIRED LT WING L/E RIB AT STA. XFS 591.250 IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE:C3 WING LT LEADING EDGE AT STA 735 RIB IS CRACKED. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED SHIM & REPAIR DOUBLER AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE: C3, WING LT L/E AT STA XFS 578 RIB IS CRACKED. NDT VERIFIED CRACK .5 INCH LONG. STOP DRILLED CRACK. NDT VERIFIED CRACK TERMINATES AT STOP DRILL. FABRICATED REPAIR ANGLE AND SHIM AND INSTALLED IAW SRM 57-2-0 FIG 2.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE: C3, L1 DOOR HAS A CRACK ON THE LOWER FWD DOOR JAMB STARTING FROM THE EDGE AND TERMINATES AT THE FASTENER HOLE. CUT OUT CRACK ON FWD LOWER CORNER OF L1 DOOR JAMB OUTER SKIN AND INTERNAL DOUBLER. NDT VERIFIED NO CRACKS NOTED AT CUT OUTS. FABRICATED REPAIR DOUBLER, TRIPLER, AND FILLER. INSTALLED REPAIR PARTS IAW DC-8 SRM 53-2-0 FIG 15.

Part: RIB — CRACKED (RT WING) · airframe 68,469 hrs · 45,463 cycles

C3 WING RT L/E AT STA XFS 335.250 DRAIN HOLE DOUBLER IS CRACKED. NDT VERIFIED CRACK IS APPROX. .3750 INCH LONG. REMOVED INTERNAL DOUBLER ON RT WING L/E, FABRICATED REPLACEMENT DOUBLER IAW DWG 5769589-27. INSTALLED REPLACEMENT DOUBLER ON RT L/E AT STA XFS 335.250 IAW SRM 51-1-21 AND 51-1-21D.

Part: RIB — CRACKED (RT WING) · airframe 68,469 hrs · 45,463 cycles

C3 WING RT L/E AT APPROX. STA XFS 465 HAS CRACKED RIB. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE DOUBLER AND INSTALLED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT O/B SLAT) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE:C3 LEFT O/B SLOT UPPER DOOR CLOSE-OUT RIB AT I/B END BROKEN IN LOWER RADIUS. REMOVED AND REPLACED LEFT O/B SLOT CLOSE OUT RIB (PAN) IAW DC-8 SRM 51-1-21. REPAIRED LEFT O/B SLOT O/B END IAW SAA SK772-387.

Part: RIB — CHAFED (STUB WING) · airframe 68,469 hrs · 45,466 cycles

INSPECTION TYPE: C3, RT WING I/B STUB WING RIB XILD 42 HAS A DEEP CHAFF. REMOVED DAMAGED AREA. NDT VERIFIED NO CRACKS NOTED AROUND CUTOUT. FABRICATED REPAIR ANGLES (2 EA) & FILLER AND INSTALLED IAW DC-8 SRM 57-2- 0.

Part: RIB — CRACKED (LT WING) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE:C3 UPPER RIB CRACKED IN LT CENTER L/E ABOVE OPENING FOR PANEL 520B. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED TWO REPAIR DOUBLERS AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 68,469 hrs · 45,463 cycles

C3 RT WING MID L/E XFS 335 UPPER RIB IS CRACKED AT AFT END. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE DOUBLERS AND INSTALLED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE:C3 CRACKED RIB AT APPROX STA XFS 728 RIGHT WING LEADING EDGE. REMOVED PREVIOUS REPAIR AND TRIMMED OUT CRACK. NDT VERIFIED NO CRACKS NOTED AT TRIM OUT. REINSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-21 AND 51-1-20D.

Part: PRESSURE BLKHD — CRACKED (FUSELAGE) · airframe 68,469 hrs · 45,466 cycles

INSPECTION TYPE: C3, F/S 1766 FWD SIDE OF AFT PRESSURE BULKHEAD IS CRACKED 65 INCHES ABOVE FLOOR AND LBL 35. REMOVED EXISTING REPAIR AND CUT OUT CRACKED AREA. NDT VERIFIED NO CRACKS NOTED AT CUT OUT. FABRICATED FILLER, FINGER DOUBLER, & DOUBLER INSTALLED IAW SRO DWG 853007 AND SB 53-73.

Part: PRESSURE BLKHD — CRACKED (FUSELAGE) · airframe 68,469 hrs · 45,466 cycles

INSPECTION TYPE:C3 F/S 1766 FWD SIDE OF AFT PRESSURE BULKHEAD IS CRACKED 65 INCHES ABOVE FLOOR AND RBL 35. REMOVED EXISTING REPAIR DOUBLERS AND CUT OUT CRACKED AREA. NDT VERIFIED NO CRACKS NOTED AT CUTOUT. FABRICATED REPAIR DOUBLERS & FILLER AND INSTALLED IAW SRO DWG 8530009 AND SB 53-73.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE: C3, HEAVY CORROSION ON CUSP, LT SIDE MAIN CABIN, STA 1153. REMOVED TEE ANGLE AND L-ANGLE. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. FABRICATED FILLER IAW SAA SK772-604. INSTALLED FILLER AND REINSTALLED T-ANGLE & L-ANGLE IAW DC-8 SRM 51-1-20D.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 68,469 hrs · 45,466 cycles

INSPECTION TYPE: C3, LEFT FWD EMERGENCY EXIT DOOR IS CRACKED AT UPPER FWD CORNER OF FRAME. TWO CRACKS VISIBLE .5 INCH AND 1.5 INCH IN LENGTH. STOP DRILLED 2 EA CRACKS. NDT VERIFIED STOP DRILLS TERMINATES CRACKS. FABRICATED REPAIR DOUBLER AND INSTALLED IAW DC-8 SRM 52-2-0 FIG 2.

Part: WEB — CRACKED (CENTER WING) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE: C3, CENTER WING FS 700 LEFT CRACK IN WEB EXTENDED PAST REPAIR. REMOVED EXISTING REPAIR. CUT OUT DAMAGED WEB. FABRICATED WEB & SPLICE DOUBLER AND INSTALLED IAW DC-8 SRM 53-2-0.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE: C3, FWD SIDE OF FS 70 BULKHEAD LOWER CHORD HAS INTERGRANULAR CORROSION AT LONGERON 32R. FOUND INTERGRANULAR CORROSION OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. REMOVED STA 70 LOWER FWD CHORD BETWEEN LONGERONS 32R & 33R. FABRICATE AND ONE -9 DOUBLER AND TWO -11 SPLICE DOUBLERS IAW DC-8 SRM 53-2-5 FIG 8C. SPLICED IN NEW SECTION OF CHORD AND INSTALLED THE -9 DOUBLER & -11 SPLICE DOUBLERS IAW DC-8 SRM 53-2-5 FIG 8C.

Part: SKIN — CRACKED (LT WING) · airframe 68,469 hrs · 45,463 cycles

INSPECTION TYPE: C3, POSSIBLE CRACK IN UPPER WING SKIN (LT) AT FASTENER ON AFT SIDE OF STRINGER 15, JUST O/B OF RIB AT XRS 74. NDT VERIFIED CRACK 1 INCH IN LENGTH. CUT OUT DAMAGED AREA 1.375 INCH DIAMETER. NDT VERIFIED NO CRACKS NOTED AT CUT OUT. FABRICATED REPAIR DOUBLER & FILLER AND INSTALLED IAW DC-8 SRM 57-2-1.

Part: CONNECTOR — INOPERATIVE (BATTERY PACK)

EMERGENCY LIGHTS INOPERATIVE. FOUND CONNECTOR LOOSE ON BATTERY PACK. RE INSTALLED SAME, SYSTEM TEST OK

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE: PFLT, EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED CONNECTIONS AT CONNECTOR ON BATTERY. SYSTEM OPS CHECKS NORMAL IAW MM 33-50-01.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. R&R EMERGENCY LGT BATT PACK. OPS CK NORMAL

Part: FITTING — LEAKING (HYD SYSTEM)

CREW REPORTED LOSING HYD SYSTEMS. DECLARED EMERGENCY. A/C LANDED W/O INCIDENT. HYD QTY DROPPED TO STANDPIPE LEVEL FOLLOWED BY RUDDER & AILERON CONTROL MANUAL LIGHTS COMING ON, (FL 390 & 150 NM FROM DESTINATION). REMOVED AND REPLACED RESERVOIR AIR PRESS REGULATOR ASPIRATOR & TEE-FITTING IAW MM 29 10 03 2, OPS CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AS PER MM 33 50 01 2.

Part: SKIN — CRACKED (LT WING)

LOWER WING SKIN CRACK OUTBOARD NR 1 ENGINE PYLON STA XW 508. FERRIED TO SAA FOR REPAIR. *S/D* CUT OUT CRACKED AREA ON SKIN, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED WING SKIN FILLER, REPAIR FILLER AND DOUBLER IAW 8110-3 APPROVED SAA SK 772-799, AS A INTERIM REPAIR FOR 18 MONTHS.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:PFLT EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. OPS CK OK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,542 hrs · 44,705 cycles

INSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT STA 1746 AT LONG 35R AND 34R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, FILLER, AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,542 hrs · 44,705 cycles

INSPECTION TYPE:C2 STA 780 LONG 35R END FITTING CRACKED. REMOVED, FABRICATED, AND INSTALLED FITTING IAW DWG 5755058 AND SRM 51-1-21.

Part: RIB — CRACKED (RUDDER) · airframe 67,542 hrs · 44,705 cycles

INSPECTION TYPE:C2 RUDDER RIB CRACKED AT STA ZR 140. REMOVED, FABRICATED, AND REPLACED RIB IAW DWG 5656223 AND SRM 51-1-21.

Part: RIB — CRACKED (RUDDER) · airframe 67,542 hrs · 44,705 cycles

INSPECTION TYPE:C2 RUDDER RIB CRACKED STA ZR 135. REMOVED, FABRICATED AND REPLACED RIB IAW DWG 5656223 AND SRM 51-1-21.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 67,542 hrs · 44,705 cycles

INSPECTION TYPE:C2 STA 272 TO 280 LONG 35R INTERCOSTAL LOWER FLANGE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 9754020 AND SRM 51-1-20D.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 67,542 hrs · 44,705 cycles

INSPECTION TYPE:C2 STA 440-460 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 67,542 hrs · 44,705 cycles

INSPECTION TYPE:C2 STA 340 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 36 AND 35R. REMOVED AND REPLACED FITTING IAW DWG 3755822, AND SRM 53-2-0 FIG 2D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,542 hrs · 44,705 cycles

INSPECTION TYPE:C2 LONG 24L IS CRACKED AT STA 978. STOP DRILLED CRACK, NDT VERIFIED CRACK TERMINATES AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-2 FIG 5.

Part: FITTING — CORRODED (FUSELAGE) · airframe 67,542 hrs · 44,705 cycles

INSPECTION TYPE:C2 STA 1152 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 34L TO 35L. REMOVED AND REPLACED FITTING IAW DWG 3755845, AND SRM 53-2-0 FIG 2D.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 67,542 hrs · 44,705 cycles

INSPECTION TYPE:C2 INTERNAL FINGER DOUBLER IS CORRODED BEYOND LIMITS STA 70-210 AT LONG 31R. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5779916, AND SRM 51-1-20D, 51-1-21.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 67,542 hrs · 44,705 cycles

INSPECTION TYPE:C2 STA 190 DOUBLER CORRODED BEYOND LIMITS BETWEEN LONGERONS 31L & 31R. REMOVED, FABRICATED & INSTALLED REPLACEMENT DOUBLER IAW DWG 5779925 & SRM 51-1-21.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 67,542 hrs · 44,705 cycles

INSPECTION TYPE:C2 CARGO PIT C DOOR CORNER CLIPS CRACKED INSIDE LIGHTENING HOLES FS STA 1170 TO 1210 AT LONG 22R APPROX. FOUND DOOR PAN/FRAME CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED CLIPS, DOUBLERS, AND DOOR PAN SECTION IAW DWG 5894025 AND SRM 52-2-0 FIG 2, 52-4-1.

Part: STIFFENER — CRACKED (LT WING) · airframe 67,542 hrs · 44,705 cycles

INSPECTION TYPE:C2 LEFT WING T/E INBOARD VERTICAL STIFFENER AT FLAP HINGE 98 IS CRACKED AT BOTTOM. REMOVED, FABRICATED, AND INSTALLED STIFFENER IAW DWG 3643320, AND SRM 51-3-0.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 67,542 hrs · 44,705 cycles

INSPECTION TYPE:C2 STA 131 TO 121 AT LBL 45 ANGLE FITTING/GUSSET IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED GUSSET IAW DWG 5597992, AND SRM 51-1-20D.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 67,542 hrs · 44,705 cycles

INSPECTION TYPE:C2 AFT SIDE OF STA -99 FINGER DOUBLER IS CORRODED BEYOND LIMITS AT RBL 60. REMOVED, FABRICATED AND INSTALLED DOUBLER DWG 5612298.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,542 hrs · 44,705 cycles

INSPECTION TYPE:C2 STA 89 DOUBLER, FINGER DOUBLER AND WEB ARE CORRODED BEYOND LIMITS AT RBL 30. CUT OUT CORRODED AREA ON WEB, FABRICATED AND INSTALLED FILLER, DOUBLER, AND FINGER DOUBLER IAW DWG 5612298, AND SR08530026.

Part: RIB — CRACKED (HORIZ STAB) · airframe 67,542 hrs · 44,705 cycles

INSPECTION TYPE:C2 LEFT HORIZONTAL STAB L/E UPPER RIB IS CRACKED AT FASTENER END AT XFS 166.250. STOP DRILLED CRACK, NDT VERIFIED NO CRACKS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 55-3-0 FIG 8.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,542 hrs · 44,705 cycles

INSPECTION TYPE:C2 R-1 DOOR UPPER FWD CORNER HAS A REPAIR THAT DOES NOT CONFORM TO THE SRM AT STA 160 AT LONG 11R. REMOVED DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 14.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. SECURED GROUND IAW DC8 MM 20-00. REMOVED AND REPLACED LIGHT BULB IN EMERGENCY EXIT ASSY AT ENTRY DOOR IAW DC8 MM 33-50, OPS CHECK GOOD.

Part: FABRIC — FRAYED (EVA SLIDE)

INSPECTION TYPE:PFLT EMERGENCY ESCAPE SLIDE GIRT BAR HAS FABRIC ATTACHMENT FRAYING. REMOVED AND REPLACED SLIDE.

Part: LONGERON — CORRODED (FUSELAGE)

INSPECTION TYPE:N/A CORROSION AT LONGERON 34.

Part: BULKHEAD — CRACKED (FUSELAGE)

INSPECTION TYPE:N/A FWD FRAME PRESS BULKHEAD LONGERON 35 CRACKED.

Part: RIB — CRACKED (RT WING)

INSPECTION TYPE:N/A RT WING T/E RIB CRACKED AT FORWARD SURFACE VERTICAL CHANNEL AT XW33. THIRD OUTBOARD WAS PREVIOUSLY REPAIRED PER A/C ENGINEERING AMC HAS ASSIGNED INFORMATIONAL ITEM I226648 ASSIGNED.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHTS CIRCUIT BREAKER OPENED IN FLIGHT. PERFORMED EMERGENCY LIGHT BATTERY TEST PER MM REF 33-50-01 EMERGENCY LIGHTING CHECKS GOOD

Part: SKIN — CORRODED (FUSELAGE) · airframe 67,542 hrs · 44,705 cycles

INSPECTION TYPE:C2 EVIDENCE OF CORROSION UNDER NR 2 ADF ANTENNA, CORRODED BEYOND LIMITS STA 70 TO 190 LONG 31L TO 31R. REMOVED AND REPLACED SKIN BETWEEN STA 70 TO 190 LONG 31L TO 31R IAW DWG 5779925, SRM 53-1-0, 51-1-21, 51-1-20D.

Part: SLIDE — LOOSE (CABIN)

INSPECTION TYPE:IN, ESCAPE SLIDE NEEDS REPACKING. RESECURED SLIDE TO DOOR.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:PF, EMERGENCY LIGHTS FAILED. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CK NORMAL.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, STA 1690, LONG 26 LT, FWD SIDE END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG. 4641326,AND SRM. 51-1-21

Part: FITTING — CRACKED (MLG WW) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, STA 958, WHEEL WELL KEELBEAM LOWER DOOR SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG. 5616306, AND SRM. 51-1-20D.

Part: SPAR CAP — CORRODED (RT WING) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1 RT WING AUX. TANK SPAR UPPER CAP IS CORRODED BEYOND LIMITS BETWEEN XFS 107.5 AND XFS 126.25 REPAIRED SPAR CAP I.A.W. SRM. 57-2-1 FIG. 36.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1. STA 1746 BL 0 TO RBL 30 UPPER FLOORBEAM SUPPORT CHANNEL IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED CHANNEL I.A.W. DWG. 5755032,AND SRM. 51-1-20D ***CPCP***

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1. STA 1746 BL 0 TO LBL 30 FLOORBEAM SUPPORT CHANNEL IS CORRODED. REMOVED, FABRICATED, AND REPLACED CHANNEL I.A.W. DWG. 5755032,AND SRM. 51-1-20D

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, STA 1764, RBL. 8 HAS FLOOR SUPPORT CHANNEL CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED CHANNEL IAW. DWG. 5755032, AND SRM. 51-1-20D ***CPCP***

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, STA 1702 - 1723, RBL 30 FLOOR SUPPORT CHANNEL IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED CHANNEL IAW DWG. 5755032,AND SRM. 51-1-20D,51-1-21 ***CPCP***

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1. STA 1766, RBL 20 - 24 FLOORBOARD SUPPORT CHANNEL IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED CHANNEL I.A.W. DWG. 5755032,AND SRM. 51-1-20D

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1. STA 1766, LBL 20 - 23 FLOORBOARD SUPPORT CHANNEL IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED CHANNEL I.A.W. DWG.5755032,AND SRM. 51-3-0.

Part: FRAME — CRACKED (COCKPIT) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, STA. -12, LONG 14 LT, FRAME IS CRACKED. REPAIRED FRAME IAW E.O.DC8-5310-11728-A,AND DC8-53A-011

Part: RIB — CRACKED (RT WING) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE:C1 RT WING L/E. UPPER RIB IS CRACKED AT XFS 622.5 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1. STA 640 BULKHEAD VERTICLE STIFFENER IS CRACKED AT RBL 12. REPAIRED STIFFENER I.A.W. SRM. 53-2-0 FIG. 1B

Part: BEAM — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, STA 1766 BULKHEAD AFT SIDE 5TH J-BEAM FROM BOTTOM IS CRACKED AT BL 0. REPAIRED J-BEAM I.A.W. SRM. 53-2-5 FIG. 26.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1. LONG 33 RT INTERCOSTAL IS CRACKED AT STA 240 REMOVED, FABRICATED, AND REPLACED INTERCOSTAL I.A.W. DWG. 9759429, AND SRM. 51-1-21

Part: BEAM — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, STA 1766, AFT SIDE OF BULKHEAD 2ND J-BEAM FROM BOTTOM IS CRACKED AT BL.0. REPAIRED J-BEAM I.A.W. SRM. 53-2-5 FIG. 26

Part: SKIN — CRACKED (RT WING) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1 RT WING L/E. UPPER SKIN IS CRACKED AT XFS 572.5 REPAIRED SKIN I.A.W. SRM. 57-2-1 FIG. 38

Part: ANGLE — CORRODED (COCKPIT) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, STA -80, RBL 26 ANGLE IS CORRODED BEYOND LIMITS OBD. OF F/O OBD SEAT TRACK REPAIRED ANGLE IAW SRM. 53-2-0 FIG. 1B

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, STA 1220 LONG 32 RT BANNANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W DWG. 3755847, AND SRM. 51-1-20D

Part: DOUBLER — CRACKED (RT WING) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1 RT WING LOWER INTERNAL DOUBLER IS CRACKED AT XFS 597.5 REMOVED, FABRICATED, AND REPLACED DOUBLER I.A.W. DWG. 5769600,AND SRM. 51-1-20D,51-1-21

Part: LONGERON — CORRODED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1. STA 280 - 300, LONG 27 LT IS CORRODED BEYOND LIMITS. REPAIRED LONGERON I.A.W. SRM. 53-2-2 FIG. 10.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, STA 1766, AFT SIDE LONG 17 LT, END FITTING AND LONGERON ARE CRACKED. REMOVED AND REPLACED FITTING, AND REPAIRED LONGERON IAW DWG. 4772397,AND SRM. 53-2-2 FIG. 11

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, STA 1766, AFT SIDE, 1ST J-BEAM FITTING IS CRACKED AT 35 RT. REMOVED AND REPLACED FITTING IAW DWG. 3753645,AND SRM. 51-1-20D

Part: DOUBLER — CRACKED (RT WING) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1 RT WING L/E. INTERNAL WRAP-AROUND INTERNAL DOUBLER IS CRACKED AT XFS 572.5 REMOVED, FABRICATED, AND REPLACED DOUBLER I.A.W. DWG. 5769600,AND SRM 51-1-21,51-1-20D

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1. STA 80 - 100, LONG 33 RT INTERCOSTAL IS CRACKED. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL I.A.W. DWG. 5779925,AND SRM. 51-1-21

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, STA 1766, LONG 17 RT, LONGERON AND END FITTING ARE CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING AND LONGERON IAW DWG. 4772397, AND SRM 51-1-20D, AND 51-1-21.

Part: FITTING — CRACKED (AFT FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, STA 1766, BULKHEAD LONG 10 RT, END FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG. 4772397,AND SRM. 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1. STA 610, LONG 33 LT, LONGERON SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3750330,AND SRM. 51-1-20D

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1. STA 1240 - 1260, LONGERON 33 RT IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL I.A.W. DWG. 9753792,AND SRM. 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, STA 1230, LONG 33 RT, BANNANA FITING IS CRACKED REMOVED AND REPLACED FITTING IAW DWG. 5755847, AND SRM. 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, STA 1328 LONG 21 RT LOWER CUSP TO FRAME FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 9755584, AND SRM. 51-1-20D

Part: LONGERON — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE:C1 STA. 1260 - 1280, LONG 35 LT, IS CRACKED. REMOVED, FABRICATED, AND REPLACED LONGERON SEGMENT IAW DWG 3758593, AND SRM. 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE:C1, STA 1230 LONG 33R INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1. STA 1240 - 1260 BETWEEN LONG 33 RT AND 34 RT SEAT TRACK SUPPORT TO INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 4758514, AND SRM. 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1. STA 1220, LONGERON 35 RT, TORQUE BOX SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 9754055,AND SRM. 51-3-0

Part: LONGERON — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE:C1 STA. 1340-1360, LONG 36, IS CRACKED. REPAIRED LONGERON IAW 8110-3 APPROVED DH SK 772-713

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, STA 1230 BETWEEN LONG 34 RT - 35 RT BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3755843,AND SRM. 53-2-0 FIG. 2D

Part: RIB — CRACKED (LT WING) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1 LT WING L/E. UPPER RIB IS CRACKED AT XFS 379. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2

Part: SKIN — CRACKED (LT WING) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE:C1 LT WING L/E. UPPER SKIN IS CRACKED AT XFS 297.5 REPAIRED SKIN I.A.W. E.O. DC8-5720-7767A

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C123 STA. 781 LONG. 13 RT ATTACH FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING I.A.W. DWG. 3779970,AND SRM. 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE:C1 STA. 857 LONG. 18L INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AFT SIDE REMOVED, FABRICATED AND REPLACED FITTING I.A.W. DWG. 4750420,AND SRM. 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE:C1 STA. 902 LONG. 18L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING I.A.W. DWG. 4779496,AND SRM. 51-1-20D

Part: BRACKET — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, STA 1702, CANTED FRAME TO FRAME STA 1717, TIE BRACKET IS CRACKED AT LONG 14 RT. REMOVED, FABRICATED, AND REPLACED BRACKET IAW DWG 5612143, AND SRM. 51-1-20D

Part: ANGLE — CRACKED (LT WING TE FLAP) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE:C1, LEFT WING REAR SPAR VERTICAL ANGLE O/B OF FLAP HINGE CANOE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 3643320, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, STA 1766, LONG 10 RT, FWD SIDE END FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG. 4772397, AND SRM 51-1-20D.

Part: ANGLE — CRACKED (LT WING) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, LT WING L/E VERTICLE ANGLE AT XS 250 IS CRACKED. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG. 5769515, AND SRM. 51-1-20D

Part: RIB — CRACKED (LT WING) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE:C1 LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 597.5 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE:C1, STA 1766 I/B OF LONG 3R T-CHORD ON AFT PRESSURE IS CRACKED. REPAIRED CHORD IAW 8110-3 APPROVED DH SH 772-494.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, STA. 834 LONG. 18L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3779978,AND SRM. 51-1-20D

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE: C1, STA 1220, LONG 22 RT SKIN IS CRACKED ON AFT UPPER CORNER OF CARGO DOOR CUTOUT REPAIRED SKIN IAW SRM 53-2-0 FIG. 21.

Part: SKIN — CRACKED (RT WING) · airframe 66,340 hrs · 43,860 cycles

INSPECTION TYPE:C1, RIGHT WING L/E LOWER SKIN IS CRACKED AT XFS 572.5. REPAIRED SKIN IAW DC8-5720-4087-B.

Part: ENGINE — FAILED (NR 1)

INSPECTION TYPE:N/A, NR 1 ENGINE FLAME-OUT ON DEPARTURE. ATTEMPTED RE-START, NOT SUCCESSFUL. CONTINUED RDU ON REMAINING 3 ENGINES, RAN APPROPRIATE CHECK LISTS. DEBRIEFED FLT CREW ON NR 1 ENG FLAME-OUT. ALSO, VERIFIED NR 1 ENG FUEL USED AT 700 LBS FOR FLIGHT. ACARS WAS NR 1 ENG START AT 0922Z AND IN TIME OF 1028Z. ACCOMP NR 1 ENG INSP PER MM 71-00-00 PAGE 165-168. NO PROBLEMS NOTED FROM START. OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS WILL NOT TEST. REPLACED EMERGENCY LIGHT BATTERY AND RELAY UNIT PER MM 33-50-01, LIGHTS TEST OK.

Part: SENSOR — SHORTED (RT MLG)

AFTER RETRACTING GEAR, DOORS NOT LATCHED LIGHT REMAINED ILLUMINATED AND ALTERNATE GEAR DOOR LIGHT, LEFT SIDE WAS ILLUMINATED. RECYCLED THE GEAR, WITH SAME INDICATIONS. PERFORMED ADJ/TEST OF LT AND RT MAIN GEAR DOOR UPLATCH MECHANISM PER MM 32-31-04. FOUND RT PROX SENSOR WIRE BARE AND GROUNDING ON UPLATCH MECHANISM CAUSING RED DOORS NOT LATCHED LIGHT. REPLACED RT GEAR DOOR PROX SWITCH. COULD NOT DUPLICATE LT DOOR ALTERNATE AMBER LIGHT. REPLACED LT AND RT ALTERNATE DOOR SWITCHES, OPS GOOD PER MM 32-31-04.

Part: SENSOR — INOP (RT MLG)

INSPECTION TYPE-N/A, AFTER RETRACTING GEAR, DOORS NOT LATCHED LIGHT REMAINED ILLUMINATED AND ALTERNATE GEAR DOOR LIGHT, LEFT SIDE WAS ILLUMINATED. RECYCLED THE GEAR, WITH SAME INDICATIONS. PERFORMED ADJ/TEST OF LT AND RT MAIN GEAR DOOR UPLATCH MECHANISM PER MM 32-31-04. FOUND RT PROX SENSOR WIRE BARE AND GROUNDING ON UPLATCH MECHANISM CAUSING RED DOORS NOT LATCHED LIGHT. REPLACED RT GEAR DOOR PROX SWITCH. COULD NOT DUPLICATE LT DOOR ALTERNATE AMBER LIGHT. REPLACED LT AND RT ALTERNATE DOOR SWITCHES, OPS GOOD PER MM 32-31-04.

Part: FITTING — CRACKED (BS 1240)

INSPECTION TYPE:D STA 1240 BTWN STR 32R-33R, THE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4758514 AND SRM 51-1-20D.

Part: FITTING — CORRODED (BS 879)

INSPECTION TYPE:D STA 879 AT LONG 24R, THE CUSP TIE FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW DWG 3641004 AND SRM 53-2-0 FIG 8.

Part: INTERCOSTAL — CORRODED (BS 1038)

INSPECTION TYPE:D INTERCOSTAL AT STA 1038 AND STR 35R HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5716454 AND SRM 53-4-1.

Part: DOUBLER — CRACKED (WS 22.75)

INSPECTION TYPE:D, LT WING FUEL ACCESS PANEL DOUBLED (LANDING) IS CRACKED IN 3 PLCS REF STA. XRS 22.750 AND STR.6. REPAIRED AREA IAW SRM 57-2-1 FIG 36.

Part: FITTING — CORRODED (BS 1520)

INSPECTION TYPE-D, CORROSION BLEND OUTS ON FRAME TO CUSP FITTING AT FS 1520 RT SIDE BEYOND SRM LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 467.323)

INSPECTION TYPE-D, LT WING L/E RIB AT STA XS467.323 IS CRACKED. REPAIRED IAW SRM 57-2-0.

Part: AILERON — CORRODED (LT WING)

INSPECTION TYPE:D, THE LT INBD AILERON HAS AREAS OF LIGHT SURFACE CORROSION THROUGHOUT ENTIRE INNER SURFACE OF FORWARD SPAR AREA. REMOVED AND REPACED THE LT INBD AILERON PER MM 27-11-01.

Part: RIB — CRACKED (WS 484.895)

INSPECTION TYPE:D, RT WING L/E AT STA XFS 484.895, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 297)

INSPECTION TYPE:D, RT WING L/E AT STA XFS297.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 397)

INSPECTION TYPE:D, RT WING L/E AT STA XFS 397.000, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 442.185)

INSPECTION TYPE:D, RT WING L/E AT STA XFS442.185, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 291.5)

INSPECTION TYPE:D, RT WING L/E AT STA XFS291.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 781)

INSPECTION TYPE:D LTH MAIN DECK FLOORBEAM END FITTING IS CRACKED AT STA 781 AND 21L. REMOVED AND REPLACED FITTING IAW DWG 5641007 AND SRM 51-1-20D.

Part: FRAME — CRACKED (LT WINDSHIELD)

INSPECTION TYPE-D, CAPT'S FWD WINDSHIELD FRAME CRACKED. REPAIRED IAW SRM 53-2-0.

Part: SPLICE — CRACKED (BS 1690)

INSPECTION TYPE-D, FS 1690, THE LONG 26R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED LONG SPLICE FITTING.

Part: ANGLE — CRACKED (BS 798)

INSPECTION TYPE:D, L ANGLE CRACKED AT STA 798 LBL54. STOP DRILLED CRACK AND REPAIRED IAW SRM 53-2-0 FIG 1B.

Part: CHANNEL — CRACKED (BS 790)

INSPECTION TYPE:D, U-CHANNEL CRACKED BOTTOM OF FUSELAGE AT STA 790 RIB L16. REMOVED AND RPLACED U-CHANNEL PER SRM 51-3-0.

Part: FRAME — CRACKED (RT WINDSHIELD)

INSPECTION TYPE-D, F/O'S FWD WINDSHIELD FRAME CRACKED. REPAIRED IAW SRM 53-2-0.

Part: FRAME — CRACKED (BS 660)

INSPECTION TYPE-D, FS 660 BELOW STR 21R - FRAME HAS A 3 INCH CRACK. REPAIRED CRACK BY WELDING IAW DPS 10.225.

Part: CHANNEL — CRACKED (BS 790)

INSPECTION TYPE:D, U-CHANNEL CRACKED BOTTOM OF FUSELAGE AT STA 790, LBL 16. REMOVED AND REPLACED U-CHANNEL PER SRM 51-3-0.

Part: SPLICE — CRACKED (BS 440-460)

INSPECTION TYPE-D, FS 440 TO 460, AT LONG 31L, THE SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING PER SRM 51-1-20D.

Part: RIB — CRACKED (WS 188.75)

INSPECTION TYPE:D, RT WING L/E AT STA XFS188.750, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: LONGERON — CRACKED (BS 120/140)

INSPECTION TYPE:D LONGERON 32R IS CRACKED AT THE FRAME ATTACH BOLT AT STA 120 AT 140. REMOVED AND REPLACED SECTION OF LONGERON IAW SRM 53-2-2.

Part: FITTING — CRACKED (BS 440-460)

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

Part: INTERCOSTAL — CRACKED (BS 70)

INSPECTION TYPE:D STA 70 AT RBL16-24, THE INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5613064 AND SRM 51-1-21.

Part: RIB — CRACKED (WS 466.5)

INSPECTION TYPE-D, RT WING L/E RIB AT STA XFS 466.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.

Part: FITTING — CORRODED (WS 1286)

INSPECTION TYPE:C, STA 1286 AT STR 19L, THE DOOR FRAME SUPPORT FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW DWG 4640269 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1180)

INSPECTION TYPE:D STA 1180 AT STR 21R, THE FRAME TO CUSP TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754043 AND SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1222)

INSPECTION TYPE:D HOLD DOWN FITTING AT STA 1222 AND STR 31R HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED FITTING IAW 8110-3 APPROVED DHC SK772-781 AND SRM 51-1-20D.

Part: FITTING — CORRODED (BS 40)

INSPECTION TYPE:D, MAIN CABIN AT STA 40 STR 21R, THE FRAME TO CUSP TIE FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW DWG 4597643 AND SRM 51-1-20D.

Part: FRAME — CRACKED (BS 1580)

INSPECTION TYPE:D STA 1580L, FRAME IS CRACKED IN 2 PLACES AT STR 21L. REPAIRED AREA IAW SRM 53-4-1 FIG 51.

Part: LONGERON — CORRODED (BS 8-70)

INSPECTION TYPE-D, LONGERON 31R AT FS 8 TO 70 EXFOLIATED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-20 AND DWG 5613862.

Part: RIB — CRACKED (WS 0 .7095)

INSPECTION TYPE-D, RT WING L/E RIB AT STA XILD 0.7095 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 113.75)

INSPECTION TYPE:D, LT WING L/E AT STA XFS 113.750 THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 227.335)

INSPECTION TYPE-D RT WING L/E RIB AT STA XS 227.335 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 113.25)

INSPECTION TYPE:D, RT WING L/E RIB AT STA XFS 113.75 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED RIB PER SRM 57-2-0 FIG 2.

Part: INTERCOSTAL — CRACKED (WS 201.25)

INSPECTION TYPE:D, RT WING L/E I/B OF THE STA XFS201.25 RIB, THE INTERCOSTAL IS CRACK EDAT THE I/B END. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW DWG 5769859 AND SRM 51-1-21.

Part: INTERCOSTAL — CRACKED (BS 25-35)

INSPECTION TYPE:D STA 25 TO 35 AT STR 32L, THE INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5645313 AND SRM 51-1-21.

Part: DOUBLER — CRACKED (WS 7)

INSPECTION TYPE-D, LT WING L/E LWR SKIN INTERNAL DOUBLER AT STA XOLDI 7 IS CRACKED. REMOVED DOUBLER, FABRICATED AND INSTALLED PER DWG 5769891 AND SRM 51-1-20D, 51-1-21.

Part: RIB — CRACKED (WS 329)

INSPECTION TYPE:D, LT WING L/E AT STA XFS329.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: ANGLE — CRACKED (LT WING)

INSPECTION TYPE:D, LT WING I/B SLOT BOX, O/B AFT VERTICAL ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 69753293 AND SRM 51-1-20D.

Part: DOUBLER — CORRODED (BS 25)

INSPECTION TYPE-D, FS 25 AT LONG 31R, AFTER CORROSION REMOVAL THE FINGER DOUBLER IS OUT OF LIMITS. REMOVED DAMAGED FINGER DOUBLER, FABRICATED AND INSTALLED PER DWG 4640929 AND SRM 51-1-21.

Part: RIB — CRACKED (WS 7095)

INSPECTION TYPE:D, LT WING L/E RIB AT STA XILD .7095 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (WS 597.5 - 638.7)

INSPECTION TYPE-D, LT WING L/E UPPER SKIN XFS 597.5 TO 638.75 IS CRACKED 4 PLACES. REPAIRED IAW SRM 57-2-1.

Part: SKIN — CRACKED (WS 338)

INSPECTION TYPE-D, LT WING L/E UPPER SKIN AT STA XFS 338 IS CRACKED. CUT OUT DAMAGE AND REPAIRED PER SRM 57-2-1 FIG 38.

Part: SHEAR TIE — CORRODED (BS 1229)

INSPECTION TYPE-D, FS 1229 BTWN STR 35R-36 SHEAR TIE FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-2-0.

Part: LONGERON — CORRODED (BS 1520-1540)

INSPECTION TYPE-D, FS 1520 TO 1540, LONG 34L HAS HEAVY CORROSION. CUT OUT DAMAGED LONGERON AND REPAIRED PER SRM 53-2-2 FIG 11.

Part: SKIN — CRACKED (WS 74)

INSPECTION TYPE:D, LT WING UPPER SKIN AT STR 10 IS CRACKED AT STA XRS74 (STRESS CORR CRACK). REPAIRED AREA IAW SRM 57-3-1 FIG 10.

Part: RIB — CRACKED (WS 304)

INSPECTION TYPE:D, LT WING L/E AT STA XFS304.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: TRACK — CORRODED (BS 1320-1400)

INSPECTION TYPE:D STA 1320-1400 ABOVE STR 33R, THE CARGO TRACK AND SPLICE BLOCK HAVE HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED TRACK AND BLOCK IAW DWG 5759223.

Part: ANGLE — CRACKED (WS 250.089)

INSPECTION TYPE-D, RT INBD SLOT BOX, O/B AFT VERTICAL ANGLE IS CRACKED. REMOVED, FABRICATED, AND INSTALLED VERTICAL ANGLE PER DWG 9753293 AND SRM 51-1-21, 51-3-0.

Part: SHEAR TIE — CRACKED (BS 1237)

INSPECTION TYPE-D, FS 1237 BTWN STR 33R TO 34R SHEAR TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1260-1280)

INSPECTION TYPE-D, FS 1260 TO 1280 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING PER DWG 3754473 AND SRM 51-1-20D.

Part: FRAME — CRACKED (BS 1220)

INSPECTION TYPE-D, FS 1220 ABOVE LONG 35R TO 36 THE FRAME HAS A 5 INCH CRACK. REMOVED AND REPLACED THE FRAME CAP PER DWG 9754055 AND SRM 51-1-20D AND 51-1-22 FIG 47.

Part: FITTING — CRACKED (BS 1231)

INSPECTION TYPE-D, FS 1231 ABOVE LONG 35R, THE FRAME TIE FITTING IS CRACKED. REMOVED AND REPLACED FRAME TIE FITTING PER DWG 3758570 AND SRM 51-1-20D.

Part: SKIN — CRACKED (WS 329/335.25)

INSPECTION TYPE-D, RT WING L/E UPPER SKIN AT STA XFS 329.0 AND 335.25 IS CRACKED IN TWO PLACES. REPAIRED PER SRM 57-2-1 FIG 38.

Part: FITTING — CRACKED (BS 1260-1280)

INSPECTION TYPE-D, FS 1260 TO 1280 LONG 34L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING PER DWG 3759222 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1239)

INSPECTION TYPE-D, FS 1239 ABOVE LONG 35R, THE TIE FITTING IS CRACKED. REMOVED CRACKED FITTING, FABRICATED AND INSTALLED PER DWG 3758495 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1340-1360)

INSPECTION TYPE:D, STA 1340-1360 STR 36 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779919 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 980)

INSPECTION TYPE:D LONG 23R END FITTING JUST AFT OF FS 980 IS CRACKED. REMOVED AND REPLACED FITTING PER DWG 3753306-1 AND SRM 51-1-20D.

Part: ANGLE — CRACKED (NR 1 PYLON)

INSPECTION TYPE:D, THE NR 1 PYLON OUTBOARD ANGLE DOUBLER AT THE FRONT SPAR IS CRACKED. REMOVED FABRICATED AND REPLACED ANGLE IAW DWG 5803961 AND SRM 51-1-20D AND 51-3-0.

Part: FITTING — CORRODED (BS 1180)

INSPECTION TYPE:D C-3 DOOR FWD TORQUE BOX FWD. SHEAR TIE HAS HEAVY CORROSION STA 1180 BTWN STR 35R-36. REMOVED AND REPLACED FITTING IAW DWG 3755845 AND SRM 53-2-0 FIG. 2D.

Part: FITTING — CRACKED (BS 1180)

INSPECTION TYPE-D, FS 1180 AT LONG 27L, THE DOOR OPEN STOP/FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED FITTING PER DWG 3755854 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 616.25)

INSPECTION TYPE-D, LT WING L/E AT STA XFS616.25, THE LWR L/E RIB IS CRACKED AT THE AFT BEND. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: ANGLE — CRACKED (RT WING)

INSPECTION TYPE-D, RT OTBD WING SLOT OTBD AFT VERTICAL ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED ANGLE PER DWG 9753297 AND SRM 51-1-2, 51-1-20D.

Part: RIB — CRACKED (WS 841.25)

INSPECTION TYPE:D, LT WING L/E RIB AT STA XFS 841.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 304)

INSPECTION TYPE:D, RT WING L/E RIB AT STA XFS304.000 IS CRACKED AT THE LWR AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SPLICE — CRACKED (BS 1040-1060)

INSPECTION TYPE-D, LONGERON 31R SPLICE FITTING CRACKED BTWN FS 1040 TO 1060. REMOVED AND REPLACED FITTING IAW SRM 51-1-20.

Part: FRAME — CORRODED (BS 1100)

INSPECTION TYPE:D STA 1100 AT LONG 36 THE FRAME UPPER CAP HAS HEAVY CORROSION. REMOVED AND REPLACED CAP IAW DWG 5764343 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 722.5)

INSPECTION TYPE:D, LT WING L/E AT STA XFS722.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 1238)

INSPECTION TYPE-D, FS 1238 ABOVE LONG 33R, THE TIE FITTING IS CRACKED. REMOVED CRACKED FITTING, FABRICATED AND INSTALLED PER DWG 4758514 AND SRM 51-1-20D.

Part: FITTING — CRACKED (RT HORZ STAB)

INSPECTION TYPE:D, RT HORIZ STAB L/E ON THE INBD END THE UPPER AND LOWER TEE FITTINGS ARE CRACKED. REMOVED AND REPLACED FITTINGS IAW SRM 53-1-0.

Part: SKIN — CRACKED (WS 304)

INSPECTION TYPE-D, RT WING L/E LWR SKIN AT STA XFS 304.0 IS CRACKED JUST FWD OF THE SPAR. STOP DRILLED CRACK AND REPAIRED PER EO DC8-5720-4087.

Part: FITTING — CRACKED (BS 1140)

INSPECTION TYPE:D STA 1140 AT STR 35L, THE INTERCOSTAL ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE (FITTING) IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 980)

INSPECTION TYPE-D, LONG 22R END FITTING JUST AFT OF FS 980 CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20.

Part: FITTING — CRACKED (BS 1241)

INSPECTION TYPE-D, FS 1241 ABOVE LONG 35R, THE TIE FITTING IS CRACKED. REMOVED CRACKED FITTING, FABRICATED AND INSTALLED PER DWG 3758498 AND SRM 51-1-20D.

Part: SKIN — CRACKED (WS 90)

INSPECTION TYPE-D, RT WING T/E UPPER SKIN AT THE AUX SPAR, 16 O/B OF THE MLG TRUNNION IS CRACKED. CUT OUT DAMAGE AND REPAIRED PER EO DC8-5720-7767.

Part: CLIP — CRACKED (WS 262)

INSPECTION TYPE-D, RT WING L/E ABOVE THE NR 3 PYLON, THE RIB FWD ATTACH CLIP IS CRACKED. REMOVED, FABRICATED AND INSTALLED CLIP PER DWG 9753294 AND SRM 51-1-21.

Part: GUSSET — CORRODED (BS 1100)

INSPECTION TYPE-D, FRAME TO INTERCOSTAL GUSSET AT STA 1100 AT LONG 35L HAS MODERATE CORROSION. REMOVED GUSSET, FABRICATED AND INSTALLED PER DWG 9758507 AND SRM 51-1-20D.

Part: SKIN — CRACKED (WS 591.25)

INSPECTION TYPE-D, RT WING L/E UPPER SKIN AT STA XFS 591.25 IS CRACKED. REPAIRED PER EO DC8-5720-7767.

Part: DOUBLER — CRACKED (WS 7)

INSPECTION TYPE:D, RT WING L/E LWR INTERNAL DOUBLER AT STA XOLDI7.00 IS CRACKED. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769891 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1260-1280)

INSPECTION TYPE-D, FS 1260 TO 1280 LONG 34R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING PER DWG 3759222 AND SRM 51-1-20D.

Part: SHEAR TIE — CORRODED (BS 640)

INSPECTION TYPE:D, SHEAR TIE BLOWNOUT AT FS 640 BETWEEN LONG 35L AND 35R. REMOVED, FABRICATED AND REPLACED SHEAR TIE PER DWG 5616509 AND SRM 51-1-4 AND 51-1-20D.

Part: RIB — CRACKED (WS 828.75)

INSPECTION TYPE-D, RT WING L/E RIB AT STA XFS 828.75 IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED PER SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 585)

INSPECTION TYPE-D, RT WING L/E RIB AT STA XFS 585.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 616.25)

INSPECTION TYPE-D, RT WING L/E RIB AT STA XFS 616.25 IS CRACKED AT THE AFT LWR END. STOP DRILLED AND REPAIRED PER SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 610)

INSPECTION TYPE-D, RT WING L/E RIB AT STA XFS 610.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED PER SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 785)

INSPECTION TYPE:D, RT WING L/E RIB AT STA XFS 785.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 641.25)

INSPECTION TYPE-D, RT WING L/E RIB AT STA XFS 641.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED PER SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 653.75)

INSPECTION TYPE-D, RT WING L/E RIB AT STA XFS 653.75 IS CRACKED AT THE AFT LOWER FASTENER. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 70)

INSPECTION TYPE-D, FS 70 THE LONG 28L END FITTING IS CRACKED. REMOVED AND REPLACED THE END FITTING PER SRM 51-1-21, 51-1-20D AND DWG 4611067.

Part: FUEL PUMP — MALFUNCTIONED (NR 4 ENGINE)

DURING CRUISE AT 35.0 NR 4 ENGINE FLAMED OUT. PERFORMED ENGINE FLAMEOUT PROCEDURE AND ENGINE START CHECKLIST WITH A SUCCESSFUL ENGINE START. ALL FURTHER INDICATIONS AND PARAMETERS WERE NORMAL. PERFORMED 71-00 FAULT 51 PG 101-104 CFM56. REPLACED ENGINE DRIVEN BOOST PUMP PER MM 73-10-01 PG 201-206. SYSTEM OPS CHECK AND LEAK CHECKS OK P/N OFF/ON 64-1119-4 S/N OFF FB74919 S/N ON FB69547.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:DAL EMG EVAC LIGHTS INOP. FOUND ON DAILY INSPECTION. REMOVED AND REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, CHECKS GOOD MM 33-50-0.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS DIDN'T TEST ON PREFLIGHT. REPLACED EMERGENCY LIGHT BATTERY PACK.

Part: RIB — CRACKED (WS 316.5)

INSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 316.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 329)

INSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 329 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACKED AND REPAIRED PER SRM 57-2-0 FIG 2.

Part: CASTING — CRACKED (WS 98)

INSPECTION TYPE: C. RT WING T/E, OUTBOARD OF MLG TRUNNION AND FWD OF AUXILIARY SPAR, THE STA 98 FLAP HINGE LWR ATTACH CASTING CRACKED. REMOVED CRACKED CASTING, FABRICATED REPLACMENT CASTING INSTALLED CASTING PER SRM 51-1-20D, AND SRM 51-3-1.

Part: RIB — CRACKED (WS 366.)

INSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 366.5 IS CRACKED AT THE AFT UPPER EDGE. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 360.2)

INSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 360.25 IS CRACKED AT THE AFT UPPER EDGE. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (LT AILERON)

INSPECTION TYPE-C, LT O/B AILERON AT CENTER HINGE CUTOUT, SKIN DOUBLER IS CRACKED 2 PLACES. REMOVED DAMAGED DOUBLER, FABRICATED AND INSTALLED DOUBLER PER SRM 57-8-01 FIG 4 AND 51-1-20.

Part: RIB — CRACKED (WS 6.225)

INSPECTION TYPE: C. RT WING L/E RIB AT STA. XOLDI 6.225 CRACKED APPROX. 2.8 INCHES. REMOVED DAMAGED AREA PER SRM 57-2-0. FABRICATED FILLER, DOUBLER, AND INTERCOSTAL PER SRM 57-2-0 AND INSTALLED PER SRM 51-1-20D.

Part: UPLATCH MECH — MALFUNCTIONED (NOSE GEAR)

INSPECTION TYPE: DLY. ON TAKEOFF ROLL, HEARD BUZZING NOISE LIKE A RELAY CHATTERING. ON GEAR RETRACTION COULD FEEL BUZZING IN THE HANDLE, BUZZING STOPPED AS GEAR STARTED UP. WHEN PLACING GEAR HANDLE INTO THE UPLATCH POSITION THE NOSE GEAR FELL OUT OF WHEEWELL AND FULLY EXTENDED. RECYCLED GEAR DOWN AND THEN UP, OPERATION WAS NORMAL. SECOND UPLATCH CHK WAS NORMAL. LIFTED NOSE OF ACFT OFF GROUND AND CYCLED NOSE GEAR. NOSE GEAR PASSED UPLATCH TEST EACH TIME. INSPECTED UPLATCH MECHANISM, NO DEFECTS FOUND. SYSTEMS OPERATED NORMALLY IAW M/M 32-31-06, M/M 32-20-00, PG 501.

Part: SKIN — CRACKED (LT WING TE)

INSPECTION TYPE: DLY. FOUND CRACK IN WING SKIN AT LEFT DUMP SHOOT AREA. CRACKED THROUGH RIVET, EDDY CURRENT CRACK FOUND TO BE 1.25 INCHES IN LENGTH. REPAI RED LOWER TRAILING EDGE WING COVE PANEL IAW SRM 51-1-9A.

Part: RETRACT MECH — MALFUNCTIONED (NLG)

PILOT REPORTED ON FIRST AND SECOND ATTEMPTS TO LOWER GEAR, THE NOSE LANDING GEAR LIGHT DID NOT ILLUMINATE. DURING THIRD ATTEMPT ALL 3 LIGHTS GREEN AND HEARD VERY LOUD SOUND IN NOSEWHEEL AREA. MAINTENANCE LUBED THE NOSE GEAR AND RELAMPED NOSE INDICATOR. RETRACTED AND EXTENDED NOSE GEAR SEVERAL TIMES, ALL CHECK NORMAL.

Part: FINGER DOUBLER — CORRODED (FS 1510)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FINGER DOUBLER, F.S. 1510, LONGERON 30 RT. REPLACED IAW SRM 51-1-21.

Part: LONGERONS — CORRODED (FS 1490-1620)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERONS 36 AND 35R, F.S. 1490-1620. REPLACED SECTIONS IAW SRM 51-1-20D.

Part: FITTING — CRACKED (FS 1650)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED LONGERON END FITTINGS AT F.S. 1650 ON LONGERONS 32R AND 34R. REPLACED IAW SRM 51-1-20D.

Part: SLIDE — FRAYED (ENTRY DOOR)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FWD ENTRY DOOR SLIDE GIRT FRAYED AND EXP DATE HAS THREE MONTHS LEFT. REPLACED ASSY IAW M/M 25-60-01.

Part: FITTING — CRACKED (BS 702)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED FRAME END FITTING BELOW LONGERON 21L, F.S. 702. REPLACED IAW SRM 51-1-20D.

Part: DOUBLER — CORRODED (FS 1620)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON INNER DOUBLER AT F.S. 1620, LONGERONS 32L-33L. REPLACED IAW SRM 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND 0.75 INCH CRACK AT SKIN LOWER FWD CORNER OF LT GROUND AIR CONNECT CUT OUT. REPAIRED IAW E.O. DC8-5330-0793.

Part: LONGERON — CRACKED (FS 1650)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 32R CRACKED AT F.S. 1650. REPLACED IAW SRM 51-1-20D.

Part: LONGERON — CRACKED (FS 1650)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 29R CRACKED AT F.S. 1650. REPLACED IAW SRM 51-1-20D.

Part: SHEAR TIE — CORRODED (FS 140)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME SHEAR TIE, F.S. 140, BETWEEN LONGERONS 36-35R. REPAIRED IAW SRM 53-2-0.

Part: SKIN — CRACKED (FS 1740-1746)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKS ON OUTER FUSELAGE SKIN F.S. 1740 BETWEEN LONGERONS 17R TO 18R, AND F.S. 1746, LONGERON 14L. REPAIRED IAW SRM 53-2-0.

Part: LONGERON — CRACKED (FS 1650)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED LONGERON 34R AT F.S. 1650. REPLACED IAW SRM 51-1-20D.

Part: DOUBLER — CORRODED (FS 550)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION AT END OF DOUBLER F.S. 550, B-BAG BIN DOOR LOWER JAMB. REPAIRED IAW SRM 53-2-0.

Part: SKIN — CORRODED (BS 1350-1490)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION BULGE ON FUSELAGE BELLY SKIN, F.S. 1350-1490. REPLACED IAW SRM 51-1-20D, 51-1-21.

Part: BATHTUB FITTING — CORRODED (FS 280)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON BATHTUB FITTING F.S. 280, LONGERON 33A RT. REPLACED IAW SRM 51-1-20D.

Part: LONGERONS — CRACKED (FS 1650)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED LONGERONS 29L, 29R, AND 33L AT F.S. 1650, P\N 575778 AND P/N 575779. REPAIRED IAW E.O. DC8-5310-7156.

Part: SKIN — CORRODED (FS 1663-1680)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE BELLY SKIN F.S. 1680-1663, LONGERON 32R. REPLACED IAW SRM 51-1-21, 51-1-20D.

Part: SKIN — CORRODED (FS 1620-1640)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE SKIN, F.S. 1620-1640, BETWEEN 29R-30R. REPAIRED IAW E.O. DC8-53-1407.

Part: SKIN DOUBLER — CORRODED (FUSELAGE)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LT AND RT INNER SKIN DOUBLERS, F.S. 1610-1660, LONGERON 31R AND F.S. 1613-1650 LONGERON 31L. REPLACED IAW SRM 51-1-20D.

Part: ANGLE — CRACKED (FS 798)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND 4.0 INCH CRACK ON FLOOR BEAM TO CENTER WING BOX ATTACH ANGLES, F.S. 798, LBL 50, 6.0 INCH CRACK ON SAME, F.S. 798, RBL 50. REPLACED IAW SRM 51-1-20D.

Part: EEL DISARM — INOP (FLIGHT DECK)

DURING POST FLIGHT CHECK, MAINTENANCE FOUND EMER DISARM CHECK INOP. SECURED OVERHEAD PANEL CAMLOCS (2 EACH) EMER DISARM CHECK. CHECKS NORMAL. EMER LIGHTS, OPS CK NORMAL.