N703UP

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

ENTRY AREA EMERGENCY OVERHEAD LIGHT INOP. RELAMPED THE ENTRY AREA OVERHEAD LIGHT. OPS CKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHTS OVER ENTRY DOOR INOP. RELAMPED THE OVERHEAD ENTRY DOOR LIGHT ASSY. OPS CKS NORMAL.

Part: LINE — FAILED (HYD SYSTEM)

LOSS OF HYDRAULICS ON TAXI IN. HYDRAULIC LEAK RT WHEEL WELL. HYDRAULIC LINE TO THE RIGHT GEAR OVERCENTER LINK ACTUATOR FAILED. FOUND PRESSURE LINE TO R/H GEAR BUNGEE CYLINDER LEAKING. REPLACED LINE WITH TEMP LINE IAW 32-32903-2. REPOSITIONED LINES AND LK CK OK. D-336367 ISSUED FOR FOLLOW UP CHECK WITHIN 200 DAYS & PERM REPAIR NO LATER THAN C CHECK.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHT BATTERY DEAD R&R EMERGENCY EXIT LIGHT BATTERY PACK W/R/T M/M 33-50-01-2 OPS CK GOOD.

Part: REPAIR — MISINSTALLED (BS 560 L22R) · airframe 66,955 hrs · 28,063 cycles

C-2 DOOR JAMB UPPER AFT CORNER REPAIR DOES NOT MEET REQUIREMENTS OF SRM 53-2-0, AND DWG SRO 8530019. REMOVED EXISTING DOUBLER ON C-2 DOOR JAMB UPPER AFT CORNER IAW SRM 53-2-0 FIG 20, FABRICATED AND INSTALLED FILLERS DOUBLER AND TRIPLER IAW SRM53-02-00 FIG 20 AND SRO 8530019.

Part: DOOR FRAME — GOUGED (CARGO DOORWAY) · airframe 66,955 hrs · 28,063 cycles

INSPECTION TYPE:C1 D-PIT AFT LOWER DOOR SURROUND FRAME FITTING HAS DEEP GOUGE. REMOVED AND REPLACED FRAME FITTING IAW SRM 51-3-0.

Part: FRAME — GOUGED (BS 1140 L34R) · airframe 66,955 hrs · 28,063 cycles

C-PIT STA 1140 FRAME UPPER FLANGE ABOVE LONGERON 34R HAS DEEP, LONG DRILL WALK. REMOVED AND REPLACED FRAME UPPER CAP IAW SRM 20-15-00-2,51-3-2 AND 51 -1-20D.

Part: ATTACH FITTING — CRACKED (BS 1240 L33R) · airframe 66,955 hrs · 28,063 cycles

INSPECTION TYPE:C1 LONGERON ATTACH FITTING CRACKED AT STA 1240 L33R. REMOVED AND REPLACED LONGERON ATTACH FITTING AT STA 1240 L33R IAW SRM 51-1-20D, AND SRM 51-1-8.

Part: SPAR CAP — CRACKED (BS 857) · airframe 66,955 hrs · 28,063 cycles

RT WW LWR SPAR CAP CRACKED 1/2" LONG AT STA 857.125. STOP DRILLED CRACK AT AT RT WW LWR SPAR CAP IAW SRO 8570009 INSTALLED -47 PLUG IN WING SKIN, FABRICATED AND INSTALLED REPAIR ANGLES, AND -66 SPACER IAW SRO 8570009, AND SRM 51-1-20D AT STA 857.125 RT WW LWR SPAR CAP.

Part: WEB — CRACKED (FS1220 L33L) · airframe 66,955 hrs · 28,063 cycles

FOUND PIT SLIDING CARGO DOOR TORQUE BOX UPPER WEB CRACKED STA 1220 L33L. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-02-00, AND 51-1-21.

Part: BULKHEAD — CORRODED (BS 1788) · airframe 66,955 hrs · 28,063 cycles

INSPECTION TYPE:C1 IN 60 HOLE CORROSION ON WEB UNDER L-ANGLE OF BULKHEAD JUST AFT OF HOLE ENTRANCE. REMOVED CORRODED WEB AND ANGLE AT STA 1788 IAW SRM 53-02-00-0. FABRICATED AND INSTALLED REPAIR WEB AND ANGLE AT STA 1788 IAW SRM 53-02-00-0, 53-05-03-0, AND SRM 51-1-21.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,955 hrs · 28,063 cycles

INSPECTION TYPE:C1 IN 60 HOLE, FRAME FITTING ON FIRST LATERAL FRAME SUPPORT RT CENTER ABOVE ENTRANCE HAS BAD CORROSION AROUND FASTENERS. REMOVED AND REPLACED FITTING IAW SRM 51-1-21, 51-1-20D AND DWG 3753645.

Part: SUPPORT CHANNEL — BROKEN (BS 360 L34L) · airframe 66,955 hrs · 28,063 cycles

INSPECTION TYPE:C1 STA 360 L34L FLOOR SUPPORT CHANNEL BROKEN. REMOVED, FABRICATED AND INSTALLED SUPPORT CHANNEL IAW SRM 51-1-21 AND DWG 9759429.

Part: SHEAR TIE — CORRODED (FS1400 L35-36R) · airframe 66,955 hrs · 28,063 cycles

INSPECTION TYPE:C1 AFTER REMOVAL OF SKIN FOUND SHEAR TIE CORROSION OUT OF LIMITS AND CRACKED AT STA 1400 BETWEEN L35R- L36. REMOVED, FABRICATED AND INSTALLED SHEAR TIE IAW SRM 51-1-21, 51-1-20D, 53-02-33.

Part: SHEAR TIE — CORRODED (FS 1380 L34L) · airframe 66,955 hrs · 28,063 cycles

AFTER REMOVAL OF SKIN FOUND SHEAR TIE CORRODED OUT OF LIMITS AND CRACKED AT STA 1380 L34L AND L35L. REMOVED SHEAR TIE AT FS 1380 L34L-L35L IAW SRM 51-01-20D. FABRICATED AND INSTALLED SHEAR TIES AT STA 1380 L34L-L35L IAW SRM 53-02-00-0, 51-1-8, AND SRM 51-1-20D.

Part: SHEAR TIE — CRACKED (FS1440 L33-34R) · airframe 66,955 hrs · 28,063 cycles

INSPECTION TYPE:C1 AFTER REMOVAL OF SKIN FOUND SHEAR TIE CORRODED OUT OF LIMITS AND CRACKED AT STA 1440 BETWEEN L33R-L34R. REMOVED, FABRICATED AND INSTALLED SHEAR TIE IAW 53-04-01 FIG 51, 51-1-20D AND 51-1-21.

Part: FINGER DOUBLER — CORRODED (FS1350-1390 L31R) · airframe 66,955 hrs · 28,063 cycles

INSPECTION TYPE:C1 AFTER SKIN REMOVAL FOUND FINGER DOUBLER CORRODED OUT OF LIMITS AND CRACKED STA 1350 - 1390 L31R. REMOVED, FABRICATED AND INSTALLED FINGER DOUBLER IAW SRM 53-04-01-0, 51-1-20D.

Part: SHEAR TIE — CORRODED (FS 1380 L35R) · airframe 66,955 hrs · 28,063 cycles

AFTER SKIN REMOVAL FOUND SHEAR TIE CORRODED OUT OF LIMITS AND CRACKED AT STA 1380 L35R-L36. REMOVED SHEAR TIE AT STA 1380 L35R-L36 IAW SRM 51-1-21. FABRICATED AND INSTALLED SHEAR TIE AT STA 1380 L35R-L36 IAW SRM 53-02-00-0, 51-1-8, SRM 51-1-21, 51-1-20D.

Part: SHEAR TIE — CRACKED (BS 1380 L31-32R) · airframe 66,955 hrs · 28,063 cycles

INSPECTION TYPE:C1 AFTER REMOVAL OF SKIN FOUND SHEAR TIE CORRODED OUT OF LIMITS AND CRACKED AT STA 1380 BETWEEN L31L-L32L. REMOVED, FABRICATED AND INSTALLED SHEAR TIE IAW SRM 53-04-01 FIG 51, 51-1-20D AND 51-1-21.

Part: KEELBEAM — CRACKED (BS 960) · airframe 66,955 hrs · 28,063 cycles

FITTING CRACKED ON RT CORNER IN RADIUS OF KEEL BEAM STA 960. REMOVED AND REPLACED L ANGLE AT STA 960 RT IAW SRM 51-1-2OD, 51-1-15 AND SRM 51-3-0.

Part: FITTING — CRACKED (FS 822 L22L) · airframe 66,955 hrs · 28,063 cycles

FOUND FRAME ATTACH FITTING CRACKED AT STA 822.500 L22L AFT SIDE. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 53-1-0 AND 51-3-2.

Part: ATTACH FITTING — CORRODED (BS 834 L22R) · airframe 66,955 hrs · 28,063 cycles

INSPECTION TYPE:C1 FRAME ATTACH FITTING HEAVY CORRODED AT STA 834.500 L22R. REMOVED AND REPLACED FRAME ATTACH FITTING IAW SRM 51-1-20D.

Part: LONGERON — CRACKED (BS 1440 L32L) · airframe 66,955 hrs · 28,063 cycles

FOUND POSSIBLE CRACK ON LONG 32L AT FS 1440. REMOVED DAMAGED LONGERON FROM STA 1350-1490, FABRICATE AND INSTALLED REPLACEMENT LONGERON SECTION IAW SRM 51-1-20D, 51-3-2 AND DWG 3645897.

Part: FLOORBEAM — CORRODED (BS 50 RBL10-50) · airframe 66,955 hrs · 28,063 cycles

INSPECTION TYPE:C1 IN A/C COMPT CEILING, FLOORBEAM STA 50 BETWEEN RBL 10-25 HAS CORROSION. REMOVED CORRODED UPPER FLANGE OF FLOORBEAM AT STA 50 RBL 10 -25 IAW SRM 51-1-8, AND SRM 53-2-0 FIG 1F. FABRICATED AND INSTALLED REPAIR FLANGE, REPAIR ANGLE AND REPAIR WEB AT STA 50 RBL 10-25 IAW DWG 3774606, AND SRM 53-03-01, 51-1-8 AND SRM 51-1-20D

Part: FITTING — CRACKED (BS 857 L7L) · airframe 66,955 hrs · 28,063 cycles

LONGERON END FITTING CRACKED AT STA 857.125 L7L. REMOVED AND REPLACED LONGERON END FITTING AT STA 857.125 L7L IAW 51-3-2 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 680 L5R) · airframe 66,955 hrs · 28,063 cycles

FOUND LONGERON END FITTING CRACKED AT STA 680 L5R. REMOVED AND REPLACED LONGERON END FITTING AT STA 680 L5R IAW SRM 51-01-21, 51-03-02-0 AND SRM 51-01-20D.

Part: FITTING — CRACKED (BS 902 L8R) · airframe 66,955 hrs · 28,063 cycles

FOUND LONGERON END FITTING AT STA 902.125 L8R IS CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 902.125 L8R IAW SRM 51-1-21, 51-1-20D, AND SRM 51-3-0.

Part: FITTING — CRACKED (FS 1150 L18R) · airframe 66,955 hrs · 28,063 cycles

FOUND ATTACH FITTING CRACKED AT STA 1150 L18R. REMOVED, FABRICATED AND INSTALLED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 700 L13R) · airframe 66,955 hrs · 28,063 cycles

FOUND FITTING CRACKED AT STA 700 L13R FWD SIDE. REMOVED CRACKED FITTING AT STA 700 L13R IAW SRM 51-1-20D. FABRICATED AND INSTALLED FITTING AT STA 700 L13R IAW DWG 3779978, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FS 820 L18L) · airframe 66,955 hrs · 28,063 cycles

FOUND FITTING CRACKED AT STA 820 L18L . REMOVED AND REPLACED END FITTING AT STA 820 L18L IAW SRM 51-1-20D, 51-03-02-0 AND SRM 51-01-08-0.

Part: FITTING — CRACKED (FS 834.500 L22R) · airframe 66,955 hrs · 28,063 cycles

INSPECTION TYPE:C1 FITTING CRACKED AT STA 834.500 L22R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1160) · airframe 66,955 hrs · 28,063 cycles

INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 1160 L19R AFT SIDE. REMOVE AND REPLACE FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 857 L9L) · airframe 66,955 hrs · 28,063 cycles

FOUND LONGERON END FITTING CRACKED AT STA.857.125 L9L. REMOVED AND REPLACED END FITTING IAW SRM 51-1-21 AND 51-1-20D.

Part: FITTING — CRACKED (FS 902 L4L) · airframe 66,955 hrs · 28,063 cycles

FOUND LONGERON END FITTING CRACKED AT STA 902.125 L4L. REMOVED AND REPLACED END FITTING AT STA 902.125 L4L IAW SRM 51-1-20D, 51-3-0 AND SRM 51-1-21.

Part: SKIN — CORRODED (BS 1350 L31L-32R) · airframe 66,955 hrs · 28,063 cycles

INSPECTION TYPE:C1 UPON REMOVAL OF D-PIT SCUFF PLATE FOUND LWR SKIN CORRODED IN SEVERAL AREAS BEYOND LIMITS. REMOVED AND REPLACED LWR BELLY SKIN AT STA 1350-1450 L31L TO L32R IAW SRM 51-01-20D, 51-01-21, AND DWG 5615572

Part: SKIN — CRACKED (BS 1746 L17L) · airframe 66,955 hrs · 28,063 cycles

FOUND FUSELAGE SKIN CRACKED 1" LONG AT STA 1746 L17L. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7, 51-1-21 AND 51-1-20D.

Part: FITTING — CRACKED (BS 1180 L20R) · airframe 66,955 hrs · 28,063 cycles

FOUND STA 1180 L20R FITTING CRACKED. REMOVED AND REPLACED END FITTING AT STA 1180 L20R IAW SRM 51-1-20D, 51-3-2 AND 51-1-8.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD PER AMM 33-50-01-2.

Part: INDICATOR — INOPERATIVE (COCKPIT)

ALL 3 (CAPT'S, FO'S & ALTERANTE) AIRSPEED INDICATIONS ARE UNRELIABLE. AIR TURN BACK - EMERGENCY DECLARED. REPLACED STANDBY ALT/AIRSPEED INDICATOR PER MM 34-11-02-4. R&R AUXILIARY PITOT STATIC DRAIN. SYSTEM OPS CKS NORMAL IAW AMM 34-12-00-5.

Part: ADC — FAILED (NR 1)

INSPECTION TYPE:N/A ATB - AFTER T/O LOST NR 1 ADC, PULLED C/B COULD NOT RESTORE, XFRD TO NR 2 ADC ON CAPT SIDE. ATB DUE TO SLIGHT ELEC BURNING SMELL. REMOVED AND REPLACED AIR DATA COMP IAW MM 34-11-01-4 AND NR 1 ADC SELECT XFR RELAY IAW MM 20-50-16-2. CHECK WIRE FROM C/B'S TO RELAY TO ADC NO DEFECTS NOTED. AIR DATA COMPUTER & XFR RELAY NEEDS OPS CHECK. PERFORMED ADC TEST PER MM 34-11-00.

Part: INTERCOSTAL — CRACKED (FUSLEAGE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, STATION 25 CUSP WEB/INTERCOSTAL IS CRACKED AT LONG 21L. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B.

Part: BEARING — CORRODED (HORIZONTAL STAB) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, LEFT HORIZONTAL STAB HINGE BEARING WILL NOT ACCEPT GREASE. DISASSEMBLED HINGE. FOUND STAB BEARING BORE CORRODED. REPAIRED PER SAA SK 703-677 AND UPS EO DC8-5510-19991-A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, STATION 1270 LONG 35L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3759258 AND SRM 51-1-20D, 51-3-0.

Part: RIB — CRACKED (RT WING LE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, RT WING O/B LEADING EDGE LOWER RIB IS CRACKED AT XFS 825. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2.

Part: ANGLE — CRACKED (A/C COMPARTMENT) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, STATION 55, LBL 50 TWO INTERCOSTAL ANGLE SUPPORTS ARE CRACKED. REMOVED, FABRICATED AND INSTALLED ANGLE SUPPORTS IAW DWG 4888755, 4888754 AND SRM 51-1-21.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, FUSELAGE SKIN IS CRACKED AT FASTENER HOLE AT STATION 1342 LONG 31R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, INTERNAL FINGER DOUBLER IS CORRODED BEYOND LIMITS STATION 1260-1350 LONGERON 31R. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW SRM 53-4-1 FIG 17A, 51-1-20D, 51-1-21.

Part: BRACKET — CRACKED (RT OB AILERON) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, RIGHT O/B AILERON HINGE BRACKET IS CRACKED AT STATION 610.882. REMOVED AND REPLACED BRACKET IAW DWG 3653812 AND SRM 51-1-21.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, STATION 1270 LONG 36 IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION BETWEEN STATION 1270 - 1310, FABRICATED AND INSTALLED STRAP DOUBLERS AND CHANNELS IAW UPS ENGINEERING FILE DC8-53-20393 AND SAA SK 703-514.

Part: RIB — CRACKED (RT WING LE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, RIGHT WING CENTER L/E LOWER RIB HAS A HOLE WORN THRU AT XFS 416. REMOVED DAMAGE, NDT VERIFIED NO CRACKS AT DAMAGE REMOVAL. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, STATION 1240 LONG 33R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4758514 AND SRM 51-1-20D.

Part: FITTING — CRACKED (AFT CARGO BAY) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, STATION 1200 LONG 27L BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755849 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSLEAGE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, STA 1270 LONG 36 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3759222 AND SRM 51-1-20D.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, FUSELAGE SKIN IS CORRODED BEYOND LIMITS AT STATION 1265 AT LONG 36. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, LONGERON 35R INTERCOSTAL TO FRAME ATTACH FITTING AT STA 1230 IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758570 AND SRM 51-1-20D.

Part: RIB — CRACKED (RT WING LE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIBS ARE CRACKED AT XFS 410.25, XFS 347.75, XFS 354. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING LE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 641.25. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING LE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XS 478.897. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING LE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, RT WING L/E UPPER RIB IS CRACKED AT XFS 728.75. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, STATION 1235, LONG 33R SUPPORT ANGLE IS CRACKED AND INTERCOSTAL IS GOUGED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED SUPPORT ANGLE AND INTERCOSTAL IAW DWG 9754949, 4758514 AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (RT WING LE.) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, RT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 597.5. REMOVED, FABRICATED AND REPLACED INTERNAL DOUBLER IAW DWG 5760545 AND SRM 51-1-21, 51-1-20D.

Part: RIB — CRACKED (RT WING LE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, RIGHT WING L/E LOWER RIBS ARE CRACKED AT XFS 847.5, XFS 791.25. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILL TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (FLOORBEAM) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, MAIN CABIN FLOORBEAM SUPPORT FITTING IS CRACKED AT STA 798, RBL 23. REMOVED AND REPLACED FITTING IAW DWG 3773906 AND SRM 51-1-20D.

Part: INTERCOSTAL — CRACKED (AC. COMPARTMENT) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, STATION 55 LBL 50 INTERCOSTAL IS CRACKED BELOW CEILING. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5758542 AND SRM 51-1-20D.

Part: SUPPORT — CRACKED (A/C COMPARTMENT) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE:C3 A/C BAY CEILING SUPPORT ANGLE IS CRACKED AT STATION 55 LBL 30. REMOVED, FABRICATED AND REPLACED ANGLE FITTING IAW DWG 4774654 AND SRM 51-1-20D.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, FLOOR SUPPORT FITTING IS CRACKED AT STATION 340 LONG 36-33L. REMOVED AND REPLACED FITTING IAW DWG 9754002 AND SRM 51-1-20D.

Part: FLOOR SUPPORT — CRACKED (MAIN CABIN) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, MAIN CABIN FLOOR SUPPORT CHANNEL IS CRACKED AT STA 863 AT LBL 23. REMOVED, FABRICATED AND REPLACED SUPPORT CHANNEL IAW DWG 5758265 AND SRM 51-1-20D.

Part: SUPPORT FITTING — CRACKED (FLOORBEAM) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, MAIN CABIN FLOORBEAM SUPPORT FITTING IS CRACKED AT STA 822 RBL 23. REMOVED AND REPLACED FITTING IAW DWG 3773906 AND SRM 51-1-20D.

Part: SUPPORT FITTING — CRACKED (CABIN SUBFLOOR) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, FLOORBEAM SUPPORT FITTINGS ARE CRACKED AT STATION 798 AND 822 AT LBL 23. REMOVED, FABRICATED AND REPLACED FITTINGS IAW DWG 3773906 AND SRM 51-1-20D.

Part: SUPPORT FITTING — CRACKED (FLOORBEAM) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, MAIN CABIN FLOORBEAM SUPPORT FITTING IS CRACKED AT STATION 742 RBL 23. REMOVED AND REPLACED FITTING IAW DWG 3773906 SRM 51-1-20D, 51-3-0.

Part: SUPPORT FITTING — CRACKED (TE FLAP) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, RIGHT O/B FLAP HINGE 219 I/B SUPPORT FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3653781 AND SRM 51-1-20D.

Part: RIB — CRACKED (LT WING LE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 828.75, XFS 816.25, XFS 810, XFS 803.75. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING LE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 791.250. STOPODRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING LE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 766.250. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING LE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 778.75. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING LE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE:C3 LEFT WING CENTER L/E UPPER RIB IS CRACKED AT XS 491. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.

Part: PANEL — CORRODED (LT OB.AILERON) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, LT WING OUTBOARD AILERON WEIGHT PANEL IS CORRODED BEYOND LIMITS BETWEEN XA 614 TO XA 638. REMOVED, FABRICATED AND REPLACED WEIGHTED PANEL IAW DWG 5764617 AND DOUBLER IAW DWG 5763133 AND SRM 51-1-21, 51-3-0.

Part: RIB — CRACKED (RT WING LE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 835. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING LE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, LT WING L/E LOWER RIB IS CRACKED AT XFS 822.5. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING LE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE:C3 LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 372.75, XFS 379. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, SUBFLOOR INTERCOSTAL IS CRACKED AT STATION 1736 RBL 35. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 3755032 AND SRM 51-1-20D.

Part: LONGERON — CRACKED (AFT CABIN) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, STATION 1731 LONG 14L IS CRACKED. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 53-2-2 FIG 12.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, STATION 1735 LONGERON 13R IS CRACKED. REMOVED DAMAGED LONGERON SECTION BETWEEN STATION 1716-1742, FABRICATED AND INSTALLED LONGERON SECTION, STRAPS AND INSTALLED SPLICE FITTING IAW SRM 53-2-2 FIG 10.

Part: SUPPORT — CRACKED (INTERCOSTAL) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, INTERCOSTAL SUPPORT CLIP IS CRACKED ON FWD SIDE OF AFT PRESSURE BULKHEAD STATION 1766 AT LONG 4L. REMOVED, FABRICATED AND REPLACED SUPPORT CLIP IAW DWG 5773844 AND SRM 51-1-20D.

Part: RIB — GOUGED (NR 1 SPOILER) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE:C3 LEFT WING TRAILING EDGE NR 1 SPOILER OUTBOARD DOWN STOP RIB IS GOUGED BEYOND LIMITS AT XW 90. BLENDED OUT GOUGE, NDT VERIFIED NO CRACKS, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE:C3 RIGHT STATION 1723 SHEAR TIE AND FRAME SECTION ARE CORRODED BEYOND LIMITS BETWEEN LONG 30R AND 31R. REMOVED, FABRICATED AND REPLACED SHEAR TIE AND FRAME SECTION IAW SRM 53-5-3 FIG 3 AND 53-2-0 FIG 2.

Part: FLOOR SUPPORT — CORRODED (AFT CABIN) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE: C3, AFT PRESSURE BULKHEAD FWD SIDE FLOOR SUPPORT CHANNEL AND ANGLE IS CORRODED BEYOND LIMITS STATION 1766 LBL 5 - LBL 15. REMOVED, FABRICATED AND REPLACED SUPPORT CHANNEL AND ANGLE IAW DWG 5753522, 5755032 AND SRM 51-1-20D, 51-1-21, 51-3-0.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,095 hrs · 27,384 cycles

INSPECTION TYPE:C3 FUSELAGE SKIN IS CORRODED BEYOND LIMITS STATION 1690-1700 LONG 35L-35R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

DURING CLIMB OUT MAIN CARGO COMPARTMENT SMOKE INDICATOR ILLUMINATED. REMOVED AND REPLACED NR 6 SMOKE DETECTOR ASSEMBLY REF 26-10-07, ADJ/TEST OPS GOOD.

Part: PRESSURE PANEL — CORRODED (RT MLG WW)

BULGE AND POPPED FASTENERS IN RT W/W PRESSURE PANEL POSSIBLE FERRY FOR REPAIR. FABBED REPAIR PARTS IAW REO G08940, ALODINED & PRIMED IAW DC8 SRM 51 -1-8 FABBED STIFFENER SPLICES AND STRAPS IAW DAC DWG SR08530029, INSTALLED REPAIR SPLICES AND STIFFENER IAW DC8 SRM 51-1-20D & 51-1-21 INSTALLED CABLE PULLEY AND BRACKET IAW DC8 SRM 51-3-0

Part: FLOORBEAM — CORRODED (FUSELAGE)

STA 990, RT SIDE OUTBOARD FLOORBEAM LOWER FLANGE CORRODED POSSIBLE FERRY FOR REPAIR. FABBED REPAIR PARTS IAW REO G08940, ALODINED & PRIMED IAW DC8 SRM 51 -1-8 FABBED STIFFENER SPLICES AND STRAPS IAW DAC DWG SR08530029, INSTALLED REPAIR SPLICES AND STIFFENER IAW DC8 SRM 51-1-20D

Part: WIRE — BROKEN (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS REMAINED ON AFTER SWITCHING TO SHIPS POWER. REPAIRED BROKEN WIRE AT EMERGENCY BATTERY PACK CANNON PLUG, OPS CHECK GOOD PER MM 33-50-02.

Part: CONNECTOR — BURNED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS REMAINED ON. FOUND BURNT CONTACTS ON CANNON PLUGS. AIRCRAFT 779 COVERED FLIGHT PARTS ON ORDER.

Part: CLIP — CRACKED (RT WING) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 RT WING CLIP CRACKED AT XW467 BETWEEN S62 AND S63. REMOVED AND REPLACED CLIP IAW SRM 51-1-20D AND DAC DWG 5804006.

Part: CLIP — CRACKED (LT WING) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 LEFT WING NR 1 ALT TANK HAS 2 ATTACH CLIPS CRACKED AT O/B SKATE ANGLE AT XW485 BETWEEN STRINGER 62 & 63. REMOVED, FABRICATED ONE CLIP, REPLACED OTHER CLIP AND INSTALLED BOTH CLIPS IAW DWG 5804006 AND 5804007 AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 STA 1753 CANTED FRAME HAS LONGERON 15L CRACKED. CUT OUT DAMAGED SECTION OF LONGERON, FABRICATED AND INSTALLED LONGERON REPAIR IAW SRM 53-2-2 FIG 10.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 LOWER FLANGE CRACKED ON LONG 15R, STA 1753. REMOVED CRACKED LONGERON SECTION. FABRICATED SPLICE AND INSTALLED REPLACEMENT LONGERON SECTION PER 53-2-2 FIG 10.

Part: FITTING — CRACKED (LT WING) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 STRINGER FITTING CRACKED BETWEEN XRS 50 AND XRS 74 AT STRINGER 51 IN LEFT WING TANK. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D, 51-1-20D, 51-1-23.

Part: PAN — CRACKED (FUSELAGE) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 STA 200 LONG 20R WEB AND DOOR PAN ARE CRACKED AT R-1 DOOR AFT LOWER CORNER. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED REPAIR DOUBLERS ON PAN AND WEB IAW SRM 53-2-0 FIG 23 AND DWG 5615700.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 LONGERON 11R CRACKED AT R2 DOOR UPPER AFT CORNER. REMOVED CRACKED LONGERON SECTION FROM 1570 TO 1690. INSTALLED REPLACEMENT SECTION IAW SRM 53-1-0, 51-1-21, 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 341.5. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATED, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 LEFT WING CENTER L/E VERTICAL ATTACH ANGLE IS CRACKED AT LOWER END AT XS 520. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW DWG 9753297 AND SRM 51-1-20D.

Part: DOUBLER — BROKEN (LT WING) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 LT WING LOWER SPAR CAP DOUBLER BROKEN, PIECE MISSING AT XS520. REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM 57-2-1 FIG 14 A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 STA 388 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754473 AND SRM 53-1-0, 51-1-20D.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 L2 LOWER AFT FRAME CRACKED AT STA 1660 NEAR 19L. REMOVED DAMAGED FRAME SECTION. FAB AND INSTALLED FRAME SECTION, FILLER AND DOUBLER PER DAC DWG 5751040, DC8-5310-11728 AND DC8-53A-011.

Part: STIFFENER — CRACKED (HORIZ STAB) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 LEFT HORIZONTAL STAB L/E STIFFENER IS CRACKED AT XAR 0. REMOVED AND REPLACED STIFFENER IAW DWG 5654501 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 FRAME FITTING IS CRACKED AT STA 781 ON FWD SIDE ABOVE WING CENTER SECTION LBL 59. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 5641007, 8110-3 APPROVED DH SK 703-641 AND DC8-53-20143A.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 STA 118 LONG 36 IS CORRODED BEYOND LIMITS. REMOVED CORRODED LONGERON SECTION STA 100-130, FABRICATED AND INSTALLED LONGERON REPAIR IAW SRM 53-2-2 FIG 10.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 X-RAY REVEALED ONE INCH CRACK AT R2 DOOR UPPER AFT DOUBLER STA 1660 LONG 11R. CUT OUT DAMAGE. NDT VERIFIED ALL DAMAGE REMOVED. FABRICATED AND INSTALLED FILLER AND DOUBLERS PER SRM 53-1-0 FIG 16.

Part: SKIN — CRACKED (LT WING) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 LEFT WING CENTER L/E UPPER SKIN IS CRACKED AND HAS INTERGRANULAR CORROSION BETWEEN XFS 341 TO XFS 366.5. CUT OUT CRACKED AND CORRODED AREAS, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED DOUBLER AND FILLERS IAW SRM 57-2-1 FIG 38 AND UPS DC8-57-20040 AND DH SK 703-448.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 L35L HEAVILY CORRODED AT SPILCE FITTING, STA 1690. CUT OUT CORRODED SECTION OF LONG, FABRICATED AND INSTALLED LONGERON REPAIR IAW SRM 53-2-2 FIG 10.

Part: SKIN — CORRODED (LT WING) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 LEFT WING CENTER L/E UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 329. CUT OUT CORRODED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 38.

Part: WEB — CORRODED (FUSELAGE) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 STATION 1322 LONG 21L AT LBL 67 CUSP IS CORRODED BEYOND LIMITS. CUT OUT CUSP SECTION BETWEEN STA 1250-1390, FABRICATED AND INSTALLED REPAIR SECTION OD CUSP IAW DWG J060296 AND SRM 53-2-5 FIG 15.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 STA 1580 FUSELAGE FRAME IS CRACKED AT LOWER END AT LONG 21L. REMOVED DAMAGED AREA, NDT VERIFIED NO CRACKS AROUND CUTOUT, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EO DC8-53A-011.

Part: SKIN — CRACKED (LT WING) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 LEFT WING L/E LOWER SKIN IS CRACKED AT DRAIN HOLE AT XFS 597.5. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATED, FABRICATED AND INSTALLED DOUBLER IAW EO DC8-5780-4087-B APPX C.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,149 hrs · 26,648 cycles

INSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED BEYOND PREVIOUS REPAIR CUTOUT, AT STATION 25 BETWEEN LONG 10L TO 11L AT L-1 DOOR FWD UPPER CORNER OPENING. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS, FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW SRM 53-2-0 FIG 15.

Part: ANGLE — CRACKED (MLG WW)

INSPECTION TYPE:B STA 958 CRACKED T-ANGLE ATTACHED TO KEEL BEAM. REMOVED AND REPLACED TEE IAW DRAWING 5616306.

Part: ANGLE — CRACKED (FUSELAGE)

INSPECTION TYPE:PFLT, CRACKED T-ANGLE ATTACHED TO KEEL BEAM. *S/D* REMOVED AND REPLACED TEE.

Part: RELAY — FAILED (COCKPIT)

INSPECTION TYPE:N/A, CREW PREFLT-MASTER WARNING LIGHT FAILS TO RESET. REMOVED AND REPLACED R2-94 RELAY R2-100.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:IN EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK. TESTS OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP ON PRE-DEPARTURE CHECK. REPLACED BATTERY PACK.

Part: BATTERY PACK — INOPERATIVE (COCKPIT)

INSPECTION TYPE:PFLT EMERGENCY LIGHT INOP R/R BATTERY PACK ASSY PER MM 33-50-00

Part: COUPLING — LEAKING (RT WING)

INSPECTION TYPE:N/A PIREP-FUEL LEAKING FROM RH WING ***SUPPLEMENTAL MRR*** FOUND GAMA COUPLING LEAKING RT INBD WING REPAIRED COUPLING NOTE: THIS WAS ON THE DAILY EXCP AGAINST 703 WHEN IT SHOULD HAVE BEE N TAIL 801 LOG PAGE ON THIS MRR IS ON 801 VOIDED THIS AND RESUBMITTE D ON UPS00834556

Part: CONTROLLER — SLUGGISH (RUDDER)

INSPECTION TYPE:N/A, RUDDER REMAINS ULTRA SENSITIVE AFTER T/O W/FLAPS UP AND YAW DAMPER ON OR OFF. MILD PRESSURE ON RUDDER PEDAL RESULTS IN LARGE YAW DEFLECTIONS IN FLIGHT. PERFORMED ADJ/TEST FOR RUDDER HYD PRESSURE REDUCER VALVE CHECK IAW MM 27-21-07. ACCOMPLISHED TASK NR 0224 FUNCTIONAL CHECK FOR RUDDER HIGH PRESSURE ANNUNCIATOR SYSTEM AND FOUND NORMAL. ALSO VERIFIED PHYSICALLY ALL COMPONENTS ON TAIL SECTION AND FOUND OK. OPERATED RUDDER SEVERAL TIMES, CHECKED NORMAL. UNABLE TO DUPLICATE PROBLEM. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK.

Part: BATTERY PACK — INOPERATIVE (CABIN)

EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. EMERGENCY LIGHTS OPS CHECK GOOD IAW 33-50-00

Part: FITTING — CRACKED (BS 1140)

INSPECTION TYPE:C1 STA 1140 LONGERON 33R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1140)

INSPECTION TYPE:C1 STA 1140 LONGERON 33R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514, AND SRM 51-1-20D.

Part: FITTING — FITTING (BS 1050)

INSPECTION TYPE:C1 STA 1050 LONGERON 31L CENTER SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 51-1-20D.

Part: ANGLE — CORRODED (BS 80)

INSPECTION TYPE:C1, STA 80 LBL 36 HORIZONTAL ANGLE AND WEB WERE CORRODED BEYOND LIMITS. REPAIRED PER SRM 53-2-0 FIG 1B.

Part: RIB — CRACKED (RT WING)

INSPECTION TYPE:C1, RT WING L/E NR 3 STUB WING UPPER RIB CRACKED AT XILD .7095. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-3-1 FIG 3, 51-1-21, 51-1-20D.

Part: RIB — CRACKED (WS 227)

INSPECTION TYPE:C1, RT WING L/E NR 3 STUB WING UPPER RIB CRACKED AT XS227.335. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2, 51-1-21, 51-1- 20D.

Part: RIB — CRACKED (WS 207)

INSPECTION TYPE:C1, RIGHT WING NR 3 STUB WING UPPER WAS CRACKED AT XFS207.5. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-3-0 FIG 3, 51-1-21, 51-1-20D.

Part: SKIN — CRACKED (BS 1050)

INSPECTION TYPE:C1, INTERNAL SKIN BULGED AND CRACKED STA 1050 AT LONG 36. REPAIRED IAW DH SK 703-443.

Part: SHEAR TIE — CRACKED (BS 680)

INSPECTION TYPE:C1 STA 680 LONGERON 31L-32L SHEAR TIE IS CRACKED. REMOVED FABRICATED, AND REPLACED SHEAR TIE IAW DWG 3753753, AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 256)

INSPECTION TYPE:C1, RT WING L/E NR 3 STUB WING UPPER WAS CRACKED AT XS 256.339. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2, 51-1-20D, 51-1-21.

Part: SHEAR TIE — CRACKED (BS 680)

INSPECTION TYPE:C1 STA 680 LONGERON 33L-34L SHEAR TIE IS CRACKED. REMOVED, FABRICATED, AND REPLACED SHEAR TIE IAW DWG 3753753, AND SRM 51-1-20D.

Part: FRAME — CORRODED (BS 1380)

INSPECTION TYPE:C1 STA 1380 FRAME LOWER FLANGE CORRODED BEYOND LIMITS AT LONGERON 33L. REPAIRED IAW DC8-53A-010, AND DC8-5310-11728-A.

Part: SEAT TRACK — CORRODED (BS 1380)

INSPECTION TYPE:C1, STA 1380 RBL 24 SEAT TRACK CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A.

Part: FRAME — CORRODED (BS 1040)

INSPECTION TYPE:C1 STA 1040 FRAME UPPER FLANGE AT LONGERON 31L IS CORRODED BEYOND LIMITS. REPAIRED IAW SRM. ADDENDUM DC8-5310-11728-A.

Part: SEAT TRACK — CORRODED (BS 1380)

INSPECTION TYPE:C1, STA 1380 RBL 24 SEAT TRACK CORRODED BEYOND LIMITS. REMOVED AND REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A, 51-3-0.

Part: FRAME — CORRODED (BS 280)

INSPECTION TYPE:C1 STA 280 FRAME HAS HEAVY CORROSION BETWEEN 35L TO 35R UNDER FLANGE. REPAIRED IAW SRM 53-2-0 FIG 23.

Part: RIB — DAMAGED (WS 257)

INSPECTION TYPE:C1 RIGHT WING L/E RIB AT XW 257.5 IS DAMAGED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED RIB IAW DWG 5769517, AND SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1160)

INSPECTION TYPE:C1 STA 1160 LONGERON 34L BATH TUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3755845, AND SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 1020 & 1040)

INSPECTION TYPE:C1 STA 1020 AND 1040 LONGERON 31L ATTACHMENT FLANGES ARE CORRODED BEYOND LIMITS. REPAIRED IAW 8110-3 APPROVED DH SK 703-287.

Part: INTERCOSTAL — CORRODED (BS 1440 - 1447)

INSPECTION TYPE:C1, STA 1440-1447 LONG 34R INTERCOSTAL UPPER FLANGE CORRODED BEYOND LIMITS. REMOVED, FABRICATED, REPLACED INTERCOSTAL IAW DWG 5616674, SRM 51-1 -21, 51-1-20D.

Part: FLOOR BEAM — CORRODED (BS 80)

INSPECTION TYPE:C1 STA 80 RBL 50 UPPER AFT FLOOR BEAM FLANGE IS CORRODED BEYOND LIMITS. REPAIRED IAW 8110-3 APPROVED DH SK 703-301.

Part: INTERCOSTAL — CORRODED (BS 1390)

INSPECTION TYPE:C1, STA 1390 AT LONG 34R INTERCOSTAL AND INTERCOSTAL SPLICE CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED IAW DWG 56166674 SRM 51-1-20D, 51-1-21.

Part: DOUBLER — CORRODED (BS 290 - 940)

INSPECTION TYPE:C1 STA 920-940 LBL 62 PRESSURE WEB AND FINGER DOUBLER ARE CORRODED BEYOND LIMITS. REPAIRED IAW 8110-3 DH SK 703-151, AND DWG 5645332.

Part: FITTING — CRACKED (BS 924)

INSPECTION TYPE:C1 STA 924 LBL 62 FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3649114, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 440 - 460)

INSPECTION TYPE:C1 LONGERON 31L SPLICE FITTING IS CRACKED AT STA 440-460. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1140)

INSPECTION TYPE:C1 STA 1140 LONGERON 35R AFT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758497, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1140)

INSPECTION TYPE:C1 STA 1140 LONGERON 35L AFT. FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758497, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1220)

INSPECTION TYPE:C1 STA 1220 LONGERON 33R-34R BATH TUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755841, AND SRM 53-2-0 FIG 2G.

Part: RIB — CRACKED (WS 329)

INSPECTION TYPE:C1 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: RIB — CRACKED (WS 616)

INSPECTION TYPE:C1 LEFT WING L/E AT STA XFS616.250, THE LOWER L/E RIB FWD OF ACCESS PANEL OPENING HAS A 3 INCH CRACK. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 1340 - 1360)

INSPECTION TYPE:C1 STA 1340-1360 LONGERON 36 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779919, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1180)

INSPECTION TYPE:C1, STA 1180 AT LONG 27L FITTING WAS CRACKED (DOOR OPEN/STOP/FRAME FITTING). REMOVED AND REPLACED FITTING IAW DWG 3755854 AND SRM 51-1-20D.

Part: DOUBLER — CORRODED (COCKPIT)

INSPECTION TYPE:C1 STA 8 TO -12 FINGER DOUBLER HAS BULGING CORROSION AND POPPED RIVETS IN COCKPIT SUBFLOOR. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5645828, AND SRM 51-1-21.

Part: FRAME — CORRODED (BS 1140)

INSPECTION TYPE:C1 STA 1140 FRAME HAS HEAVY INTERGRANULAR CORROSION BETWEEN LONGERON 34R AND 35R. REPAIRED IAW APPROVED 8110-3 DHSK 703-990 .

Part: RIB — CRACKED (WS 297.5)

INSPECTION TYPE:C1, LEFT WING L/E AT STA XFS297..500, THE LOWER 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 1360)

INSPECTION TYPE:C1 STA 1360 LEFT TOP SIDE CUSP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4640162, AND SRM 51-1-20D.

Part: SKIN — CRACKED (LT WING)

INSPECTION TYPE:C1 LEFT O/B SLOT VANE EXTERIOR SKIN IS CRACKED AT THE O/B END. REPAIRED AREA IAW SRM 57-2-0 FIG 2A.

Part: FITTING — CRACKED (BS 1160)

INSPECTION TYPE:C1 STA 1160 LONGERON 34R-35R BATH TUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755841, AND SRM 53-2-0 FIG 17.

Part: SKIN — CRACKED (WS 572)

INSPECTION TYPE:C1, RT WING L/E AT STA XFS572.00, THE INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769891 AND SRM 51-1-21.

Part: FITTING — CRACKED (BS 1160)

INSPECTION TYPE:C1 STA 1160 LONGERON 22R FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3893497, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 834)

INSPECTION TYPE:C1 STA 834 LONGERON 18R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779874, AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN)

INSPECTION TYPE:C1 STA 759 RBL 24 SEAT TRACK TO FLOORBEAM FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755222 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 834 - 857)

INSPECTION TYPE:C1, STA 834-857, LONGERON 4L END FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3779659 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 442.185)

INSPECTION TYPE:C1 RT WING L/E AT STA XS442.185, 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 448)

INSPECTION TYPE:C1, RT WING L/E AT STA XFS 448.581, 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 1220)

INSPECTION TYPE:C1, LONGERON 18R TO INTERCOSTAL ATTACH FITTING IS CRACKED AT STA 1220. REMOVED AND REPLACED FITTING IAW DWG 3779978 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 834 - 857)

INSPECTION TYPE:C1 STA 834-857 LONGERON 5L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659, AND SRM 51-1-20D, 51-1-21.

Part: SEAT TRACK — CRACKED (BS 1040)

INSPECTION TYPE:C1 STA 1040 RBL 24 SEAT TRACK IS CRACKED. REPAIRED IAW SRM 53-2-3.

Part: FITTING — CRACKED (BS 789)

INSPECTION TYPE:C1, SEAT TRACK TO FLOORBEAM ATTACH FITTING IS CRACKED AT STA 798 RBL24. REMOVED AND REPLACED FITTING IAW DWG 3755222 AND SRM 51-1-20D.

Part: FRAME — CORRODED (BS 1220)

INSPECTION TYPE:C1, STA 1220 FRAME ABOVE LONG 34L TO LONG 36 WAS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FRAME IAW DWG 9754002 AND SRM 51-1-21.

Part: SKIN — CORRODED (BS 620)

INSPECTION TYPE:C, STA 620 LONG 35L TO LONG 36 SKIN HAD BULGING CORROSION. REPAIRED IAW 8110-3 APPROVED DH SK703-767.

Part: FRAME — CORRODED (BS 180)

INSPECTION TYPE:C1 STA 180 BETWEEN STR 33R-34R, THE FRAME HAS HEAVY CORROSION. REPAIRED AREA IAW UPS EO DC8-5310-11728A.

Part: FITTING — CRACKED (BS 1040 - 1060)

INSPECTION TYPE:C1, STA 1040-1060 STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN)

INSPECTION TYPE:C1, STA 717 RBL 24 THE SEAT TRACK TO FLOORBEAM FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755222-2, AND SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 455)

INSPECTION TYPE:C1, STA 455 LONG 36 WAS CORRODED BEYOND LIMITS. REPAIRED IAW SRM 53-2-2 FIG 10 AND 8110-3 APPROVED DH SK 703- 762.

Part: FITTING — CRACKED (BS 620)

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

Part: RIB — CRACKED (WS 304)

INSPECTION TYPE:C1 RIGHT WING L/E AT XFS304 UPPER RIB IS CRACKED STOP DRILLED CRACK AND REPAIRED I.A.W. SRM 57-2-0 FIG. 2

Part: FITTING — CRACKED (BS 1160)

INSPECTION TYPE:C1 STA 1160 LONGERON 19R ANGLE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750419, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 834 - 857)

INSPECTION TYPE:C1 STA 834-857 LONGERON 7R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 620 - 640)

INSPECTION TYPE:C1, STA 620-640 LONG 31L SPLICE FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1180)

INSPECTION TYPE:C1 STA 1180 AT LONGERON 17R, THE ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 408.34)

INSPECTION TYPE:C1 RT WING L/E AT STA XS408.3434, 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 1180)

INSPECTION TYPE:C1, STA 1180 LONGERON ATTACH FITTING 18R IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (WS 335)

INSPECTION TYPE:C1 RIGHT WING L/E AT STA XFS 335.250 INTERNAL DOUBLER IS CRACKED. REMOVED, FABRICATED, AND REPLACED IAW DWG 5718963, AND SRM 51-1-21, 51-1-20D.

Part: SHEAR TIE — CRACKED (BS 1520)

INSPECTION TYPE:C1 STA 1520 BETWEEN LONGERON 36 AND 35R SHEAR TIE IS CRACKED. REPAIRED IAW SRM 53-2-0 FIG 2A AND 2B.

Part: FITTING — CRACKED (BS 380)

INSPECTION TYPE:C1, STA 380 LONG 27L SPLICE FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754220, AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (BS 758)

INSPECTION TYPE:C1 STA 758 LONGERON 18R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779874, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1040 - 1060)

INSPECTION TYPE:C1 STA 1040-1060 LONGERON 1 FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750271, AND SRM 51-1-20D.

Part: SEAT TRACK — CRACKED (BS 865)

INSPECTION TYPE:C1 STA 865 RBL 24 SEAT TRACK IS CRACKED AT UPPER FLANGE. REPAIRED IAW SRM 53-2-3.

Part: FITTING — CRACKED. (BS 717)

INSPECTION TYPE:C1, FLOORBEAM ATTACH FITTING IS CRACKED AT STA 717 LBL24. REMOVED AND REPLACED FITTING IAW DWG 3755222 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 781)

INSPECTION TYPE:C1 STA 781 LONGERON 18R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779874, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 798)

INSPECTION TYPE:C1 STA 798 LONGERON 13L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751642, AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 16.225)

INSPECTION TYPE:C1, RT WING L/E AT STA XOLDI6.225, THE LOWER L/E RIB IS CRACKED AT THE AFT END. REPAIRED AREA IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 834 - 857)

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

Part: FITTING — CRACKED (BS 902 - 920)

INSPECTION TYPE:C1 STA 902-920 LONGERON 1 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750521,AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1220)

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

Part: FITTING — CRACKED (BS 857)

INSPECTION TYPE:C1, STA 857 LONG 4R END FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758498 AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (BS 1160)

INSPECTION TYPE:C1, STA 1160 AT 17R LONG TO FRAME FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 822)

INSPECTION TYPE:C1 STA 822 LBL 62 INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4753360, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1220)

INSPECTION TYPE:C1 STA 1220 LONGERON 17R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750419, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1230)

INSPECTION TYPE:C1 STA 1230 LONGERON 19R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750418, AND SRM 51-1-20D.

Part: CUSP — CRACKED (BS 400 - 405)

INSPECTION TYPE:C1 STA 400-405 RT HORIZONTAL FLANGE IS CRACKED. REPAIRED IAW SRM 53-2-5 FIG 15.

Part: FITTING — CRACKED (BS 798)

INSPECTION TYPE:C1 STA 798 LONGERON 18L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779874, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 380)

INSPECTION TYPE:C1 STA 380 LONGERON 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754473, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 781)

INSPECTION TYPE:C1 STA 781 RBL 24 SEAT TRACK TO FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755222, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 702)

INSPECTION TYPE:C1 STA 702 RBL 24 SPLICE FITTING UNDER SEAT TRACK IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755222, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 857)

INSPECTION TYPE:C1, STA 857 LONG 18L INTERCOSTAL TO FRAME FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779498 AND SRM 51-1-20D.

Part: SKIN — CRACKED (WS 324)

INSPECTION TYPE:C1, LT WING L/E UPPER SKIN AT STA XFS.324.0 AT THE SPAR IS CRACKED BETWEEN 2 FASTENERS. REPAIRED AREA IAW UPS EO DC8-5720-7767A.

Part: RIB — CRACKED (WS 335.25)

INSPECTION TYPE:C1 RT WING L/E ATV STA XFS335.25, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED AREA IAW SRM 57-2-0 FIG 2 AND 57-3-1.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:C1 STA 680 LONGERON 11L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779498, AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 857)

INSPECTION TYPE:C1, STA 857 LONG 19R INTERCOSTAL TO FRAME ATTACH FITTING CRACKED. REMOVED, FABBED, AND REPLACED FITTING IAW DWG 3779498, SRM 51-1-20D.

Part: SKIN — CRACKED (WS 360.250)

INSPECTION TYPE:C1, RT WING L/E UPPER SKIN IS CRACKED AT STA XFS 360.250. REPAIRED AREA IAW UPS EO DC8-5720-7767A.

Part: SKIN — CORRODED (WS 634 - 635)

INSPECTION TYPE:C1 LEFT WING L/E LOWER SKIN IS CORRODED BEYOND LIMITS XFS 634-635. REPAIRED IAW SRM. ADDENDUM DC8-5720-4087-B.

Part: SKIN — CRACKED (WS 597.500)

INSPECTION TYPE:C1, RT WING L/E UPPER SKIN IS CRACKED AT STA XFS597.500. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-7767-A.

Part: LONGERON — CORRODED (BS 1360)

INSPECTION TYPE:C1 STA 1360 LONGERON 35R LOWER SIDE OF FLANGE IS CORRODED BEYOND LIMITS. REPAIRED IAW 8110-3 APPROVED DH SK 703-788.

Part: SKIN — CRACKED (WS 335 - 338)

INSPECTION TYPE:C,1 RT WING L/E LOWER EXTERNAL SKIN IS CRACKED AT THE DRAIN HOLE STA XFS335.750 AND XFS338.750. REPAIRED AREA IAW DC8-5720-4087-B.

Part: RIB — CRACKED (WS 797.500)

INSPECTION TYPE:C1 RT WING L/E AT STA XFS797.500, THE L/E RIB IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CORRODED (WS 372)

INSPECTION TYPE:C1, INTERNAL DOUBLER CORRODED RIGHT WING L/E AT XFS 372.750. REMOVED, FABRICATED AND REPLACED INTERNAL DOUBLER IAW DWG 5641253, AND SRM 51-1-21, 51-1-20D.

Part: RIB — CRACKED (WS 791.250)

INSPECTION TYPE:C1, RT WING L/E AT STA XFS791.250, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: STIFFNER — CRACKED (WS 250)

INSPECTION TYPE:C1 RIGHT WING L/E VERTICLE STIFFENER (OTBD END OF SLOT) IS CRACKED AT XS250.089. REMOVED, FABRICATED, AND REPLACED STIFFENER IAW DWG 9753293, AND SRM 51-1-21, 51-1-20D.

Part: SKIN — CRACKED (WS 571)

INSPECTION TYPE:C1, RT WING L/E LOWER SKIN INTERNAL DOUBLER AT STA. XFS571.00 IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-20D.

Part: FRAME — CRACKED (BS 660)

INSPECTION TYPE:C1, STA 660 AT 21R TO 22R FRAME WAS CRACKED. REMOVED, FABRICATED AND INSTALLED FRAME IAW DWG 3646688 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 622.50)

INSPECTION TYPE:C1 RT WING L/E AT STA. XFS622.50, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (WS 427)

INSPECTION TYPE:C,1 LEFT WING LOWER SKIN AT STA XFS427.0 19 INCHES FWD OF THE SPAR IS CRACKED AT 3 FASTENERS. REPAIRED AREA IAW DC8-5720-4087.

Part: RIB — CRACKED (WS 6.225)

INSPECTION TYPE:C1 RT WING L/E AT STA XOLDI 6.225, THE UPPER L/E RIB IS CRACKED AT MID-SPAN. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 591.25)

INSPECTION TYPE:C1, LT WING L/E RIB AT STA XFS591.25 IS CRACKED AT THE UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 635)

INSPECTION TYPE:C1, RT/H WING L/E AT STA XFS635..00, THE LOWER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (WS 503.789)

INSPECTION TYPE:C1, RT WING L/E UPPER SKIN IS CRACKED AT FRONT SPAR, STA XS503.789. REPAIRED AREA IAW UPS EO DC8-5720-7767A.

Part: SKIN — CORRODED (WS 195)

INSPECTION TYPE:C1 RIGHT WING L/E UPPER SKIN CORRODED BEYOND LIMITS AT XFS 195. REPAIRED IAW 8110-3 APPROVED DH SK 703-163.

Part: SKIN — CRACKED (WS 485)

INSPECTION TYPE:C1, LT WING L/E LOWER SKIN AT STA XW485.5 AT THE L/E IS CRACKED AT 2 SCREW HOLES. REPAIRED AREA IAW DC8-5720-4087-B.

Part: FITTING — CRACKED (BS 70)

INSPECTION TYPE:C1 STA 70 LONGERON 33R END FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 4611067, AND SRM 51-1-20D.

Part: SKIN — CRACKED (BS 418)

INSPECTION TYPE:C1 STA 418 LONGERON 20L LEFT FWD TYPE 1 DOOR JAMB IS CRACKED AT AFT LOWER CORNER EXTERNAL SKIN. REPAIRED IAW 8110-3 APPROVED DH SK 703-201.

Part: FITTING — CRACKED (BS 70)

INSPECTION TYPE:C1 STA 70 LONGERON 32R END FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 4611067, AND SRM 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE)

INSPECTION TYPE:C1 AFT LT PASSENGER DOOR JAMB LOWER FWD CORNER HAS 2 SMALL CRACKS. REPAIRED IAW SRM. ADDENDEM DC8-5330-10151-B.

Part: FRAME — CRACKED (BS 55)

INSPECTION TYPE:C1 STA 55 FRAME CRACKED AT ROD ATTACH POINT AT LONGERON 24L. REPAIRED IAW SRM 53-2-0 FIG 2.

Part: FITTING — CRACKED (COCKPIT)

INSPECTION TYPE:C1 LOWER SLIDING WINDOW RAIL SUPPORT FITTING IS CRACKED AT FIRST OFFICERS SIDE. REPAIRED IAW 8110-3 DH SK 703-398.

Part: COWL — DAMAGED (NR 3 & 4 ENGINE)

INSPECTION TYPE:N/A, UPON LANDING NUMBER 3 AND 4 ENGINE COWLS CONTACTED RUNWAY. *S/D* REMOVED AND REPLACED NUMBER 3 AND 4 ENGINE AND DAMAGED FAN COWLS PER MM 71-10-02 AND TC 9071-1, 9071-2. PERFORMED ENGINE RUNS PER TC 9071-2 AND 9071- 3. REFER TO LOG PAGES 371266 TO LOG PAGES 371273, OPERATIONAL CHECKS.

Part: SKIN — CRACKED (RT WING)

1.5 INCH CRACK RIGHT WING LOWER SURFACE INB'D OF NR 3 PYLON. CRACK IS ON BOTH SIDES OF RIVET. REPAIRED AREA IAW SRM 57-2-1 FIG 35 AND SRM 57-2-1.

Part: CYLINDER — FAILED (LT AILERON)

INSPECTION TYPE:N/A, LOSS OF MAIN RESERVOIR HYDRAULIC FLUID. AILERON AND RUDDER MAN LIGHT ON, PRESSURE FLUCTUATED. RAN LOSS OF HYDRAULICS CHECKLIST, RECOVERED NORMAL GEAR, FLAPS, BRAKES, NW STEERING. FLT CONT NOTIFIED, DECLARED INFLIGHT EMERGENCY W/ATC. NORMAL LANDING. REMOVED AND REPLACED LEFT AILERON POWER CYLINDER IAW MM 27-11-06, NO LEAKS OR CHECKS NOTED.

Part: INTERCOSTAL — CORRODED (BS 1560)

INSPECTION TYPE:SVC, AFT ACCY COMPARTMENT, CORROSION AT INTERCOSTAL ATTACH ANGLE AROUND FASTENERS AND ANGLE, FS 1560 LONGERON 26L. REMOVED INTERCOSTAL(P/N 5615377-93) FAB AND INSTALLED NEW INTERCOSTAL IAW TIMCO REO 06698.

Part: SEAT TRACK — CORRODED (BS 1570)

INSPECTION TYPE:SVC, AFT ACCY COMPARTMENT, SEAT TRACK CORRODED BEYOND LIMITS AT FS L3L10. REMOVED SEAT TRACK FROM FS 1500-1700 L3L10 AND SPLICED IN NEW SEAT TRACK SECTION, INSTALLED SPLICES AND REINSTALLED FLOORBOARDS AND CARGO SYSTEM IAW DC8 SRM 53-2-3, 51-1-24, 51-1-8 & 51-3-0.

Part: SEAT TRACK — CORRODED (BS 1440)

INSPECTION TYPE-D/CK, SEAT TRACK F FUSELAGE STATION 1440 CORRODED. REMOVED SEAT TRACK SECTION FUSELAGE STATION 1430 TO 1450, CUT AND DRILLED NEW SECTION AND INSTALLED SECTION IAW DC8 SRM 51-1-8, 51-3-0, 53-1-2 AND EO DC8 5320 5167.

Part: FITTING — CRACKED (BS 300)

INSPECTION TYPE:D/CK, STA 300 L27 TO 28 L 'Z' FITTING CRACKED. REMVOED FITTING FABBED ANGLES IAW DC8 SRM 53 2 0. ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51 1 8. INSTALLED FITTING AND SPLICE ANGLES IAW DC8 SRM 51 1 20D AND 53 2 0.

Part: SEAT TRACK — CRACKED (BS 1758)

INSPECTION TYPE:D/CK FUSELAGE MAIN CABIN INTERIOR FLOOR BOARD SUPPORT CHANNEL HAVE CORROSION AND SEAT TRACK E AT STA 1758 BLO IS CRACKED. REMOVED CRACKED HAT CHANNEL. REMOVED CORROSION FROM LEFT HAND FLOOR BOARD OUT OF LIMITS IAW DC8 SRM 53 2 0, LOCATED AND DRILLED NEW SECTION OF HAT IAW DC8 SRM 51 1 247. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED SEAT TRACK 1752 TO 1760 IAW SRM 51 1 20D. PRIMED HAT SECTION IAW DC8 SRM 51 1 8. INSTALLED ON AC IAW DC8 SRM 51 13 0.

Part: FITTING — DAMAGED (LT WING)

INSPECTION TYPE-C, 505-E XRS 74.9. STRINGER 51 END FITTING HAS ELONGATED HOLE THROUGH FITTING'S WING SKIN. INSTALLED BUSHING IAW DC8-SRM 51-1-25 AND REO 04389. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED NEW FITTING IAW 51-1-20D, DC8 SRM 51-1-11 AND DC8 SRM 51-3-0 AND REO-04389.

Part: FITTING — CRACKED (BS 320)

INSPECTION TYPE:D/CK STA 320 AT LONG 35 L FITTING IS CRACKED. REMVOED EXISTING FITTING FABRICATED SPLICES IAW DC8 SRM 53 2 0. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED FITTING IAW DC8 SRM 5 1 1 20D.

Part: INTERCOSTAL — CORRODED (BS 1710-1730)

INSPECTION TYPE-D/CK, FLOORBEAM INTERCOSTAL AT STA 1710 TO 1730 RBL 12 HAS CORROSION. FABRICATED SUPPORT IAW DAC DWG 5755032, ALODINED AND PRIMED NEW SUPPORT. INSTALLED NEW SUPPORT IAW DC8 SRM 51-1-21 AND 51-1-20D AND 51-3-0.

Part: WEB — CRACKED (RT AILERON)

INSPECTION TYPE-C, RT I/B AILERON, O/B END WEB CRACKED (CLOSURE RIB). REMOVED CLOSURE RIB, FABBED REPAIR DOUBLER FOR IT AND INSTALLED IAW REO 0429A REVA, DC8-SRM 51-1-8 AND DC8 SRM 51-1-21.

Part: FITTING — CRACKED (RT WING)

INSPECTION TYPE-C, FWD OF ACCESS 560-B, 30 FT INBD OF XW408 CRACKED IN STRINGER END FITTING. REMOVED CRACKED FITTING, DRILLED NEW FITTING IAW DC8 SRM 51-3-2 AND INSTALLED IAW DC8 SRM 51-1-20D.

Part: LONGERON — DAMGED (BS 340)

INSPECTION TYPE:D/CK STA 340 L28L LONGERON IS DAMAGED AT Z FITTING. BLENDED OUT DAMAGED IAW UPS DC8 SRM 53 2 0. FABBED REPAIR STRAP IAW REO 04279 AND DC8 SRM 51 1 24. ALODINED AND PRIMED REPAIR AREA AND STRAP IAW DC8 SRM 51 1 8. INSTALLED REPAIR IAW REO 04279 AND DC8 SRM 51 1 20D.

Part: LONGERON — CORRODED (BS 190-390)

INSPECTION TYPE:D/CK, L33 LEFT STA 190 TO 390 REQUIRED REPLACEMENT. REMOVED LONGERON STA 190-390, DRILLED NEW LONGERON HALVES IAW DC8 SR M 51 1 24. INSTALLED LONGERON WITH HI-LOKS AND RIVET6S IAW DC8 SRM 5 1 1 20D AND 51 1 21.

Part: EXTRUSION — CORRODED (BS 1740)

INSPECTION TYPE:D/CK SURFACE CORROSION ON FLOOR STRUCTURE AT STA 1740. REMOVED CORROSION AND DAMAGED EXTRUSION FABBED NEW EXTRUSION IAW DC8 SRM 53 7 1 AND DWGT 5755032. INSTALLED EXTRUSION IAW DC8 SRM 51 1 20D. ALODINED AND PRIMED IAW DC8 SRM 51 1 8.

Part: RIB — CRACKED (LT WING)

INSPECTION TYPE:D/CK LEFT WING MIDDLE LEADING EDGE RIB CRACKED AT FUEL DOOR. RECEIVED REO FABRICATED PARTS HEAT TREATED IAW REO 04277. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED IAW REO 04277 AND DC8 SRM 51 1 20D.

Part: FLOORBEAM — CORROSION (BS 60-70)

INSPECTION TYPE:D/CK CORROSION BETWEEN LAV SUB FLOOR, FLOORBEAMS AND SEAT TRACK, LAV AREA STA 60-70. REMOVED CORROSION FOUND CRACK FLOORBEAM STA 55 RBL 33. REMOVED DAMAGED AREA FABBED REPAIR FILLER AND ANGLE AND INSTALLED PER REO 4350. ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51 1 8.

Part: PULLEY BRACKET — CORRODED (RT MLG WW)

INSPECTION TYPE:D/CK RIGHT MAIN WHEEL WELL FLAP CONTROL PULLEYS WORN AND HARDWARE EVIDENCE OF CORROSION JUST ABOVE GEAR DOOR UPLOCK OTBD. REMOVED AND REPLACED PULLEY BRACKET ON RIGHT SIDE IAW DC8 SRM 51 3 0. REMOVED AND REPLACED PULLEY HARDWARE IAW DC8 MM 20 17 00.

Part: FRAME — CORRODED (BS 150)

INSPECTION TYPE-D/CK, MAIN CABIN STA 150 AT RIGHT HAND CUSP, INSIDE R-1 DOOR, FRAME BOTTOM FWD CORNER CORRODED. REMOVED ANGLE, DRILLED UP REPAIR ANGLE IAW3 DC8 SRM 53-30 AND INSTALLED IAW DC8 SRM 51-1-20.

Part: SEAT TRACK — CORRODED (BS 844-850)

INSPECTION TYPE:D/CK CABIN SEAT TRACK H CORRODED AT STA 844 TO 850. REMOVED CORROSION IAW DC8 SRM 51 1 8 NOT WITHIN LIMITS. REMOVED DAMAGED SECTION STA 844 TO 850. FABRICATED NEW SECTION OF TRACK AND SPLICES IAW DC8 SRM 53 2 3. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED IAW DC8 SRM 51 1 20D AND 51 3 0 AND 53 2 3.

Part: BRACKET — CRACKED (EMER EXIT DOOR)

INSPECTION TYPE-C, LT AFT OVERWING EXIT DOOR HAS 2 CRACK IN WINDOW FRAME TEE AT FWD LWR CORNER. REMOVED CRACKED BRACKET AND INSTALLED NEW ONE IAW DC8 SRM 51-1-2- AND 51-1-20D.

Part: SEAT TRACK — CORRODED (CARGO COMPT)

INSPECTION TYPE-C, UPPER CARGO SEAT TRACK (LOWER SIDE) CORRODED AT STA 1400, RBL 60. REMOVED SEAT TRACK FS 1370 TO 1430 IAW SRM 53-4-1. DRILLED UP NEW TRACK AND SPLICES IAW DC8 SRM 53-4-1 AND 53-2-3. ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51-1-8. INSTALLED NEW TRACK IAW 51-3-0 AND 51-1-17.

Part: SEAT TRACK — GOUGED (BS 270)

INSPECTION TYPE:D/CK, CABIN SEAT TRACK I IS GOUGED WORN AND CORRODED STA 270. REMOVED SEAT TRACK PLUG PRIMED SEAT TRACK PLUG IAW DC8 SRM 51 1 8. INSTALLED NEW SEAT TRACK PLUG IAW DC8 SRM 53 2 3.

Part: SPLICE — CORRODED (BS 1320-1340)

INSPECTION TYPE-D/CK, UPPER CARGO SEAT TRACK REPAIR SPLICE CORRODED, MISSING STRAP OPEN HOLES AND 1 STRAP STA 1320 TO 1340 LBL 52. FABBED NEW STRAP, ALODINED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-3 AND 51-1-8.

Part: SEAT TRACK — CORORDED (BS 516-530)

INSPECTION TYPE:D/CK, CABIN SEAT TRACK CORRODED STA 516-530. REMOVED SEAT TRACK STA 410 590. FABBED NEW SPLICES, DRILLED NEW TRACK IAW DC8 SRM 53 3 2 AND 53 21 0. INSTALLED IAW DC8 SRM 53 2 3 AND 51 1 8 AND 51 3 0.

Part: SEAT TRACK — CORRODED (BS 1240)

INSPECTION TYPE:D/CK SEAT TRACK B-C CORRODED AT STA 1240. REMOVED DAMAGED TRACK STA 1190 TO 1270. FABRICATED AND INSTALLED NEW TRACK IAW DC8 SRM 51 3 0 AND 51 1 8 AND 53 2 3.

Part: FITTING — CORRODED (BS 1460)

INSPECTION TYPE:D/CK, ALC COMPARTMENT STA 1460 ABOVE LONGERON 34 R FITTING CORRODED INSIDE TORQUE BOX. REMOVED FITTING IAW DC8 SRM 51 1 21. DRILLED UP NEW FITTING IAW DC8 SRM 51 1 2. INSTALLED NEW FITTING IAW DC8 SRM 51 3 0.

Part: FLOORBEAM — CORRODED (BS 1240)

INSPECTION TYPE:D/CK, AFT PIT BOTTOM OF CABIN FLOOR CORRODED 4 PLACES, BTL 12 L, 34R, 12R, AND 34R, STA 1240. CUT OUT DAMAGED IAW DC8 SRM 53 2 3 FIG 10, FABBED DOUBLERS FILLER, REPAIRED ANGLE AND INSTALLED IAW DC8 SRM 53 2 3 FIG 10, DC8 SRM 51 1 21, 51 1 20D. ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51 1 8.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:D/CK MAIN CABIN STA 680 AT L6L END FITTING. REMOVED CRACKED FITTING DRILLED AND INSTALLED NEW ONE IAW DC8 SRM 5 1 1 24 AND 51 1 20D.

Part: LONGERON — CORRODED (BS 640-660)

INSPECTION TYPE:D/CK, CORROISON ON LONGERON 31 RIGHT BETWEEN STA 640 AND 660. REMOVED CORROSION FABBED REPAIR STRAP PER REO 04338. ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51 1 8. INSTALLED STRAP IAW DC8 SRM 5 1 1 20D AND 51 1 16.

Part: ANGLE — CORRODED (BS 70)

INSPECTION TYPE:D/CK CORRODED HARDWARE AT STA 70 IN FLOORBEAM AFT OF LAV AREA. REMOVED CORRODED ANGLE AND REPLACED IAW DC8 SRM 51 1 20D AND 51 1 11.

Part: WEB — BULGED (BS 1324)

INSPECTION TYPE:D/CK AFT LOWER CARGO LEFT HAND TUNNEL HORIZONTAL WEB HAS REPAIR DOUBLER BULGED AT STA 1324 LBL 54. REMOVED REPAIR DOUBLER IAW SRM 51 1 21. FABBED NEW REPAIR DOUBLER IAW DC8 SRM 53 2 0. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED NEW REPAIR DOUBLER IAW DC8 SRM 51 1 21.

Part: SEAT TRACK — CORRODED (BS 1010-1030)

INSPECTION TYPE-D/CK, MAIN CARGO SEAT TRACK ALONG LEFT SIDE, STA 1010 TO 1030 CRACKED AND CORRODED. REMOVED TRACK STA 1010 TO 1090, FABBED AND INSTALLED NEW STICK IAW DC8 SRM 53-2-3.

Part: FITTING — CRACKED (CARGO DOOR)

INSPECTION TYPE-C, PIT DOOR CLOSE OUT FITTING CRACKED AT FS 1420 BL 0. REMOVED DOOR BARRIER CLOSE OUT. FABRICATED DOUBLER IAW DC8 SRM 53-2- 0. ALODINED AND PRIMED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-8, 51-1-20. FABRICATED FITTING IAW 5616673. ALODINED/PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-20. INSTALLED CLOSEOUT IAW DC8 SRM 51-3-0.

Part: SEAT TRACK — CORRODED (BS 1000-1140)

INSPECTION TYPE:D/CK UPPER CARGO SEAT TRACK RBL 60 CORRODED IN SWIVEL PLACES STA 1000 TO STA 1140. REMOVED CORRODED SEAT TRACK IAW DC8 SRM 53 2 3. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED NEW TRACK AND SPLICES IAW DC8 SRM 5 3 2 3 AND 51 3 0.

Part: SEAT TRACK — GOUGED (BS 575)

INSPECTION TYPE-C, CABIN SEAT TRACK H GOUGED AND CRACKED AT STA 575. REMOVED DAMAGE OUT IAW DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR PLUG AT STA 575 SEAT TRACK H IAW DC8- SRM 51-30.

Part: FRAME — CRACKED (BS 220)

INSPECTION TYPE-D/CK, FRAME CRACKED FUSELAGE STATION 220 L36 FWD FACE. REMOVED BOTTOM CRACKED PART OF FRAME, FABBED DOUBLER, FILLER AND STRAP AND INSTALLED REPAIR PIECES IAW REO 04355 AND DC8 SRM 51-1-21 AND 51-1-8.

Part: SEAT TRACK — CORRODED (BS 1130-1140)

INSPECTION TYPE-D/CK, AFT 6 PIT FLOOR TRACK STA 1130 TO 1140 AT BL 45L CORRODED. REMOVED DAMAGED SECTION OF SEAT TRACK AND SPLICED NEW SECTION IN IAW DC8 SRM 53-2-3 AND 51-1-8.

Part: FITTING — CORRODED (BS 300)

INSPECTION TYPE:D/CK, LOWER FWD CARGO COMPARTMENT STA 300 BATH TUB FITTING CORRODED LONGERON 36 TO LONGERON 35 RIGHT. REMOVED FITTING REPLACED WITH NEW FITTING IAW DC8 SRM 51 1 20D.

Part: FITTING — CORRODED (BS 320)

INSPECTION TYPE:D CHECK, LOWER FWD CARGO COMPT STATION 320.000 LONG 33 LEFT TO LONG 32 LEFT, CORRODED BATHTUB FITTING. REMOVED AND FITTING IAW DC8 SRM 51-1-20D. RECEIVED NEW PART NR 3755822 05N LOCATED AND DRILLED NEW PART IAW DC8 SRM 51-3-2. REMOVED CORROSION AT STRUT AND HOLES IAW DC8 SRM 51-1-8. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW PART IAW DC8 SRM 51-1-50D.

Part: WEB — CRACKED (CARGO COMPT)

INSPECTION TYPE:D/CK FWD LWR CARGO COMPT RIGHT HAND TUNNEL AT CUSP WEB ABOVE FWD TORQUE BOX IS CRACKED. FABBED DOUBLER IAW DC8 SRM 53 2 0. ALODINED AND PRIMED IAW DC8 SRM 5 1 1 8. INSTALLED PART IAW DC8 SRM 51 3 0 AND 51 1 21 AND 51 1 21A.

Part: FITTING — CORRODED (BS 280)

INSPECTION TYPE:D/CK BATH TUB CORRODED FS 280 L 28 TO 29R. REMVOED FITTING FABBED SPLICES FOR NEW FITTING IAW DC8 SRM 53 2 0 FIG 2D. INSTALLED NEW FITTING WITH SPLICES IAW DC8 SRM 53 2 0 FIG 2 D AND 51 1 20D.

Part: FITTING — CORRODED (BS 300)

INSPECTION TYPE-C, LWR FWD CARGO COMPT STN 300.00, LONG 33L AND 32L CORRODED BATH TUB FITTING. REMOVED OLD FITTING IAW DC8 SRM 51-1-20D. RECEIVED NEW PART 3755822- 505. LOCATED AND DRILLED NEW PART IAW DC8 SRM 51-3-2. REMOVED CORROSION, ALODINED AND PRIMED IAW DC8 SRMK 51-1-8. INSTALLED IAW SRM 51-1- 20D.

Part: LONGERON — CORRODED (BS 1610-1620)

INSPECTION TYPE-D/CK, AFT ACCESORY SECTION LONGERON CRACKED AND CORRODED STA 1610 TO 1620 AND LONG 24L. REMOVED SECTION OF LONGERON AND REPLACED WITH NEW IAW DC8 SRM 53-2-2 AND 51-1-20D, INSTALLED SKIN DOUBLER ON FUSELAGE IAW DC8 SRM 53-2-1 FIG 7.

Part: FITTING — CORRODED (BS 340)

INSPECTION TYPE:D/CK, FWD LWR CARGO COMPT ZX SLIDE AREA BATH TUB FITTING CORRODED AT STA 340L AT L29L. REMOVED CORROSION FROM FITTING IAW DC8 SRM 53 2 0. REMOVED CORRODED FITTING MATERIAL ID REPAIR ANGLE 7075 T6 .125 PO 249743 IAW DC8 SRM 53 2 0. RECEIVED FITTING FROM CUSTOMER TAG 00233648. FABRICATED REPAIR ANGLE IAW DC8 SRM 53 2 0. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED FITTING IAW DC8 SRM 51 1 20D.

Part: FITTING — CORRODED (BS 300)

INSPECTION TYPE:D/CK, LWR FWD CARGO COMPT STA 300.000 LONGERON 29 LEFT TO 28L. CORRODED BATH TUB FITTING. REMOVED CORRODED FITTING, FABRICATED REPAIR ANGLES AND CUT NEW FITTING IAW DC8 SRM 53 2 0. DRILLED NEW FITTING AND REPAIR ANGLES IAW DC8 SRM 53 2 0. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED REPAIR ANGLES AND NEW FITTING IAW DC8 SRM 53 2 0 AND 51 1 20D.

Part: FITTING — CORRODED (BS 300)

INSPECTION TYPE:D/CK, FWD LWR CARGO COMPT X SLIDE DOOR AREA BATH TUB FITTING CORRODED STA 300 L AT L32 L. FABRICATED REPAIR ANGLES IAW DC8 SRM 53 2 0. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED NEW FITTING IAW DC8 SRM 51 1 20D.

Part: LONGERON — CRACKED (BS 1630-1640)

INSPECTION TYPE:D/CK AFT ACCESSORY SECTION HAS CRACKED LONGERON STA 1630-1640 AND LONGERON 24 LEFT. REMOVED SECTION OF LONGERON AND REPLACED WITH NEW IAW DC8 SRM 53 2 2 AND 51 1 20D. INSTALLED SKIN DOUBLER AND FUSELAGE IAW DC8 SRM 53 2 1 FIG 7.

Part: BRACKET — CORRODED (BS 1720)

INSPECTION TYPE:D CHECK, VERTICAL STAB FRONT SPAR ATTACH ANGLE IS CORRODED STA 1720 AT LONGERON 13 RIGHT. REMOVED CORROSION FROM VERTICAL STAB FRONT SPAR ATTACH ANGLE AT FS 1720 LONGERON 13 RIGHT IAW DC8 SRM 51-1-8 ALODINED AND PRIMED AREA IAW DC8 SRM 51-1-8

Part: LONGERON — CRACKED (BS 1260-1280)

INSPECTION TYPE:D/CK AFT 6 PIT STA 1260-1280 LONGERON 34 LEFT CRACKED. REMOVED CRACKED LONGERON 34 LEFT STA 1260-1350 IAW DC8 SRM 51 1 20D. DRILLED NEW LONGERON IAW DC8 SRM 51 1 20D. INSTALLED NEW LONGERON I 9AW DC8 SRM 51 1 20D NAD 51 3 0.

Part: SPAR — CORRODED (VERT STAB)

INSPECTION TYPE:D, CK VERTICAL STABILIZER FRONT SPAR CORRODED STA 1730 AT LONGERON 11 RIGHT. REMOVED CORROSION FROM FRONT SPAR OF VERTICAL STABILIZER IAW DC8 SRM 51-1-8 ALODINED AND PRIMED AREA IAW DC8 SRM 51-1-8.

Part: FITTING — CRACKED (BS 1695)

INSPECTION TYPE:D CHECK, STA 1695 BATH TUB FITTING CRACKED AT LONGERON 28 RIGHT. REMOVED BATH TUB FITTING LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-21 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D. TORQUES IAW DC8 SRM 51-3-1 .

Part: BULKHEAD BEAM — CORRODED (BS 1756)

INSPECTION TYPE:D CHECK, FORWARD SIDE OF AFT PRESSURE BULKHEAD VERTICAL BEAM FWD CAP IS CORRODED ON RIGHT SIDE 8 FROM TOP. REMOVED CORROSION ALODINED AND PRIMED IAW DC8 SRM 51-1-8.

Part: LONGERON — CRACKED (BS 80)

INSPECTION TYPE:D/CK, FWD LOWER CARGO COMPT L37 R CRACKED AT END AT STA 80R. REMOVED CRACKED LONGEORN FABBED FITTING IAW DWG 3757600. ALODINED AND PRIMED NEW FITTING INSTALLED NEW FITTING IAW DC8 SRM 51 1 20D.

Part: FITTING — CRACKED (BS 1695)

INSPECTION TYPE:D CHECK, STA 1695 BATH TUB FITTING CRACKED AT LONGERON 30 LEFT. REMOVED BATH TUB FITTING LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-21. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D. TORQUED BOLT IAW DC8 SRM 51-3-1.

Part: FITTING — CRACKED (BS 1685)

INSPECTION TYPE:D CHECK, STA 1685 BATH TUB FITTING CRACKED AT LONGERON 34 LEFT. REMOVED BATH TUB FITTING LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-21 A ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D. TORQUED BOLT IAW DC8 SRM 51-3-1.

Part: FITTING — CRACKED (BS 1695)

INSPECTION TYPE:D CHECK, STA 1695 BATH TUB FITTING CRACKED AT LONGERON 26 LEFT. REMOVED BATH TUB FITTING LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-10-21 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D. TORQUED BOLT IAW DC8 SRM 51-3-1.

Part: SPAR — CORRODED (VERT STAB)

INSPECTION TYPE:D CHECK VERTICAL STABILIZER 5 LEFT FRONT SPAR CORRODED STA 1700-1740 FROM LONGERON 9 LEFT TO 18 LEFT ( AFT CABIN). REMOVED CORROSION IAW 51-1-8 TIMCO RFTS ENGINEERING DISPOSITION ALODINED AND PRIMED IAW DC8 SRM 51-1-8.

Part: FITTING — CRACKED (BS 1695)

INSPECTION TYPE:D CHECK, STA 1695 BATH TUB FITTING CRACKED AT LONGERON 30 RIGHT. REMVOED BATH TUB FITTING LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-21 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D. TORQUED IAW DC8 SRM 51-3-1 .

Part: FITTING — CRACKED (BS 1685)

INSPECTION TYPE-D/CK, STA 1685 BATHTUB FITTING CRACKED AT LONGERON 26L. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-4, 51-1-20D. INSTALLED IAW DC8 SRM 51-3-0.

Part: FITTING — CORRODED (BS 1695)

INSPECTION TYPE:D CHECK, STA 1695 BATH TUB FITTING CORRODED AT LONGERON 26 RIGHT. REMOVED BATH TUB FITTING LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-21 ALODINED AND PRIMED IAW DC8 SRM 51-1-8 INSTALLED NEW FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D. TORQUED BOLTS IAW DC8 SRM 51-3-1 .

Part: FRAME — CORRODED (FUSELAGE)

INSPECTION TYPE:D/CK, FLC STA TO FRAME CORRODED BETWEEN LONGERON 27 RIGHT AND LONGERON 26 RIGHT. FABBED DOUBLER IAW DC8 SRM 53 2 58 FIG 8C-2 AND REO 04362, ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51 1 8. INSTALLED DOUBLER IAW DC8 SRM 51 1 11 AND 51 1 20D AND 51 1 21.

Part: SPAR — CORRODED (VERT STAB)

INSPECTION TYPE:D CHECK, VERTICAL STABILIZER FRONT SPAR LOWER CAP CORRODED STA 1750 FROM X 10 TO X 30. REMOVED CORROSION FROM VERTICAL STAB FRONT SPAR LOWER CAP AT FS 1750 FROM X30 TO X10 IAW DC8 SRM 51-1-8. ALODINED AND PRIMED AREA IAW DC 8 SRM 51-1-8

Part: DOUBLER — DAMAGED (CARGO DOOR)

INSPECTION TYPE-C, LT SIDE FUSELAGE, FWD LT CORNER OF MAIN CARGO DOOR, REPAIR DOUBLER DAMAGED. BLENDED OUT DAMAGED EDGE OF LOWER SKIN IAW SRM 53-2-0 FIG 1F SHT 3 PG 2P. REPAIRED PER REO04323 REV B BY INSTALLING DOUBLER.

Part: LONGERON — CRACKED (BS 220)

INSPECTION TYPE:D/CK, FWD LOWER CARGO COMPARTMENT LONGERON 36 CRACKED FROM FWD TORQUE BOX TO STA 220. REMOVED LONGERONS, REMOVED CORROSION FROM HANGER IAW DC8 SRM 51 1 8. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. DRILLED NEW LONGERONS FORF IT IAW DC8 SRM 51 1 24. INSTALLED LONGERONS WITH HI-LOKS IAW DC8 SRM 51 1 20D.

Part: ANGLE — CRACKED (FWD FUSELAGE)

INSPECTION TYPE-C, LT RAIN REMOVAL PLENUM HAS 1 CRACK ON SUPPORT ANGLE (I/B SIDE OF CHAMBER). FABBED, INSTALLED REPAIR ANGLE IAW REO04273.

Part: SKIN — TORN (RT WING)

INSPECTION TYPE-D/CK, RIGHT WING TOP EXTERIOR SURFACE REAR SPAR AT NR 5 SPOILER SKIN IS TORN. CUT OUT DAMAGED SKIN AREA, FABRICATED FILLER AND DOUBLER IAW REO DC8 5720 7767 APPENDIX A AND INSTALLED IAW SRM 51-1-21.

Part: DOUBLER — CRACKED (CARGO DOOR)

INSPECTION TYPE:N/A, PIT DOOR NR 1 HAS CRACK AT BOTTOM, DAMAGE TO PREVIOUS REPAIR. REMOVED DAMAGED DOUBLER, REPAIRED SKIN PER SRM 52-2-2, REPLACED DOUBLER OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, SHIP EMERGENCY BATTERY INOP. REMOVED AND REPLACED SHIPS EMERGENCY BATTERY IAW M/M 34-28-00.

Part: ACTUATOR — FAILED (RT TE FLAPS)

INSPECTION TYPE-N/A, AFTER LANDING ROLLOUT WHEN RETRACTING FLAPS, RES LOW LIGHT CAME ON FLAPS WOULD NOT RETRACT, HYD QTY FALLING RAPIDLY, SYS PRS WENT TO 0 PSI. FOUND RT W/FLAP ACT CYL BROKE AT COMPENSATING LINK, AND UP-HYD PRS LINE CRACKED AT FITTING. REPLACED SAME CYL, PER 27-51-09. SERVICED LOCK-OUT PER 27-51-01, OPS CKD AND LEAK CKD NORMAL PER 27-51-09.

Part: FITTING — CRACKED (BS 20)

INSPECTION TYPE-C, FS 20 LONGERON END FITTING CRACKED, LONGERON 20R. REPLACED FITTING PER SRM 51-1-20D.

Part: SKIN — CRACKED (WS 528)

INSPECTION TYPE-C, LT WING LEADING EDGE UPPER SURFACE STA XFS 528 HAS A 2 INCH CRACK FROM AFT EDGE OF RIVET HOLE. REPAIRED PER SRM ADDENDUM DC8-5720-7767.

Part: FITTING — CRACKED (BS 1150)

INSPECTION TYP-C, LONGERON 31R FS 1150 END FITTING CRACKED. REPLACED FITTING PER SRM 51-1-20D.

Part: VANE — DELAMINATED (NR 2 TE FLAP)

INSPECTION TYPE-C, LEFT FLAP NR 3 VANE DELAMINATED. REPLACED VANE PER MM 27-51-14.

Part: FITTING — CRACKED (BS 1150-1230)

INSPECTION TYPE-C, 4 BANANA FITTINGS CRACKED AT C-BAG BIN DOOR JAMB FS 1150 TO 1230 LONGERONS 31R TO 33R. REPLACED FITTINGS PER SRM 51-1-20D.

Part: VANE — DELAMINATED (NR 2 TE FLAP)

INSPECTION TYPE-C, LT WING NR 2 FLAP VANE DELAMINATED. REPLACED VANE PER MM 27-51-14.

Part: DOUBLER — CORROSION (BS 8-70)

INSPECTION TYPE-C, FINGER DOUBLER AT FS 8 TO 70, LONGERON 31R, HAS HEAVY CORROSION. REPLACED DOUBLER PER SRM 51-1-21.

Part: DOUBLER — CRACKED (BS 210)

INSPECTION TYPE-C, LONGERON 31L FINGER DOUBLER CRACKED AT FASTENER HOLE, FS 210. REPLACED DOUBLER SECTION PER SRM 53-2-0.

Part: T-FITTING — CORROSION (BS 1160-1240)

INSPECTION TYPE-C, 3 T-FITTINGS HEAVY CORROSION AT C-DOOR JAMB LONGERON 33R FS 1160 TO 1240, NR 2, NR 5 AND NR 3 FITTINGS. REPLACED FITTINGS PER SRM 53-2-0.

Part: TRACK — CORROSION (BS 40)

INSPECTION TYPE-C, HEAVY CORROSION ON TRACK NR 1 FWD END OF POSITION NR 2. REPAIRED TRACK PER SRM 53-2-3.

Part: TRACK — CORROSION (BS 340)

INSPECTION TYPE-C, HEAVY CORROSION ON TRACK NR 1 FWD END OF POSITION 1. REPAIRED TRACK PER SRM 53-2-3.

Part: DNLOCK SWITCH — FAILED (NLG)

CREW REPORTED, NOSE LANDING GEAR DID NOT GIVE A GROUND INDICATION. COMPLETED CHECKLIST DID FLYBY AND DECLARED EMERGENCY. LANDED AFTER MAINTENANCE AND TOWER VISUALLY CHECKED GEAR DOWN.

Part: EVAC SLIDE — UNSECURED (EMER EXIT SLIDE)

WHILE ON GROUND, MAINTENANCE FOUND ENTRY DOOR EVAC SIDE GIRTH BAR FAILED TO LATCH. MAINTENANCE RE-PACKED EVAC SLIDE.

Part: EEL — INOPERATIVE (MAIN DECK)

WHILE ON GROUND, MAINTENANCE FOUND FWD CREW ENTRY EMER LT AND EMER LT FWD OF CREW LADDER (MAIN DECK CEILING) INOP. MAINTENANCE INSTALLED LIGHT AND BATTERY PACK. OPS CK OK.

Part: SLIDE — UNSECURED (EMER EXIT DOOR)

WHILE ON GROUND, MAINTENANCE FOUND ENTRY DOOR EVACUATION SLIDE GIRTH BAR FAILED TO LATCH. REPACKED EVACUATION SLIDE.

Part: FAN — FAILED (COCKPIT)

PILOT REPORTED, ELECTRICAL SMOKE SMELL IN COCKPIT ON APPROACH TO SDF. TURNING OFF RECIRC FAN CLEARED SMELL. T/S AND FOUND RECIRC FAN MOTOR HAD BURNED UP AND WOULD NOT RESET. DEFERRED RECIRC FAN ORDER MEL 21-16.

Part: HYD PUMP — FAILED (NR 2 HYD SYST)

DURING CRUISE AT FL 350, HYD PRESSURE AND FLUID DECREASED, RAN ABNORMAL CHECKLIST. FLUID STOPPED AT AUX LEVEL, LANDED DFW, EMERGENCY DECLARED. REMOVED AND REPLACED RUDDER PUMP, NR 2 ENG PUMP, CASE DRAIN AND SYSTEM FILTERS. SERVICED HYD SYS AND CHANGED CASE DRAIN FILTERS AGAIN. OPENED DEFERRAL TO REPLACE CASE DRAIN AND SYS FILTERS IN 20 HOURS PER M/M 27-24-02.

Part: DOOR LIGHT — ILLUMINATED (LANDING GEAR)

DURING CLIMB OUT TO BOS FROM SDF, DOORS NOT LATCHED LIGHT CAME ON DURING GEAR RETRACTION. CREW RAN APPROPRIATE CHECKLIST, CYCLED GEAR TWICE, LIGHT WENT OUT. MAINTENANCE NOTED COMMENT.

Part: UPLATCH MECH — OUT OF ADJUST (LT/RT MLG)

PILOT REPORTED THAT AFTER TAKE OFF GEAR NOT LATCHED LIGHT ILLUMINATED AFTER GEAR RETRACTION. CYCLED GEAR AND LIGHT EXTINGUISHED. ADJUSTED UPLATCH CLEARANCE PER MM 32-31-04, TEST GOOD.

Part: UPLATCH MECH — LACK OF LUBE (MLG DOOR)

PILOT REPORTED, AT 250 KNOTS ON CLIMBOUT, DOORS NOT LATCHED LIGHT ILLUMINATED. COMPLIED WITH AOM CHECKLIST. NO ALTERNATE DOOR WARNING ISOLATE LIGHTS WERE ILLUMINATED. AFTER RECYCLING GEAR, DOOR NOT LATCHED LIGHTS REMAINED ON. HOWEVER LIGHT EXTINGUISHED WHEN ANOTHER UPLATCH CHECK WAS PERFORMED. LIGHT REMAINED OUT UP TO EN ROUTE SPEEDS. CLEANED AND LUBRICATED MAIN GEAR UPLATCH MECHANISMS. OPS CK, SYSTEM PER 32-31-04. NO DEFECTS NOTED AT THIS TIME, OK FOR SERVICE.

Part: SWITCH — INTERMITTENT (LT MLG DOOR)

PILOT REPORTED THAT AT 230 KNOTS ON CLIMBOUT, GOT A FLICKERING THEN STEADY DOOR NOT LATCHED LIGHT. COMPLIED WITH QRH CHECKLIST. LIGHT WENT OUT AFTER GEAR WAS CYCLED. FOUND LT UPLATCH SWITCH INTERMITTENT. REPLACED DOOR SWITCH PER MM 32-31-04.

Part: RECIRC FAN — FAILED (FLIGHT DECK)

(SUPPLEMENTAL MRR) PILOT REPORTED BURNING ELECTRICAL SMELL IN FLIGHT DECK. FLIGHT CREW DONNED OXYGEN MASK AND PERFORMED PACK SMOKE CHECK LIST. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MECHANIC INFORMED FLIGHT CREW THAT THE RECIRC FAN MOTOR WAS BURNING/SMOKING. REPLACED RECIRC FAN PER MM 21-21-0. OPS CK GOOD.

Part: BELTFRAME — CORRODED (FS 1060)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME AT FS 1060, LONGERON 29-30L. FABRICATED AND INSTALLED REPAIR PER SRM 51-1-20D, 51-1-8.

Part: FITTINGS — CORRODED (FS 1540, 1560)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME END FITTINGS AT FS 1540 AND 1560, LONGERON 21R. REPLACED FITTINGS PER SRM 51-1-20D.

Part: FITTING — CORRODED (FS 1260-1280)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION AND CRACKED SPLICE FITTING AT FS 1260-1280, LONGERON 36. REPLACED FITTING PER SRM 51-3-0, 51-1-20D.

Part: FITTING — CORRODED (FS 1580)

WHILE IN 'C' CHECK, MAINTENANCE FOUND FLOOR SUPPORT FITTING CORRODED AT FS 1580, LONGERON 21L. REPLACED FITTING PER SRM 51-1-20D.

Part: SKIN — CORRODED (RT WING XFS 416)

WHILE IN 'C' CHECK, MAINTENANCE FOUND RT WING LEADING EDGE UPPER SURFACE HAS CORROSION BULGE AT STA XFS 416. REPAIRED SKIN PER SRM 57-2-0.

Part: SKIN — CORRODED (FS 621)

WHILE IN 'C' CHECK, MAINTENANCE FOUND HEAVY CORROSION ON INNER SKIN AND DOUBLER AT FS 621, LONGERON 34L. REPAIRED PER UPS EO DC8-5330-6792A.

Part: FITTING — CORRODED (FS 350)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON B/T FITTING AT FS 350, LONGERON 28L. REPLACED FITTING PER SRM 51-1-20D.

Part: LONGERON — CORRODED (FS 60-80)

WHILE IN 'C' CHECK MAINTENANCE FOUND CORROSION ON LONGERON 21R, FS 60-80. REPAIRED LONGERON PER SRM 53-2-5.

Part: WEB — CORRODED (FS 140)

WHILE IN 'C' CHECK, MAINTENANCE FOUND WEB ON TOP OF FLOOR BEAM CORRODED AT FS 140, RBL 65. REPAIRED PER SRM 53-2-0.

Part: FLOOR BEAM — CORRODED (FS 140)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM AT FS 140, RBL 65. REPAIRED PER UPS EO DC8-5310-6794A.

Part: SKIN — CRACKED (FWD X-SLIDE DOOR)

WHILE IN 'C' CHECK, MAINTENANCE FOUND A CRACK ON FWD CROSS SLIDE DOOR SKIN (OUTER), FS 310, LONGERON 25R. INSTALLED REPAIR PER SRM 52-2-3.

Part: SEAT TRACK — CORRODED (FS 55-280)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON NR 9 SEAT TRACK AT FS 55-280. REPLACED SEAT TRACK PER SRM 53-2-3.

Part: SPLICE SUPPORT — CORRODED (FS 1640-1655)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION AT SEAT TRACK SPLICE SUPPORT, NR 8 TRACK, FS 1640-1655, RBL 36. REPLACED SPLICE SUPPORT PER SRM 53-2-3 AND MM 53-40-02.

Part: DOUBLER — CRACKED (AFT HEAT EX DOOR)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON DOUBLER LT AFT HEAT EXCHANGER DOOR CUT OUT. INSTALLED REPAIR PER UPS EO DC8-5330-4732D.

Part: FLOOR BEAM — CORRODED (FS 1640)

WHILE IN C CHECK, MAINTENANCE FOUND CORROSION AT FLOOR BEAM AT FS 1640, RBL 30-40. REPAIRED PER UPS EO DC8-5310-6793A.

Part: LONGERON — CRACKED (BS 1270)

WHILE IN "C" CHECK, MAINTENANCE FOUND LONGERON 36 HAS 1.8 INCH CRACK ON AFT END AT STA 1270. MAINTENANCE REPAIRED IAW UPS EO DC8-5310-6795-A.

Part: FITTING — CRACKED (BS 660)

WHILE IN "C" CHECK, MAINTENANCE FOUND STA 660 BELTFRAME DOOR FITTING CRACKED AT LONGERON 36. MAINTENANCE REPLACED FITTING IAW SRM 51-1-20D.

Part: VANE — DELAMINATED (RT TE FLAP)

WHILE IN 'C' CHECK, MAINTENANCE FOUND RIGHT WING NR 5 FLAP VANE DELAMINATED. MX REPLACED VANE PER MM 27-51-14.

Part: VANE — DELAMINATED (LT TE FLAP)

WHILE IN 'C' CHECK, MAINTENANCE FOUND LEFT WING NR 5 FLAP VANE DELAMINATED AT LOWER SURFACE. MX REPLACED VANE PER MM 27-51-14.

Part: FITTING — CRACKED (BS 759)

WHILE IN 'C' CHECK, MAINTENANCE FOUND FLOOR BEAM FITTING CRACKED AT STA 759, LBL 48. MX REPLACED FITTING PER SRM 51-1-20D.

Part: BELTFRAME — CRACKED (BS 1040)

WHILE IN 'C' CHECK, MAINTENANCE FOUND BELTFRAME WITH 2 INCH CRACK AT STA 1040 BETWEEN LONGERON 20R AND 21R. MX REPLACED FRAME SECTION PER SRM 51-1-20D.

Part: FITTING — CRACKED (BS 781)

WHILE IN 'C' CHECK, MAINTENANCE FOUND 2 FLOOR BEAM FITTINGS CRACKED AT STA 781, RBL 48 AND LBL 48. MX REPLACED FITTINGS PER SRM 51-1-20D.

Part: SKIN — DELAMINATED (NR 1 SPOILER)

WHILE IN 'C' CHECK, MAINTENANCE FOUND NR 1 SPOILER UPPER SURFACE DELAMINATED ON LEFT WING. MX REPLACED SPOILER ASSY PER MM 27-61-01.

Part: SHEAR TIE — CRACKED (BS 1600)

WHILE IN 'C' CHECK, MAINTENANCE FOUND SHEAR TIE CRACKED 2 INCHES AT STA 1600, LONGERON 23L. MX REPLACED SHEAR TIE PER SRM 53-2-0.

Part: SHEAR TIE — CRACKED (BS 640)

WHILE IN 'C' CHECK, MAINTENANCE FOUND 2 SHEAR TIES CRACKED AT STA 640, AFT AND FWD OF LONGERON 27L. MX REPAIRED SHEAR TIES PER SRM 53-2-0 FIGURE 2A.

Part: FITTING — CRACKED (BS 1240)

WHILE IN 'C' CHECK, MAINTENANCE FOUND FUSELAGE FRAME FITTING CRACKED JUST FWD AND BELOW LIMIT SWITCH, STA 1240, LONGERON 25R. MX REPLACED FITTING PER SRM 51-1-20D.