N826AX

Part: BOLT — BROKEN (LT MLG) · airframe 77,467 hrs · 28,104 cycles

LEFT MAIN LANDING GEAR STRUT LEAKED. FOUND TORSION LINK APEX BOLT DAMAGED/BROKE ON LEFT MAIN LANDING GEAR. REPLACED TORSION LINK APEX BOLT ON LEFT MAIN LANDING GEAR REPACK ON (AVBORNE) NR WX-314, IAW DC8 MM. REPLACED LEFT MAIN LANDING GEAR DOOR RETRACT ACTUATOR (P/N: 5715583-5001, S/N: 131) AND LEFT MAIN LANDING GEAR RETRACT ACTUATOR (P/N: 5774035-5507ABX1, S/N: PPC003) IAW DC8 MM. ALL WORK ACCOMPLISHED ON ABX L/P 033909-089/2 AND AVBORNE'S WO 26627, NR WX-314, WX-315, WX-316, AND WX-317.

Part: ENGINE — LEAKING (NR 3) · airframe 77,409 hrs · 28,070 cycles

NR 3 ENGINE SHUT DOWN IN FLIGHT (STA SDF) DUE TO LOSS OF OIL. FERRIED AIRCRAFT BACK TO ILN. REMOVED AND REPLACED NR 3 ENGINE PER JOB CARD 8090507 IN WORK PACK 600261630.

Part: CTC — DEFECTIVE (NR 2) · airframe 77,195 hrs · 27,923 cycles

NR 2 CTC SMOKED AND MADE LOUD NOISE, STA. MIA. REMOVED AND REPLACED NR 2 CTC IAW DC8 MM 21-10-01-4. OPS CHECKED GOOD.

Part: PUMP — LEAKING (RUDDER) · airframe 77,043 hrs · 27,815 cycles

LOSS OF HYDRAULIC QUANTITY NOTED DURING DESCENT. FOUND STANDBY RUDDER PUMP OVERBOARD DRAIN LEAKING. REMOVED AND REPLACED STANDBY RUDDER PUMP IAW D8C MM 27-24-02. ALSO, CHECKED BYPASS LINE CHECK VALVE OPERATION. OPERATED NORMALLY. REINSTALLED CHECK VALVE. SYSTEM OPS CHECKED GOOD.

Part: FITTING — CRACKED (BS 50) · airframe 76,958 hrs · 27,728 cycles

INTERCOSTAL CORNER FITTING CRACKED FUSELAGE STA 50, RIGHT BUTT LINE 50, FORWARD OF FLOORBEAM. REMOVED CRACKED CORNER FITTING IAW DC8 SRM 51-1-20D. FABRICATED NEW CORNER FITTING IAW REA D853-52924 AND INSTALLED AT STA 50, RIGHT BUTT LINE 50, FORWARD OF FLOORBEAM IAW DC8 SRM 51-1-20D.

Part: DOUBLER — CORRODED (BS 781-798) · airframe 76,958 hrs · 27,728 cycles

CORROSION ON BELLY SKIN DOUBLER IN 4 AREAS BETWEEN STA 781 AND STA 798, LEFT BUTT LINE 4 TO LEFT BUTT LINE 10. REMOVED CORROSION ON BELLY SKIN DOUBLER IAW DC8 SRM 51-1-8. THREE AREAS WITHIN LIMITS IAW DC8 SRM 53-02. REMAINING AREA OUT OF LIMITS. ACCOMPLISHED REPAIR IAW REA D853-52923.

Part: FRAME — CORRODED (BS 1734) · airframe 76,958 hrs · 27,728 cycles

MAIN CARGO STA 1734 BUTT LINE 0, LONGERON 35 LEFT - 35 RIGHT, SURFACE CORROSION ON FRAME. REMOVED CORROSION FROM FRAME. DAMAGE WAS OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 53-2-0 FIG 2, SHT 2.

Part: SUPPORT BRACKET — CORRODED (BS 1160) · airframe 76,958 hrs · 27,728 cycles

AFT CARGO COMPARTMENT, TORQUE BOX FORWARD SIDE AT STA 1160, BETWEEN LONGERON 31 RIGHT & 32 RIGHT, ANGLE AND WEB HAD CORROSION. REMOVED CORROSION, TREATED AND PRIMED. FABRICATED NEW SUPPORT BRACKET, FOUND TO BE OUT OF LIMITS. WORK ACCOMPLISHED IAW REA D853-52918. INSTALLED SUPPORT BRACKET AND FASTENERS IAW DC8 SRM 53-2-0, 51-1-8, 51-1-20D AND 51-1-21.

Part: FLOORBEAM — CORRODED (BS 920) · airframe 76,958 hrs · 27,728 cycles

UPPER HORIZONTAL CAP OF FLOORBEAM CORRODED AT STA 920, LEFT BUTT LINE 10. REMOVED CORROSION. DAMAGE OUT OF LIMITS. FLOORBEAM REPAIRED IAW REA D853-52567.

Part: INTERCOSTAL — CORRODED (BS 30) · airframe 76,958 hrs · 27,728 cycles

UPPER CARGO, STA 30, LEFT BUTT LINE 48, INTERCOSTAL HAD CORROSION JUST AFT OF MAIN CARGO DOOR CONTROL BOX. REMOVED CORROSION ON INTERCOSTAL BEAM AT STA 30, LEFT BUTT LINE 48, AND DETERMINED AREA WAS OUT OF LIMITS. FABRICATED DOUBLER, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0, FIG 1F, 53-2-0, FIG 23, 51-1-8, 51-1-21 AND LWR 200302015.

Part: FRAME — CORRODED (BS 1100) · airframe 76,958 hrs · 27,728 cycles

STA. 1100, LONGERON 18 RT, FRAME CORRODED. REPAIRED FRAME AT STA. 1100, LONGERON 18 RT IAW SRM 53-2-0, FIGURE 2.

Part: FLOORBEAM — CORRODED (BS 880) · airframe 76,958 hrs · 27,728 cycles

MAIN CABIN, STA 880, RIGHT BUTT LINE 63, FLOORBEAM LOWER CHORD, FORWARD SIDE CORRODED. REPAIRED FLOORBEAM STA 880, RIGHT BUTT LINE 63 IAW REA D853-52566MR.

Part: STIFFENER — CORRODED (BS 940) · airframe 76,958 hrs · 27,728 cycles

DURING REMOVAL OF LEFT LONGERON, STIFFENER AT STA 940, LONGERON 24 LEFT, LEFT WHEEL WELL, WAS FOUND CRACKED ON BOTTOM OF BASE. FABRICATED NEW STIFFENER FOR STA 940, LONGERON 24 LEFT IAW REA D853-52556, PO NR 1123110.

Part: ACCESS PANEL — LEAKING (RT WING) · airframe 76,958 hrs · 27,728 cycles

12 BLIND RIVETS LEAKING UPON PRESSURE CHECKS. RIGHT WING, STRINGER NR 7 NEAR ACCESS PANEL 505F. REMOVED 12 BLIND FASTENERS ON STRINGER NR 7 NEAR ACCESS PANEL 505F OF THE RIGHT WING AND WET INSTALLED NEW FASTENERS IAW DC8 SRM 51-1-21 USING 1422 B1/2 SEALANT.

Part: ACCESS PANEL — LEAKING (RT WING) · airframe 76,958 hrs · 27,728 cycles

16 BLIND RIVETS LEAKING UPON PRESSURE CHECKS. RIGHT WING, STRINGER NR 5 NEAR ACCESS PANEL 505F. REMOVED 16 BLIND FASTENERS ON STRINGER NR 5 NEAR ACCESS PANEL 505F OF THE RIGHT WING AND WET INSTALLED NEW FASTENERS IAW DC8 SRM 51-1-21 USING 1422 B1/2 SEALANT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 76,958 hrs · 27,728 cycles

MAIN CABIN, STA 798, BUTT LINE 0 - RT BUTT LINE 48, FLOORBEAM CORRODED. REMOVED NUT PLATES, CLEANED CORROSION ON FLOORBEAM AT STA 798, BUTT LINE 0 - RT BUTT LINE 48, BLENDED AREA, OUT OF LIMITS AT .088 INCH MATERIAL REMAINING FROM ORIGINAL THICKNESS OF .186 INCH. FABRICATED REPAIR ANGLE FROM 7075-T-6511 .125 INCH EXTRUSION P/O NR 1122772, TREATED, PRIMED, AND INSTALLED ANGLE AND NUT PLATES IAW SRM 51-1-8, SSRM DWG K04881, LWR 200302015, SRM 51-1-21A AND 53-2-0, CORROSION CONFINED BETWEEN RT BUTT LINE 33 - 48.

Part: FLOOR SUPPORT — CRACKED (BS 25-35) · airframe 76,958 hrs · 27,728 cycles

FLOOR SUPPORT HAT CHANNEL AT APPROXIMATELY LEFT BUTT LINE 34 BETWEEN STA 25 AND STA 35 WAS CRACKED AND HOLES DAMAGED. REMOVED DAMAGED HAT CHANNEL AND SHIM FROM STA 25 - 35, LEFT BUTT LINE 34. DAMAGE BEYOND REPAIRABLE LIMITS. FABRICATED NEW HAT CHANNEL AND SHIM. ALL PARTS TREATED, PRIMED AND INSTALLED IAW REA D853-52548, DC8 SRM 51-3-1, 51-21-1, 51-1-8, 53-3-1, 51-1-20 AND LWR 200302015.

Part: WEB — CORRODED (FUSELAGE) · airframe 76,958 hrs · 27,728 cycles

CENTERLINE WEB AT STA 800 - 857, BUTT LINE O CORRODED. FABRICATED WEB AT STA 800 - 857, BUTT LINE 0 IAW REA D853-52543. MATERIAL USED .080 7075-T6, P/O NR 1113384.

Part: TRIPLER — CORRODED (FUSELAGE) · airframe 76,958 hrs · 27,728 cycles

EXISTING TRIPLER CORRODED AT STA 857, RT BUTT LINE 50. FABRICATED TRIPLER AT STA 857, RT BUTT LINE 50 IAW REA D853-52539. MATERIAL USED .190 7075-T6, P/O NR 1073367.

Part: SPLICE — CORRODED (STA. 857) · airframe 76,958 hrs · 27,728 cycles

SHIM SPLICE CORRODED AT STA 857, LEFT BUTT LINE 20. FABRICATED SHIM AT STA 857, LEFT BUTT LINE 20 IAW DC8 REA D853-52536. MATERIAL USED .090 P/O NR 1112038.

Part: WEB — CORRODED (STA. 847) · airframe 76,958 hrs · 27,728 cycles

PSI WEB FROM STA 847, LEFT BUTT LINE 40 - 60 CORRODED. FABRICATED PSI WEB FROM STA 847, LEFT BUTT LINE 40 - 60 IAW DC8 REA D853-52534. MATERIAL USED .063 2024-T3, P/O NR 1118786.

Part: WEB — CORRODED (FUSELAGE) · airframe 76,958 hrs · 27,728 cycles

WEB CORRODED AT STA 857, RT BUTT LINE 46. FABRICATED WEB AT STA 857, RT BUTT LINE 46 USING .071 7075-T6, P/O NR 1084025 IAW REA D853-52538.

Part: WEB — CORRODED (FUSELAGE) · airframe 76,958 hrs · 27,728 cycles

WEB CORRODED AT STA 857, LT BUTT LINE 46. FABRICATED WEB AT STA 857, LT BUTT LINE 46 USING .063 7075-T6, PO NR 1118787 IAW REA D853-52535.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 76,958 hrs · 27,728 cycles

RT PRESSURE PANEL AT STA 857, RT BUTT LINE 40 ATTACH ANGLE CORRODED. FABRICATED ATTACH ANGLE RT PRESSURE PANEL AT STA 857, P/N: 5644678 IAW REA D853-52534.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 76,958 hrs · 27,728 cycles

LOWER CHORD AT STA 857, RT BUTT LINE 23 CORRODED. FABRICATED CHORD AT STA 857, RT BUTT LINE 23 IAW REA D853-52537. MATERIAL USED P/N: AND-10134-1407, P/O NR1122772.

Part: DOUBLER — CORRODED (STA 1180) · airframe 76,958 hrs · 27,728 cycles

CORROSION ON TOP OF LONGERON REINFORCEMENT DOUBLER IN AFT CARGO BILGE AT STA 1180, LONGERON 36 TO 34 RIGHT. REMOVED DOUBLER AT STA 1200 LONGERON 34 RIGHT TO 36. REMOVED CORROSION FROM DOUBLER. FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, PRIMED AND INSTALLED NEW DOUBLER FROM 7075-T6.125 P/O NR 119160 IAW DC8 SRM 51-1-8, 51-1-20D, LWR 200302015 AND SSRM DWG K0T142.

Part: FINGER DOUBLER — DAMAGED (FUSELAGE) · airframe 76,958 hrs · 27,728 cycles

INSIDE CENTER TANK, STA 857, LT BUTT LINE 20, AFT FINGER TAB OF DOUBLER BROKEN OFF. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW REA D853-52530.

Part: FLOORBEAM — CORRODED (BS 120) · airframe 76,958 hrs · 27,728 cycles

FOUND MAIN CABIN FLOORBEAM AT STA 120, RIGHT BUTT LINE 51, FORWARD SIDE OF T CAP, CORRODED. REMOVED DAMAGED AREA AND REPLACED WITH ANGLE DOUBLER REPAIR ON FLOORBEAM STA 120, RIGHT BUTT LINE 51 IAW DC8 SRM 51-1-8, 53-2-0, 51-3-0, 53-7-3, 53-0, 51-2-0, 51-1-8, 51-3-1 AND ABX SRM 93-01-14.

Part: FLOORBEAM — CORRODED (BS 55) · airframe 76,958 hrs · 27,728 cycles

MAIN CARGO, STA. 55, LBL 20, CORROSION ON UNDERSIDE OF FLOORBEAM CORNER. REMOVED A 3.5 INCH X .7500 INCH SECTION OF UPPER FLANGE FLOORBEAM AT STA. 55, LBL 20 IAW SRM DWG K04881. FABRICATED REPAIR ANGLE, SHIM AND FILLER IAW SRM DWG K04881.

Part: DOUBLER — CORRODED (CENTER WING) · airframe 76,958 hrs · 27,728 cycles

DOUBLER CORRODED TOP OF WING CENTER SECTION PRESSURE DECK, STA. 683, RT BUTT LINE 10. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-8 AND REA D853-52529.

Part: DOUBLER — CORRODED (FS 683) · airframe 76,958 hrs · 27,728 cycles

DOUBLER CORRODED TOP OF WING CENTER SECTION PRESSURE DECK, STA 683, LONGERON 22 LEFT, LEFT BUTT LINE 10. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-8 AND REA D853-52529.

Part: FLOORBEAM — CORRODED (BS 55) · airframe 76,958 hrs · 27,728 cycles

MAIN CARGO, STA 55, LEFT BUTT LINE 20, CORROSION ON UPPER FLANGE FLOORBEAM. REMOVED 3.5 X .75 INCH SECTION OF UPPER FLANGE FLOORBEAM. ACCOMPLISHED FLOORBEAM REPAIR IAW SSRM DWG K04881.

Part: SKIN — MISDRILLED (BS 857) · airframe 76,958 hrs · 27,728 cycles

FOUND UPPER CARGO STA 857, LEFT BUTT LINE 60 - RIGHT BUTT LINE 60, 5 FASTENERS MIS-DRILLED IN TOP OF CENTER TANK TO SPAR SKIN. REAMED HOLES TO REMOVE DAMAGE, FABRICATED REPAIR BUSHINGS FOR 11 HOLES. INSTALLED REPAIR BUSHINGS WITH WET SEALANT IN HOLES. CONTOURED LOWER BUSHING SURFACE, IN TANK, TO SPAR ANGLE. REF ENGINEERING AUTHORIZATION, BUSHINGS IAW DC8 SRM 51-1-25.

Part: SKIN — MISDRILLED (BS 854) · airframe 76,958 hrs · 27,728 cycles

FOUND UPPER CARGO STA 834, BUTT LINE 0, 4 FASTENERS MIS-DRILLED IN TOP OF CENTER WING SKIN ON TANK. MIS-DRILLED HOLES CLEANED UP, HOLES OPENED UP TO 0.312" AND 0.308", FASTENERS INSTALLED IAW DC8 SRM 51-1-20 ON SPLICE DOUBLER INSTALLATION.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 76,958 hrs · 27,728 cycles

CORROSION FOUND UNDER THREE FASTENERS ON PRESSURE WEB IN RT WHEEL WELL, STA. 857, RT BUTT LINE 27. CORROSION FOUND TO BE OUT OF LIMITS ON PRESSURE WEB IN RT WHEEL WELL, STA. 857, RT BUTT LINE 27 IAW SRM 51-1-8 AND 53-2-0. FABRICATED AND INSTALLED REPAIR IAW REA D853-52533.

Part: FLOORBEAM — CORRODED (BS 857) · airframe 76,958 hrs · 27,728 cycles

MAIN CABIN, STA. 857, LBL 12, FLOORBEAM UPPER CAP CORRODED. REMOVED CORROSION ON FLOORBEAM STA. 857, LBL 12. MATERIAL LOSS OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM DWG K04881.

Part: DOUBLER — CORRODED (STA 1180) · airframe 76,958 hrs · 27,728 cycles

CORROSION ON TOP OF LONGERON REINFORCEMENT DOUBLER IN AFT CARGO BILGE AT STA 1180, LONGERON 35 RIGHT. REMOVED CORROSION AT STA 1180, LONGERON 35 RIGHT. FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, PRIMED AND INSTALLED NEW DOUBLER FROM 7075-T6, 0.125", PO NR 111960 IAW DC8 SRM 51-1-8, 51-1-20D, 53-2-0, LWR 200302015 AND SSRM DWG K07142.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 76,958 hrs · 27,728 cycles

CORROSION FOUND ON STR 31 L (LONGERON) FROM STA. 610 - 730 IN MID ACCESSORY COMPARTMENT. REMOVED AND REPLACED LONGERON 31 LT FROM STA. 610-730 REF SRM 51-1-20 AND DPS 3.67-22.

Part: SHEAR TIE — CRACKED (STA 440) · airframe 76,958 hrs · 27,728 cycles

FOUND SHEAR TIE CRACKED AT STA 440, LONGERON 31 RIGHT (REF. NRC HY-275). REMOVED AREA STRUCTURE FOR ACCESS, REMOVED DAMAGED AREA OF FORMER SECTION/SHEAR TIE, LONGERON 30 RIGHT AND LONGERON 31 RIGHT, STA 440. FABRICATED REPAIR PARTS: 1 FORMER SECTION FROM 0.071" 2024-T3 AND 1 SPLICE DOUBLER FROM 0.071" 2024-T3. BOTH PO NR 1122792. FIT, TREATED, AND PRIMED PARTS. INSTALLED REPAIR PARTS. REINSTALLED STRUCTURE REMOVED FOR ACCESS REF DC8 SRM 53-2-0, FIG 2B.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 76,958 hrs · 27,728 cycles

KEEL BEAM CORRODED AT AFT BULKHEAD OF MID ACCESSORY COMPARTMENT, STA 680, BUTT LINE 0, CORROSION APPEARED TO EXTEND UNDER WING CENTER SECTION. REMOVED CORROSION AT KEEL BEAM STA 620 FWD OF BULKHEAD AND UNDER BULKHEAD AS REQUIRED REF SRM 51-1-8, REF REA D853-52595-MR FOR REPAIR PROCEDURE TO REINFORCE KEEL BEAM. TREATED AND PRIMED AS REQUIRED REF, LWR 200302015 AND SRM 51-1-8.

Part: BULKHEAD — CORRODED (BS 980) · airframe 76,958 hrs · 27,728 cycles

FOUND CORROSION ON RIGHT WHEEL WELL, STA 980, LONGERON 24 RIGHT, AFT BULKHEAD UNDER LOWER SIDE OF DIAGONAL FRAME. REMOVED BRACKET AT STA 980 IAW DC8 SRM 51-3-0, 51-1-S0D. REMOVED CORROSION IAW DC8 SRM 53-2-0. ORIGINAL MATERIAL MEASURED .047" AND .046", OUT OF LIMITS 27 PERCENT AND 25 PERCENT IAW DOUGLAS NDT SRM. FABRICATED FILLERS AND DOUBLER 7075-T6 0.063" PO NR 1118787 IAW DC8 SRM 53-2-0, FIG 1D. TREATED AND PRIMED FABRICATED PARTS IAW DC8 SRM 51-1-8, INSTALLED DOUBLER, FILLERS, AND BRACKET AT STA 980 IAW DC8 SRM 53-2-0, FIG. 1D.

Part: ATTACH FITTING — CRACKED (BS 680) · airframe 76,958 hrs · 27,728 cycles

FOUND CORNER FITTING OF CENTER WING BOX UPPER SURFACE AT STA 680, RIGHT BUTT LINE 62 WAS CRACKED. REMOVED CRACKED FITTING AT CENTER WING BOX UPPER SURFACE STA 680, RIGHT BUTT LINE 62 IAW DC8 SRM 51-1-20D AND SRM 51-3-1, DRILLED, REAMED AND COUNTERSUNK CORNER FITTING IAW DC8 SRM 51-1-20D AND 51-1-24, INSTALLED CORNER FITTING ON CENTER WING BOX UPPER SURFACE AT STA 680 RIGHT BUTT LINE 62 IAW DC8 SRM 51-1-20D AND SRM 51-3-1 (P/N: 3642974-2 PO NR 1122453).

Part: FINGER DOUBLER — CORRODED (FS 1540-1560) · airframe 76,958 hrs · 27,728 cycles

CORROSION FOUND ON FINGER DOUBLER AT STA 1540, LONGERON 31 RIGHT, RIGHT BUTT LINE 25. REPAIRS ACCOMPLISHED AT STA 1540 - 1560, LONGERON 31 RIGHT IAW REA D853-52525.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 76,958 hrs · 27,728 cycles

STA. 680 KEELBEAM INSIDE HEAVY CORROSION ON KEELBEAM TO PRESSURE WEB FOUND DURING ACCOMPLISHMENT OF NR HY-055. REMOVED CORROSION AT KEELBEAM STA. 680, BEHIND BULKHEAD AS REQUIRED REF. SRM 51-1-8 AND REA D853-52595-MR FOR REPAIR PROCEDURE TO REINFORCE KEELBEAM. TREATED AND PRIMED KEELBEAM AS REQUIRED REF. LWR 200302015 AND DC8 SRM 51-1-8.

Part: FINGER DOUBLER — CORRODED (STA. 1480-1500) · airframe 76,958 hrs · 27,728 cycles

AFT LOWER CARGO HAD CORRODED FINGER DOUBLER ON INTERIOR SKIN LOCATED AT STA 1480, LEFT BUTT LINE 32, STRINGER 31 LEFT. REPAIRED FINGER DOUBLERS AT STA 1480 AND 1500, LONGERON 31 LEFT IAW REA D853-52524.

Part: KEELBEAM — CORRODED (BS 700-740) · airframe 76,958 hrs · 27,728 cycles

BS 700 - 740, LEFT BUTT LINE 10, LEFT SIDE OF KEELBEAM, CORROSION ON THE LOWER CENTER WING SPLICE DOUBLER. CLEANED CORROSION, TREATED, AND PRIMED IAW DC8 SRM 51-1-8, 53-2-0, LWR NR 200302015. FABRICATED AND INSTALLED REPAIR DOUBLER IAW REA D853-52564.

Part: FLOORBEAM — CORRODED (BS 70) · airframe 76,958 hrs · 27,728 cycles

FOUND MAIN CABIN, STA 70, RIGHT BUTT LINE 43-51, LOWER SIDE OF FLOORBEAM CORRODED OUT OF LIMITS. FOUND LOWER SIDE OF FLOORBEAM CORRODED OUT OF LIMITS AT STA 70, RIGHT BUTT LINE 43-51. FABRICATED FILLER AND DOUBLER AND INSTALLED. ALL WORK IAW DC8 SRM 51-1-8, 53-7-3, 51-2-0, 53-2-0, AND LWR 200302015.

Part: FLOORBEAM — CORRODED (BS 680) · airframe 76,958 hrs · 27,728 cycles

FOUND MAIN CABIN, STA 680, RIGHT BUTT LINE 26, LOWER SIDE OF FLOORBEAM CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, ORIGINAL MATERIAL THICKNESS 0.178", REMAINING THICKNESS 0.107" AND OUT OF LIMITS IAW DC8 SRM 53-2-0. VERIFIED REPAIR AINGLE AS AND10134-1407 PO NR 1122486. FABRICATED, LOCATED, AND DRILLED REPAIR PARTS IAW ABX DWG K04881. PRECOATED ALL BARE METAL IAW LWR NR 200302015, AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D AND ABX DWG K04881.

Part: FLOORBEAM — CORRODED (BS 920) · airframe 76,958 hrs · 27,728 cycles

FOUND MAIN CABIN, STA 920, RIGHT BUTT LINE 31, FLOORBEAM CORRODED AT NUTPLATES. REMOVED CORROSION STA 920, RIGHT BUTT LINE 31. MATERIAL LOSS OUT OF LIMITES. FABRICATED REPAIR ANGLES AND INSTALLED IAW DWG K04881 OUT OF 7075 "0", PO NR 1108502 0.063", HEAT TREATED TO T6.

Part: SKIN — CORRODED (FUSELAGE) · airframe 76,958 hrs · 27,728 cycles

FUSELAGE SKIN, STA 1100 TO 1120 AT RT AFT BODY FAIRING, SKIN CORRODED. REMOVED CORROSION AND INSTALLED REPAIRS BETWEEN STA 1100 LONGERON 29 RT TO STA 1120 LONGERON 30 RT IAW REA D853-52518-MR AND SRM 51-1-8, PG 20.

Part: FLOORBEAM — CORRODED (BS 120) · airframe 76,958 hrs · 27,728 cycles

MAIN CABIN, BS 120, RIGHT BUTT LINE 50, FLOORBEAM HAD EXCESSIVE MATERIAL LOSS. REMOVED DAMAGED AREA AND REPLACED WITH ANGLE DOUBLER AND FILLER ON FLOORBEAM BS 120, RIGHT BUTT LINE 50 IAW DC8 SRM 51-1-8, 53-2-0, 51-3-0, 53-7-3, 53-0, 51-2-0, 51-1-8, 51-3-1, 51-1-21 AND ABX SSRM 93-01-14.

Part: FLOORBEAM — CRACKED (BS 900) · airframe 76,958 hrs · 27,728 cycles

MAIN CABIN, STA 900, RIGHT BUTT LINE 54, FLOORBEAM CRACKED ON AFT SIDE UPPER CAP, FROM OUTBOARD END OF BEAM TOWARD INBOARD THROUGH TWO FASTENER HOLES. REPAIRED AREA IAW REA D853-52925 BY TRIMMING OUT CRACKED AREA AND INSTALLING A FILLER.

Part: AIR DUCT — DENTED (NR 4 ENGINE) · airframe 76,958 hrs · 27,728 cycles

NR 4 ENGINE L/S TRANSITION AIR DUCT HAD SEVERAL DENTS. 2 DENTS AT 9 AND 11 O'CLOCK POSITIONS OUT OF LIMITS IAW DC8 SRM 51-1-9A. CLEANED UP AREA OF DENTS AT 9 AND 11 O'CLOCK POSITIONS AND REPAIRED IAW DC8 SRM 51-1-9A. 2 MORE DENTS AT 11 O'CLOCK POSITION ARE WITHIN LIMITS AND CLEANED UP AREAS AND REPAIRED IAW DC8 SRM 51-1-9A. TREATED REPAIRS IAW LWR200302015 AND PRIMED IAW DC8 51-1-3.

Part: STIFFENER — CORRODED (FS 980) · airframe 76,958 hrs · 27,728 cycles

LOWER AFT CARGO FORWARD BULKHEAD LEFT SIDE FRAME CORRODED AT BOTTOM STA 980, 30 LEFT. REMOVED OLD STIFFENER IAW DC8 SRM 51-3-1 AND 51-1-21 WHICH HAD CORROSION OUT OF LIMITS IAW DC8 SRM 53-2-0 AND REPLACED WITH NEW STIFFENER PO NR 1122166 IAW DC8 SRM 51-1-21 AND 51-3-1.

Part: LONGERON — CORRODED (BS 598) · airframe 76,958 hrs · 27,728 cycles

FORWARD CARGO BAY, CORROSION IN LONGERON 36, STA 598 OUT OF LIMITS. REPAIRED LONGERON 36 IAW DC8 SRM 53-2-2 AND SPLICE WITH NEW SECTION FROM EXTRUSION P/N: S2645716 IAW DC8 SRM 53-2-2-, PG 6.

Part: CASE — WORN (EXHAUST NOZZLE) · airframe 76,958 hrs · 27,728 cycles

NR 2 ENGINE EXHAUST NOZZLE 6 O'CLOCK POSITION, CASE WORN. REMOVED DAMAGED EXISTING DOUBLERS IAW DC8 SRM 51-1-21. FABRICATED NEW DOUBLERS IAW SSRM DWG NR 78-841 FROM 0.051 301 1/2HD PO NR 1121624, PRIMED CONTACT SURFACE IAW DC8 51-1-8. INSTALLED NEW DOUBLER IAW SSRM DWG NR 78-841 AND DC8 SRM 51-1-21.

Part: DOUBLER — CORRODED (FS 940) · airframe 76,958 hrs · 27,728 cycles

CORRODED DOUBLER IN MAIN CARGO BELOW FLOOR LEVEL AGAINST ABOVE LEFT WHEEL WELL PRESS DECK, STA 940, LEFT BUTT LINE 67. REMOVED, FABRICATED AND REPLACED DOUBLERS IN MAIN CARGO BELOW FLOOR LEVEL AGAINST ABOVE LEFT PRESS DECK STA 940, LEFT BUTT LINE 67 IAW DC8 SRM 51-1-8, 53-2-0, 51-1-20, 51-9-0, 51-1-20D, 53-3-0, 51-3-1 AND DPS 4.710-2.

Part: COWLING — SCORED (NR 1 ENGINE) · airframe 76,958 hrs · 27,728 cycles

NR 1 ENGINE, OUTBOARD FORWARD COWL HOLD OPEN ROD HAD SCORED INNER SIDE OF COWL. REMOVED PREVIOUS REPAIR, FABRICATED NEW DOUBLER, AND APPLIED COMPOSITIE REPAIR IAW DC8 SRM 51-1-9A, TREATED DOUBLER IAW LWR 200302015 AND PRIMED IAW DC8 SRM 51-1-8.

Part: PRESSURE PANEL — CORRODED (FS 980) · airframe 76,958 hrs · 27,728 cycles

DOUBLER CORRODED TOP OF RIGHT WHEEL WELL PRESSURE DECK IN MAIN CARGO, STA 980, RIGHT BUTT LINE 30. REMOVED, FABRICATED, AND INSTALLED DOUBLER AT TOP OF RIGHT WHEEL WELL PRESSURE DECK IN MAIN CARGO STA 980 RIGHT BUTT LINE 30 IAW DC8 SRM 51-1-21, 51-1-14, 51-9-0 AND DPS 3.695.

Part: ATTACH ANGLE — CRACKED (FS 160) · airframe 76,958 hrs · 27,728 cycles

FORWARD CARGO BAY DENT ON GILLINER ATTACH ANGLE, STA. 160, BETWEEN LONGERON 36 LEFT TO 35 LEFT. REMOVED DENT IN FORWARD CARGO BAY GILLINER ATTACH ANGLE STA 160, LONGERON 36 LEFT - 35 LEFT, FOUND TO BE CRACKED, REPAIRED. REMOVED GILLINER ATTACH ANGLE IAW DC8 SRM 51-1-21, WELDED ATTACH ANGEL IAW ABX PROCESS STDS MANUAL 900-7-2-1, TREATED IAW LWR 200302015-4/15/O3, PRMIED IAW DC8 SRM 51-1-8. REINSTALLED GILLINER ANGLE IAW DC8 SRM 51-1-20D.

Part: FRAME — TOOL DAMAGE (FS 120) · airframe 76,958 hrs · 27,728 cycles

FORWARD CARGO BAY DRILL START IN FRAME RADIUS, STA 120, ABOVE LONGERON 31 RIGHT, RIGHT BUTT LINE 33. ORIGINAL MATERIAL 7075-T6 0.090" PER DC8 SRM 53-4-1, PG 125. FABRICATED REPAIR ANGLE FROM 7075-0 FIG 2, HEAT TREATED IAW DC8 SRM 51-1-4, SHIM FROM 7075-T6 0.050" PO NR 1118787, TREATED IAW LWR 200302015, PRIMED IAW 51-1-8, INSTALLED DOUBLER AND SHIM IAW 51-1-20D PG 1 AND 51-1-21.

Part: FITTING — CRACKED (BS 1580) · airframe 76,958 hrs · 27,728 cycles

AFT CARGO, RT SIDE, STA. 1580 HAD CRACKED FITTING, RBL 58, LONGERON 21 RT. REMOVED AND REPLACED CRACKED FITTING AT STA. 1580, RBL 58 IAW SRM 51-1-21 AND 51-3-1.

Part: FLOORBEAM — CORRODED (FS 1660) · airframe 76,958 hrs · 27,728 cycles

MAIN DECK AFT ACCESSORY COMPARTMENT, STA 1660, LEFT BUTT LINE 44, LONGERON 22 LEFT, FLOORBEAM HAD CORROSION. CLEANED UP SURFACE CORROSION WITH NEGLIGIBLE MATERIAL LOSS EXCEPT FOR AROUND ONE FASTENER HOLE. REPAIRED CORROSION DAMAGE IAW DC8 SRM 51-1-8, PG 20, 53-2-0, 51-5-0, 53-2-0, FIG 18, LWR200302015-4/15/03, AND DC8 SRM 51-1-8, PG 14. REPAIR MATERIAL ALUMINUM EXTRUSION P/N AND10136-2001 7075-T6 0.063" PO NR 1120529 AND 7075-T6 0.063 PO NR 1118787.

Part: ANGLE — CORRODED (BS 857) · airframe 76,958 hrs · 27,728 cycles

FOUND CORNER ANGLE ON PRESSURE WEB CORRODED ON FORWARD BULKHEAD IN RIGHT WHEEL WELL, STA 857, RIGHT BUTT LINE 48. NEW CORNER ANGLE FABRICATED IAW REA D853-52555. ANGLE INSTALLED IAW DC8 SRM 51-1-20 AT STA 857, RIGHT BUTT LINE 48.

Part: SKIN — DAMAGED (STA. 440) · airframe 76,958 hrs · 27,728 cycles

LOWER FUSELAGE SKIN, STA 400, LONGERON 31 RIGHT, FASTENER HEADS SHEARED. REMOVED DAMAGED FASTENERS, NOTED CORROSION ON INTERNAL FINGER DOUBLER AT STA 440 LONGERON 31 RIGHT. REPAIRED FINGER DOUBLER IAW REA D853-52523. ELONGATED AND OVER-SIZED HOLES AT STA 440, BETWEEN LONGERON 30 RIGHT AND 31 RIGHT. REMOVED DAMAGED SKIN AREA. FABRICATED: 1 FILLER 0.071" 7075-T6 PO NR 1084025, 1 EXTERNAL DOUBLER P.080" 7075-T6 PO NR 1113384, 2 INTERNAL DOUBLERS .050" 7075-T6 PO NR 1112267. FIT, TREATED AND PRIMED PARTS. INSTALLED REPAIR PARTS AND FASTENERS REF DC8 SRM 53-2-1, FIG 7, SHEETS 1 AND 4.

Part: ANGLE — CORRODED (BS 857) · airframe 76,958 hrs · 27,728 cycles

CORROSION LOWER ANGLE ON PRESSURE WEB ON FWD BULKHEAD STA. 857, FORWARD OF RT. WHEEL WELL, APPROXIMATELY LONGERON 24. WING TO BODY ANGLE AT STA. 857 CORRODED BEYOND LIMITS. ANGLE REMOVED FROM LBL13 - RBL 57.5 AND NEW SECTION INSTALLED IAW SRM 51-1-20.

Part: FITTING — CORRODED (STA. 879) · airframe 76,958 hrs · 27,728 cycles

FOUND STA 900, L-24, CORROSION ON FORWARD SECTION AND AFT OF FITTING AT ATTACH POINT TO L-24. REMOVED AND REPLACED FITTING WITH NEW PART IAW DC8 SRM 51-10-1. POSITIONED, DRILLED UP HOLES, REAMED AND INSTALLED FITTING AT STA 879 (900) L-24 IN LEFT WHEEL WELL IAW DC8 SRM 51-1-20.

Part: FITTING — CRACKED (STA. 880) · airframe 76,958 hrs · 27,728 cycles

UPPER FORWARD MOST SUPPORT ANGLE WAS CRACKED IN 2 PLACES ON TOP OF L-24 FITTING IN RIGHT WHEEL WELL. REMOVED AND REPLACED CRACKED FITTING TOP OF L-24 RIGHT WHEEL WELL STA 880, P/N: 5750198-502 IAW DC8 SRM 51-1-20D.

Part: SUPPORT FITTING — CRACKED (BS 940) · airframe 76,958 hrs · 27,728 cycles

SUPPORT FITTING WAS CRACKED ON LONGERON 24 RIGHT IN RIGHT MAIN LANDING GEAR WHEEL WELL AT APPROXIMATELY STA 940. REMOVED SUPPORT FITTING BRACKET ON LONGERON 24 STA 940 RIGHT MAIN LANDING GEAR, NEW BRACKET FABRICATED BY OUTSIDE VENDOR, REF REA D853-52521, PO NR 1122790, DRILLED AND TRIMMED FABRICATED PART IAW REA D853-52521, STEP NR 5, INSTALLED SUPPORT FITTING BRACKET ON LONGERON 24, STA 940 RIGHT MAIN LANDING GEAR IAW DC8 SRM 51-1-20D.

Part: CUSP WEB — CORRODED (BS 1020-1140) · airframe 76,958 hrs · 27,728 cycles

CORROSION ON CUSP LINE EXTRUSION, STA. 1020 TO STA. 114O, LONGERON 21 RT. CORRODED BEYOND LIMITS. REMOVED AND REPLACED CUSP EXTRUSION IAW SRM 53-2-5, FIG. 15 AND 15A.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 76,958 hrs · 27,728 cycles

CORROSION RUNNING THE ENTIRE FLOORBEAM, FORMER AND FASTENERS AT STA. 1640, LONGERON 22 RT, UNDERSIDE AFT. CORRODED BEYOND LIMITS AT RBL 53-60. REMOVED END CAP AND DOUBLER L/S. REMOVED CORROSION IAW SRM 53-2-0, PG 2P, FIG 1F AND INSTALLED END CAPS AND DOUBLER. CUT OUT CORROSION AT RBL 55. FABRICATED DOUBLER AND FILLER AND INSTALLED.

Part: KEELBEAM — CORRODED (BS 610-710) · airframe 76,958 hrs · 27,728 cycles

CORROSION FOUND ON SURFACE OF KEEL BEAM IN MID CARGO BAY BILGE AREA, STA 610 TO 710 APPROXIMATELY BUTT LINE 0. MULTIPLE BLENDED AREAS ON BOTH HORIZONTAL LEGS RANGING FROM 0.010" MIN TO MAX BLEND DEPTH OF 0.141". REMOVED CORROSION ON UPPER SURFACE OF KEEL BEAM IN MID CARGO BAY BILGE AREA STA 640 IAW DC8 SRM 53-2-0, PG 2M AND REA D853-52595.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 76,691 hrs · 27,568 cycles

CORROSION DISCOVERED ALONG LONGERON 24 RIGHT, BEHIND THE INBOARD SPLICE FITTING AT STA 980 IN THE RIGHT WHEEL WELL. REMOVED CORROSION FROM THE LONGERON AND FITTING BY BLENDING. ALL REWORKED AREAS ARE WITHIN SRM LIMITS.

Part: WIRE — BROKEN (RT MLG) · airframe 76,474 hrs · 27,432 cycles

RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE WITH GEAR DOWN - RED GEAR UNSAFE LIGHT NOT ON - HORN DID NOT SOUND. RECYCLED NO HELP. FOUND WIRES G321E24 AND G324N24 BROKEN INSIDE THE CONDUIT BETWEEN P1-1398 AND S3-4. REPLACED BOTH WIRES AND WIRE G320H20 AS A PRECAUTION. PERFORMED GEAR SWING (ON WORK PACK NON ROUTINE CARD 106) IAW DC-8 MM 32-60-00-2. OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (MLG) · airframe 76,460 hrs · 27,426 cycles

RIGHT MAIN LANDING GEAR GREEN LIGHT WOULD NOT COME ON WHEN THE GEAR WAS EXTENDED. CYCLED THE GEAR TWICE AND THE LIGHT STARTED WORKING. FOUND CORROSION ON P1-1398 AND S1-210. REMOVED AND REPLACED CONNECTOR P1-1398 AND RIGHT LANDING GEAR DOWN SWITCH S1-120. PERFORMED GEAR SWING, RIGHT LANDING GEAR INDICATION OPS CHECKED GOOD IAW DC-8 AMM 32-60-00-2.

Part: ARM — LOOSE (CONTROL VALVE) · airframe 75,564 hrs · 26,948 cycles

DURING DESCENT THRU 10,000, AIRCRAFT BEGAN A ROLL TO LEFT, AUTOPILOT DISCONNECTED AND AIRCRAFT CONTINUED TO ROLL UNTIL RIGHT AILERON WAS APPLIED. DURING ROLL EVENT, AIRCRAFT HAD A MILD SHAKING. MAINTENANCE FOUND LATERAL CONTROL SPOILER POWER CONTROL VALVE ARM LOOSE. SECURED ARM IAW DC-8 AMM 27-62-09. LUBED AILERON CONTROL CABLES ON LEFT WHEEL WELL IAW DC-8 AMM 20-17-00. OPS CHECKED AILERON. SYSTEMS WORKING NORMAL IAW DC-8 AMM 27-11-00.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,475 hrs · 26,895 cycles

DURING MAINTENANCE INSPECTION, FOUND THE EMERGENCY LIGHTS INOPERATIVE. REPLACED THE EMERGENCY LIGHTS BATTERY PACK ASSEMBLY IAW DC8 MM 33-50-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 75,270 hrs · 26,784 cycles

AIR CONDITION ACCESSORY COMPARTMENT AT STA 70, LONGERON 34 RIGHT TO LONGERON 35 RIGHT, BULKHEAD ATTACH FITTING CORRODED. REPAIRED CHORD AND LONGERON FITTING IAW DC-8 SRM 51-1-24, 53-2-5 AND 51-1-8.

Part: SPAR CAP — CRACKED (CENTER WING) · airframe 75,270 hrs · 26,784 cycles

TOP SIDE OF CENTER WING BOX, STA 857, LEFT BUTT LINE 24, UPPER SPAR CAP HAD A 3 INCH CRACK. REPAIRED AREA IAW DC-8 SRM 51-1-24, 51-1-20D AND 31-3-1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,270 hrs · 26,784 cycles

RIGHT PRESSURE DECK MAIN CABIN LOWER SIDE OF FLOORBEAMS AT STA 920 AND 940 ARE EXFOLIATED. REPAIRED AREA IAW REA D853-48871MR AND REA D853-48873MR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 75,270 hrs · 26,784 cycles

AFT ACCESSORY INNER SKIN AT LONGERON 27 RIGHT, LONGERON 26 RIGHT, STA 1660 - 1680 WAS CORRODED. REPAIRED AREA IAW REA D853-4866MR.

Part: WEB — CORRODED · airframe 75,270 hrs · 26,784 cycles

MAIN CABIN FS 280 AND RIGHT CUSP HAD CORROSION. REPAIRED AREA IAW REA D853-48860MR.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,270 hrs · 26,784 cycles

LONGERON 24 LEFT, STA 980, UPPER LIP CRACKED. REPAIRED AREA IAW REA D853-48872MR.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 75,270 hrs · 26,784 cycles

ATTACH ANGLE TO UPPER PRESSURE DECK FLOOR FROM STA 960 - 980, 100 INCHES FROM RIGHT CUSP, HAD CORROSION. REPAIRED AREA IAW REA D853-48865MR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 75,270 hrs · 26,784 cycles

MAIN CABIN CENTER WING BOX HAD CORROSION AT LEFT BUTT LINE 8, STA 850. REPAIRED AREA IAW REA D857-48869MR.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,270 hrs · 26,784 cycles

AFT LOWER CARGO STA 1140, ABOVE LONGERON 35 RIGHT, RIVNUT INSTALLED THROUGH PORTION OF FASTENER HEAD. REPAIRED AREA IAW REA D853-48864MR.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,270 hrs · 26,784 cycles

LONGERON 24 LEFT CRACKED, LOWER INNER FLANGE OF BOTTLE BOLT CAVITY. REPAIRED LONGERON 23 LEFT IAW DC-8 SRM 53-2-2 AND REA D853-48861MR.

Part: FASTENER — WRONG PART (FLOOR SUPPORT) · airframe 75,270 hrs · 26,784 cycles

ATTACH ANGLE TO FLOOR SUPPORT CENTER WING BOX, RIGHT SIDE 857, ANGLE HAD IMPROPER FASTENER INSTALLED. REPAIRED AREA IAW REA D857-48854MR.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 75,270 hrs · 26,784 cycles

MID SHIP ACCESSORY COMPARTMENT, FS 640 - 660, L-36 KEEL BEEM EXTENSION CORRODED. REMOVED CORROSION IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR DOUBLER IAW ABX REA D853-48863MR, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8.

Part: PRESSURE PANEL — CORRODED · airframe 75,270 hrs · 26,784 cycles

RIGHT WHEEL WELL, CORROSION ON SPOILER CABLE BRACKET FOOT END AROUND ATTACH BOLTS, JUST ABOVE LONGERON 24, FS 920. REPAIRED AREA IAW DC-8 REA D853-48868MR.

Part: LATCH — WORN (LT MLG) · airframe 75,034 hrs · 26,643 cycles

RED GEAR UNSAFE LIGHT AND LEFT GEAR DOOR NOT LATCHED LIGHT CAME ON. BOTH LIGHTS WENT OUT AFTER PERFORMING ALTERNATE UPLATCH CHECK ABNORMAL, THRU FLAP EXTENSION. GEAR CYCLED. CHECKED GEAR DOOR LATCH MECHANISM, CHECKED TARGET, CLEANED AND LUBED SWITCH AND CYCLED GEAR DOOR SEVERAL TIMES. OPS CHECKED GOOD, LIGHT OUT ON GROUND. NO DEFECTS NOTED IAW 32-31-04.

Part: LOCK — BROKEN (COCKPIT DOOR) · airframe 74,569 hrs · 26,352 cycles

AFTER PRE-DEPARTURE CHECK WAS COMPLETED. CREW WAS UNABLE TO OPEN COCKPIT DOOR. FOUND DOOR LOCK PLUNGER BROKEN IN LOCKED POSITION. INSTALLED SLIDE LOCK ON FLIGHT COMPARTMENT SIDE OF COCKPIT DOOR. VERIFIED THAT LOCK WAS OPERABLE FROM INSIDE THE COCKPIT. REPLACED COCKPIT DOOR HANDLE IAW REA D852-47190. COCKPIT DOOR HANDLE OPS CHECKED GOOD WHEN DOOR OPENED AND CLOSED.

Part: BRACKET — DEFECTIVE · airframe 73,985 hrs · 25,965 cycles

HOT CUP CAUSED A BURNING ODOR AND SMOKE FROM PRONGS ON THE HOT CUP. REPLACED HOT CUP AND BRACKET ASSEMBLY. OPS CHECKED GOOD IAW DC-8 MM.

Part: FLOORBEAM — BENT (FUSELAGE) · airframe 73,879 hrs · 25,892 cycles

AFT CARGO, STATION 1320, RIGHT BUTT LINE 33, FLOORBEAM WAS BENT. REPAIRED AREA IAW ABX REA D853-43921MR AND DC-8 SRM 51-1-8.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,879 hrs · 25,892 cycles

L1 DOOR FORWARD LOWER AND AFT CORNER REPAIRS. REPAIRED AREA IAW ABX REA D853-43922-MR, DC-8 SRM 53-2-0, 51-1-20D, 51-1-21, AND 51-3-0.

Part: BEAM — CORRODED (STA. 940) · corrosion level 2 · airframe 73,879 hrs · 25,892 cycles

MAIN CABIN STATION 940, RIGHT BUTT LINE 68, CORROSION UNDER BEAM AND SHEAR WEB PANEL, LOWER SIDE CORNER. REPAIRED AREA IAW REA D853-43931-MR.

Part: FITTING — CORRODED (RT WING) · airframe 73,879 hrs · 25,892 cycles

RIGHT WING STATION 219, FLAP LINK SUPPORT (CANOE) WAS CORRODED AND PITTED UNDER AFT TRACK PLATES. REMOVED CORROSION FROM FLAP LINK SUPPORT FITTING AND FABRICATED REPAIR FILLERS IAW DC-8 SERVICE BULLETIN 27-164. REMOVED CORROSION FROM LEFT AND RIGHT SIDE SUPPORT HOLES, FABRICATED AND INSTALLED REPAIR BUSHINGS IAW REA D827-43940-MR.

Part: WEB — CORRODED (FS 960) · corrosion level 2 · airframe 73,879 hrs · 25,892 cycles

MAIN CABIN STATION 960, CORROSION UNDER BEAM AND SHEAR WEB BY LEFT BUTT LINE 68. REPAIRED AREA IAW ABX REA D853-43930-MR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,879 hrs · 25,892 cycles

AFT CARGO AT STA. 1300, RBL 16, FLOORBEAM WAS CORRODED. FABRICATED NEW REPAIR PARTS AND FLOORBEAM IAW ABX REA D853-43926-MR, 51-1-8, 53-2-0, 51-1-20D, 51-3-0, AND 51-1-21.

Part: FITTING — CRACKED · airframe 73,879 hrs · 25,892 cycles

CABIN UNDER FLOOR FRAME STIFFENER WAS CRACKED AT FS 780, LEFT BUTT LINE 47.0. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D, 51-3-2 AND 51-3-0.

Part: LONGERON — CORRODED (FS 36) · corrosion level 2 · airframe 73,879 hrs · 25,892 cycles

AIR COND/PRESS COMPARTMENT AT FS 36, LONGERON 31 RIGHT, AT OUTBOARD SIDE WAS CORRODED AROUND FASTENERS. FABRICATED REPAIR STRAP AND REPAIRED AREA IAW REA D853-43733-MR, SRM 53-2-0, 51-1-8, 51-1-20D.

Part: FITTING — CRACKED (XRS 408) · airframe 73,879 hrs · 25,892 cycles

#4 ALT HAD A CRACKED STRINGER END FITTING AT XRS 408. SPLICE - STRINGER 59 AFT SIDE. INSTALLED NEW END FITTING AND BOOST PUMP BRACKET IAW DC-8 SRM 51-1-24, 51-1-8, AND 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,879 hrs · 25,892 cycles

AFT ACCESSORY COMPARTMENT LONGERON END FITTING CRACKED AT FS 1690, LONGERON 32 LEFT. FABRICATED LONGERON AND FRAME REPAIRS, INSTALLED REPAIRS IAW DC-8 SRM 53-2-0, 53-2-2, 51-1-8, 51-1-20D, 51-3-0, AND REA D853-43934-MR.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,879 hrs · 25,892 cycles

MAIN CABIN, STATION 857 TO 880, BUTT LINE 0, CORROSION FOUND UNDER FINGER DOUBLER AND UNDER CABLE SUPPORT BRACKET. REPAIRED AREA IAW REA D853-43928-MR.

Part: FRAME — CORRODED (FS 1140) · corrosion level 2 · airframe 73,879 hrs · 25,892 cycles

AFT CARGO FRAME HAD CORROSION AROUND NUTPLATE AT FS 1140, LONGERON 30 LEFT. CORROSION WAS OUT OF LIMITS. TRIMMED OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 51-1-8, 53-2-0, 51-1-20D, AND REA D853-43923-MR.

Part: TRACK — CORRODED (STA. 1440) · corrosion level 2 · airframe 73,879 hrs · 25,892 cycles

AFT CARGO COMPARTMENT STATION 1440 TO 1540, RIGHT BUTT LINE 60, CORROSION UNDER FLOOR BOARD CLIP NUTS. FABRICATED 8 EACH SPLICES AND REPAIR TRACK, INSTALLED AND REPAIRED AREA IAW DC-8 SRM 51-3-0, 53-2-0, 53-2-3, AND 51-1-8.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,879 hrs · 25,892 cycles

FORWARD CARGO TEE CHORD AT FS 70 WAS CORRODED BETWEEN LONGERON 29 LEFT - LONGERON 31 LEFT. FABRICATED REPAIR DOUBLER AND REPAIRED AREA IAW DC-8 SRM 51-1-27 AND REA D853-43935-MR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,879 hrs · 25,892 cycles

RIGHT NOSE TUNNEL STATION 32, FRAME WAS CRACKED. FABRICATED NEW FRAME AND REPAIRED AREA IAW DC-8 SRM 51-1-20D, 53-3-1, 53-2-0, AND 51-1-8.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,879 hrs · 25,892 cycles

RIGHT WHEEL WELL UPPER PRESSURE DECK REPAIR DOUBLER EXFOLIATED ABOVE LONGERON 24, FS 879. REPAIRED AREA IAW ABX REA D853-43932-MR.

Part: FLAP TRACK — CORRODED (RIGHT WING) · corrosion level 2 · airframe 73,879 hrs · 25,892 cycles

RIGHT WING INBOARD FLAP, INBOARD FLAP TRACK SHOWED EVIDENCE OF WEAR AND CORROSION. REPLACED THE RIGHT WING INBOARD FLAP, INBOARD FLAP TRACKS IAW DC-8 MM 27-51-03.

Part: LONGERON — CORRODED (FS 24) · corrosion level 2 · airframe 73,879 hrs · 25,892 cycles

AIR COND/PRESS COMPARTMENT AT FS 24, LONGERON 31 RIGHT WAS CORRODED AT ATTACH ANGLE ATTACHING FASTENERS. REMOVED CORRODED CLIP LONGERON TO FRAME. INSTALLED NEW ATTACH P/N 2643619-1 IAW DC-8 SRM 51-1-21A AND 51-1-24.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,879 hrs · 25,892 cycles

AIR COND/PRESS COMPARTMENT BETWEEN FS 56-70, LONGERON 36, END FITTING WAS CORRODED. REPLACED END FITTING IAW DC-8 SRM 51-1-20D.

Part: SPAR CAP — CRACKED (RIGHT WING) · airframe 73,879 hrs · 25,892 cycles

RIGHT WING FORWARD LOWER SPAR CAP HAD CRACK INDICATIONS IN FASTENER HOLES #2 AND #4 FROM THE INBOARD SIDE. FABRICATED REPAIR PARTS AND REPAIRED AREA IAW ABX DC-8 JOB CARD J060232, DC-8 SRM 51-1-8, 51-1-20D, AND 51-1-25.

Part: LINK — BROKEN (RT TE FLAPS) · airframe 73,604 hrs · 25,686 cycles

RIGHT INBOARD FLAP DRIVE LINK BROKEN. REPLACED RIGHT STATION 98 FLAP DRIVE LINK ASSEMBLY IAW DC8 MM 27-51-04-3-0001. OPS CHECKED GOOD.

Part: CONTROL UNIT — DEFECTIVE (FUSELAGE) · airframe 7,332 hrs · 25,520 cycles

ANTI-SKID CONTROL PANEL RIGHT AND LEFT INBOARD LIGHTS ILLUMINATED ON LANDING. REDUCED BRAKING WAS EXPERIENCED ON LANDING ROLL OUT. MAINTENANCE INSPECTED AND DEFERRED THE ANTI-SKID SYSTEM IAW DC-8 MEL 32-1. LATER ON 09/15/01 THE ANTI-SKID CONTROL UNIT WAS REPLACED AND THE DEFERRAL WAS REMOVED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,164 hrs · 25,425 cycles

FRAME TO LONGERON FITTING WAS CRACKED AFT SIDE, STA 820, ABOVE LONGERON 22 RIGHT. REPLACED FITTING IAW DC-8 DWG 4753360, SRM 53-1-0 AND 51-1-20D.

Part: SPAR CAP — CRACKED (RT WING) · airframe 73,164 hrs · 25,425 cycles

RIGHT WING AFT UPPER SPAR CAP WAS CRACKED BETWEEN XCW 69.5 AND XCW 46. REPLACED RIGHT WING UPPER SPAR CAP BETWEEN XCW 0 TO XRS 74.8 IAW REA D857-41242MR.

Part: SPAR — CORRODED (WING) · corrosion level 2 · airframe 73,006 hrs · 25,341 cycles

THE RIGHT WING SPAR AFT FACE AT UPPER DIHEDRAL HAD CORROSION EXTENDING DOWN FROM THE TOP OF AFT FACE TO BOTTOM OF THE REAR SPAR. MAINTENANCE INSPECTED AND REPLACED THE SPAR WEB.

Part: PRESSURE SWITCH — MALFUNCTIONED (NR 4 ENGINE) · airframe 72,508 hrs · 25,075 cycles

AFTER LEVEL-OFF AT FL 350, NR 4 ENGINE OIL PRESSURE LIGHT STARTED FLICKERING WITH SHORT PERIODS OF BEING ON STEADY. RETARDED NR 4 THROTTLE AND LOW PRESSURE LIGHT REMAINED ONSTEADY. SHUT NR 4 ENGINE DOWN. REPLACED OIL DIFFERENTIAL PRESSURE SWITCH. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHT DID NOT ILLUMINATE WHEN TURNED ON. RELAMPED IAW DC8 MM 33-10-00. OPS CHECKED GOOD.

Part: RIB — CRACKED (WS 195)

LEFT WING LEADING EDGE UPPER RIB CRACKED AT FASTENER END AT STATION XFS 195. REPAIRED IAW DC8 SRM 57-2-0.

Part: WINDOW — LACK OF LUBE (COCKPIT)

FIRST OFFICER'S SLIDING WINDOW (EMERG EXIT) WOULD NOT OPEN. CLEANED LATCH AND LUBRICATED AS REQUIRED, OPS CHECKED GOOD.

Part: VALVE ASSY — BYPASSING (MLG)

AFTER TAKEOFF AND GEAR RETRACTED, GEAR UNSAFE LIGHT WAS ILLUMINATED. RECYCLED GEAR WITH SAME RESULTS. PERFORMED GEAR UPLATCH CHECK AND LEFT AND RIGHT MAIN GEAR AND DOORS, 'NOT LATCHED' LIGHT WAS ILLUMINATED. REPLACED SYSTEM SELECTOR VALVE FOR BYPASSING. OPS CHECKED NORMAL IAW DC8 MM 32-36-00.

Part: RIB — CRACKED (NR 4 PYLON)

NR 4 PYLON UPPER RIB HAD CRACK AT END. REPAIRED IAW DC8 SRM.

Part: MFD — MALFUNCTION (COCKPIT)

FAINT BURNING ODOR WAS REPORTED BY CREW DURING FLIGHT AND ON GROUND. PROBLEM WAS DETERMINED TO BE MULTI-FUNCTION DISPLAY (MFD). REPLACED DISPLAY UNIT IAW DC8 MM 34-20, OPS CHECKED GOOD.

Part: FILTER — DEFECTIVE (NR 2 ENGINE)

DURING DESCENT WITH THROTTLE AT IDLE, NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED WITH AN OIL PRESSURE READING OF 25 PSI. SECURED NR 2 ENGINE. WINDMILLING OIL PRESS 7 PSI, N2-23 PERCENT, N1-14 PERCENT, EGT-70 DEG, AND EPR-1.00. REPLACED MAIN OIL FILTER AND OIL PRESSURE RELIEF VALVE. CHECKED BREATHER PRESSURE IAW PRATT AND WHITNEY MANUAL 72-00 AND JT3D OHM 72-00. OPS AND LEAK CHECKED GOOD.

Part: CONNECTOR — DIRTY (MLG)

AFTER UPLATCH CHECK, UNSAFE GEAR LIGHT CAME ON. RECYCLED GEAR. SUBSEQUENT UPLATCH CHECK WAS GOOD. GEAR WELL AREA WAS FOUND TO BE SATURATED WITH DE-ICE FLUID. CLEANED FLUID FROM CONNECTORS. NO DEFECTS NOTED.

Part: SKIN — EXCESSIVE GAP (NR 3 PYLON)

DURING PREFLIGHT, FOUND EXCESSIVE GAP AT LEADING EDGE OF NR 3 PYLON. INSTALLED SEAL AND STAINLESS STEEL STRIP IAW ABX REA D854-20655.

Part: FITTING — CRACKED (BS 280)

FORWARD LOWER CARGO COMPARTMENT RIGHT SIDE FS 280 LONGERON 21R AT CROSS SLIDE DOOR CUTOUT, FORWARD UPPER CORNER FRAME TO FLOOR SUPPORT FITTING IS CRACKED. REPAIRED CRACKED FLOOR SUPPORT FITTING IAW DAC DWG 97540022 AND DC-8 SRM 51-1-24.

Part: ANGLE — CRACKED (NR 3 PYLON)

NR 3 PYLON LOWER FORWARD SUPPORT ANGLE AT TOMBESTONE IS CRACKED AT OUTBOARD FASTENER. INSTALLED NEW ANGLE IAW DC-8 SRM 51-3-0 AND DAC DWG NR 9753018.

Part: LONGERON — CRACKED (FUSELAGE)

LONGERON 24, RT HAS AN 8 INCH CRACK, EMANATING FROM BOTTLE BOLT AT 6 O'CLOCK POSITION. *S/D* REPAIRED IAW DC8 SRM 53-2-2 AND 51-1-20.

Part: PANEL — CRACKED (LT WING)

LT WING PANEL 505F HAS 12 CRACKS AT FASTENER HOLES. *S/D* REPAIRED IAW ABX REA D857-19869MR AND DC 8 SRM 51-1-8.

Part: BRAKE VALVE — DEFECTIVE (LT MLG)

DURING TAXI THE LEFT MAIN LANDING GEAR BRAKES HAD NO EFFECT IN STOPPING THE AIRCRAFT. REPLACED INBOARD BRAKE CONTROL VALVE, PERFORMED PRESSURE CHECK AND ADJUSTMENT OF BRAKE CONTROL VALVE, OPS CHECKED GOOD AND NO LEAKS NOTED IAW DC-8 MM.

Part: CONNECTOR — DIRTY (NR 2 ENGINE)

NR 2 ENGINE LOW OIL PRESSURE LIGHT CAME ON, OIL PRESSURE 50 PSI. RETARDED THROTTLE TO IDLE, LIGHT STAYED ON. SHUT DOWN ENGINE AT 1210 Z. WINDMILLED WITH 34 PSI OIL PRESSURE, 34 PERCENT N-1, 38 PERCENT N-2. VERIFIED LOW OIL PRESSURE LIGHT ON WITH OIL PRESSURE SWITCH DISCONNECTED AND OIL PRESSURE DIFFERENTIAL SWITCH DISCONNECTED. FOUND WATER AND DIRT IN CANNON PLUG P1-815, NR 2 ENGINE TO PYLON DISCONNECT. CLEANED AND RE-SET PLUG. LIGHT EXTINGUISHED. RESET PRESSURE SWITCHES, CANNON PLUGS. GROUND RAN ENGINE. LOW PRESSURE LIGHT EXTINGUISHED. SYSTEM OPS CHECKED GOOD IAW DC-8 MM 79-32-00.

Part: BATTERY RACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS WEAK. REPLACED EMERGENCY LIGHT BATTERY RACK IAW DC-8 MM 33-50-1, OPS CHECKED GOOD.

Part: POWER SUPPLY — DEFECTIVE (CABIN)

EMERGENCY LIGHTING TEST FAILED. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY IAW DC8 M.M. 33-50-2. OPS CHECK GOOD.

Part: BATTERY RACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS EXTINGUISHED AFTER APPROXIMATELY 3 SECONDS OF OPERATION. REPLACED EMERGENCY LIGHT BATTERY RACK ASSEMBLY IAW DC8 MM, OPS CHECK OF EMERGENCY LIGHTING SYSTEM WAS GOOD.

Part: FRAME — CRACKED (BS 1260)

DURING 826AX MOD, DISCOVERED FRAME CRACKED AT STATION 1260 BETWEEN LONGERON 4 RIGHT AND LONGERON 5 RIGHT. REPAIRED FRAME AT FUSELAGE STATION 1260, LONGERON 4 RIGHT AND LONGERON 5 RIGHT IAW ABX REA D853-12675MR.

Part: DOOR JAMB — MISDRILLED (BS 70-80)

DURING MODIFICATION, DISCOVERED L-1 DOOR JAM AFT TORQUE BOX COVER HAS TORN HOLES, DOUBLE DRILLED HOLES AND HOLES IN RADIUS. REPAIRED FORWARD ENTRANCE DOOR JAMB STRUCTURE AT FUSELAGE STATION 70 TO 80 IAW ABX REA D853-12671MR.

Part: SUPPORT — CORRODED (BS 140)

DURING MODIFICATION, DISCOVERED FLOOR BEAM AT VERTICAL SUPPORT FRAME AT FUSELAGE STATION 140, LONGERON 27R WAS CORRODED AT SEVERAL LOCATIONS. REPAIRED FLOOR BEAM SUPPORT AT FUSELAGE STATION 140 IAW ABX REA D853-12609MR.

Part: FLOOR BEAM — CRACKED (BS 1320)

DURING 826AX MOD, DISCOVERED CABIN FLOOR PANEL SUPPORT FRAME CRACKED AND DENTED AT STATION 1320, 30 RIGHT FROM CENTERLINE ABOVE LONGERON 29R AFT CARGO PIT. REPAIRED FUSELAGE STATION 1320 FLOOR BEAM AT RBL 30 THAT WAS CRACKED IAW ABX REA D853-12676MR.

Part: SKIN — DENTED (NR 3 PYLON)

DURING 826AX MOD, DISCOVERED A DENT AT NR 3 ENGINE PYLON, STATION YN 141.00, PYLON LOWER SURFACE. REPAIRED NR 3 ENGINE PYLON THAT WAS DENTED ON THE LOWER SURFACE AT STATION YN 141.00 IAW ABX REA D854-12587MR.

Part: SKIN — CORRODED (WS 451)

DURING 826AX MOD, DISCOVERED LEFT HAND UPPER WING AT NR 1 ENGINE BETWEEN FRONT AND MID SPAR SKIN REPAIR HAS CORRODED FASTENERS AND CORROSION BETWEEN REPAIR AND SKIN. REPAIRED LEFT HAND WING TOP PANEL PLATING THAT WAS CORRODED AT STATION XW 451 IAW ABX REA D857-12592MR.

Part: SKIN — CORRODED (BS 1050-1150)

DURING 826AX MOD, DISCOVERED BELLY SKIN AT STATION 1050 TO 1150 HAS BARE METAL AND CORROSION ON ENTIRE UNDERSIDE OF SKIN. REPAIRED CORRODED BELLY SKIN AT FUSELAGE STATION 1050 TO 1150, LONGERON 33L AND 33R IAW ABX REA D853-12613MR.

Part: DOOR JAMB — CRACKED (BS 120)

DURING 826AX MOD, DISCOVERED STATION 120 FOWARD SIDE OF MAIN CARGO DOOR SEAL RETAINER CRACKED AND BENT IN SEVERAL PLACES. REPAIRED MAIN CARGO DOOR FORWARD JAMB STRUCTURE AND WEB THAT WAS CRACKED AND BENT IN SEVERAL PLACES IAW ABX REA D853-12597MR.

Part: DOOR JAMB — MISDRILLED (BS 240-280)

DURING 826AX MOD, DISCOVERED MAIN CARGO DOOR, UPPER AFT TORQUE BOX WEB GOUGED WITH NUMEROUS MISDRILLED HOLES AT STATION 240 T0 280. REPAIRED MAIN CARGO DOOR AFT UPPER JAMB WEB AND PAN THAT WAS GOUGED WITH NUMEROUS MISDRILLED HOLES AT STATION 240 TO 280 IAW ABX REA D853-12593.

Part: DOOR JAMB — MISDRILLED (BS 280)

DURING 826AX MOD, DISCOVERED MAIN CARGO DOOR, AFT SIDE TORQUE BOX WEB AT STATION 280 THAT HAD NUMEROUS DRILL MARKS AND MISDRILLED HOLES. REPAIRED MAIN CARGO DOOR AFT JAMB STRUCTURE AND WEB AT STATION 280 THAT HAD NUMEROUS MISDRILLED HOLES IAW ABX REA D853-12582MR.

Part: FRAME — CORRODED (BS 70)

DURING 826AX MOD, DISCOVERED PRODUCTION SPLICE FRAME AT STATION 70 FORWARD SIDE CORRODED. ALSO, LONGERON END FITTING AT LONGERON 32R CORRODED. REPAIRED FUSELAGE STATION 70 LOWER FORWARD FRAME AND END FITTING IAW ABX REA D853-12580MR.

Part: DOOR FRAME — DENTED (R 1 DOOR)

DURING 826AX MOD, DISCOVERED R-1 DOOR JAMB LOWER AFT CORNER, ANGLE CORRODED AND FRAME AND COVER DENTED. REPAIRED FRAME AT FUSELAGE STATION 200 RIGHT AT FLOOR LEVEL THAT WAS CORRODED AND COVER DENTED IAW ABX REA D853-12568MR.

Part: RIB — CRACKED (LT AILERON)

DURING 826AX MOD, DISCOVERED LEFT HAND INBOARD AILERON, LIGHTING HOLE COVER, FRAME AND BULKHEAD WORN, CRACKED AND BROKEN. REPAIRED END RIB, LEFT HAND INBOARD AILERON, LIGHTING HOLE COVER THAT WAS WORN, CRACKED AND BROKEN IAW ABX REA D857-12485.

Part: FRAME — MISDRILLED (FUSELAGE)

DURING 826AX MOD, DISCOVERED FROM STATION 25 TO AFT PRESSURE BULKHEAD FRAMES GREATER THAN .100 INCH THICKNESS, HAVE NUMEROUS MISDRILLED HOLES. REPAIRED FUSELAGE FRAMES .080TO .125 INCH THICK THAT WERE MISDRILLED IAW ABX REA D853-12547MR.

Part: SUPPORT BEAM — CORRODED (BS 180)

DURING 826AX MOD, DISCOVERED THE FLOOR BEAM VERTICAL SUPPORT AT FUSELAGE STATION 180, 50 INCHES INBOARD OF CENTER LINE HAS CORROSION WHERE GILLINER SUPPORT ANGLE ATTACHES. REPAIRED THE FLOOR BEAM VERTICAL SUPPORT BEAM AT STATION 180 THAT WAS CORRODED IAW ABX REA D853-12608MR.

Part: ATTACH CHANNEL — CRACKED (NR 2 ENGINE)

DURING 826AX MOD, DISCOVERED NR 2 ENGINE RIGHT HAND AFT TRANSITION ATTACHMENT ASSEMBLY DUCT STRIP IS CRACKED ON BOTH ENDS. REPAIRED NR 2 ENGINE RIGHT HAND AFT TRANSITION BI-DUCT ATTACH CHANNEL IAW ABX REA D878-12614MR.

Part: SKIN — DAMAGED (BS 340)

DURING 826AX MOD, DISCOVERED STATION 340 LONGERON 17R, BOTH WINDOW CUTOUTS HAVE QUESTIONABLE REPAIRS. REPAIRED WINDOW CUTOUTS AT FUSELAGE STATION 340, LONGERON 17R IAW ABX REA D853-12604.

Part: DOOR JAMB — GOUGED (BS 160-180)

DURING 826AX MOD, DISCOVERED MAIN CARGO DOOR, STATION 160 TO 180, UPPER TORQUE BOX WEB REPAIR DOUBLER GOUGED. REPAIRED MAIN CARGO DOOR UPPER JAMB WEB DOUBLER AT STATION 160 IAW ABX REA D853-12590MR.

Part: SKIN — CRACKED (BS 1746-1766)

DURING 826AX MOD, DISCOVERED SKIN BULGING AND CRACKS AROUND RIVET HEADS AT LONGERON 28L, STATION 1746 TO 1766. REPAIRED FUSELAGE SKIN IAW ABX REA D853-12584MR.

Part: SKIN — CRACKED (BS 1400)

DURING 826AX MOD, DISCOVERED AT STATION 1400, LONGERON 29R TO 33R, C-4 DOOR CUTOUT HAS CRACKS. REPAIRED LOWER FUSELAGE EXTERIOR SKIN AT C-4 DOOR, STATION 1400, LONGERON 29R TO 33R IAW ABX REA D853-12449MR.

Part: LONGERONS — CRACKED (BS 130-270)

DURING 826AX MOD, DISCOVERED STATION 130 TO 270, LONGERON 16L TO 23L MAIN CARGO DOOR CUTOUT BOTTOM SECTION FUSELAGE SKIN HAS CRACKS, GOUGED, DENTS AND QUESTIONABLE REPAIRS. REPAIRED MAIN CARGO DOOR AT STATION 130 TO 270, LONGERON 16L TO 23L, BOTTOM SECTION OF FUSELAGE SKIN THAT WAS CRACKED, GOUGED AND DENTED IAW ABX REA D853-12483MR.

Part: LONGERON — CORRODED (BS 1070-1085)

DURING 826AX MOD, DISCOVERED LONGERON 27L WAS CORRODED AT STATION 1070 TO 1085 AT AFT CARGO PIT. REPAIRED CORRODED LONGERON 27L AT STATION 1070 TO 1085 IAW ABX REA D853-12471MR.

Part: BARRIER DOOR — CRACKED (AFT PIT)

DURING 826AX MOD, DISCOVERED THAT THE AFT ACCESSORY COMPARTMENT DOOR WAS CRACKED AT BOTH LEFT HAND AND RIGHT HAND SIDES. REPAIRED AFT LOWER PIT, AFT BARRIER COMPARTMENT DOOR THAT WAS CRACKED ON BOTH LEFT HAND AND RIGHT HAND SIDES IAW ABX REA D853-12475MR.

Part: FRAME — CRACKED (FUSELAGE)

DURING 826AX MOD, DISCOVERED STATION 1580 AT APPROXIMATELY LONGERON 8L, FROM STATION 25 TO AFT PRESSURE BULKHEAD, STATION 1580 AT CUSP AREA FRAMES OF .100 INCH THICKNESS OR LESS, HAVE NUMEROUS DRILLED HOLES, FRAME END IS CRACKED AND CORRODED. REPAIRED FUSELAGE FRAMES LESS THAN .080 INCH THICK AT STATIONS 25 TO AFT PRESSURE BULKHEAD, STATION 1580 AT CUSP AREA, AND STATION 1580, LONGERON 8L, IAW ABX REA D853-12348MR.

Part: SKIN — GOUGED (BS 340)

DURING 826AX MOD, DISCOVERED STATION 340, LONGERON 31R, LONGERON 24R-25R, LONGERON 27R FUSELAGE SKIN, STATION 180 LONGEON 25R C1 DOOR AFT BOTTOM CUTOUT HAS GOUGE. REPAIRED FUSELAGE SKIN AT STATION 340, LONGERON 31R, LONGERON 24R-25R, LONGERON 27R AND STATION 180, LONGERON 25R IAW ABX REA D853-12441MR.

Part: HINGE FITTING — CHAFED (LT TE FLAP)

DURING 826AX MOD, DISCOVERED LEFT HAND INBOARD FLAP INBOARD HINGE ARM CHAFED. REPAIRED HINGE FITTING ON INBOARD FLAP, INBOARD HINGE THAT WAS CHAFED IAW ABX REA D857-12329MR.

Part: FRAME — CORRODED (BS 460)

DURING 826AX MOD, DISCOVERED FRAME SECTION, GUSSET PLATE AND VERTICAL FLOOR SUPPORT FRAME AT STATION 460 BETWEEN LONGERON 27R AND LONGERON 25R HAS AREAS ON CORROSION. REPAIRED FUSELAGE STATION 460 FRAME SECTION, GUSSET PLATE AND VERTICAL FLOOR SUPPORT FRAME AT LONGERON 26R THAT HAS AREAS OF CORROSION IAW ABX REA D853-12361MR.

Part: THRESHOLD — CORRODED (FWD ENTRY DOOR)

DURING 826AX MOD, DISCOVERED LEFT FWD ENTRY DOOR THRESHOLD AREA HAS CORRODED FASTENERS AND DOUBLE DRILLED HOLES. REPAIRED LEFT FORWARD ENTRY DOOR THRESHOLD/SILL THAT WAS CORRODED AND HAD DOUBLE DRILLED HOLES IAW ABX REA D853-12484MR.

Part: BLKHD STIFFENER — CRACKED (BS 1766)

DURING 826AX MOD-DISCOVERED CRACK ON CENTER STIFFENER AT STATION 1766. REPAIRED HORIZONTAL STIFFENER AT AFT PRESSURE BULKHEAD IAW ABX REA D853-12702MR.

Part: FRAME — MISDRILLED HOLES (BS 702)

DURING 826AX MOD-DISCOVERED STATION 702, LONGERON 1-21 RIGHT FRAME HAS NUMEROUS DRILLED HOLES AND CORROSION. REPAIRED FUSELAGE STATION 702, LONGERONS 1-21 RIGHT FRAMES THAT HAD NUMEROUS MISDRILLED HOLES AND CORROSION.

Part: FRAME — CRACKED (BS 1700)

DURING 826AX MOD-DISCOVERED FRAME REPAIR AT STATION 1700, LONGERON 16R TO LONGERON 21R NOT PER SRM, WRONG HARDWARE, AND EDGE DISTANCE, ALSO, CORROSION AND BARE METAL IN UPPER CARGO AREA. REPAIRED FUSELAGE FRAME AT STATION 1700, LONGERON 21 RIGHT IAW ABX REA D853-12696MR.

Part: DOUBLER — CRACKED (WS 527)

DURING 826AX MOD-DISCOVERED RIGHT WING LEADING EDGE INTERIOR DOUBLER CRACKED AT STATION 527, OUTBOARD END OF CENTER LEADING EDGE SECTION. REPAIRED INTERNAL DOUBLER ON RIGHT WING LEADING EDGE AT STATION XRS 527 IAW ABX REA D853-12692MR.

Part: CUSP — GOUGED (BS 1050)

DURING 826AX MOD-DISCOVERED CUSP AT STATION 1050 LEFT SIDE HAS A DEEP MACHINE GOUGE. REPAIRED CUSP AT FUSELAGE STATION 1050 LEFT SIDE THAT WAS GOUGED IAW ABX REA D853-12141MR.

Part: FRAME — MISDRILLED (BS 1060/1100)

DURING 826AX MOD-DISCOVERED STATION 1060 AND 1100 FRAME AT CUSP HAS DOUBLE DRILLED HOLES, ALSO, FRAME END FITTING HAS CORROSION. REPAIRED FUSELAGE FRAMES AT STATION 1060 AND 1100 THAT WERE MISDRILLED IAW ABX REA D853-12715MR.

Part: WINDOW CUTOUT — ILLEGAL REPAIR (BS 940)

DURING 826AX MOD-DISCOVERED AT STATION 940 RIGHT, WINDOW CUT-OUT HAS QUESTIONABLE REPAIR. REPAIRED WINDOW CUT-OUT AT FUSELAGE STATION 940 RIGHT IAW ABX REA D853-12603MR.

Part: SEAT TRACKS — CORRODED (CABIN)

DURING 826AX MOD-DISCOVERED SEAT TRACK ROW 'F', STATION 857 ROW 'B', STATION 420, STATION 500, ROW 'C', STATIONS 1470-1490, ROW 'F', STATION 950 AND STATIONS 990-1300 HAVE CORROSION, ARE CHAFED, AND HAVE WORN SCALLOPS. FABRICATED DUAL SEAT TRACKS AT NUMEROUS ROWS AND STATIONS IAW ABX REA D853-12705MR.

Part: FRAMES — MISDRILLED (BS 600-660)

DURING 826AX MOD-DISCOVERED CIRCUMFERENTIAL FRAMES FROM STATIONS 600 TO 680, FROM CUSP TO LONGERON 1-21 LEFT/RIGHT HAVE SEVERAL MIS-DRILLED HOLES AND FASTENERS WITH DRILLED OFF HEADS. REPAIRED FUSELAGE FRAMES AT STATIONS 600-660, LONGERONS 1-21 LEFT/RIGHT IAW ABX REA D853-12694MR.

Part: SEAT TRACKS — WORN (CABIN)

DURING 826AX MOD-DISCOVERED MAIN CABIN SEAT TRACK ROW 'F', STATIONS 1590-1630, STATION 270, AND STATIONS 1540-1580, ROW 'B', STATIONS 1470-1500, AND AT STATIONS 45-70, SCALLOPS WORN, NICKS, GOUGES, BULDGE AREAS AROUND FASTENERS. FABRICATED TRIPLE SEAT TRACK AT VARIOUS ROWS AND STATIONS IAW ABX REA D853-12706MR.

Part: ANGLE — CRACKED (WS 207.5)

DURING 826AX MOD-DISCOVERED LEFT WING STATION 207.500 INBOARD OF STUB WING ANGLE AND NR 3 LEADING EDGE SLAT INBOARD INTERIOR END CRACKED. REPAIRED FORMER ATTACH ANGLE, PYLON STUB WING AT STATION 207.500 IAW ABX REA D857-12693MR.

Part: PRESSURE PANEL — CORRODED (BS 920-940)

DURING 826AX MOD-DISCOVERED STATIONS 920-940 AREA BELOW CENTER FLOOR TRACK HAS CORROSION. REPAIRED PRESSURE PANEL AT XCW 0.0, FUSELAGE STATIONS 920-940 IAW ABX REA D853-12711MR.

Part: FRAME — MISDRILLED (BS 742)

DURING 826AX MOD-DISCOVERED STATION 742, LONGERON 1-21 RIGHT AND LONGERON 21 LEFT, HAVE DRILLED HOLES AND CORROSION ON FRAMES. REPAIRED FUSELAGE FRAMES AT STATION 742 IAW ABX REA D853-12707MR.

Part: DOUBLER — CORRODED (BS 1050-1350)

DURING 826AX MOD-DISCOVERED INTERNAL DOUBLER AT STATIONS 1120 TO 1260 HAVE BARE METAL AND CORROSION, ALSO A CUT-OUT AREA OF PREVIOUS REPAIR AT STATION 1170. REPAIRED INTERNAL DOUBLER AT FUSELAGE STATIONS 1050-1350 THAT WAS CORRODED IAW ABX REA D853-12704MR.

Part: FRAME — CORRODED (BS 1700)

DURING 826AX MOD-DISCOVERED FRAME AND GUSSET CRACKED AND CORRODED AT STATION 1700 AT LONGERON 21L. REPAIRED CRACKED AND CORRODED FRAMES AND GUSSETS AT LONGERON 21L, STATION 1700 IAW ABX REA D853-12697MR.

Part: FRAME — MISDRILLED (FS 680)

DURING 826AX MOD, DISCOVERED STATION 680 LONGERON 1 TO 21 LEFT, STATION 600 TO 680 FROM CUSP TO LONGERON 5R HAVE DRILLED HOLES, CORROSION AND FASTENERS WITH DRILLED OFF HEADS. REPAIRED FUSELAGE STATION 680 FRAME IAW ABX REA D853-12695MR.

Part: FRAME — ELONGATED HOLE (BS 1040)

DURING 826AX MOD-DISCOVERED THAT STATION 1040 HAS OBLONG HOLE, ABOVE LONGERON 29R AFT CARGO PIT. REPAIRED FUSELAGE FRAME 1040 AT LONGERON 29R IAW ABX REA D853-12678MR.

Part: SKIN — CORRODED (BS 1440-1460)

DURING 826AX MOD, DISCOVERED SKIN CORRODED ON INNER SURFACE BETWEEN LONGERON 31 RIGHT AND 29 RIGHT AT STATION 1440 TO 1460. REPAIRED UPPER FUSELAGE SKIN AT C-4 DOOR THAT WAS CORRODED ON INNER SURFACE IAW ABX REA D853-12672MR.

Part: WEB — CORRODED (BS 834-857)

DURING 826AX MOD, DISCOVERED CORROSION ON STATION 857 AT LOWER SPAR CAP RIGHT WHEEL WELL FORWARD BULKHEAD AND BL 0 ATTACH ANGLE CORRODED UNDER KEEL WEB. REPAIRED WEB AND TEE AT BL 0, STATION 834 TO 857 THAT WERE CORRODED IAW ABX REA D853-12674MR.

Part: FRAME — DAMAGED (BS 260)

DURING 826AX MOD-DISCOVERED STATION 260 FRAME FROM LONGERON 30 LEFT TO LONGERON 35 LEFT FRAME HAS PREVIOUS REPAIR NOT PER SRM. REPAIRED FUSELAGE FRAME AT STATION 260 BETWEEN LONGERON 30 LEFT TO LONGERON 35 LEFT IAW ABX REA D853-12698MR.

Part: TIP CAP — DENTED (LT ELEVATOR)

DURING 826AX MOD, DISCOVERED LEFT HAND ELEVATOR OUTBOARD TIP CAP DENTED. REPAIRED LEFT HAND ELEVATOR OUTBOARD TIP CAP THAT WAS DENTED IAW ABX REA D853-12346MR.

Part: FRAME — BENT (BS 1613)

DURING 826AX MOD, DISCOVERED L-2 DOOR JAMB LOWER TORQUE BOX FRAME IS BENT AT FUSELAGE STATION 1613. REPAIRED FUSELAGE STATION 1613 FRAME ON L-2 DOOR THAT WAS BENT IAW ABX REA D853-12374MR.

Part: DOOR JAMB — BENT (BS 1620)

DURING 826AX MOD, DISCOVERED R-2 DOOR JAMB LOWER FOWARD CORNER AT FUSELAGE STATION 1620, STRUCTURE IS BENT. REPAIRED R-2 DOOR JAMB FORWARD CORNER FRAME AT FUSELAGE STATION 1620 THAT WAS BENT IAW ABX REA D853-12345MR.

Part: SKIN — MISREPAIRED (BS 360)

DURING 826AX MOD, DISCOVERED STATION 360, LONGERON 27R-29R, BOTH REPAIRS HAVE NO FINGER DOUBLERS. REPAIRED FUSELAGE SKIN AT FUSELAGE STATION 360, LONGERON 27R-29R, THAT HAD NO FINGER DOUBLERS IAW ABX REA D853-12442MR.

Part: SKIN — CRACKED (NR 3 ENGINE)

DURING 826AX MOD-DISCOVERED NR 3 ENGINE THRUST REVERSER INBOARD SKIN CRACKED AT YN 232. REPAIRED NR 3 THRUST REVERSER INNER SKIN AND FRAME THAT WAS CRACKED AT YN 232 IAW ABX REA D878-12841MR.

Part: TEE DOUBLER — CRACKED (NR 1 PYLON)

DURING 826AX MOD, DISCOVERED NR 1 PYLON TEE DOUBLER LEAKS FUEL. REPAIRED NR 1 TEE DOUBLER THAT WAS CRACKED IAW ABX REA D854-13070MR.

Part: LONGERON — CORRODED (BS 1020)

DURING 826AX MOD, DISCOVERED FUSELAGE FRAME 1020 CORRODED ON UPPER FLANGE BETWEEN LONGERON 28L AND 29L. REPAIRED CORRODED FUSELAGE STATION 1020 FRAME AT LONGERON 28L, UPPER FRAME IAW ABX REA D853-13068MR.

Part: LONGERON — CORRODED (BS 1580)

DURING 826AX MOD, DISCOVERED THE LONGERON 1 AT STATION 1615 CORRODED. REPAIRED CORRODED LONGERON 1 AT STATION 1615 IAW ABX REA D853-13069MR.

Part: SEAT TRACKS — CORRODED (CABIN)

DURING 826AX MOD-DISCOVERED SEAT TRACK ROW 'B' AT STATION 270, MAIN CABIN SEAT TRACK 'F', STATIONS 1590-1630 AND MAIN CABIN SEAT TRACK 'B', STATIONS 1470-1500 CORRODED AND SCALLOPS WORN. FABRICATED TRIPLE SEAT TRACKS FOR STATIONS 270, 1590-1630, AND 1470-1500 THAT WERE CORRODED AND HAD WORN SCALLOPS IAW ABX REA D853-12706MR.

Part: LONGERONS — DOUBLE DRILLED (BS 160/280/1320)

DURING 826AX MOD-DISCOVERED FRAME AT STATION 160, LONGERON 6-9R, STATION 280, LONGERON 7-10R AND STATION 1320, LONGERON 7-10L IS DOUBLE DRILLED. REPAIRED FUSELAGE FRAMES WITH DOUBLE DRILLED HOLES AT STATION 160, LONGERON 6-9R, STATION 280, LONGERON 7-10R AND STATION 1320, LONGERON 7-10 IAW ABX REA D853-12862MR.

Part: FLOORBEAM — CORRODED (BS 55)

DURING 826AX MOD-DISCOVERED MAIN CABIN FLOORBEAMS, ATTACH FITTINGS, GUSSETS AND BRACKETS HAVE CORROSION FROM BL ZERO TO RIGHT CUSP BS 55.000 IN MAIN CABIN. REPAIRED FUSELAGE STATION 55.000 FLOORBEAM THAT HAD AREAS OF CORROSION IN THE MAIN CABIN IAW ABX REA D853-12718MR.

Part: FITTING — CRACKED (BS 759)

DURING 826AX MOD-DISCOVERED STATION 759, LONGERON 22L, FRAME END FITTING HAS CRACKED. REPAIRED FUSELAGE STATION 759 FRAME END FITTING THAT WAS CRACKED IAW ABX REA D853-12851MR.

Part: SKIN — CRACKED (RT AILERON)

DURING 826AX MOD-DISCOVERED RIGHT OUTBOARD AILERON SKIN AND DOUBLER CRACKED. REPAIRED RIGHT OUTBOARD AILERON NOSE SKIN AND DOUBLER CRACK IAW ABX REA D857-12844MR.

Part: SKIN — CORRODED (CTR WING)

DURING 826AX MOD-DISCOVERED STATION 857, RBL 46 HAS PREVIOUS GRIND-OUT FROM CORROSION REMOVAL, APPROXIMATELY 4 INCHES BY 6 INCHES. REPAIRED CENTER WING, UPPER SKIN AT AFT SPAR RBL 46.000 THAT HAD A PREVIOUS GRIND OUT IAW ABX REA D857-12854MR.

Part: FLOOR BEAM — CORRODED (BS 824)

DURING 826AX MOD-DISCOVERED FLOOR BEAM AT STATION 824 AT APPROXIMATELY RBL 36 CORRODED. REPAIRED CORRODED FLOOR BEAM AT STATION 822 AT RBL 36 IAW ABX REA D853-13076MR.

Part: SKIN — CRACKED (WS 257 LE)

DURING 826AX MOD, DISCOVERED THE CENTER LEADING EDGE SKIN CRACKED BETWEEN ATTACH HOLES ON INBOARD END LEADING AREA. REPAIRED LEFT HAND WING CENTER CRACKED LEADING EDGE AT STATION XW=257 IAW ABX REA D857-13077MR.

Part: SKIN — CRACKED (BS 980)

DURING 826AX MOD-DISCOVERED CORROSION ON SKIN AND FITTING CRACKED OVER LONGERON 24 IN THE LEFT WHEELWELL AT STATION 980. REPAIRED FUSELAGE STATION 980 FITTING AND SKIN THAT WAS CRACKED IN THE LEFT WHEELWELL IAW ABX REA D853-12861MR.

Part: LONGERON — CORRODED (BS 360-420)

DURING 826AX MOD-DISCOVERED LONGERON 27L, FUSELAGE STATIONS 360-420 HAVE SEVERAL SPOTS OF CORROSION. REPAIRED LONGERON 27L UPPER FLANGE AT FUSELAGE STATION 360 J-420 THAT WAS CORRODED IAW ABX REA D853-12871MR.

Part: SKIN — IMPROPER REPAIR (BS 1160-1180)

DURING 826AX MOD-DISCOVERED STATIONS 1160-1180, LONGERONS 32R-34R, FUSELAGE SKIN HAS A 5.5 INCH BY 3.5 INCH CUT-OUT FROM PREVIOUS REPAIR. REPAIRED STATIONS 1160-1180 FUSELAGE SKIN AND TITANIUM DOUBLER CUT-OUT AT THE AFT LOWER CARGO COMPARTMENT FORWARD DOOR AREA IAW ABX REA D853-12875MR.

Part: BLIND HUCK — IMPROPER INSTL (BS 851)

DURING 826AX MOD-DISCOVERED RBL 42, STATION 851 BLIND HUCK IMPROPERLY PULLED. REPAIRED CENTER WING , AFT STRINGER RBL 40.00, BLIND HUCK THAT WAS IMPROPERLY PULLED IAW ABX REA D857-13071MR.

Part: FRAME — CORRODED (BS 1400)

DURING 826AX MOD-DISCOVERED CORROSION ON FRAME AT STATION 1400, LONGERON 31L TO LONGERON 33R AT AFT CARGO. REPAIRED CORRODED FRAME SPLICE AT FUSELAGE STATION 1400 IAW ABX REA D853-12854MR.

Part: SKIN — DAMAGED (BS 1055)

DURING 826AX MOD-DISCOVERED BLEND-OUT IN BELLY SKIN AT STATION 1055, BETWEEN LONGERON 34L-35L. REPAIRED EXTERIOR BELLY SKIN THAT WAS DAMAGED AT FUSELAGE STATION 1050, LONGERON 34L-35L IAW ABX REA D853-12838MR.

Part: FLOORBEAM — CORRODED (BS 834)

DURING 826AX MOD-DISCOVERED FLOORBEAM AT STATION 834, LEFT, CORRODED THROUGH AND AROUND 'B' NUT. REPAIRED FUSELAGE STATION 834 FLOORBEAM THAT WAS CORRODED IAW ABX REA D853-12853MR.

Part: FRAME — CORRODED (BS 702)

DURING 826AX MOD, FOUND NUMEROUS DRILLED HOLES AND CORROSION IN STATION 702 L1-L21R FRAME. REPAIRED STATION 702 L1-21R FRAME IAW ABX REA D853-12703MR.

Part: LONGERON — CORRODED (FS 1080)

DURING 826AX MOD, FOUND LONGERON L27L CORRODED AT FS 1080 IN THE AFT CARGO PIT. REPAIRED LONGERON L27L AT FS 1080 IAW ABX REA D853-12471MR.

Part: TIP CAP — DENTED (LT ELEVATOR)

DURING 826AX MOD, FOUND DENT IN LEFT HAND ELEVATOR OUTBOARD TIP CAP. REPAIRED LEFT HAND ELEVATOR OUTBOARD TIP CAP IAW ABX REA D855-12346MR.

Part: DOOR JAMB — MISDRILLED (CARGO DOOR)

DURING 826AX MOD, FOUND NUMEROUS DRILL MARKS AND MISDRILLED HOLES ON MAIN CARGO DOOR AFT SIDE TORQUE BOX WEB STA 280. REPAIRED MAIN CARGO DOOR AFT JAMB STRUCTURE AND WEB IAW ABX REA D853-12582MR.

Part: FLOOR BEAM — CORRODED (FS 180)

DURING 826AX MOD, FOUND FLOOR BEAM SUPPORT LEG AT FS 180 CORRODED. REPAIRED FLOOR BEAM SUPPORT AT FS 180 IAW ABX REA D853-12608MR.

Part: HINGE — CHAFED (LT TE FLAP)

DURING 826AX MOD, FOUND LEFT HAND INBOARD FLAP, INBOARD HINGE ARM CHAFED. REPAIRED INBOARD FLAP INBOARD HINGE IAW ABX REA D857-12329MR.

Part: SILL — CORRODED (PAX DOOR)

DURING 826AX MOD, FOUND LEFT FORWARD ENTRY DOOR THRESHOLD AREA HAS CORRODED FASTENERS AND DOUBLER DRILLED HOLES. REPAIRED LEFT FORWARD ENTRY DOOR SILL IAW ABX REA D853-12484MR.