N825AX

Part: STRAP — CORRODED (BS 902) · airframe 72,113 hrs · 26,576 cycles

CORROSION ON ANGLE STRAP ON TOP OF MAIN LANDING GEAR WHEEL WELL BOX FORWARD OF FLOORBEAM STA 902, LEFT BUTT LINE 65. REMOVED CORROSION IAW DC8 SRM 51-1-8. DETERMINED TO BE OUT OF ACCEPTABLE LIMITS IAW DC8 SRM 53-2-0. REMOVED AND REPLACED WITH NEW FABRICATED ANGLE IAW DC8 SRM 51-1-21.

Part: CABIN PRESSURE — UNKNOWN · airframe 72,091 hrs · 26,555 cycles

DURING CLIMB AT FL310, CABIN RATE OF CLIMB WENT FROM 500 FPM TO 6,000 FPM. COULD NOT STOP THE CABIN FROM CLIMBING USING AUTO OR MANUAL LEVER. CABIN WENT TO 11,000 FT. DONNED OXYGEN AND STARTED DESCENT. AT ABOUT FL290, REGAINED CONTROL OF BOTH AUTO AND MANUAL PRESSURIZATION. LUBRICATED PRESSURIZATION OUTFLOW VALVE AND SCOOP AS REQUIRED. INSPECTED CABIN PRESSURE SAFETY VALVES AND NO DEFECTS NOTED. PRESSURIZED AIRCRAFT IAW DC8 MM. OPS CHECKED GOOD.

Part: TRANSMITTER — DEFECTIVE (OIL PRESS INDICA) · airframe 71,976 hrs · 26,442 cycles

NR 3 ENGINE OIL PRESSURE PEGGED OFF SCALE HIGH. ENGINE WAS SECURED AND FLIGHT CONTINUED ON TO IAD. OIL PRESSURE REMAINED PEGGED OUT HIGH. PERFORMED ENGINE INSPECTION IAW P&W JT3D MM 72-00. OIL FILTER FOUND CLEAN. REMOVED AND REPLACED OIL PRESSURE TRANSMITTER IAW DC-8 AMM. GROUND RUN CHECKED GOOD.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 71,551 hrs · 26,051 cycles

DURING DESCENT, CABIN PRESS WENT TO 2000 FT/MIN. RATE OF CLIMB UP TO 9500 CABIN ALT WITH NO CONTROL EITHER MANUALLY OR AUTOMATICALLY. RECOVERED AT FL 19000. COULD NOT DUPLICATE. CREW VERBAL, HEAVY RAINS LEAVING ILN. SUSPECT ICE BUILD-UP. INSPECTED OUTFLOW VALVE SUGAR SCOOP AND ASSOCIATED LINKAGE. CLEANED AND RESEATED CANNON PLUG CONNECTOR AT VALVE ACTUATOR. NO DISCREPANCY NOTED. TESTED OUTFLOW VALVE, GOOD REF DC-8 AMM 21-31-04-5-0001.

Part: CONTROL BOX — DEFECTIVE (MLG) · airframe 71,322 hrs · 25,732 cycles

AFTER TAKEOFF, GEAR WARNING LIGHT REMAINED ON. LANDING GEAR AND DOOR INDICATOR PANEL SHOWED NOSE GEAR. RECYCLED, SAME RESULT. CONSULTED ABNORMAL AND PROCEEDED TO DESTINATION. MAINTENANCE AT ILN: DURING SELF TEST OF PROX SWITCH CONTROL BOX, NOSE GEAR UP LIMIT FAILED IN B POSITION. REPLACED PROX CONTROL BOX IAW DC8 MM 32-60-00. NOSE GEAR UP LIMIT TESTED GOOD IN POSITION A AND B. NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR UP. INSTALLED NOSE LANDING GEAR UP LIMIT PROX SWITCH AND ADJUSTED IAW DC-8 MM. COMPLIED WITH POSITION WARNING SYSTEM TEST IAW DC8 MM 32-60-00-2.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 71,222 hrs · 25,723 cycles

AFT ACCESSORY COMPARTMENT CORROSION AT FUSELAGE SKIN AND DOUBLER LONGERON 33 RIGHT, FS 1620 - 1628, ADJACENT TO OUTFLOW VALVE. REPAIRED AREA IAW REA D853-48508MR.

Part: SPAR — CRACKED (RT WING) · airframe 71,222 hrs · 25,723 cycles

RIGHT WING REAR SPAR XRS 139 JACKPAD TO REAR SPAR FITTING CRACKED. REPAIRED AREA IAW REA D857-48845MR.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 71,222 hrs · 25,723 cycles

FORWARD CARGO LOWER LEFT SKIN FINGER DOUBLER CORRODED UNDERNEATH FROM STA 200 TO 220, LONGERON 35 LEFT TO 33 LEFT, BUTTLINE 7 TO BUTTLINE 20. REPAIRED AREA IAW REA D853-48505MR.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,222 hrs · 25,723 cycles

RIGHT WHEEL WELL LONGERON 24 FITTING WAS CRACKED JUST UNDER BOTTLE BOLT. REMOVED AND REPLACED LONGERON 24 RIGHT IAW ABX REA D853-48504MR.

Part: ANGLE — GOUGED (LT WING) · airframe 71,222 hrs · 25,723 cycles

LEFT WING OUTBOARD FLAP STA 219 FOLD HINGE COVER WELL OUTBOARD LOWER SIDE GOUGED. REPAIRED AREA IAW REA D827-48510MR.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 71,222 hrs · 25,723 cycles

FORWARD ACCESSORY AT STA 25, LONGERON 31 LEFT WAS CORRODED. REPAIRED AREA IAW REA D853-48515MR.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,145 hrs · 25,655 cycles

DURING MAINTENANCE INSPECTION, FOUND THE EMERGENCY LIGHT BATTERY DEAD. REPLACED EMERGENCY BATTERY PACK. SYSTEM CHECKED GOOD IAW DC8 MM 33.

Part: TRANSMITTER — DEFECTIVE (NR 4 ENG OIL) · airframe 71,129 hrs · 25,642 cycles

NR 4 ENGINE OIL PRESSURE INDICATED + 100 PSI AT TOP OF CLIMB. SECURED ENGINE AT 0325Z, RETURNED TO 22 PSI AT 0345. REPLACED NR 4 OIL PRESSURE TRANSMITTER, NR 4 OIL PRESSURE RELIEF VALVE AND MAIN ENGINE OIL FILTER. RAN NR 4 ENGINE, OIL PRESSURE AT IDLE 41 PSI AND 50 PSI AT POWER. LEAK AND OPS CHECKED GOOD IAW DC-8 MM.

Part: LONGERON — CORRODED · corrosion level 2 · airframe 70,810 hrs · 25,356 cycles

DURING LINE OPERATIONS AT ILN, LONGERON 36 WAS FOUND TO HAVE INTERGRANULAR CORROSION IN THE LOWER FLANGE AT STA 1420. REPAIRED LONGERON IAW ABX REA D853-46872MR.

Part: THRESHOLD — BENT (PAX DOORWAY) · airframe 70,780 hrs · 25,331 cycles

MAIN CABIN DOOR THRESHOLD LIP WAS RAISED PREVENTING DOOR FROM OPENING. REPAIRED RAISED LIP ON THRESHOLD OF MAIN CABIN DOOR AS REQUIRED IAW DC-8 MM.

Part: CONTROL ARM — DEFECTIVE (E & E BAY) · airframe 70,672 hrs · 25,247 cycles

WITH GEAR HANDLE DOWN, GREEN LIGHTS NOT ON, RED LIGHTS NOT ON EITHER. ACCOMPLISHED ABNORMAL PROCEDURE, STILL NO LIGHTS. OTHER CHECKLIST ITEMS INDICATED ALL GEAR WAS DOWN AND LOCKED. FOUND GEAR WARNING INTERLOCK CIRCUIT BREAKER INTERMITTENT (D-3). REPLACED CIRCUIT BREAKER AND PROXIMITY SENSOR BOX. SYSTEM OPS CHECKED GOOD IAW MM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 70,276 hrs · 24,896 cycles

FORWARD CARGO, STATION 300 - 320, LONGERON 35 LEFT, ATTACH ANGLE CRACKED. REPAIRED AREA AND INSTALLED NEW SECTION OF LONGERON, NEW -Z- FITTINGS, SPLICES AND NEW WEB IAW DC-8 SRM 51-1-20D, 53-2-0, 51-1-8, 51-1-24 AND REA D853-43046MR.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 70,276 hrs · 24,896 cycles

DURING C-CHECK, THE FITTING (P/N 9755584-508) WAS DAMAGED. R&R IAW REA D853-43051-MR AND FAA FORM 8110-3.

Part: LIGHT — INOPERATIVE (SMOKE DETECTOR) · airframe 70,225 hrs · 24,837 cycles

ON CLIMBOUT, UPPER CARGO SMOKE LIGHT CAME ON. NO SMOKE OR UNUSUAL SMELLS NOTED. NR 3 SMOKE DETECTOR APPEARED TO GIVE FALSE INDICATION. RELAMPED THE NR 3 UPPER CARGO SMOKE DETECTOR. OPS CHECKED GOOD IAW DC-8 MM 26-10-00.

Part: CONTROL BOX — DEFECTIVE (E/E BAY) · airframe 70,066 hrs · 24,693 cycles

RED GEAR UNSAFE LIGHT ILLUMINATED. LANDING GEAR AND DOOR LATCHING SELECTOR INDICATED RIGHT MAIN DOOR UNLATCHED. FOLLOWED ABNORMAL PROCEDURE AND ALL INDICATIONS RETURNED TO NORMAL. REPLACED THE GEAR PROXIMITY CONTROL BOX IAW DC-8 MM 32-10-00. OPS CHECKED GOOD.

Part: PROXIMITY SWITCH — MALFUNCTIONED (RT MLG DOOR) · airframe 70,032 hrs · 24,665 cycles

AFTER GEAR RETRACTION RECEIVED RED GEAR UNSAFE LIGHT ILLUMINATION WITH UNSAFE LIGHT ILLUMINATED WITH GEAR UP. RAN ABNORMAL PROCEDURES AND RECEIVED RIGHT MAIN LANDING GEAR DOOR NOT LATCHED LIGHT MOMENTARILY THEN RIGHT MAIN LANDING GEAR DOOR LIGHT WENT OUT ACCOMPANIED BY RED GEAR UNSAFE LIGHT GOING OUT. THEN DURING DESCENT, RECEIVED ABOVE INDICATION AGAIN. COMPLIED WITH ADJ/TEST OF MAIN GEAR DOOR CLOSED PROXIMITY SWITCH. FOUND RIGHT GEAR DOOR PROXIMITY SWITCH TO BE MALFUNCTIONING. REPLACED GEAR DOOR CLOSED PROXIMITY SWITCH IAW DC-8 MM 32-60-00-2. COMPLIED WITH ADJ/TEST OF MAIN GEAR DOOR CLOSED PROXIMITY SWITCH AGAIN. SYSTEM OPS CHECKED GOOD. NO OTHER DEFECTS NOTED.

Part: UPLOCK — OUT OF ADJ (RT MLG) · airframe 70,022 hrs · 24,658 cycles

RED GEAR UNSAFE LIGHT CAME ON AT CRUISE AND THE RIGHT GEAR DOOR LANDING GEAR AND LIGHT WENT OUT. PERFORMED LANDING GEAR DOOR SWITCH TEST AND ADJ/TEST MAIN GEAR DOOR. CLOSED PROXIMITY SWITCH. BOTH CHECKED GOOD. ADJUSTED DOOR UPLATCH TURNBUCKLES IAW DC-8 MM 32-30-00-2. CLEANED AND LUBED SWITCHES. SYSTEM CHECKED GOOD ON THE GROUND.

Part: VALVE — DEFECTIVE (BRAKE SYS) · airframe 69,795 hrs · 24,470 cycles

THE LEFT MAIN LANDING GEAR WHEEL BRAKES WOULD NOT OPERATE. MAINTENANCE INSPECTED AND FOUND THE BRAKE HYDRAULIC POWER VALVE ASSY TO HAVE A BROKEN FORK. THE POWER VALVE WAS REPLACED IAW DC-8 MM 32-42-02.

Part: WINDOW — STUCK (COCKPIT) · airframe 69,636 hrs · 24,401 cycles

FIRST OFFICERS CLEARVIEW WINDOW DID NOT OPEN ALL THE WAY. MAINTENANCE INSPECTED AND REPLACED LOWER AFT HOOK SPRING AND ADJUSTED IAW DC-8 MM 56-10-03. PRESSURIZATION AND WINDOW OPERATION CHECKED GOOD.

Part: WINDOW — STUCK (COCKPIT) · airframe 69,636 hrs · 24,401 cycles

FIRST OFFICERS CLEARVIEW WINDOW WOULD NOT OPEN COMPLETELY. MAINTENANCE INSPECTED AND OPERATED THE FIRST OFFICERS CLEARVIEW WINDOW SEVERAL TIMES. THE WINDOW OPERATED NORMALLY IAW DC-8 MM 56-10.

Part: WINDOW — OUT OF ADJ (COCKPIT) · airframe 69,131 hrs · 24,172 cycles

FIRST OFFICER''S CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED SERRATED HOOK STOP ON AFT OF FIRST OFFICER''S CLEARVIEW WINDOW. OPS CHECKED GOOD PER DC8 MM.

Part: RACK — MALFUNCTIONED (CABIN) · airframe 68,819 hrs · 24,003 cycles

EMERGENCY LIGHTS BLINKED ON/OFF EVERY 2.5 MINUTES. REPLACED EMERGENCY LIGHT RACK ASSEMBLY IAW DC8 MM, OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 68,813 hrs · 24,001 cycles

EMERGENCY BATTERY CHARGING CIRCUIT BREAKER WOULD NOT RESET. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC9 MM, OPS CHECKED GOOD.

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

AFTER GEAR RETRACTION, RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLED GEAR TWICE, UNSAFE LIGHT REMAINED. USED ABNORMAL PROCEDURES TO DETERMINE RIGHT GEAR DOOR UNSAFE AND SECURED DOOR TO NORMAL. ADJUSTED CABLE TENSION AND REPLACED OVERCENTER SPRING.

Part: FITTING — CORRODED (BS 1240)

EXFOLIATED BATHTUB FITTING AT STATION 1240, LONGERON 31 LEFT. REPLACED FITTING IAW DC8 SRM 53-2-0 AND ABX REA D853-24927MR.

Part: FITTING — CORRODED (BS 1200)

CORRODED BATHTUB FITTING AT STATION 1200, LONGERON 29 LEFT. REPLACED FITTING IAW ABX REA D853-249279 AND DWG 93755842.

Part: FITTING — CORRODED (BS 1220)

EXFOLIATED BATHTUB FITTING AT LONGERON 29 LEFT, STATION 1220. REPLACED FITTING IAW ABX REA D853-24927 AND DC8 SRM 51-1-21D.

Part: FITTING — CORRODED (BS 1220)

BATHTUB FITTING CORRODED AT STATION 1220, LONGERON 31 LEFT. REPLACED FITTING IAW DC8 SRM 51-1-20D AND ABX REA D853-24927-1MR.

Part: FITTING — CORRODED (BS 1260)

CORRODED BATHTUB FITTING AT LONGERON 28 LEFT, STATION 1260. REPLACED FITTING IAW DWG 3755842, ABX REA D85324928MR AND DC8 SRM 53-2-0.

Part: FITTING — CORRODED (BS 1220)

BATH TUB FITTING CORRODED AT STATION 1220, LONGERON 31 LEFT. REPLACED FITTING IAW DWG 3755844, ABX REA D853-219271MR AND DC8 SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1260)

BATHTUB FITTING AT STATION 1260, LONGERON 30 LEFT. REPLACED FITTING IAW DC8 SRM 51-1-21D, DWG 3755842 AND ABX REA D853-249271.

Part: FITTING — CORRODED (BS 1260)

EXFOLIATED BATHTUB FITTING AT STATION 1260, LONGERON 31 LEFT. REPLACED FITTING IAW DC8 SRM 53-2-0 AND ABX REA D853-24921.

Part: FITTING — CORRODED (BS 1260)

CORRODED BATHTUB FITTING AT LONGERON 28 LEFT, STATION 1260. REPLACED FITTING IAW DWG 3755842, ABX REA D853-24928 AND DC8 SRM 53-2-0.

Part: FITTING — CRACKED (BS 1080)

LEFT CUSP LOWER FITTING CRACKED AT STATION 1080. REPAIRED IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1080)

LEFT CUSP LOWER ATTACH FITTING CRACKED AT STATION 1080. REPAIRED IAW DC8 SRM 51-1-20D.

Part: GUSSETT — CORRODED (BS 1240)

GUSSETT PLATE HAD EXFOLIATION CORROSION AT STATION 1240, LONGERON 24 L. REPLACED GUSSETT IAW DWG 9755849, DC9 SRM 51-1-20 AND ABX REA D853-24930.

Part: BULKHEAD — CRACKED (BS 1540)

CRACKED INTERCOSTAL ON AFT BULKHEAD, STATION 1540 RIGHT. REPAIRED IAW DC8 SRM AND DWG 5646608.

Part: GUSSET — CORRODED (BS 1220)

GUSSET HAD EXFOLIATED CORROSION AT STATION 1220 LONGERON 24 LEFT. REPLACED GUSSET IAW DC8 SRM 51-01-20D AND ABX REA D853-24930.

Part: CHANNEL — CRACKED (LT MLG WW)

LEFT MAIN LANDING GEAR SUPPORT STRUCTURE CRACKED, AFT SIDE OF LANDING GEAR CUTOUT. INSTALLED REPLACEMENT CHANNEL IAW DWG 5611020 AND DC8 SRM 51-1-21.

Part: GUSSETT — CORRODED (BS 1220)

GUSSETT HAS EXFOLIATION CORROSION AT STATION 1220, LONGERON 24L. REPLACED GUSSETT IAW DC8 SRM 51-1-20D AND ABX REA D853-24930.

Part: FRAME — CORRODED (BS 1600)

CORROSION FOUND ON STATION 1600 FRAME LOWER FLANGE BETWEEN LONGERON 34 LEFT AND 34 RIGHT. REPAIRED IAW SRM 53-2-0.

Part: BKHD INTERCOSTAL — CRACKED (BS 1540)

CRACKED INTERCOSTAL ON AFT BULKHEAD, STATION 1540 RIGHT. REPAIRED IAW DC8 SRM 51-1-21 AND DWG 5646608.

Part: GUSSET — CORRODED (BS 1240)

GUSSET PLATE HAD EXFOLIATED CORROSION AT STATION 1240 LONGERON 24 LEFT. REPLACED GUSSETT IAW DWG 9755849 AND DC8 SRM 51-01-20D AND ABX RE AND 853-24930.

Part: FRAME — CORRODED (BS 1600)

CORROSION ON STATION 1600 FRAME, LOWER FLANGE, BETWEEN LONGERONS 34 LEFT AND 34 RIGHT. REPAIRED IAW DC8 SRM 53-2-0.

Part: CHANNEL — CRACKED (LT MLG WW)

LEFT MAIN LANDING GEAR SUPPORT STRUCTURE CRACKED AT AFT SIDE OF LANDING GEAR CUT-OUT. REPLACED CHANNEL IAW DWG 5611020 AND DC8 SRM 51-01-21.

Part: SKIN — CORRODED (LT HORIZ STAB)

LEFT HORIZONTAL STABILIZER LEADING EDGE, UPPER SURFACE HAD BULGING CORROSION ALONG AFT END FROM STATION XFS235 TO XFS320. REPAIRED IAW DC8 SRM 55-21.

Part: FORMER — CRACKED (WS 6.225)

LEFT WING INBOARD FORMER CRACKED ABOVE DUCT AT STATION XOLD 6.225. REPAIRED DAMAGE IAW DC8 SRM.

Part: RIB — CRACKED (WS 841)

RIGHT WING OUTBOARD LEADING EDGE UPPER RIB CRACKED INSIDE PANEL 517B AT STATION FS 841. REPAIRED IAW DC8 SRM 51-1-20D.

Part: RIB — CRACKED (WS 841)

RIGHT WING OUTBOARD LEADING EDGE UPPER RIB WAS CRACKED INSIDE PANEL 517B AT STATION FS 841. REPAIRED IAW DC8 SRM 51-1-20D.

Part: STRUCTURE — CRACKED (LT MLG WW)

ONE-HALF INCH CRACK IN LEFT MAIN LANDING GEAR WHEEL WELL STRUCTURE. REPAIRED IAW DC8 SRM 57-2-0.

Part: SKIN — CRACKED (NR 2 PYLON)

LEFT WING INBOARD NR 2 PYLON LOWER AFT SKIN CRACKED AT LOWER TRAILING EDGE. REPAIRED IAW DC8 SRM 57-2-1.

Part: SKIN — CRACKED (LT WING)

LEFT WING INBOARD NR 2 PYLON, LOWER AFT SKIN CRACKED AT LOWER TRAILING EDGE. REPAIRED IAW DC8 SRM 57-2-1.

Part: RIB — CRACKED (WS 822)

RIGHT WING LEADING EDGE UPPER RIB AT STATION XFS 822 CRACKED AT FASTENER END. REPAIRED IAW DC8 SRM 51-1-8 AND DWG K05056.

Part: RIB — CRACKED (WS 822)

RIGHT WING LEADING EDGE UPPER RIB AT STATION XFS 822 CRACKED AT FASTENER END. REPAIRED IAW DC8 SRM 51-1-8.

Part: STRUCTURE — CRACKED (LT SERV DOOR)

LEFT CENTER SERVICE DOOR HAD CRACK IN STRUCTURE. REPAIRED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-8 AND 52-20-0.

Part: FITTING — CRACKED (LT AILERON)

LEFT INBOARD AILERON INBOARD HINGE FITTING WAS CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-21.

Part: RIB — CRACKED (WS 736)

RIGHT WING LEADING EDGE RIB CRACKED AT STATION XFS 736. REPAIRED IAW DC8 SRM 51-1-8 AND DWG K05056.

Part: SKIN — CRACKED (CARGO DOOR)

LOWER CARGO DOOR (C2) INTERIOR SKIN CRACKED AT LOWER FORWARD CORNER. REPAIRED IAW DC8 SRM 52-4-2.

Part: SKIN — CRACKED (LT SERV DOOR)

TWO LIGHTENING HOLES IN FORWARD, LEFT SERVICE DOOR STRUCTURE WERE CRACKED. REPLACED SKIN PANEL IAW DC8 SRM 51-1-8, 51-3-0 AND DWG 5755530.

Part: RIB — CRACKED (WS 772)

RIGHT WING LEADING EDGE RIB CRACKED AT STATION ATXFS772. REPAIRED IAW DC8 SRM 51-1-20.

Part: FITTING — CRACKED (LT AILERON)

LEFT INBOARD AILERON, INBOARD HINGE FITTING CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-21.

Part: DOOR — CRACKED (LT SERV DOOR)

LEFT CENTER SERVICE DOOR HAD CRACK IN STRUCTURE. INSTALLED DOUBLER IAW DC8 SRM 51-1-8 AND 52-2-0.

Part: RIB — CRACKED (WS 772)

RIGHT WING UPPER RIB CRACKED AT STATION XFS772. REPAIRED IAW DC8 SRM 51-1-20.

Part: SKIN — CRACKED (CARGO DOOR)

LOWER CARGO C2 DOOR INTERIOR SKIN CRACKED AT LOWER FORWARD CORNER. REPAIRED IAW DC8 SRM 52-4-2 AND 51-1-20.

Part: SKIN — CORRODED (WS 761)

RIGHT WING LEADING EDGE HAD EXFOLIATED CORROSION AT INBOARD FORWARD LEADING EDGE, STATION XW 761. REPAIRED IAW DC8 SRM 57-2-1.

Part: RIB — CRACKED (WS 753.75)

UPPER RIB CRACKED AT LEFT WING OUTBOARD LEADING EDGE AT XFS 753.750. REPAIRED IAW DC8 SRM 51-1-20D AND DWG K05056.

Part: FITTING — CORRODED (BS 70)

STRINGER END CORRODED, STRINGER 4 RIGHT AND STATION 70. REPAIRED IAW DC8 SRM 51-1-20D AND 51-1-21.

Part: RIB — CRACKED (WS 772.5)

RIB CRACKED AT LEFT WING OUTBOARD SECTION AT XFS 772.5. REPAIRED IAW DC8 SRM 51-1-20D AND ABX DWG K05056.

Part: RIB — CRACKED (WS 772.5)

RIB CRACKED AT LEFT WING OUTBOARD SECTION AT STATION XFS 772.5. REPAIRED IAW DC8 SRM 51-1-20D AND DWG K05056.

Part: RIB — CRACKED (WS 753.750)

UPPER RIB CRACKED AT LEFT WING OUTBOARD LEADING EDGE AT XFS 753.750. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-20D.

Part: ANGLE — CRACKED (BS 680)

FLOORBEAM SUPPORT ANGLE CRACKED AT STATION 680, RBL 28. REPAIRED IAW DWG 4645377 AND DC8 SRM 51-1-20D.

Part: ANGLE — CRACKED (BS 680)

FLOORBEAM SUPPORT ANGLE CRACKED AT STATION 680, RBL 28. REPAIRED IAW DWG 4645517 AND DC8 SRM 51-1-20D.

Part: INTERCOSTAL — CORRODED (BS 8-20)

EXFOLIATED CORROSION ON INTERCOSTAL AT LONGERON 30L, STATION 8 TO 20 INSIDE AIR CONDITIONING BAY. REPLACED INTERCOSTAL IAW DWG 5615530 AND DC8 SRM 51-1-21.

Part: FITTING — CRACKED (BS 1040-1060)

LONGERON 31 LEFT SPLICE FITTING CRACKED AT STATION 1040 TO 1060. REPLACED FITTING IAW DC8 SRM 51-1-20D.

Part: INTERCOSTAL — CORRODED (BS 8-20)

EXFOLIATED CORROSION ON INTERCOSTAL AT LONGERON 30 LEFT STATION 8 TO 20, INSIDE AIR CONDITIONING COMPARTMENT. REPLACED INTERCOSTAL IAW DWG 5615530 AND DC8 SRM 51-1-21.

Part: FITTING — CRACKED (BS 860)

INTERCOSTAL END FITTING CRACKED AT LONGERON 19 RIGHT, STATION 860. REPLACED END FITTING IAW DWG 4750422 AND DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1040-1060)

LONGERON 31L SPLICE FITTING CRACKED AT STATION 1040 TO 1060. REPLACED FITTING IAW DC8 SRM 51-1-20.

Part: FITTING — CRACKED (BS 860)

INTERCOSTAL FITTING CRACKED AT LONGERON 18 LEFT, STATION 860. REPLACED FITTING IAW DWG 4750420 AND DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 860)

INTERCOSTAL FITTING CRACKED AT LONGERON 18 LEFT AND STATION 860. REPLACED FITTING IAW DWG 47504201 AND DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 860)

INTERCOSTAL END FITTING CRACKED AT LONGERON 19R, STATION 860. REPLACED FITTING IAW DWG 4750422 AND DC8 SRM 51-1-20D.

Part: FITTING — CORRODED (BS 290)

BATHTUB FITTING CORRODED AT STATION 290 AND LONGERON 29 LEFT. REPLACED FITTING IAW DC8 SRM 51-01-20D AND 53-2-0.

Part: WEB — CRACKED (RT WING)

CRACKED WEB GUSSETT INSIDE RIGHT WING LEADING EDGE BETWEEN PANELS 519C AND 520A ABOVE ANTI-ICE VALVE. REPAIRED IAW DC8 SRM 51-3-0.

Part: LOCK — JAMMED (COCKPIT)

COCKPIT ENTRY DOOR JAMMED IN LOCKED POSITION AND COULD NOT BE RELEASED. REPLACED LATCH ASSEMBLY IAW DC8 SRM 51-03-00. OPS CHECKED GOOD.

Part: HOSE — LEAKING (NR 2 TR UNIT)

LOSS OF HYDRAULIC FLUID DOWN TO STANDPIPE LEVEL. AILERON CONTROL MANUAL LIGHT ILLUMINATED, HYDRAULIC PRESSURE VERY LOW AND NR 2 THRUST REVERSER LIGHT WAS FLASHING. REPLACED LEAKING HYDRAULIC HOSE TO THE THRUST REVERSER PUMP. RESERVICED HYDRAULIC SYSTEM, OPS CHECKED GOOD.

Part: WINDOW — LOOSE (COCKPIT)

DURING PREFLIGHT, FOUND FIRST OFFICER'S WINDOW (ESCAPE EXIT) WOULD NOT OPEN. TIGHTENED UPPER, AFT ROLLER, OPS CHECKED NORMAL IAW DC8 MM 56-10.

Part: WINDOW — LACK OF LUBE (COCKPIT)

FIRST OFFICERS SLIDING WINDOW BINDING AND EXTREMELY HARD TO OPEN. LUBRICATED MECHANISM IAW DC8 MM, OPS CHECKED GOOD.

Part: SEAT — MALFUNCTION (LT COCKPIT)

CAPTAIN'S SEAT WOULD NOT LOCK FORWARD OR AFT. REPLACED CAPTAIN'S SEAT IAW DC8 MM, OPS CHECKED GOOD.

Part: CARGO TRACK — CORRODED (BS 270-260)

FORWARD LOWER CARGO COMPARTMENT RT SIDE CARGO TRACK CORRODED OUT OF LIMITS AT STA 270 TO STA 260. REPAIRED IAW DC-8 SRM 51-1-8 AND DAC DWG 3759264.

Part: SKIN — CRACKED (WS 207)

LT WING UPPER SURFACE, INBD STUB WING HAS VISABLE CRACKS AT FASTENER HOLE, INBD END AT FWD SPAR, XFS 207. REPAIRED IAW DC-8 SRM 51-1-20D, 51-1-21 AND 51-3-0.

Part: SKIN — CRACKED (RT WING)

RIGHT WING PANEL 505F HAS CRACKS ON LANDS. REPAIRED IAW ABX REA D857 19817 REV B.

Part: SKIN — CRACKED (LT WING)

LT WING PANEL 505F HAS CRACKS ON LANDS. REPAIRED PANEL IAW ABX REA D857-19566MR AND DC8 SRM 51-1-21.

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

DURING LANDING GEAR RETRACTION, AFTER TAKEOFF, GEAR UNSAFE LIGHT REMAINED ILLUMINATED. UPLATCH CHECK INDICATED RIGHT MAIN GEAR DOOR UNLOCKED. RECYCLED GEAR AND UNSAFE LIGHT EXTINGUISHED AFTER TEN MINUTES. UPLATCH CHECK WAS SATISFACTORY. CLEANED AND LUBRICATED RIGHT MAIN GEAR DOOR PROXIMITY SWITCH. AFTER SUBSEQUENT FLIGHT, FOUND RIGHT GEAR DOOR SEQUENCE CABLES OUT OF RIG. ADJUSTED CABLES IAW DC-8 MM, SYSTEM OPS CHECKED GOOD DURING GEAR SWING.

Part: DOOR LIGHT — ILLUMINATED (RT MLG DOOR)

DURING GEAR RETRACTION AFTER TAKEOFF, RIGHT MAIN LANDING GEAR DOOR LATCH LIGHT ILLUMINATED. RECYCLED LANDING GEAR AND LIGHTS EXTINGUISHED. INSPECTED RIGHT MAIN LANDING GEAR DOOR PROXIMITY SWITCH AND WIRING, NO DEFECTS WERE FOUND. COMPLETED RIGHT MAIN LANDING GEAR DOOR PROXIMITY SWITCH TEST, THE DOOR LATCHED NORMALLY AND ALL INDICATIONS WERE GOOD.

Part: RELIEF VALVE — DEFECTIVE (NR 4 ENGINE)

DURING DESCENT, LOW OIL PRESSURE WARNING LIGHT ILLUMINATED FOR THE NR 4 ENGINE WITH AN OIL PRESSURE INDICATION OF 33 PSI WITH ENGINE POWER AT IDLE. PERFORMED PRECAUTIONARY SHUT-DOWN OF THE NR 4 ENGINE. REPLACED MAIN OIL FILTER FOR THE NR 4 ENGINE IAW DC8 MM, CHAPTER 79. REPLACED OIL PRESSURE RELIEF VALVE FOR THE NR 4 ENGINE IAW PWA JT3D MM, CHAPTER 72. CHECKED OIL PRESSURE INDICATION IAW DC8 MM, CHAPTER 79 AND OPS CHECK WAS GOOD.

Part: UPLATCH CYLINDER — DEFECTIVE (LT MLG)

LEFT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED DURING INITIAL EXTENSION. LANDING GEAR WAS RECYCLED AND LANDING GEAR INDICATED DOWN AND LOCKED. REPLACED LEFT MAIN LANDING GEAR UPLATCH CYLINDER IAW DC8 MM CHAPTER 32. PERFORMED SEVERAL RETRACTION AND EXTENSION CHECKS AND ALL INDICATIONS WERE GOOD IAW DC8 MM CHAPTER 32.

Part: CONTROL VALVE — LEAKING (LT MLG)

LEFT MAIN LANDING GEAR HAD TO BE CYCLED TO GET DOWNLOCK INDICATION. NO GREEN DOWNLOCK INDICATION OR SPOILER PRESSURE INDICATION OCCURRED ON THE FIRST ATTEMPT. DURING THE SECOND ATTEMPT, THE LEFT MAIN LANDING GEAR LOCKED DOWN, BUT AT A SLOWER RATE THAN THE OTHER GEARS. RIGGED LEFT MAIN LANDING GEAR DOORS, CHECKED MAIN GEAR UPLOCK ROLLER CLEARANCE AND REPLACED LANDING GEAR CONTROL VALVE IAW DC8 MM, CHAPTER 32. EXTENSION, RETRACTION, UPLATCH AND FREE-FALL CHECKS WERE GOOD IAW DC8 MM, CHAPTER 32.

Part: TRANSLATING RING — CRACKED (NR 4 ENGINE)

DURING 825AX MOD, FOUND NR 4 ENGINE THRUST REVERSER TRANSLATING RING CRACKED. REPAIRED NR 4 ENGINE THRUST REVERSER TRANSLATING RING IAW ABX REA D878-11909.

Part: SPAR CAP — DAMAGED (LT TE FLAP)

DURING 825AX MOD, FOUND LEFT HAND OUTBOARD FLAP UPPER SPAR CAP IS CUT OUT. REPAIRED LEFT HAND OUTBOARD FLAP UPPER SPAR CAP IAW ABX REA D857-12466.

Part: TRANSLATING RING — CRACKED (NR 2 ENGINE)

DURING 825AX MOD, FOUND NR 2 ENGINE THRUST REVERSER TRANSLATING RING CRACKED. REPAIRED NR 2 ENGINE THRUST REVERSER TRANSLATING RING IAW ABX REA D878-11887.

Part: INSTRUMENT PANEL — MISLOCATED (COCKPIT)

DURING 825AX MOD, FOUND INSTRUMENT PANEL ON MAIN FRAME NEEDS TO BE MODIFIED TO ABX STANDARDS. REPAIRED INSTRUMENT PANEL MAIN FRAME IAW ABX REA D825-11935.

Part: SPAR CAP — SPLIT (LT TE FLAP)

DURING 825AX MOD, FOUND LEFT HAND OUTBOARD FLAP CENTER SLIDING PANEL STAINLESS STEEL DOUBLER HAS CORROSION AND AFT SPAR TOP CAP IS SPLIT. REPAIRED LEFT HAND OUTBOARD FLAP CENTER SLIDING PANEL STAINLESS STEEL DOUBLER ABD AFT SPAR TOP CAP IAW ABX REA D857-12444.

Part: FRAME — CORRODED (BS 1890)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE LOWER FRAME AT STATION 1890, FROM LONGERON 28R - 28L. REPAIRED IAW ABX REA D853-11926-MR.

Part: DOUBLER — DAMAGED (BS 1050-1350)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND INTERNAL DOUBLER AT STATION 1050 - 1350 DAMAGED. REPAIRED INTERNAL DOUBLER IAW ABX REA D853-12310-MR.

Part: ANGLE — CORRODED (BS 1020)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON CUSP ANGLE, RIGHT SIDE, AT STATION 1020, LONGERON 22R. REPAIRED CUSP ANGLE IAW ABX REA D853-11656-MR.

Part: INTERCOSTAL — CORRODED (BS 1660-1670)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE INTERCOSTAL AT FS 1667, LONGERON 23L. REPAIRED INTERCOSTAL IAW ABX REA D853-12183-MR.

Part: LONGERON — CORRODED (BS 1050-1350)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON LONGERON 36 AT STATION 1050 - 1350. REPAIRED IAW ABX REA D853-11929-MR.

Part: FRAME — CORRODED (BS 1660-1670)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE FRAME AT FS 1667. REPAIRED IAW ABX REA D853-12183-MR.

Part: FRAME — CORRODED (BS 1360)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION AT LOWER FLANGE AT STATION 1360, LONGERON 36. REPAIRED IAW ABX REA D853-12322-MR.

Part: FLOOR BEAM — CORRODED (BS 1700)

DURING D - CHECK AND AND ACCEPTANCE INSPECTIONS, FOUND CORROSION AT AFT SIDE OF FLOOR BEAM AT STATION 1700, LONGERON 31. REPAIRED FLOOR BEAM IAW ABX REA D853-12343-MR.

Part: DOOR PAN — CORRODED (C2 DOOR)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION AT C-2 DOOR PAN. REPAIRED C-2 DOOR PAN IAW ABX REA D852-12338-MR.

Part: LONGERON — DAMAGED (BS 90)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND LONGERON 22L AT STATION 90 HAD A NON-STANDARD REPAIR. REPAIRED LONGERON IAW ABX REA D853-12311-MR.

Part: DOOR DOUBLER — CRACKED (FS 156)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND GROUND PNEUMATIC DOOR INTERNAL DOUBLER CRACKED. REPAIRED IAW ABX REA D853-12283-MR.

Part: PLATING — DAMAGED (BS 1670)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND EXISTING REPAIR AT STATION 1670, LONGERONS 21L AND 17L. REPAIRED IAW ABX REA D853-12278-MR.

Part: LONGERON — CORRODED (BS 1080-1120)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON LONGERON 9R AT STATION 1080 - 1120. REPAIRED IAW ABX REA D853-11673-MR.

Part: FRAME — CORRODED (BS 1000)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE FRAME AT STATION 1000, LONGERON 35L - 35R. REPAIRED FRAME IAW ABX REA D853-12204-MR.

Part: FRAME — CORRODED (BS 1460)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE FRAME AT AFT PIT STATION 1460, LONGERON 34L TO 35R. REPAIRED FRAME IAW ABX REA D853-12195-MR.

Part: CHANNEL — CHAFED (LT MLG DOOR)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND ZEE CHANNEL ON THE LEFT MAIN LANDING GEAR DOOR CHAFED. REPAIRED CHANNEL IAW ABX REA D852-12160-MR.

Part: ANGLE — CORRODED (BS 920)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE FRAME ANGLE AT STATION 920, LONGERONS 1 - 2R. REPAIRED FRAME ANGLE IAW ABX REA D853-12190-MR.

Part: FRAME — CORRODED (BS 1200)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE FRAME AT STATION 1200, LONGERON L1. REPAIRED FRAME IAW ABX REA D853-12172-MR.

Part: FRAME — CORRODED (BS 1400)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND FRAME AT STATION 1400, LONGERON 36, CRACKED AND CORRODED. REPAIRED FRAME IAW ABX REA D853-12167-MR.

Part: DOUBLER — CORRODED (BS 1500)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE WINDOW DOUBLER AT FS 1500R. REPAIRED WINDOW DOUBLER IAW ABX REA D853-11941-MR.

Part: CORNER — CORRODED (CARGO DOOR)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION AND CRACKS IN THE FORWARD CORNER OF THE AFT DOOR OF THE AFT CARGO COMPARTMENT. REPAIRED AFT DOOR IAW ABX REA D853-11921-MR.

Part: FRAME — CORRODED (BS 1640)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE FRAME AT STATION 1640, BETWEEN LONGERON 26L AND 27L. REPAIRED IAW ABX REA D853-12163-MR.

Part: FRAME — CORRODED (BS 17)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE FRAME AT YCS 17.00, LONGERON 6R. REPAIRED FUSELAGE TAIL SECTION FRAME IAW ABX REA D853-12166-MR.

Part: JAMB — CRACKED (LT MLG DOOR)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND LEFT MAIN LANDING GEAR DOOR FORWARD JAMB ZEE CRACKED. REPAIRED MAIN LANDING GEAR DOOR FORWARD JAMB ZEE IAW ABX REA D853-11938-MR.

Part: ANGLE — CORRODED (BS 857)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE ATTACH ANGLE OF REAR SPAR AT FS 857, RBL 46.00. REPAIRED IAW ABX REA D853-11643-MR.

Part: SKIN — CRACKED (BS 1170)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND FUSELAGE SKIN AT LONGERON 21R, STATION 1170 CRACKED. REPAIRED IAW ABX REA D853-11663-MR.

Part: SKIN — DAMAGED (L2 DOOR)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND THAT PREVIOUS REPAIR ON SKIN OF L2 DOOR, LOWER FORWARD CORNER IS NOT IAW DAC DRAWING SR08530021. REPAIRED IAW DAC DRAWING SR08530021 AND ABX REA D853-11634-MR.

Part: FRAME — CORRODED (BS 1020)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE FRAME AT STATION 1020, LONGERON 33 - 34R. REPAIRED FRAME IAW ABX REA D853-11923-MR.

Part: RIB — DAMAGED (RT TE FLAP)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND RIGHT INBOARD END RIB WEB DAMAGED. REPAIRED IAW ABX REA D857-11662-MR.

Part: RIB — CRACKED (LT TE FLAP)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND LEFT INBOARD END RIB WEB DAMAGED. REPAIRED IAW ABX REA D857-11662-MR.

Part: LONGERON — CORRODED (BS 500-520)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND L36 CORRODED BETWEEN FS 500 AND FS 520. REPAIRED IAW ABX REA D853-11668-MR.

Part: DOUBLER — CORRODED (BS 920-940)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE RIGHT AND LEFT SIDES OF THE MAIN CABIN WINDOW FRAME AT FS 920 - 940. REPAIRED WINDOW DOUBLERS IAW ABX REA D853-11644-MR.

Part: DOUBLER — CORRODED (BS 1250)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE LEFT WINDOW DOUBLER AT STATION 1250. REPAIRED IAW ABX REA D853-11645-MR.

Part: CUSP — CORRODED (BS 1280-1300)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON CUSP AT LONGERON 21L, STATION 1280 - 1300. REPAIRED CUSP IAW ABX REA D853-11657-MR.

Part: KEEL BEAM — CORRODED (BS 660)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE HORIZONTAL FLANGES OF THE FORWARD KEEL TEE. REPAIRED IAW ABX REA D853-11886-MR.

Part: CUSP — CORRODED (BS 1045)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON CUSP AT STATION 1045, LONGERON 21L. REPAIRED CUSP IAW ABX REA D853-11658-MR.

Part: CUSP — CORRODED (BS 1480)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON CUSP AT STATION 1480, LONGERON 21R. REPAIRED CUSP IAW ABX REA D853-11655-MR.

Part: PLATE — WORN (LT TE FLAP)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND LEFT INBOARD FLAP, INBOARD HINGE, OUTBOARD FITTING PLATE WORN. REPAIRED IAW ABX REA D857-11652-MR.

Part: FITTING — WORN (LT TE FLAP)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND INBOARD HINGE FITTING AT INBOARD FLAP WORN. REPAIRED IAW ABX REA D857-11653-MR.

Part: SKIN — CRACKED (WS 69.5)

DURING D - CHECK AND MOD ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 90-16-05, SB 57-88, FOUND LEFT WING LOWER SKIN AT XCW 69.5, HOLES A, C, F, I, 4 AND 5 HAVE CRACK LIKE INDICATIONS NOTED BY HIGH FREQUENCY EDDY CURRENT INSPECTION. REPAIRED IAW ABX REA D857-11369-MR.

Part: SKIN — DENTED (BS 520)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND FORWARD LOWER CARGO COMPARTMENT AFT DOOR SKIN HAD A DENT AND WAS GOUGED. REPAIRED IAW ABX REA D853-11372-MR.

Part: FRAME — CRACKED (BS 180)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND FRAME CRACKED AT FS 180 BETWEEN L35L AND L36. REPAIRED FUSELAGE FRAME IAW ABX REA D853-11373-MR.

Part: SKIN — CRACKED (WS 69.5)

DURING D - CHECK AND ACCEPTANCE INSPECTIONS, WHILE COMPLYING WITH AD 90-16-05, SB 57-88, FOUND LOWER WING SKIN, RIGHT SIDE AT STATION XCW 69.5 HAD CRACK INDICATIONS. REPAIRED SKIN IAW ABX REA D857-11370-MR.