N829BX
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
229 reports on file, 1996-04-09 – 2007-12-20.
Part: WIRE — OUT OF POSITION (MLG DOOR) · airframe 92,625 hrs · 37,379 cycles
DURING CLIMB FROM KTOL GEAR DOOR WARNING LIGHT CAME ON WOULD NOT GO OUT. THE CREW RETURNED TO KTOL, AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED GEAR DOOR AND REPOSITONED WIRING AT DOOR WARNING LIGHT SOCKET OPERATIONAL CHECK WAS GOOD IAW DC8 MAINTENANCE MANUAL 32-10-0. AIRCRAFT WAS RETURNED TO SERVICE.
Part: MECHANISM — OUT OF ADJUST (RT MLG DOOR) · airframe 92,576 hrs · 37,363 cycles
DURING CLIMB-OUT FROM KTOL, MAIN LANDING GEAR DOOR LIGHT STAYED ILLUMINATED. THE CREW CYCLED THE GEAR AND THE LIGHT STAYED ON. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED RIGHT MAIN GEAR DOOR AND ADJUSTED RIGHT GEAR DOOR FOLLOWUP MECHANISM, OPERATIONAL CHECK WAS GOOD IAW DACO DC8 MAINTENANCE MANUAL 32-30-0, AND 32-31-5. AIRCRAFT WAS RETURNED TO SERVICE.
Part: STRIKER — OUT OF ADJUST (MLG DOOR) · airframe 92,575 hrs · 37,362 cycles
DURING CLIMB-OUT FROM KPHL TO KTOL, AFTER GEAR RETRACTION THE DOOR LIGHT REMAIN ON. THE CREW CYCLED THE GEAR AND THE LIGHT REMAINED ON. THE CREW CONTINUED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CLEANED UPLATCH SWITCHES AND ADJUSTED DOOR STRIKER. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE IAW DC8 MAINTENANCE MANUAL 32-12-1.
Part: UPLOCK SWITCH — DIRTY (ZONE 700) · airframe 92,574 hrs · 37,361 cycles
DURING CLIMB-OUT FROM KTOL TO KPHL, GEAR LANDING DOOR LIGHT REMAINED ON AFTER GEAR WAS RETRACTED, THE CREW CYCLED THE GEAR AND THE LIGHT REMAINED ON. THE CREW CONTINUED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE SYSTEM AND CLEANED GLYCOL FROM UPLATCH SWITCHES. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE IAW DACO MAINTENANCE MANUAL 32-12-1.
Part: STRIKER — WORN (MLG DOOR) · airframe 92,552 hrs · 37,348 cycles
DURING CLIMB FROM KRFD TO KTOL, THE LANDING GEAR DOORS LIGHT REMAINED ILLUMINATED AFTER GEAR WAS RETRACTED. THE CREW CYCLED THE GEAR AND THE LIGHT REMAINED ON. THE CREW CONTINUED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE LEFT MAIN LANDING GEAR DOOR STRIKER, THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE IAW DC8 MM 32-12-1.
Part: WIRE — DAMAGED (ZONE 700) · airframe 92,115 hrs · 37,168 cycles
DURING CLIMB FROM KEWR, THE GEAR DOOR LIGHT ILLUMINATED DURING THE UPLATCH CHECK. THE CREW CYCLED THE GEAR. THE DOOR LIGHT REMAINED ON DURING AND AFTER THE UPLATCH CHECK. THE CREW CONTINUED THE FLIGHT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE GEAR SYSTEM AND REPLACED WIRE FROM GYRO BAY TO DOOR LIGHT DIMMER. PERFORMED OPERATIONAL CHECK WAS GOOD. RETURNED AIRCRAFT TO SERVICE.
Part: UNKNOWN — MALFUNCTIONED (MLG) · airframe 91,635 hrs · 36,937 cycles
DURING CLIMB-OUT OF KTOL, THE GEAR DOOR WARNING LIGHT ILLUMINATED AFTER A SATISFACTORY GEAR UP-LATCH CHECK. THE CREW RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE MAIN LANDING GEAR DOOR SYSTEM AND REPLACED THE DOOR ACTUATORS, CONTROL VALVES, DOOR WARNING SWITCHES AND RIGGED BOTH LEFT AND RIGHT MAIN LANDING GEAR DOORS. THE OPERATIONAL CHECK AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: LIMIT SWITCH — DAMAGED (ZONE 700) · airframe 91,557 hrs · 36,908 cycles
DURING CLIMB-OUT OF KTOL, AFTER SATISFACTORY UPLATCH CHECK, THE MAIN LANDING DOOR LIGHT REMAINED ILLUMINATED. THE CREW COMPLIED WITH THE ABNORMAL PROCEDURES AND CONTINUED THE FLIGHT TO KSJC AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED WIRING OF THE RIGHT AND LEFT LANDING GEAR DOOR LIMIT SWITCHES. NO PROBLEMS NOTED. DOOR WARNING SYSTEMS OPS CHECK NORMAL. DUE TO HISTORY MAINTENANCE REPLACED RIGHT LANDING GEAR DOOR LIMIT SWITCH. PERFORMED MAIN LANDING GEAR DOOR LIMIT SWITCH TEST PER DACO MM 32-60-0. SYSTEM OPS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: SWITCH — CONTAMINATED (MLG) · airframe 91,544 hrs · 36,902 cycles
DURING TAKEOFF FROM KTOL, THE DOORS NOT LATCHED LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. THE CREW ACCOMPLISHED THE UNSATISFACTORY UP-LATCH PROCEDURE AND THE DOORS NOT LATCHED LIGHT REMAINED ON. THE CREW CONTINUED THE FLIGHT TO KLAX AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE WIRES ON THE LANDING GEAR DOOR WARNING IAW W/D 32-01-00. ALL WIRES RESISTANCE CHECKS WERE GOOD. MAINTENANCE FOUND BOTH SWITCHES HAD RESIDUAL DE-ICE FLUID THAT WAS CLEANED. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF DOOR WARNING SYSTEM SEVERAL TIMES. THE OPERATIONAL CHECK WAS GOOD IAW UAL MM 32-60-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
Earlier reports · 1996–2006 · 220 reports
2006
Part: LANDING GEAR — OUT OF ADJUST · airframe 91,356 hrs · 36,087 cycles
AFTER TAKEOFF FROM KRFD, THE LANDING GEAR DOOR LIGHT REMAINED ON AFTER GEAR UPLATCH CHECK. THE CREW CYCLED THE GEAR AND THE LIGHT STAYED ON. THE CREW PERFORMED THE UNSAFE GEAR-UP OR DOOR INDICATION ABNORMAL PROCEDURE, AND CONTINUED THE FLIGHT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE JACKED THE AIRCRAFT AND FOUND THE RIGHT MAIN GEAR DOOR NOT FULLY CLOSED WITH GEAR UP. MAINTENANCE ADJUSTED THE RIGHT MAIN GEAR DOOR FOLLOW-UP MECHANISM IAW DACO DC8 MM 32-31-5. THE OPERATIONAL CHECK GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: CONNECTOR — DIRTY (RT MLG DOOR) · airframe 91,347 hrs · 36,804 cycles
AFTER TAKEOFF FROM KSJC, THE GEAR DOOR LIGHT CAME ON WITH GEAR UP AND LOCKED. THE CREW RECYCLED THE LANDING GEAR AND THE LIGHT CAME BACK ON SEVERAL SECONDS AFTER GEAR WAS UP AND LOCKED. LIGHT FLASHED ON AND OFF DURING GEAR UPLATCH CHECK, THEN CAME ON STEADY. NO INDICATION OF GEAR DOORS ACTUALLY BEING OPEN. THE CREW CONTINUED THE FLIGHT AND LANDED AT KRFD WITHOUT INCIDENT. MAINTENANCE INSPECTED THE GEAR DOOR SWITCHES AND STRIKERS. FOUND RIGHT DOOR SWITCH AND PLUG DIRTY AND CORRODED, CLEANED SWITCH AND CONNECTOR. GEAR DOOR LIGHT INDICATION OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE IAW DC8 MM 32-60-0.
Part: SKIN — DAMAGED (ZONE 100) · airframe 90,754 hrs · 36,542 cycles
DURING PREFLIGHT INSPECTION FOUND AIRCRAFT SKIN DAMAGED ON THE RIGHT HAND SIDE BELOW THE LAV SERVICE DOOR. REPAIRED SKIN PER DC8 SRM 53-2-1.
Part: LANDING GEAR — LACK OF LUBE (NOSE) · airframe 90,754 hrs · 36,542 cycles
DURING TAKEOFF FROM KDFW THE AIRCRAFT FAILED THE GEAR UPLATCH CHECK. THE CREW PERFORMED THE UNSATISFACTORY UPLATCH CHECKLIST AND RECYCLED THE GEAR, AGAIN FAILING THE UPLATCH CHECK. THE CREW ELECTED TO RECYCLE THE GEAR AGAIN AND THE UPLATCH CHECK WAS SUCCESSFUL. THE CREW CONTINUED THE FLIGHT AND PERFORMED A ROUTINE LANDING AT KIAH. MAINTENANCE JACKED THE NOSE GEAR, INSPECTED, AND LUBED THE NOSE GEAR, OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: ACTUATOR — MALFUNCTIONED (NLG STEERING) · airframe 90,587 hrs · 36,473 cycles
ON TAKEOFF UNABLE TO KEEP AIRCRAFT ON CENTERLINE WITH RUDDER PEDALS. REJECTED TAKEOFF AT 90 KTS IN NOSE WHEEL STEERING RUDDER PEDALS VERY SLOW TO REACT. MAINTENANCE REMOVED AND REPLACED BOTH LT AND RT STEERING ACTUATORS RE-RIGGED SYSTEM AND OP CHECK OK. AIRCRAFT WAS RETURNED TO SERVICE.
Part: O-RING — FAILED (HYD SYSTEM) · airframe 89,883 hrs · 36,219 cycles
DURING FLIGHT 817 FROM KMCO TO RATL AFTER TAKEOFF A LOSS OF HYDRAULICS OCCURED. RAN LOSS OF HYDRAULIC EMERGENCY CHECK LIST. DUE TO INTENDED FLIGHT PLAN, CREW ELECTED TO RETURN TO DEPARTURE STATION KMCO AND LANDED WITHOUT INCIDENT. FOUND RIGHT AILERON CYLINDER SWIVEL O-RING BLOWN. REMOVED AND REPLACED O-RINGS, OPS AND LEAK CHECK WERE GOOD. SERVICED HYDRAULIC SYSTEM. THIS WORK WAS PERFORMED PER ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE.
2005
Part: UPLOCK — LACK OF LUBE (NLG) · airframe 89,729 hrs · 36,162 cycles
DURING CLIMB OUT, UNSATISFACTORY UPLATCH CHECK, NOSE GEAR IS EXTENDING DURING UPLATCH CHECK. CREW RETURNED AIRCRAFT TO DEPARTURE AND LANDED WITH NO INCIDENT. MAINTENANCE LUBED THE UPLATCH MECHANSIM AND CHECKED OPERATION OF UPLATCH BY GEAR RETRACTION. AN UPLATCH CHECK WAS PERFORMED SEVERAL TIMES AS WELL AS NOSE WHEEL EXTENSION/RETRACTION. OPS CHECK WAS GOOD IAW ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE.
Part: HSI — INOPERATIVE (COCKPIT) · airframe 89,713 hrs · 36,156 cycles
ON CLIMB-OUT FROM KTOL, FO'S ADI/HSI WAS INOP. CREW RETURNED AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET C/B AND GYRO PER ALL APPLICABLE MANUALS AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.
Part: SKIN — CRACKED (XE 200.2379) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, LT HORIZ STAB ELEVATOR UPPER SKIN CRACKED ½, XE 200.2379. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3. REMOVED FASTENERS IAW DC8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4085. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D EXTERNAL REPAIR DOUBLER (AL2024T3 0.040), FILLER (AL2024T3 0.016) IAW SEMAN DWG # ED-4085. CLEANED, TREATED, PRIMED AREA + FILLER + INNER SIDE OF EXTERNAL REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SEMAN DWG # ED-4085, DC8 SRM 51-1-21. PERFORMED LT ELEVATOR BALANCING IAW DC8 SRM 51-4-1 PG 1. FOUND WITHIN TOLER
Part: SKIN — ELONGATED (YN 254 S) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECTION, NR 4 PYLON UPPER PLATING HAS ELONGATED HOLES AT STA YN 254 S. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05471 DATED 10-18-05, SEMAN DWG # ED-4084 DATED 10-11-05 AND EO SEMAN # 20051341 DATED 10-18-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4084. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D (02EA) EXTERNAL REPAIR DOUBLERS (AL7075T6 0.100) + (02EA) FILLERS (AL7075T6 0.100) + FILLER (AL7075T6 0.032) IAW SEMAN DWG # ED-4084. CLEANED, TREATED, PRIMED FILLERS + INNER SIDE OF REPAIR DOUBLERS IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51
Part: FITTING — CRACKED (XW 410.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, RT FLAP SUPPORT FITTING CRACKED AT STA. XW 410.000. REMOVED AND REPLACED RT FLAP LINK SUPPORT AT STA XW 410.000 IAW DC8 MM 27-51-12 PAGES 201-204. REFER TO N/R FOR OPS CHECK.
Part: SKIN — UNBONDED (ZRT 98) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, LT RUDDER TAB SKIN UNBONDED 2 AT STA ZRT 98. REMOVED DAMAGED SKIN, CORE SECTION IAW DC8 SRM 55-2-2 PART 2 PAGE 1. FAB`D REPAIR CORE PLUG (AL. HONEY COMB CORE), REPAIR DOUBLER (ALCLAD 2024 T3 0.012) IAW DC8 SRM 55-2-2 PAR 2 PAGE 1. BONDED REPAIR CORE PLUG, REPAIR DOUBLER WITH HUSOL IAW DC8 SRM 55-2-2 PAGE 2, DC8 SRM 51-1-9 PAR 4. REFER TO N/R 2801 FOR WEIGHT AND BALANCE.
Part: VANE — ELONGATED (TE FLAPS) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, RT WING CTR L/E SLOT VANE HAS ELONGATED HOLES AT STA XILD 7095. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05461 DATED 10-10-05, SEMAN DWG NR ED-4081 DATED 10-08-05, EO SEMAN NR 20051290 DATED 10-10-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW SEMAN DWG NR ED-4081. NDT INSPECTED IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D EXTERNAL REPAIR DOUBLER, FILLER & INTERNAL DOUBLER IAW SEMAN DWG NR ED-4081. CLEANED, TREATED, INSTALLED REPAIR PARTS IAW SEMAN DWG NR ED-4081, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-20D, DC8 SRM 51-3-1 (TQ).
Part: SKIN PANEL — MISREPAIRED (STA 8.000-17.000) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECTION, EXT FS NON STANDARD REPAIR, STA 8.000 STA 17.000 BTWN L-15 AND L-16L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05447 DATED 10-05-05, SEMAN DWG # ED-4077 DATED 10-01-05 AND EO SEMAN # 20051295 DATED 10-05-05. REMOVED EXISTING DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED AREA IAW SEMAN DWG # ED-4097. PERFORMED NDT INSPECT ON AFFECTED AREA IAW DC8 NDT SPM PART 06-10-01-001. NO CORROSION NEITHER CRACK FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.071), 02 INTERNAL FINGER DOUBLERS (AL7075T6 0.032), FILLER (AL7075T6 0.050) IAW SEMAN DWG NR ED-4077. CLEANED, TREATED, PRIMED AREA + REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-
Part: DOUBLER — IMPROPER (FS 279.000) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, LT FUS FWD CTR SECTION LWR PLATING BASKET DOOR FWD JAMB EXISTING REPAIR DBLR NOT ACCOMP 3 ROWS FASTENERS PAST CUT OUT STA FS 279.000 L-35.5L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05461. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. PERFORMED DETAIL VISUAL INSP. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER AND FILLER IAW SEMAN DWG # ED-4079. CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SEMAN DWG # ED-4079, DC8 SRM 51-1-20D, DC8 SRM 51-1-21, DC8 SRM 51-3-1.
Part: FITTING — CRACKED (FS 74.000S.51) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, LT WING NR 2 MAIN TANK FITTING CRACKED, FS 74.000 S.51 (FWD EXTERNAL PART). REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. CLEANED AND APPLIED POLYURETHANE TOP COATING YELLOW IAW DC8 SRM 51-1-12 PAGES 7-25. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. TORQUED IAW DC8 SRM 51-3-1. FOR LEAK CHECK SEE JC 99116.
Part: REPAIR — MISINSTALLED (BS 272.000) · airframe 89,672 hrs · 36,136 cycles
DURING C-CHECK INSPECT, RT FUSE FWD CTR SECTION LWR PLATING FWD OF A PIT DOOR EXISTING DBLR EXCEED MAX RIVETS SPACING AT BS 272.00 L-31R. PERFORMED MAJOR REPAIR IAW FORM 8110-3 NR 05451, SEMAN DWG NR ED-4078, EO SEMAN 20051296. REMOVED REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTION IAW SEMAN DWG ED-4078. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER & REPAIR TRIPLER & FILLER INTERNAL DOUBLER & FILLER IAW SEMAN DWG ED-4078. CLEANED, TREATED, PRIMED AREA & REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM. INSTALLED REPAIR PARTS IAW SEMAN DWG ED-4078, DC8 SRM 51-1-20D, DC8 SRM 51-3-1.
Part: SKIN PANEL — IMPROPER (WS 960-980.000) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, LT MLG W/W - L-24L HAS NO STANDARD REPAIR BETWEEN BS 960.000 & 980.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-2 FIG 5, TR NR 53-123, EO SEMAN NR 20051282 DATED 09-27-05. REMOVED EXISTING REPAIR IAW DC8 SRM 51-1-20D. STOP DRILLED CRACK END IAW DC8 SRM 53-2-2. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR ANGLE, WASHERS IAW DC8 SRM 53-2-2 FIG 5. HEAT TREATED REPAIR ANGLE IAW DC8 SRM 51-1-1 PG 1, 13, 17. CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-2 FIG 5, DC8 SRM 51-1-20D, DC8 SRM 51-3-1.
Part: RIVET — IMPROPER (FS 1254.000) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1254.000 L-35.5R, UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN NR 20051198 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3). NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.125) + (02 EA) INTERNAL FINGER DOUBLERS (AL7075T6 0.050) IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3), DC8 SRM 53-4-1 FIG 16 (SHEET 1) ITEM âEâ, DC8 SRM 51-10-0 FIG 2, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA +
Part: RIVET — IMPROPER (FS 104) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, FWD LWR FUSELAGE BELLY, FS 104 L-35.75L, UPGRADE EXTERNAL DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN NR 20051192 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3). NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 O.O63â), (02 EA) INTERNAL FINGER DOUBLERS (AL7075T6 0.032â) IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1-3), DC8 SRM 53-4-1 FIG 1 ITEM âCâ, DC8 SRM 51-9-8 FIG 68ª, DC8 SRM 51-1-4 (FORMING). CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM
Part: REPAIR — IMPROPER (FS 1250.00) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, LT FUSELAGE AFT CENTER SECTION WINDOW BELT EVALUATE CONFORMITY PER SRM AT STA FS 1250.00 L-15.5 LT. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 22A, TR # 53-170, EO SEMAN # 20051302 DATED 09-28-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21. FAB`D REPAIR DOUBLER (7073) (AL7075T6 0.190) IAW DC8 SRM 53-2-0 FIG 22A (SHEET 1, 3, 14) DC8 SRM 53-4-1 FIG 19 ITEM A. CLEANED, TREATED, PRIMED AREA + REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG 22A (SHEET 3, 12, 13, 14), DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-1.
Part: RIVET — IMPROPER (FS 222) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, FWD LWR FUSELAGE BELLY, STA FS 222 L-34.75R. UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN NR 20051194 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3). NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.080) + (02 EA) INTERNAL FINGER DOUBLERS (AL7075T6 0.050) IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3), DC8 SRM 53-4-1 FIG 1 ITEM âBâ, DC8 SRM 51-9-0 FIG 68A, DC8 SRM 51-1-4 (FORMING). CLEANED, TREATED, PRIMED AREA + REPAIR PARTS IAW D
Part: DOUBLER — UNKNOWN (FS 1356.00) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, LT FUS AFT CTR SECTION LWR PLATING DOUBLER UPGRADE THICKNESS AT STA FS 1356.00 L-29 RT. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN NR 20051303 DATED 09-29-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 4). NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.090) + (02EA) INTERNAL FINGER DOUBLERS (AL7075T6 0.050) + FILLER (AL7075T6 0.080) IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 4), DC8 SRM 53-4-1 FIG 16 (SHEET 2) ITEM âCâ, DC8 SRM 51-9-0 FIG 68A, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC
Part: DOUBLER — CRACKED (XFS 250.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, RT INNER WING CTR L/E INTERNAL DOUBLER CRACK 3 AT STA XFS 250.000. REMOVED CRACKED INTERNAL DOUBLER IAW DC8 SRM 51-1-21. FABRICATED NEW INTERNAL DOUBLER (AL7075T6 0.063â) IAW DC8 SRM 57-3-1 FIG 3. CLEANED, TREATED, PRIMED AREA, DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED NEW INTERNAL DOUBLER IAW DC8 SRM 51-1-21.
Part: REPAIR — MISINSTALLED (FS 24 L-34LH) · airframe 89,672 hrs · 36,136 cycles
DURING C-CHECK INSPECT, LT NOSE SKIN FWD PAX DOOR JAMB EXISTING DBLR EXCEED OVERAGE RIVETS SPACING AND CHERRY MAX AT STA FS 24 L-36 LT. PERFORMED MAJOR REPAIR IAW FORM 8110-3, SEMAN DWG ED-4077 DATED 10-01-05 AND EO SEMAN 20051295 DATED 10-05-05. REMOVED EXISTING DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED AREA IAW SEMAN DWG NR ED-4097. PERFORMED NDT INSPECTION ON AFFECTED AREA IAW DC8 NDT SPM. NO CORROSION NEITHER CRACK FOUND. FAB`D REPAIR DOUBLER & 02 INTERNAL FINGER DOUBLERS, FILLER IAW SEMAN DWG ED-4077. CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SEMAN DWG NR ED-4077, DC8 SRM 51-1-20D, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-3-1.
Part: REPAIR — IMPROPER (BS 1550.00) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, RT FUSELAGE AFT CENTER SECTION FWD OF R-2 DOOR OPENING EVALUATE CONFORMITY PER SRM AT STA FS 1550.00 L-15.5 RT. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 22A, EO SEMAN NR 20051300 DATED 09-28-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21. FABRICATED REPAIR DOUBLER ( -7073) (AL7075T6 0.190â) IAW DC8 SRM 53-2-0 FIG 22A (SHEET 1, 3, 14), DC8 SRM 53-4-1 FIG 19 ITEM âBâ. CLEANED, TREATED, PRIMED AREA + REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG2A (SHEET 3, 12, 13, 14), DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-1 (TORQUE).
Part: VANE — DAMAGED (TE FLAP) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, RT WING INNER L/E SLOT VANE HAS ELONGATED HOLES AT STA XOLDO 67.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05463. REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER, INTERNAL DOUBLER AND FILLER IAW SEMAN DWG # ED-4082. CLEANED, TREATED, PRIMED AREA, FILLER, INTERNAL DOUBLER, INNER SIDE OF EXTERNAL REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SEMAN DWG # ED-4082, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-20D, DC8 SRM 51-3-1.
Part: RIVET — IMPROPER (FS 1384. L-34-75) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1384.000 L-35-75R, UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN # 20051199 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1-3). PERFORMED NDT INSP OF REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.080â), (02 EA) INTERNAL FINGER DOUBLERS (AL7075T6 0.050â) IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1-3), DC8 SRM 53-4-1 FIG 16 (SHEET 2) ITEM âBâ, DC8 SRM 51-9-0 FIG 68. CLEANED, TREATED, PRIMED AREA, REPAIR PARTS
Part: DOOR — CRACKED (FS 54.000) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, LT FUSE NOSE SECTION PLATING FREON SYS EXHAUST DOOR UPPER AFT JAMB CORNER CRACK DAMAGE AT STA FS 54.000, L-28L TO L-29L. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 13. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-0 FIG 13. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL2024T3 0.071) + FILLER (AL2024T3 0.050) IAW DC8 SRM 53-2-0 FIG 13. CLEANED, TREATED, PRIMED AREA + REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0 FIG 13.
Part: RIVET — IMPROPER (FS 1693.) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1693 L-30.75R. UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN # 20051202 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 5). NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.063â), INTERNAL FINGER DOUBLER (AL7075T6 0.032â), FILLER (AL7075T6 0.050â) IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 5), DC8 SRM 53-5-1 ITEM âEâ FIG 1, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51
Part: FASTENER — IMPROPER (BS 180.000) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, EXTERNAL FS REPAIR FASTENERS IMPROPER AND RIVETS EXCEED ALLOWABLE LIMITS, STA 180.000 L-19R. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN 20051309 DATED 09-29-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3). NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.071) + (04EA) INTERNAL FINGER DOUBLERS (AL7075T6 0.040â) IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3), DC8 SRM 53-4-1 FIG 6 ITEM âAâ, DC8 SRM 51-9-0 FIG 68A, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS IAW DC8 SRM 51-1-8
Part: DOUBLER — CORRODED (BS 880.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT MLG W/W PRESSURE PANEL DOUBLER CORRODED, STA 880.000 RBL 2â. REMOVED CORROSION FROM DOUBLER IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PG 2P. REMOVED CORRODED DOUBLER IAW DC8 SRM 51-1-21. FABRICATED NEW DOUBLER (AL7075T6 0.050â) IAW DC8 SRM 53-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA + DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED DOUBLER IAW DC8 SRM 51-1-21.
Part: RIVET — IMPROPER (FS 1693) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1693.000 L-30.75L. UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN # 20051203 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 5). NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.063â), INTERNAL FINGER DOUBLER (AL7075T6 0.032â), FILLER (AL7075T6 0.050â) IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 5), DC8 SRM 53-5-1 ITEM âEâ FIG 1, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA + REPAIR PARTS IAW DC8 S
Part: DOUBLER — CORRODED (XFS 847.500) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, LT OUTER WING, OTBD L/E ACCESS DOOR INTERNAL DOUBLER CORRODED, XFS 847.500. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PG 16. REMOVED CORRODED INTERNAL DOUBLER IAW DC8 SRM 51-1-21. FAB`D NEW DOUBLER (AL7075T6 0.160) IAW DC8 SRM 57-3-1 FIG 7 ITEM Q. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED INTERNAL DOUBLER IAW DC8 SRM 51-1-21.
Part: RIVET — IMPROPER (FS 1544.000) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1544.000 L-35.5L, UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN # 20051200 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3). NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.080â) + (02 EA) INTERNAL FINGER DOUBLERS (AL7075T6 0.050â) IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3), DC8 SRM 53-4-1 FIG 16 (SHEET 2) ITEM âBâ, DC8 SRM 51-9-0 FIG 68A, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED,
Part: FITTING — CRACKED (FS 74.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C-CHECK INSPECTION, LEFT WING NR 2 MAIN TANK FITTING CRACKED, FS 74.000 S.51 (FWD INTERNAL PART). REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. CLEANED AND APPLIED POLYURETHANE TOP COATING YELLOW IAW DC8 SRM 51-1-12 PAGES 7-25. INSTALLED NEW FITTING WITH FASTENERS (HI-LOKS) AND TORQUED NUTS IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1.
Part: DOUBLER — IMPROPER (XW 105.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C-CHECK INSPECTION, LEFT INBOARD FLAP L/E UPPER SKIN HAS NON STANDARD REPAIR, XW 105.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1, EO SEMAN 20051209. REMOVED DAMAGED PANEL PLATING IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 51-1-21. FABRICATED NEW PANEL PLATING (AL2024T3 0.025) + BONDED FINGER DOUBLER (AL2024T3 0.020) IAW DC8 SRM 57-7-1 FIG 1. BONDED PARTS WITH HYSOL IAW DC8 SRM 51-1-9, DC8 SRM 51-1-9A, DACO DPS 1.950. CLEANED, TREATED, PRIMED NEW PANEL PLATING INNER FACE IAW DC8 SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED NEW PANEL PLATING IAW DC8 SRM 51-1-21.
Part: SKIN — IMPROPER (XF 230.000) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECTION, RT OTBD FLAP UPPER SKIN HAS NON STANDARD REPAIR, STA XF 230.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05447 DATED 10-05-05, SEMAN DWG # ED 4072 DATED 10-01-05, EO SEMAN # 20051298 DATED 10-05-05. REMOVED EXISTING NON STANDARD REPAIR IAW DC8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4072. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D NEW PLATING SEGMENT (AL2024T3 0.071â), INTERNAL SPLICE (AL2024T3 0.080â, (02EA) EXTERNAL DOUBLERS (AL2024T3 0.080â) IAW SEMAN DWG NR ED-4072, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES
Part: DOUBLER — CRACKED (XFS 342.500) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C-CHECK INSPECTION, LEFT WING CTR L/E LWR INTERNAL DOUBLER CRACK 2 AT STA XFS 342.500. REMOVED CRACKED INTERNAL DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. FABRICATED NEW INTERNAL DOUBLER (AL7075T6 0.090â) IAW DC8 SRM 57-3-1 FIG 4. CLEANED, TREATED, PRIMED AREA + INTERNAL DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED INTERNAL DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-1.
Part: SKIN — IMPROPER (FS 360.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, FWD FUSELAGE CTR LWR PLATING AFT OF FWD BASKET DOOR EXISTING REPAIR ALL SIDES EXCEED MAXIMUM RIVETS SPACING AT STA FS 360.000 L-36. INSTALLED HILOKS IAW FAA FORM 8110-3 # 05448 DATE 10-05-05, SEMAN DWG ED 4080 DATE 10-03-05 EO SEMAN 20051310 DATE 10-05-05 DC8 SRM 51-1-20D, DC8 SRM 51-3-1. THE HILOKS WERE INSTALLED ON CTR LWR PLATING ALT OF FWD BASKET DOOR REPAIR.
Part: FITTING — IMPROPER (BS 897.375) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C-CHECK INSPECTION, RIGHT MLG W/W - L-24R FITTING HAS NO STANDARD REPAIR AT STA 879.375. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 8. REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-20D. FABIRCATED (4) REPAIR FITTING (P/N 5802677-4) FROM AL7075T7351 IAW DC8 SRM 53-2-0 FIG 8 (SHEET 1, 3, 6). CLEANED, TREATED, PRIMED AREA + REPAIR FITTING IAW DC8 SRM 51-1-8B. INSTALLED REPAIR FITTING IAW DC8 SRM 53-2-0 FIG 8 (SHEET 1, 3, 6) DC8 SRM 51-1-20D, DC8 SRM 51-3-1 (TORQUE).
Part: PAN — CRACKED (XS 250.089) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, RT INNER WING OUTBD L/E ZEE PAN CRACK 2â AT STA XS 250.089. REMOVED CRACKED SPLICE PAN IAW DC8 SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW SPLICE PAN IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D.
Part: SKIN — DENTED (XFS 78.750-85.00) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, LT HORIZONTAL STABILIZER L/E UPPER SKIN DENTED, XFS 78.750 XFS 85.00. PERFORMED MAJOR REPAIR IAW DC8 SRM 55-2-1 FIG 4, EO SEMAN # 20051292 DATED 09-27-05. REMOVED EXISTING REPAIR DOUBLER NEXT DENT IAW DC8 SRM 51-1-21. REMOVED DAMAGED AREA IAW DC8 SRM 55-2-1 FIG 4. PERFORMED NDT INSPECTION TO INDICATED AREA, NO CRACK, CORROSION FOUND IAW NDT SPM PART 06-10-01-001. FAB`D REPAIR DOUBLER, FILLER (AL7075T6 O.O50â) IAW DC8 SRM 55-2-1 FIG 4, DC8 SRM 55-3-1 FIG 1 ITEM âAâ. CLEANED, TREATED, PRIMED AREA + REPAIR DOUBLER INTERNAL PART IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR DOUBLER IAW DC8 SRM 55-2-1- FIG 4, DC8 SRM 51-1-2
Part: SKIN — DENTED (XW 77.000) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, LT INBD FLAP UPPER SKIN DENTED, XW 77.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 1, EO SEMAN #20051207 DATED 09-21-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW DC8 SRM 57-2-5 FIG 1. PERFORMED DETAIL VISUAL INSP OF REWORK AREA. NEITHER CRACK NOR CORROSION FOUND. FAB`D NEW PLATING SEGMENT (AL2024T3 0.050â), (02EA) INTERNAL SPLICES (AL2024T3 0.063â), FILLER (AL2024T3 0.020â) IAW DC8 SRM 57-2-5 FIG 1 (SHEET 1-2), DC8 SRM 57-7-1 FIG 1 ITEM âAâ. CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-3-1.
Part: SKIN — IMPROPER (XF 210.000) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECTION, RT OTBD FLAP UPPER SKIN HAS NON STANDARD REPAIR, STA XF 210.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 4, TR#57-94, EO SEMAN # 20051288 DATED 09-28-05. REMOVED DAMAGED PLATING IAW DC8 SRM 57-1-0, DC8 SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040â) IAW DC8 SRM 57-7-1 FIG 4, TR#57-94 ITEM âCâ, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA + NEW PLATING INNER FACE IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW DC8 SRM 51-1-11 PG 9. INSTALLED NEW PLATING IAW DC8 SRM 51-1-21.
Part: SKIN PANEL — BROKEN (BS 70) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECTION, LT FUSELAGE NOSE SECTION LWR PLATING UPPER AFT CORNER BROKEN OFF AT BS 70 L-33. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-2 FIG 8C-2, TR NR 53-176, EO SEMAN NR 20051299 DATED 09-29-05. PERFORMED DETAIL VISUAL INSPECT. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER IAW DC8 SRM 53-2-5 FIG 8C-2, DC8 SRM 53-2-5 FIG 8B-2, DC8 SRM 53-3-1 FIG 1 ITEM A, DC 8 SRM 53-4-1 FIG 1 ITEM C, DC8 SRM 51-9-0 FIG 68A. INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-5 FIG 8C-2, DC8 SRM 51-1-20D, DC8 SRM 51-3-1.
Part: SKIN — IMPROPER (XW 91.000) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, LT INBD FLAP L/E UPPER SKIN HAS NON STANDARD REPAIR, XW 91.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05446 DATED 10-05-05, SEMAN DWG # ED 4065 DATED 09-27-05, EO SEMAN # 20051208 DATED 10-05-05. REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4065. PERFORMED NDT INSP OF REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D NEW PLATING SEGMENT (AL2024T3 0.040â), INTERNAL SPLICE (AL2024T3 0.050â), (02EA) EXTERNAL DOUBLERS (AL2024T3 0.050â) IAW SEMAN DWG # ED-4065, DC8 SRM 51-1-4 (FORMING). CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED
Part: DOUBLER — CRACKED (XFS 341.500) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECTION, LT WING CTR L/E LWR PART INTERNAL DOUBLER CRACKED 7, XFS 341.500. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05463 DATED 10-11-05, SEMAN DWG # ED-4083 DATED 10-10-05, EO SEMAN # 20051312 DATED 10-11-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4083. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D EXTERNAL REPAIR DOUBLER (AL7075T6 0.071) + NEW INTERNAL DOUBLER SEGMENT (AL7075T6 0.080) + (02EA) INTERNAL STRAPS (AL7075T6 0.050) IAW SEMAN DWG # ED-4083. CLEANED, TREATED, PRIMED AREA + REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FA
Part: SKIN — IMPROPER (XW 435.000) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECTION, LT OTBD FLAP UPPER SKIN HAS NON STANDARD REPAIR, XW 435.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 1, EO SEMAN # 20051210 DATED 09-21-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW DC8 SRM 57-2-5 FIG 1. PERFORMED DETAIL VISUAL INSP OF REWORKED AREA. NEITHER CRACK NOR CORROSION FOUND. FAB`D NEW PLATING SEGMENT (AL2024T3 0.050â), SPLICE (AL2024T3 0.063â), FILLER (AL2024T3 0.020â) IAW DC8 SRM 57-2-5 FIG 1 (SHEET 1-2), DC8 SRM 57-7-1 FIG 4, TR#57-94 ITEMS âQâ, âVâ. CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-5 FIG
Part: REPAIR — IMPROPER (FS 245.00) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECTION, LT FUSELAGE FWD CENTER SECTION WINDOW BELT EVALUATE CONFORMITY PER SRM AT STA FS 245.00 L-15.5 LT. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 22A, TR # 53-170, EO SEMAN # 20051301 DATED 09-28-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-20D. FAB`D REPAIR DOUBLER (AL7075T6 0.100) IAW DC8 SRM 53-2-0 FIG 22A (SHEET 1, 10, 15) TR # 53-170, DC8 SRM 53-4-1 FIG 6 ITEM B, DC8 SRM 51-9-0 PAG 68A. CLEANED, TREATED, PRIMED AREA + EXT. REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED EXT REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG 22A (SHEET 1, 10, 12, 13, 15), DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-1 (TORQUE).
Part: SKIN — IMPROPER (ZONE 600) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECTION, RT WING INBD FLAP UPPER SKIN HAS NON STANDARD REPAIR. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 1, EO SEMAN NR 20051279 DATED 09-26-05. REMOVED DAMAGED PLATING IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.050â) IAW DC8 SRM 57-7-1 FIG 1 ITEM âFâ, DC8 SRM 51-1-4 (FORMING). CLEANED, TREATED, PRIMED AREA, NEW PLATING INNER FACE IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW DC8 SRM 51-1-11 PG 9. INSTALLED NEW PLATING IAW DC8 SRM 51-1-21.
Part: RIVET — OUT OF TOLERANCE (FS 10 L-22) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, LT FUSELAGE NOSE SECTION PLATING DOUBLER REPAIR EXCEED MAX RIVETS SPACING STA FS 10 L-22 LT. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05448 DATED 10-05-05, SEMAN DWG # ED 4076 DATED 10-03-05, EO SEMAN # 20051294 DATED 10-05-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21 PG 1, DC8 SRM51-1-20D. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4076. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL7075T6 0.071â, FINGER DOUBLER (AL7075T6 0.032â) IAW SEMAN DWG # ED-4076. CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED R
Part: SKIN — CRACKED (XRS172.000) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, LT WING LWR SKIN CRACK AT STA XRS 172.000 BETWEEN S-56 AND S-57. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 1, EO SEMAN # 20051287 DATED 09-29-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. STOP DRILLED CRACK END IAW DC8 SRM 57-2-1A FIG. 1 PAR. 7. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D EXTERNAL REPAIR DOUBLER (AL7075T6 0.080â) IAW DC8 SRM 57-2-1A FIG 1, DC8 SRM 51-3-1 FIG 26 ITEM âAâ. CLEANED, TREATED, PRIMED AREA, INNER SIDE OF EXTERNAL REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED EXTERNAL REPAIR DOUBLER IAW DC8 SRM 57-2-1A FIG 1, DC8 SRM
Part: SKIN — CRACKED (XW255.000) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECTION, NR 3 RT STUB WING LWR SKIN CRACK 2 AT STA XW 255.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 37, EO SEMAN NR 20051284 DATED 09-27-05. REMOVED FASTENERS IAW DC8 SRM 51-1-20D. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-1 FIG 2G. FAB`D REPAIR DOUBLER (AL7075T6 0.125â) IAW DC8 SRM 57-2-1 FIG 37. TAPERED DOUBLER FROM 0.125â TO 0.050â IAW DC8 SRM 57-2-1 FIG 37 NOTE 7. CLEANED, TREATED AND PRIMED AREA, REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-1 FIG 37, DC8 SRM 51-1-20D, DC8 SRM 51-3-1.
Part: SKIN — SCRATCHED (ZONE 800) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, EXTERNAL FUS. (C) BELLY PIT DOOR SKIN SCRATCHES OUT OF LIMITS. PERFORMED MAJOR REPAIR, REMOVED FASTENERS IAW SRM 51-1-20D. REMOVED DAMAGED SECTION IAW DWG NR ED-4075. NDT INSPECTED IAW NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL7075T6 0.190â) + FILLER PLUG (AL7075T6 0.250â) IAW DWG NR ED-4075. TAPERED REPAIR DOUBLER FROM 0.190 TO 0.08 IAW DWG ED-4075. CLEANED, TREATED, PRIMED AREA + REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW DWG NR ED-4075, SRM 51-1-20D, SRM 51-3-0, SRM 51-3-1 (TORQUE) FOR FUEL LEAK CK.
Part: FITTING — CORRODED (60.070.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, FWD ACCY COMPT FITTING CORRODED, STA 60.000, 70.000 L-34R. REMOVED CORROSION FROM FITTING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FITTING IAW SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-21 AND TORQUED NUTS IAW SRM 51-3-1 PG 2A.
Part: FITTING — CORRODED (60.-70.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, FWD ACCY COMPT, FITTING CORRODED, STA 60.000, 70.000 L-34R. PERFORMED MAJOR REPAIR IAW MSG NR 1-126059161-2 DATED 09-26-05, SRM 52-1-0 PG 1. REMOVED DAMAGED SKIN IAW SRM 51-1-21. FABRICATED NEW SKIN (AL7075T6 0.050) IAW MSG NR 1-126059161-2, SRM 52-4-1 FIG 1 ITEM Q. CLEANED, TREATED AND PRIMED AREA + NEW SKIN IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN IAW SRM 51-1-21, SRM 51-3-0, SRM 51-3-1 (TORQUE).
Part: FITTING — CRACKED (BS 834.5) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT. AFT FITTING CRACKED 3, STA 834.5 L-14RREMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9, SRM 51-3-1 (TORQUE).
Part: LONGERON — CRACKED (1786.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C-CHECK INSPECTION, AFT FUSELAGE LONGERON 17L CRACKED 1, STA 1786.000PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, EO SEMAN NR 20051285 DATED 09-27-05. REMOVED CRACKED LONGERON IAW SRM 51-1-20D. FABRICATED NEW LONGERON (EXTRUSION P/N S1616757) IAW SRM 53-5-1 FIG 7 (SHEET 1) ITEM B, SRM 51-0 FIG 50 (SHEET 37). CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11 PG 9. INSTALLED NEW LONGERON IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE), SRM 51-1-21.
Part: LONGERON — CRACKED (1786.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE LONGERON 17R CRACKED 1, STA 1786.000. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, EO SEMAN NR 20051286 DATED 09-27-05. REMOVED CRACKED LONGERON IAW SRM 53-5-1 FIG 7 (SHEET 1) ITEM B SRM 51-2-0 FIG 5 (SHEET 37). CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11 PG 9. INSTALLED NEW LONGERON IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE), SRM 51-1-21.
Part: FITTING — CRACKED (781.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT FWD FITTING CRACKED 2, STA 781.000 L-19L. REMOVED CRACKED FITTING IAW SRM 51-1-20D. FABRICATED NEW FITTING (AL7075T651) IAW MFG DWG NR 3779978, EA NR 20051313. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE).
Part: FITTING — CRACKED (1770.00) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE SPLICE FITTING CRACKED 2, STA 1770.000 RT, L-17R. REMOVED CRACKED FITTING IAW SRM 51-3-0, SRM 51-21-1. FABRICATED NEW FITTING (AL7075T651) IAW ATI REPAIR SPECIFICATION NR 2003-05, EA SEMAN NR 20051318. HEAT TREATED FROM AL7075T651 TO AL7075T6 IAW SRM 51-1-1 PG 1, 13, 17. (ENCLOSED SMN FORM NR 075) + PERFORMED NDT INSPECTION OF NEW FITTING IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA + NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-3-0, SRM 51-3-1 (TORQUE).
Part: FITTING — CRACKED (445.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, FWD LOWER FUSELAGE SPLICE FITTING CRACKED 8, STA 445, STA 455.000 L-31L. REMOVED CRACKED FITTING IAW SRM 51-1-20D, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-0 PAGE 1. TORQUED IAW SRM 51-3-1 PAGE 2A.
Part: SKIN — CRACKED (XA 470.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, RT IB AIL L/E UPPER PLATING CRACK .2500 AT STA XA 470.000. PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 1, EO SEMAN NR 20051280 DATED 09-26-05. REMOVED DAMAGED PLATING IAW SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040) IAW SRM 57-8-1 FIG 1 ITEM E, SRM 51-1-4 PG 1 (FORMING). CLEANED,TREATED, PRIMED AREA + INNER FACE OF NEW PLATING IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11 PG 9. INSTALLED NEW PLATING IAW SRM 51-1-21.
Part: FITTING — CRACKED (902.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT FITTING CRACKED 1.5, STA 902.000 L-19L. REMOVED CRACKED FITTING IAW SRM 51-1-20D. FABRICATED NEW FITTING (AL7075T651) IAW MFG DWG NR 3779498, EA NR 20051314. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA, NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE).
Part: FITTING — CRACKED (1215.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, AFT LWR CARGO BILGE INTERIOR, FITTING CRACKED 2, STA 1215.000 L-29R. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG 1. CLEANED, TREATED, PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1.
Part: FITTING — CRACKED (445.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, FWD LOWER FUSELAGE. SPLICE FITTING CRACKED 2 , STA 445.000, STA 455.000 L-31R. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D AND TORQUED IAW SRM 51-3-1.
Part: SKIN — CORRODED (XFS 710.000) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECTION, RT OUTER WING INBD L/E UPPER SKIN CORRODED, STA XFS 710.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05461 DATED 10-10-05, SEMAN DWG # ED-4070 DATED 10-07-05, EO SEMAN # 20051276 DATED 10-10-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED CORROSION ON RH OUTER WING I/B L/E UPPER SKIN, STA XFS 710.000 IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-1 FIG 2G. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4070. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.063â) + FILLER (AL7075T6 0.050) IAW SEMAN DWG # ED-4070. CLEANED, TREATED, PRIMED AREA + FILLER + INNE
Part: SKIN — CORRODED (XFS 304-310.000) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, LT WING CTR UPPER L/E CORRODED, STA XFS 304 310.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 44, EO SEMAN # 20051213 DATED 09-22-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-1 FIG 26. REMOVED CORRODED SECTION IAW DC8 SRM 57-2-1 FIG 44 (SHEET 2, 5) TR #57-102. PERFORMED NDT INSP OF REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.063â) IAW DC8 SRM 57-2-1 FIG 44 (SHEET 2, 5, 6, 8) TR # 57-102, DC8 SRM 57-3-1 FIG 4 SHEET 1 ITEM âAâ. CLEANED, TREATED, PRIMED INTERNAL FACE OF REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO
Part: FITTING — CRACKED (445.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT RT TUNNEL SPLICE FITTING CRACKED 2, STA 445.000 L-27R REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D AND TORQUED NUT IAW SRM 51-3-1 PAGE 2A.
Part: VANE — ELONGATED (XS 520.168) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, LT WING OTBD SLOT VANE HOLES ELONGATED, STA XS 520.168. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05447 DATED 10-05-05, SEMAN DWG # ED-4064 DATED 09-30-05, EO SEMAN # 20051206. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4064. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.071), INTERNAL DOUBLER, FILLER (AL7075T6 0.063) IAW SEMAN DWG NR ED-4064, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA, INNER SIDE OF REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW
Part: FITTING — CRACKED (857.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT. AFT FITTING CRACKED 1, STA 857.000 L-19LREMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1. (TORQUE)
Part: SKIN — CRACKED (XFS 597.500) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, RT OUTER WING IB L/E LOWER SKIN, .2500 IN CRACK, STA XFS 597.500. PERFORMED MAJOR REPAIR DATED 10-07-05, DWG NR ED-4069 DATED 10-06-05, EO NR 20051275 DATED 10-07-05. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. PERFORMED STOP DRILL OF 0.250 AT CRACK END IAW DWG NR ED-4069. NDT INSPECTED REWORKED AREA IAW NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL7075T6 0.063) IAW DWG NR ED-4069. CLEANED, TREATED, PRIMED AREA, REPAIR DOUBLER INNER SIDE IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR DOUBLER IAW DWG NR ED-4069, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0, SRM 51-3-1 (TORQUE).
Part: SKIN — CRACKED (XFS 285.250) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, LT WING CTR L/E SKIN CRACKED ½, STA XFS 285.250. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05451 DATED 10-07-05, SEMAN DWG # ED-4066 DATED 10-03-05, EO SEMAN # 20051212 DATED 10-07-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4066. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL7075T6 0.071) + FILLER (AL7075T6 0.063) IAW SEMAN DWG NR ED-4066, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SEMAN DWG # ED-406
Part: SKIN — CRACKED (XFS 566.250) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECTION, RT WING OTBD L/E LOWER SKIN CRACKED 1â APPROX, BETWEEN STA XFS 566.250 AND XFS 572.500. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05446 DATED 10-05-05, SEMAN DWG # ED-4068 DATED 09-27-05, EO SEMAN # 20051231 DATED 10-05-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4068. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.063â), FILLER (AL7075T6 0.050â) IAW SEMAN DWG # ED-4068. CLEANED, TREATED, PRIMED FILLER, REPAIR DOUBLER INNER FACE IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW
Part: SKIN — CRACKED (XFS335.250-340.) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, RT WING CTR L/E LOWER SKIN CRACKED 1â APPROX, BETWEEN STA XFS 335.250 AND XFS 340.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05463 DATED 10-11-05, SEMAN DWG NR ED-4067 DATED 10-11-05, EO SEMAN NR 20051227 DATED 10-11-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW SEMAN DWG NR ED-4067. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D EXTERNAL REPAIR DOUBLER (AL7075T6 0.071) + (02EA) FILLER (AL7075T6 0.063) IAW SEMAN DWG # ED-4067. CLEANED, TREATED, PRIMED AREA, FILLER, REPAIR DOUBLER INNER SIDE IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 5
Part: SKIN — CRACKED (XFS710. - 716.) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECTION, RT WING OTBD L/E LOWER SKIN CRACKED 1â APPROX, BETWEEN STA XFS 710.000 AND XFS 716.250. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05461 DATED 10-05-05, SEMAN DWG # ED-4071 DATED 10-06-05, EO SEMAN # 20051277 DATED 10-05-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED CORROSION FROM RT WING OUTBD L/E LWR SKIN (STA XFS 710.000-716.000) IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-1 FIG 2G. CUT OUT DAMAGED SECTION IAW SEMAN DWG # ED-4071. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.063â), FILLER (AL7075T6 0.050â) IAW SEMAN DWG # ED-4071. CLEANED, TREAT
Part: RIVET — IMPROPER (FS 173.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, FWD LOWER FUSELAGE BELLY, STA FS 173.000 L-35.5R. UPGRADE EXTERNAL REPAIR DOUBLER TO INCORPORATE A MINIMUM OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR, REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21. REMOVED DAMAGED SECTION IAW DWG NR ED-4059. NDT INSPECTED REWORKED AREA IAW NDT SPM. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL7075T6 0.063) INTERNAL FINGER DOUBLER (AL7075T6 0.032) IAW DWG NR ED-4059, SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM. INSTALLED REPAIR PARTS IAW SRM.
Part: DOOR — CRACKED (ZONE 500) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, LT WING NR 2 ALT TANK 506B ACCESS DOOR CRACKED. REMOVED AND REPLACED CRACKED ACCESS DOOR NR 506 B (NR 2 ALT TANK) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE) REFER TO JC 99116 FOR LEAK CHECK.
Part: FRAME — CRACKED (THRUST REVERSER) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, NR 2 ENGINE, T/R LT INTERNAL PART FRAME CRACKED 2 AT 10 OâCLOCK POSITION, YN 208.000. REMOVED DEFLECTION FAIRING SEAL, PERFORMED STOP HOLE OF 0.06 IAW CFM 56-2 MM 78-31-41 REP. 016 PAGE 2. FAB`D STIFFENER (STEEL SHEET 0.080 AMS 5504) IAW CFM 56-2 MM 78-31-41 REP. 016 PAGE 2. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW STIFFENER WITH BLIND BOLTS AND REINSTALLED DEFLECTION FAIRING SEAL IAW CFM 56-2 MM 78-31-41 REP 016 PAGE 2.
Part: SKIN — CRACKED (XA 502.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, LT WING IB AILERON UPPER PLATING CRACKED 1, XA 502.000 PERFORMED MAJOR REPAIR IAW SRM 57-7-0 FIG 1, SRM 57-8-1 FIG 1, EO SEMAN NR 20051336. REMOVED DAMAGED PLATING IAW SRM 51-1-21. FABRICATED NEW PLATING (AL7075T6 0.040) IAW SRM 57-8-1 FIG 1 ITEM R. CLEANED, TREATED, PRIMED AREA + NEW PLATING INTERNAL PART IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11 PG 9. INSTALLED NEW PLATING IAW SRM 51-1-21, SRM 51-3-0, SRM 51-3-1. FOR WEIGHT AND BALANCE SEE N/R 2815.
Part: CAP — CRACKED (STA 680.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, MID ACCY CMPT. CAP CRACKED 1, STA 680.000 BETWEEN L 27 AND L 28LPERFORMED MAJOR REPAIR IAW SRM 53-2-5 FIG 14, EO SEMAN NR 20051313 DATED 09-30-05. REMOVED FASTENERS IAW SRM 51-1-20D PG 1. STOP DRILLED ON CRACK END IAW SRM 53-2-5 FIG 14 (SHEET 1). PERFORMED NDT INSPECTION IAW NDT DPM PART 06-10-01-001. NO CRACK NOR CORROSION FOUND. FABRICATED REPAIR ANGLE (7075 O AL-0.100) IAW SRM 53-2-5 FIG 14 (SHEET 1 AND 3), AND SRM 51-1-4 PG 1 AND DPS 3-69-4 (FORMING). PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PG 1, 13 AND D.P.S 7.00-1 REV BK. CLEANED, TREATED, PRIMED AREA + REPAIR ANGLE IAW SRM 53-2-5 FIG 14 (SHEET 1 AND 3), SRM 51-1-20D PG 9 AND SRM 51-3-1 (TORQUE).
Part: SKIN — CRACKED (XRS 72.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, LT WING. UPPER SKIN AROUND HILOK CRACKED, XRS 72.000 S.9PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 17, EO SEMAN NR 20051211 DATED 09-21-05. REMOVED FASTENERS IAW SRM . REMOVED DAMAGED SECTION IAW SRM 57-2-1 FIG 17. PERFORMED NDT INSP. OF REWORK AREA IAW NDT SPM PART. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL7075T6 0.160) + FILLER PLUG (AL7075T6 0.175â) IAW SRM 57-2-1 FIG. 17, SRM 57-3-1 FIG 10. TAPERED DOUBLER FROM 0.160 TO 0.080 IAW SRM 57-2-1 FIG 17, SRM 51-10-0 PG 8 FIG 1 (SHEET 6). CLEANED, TREATED, PRIMED AREA + REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM. INSTALLED REPAIR PARTS IAW SRM. (TORQUE)
Part: RIVET — IMPROPER (FS 1683.000) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1683.000 L-35.5R, UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05448 DATED 10-05-05, SEMAN DWG NR ED-4063 DATED 10-03-05, EO SEMAN NR 20051201 DATED 10-05-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTION IAW SEMAN DWG NR ED-4063. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.080â) + FILLER INTERNAL DOUBLER (AL7075T6 0.090â) + FILLER (AL7075T6 0.071â) IAW SEMAN DWG NR ED-4063. CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEA
Part: SKIN — DELAMINATED (ZONE 300) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, VERT STAB DELAMINATED SKIN ON RUDDER TAB. REMOVED DAMAGED SECTION PLUS FABRICATED DOUBLER (AL2024T3 0.012) IAW SRM 55-2-2 PARA 2. BONDED CORE PLUS DOUBLER WITH HYSOL IAW SRM 51-1-9. REFER TO NR 2801 FOR WEIGHT.
Part: RIVET — IMPROPER (FS 1143) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1143 L-35.5L, UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05463 DATED 10-11-05, SEMAN DWG NR ED-4062 DATED 10-10-05, EO SEMAN NR 20051197 DATED 10-11-05. REMOVED EXISTING REPAIR DOUBLERS IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW SEMAN DWG NR ED-4062. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.080â) + REPAIR TRIPLER (AL7075T6 0.090) + (04EA) FINGER DOUBLERS (AL7075T6 0.050â) IAW SEMAN DWG NR ED-4062. CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8
Part: RIVET — INCORRECT (FS 76.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSP, FUSELAGE BELLY, STA FS 76.000 L-35. 75R. UPGRADE REPAIR DOUBLER TO INCORP A MINIMUM OF 3 ROWS OF RIVETS. PERFORMED REPAIR IAW NR 05446 DATED 10-05-05, DWG NR ED-4058 DATED 09-27-05, EO NR 20051191 DATED 10-05-05. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21. REMOVED DAMAGED SECTION IAW DWG NR ED-4058. NDT INSPECTED REWORKED AREA IAW NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL7075T6 0.063) + INTERNAL FINGER DOUBLER (AL7075T6 0.032) IAW DWG NR ED-4058, SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA + REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM. INSTALLED REPAIR PARTS IAW SRM. (TORQUE)
Part: RIVET — IMPROPER (FS 399.000) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECT, FWD LWR FUSELAGE BELLY, STA FS 399.000 L-35.75R UPGRADE REPAIR DOUBLER TO INCORPORATE A MINIMUM OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05448 DATED 10-05-05, SEMAN DWG NR ED-4060 DATED 10-03-05, EO SEMAN NR 20051193 DATED 10-05-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21. REMOVED DAMAGED AREA IAW SEMAN DWG NR ED-4060. PERFORMED NDT INSPECTION. NO CORROSION, CRACK FOUND IAW NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.080) + (06EA) INTERNAL FINGER DOUBLERS (AL7075T6 0.032) IAW SEMAN DWG NR ED-4060. CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURF
Part: RIVET — IMPROPER (FS 55.000) · airframe 89,672 hrs · 36,136 cycles
DURING C CHECK INSPECTION, FWD LWR FUSELAGE BELLY, STA FS 545.000 L-35.75R, UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05447 DATED 10-05-05, SEMAN DWG # ED-4061 DATED 09-27-05, EO SEMAN # 20051196 DATED 10-05-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4061. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.100â), INTERNAL FINGER DOUBLER (AL7075T6 0.032â) IAW SEMAN DWG # ED-4061, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8
Part: DOOR — CRACKED (STA -54.000) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSP, EXTERNAL FUS. FREON SYS EXHAUST DOOR AFT UPPER CORNER CRACKED .5, STA 54.000 L-2/8L L29L. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 13 (SHEET 1, 5), TR NR 53-169, EO SEMAN NR 20051190 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-3-0. REMOVED DAMAGED SECTION IAW SRM (SHEET 1). NDT INSPECTED REWORKED AREA IAW NDT SRM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL2024T3 0.071) FILLER (AL2024T3 0.050â) IAW SRM 53-2-0 FIG 13 (SHEET 1, 5), SRM 53-2-0 FIG 13, TR NR53-169. CLEANED, TREATED, PRIMED AREA + REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SRM. (TORQUE).
Part: SKIN — CRACKED (12.000 L27R) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSPECTION, NOSE SECTION. RT PRIMARY HEAT EXCHANGER AFT LWR CORNER HAS STRUCTURAL MODIFICATION CRACKED .7500 ON DOUBLER STA 12.000 L-27R. PERFORMED MAJOR REPAIR IAW MM 53-30-09, EO SEMAN NR 20051205 DATED 09-21-05. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED DAMAGED SECTION IAW SRM 53-30-09 PG 207. PERFORMED NDT INSP OF REWORKED AREA IAW NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL7075T6 0.100) + FILLER (AL7075T6 0.100) IAW MM. CLEANED, TREATED, PRIMED AREA + REPAIR PARTS IAW SRM. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW MM 53-30-09 PG 201-202, 208-209, SRM 51-1-20D, SRM 51-3-1 (TORQUE).
Part: DOOR — CRACKED (130.000 L-21L) · airframe 89,672 hrs · 36,136 cycles
DURING ROUTINE C CHECK INSP, FWD ENTRANCE DOOR.- JAMB FWD LWR CORNER CRACKED, STA 130.000 L-21L.PERFORMED MAJOR REPAIR IAW AD 2000-20-08, S/B 53-075, SRM 53-2-0 FIG 15 SHEET 2, SRM 53-2-0, TR NR 53-196, MFG DWG NR SRD8530021, EO NR 20051204 DATED 09-21-05, DWG NR 5750776. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED DAMAGED SECTION IAW SRM. NDT INSPECTED REWORKED AREA IAW NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER, REPAIR TRIPLER, FILLER, IAW SRM (SHEET 2), TR NR 53-196, DWG NR SRD85330021, SRM (FORMING). CLEANED, TREATED, PRIMED AREA REPAIR PARTS IAW SRM. APPLIED SEALANT TO FAYING SURFACES IAW SRM. INSTALLED REPAIR PARTS IAW SRM. (TORQUE).
Part: CABLE — LOOSE (TE FLAPS) · airframe 88,952 hrs · 35,730 cycles
UPON APPROACH TO SCHEDULED LANDING AT KTOL, FLAP SELECTOR HANDLE WOULD ALLOW 5 DEGREES TO BE SELECTED AND STOP. AFTER STAYING IN HOLDING PATTERN FOR APPOX 15-20 MINUTES FLAPS OPERATED NORMALLY. AIRCRAFT MADE UNEVENTFUL LANDING IN KTOL. UPON INSPECTION MX NOTED CABLE HAD COME OFF PULLEY IN GYRO BAY. MX REPOSITIONED CABLE AND PERFORMED NUMEROUS, OPS CHECK OF FLAP SYSTEM. SYSTEM CHECKED NORMAL AND AIRCRAFT WAS RETURNED TO SERVICE.
Part: TRANSCEIVER — INOPERATIVE (WX RADAR SYS) · airframe 88,733 hrs · 35,633 cycles
DURING CLIMBOUT FROM KIAH THE WEATHER RADAR WOULD NOT COME OUT OF TEST PATTERN WITH FAIL LIGHT ON. CREW RETURNED TO KIAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED, INSPECTED AND REINSTALLED THE RADAR RT. THE OPERATIONAL CHECK WAS GOOD PER ALL APPLICABLE MANUALS AND THE AIRCRAFT WAS RETURNED TO SERVICE.
2004
Part: SKIN — GOUGED (ZONE 500) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND LEFT INBOARD FLAP TOP SKIN GOUGED AT STATION XF 90. REMOVED DAMAGED AREA. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED FILLER AND DOUBLER IAW DC8 SRM 57-2-0, 51-1-8, AND 51-1-21.
Part: CURTAIN — UNSECURE (NLG WW) · airframe 87,041 hrs · 34,989 cycles
DURING TAKEOFF AND UPON GEAR RETRACTION, A NOISE WAS HEARD FROM NOSE GEAR AREA. CREW RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED GEAR DOOR BRACKETS AND HINGES FOR DEFECTS AND NONE WERE NOTED. CHECKED DOOR LINKAGES, SEALS AND MECHIANISM AND NO DEFECTS WERE NOTED. LT NOSE WHEEL WELL INSPECTION FOUND CURTAIN WAS UNSNAPPED. RESECURED NOSE WHEEL WELL CURTAIN, THEN INSPECTED GEAR DOOR. PERFORMED GENERAL INSPECTION OF NOSE GEAR, NOSE WHEELS, WHEEL WELL AND RETRACTION SYSTEM IAW ALL APPLICABLE MANUALS. NO DEFECTS NOTED AND AIRCRAFT WAS RETURNED TO SERVICE.
2003
Part: ODOR — DETECTED (CABIN) · airframe 86,871 hrs · 34,927 cycles
DURING CRUISE AN ELECTRICAL ODOR WAS IN THE CEILING AREA OF THE FLT STATION DOOR AND COURIER COMPARTMENT. CREW TURNED OFF THE CIRCUIT BREAKER LIGHT SWITCH ON THE F/E PANEL AND ODOR DECREASED. MAINTENANCE RAN COCKPIT AND COURIOUR LIGHTING FOR 3 HOURS ON GROUND AT SJC. THEY INSPECTED BALLAST POSITIONED IN OVERHEAD ABOVE COCKPIT ENTRY DOOR, INSPECTED B61 BALLAST THAT OPERATES CIRCUIT BREAKER LIGHTS. NO DEFECTS NOTED. SYSTEM CHECKED NORMAL IAW ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE.
Part: DOUBLER — CRACKED (ZONE 800) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND "D" PIT DOOR INBOARD WEB DOUBLER CRACKED. REMOVED EXISTING DOUBLER. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS. IAW DC8 SRM 53-2-0, 51-1-8, 51-1-20D, AND 53-2-0.
Part: SEAT TRACK — BROKEN (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND NUMBER "3" SEAT TRACK HAS BROKEN SCALLOPS AT STATION 70. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0.
Part: BRACKET — CRACKED (ZONE 600) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE DUCTING BRACKET CRACKED. REMOVED BRACKET, WELDED BRACKET AND REINSTALLED BRACKET IAW DC8 MM 20-16-0.
Part: LONGERON — CRACKED (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND LONGERON 15 LEFT CRACKED AT STATION 1748. REMOVED CRACKED LONGERON. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 51-1-20D, 51-1-8, 53-2-2, AND 51-3-1.
Part: SKIN — GOUGED (ZONE 800) · airframe 86,832 hrs · 45,994 cycles
DURING ROUTINE C CHECK, FOUND DOOR L-1, UPPER AFT SKIN GOUGED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 52-2-0, 51-1-8, AND 51-1-20D.
Part: TORQUE BOX — CRACKED (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND L-2 DOOR CUTOUT LOWER FORWARD TORQUE BOX WEB CRACKED. REMOVED DAMAGED WEB. FABRICATED NEW WEB, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 51-1-21, 53-2-0, 51-1-8, 51-1-20D, AND DOUGLAS DRAWING 9751060.
Part: FAIRING — GOUGED (ZONE 300) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER RUB FAIRING GOUGED ON UPPER END OF LOWER FAIRING. REMOVED FAIRING, REPAIRED AND REINSTALLED FAIRING PER ALL APPROVED DATA.
Part: SKIN — CRACKED (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT STATION 1748 LONGERON 10 RIGHT. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND FILLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED FILLER AND DOUBLER IAW DC8 SRM 53-2-1, 51-1-8, AND 51-1-20D.
Part: SEAT TRACK — MISREPAIRED (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND FIRST OFFICER FORWARD OUTBOARD SEAT TRACK HAS IMPROPER REPAIR. REMOVED EXISTING REPAIR. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-351-1-8, AND 51-1-20D.
Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 86,832 hrs · 32,908 cycles
DURING ROUTINE C CHECK, FOUND A CRACKED INTERCOSTAL FROM STATION 1640 TO 1660 AT LONGERON 10 RIGHT. REMOVED CRACKED INTERCOSTAL. FABRICATED NEW INTERCOSTAL, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW INTERCOSTAL IAW DC8 SRM 51-1-21, 51-1-8,51-3-0, AND DOUGLAS DRAWING 5772656.
Part: SKIN — MISREPAIRED (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND L-2 DOOR CUT-OUT LOWER FORWARD CORNER REPAIR DOES NOT COMPLY WITH AD 2000-20-08. REMOVED EXISTING REPAIR. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0, 51-1-20D, 51-1-21, AND 51-1-21.
Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK FOUND INTERCOSTAL CORRODED FROM STATION 1000 TO 1020 AT LONGERON 35 RIGHT. REMOVED DAMAGED INTERCOSTAL. FABRICATED NEW INTERCOSTAL, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW INTERCOSTAL IAW DC8 SRM 51-1-21, 53-2-0, 51-1-8, 51-1-20D, AND DOUGLAS DRAWING 779929.
Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND INTERCOSTAL CORRODED BETWEEN STATION 980, AND 1000 AT LONGERON 35 LEFT. REMOVED CORROSION. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-8, 51-30-30, 53-2-0, AND DOUGLAS DRAWING 5779959.
Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND INTERCOSTAL CORRODED BETWEEN STATION 980, AND 1000 AT LONGERON 35 RIGHT. REMOVED CORROSION. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-8, 51-30-30, 53-2-0, AND DOUGLAS DRAWING 5779959.
Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND SHEAR TIE CORRODED AT STATION 1020 FROM LONGERON 31 RIGHT TO LONGERON 34 RIGHT. REMOVED DAMAGED SHEAR TIE. FABRICATED NEW SHEAR TIE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 51-1-8, 53-4-1, AND 51-1-20D.
Part: RIB — CRACKED (ZONE 600) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND RIGHT WING CENTER LEADING EDGE UPPER SURFACE RIB CRACKED AT STATION 322. STOP DRILLED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-0, 51-1-8, 51-3-0, AND 57-3-3.
Part: RIB — CRACKED (ZONE 600) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND RIGHT WING CENTER LEADING EDGE LOWER SURFACE RIB CRACKED AT STATION 341. STOP DRILLED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-0, 51-1-8, 51-3-0, AND 57-3-3.
Part: CUSP WEB — CRACKED (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND CUSP WEB CRACKED AT STATION FS 670. STOP DRILLED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-21, 53-2-0, 53-4-1, AND 51-1-8.
Part: ATTACH BRACKET — CRACKED (ZONE 600) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND RIGHT WING CENTER LEADING EDGE OUTBOARD END ATTACH FASTENER HOLES CRACKED. REMOVED DAMAGED HOLES. FABRICATED REPAIR DOUBLER AND FILLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW DOUBLER AND FILLER IAW TIMCO REPAIR ENGINEERING ORDER REO-G09488.
Part: RIB — CRACKED (ZONE 600) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND RIGHT WING CENTER LEADING EDGE UPPER SURFACE RIB CRACKED AT STATION 454. STOP DRILLED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-0, 51-1-8, 51-1-20D, AND 57-3-3.
Part: SEAT TRACK — GOUGED (ZONE 100) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND SEAT TRACK NUMBER TWO GOUGED AT STATION 150. REMOVED GOUGED SEAT TRACK. FABRICATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK. IAW DC8 SRM 51-1-8, 53-2-3, AND 51-3-0.
Part: KEELBEAM — CRACKED (ZONE 100) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND KEEL BEAM ATTACH ANGLE CRACKED AT HINGE FASTENER HOLE. REMOVED DAMAGED ANGLE, FABRICATED NEW ANGLE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW ANGLE. IAW DC8 SRM 51-1-20D, 51-1-8, AND DOUGLAS DRAWING 5616306.
Part: LONGERON — CRACKED (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND LONGERON 11 RIGHT CRACKED AT STATION FS 1660. REMOVED CRACKED LONGERON. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW LONGERON, IAW DC8 SRM 51-1-21, 51-1-8, 51-1-20D, AND DOUGLAS DRAWING 3773512.
Part: WEB — CRACKED (ZONE 600) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND RIGHT INBOARD FLAP INTERNAL WEB CRACKED AT INBOARD LEADING EDGE AT STATION XF1. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 57-20-0, 51-1-8, AND 51-1-21.
Part: HINGE — ELONGATED (NR 2 ENG T/R) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND THE NR 2 ENGINE INBOARD THRUST REVERSER, FORWARD HINGE HAS AN ELONGATED HOLE. THE HOLE WAS REAMED TO ROUND AND TRUE, MANUFACTURED BUSHING AND INSTALLED TO RESTORE HINGE TO ORIGINAL DIMENSIONS IAW TIMCO REPAIR ENGINEERING ORDER, REO-G09483.
Part: INTERCOSTAL — DAMAGED (ZONE 100) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND INTERCOSTAL A HOLE IN THE RADIUS AT STATION 1390 ABOVE LONGERON 28 LEFT. REMOVED DAMAGED INTERCOSTAL. FABRICATED NEW INTERCOSTAL, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW INTERCOSTAL IAW DC8 SRM 51-1-21A, 51-1-21D, 51-1-8, AND DOUGLAS DRAWING 5750771.
Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 8,683 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND A CRACKED INTERCOSTAL AT STATION 1160 LONGERON 27 RIGHT. FABRICATED NEW INTERCOSTAL, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW INTERCOSTAL IAW DC8 SRM 51-1-20D, 51-1-8, AND DOUGLAS DRAWING 9573259.
Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND INTERCOSTAL CORRODED FROM STATION 1380 TO STATION 1390 AT LONGERON 33 LEFT. REMOVED DAMAGED INTERCOSTAL, FABRICATED NEW INTERCOSTAL, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW INTERCOSTAL IAW DC8 SRM 51-1-8, 53-4-0, AND 51-1-21.
Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND INTERCOSTAL CRACKED AT STATION 1100 AT LONGERON 27 RIGHT. REMOVED DAMAGED INTERCOSTAL, FABRICATED ANGLE REPAIR, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS. IAW DC8 SRM 51-1-8, 53-4-0, AND 51-1-21.
Part: FRAME — CRACKED (ZONE 100) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND FRAME CRACKED AT STATION 1395 LONGERON 28 RIGHT. REMOVED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0, 51-1-8, NAD DOUGLAS DRAWING 5616674.
Part: SKIN — CRACKED (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND FORWARD SERVICE DOOR, R-1, CUT-OUT LOWER AFT CORNER SKIN CRACKED. REMOVED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0, 51-1-8, 51-1-21, 51-6-1 AND 51-1-20D.
Part: SHIM — CORRODED (ZONE 600) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND RIGHT WING TRAILING EDGE SUPPORT SHIMS CORRODED AT STATION XIS59.492. REMOVED DAMAGED SHIMS. FABRICATED NEW SHIMS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SHIMS IAW DC8 SRM 51-1-8, 51-5-4, 51-3-0, TIMCO REPAIR ENGENEERING ORDER REO-G09465.
Part: SKIN — CRACKED (ZONE 200) · airframe 86,823 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND FORWARD SERVICE DOOR, R-1, CUT-OUT LOWER FORWARD CORNER SKIN CRACKED. REMOVED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS. IAW DC8 SRM DC8 SRM 53-2-0, 51-1-8, 51-1-21, 51-6-1 AND 51-1-20D.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND SEAT TRACK "F" GOUGED FROM STATION 1390 TO STATION 1455. REMOVED GOUGED SEAT TRACK. FABRICATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-1-8, 53-2-3, AND 51-3-0.
Part: FITTING — CRACKED (ZONE 600) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND RT WING INBOARD AILERON INBOARD HINGE FITTING CRACKED. REMOVED CRACKED FITTING. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW FITTING IAW DC8 SRM 51-3-0.
Part: SEAT TRACK — BROKEN (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND SEAT TRACK "B" TANG BROKEN AT STATION 260. REMOVED DAMAGED SEAT TRACK. FABRICATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-1-8, 53-2-3, AND 51-3-0.
Part: SKIN — CRACKED (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND FORWARD SERVICE DOOR CUTOUT UPPER FORWARD CORNER CRACKED. REMOVED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 53-2-0, AND 51-1-8.
Part: WEB — CRACKED (ZONE 100) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND WEB CRACKED AT STATION 1280 LONGERON 27 RIGHT. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-8, AND 51-1-21.
Part: FITTING — CORRODED (ZONE 100) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND FITTING CORRODED AT STATION FS 1124 LONGERON 27 LEFT. REMOVED DAMAGED FITTING. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW FITTING IAW DC8 SRM 51-3-0.
Part: CHANNEL — CRACKED (ZONE 600) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND NR 3 ENGINE THRUST REVERSER FIXED STRUCTURE AFT TWELVE O-CLOCK SEAL CHANNEL CRACKED. FABRICATED NEW SEAL CHANNEL, LOCATED, DRILLED, TRIMMED, AND INSTALLED NEW SEAL CHANNEL REPAIR PARTS IAW TIMCO REPAIR ENGINEERING ORDER, REO G-09505.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND SEAT TRACK "G" WORN AT STATION 670. REMOVED WORN SEAT TRACK. FABRICATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-1-8, 53-2-3, AND 51-3-0.
Part: SKIN — SEPARATED (ZONE 500) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND LEFT OUTBOARD FLAP UPPER SURFACE NUMBER THREE WEDGE FORWARD LEFT CORNER SEPARATED. INJECTED ADHESIVE, AND BONDED AREA IAW DC8 SRM 51-1-9.
Part: HINGE — CHAFED (ZONE 500) · airframe 86,832 hrs · 32,908 cycles
DURING ROUTINE C CHECK, FOUND LEFT INBOARD FLAP INBOARD HINGE FITTING OUTBOARD HINGE HALF CHAFED AT STATION XW3. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-21, AND DC8 SB 27-279.
Part: FRAME — CORRODED (ZONE 100) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND FRAME GOUGED AT STATION 1684 LONGERON 21 RIGHT. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 51-1-21, 53-2-0, AND 51-1-8.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND SEAT TRACK "F" GOUGED AT STATION 830. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SEAT TRACK SECTION AND SPLICES, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK SECTION AND SPLICES IAW DC8 SRM 51-1-8, AND 53-2-3
Part: VANE — DELAMINATED (ZONE 600) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND RIGHT OUTBOARD FLAP NUMBER SIX VANE DELAMINATED. REMOVED DAMAGED AREA, FABRICATED AND BONDED NEW OUTER SKIN, OUTER DOUBLER AND INNER FILLER IAW TPS 1001 REV E AND DOUGLAS DRAWING 5701110
Part: FLAP TRACK — WORN (ZONE 500) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND LEFT OUTBOARD FLAP VANE MOUNT TRACK WORN AT HINGE NUMBER FIVE. REMOVED DAMAGED TRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS. IAW DC8 SRM 51-3-2, 57-50-2, AND 51-1-8.
Part: HINGE — CHAFED (ZONE 600) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND RIGHT INBOARD FLAP INBOARD HINGE FITTING OUTBOARD HINGE HALF CHAFED AT STATION XW3. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-21, AND DC8 SB 27-279.
Part: WEB — TOOL DAMAGE (ZONE 600) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND RIGHT INBOARD FLAP INBOARD LEADING EDGE WEB HAS TWO RIVETS IMPROPERLY INSTALLED, ONE HAS A DOUBLE DRILLED HOLE AT STATION XW3. REMOVED DAMAGED WEB, FABRICATED NEW WEB, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW WEB. IAW DC8 SRM 51-3-0, 51-1-8, AND 51-1-21.
Part: SKIN — GOUGED (ZONE 600) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND RIGHT INBOARD FLAP TOP SKIN GOUGED AT STATION XF103. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-0, 57-7-0, AND 51-1-8.
Part: HINGE FITTING — WORN (ZONE 600) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND RIGHT OUTBOARD FLAP EXHAUST GATE OUTBOARD HINGE FITTING HAS WORN BUSHING HOLES. WORN HOLES WERE OVERSIZED, BUSHINGS WERE MANUFACTURED AND INSTALLED, HOLES WERE FINAL SIZED TO MANUFACTURES ORIGINAL DIMENSIONS IAW DC8 SRM 51-1-21, 51-9-0, 51-3-0, TIMCO REPAIR ENGINEERING ORDER REO-G09472 DATED 09/18/2003.
Part: RUB STRIP — WORN (TE FLAPS) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND RIGHT OUTBOARD FLAP EXHAUST GATE, OUTBOARD RUB STRIP WORN. REMOVED WORN RUB STRIP. FABRICATED NEW RUB STRIP, LOCATED, DRILLED, TRIMMED, AND INSTALLED NEW RUB STRIP IAW DC8 SRM 51-1-21, TIMCO REPAIR ENGINEERING ORDER REO-G094569 DATED 09/18/2003, AND DOUGLAS DRAWING 5652302.
Part: RUB STRIP — WORN (ZONE 600) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND RIGHT OUTBOARD FLAP EXHAUST GATE CUT-OUT FORWARD UPPER RUB STRIP WORN. REMOVED WORN RUB STRIP. FABRICATED NEW RUB STRIP, LOCATED, DRILLED, TRIMMED, AND INSTALLED NEW RUB STRIP IAW DC8 SRM 51-1-21, DOUGLAS DRAWING 5643970.
Part: VANE — DELAMINATED (ZONE 600) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND RIGHT INBOARD FLAP INBOARD VANE DELAMINATED NEAR INBOARD END. REMOVED VANE. REPAIRED VANE. REINSTALLED VANE PER ALL APPROVED DATA.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND SEAT TRACK "F" GOUGED AT STATION 860. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED SEAT TRACK SECTION, AND SPLICES, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK SECTION, AND SPLICES IAW DC8 SRM 51-1-8, AND 53-2-3.
Part: VANE — DELAMINATED (ZONE 600) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND RT OUTBOARD FLAP VANE DELAMINATED BETWEEN INBOARD AND CENTER HINGE. REPLACED FLAP VANE IAW DC8 SRM 27-51-14.
Part: SKIN — CRACKED (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND AFT PASSENGER DOOR, L-2, CUT-OUT UPPER AFT CORNER SKIN CRACKED. REMOVED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM DC8 SRM 53-2-0, 51-1-8, 51-1-21, 51-6-1 AND 51-1-20D.
Part: SUPPORT CHANNEL — CRACKED (ZONE 100) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND CRACKED FLOOR SUPPORT CHANNEL AT STATION 360, LONGERON 33 LEFT. REMOVED CRACKED FLOOR SUPPORT CHANNEL. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PART IAW DC8 SRM 51-1-21, 51-1-8, AND DOUGLAS DRAWING 3758633.
Part: FITTING — CORRODED (ZONE 100) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND A CORRODED FITTING UNDER NUT PLATE AT STATION 240 LONGEREON 33 RIGHT. REMOVED DAMAGED FITTING. MANUFACTURED NEW FITTING, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW TIMCO REPAIR ENGINEERING ORDER REO-G09501.
Part: FRAME SPLICE — CORRODED (ZONE 100) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND FRAME SPLICE CORRODED AT STATION 245 BETWEEN LONGERONS 34 AND 35 LEFT. REMOVED CORRODED FRAME SPLICE, FABRICATED NEW FRAME SPLICE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW FRAME SPLICE IAW DC8 SRM 53-2-0, AND TIMCO REPAIR ENGINEERING ORDER REO-G09471.
Part: SEAT TRACK — BROKEN (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND SEAT TRACK "B" TANG BROKEN AT STATION 240. REMOVED DAMAGED SEAT TRACK. FABRICATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-1-8, 53-2-3, AND 51-3-0.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND SEAT TRACK "B" GOUGED AT STATION 244. REMOVED GOUGED SEAT TRACK. FABRICATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-1-8, 53-2-3, AND 51-3-0.
Part: MOUNT — CORRODED (ZONE 100) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND ANTENNA MOUNT CORRODED AT STATION FS410, LONGERON 36. ANTENNA NOT IN USE, REMOVED MOUNT IAW TIMCO REPAIR ENGINEERING ORDER REO-G09474.
Part: SKIN — CRACKED (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND AFT SERVICE DOOR, R-2, CUT-OUT LOWER FORWARD CORNER SKIN CRACKED. REMOVED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS. IAW DC8 SRM DC8 SRM 53-2-0, 51-1-8, 51-1-21, 51-6-1 AND 51-1-20D.
Part: SKIN — CRACKED (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND AFT SERVICE DOOR, R-2, CUT-OUT UPPER AFT CORNER SKIN CRACKED. REMOVED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM DC8 SRM 53-2-0, 51-1-8, 51-1-21, 51-6-1 AND 51-1-20D.
Part: SEAT TRACK — BROKEN (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND SEAT TRACK "D" TANG BROKEN AT STATION 150. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 53-2-3, 51-1-8, AND 51-1-21.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND SEAT TRACK "E" GOUGED AT STATION 150. REMOVED GOUGED SEAT TRACK. FABRICATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-1-8, 51-1-21, 53-2-3, AND 51-3-0.
Part: SKIN — CRACKED (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND AFT PASSENGER DOOR, L-2, CUT-OUT LOWER AFT CORNER SKIN CRACKED. REMOVED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM DC8 SRM 53-2-0, 51-1-8, 51-1-21, AND 51-1-20D.
Part: FRAME — CORRODED (ZONE 100) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND FRAME CORRODED AT STATION 245 BETWEEN LONGERONS 34 LEFT AND 35 LEFT. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 53-2-0, 51-1-21,51-1-8, AND TIMCO REPAIR ENGINEERING ORDER REO-G9471.
Part: SKIN — SCRATCHED (ZONE 500) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE SCRATCHED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-1, 51-1-8, AND 51-1-20D.
Part: SKIN — DENTED (ZONE 100) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK FOUND EXTERNAL FUSELAGE SKIN DENTED AT STATION FS 1350 LONGERON 29 RIGHT. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM DC8 SRM 51-1-0, 53-2-0, 53-2-1, 51-1-8, AND 51-1-11.
Part: CLOSEOUT PANEL — DELAMINATED (ZONE 100) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND LEFT AFT PRESSURE BULKHEAD CLOSEOUT PANEL DELAMINATED. REMOVED DAMAGED PANEL. FABRICATED NEW CLOSEOUT PANEL, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW CLOSEOUT PANEL IAW TIMCO REPAIR ENGINEERING ORDER REO-G09509.
Part: FAIRING — DAMAGED (ZONE 300) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND RIGHT ELEVATOR UPPER TRAILING EDGE ATTACHMENT FAIRING HAS A HOLE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 55-3-0, 55-2-0, 51-1-21, AND 51-1-8.
Part: SPACER — CORRODED (ZONE 600) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE AT STATION XFS 422-750 SPACER CORRODED. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PART IAW REPAIR ENGINEERING ORDER REO-G09480.
Part: SKIN — CORRODED (ZONE 300) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C-CHECK, FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE UPPER SURFACE CORRODED AT STATION XFS178. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 55-2-1, 51-1-21, AND 51-1-8.
Part: SKIN — CRACKED (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND L-1 DOOR CUTOUT UPPER AFT CORNER CRACKED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS. IAW DC8 SRM 51-1-21, 53-2-0, AND 51-1-8.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND CAPTAINS LEFT FORWARD SEAT TRACK WORN. REMOVED WORN SEAT TRACK. FABRICATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-1-8, 51-1-21, AND 51-3-0.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND CAPTAINS RIGHT FORWARD SEAT TRACK WORN. REMOVED WORN SEAT TRACK. FABRICATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-1-21, AND 51-3-0.
Part: ANGLE — DAMAGED (ZONE 600) · airframe 86,832 hrs · 34,908 cycles
DURING ROUTINE C CHECK, FOUND THREE FASTENER HEADS SHEARED ON THE RIGHT WING CENTER LEADING EDGE BOTTOM AFT OF THE END OF INBOARD SLAT. REMOVED DAMAGED ANGLE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS AND FASTENERS IAW DC8 SRM 51-1-8, 51-1-21, AND DOUGLAS DRAWING 5769891.
Part: CONNECTOR — DIRTY (EGT HARNESS) · airframe 86,092 hrs · 34,454 cycles
AFTER DEPARTURE FROM LRD DURING CRUISE CREW NOTED NR 3 ENGINE EGT ROSE ABNORMALLY. CREW SHUTDOWN NR 3 ENG PER COMPANY POLICY. AIRCRAFT RETURNED TO LRD FOR AN UNEVENTFUL LANDING. UPON INSPECTION MAINTENANCE DISCOVERED DIRTY CONNECTIONS IN THE EGT HARNESS. MAINTENANCE CLEANED CONNECTIONS AND RAN ENGINE PER APPLICABLE AIRPLANE MANUALS. AFTER A GOOD OPERATIONAL CHECK THE AIRCRAFT WAS RETURNED TO SERVICE.
2002
Part: WING — CRACKED (#1 PYLON) · airframe 85,887 hrs · 34,332 cycles
AFTER LANDING AT SEA THE FLIGHT CREW NOTICED A SLOW FUEL LEAK COMING FROM THE #1 PYLON INBOARD SIDE. MAINTENANCE INSPECTED THE AIRCRAFT AND CATORGIZED IT AS A SLOW SEEP. REPAIR ACCOMPLISHED, REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND BOEINGS LETTER TIN-LIT-02-00024H. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: STATOR VANE — MALFUNCTIONED (ENGINE) · airframe 85,070 hrs · 33,994 cycles
AFTER TAKEOFF FROM TOL, THE FLIGHT CREW EXPERIENCED A WINDSHEAR WARNING ALERT. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND THE NUMBER THREE ENGINE EXCEEDED NORMAL OPERATING TEMPERATURES. THE FLIGHT RETURNED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE IN ACCORDANCE WITH THE CFM MAINTENANCE MANUAL. THE INSPECTION REVEALED A DISCREPANCY AT THE VARIABLE STATOR VANE FEEDBACK SYSTEM. MAINTENANCE CORRECTED THE DISCREPANCY, PERFORMED A SUCCESSFUL OPERATIONAL CHECK IN ACCORDANCE WITH THE COMPANY ENGINE RUN HANDBOOK. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: COWLING — DAMAGED (#1 ENGINE) · airframe 81,552 hrs · 33,958 cycles
DURING A ROUTINE MAINTENANCE PREFLIGHT IN TER, MINOR EVIDENCE OF DAMAGE TO #1 ENGINE OUTBOARD COWLING. MAINTENANCE INSPECTED THE ENGINE IN ACCORDANCE WITH AN APPROVED DER ENGINEERING DIRECTIVE EDQ11-1. NO ADDITIONAL DAMAGE WAS NOTICED AND THE ENGINE PERFORMANCE WAS NORMAL. REPLACED THE COWLINGS AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: PUMP — LEAKING (HYD SYSTEM) · airframe 84,933 hrs · 33,938 cycles
EN ROUTE FROM SEA TO ANC, THE FLT CREW NOTICED A DECLINE IN THE MAIN HYD SYS QUANTITY. THE FLT CREW NOTICED WHILE FOLLOWING COMPANY PROCEDURES THE HORIZONTAL STABILIZER ALTERNATE TRIM INOPERATIVE. THE FLT CONTINUED TO ANC FOR AN UNEVENTFUL LANDING. MX INSPECTED THE ACFT WHICH REVEALED THE STANDBY RUDDER PUMP LEAKING. MX REPLACED THE STANDBY RUDDER PUMP IN ACCORDANCE WITH THE MM. MX FOUND THE ALTERNATE STABILIZER ELECTRICAL TRIM MOTOR ELECTRICAL CONNECTOR CONTAMINATED WITH MOISTURE. MX CLEANED THE ELECTRICAL CONNECTOR AND PERFORMED A SUCCESSFUL OPS CHECK. THE ACFT WAS RETURNED TO SERVICE.
Part: WARNING LIGHT — ILLUMINATED (LANDING GEAR) · airframe 84,929 hrs · 33,937 cycles
AFTER TAKE OFF FROM ANC, THE LANDING GEAR UPLATCH CHECK FAILED AND THE LANDING GEAR UNSAFE LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO SEA FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND VERIFIED THE GEAR DOOR LATCHES IN FLIGHT POSITION AND VERIFIED THE GEAR AND DOOR LIGHTS OPERATIVE. THE AIRCRAFT IS REMOVED FROM SERVICE AND FURTHER INVESTIGATION CONTINUES AT THIS TIME. ADDITIONAL INFORMATION WILL FOLLOW AS REPAIRS ARE ACCOMPLISHED.
Part: BRACKET — LOOSE (GEAR) · airframe 84,922 hrs · 33,935 cycles
AFTER TAKE OFF FROM ANC, THE LANDING GEAR UPLATCH CHECK FAILED AND THE LANDING GEAR UNSAFE LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR SEVERAL TIMES BEFORE THE UPLATCH CHECK PASSED AND THE LANDING GEAR UNSAFE LIGHT EXTINGUISHED. THE FLIGHT CONTINUED TO SEA FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE LEFT MAIN GEAR UP LIMIT SWITCH MOUNTING BRACKET LOOSE. MAINTENANCE TIGHTENED THE BRACKET AND PERFORMED A SUCCESSFUL OPERATIONAL CHECK IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE.
2001
Part: ENGINE — LEAKING (NR 1) · airframe 84,402 hrs · 33,732 cycles
EN ROUTE FROM JFK TO BDL. WHEN LEFT AIR CONDITION PACK WAS TURNED ON SMOKE WAS EMITTING FROM THE VENTS. THE FLIGHT CREW SECURED THE PACK AND THE SMOKE SUBSIDED. THE FLIGHT CREW THEN NOTICE A DECLINE IN THE NUMBER ONE ENGINE OIL QUANTITY AND OIL PRESSURE REMAINED NORMAL. THE FLIGHT CONTINUED TO BDL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED AIRCRAFT WHICH REVEALED THE NUMBER ONE ENGINE WAS LOW ON OIL. MAINTENANCE SUSPECTS DISCREPANCIES ASSOCIATED WITH THE NR 3 STATIONARY AFT AIR/OIL SEAL. THE ENGINE WAS REPLACED AND NO DISCREPANCIES WERE NOTED WITH THE LEFT AIR CONDITIONING SYSTEM. THE AIRCRAFT WAS RETURNED TO SERVICE. ADDITIONAL INFORMATION WILL FOLLOW WHEN MADE AVAILABLE.
Part: COWLING — DAMAGED (ENGINE T/R) · airframe 83,464 hrs · 23,212 cycles
DURING DESCENT FROM RDU TO ATL, THE FLIGHT CREW NOTICED THE NUMBER THREE ENGINE THRUST REVERSER WAS VERY SLOW TO STOW AFTER DEPLOYMENT. THE FLIGHT CONTINUED TO ATL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE WHICH REVEALED A PORTION OF THE NUMBER THREE ENGING INBOARD THRUST REVERSER TRANSLATING COWLING HAD DEPARTED FROM THE ENGINE. MAINTENANCE REPLACED THE INBOARD THRUST REVERSER HALF IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE.
1999
Part: CONNECTOR — FAILED (LT MLG DOOR)
AFTER TAKEOFF FROM GDL TO TOL, WHEN THE LANDING GEAR WAS RETRACTED THE LANDING GEAR DOOR UNSAFE LIGHT WAS INTERMITTENTLY FLASHING THEN EXTINGUISHED. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTION THE LANDING GEAR WARNING SYSTEM LOCATING A DEFECTIVE CANNON PLUG ON THE LEFT GEAR DOOR WARNING SWITCH. THE CANNON PLUG WAS REPLACED AND A SUCCESSFUL OPERATIONAL TEST WAS PERFORMED.
Part: WIRE — BROKEN (LT MLG DOOR)
EN ROUTE FROM ICT TO GDL, THE LANDING GEAR DOOR UNSAFE LIGHT ILLUMIATED AFTER A SUCCESSFUL LANDING GEAR UPLATCH CHECK WAS ACCOMPLISHED. THE FLIGHT CREW CYCLED THE GEAR WITH THE WARNING INDICATION REMAINING THE SAME. THE FLIGHT CONTINUED TO GDL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTION THE LANDING GEAR LOCATING A BROKEN WIRE ON THE LEFT GEAR DOOR WARNING SWITCH. THE WIRING WAS REPAIRED AND A SUCCESSFUL OPERATIONAL TEST WAS PERFORMED.
Part: CONTROL VALVE — OUT OF ADJUST (NLG)
EN ROUTE FROM IAH TO DFW, DURING THE GEAR UPLATCH CHECK THE NOSE GEAR FAILED AND EXTENDED. THE FLIGHT CREW CYCLED THE GEAR TO PERFORM A SECOND CHECK WITH NO SUCCESS. THE FLIGHT CONTINUED TO DFW FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE NOSE LANDING GEAR CONTROL SYSTEM WHICH REVEALED DISCREPANCIES. MAINTENANCE RIG THE NOSE LANDING CONTROL VALVE LINKAGE IN ACCORDANCE WITH THE MAINTENANCE MANUAL AND PERFORMED A SUCCESSFUL GEAR SWING. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: FUEL FILTER — DIRTY (NR 1 ENGINE)
EN ROUTE FROM LAX TO TOL, THE NUMBER ONE ENGINE FLAMED OUT DURING CRUISE. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO TOL FOR AN UNEVENFULL LANDING. MAINTENANCE INSPECTED THE ENGINE AND PERFORMED THE NECESSARY TROUBLESHOOTING PROCEDURES IN ACCORDANCE WITH THE CFMI MAINTENANCE MANUAL. MAINTENANCE INSPECTED AND REPLACED THE FUEL FILTER AS PRECAUTIONARY. MAINTENANCE PERFORMED ENGINE POWER ASSURANCE CHECKS IN ACCORDANCE WITH THE COMPANY JET RUN HANDBOOK WITH NO DEFECTS NOTED.
Part: BALLAST — ODOR (COCKPIT)
EN ROUTE FROM TOL TO LAX, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT. THE FLIGHT CREW EXTINGISHED THE OVERHEAD FLUORESCENT LIGHTING SYSTM AND THE ODOR SUBSIDED. THE FLIGHT CONTINUED TO LAX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE LIGHTING SYSTEM CIRCUITRY AND BALLAST ASSEMBLY WITH NO DISCREPANCIES NOTED. MAINTENANCE PERFORMED AN OPERATIONAL TEST IN ACCORDANCE WITH THE MAINTENANCE MANUAL WITH NO DISCREPANCIES NOTED.
Part: BALLAST — DEFECTIVE (COCKPIT)
EN ROUTE TO DFW, A STRONG ODOR WAS SENSED IN THE COCKPIT WHEN THE GLARESHIELD LIGHT WAS ILLUMINATED. THE LIGHTING SYSTEM WAS TURNED OFF AND THE ODOR SUBSIDED AND THE FLIGHT CONTINUED TO DFW. MAINTENANCE INSPECTED AND FOUND THE GLARESHIELD LIGHT BALLAST DEFECTIVE. THE GLARESHIELD LIGHTING WAS PLACED ON DEFERRAL AND THE AIRCRAFT WAS RETURNED TO SERVICE.
1997
Part: PLATING — CORRODED (BS 25.5)
DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON THE EXTERNAL PLATING AT FUSELAGE STATION 25.5, BETWEEN LONGERONS 31 LEFT AND 31 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH DER APPROVED DRAWING 853-395-97 AND ENGINEERING ORDER 53-DC8-593.
Part: LONGERON — CORRODED (BS 10)
DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON LONGERON 33 RIGHT, BETWEEN FUSELAGE STATIONS 10 TO 70. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION OF LONGERON SECTION IN ACCORDANCE WITH DER APPROVED DRAWING 853-396-97 AND ENGINEERING ORDER 53-DC8-594. INSTALLATION IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL.
Part: SEAT TRACK — CRACKED (BS 240)
DURING ROUTINE C-CHECK INSPECTION, FOUND SEAT TRACK TO BE CRACKED IN MAIN CARGO COMPARTMENT BETWEEN FUSELAGE STATIONS 240 AND 247, BUTT LINE X-25. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED TRACK, FABRICATION AND INSTALLATION OF NEW SEAT TRACK PLUG IN ACCORDANCE WITH ENGINEERING ORDER 53-DC8-580 AND DOUGLAS STRUCTURAL REPAIR MANUAL 53-2-3.
Part: DOUBLER — CORRODED (BS 10)
DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON THE EXTERNAL FINGER DOUBLER BETWEEN FUSELAGE STATIONS 10 TO 70, LONGERON 33 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF NEW FINGER DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL 53-1-0.
Part: PAN — CRACKED (RT SERVICE DOOR)
DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND ON RIGHT AFT SERVICE DOOR PAN, LOWER AFT CORNER. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER IN ACCORDANCE WITH DER APPROVED DRAWING 852-386-97 AND ENGINEERING ORDER 52-DC8-590.
Part: PLATING — CRACKED (LT WING)
DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND ON LEFT WING LEADING EXTERNAL PLATING BETWEEN STATIONS 485 AND 558. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH DER APPROVED DRAWING 857-385-97 AND ENGINEERING ORDER 57-DC8-589.
Part: SKIN — CORRODED (BS 1723)
DURING ROUTINE C-CHECK INSPECTION, A CORROSION BULGE WAS FOUND BETWEEN FUSELAGE STATIONS 1723 AND 1745, LONGERON 23 LEFT. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL 53-2-1.
Part: SPLICE — CRACKED (BS 600)
DURING ROUTINE C-CHECK INSPECTION, FOUND LONGERON 31 RIGHT, SPLICE FITTING CRACKED BETWEEN FUSELAGE STATIONS 600 AND 620. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION OF A NEW FITTING IN ACCORDANCE WITH DER APPROVED DRAWING 853-373-97 AND ENGINEERING ORDER 3-DC8-578.
Part: FITTING — CRACKED (BS 1690)
DURING ROUTINE C-CHECK INSPECTION, FOUND LONGERON 23 RIGHT END FITTING CRACKED AT FUSELAGE STATION 1690. REPAIR ACCOMPLISHED REMOVAL OF FITTING, FABRICATION AND INSTALLATION OF A NEW END FITTING IN ACCORDANCE WITH DER APPROVED DRAWING 853-377-97 AND ENGINEERING ORDER 53-DC8-582.
Part: SKIN — CRACKED (BS 1766)
DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND ON THE EXTERNAL PLATING AT FUSELAGE STATION 1766, LONGERON 25 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH DER APPROVED DRAWING 853-372-97 AND ENGINEERING ORDER 53-DC8-576.
Part: PLATING — CRACKED (LT WING)
DURING ROUTINE C-CHECK INSPECTION, THE LEFT WING LOWER LEADING EDGE PLATING WAS FOUND WITH TWO CRACKS BETWEEN STATIONS XFS 294 AND 306. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREAS, FABRICATION AND INSTALLATION OF TWO INTERNAL FILLERS, AND TWO EXTERNAL REPAIR DOUBLERS IN ACCORDANCE WITH DER APPROVED DRAWING 857-384-97 AND ENGINEERING ORDER 57-DC8-588.
Part: FRAME — CRACKED (BS 1394)
DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND ON THE BELT FRAME AT FUSELAGE STATION 1394, BETWEEN LONGERONS 33 AND 36 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND A REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL 53-2-0.
Part: CONTAINER — RUPTURED (NR 1 CARGO COMPT)
DURING CLIMBOUT, FUMES WERE NOTED AS THE AIRCRAFT WAS PRESSURIZED. THE AIRCRAFT RETURNED TO OAK FOR AN UNEVENTFUL LANDING. THE SOURCE OF THE FUMES WAS DISCOVERED TO HAVE BEEN A RUPTURED CONTAINER OF ZIOLIN LOCATED IN THE NUMBER ONE CARGO POSITION. THE CONTAINER AND THE RESIDUAL LIQUID WERE REMOVED BY CONTAMINATION SPECIALISTS.
1996
Part: ENGINE — FAILED (NR 3)
EN ROUTE TOL TO DEN, THE NR 3 ENGINE WAS SHUT DOWN DUE TO FLUCTUATING FUEL FLOW AND SUBSEQUENT FLUCTUATING N1. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE N1 AND N2 SPOOLS DRAGGING TOGETHER. THE ENGINE WAS REMOVED AND REPLACED. PRELIMINARY INDICATIONS ARE A FAILURE OF THE NR 4 BEARING. (M)
Part: UPLATCH ASSY — LACK OF LUBE (NLG)
EN ROUTE FROM ORD-TOL, THE AIRCRAFT FAILED A GEAR UPLATCH CHECK, ACCOMPANIED BY A LANDING GEAR UNSAFE LIGHT. NOISE HEARD AT NOSE GEAR. TOL MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE GEAR UPLATCH DIRTY AND DRY. MAINTENANCE CLEANED AND LUBRICATED LATCH MECHANISM. PERFORMED A NOSE GEAR SWING PER DACO MM 32-30-0 AND 32-31-6 WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: GEAR HANDLE — LACK OF LUBE (COCKPIT)
ON APPROACH TO TOL, WHEN LOWERING LANDING GEAR, INDICATION SYSTEM DID NOT INDICATE DOWN FOR ALL THREE GEAR. THE GEAR WAS CYCLED AND THE INDICATION WAS NORMAL FOR ALL THREE GEAR. MAINTENANCE CLEANED AND LUBED THE GEAR HANDLE MECHANISM AND CLEANED THE HANDLE DETENT SWITCHES. SYSTEM WAS GROUND CHECKED SUCCESSFULLY IAW WITH THE DOUGLAS MM 32-60-0. (M)
Part: ELECTRICAL — ODOR (COCKPIT)
DURING TAXI IN AT IRD, CREW NOTED A FAINT ACID LIKE SMELL AROUND CIRCUIT BREAKER PANEL. ON GROUND MAINTENANCE POWERED ALL EQUIPMENT, NO ACID LIKE SMELL NOTED. (M)
Part: AIR DISTR — ODOR (CABIN)
EN ROUTE TOL-BFI - A STRONG SMELL OF HOT ELECTRICAL EQUIPMENT WAS NOTED IN THE VICINITY OF THE CIRCUIT BREAKER PANEL BULKHEAD. MX POWERED UP ALL EQUIPMENT ON THE GROUND WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: ENG ANTI-ICE — ODOR (NR 2)
EN ROUTE BETWEEN DFW AND TOL, THE USE OF THE NR 2 ENGINE ANTI-ICE PRODUCED AN ODOR SIMILAR TO A BURNED MATCH, BUT THE ODOR DISSIPATED OVER THE COURSE OF THE FLIGHT. IN TOL, A GROUND RUN WAS ACCOMPLISHED WITH THE AIRCRAFT CLOSED. BOTH AIR CONDITIONING PACKS WERE OPERATED AS WELL AS ALL FOUR ENGNE ANTI-ICE SYSTEMS. ALL SYSTEMS OPERATED NORMALLY WITH NO ODOR BEING PRODUCED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: AIR DISTR — ODOR (COCKPIT)
EN ROUTE FROM TOL-DFW - THE FLIGHT CREW NOTED A FAINT SULPHUR LIKE ODOR PRESENT AT TIMES IN COCKPIT, POSSIBLY COMING FROM THE COCKPIT LIGHTING. ON THE GROUND IN DFW, THE COCKPIT LIGHTS WERE OPERATED AND INSPECTED. THE COCKPIT LIGHTING SYSTEMS OPERATED NORMALLY AND DID NOT PRODUCE AN ODOR. (M)
Part: AIR DISTR — ODOR (CABIN)
IN CRUISE BETWEEN BFI AND TOL, IT WAS NOTED THAT A SMOKEY OR OILY SMELL WAS COMING OUT OF THE AIR CONDITIONING SYSTEM IN THE COCKPIT AND COURIER AREAS. IN TOL, MAINTENANCE CLEANED THE RECIRC FAN SCREEN, SERVICED THE LAV, AND RAN THE AIR CONDITIONING PACKS. NO ABNORMAL ODORS WERE NOTED. (M)
Part: CHANNEL — CRACKED (LT TE FLAP)
DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE INBOARD FLAP, OUTBOARD END, UPPER CENTER CHANNEL SECTION. THE CRACKED PART WAS REMOVED, FABRICATED AND INSTALLED IAW EO 8-57-067-96, AND THE AIRCRAFT SRM 51-2-0. (X)
Part: PANEL — DELAMINATED (LEFT WING)
DURING ROUTINE C-CHECK INSPECTION, A LEFT WING TRAILING EDGE HONEYCOMB PANEL WAS FOUND DELAMINATED ON THE LEFT WING UPPER SURFACE BETWEEN STATIONS XRS 436. AND XA 588.5. THE PANEL WAS REPAIRED IAW DRAWING 8-57-066-96, WHICH IS FAA DER APPROVED. (X)
Part: SKIN — CRACKED (FS -50)
DURING ROUTINE C-CHECK INSPECTION, THE FUSELAGE PLATING AT THE EXTERNAL POWER RECEPTACLE WAS FOUND CRACKED. THE CRACK WAS LOCATED BETWEEN LONGERONS 31 AND 32 RT, AT FS -50. THE CRACK WAS REMOVED, REPAIR FILLERS, DOUBLERS WERE FABRICATED AND INSTALLED IAW DRAWING 853-28-96 WHICH IS FAA DER APPROVED. (X)
Part: SPLICE FITTING — CRACKED (FS 1620)
DURING ROUTINE C-CHECK INSPECTION, LONGERON 33 LEFT, SPLICE FITTING, AT STA 1694, WAS FOUND CRACKED. THE CRACK WAS .375 INCH IN LENGTH AT THE FORWARD END OF THE FITTING. THE CRACK WAS REMOVED FROM THE SPLICE FITTING AND REINSTALLED IAW DRAWING COO-SJO-96-0139DAC AND COO-SJO-96-014DAC, WHICH IS FAA DER APPROVED. (X)
Part: SKIN — DAMAGED (FS 340)
DURING ROUTINE C-CHECK INSPECTION, THE FUSELAGE EXTERIOR PLATING WAS FOUND DAMAGED. DAMAGE WAS LOCATED AT THE FORWARD LOWER, RIGHT AFT CORNER OF THE NR 1 BASKET DOOR CUT-OUT, AT FS 340. THE DAMAGED AREA WAS REMOVED. THE REPAIR WAS ACCOMPLISHED BY FABRICATING AND INSTALLING A FILLER AND EXTERNAL DOUBLERS BETWEEN FS 328-FS 340 AND LONGERONS 29-31 RIGHT. REPAIR WAS ACCOMPLISHED IAW DRAWING 8-53-24-96 WHICH IS FAA DER APPROVED. (X)
Part: SKIN — DAMAGED (DOOR CUT OUT)
DURING ROUTINE C-CHECK INSPECTION, DAMAGED WAS NOTED TO THE LOWER FORWARD CARGO COMPARTMENT DOOR CUT-OUT AT THE FORWARD EDGE. THE DAMAGE WAS REMOVED, REPAIR FILLER AND DOUBLERS WERE FABRICATED AND INSTALLED IAW DRAWING 8-53-27-96, WHICH IS FAA DER APPROVED. (C)
Part: PANEL — DELAMINATED (RT WING)
DURING ROUTINE C-CHECK INSPECTION, A RIGHT WING TRAILING EDGE FIXED PANEL WAS FOUND DELAMINATED. THE PANEL WAS DELAMINATED BETWEEN WING STATIONS XA 589.0 AND XA 624.0. REPAIR OF THE PANEL WAS ACCOMPLISHED INSTALLING AN EXTERNAL DOUBLER IAW DRAWING 8-57-064-96, WHICH IS FAA DER APPROVED. (X)
Part: SKIN — CRACKED (FS 336)
DURING ROUTINE C-CHECK INSPECTION, AN EXTERNAL FUSELAGE SKIN CRACK, LOCATED AT FS 336.5 AND LONGERON 36, WAS FOUND. THE DAMAGED SKIN WAS REMOVED, FILLERS AND DOUBLERS FABRICATED AND INSTALLED. THE REPAIR WAS IAW WITH DRAWING 8-53-29-96, WHICH IS FAA DER APPROVED. (X)