N866UP

Part: SWITCH — STICKING (MLG HANDLE)

GEAR DOWN LIGHTS (GREEN) INOPERATIVE. CREW DECLARED EMERGENCY. REMOVED AND REPLACED LANDING GEAR LEVER SWITCH IAW DC-8 AMM 32-60-00-2. DISCREPANCY TROUBLESHOT IAW DC-8 AMM CH 32-60-00-1 AND FOUND SWITCH ACTUATION STICKY. OPS CHECKS NORMAL. GEAR SWING NOT NECESSARY PER AMM CH 3 2-60-00-2 1C.

Part: STIFFENER — CORRODED (AFT BULKHEAD)

EVIDENCE OF CORROSION FOUND ON AFT SIDE OF AFT PRESSURE BULKHEAD APPROX 18" FROM RT SIDE OF AIRCRAFT BEHIND CENTER HORIZONTAL STIFFENER. ALSO, FOUND POWDER ON TOP OF STIFFENER BELOW AREA IN QUESTION. A/C FERRIED TO SAA DEF D336666 XFER TO NRC 802138. BLENDED AREA & REMOVED OXIDATION & LIGHT SURFACE CORROSION IAW DC8 SRM 51-1-8. REQ NDT FOR MAT LOSS. THICKNESS RANGED .049"-.O50". WEB AT AFT PRSR BULKHEAD ON RH SIDE APROX 18" FROM RH SIDE OF A/C REM. OF MAT IS APPROX .001. ORIG THICKNESS 0.050 W/IN LIMITS.CLEANED OXIDATION FROM STIFFNER IAW MM 51-20-00. PRIME/TREAT IAW SRM 51-1-8.

Part: SMOKE GOGGLES — SCRATCHED (COCKPIT)

INSPECTION TYPE:N/A F/O'S SMOKE GOGGLES SCRATCHED. PLACED NEW SMOKE GOGGLES IN F/O'S STOWAGE BAG.

Part: LAMP — INOPERATIVE (COCKPIT LIGHT)

FOUND ENTRY DOOR LIGHT INOP. RELAMPED OPS CK NORMAL REF MM 33-31-01-2.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT)

NUMEROUS AUTOPILOT DISCONNECTS AFTER LEVEL OFF AND APPROACH. FD FLAG WAS INTERMITTENT AND EVENTUALLY BECAME VERY INTERMITTENT. SECURED FLT DIRECTOR AND AP. RVSM RESTRICTED. PER COMMENT ABOVE AND PERFORMED OPS CHECK FCC PER MM 2210-21-5 FCC OPS CHECK GOOD NO DEFECTS NOTED. THIS CLEARS M318550.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01-2. OPS CHECK GOOD.

Part: FINGER DOUBLER — CRACKED (BS 207 L21L) · airframe 85,856 hrs · 28,516 cycles

FOUND FINGER DOUBLER AT FS 207 HAS TWO CRACKS 3" AND 2" BELOW L21L. REMOVED FINGER DOUBLER AT FS 207 L21L IAW SRM 51-1-20D. FABRICATED AND INSTALLED FINGER DOUBLER AT FS 207 L21L IAW SRM 53-4-1 FIG 4, AND SRM 51-1-21.

Part: FITTING — CRACKED (FS216 L21L) · airframe 85,856 hrs · 28,516 cycles

NA FRAME SUPPORT ATTACH FITTING BELOW L21L AT FS 216 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, AND SRM 51-3-2 AT FS 216 L21L.

Part: DOOR FRAME — MISREPAIRED (CARGO DOOR) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE:C2 AFTER REMOVAL OF MCD AFT LWR JAMB FOUND ADDITIONAL CUT OUTS NOT PER SRM OR SRO 8530027. FABRICATED AND INSTALLED -1, -3,DOUBLERS AND -5, -7 TRIPPLER AND -11, AND -13 FILLERS IAW UPS EO DC8-5330-23194-A, SAA SK 866-833270, BOEING MESSAGES 1-136046332-5, AND 1-136046332-7, AND FAA FORM 8100-9.

Part: STIFFENER — CORRODED (FS283 APIT DOOR) · airframe 85,856 hrs · 28,516 cycles

C2 A-PIT STA 283 AT LWR FWD DOOR CUTOUT, EXTRUDED STIFFNER IS CORRODED OUT OF LIMITS. REMOVED A-PIT LWR FWD DOOR CUTOUT STIFFNER IAW SRM 51-1-24 FABRICATED AND HEAT TREATED STIFFNER IAW DWG 5733892 AND INSTALLED STIFFNER AT STA 283 LWR FWD DOOR CUTOUT IAW DWG 5733892 AND SRM 51-1-20D.

Part: STRINGER — CRACKED (#4 ALT STR.64) · airframe 85,856 hrs · 28,516 cycles

NR 4 ALT HAS CRACK ON STRINGER 64 NEAR FRONT SPAR. REMOVED, FAB`D AND INSTALLED STRINGER SPLICE IAW SRM 51-1-21, 51-1-20D.

Part: FITTING — CRACKED (BS 1490) · airframe 85,856 hrs · 28,516 cycles

FOUND CRACKED LONGERON END FITTING AT STA 1490 L33R. REMOVED LONGERON AND END FITTING IAW SRM 51-1-20D. INSTALLED LONG TRAVERSE SKIN SPLICE FITTING IAW SRM 51-1-20D AT STA 1490 L33R.

Part: FINGER DOUBLER — CRACKED (BS 1350-1490) · airframe 85,856 hrs · 28,516 cycles

FINGER DOUBLER CRACKED AND CORRODED AT STA 1350-1490 L31L. REMOVED FINGER DOUBLER AT STA 1350-1490 L31L IAW SRM 51-1-21. FABRICATED AND INSTALLED FINGER DOUBLER AT STA 1350-1490 L31L IAW SRM 51-3-2, AND SRM 51-1-8, AND 51-1-21.

Part: SHEAR TIE — CRACKED (BS 1395) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE:C2 CRACKED SHEAR TIE AT STA 1395 BETWEEN L35 AND L36 RT. REMOVED SHEAR TIE IAW SRM 53-2-0 FIG 2B, FABRICATED AND INSTALLED SHEAR TIE AND SPLICE REPAIR IAW SRM 53-2-0 FIG 2D AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1880) · airframe 85,856 hrs · 28,516 cycles

FS 1880 L36 END FITTING IS CRACKED AT FASTENER HOLE. REMOVED AND REPLACED LONGERON END FITTING IAW SRM 51-1-20D AND SRM 51-1-21.

Part: FITTING — CORRODED (BS 1890) · airframe 85,856 hrs · 28,516 cycles

C2 BS 1890 L32L END FITTING HAS CORROSION AND ELONGATED HOLES. REMOVED AND REPLACED END FITTING AT FS 1890 L32L IAW SRM 51-1-20D, AND SRM 51-3-2.

Part: SHEAR TIE — CRACKED (FS710 L35L) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE: C2 SHEAR TIE AT STA 710 L35L IS CRACKED. REMOVED SHEAR TIE AT STA 710 L35L IAW SRM 51-1-20D, FABRICATED AND INSTALLED SHEAR TIE AT STA 710 L35L IAW DWG 5750365, AND SRM 51-1-21D.

Part: LONGERON — CORRODED (BS 1880) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE:C2 LONGERON L32L CORRODED AND HAS ELONGATED HOLES AT FS 1880. REMOVED LONGERON 32L AT FS 1880 IAW SRM 51-3-0. FABRICATED AND INSTALLED LONGERON AND SPLICE FITTING AT FS 1880 L32L IAW SRM 53-02-02 AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FS17901880L36) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE:C2 FS 1790 TO FS 1880 L36 IS CRACKED AND HAS ELONGATED HOLES. REMOVED LONGERON 26 AT FS 1790 TO 1880 IAW SRM 51-1-20D FABRICATED AND INSTALLED LONGERON 36 AND SPLICE REPAIR IAW S1415997 AND SRM 51-1-20D, AND 51-1-20.

Part: ANGLE — CORRODED (BS 1190) · airframe 85,856 hrs · 28,516 cycles

C-PIT AT STA 1190 RBL 39 L-ANGLE HAS INTERGRANULAR CORROSION. REMOVED ANGLE IAW SRM 51-1-20D, FABRICATED AND INSTALLED ANGLE AT STA 1190 RBL 39 IAW DWG 5711283, SAA SK 866-833103, UPS EO FILE NUMBER DC8-53-20512, AND BOEING MESSAGE NR 1-134429123-2 DATED 10-18-2005.

Part: DOUBLER — CORRODED (FUSLEAGE) · airframe 85,856 hrs · 28,516 cycles

AT 60 HOLE INTERNAL SUPPORT DOUBLER HAS CORROSION OUT OF LIMITS AND DOUBLE DRILLED HOLES. REMOVED INTERNAL SUPPORT DOUBLER AT THE 60 HOLE IAW SRM 51-3-0. FABRICATED AND INSTALLED INTERNAL SUPPORT DOUBLER AT THE 60 HOLE IAW DWG 5649329.

Part: SKIN — CRACKED (MCD LWR AFT CRNR) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE: C2 FUSELAGE SKIN HAS A .5 INCH CRACK AT MCD LWR AFT CORNER, UNDER REMOVED SCUFF PLATE, AT PREVIOUS CUT OUT. TRIMMED OUT CRACK AT MCD LWR AFT CORNER IAW DWG SR 08530027, FABRICATED AND INSTALLED -11 FILLERS, -4 DOUBLER AND -7 DOUBLER IAW DWG SRO8530027.

Part: FITTING — CORRODED (BS 1180) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE:C2 C PIT INTERGRANULAR CORROSION ON BATH TUB FITTING AT STA 1180 L35L . REMOVED BATHTUB FITTING AT STA 1180 L35L IAW SRM 51-1-20D AND 51-1-21. REPLACED BATH TUB FITTING AT STA 1180 L35L IAW SRM 53-2-0 FIG 2D AND SRM 51-1-8.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE:C2 ANGLE CRACKED ON FWD SIDE OF APB AT L6L. REMOVED ANGLE AT FWD SIDE OF AFT PRESS BULKHEAD IAW SRM 51-1-21. FABRICATED AND INSTALLED ANGLE ON FWD SIDE OF APB AT L6L IAW DWG 5773844 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 210) · airframe 85,856 hrs · 28,516 cycles

A-BAG BIN, L28L SPLICE FITTING CRACKED STA 210. REMOVED CRACKED SPLICE FITTING AT STA 210 L28L IAW SRM 51-1-20D. FABRICATED AND INSTALLED LONGERON SPLICE FITTING AT STA 210 L28L IAW DWG 4653726 ANG SRM 51-3-2, AND SRM 51-1-20D.

Part: FITTING — CORRODED (FS1200 L26L) · airframe 85,856 hrs · 28,516 cycles

C2 C-PIT STA 1200 L26L BANANA FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED BANANA FITTING AT STA 1200 L26L IAW SRM 53-2-0, AND 51=1-20D,AND SRM 51-3-2.

Part: DOOR FRAME — CRACKED (BS 280) · airframe 85,856 hrs · 28,516 cycles

A-PIT DOOR JAMB FWD LWR CORNER O/B OF L33R STA 280 ANGLE IS CRACKED APPROX 1". REMOVED AND REPLACED DOOR FRAME JAMB FITTING IAW SRM 51-1-20D AND SRM 51-1-8.

Part: FITTING — CRACKED (BS 1180) · airframe 85,856 hrs · 28,516 cycles

C-PIT STA 1180 L26L BANANA FITTING CRACKED. REMOVED AND INSTALLED NEW BANANA FITTING AT STA 1180 L26L IAW SRM 51-3-2 AND SRM 51-1-20D.

Part: SPLICE — CRACKED (BS 440-460) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE:C2 A PIT L31L SPLICE FITTING CRACKED BETWEEN STA 440 AND 460. REMOVED AND REPLACED SPLICE FITTING AT STA 440-460 L31L IAW SRM 51-1-20D, 51-3-2.

Part: FITTING — CORRODED (BS 278 L35R) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE:C2 A-CROSS SLIDE DOOR TORQUE BOX, CORROSION ON LONGERON 35R FS 278. REMOVED BATHTUB FITTING AT STA 279 L35R-L36 IAW SRM 51-1-20D. INSTALLED NEW BATHTUB FITTING AT FS 279 L35R-L35 IAW SRM 53-04-01.

Part: FINGER DOUBLER — CRACKED (BS 920-940) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE:C2 FINGER DOUBLER CRACKED AT STA 920-940 LBL 60. REMOVED FINGER DOUBLER AT STA 920-940 LBL 60 IAW SRM 51-1-20D AND 51-3-0. FABRICATED AND INSTALLED FINGER DOUBLER AT STA 920-940 LBL 60 IAW SRM 53-07-03 FIG 004 AND SRM 51-1-21 SRM 51-1-20D.

Part: BULKHEAD — CRACKED (BS 1766) · airframe 85,856 hrs · 28,516 cycles

FOUND CRACK ON AFT PRESS BULKHEAD LBL 26, 65 INCHES FROM FLOOR CUT OUT DAMAGED AREA AT FS 1766 LBL26 IAW SRM 53-2-5 FIG 14, NDT AREA IAW SPM 06-10-01-001, NO CRACKS NOTED AT CUT OUT AREA. FABRICATED -15, -17 DOUBLERS AND -9, -11, -13 AND -19 FILLERS IAW SRM 53-2-5-1A FIG 1A AND INSTALLED REPAIR PARTS IAW SRM 53-2-5 FIG 1A PG 3.

Part: FITTING — CORRODED (FS280 L32L) · airframe 85,856 hrs · 28,516 cycles

C2 A- PIT BAG BIN, INTERGRANULAR CORROSION ON BATH TUB FITTING AT STA 280 L32L. REMOVED AND REPLACED BATH TUB FITTING AT STA 280, L32L IAW SRM 53-02-00 FIG 002D AND SRM 51-1-21.

Part: FITTING — CRACKED (BS 822.5) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE:C2 FS 822.500 RBL 24 FWD FITTING CRACKED. REMOVED AND REPLACED FITTING AT FS 822.500 RBL 24 IAW SRM 51-1-20D, 51-3-2 AND SRM 51-3-0.

Part: FITTING — CRACKED (FS 1775 L17L) · airframe 85,856 hrs · 28,516 cycles

FOUND L17L CRACKED AT END FITTING IN 60 COMPT, STA 1775. REMOVED END FITTING AT FS 1775 L17L IAW SRM 51-1-21. FABRICATED AND INSTALLED LONGERON AND END FITTING IAW SRM53-5-1 FIG 7 AND SRM 51-1-20D.

Part: SPAR — CORRODED (FS857 RBL26-46) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE:C2 PRESSURE PANEL AT STA 857 RBL 26 TO 46 REAR SPAR TO FUSELAGE ANGLE EXFOLIATED. REMOVED ANGLE CHORD AT STA 857 RBL 26 TO 46 IAW SRM 51-1-20D. LOCATED AND DRILLED RT UPPER AFT SPAR CHORD AND INSTALLED SPAR CHORD IAW SRM 51-1-20D AND SRM 53-2-05-0 FIG 16.

Part: FLOORBEAM — CRACKED (FS940 RBL60) · airframe 85,856 hrs · 28,516 cycles

FOUND FLOORBEAM CRACKED 2" LONG AT FS 940 RBL 60 UPPER FLANGE AREA. CUT OUT DAMAGED AREA OF FLOORBEAM AT STA 940, RBL 60 IAW SRM TR# 53-152, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM TR# 51-1-21 FIG 1AND SRM 51-1-20D AT STA 940 RBL60.

Part: CUSP WEB — CRACKED (FS1080 L21L) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE: C2 C CUSP CRACKED 3 INCH LONG STA 1080 L21L. REMOVED DAMAGED AREA IAW SRM 53-02-05-0 AT FS 1080 L21L FABRICATED AND INSTALLED CUSP SPLICE,-7 DOUBLER, -3 AND -5 ANGLES AND -9 CUSP IAW 51-1-21, AND SRM 53-2-5 FIG 1.

Part: FLOORBEAM — CORRODED (BS 940) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE:C2 FLOORBEAM HEAVY CORROSION STA 940 LBL 60 UNDER THE SEAT TRACK. CUT OUT DAMAGED AREA OF FLOORBEAM IAW SRM 53-2-0 AND TEMP REV 53-152, FABRICATED AND INSTALLED REPAIR ANGLE AT STA 940 LBL 60 IAW SRM 53-2-0 TEMP REV 53-152, AND SRM 51-1-20D.

Part: SPAR CAP — CRACKED (CENTER WING) · airframe 85,856 hrs · 28,516 cycles

FOUND CRACK ON CENTER WING REAR SPAR LWR CAP, INSIDE KEEL BEAM BOX RT SIDE. STOP DRILLED CRACK AT REAR SPAR IAW SK SAA 866-832589, NDT VERIFIED CRACK TERMINATES AT STOP DRILL IAW NDT SPM 06-10-01.001 REPAIRED RT WING, REAR SPAR, LWR CAP CENTER LINE AT XCW-0 IAW UPS DC8-57-20144-A, BOEING MESSAGE 1-131953277-2 DATED 10/12/05, FAA FORM 8100-9 DATED 10/12/05, AND SAA SK 866-832589-A.

Part: FINGER DOUBLER — CORRODED (BS 880) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE:C2 STA 880 RBL 65 SUBFLOOR FINGER DOUBLER HAS HEAVY CORROSION. REMOVED FINGER DOUBLER AT STA 880 RBL 65 IAW SRM 51-1-21, AND 51-3-0, FABRICATED AND INSTALLED FINGER DOUBLER AT FS 880 RBL 65 IAW SRM 53-7-3 FIG4, 51-9-0 FIG 68A, AND SRM 51-1-21.

Part: FITTING — CORRODED (BS 70) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE:C2 CORROSION ON END FITTING AT L35L BS 70 A/C COMPT. REMOVED AND REPLACED END FITTING IAW SRM 51-1-21, 51-1-8 SRM 53-2-0 AND 51-1-20D.

Part: PRESSURE PANEL — CORRODED (FS 940 RBL 65) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE:C2 FUSELAGE FLOORBEAM HEAVY CORROSION STA 940 RBL 65. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS AT STA 940 RBL 65 IAW UPS EO DC8-5330-23084-A, SAA SK 866-832597, BOEING MESSAGE 1-133200277-3 AND FAA FORM 8100-9.

Part: CUSP WEB — CRACKED (FS220 L21R) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE:C2 CUSP CRACKED 3 INCH LONG STA 220 L21R. CUT OUT DAMAGED AREA OF CUSP AT FS 220 L21R IAW SRM 51-1-21D, FABRICATED AND INSTALLED REPAIR -25 ANGLES, CUSP SPLICE AND -21 DOUBLER IAW 53-2-5 FIG 1, 53-2-5 FIG 1 AND SRM 53-02-05 FIG 5.

Part: CUSP WEB — CRACKED (FS1140-1170 L21L) · airframe 85,856 hrs · 28,516 cycles

FOUND CUSP CRACKED STA 1140 L21L. REMOVED CRACK CUSP AT FS 1140 L21L IAW SRM 53-2-5 FIG 15. FABRICATED AND INSTALLED -3 ANGLES, -7 DOUBLERS AND CUSP AT FS 1140 TO 1170 IAW SRM 53-2-5 FIG 15 AND 53-1-2 FIG 1.

Part: FITTING — CORRODED (BS 1500) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE:C2 STA 1500 L21R FUSELAGE FRAME TO CUSP FITTING HEAVY CORROSION. REMOVED FRAME FITTING TO CUSP AT FS 1500 L21R IAW 51-1-8 AND SRM 53-02-0 FIG 1F. REPLACED FUSELAGE FRAME TO CUSP FITTING IAW SRM 51-3-2, AND SRM 51-1-20D.

Part: SHEAR WEB — CORRODED (FS 857) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE:C2 HEAVY CORROSION ON RT W/W FWD BULKHEAD STA 857, RBL 26. CUT OUT CORROSION IN SHEAR WEB AT STA 857 RBL 26 AND INSTALLED REPAIR PARTS IAW UPS ENG FILE DC8-53-20517 SAA SK 866-832582, BOEING MESSAGE 1-137210970-2, AND FAA FORM 8100-9.

Part: LONGERON — CORRODED (FS690-710 L31L) · airframe 85,856 hrs · 28,516 cycles

FOUND L31L CORRODED BEYOND LIMITS IN LT BELLY STRESS PNL STA 690-710. REMOVED LONGERN 31L FS 690-710 IAW SRM 53-02--02-0. FABRICATED AND INSTALLED LONGERON 31L AND -37. REPAIR SPLICES IAW DWG 3750575 AND SRM 53-02-02-0 AND SRM 51-1-20D.

Part: PRESSURE PANEL — CORRODED (FS960 LBL57-62) · airframe 85,856 hrs · 28,516 cycles

C2 CORROSION UNDER DOUBLER ON LT W/W CEILING STA 960 LBL 57-62, CORROSION AT SAME LOCATION IN MAIN CABIN UNDER FLOORBEAM. REMOVED MLG LT WHEEL WELL HORIZ. PRESSURE PANEL WEB AT FS 960 LBL 57-62 IAW SAA SK 866-832452, AND UPS EO FABRICATED AND INSTALLED PRESSURE PANEL, REPAIR DOUBLERS, FINGER DOUBLERS AND SPLICE REPAIRS IAW EO, AND SAA SK 866-832452.

Part: SKIN — DAMAGED (RUDDER) · airframe 85,856 hrs · 28,516 cycles

INSPECTION TYPE:C2 RUDDER RIGHT SIDE HAS 18EA CREASES JUST ABOVE UPS LOGO 2ND HINGE POINT FROM TOP. REMOVED AND REPLACED SKIN ON RUDDER STA ZR53-ZR71 IAW SRM 55-02-00 FIG 6 AND SRM 51-1-21.

Part: SKIN — CORRODED (STA.1690 L28R- L) · airframe 85,856 hrs · 28,516 cycles

FOUND FUSELAGE SKIN HAS HEAVY CORROSION AND SEVERAL CRACKS AT AFT MANUFACTURING SPLICE AREA STA 1690 L32L TO L32R. REMOVED AND REPLACED SKIN FROM STA 1690 TO 1890 L28R TO L28L IAW SRM 51-1-21, 51-3-2, 51-20-00, 51-3-0 AND 51-1-20D.

Part: SKIN — DELAMINATED (RT WING SPOILER)

RT WING INBOARD SPOILER DELAMINATED.

Part: EADI — FAILED (COCKPIT)

ELECTRICAL BURNING SMELL FROM F/O'S SIDE DURING APPROACH FOR APPROX 10 - 15 SECONDS. ALL FLUORESCENT LIGHTS WERE OFF. TURNED ON ALL LIGHTS, RAN BOTH PACKS, OPERATED ALL NAVIGATION COMPT, INSPECTED ALL WIRES AT F/O'S INSTRUMENT PANEL, NO ELECTRICAL BURNING SMELL NOTED. REMOVED AND REPLACED F/O'S EADI AS PER MM 34-23-01-4 FOR HIGH TEMP AND PRECAUTIONARY OPS CKS NORMAL. OK FOR SERVICE.

Part: ENGINE — LEAKING (NR 1)

INSPECTION TYPE: C1, ENG 1 BEGAN RAPIDLY LOSING OIL QUANITY PASSING FL 250. THE OIL PRES SURE ALSO DROPPED TO 35 PSI. THE CREW COMPLETED THE INFLIGHT ENGINE SHUTDOWN CHECK LIST. DECLARED AN EMERGENCY AND RETURNED TO SAT FOR AN UNEVENTFUL LANDING. FOUND STARTER FILL PLUG LOOSE (DISCONNECTED), SERVICED STARTER AND ENGINE OIL CKD ENG CHIP DETECTORS, NO DEFECTS NOTED. DETECTORS WERE CLEAN RAN ENGINE AT IDLE NO LEAKS NOTED. RAN ENG AT T/O POWER 3 TIMES FOR 2 MINS EACH, OIL QUANTITY REMAINED STABLE & OIL PRESSURE GOOD. REMOVED AND REPLACED ENG STARTER (PRECAUTIONARY).

Part: FITTING — CRACKED (AFT LOWER CARGO) · airframe 85,040 hrs · 27,876 cycles

INSPECTION TYPE: C1, STA 1180 BATHTUB FITTING IS CRACKED BETWEEN LONG. 33R TO 34R. R & R FITTING IAW SRM. 53-2-0 FIG. 2D AND DWG. 3755841

Part: RIB — CRACKED (VERTICLE STAB LE) · airframe 85,040 hrs · 27,876 cycles

INSPECTION TYPE: C1, VERTICLE STAB LE RT RIB IS CRACKED AT ZFS 68. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATED CRACK,FABRICATED AND INSTALLED REPAIR ANGLE I.A.W. SRM. 55-2-0 FIG.2

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 85,040 hrs · 27,876 cycles

INSPECTION TYPE: C1, MAIN CABIN SEAT TRACK IS CORRODED BEYOND LIMITS AT STATION 1350 LBL 60. REMOVED, FABRICATED AND REPLACED SEAT TRACK SECTION BETWEEN STATION 1270 TO 1370 AT LBL 60 IAW DC8-5320-5167-C, DC8-53B-003.

Part: RIB — CRACKED (RIGHT WING LE) · airframe 85,040 hrs · 27,876 cycles

INSPECTION TYPE: C1, RT WING LE. RIBS CRACKED AT XFS760 UPPER,XFS 766.25 UPPER, XFS 822.5 LOWER STOP DRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATE CRACKS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM. 57-2-0 FIG. 2

Part: RIB — CRACKED (LT WING) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE:C1 LEFT WING L/E RIB IS CRACKED AT XFS 735. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE:C1 STATION 1184 BATHTUB FITTING IS CRACKED BETWEEN LONG 35R-34R. REMOVED AND REPLACED FITTING IAW DWG 3755843, AND SRM 53-2-0 FIG 2D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE:C1 BATHTUB FITTING IS CORRODED BEYOND LIMITS AT STA 1160 BETWEEN LONG 35R AND LONG 36. REMOVED AND REPLACED FITTING IAW DWG 3755845, AND SRM 53-2-0 FIG 2D.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 85,040 hrs · 27,876 cycles

INSPECTION TYPE: C1, SEAT TRACK CORRODED BEYOND LIMITS AT STA. 1188 AT RBL 60. REMOVED SEAT TRACK SECTION BETWEEN STA. 1070 TO 1210, FABRICATED AND INSTALLED REPLACEMENT SECTION I.A.W. SRM. 53-2-3 FIG. 14

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE:C1 SEAT TRACK IS CORRODED BEYOND LIMITS AT STA 1582 AT RBL 25. REMOVED SEAT TRACK SECTION BETWEEN STATION 1490 AND 1600, FABRICATED AND INSTALLED SEAT TRACK IAW DWG S2400463, AND SRM 53-2-3 FIG 13.

Part: FITTING — CRACKED (FUSELAGE) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE:C1 STATION 1204 BATHTUB FITTING IS CRACKED BETWEEN LONG 34R TO 35R. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 85,040 hrs · 27,876 cycles

INSPECTION TYPE: C1, SEAT TRACK IS CORRODED BEYOND LIMITS AT STA. 1325 LBL. 50. REMOVED SEAT TRACK SECTION STATION 1270 TO 1470, FABRICATED AND INSTALLED SEAT TRACK SECTION DC8-5320-8309

Part: FITTING — CRACKED (FUSELAGE) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE:C1 STA 340 BETWEEN LONG 33L-34L BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755822, AND SRM 53-2-0 FIG 2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE:C1 SEAT TRACK IS CORRODED BEYOND LIMITS AT REPAIR PLUG AT STA 1400 AT RBL 46. CUT OUT SEAT TRACK BETWEEN STA 1370 TO 1410, FABRICATED AND REPLACED SEAT TRACK SECTION IAW DC8-5320-8309 APPX B.

Part: SPLICE — BROKEN (FUSELAGE) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE:C1 STA 210 LONG 31L SPLICE FITTING IS BROKEN. REMOVED AND REPLACED FITTING IAW DWG 3754220 AND SRM 51-1-20D.

Part: FITTING — CRACKED (AFT LOWER CARGO) · airframe 85,040 hrs · 27,876 cycles

INSPECTION TYPE: C1, TORQUE BOX VERTICLE LEG SUPPORT FITTING IS CRACKED AT STA. 1220 LONG. 27R. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG. 3754025,AND SRM. 51-1-20D,AND SRM. 51-3-0

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE:C1 MAIN CABIN SUBFLOOR FINGER DOUBLER IS CRACKED AT STA 930 AT BL 0. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5646674 AND SRM 53-7-3 FIG 4, 51-1-20D.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 85,040 hrs · 27,876 cycles

INSPECTION TYPE: C1, LOWER FUSELAGE FRAME SUPPORT C-CHANNEL IS CRACKED AT STA 1000 AT LONG 28R. REMOVED, FABRICATED AND REPLACED SUPPORT FRAME C-CHANNEL IAW SRM 53-4-1 FIG 51.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 85,040 hrs · 27,876 cycles

INSPECTION TYPE: C1, STATION 565 LONG 33R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON BETWEEN STATION 450 TO 610 IAW DWG 3750539 SRM 53-2-2 FIG 10.

Part: SUPPORT FITTING — CRACKED (FWD LOWER CARGO) · airframe 85,040 hrs · 27,876 cycles

INSPECTION TYPE: C1, TORQUE BOX VERTICLE LEG SUPPORT FITTING IS CRACKED AT STA. 340 LONG. 27R. REMOVED AND REPLACED FITTING IAW DWG 3754025, AND SRM. 51-1-20D

Part: FITTING — CORRODED (FUSELAGE) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE:C1 BATHTUB FITTING IS CORRODED BEYOND LIMITS AT STA 340 BETWEEN LONG 27L-28L. REMOVED AND REPLACED FITTING IAW DWG 3755822 AND SRM 53-2-0 FIG 2D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 85,040 hrs · 27,876 cycles

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

Part: FINGER DOUBLER — CORRODED (COCKPIT SUBFLOOR) · airframe 85,040 hrs · 27,876 cycles

INSPECTION TYPE:C1 RT SIDE COCKPIT SUBFLOOR STA 100 NEXT TO FUSELAGE ON FLOOR FINGER DOUBLER CORRODED BEYOND LIMITS AT RBL 60. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5612298 AND SRM 51-1-20D.

Part: SUPPORT FITTING — CORRODED (LOWER CARGO) · airframe 85,040 hrs · 27,876 cycles

INSPECTION TYPE: C1, A-PIT DOOR FWD. LOWER FORWARD T-BOLT SUPPORT FITTING HAS A BACKUP FITT ING CORRODED BEYOND LIMITS AT STA. 290 AT LONG. 33R. REMOVED AND REPLACED FITTING IAW DWG. 5894282,AND SRM. 53-2-0 FIG. 2D

Part: FRAME — CRACKED (AFT CABIN) · airframe 85,040 hrs · 27,876 cycles

INSPECTION TYPE: C1, STATION 1680 FRAME IS CRACKED AT FLOOR LEVEL APPROX. LONG. 21L. CUTOUT DAMAGE, FABRICATED AND INSTALLED FRAME SPLICES AND FRAME SEGMENT IAW SRM. 53-2-0 FIG. 2

Part: FITTING — CRACKED (FUSELAGE) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE:C1 LONGERON END FITTING IS CRACKED AT STA 680 LONG 2R. REMOVED AND REPLACED END FITTING IAW DWG 3779762, AND SRM 51-1-20D AND 51-3-0.

Part: SEAT TRACK — WORN (MAIN CABIN) · airframe 85,040 hrs · 27,876 cycles

INSPECTION TYPE: C1, SEAT TRACK IS WORN BEYOND LIMITS BETWEEN STA. 480-500 AT LBL 24. REMOVED WORN SEAT TRACK STA. 470 -530, FABRICATED AND REPLACED SEAT TRACK SECTION IAW DC8-5320-5167-C,AND DC8-53B-003

Part: FRAME — CHAFED (AFT CABIN) · airframe 85,040 hrs · 27,876 cycles

INSPECTION TYPE:C1 STATION 1708 CANTED FRAME AT LONG 20R IS CHAFED BEYOND LIMITS. BLENDED OUT CHAFED AREA, AREA OF BLENDOUT BEYOND LIMITS IAW SRM 53-2-0 FIG 1F, FABRICATED AND INSTALLED ANGLE DOUBLER IAW DC8-5310-11728-A.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE:C1 MAIN CABIN SEAT TRACK IS WORN BEYOND LIMITS BETWEEN STA 340 TO 418 AT RBL 25. REMOVED, FABRICATED AND REPLACED SEAT TRACK BETWEEN STA 390-450 IAW SRM 53-2-3 FIG 8A.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE: C1, SEAT TRACK CORRODED AT STA 305 LBL58. REMOVED SEAT TRACK BETWEEN STA 290-330, FABRICATED AND REPLACED SEAT TRACK IAW SRM 53-2-3 FIG14

Part: FRAME — WORN (AFT CABIN) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE: C1, STATION 1723 CANTED FRAME AT LONG 21L HAS A HOLE WORN THRU FRAME. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 -5310-11728-A APPROX A.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 85,040 hrs · 27,876 cycles

INSPECTION TYPE:C1 STATION 320 TO 418 SEAT TRACK IS WORN BEYOND LIMITS AT LBL 45 REMOVED SEAT TRACK SECTION BETWEEN STA. 310-590,FABRICATED AND INSTALLED SEAT TRACK SECTION IAW DC8-5320-8309 APPX. B

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE:C1 SEAT TRACK CORRODED STA 1000-1040 LBL60. REMOVED SEAT TRACK STA 990-1050 LBL60, FABRICATED AND REPLACED SEAT TRACK SECTION IAW SRM 53-2-3 FIG14 AND 8.

Part: WEB — CRACKED (FUSELAGE) · airframe 85,040 hrs · 27,876 cycles

INSPECTION TYPE: C1, MAIN CABIN STA 1100 RT CUSP IS CRACKED AT LONG 21R. CUT OUT CRACKED CUSP SECTION BETWEEN STA 1080-1120, FABRICATED AND INSTALLED CUSP SECTION, DOUBLER AND SPLICES IAW SRM 53-2-5 FIG 15.

Part: LONGERON — CRACKED (AC COMPARTMENT) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE: C1, STATION 70 LONGERON 36 RT. UPPER FLANGE IS CRACKED REMOVED AND REPLACED LONGERON IAW DWG.3702969,AND SRM. 51-1-21, 51-1-20D.

Part: RIB — CRACKED (RIGHT WING LE.) · airframe 85,040 hrs · 27,876 cycles

INSPECTION TYPE: C1, RT WING LE RIBS ARE CRACKED AT XFS 610 AND XFS 616.25. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILL TERMINATES CRACKS,FABRICATED AND INSTALLED REPAIR ANGLE I.A.W. SRM. 57-2-0 FIG. 2

Part: LONGERON — CRACKED (FUSELAGE) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE: C1, STA 1730, LONG 14R CRACKED. REMOVED LONGERON SECTION 14R BETWEEN STA 1720-1766, FABRICATED AND REPLACED LONGERON SECTION IAW SRM 53-2-2 FIG10.

Part: RIB — CRACKED (LT WING) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE:C1 LEFT WING L/E LOWER RIBS ARE CRACKED AT XFS 760, XFS 785, XFS 797.5, XFS803.75, XFS 810. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING LE) · airframe 85,040 hrs · 27,876 cycles

INSPECTION TYPE: C1, RIGHT WING LE LOWER RIB IS CRACKED AT XFS 653.75, STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM. 57-2-0 FIG. 2

Part: RIB — CRACKED (RT WING) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE:C1 RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 772.500. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE:C1 RIGHT WING L/E UPPER RIBS ARE CRACKED AT XFS 728.75 AND XFS 735. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATE CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING LE) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE: C1, RT WING LE. UPPER RIB IS CRACKED AT XFS 835. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM. 57-2-0 FIG. 2

Part: SKIN — CRACKED (RT WING) · airframe 85,040 hrs · 43,393 cycles

INSPECTION TYPE:C1 RIGHT WING L/E UPPER SKIN IS CRACKED AT XFS 597.5. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW EO DC8-5720-7767-A.

Part: FITTING — CRACKED (MAIN CABIN) · airframe 85,040 hrs · 27,876 cycles

INSPECTION TYPE: C1, STA 834 FRAME TO LONGERON FITTING IS CRACKED AT LONG 14R. REMOVED AND REPLACED FITTING IAW DWG 3779978 AND SRM 51-1-20D.

Part: SLIDE — INOPERATIVE (CABIN)

LOOK AT ESCAPE SLIDE CONTAINER PARTIALLY OPEN. REPACKED AND RESECURED ESCAPE SLIDE AS REQ, A/C OK TO CONTINUE.

Part: BATTERY — DISCHARGED (FIRE DETECTOR)

INSPECTION TYPE:N/A REF: M256103 P33 LOWER CARGO FIRE DET INOP. DETECTOR BATTERY AC1296 ZERO DH. REMOVED AND REPLACED BATTERIES PER MM 26-18-02. OP GOOD, DEFERRAL CLEARED.

Part: SLIDE — LOOSE (CABIN)

ESCAPE SLIDE NOT SECURE AND GIRT BAR NOT TOTALLY IN SLIDE SLEEVE. SECURED ESCAPE SLIDE TO BRACKET WITH CAMLOCK FASTENER. REPOSITIONED GIRT BAR IN SLIDE SLEEVE. OK TO CONTINUE.

Part: AMPLIFIER — INOPERATIVE (SMOKE DETECTION)

NUMEROUS MAIN DECK SMOKE DETECTORS INOPERATIVE. REMOVED AND REPLACED SMOKE DETECTOR AMPLIFIER. ALL DETECTORS TEST OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

INSPECTION TYPE: PFLT, EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. CHECKS OK.

Part: SLIDE — INOPERATIVE (CABIN)

INSPECTION TYPE:PFLT REF M226149 EMERGENCY ESCAPE SLIDE INOP. REMOVED AND REPLACED ESCAPE SLIDE COVER WITH SERVICEABLE UNIT.

Part: PAN — CRACKED (FUSELAGE) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 L-2 DOOR LOWER PAN IS CRACKED AT STA 1630 LONG 21L. REPAIRED PAN IAW SRM 53-2-0 FIG 1B.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 STA 1620 FRAME IS CRACKED ABOVE LONG 21L. REPAIRED FRAME IAW SRM 53-2-0 FIG 1B.

Part: FITTING — CRACKED (FUSELAGE) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 STA 1140 AFT SIDE LONG 33R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514, AND SRM 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 STA 1200 LONG 35R-36 BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3755845, AND SRM 53-2-0 FIG 2D.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 STA 1260-1280 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754473, AND SRM 51-1-20D.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 STA 60 FLOORBEAM AT RBL 12 UPPER FLANGE IS CRACKED. REPAIRED FLOORBEAM IAW 8110-3 APPROVED DH SK 866-019.

Part: FITTING — CORRODED (FUSELAGE) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 STA 1225 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 31R-32R. REMOVED AND REPLACED FITTING IAW DWG 3755847, AND SRM 51-1-20D.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 STA 160 FLOORBEAM IS CORRODED BEYOND LIMITS AT RBL 38. REPAIRED FLOORBEAM IAW 8110-3 APPROVED DH SK 866-956.

Part: FITTING — CRACKED (FUSELAGE) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 STA 1152 LONG 33R BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755847, AND SRM 51-1-20D, 53-2-0 FIG 2D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 STA 1766 LONG 17R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397U1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 STA 1030-1080 LBL 24 SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 STA 1030-1080 SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 RT WHEEL WELL LONG 24R SUPPORT FITTING IS CRACKED AT STA 920. REMOVED AND REPLACED FITTING IAW DWG 5753113, AND SRM 51-1-20D, 53-2-0 FIG 8.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 STA 17 FRAME IS CRACKED AT LONG 16L-17L. REPAIRED FRAME IAW SRM 53-2-0 FIG 23.

Part: RIB — CRACKED (HORIZ STAB) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 RT HORIZONTAL STAB L/E UPPER RIB IS CRACKED AT XFS 88. REPAIRED RIB IAW SRM 55-2-0 FIG 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 STA 1600 AT LONG 20L-21L FUSELAGE SKIN AT FWD LOWER CORNER. REPAIRED SKIN IAW SRM 53-2-0 FIG 18.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 R-2 DOOR UPPER AFT CORNER SKIN IS CRACKED AT STA 1660 LONG 11R. REPAIRED SKIN IAW SRM 53-2-0 FIG 17.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 COCKPIT SUBFLOOR FINGER DOUBLER IS CORRODED BEYOND LIMITS AT STA -25 TO -8 LBL 69. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5612298, AND SRM 51-1-21.

Part: SKIN — CRACKED (LT WING) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 LEFT WING L/E SKIN IS CRACKED AT XW 485. REPAIRED SKIN IAW SRM 57-2-1 FIG 2H.

Part: RIB — CRACKED (LT WING) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 835.75, XFS 853.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C1,3 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 722.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: ANGLE — CRACKED (LT WING) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 LEFT WING L/E IB SLOT VANE IB ATTACH ANGLE IS CRACKED AT XILD .7095. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 5770138, AND SRM 51-1-21, 51-1-20D.

Part: DOUBLER — CRACKED (LT WING) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 LEFT WING L/E INTERNAL DOUBLER IS CRACKED AT XW 257. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-21, 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 LEFT WING L/E RIB IS CRACKED AT XFS 224. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: ANGLE — CRACKED (LT WING) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 LEFT WING L/E VERTICAL ATTACH ANGLE IS CRACKED AT XS 250. REMOVED,FABRICATED,AND REPLACED ANGLE IAW DWG 9753293,AND SRM 51-3-0,51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 335.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: PANEL — CORRODED (LT AILERON) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 LEFT WING OUTBOARD AILERON INBD WEIGHTED PANEL IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED WEIGHTED PANEL IAW DWG 5764617, AND SRM 57-1-0, 51-3-0.

Part: RIB — CRACKED (RT WING) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 304. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CORRODED (RT WING) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 RIGHT WING L/E INTERNAL DOUBLER IS CORRODED BEYOND LIMITS AT XFS 366.5. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-21.

Part: SKIN — CRACKED (LT WING) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 LEFT WING L/E UPPER SKIN IS CRACKED AT XFS 316.5 AND HAS A ELONGATED HOLE AT XFS 329. REPAIRED SKIN IAW 8110-3 APPROVED DH SK 866-235.

Part: SKIN — CRACKED (LT WING) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 LEFT WING L/E UPPER SKIN IS CRACKED AT XFS 666.25. REPAIRED SKIN IAW SRM 57-2-1 FIG 38.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 FUSELAGE SKIN CRACKED STA 25 LONG 10L FWD UPPER CORNER L-1 DOOR. REPAIRED SKIN IAW SRM 53-2-1 FIG 15.

Part: SKIN — DAMAGED (LT WING) · airframe 83,860 hrs · 27,062 cycles

INSPECTION TYPE:C2,3 LEFT IB SLOT VANE HAS SCREWS PULLING THRU SKIN AT XILD 7095. REPAIRED SKIN IAW SRM 57-2-1 FIG 2H.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-01, OPS CHECKS GOOD.

Part: SEAL — MISSING (FIRST AID KIT)

INSPECTION TYPE:PLFT, FIRST AID KIT MISSING SEAL. REMOVED AND REPLACED FIRST AID KIT.

Part: CONTROL VALVE — BINDING (RT AILERON)

INSPECTION TYPE:N/A AILERON BINDING, DURING CONTROL CHECKS AILERON WOULD NOT RETURN TO NEUTRAL ON ITS OWN AFTER BEING DISPLACED TO THE RIGHT. RTB *S/D* REMOVED AND REPLACED RT AILERON POWER CYLINDER/CONTROL VALVE UP TO STEP B2 AGE 204 MM 27-11-06. OPS CK LEAK CK GOOD.

Part: FLOORBEAM — CORRODED (CABIN)

INSPECTION TYPE:N/A, CORRODED FLOORBEAMS STA 1420, 1440, 1460. *S/D* REPAIRED FLOORBEAM CORROSION AT STA 1420 AND 1440 AS PER EO DC8-5310-13142A.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK.

Part: SWITCH — INOPERATIVE (RT MLG)

RIGHT MAIN LANDING GEAR INDICATED UNSAFE. CHANGED LIGHT BULBS, NO JOY. CKD FLAPS 35, NO HORN. FLY BY TOWER INDICATING GEAR WAS DOWN. LANDED STRAIGHT AHEAD - GEARS PINNED. T/S IN WORK NOW. MAYBE BAD SWITCH RIGHT GEAR DOWN. ***SUPPLEMENTAL M RR*** REMOVED AND REPLACED RT MLG DOWNLOCK SWITCH IAW MM 32-60-00 OP S CHECK GOOD. P/N ON AND OFF H14-1003, S/N ON TAG 00401758 S/N OFF 8 1640

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT INOP. REPLACED B5-55 EMERGENCY LIGHTS, OP CHECKS NORMAL.

Part: VALVE — FAILED (NLG STEERING)

LOUD NOISE AFTER TAKEOFF. GEAR WOULD NOT COME UP UNTIL FLT RELEASE HANDLE LATCH WAS USED. WHEN FLAPS WERE RETRACTED HAD A WARNING HORN AND SLOT LIGHT. DUMPED FUEL AND RETURNED TO SDF. REMOVED AND REPLACED NOSEWHEEL STEERING SHUTOFF VALVE PER MM 32-52-0 8. SYSTEM OPS CHECK NORMAL. RETRACTED GEAR OPS CHECKS GOOD P/N ON 146905 OFF 146905 S/N ON 8742 OFF 580E.

Part: CONNECTOR — FAILED (RT PACK)

INSPECTION TYPE:N/A, RIGHT PACK COMES ON BY ITSELF WITHOUT ANY COOLING. CREW DISCOVERED SMOKE IN THE COCKPIT. *S/D* REPLACED CONNECTOR P1-8001 AND REPAIRED BROKEN WIRE AR-7483255AO PER WDM 21-50, ALL OPERATIONAL CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

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

Part: O2 BOTTLE — LOW (CABIN)

INSPECTION TYPE:N/A, BOTH CREW AND COURIER 02 BOTTLES LOW. REPLACED CREW AND COURIER 02 BOTTLES CREW (P/N 6350A34-CC-C) (S/N 722518) ON (P/N 071977) FOURIER (P/N 176530-95), (S/N 302224) OFF, (S/N 782420) ON. LEAK CHECKS GOOD.

Part: INTERCOSTAL — CRACKED (BS 1240)

INSPECTION TYPE:C1, THE INTERCOSTAL AT FS 1240 AND LONGERON 33L IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE INTERCOSTAL IAW DWG 5751516 AND SRM 51-1-21.

Part: SHEAR TIE — CRACKED (BS 1060)

INSPECTION TYPE:C1 FS 1060 BETWEEN LONGERON 35R AND 36, THE SHEAR-TIE IS CRACKED. CUT OUT DAMAGED SECTION AND REPAIRED SHEAR-TIE IAW SRM 53-2-0 FIG 2B.

Part: SEAT TRACK — CORRODED (BS 440)

INSPECTION TYPE:C1 DOUBLE SEAT TRACK AT FS 440, RBL 48, IS CORRODED OUT BEYOND LIMITS. CUT OUT DAMAGED SECTION AND SPLICED IN A NEW SECTION OF SEAT TRACK IAW SRM 53-2-3.

Part: FITTING — CRACKED (BS 12)

INSPECTION TYPE:C1 AT FS -12, LONGERON 33L FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4640111 AND SRM 51-1-20D, 51-1-21, AND 51-3-0.

Part: LONGERON — CORRODED (BS 8&35)

INSPECTION TYPE:C1 BETWEEN FS 35 AND 8 LONGERON 36 IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED LONGERON IAW DWG 3615532 AND SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1220-1230)

INSPECTION TYPE:C1 FS 1220 TO 1230, LONGERON 31R END FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-3-0.

Part: FITTING — CORRODED (BS 1160)

INSPECTION TYPE:C1 FS 1160, BETWEEN LONGERON 32R AND 33R, THE BATH TUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 5-1-20D.

Part: JAMB — CRACKED (CARGO DOORWAY)

INSPECTION TYPE:C1 FS 270, THE MAIN CARGO DOOR LOWER DOOR JAMB IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE JAMB IAW DWG 5772786 AND SRM 51-1-20D AND 51-1-20.

Part: FITTING — CRACKED (BS 834)

INSPECTION TYPE:C1 FS 834 AT LONGERON 18L, THE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 385.25)

INSPECTION TYPE:C1 LT WING L/E RIB AT XFS 385.25 IS CRACKED AT THE AFT LOWER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 461.372)

INSPECTION TYPE:C1 LT WING L/E RIB AT XS 461.372 IS CRACKED AT THE AFT LOWER FASTENER. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 6.225)

INSPECTION TYPE:C1 LT WING L/E LOWER RIB AT XOLDI 6.225 IS CRACKED AT THE AFT FASTENER. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (WS 572.5)

INSPECTION TYPE:C1 RT WING L/E LOWER SKIN INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE AT XFS 572.5. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21 AND 51-1-20D.

Part: FLOORBEAM — CORRODED (BS 717)

INSPECTION TYPE:C1 FS 717, RBL 30, THE FLOORBEAM HAS HEAVY CORROSION. REPAIRED FLOORBEAM IAW DH SK866-291.

Part: FLOORBEAM — CORRODED (BS 879)

INSPECTION TYPE:C1 FS 879, RBL 12, THE CABIN FLOORBEAM HAS HEAVY CORROSION. REPAIRED FLOORBEAM IAW DH SK866-318.

Part: FLOORBEAM — CRACKED (BS 140)

INSPECTION TYPE:C1 FS 140, LBL 44, THE FLOORBEAM IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW DH SK866-902.

Part: FITTING — CRACKED (BS 350)

INSPECTION TYPE:C1 FS 350 BETWEEN LONGERON 36 AND 35L, THE BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 53-2-0 FIG 2D.

Part: FITTING — CORRODED (BS 300)

INSPECTION TYPE:C1 FS 300 BETWEEN LONGERON 34R AND 35R, THE BATH TUB FITTING HAS MODERATE CORROSION. REMOVED AND REPLACED THE FITTING IAW SRM 53-2-0 FIG 1D.

Part: SKIN — CRACKED (BS 1660)

INSPECTION TYPE:C1 THE FUSELAGE SKIN AT FS 1660, AFT ENTRY DOOR, AFT UPPER CORNER, HAS 5 CRACKS EXTENDING FROM FASTENER HOLES. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53-2-0 FIG 18.

Part: SHEAR TIE — CRACKED (BS 220)

INSPECTION TYPE:C1 FS 220, BETWEEN LONGERON 11R AND 12R, THE SHEAR TIE IS CRACKED. CUT OUT DAMAGED LEG, AND REPAIRED THE SHEAR TIE IAW SRM 53-2-0 FIG 2B.

Part: DOUBLER — CRACKED (WS 597.5)

INSPECTION TYPE:C1 RT WING L/E SKIN INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE AT XFS 597.5. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5679300 AND SRM 51-1-21.

Part: FITTING — CRACKED (BS 759)

INSPECTION TYPE:C1 EXTERNAL, CENTER SECTION KEEL BEAM FITTING AT FS 759 RT IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3758519 AND SRM 51-1-20D.

Part: SKIN — CRACKED (BS 418)

INSPECTION TYPE:C1 FUSELAGE SKIN AT FS 418, LONGERON 21L, IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW DH SK866-417.

Part: SKIN — CRACKED (LT WING)

INSPECTION TYPE:C1 LT WING L/E SKIN, ABOVE AT THE FWD END OF THE NR 1 PYLON CUT OUT IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-1A.

Part: SKIN — CRACKED (LT WING)

INSPECTION TYPE:C1 LT WING L/E SKIN AT THE FWD END OF THE NR 2 PYLON CUT OUT IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0A FIG 1.

Part: SKIN — CRACKED (RT WING)

INSPECTION TYPE:C1 RT WING L/E LOWER SKIN IS CRACKED AT THE DRAIN HOLE AT XFS 597.5. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CORRODED (BS 10)

INSPECTION TYPE:C1, A/C COMPT SKIN AT FS 10 BETWEEN LONGERON 34R AND 33R, HAS A GAP THAT LETS PRESSURIZED AIR ESCAPE AND IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SKIN IAW IAW EO DC8-5330-8942-C.

Part: SKIN — CRACKED (WS 485)

INSPECTION TYPE:C1 RT WING L/E SKIN IS CRACKED AND CORRODED AT XW 485. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-0.

Part: SKIN — CRACKED (WS 379)

INSPECTION TYPE:C1 LT WING L/E UPPER SKIN IS CRACKED AT XFS 379. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38.

Part: SKIN — CRACKED (LT WING L/E)

INSPECTION TYPE:C1 LT WING L/E UPPERSKIN AT XFS 710 IS CRACKED AT THE AFT INBD CORNER. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38.

Part: SKIN — CRACKED (WS 635)

INSPECTION TYPE:C1 LT WING L/E UPPER SKIN AT XFS 635 US CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38.

Part: SKIN — CORRODED (LT TE FLAP VANE)

INSPECTION TYPE:C1 LT OTBD SLOT VANE HAS EXFOLIATION CORROSION AT THE INBD END. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 2H.

Part: OXY BOTTLE — LEAKED (COCKPIT)

AT TOP OF CLIMB, NOTICED BOTH O2 BOTTLES WERE AT 0. REPLACED O2 BOTTLES AND LEAK CHECKED PER M/M 35-10-00 AND 35-20-00. CHECKED FOR LEAKS AT ALL REGULATORS, NO LEAKS NOTED PER 35-10-00 AND 35-20-00.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE WHEN ARMED. REPLACED BATT PACK, OPS CHECK GOOD.

Part: LINE — CRACKED (BS 198-410)

INSPECTION TYPE:N/A, ODOR IN COCKPIT AFTER BLOCK, SMELLS LIKE DIRTY SNEAKERS. SMELL EXTREMELY IRRITATING TO THE THROAT AND NOSE. FOUND CRACKED HYD LINE AT THE MAIN DECK CARGO SHUTT-OFF VALVE. REPLACED LINE.

Part: BALLAST — FAILED (RT COCKPIT)

INSPECTION TYPE-N/A, SMOKE IN FLT DECK, COMING FROM UNDER F/O'S GLARESHIELD. FOUND GLARESHIELD FLOOD LIGHTS, BALLAST (TRANSFORMER) BAD. REMOVED AND REPLACED BALLAST.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHT FAILED TO WORK DURING PRE-FLIGHT CHECK. REMOVED AND REPLACED EMERGENCY BATTERY PACK FOR EMERGENCY LIGHTS. OPS CHK GOOD.

Part: SKIN — CORRODED (CARGO DOORWAY)

INSPECTION TYPE-N/A, FOUND HI-LOK PULLED THROUGH SKIN AT LOWER BELLY NEAR PIT 33 DOOR. ALSO, FOUND 12 X 20 AREA OF CORRISION IN AREA AS ABOVE. REPAIRED AREA BY REMOVING AND REPLACING SKIN PER EO DC8-5330-10798-A.

Part: RIB — CRACKED (WS 732.75)

INSPECTION TYPE:C LT WING L/E AT STA XFS 732.750, THE L/E RIB IS CRACKED AT THE AFT LOWER END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 791)

INSPECTION TYPE:C LT WING L/E AT STA XFS 791.0. THE L/E RIB IS CRACKED AT THE LOWER AFT END. REPAIRED IAW SRM 57-2-0.

Part: FITTING — CORRODED (LT WING)

INSPECTION TYPE-C, LT WING LWR AUX SPAR TO REAR SPAR TIE FITTING HAS HEAVY CORROSION. REMOVED FABRICATED AND INSTALLED REPLACEMENT FITTING IAW 8110-3 APPROVED DHC SK 866-507.

Part: SEAT TRACK — CORRODED (BS 1130)

INSPECTION TYPE-C, FS 1130 LBL 44 TRACK IS CORRODED BEYOND ALLOWABLE LIMITS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM ADDN DC8-5320-8309-B.

Part: LONGERON — CRACKED (BS 960-980)

INSPECTION TYPE:C LONGERON 24R, CRACK HAS EXTENDED BEYOND PREVIOUS STOP DRILL AFT PAST 980 BULKHEAD AND HAS EXTENDED PAST STOP DRILL AT F/S 968 FWD TO F/S 962. REMOVED EXISTING REPAIR F/S 960-980, REMOVED LOWER FITTING F/S 960 IAW SRM 51-1-20. STOP DRILLED CRACKS IAW SRM 53-2-2 FIG 5. NDT CHECK CONFIRMED CRACK TERMINATED BY STOP DRILL. REINSTALLED EXISTING REPAIR, AND FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 7095)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XILD 7095. REPAIRED IAW SRM 57-2-0.

Part: SKIN — LIGHTNING STRIKE (BS 84)

INSPECTION TYPE:C, LIGHTNING STRIKE AT FS 84 LONG 21R, FOUND TO BE OUT OF LIMITS. REPAIRED EXTERNAL SKIN AT STA 84 LONG 21R IAW SRM 53-2-1 FIG 7.

Part: RIB — CRACKED (WS 201.25)

INSPECTION TYPE:C, LT WING L/E RIB UPPER ARM IS CRACKED BY AFT FASTENER AT STA XFS 201.250. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 778.75)

INSPECTION TYPE:C, LT WING L/E RIB UPPER AND LWR ARMS CRACKED BY AFT FSTR XFS 778.750. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 785)

INSPECTION TYPE:C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 785.000. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 816.25)

INSPECTION TYPE:C LT WING L/E RIB UPPER AND LOWER ARMS ARE CRACKED BY THE AFT FASTENER AT STA XFS816.250. REPAIRED CRACKED RIB IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 822.5)

INSPECTION TYPE:C, LT WING L/E RIB UPPER AND LWR ARMS CRACKED BY AFT FASTENER AT STA XFS 822.500. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 828.75)

INSPECTION TYPE:C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER HOLE STA 828.750. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 797.5)

INSPECTION TYPE:C, LT WING LE RIB UPPER AND LWR ARM CRACKED BY AFT FASTENER AT STA XFS 797.500, REPAIRED IAW SRM ADDN DC8-5720-4087.

Part: RIB — CRACKED (WS 810)

INSPECTION TYPE:C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 810.000. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 628.75)

INSPECTION TYPE:C, RT WING L/E AT STA XFS 628.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 735)

INSPECTION TYPE:C, LT WING L/E RIB LOWER ARM CRACKED BY AFT FASTENER STA XFS 735.000. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 647.5)

INSPECTION TYPE:C RT WING L/E AT STA XFS 647.500, THE UPPER L/E RIB IS CRACKED AT AFT END. REPAIRED IAW SRM 57-2-0.

Part: DOUBLER — CRACKED (RT AUX TANK)

INSPECTION TYPE-C, RT WING L/E AUX TANK O/B END INTERNAL DOUBLER HAS A 6 INCH CRACK. REPAIRED CRACKED INTERNAL DOUBLER IAW EO DC-8 5720-7767.

Part: RIB — CRACKED (WS 760)

INSPECTION TYPE:C, LT WING L/E RIB UPPER ARM IS CRACKED BY THE AFT FASTENER AT STA, XFS 760.000, REPAIRED IAW DC8 SRM 57-2-0.

Part: RIB — CRACKED (WS 772.5)

INSPECTION TYPE:C, LT WING L/E RIB UPPER AND LWR ARMS CRACKED BY AFT FASTENER STA XFS- 772.500. REPAIRED IAW SRM 57-2-0.

Part: SKIN — CORRODED (WS 322.75)

INSPECTION TYPE-C, RT WING L/E SECTION BETWEEN PYLONS AT XFS 322.750, L/E SKIN ON TOP AT FRONT SPAR HAS HEAVY CORROSION UNDER THE SURFACE. REPAIRED IAW SRM ADDN DC8-05720-7767-A.

Part: RIB — CRACKED (WS 366.5)

INSPECTION TYPE:C, LT WING L/E LWR ARM OF RIB CRACKED BY GUSSET AT STA XFS 366.500. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 728.75)

INSPECTION TYPE:C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA 728.750. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 803.75)

INSPECTION TYPE:C, LT WING L/E RIB UPPER AND LWR ARMS CRACKED BY AFT FSTR AT STA XFS803. 750. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 741.25)

INSPECTION TYPE:C, RT WING L/E RIB AT STA XFS 741.250 IS CRACKED AT THE UPPER AFT END. REPAIRED CRACKED RIB IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 735.75)

INSPECTION TYPE:C LT WING L/E RIB UPPER ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.735.750. REPAIRED CRACKED RIB IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 766.25)

INSPECTION TYPE:C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA XFS 766.250. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 785)

INSPECTION TYPE:C, RT WING L/E AT STA XFS 785.00, THE L/E RIB IS CRACKED AT THE UPPER AFT END. REPAIRED CRACKED RIB IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 791.25)

INSPECTION TYPE:C, LT WING L/E RIB UPPER AND LWR ARMS CRACKED BY AFT FASTENER AT STA XFS 791.250. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS I6.225)

INSPECTION TYPE:C, RT WING L/E AT STA XOLDI 6.225, THE UPPER L/E RIB HAS A 9 INCH CRACK. REPAIRED CRACKED L/E RIB AT STA XOLDI 6.225 IAW DC-8 SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 747.5)

INSPECTION TYPE:C, LT WING L/E RIB UPPER ARM IS CRACKED BY THE AFT FASTENER AT STA XF S747.500. REPAIRED IAW DC-8 SRM 57-2-0.

Part: RIB — CRACKED (WS 578.75)

INSPECTION TYPE:C LT WING L/E RIB UPPER ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.578.750. REPAIRED CRACKED L/E RIB IAW SRM 57-2-0.

Part: FRAME — CRACKED (BS 660)

INSPECTION TYPE:C FWD ACC COMP AT STA 660 BELOW STR 21R, FRAME HAS A 3 INCH CRACK NEAR RADIUS. REMOVED AND REPLACED FRAME SECTION IAW DWG 364688 AND SRM 51-1 20-D.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:C, FWD ACC COMP AT STA 680 RBL 24, SEAT TRACK SUPPORT FITTING IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DWG 5773275.

Part: FITTING — CRACKED (BS 660)

INSPECTION TYPE-C, FWD ACC COMP AT FS 660 - KEEL BEAM TIE FITTING TO STRINGER 35R IS CRACKED IN UPPER RADIUS. REMOVED AND REPLACED FITTING IAW SRM 51-3-1 AND 53-1-0.

Part: FITTING — CRACKED (BS 640)

INSPECTION TYPE-C, FWD ACC COMP FS 640 - THE KEEL BEAM TIE FITTING TO BULKHEAD FRAME IS CRACKED (TOP/INSIDE) AND BOTTOM. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: DOUBLERS — CRACKED (BS 12)

INSPECTION TYPE: CS2. LEFT AND RIGHT AFT HEAT EXCHANGERS FUSELAGE SKIN CUTOUT DOUBLERS CRACKED ON AFT LOWER CORNERS. REPAIRED PER UPS EO.

Part: WEB — CRACKED (BS 1581)

INSPECTION TYPE: CS2. FLOOR WEBBING AT FS 1581 CRACKED BOTH SIDES, LONGERONS 21L AND 21R. REPAIRED WEBBING PER RM 53-2-0.

Part: SPLICE — BROKEN (BS 190)

INSPECTION TYPE: CS2. FS 190, 2 EACH, LONGERON SPLICES BROKEN AT LONGERONS 33R AND 34R. REPAIRED SPLICES PER SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1202-1210)

INSPECTION TYPE: CS2. 2 EA BATHTUB FITTINGS CRACKED AT LONGERONS 33R A AND B, FS 1202-1210. REPLACED FITTINGS PER SRM 53-2-0 AND SRM 51-1-20D.

Part: SKIN — CORROSION (BS 1217)

INSPECTION TYPE: CS2. PERMANENT REPAIR TO BE INSTALLED DUE TO CORROSION DAMAGE ON FUSELAGE SKIN STA 1217 BELOW C-BIN DOOR CUTOUT. REPAIRED PER UPS EO.

Part: EXIT SLIDE — LOOSE (MAIN ENTRY DOOR)

INSPECTION, MAIN ENTRY DOOR EMERGENCY EXIT SLIDE UNFASTENED. RESTOWED ENTRANCE SLIDE.

Part: GIRT BAR — NOT CONNECTED (ESCAPE SLIDE)

MAINTENANCE REPORTED, ESCAPE SLIDE BAR COULD NOT BE ENGAGED. THERE IS ABOUT A 3 INCH SPACE BETWEEN BAR AND CONNECTOR. REMOVED SLIDE AND PLACED IN PFM PER UPS EO DC8-2566-7565A, DEFFERED AS PER MMOC D108876.

Part: LATCH MECH — LACK OF LUBE (LDG GEAR DOORS)

CREW REPORTED DOOR NOT LATCHED LIGHT ON AFTER GEAR RETRACTED - CHECK LIST ACCOMPLISHED: LIGHT EXTINGUISHED AFTER 4 CYCLES. INSPECTED DOOR LATCH MECHANISMS AND SWITCHES. LUBED BOTH GEAR DOOR LATCH MECHANISMS, TESTED O.K. I.A.W. DC-8-M/M 32-31-04.

Part: BATTERY PACK — DISCHARGED (FLIGHT DECK)

WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LIGHTS IN FLIGHT DECK INOP. REPLACED BATTERY PACK.

Part: PANEL — CORRODED (FS 32-12)

WHILE IN DALFORT FOR C-CHECK, MAINT FOUND FLT CABIN SUBFLOOR PRESSURE PANEL HAS HVY CORR AT SKIN JOINT FS 32 TO FS 12 LONGERON 24R. REPAIRED FOR UPS EO DC8-5310-7242-A.

Part: FITTING — CRACKED (NR 2 PYLON)

WHILE IN DALFORT FOR C-CK, MAINT FOUND .25 INCH CRACK AT NR 2 PYLON AND .75 CRACK AT NR 2 PYLON SUPPORT FITTINGS. REPLACED PER SRM 51-1-20 AND UPS EO DC8-57-580.

Part: SEAT TRACK — CORROSION (FS 863)

WHILE IN DALFORT FOR C-MAINT, FOUND MODERATE TO HEAVY CORR ON NR 7 SEAT TRACK FWD END FS 863. REPLACED TRACK SECTION FS 850 TO 950 PER SRM 53-2-3.

Part: SKIN — DELAMINATED (NR 1 SPOILER)

WHILE IN DALFORT FOR C-MAINT, FOUND LT WING NR 1 SPOILER DELAM AT LOWER SIDE. REPLACED SPOILER ASSY PER MM 27-61-01.

Part: ANGLE — CRACKED (RT MLG WW)

WHILE IN DALFORT FOR C-MAINT, FOUND RT WHEEL WELL ANGLE DOUBLER CRACKED AT FWD INBD CORNER, INBD OF SPIDER BRACKET. REPLACED ANGLE PER SRM 51-1-20D.

Part: FRAME — CRACKED (FS 76)

WHILE IN DALFORT FOR C-MAINT, FOUND FRAME HAS A 2 INCH CRACK AT FS 76, BETWEEN LONGERON 21R TO 24R. REPLACED PER SRM 51-1-21.

Part: SKIN — CRACKED (FS 1700)

WHILE IN DALFORT FOR C-MAINT, FOUND .25 INCH LONG CRACK FWD AND AFT OF RIVET HOLE AT FS 1700 LONGERON 14R TO 15R. REPAIRED PER SRM 53-2-0, FIGURE 1B.

Part: LE RIB — CRACKED (LT WING)

WHILE IN DALFORT FOR C-MAINT, FOUND UPPER LEADING EDGE RIBS CRACKED AT STA XSF 416, XSF 410, XFS 373, XFS 304, AND XFS 310, UPPER AND LOWER. REPAIRED PER MM 57-00-00, FIG 801.

Part: SKIN — CRACKED (BS 182)

(SUPPLEMENTAL MRR) DURING DAILY CHECK, MAINTENANCE FOUND ONE CRACK APPROX 2 INCHES LONG AT STA 182, LONGERON 33. NOTE: CORROSION PRESENT. REMOVED FASTENERS, STOP DRILLED CRACK, INSTALLED DOUBLER PER SRM 51-1-20.

Part: LONGERON — CRACKED (BS 81)

(SUPPLEMENTAL MRR) DURING DAILY CHECK, MAINTENANCE FOUND TWO CRACKS APPROX 1.5 INCHES LONG EACH AT STA 81, LONGERON 33. NOTE: CORROSION PRESENT. REMOVED FASTENERS, STOP DRILLED CRACKS, INSTALLED DOUBLER PER SRM 51-1-20.

Part: SKIN — CRACKED (FWD OF LT MLG DR)

(SUPPLEMENTAL MRR) DURING DAILY CHECK, MAINTENANCE FOUND CRACK JUST FWD OF LT MLG DOOR. REMOVED FASTENERS, STOP DRILLED CRACK, INSTALLED DOUBLER PER SRM 51-1-20.