N813UP

Part: FITTING — CRACKED (FS 1230 L33R) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 FITTING AT STA 1230 L33R IS CRACKED. REMOVED AND REPLACED END FITTING AT STA 1230 L33R IAW SRM 51-01-20D AND SRM 51-01-24.

Part: WEB — CRACKED (HORIZONTAL STAB) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 LT HORIZONTAL STAB AFT WEB ACCESS HOLES HAVE CRACKS AT FASTENER HOLE ON NR 5, 9, 10, AND 12. STOP DRILLED ALL CRACKS, FABBED DOUBLERS, AND INSTALLED DOUBLERS IAW DC8 SRM 55-03-00, 51-1-8, AND 55-02-00.

Part: MOUNT — ELONGATED (MLG DOOR SWITCH) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 RIGHT MAIN GEAR DOOR SWITCH MOUNT HOLES ELONGATED. FABBED AND INSTALLED DOUBLER ON RIGHT MAIN GEAR DOOR SWITCH MOUNT IAW DWG 5653490 AND SRM 51-0-20-D, 51-1-8.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 RT HORIZ STAB AFT SPAR WEB ACCESS HOLES HAVE CRACKS AT FASTNER HOLE SKIN ON NR 2, 3, 6, 7, 8, 9, 11, AND 12. STOP DRILLED ALL CRACKS AT ACCESS HOLES IN RT HORIZ STAB STA XH 28.843-149.00. FABRICATED AND INSTALLED 12 EA DOUBLERS ON RT HORIZ STAB ACCESS HOLES AT STA XH 28.843-149.00 IAW SRM 55-03-01 FIG 3, AND SRM 55-02-00 FIG 2.

Part: WINDOW FRAME — CORRODED (FS -67 L11L) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 WINDOW FRAME AT STA -67 L11L CAPT SIDE HAS EXFOLOIATED CORROSION. REPAIRED CAPT LT AFT WINDOW FRAME AT STA -67 L11L IAW SAA EA NR 008- 5310-01-A1194, UPS RAA NR DC8-53-20665, AND BAC SERV ID 1-659403655.

Part: FITTING — CRACKED (FS 1766 L19R) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 INSIDE 60 HOLE LONGERON END FITTING CRACKED AT STA 1766 L19R. REMOVED AND REPLACED LONGERON END FITTING AT STA 1766 L19R IAW SRM 51-1-21, AND SRM 51-1-20D.

Part: WINDOW FRAME — CORRODED (FS 117) · airframe 81,894 hrs · 27,384 cycles

C2 COCKPIT LT CENTER WINDSHIELD "Z" FRAME HAS HEAVY CORROSION. REMOVED, DRILLED UP, AND INSTALLED REPLACEMENT "Z" FRAME ON COCKPIT LT CENTER WINDSHIELD IAW SRM 51-21-1, AND SRM 51-03-02 FIG 005.

Part: SKIN — CORRODED (FUSELAGE) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 CORROSION INTERIOR SKIN ABOVE CAPT LT AND RT AFT SIDE WINDOW. REPAIRED SKIN AT STA -52 ABOVE CAPT LT AND RT SIDE WINDOW IAW SRM 51-09-00-0, AND DWG 5643170.

Part: FITTING — CORRODED (FS 70 L27R) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 L27R END FITTING CORRODED AT AFT SIDE OF STA 70 FRAME, A-PIT. REMOVED, AND REPLACED LONGERON END FITTING AT STA 70 L27R IAW SRM 53-2-0 FIG 001, SRM 51-1-24, AND SRM 51-1-21.

Part: SKIN — CANNING (LT ELEVATOR) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 L/ELEV UPPER INBD EXTERIOR SKIN OIL CANS. REPAIRED L/ELEV UPPER INBD SKIN IAW SRM 55-2-1, 51-1-21, AND DWG 5655942.

Part: FITTING — CRACKED (FS 1150 L33R) · airframe 81,894 hrs · 27,384 cycles

C2 BANANA FITTING CRACKED AT STA 1150 L33R. REMOVED, AND INSTALLED REPLACEMENT BANANA FITTING AT STA 1150 L33R IAW SRM 51-1-20D, AND SRM 51-01-24.

Part: SKIN — CANNING (RT ELEVATOR) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 RT ELEVATOR MIDDLE LWR SKIN HAS OIL CANNING. FABRICATED AND INSTALLED REPAIR DOUBLER ON RT ELEVATOR STA XE 103.2 IAW SRM 55-02-01 FIG 1.

Part: FINGER DOUBLER — CORRODED (FS 123 L31R) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 FINGER DOUBLER AT STA 123 L31R IS CORRODED AND CRACKED. REMOVED, FABRICATED, AND INSTALLED REPAIR FINGER DOUBLER AT STA 123 L31R IAW SRM 51-1-20D, AND DWG 5773316.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 RT ELEVATOR HAS CRACK IN EXTERIOR SKIN JUST OUTBOARD OF GEARED TAB. CUT OUT DAMAGED AREA ON RT ELEVATOR EXTERIOR SKIN IAW SRM 55-2-1 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER ON RT ELEVATOR EXTERIOR SKIN JUST OUTBOARD OF GEARED TAB IAW SRM 55-2-1 FIG 7.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 L33R SPLICE FITTING AT STA 1040-1060 IS CRACKED. REMOVED AND REPLACED LONGERON SPLICE FITTING AT STA 1040-1060 L33R IAW SRM 51-1-20D, AND SRM 51-03-02.

Part: FLOORBEAM — CORRODED (FS 55 RBL 48) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 CORROSION AND DEEP TOOLING MARKS/GOUGES ON GUSSET AT BOTTOM OF STA 55 FLOORBEAM RBL 48. REMOVED, FABRICATED, AND INSTALLED REPAIR GUSSET AT STA 55 RBL 48 FLOORBEAM IAW DWG 5641543, AND SRM 51-3-2, AND SRM 51-1-20D.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 FLOOR SUPPORT AT STA 1734 LBL 20 IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FLOOR SUPPORT AT STA 1734 LBL 20 IAW SRM 53-07-01-0 FIG 011A.

Part: INTERCOSTAL — BROKEN (FUSELAGE) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 INTERCOSTAL BETWEEN STA 1734-1746 LBL 36 IS BROKEN. REMOVED, FABRICATED, AND INSTALLED REPAIR INTERCOSTAL AT STA 1734- 1746 LBL 36 IAW DWG 5755032, AND SRM 51-1-20D.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 ATTACH FITTING CRACKED AT STA 820 L22L. REMOVED AND REPLACED ATTACH FITTING AT STA 820 L22L IAW SRM 551-03- 02, AND SRM 51-01-20B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 SEAT TRACK AT STA 1380-1400 BL 0 IS CORRODED OUT OF LIMITS. CUT OUT CORRODED SEAT TRACK FROM STA 1380-1400 BL 0 IAW SRM 53-02-03 -0 FIG 006D. INSTALLED 4 HOLE SEAT TRACK PLUG AT STA 1380-1400 BL 0 IAW SRM 51-3-0.

Part: SEAT TRACK — CORRODED (FS 1220 BL-0) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 SEAT TRACK BL-0 STA 1220-1240 CORRODED. REMOVED AND REPLACED SEAT TRACK PLUG AT STA 1220 BL-O IAW SRM 53-02-03-0 FIG 12, AND SRM 51-3-0.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C SEAT TRACK STA 65 RBL 48 HAS BROKEN LUGS. REMOVED, FABRICATED AND INSTALLED REPAIR SEAT TRACK AT STA 50 - 130 RBL 48 IAW SRM 53-21-02-4, SRM 51-3-00, AND DWG S2400463.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 STA 60 BL0 HAS CORROSION BETWEEN FLOOR BOARD AND 9G NET LATCH TRAY. REPAIRED FLOORBEAM STA 60 BL0 IAW SRM 51-03-00-0, SRM 51-1-8 AND SRM 53-03-03.

Part: DOUBLER — PUNCTURED (WING) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 REPAIR DOUBLER PUNCTURED ON WING SKIN PANEL BOTTOM SURFACE, IN LT WHEEL WELL NEAR UPLATCH. REMOVED AND REPLACED REPAIR DOUBLER ON WING SKIN PANEL IN LT WHEEL WELL IAW SRM 51-3-00, AND SRM 57-03-00-0.

Part: SKIN — CORRODED (FUSELAGE) · airframe 81,894 hrs · 27,384 cycles

INSPECTION TYPE:C2 BULGING SKIN AT STA 100 L35R. CUT OUT DAMAGED AREA AT STA 100 L35R IAW SRM 53-02-01 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLER AND FILLER AT STA 100 L35R IAW SRM 53-02-01 FIG 7.

Part: DOOR — OUT OF ADJUST (COCKPIT)

INSPECTION TYPE:N/A COCKPIT DOOR EXTREMELY HARD TO OPEN AFTER CLOSING. ADJUSTED DOOR FOR EASIER OPENING. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY AND RELAY UNIT PER AMM 33-50-01-2. OPS CHECK OK.

Part: CONTROL UNIT — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A COCKPIT EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK CONTROL UNIT PER MM 33-50-02-2.

Part: CONTROL ROD — MALFUNCTIONED (CREW ENTRY DOOR)

INSPECTION TYPE: N/A CREW ENTRY DOOR JAMMED CLOSED AFTER PARKING. LOWER HINGE CONTROL ROD ASSY REMOVED AND REPLACED. ADJUSTED VERTICAL ADJUSTMENT OF CREW ENTRY DOOR PER DC8 MM 52-11-01-5 PARA A. PRESSURIZED A/C TO 6 PSID. LEAK AND OPS CHECK GOOD.

Part: CONTROL ROD — DEFECTIVE (PAX DOOR)

INSPECTION TYPE:N/A CREW MAIN ENTRY DOOR WILL NOT OPEN; JAMMED AFTER PARKING. LOWER HINGE CONTROL ROD ASSY REMOVED AND REPLACED. ADJUSTED VERTICAL ADJUSTMENT OF CREW ENTRY DOOR PER DC8 MM 52-11-01-5 PARA 1. PRESSURIZED AIRCRAFT TO 6 PSID. LEAK & OPS CHECK GOOD. REF LP 684283/3.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

ON PREFLIGHT, EMERG LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK ASSY REF MM 33-50-01. OPS CKS NORMAL.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

ON PREFLIGHT, EMERGENCY LIGHTS FAILED PREFLIGHT TEST. THE WHITE PEANUTS LIGHTS UNDER THE GLARE SHIELD DID NOT ILLUMINATE NOR DID ANY OF THE OTHER LIGHTS ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CK OK.

Part: SMOKE GOGGLES — MISSING (COCKPIT)

INSPECTION TYPE:N/A SMOKE GOGGLES ARE MISSING FROM 2ND OBS POS. REPLACED MISSING SMOKE GOGGLES.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHTING FAILED MX TEST. RESECURED GROUNDING WIRE/LUG,OPS CKS NORMAL IAW AMM 33-50-01-2.

Part: DOOR FRAME — CRACKED (BS 1400 L28R) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 D-PIT TORQUE BOX FRAME AT L28R FS 1400 CRACKED WHERE LATCH MECHANISM ATTACHES. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER IAW SRM 51-3-0, 53-2-0 FIG 1B, 51-1-21 AND 51-1-20D.

Part: PRESSURE PANEL — CORRODED (FR 32) · airframe 81,078 hrs · 26,768 cycles

FOUND LT NOSE TUNNEL, UPPER CEILING PRESSURE PANEL HAS 2 SHEARED RIVETS CRACKS AND BULGING CORROSION AT APPROX STA -32 LBL65. REMOVED EXISTING REPAIR FINGER DOUBLER, FINGER DOUBLER "T" FITTING AND 2 ATTACH FITTINGS. REMOVED CORRODED AREA. FABRICATED AND INSTALLED FILLER, 4 REPAIR DOUBLERS, 1 REPAIR SPLICE IAW SRO 8 530026 AND SRM 51-3-0, 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (STAB LH XFS 47.5) · airframe 81,078 hrs · 26,768 cycles

FOUND LT HORIZONTAL STAB IB L/E STA XFS 47.5 RIB HAS 1/2" CRACK ON LOWER FLANGE ANGLE. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 55-2- 0 FIG 2 AND 3.

Part: RIB — CRACKED (LH STAB LE) · airframe 81,078 hrs · 26,768 cycles

FOUND LT HORIZ STAB I/B L/E STA 141.250 RIB HAS CRACK ON LWR FLANGE ANGLE. STOP DRILLED CRACK, FABBED, AND INSTALLED REPAIR IAW DC-8 SRM 55-2-0 FIG 2 AND 3.

Part: SKIN — CORRODED (RT ELEVATOR) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:CI 2AE POPPED RIVET HEADS AT I/B LOWER SKIN OF RT ELEVATOR AND OBVIOUS INTERNAL CORROSION. REMOVED AND REPLACED SKIN IAW SRM 55-2-1 PAGE 23 & 24, 51-01-22, 55-2-1 FIG 8, 51-1-21, 51-1-21D AND 51-3-0.

Part: FITTING — CORRODED (FS 1570) · airframe 81,078 hrs · 26,768 cycles

FOUND SEVERE CORROSION ON SPLICE FITTING AND AROUND FASTENERS AT BS 1570, RBL 20 AS MARKED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0 AND 51-3-2.

Part: FRAME — CRACKED (FS 240 L36) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 FUSELAGE FRAME IS CRACKED 2" LONG AT F/S 240 L36. CRACK IS IN RADIUS OF UPPER FLANGE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR SPLICE, ANGLE AND SHEAR TIE CLIP IAW SRM 53-02-00-0, 51-3-2, 51-1-21, 53-4-1 AND 51-1-20D.

Part: FITTING — CRACKED (FS 280) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 A PIT DOOR FRAME FWD SPIDER IS CRACKED STA 280 L27R. REMOVED AND REPLACED SPIDER FITTING IAW SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (DOOR FRAME) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 A PIT A/C DOOR FRAME AFT SPIDER FITTING IS CRACKED L27R. REMOVED, FABRICATED AND INSTALLED SPIDER FITTING IAW 51-1-20D, 51-3-0, DWG 3754025.

Part: WEB — CORRODED (FS 93 RBL30) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 COCKPIT SUBFLOOR STA -93 RBL 30 STATIC TUBE CONNECTING POINT PLATE HAS 4 SHEARED HEAD FASTENERS AND POSSIBLE CORROSION UNDER THE PLATE. REPAIRED IAW SAA SK 813-823093 AND UPS EO DC8-5310-23264-A.

Part: FITTING — CRACKED (FS 270 L33R) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 "A" PTI ZEE FITTING CRACKED AT STA. 270 L33R. REMOVED AND REPLACED ZEE FITTING IAW SRM 51-1-20D.

Part: DOUBLER — CORRODED (STA -55 RBL 24) · airframe 81,078 hrs · 26,768 cycles

FOUND COCKPIT SUBFLOOR FINGER DOUBLER HAS SEVERAL SHEARED HEAD FASTENERS AT STA -55 RBL 24. REMOVED FINGER DOUBLER, FOUND CORROSION OUT OF LIMITS, FABBED, AND INSTALLED REPLACEMENT DOUBLER IAW DC-8 SRM 53-3-1 AND 51-1-21.

Part: SHEAR TIE — CORRODED (FS 1240) · airframe 81,078 hrs · 26,768 cycles

FOUND SHEAR TIE CORRODED AT STA 1240 L35L. REMOVED FAB`D AND INSTALLED REPLACMENT SHEAR TIE IAW SRM 53-04-01-0 FIG 051, 51-01-04-0,53-2-0 AND 51-1-20D.

Part: LONGERON — CORRODED (BS1240-1260 L35L) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 WHILE WORKING N/R 822550 FOUND PITTING CORROSION ON STEEL LONGERON 35L I/B SIDE BETWEEN FS 1240-1260. REPAIRED LONGERON 35L IAW SAA SK 813-823057 AND UPS EO DC8-53-20522.

Part: DOUBLER — CORRODED (FS 1240-1260 35L) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 WHILE WORKING N/R 822550 FOUND INTERNAL EXFOLIATED BETWEEN STA 1240 AND 1260 L35L. CUT OUT DAMAGED AREA AND REPAIRED IAW SAA SK 813-823058, AND UPS EO DC8-53-20520.

Part: SPAR — CRACKED (BS 857) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 MLG WW FWD LWR SPAR CHORD CRACKED BETWEEN FASTENERS ON STA 857 (1.5 INCH LONG) XCW 53.500. REPAIRED SPAR CHORD IAW SRO 8570009.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 INTERGRANULAR CORROSION ON RT HORIZ STAB L/E UPPER SURFACE AT SEGMENT JOINT. CUT OUT DAMAGED AREA AND FABRICATED AND INSTALLED REPAIR IAW SAA SK 81 3-822948 AND UPS EO DC8-55-20022.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 INTERGRANULAR CORROSION ON LT HORIZ STAB L/E UPPER SKIN AT SEGMENT JOINT. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND 2 EA. FILLERS IAW SRM 55-02-01 FIG 004.

Part: FITTING — CRACKED (FS 900 L4L) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 LONGERON END FITTING POSSIBLE CRACK AT STA 900 L4L. REMOVED AND REPLACED LONGERON END FITTING IAW SRM 51-1-21 AND 51-1-20D.

Part: FITTING — CRACKED (BS 798 L19L) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 MAIN CABIN FITTING CRACKED AT STA 798 L19L. REMOVED, FABRICATED, AND INSTALLED FITTING IAW DWG 4751639 AND DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 860 L10R) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 LONGERON END FITTING CRACKED STA 860 L10R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 8-25 L19R) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 STA 8-25 LONGERON 19R IS CORRODED (EXFOLIATING). REMOVED LONGERON END FITTING, REMOVED CORROSION, AND REINSTALLED LONG END FITTING IAW SAA SK 813-822730.

Part: FINGER DOUBLER — CORRODED (BS 960-940 RBL65) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 MAIN CABIN SUB FLOOR FINGER DOUBLER CORRODED AND HAS SHEARED HEAD FASTENERS AT STA 960 TO 940 RBL 65. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FINGER DOUBLER IAW DC-8 SRM 53-07-03 FIG 4 AND 51-1-21.

Part: SHEAR TIE — CRACKED (60COMP'T L3L-L3R) · airframe 81,078 hrs · 26,768 cycles

FOUND LARGE SHEAR TIE CRACKED AT BOTH ENDS AROUND FASTENERS IN 60 COMP'T CEILING BETWEEN L3L AND L3R. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SHEAR TIE AND REPAIR PARTS IAW DWG 5612148 AND DC-8 SRM 51-1-20D.

Part: WEB — CORRODED (FS 857 RBL0-23) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 MAIN CABIN CENTER WING BOX AT STA 857 RBL 5 HAS HEAVY CORROSION ON THE UPPER REAR SPAR CAP. REPAIRED WING REAR SPAR TO FUSELAGE SHEAR WEB ATTACH ANGLE AND WING SKIN SPLICE DOUBLER IAW SAA SK 813-822678 AND UPS EO DC8-57-20145.

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 C-PIT X-SLIDE DOOR FWD LOWER INTERIOR HAS 3.00 INCH LONG CRACK ON FRAME AS SEEM WITH MIRROR THROUGH 3RD LIGHTENING HOLE AFT. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 52-2-0, 51-1-21 AND 51-1-20D.

Part: FITTING — CRACKED (FS 1140 L35L) · airframe 81,078 hrs · 26,768 cycles

FOUND C-PIT INTERCOSTAL END FITTING AT FS 1140 AT LONGERON 35L CRACKED AT UP PER FASTENER ATTACH POINT. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW DWG 3758496 9 AND DC-8 SRM 51-1-21.

Part: PRESSURE PANEL — CORRODED (FS 857 RBL 40) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 MAIN CABIN SUB FLOOR, FUEL DUMP CHUTE BRACKET UNDER THE PLATE HAS HEAVY CORROSION AT 857 RBL 40. REMOVED DAMAGED AREA AND REPAIRED IAW SAA SK 813-822556 AND UPS EO DC8- 5310-23251-A.

Part: FITTING — CRACKED (STA 1230 L31R) · airframe 81,078 hrs · 26,768 cycles

FOUND "C" PIT LONGERON END FITTING CRACKED STA 1230 L31R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (STA 450 L14L) · airframe 81,078 hrs · 26,768 cycles

FOUND STA 450 L14L SPLICE FITTING IS CRACKED. REMOVED, FABRICATED, AND INSTALLED FITTING IAW DWG 3887799 AND DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (STA 1280 L33R) · airframe 81,078 hrs · 26,768 cycles

FOUND FITTING CRACKED 1" LONG AT STA 1280 L33R. REMOVED, FABRICATED, AND INSTALLED FITTING IAW DWG 4758514 AND DC-8 SRM 51-1-20D.

Part: BULKHEAD — CRACKED (FS 1766 L11R) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 MAIN CABIN AFT PRESSURE BULKHEAD CRACKED L11R RBL 48. CUT OUT DAMAGED AREA 2 AND FABRICATED AND INSTALLED FINGER DOUBLER, DOUBLER AND 2 FILLER IAW SRM 51-1-20D, 51-3-0, 51-1-21 AND TR- 53-194.

Part: FRAME — CORRODED (FS 1240 L35L) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 FRAME HEAVY CORRODED AT STA 1240 L35L. REPAIRED FUSELAGE FRAME IAW SAA SK813-822550 REV A AND UPS EO DC8-53-20516 A.

Part: FITTING — CRACKED (BS440-460 L14R) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 MAIN CARGO COMPARTMENT RIGHT BETWEEN STA 440-460 SPLICE FITTING CRACKED L14R. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG 3887799 AND DC-8 SRM 51-1-20D.

Part: FITTING — CHAFED (BS 219) · airframe 81,078 hrs · 26,768 cycles

FOUND CANOE FITTING CHAFFED IB AND OB AT STA 219 LT OB FLAP. BLENDED OUT CHAFED AREA, SHOT PEENED IAW SRM 51-1-8, DPS 4.999-2 AND SAA SK 813-822426.

Part: FITTING — CRACKED (BS 860) · airframe 81,078 hrs · 26,768 cycles

FOUND MAIN CARGO COMPARTMENT L2R FITTING CRACKED STA 860. REMOVED AND REPLACED FITTING IAW SRM 51-1-21,51-3-0 AND 51-1-20D.

Part: FITTING — CRACKED (BS 840 L12R) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 MAIN CARGO COMPARTMENT RT STA 840 L12R INTERCOSTAL FITTING CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW DWG 3779874 AND DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (STA 900 L1) · airframe 81,078 hrs · 26,768 cycles

FOUND MAIN CARGO COMPARTMENT L1 AFT OF STA 900 FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (BS 798 L19L) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 MAIN CARGO COMPARTMENT LEFT STA 798 LONGERON 19L BOOT FITTING CRACKED IN RADIUS 4 INCHES LONG. REMOVED AND REPLACED BOOT FITTING IAW DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (STA 860 L7R) · airframe 81,078 hrs · 26,768 cycles

FOUND MAIN CARGO COMPARTMENT L7R FITTING CRACKED STA 860. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.

Part: LONGERON — CRACKED (FS 1756 L14R) · airframe 81,078 hrs · 26,768 cycles

RT AFT INTERIOR FS 1756 L14R CRACKED AT UPPER CANTED FRAME INTERSECTION. CUT OUT DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW DC-8 SRM 53-2-2 FIG 10.

Part: FITTING — CRACKED (FS 1760 L17R) · airframe 81,078 hrs · 26,768 cycles

FOUND RT AFT FUSELAGE INTERIOR FS 1760 L17R END FITTING HAS POSSIBLE CRACK AT UPPER FLANGE. NDT VERIFIED 1.5" CRACK. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51- 1-20D.

Part: LONGERON — CRACKED (STA 1716 L18L) · airframe 81,078 hrs · 26,768 cycles

FOUND STA 1716 L18L IS CRACKED AT INTERSECTION OF CANTED FRAME UPPER ATTACH FASTENER. CUT OUT DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW DC-8 SRM 53-2-2 FIG 10.

Part: DOUBLER — CRACKED (FS 260) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 MAIN CARGO COMP L11L STA 260 CARGO DOOR ANGLE CHAFED MARK. UPON REMOVAL OF REPAIR ANGLE, FOUND DOUBLER CRACKED. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DWG 5772787, SRM 53-2-0 FIG 1F AND 51-1-21.

Part: SKIN — CRACKED (R1 DOOR CUTOUT) · airframe 81,078 hrs · 26,768 cycles

INSPECTION TYPE:C1 R1 DOOR UPPER FWD CORNER OF CUT OUT IS A .5 INCH CRACK FROM FASTENER TO EDGE OF SKIN. FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER AT FWD UPPER CORNER OF R1 DOOR IAW SRM 53-2-0 FIG 14, 51-1-21 AND 51-3-0.

Part: FITTING — CRACKED (STA 1690 L3L) · airframe 81,078 hrs · 26,768 cycles

FOUND STA 1690 L3L AFT PROD SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.

Part: ENGINE — SHUTDOWN (NR 4)

NR 4 ENG SHUT DOWN IN FLT DUE TO OVER TEMP AND LOUD THUD. FROM LP 427064 ITEM 1 AND LP 427065 ITEM 3: PERFORMED THRUST LEVER STATIC TRIM IAW AMM 71-00-00 PG 595.23 TEST 9A. PERFORMED PART POWER TRIM AND INCREASED BY 10 CLICKS. PERFORMED ENG HIGH PWR RUN-UP. R & R NR 4 ENG PER TC 9071-1,2,3. OPS AND LEAK CK GOOD.

Part: SKIN — CRACKED (FUSELAGE)

1 INCH FUSELAGE SKIN CRACK AFT OF OUTFLOW VLV. REMOVED DAMAGE FROM A/C DRHODES 0557647 DAMAGE REMOVAL VERIFIED OK TO FABRICATE & INSTALL REPAIR.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

EMERGENCY LIGHTING SYS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK PER MM 33-50-01. OPS CKS GOOD.

Part: FASTENER — BROKEN (LIFE RAFT)

INSPECTION TYPE:N/A FWD LIFE RAFT OPEN AND ONE SNAP BROKEN. REPAIRED SNAP AND CLOSED LIFE RAFT CORNER.

Part: SLIDING WINDOW — BINDING (COCKPIT)

INSPECTION TYPE:PFLT F/O'S SLIDING WINDOW WILL NOT OPEN. CYCLED WINDOW, OPS CHECKS NORMAL.

Part: RELAY — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS CAME ON WITH SWITCH IN ARM POSITION. C/B RESET, LIGHTS WENT OUT. EN ROUTE EMERGENCY EXIT LIGHTS CAME ON AGAIN. WOULD NOT RESET, DISARM LIGHT TURNED OFF. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT PER MM 33-50-01-2, OPS CHECK GOOD.

Part: BLEED VALVE — INOPERATIVE (NR 2 ENGINE)

NR 2 AND NR 3 ENGINES AT IDLE DUE TO COMPRESSOR STALLS ENG NR3 FOUND CRACKS GURNS & MISSING MATERIAL ON STATOR OF LPT ACCESS THRU 517. BOROSCOPE 72-00-00 P 620, 72-31-00 72-54. ENGINE NR 2 COMPLIED WITH VISUAL & BOROSCOPE INSPECTION OF NR 2 ENG POST STALL, NR 2 ENG MASTER BLEED VALVE FEED BACK ROD BENT & BLEED VALVE ACTUATOR ARM BROKEN R & R MASTER BLEED VALVE PER MM C/W CHECK SYS ACTUATOR SYS TEST PER MM. NORMAL. LEAK CK GROUND IDLE & FLIGHT IDLE TEST & P WR ASSURANCE TEST PERFORMED IAW MM. TESTED GOOD. (CLOSED)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE:C3 AFT RT SEAT TRACK CORRODED AT STA 1680 I/B LOWER SIDE BLENDED SEAT TRACK TO 100 PERCENT MAT LOSS AND FOUND OUT OF LIMITS IAW DC8 53-2-0 FIG 1F. DRILLED, LOCATED NEW SEAT TRACK IAW DC8 SRM 51-1-24 AND 5 3-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW SEAT TRACK AND SPLICE IAW DC8 SRM 51-3-0 AND 53-2-3. REINSTALLED FLOOR PNL F216 AND ADJACENT PLANKS IAW DC8 SRM 51-3-0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, L2 AFT PAX DOOR UPPER AFT CORNER HAS CRACK INDICATION. REMOVED CRACKED INTERNAL STEEL DOUBLER, MATERIAL ID FOR NEW DBLR IS 17-7 DH .025 INCH LOT 360348 IAW DAC DWG 5750985 AND 4751734, HEAT TREATED TO HT170 IAW DAC DWG 4751734, PRIMED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-8 AND 51-1-21.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, LONGERON 35L CORRODED AT STA 280-300 FWD PIT. REMOVED CORR IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. CUT OUT DAMAGE L-ANGLE IAW DC8 SRM 53-2-2. RECEIVED LONG SECT, LOCATED, DRILLED & TRIMMED LONG SECTION & -31 SPLICES IAW DC8 SRM 53-2-2. ALODINED, PRIMED AND INSTALLED LONGERON SECTION AND SPLICE IAW DC8 SRM 51-1-8 & 53-2-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE:C3 FLOORBEAM UPPER FWD FLANGE CORRODED FS 1300 LBL 12. REMOVED CORR FROM UPPER & LOWER SURFACE OF FLOORBEAM FLANGE, OUT OF LIMITS IAW DC8 SRM 51-1-8 & 53-2-0; FABBED RPR ANGLE AND STRAP IAW DC8 SRM TR 53-124. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLE AND STRAP IAW DC8 SRM TR 53-124.

Part: FLOOR PANEL — CORRODED (STA 120) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, FLOOR PANELS CORRODED FS 120 RBL 36. REMOVED CORR IAW DC8 SRM 51-1-8, CUT DAMAGE AND FABRICATED REPAIR DOUBLER AND FILLER IAW DC8 SRM 53-2-3, INSTALLED DOUBLER AND FILLER IAW DC8 SRM 51-1-21. FABRICATED SPLICE IAW DC8 SRM 53-2-3. INSTALLED FLOOR PANEL & SPLICE PLATE IAW DC8 SRM 51-3-0, INSTALLED FLOOR BOARD IAW DC8 SRM 51-3-0.

Part: FLOOR PANEL — CORRODED (FUSLEAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE:C3 FLOOR PANEL CORRODED FS 1300 LBL 12. CUT AND REMOVED SECTION OF FWD PANEL, FABBED NEW SECT OF FLOOR PANEL AND SPLICE PLATES ALL IAW DC8 SRM 53-2-3 FIG 9. ALODINED & PRIMED IAW DC 8 SRM 51-1-8, INSTALLED NEW SECT OF FLOOR PANEL AND SPLICE PLATES IAW DC8 SRM 53-2-3 FIG 9. CUT OUT CORROSION ON AFT PANEL, FAB REPAIR DOUBLER & FILLER, ALODINED, PRIMED & INSTALLED IAW DC8 SRM 53-2-3, 51-1-8.

Part: ATTACH FITTING — CRACKED (LT WING LE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, LT WING CENTER L/E, O/B ATTACH POINT THAT ATTACHES L/E TO STUB WING IS CRACKED. REMOVED CRACKED ANGLE IAW DC8 SRM 51-3-0, MAT ID IAW DC8 DWG 9753297-7, .080 7075-0 PO 422932. RECEIVED PART FROM HEAT TREAT .080 7075-0-TO .080 7075-T6, FABRICATED ANGLE IAW DC8 DWG 9753197, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED ANGLE IAW DC8 SRM 51-1-21 AND 51-3-0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, L2 AFT PASSENGER UPPER AFT DOOR JAMB CORNER EXT FUSELAGE SKIN CRACKED AT 2 FASTENERS CRACKS MARKED. REPAIRED IAW DC8 SRM 53-2-0; REMOVED FASTENERS, TRIMMED OUT CRACKS IAW DC 8 SRM 53-2-0, PERFOMRED E/C INSP IAW DAC NDT SPM 06-10-01.001. NO CRACKS NOTED. FABBED RPR PARTS IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED PARTS IAW DC8 SRM 53-2-0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE:C3 L1 FWD PASSENGER LWR AFT DOOR JAMB CORNER EXT FUSELAGE SKIN CRACKED AT FASTENER HOLE MARKED. REPAIRED L1 FWD PASSENGER LWR AFT DOOR JAMB CORNER IAW DC8 SRM 53-2-0 FIG 15.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, LONGERON 6R STA 12 HAS CORROSION ON FLANGE. REMOVED CORR OUT OF LIMITS IAW DC8 SRM 51-1-8 & 53-2-0. MAT ID PO 409830 .2 7075-T6.050 IAW REO G09499 PG 4. FABBED REPAIR DOUBLER IAW REO G0949 9, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR IAW REO G09 499 AND DC8 SRM 51-1-20D.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, AFT ACCY COMPT FS 1580 FLOORBEAM REPAIR ANGLE IS CORRODED AT RBL 48. REMOVED FLOORBEAM REPAIR, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED NEW REPAIR ANGLE, ALODINED AND PRIMED IAW DC8 SRM 53-2-0 AND 51-1-8 AND INSTALLED ANGLE IAW DC8 SRM 51-1-20D, 51-3-0.

Part: FLOORBEAM — CORRODED (FUSLEAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, FLOORBEAM REPAIR ANGLE CORRODED FS 1680 LBL 20. REMOVED CORRODED REPAIR ANGLE IAW DC8 SRM 51-3-0. FABBED REPAIR ANGLE AND STRAP IAW DC8 53-2-0 & 53-2-04. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLE, STEEL STRAP, SUPPORT ANGLE AND REINSTALLED FLOOR BOARD IAW DC8 SRM 51-3-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, SEAT TRACK -E- FROM FS 1000-1300 IS CORRODED. REMOVED CORROSION ON SEAT TRACK IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. LOCATED AND DRILLED REPAIR SPLICES AND SEAT TRACKS IAW DC8 EO D C8-5320-5167 AND DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED SEAT TRACK IAW DC8 SRM 51-3-0, REINSTALLED FLOOR BOARDS RBL 36 AND 27 IAW DC8 SRM 51-3-0 STA 1000-1380.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, BULKHEAD AT STA 680 LONG 33L AFT SIDE OF PRESSURE DOME CRACKED IN RADIUS (LOWER). REMOVED AND REPLACED PRESSURE DOME STA 680 LT SECTION IAW DC8 SRM 51-1-202D AND 51-3-0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, END FITTING AT STA 1766 L28R MISSING FASTENER. AFTER FURTHER INSP, CRACKED. REMOVED END FITTING AT STA 1766 L28R IAW DC8 SRM 51-1-20D. LOCATED, DRILLED, AND DEBURRED NEW PART P/N 4772397-1N PO 423837.1 IAW DC8 SRM 51-1-24. INSTALLED NEW PART (END FITTING) AT STA 1766 L28R IAW DC8 SRM 51-1-20D. END FITTING CRACKED OUT OF LIMITS IAW DC8 SRM 53-2-0 AND DAC DWG 4772397U1.

Part: FRAME — CORRODED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, CANTED FRAME AT FS 1746 AT LONG 34R FWD SIDE OF FRAME HAS CORROSION. FRAME SPLICE ANGLES CORRODED BEYOND LIMITS IAW DC8 SRM 53-2-0. FABBED NEW CHANNEL IAW DC8 DWG 56212148, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED CHANNEL IAW UPS DC8 SRM 51-1-20.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, AT FUSELAGE STA 700 (APPROX) INSIDE STRESS PANEL AREA, SHEAR TIE ON LT SIDE CRACKED. FABRICATED SHEAR TIE FROM MAT 7075-0.071 AND HEAT TREATED TO T-6 IAW DAC DWG 5750365 & TPS 1003 REV A FOR HEAT TREAT. LOCATED, DRILLED, AND DEBURRED IAW DC8 SRM 51-1-24, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, MAIN CABIN CENTER LINE SEAT TRACK FS 1338 TO 1357 HAS CORROSION. REMOVED CORR IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. INSTALLED CENTER SEAT TRACK & 8 SPLICES AND 1 SPLICE FITTING STA 1270-1350 IAW DC8 SRM 51-3-0. FLOOR BOARD AT STA 1270 1350 LT WAS REMOVED FOR FOM, REINSTALL FLOOR BOARD IAW DC8 SRM 51-3-0.

Part: FRAME — CORRODED (COCKPIT) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, COCKPIT UNDER FLOOR AREA STA -117 LT SIDE BOTTOM OF FRAME AT CUSP AREA HAS CORROSION ON DWD AND AFT SIDE OF FRAME. REMOVED KICK PANEL LT COCKPIT FLOOR. REMOVED FRAME, OUT OF LIMITS. REMOVED 2 EA T-ANGLE ATTACH ANGLES. RECEIVED Z-FRAME HT TREATED TO T-6 CONDITION FABBED IAW DAC DWG 5613861. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW Z-FRAME IAW DC8 SRM 51-1-20D & 51-3-0. REINSTALLED KICK PANEL. REMOVED IAW DC8 SRM 51-3-0.

Part: INTERCOSTAL — CRACKED (CARGO PIT) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, CRACK IN D-PIT DOOR HINGE LWR FWD HINGE. REMOVED INTERCOSTAL IAW DC8 SRM 51-1-21 & 51-3-0, MAT'L ID 2024-0.050 INCH PO 414492.1 IAW DAC DWG 5616673 HT TREATED FROM 2024-0 TO 2024T4, LOCATED AND DRILLED INTERCOSTAL IAW DC8 SRM 51-1-24. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED INTERCOSTAL IAW DC8 SRM 51-1-21 AND 51-3-0.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, AFT FUSELAGE INTERIOR L17 RIGHT CRACKED BETWEEN FS 1768-1776. REMOVED L-17RT TO FOM, FABBED NEW -35 SPLICE DOUBLER IAW DAC DWG 56493 27, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, LOCATED, DRILLED, DEBURRED, AND INSTALLED NEW LONGERON IAW DC8 SRM 51-1-21 AND 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, AFT FUSE INTERIOR L10LT END FITTING CRACKED BETWEEN FS 1766-1772. REMOVED L10LT END FITTING TO FOM, LOCATED, DRILLED, DEBURRED, AND INSTALLED NEW END FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, AFT FUSELAGE INTERIOR L17 LEFT CRACKED BETWEEN FS 1768-1777. REMOVE CRACKED LONGERON IAW UPS DC8 SRM 51-1-20 & 51-1-21. LOCATE NEW LONGERON AND DRILL EXISTING FASTENER HOLES IAW UPS DC8 SRM 51-3-2. INSTALLED NEW LONGERON IAW UPS DC8 SRM 51-1-20D AND 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE:C3 AFT FUSE INTERIOR L17LT END FITTING CRACKED BETWEEN FS 1766-1772. REMOVED CRACKED LONGERON END FITTING AND INSTALLED NEW FITTING IAW UPS DC8 SRM, 51-1-20D AND 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, AFT FUSELAGE INTERIOR L10 RT END FITTING CRACKED BETWEEN FS 1768-1772. REMOVED L10 RT END FITTING TO FOM, LOCATED, DRILLED, DEBURRED AND INSTALLED NEW END FITTING IAW DC8 SRM 51-1-21 & 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, AFT FUSE INTERIOR L17 RT END FITTING CRACKED BETWEEN FS 1766-FS 1772. REMOVED L17 RT END FITTING TO FOM, LOCATED, DRILLED, DEBURRED AND INSTALLED NEW END FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D.

Part: ATTACH FITTING — CRACKED (BOOST PUMP) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, NR 4 ALT HAS FWD BOOST PUMP MOUNT FITTING CRACKED AT S-59. REMOVED AND REPLACED FITTING WITH NEW FITTING PO SP0938702 IAW DC8 SRM 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, FRAME CORRODED AT STA 260 BETWEEN LONGERONS 35L-35R. REMOVED CORR IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. CUT OUT DAMAGE SECTION OF FRAME IAW DC8 SRM 53-2-0. FABBED FRAME, 4 EA RPR ANGLES, & STRAPS IAW DC8 SRM 51-1-1, 53-4-1, DC8 TEMP REV 53-125, DRILLED & TRIM IAW DC8 SRM 51-1-20D, 53-2-0 & TEMP REV 53-125. ALODINED & PRIMED AND INSTALLED IAW DC8 SRM 51-1-8 & 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, AFT PIT AT STA 1220 STR 34R INSIDE TORQUE BOX AREA FITTING CRACKED. REMOVED FITTING CRACKED IAW DC8 SRM 51-1-20D, REC'D NEW Z-FITTING AND 2 EA PLATES P/N 3755841-1, P/N 3755841-3, P/N 3755841-5. LOCATED, DRILLED, AND TRIMMING IAW DC8 SRM 53-2-0, AND 51-1-20D. INSTALLED Z-FITTING AND PLATES IAW DC8 SRM 51-1-20D.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, L1 DOOR CORNER UPPER FWD CORNER IS NOT PER SRM. FABBED -15 -17 DOUBLERS, -19 FILLER IAW DC8 SRM 53-2-0 FIG 15 TR 53- 155. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLERS & FILLER IAW DC8 SRM 51-1-20D. RE-INSTALLED FOM PARTS IAW DC8 SRM 51-1-21, 51-1 -21A, 51-1-20D, 51-3-0.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, LONGERON 36 CORRODED AT STA 220-240 FWD PIT. REMOVED CORR IAW DC8 SRM 51-1-8 ORIG .080 INCH, REMOVED .027 INCH, REMAINING .053 INCH OUT OF LIMITS IAW DC8 SRM 53-2-0. CUT OUT DAMAGE IAW DC8 SRM 53-2-2. RECEIVED LONG SECTION, LOCATED, DRILLED, & TRIMMED IAW DC8 SRM 53-2-2. ALODINED & PRIMED AND INSTALLED SPLICE, LONGER SECTION AND -33 SPLICE IAW DC8 SRM 51-1-8, 53-2-2, & DAC DWG 9754913.

Part: FRAME — CORRODED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, AFT PIT AT STA 1040 STR 34R FRAME HAS CORROSION UNDER NUT PLATE. REMOVED CORR IAW DC8 SRM 51-1-8 ORIG .080 INCH, REMOVED .070 INCH, REMAINING .010 INCH OUT OF LIMITS IAW DC8 SRM 53-2-0. FAB RPR ANGLE AND 2 FILLERS IAW UPS EO DC8-5310-11728. REMOVED DAMAGED AREA IAW UPS EO DC8-5310-11728. ALODINED & PRIMED IAW DC8 SRM 51-1-8, INSTALLED RPR ANGLE AND FILLERS IAW DC 8 SRM 51-1-20D AND UPS EO DC8-5310-11728.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, R2 AFT SERVICE DOOR HAS CRACK INDICATION AT UPPER AFT CUTOUT CRACKED AREA IAW DC8 SRM 53-2-0 FIG 16, TR 53-130 & TR53-156 PERFORMED HFEC IAW MD NDT SPM 06-10-01.001 NO CRACKS NOTED. REMOVED INTERCOSTAL ABOVE R2 DOOR, 2 EA CLIPS, TOP AFT DOOR STOP FITTING. OPENED R2 DOOR TORQUE BOX WEB. FABBED DOUBLERS AND TRIPLERS AND REPAIRED DOOR FRAME RE-ASSEMBLED FRAME IAW DC8 SRM 53-2-0 FIG 16, TR53-130, TR53-156.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 80,221 hrs · 26,068 cycles

INSPECTION TYPE: C3, FWD PIT SMOKE BARRIER UPPER ATTACH ANGLE CORRODED NEAR CENTER LINE. REMOVED CORR IAW DC8 SRM 51-1-8, ORIG .063 INCH, REMOVED .014 INCH, REMAINING .049 INCH OUT OF LIMITS IAW DC8 SRM 53-2-0. FORMED 2 ANGLES AND SPLICE ANGLE IAW DC8 SRM 51-1-4 & DAC DWG 9887940, HT TREATED IAW DC8 SSRM 51-1-1, ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED 2 ANGLES AND SPLICE ANGLE IAW DC8 SRM 51-1-21.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS TEST INOP. REPLACED EMERGENCY LIGHTS BATTERY AND RELAY PACK PER MM 33-50-01.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:IN EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK, OPS GOOD.

Part: FITTING — CORRODED (FUSELAGE) · airframe 79,076 hrs · 25,242 cycles

INSPECTION TYPE:C2 FWD PIT STA 272 L33R INSIDE TRQ BOX LWR FITTING CORRODED. REMOVED & REPLACED ZEE FITTING.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 79,076 hrs · 25,242 cycles

INSPECTION TYPE:C2 FWD PIT STA 280-300 L35R HAS AREA OF CORROSION. REMOVED DAMAGED SECTION OF LONGERON SPLICED NEW SECTION IAW SRM 53-2 -2.

Part: FITTING — CORRODED (FUSELAGE) · airframe 79,076 hrs · 25,242 cycles

INSPECTION TYPE:C2 FWD PIT STA 272 L33R INSIDE TQ BOX LWR FITTING CORRODED. R&R ZEE FITTING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 79,076 hrs · 25,242 cycles

INSPECTION TYPE:C2 FWD PIT STA 320 L35L INBD FWD CORNER OF Z FITTING HAS CORROSION & CRACK. RMVD ZEE FITTING IAW DC8 SRM 51-1-20D FABRICATE SPLICES IAW DC8 SRM 53-2-0, INSTALLED ZEE FITTING/SPLICES IAW DC8 SRM 53-2-0 & 51-1-20D

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 79,076 hrs · 25,242 cycles

INSPECTION TYPE:C2 FLC AT STA 612-620 AT L36 CORRODED. REPAIRED IAW REO G08340.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 79,076 hrs · 25,242 cycles

INSPECTION TYPE:C2 FWD CARGO PIT AT FS 280 AT L31R-33R DOORWAY FWD TORQUE BOX WEB LWR ATTACH ANGLE IS CORRODED. REMOVED & REPLACED FITTING IAW DC8 SRM 51-1-20D.

Part: STIFFENER — CRACKED (HORIZ STAB) · airframe 79,076 hrs · 25,242 cycles

INSPECTION TYPE:C2 RT HORIZ STAB LE INBD END AT FUSELAGE CRACKED. REMOVED STIFFENER, TRACK & TRACK BEARING & SHIMS IAW DC8 51. FABBED & INSTALLED NEW STIFFENER P/N 5654501 IAW DC8 SRM 51-1-20D. REINSTALLED TRACK SHIMS AND NEW TRACK BEARING IAW DC8 SRM 51-3-0.

Part: FITTING — CORRODED (FUSELAGE) · airframe 79,076 hrs · 25,242 cycles

INSPECTION TYPE:C2 FWD CARGO PIT FS 300 BETWEEN LONG 34R-35R ZEE FITTING IS CORRODED. REMOVED & REPLACED ZEE FITTING FABBED SPLICES IAW DC8 SRM 53-2-2.

Part: FITTING — CORRODED (FUSELAGE) · airframe 79,076 hrs · 25,242 cycles

INSPECTION TYPE:C2 MAIN CABIN LT CUSP AT STA 1260 HAS CORROSION ON FRAME FITTING AROUND FASTENERS. REMOVED CORROSION, NOT OUT OF LIMITS. REMOVED FITTING AND INSTALLED NEW PART.

Part: PANEL — CRACKED (LT WING) · airframe 79,076 hrs · 25,242 cycles

INSPECTION TYPE:C2 LT UPPER DINEDRAL CRACKED. REMOVED FILLET ATTACH ANGLE IAW DC8 SRM 51-1-20D & 51-1-21. REMOVED DAMAGED AREA. FABBED REPAIR FILLER IAW REO G08337. FABBED REPAIR DOUBLERS IAW TIMCO REO G08337. CUT OUT AREA IAW DC8 SRM 51-1-8. INSTALLED ALL REPAIR PARTS IAW REO G0 8337.

Part: FITTING — CORRODED (FUSELAGE) · airframe 79,076 hrs · 25,242 cycles

INSPECTION TYPE:C2 AFT PIT STA 1200-1220 L34L-L35L SKIN & FITTING CORRODED. REMOVED CORROSION, OUT OF LIMITS. REMOVED FITTING. RECEIVED NEW FITTING P/N 3755845-1N. FAB REPAIR ANGLE IAW DC8 SR M 53-2-0. INSTALLED FITTING IAW DC8 SRM 51-1-8 & 51-1-20D

Part: FITTING — CORRODED (FUSELAGE) · airframe 79,076 hrs · 25,242 cycles

INSPECTION TYPE:C2 FITTING CORRODED AT FASTENER HOLE FWD SIDE AT STA 1480R IN CUSP AREA. REMOVED & REPLACED FITTING IAW DAC DWG 4640162.

Part: DOOR — CORRODED (AFT ACCY DOOR) · airframe 79,076 hrs · 25,242 cycles

INSPECTION TYPE:C2 AFT ACC COMPT FS 1540 BULKHEAD DOOR CORRODED ALONG BOTTOM FWD SIDE. REMOVED DOOR, REMOVED CORROSION AND FOUND OUT OF LIMITS. FABRICATE REPAIR DOUBLER & FILLER MM 52-30-00. INSTALL FILLER & DOUBLER IAW DC SRM 51-1-21 AND REINSTALLED DOOR IAW DC SRM 51-3-0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 79,076 hrs · 25,242 cycles

INSPECTION TYPE:C2 CUSP FITTING BTW STA 1080R & 1100R SUSPECTED CRACK. REPAIRED AREA IAW DC8 SRM 53-2-5.

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,076 hrs · 25,242 cycles

INSPECTION TYPE:C2 CORROSION ON INNER SKIN IN AFT PIT FS 1080 LONG 36. REMOVED CORROSION IAW DC8 SRM 51-1-8 FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED DAMAGED SECTION OF SKIN IAW DC SRM 51-1-20D. INSTALLED NEW SECTION OF BELLY SKIN IAW DC SRM 51-1-20D 51-1-21 & 51-3-0.

Part: REGULATOR — INOPERATIVE (CAPTAINS O2)

CREW PREFLIGHT -CAPTAINS O2 REGULATOR FAILED. R&R CAPTS 02 REGULATOR

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHT BATTERY PACK DEAD. REPLACED BATTERY PACK. OPS CK OK.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, DURING PREFLIGHT EMERG LIGHTS FOUND TO BE INOP. REMOVED AND REPLACED EMERG LIGHT PACK MM 33-60-00, CHECKED OK. P/N ON 5708458-503, P/N OFF 60-1223-5.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, CHECK OK.

Part: SLIDE — DETACHED (CABIN)

INSPECTION TYPE:N/A, ESCAPE SLIDE FELL OUT OF CONTAINER WHEN S/O ATTEMPTED TO ARM. *S/D* REPACKED SLIDE TO FREE UP GIRT BAR.

Part: SPLICE — CRACKED (WS 710)

INSPECTION TYPE:C1, RT WING L/E SPLICE AT XFS 710 WAS CRACKED. REMOVED, FABRICATED AND REPLACED THE SPLICE IAW SRM 57-3-3 AND 51-3-0.

Part: DOUBLER — CRACKED (WS 336)

INSPECTION TYPE:C1 RT WING L/E LWR SKIN INTERNAL DOUBLER AT XFS 336 IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589 AND SRM 51-1-20D AND 51-1-21.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:C1 THE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT FS 680, AT LONGERON 11R. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 450)

INSPECTION TYPE:C1 THE LONGERON 32R SPLICE FITTING AT FS 450 IS CRACKED. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 280)

INSPECTION TYPE:C1, BATH TUB FITTING FS 280, LONG 33R TO 34R IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: JAMB — CRACKED (BS 192)

INSPECTION TYPE:C1, THE RT FWD SERVICE DOOR JAMB AT LONG 19R, AT THE LWR AFT CORNER OF THE JAMB IS CRACKED BEYOND LIMITS, FS 192. CUT OUT THE DAMAGED AREA AND REPAIRED THE WEB IAW SRM 53-2-0.

Part: LONGERON — CORRODED (BS 8-12)

INSPECTION TYPE:C2 LONGERON 5R AT FS -12 TO 8 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION AND SPLICED IN A NEW LONGERON IAW SRM 53-2-2.

Part: SPLICE — CRACKED (BS 640-660)

INSPECTION TYPE:C1, THE LONGERON 30R SPLICE FITTING AT FS 640 TO 660 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: DOUBLER — CORRODED (BS 12-32)

INSPECTION TYPE:C2, THE FINGER DOUBLER AT FS -12 TO -32 AT LONG 21L IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION OF THE FINGER DOUBLER, FABRICATED A REPLACEMENT SECTION AND INSTALLED IAW SRM 53-3-3 FIG 1 & SRM 51-1-21.

Part: SPLICE — CRACKED (BS 640-660)

INSPECTION TYPE:C1, LONGERON 34R SPLICE FITTING AT FS 640 TO 660 IS CRACKED. REMOVED, FABRICATED AND REPLACED THE SPLICE FITTING IAW SRM 51-3-0 AND DWG 5800471.

Part: FITTING — CRACKED (BS 1040-1060)

INSPECTION TYPE:C1, LONG 31L SPLICE FITTING AT FS 1040 TO 1060 WAS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 5-1-20D.

Part: FITTING — CRACKED (BS 1040-1060)

INSPECTION TYPE:C1 LONGERON 31R SPLICE FITTING IS CRACKED AT FS 1040 TO 1060. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (WS 475)

INSPECTION TYPE:C1, THE RT O/B SLOT, LWR DOOR, INNER FITTING IS CRACKED AT XS 475. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-21.

Part: FITTING — CRACKED (BS 1040-1060)

INSPECTION TYPE:C1, LONG 35R SPLICE FITTING AT FS 1040 TO 1060 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 454.976)

INSPECTION TYPE:C1 LT WING L/E RIB AT XS 454.976 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 316.5)

INSPECTION TYPE:C1 RT WING L/E RIB AT XFS 316.5 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 366.5)

INSPECTION TYPE:C1 RT WING L/E RIB AT XFS 366.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 478.897)

INSPECTION TYPE:C1 RT WING L/E RIB AT XS 478.897 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 497.491)

INSPECTION TYPE:C1 RT WING L/E RIB AT XS 497.491 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.

Part: LONGERON — CORRODED (BS 104)

INSPECTION TYPE:C1 HEAVY CORROSION IN THE CENTER CHANNEL OF LONGERON 34R AT FS 104, AROUND THE FASTENERS. CUT OUT DAMAGED LONGERON 34R BETWEEN FS 90 AND 110 AND SPLICED IN A NEW SECTION OF LONGERON IAW SRM 53-2-2.

Part: STIFFENER — CORRODED (BS 869)

INSPECTION TYPE:C1, SPOT OF HEAVY CORROSION ON THE HORIZONTAL FITTING AT RBL 35, FS 869. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: DOUBLER — CORRODED (BS 902-920)

INSPECTION TYPE:C1 FS 920 TO 902, RBL 68, THE FINGER DOUBLER HAS SEVERAL POPPED RIVET HEADS AND BULGING. REMOVED, FABRICATED, AND REPLACED THE FINGER DOUBLER IAW DWG 5645332 AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (WS 570)

INSPECTION TYPE:C1 RT WING L/E LWR SKIN INTERNAL DOUBLER AT XFS 570 IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21.

Part: FRAME — CRACKED (BS 131)

INSPECTION TYPE:C1, FS -131, 8 BELOW THE SUBFLOOR, THE FRAME O/B FLANGE IS CRACKED AND CORRODED. STOP DRILLED THE CRACK, REMOVED THE CORROSION, AND REPAIRED THE FRAME CAP IAW DH SK813-878. FRAME CAP WITHIN LIMITS AFTER CORROSION REMOVAL IAW SRM 53-2-0.

Part: FITTING — CRACKED (BS 759)

INSPECTION TYPE:C1, FS 759, RBL 48, THE FWD FITTING WAS CRACKED AT THE BOTTOM I/B FASTENER. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 270)

INSPECTION TYPE:C1, LONGERON 34R IS CORRODED BEYOND LIMITS AT FS 270. CUT OUT DAMAGED SECTION OF LONGERON 34R BETWEEN FS 250 & 290 AND SPLICED IN A NEW SECTION IAW SRM 53-2-2 FIG 10.

Part: SKIN — CRACKED (WS 340)

INSPECTION TYPE:C1, RT WING L/E LWR SKIN AT XFS 340, 17 FWD OF THE SPAR WAS CRACKED AT 1 FASTENER HOLE. STOP DRILLED CRACK AND REPAIRED THE SKIN IAW EO DC8-5720-7767-A.

Part: FITTING — CRACKED (BS 834-857)

INSPECTION TYPE:C1, THE LONG 10R END FITTING AT FS 834 TO 857 WAS CRACKED. REMOVED AND REPLACED THE END FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1270)

INSPECTION TYPE:C1, LONGERON 31L SPLICE FITTING AT FS 1270 WAS CRACKED. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 902)

INSPECTION TYPE:C1 THE INTERCOSTAL TO FRAME ATTACH FITTING AT FS 902, LONGERON 18L IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE FITTING IAW DWG 4750423 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 857)

INSPECTION TYPE:C1, THE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT FS 857, LONG 18R. REMOVED, FABRICATED AND REPLACED THE FITTING IAW DWG 3779498 AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (WS 597.5)

INSPECTION TYPE:C1 RT WING L/E LWR SKIN INTERNAL DOUBLER AT XFS 597.5 IS CRACKED IN TWO PLACES. REMOVED, FABRICATED AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21.

Part: FITTING — CRACKED (BS 1270)

INSPECTION TYPE:C1, LONGERON 35L SPLICE FITTING AT FS 1270 WAS CRACKED. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1155)

INSPECTION TYPE:C1, FS 1155 AT LONG 32R, THE ANGLE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 340)

INSPECTION TYPE:C1, BATHTUB FITTING HAD HEAVY CORROSION AT FS 340, LONG 28L. REMOVED AND REPLACED THE FITTING IAW SRM 53-2-0 FIG 2D.

Part: SKIN — CRACKED (WS 560)

INSPECTION TYPE:C1 LT WING L/E SKIN AT XFS 560 IS CRACKED AT 1 FASTENER HOLE. CUT OUT DAMAGED AREA AND REPAIRED SKIN IAW SRM 57-2-1 FIG 24.

Part: JAMB — CRACKED (BS 1660)

INSPECTION TYPE:C1 AFT ENTRY DOOR AFT JAM WEB HAS A RIVNUT PULLED THROUGH AND IS CRACKED AT FS 1660 AND LONGERON 15L. CUT OUT DAMAGED AREA AND REPAIRED THE WEB IAW SRM 53-2-0.

Part: SKIN — CORRODED (WS 404)

INSPECTION TYPE:C1 BULGING CORROSION, LT WING L/E UPPER SKIN AT XFS 404. CUT OUT DAMAGED AREA AND REPAIRED SKIN IAW DH SK813- 334.

Part: FITTING — CRACKED (BS 380)

INSPECTION TYPE:C1 MAIN CABIN, FS 380, THE LONGERON 16R END FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE FITTING IAW DH SK813-507 AND SRM 51-1-20D AND 51-1-21.

Part: SKIN — CRACKED (WS 204)

INSPECTION TYPE:C1, RT WING L/E UPPER SKIN AT XFS 204, JUST I/B OF THE I/B SLOT WAS CRACKED AT 1 RIVET HOLE. STOP DRILLED CRACK AND REPAIRED SKIN IAW SRM 57-2-1 FIG 38.

Part: SKIN — CRACKED (WS 475)

INSPECTION TYPE:C1, THE RT O/B SLOT LWR DOOR SKIN AT XS 475, IS DENTED AND CRACKED. CUT THE DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 57-2-0.

Part: FRAME — CRACKED (BS 55)

INSPECTION TYPE:C1 FS 55 FRAME AT LONGERON 24L IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED FRAME IAW SRM 53-2-0 FIG 2.

Part: SKIN — CRACKED (WS 597.5)

INSPECTION TYPE:C1 RT. WING L/E LWR SKIN @ XFS 597.5, IS CRACKED 2 PLACES, AT THE DRAIN HOLE & AT THE RIVET HOLE JUST FWD OF THE DRAIN. STOP DRILLED CRACK & REPAIRED THE SKIN IAW E.O. DC8-5720-4087-A

Part: SWITCH — FAILED (PASSENGER DOOR)

INSPECTION TYPE:ASN, CABIN DOOR OPEN LIGHT ILLUMINATED IN FLIGHT. ACARS SENSORS (MAIN CREW) CONFIRMED DOOR. AIRCRAFT MAINTAINED DIFFERENTIAL PRESSURIZATION. DOOR APPEARS CLOSED AND SECURE. REPLACED LEFT AFT SERVICE DOOR MICROSWITCH AND CHECKED PER 52-70.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECK OK. (P/N 60-1223-5) (S/N 262) OFF, (P/N 5708458-503) (S/N PTL 1005) ON.

Part: SEAT TRACK — CORRODED (BS 1070-950)

INSPECTION TYPE:C STA 950 TO 1070 LBL 59, THE SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF TRACK FROM STA 930 TO 1070 IAW SRM 53-2-3.

Part: RIB — CRACKED (LT WING)

INSPECTION TYPE:C LT WING L/E RIB ABOVE NR 1 ENGINE IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.

Part: SEAT TRACK — CORRODED (BS 1070)

INSPECTION TYPE:C STA 1070 AT BL0 THE SEAT TRACK IS CORRODED. REMOVED, FABRICATED REPLACEMENT SECTION OF TRACK IAW SRM 53-2-3.

Part: CLIP — CRACKED (BS 1766)

INSPECTION TYPE-C, LONG 5R AFT BULKHEAD CLIP IS CRACKED AT STA 1766. REMOVED AND REPLACED CLIP IAW DWG 5773844.

Part: SEAT TRACK — CORRODED (BS 300)

INSPECTION TYPE:C STA.300, RBL59, THE SEAT TRACK IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK FROM STA 280-330 IAW SRM 53-2-3.

Part: RIB — CRACKED (WS 378)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM IS CRACKED BY THE AFT FASTENER AT STA XFS 378.00. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (LT WING)

INSPECTION TYPE-C, LT WING LWR SKIN DOUBLER ON NR 2 ENG STUB WING JUST FWD OF CUTOUT IS CRACKED. REMOVED DOUBLER AND STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2- 1A.

Part: RIB — CRACKED (WS 304)

INSPECTION TYPE-C, LT WING L/E RIB LWR ARM REPAIR DOUBLER IS CRACKED AT STA XFS.304. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 828.75)

INSPECTION TYPE-C, LT WING L/E RIB LWR ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.828.750. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FLOORBEAM — CORRODED (BS 320)

INSPECTION TYPE-C, STA 320 AT RBL 50 THE LOWER CHANNEL OF THE FLOORBEAM IS CORRODED BEYOND LIMITS. REPAIRED AREA IAW 8110-3 APPROVED DHC SK 813-472.

Part: RIB — CRACKED (WS 747.5)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.747.500. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SEAT TRACK — CORRODED (BS 580)

INSPECTION TYPE:C STA 580 AT LBL 59, THE SEAT TRACK IS CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-2-3.

Part: RIB — CRACKED (WS 791.25)

INSPECTION TYPE-C, LT WING L/E RIB LWR ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.791.250. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 629)

INSPECTION TYPE:C RT WING L/E UPPER RIB AT STA XFS629.00 IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CORRODED (BS 1863)

INSPECTION TYPE-C, STA 1861 TO 1873 AT STR 2R THE DOUBLER EXTENDING UNDER THE LONGERON HAS CORROSION. REPAIRED THE AREA IAW 8110-3 APPROVED DHC SK 813-380.

Part: RIB — CRACKED (WS 822.5)

INSPECTION TYPE-C, LT WING L/E RIB LWR ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.822.500. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 653.75)

INSPECTION TYPE-C, LT WING L/E RIB LWR ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.653.750. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 778.75)

INSPECTION TYPE-C, LT WING L/E RIB LWR ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.778.750. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 672)

INSPECTION TYPE:C RT WING L/E RIB (UPPER) AT STA XFS672.00 IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG.2.

Part: FITTING — CRACKED (RT TE FLAP)

INSPECTION TYPE:C RT O/B SLOT TORQUE TUBE END FITTING IS CRACKED. REMOVED AND REPLACED END FITTING IAW SRM 51-1-21.

Part: RIB — CRACKED (WS 772.5)

INSPECTION TYPE-C, LT WING L/E RIB LWR ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.772.500. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SEAT TRACK — CORRODED (BS 1045)

INSPECTION TYPE:C STA 1045 AT BLO, THE SEAT TRACK HAS HEAVY CORROSION, THE LOCK TANG ON RT SIDE IS CRACKING. REMOVED FABRICATED REPLACEMENT SECTION OF TRACK FROM STA 990-1070 IAW SRM 53-2-3.

Part: SEAT TRACK — CORRODED (BS 1230)

INSPECTION TYPE:C STA 1230 AT LBL 59, THE SEAT TRACK IS CORRODED ALSO AT STA 1290. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF TRACK FROM STA 1130 TO 1270 IAW SRM 53-2-3.

Part: SEAT TRACK — CORRODED (BS 25)

INSPECTION TYPE:C 2ND OBSERVERS FWD SEAT TRACK HAS HEAVY CORROSION, AROUND THE MOUNTING SCREWS. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-3-1.

Part: SKIN — CRACKED (WS 422.750)

INSPECTION TYPE-C, LT WING LWR L/E SURFACE IS CRACKED JUST FWD OF EXISTING DOUBLER AT STA 422.750. STOP DRILLED CRACK AND REPAIRED IAW DC8-5720-4087.

Part: RIB — CRACKED (BS 660)

INSPECTION TYPE-C, LT WING L/E RIB LWR ARM IS CRACKED BY THE AFT FASTENER AT STA 660. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SEAT TRACK — CORRODED (BS 510)

INSPECTION TYPE:C STA 510 TO 550 BL 0, THE SEAT TRACK HAS HEAVY CORROSION. REMOVED DAMAGED SECTION OF SEAT TRACK AND SPLICED REPLACEMENT SECTION FROM STA 430 TO 550 BL O IAW 53-2-3 FIG. 14.

Part: SKIN — CORRODED (RUDDER)

INSPECTION TYPE:C RUDDER, UPPER AFT CORNER LT SIDE HAS HEAVY CORROSION. REMOVED AND REPLACED RUDDER IAW MM 27-21-01.

Part: DOUBLER — CORRODED (BS 1786)

INSPECTION TYPE-C, STA 1786 AT STR 28L THE INTERNAL DOUBLER HAS CORROSION. REPAIRED THE AREA IAW 8110-3 APPROVED DHC SK 813-379.

Part: CLIP — CRACKED (WS 6.225)

INSPECTION TYPE-C, LT WING L/E RIB IS CRACKED AT STA XOLDI6.225. REMOVED FABRICATED AND REPLACED CLIP IAW DWG 5769589.

Part: RIB — CRACKED (WS 616.25)

INSPECTION TYPE-C, LT WING L/E RIB LWR ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.616.250. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 693)

INSPECTION TYPE:C RT WING L/E RIB AT STA. XFS693.00 IS CRACKED ON THE UPPER AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG.2.

Part: RIB — CRACKED (WS 785)

INSPECTION TYPE-C, LT WING L/E RIB LWR ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.785.00. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 622.5)

INSPECTION TYPE-C, LT WING L/E RIB LWR ARM IS CRACKED AT THE AFT FASTENER AT STA XFS.622.500. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: PANEL — CRACKED (LT WING)

INSPECTION TYPE-C, LT WING O/B SLOT O/B PANEL LAND IS CRACKED. REMOVED AND REPLACED ANGLE FITTING IAW DWG 5769857-613.

Part: ANGLE — CRACKED (BS 860)

INSPECTION TYPE:C EXTERIOR FUSELAGE CENTER TANK AT STA 860 BLB 60 SUPPORT ANGLE IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 53-2-0 FIG 1B.

Part: SKIN — CRACKED (WS 74.8)

INSPECTION TYPE-C, RT WING TOP AT STA XRS.74.5 AND WING STRINGER 9, THE SKIN IS CRACKED IN 2 PLACES. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 10.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK, OPS CK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK. P/N OFF 57084558-503; S/N OFF 2054; P/N ON 60-1223-5, S/N ON 3889 OPS CHECK GOOD.

Part: FITTING — CRACKED (BS 1600)

INSPECTION TYPE-B, FLOOR SUPPORT FITTING CRACKED FROM CORROSION AT APPROX STA 1600 AFT ACCESSORY COMPT LT SIDE. REMOVED DAMAGED FITTING, REMOVED CORROSION DYE PENETRANT, INSPECTION NO CRACK. SOME CORROSION STILL EXISTS AND COVERED ON EO DC8-5330-7059A. INSTALLED OLD FITTING ON FLOORBEAM IAW DC8- 5330-7059A.

Part: FLOORBEAM — CORRODED (BS 1600)

INSPECTION TYPE-B, FLOORBEAM CORRODED IN AFT ACCESSORY COMPT APPROX AT STA 1600 APPROX 12 FROM LT SIDEWALL. BLENDED CORROSION, AWAITING REPAIR INSTRUCTIONS FROM DAC 920. REMOVED DAMAGED AREA OF FLOORBEAM, FABRICATED AND DRILLED REPAIR DOUBLER PER EO DC8-5310-8605B. TREATED PRIMED AND INSTALLED DOUBLER PER EO DC8-5310-8605B.

Part: SKIN — CRACKED (CARGO DOOR)

INSPECTION TYPE-N/A, FUSELAGE SKIN BELOW NR 4 PIT DOOR IS HIGHLY CORRODED, HAS 4 EA CRACKS 1 TO 2 IN LENGTH. *S/D* REMOVED AND REPLACED FUSELAGE SKIN STA 1350 TO 1490 PER DAC DRAWING 5615372.

Part: DUCTS — DIRTY (COCKPIT)

INSPECTION TYPE: CS2. (AIR TURN BACK) STRONG SMELL AND SKYDROL FUMES INSIDE COCKPIT DURING TEST FLIGHT. FOUND SKYDROL RESIDUES ON AIR CYCLE MACHINE DUCTS, WATER SEPARATOR SOCK DUE TO LEAK DURING MAINTENANCE CHECK. CLEANED DUCTS AND REPLACED SOCKS PER MM 21-55-01.

Part: ACM — MALFUNCTIONED (LEFT)

INSPECTION TYPE N/A, STRONG SMELL OF SKYDROL IN COCKPIT. TRANSFERRED TO N/R CARD 351733/3733, REMOVED ACM DUCTS, WATER SEPARATOR AND CLEANED AND REPLACED DUCTS, INSTALLED NEW SOCK IN WATER SEPARATOR AFTER CLEANING AND REPLACED LT ACM PER M/M 21-55-01.

Part: ANGLE — CORROSION (BS 70)

INSPECTION TYPE-CS2, HEAVY CORROSION AT FS 70 CAP ANGLE FWD SIDE BETWEEN LONGERONS 31L TO 31R. REPAIRED PER UPS EO.

Part: WEB — CRACKED (BS 980)

INSPECTION TYPE: CS2. RT WHEELWELL FS 980 CENTER FRAME INNER WEB CRACKED AT SPLICE. REPAIRED WEB PER SRM 53-2-0.

Part: FRAME — CORROSION (BS 1730)

INSPECTION TYPE-CS2, HEAVY CORROSION AT BELT FRAME FS 1730 LONGERON 22L TO 22R. REPLACED FRAME SECTION PER SRM 51-1-20D.

Part: ANGLE — CORROSION (BS1540)

INSPECTION TYPE: CS2. FS 1540 LONGERON 30L VERTICAL SUPPORT ATTACH ANGLE HAS EXFOLIATED CORROSION. REPLACED ANGLE PER SRM 51-1-21.

Part: FLOORBEAM — CORROSION (BS 680)

INSPECTION TYPE-CS2, HEAVY EXFOLIATED CORROSION AT CABIN FLOORBEAM FS 680 UPPER FLANGE RBL 60. REPAIRED PER UPS EO.

Part: RIB — CRACKED (RT WING LE)

INSPECTION TYPE-CS2, RT WING LEADING EDGE WING 3 RIBS CRACKED AT STA XFS212, XFS242 AND XFS285. REPAIRED RIBS PER MM 57-00-00 FIG 801.

Part: FLOOR PANS — CORROSION (BS 55)

INSPECTION TYPE: CS2. FS 55 RBL 30 AND RBL 20. RECESSED FLOOR PANS HAVE EXFOLIATED. CORROSION REPLACED FLOOR PANS PER SRM 51-1-20D.

Part: INTERCOSTAL — CORROSION (BS 50-40)

INSPECTION TYPE: CS2. INTERCOSTAL BEAM HAS EXFOLIATED CORROSION FS 40 TO 50 RBL 30 AT CABIN FLOOR BEAM. REPLACED INTERCOSTAL SECTION PER SRM 51-1-20D.

Part: FLOORBEAM — CORROSION (BS 12)

INSPECTION TYPE-CS2, FS 12 LBL 40 TO 60 FLOORBEAM LOWER FLANGE HAS EXFOLIATED CORROSION. REPAIRED PER UPS EO.

Part: SKIN — CORROSION (BS 25-70)

INSPECTION TYPE-CS2, FUSELAGE SKIN HEAVY CORROSION FS 70 TO 25 LONGERONS 21L TO 31L. REPAIRED SKIN PER DAL DRAWING NR 5613861 AND UPS EO.

Part: DOUBLER — CORROSION (BS 1690-1710)

INSPECTION TYPE-CS2, HEAVY CORROSION AT LONGERON 28L DOUBLER FS 1690 TO 1710. REPLACED DOUBLER PER SRM 51-1-20D AND SRM 51-1-21.

Part: FITTING — CRACKED (BS 1781)

INSPECTION TYPE-CS, VERTICAL ATTACH FITTING FOR THE TAIL SKID CARTRIDGE HAS A 6 INCH LONG CRACK ON BOTTOM FACE. REPLACED FITTING PER SRM 51-3-0 AND SRM 51-1-23.

Part: LONGERON — CORROSION (BS 1740-1766)

INSPECTION TYPE-CS2, FS 1740 TO 1766 HEAVY CORROSION AT LONGERON 34R. REPLACED LONGERON SECTION PER SRM 51-1-20D.

Part: DOUBLER — CORROSION (BS 1766-1810)

INSPECTION TYPE-CS2, HEAVY CORROSION AT BELLY DOUBLER FS 1766 TO 1810. REPLACED DOUBLER PER SRM 51-1-20D.

Part: FLOORBEAM — CORROSION (BS 1730)

INSPECTION TYPE-CS2, FS 1730, FLOORBEAM HAS MODERATE CORROSION DAMAGE FROM BL 0 TO LBL 60. REPLACED FLOORBEAM SECTION PER SRM 51-1-20D.

Part: FITTING — CORROSION (BS 70)

INSPECTION TYPE-CS2, HEAVY CORROSION ON LONGERONS FITTING FS 70 FWD SIDE LONGERON 6R. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CORROSION (BS 70)

INSPECTION TYPE-CS2, HEAVY CORROSION ON LONGERON 4R END FITTING FWD SIDE OF FS 70. REPLACED FITTING PER SRM 51-1-20D AND SRM 51-3-0.

Part: FITTING — CORROSION (BS 70)

INSPECTION TYPE-CS2, HEAVY CORROSION ON LONGERON 8L END FITTING FWD SIDE OF FS 70. REPLACED FITTING PER SRM 51-1-20 AND SRM 51-1-21.

Part: FITTING — CORROSION (BS 70)

INSPECTION TYPE-CS2, HEAVY CORROSION AT FITTINGS FWD SIDE OF FS 70 LONGERONS 3L AND 1. REPLACED FITTINGS PER SRM 51-1-20D.

Part: ANGLE — CORROSION (BS 280)

INSPECTION TYPE: CS2. HEAVY CORROSION ON SUPPORT ANGLE FS 280 AFT SIDE LONGERON 27L. REPLACED ANGLE PER SRM 51-1-20D.

Part: FITTING — CRACKED (RRS 98)

INSPECTION TYPE: CS2. FLAP ACTUATOR ATTACH FITTING CRACKED AND CORRODED ON RT WING REAR SPAR STA 98. REPLACED FITTING PER MM 20-16-00.

Part: FITTING — CRACKED (RSS 97)

INSPECTION TYPE: CS2. FLAP SUPPORT FITTING CRACKED AND CORRODED ON RT WING REAR SPAR STA 97. REPAIRED PER UPS EO DC8-57-0720.

Part: DOUBLER — CRACKED (NR 2 PYLON)

INSPECTION TYPE: CS2. NR 2 PYLON LOWER DOUBLER JUST ABOVE T-DOUBLER CRACKED ON FWD SIDE. REPAIRED PER UPS EO'S DC8-57-0717/-0726.

Part: SKIN — CORROSION (RT ELEVATOR)

INSPECTION TYPE: CS2. RT ELEVATOR UPPER MIDDLE SKIN HAS MODERATE CORROSION DAMAGE. REPLACED MIDDLE UPPER SKIN PER SRM 51-1-21.

Part: DOUBLER — CRACKED (LT WING LE)

INSPECTION TYPE: CS2. LT WING LEADING EDGE SKIN DOUBLER CRACKED AT DRAIN HOLE STA XFS597 **(MRR FILED OPEN)** REPAIRED PER UPS EO.

Part: FRAME — CORROSION (BS 1338)

INSPECTION TYPE-CS2, HEAVY CORROSION ON WEB FRAME FS 1338, LONGERON 11L. REPAIRED WEB PER SRM 53-2-0.

Part: FLOORBEAM — CORROSION (BS 55)

INSPECTION TYPE-CS2, MAIN CABIN FLOORBEAM FS 55 HEAVY CORROSION ON RBL 28 TO RBL 45. REPAIRED PER UPS EO.

Part: FITTING — CORROSION (BS 937)

INSPECTION TYPE: CS2. HEAVY CORROSION AT FS 937 LONGERON FITTING AT LONGERON 24R. REPAIRED PER UPS EO.

Part: SEAT TRACK — CORROSION (BS 640-1280)

INSPECTION TYPE: CS2 EXFOLIATED CORROSION ON CABIN SEAT TRACK, AT SEVERAL PLACES FS 640 THROUGH FS 1280 TRACK NR 9. REPLACED TRACK SECTION PER SRM 53-2-3.

Part: FRAME — CRACKED (BS 200)

INSPECTION TYPE-CS2, BELTFRAME FS 200 VERTICAL SUPPORT FRAME WEB AT LONGERON 27R IS CRACKED. REPLACED WEB SECTION PER SRM 53-2-0 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 880)

INSPECTION TYPE-CS2, B/T FITTING CRACKED AT FS 880 LONGERONS 23L TO 24L. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CRACKED (BS 700)

INSPECTION TYPE: CS2. FS 700 FLOOR BEAM TO LONGERON 23R FITTING IS CRACKED. REPLACED FITTING PER SRM 51-1-20D.

Part: TRAP FITTING — CRACKED (LT MLG WW)

INSPECTION TYPE: CS2. LT TRAPEZOID FITTING CRACKED IN VERTICAL WEB. REPLACED FITTING PER DAC DRAWING NR 5750127.

Part: FITTING — CRACKED (BS 920)

INSPECTION TYPE-CS2, FS 920 LONGERON 24R FITTING IS CRACKED. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE: CS2. CRACKED FITTING FS 680 LONGERON 36. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CRACKED (FS 960 L24L)

INSPECTION TYPE-CS2, FS 960 LONGERON 24L FITTING IS CRACKED. REPLACED FITTING PER SRM 51-1-20D.

Part: DEFELCTOR — CRACK (NR 3 NR 3 ENG)

INSPECTION TYPE-CS2, NR 3 ENGINE NOSE COWL ANTI-ICE D-DUCT INNER WING DEFLECTOR CRACKED AND PIECES MISSING. REPAIRED PER SRM ADDENDUM/EO.

Part: FITTING — CRACKED (BS 879)

INSPECTION TYPE: CS2. FS 879 LONGERON 24R B/T FITTING IS CRACKED. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CRACKED (FS 1690)

INSPECTION TYPE-CS2, LONGERON 24R END FITTING CRACKED AT FS 1690 FWD SIDE. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CORROSION (BS 70)

INSPECTION TYPE-CS2, MODERATE CORROSION DAMAGE ON END FITTING FS 70 LONGERON 33R. REPLACED FITTING PER SRM 51-1-20D AND SRM 51-1-2.

Part: FITTING — CORROSION (BS 980)

INSPECTION TYPE: CS2. RT WHEELWELL AFT CANTED BULKHEAD FITTING FS 980 RBL 38. HEAVY CORROSION. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CRACKED (FS 1680)

INSPECTION TYPE-CS2, LONGERON 24 END FITTING CRACKED AT FS 1680 AFT SIDE. REPLACED FITTING PER SRM 51-1-20D.

Part: LONGERON — CORROSION (BS 1140)

INSPECTION TYPE-CS2, FS 1140 AT LONGERON 29L HAS HEAVY CORROSION. REPAIRED LONGERON PER UPS EO.

Part: SHEAR TIE — CRACKED (BS 702)

INSPECTION TYPE: CS2. FS 702 RBL 8 SHEAR TIE CRACKED AND HEAVILY CORRODED IN KEEL AREA. REPAIRED SHEAR TIE PER SRM 53-2-0, FIG 2 AND SRM 51-1-20D.

Part: FITTING — CORROSION (BS 878)

INSPECTION TYPE: CS2. HEAVY CORROSION AT FS 878 LONGERON 23R ATTACH FITTING. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CORROSION (BS 130)

INSPECTION TYPE-CS2, HEAVY CORROSION ON COCKPIT SUBFLOOR AND VERTICAL RETAINER FITTING FS 130 RBL 40. REPLACED FITTING PER SRM 51-1-20D.

Part: SKIN — CORROSION (RT ELEVATOR)

INSPECTION TYPE: CS2. MODERATE CORROSION ON RT ELEVATOR BOTTOM SKIN JUST FORWARD OF THE OUTBOARD END OF GEAR TAB. REPLACED MIDDLE LOWER SKIN PANEL PER SRM 51-1-21.

Part: SHEAR TIE — CORROSION (BS 1720)

INSPECTION TYPE: CS2. FS 1720 AT LONGERON 26R HEAVY CORROSION ON SHEAR TIE. REPLACED SHEAR TIE SECTION PER SRM 51-1-20D.

Part: LONGERON — CORROSION (BS 1520-1540)

INSPECTION TYPE-CS2, MODERATE CORROSION OUT OF LIMITS AT LONGERON 26L BETWEEN FS 1520 TO 1540. REPAIRED LONGERON PER SRM 53-2-2, FIG 10.

Part: LONGERON — CORROSION (BS 300-280)

INSPECTION TYPE: CS2. HEAVY CORROSION ON LONGERON 32L FS 280-300. REPAIRED LONGERON PER SRM 53-2-2 FIG 10.

Part: FITTING — CORROSION (BS 280)

INSPECTION TYPE: CS2. MODERATE CORROSION ON B/T FITTING FS 280 BETWEEN LONGERONS 31L-32L. REPLACED FITTING PER SRM 53-2-0 FIG 2D.

Part: FRAME — CORROSION (BS 1040)

INSPECTION TYPE: CS2. SPLICE FITTING HEAVY CORROSION ON BELT FRAME FS 1040, LONGERON 27R. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CORROSION (BS 920)

INSPECTION TYPE: CS2. FS 920 LONGERON 23L RIGHT HAND ATTACH FITTING HAS MODERATE CORROSION. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CORROSION (BS 300)

INSPECTION TYPE: CS2. MODERATE CORROSION AT B/T FITTING FS 300, LONGERON 27L. REPLACED FITTING PER SRM 53-2-0.

Part: FITTING — CORROSION (BS300)

INSPECTION TYPE: CS2. MODERATE CORROSION ON FITTING FS 300, BETWEEN LONGERONS 35R-36. REPLACED FITTING PER SRM 51-1-20D.

Part: LONGERON — CORROSION (BS 430)

INSPECTION TYPE: CS2. FS 430 LONGERON 30R HEAVY CORROSION. REPAIRED LONGERON PER SRM 53-2-3 AND SRM 51-1-20D.

Part: FITTING — CORROSION (BS 320)

INSPECTION TYPE: CS2. MODERATE CORROSION AT LONGERON 21L TO BELT FRAME FITTING FS 320. REPLACED FITTING PER SRM 51-1-20D.

Part: LONGERON — CORROSION (BS 200-220)

INSPECTION TYPE-CS2, HEAVY CORROSION AT LONGERON 8R, FS 200 TO 220. REPLACED LONGERON SPLICE PER SRM 51-1-20D.

Part: LONGERON — CORROSION (BS 1260-1280)

INSPECTION TYPE-CS2, HEAVY CORROSION ON LONGERONS 7R AND 8R AT FS 1260 TO 1280. INSTALLED LONGERON SPLICES PER SRM 51-1-21 AND SRM 51-1-20D.

Part: SKIN — CORROSION (BS 1690-1910)

INSPECTION TYPE-CS2, LOWER BELLY SKIN FS 1690 TO 1910 HEAVY CORROSION. REPLACED SKIN SECTION PER SRM 51-1-21 AND SRM 51-1-20D.

Part: FRAME — CORROSION (BS 120-140)

INSPECTION TYPE-CS2, HEAVY CORROSION ON FRAME BOX BETWEEN LONGERONS 8R TO 9R, FS 120 TO 140. SPLICED FRAME BOX PER SRM 51-1-20D AND SRM 51-1-21.

Part: DOUBLER — CORROSION (BS 52-67)

INSPECTION TYPE-CS2, HEAVY CORROSION ON FUSELAGE FWD NOSE SECTION PANEL DOUBLER FS 52 TO 67 LONGERON 22R. REPAIRED PER UPS EO.

Part: FRAME — CORROSION (BS 1380)

INSPECTION TYPE-CS2, HEAVY CORROSION ON BELT FRAME AFT SIDE FS 1380 LONGERON 7L. REPAIRED FRAME PER SRM 53-2-0 FIG 2 SHEET 4.

Part: LONGERON — CORROSION (BS 1500-1520)

INSPECTION TYPE-CS2, MODERATE CORROSION DAMAGE AT LONGERON 1, FS 1500 TO 1520. SPLICED LONGERON SECTION PER SRM 51-1-21.

Part: FRAME — CORROSION (BS 1360)

INSPECTION TYPE-CS2, BELT FRAME AT FS 1360 FWD SIDE HAS HEAVY CORROSION AT LONGERON 5L. REPAIRED FRAME PER SRM 53-2-0.

Part: DOUBLER — CORROSION (BS 32-12)

INSPECTION TYPE-CS2, HEAVY CORROSION ON FWD NOSE SECTION RT SIDE DOUBLER FS 32 TO FS 12 RBL 25 TO RBL 45. REPAIRED PER UPS EO.

Part: FRAME — CORROSION (BS 1640)

INSPECTION TYPE-CS2, HEAVY CORROSION ON BELT FRAME FS 1640 LONGERON 2R TO 10R. REPLACED FRAME SECTION PER SRM 51-1-20D.

Part: FITTING — CRACKED (NR 4 SPOILER)

INSPECTION TYPE: CS2. 2 EA LT WING NR 4 SPOILER INBOARD AND OUTBOARD ATTACH FITTINGS CRACKED. REPLACED FITTINGS PER MM 27-61-01.

Part: FRAME — CORROSION (BS 1520)

INSPECTION TYPE-CS2, HEAVY CORROSION ON BELT FRAME FS 1520 LONGERON 1L. REPAIRED FRAME PER SRM 53-2-0 FIG 2.

Part: LONGERON — CRACKED (BS 857)

INSPECTION TYPE: CS2. LONGERON 24L CRACKED (3 EA) AT BOTTLE BOLT HOLE FS 857. REPLACED LONGERON SECTION PER DAC DRAWINGS NR 5779948 AND 5779938.

Part: SKIN — DELAMINATED (NR 4 SPOILER)

INSPECTION TYPE-CS2, RT WING NR 4 SPOILER DELAMINATED. REPLACED SPOILER PER MM 27-61-01.

Part: RIB — CRACKED (LT WING LE)

INSPECTION TYPE: CS2. LT WING LEADING EDGE 9 EA RIBS CRACKED AT WS XFS730, XFS750, XFS755 , XFS760, XFS765, XFS775, XFS780, XFS785 AND XFS800. REPAIRED RIBS PER MM 57-00-00 FIG 801.

Part: RIB — CRACKED (RT WING LE)

INSPECTION TYPE-CS2, RT WING LEADING EDGE 4 RIBS CRACKED AT STA XFS820, XFS800, XFS695 AND XFS680. REPAIRED RIBS PER MM 57-00-00, FIG 801.

Part: FITTING — CRACKED (WS 410)

INSPECTION TYPE: CS2. LT WS XRS410 CANOE FITTING OUTBOARD SIDE BRACE FITTING CRACKED INSIDE CHANNEL. REPLACED FITTING PER SRM 51-1-20D.

Part: SKIN — CRACKED (MAIN ENTRY DOOR)

INSPECTION TYPE: CS2. FORWARD ENTRY DOOR OUTER SKIN LOWER FWD CORNER CRACKED. REPAIRED SKIN PER SRM 52-2-0.

Part: RIB — CRACKED (LT WING LE)

INSPECTION TYPE: CS2. LT WING LEADING EDGE ASSY 7 EA RIBS CRACKED AT WS XFS550 UPPER, XFS 565 LOWER, XFS565 UPPER, XFS570 UPPER, XFS575 UPPER, XFS580 UPPER AN D XFS585 UPPER RIBS. REPAIRED PER MM 57-00-00 FIG 801

Part: RIB — CRACKED (RT WING LE)

INSPECTION TYPE: CS2. RT WING LEADING EDGE UPPER RIB CRACK AT STA XFS560. REPAIRED RIB PER MM 57-00-00 FIG 801.

Part: WEB — CRACKED (BS 340)

INSPECTION TYPE-CS2, WEB CRACKED FS 340 RBL 48 ABOVE A BIN DOOR JAMB. REPAIRED WEB PER UPS EO.

Part: LONGERON — CRACKED (FS 857)

INSPECTION TYPE-CS2, LONGERON 24R AT FS 857, CRACKED AT BOTTLE BOLT HOLE. REPLACED LONGERON PER DRAWING NR 5750198 DAC.

Part: RIB — CRACKED (LT WING LE)

INSPECTION TYPE: CS2. LT WING LEADING EDGE ASSY 7 EA RIBS CRACKED AT WS XFS985 LOWER, XFS 600 UPPER, XFS605 UPPER, XFS610 UPPER, XFS615 UPPER, XFS625 UPPER AN D XFS645 UPPER RIBS. REPAIRED RIBS PER MM 57-00-00 FIG 801.

Part: TRIM TAB — DELAMINATED (LT AILERON)

INSPECTION TYPE: CS2. LT AILERON TRIM TAB DELAMINATED. REPLACED TAB PER MM 27-13-01.

Part: FITTING — CRACKED (AFT ENTRY DOOR)

INSPECTION TYPE: CS2. LT AFT ENTRY DOOR FITTING CRACKED INSIDE 2ND LIGHTNING HOLE FROM TOP FWD SIDE. REPLACED FITTING PER SRM 51-1-20D.

Part: SKIN — DELAMINATED (NR 4 SPOILER)

INSPECTION TYPE-CS2, LT WING NR 4 SPOILER DELAMINATED. REPLACED SPOILER ASSY PER MM 27-61-01.

Part: SKIN — DELAMINATION (NR 3 SPOILER)

INSPECTION TYPE: CS2. NR 3 SPOILER PANEL DELAMINATED ON RT WING. REPLACED SPOILER PER MM 27-61-01.

Part: LANYARD — FRAYED (MAIN ENTRY DOOR)

INSPECTION TYPE: CS2. EVACUATION SLIDE LANYARD ASSY CABLE FRAYED. REPLACED LANYARD PER MM 25-60-01.

Part: SKIN — CORROSION (BS 120-140)

INSPECTION TYPE: CS2. HEAVY CORROSION AT FUSELAGE SKIN PANEL FS 120-140 BETWEEN LONGERONS 3 5L-35R. REPAIRED PER UPS EO.

Part: SKIN — CRACKED (NLG CUTOUT)

INSPECTION TYPE-CS2, .5 INCH LONG CRACK AT NOSE GEAR WHEEL WELL CUTOUT. REPAIRED PER UPS EO AND SRM 51-1-21.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE)

MAINTENANCE REPORTED ESCAPE SLIDE CONTAINER INSECURE. SLIDE BAR WOULD NOT ENGAGE IN CLIPS. SECURED AND RE-POSITIONED.

Part: BATTERY PACK — DISCHARGED (FLIGHT DECK)

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

Part: PACK — MALFUNCTIONED (LT PACK)

SUPPLEMENTAL MRR - UPON PUSH BACK AT SAN JUAN, LEFT PACK OVERHEATED 200 DEGREES, SMOKE IN COCKPIT, BLOCK TURNBACK. DEFERRED AS PER MEL 21-38-1 AND MMOC. MAINTENANCE PROCEDURES PERFORMED. OPS CHECK LT PACK, NO OVERTEMP, NO PACK TRIP, NO SMOKE IN COCKPIT. OAT 95F PACK TEMP 130F THROUGH FULL RANGE. OK FOR SERVICE.

Part: EEL BATTERY PACK — DISCHARGED (FLIGHT DECK)

PILOT REPORTED, EMERGENCY LIGHTS CAME ON IN FLIGHT, ALL ELECTRICAL SYS GOOD. COULD NOT TURN OFF LIGHTS WITH ARM /DISARM SWITCH. REPLACED EMERGENCY BATTERY PACK ASSY.

Part: STIFFENER — CRACKED (NR 1 PYLON)

WHILE IN 'C' CHECK MAINTENANCE FOUND CRACK ON NR 1 PYLON HORIZONTAL STIFFENER AT STA 364-942. REPAIRED PER UPS EO FILE NR DC8-54-0029.

Part: RIBS — CRACKED (LT WING)

WHILE IN 'C' CHECK MAINTENANCE FOUND CRACKS ON LT WING, LWR SURFACE, UPPER RIBS 13, 29, 24, AND 14. REPAIRED PER MM 57-00-00.

Part: ANGLE — CRACKED (FS 1766)

WHILE IN 'C' CHECK MAINTENANCE FOUND CRACK ON RT VERT. STAB. TO FUSELAGE ATTACH ANGLE, FS 1766. INSTALLED REPAIR PER SRM 53-2-5.

Part: SKIN — CRACKED (LT WING LE)

WHILE IN 'C' CHECK MAINTENANCE FOUND CRACK ON LT WING L/E, LWR SKIN SCREW HOLE ON I/B END. INSTALLED REPAIR PER SRM 57-2-0.

Part: BULKHEAD BEAM — CRACKED (FS 1766)

WHILE IN 'C' CHECK MAINTENANCE FOUND CRACK ON AFT PRESSURE BULKHEAD, 'J' BEAM, THIRD FROM TOP AT FS 1766, RBL 1, THRU ACCESS HOLE 60. REPAIRED PER SRM 53-2-0.

Part: DOUBLER — CORRODED (RT WING)

WHILE IN 'C' CHECK MAINTENANCE FOUND CORROSION ON RT WING L/E LWR SURFACE DOOR DOUBLER AT STA XFS 360-366. REPAIRED PER UPS EO FILE NR DC8-57-0539.

Part: WHEEL — FAILED (LT MLG)

PILOT REPORTED LEFT MAIN GEAR DOOR LIGHT ON AFTER GEAR RETRACTION. RAN CHECKLIST, NO HELP. FLEW AT REDUCED AIRSPEED. NR 1 WHEEL RIM FAILURE. CHANGED NR 1 AND NR 2 TIRE ASSY. CYCLED GEAR DOORS. DOOR LIGHTS CHECKED OK IAW 32-40-01.