N6161C

Part: ACTUATOR BOLT — BROKEN (RT MLG)

PERFORMED GEAR UP LATCH CHECK AND DOOR'S NOT LATCHED AND GEAR NOT AND LATCHED LIGHT ILLUMINATED. CYCLED GEAR AND PERFORMED CHECKLIST AND LIGHTS REMAINED ON. SECURED RIGHT MLG ACTUATOR, INSTALLED AND SAFTIED ALL THREE GEAR PINS FOR FLIGHT. THIS A/C HAS BEEN INSPECTED AND FOUND SAFE FOR INTENDED FERRY FLIGHT. ON POSTFLIGHT FOUND RT MAIN GEAR CYLINDER BOSS BOLT BROKEN. REMOVED AND REPLACED RETRACT PIN RT MLG IAW DC8 OHM CHAPT 32-2-1 AND SB 32-101. PERFORMED LANDING GEAR ACTUATOR INSTALLATION IAW DC8 MM 32-4-2, LANDING GEAR EXTENSION AND RETRACTION OPS CHECK NORMAL IAW DC8 MM 32-3-0. NO LEAKS OR DEFECTS NOTED.

Part: RETRACT MECH — MALFUNCTIONED (NLG DOORS)

NOSE GEAR DOOR OPEN AFTER GEAR RETRACTION, HAD LOUD NOISE AND STRONG VIBRATION. CLOSED NOSE GEAR DOOR, OPS CHECK GOOD IAW MM REFERENCE 32-2-5.

Part: WIRE — CHAFED (NR 2 ENGINE)

NR 2 ENGINE FIRE INDICATION ON CLIMBOUT. INDICATION STOPPED UPON RETARDING POWER LEVER. FIRE TEST CHECKED GOOD. CONTINUED FLIGHT WITH NR 2 ENGINE BLEED VALVE CLOSED. REPAIRED WIRING AT LEFT AFT DOOR. CHECKS GOOD ON GROUND.

Part: SEQUENCE VALVE — LEAKING (NR 2 ENGINE)

NR 2 ENGINE HAD FIRE WARNING BELL COME ON IN LANDING WITH POWER LEVER IN REVERSE, WENT OFF ON ENGINE SHUTDOWN. TROUBLESHOT AND FOUND THRUST REVERSER SEQUENCE VALVE LEAKING. REMOVED AND REPLACED VALVE IAW MM 78-8-6. LEAK AND OPS CHECKED THRUST REVERSER, NO DEFECTS NOTED. PERFORMED HIGH POWER RUN AT TAKEOFF POWER. NO BELL ON WARNING. OPS OK.

Part: FIRE LOOP — SHORTED (NR 2 ENGINE)

KMIA - TRIP NR 84655: ON DESCENT INTO KMIA, HAD INTERMITTENT FIRE WARNING NR 2 ENGINE. TROUBLESHOT SYSTEM, FOUND AFT OUTBOARD FIRELOOP SHORTED AGAINST COWLING. INSULATED AND PROPERLY SECURED LOOP. CHECKED SYSTEM OPERATION WITH ENGINE AT TAKEOFF POWER GOOD. SYSTEM OPS GOOD IAW DMM CHAPTER 26.

Part: SKIN — DAMAGED (BS 550-556)

DURING B-CHECK INSPECTION, FOUND SKIN PUNCTURED, ON BOTTOM B-PIT ON FUSELAGE 12 BELOW DOOR SILL. REMOVED DAMAGED MATERIAL AND REPAIRED IAW AIA ENGINEERING SKETCH NR AIA/E/2413, FAA/DER APPROVED ON FORM 8110-3 DATED 11-19-96. NON-ROUTINE TASK CARD NR 89763.

Part: SKIN — DAMAGED (BS 400-420)

ON CREW PREFLIGHT, CARGO LOADING DAMAGE WAS NOTED ON RIGHT HAND SIDE OF FUSELAGE, JUST AFT OF A PIT DOOR, AT APPROXIMATE LONGERON 28, FUSELAGE STA 412. SKIN PUNCTURED AND LONGERON 28 DENTED AND CRACKED. REMOVED DAMAGED AREA AS REQUIRED. COMPLIED WITH FLUSH REPAIR AND LONGERON 28 REPAIR BETWEEN RIGHT HAND FUSELAGE STA 400 TO 420 IAW AIA ENGINEERING SKETCH NR AIA/E/2333, FAA DER APPROVED 9-15-96. NO FURTHER ACTION REQUIRED.

Part: PS4 LINE — LOOSE (NR 1 ENGINE)

NR 1 ENGINE FIRE CAME ON INTERMITTENTLY DURING FLIGHT WITH BLEED AIR ON FIRE WARNING TEST OK. TIGHTENED LOOSE LINE TO PRBC ON NR 1 ENGINE. RAN ENGINE AT VARIOUS POWER SETTING WITH BLEED ON, NO LEAKS NOTED. NO FIRE WARNING, OPS CHECK NORMAL.

Part: SKIN — BULGED (BS 600)

DURING C-2 CHECK, INSPECTION FOUND FS 600 L-36 BULGE IN SKIN. REPAIRED BULGE IN SKIN PER DC-8 SRM 53-2-1 FIGURE 7. TASK NR 80841, CORROSION CARD NR 5570-0551.

Part: SKIN — DAMAGED (AILERON)

DURING C-2 CHECK, INSPECTION FOUND OUTBOARD AILERON INBOARD LOWER SKIN DAMAGED. REPAIRED LOWER SKIN IAW AIA EA DWG 22486161 SKETCH NR AIA/E/2249, TASK NR 80134, CORROSION CARD NR 111R-0551.

Part: SPLICE PLATE — CORRODED (BS 1490)

DURING C-2 CHECK, INSPECTION FOUND STA 1490 S-30 LEFT IN AFT ACCESSORY COMPARTMENT SPLICE PLATE CORRODED. REMOVED AND REPLACED SPLICE PLATE IAW SRM 51-1-21 AND 51-3-1. TASK NR 80534, CORROSION CARD NR 5600-0551.

Part: SKIN — CRACKED (WS 310-329)

DURING C-2 CHECK, INSPECTION FOUND UPPER SKIN ON LEADING EDGE AT STA XFS 310 TO 329 WAS CRACKED AROUND SCREW HOLES. REPAIRED IAW DC8 SRM 57-2-1. TASK NR 80061, CORROSION CARD NR 116L-0550 AND 116R-0550.

Part: FITTING — CORRODED (BS 310)

DURING C-2 CHECK, INSPECTION FOUND BATHTUB FITTING AT FS 310 STRINGER 26R CORRODED. FITTING WAS CORRODED BEYOND LIMITS. REPLACED BATHTUB FITTING IAW DC8 SRM CHAPTERS 51-1-8, 51-1-20D, 51-1-21, 51-3-0 AND 53-2-2. TASK NR 80996, CORROSION CARD NR 5670-0551.

Part: LINK ASSY — CRACKED (TE FLAPS)

DURING C-2 CHECK, INSPECTION FOUND INBOARD MOST FLAP CARRIAGE LINK ASSEMBLY FWD END APPEARS CRACKED. REMOVED AND REPLACED INBOARD MOST FLAP CARRIAGE LINK ASSEMBLY. TASK NR 79978, CORROSION CARD NR 124L-0551.

Part: FITTING — CORRODED (BS 310)

DURING C-2 CHECK, INSPECTION FOUND BATHTUB FITTING AT FS 310 STRINGER 25R CORRODED. REMOVED AND REPLACED BATHTUB FITTING IAW DC8 SRM 51-1-8, 51-1-21, 53-2-0 AND 51-1-20D. TASK NR 80997, CORROSION CARD NR 557R-0551.

Part: SEAT TRACK — CORRODED (BS 1000)

DURING C-2 CHECK, INSPECTION FOUND SEAT TRACK AT CENTER BL FS 1000 TO FS 850 CORRODED AT ATTACH POINTS. REMOVED AND REPLACED SEAT TRACK IAW DC8 SRM 51-1-21. TASK NR 80937, CORROSION CARD NR 5700-0553.

Part: FLOOR BEAM — CORRODED (BS 940)

DURING C-2 CHECK, INSPECTION FOUND FS 940 FLOOR BEAM CORRODED AT RBL 8. REPAIRED IAW AIA EA DRAWING NR 2259 FILE NR 22596161 DATED 7-26-96. TASK NR 80862, CORROSION CARD NR 2000-0551.

Part: SKIN — CORRODED (BS 540)

DURING C-2 CHECK, INSPECTION FOUND FS 540 L-36 LOWER BELLY SKIN CORRODED. REMOVED CORROSION, CLEANED AREA, TREATED INSTALLED PATCH AS PER SRM 51-1-8 SRM 53-2-1 CLASS I. TASK NR 81484, CORROSION CARD NR 5570-0551.

Part: SEAT TRACK — CORRODED (BS 640-860)

DURING C-2 CHECK, INSPECTION FOUND FS 640 TO 860 LBL 25 SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK IAW DC8 SRM 53-2-3. TASK NR 80951, CORROSION CARD NR 2000-0551.

Part: FLOOR BEAM — CORRODED (BS 920)

DURING C-2 CHECK, INSPECTION FOUND FLOOR BEAM AT FS 920 CORRODED AT RBL 33. REMOVED AND TREATED CORROSION IAW SRM 51-01-08. REPAIRED FLOOR BEAM IAW AIA EA DRAWING NR 2256. TASK NR 80863, CORROSION CARD NR 2000-0551.

Part: SPLICE FITTING — CORRODED (BS 1140-1160)

DURING C-2 CHECK, INSPECTION FOUND AFT BELLY PIT SPLICE BETWEEN FS 1160 AND 1140 ON STRINGER 33R CORRODED. REMOVED SPLICE FITTING AND FOUND CRACK IN AFT STRINGER. REPAIRED CRACKED STRINGER IAW DC8 SRM 53-2-2 AND INSTALLED NEW SPLICE FITTING IAW DC8 SRM 53-2-2. TREATED AND PRIMED IAW DC8 SRM 51-1-8. TASK NR 80541, CORROSION CARD NR 5590-0551.

Part: SPAR — CORRODED (CENTER WING)

DURING C-2 CHECK, INSPECTION FOUND CENTER WING LOWER FRONT SPAR HAS HEAVY EXFOLIATION CORROSION FROM STATION XCW 17R TO XCW 405R AT PREVIOUS REPAIR. REPAIRED SPAR IAW DC8 S/B 57-30R4 AND DRAWING SR08570012. TASK NR 80079, CORROSION CARD NR 2000-0551.

Part: SPAR CAP — CORRODED (CENTER WING)

DURING C-2 CHECK, INSPECTION FOUND CENTER WING FRONT SPAR LOWER CAP CORRODED AND CRACKED APPROXIMATELY STATION XCW 23L TO XCW 43L. REPAIRED IAW DC8 S/B 57-30R4 DRAWING NR SR08570012. TASK NR 80082, CORROSION CARD NR 2000-0551.

Part: FLOOR BEAM — CORRODED (FS 740)

DURING C-2 CHECK, INSPECTION FOUND FS 740 FLOOR BEAM CORRODED AT RBL 27. REPAIRED IAW SKETCH AIA/E/2269 AND APPROVED FAA FORM 8110-3. TASK NR 81013, CORROSION CARD NR 5700-0553.

Part: WEB — DAMAGED (PAX DOOR AREA)

DURING C-2 CHECK, INSPECTION FOUND WEB ABOVE LEFT HAND AFT ENTRANCE DOOR DAMAGED. REMOVED AND REPLACED WEB IAW DC8 SRM 53-2-0, 51-1-21, AND 51-1-11. TASK NR 80958, WORK CARD NR 3043.

Part: FITTING — CORRODED (BS 310)

DURING C-2 CHECK, INSPECTION FOUND FS 310 L-31R END FITTING CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-8, 51-1-21, 51-1-20D AND 51-1-22. TASK NR 82166, CORROSION CARD NR 5570-0551.

Part: SEAT TRACK — CORRODED (CABIN)

DURING C-2 CHECK, INSPECTION FOUND SEAT TRACK AT RBL 50 CORRODED AT ATTACH POINTS. REMOVED AND REPLACED SEAT TRACK IAW DC8 SRM 51-1-21 AND 51-3-0. TASK NR 80938, CORROSION CARD NR 5700-0553.

Part: VERT STIFFENER — CORRODED (WING FRONT SPAR)

DURING C-2 CHECK, INSPECTION FOUND CENTER WING FRONT SPAR VERTICAL STIFFENER CORRODED AND CRACKED LOWER END APPROXIMATELY STA XCW 23R. REPAIRED IAW DC8 SRM 57-2-0 AND 51-1-8. TASK NR 80080, CORROSION CARD NR 2000-0551.

Part: FITTING — CORRODED (DOOR JAMB)

DURING C-2 CHECK, INSPECTION FOUND CORROSION IN FWD DOOR JAM ON REAR SERVICE DOOR RIGHT HAND. CLEANED CORROSION ON FITTING IN FWD DOOR JAM AND FOUND TO BE OUT OF LIMITS IAW DC8 SRM. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D. TREATED AND PRIMED IAW DC8 SRM 51-1-8. TASK NR 81023, WORK CARD NR 3057.

Part: SPLICE PLATE — CORRODED (BS 1490)

DURING C-2 CHECK, INSPECTION FOUND STA 1490 STRINGER 28R IN AFT ACCESSORY COMPARTMENT SPLICE PLATE CORRODED. REMOVED CORRODED SPLICE PLATE AND REPLACED WITH NEW SPLICE PLATE IAW DC8 SRM 51-1-21 AND DC8 SRM 51-3-1. TASK NR 80535, CORROSION CARD NR 5600-0551.

Part: FITTING — CORRODED (BS 560)

DURING C-2 CHECK, INSPECTION FOUND FS 560 L36 BULGE IN SKIN. REMOVED CORROSION, TREATED AREA AND REPLACED LONGERON END FITTING. DRAWING NR 5774353, TASK NR 80840, CORROSION CARD NR 5570-0551.

Part: STRINGER — CORRODED (BS 275-295)

DURING C-2 CHECK, INSPECTION FOUND STRINGER 24R CORRODED BETWEEN FS 295 AND FS 275. REMOVED AND REPLACED STRINGER IAW DC8 SRM 51-1-8, 51-1-21, 51-1-20D, 51-1-22 AND 53-2-2 FIGURE 10. TASK NR 81001 CORROSION CARD NR 5570-0551.

Part: INTERCOSTAL — CORRODED (BS 1020)

DURING C-2 CHECK, INSPECTION FOUND INTERCOSTAL AT FS 1020 CORRODED BELOW NUTPLATES AT STRINGER 33R. REMOVED AND REPLACED INTERCOSTAL AT FS 1020 IAW DC8 SRM 53-2-0, AND 51-1-21. TREATED AND PRIMED IAW DC8 SRM 51-1-8. TASK NR 80645, CORROSION CARD NR 5590-0551.

Part: ANGLE — CORRODED (BS 310)

DURING C-2 CHECK, INSPECTION FOUND FS 310 T-CHORD CORRODED FROM L-28LT TO 28RT. REMOVED SECTION OF FWD ANGLE FROM 28R-28L. INSTALLED NEW ANGLE IAW SRM 53-2-5 FIGURE 8C. TASK NR 82169, CORROSION CARD NR 5570-0551.

Part: FITTING — CORRODED (BS 310)

DURING C-2 CHECK, INSPECTION FOUND BATHTUB FITTING AT FS 310 STRINGER 31L CORRODED. REMOVED AND REPLACED FITTING PER SRM 53-2-0, 51-1-21, 51-1-20D AND 51-3-0. TASK NR 81008, CORROSION CARD NR 5570-0551.

Part: FLOOR BEAM — CORRODED (BS 295)

DURING C-2 CHECK, INSPECTION FOUND CORROSION ON UPPER FLOOR BEAM FS 295 RBL 36. REPLACED UPPER FLOOR BEAM FS 295 RBL 36 IAW DC8 SRM 51-1-20 AND AIA ENGINEERING REPORT NR 96 AIA-105. TASK NR 81000, CORROSION CARD NR 5700-0553.

Part: VERT STIFFENER — CORRODED (CENTER WING)

DURING C-2 CHECK, INSPECTION FOUND CENTER WING FRONT SPAR VERTICAL STIFFENER CORRODED AND CRACKED APPROXIMATELY STATION XCW 29L. REPAIRED IAW DC8 SRM 57-2-0, 51-1-20 AND 51-1-8. TASK NR 80083, CORROSION CARD NR 2000-0551.

Part: ANGLE — CORRODED (BS 857)

DURING C-2 CHECK, INSPECTION FOUND STA 857 FWD GEAR BOX UNDER FLOOR CENTER SECTION HAS CORROSION AT FRAMES. REPAIRED IAW AIA/E/2254 AND APPROVED FAA FORM 8110-3. TASK NR 80186 CORROSION CARD NR 2000-0557.

Part: STRINGER — CORRODED (BS 295-310)

DURING C-2 CHECK, INSPECTION FOUND STRINGER 24R CORRODED BETWEEN FS 310 AND FS 295. REMOVED AND REPLACED STRINGER IAW DC8 SRM 51-1-8, 51-1-21, 51-1-20D, AND 51-1-22. TASK NR 80999, CORROSION CARD NR 5570-0551.

Part: LONGERON — CORRODED (BS 1280)

DURING C-2 CHECK, INSPECTION FOUND FS 1280 L-35 LT LONGERON HAS SURFACE CORROSION. CORROSION FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. REPAIRED LONGERON 35 LT IAW DC8 SRM 53-2-2 AND 51-1-21. TREATED AND PRIMED IAW DC8 SRM 51-1-8. TASK NR 80549, CORROSION CARD NR 557L-0552.

Part: FITTING — CORRODED (BS 1490)

DURING C-2 CHECK, INSPECTION FOUND STATION 1490 STRINGER 29L IN AFT ACCESSORY COMPARTMENT SPLICE PLATE CORRODED, MARKED. CLEANED AND TREATED CORROSION IAW 51-1-8 WITHIN LIMITS 53-2-0 AND REPLACED FITTING PER SRM 51-1-20D. TASK NR 80533 CORROSION CARD NR 5600-0551.

Part: FLOOR BEAM — CORRODED (BS 902)

DURING C-2 CHECK, INSPECTION FOUND FLOOR BEAM CORRODED AND CRACKED AT FS 902 LBL 40. REMOVED AND TREATED CORROSION IAW DC8 SRM 51-01-08. REPAIRED FLOOR BEAM IAW AIA EA DRAWING NR 2253. TASK NR 80912, CORROSION CARD NR 5700-0553.

Part: ANGLE — CRACKED (WING FRONT SPAR)

DURING C-2 CHECK, INSPECTION FOUND CENTER WING FRONT SPAR VERTICAL STIFFENER LOWER ATTACH ANGLE CRACKED APPROXIMATELY STA XCW 35R. REPAIRED IAW DC8 DRAWING NR SR08570012. TASK NR 80081, CORROSION CARD NR 2000-0551.

Part: ANGLE — CORRODED (BS 565)

DURING C-2 CHECK, INSPECTION FOUND FS 565 DOOR JAMB FRAME ANGLE CORRODED. REPLACED ANGLE IAW SRM 53-2-0, 51-1-21, 51-3-0. TASK NR 80686, CORROSION CARD NR 5590-0551.

Part: FRAME — CORRODED (BS 1200)

DURING C-2 CHECK, INSPECTION FOUND AFT BELLY PIT CORROSION ON FS 1200 BETWEEN STRINGER 33R TO 33L. REMOVED CORROSION FROM FRAME AND FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. REPAIRED FRAME IAW DC8 SRM 53-2-0 FIGURE 2, 51-1-21. TREATED AND PAINTED IAW DC8 SRM 51-1-8. TASK NR 80537, CORROSION CARD NR 5590-0551.

Part: SEAT TRACK — CORRODED (BS 830-980)

DURING C-2 CHECK, INSPECTION FOUND SEAT TRACK AT LBL 50 CORRODED AT ATTACH POINTS FROM FS 830 TO FS 980. REMOVED AND REPLACED SEAT TRACK AT LBL 50. TASK NR 80939, CORROSION CARD NR 5700-0553.

Part: SKIN — CORRODED (BS 540)

DURING C-2 CHECK, INSPECTION FOUND FS 540 L36 LOWER BELLY SKIN CORRODED. REMOVED CORROSION AND INSTALLED REPAIR PER SRM 53-2-1. TASK NR 80746, WORK CARD NR 0011.

Part: INTERCOSTAL — CORRODED (BS 1020)

DURING C-2 CHECK, INSPECTION FOUND INTERCOSTAL AT FS 1020 CORRODED AT STRINGER 33R. REMOVED AND REPLACED INTERCOSTAL AT FS 1020 IAW DC8 SRM 53-2-0 AND 51-1-21. TREATED AND PRIMED IAW DC8 SRM 51-1-8. TASK NR 80644, CORROSION CARD NR 5590-0551.

Part: WIRE — BROKEN (NR 1 ENGINE)

SBGR - FLT 9999 - ON CLIMB-OUT FROM SBGR, NR 1 ENGINE FIRE WARNING CAME ON, PERFORMED FIRE WARNING SHUT-DOWN. AT TIME OF FIRE WARNING, NR 1 ENGINE PARAMETERS WERE NORMAL. ENGINE WAS SHUT DOWN AT 1630Z, OIL PRESSURE WAS MAINTAINED AT 30 PSI, N1 26 PERCENT, N2 40 PERCENT. REPAIRED BROKEN WIRE AT FIRE LOOP CANNON PLUG. OPS CHECKED NORMAL ON RUN IAW 24-10. (X)

Part: BRACKETS — LOOSE (NR 4 ENGINE)

KMIA - FLT 68305 - MASTER FIRE WARNING SHUT DOWN. IN MIA TERMINAL AREA, NR 4 ENGINE MASTER FIRE WARNING, SHUT DOWN NR 4 ENGINE. NORMAL LANDING. FOUND SEVERAL FIRE LOOP MOUNTING BRACKETS LOOSE AND GROMMETS MISSING. REPAIRED AND REPLACED MOUNTING BRACKETS. INSTALLED MISSING GROMMETS. RAN ENGINE AT TAKEOFF POWER FOR 5 MINUTES WITH BLEED AIR ON. NO FIRE WARNING. FIRE WARNING SYSTEM OPS NORMAL IAW MM 26-2-0. REFERENCE, OPERATOR CONTROL NR 95ZZZX6782. (X)

Part: GROMMETS — MISSING (NR 4 ENGINE)

KMIA - FLT 68305 - MASTER FIRE WARNING SHUT DOWN. IN MIA TERMINAL AREA, NR 4 ENGINE MASTER FIRE WARNING, SHUT DOWN NR 4 ENGINE. NORMAL LANDING. FOUND SEVERAL FIRE LOOP MOUNTING BRACKETS LOOSE AND GROMMETS MISSING. REPAIRED AND REPLACED MOUNTING BRACKETS. INSTALLED MISSING GROMMETS. RAN ENGINE AT TAKEOFF POWER FOR 5 MINUTES WITH BLEED AIR ON. NO FIRE WARNING. FIRE WARNING SYSTEM OPS NORMAL IAW MM 26-2-0. REFERENCE, OPERATOR CONTROL NR CKSA95140.

Part: FIRE DETECTOR — GROUNDED (NR 4 ENGINE)

KMIA - FLT 68166 - AT 30,000 FEET, FIRE WARNING ON NR 4 ENGINE, WITH LIGHT IN HANDLE AND BELL, AFTER PULLING NR 4 POWER LEVER TO IDLE. FIRE WARNING WENT OUT. FOUND FIRE WARNING DETECTOR LOOP GROUNDED TO AFT INBOARD COWL. REPAIRED AS NECESSARY. OPS CHECK NORMAL ON RUN-UP IAW MM 26-2-3. (X)

Part: SWITCH — FAILED (FE PANEL)

KMIA - SMOKE COMING FROM F/E ELECTRICAL PANEL. AFTER REMOVING THE PANEL, TROUBLESHOT AND FOUND SWITCH BURNED. REINSTALLED THE PANEL, DISCONNECTED THE NR 2 AND DMI'D IT IAW 24-1-1 AS ITEM NR 274. (M)

Part: FIRE LOOP — FAILED (NR 4 ENGINE)

EINN - FIRE INDICATION ON NR 4 ENGINE AFTER TAKEOFF. SHUT ENGINE DOWN IAW F.O.M. SHOT BOTH FIRE AGENT BOTTLES ON RIGHT WING, FIRE INDICATION CONTINUED, RETURNED TO AIRPORT. REMOVED AND REPLACED FORWARD OUTBOARD FIRE LOOP PER DC-8 MM 26-2-1. FIRE LOOP OPS CHECKS GOOD PER DC-8 MM 26-2-0. REMOVED AND REPLACED BOTH RIGHT WING BOTTLES PER DC-8 MM 26-4-1. (X)