N13891

Part: WEB — CORRODED (FUSELAGE) · airframe 52,772 hrs · 29,173 cycles

INSPECTION FOUND CUSP WEB CORRODED AT STA 195, LBL 22-LBL 44. THE CORRODED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 1 AND 51-30-2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,772 hrs · 29,173 cycles

INSPECTION FOUND A 1 INCH CRACK IN WEB SKIN JUST FORWARD OF TRIM AT TAIL COMPARTMENT STA 1485, RT SIDE. THE AFT ACCESSORY VENT RT BOX WAS REMOVED IAW SRM 51-30-1. THE REPAIR DOUBLER WAS REMOVED AND A NEW REPAIR DOUBLER WAS INSTALLED IAW SRM 51-30-2, 53-01, FIGURE 4. THE AFT ACCESSORY VENT RT BOX WAS REINSTALLED IAW SRM 51-30-1.

Part: BEAM — CORRODED (LT LAVATORY) · airframe 52,772 hrs · 29,173 cycles

INSPECTION FOUND LEFT LAV I/B FORWARD AFT BEAM ON FLOOR BENT AND CORRODED AT FORWARD END. THE LAV BEAM WAS REMOVED AND A NEW BEAM WAS INSTALLED IAW 51-10-2, 51-10-3, AND 51-30-1.

Part: SKIN — DENTED (FUSELAGE) · airframe 52,772 hrs · 29,173 cycles

INSPECTION FOUND THE LEFT FUSELAGE SKIN DENTED AT STA 389 - 436, LONGERON 22L. REPAIRED IAW ECRA 5331-01082 AND EA 9-5331-2-A0754.

Part: WEB — TORN (FUSELAGE) · airframe 52,771 hrs · 29,173 cycles

CUSP WEB TORN FS 214 AT RBL 10 TO RBL 14. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-30-8.

Part: SKIN — DENTED (FUSELAGE) · airframe 52,771 hrs · 29,173 cycles

LEFT EXTERIOR SKIN DENTED AT STA 200 BETWEEN LONG 22L AND 23L. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-04 AND 51-10-4.

Part: SKIN — DENTED (FUSELAGE) · airframe 52,771 hrs · 29,173 cycles

EXTERIOR SKIN DENTED AT STATION 265 AT LONGERON 20R. REWORKED DENT. FABRICATED AND INSTALLED DOUBLER PER SRM 53-04 FIG 38 AND 51-30-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,771 hrs · 29,173 cycles

FLOOR SUPPORT CORRODED AT STATION 256 CENTER. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-5 AND 53-14-2 FIG 4 SHEET 1.

Part: SKIN — DENTED (AFT CARGO DOOR) · airframe 52,771 hrs · 29,173 cycles

AFT CARGO DOOR SKIN CENTER AFT IS DENTED. REMOVED DAMAGED AREA. REPAIRED SKIN PER SRM 51-50-1 FIG 1 AND 52-05 FIG 3.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 52,771 hrs · 29,173 cycles

MID PIT RT AFT TRACK SECTION FORWARD END OUTBOARD EDGE CORRODED. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED NEW SECTION OF TRACK PER SRM 51-10-3, 53-01, 51-10-4, 51-30-1, AND 51-30-2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 52,771 hrs · 29,173 cycles

TAIL COMPARTMENT STA 1446 LONG 6R IS CRACKED 1 INCH. REMOVED CRACKED LONGERON. FABRICATED AND INSTALLED NEW LONGERON PER SRM 53-02, 51-10-4 AND 51-10-3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,771 hrs · 29,173 cycles

RIGHT INBOARD SEAT TRACK CORRODED AT STATION 200 TO 266. REMOVED AND REPLACED SEAT TRACK SECTION PER SRM 51-30-1, 51-30-2, 51-30-5, 53-05 FIG 4F AND 51-10-4.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,771 hrs · 29,173 cycles

STA 200 RBL 10 - RBL 46 FLOOR SUPPORT HAS ELONGATED HOLES AND CORROSION. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,771 hrs · 29,173 cycles

STA 200 LBL 12 FLOOR SUPPORT IS CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 1-30-5.

Part: WEB — CORRODED (CABIN) · airframe 52,772 hrs · 29,173 cycles

INSPECTION FOUND CUSP WEB CORRODED AT FS 1076 - 1086, RBL 58. THE FASTENERS AND FRAME FITTINGS WERE REMOVED FROM AROUND THE CORRODED AREA AND THE CORRODED AREA WAS CUT OUT. A REPAIR WEB AND FRAME FITTING WERE INSTALLED IAW SRM 51-30-2, 53-14-3, 51-10-3, AND 53-01, FIGURE 4.

Part: WEB — PUNCTURED (CABIN) · airframe 52,772 hrs · 29,173 cycles

INSPECTION FOUND SUB FLOOR PUNCTURED AT FS 170, RBL 15.5, 21, 26, 36, AND 41. THE PUNCTURED AREAS WERE CUT OUT IAW SRM 53-01, FIGURE 1. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-14-1, FIGURE 4, 51-30-4, 51-10-3, AND 51-30-2.

Part: WEB — CRACKED (CABIN) · airframe 52,772 hrs · 29,173 cycles

INSPECTION FOUND A 5 INCH CRACK IN CUSP WEB AT FS 886, LBL 50. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FIGURE 2. A DOUBLER WAS INSTALLED IAW SRM 53-01, 51-10-4, AND 51-20-0.

Part: STRUCTURE — DENTED (CABIN) · airframe 52,771 hrs · 29,173 cycles

UPPER AFT EMERGENCY WALKWAY DENTED AT AFT SECTION AFT OF EXIT PAINT. CUT OUT DAMAGED SECTION PER SRM 53-01 FIG 2. VERIFIED NO CRACKS PAST CUTOUT AREA. FABRICATED AND INSTALLED DOUBLER PER SRM 53-01 FIG 2.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,773 hrs · 29,173 cycles

INSPECTION FOUND AFT VENTRAL DOOR THRESHOLD AREA UNDER FLOOR L-CHANNEL CORRODED AT FS 1338. SUPPORT ANGLES WERE REMOVED AND REPLACED IAW SRM 51-10-4 AND EA 9-5320-2-A0765.

Part: SKIN — GOUGED (NR 5 SLAT) · airframe 52,772 hrs · 29,173 cycles

INSPECTION FOUND LT WING NR 5 SLAT LOWER SKIN GOUGED AT I/B END. A DOUBLER WAS INSTALLED IAW SRM 57-03, FIGURE 4, 51-10-3, AND 51-30-8.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,772 hrs · 29,173 cycles

INSPECTION FOUND LT LAV FLOORBEAM BOLT HOLES CORRODED AT FS 1338. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-10-3, 51-30-05, 51-30-02, AND EA 9-5321-2-A0762.

Part: STOP — CRACKED (CARGO DOOR) · airframe 52,772 hrs · 29,173 cycles

INSPECTION FOUND A 2 INCH CRACK IN BOTH THE AFT AND FWD LOWER DOOR STOPS ON FWD CARGO DOOR. THE CRACKS WERE STOP DRILLED IAW SRM 52-03. DOUBLERS WERE INSTALLED AT EACH LOCATION IAW SRM 51-10-4, 51-10-3, 51-30-2, 51-30-7, 52-03, FIGURE 8, AND ECRA 5230-01554.

Part: WEB — CRACKED (CABIN SUBFLOOR) · airframe 52,772 hrs · 29,173 cycles

INSPECTION FOUND THREE .5 INCH CRACKS IN SUBFLOOR BETWEEN FS 150 AND 168, LBL 22. THE CRACKED AREA WAS REMOVED IAW SRM 53-01, FIGURE 1. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-4, 51-10-3, AND 51-30-0.

Part: SUPPORT BRACKET — CHAFED (FUSELAGE) · airframe 52,771 hrs · 29,173 cycles

FORWARD FUSELAGE STATION 37 RIGHT HAND PAN SUPPORT HAS DEEP CHAFE. REMOVED AND REPLACED SUPPORT, FABRICATED AND INSTALLED DOUBLER PER SRM 53-01 FIG 1, 51-30-2, 53-02-2 FIG 2 AND 51-10-4.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 52,772 hrs · 29,173 cycles

INSPECTION FOUND LT FUSELAGE EXTERIOR SKIN CREASED AT STA 218 BETWEEN LONGERON 18L AND 19L. THE CREASED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 25. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 51-10-3, 51-30, 51-30-5, AND 53-04, FIGURE 25.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,772 hrs · 29,173 cycles

INSPECTION FOUND A 6 INCH CRACK IN CUSP WEB AT FS 886, RBL 44 - 45. THE CRACKED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2A, 51-10-3, AND 51-30-2.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 52,771 hrs · 29,173 cycles

RT HAND OUTBOARD SEAT TRACKS STA 1125 - 1200 IS CORRODED OUT OF LIMITS. REMOVED SECTION OF SEAT TRACK FROM STA 1125 - 1230 IAW SRM 53-05 FIG 4, RECEIVED SEAT TRACK ON TRAVELLER T9021, DRILLED AND LOCATED IAW SRM 51-10-4, TREATED AND PRIMED SEAT TRACK AND SPLICE IAW SRM 51-10-3, INSTALLED SEAT TRACK AND SPLICE IAW SRM 53-05 FIG 4.

Part: WEB — PUNCTURED (FUSELAGE) · airframe 52,771 hrs · 29,173 cycles

SUB FLOOR PUNCTURED APPROX FS 170 - RBL 10. CUT OUT DAMAGED AREA IAW SRM 53-01 FIG 1. FABRICATED DOUBLER IAW SRM 53-14-1 FIG 4. LOCATED AND DRILLED IAW SRM 51-30-4. TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED IAW SRM 51-30-2.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,771 hrs · 29,173 cycles

RIGHT HAND CUSP WEB FS 245 AT RBL 44 CRACKED (.5 INCH) AND PUNCTURED. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 2, 51-10-3, AND 51-30-2.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,771 hrs · 29,173 cycles

RT SIDE CUSP WEB FS 245 APPROX RBL 44 CRACKED AND PUNCTURED. CUT OUT PUNCTURED PER SRM 53-01 FIG 2, FABBED REPAIR DOUBLER PER SRM 53-01 FIG 2, TREATED AND PRIMED PER SRM 51-10-3, INSTALLED PER SRM 51-30-2.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 52,771 hrs · 29,173 cycles

FLOORBEAM CORRODED AT STA 218 LBL 10 - RBL 10. REMOVED AND REPLACED FLOORBEAM PER SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 52,771 hrs · 29,173 cycles

FLOORBEAM ELONGATED HOLES AND CORROSION AT STA 160 LBL 5 - RBL 5. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED BEAM PER SRM 51-30-5, 51-10-4, AND 51-10-3.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 52,771 hrs · 29,173 cycles

FLOORBEAM CORRODED AT FORWARD ENTRY STA 168 RBL 9 - RBL 43. REPLACED FLOORBEAM PER SRM 51-10-04, 51-30-03, 51-30-2, AND 51-30-5.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 52,771 hrs · 29,173 cycles

STA 160 - 195 LBL 44 FLOOR SUPPORT IS CORRODED AND HAS ELONGATED HOLES FWD ENTRY. REMOVED FLOOR IAW SRM 51-30-2, FLOOR SUPPORT, FABBED ON TRAVELLER T-8979, DRILLED FLOOR SUPPORT IAW SRM 51-10-4, TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED FLOOR SUPPORT IAW SRM 51-30-5.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 52,771 hrs · 29,173 cycles

STA 218 LBL 10 - RBL 10 FLOORBEAM OUT OF LIMITS FWD ENTRY. REMOVED FLOOR SUPPORT IAW SRM 51-30-2, RECEIVED NEW FLOORBEAM ON T9010, LOCATED AND DRLLED IAW SRM 51-10-4, TREATED AND PRIMED IAW SRM 51-10-3, INSTALLED FLOORBEAM IAW SRM 51-30-5.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 52,771 hrs · 29,173 cycles

STA 160 - 195 LBL 54 FLOOR SUPPORT IN FWD ENTRY IS CORRODED BEYOND LIMITS. REMOVED FLOOR SUPPORT ON TRAVELLER T8983, FOUND CORROSION ON SUB FLOOR. REMOVED CORROSION IAW SRM 51-0-3, SUB FLOOR OUT OF LIMITS. SEE ATTACHED 44.0008 MAT ID 7075-T6.020/BATCH 00001943.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,771 hrs · 29,173 cycles

CUSP WEB HEAVILY CORRODED AT FS 224 APPROX LBL 58. FABRICATED CUSP WEB AT FAB SHOP ON TRAVELLER T9073. TREATED AND PRIMED IAW SRM 51-10-3, LOCATED AND TRIMMED AND DRILLED IAW SRM 51-10-4, TO BE INSTALLED ON NR 6215847 ZONE 020 SEQ 0047.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 52,771 hrs · 29,173 cycles

STA 148 - 200 RBL 7 FLOOR SUPPORT CORRODED OUT OF LIMITS FWD ENTRY. REMOVED FLOOR SUPPORT IAW SRM 51-10-2, RECEIVED NEW PART ON TRAVELLER T9013, LOCATE AND DRILL HOLES IAW SRM 51-10-4, INSTALLED FLOOR SUPPORT IAW SRM 51-30-1.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 52,771 hrs · 29,173 cycles

STA 148 - 200 RBL 54 FLOOR SUPPORT CORRODED BEYOND LIMITS (FWD ENTRY). REMOVED FLOOR SUPPORT IAW SRM 51-10-2, RECEIVED NEW FLOOR SUPPORT TRAVELLER T9012, TREATED AND PRIMED IAW SRM 51-10-3, DRILLED FLOOR SUPPORT IAW SRM 51-10-4, INSTALLED SUPPORT IAW SRM 51-30-1.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,771 hrs · 29,173 cycles

CUSP WEB HEAVILY CORRODED AT FS 224 APPROX LBL 58. FABRICATED CUSP WEB AT FAB SHOP ON TRAVELLER T9073, TREATED AND PRIMED IAW SRM 51-10-3, LOCATED, TRIMMED AND DRILLED IAW SRM 51-10-4, TO BE INSTALLED ON NR 6215847 ZONE 020 SEQ 0047.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 52,771 hrs · 29,173 cycles

FLOOR SUPPORT CORRODED IN FORWARD ENTRY AREA STA 160 - 195 LBL 54. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-2, AND 51-10-03.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 52,771 hrs · 29,173 cycles

STA 160 - 200 RBL 44 FLOOR SUPPORT OUT OF LIMITS FWD ENTRY. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-5, RECEIVED FLOOR SUPPORT FROM TRAVELER T9018, LOCATED AND DRILLED SUPPORT IAW SRM 51-10-04.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 52,771 hrs · 29,173 cycles

STA 168 LBL 16-BLL 38 FLOORBEAM HAS CORROSION FWD ENTRY. REMOVED FLOORBEAM IAW SRM 51-30-2, SENT TO FAB SHOP FOR NEW FLOORBEAM, TREATED AND PRIMED IAW SRM 51-10-3, LOCATED AND DRILLED FLOOR SUPPORT IAW SRM 51-10-3, LOCATED AND DRILLED FLOOR SUPPORT IAW SRM 51-10-4, INSTALLED IAW SRM 51-30-2 TRAVELLER T8978.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,771 hrs · 29,173 cycles

STA 148 - 200 LBL 7 FLOOR SUPPORT IS CORRODED BEYOND LIMITS FWD ENTRY. REMOVED FLOOR SUPPORT AND ROUTED TO FAB (REMOVAL PER SRM 51-30-2) RECEIVED FROM FAB-FABBED PER SAMPLE ON TRAVELLER T-8977, INSTALLED SUPPORT IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 52,771 hrs · 29,173 cycles

STA 200 LBL 5- FLOORBEAM IS CORRODED OUT OF LIMITS FWD ENTRY. REMOVED BEAM FOUND TO BE OUT OF LIMITS, FAB NEW BEAM ON T8981, TREATED AND PRIMED IAW SRM 51-10-3, DRILLED AND INSTALLED IAW SRM 551-30-2.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 52,771 hrs · 29,173 cycles

STA 195 - 200 LBL 17 FLOOR SUPPORT IS CORRODED OUT OF LIMIT (FWD ENTRY). REMOVED FLOOR SUPPORT IAW SRM 51-30-2, ROUTED TO FAB SHOP, RECEIVED NEW FLOOR SUPPORT ON TRAVELLER T8982, FINISHED FAB PER SAMPLE PER TRAVELLER T8982, INSTALLED IAW SRM 51-30-2.

Part: SKIN — GOUGED (AILERON) · airframe 52,771 hrs · 29,173 cycles

RT AILERON LWR SURFACE SKIN IS GOUGED AT L/E APPROX 18 INCHES O/B OF DAMPERS. REMOVED AILERON IAW MD-80 MM 27-10-01. REPAIRED AILERON IAW MD-80 SRM 57-01 FIG 5 SHEET 2, PERFORMED WEIGHT AND BALANCE IAW SRM 57-50-01, WEIGHT AND BALANCE IS WITHIN LIMITS. INSTALLED AILERON IAW MD-80 MM 27-10-01, AILERON RIG CHECK TO BE ACCOMPLISHED ON CARD 6211005 ZONE 012 SEQ 0080.

Part: SKIN — GOUGED (AILERON) · airframe 52,771 hrs · 29,173 cycles

RIGHT AILERON LOWER SURFACE SKIN IS GOUGED (.5 INCH) AT LEADING EDGE 18 INCHES OUTBOARD OF DAMPERS. REMOVED AILERON IAW MD-80 MM 27-10-01, REPAIRED AILERON IAW MD-80 SRM 57-01 FIG 5 SHEET 2, PERFORMED WEIGHT AND BALANCE IAW SRM 57-50-01, WEIGHT AND BALANCE IS WITHIN LIMITS. INSTALLED AILERON IAW MD-80 MM 27-10-01, AILERON RIG CHECK TO BE ACCOMPLISHED ON CARD 6211005 ZONE 012 SEQ 0080.

Part: OIL SYST — OVERSERVICED (APU)

A MODERATE AMOUNT OF SMOKE APPEARED IN THE COCKPIT AND CABIN AFTER TAKEOFF FROM EWR WITH THE PNEUMATIC PRESSURE GAUGE READING 70 PSI. THE SMOKE SLOWLY DISSIPATED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED BOTH ENGINE SADDLE STRAPS WITH NO DEFECTS NOTED. THE APU WAS FOUND OVERSERVICED WITH OIL. THE OIL WAS DRAINED AND THE APU OIL WAS RESERVICED. BOTH COALESCER BAGS WERE REMOVED AND REPLACED. BOTH ACM'S WERE INSPECTED AND FOUND PROPERLY SERVICED WITH NO LEAKS NOTED. A HIGH POWER ENGINE RUN WAS PERFORMED FOR 10 MINUTES WITH NO SMOKE OR ODOR NOTED.

Part: POWER SUPPLY — INOPERATIVE (EMER EXIT)

INSPECTION FOUND THE LT AND RT INTERIOR OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. THE POWER SUPPLY WAS REMOVED AND REPLACED.

Part: VALVE — INOPERATIVE (RIGHT)

WHEN ICE WAS ENCOUNTERED AT 26,000 FEET, THE ENGINE ANTI-ICE AND AIRFOIL ICE PROTECTION SYSTEM WAS ACTIVATED. IMMEDIATELY AFTERWARDS THE L&R AC TEMP HIGH LIGHTS, L&R ICE PROTECTION HIGH LIGHTS, ICE PROTECTION SUPPLY PRESSURE LIGHT AND AIRFOIL PROTECTION LIGHT ILLUMINATED AND SMOKE ENTERED THE COCKPIT. THE EFFECTED SYSTEMS WERE SHUTDOWN IAW WITH CHECKLIST PROCEDURES AND THE SMOKE CLEARED. THE AIRCRAFT WAS RETURNED TO ORD WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT AUGMENTATION VALVE AT FAULT. THE RT AUGMENTATION VALVE WAS REMOVED AND REPLACED IAW MM 36-10-01. BOTH ENGINES WERE RUN AND ALL SYSTEMS CHECKED GOOD.

Part: CLIPS — OUT OF ADJUST (TAIL CONE)

THE PULL FROM CLIPS AT INTERIOR TAIL CONE RELEASE HANDLE WAS HIGH AT 50 POUNDS. THE TAIL CONE HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00.

Part: BULBS — INOPERATIVE (LANDING GEAR)

THE LT MLG DOWN AND LOCKED GREEN LIGHTS DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED ON APPROACH TO PBI. THE BULBS WERE CHANGED DURING A GO AROUND AND THE GREEN LIGHTS ILLUMINATED NORMALLY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED THE LANDING GEAR INDICATION SYSTEM AND ALL CHECKED NORMAL.

Part: BOLT — SHEARED (LT MLG ACTUATOR)

THE AIRCRAFT HAD A BRIEF HISTORY OF THE LT MLG RED LIGHT REMAINING ILLUMINATED AFTER GEAR RETRACTION. MAINTENANCE FOUND LOWER BOLT OF THE LT MAIN GEAR ACTUATOR LOWER MOUNT POINT SHEARED. THE BOLT WAS REMOVED AND REPLACED, A GEAR RETRACTION WAS PERFORMED IAW MM 32-10-00 AND OPERATION AND INDICATIONS CHECKED GOOD.

Part: PROX SW CONTL — INOPERATIVE (NLG)

THE NOSE GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION WITH THE GEAR HANDLE IN THE UP POSITION. THE CHECKLIST WAS RUN AND THE LIGHT BLINKED OFF AND ON INTERMITTENTLY. THE LIGHT EXTINGUISHED AND REMAINED OUT AFTER ABOUT TEN MINUTES. THE FLIGHT WAS CONTINUED TO EWR WHERE IT LANDED WITHOUT FURTHER PROBLEM. THE PROXIMITY SWITCH CONTROL WAS REMOVED AND REPLACED. INDICATIONS AND OPERATIONAL CHECKS WERE GOOD.

Part: CLIPS — OUT OF ADJUST (TAILCONE)

MORE THAN 30 POUNDS OF FORCE WAS REQUIRED TO PULL THE INTERIOR TAILCONE RELEASE HANDLE FROM CLIPS. THE RETAINING CLIPS WERE ADJUSTED TO SPECIFICATIONS PER MM 53-53-00.

Part: OVEN — FIRE (AFT GALLEY)

SMOKE BEGAN COMING FROM AFT GALLEY OVENS WHILE EN ROUTE. A FIRE EXTINGUISHER WAS USED TO EXTINGUISH OVEN FIRE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AFT GALLEY OVENS AND FOUND PAPER BURNED INSIDE OF OVENS. THE FIRE HAD BEEN CONTAINED TO INSIDE OF OVENS. THE PAPER WAS REMOVED AND OPERATION OF THE OVENS CHECKED GOOD. THE FIRE EXTINGUISHER WAS REMOVED AND REPLACED.

Part: PROX SWITCH — INOPERATIVE (RT MLG)

TPA - FLT 0365 - THE RT MLG RED UNSAFE LIGHT ILLUMINATED INTERMITTENTLY WITH THE GEAR HANDLE IN THE DOWN POSITION WHEN APPROACHING TPA. CYCLING THE GEAR DID NOT HELP. THE GEAR WAS VISUALLY CONFIRMED DOWN AND LOCKED. THE RED LIGHT CAME ON CONTINUOUSLY UPON LANDING, AND WAS ACCOMPANIED BY CAWS LANDING GEAR ANNUNCIATION. THE AIRCRAFT TAXIED TO THE GATE NORMALLY. MAINTENANCE FOUND RT MLG DOWNLOCK PROXIMITY SWITCH AT FAULT. THE PROXIMITY SWITCH WAS REMOVED AND REPLACED. THE PROXIMITY SWITCH TESTED GOOD. (X)