N35836

Part: CLIP — OUT OF ADJ (TAILCONE) · airframe 46,862 hrs · 22,401 cycles

THE TAILCONE EXTERIOR RELEASE HANDLE PULL FROM CLIPS WAS LOW. THE CLIPS WERE ADJUSTED IAW MM 53-53-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,862 hrs · 22,401 cycles

INSPECTION FOUND A CRACK IN TAIL COMPARTMENT CANTED FRAME AT STA 1446, L3R AN L26L. THE CRACKED FRAME CAP WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: FITTING — CRACKED (GRD SPOILER) · airframe 46,862 hrs · 22,401 cycles

INSPECTION FOUND A 2.5" CRACK IN R/H WING GROUND SPOILER ACTUATOR FITTING. A DOUBLER WAS INSTALLED IAW ECRA 5740-01317 AND DRAWING SRO9570010.

Part: FITTING — CRACKED (GRD SPOILER) · airframe 46,862 hrs · 22,401 cycles

INSPECTION FOUND A 2.25" CRACK IN L/H WING LEFT I/B GROUND SPOILER ACTUATOR SUPPORT FITTING. REPAIRED IAW ECRA 5740-01317 AND DRAWING SR09570010.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 46,862 hrs · 22,401 cycles

INSPECTION FOUND MID BAGGAGE BIN LOWER DOOR JAMB CORRODED AROUND H-SHEAR AT STA 636-693. A REPAIR DOUBLER AND SPACER WERE INSTALLED IAW SRM 53-05, FIGURE 63.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 46,862 hrs · 22,401 cycles

INSPECTION FOUND AFT BAGGAGE BIN LOWER DOOR JAMB CORRODED BETWEEN STA 1155-1211. A Z-ANGLE BEAM REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 63.

Part: ACM — LEAKING (LT PACK) · airframe 42,839 hrs · 20,237 cycles

WHEN THROTTLES WERE BROUGHT UP FOR TAKEOFF (DURING TAKEOFF ROLL) A NOXIOUS FOUL ODOR ENTERED THE AIRCRAFT THROUGH THE AIR CONDITIONING PACKS. THE CREW AND PASSENGERS BECAME NAUSEOUS. THE FLIGHT CREW DONNED THEIR O2 MASKS AND THE AIRCRAFT WAS RETURNED TO IAH. MAINTENANCE FOUND THE LT ACM LEAKING OIL INTO THE PNEUMATIC DUCTS. THE LT ACM WAS REMOVED AND REPLACED IAW MM 21-51-01. OPERATIONAL CHECKS WERE GOOD WITH NO LEAKS NOTED. A BURNOUT PROCEDURE WAS PERFORMED IAW MM 21-20-02. THE PACKS WERE OPERATED WITH ENGINES RUNNING AT TAKEOFF POWER AND NO FOUL ODOR WAS NOTED. AN EVALUATION FLIGHT WAS CONDUCTED AND NO ABNORMAL INDICATIONS OR ODORS WERE OBSERVED.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

INSPECTION FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. A NEW POWER SUPPLY AND BATTERY PACK WERE INSTALLED IAW MM 33-53-00, PAGE 407.

Part: FAIRING — GOUGED (NR 4 LE SLAT)

LEFT WING NR 4 SLAT TRACK CAN GOUGED. WELDED CAN PER DRWG 5935801 AND INSTALLED PER MM 27-80-01.

Part: SKIN — GOUGED (BS 1041)

FUSELAGE SKIN IS GOUGED UNDER AFT END OF ADF ANTENNA. BLENDED GOUGE AND INSTALLED REPAIR PER SRM 53-04 FIG 38 VIEW G.

Part: TAIL CONE — OUT OF ADJUST (BS 1510)

TAIL COMPARTMENT INTERIOR TAIL CONE RELEASE HANDLE PULL TOO HIGH (45 LBS). RIGGED TAIL CONE RELEASE MECHANISM PER MM 53-53-00.

Part: BRACKET — CRACKED (LT EMER EXIT DR)

LEFT FORWARD EMERGENCY EXIT DOOR SEAL RETAINER SUPPORT BRACKET CRACKED AT RIVET (.5). REPLACED FORWARD LOWER RETAINER BRACKET PER SRM 51-30-2.

Part: RETAINER — CORRODED (LT EMER EXIT DR)

LEFT FORWARD EMERGENCY EXIT DOOR CORROSION FOUND AT LOWER AFT CORNER SEAL RETAINER. REMOVED AND REPLACED SEAL RETAINER PER SRM 51-30-2.

Part: JAMB — CORRODED (CARGO DOORWAY)

FORWARD CORGO DOOR JAMB PAN LOWER SECTION IS CORRODED. INSTALLED SPLICE REPAIR ON DOOR JAMB PER SRM 53-05 FIG 44.

Part: SEAT TRACK — CORRODED (BS 1136-1174)

SEAT TRACK NR 2 CORROSION AT NUT PLATE HOLES FROM STA 1136 - 1174. REPLACED SEAT TRACK LEFT CENTER STA 1079 - 1305 PER SRM 51-30-01.

Part: DOUBLER — CRACKED (AFT SERV DOOR)

AFT SERVICE DOOR DOUBLER AROUND HOLD OPEN HOOK CRACKED (1) OUTER SKIN. INSTALLED DOUBLER REPAIR PER EC/RA 5205-01008.

Part: SEAT TRACK — CORRODED (BS 1105)

LEFT MOST INBOARD SET TRACK HAS CORROSION AT CENTER CHANNEL STA 1105. REMOVED AND REPLACED SEAT TRACK PER SRM 53-05 FROM STA 1041 - 1309.

Part: SEAT TRACK — CORRODED (BS 200-237)

RIGHT CENTER SEAT TRACK CORRODED STA 200 AND 237. REMOVED AND REPLACED SEAT TRACK STA 200 - 247 PER SRM 51-30-1.

Part: BULKHEAD DOUBLER — CORRODED (BS 1338)

CORROSION AT AFT PRESSURE BULKHEAD AND VERTICAL BULKHEAD INTERSECTION AT STA 1338 FROM L-29LT TO L-29RT. REMOVED CORROSION AND INSTALLED SERVICEABLE JACK PAD DOUBLER PER SRM 51-10-3 AND DRAWING NR PL J936439 AND J936667.

Part: SKIN — HOLE (BS 383)

TEMPORARY REPAIR APPROXIMATELY STA 383 L-29LT WHERE PREVIOUS PHONE ANTENNA INSTALLED. INSTALLED DOUBLERS PER SRM 53-04 FIG 38.

Part: BEAM — CRACKED (FWD SERV DOOR)

HOU - FORWARD SERVICE DOOR NR 4 BEAM IS CRACKED AT FORWARD END 1.5 INCH. INSTALLED NEW BEAM PER SRM 51-30-2 AND 51-30-1. (M)

Part: ANGLE — CRACKED (DORSAL FIN)

HOU - RIGHT INNER ATTACH ANGLE CRACKED 1 INCH, DORSAL FIN. REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-30-2. (M)

Part: BEAM — CRACKED (PAX DOOR)

HOU - MAIN CABIN DOOR NR 1 BEAM IS CRACKED AT BOTH ENDS .625 INCH FORWARD AND 1 INCH AFT. REMOVED AND REPLACED BEAM PER SRM 51-30-0. (M)

Part: ANGLE — CRACKED (DORSAL FIN)

HOU - LEFT INNER ATTACH ANGLE CRACKED 1 INCH, DORSAL FIN. REMOVED AND REPLACED ANGLE PER SRM 51-30-2. (M)

Part: ESCAPE LINE — FRAYED (LT EMER EXIT)

LEFT OVERWING EMERGENCY EXIT ESCAPE LINE IS FRAYED AT ATTACH HOOK. REPLACED ESCAPE LINE PER MM 25-61-00.

Part: ESCAPE LINE — FRAYED (RT EMER EXIT)

RIGHT OVERWING EXIT ESCAPE LINE IS FRAYED AT ATTACH HOOK. REPLACED ESCAPE LINE PER MM 25-61-00.

Part: FUSE — BLOWN (MID PWR SUPP)

INSPECTION FOUND MIDDLE SECTION OF SEAT MOUNTED EMERGENCY PATH LIGHTING INOPERATIVE. MAINTENANCE FOUND MOST OUTBOARD FUSE OF MIDDLE POWER SUPPLY PACK BLOWN. THE FUSE WAS REMOVED AND REPLACED AND OPERATION OF THE LIGHTING WAS RESTORED.

Part: SLIDE — FELL OFF (L1 DOOR)

FORWARD ENTRY DOOR SLIDE FELL OFF DOOR. REINSTALLED SLIDE PACK PER MAINTENANCE MANUAL.

Part: T/R CNTL VALVE — RUPTURED (LT ENGINE)

SFO - FLT 0165 - THE MAIN CABIN BEGAN TO FILL WITH SMOKE DURING TAXI TO TERMINAL AFTER LANDING AT SFO. THE AIRCRAFT WAS STOPPED ON THE TAXIWAY, THE L-1 DOOR AND TAIL CONE EMERGENCY SLIDES WERE DEPLOYED, AND THE PASSENGERS EVACUATED AS A PRECAUTIONARY MEASURE. MAINTENANCE FOUND LT THRUST REVERSER CONTROL VALVE RUPTURED. THIS PERMITTED HYDRAULIC LEAKAGE INTO THE APU AIR INLET RESULTING IN SMOKE. LT THRUST REVERSER CONTROL VALVE REMOVED AND REPLACED, OPERATIONAL AND LEAK CHECKS GOOD. BOTH L-1 DOOR AND TAIL CONE SLIDES REMOVED AND REPLACED AND TAIL CONE RESINSTALLED. ENGINES RUN TO PURGE SYSTEM OF FUMES. THE COALESCER BAGS WERE REPLACED. (X)