N535UA

Part: COVER — LOOSE (CABIN) · airframe 75,726 hrs · 27,643 cycles

EMERGENCY LIGHTING STRIP BY 8BAC - 9ABC IS LOOSE. SECURED EMER PATH LIGHTING CLEAR COVER FROM 8ABC TO 9ABC.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,136 hrs · 27,457 cycles

AFT CARGO COMPARTMENT FRAME CORRODED BS 1480 RBL 27.5. CORROSION ON FRAME BS 1480 RBL 27.5 HAS 100% MATERIAL LOSS. REMOVED, FABRICATED & REPLACED FRAME SECTION IAW SRM 51-40- 02, PARA 4, FIG 8 & PARA 7D, FIG 12.

Part: STRINGER — DAMAGED (FUSELAGE) · corrosion level 5 · airframe 75,136 hrs · 27,457 cycles

BLIND FASTENER ON UPPER EXTERNAL FUSELAGE AT BS 572, STRINGER 6L. R & R BLIND FASTENERS WITH SOLID FASTENER ON UPPER FUSELAGE AT BS 572 STRINGER 6L IAW SRM 53-00-01. REPAIRED DAMAGE STRINGER COMMON TO THE BLIND FASTENER HOLE AT BS 572 STRINGER 6L IAW SRM 53-00-03 REPAIR 1 FIG 201. STRINGER REPAIR AT BS 572 STRINGER 6L IS A CAT A REPAIR ZONE 1 WITH REPEAT INSPECTION. ACCOMPLISHED HFEC OF FASTENER HOLES & 10 EA HOLES COMMON TO REPAIR IAW NDTM 51-00-16, NO DEFECTS NOTED.

Part: SKIN — DENTED (FUSELAGE) · airframe 75,136 hrs · 27,457 cycles

SMALL DENT RT FUSE BS 1625 BELOW STRINGER 18 JUST FWD & BELOW 4 RT. REPAIRED DENT IN FUSELAGE EXTERNAL SKIN BS 1625 BETWEEN STRINGER 18R & STRINGER 19R IAW SRM 53-00-01 FIG 201 REPAIR 2. DENT WAS ON DOUBLER NO ALLOWABLE LIMITS NOTED.

Part: SKIN — DENTED (FUSELAGE) · airframe 75,136 hrs · 27,457 cycles

FUSE SKIN DENT AT STATION 275 JUST BELOW STRINGER 19R. CUT OUT DAMAGE & SKIN THICKNESS IS .045 INCH AREA. INSTALLED REPAIR DOUBLER THICKNESS IS .050 IAW SRM 53-00-01 REPAIR 3 FG 201.

Part: UNKNOWN — UNKNOWN (STALL WARNING) · airframe 74,673 hrs · 27,330 cycles

STALL WARNING TEST, WITH RT AOA SENSOR CB OPEN F31 & FLIGHT OFFICER`S ALT AIR DATA SELECTED, ELEX WARNING STATUS WILL NOT CLEAR & THEREFORE NO STICK SHAKER. SWAPPED STALL WARNING CARDS M938, M615 & TRIED AIR DATA COMPUTER. NO HELP. SUSPECT CAPTAIN`S AOA SENSOR.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 74,563 hrs · 27,299 cycles

FIRST OFFICER`S INSTRUMENT BACKGROUND LIGHTING INOPERATIVE. CYCLED CB N-29, BACKGROUND NOT WORKING.

Part: WARNING SYSTEM — FAULTY (HYDRAULIC SYS) · airframe 74,347 hrs · 27,229 cycles

RT HYD SYS PRESS LIGHT INTERMITTENT WITH HYD PUMPS OFF.

Part: BLADE — NICKED (NR 2 ENGINE) · airframe 73,609 hrs · 26,991 cycles

NR 2 ENG INLET FAN BLADE NICKED. BLENDED FAN BLADE AMM 72-31-02.

Part: APU — SHUTDOWN (APU BAY) · airframe 73,544 hrs · 26,965 cycles

APU SHUTDOWN WITH FAULT LIGHT ILLUMINATED

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 73,191 hrs · 26,849 cycles

EMERGENCY EXIT LIGHT INOPERATIVE ON OUTSIDE OF DOOR 2L. RELAMPED, CHECKED OKAY, IAW MM 33-51-00.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 72,998 hrs · 26,788 cycles

COMPLETE LOSS OF UPFRONT CONTROL. AUTO PILOT & AUTO THROTTLE CUT IN & OUT EVEN ONCE DISENGAGED. ALL LIGHT & CONTROLS ON MCP FLASHING & INCORRECT.

Part: SIGN — DETACHED (CABIN) · airframe 72,897 hrs · 26,750 cycles

OVERWING EXIT SIGN RT SIDE DETACHED. SECURED EXIT SIGN OVER EXIT ROW.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 72,808 hrs · 26,718 cycles

R2 DOOR SLIDE PRESSURE LOW. MAINT TEXT: ABOVE SHOULD READ DOOR 2R EMERGENCY POWER RESERVOIR LOW. (DOOR ASSIST BOTTLE). REPLACED DOOR ASSIST BOTTLE AT MED 2R IAW AMM. INSPECTED DOOR 2R ASSIST BOTTLE IAW AMM.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 72,784 hrs · 26,710 cycles

HYDRAULIC LEAK IN NOSE GEAR AREA. FOUND HYDRAULIC LINE STAINLESS TUBE LEAKING THROUGH THE SIDE OF THE TUBE SUSPECT SMALL CRACK. REMOVED LEAKING HYDRAULIC LINE. INSTALLED LINE AND LEAK CHECKED.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 72,768 hrs · 26,706 cycles

L1 DOOR ASSIST BOTTLE PRESSURE LOW. REPLACED BOTTLE.

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 72,710 hrs · 26,692 cycles

LEFT HYDRAULIC ENGINE PUMP EICAS ON CLIMBOUT WITH LT ENGINE PUMP PRESSURE LIGHT ALSO ON. REPLACED LEFT ENGINE DRIVEN PUMP, OPS AND LEAK CHECKED OKAY.

Part: FLOORBEAM — DAMAGED (BS 1681) · airframe 72,480 hrs · 26,621 cycles

UNABLE TO MAINTAIN EDGE MARGIN ON LOWER FLANGE OF FLOORBEAM AT BS 1681, RBL 45.5 AND LBL 45.5. REPAIRED FLOORBEAM LOWER FLANGE IAW EA 130728IR AND UAL ECRA 5360-01327. CAT "A" PERMANENT REPAIR. MAJOR REPAIR

Part: FLOOR SUPPORT — CORRODED (BS 1681-1701) · corrosion level 2 · airframe 72,480 hrs · 26,621 cycles

FLOOR SUPPORT BS 1681-1701, RBL 51, HAS CORROSION AROUND FASTENER HOLE. REPLACED FLOOR SUPPORT IAW ECRA 5360-01326 AND EA 130738.

Part: SKIN — WORN (LT WING TE FLAP) · airframe 72,480 hrs · 26,621 cycles

LEFT WING INBD FLAP UPPER MID SURFACE OTBD DEPTH WEAR LINE IN PREVIOUS REPAIR. REPAIRED IAW REO G12307, REV C & D .

Part: SPAR — GOUGED (RUDDER) · airframe 72,480 hrs · 26,621 cycles

RUDDER HINGE (FITTING ON FRONT RUDDER SPAR) IS GOUGED. BLENDED GOUGES IAW ECRA 5530-01705 AND EA 130685. ACCOMPLISHED HFEC IAW NTM 51-00-19, PT 6, NO DEFECTS NOTED.

Part: SKIN — DENTED (BS 327 S2R) · airframe 72,480 hrs · 26,621 cycles

EXTERNAL FUSELAGE SKIN CROWN BS 327, RBL 10, S2R DENTED. FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE AND INSTALLED DOUBLER.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 72,480 hrs · 26,621 cycles

BS 1640, RBL 58 FLOORBEAM UPPER FLANGE FWD END CRACKED AND HAS CORROSION ON UPPER AND LOWER SURFACE. BLENDED CORROSION, WAS OUT OF LIMITS, REPAIR.

Part: SKIN — DENTED (BS 575) · airframe 72,480 hrs · 26,621 cycles

LOWER EXTERNAL FUSELAGE SKIN 8 INCHES BELOW FWD CARGO DOOR CUT OUT BS 575 S26-27R DENTED. FOUND IT TO BE OUT OF LIMITS. REPAIRED IAW ECRA 5330-04 635.

Part: SKIN — DAMAGED (BS 1680 S30) · airframe 72,480 hrs · 26,621 cycles

DENT BS 1680, BETWEEN S29L & 29R IAW SRM 53-00-01 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01. REPAIRED IAW SRM 53-00-01, REP B.

Part: WEB — FAULTY (STA 1681-1720 LB) · airframe 72,480 hrs · 26,621 cycles

SHEAR WEB, BS 1681-1720, LBL 55 - RBL 55 DAMAGED. REPLACED SHEAR WEB IAW ECRA 5360-01317 AND EA 130684. MAJOR REPAIR.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 72,480 hrs · 26,621 cycles

RIGHT WING INBD MAIN FLAP, OTBD UPPER SKIN HAS CHAFING DAMAGE 18 INCHES AFT OF LE, 0-10 INCHES INBD OF OTBD END OF FLAP. ACOMPLISHED NDT OF DAMAGED AREA IAW NTM PT 4, 51- 00-10 AND HFEC IAW NTM PT 6, 51-00-19, NO DEFECTS NOTED. BLENDED AREA, FABRICATED AND INSTALLED BONDED DOUBLER IAW ECRA 5750-04564 AND EA130712.

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 72,480 hrs · 26,621 cycles

WHILE WORKING BS 1681, FLOORBEAM, CORROSION WAS FOUND AT BS RBL 45 AND 55 UNDER FWD SIDE OF BEAM UPPER FLANGE. CORROSION IS 100 PERCENT MATERIAL LOSS. REMOVED PART IAW SRM 51-40-02. FAB NEW PART REF WO27297-2400-0199 FROM BAC 1518-347-7075-T65U AND ANODIZED IAW DWG 146N5111. PRIMED & PAINTED IAW SRM 51-20-01 AND AMM 51-20-10. INSTALLED NEW PART AT BS 1681 LBL IAW SRM 51-40-02 AND DWG 146N5111. ID'D PART IAW GMM 01-01-1-07. REPAIR ACCOMPLISHED IAW SRM 51-40-02, SRM 51-40-05, DWG 146N5111, SRM 51-20-01, AMM 51-21 -10, AMM 51-24-03 AND GMM 1-0-1-07. REF IND N-R CARD 1930785.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 72,480 hrs · 26,621 cycles

MAIN CABIN STA 324, RBL 42 FLOORBEAM UPPER SURFACE HAS AREAS OF CORROSION. MAJOR REPAIR ACCOMPLISHED: REMOVED FLOORBEAM UPPER FLANGE CORROSION, FOUND OUT OF LIMITS. INSTALLED FLOORBEAM UPPER CHORD SPLICE REPAIR AND PARTIAL UPPER CHORD REPLACEMENT AT STA 324 IAW SRM 53-10-8, REPAIR 1. CAT B REPAIR.

Part: SKIN — DENTED (STA 1700+10) · airframe 72,480 hrs · 26,621 cycles

LT EXTERIOR SKIN STA 1700+10, 3" BELOW STR 25L DENTED. EVALUATED AND FOUND THAT THE DAMAGE REQUIRES REPAIR . CUT OUT DENT AND REPAIRED IAW ECRA 5360-01316. SKIN HAS BEEN REPAIRED AT BS 1710 JUST ABOVE S-26 IAW ECRA 5360-01316 TO STAGE 1 & 2 STANDARDS. A NEW FAA FORM 8100-9 MUST BE RECEIVED AND THE INSPECTION ACCOMPLISHED NOT LATER THAN 23,379 CYCLES (PTC 50,000) REPAIRED IAW ECRA 5360-01316 TO STAGE 1 & 2 STANDARDS. AN FAA FORM 8100-9 MUST BE RECEIVED AND THE INSPECTION ACCOMPLISHED COT LATER THAN 23,379 CYCLES (PTC 50,000). MF2918 CREATED TO MONITOR.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 72,480 hrs · 26,621 cycles

FWD CABIN FLOORBEAM AT BS 365 FROM BL 0 TO RBL 56 CORRODED. REPAIRED FLOORBEAM LBL 12 TO RBL 65 IAW ECRA 5310-05536. HFEC CUTOUT & FASTENER HOLES, NO DEFECT NOTED. REPAIR IS STRUCTURALLY ACCEPTABLE AS CAT A REPAIR AS DEFINED IN SRM 51-00-06. MAJOR REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 72,480 hrs · 26,621 cycles

UPON F/O WALKAROUND FOUND DENT IN FUSELAGE FWD RT SIDE APPROX 4 FT AFT OF NOSE NR. DENT IS SMOOTH AND CRACK FREE, WITHIN LIMITS IAW SRM. OK AS IS. INSTALLED YELLOW DOT. DUPLICATE DEFECT REF CF9052. DENT MARKED IAW GMM06-35-05 AND ECRA 2060-01042 ON CF9052.

Part: FRAME — DENTED (BS 600 S24L) · airframe 56,432 hrs · 20,636 cycles

FWD CARGO BAY BS 600 AT S24L, FRAME INBOARD FLANGE DENTED. CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR IAW SRM 53-00-07 REPAIR 5. MAJOR REPAIR.

Part: FRAME — DENTED (BS 620 S24-25L) · airframe 56,432 hrs · 20,636 cycles

FORWARD CARGO BAY BS 620 STRINGERS 24-25L, FRAME INBOARD FLANGE DENTED. REMOVED DAMAGED SECTION OF FRAME AND FABRICATED A REPAIR ANGLE, STRINGER CLIP AND SHEAR TIE. MAJOR REPAIR.

Part: FRAME — DENTED (BS 580 S23-24L) · airframe 56,432 hrs · 20,636 cycles

FORWARD CARGO BAY AT BS 580 BETWEEN STRINGERS 23 & 24L, FRAME INBOARD FLANGE DENTED. CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR. PER SRM 53-00-07 REPAIR 5. MAJOR REPAIR.

Part: FRAME — DENTED (BS 1560 S26R) · airframe 56,432 hrs · 20,636 cycles

AFT CARGO BAY FRAME INBOARD FLANGE AT BS 1560 AND S26R DENTED. CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR IAW SRM 53-00-07 REPAIR 5. MAJOR REPAIR.

Part: FRAME — DENTED (BS 1500 S26L) · airframe 56,432 hrs · 20,636 cycles

AFT CARGO FRAME INBOARD FLANGE IS DENTED AT BS 1500 AND S26L. CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR IAW SRM 53-00-07 REPAIR 5. MAJOR REPAIR.

Part: SMOKE GOGGLES — FAULTY (CAPTAIN'S) · airframe 71,916 hrs · 26,434 cycles

CAPTAIN'S SMOKE GOGGLES ELASTIC HEADBAND STRETCHED OUT, DOES NOT PROVIDE SNUG FIT. REPLACED SMOKE GOGGLES.

Part: ENGINE — FAULTY (NR 1) · airframe 71,891 hrs · 26,423 cycles

NR 1 ENGINE PROBLEM, RETURNED TO FIELD.

Part: FLAPPER VALVE — BROKEN (WASTE DISPOSAL) · airframe 71,696 hrs · 26,355 cycles

AFT LAV DUMP VALVE FLAPPER ON WASTE DRAIN IS BROKEN OFF. REMOVE ALL BOLTS OUTSIDE HOLDING LAV DOOR FLAPPER. NEEDS REPLACEMENT OF FLAPPER ASSY PARTS ON TOOL CART IN BACK OF PLANE. REMOVED VALVE PER AMM. VALVE NEEDS TO BE INSTALLED AFTER HEATER GASKET HAS BEEN REPLACED. REPLACED FLAPPER VALVE ASSY.

Part: ENGINE — OIL CONSUMPTION (NR 2) · airframe 71,496 hrs · 26,291 cycles

EXCESSIVE OIL CONSUMPTION FOR THE NR 2 ENGINE . REPLACED THE FUEL COOLED OIL COOLER IAW AMM AND THE FCOC BYPASS VALVE IAW AMM. REMOVED AND REPLACED FUEL OIL HEAT EXCHANGER AND BYPASS VALVE.

Part: UNKNOWN — ODOR (CABIN) · airframe 71,292 hrs · 26,216 cycles

CREW REPORTED TO MM THAT UNDER TOW ODOR IN CABIN ELECTRICAL-BURNING PLASTIC. ACCOMPLISHED CHECKS PER MM 05-51-56, CHECKED ALL C/B PANELS, RECIRC FANS, GALLEY OVENS, COFFEEMAKERS, HOTPLATES, CHILLERS, EQP COOLING FANS, RAN PACKS HIGH HEAT, CHECKED WINDOWS AFTER WINDOW HEAT IS ON NO ARCING NOTED, CHECKED CABIN LIGHTS NO DEFECTS NOTED.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 71,090 hrs · 26,153 cycles

BURNED PLASTIC SMELL IS EMANATING FROM FORWARD GALLEY OVENS. REMOVED BURNT PLASTIC MATERIAL FROM OVEN, RAN OVEN 12 MINS, OPS CHECK NORMAL.

Part: FAN — FAULTY (CABIN) · airframe 70,990 hrs · 26,117 cycles

DUE TO SMOKE IN THE CABIN NEED TO REPLACE BOTH RECIRCULATION FILTERS. REMOVED AND REPLACED RECIRCULATION FANS- MR21560 AND MR21759. OPERATION OK AND NO AIR LEAKAGE. REPLACED BOTH FILTERS PER AMM.

Part: PLUG — LEAKING (CABIN) · airframe 70,813 hrs · 26,043 cycles

FROM EXIT ROW BACK, MINIMAL AIRFLOW. UNUSED GASPER AIR DUCT PLUGS IN MAIN OVERHEAD DISTRIBUTION DUCT AT ROW 35 LEAKING. RE-SECURED PLUGS & OPS CHECK LEAK CHECK OKAY.

Part: NUT — LOOSE (CABIN SEAT) · airframe 70,602 hrs · 25,971 cycles

21DEF SEATS LOOSE IN TRACK. REMOVED AND REPLACED FWD ANTI-RATTLING LOCKING NUT REF IPC 25-25-13A-001M ITEM 120 AND AMM. SEAT ROW 21R, SEAT ASSY SECURED. ACCOMPLISHED INSPECTION AND REINSTALLATION OF SEAT ROW ASSY 21 RT SIDE PER MM, SEAT SECURED.

Part: MODULE — FAILED (STALL WARNING) · airframe 70,395 hrs · 25,906 cycles

STALL WARNING OPERATIONAL CHECK, FAILS STEP B.(17). WITH R AIR DATA AOA SENSOR C-B (11F31) PULLED AND F/O'S ALT INST SELECTED, 'WARN ELEX' MESSAGE STAYS ON EICAS & R STALL WARNING WILL NOT TEST. REPLACED STALL WARNING MODULE M938 AND CHECKED OKAY.

Part: LATCH — FAULTY (FUEL PANEL) · airframe 69,451 hrs · 25,595 cycles

CENTER PUMPS INDICATE ON W- ALL PUMPS ON WHILE ON GROUND. FOUND FUEL PANEL FALSE LATCHED. CYCLED FUEL DOOR. OP'S CHECK NORMAL.

Part: BLADE — DAMAGED (NR 2 FAN) · airframe 67,953 hrs · 25,050 cycles

ON WALKAROUND, FOUND BLADE DAMAGEED ON ENGINE NR 2. REPAIRED NR 2 ENGINE FAN BLADE PER AMM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,340 hrs · 24,815 cycles

EXIT LIGHT ON CEILING AT ROW 20 INOPERATIVE. REPLACED POWER SUPPLY M10699, GROUND CHECKED GOOD.

Part: LENS — MISSING (R4 DOOR SLIDE) · airframe 67,302 hrs · 24,800 cycles

SLIDE LIGHT MISSING FROM DOOR 4R. REPLACED MISSING SLIDE ARMED LENS CAP TO DOOR 4R.

Part: BOLT — UNSECURE (ENGINE MOUNT) · airframe 67,079 hrs · 24,708 cycles

FOUND AFT INBD BOLT ON ENG AFT MOUNT NOT SEATED. REPLACED ALL AFT MOUNT BOLTS AND AFT MOUNT ON SMB W-US Q0508E & Y1556H.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 66,941 hrs · 24,661 cycles

ONE DOOR ASSIST BOTTLE READING ZERO AT DOORS 1L. REPLACED 1L EMP PER MM.

Part: CIRCUIT CARD — MALFUNCTIONED (FIRE DETECTION) · airframe 66,856 hrs · 24,631 cycles

NO BOTTLE DISCHARGE LIGHTS ON FIRE TEST. REPLACED CARGO DETECTION PANEL AND CARGO DETECTION CARD. OPS CHECKED OK. OK FOR SERVICE.

Part: HEAT EXCHANGER — MALFUNCTIONED (A/C PACK) · airframe 66,847 hrs · 24,628 cycles

RIGHT PACK PUTTING OUT 90 DEGREE AIR. REPLACED RT PACK LOW LEVEL CTR L VALVE, NO HELP. RT PACK OUT TEMP STILL AT 81 DEGREES. LEFT PACK 34 DEGREES. REPLACED HEAT EXCHANGERS PER MM AND CONDENSER.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 66,665 hrs · 24,563 cycles

NR 1 PYLON SUPPORT FOR FINGER SEAL WEAR ANGLE HAS CRACKS AT FASTENER HOLES ON BOTTOM OF PYLON. REMOVED FINGER SEAL ANGLE. PICK UP HOLES IN NEW ANGLE. STARTED TO INSTALL UPPER AFT ANGLE, LOWER SUPPORT WEB IN WORK AREA. COMPLETED INSTALLATION

Part: PACKING — LEAKING (FLAP DRIVE) · airframe 66,665 hrs · 24,563 cycles

LT WHEEL WELL, SEVERAL AREAS FWD AND OVER DOOR HINGE HAVE HYDRAULIC FLUID PUDDLING FROM LEAKS. FOUND TRAILING EDGE FLAP POWER DRIVE UNIT CONTROL VALVE MODULE LEAKING. SUSPECT IT NEEDS PACKING. RPL PACKINGS ON UNIONS OF 3 PRESS TUBES ON FLAP POWER DRIVE UNIT CONTROL VALVE, NEEDS LEAK CK. CYCLD FLAPS THRU FULL TRAVEL WITH NO LEAKS NOTED.

Part: SUPPORT — WORN (NR 1 NAC FIRWALL) · airframe 66,665 hrs · 24,563 cycles

NR 1 ENG PYLON HAS WEAR TO STRUT FIREWALL IN EXCESS OF 25 PERCENT. INSTALLED UPPER AFT ANGLE, LOWER SUPPORT WEB.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 65,337 hrs · 24,070 cycles

EMERGENCY LIGHT AT SEATS 9ABC TO SEATS 14ABC FOUND INOPERATIVE. REPLACED BATTERY, CHECKS GOOD.

Part: FEEDER CABLE — DISCONNECTED (EMERGENCY LIGHT) · airframe 64,871 hrs · 23,890 cycles

EMERGENCY FLOOR LIGHTING BETWEEN ROW 9 AND 13 IS INOP. RECONNECTED POWER FEEDER TO POWER STRIP, AND REPLACED EMERGENCY TRACK COVER, P-N 560-0801.

Part: STRINGER — DAMAGED (BS 1015 S6L) · airframe 64,833 hrs · 23,878 cycles

STRINGER DAMAGED AT STA 1015, L6. MAJOR REPAIR ACCOMPLISHED: CUT-OUT DAMAGED STRINGER SECTION AND FABRICATED NEW STRINGER SECTION AND REPAIR SPLICES IAW SRM 53-00-03 AND INSTALLED IAW REO G13172, REV IR, AND UAL EVA 73171 ON NON ROUTINE. CF CAN BE CLEARED. NEW 8100-9 RECEIVED 29OCT10. EC 50-5330-200ZA CONTAINS INSPECTIONS REQUIRED BY DTA IN 8100-9. RECEIVED 8100-9 NO FURTHER ACTION REQUIRED.

Part: LIGHT — UNSECURE (ROW 9) · airframe 64,777 hrs · 23,855 cycles

ESCAPE LIGHT STRIP NEAR ROW 9 COMING LOOSE. REINSTALLED KNOCKED-LOOSE EMERGENCY LIGHT STRIP END.

Part: ACCESS PANEL — LEAKING (RT WING) · airframe 64,635 hrs · 23,796 cycles

RIGHT UNDERWING FURTHEREST INBD FUEL PANEL LEAKING FUEL. TIGHTENED PANEL NO HELP. REMOVED CENTER TANK ACCESS PANEL 531AB. FOUND PANEL 531AB REMOVED. REINSTALLED PANEL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,294 hrs · 23,674 cycles

LT OVERWING FWD EMERGENCY LIGHT INOP. REPLACED AND OPS CHECKED THE LIGHT BULB MM. OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 64,294 hrs · 23,674 cycles

OVERWING HATCH LIGHT ASSY ROW 15 AND 16 SEATS ABC EMERGENCY LIGHT INOP. CLEANED THE ELECTRICAL CONNECTORS & OPS CHECKED THE OVERWING LIGHT ASSY AT ROW 15 AND 16 ABC. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,294 hrs · 23,674 cycles

OVERHEAD BAGGAGE ROWS 6 AND 11 EMERGENCY LIGHT INOP. RELAMPED AND OPS CHECKED THE OVERHEAD BATTERY EMERGENCY LIGHT. INSPECTED BY QC STAMP NR 816. OPS CHECKED GOOD.

Part: CONNECTOR — BURNED (NR 1 ADI) · airframe 64,175 hrs · 23,629 cycles

CONNECTOR TO ADI HAS BURNED PINS. REPLACED CAPT. EADI CONNECTOR D87. INSTALLED NEW LEFT EADI AND RESET CB. FINAL OPS CHECK SATISFACTORY.

Part: DRAIN — CLOGGED (GALLEY) · airframe 64,056 hrs · 23,586 cycles

FWD GALLEY SINK DRAIN LEAKING BEHIND GALLEY. GALLEY HAS TO BE REMOVED TO ACCESS LEAK. DRAIN SYS MADE INOPERATIVE. FWD GALLEY AND FWD LAV DRAIN CLOGGED, WATER BACK-UP, OVERFLOW BEHIND AND UNDER CHILLER. NO LEAKS NOTED. FOUND BAD SECTION OF HOSE IN E&E COMPT REMOVED BLOCKAGE AND RPL HOSE. OPS OKAY.

Part: BOTTLE — LOW (R2 DOOR ASSIST) · airframe 64,056 hrs · 23,586 cycles

DOOR 2 RT DOOR ASSIST BOTTLE READING ZERO. REPLACED EMERGENCY POWER RESERVOIR.

Part: SLEEVE — DENTED (THRUST REVERSER) · airframe 63,647 hrs · 23,440 cycles

NR 1 ENGINE RT-INBD REVERSER TRANSLATING SLEEVE HAS DENT 12 INCHES LONG AND MAX AT 2 INCH WIDE WITH NO VISABLE CRACKING OR PUNCTURE AND WITH AUDIABLE CRUSHED CORE SOUND AS DEFINED IN GNMM 3-0-0-023 AND GNMM 3-0-0 22 DENT IS STILL BONDED TO CORE AND NOT DELAMINATED, MAX DEPTH OF DENT IS.055 AT DEEPEST POINT. DENT LIMIT EXCEEDED REF SRM 54-31-01 FIGURE 101. APPLIED SPEED TAPE AND ACP OP CHECK. VISUAL CK NR1 ENG RT INBD REVERSER TRANSLANTING SLEEVE, NO SOUND OF DELAMINATION AND SPEED TAPE IS SECURED AS REQUIRED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,212 hrs · 23,275 cycles

LT LOWER STATIC PORT FAILED WAVINESS INSPECTION. MAJOR REPAIR ACCOMPLISHED: PRIOR TO DOUBLER BEING MADE SKIN WAS CHECKED FOR SCRIBE AND SKIN WAS PEN INSPECTED. DOUBLER REMOVED AND REPLACED REF SRM. SCRIBE INSP ACP, PEN INSP SKIN ACP.

Part: GIRT BAR — OBSTRUCTED (DOOR 3R) · airframe 63,211 hrs · 23,274 cycles

ARM-DISARM LEVER ON 3R IS STUCK. REMOVED DEBRIS FROM THE AFT AREA OF THE GIRT BAR.CHECKS OKAY.

Part: RESERVOIR — DISCHARGED (R2 DOOR) · airframe 62,727 hrs · 23,086 cycles

DOOR 2R EMERGENCY POWER RESERVOIR REQUIRES REPLACEMENT DUE TO SLIDE DEPLOYMENT. REPLACED RESERVOIR.

Part: INSERT — STRIPPED (GIRT BAR) · airframe 61,532 hrs · 22,642 cycles

R-4 DOOR GIRT BAR INSERT STRIPPED. REMOVED AND REPLACED THE GIRT BAR AND CHECKED GIRT BAR ADJUSTMENT. ADJUSTMENT WITHIN LIMITS. CHECKED MINIMUM SLIDE ENGAGEMENT FOUND TO BE ABOVE .375" ON BOTH ENDS AS DOCUMENTED ON NON ROUTINE.

Part: STRINGER — DAMAGED (BS 1015, S6L) · airframe 61,532 hrs · 22,642 cycles

STRINGER DAMAGED AT STA 1015, L6. MAJOR REPAIR ACCOMPLISHED: CUT-OUT DAMAGED STRINGER SECTION. FABRICATED & INSTALLED NEW STRINGER SECTION AND REPAIR SPLICES.

Part: SKIN — DAMAGED (BS 1015, S6L) · airframe 61,532 hrs · 22,642 cycles

FUSELAGE SKIN DAMAGED STA 1015, STR 6L. MAJOR REPAIR ACCOMPLISHED: CUT-OUT DAMAGE IN FUSELAGE SKIN IAW SRM 53-00-01. ACCOMPLISHED HFEC IAW NDT 6-51-00-19, NO CRACKS NOTED. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-00-01.

Part: BRACKET — DAMAGED (PAX DOOR ASSIST) · airframe 61,532 hrs · 22,642 cycles

MAIN CABIN DOOR 2L EMERGENCY POWER ASSIST BOTTLE CLAMP GOUGED OXYGEN GENERATOR HOLD-DOWN CLAMP. FABRICATED AND INSTALLED NEW HOLD DOWN BRACKET.

Part: BEARING — CORRODED (R4 DOOR) · airframe 61,532 hrs · 22,642 cycles

DOOR R4 LWR ROLLER CAM BEARING BLEEDING CORROSION. INSTALLED NEW FWD AND AFT ROLLER BEARINGS. ADJUSTMENT CHECK GOOD.

Part: BATTERY PACK — DISCONNECTED (EMERGENCY LIGHTS) · airframe 61,532 hrs · 22,642 cycles

EMERGENCY FLOOR LIGHTING FROM SEAT 9-15 STRIP INOPERATIVE. FOUND BATTERY M10567 DISCONNECTED. RECONNECTED PACK M10567. OPS CHECKS NORMAL.

Part: PANEL — DELAMINATED (THRUST REVERSER) · airframe 60,185 hrs · 22,111 cycles

NR 2 ENGINE OUTBOARD RVR UPPER BIFURCATION PNL HAS DELAM. ROUTED TO SFO FOR REPAIR. BEGAN FITTING DOUBLERS TO UPPER BIFURCATION. COMPLETED INSTALLATION OF DOUBLERS REPAIR.

Part: TRANSCEIVER — ODOR (WX RADAR) · airframe 59,797 hrs · 21,961 cycles

ELECTRICAL ODOR IN FLT DECK. FLIGHT DIVERTED. OPENED FWD PIT ACCESS TO EQUIP COOLING FANS AND RECIRC FAN, NO ODORS OR OVERHEATED CONECTOR S NOTED. FANS OP CK NORMAL. CHECKED FWD E&E AREA AND NOTED HOT ODOR, FOUND WX TR UNIT EXTREMELY HOT DUE TO FAN FILTER CLOGGED WITH DEBRIS. 05013 CLEANED FILTER AND UNIT COOLED DOWN, REPLACED WX TRANCEIVER DUE SEVERE OVERHEAT. NO SMOKE OR ELECTRICAL ODOR NOTED. WX OP CHECKS OKAY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,769 hrs · 21,160 cycles

NR 2 LT MAIN ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED. OPS CHECK GOOD.

Part: SENSOR — FAILED (BLEED AIR SYS) · airframe 56,942 hrs · 20,848 cycles

PER CREW LEFT ENG BLEED LIGHT CAME ON. RTFL. FAN AIR TEMP SENSOR FAILURE. REPLACED FAN AIR TEMP SENSOR AND FAN AIR OVERTEMP SWITCH. ACCOMPLISHED A HIGH POWER RUN, ALL SYSTEMS NORMAL.

Part: LIGHT — NO TEST (DOOR 3R) · airframe 56,726 hrs · 20,752 cycles

DOOR 3R ARM LIGHT WILL NOT ILLUMINATE. SUPPLEMENTAL DATA UPDATE CAUSE, DEBRIS UNDER GIRT BAR. REMOVED DEBRIS AND CLEANED SWITCHES, OPS CHECKS OK, ARMS/DISARMS NORMALLY.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 56,655 hrs · 20,720 cycles

NR 1L DOOR ESCAPE SLIDE BOTTLE PRESSURE LOW. FOUND DURING NR 3 SERVICE. REPLACED SLIDE, TESTS GOOD.

Part: FRAME — DENTED (BS 540 S24L) · airframe 56,435 hrs · 20,638 cycles

DENTED FUSELAGE FRAME, INBOARD FLANGE AT BS 540 BETWEEN STR 24L AND 25L. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGED FRAME FLANGE. FABRICATED & INSTALLED A REPAIR ANGLE J-SECTION, STRINGER CLIP (P/N 140N2001-80) & SHEAR TIE (P/N 140N2002-664).

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 56,432 hrs · 20,636 cycles

LT WING INBD FLAP UPPER MID SURFACE OTBD DEPTH WEAR LINE IN PREVIOUS REPAIR. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW METAL DOUBLER.

Part: SKIN — DENTED (BS 620-640) · airframe 56,432 hrs · 20,636 cycles

LEFT EXTERNAL FUSELAGE AT BS 620-640 AT STR 15L-16L SKIN IS DENTED. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (BS 540 S24L) · airframe 56,432 hrs · 20,636 cycles

DENTED FUSELAGE FRAME, INBOARD FLANGE AT BS 540 BETWEEN STR 24L AND 25L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED, CUTOUT DAMAGED FRAME FLANGE. FABRICATED AND INSTALLED A REPAIR ANGLE J-SECTION, STRINGER CLIP (P/N 140N2001-80) AND SHEAR TIE (P/N 140N2002-664).

Part: FRAME — DENTED (BS 1400 S25L) · airframe 56,432 hrs · 20,636 cycles

AFT PIT LT SIDE, FRAME INBOARD FLANGE DENTED AT BS 1400 ABOVE STR 25L. REPAIRED IAW REO G12301 REV B AND EVA 71401 BY MECH 7762 AND INSP BY QC 177 ON NR 27640. THIS RPR HAS RECEIVED ONLY 1ST STAGE APPROVAL PENDING FATIGUE AND DTA EVALUATION BY BOEING TO SHOW COMPLIANCE WITH 14 CFR 25.571 AND 26.43D. ACFT MUST BE REMOVED FROM SERVICE ON 08APR09 UNLESS A NEW 8100-9 IS ISSUED PRIOR TO THAT DATE SHOWING COMPLIANCE.

Part: CREASE BEAM — GOUGED (BS 760-780 S17L) · airframe 56,432 hrs · 20,636 cycles

CABIN BETWEEN BS 760-780 LT AT STR 17L, CREASE BEAM OUTER SPLICE IS GOUGED. MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGED SPLICE FITTING. MACHINED AND INSTALLED A NEW SPLICE (P/N 143N5548-7).

Part: CABLE — OUT OF ADJUST (R4 DOOR) · airframe 56,432 hrs · 20,636 cycles

R4 DOOR FAILS EMERGENCY POWER CABLE TRAVEL CHECK. FOUND CABLE OUT OF ADJUSTMENT. REMOVED DOOR LINER AND ADJUSTED SET SCREW PER MM 52-11-32 AND OPS CHECK GOOD.

Part: CAM — FAILED (L1 DOOR) · airframe 56,432 hrs · 20,636 cycles

L-1 DOOR EMERGENCY POWER ACTUATOR CABLE FAILS TRAVEL CHECK. FOUND ACTUATOR CAM FAILED. REPLACED EMERGENCY POWER A CTUATING CAM

Part: SKIN — OUT OF TOLERANCE (FUSELAGE) · airframe 56,432 hrs · 20,636 cycles

DOOR 2L UPPER HINGE CUTOUT REQUIRES DOUBLER TO BE INSTALLED. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGE AND PERFORMED A .040" INSURANCE CUT. LOCATED AND INSTALLED DOUBLER.

Part: SKIN — OUT OF TOLERANCE (FUSELAGE) · airframe 56,432 hrs · 20,636 cycles

DOOR R2 UPPER HINGE ARM CUTOUT REQUIRES DOUBLER TO BE INSTALLED. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED, PERFORMED INSURANCE CUT. LOCATED AND INSTALLED DOUBLER AS PREVENTATIVE REPAIR.

Part: PAN — GOUGED (L1 DOOR) · airframe 56,432 hrs · 20,636 cycles

L-1 DOOR HANDLE PAN GOUGED. REPLACED PAN.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 56,432 hrs · 20,636 cycles

R-1 DOOR IS OUT OF ADJUSTMENT, FAILS THE MIDWAY CHECK, GIRT BAR DOES NOT RELEASE. GIRT BAR OUT OF ADJUSTMENT. ADJUSTED GIRT BAR, OPS CHECKS GOOD.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,432 hrs · 20,636 cycles

FWD PIT AT STA 620 BETWEEN STR 24L AND 25L, FRAME INBOARD FLANGE DENTED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF FRAME INBD FLANGE. FABRICATED & INSTALLED A REPAIR ANGLE, STRINGER CLIP (140N2001-80) & SHEAR TIE (140N2002-724).

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 56,432 hrs · 20,636 cycles

L-4 DOOR EMERGENCY POWER BOTTLE HAS LOW PRESSURE INDICATION. REPLACED L4 DOOR EMERGENCY POWER BOTTLE.

Part: FRAME — DENTED (BS 1440 S26L) · airframe 56,432 hrs · 20,636 cycles

AFT PIT LT SIDE FRAME INBOARD FLANGE IS DENTED AT BS 1440 ABOVE STR 26L. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGE. HFEC INSPECTED. NO CRACKS NOTED. INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (BS 1600 S26L) · airframe 56,432 hrs · 20,636 cycles

AFT PIT FRAME INBOARD FLANGE DENTED AT BS 1600 AND STR 26L. CUTOUT DAMAGE. NO CRACKED NOTED. INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (BS 1530 S26R) · airframe 56,432 hrs · 20,636 cycles

AFT PIT FRAME INBOARD FLANGE AT STA 1560 AND STR 26R IS DENTED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR.

Part: FRAME — DENTED (BS 580 S26-24L) · airframe 56,432 hrs · 20,636 cycles

FWD PIT AT STA 580 BETWEEN STR 23L AND 24L , FRAME INBOARD FLANGE DENTED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR.

Part: FRAME — DENTED (BS 1500 S26L) · airframe 56,432 hrs · 20,636 cycles

AFT PIT FRAME INBOARD FLANGE IS DENTED AT STA 1500 AND STR 26L. CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR IAW SRM 53-00-07 RPR 5. THIS IS A CAT B ZONE 1 RPR WHICH REQU IRES SUPPLEMENTAL VISUAL AND NDT INSPECTIONS TO BEGIN WHEN ACFT REACHES 50,000C AND 12,000C THEREAFTER. CURRENT CYCLES IS 20,636 PER SRM 53-00-07 RPR 5 TABLE II.

Part: SKIN — BURNED (BS 430 S22-26R) · airframe 56,432 hrs · 20,636 cycles

BURN IN SKIN STA 430 BETWEEN STR 22R AND 23R.

Part: FRAME — DENTED (BS 600 S24L) · airframe 56,432 hrs · 20,636 cycles

FWD PIT AT STA 600 AT STR 24L, FRAME INBOARD FLANGE DENTED. CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR IAW SRM. THIS IS A CAT B ZONE 2 RPR WHICH REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTIONS TO BEGIN WHEN ACFT REACHES 45,636C AND 11,000C THEREAFTER. CURRENT CYCLES IS 20,636 PER SRM 53-00-07 RPR 5 TABLE II.

Part: STRUCTURE — CORRODED (BS 324) · airframe 56,432 hrs · 20,636 cycles

MAIN CABIN T-CAP PREVIOUS REPAIR CORRODED AT BS 324 AND RBL 35. REMOVED DAMAGED AREA, FABRICATED RPR MATERIAL AND INSTALLED IAW SRM 51-40-02 AND MM 53-00- 98

Part: PIN — CRACKED (NR 1 PYLON) · airframe 56,432 hrs · 20,636 cycles

NR 1 PYLON, LT MIDSPAR FUSE PIN HAS CRACK INDICATIONS IN INSIDE DIAMETER. MAJOR REPAIR ACCOMPLISHED: MIDSPAR FUSE PIN IS REPLACED WITH NEW PIN (P/N 311N5500-1).

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 56,325 hrs · 20,600 cycles

EXTERIOR EMERGENCY DOOR NR 2 SLIDE LIGHT IS INOP. RELAMPED.

Part: WIRE — SHORTED (LAV DOOR) · airframe 55,843 hrs · 20,426 cycles

FLIGHT DIVERTED DUE CABIN FIRE DETECTION FAULT. FOUND LAV DOOR SWITCH OVERHEAT CAUSED BY SUPPLY WIRES OVERHEATING DUE TO ELECTRICAL SHORT. FOUND PINCHED WIRES. REPLACED SWITCH AND REPAIRED LAV SWITCH WIRING. ALL OPS CHECKED NORMAL.

Part: STRUCTURE — CORRODED · airframe 55,168 hrs · 20,172 cycles

FOUND CORROSION IN THE BORE OF THE NR 4 AFT TORQUE LINK FWD ATTACH POINT.

Part: SKIN — BURNED (BS 430 S22-23R) · airframe 55,099 hrs · 20,148 cycles

BURN IN SKIN STA 430 BETWEEN STR 22R AND 23R & ADJACENT FASTENER AT STA 385 AND STR 24R. MAJOR REPAIR ACCOMPLISHED. REMOVED BURN AND INSTALLED BLIND FASTENERS AND SKIN REPAIR.

Part: CONTROL UNIT — MALFUNCTIONED (ELEVATORS) · airframe 54,292 hrs · 19,845 cycles

CREW REPORTS RT ELEVATOR PCU EICAS MESSAGE. 09-07-07 FOUND MIDDLE ACTUATOR FAULT ON RT ELEVATOR DURING CHECK. REPLACED RT CENTER ELEVATOR POWER CONTROL UNIT.

Part: LIGHT — INOPERATIVE (EVAC SLIDE) · airframe 52,561 hrs · 19,237 cycles

DOOR 2R SLIDE GIRT BAR ENGAGEMENT LIGHT INOP. CLEANED SOCKET, ARMED AND DISARMED DOOR 2R SEVERAL TIMES AND LIGHT FUNCTIONED NORMALLY. THE DISCREPANCY IS ATTRIBUTED TO SHORTING OF CONNECTION DUE TO ACCUMULATION OF DIRT. THERE WAS NO NEED TO CHANGE ANY PART OR COMPONENT.

Part: SKIN — DAMAGED · airframe 38,692 hrs · 14,209 cycles

JETWAY DAMAGE FORWARD OF DOOR 2L JUST BELOW FLOOR LEVEL. DAMAGE IS 10" BY 5" PUNCTURE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER AND TRIPLER REPAIR.

Part: ENGINE — POWER LOSS (NR 2) · airframe 38,042 hrs · 13,960 cycles

POWER LOSS IN NR 2 ENGINE. THE TEST ON THE FUEL CONTROL UNIT P/N 779100-5, S/N F22470 EXHIBITED SEVERAL PARAMETERS THAT WERE OUT-OF-LIMITS. HOWEVER NONE WERE DEEMED TO HAVE BEEN THE CAUSE OF THE ENGINE SURGE EXPERIENCED ON-WING. FURTHERMORE, THE TESTS FOUND OUT OF SPEC ARE TYPICAL OF UNITS THAT HAVE ACCRUED NEARLY 10,000 FLIGHT HOURS. FUEL PUMP IS ALSO BEING DISASSEMBLED AND NO NOTICEABLE FAILURES HAVE BEEN IDENTIFIED.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,571 hrs · 13,770 cycles

FORWARD EXTERNAL RIGHT HAND SIDE STATION 350 STR 25R JUST FWD AND ABOVE NLG SKIN HAS DENT. MAJOR REPAIR ACCOMPLISHED. INSTALLED TRIPLER REPAIR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,571 hrs · 13,770 cycles

RIGHT HAND CABIN CREASE BEAM WEB UPPER SURFACE CORRODED BETWEEN STATION 1000 & 1020 WL 208. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB.

Part: FRAME — BENT · airframe 37,571 hrs · 13,770 cycles

AFT PIT FRAME BENT AND GOUGED ABOVE STRINGER 26L STATION 1400. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 37,571 hrs · 13,770 cycles

AFT PIT FRAME AT STATION 1600 IS DENTED BETWEEN STRINGER 25 AND 26R. MAJOR REPAIR ACCOMPLISHED. INSTALLED EXTERNAL DOUBLER.

Part: CREASE BEAM — CORRODED (FUSELGE) · airframe 37,571 hrs · 13,770 cycles

CABIN CREASE BEAM WEB UPPER O/B CORRODED BETWEEN STATION 1160 AND 1180 RBL 70 STR 17R. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WEB.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,571 hrs · 13,770 cycles

CABIN CREASE BEAM INNER CHORD CORRODED STATION 730 LBL 69. MAJOR REPAIR ACCOMPLISHED. INNER CHORD REPLACED.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,571 hrs · 13,770 cycles

CABIN CREASE BEAM WEB IS CORRODED STATION 1020-1040 LBL 68-70, WL 208. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,571 hrs · 13,770 cycles

STATION 325-365, RBL 70, WL 208 CREASE BEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. CREASE BEAM DAMAGE BLEND BETWEEN STATION 325-365.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 37,571 hrs · 13,770 cycles

CABIN INTERCOSTAL CORRODED AT NUT PLATE HOLES, STATION 735, WL 208, LBL 66. MAJOR REPAIR ACCOMPLISHED. BLENDED CORROSION.

Part: CLIP — CORRODED (FUSELAGE) · airframe 37,571 hrs · 13,770 cycles

CABIN CREASE BEAM CLIP IS CORRODED, STATION 1037, LBL 70, WL 208. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,571 hrs · 13,770 cycles

CABIN FLOORBEAM UPPER T-CAP CORRODED AT STATION 324 FROM 35 RBL TO 60 RBL AT STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW T-CAP FROM LBL 7 TO RBL 70.

Part: SKIN — CORRODED (FUSELAGE) · airframe 37,571 hrs · 13,770 cycles

EXTERNAL FUSELAGE SKIN LT SIDE STATION 623, BETWEEN STRINGER 15L AND 16L HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. BLENDED CORROSION.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,571 hrs · 13,770 cycles

LEFT HAND SIDE OF FUSELAGE, 7 FT FWD OF DOOR 2L LOWER EDGE, HAS DENT THAT IS 4 INCHES LONG AND 3 INCHES WIDE WITH A DEPTH OF .095. DENT IS NEXT TO SKIN DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,571 hrs · 13,770 cycles

RIGHT I/B SEAT TRACK AT RBL 25 CORRODED STATION 680 TO STATION 700 ON I/B FLANGE. MAJOR REPAIR ACCOMPLISHED. SEAT TRACK REPLACED FROM STA 620-700.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 37,571 hrs · 13,770 cycles

CABIN FLOOR INTERCOSTAL CORRODED ON UPPER SURFACE AT STATION 310 TO 324 RBL 40 STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW INTERCOSTAL U-CHANNEL.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,571 hrs · 13,770 cycles

LT CABIN FLOOR CREASE BEAM WEB CORRODED STATION 920 TO 940 LBL 58 STRINGER 17L. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW WEB.

Part: FRAME — CORRODED · airframe 37,571 hrs · 13,770 cycles

AFT PIT FRAME STATION 1500 RBL 15 CORRODED. MAJOR REPAIR ACCOMPLISHED.REPAIR DOUBLER INSTALLED ON FRAME 1500.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,571 hrs · 13,770 cycles

CABIN FLOORBEAM TOP FLANGE CORRODED BODY STATION 1640, RBL 44 THROUGH RBL 62. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE REPAIR.

Part: FRAME — CORRODED · airframe 37,571 hrs · 13,770 cycles

AFT PIT FRAME AT STATION 1200 STRINGER 30 TOP FLANGE HAS EXCESSIVE MATERIAL LOSS FROM CORROSION REMOVAL. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.INSTALLED FRAME CAP REPAIR STRAP.

Part: FRAME — BENT · airframe 37,571 hrs · 13,770 cycles

AFT PIT FRAME BENT ABOVE STRINGER 25LH STATION 1460. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.INSTALLED FRAME CAP WEB CUTOUT INTERNAL AND EXTERNAL DOUBLER AND TRIPPLER REPAIR.

Part: STRINGER — GOUGED · airframe 37,571 hrs · 13,770 cycles

FORWARD CABIN STRINGER 2R IS GOUGED AT STATION 460. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW SECTION WITH SPLICE AT 470 STATION.

Part: INTERCOSTAL — CRACKED · airframe 37,571 hrs · 13,770 cycles

CABIN FLOOR INTERCOSTAL AT STATION 357 RBL 25" STRINGER 17R IS CRACKED OUT AROUND NUTPLATE HOLE. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW U- CHANNEL INTERCOSTAL BETWEEN STATION 345 AND 365.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,571 hrs · 13,770 cycles

AFT PIT FRAME CORRODED, STATION 1480 RBL 27 STRINGER 27 UNDERNEATH RT Z ANGLE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,571 hrs · 13,770 cycles

CABIN FLOORBEAM 1681 RBL 12 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP AND ANGLE REPAIRS WITH FILLER.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 37,571 hrs · 13,770 cycles

AFT CABIN PRESSURE DECK CORRODED AT STATION 1681 RBL 12. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 37,571 hrs · 13,770 cycles

CABIN FLOORBEAM STATION 1420 TOP SURFACE HAS GOUGES AROUND FASTENER HOLES, LBL 18 TO RBL 5 AT WL 208. MAJOR REPAIR ACCOMPLISHED. INSTALLED REINFORCEMENT STRAPS.

Part: FRAME — DENTED · airframe 37,571 hrs · 13,770 cycles

AIRCRAFT FRAME IN AFT PIT DENTED, STATION 1420 BETWEEN STRINGER 25 AND STRINGER 26L. MAJOR REPAIR ACCOMPLISHED.REMOVED DAMAGE, INSTALLED DOUBLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,571 hrs · 13,770 cycles

CABIN FLOORBEAM 365 EXCESSIVE MATERIAL LOSS FROM CORROSION REMOVAL. MAJOR REPAIR ACCOMPLISHED. INSTALLED UNDER FLANGE STRAP.

Part: AIR DISTRIBUTION — ODOR (CABIN)

AIRCRAFT RETURNED TO FIELD DUE TO ODOR OF KEROSENE AT ROWS 19 AND 20. *S/D* CHECKED BOTH CARGO PITS FOR FLAMMABLES AND AIR CONDITIONING BAYS FOR FUEL LEAKS, CHECKED OK. CHECKED OVERHEAD BINS AT RIGHT HAND SECTION OF CABIN. FOUND INSECTICIDE, CLEANED THE AREA.

Part: EEC — MALFUNCTIONED (LT ENGINE)

LEFT ENGINE COMPRESSOR STALLED AT 5000 FEET AFTER TAKE-OFF. ACCOMPLISHED BOROSCOPE INSPECTION PER MM 72-00-97. REPLACED EEC (ELECTRONIC ENGINE CONTROL) PRECAUTIONARY. INSPECTED ALL STATOR VANE LINKAGES AND ARMS, FOUND NO PROBLEMS. NO FURTHER DISCREPANCIES WERE REPORTED.

Part: BATTERY PACK — DISCHARGED (CABIN)

EXIT LIGHT ABOVE DOOR 1R WILL NOT ILLUMINATE DURING EMERGENCY LIGHT TEST. REPLACED BATTERY PACK, OPERATION CHECKS NORMAL.

Part: TRACK — DAMAGED (CABIN)

EMERGENCY EXIT LIGHTS FLOOR TRACK LENS AT ROWS 1 THROUGH 2 ARE DAMAGED. REPLACED EMERGENCY EXIT LIGHTS FLOOR TRACK COVER.

Part: LAMP — FAILED (CABIN)

EMERGENCY LIGHT IN BULLNOSE ABOVE SEAT ROW 33ABC IS INOP. LAMP BURNED OUT. REPLACED LAMP.