N569UA

Part: LIFE VEST — MISSING (COCKPIT) · airframe 68,871 hrs · 25,365 cycles

1ST OBSERVER`S LIFE VEST MISSING. INSTALLED NEW LIFE VEST AT 1ST OBSERVER`S STATION.

Part: ANTI-ICE VALVE — FAILED (LT WING) · airframe 68,832 hrs · 25,352 cycles

LT WING HEAT ON IN FLIGHT & FAILED, HAD WING LIGHT & EICAS. R & R LT THERMAL ANTI ICE VLV IAW AMM.

Part: UNKNOWN — FAULTY (WINDOW HEAT) · airframe 68,832 hrs · 25,352 cycles

RT SIDE WINDOW HEAT INOPERATIVE. TRIED RESET IAW QRH STILL INOPERATIVE. FAULTS CONTROL UNIT, REPLACED WHCU M191, NO HELP. SWAPPED M191 & M192, NO HELP. STILL FAULTS CONTROL UNIT. ALL WHCU INSTALLED IN ORIGINAL POSITION SEE SEQ 8322006 FOR COMPLETION.

Part: PIN — STICKS (CARGO BAY) · airframe 68,737 hrs · 25,320 cycles

SECONDARY BARRIER MID LATCH PIN STICKS MAKING IT HARD TO INSTALL & REMOVE BARRIER. LOWER ATTACH PLATE, OPERATIONS GOOD.

Part: LINE — LEAKING (BRAKE SYSTEM) · airframe 68,711 hrs · 25,312 cycles

FOUND HYD LEAK NR 3 BRAKE LINE. R & R NR3 BRAKE PRESS LINE.

Part: BLEED VALVE — FAULTY (ENGINE) · airframe 68,597 hrs · 25,278 cycles

ON CLIMB EPR & N1 FLUCTUATED N2 EGT FF DID NOT FLUCTUATE IN CRUISE, ALL NORMAL. REPLACED 14TH STG BLD VAL & BLD VAL CONVERTER ON PTT SEQ 5972002 & 5972003, OPERATIONS CHECKED GOOD.

Part: ENGINE — SURGES (LEFT) · airframe 68,594 hrs · 25,277 cycles

AFTER DESELECTING TAI ON CLIMB, LT ENG CONT SURGING BETWEEN 1.4 & 1.5 EPR UNTIL LEVEL OFF.

Part: HANDLE — UNSECURE (COCKPIT WINDOW) · airframe 68,573 hrs · 25,270 cycles

FIRST OFFICER`S WINDOW CRANK HANDLE CAME OFF. REINSTALLED & SECURED WINDOW CRANK HANDLE, OPERATIONS CHECKED GOOD.

Part: COVER — LOOSE (CABIN) · airframe 68,549 hrs · 25,261 cycles

AFT CABIN EMERGENCY TRACK LIGHTING COVER LOOSE BY AFT LAVATORY. SECURED TRACK LIGHTING COVER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,454 hrs · 25,232 cycles

EMERGENCY EXIT LIGHTS ON FLOOR DOOR 1L INOPERATIVE BY CLOSET. SECURED LOOSE EMERGENCY EXIT LIGHT STRIP TO POWER CABLE & INSTALLED NEW END CAP, CHECKED OKAY.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 68,420 hrs · 25,221 cycles

2L SLIDE ARM LIGHT INOPERATIVE. RELAMPED BULBS.

Part: WIRE HARNESS — SHORTED (NR 2 GENERATOR) · airframe 68,051 hrs · 25,093 cycles

NR 2 GENERATOR WIRE SHORTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,038 hrs · 25,086 cycles

EMERGENCY EXIT LIGHTS AT ROW 36 -40 ARE INOPERATIVE. REPLACED LAMP. OPS CHECKED NORMAL.

Part: SAFETY WIRE — MISSING (LT GENERATOR) · airframe 68,031 hrs · 25,084 cycles

MAINTENANCE ITEM DISPLAY-LEFT GENERATOR DRIVE SAFETY WIRE NOT SECURED. REPLACED MISSING SAFETY WIRE ON LT GENERATOR SWITCH AS REQUIRED.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 68,031 hrs · 25,084 cycles

SMOKE IN FLIGHT DECK, RETURN TO FIELD. PERFORMED SMOKE IN THE CABIN INSPECTION AMM 05-51-56. FOUND ENGINE BAD. IAW PTT SEQ 0312038 R & R NR 1 ENGINE AS PER TOD 71-00-02 CONFIG 1 PAGE 401-424, ALL CHECKED GOOD, NO LEAKS NOTED. IAW PTT SEQ 0312049 PERFORMED BURN OUT IAW AMM 21-00-01 STEP(3) E & REPLACED RECIRCULATION FILTERS IAW AMM 21-25-02. OPERATION CHECKED NORMAL.

Part: APU — FAILED · airframe 67,676 hrs · 24,961 cycles

ZERO AIR PRESSURE FROM APU AFTER STARTED ON TAXI IN. SUSPECT APU FLOW SENSING MODULE BAD. REPLACED APU IAW AMM, OPS CHECKED GOOD 35 PSI.

Part: APU — ODOR (CABIN) · airframe 67,666 hrs · 24,958 cycles

STRONG OIL ODOR IN AFT CABIN AND AND FWD 5 ROWS OF GALLEY. VERIFIED OIL OIL PRESENT WHILE RUNNING APU, WENT AWAY AFTER APU OFF. VERIFIED NO OIL ODOR PRESENT WHILE RUNNING PACKS OF GROUND AIR UNIT. THE APU BLEED VALVE INOPERATIVE "CLOSED". APU PNEUMATICS INOPERATIVE IAW AMM 49-11-00, FIM 49-11.

Part: DRAIN — LEAKING (NR 1 ENGINE FUEL) · airframe 67,665 hrs · 24,957 cycles

FUEL DRIPPING FROM UNDER NR 1 ENG FAN COWLS. FOUND FUEL LEAK FROM FUEL FILTER HOUSING DRAIN PLUG. TIGHTENED PLUG, WET MOTORED NR 1 ENGINE, NO LEAKS NOTED.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 67,588 hrs · 24,933 cycles

FOUND PUDDLE OF HYDRAULIC FLUID UNDER RT MLG. REPLACED NR 8 BRAKE HOSE ASSY. RESET HYDRAULIC FUSE, NO LEAKS NOTED AND NR 8 BRAKES ACTUATES NORMAL.

Part: ACTUATOR — LEAKING (LT AILERON) · airframe 67,444 hrs · 24,884 cycles

PUSH CREW NOTICED HYD FLUID UNDER LEFT WING NEAR AILERON ON WALKAROUND WITH HYD PRESSURIZED. AILERON PCA REPLACED. NO LEAKS NOTED.

Part: FAUCET — DAMAGED (LAVATORY) · airframe 67,098 hrs · 24,776 cycles

POTABLE WATER SYS INOPERATIVE. REPLACED FWD LAVATORY FAUCET.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 66,985 hrs · 24,741 cycles

FOUND CRACKED BRACKET. INSTALLED NEW BRACKET.

Part: SKIN — DENTED (BS 590-592 S27L) · airframe 66,969 hrs · 24,734 cycles

FUSELAGE SKIN, BS 590 - 592, ONE INCH BELOW S27L, DENTED. REPAIRED IAW ECRA5330-04561 AND REO-G16173REVC.

Part: SKIN — DENTED (BS 522 S15-16L) · airframe 66,969 hrs · 24,734 cycles

FUSELAGE SKIN DENTED BS 522, S15-16L. REPAIRED IAW REO G16174B. MAJOR REPAIR.

Part: SKIN — DENTED (BS 1520-1540) · airframe 66,969 hrs · 24,734 cycles

FUSELAGE SKIN DENTED, BS 1520-1540, S22-23L, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. CUT OUT DAMAGE, INSTALLED DOUBLER IAW SRM 53-00-01, FIG 201, REPAIR 3.

Part: SKIN — CRACKED (RT WING) · airframe 66,951 hrs · 24,727 cycles

ON MX WALK AROUND, FOUND PANEL ON RIGHT WING JUST O/B OF NR 2 ENGINE, FWD OF T/E FLAP, LOWER SURFACE CRACKED. REPAIRED IAW ECRA5722-01044.

Part: TUBE — DEFECTIVE (MINITEL) · airframe 66,828 hrs · 24,692 cycles

BOOM MIKE DOES NOT STAY SCREWED INTO F/O'S MINITEL HEADSET. *SUPPLEMENTAL DATA UPDATE* REPLACED VOICE TUBE ON FO MINITEL.

Part: COVER — DAMAGED (L2 DOOR SLIDE) · airframe 66,782 hrs · 24,680 cycles

L2 DOOR SLIDE COVER DAMAGED, CUT, PUNCTURE 2 1/4 INCHES LONG, 1/8 INCHES DEEP. REPAIRED IAW AMM 25-00-00-80 1 REPAIR 2 STEP J.

Part: SEAT BELT — DEFECTIVE (COCKPIT) · airframe 66,556 hrs · 24,599 cycles

CAPTS R SEAT BELT UNSAFE FOR CONTINUED USE, REPEAT GRIPE. SLIPS LOOSE THRU BELT SNUBBER. REPLACED CAPT LAP BELT ASSY, OP CHECK GOOD.

Part: SEAL — UNSECURE (SERVICE DOOR) · airframe 66,543 hrs · 24,595 cycles

PASSENGER ENTRY - SERVICE DOORS R AFT EVAC SLIDE ARM LEVER DIFFICULT TO POSITION. CREW COMMENTS: SKIRT NEEDS ADJUSTMENT. SECURED SKIRT SEAL TO BUSTLE. TESTED AND INSPECTED ARMING MECHANISM: ALL SATISFACTORY. BRIEFED OUTBOUND FLIGHT ATTENDANT. LEFT DOOR IN THE DISARMED POSITION.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 66,391 hrs · 24,545 cycles

R4 DOOR WILL NOT ARM. REMOVED DEBRIS FROM R4 DOOR GIRT BAR, ARMS AND DISARMS NORMALLY.

Part: SKIN — DEBONDED (FUSELAGE) · airframe 66,352 hrs · 24,532 cycles

SKIN TO BEAR STRAP IS DISBONDED AROUND REPAIR CUTOUT. REPAIRED WITH DOUBLER AND TRIPLER PER EA 5330-04213 AND ECRA 5330-04415.

Part: SKIN — DEBONDED (FUSELAGE) · airframe 66,352 hrs · 24,532 cycles

SKIN TO BEAR STRAP DISBONDED AROUND REPAIR CUTOUT. REPAIRED WITH DOUBLER AND TRIPLER PER EA 5330-04213 AND ECRA NR 5330-04415.

Part: INDICATOR — OBSTRUCTED (L1 DOOR) · airframe 66,323 hrs · 24,523 cycles

L1 DOOR ARMED INDICATOR STICKS. LINING WAS BINDING AGAINST SLIDE INDICATOR. INSTALLED LOWER DOOR LINER AND INNER HANDLE PER AMM.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 66,138 hrs · 24,457 cycles

DOOR 2R PAX DOOR EMERGENCY POWER RESERVOIR PRESSURE BELOW LIMITS PER JOB CARD 5-5650-A STEP 7(C). REMOVED AND REPLACED DOOR 2R EMERGENCY PWR RESERVOIR BOTTLE ASSY IAW AMM.

Part: BATTERY — FAULTY (MAIN) · airframe 65,562 hrs · 24,256 cycles

MAIN BATTERY CHARGER STATUS MESSAGE WILL NOT CLEAR. REPLACED MAIN BATTERY. TEST OK & MESSAGE CLEARED.

Part: STRIP — DISCONNECTED (CABIN) · airframe 65,180 hrs · 24,131 cycles

F/A NOTICED SOME EMERGENCY EXIT LIGHTS INOP WHEN EXT PWR DROPPED OFF. FOUND EMERGENCY FLOOR LIGHT STRIP SLIGHTLY DISCONNECTED NEAR ROW 12 AND EMERGENCY LIGHT COVER COMPLETELY DAMAGED. RECONNECTED AND OPS CHECKED ALL EMERGENCY LIGHTING CHECKED GOOD. REPLACED EMERGENCY FLOOR LIGHT COVER FROM ROW 8 TO ROW 14.

Part: FEEDER CABLE — LOOSE (EMERGENCY LIGHT) · airframe 64,985 hrs · 24,067 cycles

EMERGENCY LIGHTING AT 11C LOOSE. REPLACED FEEDER CABLE FROM THE WALL TO THE LIGHTS. GROUND CHECK OK. PERFORMED OPERATION CHECK AND INSPECTED PROPER INSTALLATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,335 hrs · 23,861 cycles

EMERGENCY LIGHTS FROM ROW 8 TO 14 ARE INOPERATIVE. RELAMPED IAW AMM 33-51-11. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,732 hrs · 23,654 cycles

CREW REPORTED EMERGENCY LIGHTS INOPERATIVE ROW 8 TO 11. REPLACED FAULTY LIGHT, OPS SATISFACTORY.

Part: PCA — OUT OF ADJUST (SPEED BRAKE) · airframe 63,604 hrs · 23,609 cycles

WHEN SPEED BRAKES DEPLOYED AC INITIALLY BANKS LEFT THEN HOLDS A 1 DEGREE AILERON TRIM RIGHT. MAINT TEXT: PER CREW VERBAL: CREW DEPLOYED SPEED BRAKES AT ALTITUDE WITH A-P ON AND OFF. WITH A-P OFF AIRCRAFT BEGINS TO SLOWLY BANK LT WING DOWN AS SOON AS SPEED BRAKE HANDLE IS MOVED. ALL TRIM SETTINGS WHERE NEUTRAL. ADJUSTED SPOILER POWER CONTROL ACTUATORS NR 3, 4, 5 & 6 IAW AMM.

Part: ACTUATOR — OUT OF ADJUST (SPOILER) · airframe 63,604 hrs · 23,609 cycles

WHEN SPEED BRAKES DEPLOYED AC INITIALLY BANKS LEFT THEN HOLDS A 1 DEGREE AILERON TRIM RIGHT. MAINT TEXT: PER CREW VERBAL: CREW DEPLOYED SPEED BRAKES AT ALTITUDE WITH A-P ON AND OFF. WITH A-P OFF AIRCRAFT BEGINS TO SLOWLY BANK LT WING DOWN AS SOON AS SPEED BRAKE HANDLE IS MOVED. ALL TRIM SETTINGS WHERE NEUTRAL. ADJUSTED SPOILER POWER CONTROL ACTUATORS NR 3, 4, 5, & 6 IAW AMM.

Part: ROD — OUT OF ADJUST (NLG STEERING) · airframe 63,427 hrs · 23,546 cycles

WITH TILLER CENTERED PLANE VEERS NOTICEABLY TO THE RIGHT. STEERING INPUT ROD, OPS OKAY.

Part: SLIDER — DEFECTIVE (GIRT BAR) · airframe 63,351 hrs · 23,520 cycles

DOOR 1L NO ARMED LIGHT WHEN DOOR IS ARMED. NO TIME. REPLACED GIRT BAR SLIDER ASSY AFT SIDE, OPS CHK GOOD. PINNED SLIDE AND BOTTLE PER AMM.

Part: SLIDER — MISSING (GIRT BAR) · airframe 63,355 hrs · 23,521 cycles

DOOR 1L GIRT BAR AFT SLIDER MISSING. REPLACED SLIDER ON AFT SIDE OF DOOR 1L. PINNED BOTTLE AND SLIDE ASSY REMOVED PER MM.

Part: COVER — SEPARATED (L2 DOOR) · airframe 62,547 hrs · 23,234 cycles

CREW REPORT: DOOR 2L EXIT SIGN COVER SEPARATED AND IS ON THE OPEN DOOR NOW. SECURED EXIT SIGN COVER.

Part: SEQUENCE VALVE — FAULTY (NLG) · airframe 62,178 hrs · 23,091 cycles

UNSAFE NOSE GEAR ON FINAL. REPLACED GEAR SEQUENCE VALVE UNDER SEQUENCE 1782008 AND RPL FLOW CONTROL VALVE UNDER SEQUENCE 1782006. PERFORMED RETRACTION, NO ADDITIONAL FAULTS NOTED.

Part: UNKNOWN — DAMAGED · airframe 61,684 hrs · 22,920 cycles

HAIL DAMAGE.

Part: OXYGEN SYSTEM — LOW PRESSURE (CREW O2) · airframe 61,592 hrs · 22,887 cycles

CREW REPORT: OXYGEN CREW NEEDS SERVICING. SERVICED CREW O2 PER AMM.

Part: SEAT — UNSECURE (CABIN) · airframe 61,528 hrs · 22,868 cycles

CREW REPORTS SEAT 20 ABC ARE NOT ATTACHED TO THE FLOOR TRACKS. SECURED SEAT ROW 20ABC. UPON FURTHER INSPECTION SEAT ROWS 21ABC AND 28DEF FRONT ANTI-RATTLE CLIPS FOUND TO BE SLIGHTLY LOOSE. SEAT ROWS WERE SECURE IN THE TRACK. ADJUSTED ANTI-RATTLE CLIPS.

Part: FRAME — CORRODED (BS 1400) · airframe 61,525 hrs · 22,866 cycles

AFT CARGO PIT AT STA 1400, LBL 3 FRAME HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. BLENDED OUT CORROSION IAW EA PD57-53-144 & EVA-80955. ACCOMPLISHED NDT OF BLENDED AREA & EXISTING FASTENER HOLES PER EA. FABRICATED & INSTALLED REPAIR DOUBLER, REPAIR CLIPS & REPAIR SHEAR TIE & RETAINER PER EA BETWEEN STRINGERS S-27L & S-29L.

Part: FLOORBEAM — CORRODED (BS 310.5) · airframe 61,525 hrs · 22,866 cycles

FLOORBEAM AT STA 310.5 RBL 35-39 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION DAMAGE & ACCOMPLISHED NDT OF CUT-OUT AREA & HFEC SCAN OF FASTENER HOLES COMMON TO REPAIR PER EA PD57-53-135. FABRICATED & INSTALLED TEE SECTION REPAIR, REPAIR ANGLES & REPAIR STRAPS REF EA PD57-53-135.

Part: STRINGER — GOUGED (BS 1640 S8L) · airframe 61,525 hrs · 22,866 cycles

GOUGE ON STR 8L AT STA 1640. MAJOR REPAIR ACCOMPLISHED. BLENDED GOUGE AREA PER EVA 80943 AND EA PD57-53-142 ON NR 2673N00418.

Part: CREASE BEAM — CORRODED (BS 1020-1040) · airframe 61,525 hrs · 22,866 cycles

CORROSION ON CREASE BEAM INNER CHORD AROUND FASTENERS AT STA 1020 - 1040, MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION & FOUND OUT OF LIMITS PER SRM. ACCOMPLISHED NDT OF DAMAGE CUTOUT & HFEC SCAN OF HOLES COMMON TO REPAIR REF EA PD57-53-141. FABRICATED & INSTALLED REPAIR, REPLACE SPLICE CHANNEL & REPAIR SLICE STRAP PER EA.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 61,525 hrs · 22,866 cycles

CORROSION ON FLOORBEAM AT STA 324 BL 53R. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM, SPLICE ANGLES AND SPLICE STRAPS PER EA PD57-53 -136 AND EVA 80900 ON NR 2673N00125.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,525 hrs · 22,866 cycles

EEL LIGHTS INOP AT SEAT ROW 27. RELAMPED EMERGENCY LIGHT SEAT ROW 27ABC, OPS CHECK GOOD PER AMM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,525 hrs · 22,866 cycles

CORROSION ON CREASE BEAM AT STA 997, RBL 64, WL 209. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION, BLENDED AREA, ACCOMPLISHED HFEC, NO CRACKS DETECTED IAW PEMCO EA PD57-53-145 ON PEMCO NR 2673N00384.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,525 hrs · 22,866 cycles

EEL LIGHTS INOP AT SEAT ROW 13. RELAMPED SEAT, OPS CHECKED GOOD PER AMM.

Part: FITTING — WORN (TE FLAP) · airframe 61,525 hrs · 22,866 cycles

LEFT I/B AFT FLAP, FWD I/B ROLLER FITTING IS WORN. MAJOR REPAIR ACCOMPLISHED: FABBED REPLACEMENT END-RIB REF BOEING DWG 113N2808, INSTALLED END-RIB (P/N 113N2808-1) ON LEFT I/B AFT FLAP IAW SRM ON NR 2673N00629.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,525 hrs · 22,866 cycles

CORROSION STA 1620, BL 0, STR 29L AND STR 29R ON FRAME TO SKIN TO SUPPORTS. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE, FABBED AND INSTALLED DOUBLER, FILLER, ATTACH ANGLE AND CLIPS PER EA PD57-53-139 ON NR 2673N00306.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 61,525 hrs · 22,866 cycles

CORROSION ON BEAR STRAP STA 1620, STR 29L TO STR 29R. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER PER PEMCO EA PD57-53-143 AND EVA 80942 ON PEMCO NR 2673N00306. THIS REPAIR MUST RECEIVE A NEW FAA FORM 8100-9 SHOWING COMPLIANCE TO 14 CFR 25.571 AND 26.43(D) AND DTI INCORPO RATED IN THE ACFT MAINT PROGRAM WITHIN 24 MO. FROM 06-16-11 FOR THIS REPAIR APPROVAL TO REMAIN VALID AFTER 06-16-13. IF A NEW 8100-9 APPROVAL IS NOT OBTAINED ON OR BEFORE 06-16-11, THE ACFT BECOMES UNAIRWORTHY. RECEIPT IS TRACKED BY DTA 11-098.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,525 hrs · 22,866 cycles

CORROSION AT FLOORBEAM STA 365 AT RBL 38. MAJOR REPAIR ACCOMPLISHED: CORROSION WAS BEYOND SRM LIMITS & THE UPPER CHORD OF THE FLOORBEAM REQUIRED REPLACEMENT PER THE INSTRUCTIONS ON PEMCO EA PD57-53-137 WITHOUT DEVIATION. THIS IS CONSIDERED A PERMANENT REPAIR WITH 8100-9 DATED JUNE 7 2011.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,525 hrs · 22,866 cycles

FLOORBEAM STA 1640 RBL 41 TO RBL 52 HAS SIGNS OF CORROSION. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION FROM FLOORBEAM BETWEEN RBL41-52 & FOUND OUT OF LIMITS. FABRICATED & INSTALLED T-CHORD SECTION, ANGLES & REPAIR PARTS AMT & INSP'D.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 61,512 hrs · 22,860 cycles

EMER PATH LIGHTING IN ALL ROWS EXCEPT 22-30 CAME ON WHILE ON FINAL. SWITCH IN ARM POSITION. BATTERY PACK REPLACED AND ACCOMPLISHED OP CK, NO FAULTS FOUND.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 61,512 hrs · 22,860 cycles

EMERGENCY EEL LIGHT AFT CABIN LAV INOP NOT HOOKED UP. REPAIRED LIGHT AND ACCOMPLISHED OP CKS. NO FAULTS FOUND.

Part: SKIN — GOUGED (BS 610) · airframe 61,335 hrs · 22,799 cycles

LEFT SIDE FUSELAGE APPROX STA 610.0 AND WL 206.0. A DENT WITH GOUGE APPROX 3.0 X 2.0 INCHES IN AREA AND .50 DEEP WITH DISPLACED METAL. INITIAL NDT INSP INDICATED SKIN AT 0.063IN WITH A MAX LOST OF 0.010IN AT A READING OF SKIN THICKNESS OF 0.053IN. THIS INSPECTION WAS ACCOMPLISHED WITH NO BLENDING DONE TO ADDRESS THE GOUGED SKIN AND UNABLE TO CHECK SKIN FOR CRACKS WITH HFEC INSP. CUT OUT DAMAGE FOR REPAIR 3 OF SRM. UA-EVA-80806 HAS BEEN ISSUED RPR IS NOW COMPLETE. REPAIR IS CONSIDERED AS PERMANENT.

Part: RESERVOIR — LOW PRESSURE (R1 DOOR) · airframe 61,285 hrs · 22,782 cycles

DOOR 1R SLIDE PRESS GAUGE NOT IN GREEN BAND. REPLACED EMERGENCY POWER RESERVOIR PER MM. PRESSURE IS OKAY.

Part: DOOR — DAMAGED (NLG) · airframe 61,230 hrs · 22,761 cycles

AIRCRAFT HAS EXPERIENCED LIGHTNING STRIKE. DURING CLIMB NORTEAST OF IAD AT 12000 EXPERIENCED LIGHTNING STRIKE NOSE OF A/C. ACP'D LIGHTENING STRIKE INSP PER MM. SIX RIVETS HAD STATIC DISCHARGE FROM LIGHTENING STRIKE BETWEEN STA 347 AND 353 STRINGER AREA S25 TO S28. INSP AND FOUND DAMAGE TO BE WITHIN LIMITS PER AMM. LT FWD NOSE GEAR DOOR NEEDS TO BE PAINTED. DOOR HAS BEEN PRIMED AND IS IN SHEETMETAL SHOP. REMOVED DAMAGES. STARTED COMPOSITE RPR. REPAIR STARTED AT 0645 FOR 240 MIN. WILL NEED TO REMOVE BAGGING MAT'L AND PAINT RPR. CURE COMPLETE. PRIMED AND PAINTED FIRST COAT OF BLUE. RT NOSE GEAR DOOR AND ATTACHING HARDWARE HAVE BURN HOLES. APPRX 30 RIVETS AND VHF ANTENNAS WELL. RVI PICS LOADED. RT GEAR DOOR,170-3774 AOG'D PRECAUTIONARY. REPLACED RT NLG DOOR.

Part: RELAY — FAULTED (MASTER BATTERY) · airframe 61,072 hrs · 22,703 cycles

MAIN BATTERY CHARGER MESSAGE, SUSPECT RIGHT BUS NOT POWERED. REPLACED MAIN SHIP BATTERY AND MAIN BATTERY CHARGER, NO HELP. REPLACED MAIN BATTERY CHARGER DISABLE RELAY K115, NO HELP. PER FIM 24-31-00 P106 PAGE BLOCK 7. FOUND A1-90VAC, B1-77VAC, C1-115VAC. TRACED BACK TO RELAY K102 IN THE P34 PANEL AS BAD, REPLACED K102 RELAY, MESSAGE CLEARED. CHECKED GOOD.

Part: ENGINE — MAKING METAL (NR 2) · airframe 60,973 hrs · 22,663 cycles

NR 2 ENGINE LARGE METAL DEBRIS FOUND IN INTERMEDIATE PRESSURE CHECK VALVE DURING C-CHECK MAINTENANCE. BORESCOPE INSPECTED PER MM. NO LIMITING DEFECTS NOTED. REQUIRES FOLLOW UP BOROSCOPE INSPECTION. DUE TO METAL FOUND IN INTERMEDIATE CHECK VALVE FOLLOW UP BOROSCOPE INSPECTION OF HPC STAGE 6 THROUGH 17 PER AMM WITHIN 50 CYCLES PER AMM. NO LIMITING DEFECTS NOTED.

Part: FLOORBEAM — DAMAGED (BS 1661) · airframe 60,973 hrs · 22,663 cycles

AFT FUSELAGE STA 1661 CABIN FLOOR SUPPORT HAT CHANNEL EXFOLIATED RBL 0 AS SEEN THRU AFT PIT COMPARTMENT. NUT PLATE BLOWN THRU MATERIAL. REPLACED ON SMB W-U E9886H. DUP OF BASE WRITE UP K6124C.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,707 hrs · 22,563 cycles

CREW REPORTED COACH INTERIOR EMERGENCY LIGHTS ARE ON INFLIGHT WITH THE CONTROL SWITCHES OFF AND NO EICAS MESSAGE. CYCLED BOTH COCKPIT SWITCH AND AFT F/A SWITCH TO TRY TO EXTINGUISH, NO HELP. REPLACED POWER SUPPLY M10818 AND BATTERY PACKS AT M10818, M10817AND M10770. TESTED INPUT VOLTAGE TO ABOVE POWER SUPPLIES, ON SIGNAL AND OFF SIGNAL. FOUND ALL OK. LIGHT OPS TEST AND SYS TEST OK.

Part: UNKNOWN — NOISY (COCKPIT) · airframe 60,663 hrs · 22,544 cycles

FLT DECK EXCESSIVELY NOISY WITH BOTH RECIRC FANS ON. SERVICE TIP 21-22-00, LEFT PACK CONTROL VALVE AND TCV ALREADY REPLACED. LM4517 ALREADY ACCOMPLISHED. WIND NOISE AND NOISE LEVEL NOTED HIGH. USING SVC TIP21-22-00 901 DECIBEL READINGS 72-75 AND AIRFLOW WITHIN LIMITS TESTING AT S21. AIRFLOW THROUGHOUT CABIN NORMAL.

Part: SWITCH — DIRTY (COCKPIT) · airframe 60,638 hrs · 22,534 cycles

ALL EMERGENCY LIGHTS INOP FROM MID CABIN AND AFT. SAMC TEXT: WHEN LOCAL AMT ARRIVED AT AIRCRAFT, ALL EMERGENCY LIGHTS WERE OFF. TURNED EMERGENCY LIGHT SW ON, AND ALL EMERGENCY LIGHTS WERE INOP FROM OVERWING TO AFT OF CABIN. SUSPECT BATTERY PACKS DEPLETED AND NEED TO BE RECHARGED. EMERGENCY LIGHTS ND TO BE TROUBLESHOT AND CORRECTED. SUSPECT S10295 OR S10035. FOUND EMERGENCY LIGHTS CONTROL SWITCH IN FLIGHT DECK WITH DIRTY CONTACTS, LIGHT WOULD COME ON INTERMITTENTLY WHILE IN ARM POSITION. CLEANED CONTACTS AND CHECKED SEVERAL TIMES. NO DEFECTS NOTED. NOTE: AIRCRAFT EMERGENCY LIGHTS SYSTEM CHECKED GOOD AND BATTERIES HAVE BEEN CHARGED IN ACCORDANCE WITH MM. FLIGHT DECK EEL SWITCH PCN 563-1457 IF REQUIRED.

Part: FEEDER CABLE — FAULTED (EMERGENCY LIGHTS) · airframe 60,573 hrs · 22,504 cycles

FOUND EMERGENCY LIGHT INOPERATIVE IN FRONT OF AFT LAV. REPLACED FEED CABLE PER WDG.

Part: CONTROL SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 60,573 hrs · 22,504 cycles

REPLACED EMERGENCY LIGHT CONTROL SWITCH IN AFT ATTENDANT PANEL (S10579), TEST PER MM. OPS CHECKED OK.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 60,573 hrs · 22,504 cycles

DUE TO EMERGENCY LIGHTS ILLUMINATED FOR INDETERMINATE AMOUNT OF TIME, ELECTRICAL POWER SHOULD REMAIN ON AIRCRAFT. BATTERIES WILL BE FULLY CHARGED DUE TO TIME TABLE CHART. REPLACED FEEDER LINE IN AFT SECTION OF ACFT. OPS CHECKED EMERGENCY LIGHTS, SYS OPS NORMAL. ACCOMPLISHED OPS CHECK OF EMERGENCY LIGHT SYS OPS NORMAL. ACCOMPLISHED EMERGENCY LIGHT TEST, SYS OPS NORMAL.

Part: FIRE DETECTOR — CONTAMINATED (AFT CARGO BAY) · airframe 60,236 hrs · 22,386 cycles

AFT CARGO PIT FIRE DETECTOR AIR SAMPLING ORIFICE INBD OF CARGO DOOR CLOGGED, CLEANED ORIFICE. DETECTOR WITHIN TOLERANCE.

Part: CAP — DISLODGED (EMERGENCY LIGHT) · airframe 59,877 hrs · 22,240 cycles

EMERGENCY ESCAPE PATH LIGHTING END CAPS FELL OFF AT 9C AND AT FRONT OF F/C NEAR BARRIER. REPLACED EMERGENCY LIGHT STRIP END CAPS.

Part: SWITCH — LOOSE (EMERGENCY LIGHT) · airframe 58,383 hrs · 21,674 cycles

EMERGENCY LIGHT SWITCH VERY LOOSE. SECURED EMERG LIGHT SW FLT DECK. CHECKS OK.

Part: LIGHT — OBSTRUCTED (AFT LAV STRIP) · airframe 57,597 hrs · 21,371 cycles

DURING 'A' CHECK FOUND AFT LAV EMERGENCY LIGHT STRIP COVER WITH CARPET. TRIMMED CARPET FOR EMERGENCY LIGHTS, SPLICED CUT POWER FEEDER WIRE, EMERGENCY LIGHTS OPERATES NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,597 hrs · 21,371 cycles

NR 4 LT SERVICE ENTRY DOOR EMERGENCY LIGHT IS INOPERATIVE. REPLACED LAMP. OPS CHECKED GOOD.

Part: LIGHT — OBSTRUCTED (MID CABIN AREA) · airframe 57,597 hrs · 21,371 cycles

DURING 'A' CHECK FOUND MID CABIN EMERGENCY LIGHT COVERED WITH CARPET. TRIMMED CARPET FOR EMERGENCY LIGHT STRIP, EMERGENCY LIGHT OPERATES NORMAL.

Part: TRIM SYSTEM — UNKNOWN · airframe 68,101 hrs · 19,815 cycles

RUDDER TRIM BEYOND LIMITS. CHECKED FOR FLOATING SPOILERS. FOUND RT AILERON DOWN .3 ADJUST AILERON PCU IAW MM TO .060 DOWN. CHECKED RIG OF RATIO CHGER AND PCU'S. RATIO CHANGER CKD GOOD. BROUGHT RUDDER IN RIG BY ADJUSTING PCU'S. RUDDER CENTERED .050 DIFF WHEN GOING TO HIGH SPEED FROM LOW AND BACK. CHECKS GOOD IAW MM. INSPECTED DISTURBED COMPONENTS & VERIFIED PROPER OPERATION. FOUND IN AIRWORTHY CONDITION.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 57,046 hrs · 21,160 cycles

EMERGENCY LIGHT NEEDS END CAPS AT SEATS 6B AND 13C. RESPLICED EMERGENCY LIGHT STRIP.

Part: CHARGER — FAILED (APU BATTERY) · airframe 56,242 hrs · 20,840 cycles

L GEN FAILURE & APU AUTO SHUTDOWN, RTFL (TWICE). APU BATTERY CHARGER VOLT FLUX. REPLACED APU BATTERY CHARGER (P/N 4-254-02, S/N 57). DUE TO (2) APU AUTO SHUTDOWNS APU NEEDS TO BE REPLACED. REPLACED APU. OPS CHECK NORMAL. IDG IS LEAKING ON NR 1 ENGINE AFTER IDLE RUN. DISCONNECTED IDG. REPLACED IDG. LEAK CHECK AND OP CHECK GOOD.

Part: GUARD — BROKEN (LIGHT SWITCH) · airframe 55,397 hrs · 20,527 cycles

EMERGENCY LIGHT SWITCH GUARD BROKEN ON OVERHEAD PANEL. REPLACED GUARD.

Part: CARTRIDGE — OUT OF TOLERANCE (EVAC SLIDE) · airframe 55,363 hrs · 20,518 cycles

NEED TO REPLACE THE LT OVERWING SLIDE MASTER CONTROL VALVE SQUIB. REPLACED THE LT UNFIRED MASTER CONTROL VALVE SQUIB. ACP SQUIB TEST, OPS CHECKED GOOD.

Part: LIGHT — FAULTY (DOOR 2R EXTERIOR) · airframe 55,295 hrs · 20,496 cycles

DOOR 2R EXTERIOR EMERGENCY LIGHT DID NOT TEST. FOUND DOOR 2 RIGHT SLIDE LIGHT OPERATING NORMALLY.

Part: TERMINAL — BROKEN (CIRCUIT BREAKER) · airframe 55,238 hrs · 20,470 cycles

AFTER TAKE OFF CREW REPORTED, RT FWD FUEL BOOST PUMP AND LEFT FUEL OVERRIDE AND FWD EQUIPMENT COOLING 1 CB POPPED. TERMINAL BROKE AT L. GEN BKR C901 TERM L-3. REPLACED LUG ON LEFT GENERATOR BREAKER C901, WIRE W2018-0003-06. ALL SYSTEMS OPERATE NORMALLY.

Part: SWITCH — FAULTY (CABIN) · airframe 53,563 hrs · 19,812 cycles

AFTER ENG START AND TAXI FOLLOWING EMERGENCY EXIT LIGHTS CAME ON WITH SW ARMED: EEL ROW 16-24, RANDOM STOW BIN LIGHTS FROM ROW 16-33, & DOOR 3L&R SIGNS. NOTHING FWD OF OVERWING EXITS TO COCKPIT CAME ON. FOUND ABOVE LIGHTS WERE PART OF AFT EMER TEST LIGHT SW CIRCUIT. REPLACED DOOR 3L EMER LIGHT TEST SWS 10295, ALL EMER LIGHTS TEST OK. RAN ENGS AND ACCOMPLISHED TAXI TEST, UNABLE TO DUPLICATE.

Part: SWITCH — FAULTY (EMERGENCY LIGHTS) · airframe 53,563 hrs · 19,812 cycles

AFTER ENG START AND TAXI FOLLOWING EMERGENCY EXIT LIGHTS CAME ON WITH SW ARMED: EEL ROW 16-24, RANDOM STOW BIN LIGHTS FROM ROW 16-33, & DOOR 3 LT &RT SIGNS. NOTHING FWD OF OVERWING EXITS TO COCKPIT CAME ON. FOUND ABOVE LIGHTS WERE PART OF AFT EMER TEST LT SW CIRCUIT. REPLACED DOOR 3L EMER LT TEST SW S 10295, ALL EMER LIGHTS TEST OK. RAN ENGS AND ACCOMPLISHED TAXI TEST, UNABLE TO DUPLICATE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 53,453 hrs · 19,766 cycles

EMERGENCY LIGHT PROBLEM DISCOVERED ON 1SV. REPLACED POWER SUPPLY M10818, M10817 AND BATTERY PACKS FOR BOTH POWER SUPPLIES.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 53,453 hrs · 19,766 cycles

EMERGENCY LIGHT PROBLEM DISCOVERED ON 1SV. REPLACED POWER SUPPLY M10818, M10817 AND BATTERY PACKS FOR BOTH POWER SUPPLIES.

Part: LIGHT — SHORTED (EXTERIOR) · airframe 53,451 hrs · 19,765 cycles

DOOR 2R AND PARTS OF AFT CABIN EMERGENCY EXIT LIGHTS ARE ON. REPLACED SHORTED BULB FOR DOOR 2 RIGHT EXTERNAL EMERGENCY LIGHT AND REPLACED INOP BATTERY PACK AT STA LOC 1240 ITEM M10699 REF WDM 33-51-14 PG 1 AND MM 33-51-06 AND MM 33-51-07. SYS CHECKED NORMAL.

Part: LIGHT — SHORTED (EXTERIOR) · airframe 53,451 hrs · 19,765 cycles

DOOR 2R AND PARTS OF AFT CABIN EMER EXIT LIGHTS ARE ON. REPLACED SHORTED BULB FOR DOOR 2 RIGHT EXTERNAL EMERGENCY LIGHT AND REPLACED INOP BATTERY PACK AT STA LOC 1240 ITEM M10699 REF WDM 33-51-14 PG 1 AND MM 33- 51-06 AND MM 33-51-07. SYS CHECKD NORMAL.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 53,258 hrs · 19,695 cycles

OXYGEN PRESSURE 480. FOUND LEAK AT FIRST OBSERVER'S O2 MASK. REPLACED & LEAK CHECKED OKAY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,032 hrs · 19,610 cycles

AFT OF WING LT EMERGENCY LIGHT INOP. FOUND LAMP INOPERATIVE. RELAMPED- OPS CHECKED GOOD.

Part: LIGHT — UNSECURE (L2 DOOR) · airframe 52,638 hrs · 19,464 cycles

EXIT LIGHT DOOR 2L NEEDS RE-ATTACH. *S/D* REPLACED EXIT SIGN, OPS CHECKED GOOD.

Part: MICROPHONE — DEFECTIVE (CAPTAIN'S) · airframe 52,528 hrs · 19,428 cycles

CAPT HAND MIC DEFECTIVE. SHORTED MIC. REPLACED CAPT HAND MIC ASSY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,656 hrs · 18,718 cycles

EEL LIGHT OUT ADJACENT TO FWD GALLEY. REATTACHED ELL LIGHT ASSY- OPS CHECKS NORMAL.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 49,618 hrs · 18,356 cycles

INTERIOR EMERGENCY LIGHTS ON (DOORS 3 RT & LT INTERMITTENT EXIT PATH) WITHOUT MANUAL ACTIVATION. REPLACED INBOARD BATTERY PACK AT STATION 1680.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 49,447 hrs · 18,295 cycles

VARIOUS EMERGENCY EXIT LIGHTS ARE ON AND WILL NOT TURN OFF WITH SWITCHES. FLOOR LIGHTS AT ROWS 23-31 AND CEILING AT 14-23. ACCOMPLISHED TEST OF EACH SECTION AND ALL LIGHTS TEST.

Part: BOTTLE — READS LOW (R1 DOOR ASSIST) · airframe 48,403 hrs · 17,922 cycles

DOOR 1R ASSIST BOTTLE HAS LOW AIR PRESSURE. [06-14-07] REPLACED BOTTLE.

Part: FILTER — CLOGGED (HYDRAULIC SYS) · airframe 48,236 hrs · 17,865 cycles

LANDED UNDER AMBER ALERT DUE TO LOSS OF LEFT HYDRAULIC PRESSURE. REPLACED EDP FILTER MODULE ELEMENT IN LEFT TAIL SAIL AREA. CLEANED AREA AND SERVICED HYDRAULIC SYSTEM AND OPERATED FLIGHT CONTROL SYSTEM FOR FINAL TESTING.

Part: GIRT BAR — LACK OF LUBE (DOOR 3L) · airframe 48,150 hrs · 17,828 cycles

THE 3L DOOR WILL NOT DISARM. [SUP 05-18-07] LUBED GIRT BAR, OP'S CHECKED NORMAL ON GROUND. FOUND WATER UNDER GIRT BAR AREA INDICATING POSSIBLE ICE BUILD-UP IN THE AREA.

Part: LINE — BROKEN (FUEL SYSTEM) · airframe 47,463 hrs · 17,570 cycles

LT MAIN TANK TRANSFERRED INTO C TANK. L TANK TRANSFERRED APPROX 100 LBS EVERY 20 MINS INTO CTR TANK. SUPPLEMENTAL DATA UPDATE NOTED THAT TRANSFER IS CONSISTENT THROUGHOUT FLIGHT REALM AT APPROX 300 LBS PER HR AND EVENTUALLY CAUSED A CONSISTENT IMBALANCE BETWEEN LEFT AND RT TANK. FUEL QTY INDICATION OKAY AND NO FUEL QTY FAULTS. REPLACED BROKEN FUEL SCAVENGE LINE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,707 hrs · 16,182 cycles

EMERGENCY FLOOR PROX LIGHTS INOPERATIVE FROM ROWS 31 THROUGH ROW 34. REPLACED POWER SUPPLY M10817.

Part: CONNECTOR — DAMAGED (LT IDG) · airframe 40,568 hrs · 14,963 cycles

DIVERTED DUE TO LEFT 115V AC BUS VOLTAGE PULSATING. *S/D* REPLACED LEFT INTEGRATED DRIVE GENERATOR (IDG). SHOP FINDINGS: DAMAGED IDG CONNECTOR AND DAMAGED TERMINAL T2.

Part: VIBRATOR — MALFUNCTIONED (ALTIMETER) · airframe 40,117 hrs · 14,813 cycles

FLIGHT DIVERTED TO ORD WITH A STANDBY ALTIMETER VIBRATOR.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,073 hrs · 14,791 cycles

AFT PIT FRAME DENTED STA 1440, BETWEEN STR 25L AND 28L. *S/D* MAJOR REPAIR ACCOMPLISHED. TYPICAL DAMAGE TO THE AFT PIT FRAMES DUE TO CARGO LOADING. INSTALLED DOUBLER REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,073 hrs · 14,791 cycles

FUSELAGE SKIN AND DOUBLER DENTED AT STA 600 STR 19L IN 3 PLACES ON SKIN AND ONE ON DOUBLER. INSTALLED SKIN SPLICE REPAIR WITH DOUBLER, SPLICE DOUBLERS AND FILLERS.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,073 hrs · 14,791 cycles

FWD PIT FRAME DENTED AT STA 580 STRINGER 25L. MAJOR REPAIR ACCOMPLISHED. TYPICAL DAMAGE TO THE FORWARD PIT FRAMES DUE TO CARGO LOADING. CUT OUT DAMAGE & INSTALLED NESTED ANGLE REPAIR OUTSIDE FRAME SECTION.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 40,073 hrs · 14,791 cycles

DURING ACCOMPLISHMENT OF A SKIN SPLICE REPAIR FROM BS 590 TO BS 640, DAMAGE TO STR 16L WAS FOUND IN THIS AREA. SKIN AND STRINGER DAMAGE CAUSED BY TYPICAL JETWAY DAMAGE. NEW SECTION OF STRINGER WAS SPLICED IN FOR REPAIR PURPOSES.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,073 hrs · 14,791 cycles

AFT PIT FRAME UPPER FLANGE DENTED AT BS 1420 STR 26L. MAJOR REPAIR ACCOMPLISHED. TYPICAL AFT PIT FRAME DENT DAMAGE FROM CARGO LOADING. INSTALLED J-ANGLE DOUBLER.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,073 hrs · 14,791 cycles

AFT PIT FRAME UPPER FLANGE DENTED AT BS 1600 STR 25L. MAJOR REPAIR ACCOMPLISHED. TYPICAL AFT PIT FRAME DENT DAMAGE FROM CARGO LOADING. INSTALLED J-ANGLE DOUBLER.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,073 hrs · 14,791 cycles

AFT PIT FRAME UPPER FLANGE DENTED AT BS 1500 STR 26L. MAJOR REPAIR ACCOMPLISHED. TYPICAL AFT PIT FRAME DENTS FROM CARGO LOADING. INSTALLED J-ANGLE REPAIR.

Part: SPAR — DAMAGED (WING) · airframe 40,073 hrs · 14,791 cycles

DAMAGE FOUND AT WBL 265 WING FRONT SPAR AT THE DRY BAY ACCESS HOLE NUT PLATE ATTACHMENT. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED FREEZE PLUGS IN 3 HOLES AND INSTALLED NEW DOUBLER.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,073 hrs · 14,791 cycles

AFT PIT FRAME DENTED AT BS 1600 STR 26R. MAJOR REPAIR ACCOMPLISHED. TYPICAL AFT PIT FRAME DENTS FROM CARGO LOADING. INSTALLED J-ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,073 hrs · 14,791 cycles

AFT PIT FRAME UPPER FLANGE DENTED AT BS 1540 STR 26L. MAJOR REPAIR ACCOMPLISHED. TYPICAL AFT PIT FRAME DENTS FROM CARGO LOADING. INSTALLED J-ANGLE DOUBLER.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,073 hrs · 14,791 cycles

AFT PIT FRAME UPPER FLANGE DENTED AT BS 1400 STR 26L. MAJOR REPAIR ACCOMPLISHED. TYPICAL AFT PIT FRAME DENTS FROM CARGO LOADING. INSTALLED J-ANGLE REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,073 hrs · 14,791 cycles

CABIN FLOORBEAM CAP AT BS 1640 RBL 51 TO RBL 60 IS CORRODED BEYOND ALLOWABLE LIMITS. MAJOR REPAIR ACCOMPLISHED. TYPICAL FLOOR STRUCTURE CORROSION. INSTALLED STRAP REPAIR.

Part: FAN · airframe 32,291 hrs · 11,933 cycles

ACRID ODOR IN THE CABIN. SUPPLEMENTAL DATA UPDATE RIGHT RECIRCULATION FAN INOP. REPLACED RECIRCULATION FAN.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 29,569 hrs · 10,946 cycles

FUSELAGE SKIN PUNCTURED STA 1816 STR 21R. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER.

Part: SHAFT — TWISTED (BOTTLE VALVE)

DURING SHOP OVERHAUL OF SLIDE, REMOVED FOR TIME EXPIRATION. THE SLIDE FAILED TO INFLATE TO MANUFACTURER'S SPECIFICATIONS. UPON DISASSEMBLY OF THE BOTTLE VALVE THE SHAFT WAS FOUND TO BE TWISTED. *S/D* REPLACED BOTTLE VALVE.