N342AX

Part: O-RING — CUT (STARTER ASSY) · airframe 97,923 hrs · 17,559 cycles

RIGHT ENGINE OIL PRESSURE IN CAUTION RANGE AT TOP OF CLIMB. RIGHT ENGINE OIL QUANTITY ZERO. SHUT DOWN ENGINE AT OIL PRESSURE IN THE RED.

Part: DRIVE UNIT — FAILED (WX RADAR) · airframe 97,452 hrs · 17,434 cycles

BOTH WX RADARS FAILED IN FLIGHT - REMOVED AND REPLACED WX RADAR ANTENNA AND R WX (?) IAW B763 AMM CHP 34-43 OPS CHECKS GOOD

Part: EEC — FAILED · airframe 94,550 hrs · 16,715 cycles

R ENG CONTROL STATUS MESSAGE. RIGHT ENGINE EEC PWR CH B CIRCUIT BREAKER POPPED. CORRECTIVE ACTION: R&R R ENGINE ECU IAW AMM 73-21-15 OPS CHECK GOOD

Part: PROCESSOR — INTERMITTENT (FUEL QTY) · airframe 89,362 hrs · 15,575 cycles

STATUS MESSAGE FUEL QTY IND L MAIN INDICATOR BLANK, RETURNED AND WENT BLANK SEVERAL TIMES. CORRECTIVE ACTION: TROUBLSHOT PER FIM 28-41 FAULT TREE 851 RANG OUT HIZ WIRES TO FTYS, NO DEFECTS FOUND. INSPECTED WIRING BEHIND FUEL QTY PROCESSOR BULK HEAD RACK NO DEFECTS FOUND. SUMPED L/WING TANK FUEL SYSTEM IAW B767 28-00 AND 12-11. REPLACED FUEL QTY PROCESSOR UNIT IAW B767 AMM 28-41 OPS CHK GOOD

Part: ACTUATOR — LEAKING (RT ELEVATOR) · airframe 87,163 hrs · 15,111 cycles

CENTER HYDRAULIC QUANTITY EICAS IN FLIGHT DROPPED TO 0.33 WITH CENTER SYSTEM TURNED OFF . CORRECTIVE ACTION: FOUND RH INBOARD ELEVATOR PCA LEAKING. REMOVED AND REPLACED RH INBOARD ELEVATOR PCA IAW B767 AMM 27-31-05. OPS AND LEAK CHECK GOOD AT THIS TIME.

Part: IDG — DISCONNECTED (RIGHT) · airframe 80,011 hrs · 13,656 cycles

INFLIGHT THE RT IDG DRIVE LIGHT ILLUMINATED FOLLOWED BY RT GENERATOR CONTROL LIGHT EICAS MESSAGES RT GEN DRIVE & RT GEN OFF. DRIVE DISCONNECTED IAW CHECKLIST. C/W FIM 24-20, FT 801 AND 24-20, TASK 804 SYSTEM IS OK. SERVICED RT IDG IAW AMM 12-13 C/W FIM 24-20 FT 813. NO CORROSION OR WEAR NOTED. C/W LOAD TEST IAW AMM 24-11-00. NO DEFECTS NOTED. 2 LEGS LATER DRIVE LIGHT REAPEARED AND, R & R RIGHT ENGINE IDG IAW AMM 24-11 AND WORK CARD 24-R04 AND WC 24-003-01. OPS CHECKED GOOD. NO DEFECTS NOTED. NO LEAKS NOTED.

Part: OVEN — FIRE (GALLEY) · airframe 77,185 hrs · 13,090 cycles

AFTER LEVEL OFF, F/A REPORTED FIRE IN AFT NR 3 GALLEY OVEN. PERFORMED INSPECTION OF AFT GALLEY OVEN. FOUND FOOD TRAYS AND FOOD BURNED. COMPLIED WITH OPS CHECKS OF OVEN NR 3 AND NR 1, 2, 4 AND NR 5 OVENS IAW CMM 25-36-22, NO FAULTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: LANYARD — INOPERATIVE (SLIDE) · airframe 76,395 hrs · 12,910 cycles

DURING OPS CHECK OF ESCAPE SLIDE SYSTEM, ESCAPE SLIDE OPERATED AS REQUIRED, BUT THE SLIDE LIGHTS DID NOT ACTIVATE DURING REVIEW. IT WAS FOUND THAT THE ACTIVATION LANYARD APPEARED TO BE TOO LONG WHEN THE SLIDE WAS FULLY DEPLOYED TO ACTIVATE THE LIGHTS. REPLACED SLIDE/RAFT ASSY IAW AMM 25-66-00/201.

Part: CONTROL PANEL — FAILED (ILS) · airframe 75,081 hrs · 12,629 cycles

ILS TUNING KNOB NOT SECURE. SLIGHT BUMP WILL CHANGE COURSE BY 10 DEGREE. UNABLE TO PROCEED WITH ETOPS FLIGHT. R & R ILS CONTROL PANEL IAW MM 34-31. OPS CHECKS GOOD.

Part: WIRE HARNESS — SHORTED (ENGINE) · airframe 72,118 hrs · 12,040 cycles

OIL TEMP INDICATING SYSTEM OIL TEMP LT ENGINE HIGH, OIL PRESSURE NORMAL. SHUTDOWN LT ENGINE IAW QRH. R & R NR1 ENGINE SEC IAW AMM 73-21 (GROUND TEST OF EEC CHECKED OK AT THIS TIME) R & R ECM CABLE W13 IAW GE ESM 72-00, R & R NR 1 ENG OIL TEMP SENSOR REF AMM 79-34, RAN NR 1 ENG IAW AMM 72-00 OIL TEMP CK'S NORMAL AT THIS TIME, LEAK CK OF SENSOR GOOD.

Part: ENGINE — OVERTEMP (LEFT) · airframe 72,070 hrs · 12,030 cycles

TEMP LT ENGINE HIGH 179 ON BOTH LT AND RT EICAS COMPUTERS QRH FOLLOWED THRUST ON LT ENGINE REDUCED TO IDLE DUE TO OTHER INDICATIONS NORMAL ENGINE SHUTDOWN AND SECURE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 68,572 hrs · 11,390 cycles

RIGHT 2ND FROM AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT ASSY, OPS CHECK NORMAL AT THIS TIME IAW AMM 33-51.

Part: CHARGER — DEFECTIVE (EMERGENCY LIGHTS) · airframe 68,572 hrs · 11,390 cycles

LEFT 3RD FROM AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R BATTERY CHARGER. OPS CHECK NORMAL AT THIS TIME IAW AMM 33-51.

Part: BRACKET — CORRODED (BS 1197) · corrosion level 2 · airframe 68,243 hrs · 11,328 cycles

BRACKET CORRODED AT FS 1197, S 6 LT. R & R BRACKET AT FS 1197, STR 6L IAW SRM 51-40-02-0G-0 PARA 7.D.

Part: FITTING — CORRODED (LAVATORY) · corrosion level 2 · airframe 68,243 hrs · 11,328 cycles

LOWER PORTION OF LAV "E" IS CORRODED AROUND TIE DOWN AREAS (AFT SIDE). MFG END WALL FITTING IAW ESO 25-34. ALODINED FITTING IAW MM 51-21-04. PRIMED FITTING IAW MM 51-21-10. INSTALLED HELICOILS IAW SOPM 20-50-22 REV 5 INSTALLED END WALL FITTINGS IAW CMM 25-40-81, PG 629. LAYED UP AND CURED FIBERGLASS .

Part: STRINGER CLIP — CORRODED (BS 1285) · corrosion level 2 · airframe 68,243 hrs · 11,328 cycles

ANGLE CORRODED AFT OF FRAME RT FS 1285 AT FLOOR LINE. REMOVED CORRODED ANGLE FOR REPLACEMENT-FABRICATED NEW STRINGER CLIP IAW DWG 146T1510. INSTALLED NEW STRINGER CLIP IAW SRM 51-40-02, PAR 7.

Part: ATTACH ANGLE — CORRODED (BS 742) · corrosion level 2 · airframe 68,243 hrs · 11,328 cycles

STA 742, UPPER ATTACH ANGLE FOR CURTAIN CORRODED AT CURTAIN ATTACH POINTS. REMOVED UPPER ATTACH ANGLE AT STA 742FLC IAW SRM 51-40-02-06-0, PARA 4, FABRICATED NEW UPPER ATTACH ANGLE IAW DWG NR453T1742 INSTALLED NEW ATTACH ANGLE IAW SRM 51-40-02-06-0, PARA 4.

Part: STRAP — CORRODED · corrosion level 2 · airframe 68,243 hrs · 11,328 cycles

FLOORBEAM CORRODED JUST INBD OF R2 CUT OUT. REMOVED AND FABRICATED AND REPLACED FLOOR SUPPORT GUSSET STRAP IAW SRM 51-40-02 PARA 4 & 7.

Part: FRAME — CORRODED (BS 1270) · corrosion level 2 · airframe 68,243 hrs · 11,328 cycles

RIGHT FS 1270 FRAME CORRODED AT BASE. REMOVED CORROSION BLENDED AREA BEYOND LIMITS IAW SRM 53-00-15, FIG 101, PG 113, DETAIL XII. INSPECTED AREA IAW NDT PART 4 51-00-10, FOUND THICKNESS AROUND BLEND TO BE .175 . REPAIRED AREA IAW EO B7653-04.

Part: FITTING — GOUGED (AILERON) · airframe 68,243 hrs · 11,328 cycles

INBD AILERON OTBD UPPER END HEAVILY GOUGED BY T/E SEAL. R & R FAIL-SAFE FITTING IAW SRM 51-40-02.

Part: ANGLE — CORRODED (BS 1329) · corrosion level 2 · airframe 68,243 hrs · 11,328 cycles

ANGLE CORRODED RT FS 1329 ON MOST OTBD WEB (M). BLENDED AREA OUT OF LIMITS IAW SRM 53-00-15, FIG 101, PG 113, DETAIL XII. REPAIRED AREA IAW SRM 51-70-11, FIG 1, PG 6 USING 7075-T6, .050.

Part: FLOORBEAM — CORRODED (BS 1480) · corrosion level 2 · airframe 68,243 hrs · 11,328 cycles

FLOORBEAM AT STA 1480, RBL 48-57 IS CORRODED ON UPPER FLANGE. AREA UNDER F4 LAV. REPAIRED CORRODED FLOORBEAM IAW REA 46824, REA 01.

Part: FLOOR PANEL — CORRODED (LAVATORY) · corrosion level 2 · airframe 68,243 hrs · 11,328 cycles

F1 LAV FLOOR STRUCTURE CORRODED ON INBD SIDE. REPAIRED DAMAGED AREA IAW SRM 53-00-51, REPAIR 1.

Part: FLOORBEAM — CORRODED (BS 1518) · corrosion level 2 · airframe 68,243 hrs · 11,328 cycles

FLOORBEAM AT FS 1518 AND BL -0- IS CORRODED AT LOWER END. REPAIRED LOWER FLANGE OF FLOORBEAM, PN 146T5143-1 IAW SRM 51-70-12, REF RFTS T-46825. REMOVED NUTPLATES ON FLOORBEAM AT STA 1518 AT LOCATION 12L AND 24L. REMOVED CORROSION. REMOVED CORROSION IAW SRM 53-00-51/101, DETAIL 1.

Part: FLOORBEAM — CORRODED (BS 287) · corrosion level 2 · airframe 68,243 hrs · 11,328 cycles

FLOORBEAM UPPER FLANGE IS CORRODED ON UPPER SURFACE AT BS 287, APPROX BL 48. CUTOUT DAMAGED FLOORBEAM IAW SRM CH 53-00-51, FIG 201. EDDY CURRENT INSP. REQUIRED-EDDY CURRENT CUTOUT AREA IAW NDT MANUAL PART 6 51-00-19. NO DEFECTS NOTED. FLOORBEAMS REQUIRES REPAIR. REPAIRED FLOORBEAM IAW SRM 53-00-51 REPAIR I.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 67,780 hrs · 11,250 cycles

BIRD STRIKE ON RT WING OTBD FLAP LOWER SURFACE OTBD OF INBD FLAP VORTELON BY 42" AND 10" FROM T/E WITH SURFACE CRACK 9" PARALEL TO SEAM. DENT AREA 5" RND. R & R RT OTBD FLAP IAW MM 27-11 & SB 767-27A0155.

Part: STRUCTURE — DAMAGED (RT MLG STRT DOOR) · airframe 67,225 hrs · 11,146 cycles

ON POST FLIGHT WALKAROUND INSP, FOUND RT STRUT GEAR DOOR DETATCHED FROM MOUNTS AND DAMAGED ALSO CAUSING DAMAGE TO TRUNNION DOOR. SHOCK STRUT DOOR & TRUNNION DOOR REPLACED REF SAL MX ORDER 152030292C4-0010 FOR WORK PERFORMED AND CERTIFICATION FOR RTS IAW LOG.

Part: IRU — INACCURATE · airframe 65,324 hrs

C IRS FAULT LIGHT ON LOCALIZER MAP WAS 7.5 MILES LT 34-21-1 SIT NR 3 NOTE( R IRS PREVIOUSLY DEFERRED). REPLACED CTR IRU IAW MM 34-21. OPS CHECK GOOD TEST NR 40, ALSO ACC.

Part: SLIDE — PARTIAL INFLATE (L1 DOOR) · airframe 64,536 hrs · 10,680 cycles

L-1 DOOR DID NOT OPEN FULLY DURING SLIDE DEPLOYMENT. OPS CKD L-1 DOOR DURING SLIDE DEPLOYMENT WITH FAA CKS GOOD.

Part: LIGHT — BURNED OUT (ESCAPE SLIDE) · airframe 64,536 hrs · 10,680 cycles

R-2 SLIDE LIGHTS DID NOT OPERATE WHEN SLIDE WAS DEPLOYED. R-2 DOOR SLIDE REPLACED ON LOG PAGE 92473 ITEM 4 (REPLACED R-2 SLIDE IAW W/C 76SWF-002).

Part: COVER — MISSING (RT ENGINE) · airframe 64,536 hrs · 10,680 cycles

OIL QTY AND PRESSURE LOSS ON RT ENG, NO TEMP OR ENG EXCEEDENCES, NO INFLIGHT SHUTDOWN. OIL PRESSURE DROPPED TO 10 PSI PRIOR TO RT ENG SHUTDOWN. FOUND CRANK PAD COVER NOT INSTALLED. INSTALLED CRANK PAD COVER IAW 72-00-00-982-007-H00. PERFORMED NO OIL PRESSURE INSP IAW AMM 72-00-00-206-096-H00. NO DEFECT NOTED.