N652GT

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 88,170 hrs · 27,014 cycles

ON APPROOACH RECEIVED TRAILING EDGE FLAP DISAGREE MESSAGE. PERFORMED GO AROUND, DECLARED EMERGENCY AND LANDED WITHOUT ANY INCIDENTS.

Part: WARNING MESSAGE — FALSE ACTIVATION (SLAT ASYM) · airframe 87,621 hrs · 26,654 cycles

ON APPROACH TO CVG AT 4,000 FEET SELECTED FLAPS TO POSITION 1 AND RECEIVED A LE SLAT ASYM MESSAGE. DECLARED AN EMERGENCY AND CONTINUED THE APPROACH. LANDED AIRCRAFT WITHOUT FURTHER INCIDENT. FLAP/SLAT SYSTEM OPERATED NORMALLY WITH NO MESSAGES AFTER LANDING.

Part: FLAP TRACK — WORN (LT WING) · airframe 87,614 hrs · 26,650 cycles

OUTBOARD FLAP TRACK SUPPORT BEAMS NO.'S 1, 2, 7, AND 8 ATTACHMENT HOLES BUSHING REPAIR.

Part: STRUT — CRACKED (ZONE 400) · airframe 87,614 hrs · 26,650 cycles

ENG NO. 2 PYLON RH STRUT SIDE AFT TRAPEZOIDAL ACCESS DOOR CRACKED.

Part: FRAME — DAMAGED (NACELLE) · airframe 87,614 hrs · 26,650 cycles

ENG INBD COWLING FRAME DAMAGE

Part: STIFFENER — WORN (NACELLE) · airframe 87,614 hrs · 26,650 cycles

ENG NO. 2 LH INBOARD THRUST REVERSER STIFFENER DAMAGED

Part: PRESSURE BLKHD — DENTED (BS 1582) · airframe 87,614 hrs · 26,650 cycles

FUSELAGE SECT 48, AFT PRESSURE BULKHEAD AT F.S. 1582 AROUND 9 O'CLOCK POSITION DENT REPAIR.

Part: FLOORBEAM — CORRODED (BS 347 RBL55-89) · airframe 87,614 hrs · 26,650 cycles

FUSELAGE SECTION 41, FLOOR BEAM AROUND F.S. 347 BETWEEN RBL 54.75 - 88.5 CORROSION OUT OF LIMITS.

Part: SKIN — DAMAGED (BS 632-654 S25L) · airframe 87,614 hrs · 26,650 cycles

FUSELAGE SECT 43 AT FUSLEAGE SKIN BETWEEN F.S. 632-654 AT STR 25 LH ELONGATED HOLE.

Part: FITTING — DAMAGED (RT WING TE FLAP) · airframe 87,614 hrs · 26,650 cycles

RH WING INBOARD FLAP-OUTBOARD LINKAGE FITTING BLEND OUT REPAIR.

Part: FLOORBEAM — CORRODED (BS 228 LBL11-26) · corrosion level 3 · airframe 87,614 hrs · 26,650 cycles

FUSELAGE SECTION 41, FLOOR BEAM AROUND F.S. 228 BETWEEN LBL 11-26 CORROSION FOUND OUT OF LIMITS.

Part: KEELBEAM — CORRODED (ZONE 100) · airframe 86,456 hrs · 25,874 cycles

CORROSION ON RH KEEL BEAM INBOARD LOWER CHORD AT STA 1032 AND 1072, LBL10.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 85,188 hrs · 24,932 cycles

R/H WING UPPER SURFACE HAS CORROSION AROUND OVERWING FUELING CAP HOUSING.(<P>EVALUATED RH OVERWING FUEL PORT AND FOUND OUT OF LIMITS IAW B767 SRM 57-20-01-1A-1. REPAIRED RH OVERWING FUEL PORT IAW FAS EA 21026 REV. IR.</P>)

Part: PANEL — BROKEN (THRUST REVERSER) · airframe 85,188 hrs · 24,932 cycles

#1 ENG. BOTTOM THRUST REVERSER LOUVERED EXHAUST DOOR JUST AFT OF LT T/R HAD 2 SQ IN BROKEN OFF SECTION.(<P>REPAIRED #1 OB TR BOTTOM SECTION TE IAW FAS EA 21024 REV. IR</P>)

Part: SKATE ANGLE — CRACKED (NR 1 NACELLE) · airframe 85,188 hrs · 24,932 cycles

#1 ENG PYLON PNL 437DB FWD ATTACH RH SIDE SKATE ANGLE ON BOTTOM OF WING HAS 5IN LENGTH CRACK.(<P>REMOVED DAMAGED SECTION OF SKATE ANGLE AND REPAIRED IAW FAS EA 21027 REV. IR</P>)

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 85,188 hrs · 24,932 cycles

L/WING #4 SLAT EXTERIOR AREA DELAMINATED. EVALUATED #4 SLAT AND FOUND OUT OF LIMITS IAW B767 SRM 51-10-06-0G-0. REPAIRED #4 SLAT TE WEDGE IAW B767 SRM 57-43-02-2R-1</P>)

Part: SKIN — NICKED (RT WING) · airframe 85,188 hrs · 24,932 cycles

RH WING UPPER SKIN WITH SMALL NICK(<P>REPAIRED SMALL NICK ON RH WING IB FLAP UPPER SKIN IAW B767 SRM 57-53-01-2R-1 DET. 1 AND SRM 51-70-17 PER. 4B. REFINISHED SURFACE PROTECTION IAW B767 AMM 51-21-12 AND B767 SRM 57-53-01</P>)

Part: KEELBEAM — CORRODED (BS 990 LBL 8) · corrosion level 2 · airframe 85,188 hrs · 24,932 cycles

KEEL BEAM STA. 990 APPROX. AROUND NUTPLATE CORRODED. REMOVED AND REPLACED KEEL BEAM REPAIR AT STA. 990 LBL8 IAW SRM 53-50-00-2R, 51-40-02-0G-0 AND 51-20-01.

Part: STRINGER SPLICE — CORRODED (BS 1295-1307) · corrosion level 2 · airframe 85,188 hrs · 24,932 cycles

LOWER FUSELAGE HAS ROW OF FASTENERS PULLING THROUGH THE SKIN WITH EVIDENCE OF SKIN PILLOWING BS 1295 TO BS 1307 STRINGER 37L(<P>REMOVED, FABRICATED AND REPLACED STR.37L SPLICE FROM STA.1295 TO STA. 1307 IAW B767 SRM 51-40-02, 51-40-05, DWG. # 146T3003 REV. W, TREATED, PRIMED AND TOPCOATED IAW B767 SRM 51-20-01, AMM 51-20-10. APPLIED CIC IAW 51-24-03</P>)

Part: START VALVE — FAILED (RT ENGINE) · airframe 85,117 hrs · 24,891 cycles

RIGHT STARTER CUTOUT EICAS MSG ON ENGINE START. MOVED TO DMI 141666 PER MEL 80-00-02-01, CAT C, EXP 09FEB21. LP 1335167: R & R START VLV OPS, LEAK CK SATISFACTORY. OK FOR SRV REF AMM 80-11-02. THIS CLEARS MDDR 141666. PLACARD REMOVED.

Part: EADI — MALFUNCTIONED (COCKPIT) · airframe 84,307 hrs · 24,393 cycles

CA PFD, EICAS, FO PFD WENT BLANK. FIRE MARSHALL SMELLED SMOKE IN COCKPIT.(<P>REPLACED CA EADI &AMP; EHSI. REPLACED F/O EADI AND UPPER EICAS SCREENS IAW AMM 31-41-01. CKS GOOD. C/W SMOKE INSPECTION IAW AMM 05-51-56, NO SMOKE/ FUMES PRESENT.</P><P>OFF: P/N 622-7999-003 S/N 109492</P><P>&NBSP; &NBSP; &NBSP; &NBSP; &NBSP;P/N&NBSP;622-7999-003&NBSP; S/N KVXB</P><P>&NBSP; &NBSP; &NBSP; &NBSP; &NBSP;P/N&NBSP;622-7999-003&NBSP; S/N&NBSP;114432</P><P>&NBSP; &NBSP; &NBSP; &NBSP; &NBSP;P/N&NBSP;622-7998-003&NBSP; S/N&NBSP;7PWC</P>)

Part: ESCAPE REEL — NOT REPORTED (MAIN ENTRY) · airframe 83,810 hrs · 24,082 cycles

MAIN ENTRY DESCENT DEVICE NEEDS TO BE REPLACED. REMOVED AND REPLACED MAIN ENTRY DESCENT DEVICE IAW B767 AMM 25-61-03.

Part: ELT — NOT REPORTED (CABIN) · airframe 83,810 hrs · 24,082 cycles

EMERGENCY LOCATOR TRANSMITTER. REMOVED AND REPLACED EMERGENCY LOCATOR TRANSMITTER IAW AMM 25-63-03.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 83,448 hrs · 23,856 cycles

COCKPIT EMERGENCY FLASHLIGHT INOP(<P>REPLACED FLASHLIGHT BATTERY PER AMM 25-60-00&NBSP;</P>)

Part: CONNECTOR — MELTED (COCKPIT) · airframe 83,086 hrs · 23,647 cycles

ELECTRICAL BURNING SMELL ON APPROACH RAN SMOKE/FIRE/FUMES AND SMELL SUBSIDED. PERFORMED ENGINE IDLE RUN IAW AMM 71-00-00 WHILE OPERATING PACKS IAW AMM 21-00-00 NO BURNING SMELL DETECTED. INSPECTED LT AND RT PACKS FOR OIL CONTAMINATIONIAW AMM 21-00-21 NO OIL CONTAMINATION FOUND. OK FOR SERVICE AT THIS TIME CONDITIONAL INSPECTION C/W IAW AMM 05-51-56, UPON FURTHER TROUBLESHOOTING DISCOVERED RIGHT TAXI RUNWAY TURN OFF SWITCH CONNECTOR MELTED AT P5 PANEL. REMOVED AND REPLACED PANEL P/N 233N3214-22 S/N 000028 ON THE P5 PANEL. OPS CHECK GOOD IAW AMM 33-42-00 AND 33-11-00.

Part: FUEL CONTROL — FAULTY (NR 1 ENGINE) · airframe 82,896 hrs · 23,529 cycles

ON TAKE OFF LEFT ENG FAILED TO MAKE TAKE OFF THRUST. TARGET EPR WAS 1.38. LEFT ENGINE DIDNT GO ABOVE 1.31. LEFT EEC EICAS MSG CAME ON JUST OVER 80 KNTS. REJECTED TAKE OFF. REMOVED AND REPLACED NR 1 ENGINE FUEL CONTROL IAW AMM 73-21-01. NO LEAKS DETECTED OPS CHECKED GOOD.

Part: WEB — CRACKED (FUSELAGE) · airframe 82,775 hrs · 23,459 cycles

CRACKED WEB FOUND ON FRAME IN AFT CARGO BY LOWER AREA AT FS 1395, STR 39R, RBL 4.0. PERFORMED WEB REPAIR AT FR STA 1395, STA 39R, RBL 4.0 REF SRM 53-00-07-2R-3 REPAIR 3.

Part: CONTROL VALVE — MALFUNCTIONED (APU) · airframe 82,219 hrs · 23,050 cycles

APU PUT OUT LOW PNEUMATIC PRESSURE 10 PSI. REMOVED AND REPLACED APU SURGE CONTROL VALVE IAW AMM 49-53-01. OPS CHECKED NORMAL.

Part: WARNING MESSAGE — ILLUMINATED (MAIN CARGO DOOR) · airframe 81,610 hrs · 22,605 cycles

MAIN CARGO DOOR WARNING AT FLT 220. NO DECOMPRESSION.

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR) · airframe 81,443 hrs · 22,468 cycles

AFTER TAKEOFF AT APPROX 6000 MASTER WARNING AND MAIN CARGO DOOR LIGHT ILLUMINATED AND REMAINED ON.

Part: FITTING — CRACKED (NR 1 PYLON) · airframe 80,989 hrs · 22,124 cycles

ENG 1 PYLON CLOSEOUT ANGLE INBD, 2ND FASTENER TO OTBD HOLE HAS A CRACK EMANATING FROM HOLE AT NAC STATION 257. PERFORMED REPAIR AT PYLON 1 INBD MID-SPAR FITTING IAW INSTRUCTIONS PROVIDED BY SR 4-3164145989.

Part: UNKNOWN — UNKNOWN (CARGO DOOR) · airframe 80,327 hrs · 21,757 cycles

MAIN DECK CARGO DOOR, FWD 6 LOCK LATCHES SHOWING RED WHEN DOOR IS LOCKED. PERFORMED MAIN DECK CARGO DOOR ADJUSTMENT TEST IAW SFMM 52-32-00 & EO 6752A022.

Part: SKIN — GOUGED (FUSELAGE) · airframe 80,327 hrs · 21,757 cycles

SKIN AT STATION 1180 RT SIDE HAS A GOUGE WHERE WING TO BODY FAIRING MOUNTS. REMOVED FASTENER, REWORKED AREA, INSTALLED NEW FASTENER AS REQUIRED & RESTORED FINISH IAW SRM GUIDELINES & SR 3-3261261089.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 80,290 hrs · 21,720 cycles

GEAR DISAGREE WITH ALL GEAR INDICATED GREEN. EICAS GEAR DISAGREE AMBER GEAR LIGHT ON, WENT OUT AFTER LDG. PERFORMED FIM BITE FOR FAULT CODE 32-30-13-00, FOUND FAULT CODE 422 LG LEVER DOWN. INSTALLED GEAR PINS & CYCLED GEAR HANDLE SEVERAL TIMES. OPERATIONS CHECKED NORMAL EVERY TIME IAW AMM SUBTASK 32-31-01-714-020, FIM 32-09 FAULT TREE 805, AMM 32-61-03 & AMM 32-61-02. NO FAULTS FOUND, OK FOR SERVICE.

Part: FLOOR PANEL — DENTED (CARGO BAY) · airframe 79,209 hrs · 20,970 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL HAS A DENT AT STATION & NBSP 1100 LBL 75 INCHES. INSTALLED REPAIR TO DAMAGE AREA AT MAIN CARGO FLOOR PANEL AT STATION & NBSP 1100 LBL 75 INCHES, IAW B767 SRM 53-00-50 PG 201 BR FIG 4B.

Part: FLOOR PANEL — DENTED (CARGO BAY) · airframe 79,209 hrs · 20,970 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL HAS A DENT AT STATION 470 LBL 55 INCHES. INSTALLED REPAIR TO DAMAGE AREA AT MAIN CARGO FLOOR PANEL & NBSP STATION 470 LBL 55 INCHES, IAW B767 SRM 53-00-50 PG 201 FIG 4B.

Part: FLOOR PANEL — DENTED (CARGO BAY) · airframe 79,209 hrs · 20,970 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL HAS A DENT AT STATION & NBSP 1050 LBL 6". INSTALLED REPAIR TO DAMAGE AREA AT MAIN CARGO FLOOR PANEL AT STATION & NBSP 1050 LBL 6'', IAW B767 SRM 53-00-50 PG 201BR FIG 4B.

Part: FLOOR PANEL — DENTED (CARGO BAY) · airframe 70,209 hrs · 20,970 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL HAS A DENT AT STATION 470 LBL 55". INSTALLED REPAIR TO DAMAGE AREA AT MAIN CARGO FLOOR PANEL AT STATION & NBSP 1200 BL 0', IAW B767 SRM 53-00-50 PG 201 BR FIG 4B.

Part: WINDOW — CRACKED (L1 DOOR) · airframe 78,973 hrs · 20,821 cycles

WINDOW L1 OUTER PANE CRACKED. R & R L1 WINDOW IAW AMM 56-11-01.

Part: RADOME — DAMAGED · airframe 78,460 hrs · 20,440 cycles

ON POST FLIGHT, FOUND BIRD STRIKE ON RADOME. R & R NOSE RADOME IAW 53-12-01, CHP 5 INSPECTION 05-51-18.

Part: HINGE BRACKET — DAMAGED · airframe 78,306 hrs · 20,311 cycles

FOUND DAMAGE FASTENER RECEPTICLE DOOR PROTECTOR HINGE SUPPORT, PART 1 OF EO 6753A090 ACCOMPLISHED, NO FURTHER DAMAGE NOTED.

Part: MOUNT — SEPARATED (CARGO B AY) · airframe 78,284 hrs · 20,288 cycles

CARGO BAY BARRIER DOOR FOWARD MOUNTING POINT SEPARATED FROM CEILING. ACCOMPLISHED EO 6753A087 PART NR 1 TEMP REPAIR.