N705DN

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 49,914 hrs · 4,413 cycles

(AIRCRAFT 7105, L/P 0846154) EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:604 / INTERIOR. INSTALLED LENS OPS CHECK GOOD.

Part: FLAP — PUNCTURED (RT WING) · airframe 48,983 hrs · 4,336 cycles

INBD RIGHT TRAILING EDGE FLAP PUNCTURE/HOLE. INSTALLED PERM REPAIR PER ERA 571754-14 REV ORIGINAL SECTION III.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,534 hrs · 4,298 cycles

(AIRCRAFT 7105, L/P 0708199) EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:405 / / INTERIOR. REPLACED LENS AT EMERGENCY FLOOR LIGHTING LOG 405.

Part: COVER — DAMAGED (CABIN) · airframe 48,154 hrs · 4,268 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:406. INSTALLED NEW LIGHT COVERS.

Part: COVER — DAMAGED (CABIN) · airframe 48,154 hrs · 4,268 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:405. INSTALLED NEW LIGHT COVER.

Part: FUSE — BLOWN (CABIN) · airframe 48,044 hrs · 4,259 cycles

ON SVC CHK FOUND SEAT 10 THRU 12 EMERG LIGHTS INOP. RECHECKED FUSES AT CHARGER M33098. FOUND 1 EA FUSE BLOWN. REPLACED, OPS CHKD ALL NOW NML PER AMM 33-51.

Part: CONTROL UNIT — MALFUNCTIONED (COOLING FAN) · airframe 47,271 hrs · 4,189 cycles

RECEIVED AN EQUIP COOLING OVERHEAT EICAS DURING TAKEOFF ALONG WITH A FAINT ODOR. COMPLETED CHECKLIST AND EICAS LIGHT OUT. AFTER CHECKLIST COMPLETE, HAD STATUS MESSAGE EQUIP COOLING FAN R ON FOR REST OF FLIGHT. REPLACED COOLING FAN & CONTROLLER , CONNECTOR DB21582 . FOUND EXISTING FAULT MESSAGE 21-14024. RT EQUIP COOLING SUPPLY FAN. R & R THE ELCU IAW MM 24-51.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 47,059 hrs · 4,169 cycles

ROWS 10, 11 & 12 B,C EMERGENCY ROW LIGHTS INOP. R&R BATTERY CHARTER M33098 IAW AMM 33-52 OPS CK GOOD.

Part: ACTUATOR — MALFUNCTIONED (NLG STEERING) · airframe 45,341 hrs · 4,018 cycles

ABORTED TAKE OFF AT 30 KNOTS FOR MAIN GEAR STEERING CONTROL MESSAGE. RETURNED TO THE GATE. REPLACED THE LT MAIN GEAR STEERING AND LOCKING POWER CONTROL ACTUATOR IAW AMM 32-53. OPS CHECKED NORMAL.

Part: FAN — FAILED (EQUIPMENT COOLIN) · airframe 43,682 hrs · 3,878 cycles

DURING TAXI OUT, THERE WAS A VERY STRONG ELECTRICAL ODOR THAT DID NOT DISSIPATE. STATUS MESSAGE EQUIP COOLING FAN RT DISPLAYED. CONFIRMED THE RT FAN IS RUNNING WARM & GENERATING THE BURNING ODOR. CIRCUIT BREAKER ON P210 PULLED & ELECTRICAL CONNECTOR ON FAN DISCONNECTED, CAPPED & STOWED. R & R THE COOLING FAN IAW AMM 21-27. CHECKED OK.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 40,944 hrs · 3,635 cycles

AFT CARGO FLOOR PANELS 151LF FOUND DAMAGE. FABRICATED NEW FLOOR PANELS IAW DWG 453W5210.

Part: SKIN — DAMAGED (BS 1727-1737) · airframe 40,924 hrs · 3,632 cycles

BS 1727 - 1737, STRINGER 44 - 45L, SKIN AREA FOUND WITH EXISTING BLEND OUT AREA. FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 102 ALLOWABLE DAMAGE 1. DAMAGE TRIMMED OUT AND REPAIRED IAW ERA 552724-14, REV ORIGINAL

Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,924 hrs · 3,632 cycles

EXISTING BLENDOUT AT STA 1990 , S-28L TO S-29L MEASURED AND FOUND OUT OF LIMIT: ORG THK 0.075", MATERIAL REMAINED 0.056" (L=1.4' X 1.2") AS PER SRM 53-00-01 FIG 102. DAMAGED AREA TRIMMED OUT (L=2" X 1") AND REPAIR CARRIED OUT AS PER SRM 53-00-010 REPAIR 7 FIG 202. THIS REPAIR CLASSIFIED AS CATEGORY B REPAIR.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 40,163 hrs · 3,563 cycles

SEATS 1C, 2C, 4C, AND 10C EMERGENCY LIGHTS LENSES MISSING. INSTALLED MISSING LENSES.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 39,902 hrs · 3,542 cycles

EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED. INSTALLED EXIT SIGN COVER.

Part: SKIN — GOUGED (FUSELAGE) · airframe 40,924 hrs · 3,632 cycles

INSPECTION AT STATION 1392 S3-L CUTOUT DAMAGE FOUND SMALL GOUGE IN CROWN AREA. LOCATED AT 1" HOLE DAMAGE APPROXIMATELY 1" AWAY FROM HOLE DAMAGE AT THE 7 OCLOCK POSITION. GOUGE IS ROUGHLY 1/4" IN AREA. ALLOWABLE DAMAGE 1 AND IS WITHIN LIMITS. TREATED + PRIMED. PERFORMED THICKNESS MEASUREMENTS FOR DAMAGE AREA OBTAINED A MEASUREMENT OF .096 REMAINING MATERIAL DELTA QC 1993 IN BLEND OUT AREA DELTA QC 1993 REPAIRED PER ERA 526747-14 REV A.

Part: SKIN — CORRODED (BS 2268-2344) · corrosion level 2 · airframe 19,895 hrs · 1,734 cycles

INTERNAL SKIN & STRINGERS CORRODED FROM BS 2268.5 TO 2344.5, STRINGERS 22 RT AND 23 RT, REMOVED DAMAGE ON SKIN AND STRINGERS. EVALUATED CLEANED AREA AND FOUND STA 2344.5- 2350 BETWEEN STRINGERS 40R AND 43R OUT OF LIMITS IAW SRM 53-00-01 (472795). ALL OTHER BURNISHED AREAS OF SKIN WERE FOUND WITHIN LIMITS IAW SRM ALLOWABLE DAMAGE 1 (472795). REMOVED REMAINING FASTENERS AND CUT OUT DAMAGED FUSELAGE SKIN REF SRM 53-80-01 (309658). COMPLIED WITH HFEC INSP OF CUTOUT IAW 53-80-01, STEP 4E. NO ITEMS NOTED. FABRICATED REPAIR PARTS, TREATED AND PAINTED IAW SRM 53-80-01 AND SOPM 20-44-04 (481499) COMPLETED STEP 4H ZERO. TIME HOLES BHEC INSPECTION NO ITEMS (316852,410927) OK TO TREAT AND PAINT (410927). TREATED AND PAINTED IAW SRM 53-80-01 (430363,989816). OK TO INSTALL PARTS (989816) INSTALLED DOUBLER IAW SRM 53-80-01 AND COMPLETED REPAIR IAW SRM 53-80-01.

Part: PANEL — DAMAGED (WING) · airframe 19,799 hrs · 1,723 cycles

WING EXTENSION T/E CLOSEOUT PANEL DAMAGED. C/A REMOVED PANEL AND ROUTED TO 382 FOR REPAIR(312579). REPAIRED PANEL IAW SHOP ORDER FZ9480 NDS INSTALLED. (134146) OK TO INSTALL CLOSEOUT PANEL FOR LT WING T/E EXTENSION. INSTALLED PANEL (204965) PANEL PAINT COMPLETED BY PAINT SHOP.

Part: STRINGER — CORRODED (BS 2350 S40R) · corrosion level 2 · airframe 19,822 hrs · 1,727 cycles

STRINGER 40R FOUND TO HAVE CORROSION DAMAGE AT BS 2350. ERA 510962-14 ACCOMPLISHES PERMANENT REPAIR. ENGINEERING HAS DETERMINED THE STRUCTURE REPAIRED IAW ER/A 510962-14, REVISION ORIGINAL,

Part: OIL SYSTEM — LOW (NR 2 ENGINE) · airframe 19,803 hrs · 1,724 cycles

ACFT DIVERTED. FLIGHT CREW INITIATED THE SHUTDOWN OF THE NR 2 ENGINE ONCE OIL QUANTITY REACHED 3 TO 2 QUARTS INDICATED AND THE SHUTDOWN WAS ACCOMPLISHED WITH POSITIVE OIL PRESSURE AND NORMAL OIL TEMPERATURE. REPLACED NR 2 ENGINE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,043 hrs · 1,655 cycles

R2 DOOR EPAS BATTERY PACK GREEN TEST LIGHT NOT ILLUMINATE. REPLACED BATTERY PACK AND CHECK OK IAW AMM 52-11.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 10,283 hrs · 866 cycles

NUMBER 2 OVEN (A815) IN MID-RIGHT AFT GALLEY HAD SMOKE COMING OUT WHEN TURNED ON. OVEN WAS TURNED OFF AND NOT USED. MAINTENANCE REMOVED OVEN AND INSPECTED SURROUNDING AREA. NO ARCING, NO ELECTRICAL SMELL, AND NO DISCOLORATION WAS FOUND. MAINTENANCE ALSO CHECKED ELECTRICAL PLUG BUT FOUND NO TROUBLE. DEFERRED PER NEF 253-30.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 4,917 hrs · 401 cycles

AS T/O PWR WAS ADDED DOOR FWD CARGO EICAS MSG AND TONE SOUNDED TAKE OFF WAS DISCONTINUED. SPEED LESS THAN 60 KTS. FWD TO MCO AND PLACARD IAW MEL M52-71-01. TRANSFERED TO MCO FWD CARGO DOOR VERIFIED CLOSED. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: PCU — LEAKING (FLAPERON) · airframe 2,317 hrs · 174 cycles

EICAS RT HYD QTY LOW. SECURED RT HYD UNTIL 20 MIN FROM LDG. ON APPROACH TURNED ON RT HYD WENT TOWARDS .01, HOWEVER PRESS REMAINED AT 3000 PSI EXCEPT SLIGHT DROPS DURING DEMANDS, THROUGHOUT LANDING AND ROLLOUT. FOUND RT INBOARD FLAPERON PCU LEAKING. REMOVED AND REPLACED PCU. LEAK CHECK AND TESTED NORMAL. RIGGING AND ADJUSTMENT. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.