N144DA

Part: SKIN — DELAMINATED (VERTICAL STAB) · airframe 61,208 hrs · 20,057 cycles

DURING WALK AROUND INSPECTION, FOUND AREA OF DELAMINATION ON RIGHT VERTICAL STABILIZER PANEL LOCATED AT FSS 220 AND BL 1750. DELAMINATION IS OUT OF SRM LIMITS. REPAIRED IAW SRM 51-70-10, REP 4

Part: SEAT TRACK — BROKEN · airframe 61,096 hrs · 20,023 cycles

SEAT TRACK BROKEN. CUT OUT DAMAGED SECTION OF SEAT TRACK & FABRICATED A REPAIR IAW SRM 53-00-52 REPAIR 1 FIG.201 AND INSTALLED THE REPAIR IAW SRM 53-00-52, REPAIR 1, FIG 201.

Part: STRUCTURE — CRACKED (BS 1809) · airframe 57,985 hrs · 19,262 cycles

LEFT HORIZONTAL INNER CHORD CRACKED OUT OF FASTENER, BS 1809, REPAIRED IAW SRM 53-80-08.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 49,905 hrs · 17,309 cycles

EMERGENCY LIGHTS AT SEAT 5FE ARE INOPERATIVE. MX FOUND A WIRE DISCONNECTED. CONNECTED WIRE SYS OPS NORMAL.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 49,685 hrs · 17,247 cycles

NR 2 PYLON FWD UPPER PYLON DRAIN HOLE CRACKED. REPAIRED IAW ERA 519157-14.

Part: SQUIB — INOPERATIVE (SLIDE) · airframe 48,200 hrs · 16,897 cycles

DURING CHANGE OF LT WING SLIDE BOTTLE, FOUND RT WING SPOILER BLOW DOWN SQUIB BAD. REPLACED RT WING SPOILER OVERRIDE ACTUATOR SQUIB.

Part: FRAME — CRACKED (BS 903 S20-21L) · airframe 44,666 hrs · 16,034 cycles

FS 903 LT BETWEEN STR 20L AND STR 21L FRAME CHORD CRACKED. CHORD CRACK REPAIR ACCOMPLISHED AS PER ERA 501545-14AD REV ORG SECTION 1.

Part: SPAR — CRACKED (NR 1 NACELLE) · airframe 44,666 hrs · 16,034 cycles

NR 1 PYLON FWD UPPER SPAR WEB LT DRAIN HOLE FOUND CRACKED. REPAIRED AS PER ERA 502699-14AD, REV ORG NRC 52915.

Part: FRAME — CRACKED (BS 903 S20R-21L) · airframe 44,666 hrs · 16,034 cycles

FS 903 RT BETWEEN STR 20R AND STR 21L INNER CHORD CRACKED. TRIMMED OUT AND REPAIRED AS PER ERA 501546-14AD REV ORG SECTION 1.

Part: TEE FITTING — CORRODED (BS 955 BULKHEAD) · airframe 44,666 hrs · 16,034 cycles

RIGHT BS 955 REAR SPAR BULKHEAD FITTING FOUND CORRODED AT TEE FITTING. REPLACED TEE FITTING AS PER ERA 501536-14AD, REV ORG.

Part: TEE FITTING — CRACKED (BS 955 BULKHEAD) · airframe 44,666 hrs · 16,034 cycles

LEFT BS 955 REAR SPAR BULKHEAD FITTING CRACKED AT TEE FITTING. TEE FITTING REPLACED AS PER ERA 501535-14AD, ORG.

Part: FAILSAFE — CORRODED (BS 955 BULKHEAD) · airframe 44,666 hrs · 16,034 cycles

LT STA 955 REAR SPAR BULKHEAD FAIL SAFE STRAP FASTENER HOLE CORRODED. REPAIRED AS PER ERA 501535-14AD, REV ORG.

Part: FAILSAFE — CRACKED (BS 955 BULKHEAD) · airframe 44,666 hrs · 16,034 cycles

RIGHT BS 955 REAR SPAR BULKHEAD FAILSAFE STRAP CRACKED, AREA TRIMMED OUT AND REPAIRED AS PER ERA 501536-14AD REV. ORG

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 44,666 hrs · 16,034 cycles

RT I/B MAIN FLAP O/B L/E FAIRING IS DELAMINATED IN 3 PLACES. REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 TABLE 1 AND 51-70-05 PAR 5A(1) FIG 5.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 44,666 hrs · 16,034 cycles

FS 955 LT REAR SPAR BLKHD "T" FITTING AT FAILSAFE IS CRACKED AT A HOLE, WORKING FROM A PRI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,666 hrs · 16,034 cycles

FS 903 BETWEEN STR 20R-21R FRAME INNER CHORD IS CRACKED, WORKING FROM PRI.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 44,666 hrs · 16,034 cycles

LT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING IS DELAMINATED IN 2 PLACES AND HAS BEEN REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 TABLE 1 AND SRM 51-70-05 PAR 5A(1) FIG 5.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 44,666 hrs · 16,034 cycles

FS 955 RT REAR SPAR BLKHD "T" FITTING HAS A FASTENER HOLE CORRODED, WORKING ON PRI.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 44,666 hrs · 16,034 cycles

NR 4 SLAT T/E WEDGE IS DELAMINATED IN 2 PLACES AND REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 FIG 201 AND 51-70-10 REPAIR 4 FIG 202 SHT 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,666 hrs · 16,034 cycles

FS 903 LT BETWEEN STR 20L-21L FRAME INNER CHORD IS CRACKED, WORKING FROM PRI.

Part: FAIRING — GOUGED (HORIZ STAB) · airframe 44,666 hrs · 16,034 cycles

LT HORIZONTAL STAB L/E FAIRING 332DL IS GOUGED AND REPAIRED PER B767-300 SRM 55-10-01 REPAIR 1 FIG 201 AND 51-70-10 REPAIR 4 FIG 201 SHT 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 44,666 hrs · 16,034 cycles

FS 927 AT STR 20R-21R FRAME TO WING CENTER SECTION FITTING IS CRACKED AND BEING REPLACED PER B767-300 SRM 51-10-02 PG 8 PARA 9 AND DWG 100T1410.

Part: FAILSAFE — CRACKED (BS 955) · airframe 44,666 hrs · 16,034 cycles

RIGHT FUSELAGE STATION 955 REAR SPAR BULKHEAD FAILSAFE STRAP FASTENER HOLE CRACKED.

Part: FAILSAFE — CRACKED (BS 955) · airframe 44,666 hrs · 16,034 cycles

LEFT FUSELAGE STATION 955 REAR SPAR BULKHEAD FAIL SAFE STRAP FASTENER HOLE FOUND CORROSION AND CRACKED.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 37,201 hrs · 14,381 cycles

FOUND ON PDC/DRC CHECK, EMERGENCY LIGHT IS INOPERATIVE AT THE BASE OF LAVATORY 215. MX REPAIRED A BROKEN WIRE FOUND AT BASE. SYS OPS IS NORMAL. (DL76P101504)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 36,330 hrs · 14,190 cycles

EMERGENCY PATH LIGHT AT 3AB IS INOPERATIVE. MX FOUND CONNECTORS DISCONNECTED AND RECONNECTED THEM. SYS OPS IS NORMAL.

Part: CONTROL PANEL — ODOR (GALLEY) · airframe 36,257 hrs · 14,174 cycles

ACRID ODOR IN COCKPIT DURING CRUISE AND IN DESCENT LASTING FOR APPROX. 10 SECONDS EACH TIME. FOUND GALLEY CONTROL PANEL AT 1R WITH ACRID ODOR. SUSPECT 5 AMP FREEZER C/B AS SOURCE. (NOT TRIPPED) REPLACED C/B AND OPERATED FOR SEVERAL HOURS WITH NO DISCREPANCIES NOTED. OK FOR SVC. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: TURBINE BLADES — DAMAGED (NR 2 ENGINE) · airframe 35,373 hrs · 13,986 cycles

NR 2 ENGINE FAILED, OP 5067 BOROSCOPE 2ND STAGE. PERFORMED NR 2 OP 5067 ENG BOROSCOPE. FOUND ONE 2ND STG HPT BLADE DAMAGE. ALSO AP-9 DAMAGE EMP 221084. SEE ITEM 009 FOR ENGINE REPLACEMENT.

Part: INDICATOR — MALFUNCTIONED (ADIS) · airframe 35,315 hrs · 13,974 cycles

RTB DUE TO INOPERATIVE SPEED FLAG ON ADIS RESET TMC C/BS. FLAGS CLEARED - NO ADC FAULTS. TMC TESTS GOOD. A/T SERVO TESTS GOOD.

Part: STARTER — INOPERATIVE (NR 2 ENGINE) · airframe 32,564 hrs · 13,408 cycles

APU START 15-20 PSI RT ENG BEGAN TO START W/N2 AT LEAST 8 THEN ROLLED BACK. START VALVE LITE NORMAL. TRIED AIR FROM LT ENG NR N2 OR OIL PRESS. REMOVED AND REPLACED NR 2 ENG STARTER. OPS CKS NML. INSTALLED STARTER BORROWED FROM AIR CANADA AIRLINES MFG P/N 774860A4 S/N MK94194 LEAK CK GOOD. STARTER SERVICED WITH MODIL II OIL.

Part: GENERATOR — FAULTED (LEFT ENGINE) · airframe 31,942 hrs · 13,260 cycles

AFTER PUSHBACK LT GEN DID NOT AUTOMATICALLY PICK UP THE LOAD. MANUAL RESET BROUGHT GEN ONLINE. DUE TO MULTIPLE EICAS MSGS RE EECS ACFT RETURNED TO GATE. BIT BPCU NO LAST FAULTS NOTED. RAN LT ENG AT GATE WITH NO DISCREPANCIES NOTED. OK FOR SVC.

Part: IDG — INOPERATIVE (NR 1 ENGINE) · airframe 31,792 hrs · 13,223 cycles

ON NR 2 ENG START NR 1 GEN FELL OFF LINE. L ENG EEC C1 STATUS MSG BIT BPCU LEFT ENG FAULT LOW FREQ TRIP. BIT PIMU ON LT ENG HAD NUMEROUS FAULTS DUE TO POWER DROPPING OFF RESET PIMU. PERFORMED TWO ENG RUNS NO MSGS ON EPCS PG OR PIMU. DISC LT IDG DUE TO HISTORY. FWD TO MCO AND PLAC PER MEL 24-00-01. REMOVED AND REPLACED NR 01 ENG IDG PER M/M. LK/OPS CK GOOD. MCO/PLAC REMOVED. A/C OK FOR SVC.

Part: GCU — FAILED (NR 1) · airframe 31,785 hrs · 13,217 cycles

LT ENG GENERATOR FAILED ON TAXI OUT DURING X BLEED START. REPLACED LEFT GCU RAN ENG OPS CK OK.

Part: PROBE — UNKNOWN (NR 2 ENGINE) · airframe 31,699 hrs · 13,195 cycles

RIGHT ENGINE CONTROL EICAS MESSAGE AFTER ENGINE START. REPLACED P2/T2 PROBE, OPS NORMAL.

Part: TRANSMITTER — FAILED (TE FLAP) · airframe 31,431 hrs · 13,128 cycles

RTB - FLAPS WILL NOT LOWER AND FLAP DISAGREE EICAS MSG. T/S PER FIM 27-51-00 FIG 105. DIRECTED TO FIM 27-51-00 FIG 11, CHECKS OK UP TO STEP 5-SHEET 3 FIG 114C. SUSPECT BYPASS VLV - 318717- FOUND NR 4 FLAP POS XMITTER OUT OF RANGE. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: STARTER — FAILED (NR 1 ENGINE) · airframe 29,996 hrs · 12,735 cycles

NR 1 ENG NO START NO ROTATION, FOUND STARTED AT FAULT. REPLACED STARTER.

Part: HYDRAULIC LINE — LEAKING (THRUST REVERSER) · airframe 27,997 hrs · 12,221 cycles

ON LANDING ROLLOUT, AFTER ACTUATING THRUST REVERSERS LOST RT HYDRAULIC QTY. FOUND REVERSER HYDRAULIC LINE WITH HOLE IN IT. PERFORMED TEMP REPAIR PER MM 20-10-09-358-151. CYCLED REVERSER AND ALL HYDRAULIC SYSTEMS SEVERAL TIMES. OPS NORMAL. OLD BAD HYDRAULIC LINE LOCATED IN MCO POUCH.

Part: INDICATOR — ODOR (COCKPIT) · airframe 26,849 hrs · 11,934 cycles

CAPTAINS VSI WENT BLANK. DETECTED FAINT ELECTRICAL ODOR. PULLED VSI CIRCUIT BREAKER. ODOR DISSIPATED. REPLACED CAPTS VSI, OPS TESTS GOOD.

Part: LOOP — UNKNOWN · airframe 25,299 hrs · 11,548 cycles

PASSING 28000 FT T/O PLUS 15 MIN CLIMB PWR RT DUCT BLEED LIGHT AND EICAS MSG. COMPLETED WITH QRH PROCEDURE RT DUCT BLEED LEAK EXTINGUISHED PASSING 32500 FEET. VISUALLY INSPECTED PNEU DUCTING AND CLAMPS ALONG WITH CHECKING FOR LEAKS FROM RT ENG PYLON TO RT ECS BAY NO DISCREPANCIES FOUND. VISUALLY INSP OVERHEAT ELEMENTS AND CLAMPING FROM ABOVE PYLON TO RT ECS BAY NO DISCREPANCIES NOTED. REPLACED LOOPS TS216 TS 217 TS218 TS 219 TS215. REPLACED BOTH TERMINAL STRUT SWITCHES RAN RT ENG TO T/O AND CLB PWR NO EICAS MSG OR LIGHT.

Part: CONTROL MODULE — MALFUNCTIONED (SPOILERS) · airframe 25,291 hrs · 11,544 cycles

SPOILERS CAUTION LIGHT ON TAXI OUT. RESET PCA3 FAULT ON 2L SPOILER CONTROL MODULE. OPERATED SPOILERS ALL MODES WITH DIFFERENT POWER SOURCES.

Part: CIRCUIT CARD — DEFECTIVE (NR 2 ENGINE) · airframe 25,193 hrs · 11,519 cycles

RIGHT DUCT LEAK LIGHT INFLIGHT CLIMBING THRU FL210. CHECKED ALL DUCTS FROM RT ENGINE TO THE RT ISOL VALVE. REPLACED WHEEL WELL OVHT ECS DUCT LEAK DETECTION SYS CONTROL CARD. RAN ENGINES AT IDLE FOR 30 MINUTES, T/O POWER FOR 10 MINUTES AND 15 MINUTES AT CLIMB POWER. NO TROUBLE NOTED.

Part: FAN — ODOR (CABIN) · airframe 22,559 hrs · 10,607 cycles

EQUIPMENT COOLING OVHT LIGHT ON OVERHEAD PANEL ACCOMPANIED BY BURNING SMELL IN COCKPIT. FOUND EICAS MSG FWD EQUIP SUPPLY FAN 1 PULLED AND COLLARD C/B H-18 FWD TO MCO AND PLAC 21-58-03B FWD SUPPLY FAN MOTOR BURNED UP NEEDS NEW FAN ASSY. REMOVED AND REPLACED FWD EQUIP. COOLING FAN 1 AND OPS CK GOOD. MCO PLACARD REMOVED.

Part: TURBINE — DAMAGED (NR 2 ENGINE) · airframe 16,916 hrs · 8,297 cycles

ON T/O ROLL APPROX 130 KTS CREW EXPERIENCED LOUD BANG AND FLASH FOLLOWED BY YAW TO THE RIGHT. EGT REPORTED OFF SCALE ON RT ENG. PASSENGERS REPORTED SMOKE FROM ENG. BOTH FIRE BOTTLES AND RTO PERFORMED. MTC FOUND METAL IN THE TAILPIPE AND EGT RECORDED AT 729 FOR 56 SEC. REPLACED ENGINE.

Part: SMOKE DETECTOR — MALFUNCTIONED (MID GALLEY) · airframe 16,699 hrs · 8,184 cycles

MID CABIN SMOKE ALARM WENT OFF ON T/O. F/A NOTIFIED CREW SHORTLY AFTER T/O. THOROUGHLY INSPECTED AIRCRAFT, RAN ENGINES AND SYSTEMS, UNABLE TO DUPLICATE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,301 hrs · 7,992 cycles

ON LAYOVER FOUND EMERGENCY LIGHTS INOPERATIVE AT FWD F/A OVERHEAD AND AFT OVERHEAD AT SEAT 47 C AN E. RELAMPED OPERATION OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,278 hrs · 7,447 cycles

EMERGENCY PATH LIGHTS INOP IN FIRST CLASS. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK.

Part: ODOR — DETECTED (CABIN) · airframe 11,642 hrs · 5,611 cycles

AFTER TAKE OFF, FLT ATTENDANT REPORTED STRANGE FUMES & ODOR IN MIDSECTION GALLEY AREA. LT ENGINE BLEED AND PACK TURNED OFF AND ODOR SUBSIDED & DISSIPATED. BLEED AND PACK LT OFF. REMAINDER OF FLT UNEVENTFUL. INSPECTED INLET EXHAUST - NO VISIBLE OIL - PERF PNEUMATIC CHECK PER 21-00-21 NO VISIBLE SMOKE IDLE POWER. RAN LT PACK LT ENGINE BLEED ONLY IDLE - NO SMOKE / ODOR. NEEDS HP CHECK. 985989 - RAN ENGINE AT HIGH POWER SETTING FOR 5 MINUTES WITH LT BL PACK ON - NO UNUSAL ODORS OR SMOKE. LT PNEUMATIC PACK OK.

Part: SKIN — DENTED (FS 374, S-17L) · airframe 10,240 hrs · 4,923 cycles

FUSELAGE / SKIN / FS 374 / STRG. 17L / SKIN LAP JOINT : DENT REPAIR THE FUSELAGE SKIN AT FS 374 AT THE STRINGER 17L LAP JOINT WAS DENTED. THE DENT WAS REMOVED WITH A 4.5" X 3.9" CUTOUT IN THE UPPER AND LOWER SKIN OF THE LAP JOINT. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 383329-14, REV B.

Part: BOLT — SHEARED (L/E SLAT) · airframe 10,010 hrs · 4,814 cycles

ON TAXI OUT, GOT L/E ASYMMETRY T/S AND FOUND PROX SENSOR TARGET AT S286 LEFT SLAT NR 5 EXTEND PLATE MISSING AND ATTACH SCREW SHEARED. INSTALLED NEW TARGET AND ATTACHING SCREW. SYSTEM OPS NORMAL.

Part: CHIP DETECTOR — CRACKED (NR 1 ENGINE) · airframe 7,494 hrs · 3,588 cycles

THE MAIN ENGINE CHIP DETECTOR BOSS SLOTS (3 EA) HAD BEGUN TO FAIL (CRACK) AT THE WEAKEST AREA OF THE BOSS. REPLACED THE BOSS AND DETECTOR

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 5,054 hrs · 2,396 cycles

FIRST CLASS SEAT EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. LIGHT OPERATION NORMAL.

Part: LIGHT — LOOSE (ROW 11) · airframe 3,301 hrs · 1,545 cycles

EMERGENCY TRACK LIGHT PULLED FREE AT ROW 11F. REPAIRED SAME.

Part: SLIDE — DETACHED (LT SERVICE DOOR)

LT AFT SERVICE DOOR SLIDE PACK ASSY DROPPED 6 INS OFF DOOR. REMOVED SLIDE AND INSTALL PIN. REPLACED LT AFT SERVICE DOOR SLIDE PACK. CKD OPERATION OF LT AFT DOOR OK. REMOVED AND REPLACED PIN CKD OP OF GIRT/ARM LEVER OK PER M/M.