N129DL

Part: CRANK ASSY — CORRODED (TE FLAP) · corrosion level 2 · airframe 88,684 hrs · 36,763 cycles

CORROSION LEVEL 2, AT C CHECK, PITTING WAS FOUND ON THE NR 2 CRANK ARM ASSY OF THE LT OUTBOARD FLAP. REPLACED CRANK.

Part: ACTUATOR — CORRODED (TE FLAP) · airframe 88,684 hrs · 36,763 cycles

RIGHT WING O/B FLAP ROTARY ACTUATOR NR 8 ARM ASSY SHAFT PITTED/CORRODED. REPLACED.

Part: ACTUATOR — CORRODED (TE FLAPS) · airframe 84,003 hrs · 35,334 cycles

CORROSION LEVEL: 2, LT OTBD FLAP ROTARY ACTUATOR CORRODED, NR 1 POSITION. REPLACED LT OTBD FLAP ROTARY ACTUATOR DUE TO CORROSION. LP1907932.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 80,807 hrs · 34,405 cycles

TWO LEFT OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED FUSE ON THE POWER SUPPLY. SYSTEM OPS ARE NORMAL.

Part: LIGHT — UNSECURE (SEAT 36B) · airframe 79,162 hrs · 33,914 cycles

EMERGENCY LIGHTS AT SEAT 36B IS BROKEN FROM SEAT. REPLACED EMERGENCY LIGHT HOUSING. SYS OPS IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,117 hrs · 33,902 cycles

MAIN LT SIDE OVERHEAD EMERGENCY LIGHTS ARE INOPERATIVE AT ROWS 12-29. MX REPLACED THE BATTERY AND POWER SUPPLY. SYS OPS IS NORMAL.

Part: STRINGER — CRACKED (BS 488) · airframe 78,820 hrs · 33,813 cycles

FWD CARGO COMPARTMENT BS 488 S35R, STRINGER FOUND CRACKED. FOUND OUT OF LIMITS IAW SRM 53-00-03, FIG 101, REV 92, AND REPAIRED IAW SRM 53-00-03, FIG 201 REPAIR 2.

Part: FLOORBEAM — CORRODED (BS 287) · airframe 78,107 hrs · 33,601 cycles

BS 287, RBL 60, FLOORBEAM UPPER TEE CORRODED. REPAIR STRAP AND PARTS REMOVED AND NEW REPAIR CARRIED OUT IAW IAW PRI ER/A 515529-14.

Part: STRINGER — CRACKED (BS 468-476) · airframe 78,820 hrs · 33,813 cycles

FWD CARGO COMPARTMENT BS 468-476 S34R, STRINGER CRACKED, FOUND OUT OF LIMITS IAW SRM 53-00-03, FIG 101, REV 92. REPAIR CARRIED OUT IAW SRM 53-00-03, FIG 201 REPAIR 2, REV 92.

Part: FRAME — CRACKED (BULKHEAD) · airframe 78,107 hrs · 33,601 cycles

DURING OPEN-HOLE HFEC INSPECTION ON BS 1809.5 BULKHEAD OUTER FRAME, LT PERMANENT REPAIR HFEC INSPECTION IAW STEP 3, FOUND CRACK INDICATION ON FWD CHORD, MOST OTBD THIRD FASTENER FROM TOP, FIVE O'CLOCK POSITION BS 1809.5 BULKHEAD FWD & AFT CHORD REPLACEMENT ACCOMPLISHED IAW ER/A 514965-14AD PRI REV.

Part: SKIN — CORRODED (BS 1197) · airframe 78,107 hrs · 33,601 cycles

EXTERIOR SKIN AT BS 1197+112, BETWEEN S39 RT AND LT FOUND CORRODED. REPAIR ACCOMPLISHED IAW PRI 514664-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,107 hrs · 33,601 cycles

DURING OPEN HOLE HFEC INSPECTION IAW 514664-14, PRI REV 0, STEP 6 ON FASTENER HOLES. FOUND FIVE HOLES DAMAGED WITH CRACK INDICATIONS. REPAIR AND SKIN TRIMMED-OUT IAW ER/A 514664-14AD, REV ORIGINAL STEP 7 AND REFER TO ER/A 514664-14AD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,107 hrs · 33,601 cycles

DURING OPEN HOLE HFEC INSPECTION IAW 514664-14 PRI REV 0, STEP 5 ON CUT-OUT PERIPHERY OF REPAIR. FOUND FOUR CRACKS APPROX 0.25" TO 1.0". CRACKED AREA TRIMMED-OUT IAW ER/A 514664-14AD.

Part: STRINGER — CORRODED (BS 428) · airframe 78,107 hrs · 33,601 cycles

FWD CARGO COMPARTMENT BS 428, S33L STRINGER CORRODED. FOUND OUT OF LIMITS IAW SRM 53-00-03, FIG 101, REV 92 AND REPAIR CARRIED OUT IAW SRM 53-00-03, FIG 201.

Part: STRINGER — CORRODED (BS 430 S35R) · corrosion level 2 · airframe 78,107 hrs · 33,601 cycles

FWD CARGO COMPARTMENT BS 430, S35R, STRINGER CORROSION AREA CRACKED FOUND OUT OF LIMITS IAW SRM 53-00-03, FIG 101, REV 92 AND REPAIR CARRIED OUT IAW SRM 53-30-03, REPAIR 1.

Part: STRINGER — CORRODED (BS 456-478) · corrosion level 2 · airframe 78,107 hrs · 33,601 cycles

FWD CARGO BS 456-478, STRINGER 36R FOUND CORRODED. CORROSION AREA FOUND OUT OF LIMITS IAW SRM 53-00-03, FIG 101, REV 92 AND REPAIR CARRIED OUT IAW SRM 53-00-03, FIG 201, REPAIR.

Part: STRINGER — CORRODED (BS 424 S34R) · corrosion level 2 · airframe 78,107 hrs · 33,601 cycles

FWD CARGO COMPARTMENT BS 424 S34R STRINGER FOUND CORRODED. FOUND OUT OF LIMITS IAW SRM 53-00-03, FIG 101, REV 92 AMD REPAIR CARRIED OUT IAW SRM 53-00-03, FIG 201, REPAIR 2.

Part: BULKHEAD — CRACKED (BS 1809.5) · airframe 78,107 hrs · 33,601 cycles

DURING HFEC OPEN HOLE INSPECTION AT BS 1809.5, LT BULKHEAD ON AREA WITH RUB STRIPS INSTALLED, CRACK INDICATION FOUND ON LWR FWD HOLE AT SECOND LAYER FROM INBD APPROX THREE O'CLOCK POSITION IAW CARD 5310-01376-1603, STEP 3, BS 1809.5 BULKHEAD OUTER CHORD, LT PERMANENT REPAIR.

Part: STRINGER — CORRODED (BS 446) · corrosion level 2 · airframe 78,107 hrs · 33,601 cycles

FWD CARGO COMPARTMENT BS 446, S33L, STRINGER CORRODED. FOUND OUT OF LIMITS SRM 53-00-03, FIG 101, REV 92 AND REPAIR CARRIED OUT IAW SRM 53-00-03, FIG 201.

Part: STRINGER — CORRODED (BS 418-424) · corrosion level 2 · airframe 78,107 hrs · 33,601 cycles

FWD CARGO COMPARTMENT BS 418-424 S35L, STRINGER CORRODED. FOUND OUT OF LIMITS IAW SRM 53-00-03, FIG 101, REV 92 AND REPAIR CARRIED OUT SRM 53-00-03, FIG 201, REPAIR 2.

Part: BULKHEAD — CRACKED (BS 1809.5) · airframe 78,107 hrs · 33,601 cycles

DURING OPEN HOLE INSPECTION ON BS 1809.5, BULKHEAD OUTER FRAME, LT PERMANENT REPAIR HFEC INSPECTION IAW STEP 1, FOUND CRACK INDICATION ON SECOND LAYER FROM INBD, SECOND ROW FROM AFT SEVENTH FASTENER FROM TOP, TWO O'CLOCK POSITION. R & R FWD FRAME IAW BS 53A007, FIG 07 AND REFER ER/A 514965-14AD.

Part: STRINGER — CORRODED (BS 444 S34L) · airframe 78,107 hrs · 33,601 cycles

FWD CARGO COMPARTMENT BS 444 S34L STRINGER CORRODED. FOUND OUT OF LIMITS IAW SRM 53-00-03, FIG 101, REV 92 AND REPAIR CARRIED OUT IAW SRM 53-00-03, FIG 201, REPAIR 2.

Part: STRINGER — CORRODED (BS 425) · corrosion level 2 · airframe 78,107 hrs · 33,601 cycles

FWD CARGO COMPARTMENT BS 425 S34L STRINGER CORROSION REPAIR CARRIED OUT IAW SRM 53-00-03.

Part: FLOORBEAM — CRACKED (BS 325) · airframe 78,107 hrs · 33,601 cycles

CABIN BS 325, LBL33 FLOORBEAM UPPER TEE FOUND CRACKED. REPAIRED IAW SRM 53-00-51, FIG 201, REPAIR 1.

Part: STRINGER — CRACKED (BS 654 S19L) · airframe 78,107 hrs · 33,601 cycles

DURING INSULATION BLANKET REMOVAL BS 654+ 44 S19L STRINGER END FOUND CRACKED. REPAIRED IAW SRM 53-00-03, FIG 201, REPAIR 1.

Part: STRINGER — CRACKED (BS 654 S19R) · airframe 78,107 hrs · 33,601 cycles

DURING INSULATION BLANKET REMOVAL BS 654+ 22 S19R, STRINGER END FOUND CRACKED. REPAIRED IAW SRM 53-30-03, FIG 201, REPAIR 2.

Part: STRINGER — CRACKED (BS 654 S19R) · airframe 78,107 hrs · 33,601 cycles

DURING INSULATION BLANKET REMOVAL FOR BLANKET MOD, CABIN STA 654+ 44 S19R STRINGER END FOUND CRACKED. REPAIRED IAW SRM 53-00-03, REPAIR 1.

Part: FLOORBEAM — CRACKED (BS 325) · airframe 78,107 hrs · 33,601 cycles

BS 325, BL 0 FLOORBEAM UPPER TEE FOUND CRACKED. REPAIRED IAW SRM 53-00-51, REPAIR 1.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 77,822 hrs · 33,515 cycles

EMERGENCY LIGHTS AT SEATS 10B AND 44F ARE INOPERATIVE. MX SECURED CONNECTORS. SYS OPS IS NORMAL.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,752 hrs · 33,486 cycles

DURING A CHECK FOUND LT SIDE F2ST CLASS EMEREGENCY LIGHTS INOPERATIVE AT ROWS 13-20 RT SIDE. MX REPAIRED WIRE CONNECTOR AT ROW 10AB. ALL LIGHTS OPS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,690 hrs · 33,469 cycles

ON WALK AROUND FOUND FWD CABIN SECTION LT AND MID SECTION RT EMERGENCY LIGHTS INOPERATIVE. MX REPLACED THE POWER SUPPLY. SYS OPS IS NORMAL.

Part: CHILLER — INOPERATIVE (AFT GALLEY) · airframe 76,796 hrs · 33,205 cycles

FUMES IN AFT GALLEY REPORTED BY FLIGHT CREW. LEFT AFT CHILLER INOPERATIVE, AFT LT CHILLER CONTROL CIRCUIT BREAKER COLLARD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 74,167 hrs · 32,458 cycles

CORROSION IN FUSELAGE SKIN LAP JOINT AT FS 784 AND STR 36R. REPAIRED PER ERA 498402-14.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 71,560 hrs · 31,769 cycles

DURING SERVICE CHECK, MX FOUND EMERGENCY LIGHTS ROWS 14-21 FG OFF. A WIRE WAS DISCONNECTED AT SEAT 13. MX RECONNECTED WIRE. SYS OPS IS NORMAL.

Part: LIGHT — INOPERATIVE (L1 CLOSET) · airframe 71,390 hrs · 31,726 cycles

EMERGENCY LIGHTS AT L1 CLOSET DOOR ARE INOPERATIVE. MX RE-SECURED THE LIGHT ASSY. SYS OPS IS NORMAL.

Part: FITTING — CRACKED (RT WING) · airframe 65,243 hrs · 30,000 cycles

FOUND AT PSV21 RT OB FLAP DEFLECTION CONTROL TRACK FITTING CRACKED. REPLACED FITTING.

Part: FITTING — CRACKED (LT WING) · airframe 65,243 hrs · 30,000 cycles

FOUND DURING PSV21 LT OTBD FLAP DEFLECTION TRACK FITTING ON AFT SPAR CRACKED. REPLACED FITTING.

Part: FRAME — CRACKED (BS 903.5 WL 190) · airframe 60,991 hrs · 28,441 cycles

DURING HMV, THE LT AND RT STA 903.5 FRAME INNER CHORDS WERE FOUND CRACKED AT WL 190. THE STUB BEAM FITTINGS WERE ALSO CRACKED.

Part: FRAME — CRACKED (BS 1809.5) · airframe 60,991 hrs · 28,441 cycles

DURING HMV, STA 1809.5 BULKHEAD OUTER CHORD WAS FOUND CRACKED BETWEEN S-7R AND S-8R. CHORD WAS REPAIRED PER BOEING INSTRUCTIONS.

Part: BULKHEAD — CRACKED (NR 2 PYLON) · airframe 60,991 hrs · 28,441 cycles

DURING HMV AT HAECO, THE NR 2 PYLON AFT BULKHEAD WAS FOUND CRACKED IN ONE HOLE.

Part: FITTING — CRACKED (NR 2 PYLON) · airframe 60,991 hrs · 28,441 cycles

DURING HMV, ONE HOLE IN THE NR 2 PYLON BULKHEAD FITTING COMMON TO THE UPPER SPAR FITTING WAS FOUND CRACKED. CRACK WAS REPAIRED PER INSTRUCTIONS APPROVED BY BOEING.

Part: SKIN — DENTED (BS 228-236) · airframe 60,991 hrs · 28,441 cycles

DURING HMV AT HAECO, EXISTING REPAIRS WERE FOUND IN THE CROWN SKIN AREA WHICH WERE DIMPLED AND WAVY. THERE WERE ALSO UNREPAIRED DENTS IN THE ADJACENT AREA.

Part: STIFFENER — CRACKED (LT WING) · airframe 60,991 hrs · 28,441 cycles

DURING HMV AT HAECO, THE WING CENTER SECTION FRONT SPAR LBL 10.94 STIFFENER WAS FOUND CRACKED.

Part: FLOORBEAM — CRACKED (BS 347) · airframe 60,991 hrs · 28,441 cycles

FLOORBEAM BS 347 HAD CRACKS IN UPPER CHORD BETWEEN LBL 10 AND RBL 20. DUE TO A WEB REPAIR NEAR RBL 29.5. A SPLICE REPAIR WAS DONE BETWEEN LBL 27 AND RBL 30.5.

Part: FLOOR SUPPORT — CRACKED (STA 999 LBL 33) · airframe 60,991 hrs · 28,441 cycles

BS 999 LBL 33 FLOOR SUPPORT FOUND CRACKED. REPAIRED FLOOR SUPPORT PER SRM 53-00-51 REPAIR NR 3 FIG 201.

Part: FLAP TRACK — DAMAGED (WING) · airframe 59,689 hrs · 27,999 cycles

DAMAGE FOUND ON ATTACH HOLES FOR RT I/B FLAP O/B TRACK. REPAIRED DAMAGE PER ERA 089397-14MA. C/W STEP 13 TO SUBMIT MRR PER SAME ERA.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 58,920 hrs · 27,676 cycles

F/O FWD WINDSHIELD SHATTERED IN CRUISE. REMOVED AND REPLACED WINDOW PER M/M. REMOVED AND REPLACED WINDOW HEAT CONTROLLER. F/O WINDSHIELD CHECKS OK

Part: PROJECTOR — FAILED (NR 3) · airframe 53,650 hrs · 25,584 cycles

PROJECTOR AT SCREEN 3 FAILED ACCOMPANIED WITH ELECTRICAL ODOR. SHUT OFF SYSTEM PULLED C/B T8 ON OVERHEAD, ODOR DISSIPATED. REPLACED PROJECTOR.

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 51,118 hrs · 24,331 cycles

VERTICAL STABILIZER LEFT LOWER PANEL ASSY, FWD TORQUE BOX FSS 12 - FSS 271 DELAMINATION. REPAIRED PER ER/A 088833-14.

Part: ENGINE — UNSERVICEABLE (#1 ENGINE) · airframe 46,213 hrs · 21,885 cycles

ON TAKE OFF ROLL ABOUT 130 KIAS, LEFT ENGINE TEMP WENT TO 975, PULLED THROTTLE BACK TO KEEP WITHIN LIMITS, CONTINUED TAKE OFF AT 150 AGL, LEFT ENGINE ROLLED BACK TO IDLE AND TEMPWENT TO 1100. POWER CAME BACK TO IDLE AND RETURNED TO FIELD.THE ENGINE WAS NOT SHUTDOWN UNTIL AFTER LANDING. RPLCD NBR 1 ENG PER TRANS 1T144

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,042 hrs · 20,830 cycles

THE LOWER FORWARD CORNER OF THE BULK CARGO DOOR CUTOUT WAS FOUND TO BE CRACKED IN THE SKIN ONLY. AT THE SAME LOCATION, THE SKIN AND BEARSTRAP HAD BEEN PREVIOUSLY REWORKED PER SRM ALLOWABLE EDGE DAMAGE LIMITS. ER/A 397956-14

Part: HARNESS — DEFECTIVE (CABIN) · airframe 43,581 hrs · 20,622 cycles

SEAT 37A EMERGENCY LIGHT INOP ON TEST. REPLACED LIGHT HARNESS.

Part: WIRE — SHORTED (CABIN) · airframe 43,183 hrs · 20,438 cycles

ON L/O FOUND EMERGENCY LIGHTS INOP. LEFT AND RIGHT SIDES SEAT ROW 35 AFT FLOOR TRACK LIGHTING. T/S PER WDM TRIED PWR SUPPLY, NO HELP. ISOLATED SHORT IN WIRING TO SEAT 35AB. REPAIRED SAME.

Part: HARNESS — SHORTED (GALLEY) · airframe 40,490 hrs · 19,146 cycles

AFT GALLEY C/B POPPED FOUND WIRE BUNDLE SHORTED TO CHILLER FRAME BURNED HOLE THRU FRAME. REPAIRED WIRE BUNDLE AND REPLACED SUPPORT BRACKET.

Part: WIRE — CHAFED (ROW 20FG)

A PASS AT SEAT 20E REPORTED ARCING AROUND HIS READING LIGHT THE PASS. READING LIGHTS IN THE AREA FAILED AND THE ENTERTAINMENT AUDIO THROUGH OUT THE AIRCRAFT FAILED. REPAIRED CHAFED POWER WIRES ABOVE SEATS 20 F AND G, OPS CK NORMAL.

Part: FLOORBEAM — CRACKED (BS 1329)

DURING REPLACEMENT OF AN OVERHEAD CEILING PANEL IN THE AFT BAG BIN DAMAGE WAS FOUND ON THE BS 1329 FLOORBEAM AT LBL 11 AND RBL 11. REPAIRED PER ERA 333177-14, REV A.

Part: BULB — FAILED (RT MLG)

ON FINAL APPROACH, LANDING GEAR SELECTED DOWN, RIGHT MAIN GEAR SHOWED UNSAFE. ACCOMPLISHED ALTERNATE GEAR EXTENSION PROCEDURE AND LANDING WITH UNSAFE INDICATION. LANDING AND ROLLOUT WITHOUT INCIDENT. RELAMPED RIGHT MAIN GEAR LIGHT IN COCKPIT. ALL INDICATION NORMAL.

Part: WEDGE — DELAMINATED (NR 8 LE SLAT)

THE RT NR 8 SLAT WAS FOUND WITH A 2.5 DIAMETER AREA OF DELAMINATION ON THE UPPER SKIN OF THE TRAILING EDGE WEDGE. THE DAMAGE WAS TRIMMED AWAY AND REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364264-14AD.

Part: CHILLER — FAILED (FORWARD)

DURING TURN TO FINAL, SMELLED FUMES IN COCKPIT. F/AS COULD NOT SMELL THE FUMES IN CABIN AND COULD NOT DETERMINE THE SOURCE. WHILE TAXIING IN RECEIVED AN EICAS LT PACK TEMP MSG WITH INOP, LT IN LT PACK SW. ODD SMELL COMING FROM FORWARD CHILLER. PULLED AND CLAMPED C/B. REPLACED CHILLER.

Part: ENGINE — FAILED (NR 2)

SMOKE IN CABIN, LANDED IN JAX. AFTER INSPECTION FOUND NR 2 ENG WITH METAL IN TAILPIPE AND FAN SEIZED. ENG BEING SHIPPED TO JAX FOR REPLACEMENT. REPLACED NR 2 ENGINE, OPS CHECK GOOD.

Part: WIRE — BROKEN (CABIN)

EMERGENCY FLOOR LIGHT AT SEAT 13 F/G TO MID LAV INOP. FOUND DAMAGE WIRE, RESPLICED WIRES AND CKS OK.

Part: WIRE — CHAFED (E/E COMPT)

FOUND NUMEROUS CIRCUIT BREAKERS TRIPPED ON P6-4 PANEL. REPAIRED WIRES JUST AFT OF CHILLER UNIT IN E/E AREA IN WIRE RUN W272. OPERATIONAL CHECK GOOD.

Part: FAN — FAILED (AC DIST)

ON DESCENT, FTL DECK AND CABIN CREW REPORTED SMOKE ODOR. THEN LEFT RECIC FAN ADVISORY MESSAGE ILLUMINATED, DEACTIVATED FAN. FAN WAS REPLACED OPERATION NORMAL.