N136DL

Part: SHROUD — FAILED (EMERGENCY LIGHT) · airframe 72,469 hrs · 30,020 cycles

EMERGENCY FLOOR LIGHTING INOPERATIVE AT 46A. MAINTENANCE REPLACED EMERGENCY LIGHT SHROUD AT 46 A/B. SYS OPS IS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,793 hrs · 29,829 cycles

EMERGENCY LIGHT INOPERATIVE AT 19B. MAINTENANCE INSTALLED A NEW EMERGENCY LIGHT ASSEMBLY..

Part: SKIN — CRACKED (BS 1725) · airframe 69,921 hrs · 29,312 cycles

BS 1725 S7R SKIN CRACKED, REPAIRED IAW ERA 522378-14AD.

Part: FLOOR SUPPORT — CORRODED (BS 1483) · airframe 69,921 hrs · 29,312 cycles

RT AFT LAVATORY OTBD FLOOR SUPPORT CORRODED AT ZEE ANGLE RADIUS FOR R2 DOOR THRESHOLD, BS 1483.

Part: SKIN — CORRODED (BS 933-955) · corrosion level 2 · airframe 69,921 hrs · 29,312 cycles

INSPECTION FOUND CORROSION AT UPPER CENTER WING SKIN PANEL RT SIDE, RBL 97 AND BETWEEN BS 933 AND 955. REPAIRED IAW ERA 522253-14.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 69,921 hrs · 29,312 cycles

STRINGER 7 END TIE FITTING DAMAGED. REPAIRED IAW ERA 522-483-14.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 69,715 hrs · 29,248 cycles

ROW 35GF EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE. OPS CHECKED NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 69,715 hrs · 29,248 cycles

ROW 4AB AFT EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT CONNECTOR. OPS NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 62,786 hrs · 27,285 cycles

EMERGENCY OVERHEAD PROXY LIGHTS AT ROW 4 AND 17 ARE INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT ROW 4 AND SEAT 17A. SYSTEM OPERATION IS NORMAL.

Part: RIB — CRACKED (NR 1 ENGINE) · airframe 61,335 hrs · 26,886 cycles

NR 1 ENGINE AFT FAN ASSY / AFT FAN CASE FWD RIB CRACKED AT 12 O'CLOCK POSITION DURING INSTALLATION. NR 1 ENGINE AFT FAN CASE CRACKED FWD T RIB REPAIRED IAW ER/A 488809-14 REV ORIGINAL.

Part: FITTING — DAMAGED (NR 2 PYLON) · airframe 61,335 hrs · 26,886 cycles

NR 2 PYLON O/B MID SPAR FITTING BOTH I/B AND O/B HOLES DIA FOUND GREATER THAN 0.875"-0.877" DURING ACCOMPLISHMENT OF EA 01-074904-03AD REV D. NR 2 PYLON O/B MID SPAR UNDERWING FITTING I/B AND O/B HOLES REWORKED AND REPAIRED PER ER.A 488810-14AD REV ORIG.

Part: FITTING — DAMAGED (NR 1 PYLON) · airframe 61,335 hrs · 26,886 cycles

NR 1 PYLON O/B MID SPAR FTF BOTH I/B AND O/B HOLES DIAMETER FOUND GREATER THAN 0.875"-0.877" DURING ACCOMPLISHMENT OF EA 01-074904-03AD REV D. NR 1 PYLON O/B MID SPAR UNDERWING FTG BOTH I/B AND O/B HOLES REWORKED AND REPAIRED IAW ER/A 488810-14AD REV ORIGINAL.

Part: FITTING — DAMAGED (NR 1 PYLON) · airframe 61,335 hrs · 26,886 cycles

NR 1 PYLON I/B MID SPAR FITTING BOTH I/B AND O/B HOLE DIA FOUND TO BE GREATER THAN 0.875"-0.877" DURING ACCOMPLISHMENT OF SIP MOD PER EA 01-074904-03AD REV D. NR 1 PYLON MID SPAR UNDER WING FITTING BOTH I/B AND O/B HOLES REWORKED AND REPAIRED PER ER/A488810-14AD REV ORIG.

Part: FITTING — DAMAGED (NR 2 PYLON) · airframe 61,335 hrs · 26,886 cycles

NR 2 PYLON I/B MID SPAR FTG I/B HOLE DIA FOUND GREATER THAN 0.875"-0.877" DURING ACCOMPLISHMENT OF SIP MOD PER EA 01-074904-03AD REV D. NR 1 PYLON I/B MID SPAR UNDERWING FTG I/B HOLE. REWORKED AND REPAIRED PER ER/A 488810-14AD REV ORIGINAL.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 61,335 hrs · 26,886 cycles

FUSELAGE SKIN EXTERIOR SURFACE AT STA 390 LT STR 12L PREVIOUS EXTERNAL REPAIRED DOUBLER UN-IDENTIFIED. AREA EVALUATED AND FOUND REPAIR NOT COMPLIED WITH APPROVED REPAIR PER SRM AND 02EA OVERSIZED FASTENER INSTALLED. EXISTING REPAIR REMOVED EVALUATED AND AREA REPAIRED PER ER/A488798-14 REV ORIG.

Part: SPAR — CRACKED (RT PYLON) · airframe 61,335 hrs · 26,886 cycles

DURING HFEC OPEN HOLE INSP OF FASTENER HOLES PER SB767-54-0081 REV 1 FIG 20 THE OUTBOARD AFT FASTENER HOLE FOUND WITH CRACK INDICATION IN THE AFT SPAR WEB AND MID STRUT BULKHEAD FITTING. 767 SIP MOD (GE ENGINE) - RT STRUT, FREEZE PLUG REPAIR ON OUTBOARD AFT FASTENER HOLE COMMON TO FWD UPPER SPAR FITTING, AFT UPPER SPAR WEB, MID STRUT BULKHEAD FITTING IAW ER/A 488789-14AD .

Part: STRAP — CRACKED (NR 2 PYLON) · airframe 61,335 hrs · 26,886 cycles

767 SIP MOD (GE ENGINE)-RT WING (01EA) FASTENER HOLE ON NR 2 STRUT STRAP ,CHORD P/N :311T3156-1 FOUND GOUGED WHEN ACCOMPLISHING SB 767-54-0081 FIG 7 OPEN HOLE. HFEC INSPECTION, DAMAGED FASTENER HOLE 01 EA AT NR 2 PYLON I/B FWD MOST HOLE COMMON TO MID SPAR FITTING & HORIZONTAL CHORD REPAIRED PER ER/A488815-14AD.

Part: SKIN — CRACKED (RT WING) · airframe 61,335 hrs · 26,886 cycles

HFEC OPEN HOLE INSP CARRIED OUT ON RT WING UPPER LINK PITCH LOAD FITTING, COMMON TO WING IN REF TO SB B767-54-0081, FIG 38, REV 1 AND FOUND 03EA HOLES WITH CRACK INDICATION ON UPPER SKIN. 03 EA HOLES ON RT WING UPPER SKIN REPAIRED IAW ER/A 488787-14AD, REV 0.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 61,335 hrs · 26,886 cycles

AFT CARGO STA 1197 AT RBL 6.5 AND RBL 44.0 FLOORBEAM UPPER CHORD FOUND CORRODED. FLOORBEAM UPPER CHORD TRIMMED AT RBL 0 AND REMOVED BET RBL0 TO RBL 44.0 AND SECTIONAL CHORD REPAIR CARRIED OUT IAW SRM 53-00-07, FIG 201, REPAIR 4 OTIS.

Part: FLOORBEAM — CORRODED (BS 1219) · airframe 61,335 hrs · 26,886 cycles

AFT CARGO STA 1219, LBL 35.0 AND LBL 44.0 FLOORBEAM UPPER CHORD FOUND CORRODED. FLOORBEAM UPPER CHORD TRIMMED AT LBL 14 AND REMOVED BET LBL 14 TO LBL 44.0 AND SECTIONAL CHORD REPAIR CARRIED OUT IAW SRM 53-00-07, FIG 201, REPAIR 4 OTIS.

Part: SPAR — CRACKED (NR 1 PYLON) · airframe 61,335 hrs · 26,886 cycles

NR 1 PYLON MID SPAR FWD WEB FOUND CRACKED DURING ACCOMP OF SB 767-54-0081 REV 1. NR 1 PYLON MID SPAR CRACKED WEB REPAIRED IAW ER/A 488781-14.

Part: FLOORBEAM — CORRODED (BS 287) · airframe 61,335 hrs · 26,886 cycles

FWD GALLEY AREA FLOORBEAM AT STA 287 UPPER HORIZ FLANGE UPPER SURFACE FOUND CORRODED AT RBL22 (NRC 0634 ) AND RBL 62 (NRC 0635). CORROSION AT RBL 62 IS ON EXISTING REPAIR. CABIN FLOORBEAM AT STA 287 UPPER HORIZ FLANGE CUT AND TRIMMED BET RBL8 TO RBL45 FROM RBL45 TO RBL 84.5 EXISTING REPAIRED TEE REMOVED AND NEW TEE REPAIR CARRIED OUT IAW SRM 53-00-51, FIG 201, REPAIR 1 BET RBL 8 TO RBL 84.5.

Part: STRINGER SPLICE — CORRODED (BS 434 S34R) · airframe 61,335 hrs · 26,886 cycles

FWD CARGO: STRINGER 34 RT AT STA 434 FOUND CORRODED. STA 434, STRINGER 34R REPAIRED IAW SRM 53-30-03, FIG 201, REPAIR 1.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 56,274 hrs · 25,530 cycles

CTR HYD QTY DROPPING IN FLT, FOUND HYD LINE FROM BRAKE CNTRL VALVE SOLENOID TO "T" FITTING ON OUTBOARD SIDE OF VALVE LEAKING. FLT CREW VERBAL PUMPS TURNED OFF AT .4 QTY REPLACED HYD LINE FROM BRAKE CONTROL VALVE SOLENOID TO T FITTING ON OUTBOARD SIDE OF VALVE. CYCLED ELEC PUMPS AND ADP. CYCLED GEAR HANDL AND FLT CONT SVCD HYD TO FULL

Part: STARTER — OVERHEATED (APU) · airframe 55,961 hrs · 25,448 cycles

AFTER APU START NOTICED ACRID SMELL IN CABIN. NO VISIBLE SMOKE. FOUND STARTER ON APU BURNED. APU BATTERY AND CHARGER DEAD. REMOVED AND REPLACED APU BATTERY/CHARGER AND STARTER IAW AMM. CHECKED SPRAG CLUTCH NTF. ACFT OK FOR SERVICE.

Part: ACTUATOR — MALFUNCTIONED (NR 6 SPOILER) · airframe 54,715 hrs · 24,994 cycles

ON DEPARTURE FROM LAS CREW REPORTED TO DISPATCH THAT L HYD QTY READ ZERO. DISPATCH NOTIFIED MCC THAT ACFT WAS RETURNING TO LAS. REMOVED AND REPLACED NR 6 SPOILER PCA PER AMM. PERFORMED REQUIRED INSPECTION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,134 hrs · 24,777 cycles

HMV AT YVR, THE INNER CHORD OF THE RT STA 903.5 FRAME WAS FOUND CRACKED. THE CRACK WAS REPAIRED PER ER/A 01-098604-14AD INSTRUCTIONS. NOTE: AT THE TIME OF ISSUE, THE ER/A WAS NEVER FORMALLY APPROVED, NOR WAS AN MRR ISSUED. THIS SUBMITTAL CORRECTS THIS SITUATION.

Part: SKIN — DENTED (FUSELAGE) · airframe 54,134 hrs · 24,777 cycles

HMV AT ACTS, A FUSELAGE SKIN DENT WAS FOUND AND REPAIRED PER ER/A 01-098988-14. NOTE: AT THE TIME OF ISSUE, THE ER/A WAS NEVER FORMALLY APPROVED, NOR WAS AN MRR SUBMITTED. THIS SITUATION HAS NOW BEEN CORRECTED.

Part: APU — MALFUNCTIONED · airframe 52,433 hrs · 24,226 cycles

SMOKE DETECTORS AT STATIONS 214-215-219 SOUNDED DUE TO LIGHT OIL MIST IN THE CABIN, ALL 3 MID LAVS. THIS HAPPENS ONLY ON THE GROUND WITH APU AIR AND NO ENGS RUNNING. FWD APU TO MCO AND PLACARD PER MEL 49-11-01A. REPLACED APU PER M/M. LEAK CKS GOOD. GENERATOR CKS GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 52,125 hrs · 24,101 cycles

FOUND EMERGENCY LIGHT AT SEAT 26F INOP. REPAIRED BROKEN WIRE AND RELAMPED.

Part: ACTUATOR — CRACKED (NR 5 SPOILER) · airframe 51,375 hrs · 23,822 cycles

DURING TAXI C HYD LOW PRESS LIGHT ILLUM AND QTY WENT TO 0. A/C TOWED BACK TO GATE. FOUND NR 5 SPOILER ACT HOUSING CRACKED. REPLACED SAME, OP CHK AND LEAKS NORMAL.

Part: CONTROL CABLE — BROKEN (LT AILERONS) · airframe 50,545 hrs · 23,551 cycles

LEFT OUTBOARD AILERON LOCKED IN DOWN POSITION. FOUND CABLE A3B-3 FOR LT O/B AIL BROKEN JUST O/B OF THE LT O DROOP QUADRANT. REMOVED BROKEN CABLE RECEIVED NEW CABLE FROM BOEING P/N BACC2C4C04961FG. REPLACED CABLE A3B PER OPN 2000 CABLE REPLACEMENT AND RIGGED. CHECKED PER M/M.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 43,600 hrs · 20,939 cycles

LIGHTENING STRIKE BLEND OUT AT STA 390 STR 12L BEYOND LIMITS REF SRM 53-00-01 FIG 101. SKIN REPAIRED PER SRM 53-00-01 FIG 201 CAT B REPAIR REPEAT INSPECTIONS PER SRM 53-00-01 FIG 201. AIRCRAFT LOG ITEM F744553.

Part: SMOKE — DETECTED (CABIN) · airframe 42,897 hrs · 20,604 cycles

VISIBLE HAZE / FUMES IN AFT CABIN WITH ENGINE ANTI-ICE ON. RAN ENGINE AND APU WITH PACKS ON, RAN CARGO HEAT, RAN GALLEY OVENS AND ENTERTAINMENT SYSTEM. RAN POTABLE WATER COMPRESSOR, NO SIGNS OF FUMES OR HAZE.

Part: TUBE — UNSERVICEABLE (HYD SYSTEM) · airframe 42,000 hrs · 20,177 cycles

C-HYD QTY DRAINED TO 0 WITH SUBSEQUENT C-SYS FAILURE. FOUND CRACKED HYD LINE RT WHEEL WELL REF IPC 32-31-55- 01 ITEM 519. INSTALLED INTERIM LINE. LEAK CHECK OK. LINE TO BE INSPECTED WITHIN 175 FLT HRS AND REPLACED WITH PERMANENT LINE WITHIN 350 FLT HRS, NEEDS NEW LINE DAL P/N 321204711.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,937 hrs · 19,633 cycles

1L DOOR SLIDE LIGHT INOP. REPAIRED SAME.

Part: LANYARD — SEPARATED (ESCAPE SLIDE) · airframe 37,716 hrs · 17,946 cycles

DOOR DIFFICULT TO ARM/DISARM. SLIDE PACK FELL OUT WHILE DOOR WAS OPENING (2R). INSTALLED NEW SLIDE, OPS NORMAL.

Part: CHARGER — FAILED (EMERGENCY LIGHT) · airframe 36,343 hrs · 17,282 cycles

LOWER EMERGENCY LIGHTS AT FWD LT AND RT DOORS EXIT SIGNS INOPERATIVE. REPLACED BATTERY CHARGER AND BATTERY PACK OPS CK GOOD

Part: LIGHT — INOPERATIVE (ESCAPE SLIDE) · airframe 36,234 hrs · 17,228 cycles

2L DOOR SLIDE LIGHT INOPERATIVE, RELAMPED - OPS NORMAL.

Part: IDG — FAILED (LT ENGINE) · airframe 34,578 hrs · 16,397 cycles

BOTH GENS FAILED AT 1500 FT AFTER TAKEOFF FOR ABOUT 10 SEC/RT GEN CAME BACK ON LINE. LEFT GEN REMAINED FAILED. CK'D OIL LEVEL ON RT IDG FOR CORRECT SERVICING, ALL GOOD. RAN RT ENG, RT IDG CKS GOOD. REPLACED LT ENG IDG PER M/M. RAN LT ENG, IDG OPS AND LEAK CKS GOOD.

Part: MANIFOLD — DEFECTIVE (NR 2 ENGINE) · airframe 34,269 hrs · 16,248 cycles

ENGINE FLAME-OUT ON CLIMBOUT AT 34000. RETURNED FOR LANDING AT MCO. ENGINE FAILED NO MORE THAN 27 MINUTES FROM LANDING. REPLACED FUEL MANIFOLDS AT 11 O'CLOCK AND 6 O'CLOCK POSITIONS RAN NR 2 ENG PER PFHB TEST 4 T/O POWER AND LEAK CK ALL PARAMETERS OK OK FOR SVC. ALSO REPLACED RIGHT ENGINE FUEL FILTER.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 33,337 hrs · 15,780 cycles

FLASHLIGHT INOP FWD AC. REPLACED SAME.

Part: SKIN — DENTED (FUSELAGE) · airframe 32,181 hrs · 15,235 cycles

AN EXISTING SKIN REPAIR WAS FOUND WITH A DENT AREA AT THE UPPER EDGE ROW OF THE REPAIR AT BS 1197+78. THE EXISTING REPAIR WAS REMOVED AND ALL UNDELYING DAMGE CUTOUTS COMBINED INTO ONE CUTOUT EXTENDING FROM STRINGER 38L TO STRINGER 36L.THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B767 SRM 53-00-01, FIG. 212 AND ER/A 380365-14.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 32,181 hrs · 15,235 cycles

ON L/O FOUND RIGHT OVERWING FORWARD EMERGENCY LIGHT INOP. RELAMPED

Part: PANEL — FAILED (COCKPIT OVERHEAD) · airframe 30,742 hrs · 14,518 cycles

ON DESCENT, SMOKE IN COCKPIT WITH BURNING RUBBER SMELL, SMOKE VISIBLE TO THE EYE. DECLARED EMERGENCY. C/W APPLICABLE POM. FOUND LT R-W T/O SWTCH LIGHT ASSY AND TERMINAL WIRE LUG BURNT AND MELTED. REPLACED WHOLE PANEL ASSY, OPS CKS GOOD.

Part: ENGINE — LEAKING (NR 1) · airframe 30,579 hrs · 14,435 cycles

LOSS OF OIL QTY DURING FLT WITH DECREASING OIL PRESSURE. AT TOP OF DESENT WITH THROTTLE TO IDLE OIL PRESSURE WENT THRU 10 PSI INTO RED AREA AND CREW SHUT DOWN ENG. ENG WINDMILLED FOR 15 MIN WITH ZERO OIL PRESSURE. REPLACED ENGINE.

Part: A/C PACK — MALFUNCTIONED (LEFT) · airframe 29,874 hrs · 14,111 cycles

AFTER APPLYING TAKEOFF POWER THE COCKPIT AND FORWARD FLIGHT ATTNDS SMELLED A VERY STRONG ELECTRICAL BURNING SMELL NOT ACCOMPANIED BY SMOKE. NORMAL RETURN TO KTPA.

Part: FLOORBEAM — DAMAGED (BS 500)

DAMAGE FROM CONTACT WITH A CARGO CONTAINER WAS FOUND ON THE BS 500 FLOORBEAM BETWEEN RBL AND LBL 11. THE DAMAGE NECESSIATED REMOVAL THE FLOORBEAM SECTION BETWEEN R/LBL 11. REPAIRED PER ERA 333197-14, REV A.

Part: STRIP — DAMAGED (CABIN)

WKG MCO-CLOSET 2L EMER TRACK LIGHTING STRIP DAMAGED. REPLACED STRIP, OPS CK NRML. REMOVED MCO.

Part: SKIN — DAMAGED (BS 368-375)

A HOLE WAS FOUND IN THE FUSELAGE SKIN BETWEEN STA 368-375 AND STR 20L-21L. THE HOLE MEASURED APPROX 3 INCHES DIAMETER AND HAD SEVERAL LARGE CRACKS EMINATING FROM THE HOLE. THE DAMAGED SKIN WAS TRIMMED OUT TO AN APPROX 8 FWD/AFT BY 7 CIRCUMFERENTIAL HOLE. TIME LIMITED REPAIR PER B767-300 SRM 53-00-01, FIG. 201 EXCEPT INSTALL DOUBLER AND FASTENERS AS SHOWN IN FIG; PERMANENT REPAIR - CONTACT LIAISON ENGINEERING - LIMITED TO 12 MONTHS SERVICE; VISUAL INSPECT EVERY 1000 FLIGHT CYCLES.

Part: LINE — CRACKED (LT HYD SYST)

LT HYD PRESS CAUTION WITH LT HYD QTY AND RUDDER RATIO ADVISORY MESSAGES ILLUMINATED. LT HYD QTY READS ZERO.

Part: IDG — OVERHEATED (NR 2 ENGINE)

ON CLIMBOUT, HAD RT ENG STARTER EICAS MSG. ACCOMPLISHED STARTER CUTOUT PROCEDURE WITH NO AVAIL. WITHIN A COUPLE OF MINUTES HAD RT ENG FIRE ANNUNICATED. ENGINE SHUTDOWN FIRE BOTTLES, BOTH USED. RT ENG IDG OVERHEATED CAUSING ENGINE FIRE.

Part: ARMED LIGHT — FAILED (2 L DOOR)

2L DOOR SLIDE ARMED LIGHT NOT ILLUMINATING WHEN THE SLIDE IS ARMED. LIGHT ASSY PRESS-TO-TESTS NORMALLY. CORRECTIVE ACTION - FORWARD TO MCO AND PLACED PER MEL. REPLACED LIGHT ASSEMBLY OPERATION NORMAL.

Part: LAMP — FAILED (2L DOOR)

SLIDE LIGHT 2L DOOR INOP. RELAMPED, OPN NML.

Part: DISPENSER — SHORTED (AFT GALLEY)

DURING CRUISE, FLIGHT ATTENDANT REPORTED SMOKE AND BURNING ODOR FROM COFFEEMAKERS IN AFT GALLEY. REMOVED POWER, AND ODOR STOPPED. FOUND THE RIGHT REAR COFFEEMAKER SHORTED. REPLACED COFFEEMAKER OPERATION NORMAL.