N130DL

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,982 hrs · 34,963 cycles

AFT EMERGENCY CEILING LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE M734 POWER SUPPLY AND BATTERY AT SEAT 45. SYSTEM OPS NORMAL.

Part: SKIN — DAMAGED (BS 654) · airframe 82,651 hrs · 34,867 cycles

LIGHTNING STRIKE ON SKIN BS 654+44 AND TWO INCHES BELOW S24R. REPAIRED IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 721) · airframe 82,651 hrs · 34,867 cycles

LIGHTNING STRIKE ON SKIN AT BS 721 S24R. REPAIRED IAW SRM 53-00-01.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,502 hrs · 34,827 cycles

EMERGENCY LIGHTS AT ROWS 25-34 ARE INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK AND CHARGER. SYSTEM OPS ARE NORMAL.

Part: FRAME — CRACKED (BS 859) · airframe 81,541 hrs · 34,564 cycles

INNER ANGLE CRACKED ON FWD SIDE OF FRAME BS 859.5 BELOW WL 200 . REPAIRED IAW WC 5311-01195-09-01A.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 81,012 hrs · 34,421 cycles

FOUND RT INBD T/E FLAP PUNCTURED AND GOUGED ON TOP SURFACE. DAMAGE LOCATED UNDER OTBD SECTION OF NR 7 SPOILER. TIME LIMITED REPAIR IAW ERA 524625-14.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,495 hrs · 34,265 cycles

EMERGENCY ESCAPE PATH LIGHTS FIRST 6 ROW ON RT SIDE ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. SYSTEM OPS ARE NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 80,253 hrs · 34,191 cycles

EXIT LIGHT ABOVE 1L DOOR AND 1R DOOR HANDLES NOT OPERATING DURING EMERGENCY LIGHT TEST. REPLACED BATTERY PACK IN CHARGER M1208.

Part: SKIN — DAMAGED (BS 604-610) · airframe 78,652 hrs · 33,711 cycles

FOUR LIGHTNING STRIKES ON SKIN BETWEEN BS 604 -610 STRINGERS 34 - 35L. DRILLED OUT DAMAGE ON UPPER TWO STRIKES AND CUT OUT DAMAGE ON LOWER TWO STRIKES. C/W HFEC INSPECTION OF UPPER TWO STRIKES IAW SRM 53-00-01, REPAIR 8, SECTION 1. NO DISCREPANCIES. C/W PRI 51488-14 REV 0, 1, 2, 3, & 4. (369710) C/W ERA 514488-14 REV, ORIGINAL PERMAMANT REPAIR.

Part: SLIDE — UNKNOWN (OVERWING) · airframe 78,245 hrs · 33,588 cycles

OVERWING SLIDES DISARMED. REARMED SLIDES. SYSTEM CHECKS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 78,210 hrs · 33,578 cycles

FOUND ONE EXIT EMERGENCY LIGHT INOPERATIVE. R & R POWER SUPPLY AND BATTERY, OPS CHECKED OK IAW AMM 33-.

Part: FLOORBEAM — DAMAGED (BS 287) · airframe 87,400 hrs · 36,230 cycles

ELONGATED HOLES AT BS 287 FLOORBEAM TO FRAME INTEGRATION AT RBL 85. REPAIR IAW ER/A 00-512821.

Part: FLOORBEAM — CORRODED (FS 287 RBL 11-77) · airframe 78,019 hrs · 33,529 cycles

CABIN-FWD GALLEY STA 287 RBL 11-77 FLOORBEAM UPPER TEE CORROSION. REPAIRED IAW ERA 512480-14, REV. ORG.

Part: STRUCTURE — CORRODED (BS 852 RBL77-88) · airframe 78,019 hrs · 33,529 cycles

CABIN - STA 852, RBL 77-88 FOUND CORRODED ON CENTER WING SECTION UPPER SURFACE AND REPAIR CARRIED OUT IAW ER/A 511834-14, REV O.

Part: FLOORBEAM — CRACKED (BS 303) · airframe 78,019 hrs · 33,529 cycles

CABIN STA 303,LBL 33 FLOORBEAM WEB FOUND CRACKED AND REPAIRED CARRIED OUT IAW ER/A 511855-14, REV 0.

Part: FLOORBEAM — CORRODED (FS 287 RBL 11-77) · airframe 78,019 hrs · 33,529 cycles

CABIN-FWD GALLEY STA 287, RBL 11-77 FLOORBEAM UPPER TEE FOUND CORROSION WITH ELONGATED HOLES IN FRAME. REPAIRED IAW ERA 512821-14, REV ORG.

Part: LONGERON — DAMAGED (BS 783) · airframe 78,019 hrs · 33,529 cycles

TEN FASTENER HOLES FOUND WITH SHORT EDGE CONDITION ON RT LONGERON, BS 783. ACCOMPLISHED IAW ER/A 511858-14AD, REV ORIGINAL.

Part: LONGERON FITTING — CRACKED (RT WING) · airframe 78,019 hrs · 33,529 cycles

RT UNDERWING LONGERON FITTING ROUND CRACKED AND REPLACEMENT CARRIED OUT IAW EA 01-499898-03AD.

Part: SKIN — CORRODED (BS 1197-1219) · airframe 78,019 hrs · 33,529 cycles

LWR FX-REPAIR DOUBLER AT STA 1197+110 - 1219 STR 37L - 37R EXTERNAL SURFACE CORRODED. COMPLIED WITH ER/A 512461-14, REV O.

Part: SKIN — CORRODED (BS 1153-1197) · airframe 78,019 hrs · 33,529 cycles

DURING STRINGER REPAIR FOUND CORROSION ON FX SKIN FROM STA 1197 TO STA 1197+22 STR 36R. REPAIR IAW ERA 512462-14, REV ORIGINAL.

Part: STRUCTURE — CRACKED (BS 1725.5) · airframe 78,019 hrs · 33,529 cycles

CRACKED LOCATION ON STRIP AT STR 7R, TRIMMED OFF IAW SRM 53-80-01, REPAIR 5, FIG 201. REV 91.02. REPAIR PARTS FABRICATED IAW SRM 53-80-01, FIG 201, REPAIR 5. REV 91.02 REPAIR PARTS AT BS 1725.5, STR 7R INSTALLED IAW SRM 53-80-01 FIG 201. REPAIR 5. REV 91.02.

Part: WIRE — CUT (CABIN) · airframe 75,556 hrs · 32,809 cycles

EMERGENCY FLOOR LIGHTING DAMAGED LEFT SIDE ROW 11-20/35-46. RIGHT SIDE ROW 1-11/25-34. RT FWD COAT CLOSET RED LIGHT INOP. WIRE BEHIND SEAT 5A NEEDS SPLICE INSTALLED. WIRE WAS CUT. REPAIRED WIRING BEHIND SEAT 5A. FOUND WIRES SHORTED AT SEAT 17AB. REPAIRED SAME. RE-INSTALLED ORIG POWER SUPPLY M9008. REPLACED FUSES F1 AND F3 ON POWER SUPPLIES M9008 AND M9009 ALL PER B767 WSPM CH 20. ALL EMERGENCY LIGHTS NOW OPS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 75,354 hrs · 32,755 cycles

EMERGENCY LIGHTS AT SEATS 35-46 LEFT ARE INOPERATIVE. MTC REPLACED THE POWER SUPPLY M9010. SYSTEM OPERATION IS NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 75,109 hrs · 32,688 cycles

MAINTENANCE FOUND EMERGENCY LIGHTS INOPERATIVE AT ROWS 39-46 RT SIDE AND 25-32 LEFT SIDE. THE BATTERY CHARGER WAS REPLACED. SYSTEM OPERATION IS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 74,353 hrs · 32,475 cycles

EMERGENCY LIGHTS AT SEATS 25-34FG AND ROWS 35-44ABC ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND POWER SUPPLY PER AMM. SYSTEM OPERATION IS GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 74,326 hrs · 32,468 cycles

SEAT MOUNTED EMERGENCY LIGHTS ROWS 25-34FG AND 34-46AB ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER M9010 SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,204 hrs · 31,893 cycles

DURING OP 2525 FOUND EMERGENCY LIGHT INOPERATIVE FROM ROWS 1-12 RIGHT SIDE AND 13-21 LEFT SIDE. MAINTENANCE REPLACED M9008 AND M9009 PER AMM. SYSTEM OPERATION IS NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 71,588 hrs · 31,730 cycles

EMERGENCY LIGHTS AT ROWS 1-12 RT SIDE AND 13-21 LT SIDE ARE INOPERATIVE. MX REPLACED THE BATTERY CHARGER AND BATTERY ASSY, M9009. SYS OPS IS NORMAL.

Part: CONTROL ROD — LACK OF LUBE (AILERON) · airframe 66,853 hrs · 30,482 cycles

RTB DUE TO ON TAXI OUT AILERONS BINDING. DURING FLT CONTROL CHECK BINDING OCCURRED 1/2 WAY THRU LEFT ACTUATION. MULTIPLE OCCURRENCES BOTH SIDES LT AND RT BIND INTERMITTENTLY. T/S PER FIM 27-11-00-101. REMOVED, CLEANED, LUBRICATED AND REINSTALLED CONTROL RODS AND LUBED TOWER SHAFTS. OPS CHECK GOOD RII C/W.

Part: TARGET — UNSERVICEABLE (NR 10 SLAT) · airframe 64,540 hrs · 29,728 cycles

AFTER TAKEOFF APPROX 200FT AGL, THE STICK SHAKER ACTIVATED. AIRSPEED WAS NML AND FLAPS 15DEG. DURING FLAP RETRACTION RECEIVED LEADING EDGE SLAT ASYM CAUTION MSG. PERFORMED QRH PROCEDURE. FOUND DAMAGED TARGET AT NR 10 SLAT INBD TRACK. REPLACED SAME. REPLACED PROX BOX DUE TO NOT INDICATING TARGET PROBLEM.

Part: SKIN — CORRODED (BS1175-1197 S36R) · airframe 60,704 hrs · 28,426 cycles

DURING HMV3 AT MOBILE AEROSPACE ENGINEERING, FOUND AFT PIT AT S36R OTBD LOWER FLANGE EXFOLIATED BS 1175 TO BS1197. REMOVED DAMAGED AREA AND INSTALLED REPAIR STRINGER AND FUSE DOUBLER REF SRM 53 00 01 FIG 201 REPAIR 12.

Part: BULKHEAD — PUNCTURED (BS 1528) · airframe 60,704 hrs · 28,426 cycles

DURING HMV AT MOE, THE AFT PRESSURE BULKHEAD SUSTAINED TOOLING DAMAGE WHICH RESULTED IN A PUNCTURE IN THE WEB.

Part: FRAME — CRACKED (BS 903.5) · airframe 60,704 hrs · 28,426 cycles

DURING HMV3, THE LT BS 903.5 INBOARD CHORD WAS FOUND CRACKED AT WL 190.

Part: SKIN — DAMAGED (BS 785-915 S8L) · airframe 60,704 hrs · 28,426 cycles

DURING HMV3 AT MOBILE AREOSPACE ENGINEERING, FOUND LT FUSELAGE STA 785.9-915, S2L, S8L HAS LIGHTNING STRIKES. REMOVED DAMAGE AND FAB`D DOUBLER REF SRM 530001 REPAIR 4.

Part: SKIN — DAMAGED (BS 915-1065) · airframe 60,704 hrs · 28,426 cycles

LT FUSE STA 915-1065, S4-7L HAS LIGHTNING STRIKE DAMAGE. REMOVE DAMAGED AREA INSTALLED DOUBLER REF SRM 530001 REPAIR 4.

Part: FLOORBEAM — CORRODED (BS 1219) · airframe 60,704 hrs · 28,426 cycles

DURING HMV3 FOUND AFT PIT STA 1219 UPPER CHORD CORRODED OUT OF LIMITS AT LBL 23 TO LBL 30. REMOVED DAMAGE SECTION AND REPAIRED PER SRM 53-00-07 REPAIR NR 4.

Part: FLOORBEAM — CORRODED (BS 287 RBL 26) · airframe 60,704 hrs · 28,426 cycles

DURING HMV3 AT MOBILE AEROSPACE ENGINEERING, FOUND MAIN CABIN FLOORBEAM T-CAP EXFOLIATED AT RBL 26, STA 287. REMOVED DAMAGED SECTION OF T-CAP AND REPAIRED PER SRM 53-00-51D.

Part: SKIN — DENTED (BS 1562 S26L) · airframe 60,704 hrs · 28,426 cycles

DURING HMV3 AT MOBILE AEROSPACE ENGINEERING, FOUND LWR FUSELAGE HAS DENT WITH OVER BURNISHED FASTENERS AT S26L STA 1562. REMOVED DAMAGE AND REPAIRED PER SRM 53-00-01 LAP SPLICE REPAIR.

Part: STRUCTURE — CORRODED (BS 1197) · airframe 60,704 hrs · 28,426 cycles

DURING HMV 3 AT MAE, FOUND AFT PIT STA 1197+66 LBL 36 T CHORD CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-00-07. REPAIRED PER SRM 53-00-07 REPAIR 4.

Part: PUMP — LEAKING (RT ENGINE) · airframe 60,624 hrs · 28,403 cycles

RT HYD EICAS MSG RT HYDS DROPPED TO .016 THEN R HYD PUMP MSG CAME ON. OPENED UP RT ENG. FOUND RT ENG HYD PUMP LEAKING. SUSPECT ENG HYD PUMP FAILURE. PULLED RT T HANDLE. FOUND EDP CASE SEAM LEAKING. NO METAL IN CASE DRAIN OR PRESSURE FILTERS. FILTERS REPLACED. REPLACED EDP. ON LEAK CK FOUND PRESSURE HOSE LEAKING. REPLACED PRESSURE HOSE. LEAK CK GOOD. COWLS CLOSED HYDS SERVICED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 59,280 hrs · 27,906 cycles

EMERGENCY PATH LIGHTS AT SEATS 13FG - 17FG DIM, 18FG, 19FG, AND 20FG INOP. REMOVED AND REPLACED BATTERY PACK ASSY.

Part: HOUSING — CRACKED (BRAKE MODULE) · airframe 56,439 hrs · 26,846 cycles

AFTER LANDING, RT HYD SYSTEM QUANTITY DROPPED TO 0, FOUND HOUSING ON BRAKE FUSE P/N V6-4360-2, RT WING BRAKE MODULE, CRACKED. REPLACED HOUSING.

Part: PROJECTOR — ODOR (CABIN) · airframe 55,087 hrs · 26,313 cycles

FLT 683 ATL - MBJ DIVERSION TO MCO, STRONG ODOR MID CABIN. ELECTRICAL SMELL. FOUND MID CABIN MOVIE PROJECTOR SOURCE OF SMELL. REPLACED PROJECTOR. ALL CKS OK. NO FURTHER SMELL NOTED.

Part: BOLT — LOOSE (NR 2 ENGINE) · airframe 55,073 hrs · 26,307 cycles

RT ENG FIRE IND INTERMIT DURING CLM. S/D ENG AND ATB TO ATL.C/A FOUND 4 BOLTS LOOSE ON HPT NOZZLE COOLING DUCTS AT HPC CASE 230 AND 330 POSITION. TIGHTENED SAME. REINSTALLED RMVD LOOPS. CKD SECURITY OF ALL LOOPS. RAN ENG AT 90 PCT FOR 5 MIN AND 103 PCT FRO 5 MIN. ALL CKS GOOD.

Part: BALL JOINT — UNKNOWN (NR 2 ENGINE) · airframe 55,072 hrs · 26,306 cycles

ON TAKEOFF GOT VERY RAPID INTERMITTENT R ENG FIRE WARNING. ALSO, GOT INTERMITTENT R ENG FIRE LOOP 1 STATUS MSG. FIRE WARNING GOES AWAY WHEN BELOW ABOUT 85 PERCENT N1. T/S PER FIM. FIRE AND O/H LOOP RESISTANCE VALUES NORM. RAN ENG TO TAKEOFF POWER PER PFHB. RT ENG FIRE LOOP 1 MSG AT 80 % N1. FIRE WARNING AT 103 PERCENT N1. OPENED RT ENG EVIDENCE OF DUCT LEAK JUST UPSTREAM OF PRECOOLER. BACK PRESSURED WITH APU AIRFOUND MULTIPLE DUCT LEAKS. REPLACED CLAMP AND SEAL 8TH STAGE DUCT TO PRECOOLER. REPLACED BALL JOINT AT 8TH STAGE CHECK VALVE. TIGHTENED BALL JOINTS AT HPSOV AND 8TH STAGE CK VLV.

Part: CONNECTOR — DAMAGED (ANTISKID MODULE) · airframe 48,798 hrs · 23,215 cycles

UPON TOUCHDOWN - NORMAL RATE APP 140 KTS. AUTOBRAKES DISARMED, AUTO SPEEDBRAKE DID NOT EXTEND UNTIL T/R EXTENDED,WHEEL BRAKES LEFT SIDE NEVER GOT ABOVE 0 INDICATION;RT SIDE BRAKES UP 5 & 6. EXITED AT EOR DUE TO BRAKING. REPLACED WHEEL ASSY 1,2,5,& 6. PERFORMED BURST TIRE INSP PER05-51-16-2. DURING TRANSDUCER SPIN TEST FOUND NR 1 BRAKE NOT RESPONDING; FOUND PUSHED BACK PIN ON CANNON PLUG FOR ANTISKID VALVE MODULE. RESEATED, SYS CKS OK.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 45,866 hrs · 21,805 cycles

AFTER APU WENT TO RUN, APU ANNUNCIATED FAULT AND SHUT DOWN (ACCOMPANIED BY ACRID SMELL MOMENTS LATER). RESET APU ECU, RAN APU UNDER LOAD NO FAULTS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,930 hrs · 21,368 cycles

DURING S/C FOUND FWD RIGHT CEILING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK.

Part: HARNESS — BURNED (CARGO BAY) · airframe 42,071 hrs · 19,993 cycles

ON L/O FOUND SEVERAL CIRCUIT BRAKERS POPPED. T/S AND FOUND WIRE BUNDLE SHORTED AND BURNT ABOVE C-1 CARGO DOOR CEILING. REPLACED/REPAIRED APPROX 80 WIRES. INCIDENT UNDER INVESTIGATION.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 41,962 hrs · 19,944 cycles

THE FUSELAGE SKIN WAS PUNCTURED AT FS 1197+88 BETWEEN STRINGERS 35L & 36L. THE DAMAGE WAS REMOVED WITH A 12 X 12 INCH CUTOUT CENTERED OVER THE STRINGER 36L SKIN LAP JOINT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND STRUCTURAL FILLER PER B767 SRM 53-00-01-2-212 AND ER/A 379789-14, REV A.

Part: BULKHEAD CAP — CRACKED (BS 1809)

THE OUTER CHORD OF THE FS 1809.5 BULKHEAD WAS FOUND WITH A CRACK AT RBL 45 & WL 250. THE CRACK IS TYPICAL OF THAT DOCUMENTED IN BAC S/B 767-53-0078. THE CRACK WAS REPAIRED PER THE PROCEDURES OF THE S/B AND ER/A 368310-14.

Part: ACTUATOR — CRACKED (NLG)

NOSE GEAR ACTUATOR FOUND CRACKED AT LOWER END. FOUND DURING LETTER CHECK VISIT.

Part: STARTER — FAILED (APU)

APU INOP, WILL NOT START. FOUND APU STARTER OVERHEATED AND BURNED ON OUTER CASE. REPLACED STARTER, APU OPS NORMAL.

Part: GCU — FAILED (NR 2 ENGINE)

DURING CLIMBOUT AT APPROX FL 250 PILOTS NOTICED ODOR IN COCKPIT. THE ODOR BECAME STRONGER, SEVERAL MINUTES LATER THE RT GEN OFF LIGHT ILLUMINATED WITH ASSOCIATED EICAS LIGHTS. THE INTENSITY OF ODOR REQUIRED USE OF COCKPIT OXYGEN MASKS. A/C DIVERTED TO JAX. REPLACED GCU, IDG AND PYLON DISCONNECTS D4216P AND D4266J. RAN ENGINE, SYSTEM CHECKS NORMAL.

Part: IDG — INOPERATIVE (NR 1 ENGINE)

AFTER GEAR RETRACTION, LOST LEFT ELEC BUSS. COULD NOT RETURN POWER TO BUSS, APU WOULD NOT PICK UP BUSS. PERFORMED BITE, REPLACED BPCU AND LEFT GCU, DISCONNECTED LT IDG AND SERVICED APU.

Part: EEL BULB — FAILED (CABIN)

DURING LAYOVER, RIGHT AND LEFT AFT ESCAPE SLIDE LIGHT OUT. RELAMPED, LIGHT CHECKS GOOD.

Part: EEL BULB — FAILED (CABIN)

OVERHEAD EMERGENCY WALKWAY LIGHTS INOP AT 39F, 47C AND 28C. RELAMPED, OPERATIONAL OK.

Part: SKIN — LIGHTNING STRIKE (FWD FUS)

FOUND DURING LETTER CHECK. SEVERAL LIGHTNING STRIKES ABOVE COCKPIT AREA. REPAIRED PER SRM 53-00-01.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

FOUND DURING LETTER CHECK, LIGHTNING STRIKE ABOVE L/E OF LEFT WING. REPAIRED PER SRM 53-00-01, DYE CHECKED OK AND PAINTED.