N315AA

Part: INVERTER — DAMAGED · airframe 76,211 hrs · 18,054 cycles

CREW REPORTED EICAS MESSAGE STBY INVERTER DISPLAYED, SMOKE IN THE CABIN & A STRONG ELEC BURNING ODOR. THE FLIGHT WAS DIVERTED TO NEAREST SUITABLE AIRPORT. THE STATIC INVERTER WAS REPLACED IAW AMM. 767 FAULT ISOLATION MANUAL PROCEDURES 24-33-807 808 WERE ACCOMPLISHED. RELAYS K104 & K106 WERE INSPECTED WITH NO DISCREPANCIES FOUND. CAUSE PENDING SHOP FINDINGS OF REMOVED COMPONENT.

Part: ENGINE — BIRD INGESTION (LEFT) · airframe 76,192 hrs · 18,048 cycles

ON ROTATION, BIRD STRIKE TO THE LT ENG. CREW HEARD LOUD NOISE & FELT AIRFRAME VIBRATION. LT ENG VIBRATION INDICATED OVER 4.5 & LT THRUST LEVER BEGAN REDUCING TO IDLE. LT ENG WAS SHUTDOWN & CREW PERFORMED AIR TURN BACK. PERFORMED BIRD STRIKE INSPECTION. REPLACE DAMAGED FAN BLADES IAW AMM. FOREIGN OBJECT DAMAGE, BIRD.

Part: POWER SUPPLY — SHORTED (CDU) · airframe 75,040 hrs · 17,526 cycles

DURING EXTENDED GROUND TAXI, LT FLIGHT MANAGEMENT COMPUTER FAILED MESSAGE DISPLAYED, FOLLOWED BY SMOKE FROM THE LT CDU & THE LT CDU CIRCUIT BREAKER TRIPPED OPEN. THE CDU WAS REMOVED FOR INSPECTION & NO DAMAGE TO THE WIRING OR CONNECTORS ASSOCIATED WITH THE CDU WAS FOUND. SHOP FINDINGS FOR CDU, KEYBOARD IN POOR SHAPE, UNIT SMELLS OF SMOKE, LOW VOLTAGE POWER SUPPLY IS SHORTED, DIMMER POTENTIOMETER INTERMITTENT & LAMPS ARE OUT.

Part: RIB — CRACKED (LT WING) · airframe 74,884 hrs · 17,451 cycles

LEFT WING MAIN TRACK RIB AT OSS 1094 IS CRACKED WHERE TRACK BEARING ATTACHES. REMOVED DAMAGE IAW BCSF 767-200 57-41-09 FIG 101 & COMPLIED WITH RGA NR B657 - 60775 MR. CRACKED 1/2 INCH, LOC AT OSS 1094, PN 114T2118-7, PN RIB, SN NA. AIRCRAFT WAS GROUNDED.

Part: FAIRING — CRACKED (VERTICAL STAB) · airframe 74,884 hrs · 17,451 cycles

VERTICAL STABILIZER AFT AT BASE UNDER 324AL METAL CHAFED & KNIFE EDGED. SRM 51-40-02 APPLIED TOP COAT IAW BOE 767 SRM 51-20-00. CRACKED CHAFED 4 INCHES, LOC FROM 1746 TO 1767, PN 148T7501017, PN FAIRING, SN NA. AIRCRAFT WAS GROUNDED.

Part: RIB — CRACKED (LT WING) · airframe 74,884 hrs · 17,451 cycles

LEFT WING MAIN TRACK RIB AT OSS 1097 IS CRACKED WHERE THE TRACK BEARING ATTACHES. R & R IAW B767-200 SR SRM 51-40-02, REPAIRED 21E1 IAW REA NR B657-60774 MR. PN 114T2119-1 SN NSN CRACKED LENGTH .125, PN ASSEMBLY RIB STR & WS LOCATION AT OSS 1097. AIRCRAFT WAS GROUNDED.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,884 hrs · 17,451 cycles

CLIP ON STRINGER 2 RT AT STATION 1678 CRACKED. R & R CLIP IAW DRAWING 148T1121 & SRM 51-20- 02. PN 148T1303-1 SN NA CRACKED 1/4 INCH, PN CLIP FS & BS LOCATION 1678 TO 1678 STRINGER & WS LOCATION R2 TO R2. AIRCRAFT WAS GROUNDED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,884 hrs · 17,451 cycles

FORWARD LOWER CARGO FUSELAGE STATION 549 RBL 6 THE STRUCTURE FOR THE LATERAL GUIDE NUTPLATES IS CORRODED. R & R 452T2704-1 INTERCOSTAL IAW DRAWING 451T2501 & SRM 51-40-02. R & R WEB FLOOR FS 522 - 549 RBL12 - LBL12 & INSTALLED LATERAL GUIDE AT FS 549 RBL 6 IAW DRAWING 143T5000 & SRM 51-40-02. LEVEL 2, LOC FROM FS 549 RBL 12 TO FS549 LBL12, PN 452R2704-1, PN INTERCOSTAL SUPPORT, SN NA. AIRCRAFT WAS GROUNDED.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,884 hrs · 17,451 cycles

FORWARD LOWER CARGO FUSELAGE STATION 412 LBL 46 LOWER SIDE OF UPPER CHORD, BELOW CARGO FLOOR, IS SPLIT WITH INTERNAL CORROSION AT NUTPLATE LOCATION. REMOVED PDU L1 & L2, REMOVED ROLLER TRAYS. R & R DRILLED & INSTALLED CORD PT STATION 412, REINSTALLED ROLLER TRAYS, & PDUS IAW B767-200 SRM 51-40-02, AMM 25-53-52 & DRAWING 141T1224. LEVEL 2 CORRODED, LOC STATION 412 LBL46 PN 141R1224Y6, PN 141R1224Y6, SN NA. AIRCRAFT WAS GROUNDED.

Part: PLATE — CRACKED (FUSELAGE) · airframe 74,884 hrs · 17,451 cycles

UPPER CARGO FLOOR PANEL MOUNTING PLATE UNDER CARGO LOCK MOUNT IS CRACKED FS 1021 LBL 45. R & R MATCH DRILLED TO FLOOR PANEL, FLOOR PANEL MOUNTING PATE AT FS 1021 LBC 45 IAW B767 SRM 51-40-02, 51-40-05, PN PLATE, CRACK LENGTH 1 INCH, PN 457T4101-2, SN NSN, LOC FS 1021 LBL 45. AIRCRAFT WAS GROUNDED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,884 hrs · 17,451 cycles

FORWARD LOWER CARGO FUSELAGE STATION 478 AFT SIDE OF CHORD AT LBL 38 UNDERSIDE OF CHORD IS CORRODED AT NUTPLATE. R & R CORD ON NR 0259. NEW CORD WAS DRILLED IAW BOE 767 SRM 51-40-05 ROLLER TRAYS WILL BE REINSTALLED ON NR 0250 ENTRY 4 CORD WAS OUT OF LIMITS IAW BOE 767 SRM 53-00-51. PN 143T1060-1, PN UPPER CORD FRAME, CORRODED LEVEL 2, FS & BS A/C LOC STATION 478 LBL 38. AIRCRAFT WAS GROUNDED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,884 hrs · 17,451 cycles

FORWARD LOWER CARGO FUSELAGE STATION 478 AFT SIDE OF CHORD AT LBL 20 UNDERSIDE OF CHORD IS CORRODED AT NUTPLATE. REMOVED OLD CORD DRILLED NEW ONE IAW BOE 767 SRM 51-40-05 INSTALLED NEW CORD IAW BOE 767 SRM 51-40-02, OLD CORD WAS FOUND TO BE OUT OF LIMITS IAW BOE 767 SRM 53-00-01. PN 143T1060-1, PN UPPER FRAME CORD, FS & BS LOC A/C STATION 478 LBL 20 TO STATION 478 TO LBL 23, CORRODED LEVEL 2. AIRCRAFT WAS GROUNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 74,884 hrs · 17,451 cycles

CORROSION ON FLAT PANEL IN WW AT STATION 973 LBL 6 & ON ANGLE AT STATION 977 LBL 6. REMOVED CORROSION IAW B767-200 SRM 53-50-12. COMPLIED WITH REA NR B653-60754-MR. PN 145T8612-1, PN KEEL BEAM WEB FS & BS LOC. ON A/C BS 973 TO BS 977, STRINGER & WS LOC. ON A/C: LBL 6, CORRODED. AIRCRAFT WAS GROUNDED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,884 hrs · 17,451 cycles

BEHIND FWD LOWER CARGO AFT SIDE OF FUSELAGE STATION 742 SHEAR TIE CORRODED BETWEEN STRINGER 35L - STRINGER 36L. INSTALLED NEW SHEET TIE IN FWD LOWER CARGO AT STATION 742 BETWEEN STRINGER 35L - STRINGER 36L IAW B767 SRM 51- 40-02. LEVEL 2, LOC FROM 742, LOC. FROM STRINGER 35L TO STRINGER 36L, PN 140T2102-243, PN SHEAR TIE, SN NA. AIRCRAFT WAS GROUNDED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,884 hrs · 17,451 cycles

AREA BEHIND FWD LOWER CARGO AT FUSELAGE STATION 742 STRINGER 38L - STRINGER 39L SHEAR TIE CORRODED. INSTALLED SHEER TIE IN FWD LOWER CARGO AT STATION 742 BETWEEN 538L & 539L IAW B767 SRM 51-40-02. LEVEL 2 CORRODED, LOC FROM 742, LOC FROM 538L TO 539L, PN 140T21020253, PN SHEAR TIE, SN NSN. AIRCRAFT WAS GROUNDED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,884 hrs · 17,451 cycles

FORWARD LOWER CARGO FUSELAGE STATION 720 LBL 41 UPPER & LOWER CHORD IS CORRODED & SEPARATING INCLUDING 3 INCHES OTBD ON LOWER SIDE. REPLACED T CHORD. LOCATED, DRILLED & INSTALLED IAW DRAWING 143T1213. LEVEL 2 CORROSION LOC FROM FS 720 LBL43 TO FS 720 RBL 43, PN 143T1060- 15, PN T CHORD FRAME ASSEMBLY, SN NA. AIRCRAFT WAS GROUNDED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,884 hrs · 17,451 cycles

FORWARD LOWER CARGO FUSELAGE STATION 580 LBL 13 ON LOWER SIDE OF INTERCOSTAL CORRODED. REPLACED & INSTALLED NEW INTERCOSTAL AT STATION S80 LBL 13 IAW B767 SRM 51-40- 02 & IAW B767 SRM 53-00-04, INSTALLED PDO AT STATION 580 LBL 13 IAW B767 AMM 25-53- 0. LEVEL 2 CORROSION, LOC. FROM 580 TO LBL 13 538L, PN 143T5021-31, PN INTERCOSTAL, SN NSN. AIRCRAFT WAS GROUNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 74,884 hrs · 17,451 cycles

CORROSION ON KEEL BEAM AT STATION 951 RBL 12 LOWER SURFACE. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION, PN 145T8611-65, PN KEEL BEAM CHORD, SN NA, LOC FS 951 RBL 12, AIRCRAFT WAS GROUNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 74,884 hrs · 17,451 cycles

SPOT OF CORROSION ON KEEL BEAM UPPER SURFACE AT STATION 814 RBL 9 ADJACENT TO NUTPLATE. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101. COMPLIED WITH REA NR B653-60753-MR. CORROSION, PN 145T8611-5, PN KEEL BEAM CHORD, SN NA, LOC 814 RBL 9. AIRCRAFT WAS GROUNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 74,884 hrs · 17,451 cycles

LEFT HAND KEEL CHORD UPPER FLANGE HAS CORROSION AT STATION 985 - 995 LBL 10.75. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION PN 145T8611-5, PN KEEL BEAM CHORD LT, SN NA, LOC FS 985 -FS 995, LBL 10.75 TO LBL 10.75. AIRCRAFT WAS GROUNDED.

Part: PANEL — CORRODED (CARGO BAY) · airframe 74,884 hrs · 17,451 cycles

FORWARD LOWER CARGO FUSELAGE STATION 630 BILGE PANEL COVER CORRODED ON TOP AT LBL PO 0039309. LEVEL 2 CORROSION PN 143T5000-122, PN BILGE PANEL, SN NA. LOCATION FROM 632 TO 610 LOCATION FROM LBL 11 TO LNL 11. AIRCRAFT WAS GROUNDED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,884 hrs · 17,451 cycles

BEHIND FWD LOWER CARGO AFT SIDE OF FUSELAGE STATION 742 SHEAR TIE CORRODED BETWEEN STRINGER 38R - STRINGER 39R. R & R SHEAR TIE AT STATION 742 BETWEEN G38R & 39R IAW B767-200 SRM 51-40-02. LEVEL 2 CORROSION, PN 140T2102U254, PN SHEAR TIE, SN NSN, LOC FROM 742 LOC FROM 38R TO 39R. AIRCRAFT WAS GROUNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 74,884 hrs · 17,451 cycles

CORROSION ON KEEL BEAM UPPER & LOWER SURFACE ADJACENT TO NUTPLATE AT STATION 801 LBL 9. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION, PN 145T8611-6, PN KEEL BEAM CHORD, SN NA, LOC FS 801, LBL 9. AIRCRAFT WAS GROUNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 74,884 hrs · 17,451 cycles

CORROSION ON KEEL BEAM AT STATION 827 LBL 11. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION, PN 145T8611-5, PN KEEL BEAM CHORD LT, SN NA, LOC FS 827, LBL 11. AIRCRAFT WAS GROUNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 74,884 hrs · 17,451 cycles

CORROSION ON KEEL BEAM AT STATION 808 RBL 10 LOWER SURFACE. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION, PN 145T8611-6, PN KEEL BEAM CHORD, SN NA, LOC STATION 808 RBL 10, AIRCRAFT WAS GROUNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 74,884 hrs · 17,451 cycles

CORROSION ON KEEL BEAM AT STATION 955 LBL 12. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION, PN 145T8611-5, PN KEEL BEAM CHORD, SN NA, LOC FS 955, LBL 12. AIRCRAFT WAS GROUNDED.

Part: BRACKET — CRACKED (LT WING) · airframe 74,884 hrs · 17,451 cycles

LEFT WING RIB 19 FUEL LINE PN 344T0010-38 SUPPORT BRACKET LOWER AFT SIDE CRACKED. R & R BRACKET IAW B767 SRM 51-40-02 & FABRICATED BRACKET IAW DRAWING NR 344T0052. PN 344T0052-2, PN BRACKET ASSEMBLY FUELING MANIFOLD, SN NSN, CRACKED 1.5 INCHES FS & BS LOC ON AC WS 668.20. AIRCRAFT WAS GROUNDED.

Part: CIRCUIT BOARD — MALFUNCTIONED (OVERHEAT) · airframe 74,692 hrs · 17,361 cycles

EICAS STATUS MESSAGES LT ENG OH LP2 AND LT ENG OH LP 1. EICAS MESSAGE FIRE/OVHT SYS ILLUMINATED ON DESCENT. CONTINUITY CHECK AND RESTANCE CHECK D2834, D2840, PIN 19, 20 READ1.50K, PIN 18 TO PIN 19, 20. OPEN IAW FIM 26-11 FIG 104.LEAKS TEST C/W. NO LEAK AT ALL AROUND LP 1 AND LP 2. CONTINUITY & MEG CHECK D154P, D4230 TO LP 1 &LP 2 NO PROBLEMS FOUND. R & R AFOLTS CARD M10224. OPS CHECKED GOOD IAW AMM 26-11-01.

Part: CDU — FAILED · airframe 74,356 hrs · 17,195 cycles

CREW REPORTED A LOUD SQUEAL THEN THE RT FMC CDU BLANKED AND TRIPPED CIRCUIT BREAKER 11E29, REPORTED A BURNED ODOR IN THE COCKPIT. INSPECTED RT CDU CONNECTOR AND WIRING, ALL OK. ALSO, CHECKED LT CDU CONNECTOR AND WIRING ALL OK. CONFIRMED CDU SMELLS BURNED AND COCKPIT ODOR HAS DISSIPATED. R & R RT FMC CDU, THE SYS TESTED GOOD IAW MM 34-61-02, ACFT WAS GROUNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 73,335 hrs · 16,780 cycles

SEVERAL POCKETS OF CORROSION ON EXTERNAL SURFACE ON RIGHT KEEL CHORD. REMOVED CORROSION ON EXTERNAL SURFACE OF RIGHT KEEL BEAM, COMPLIED WITH REA B653-60395-MR. SHOT PEEN PER BOEING 767 SOPM 20-10-031, ACFT WAS GROUNDED.

Part: COWLING — CHAFED (LT ENGINE) · airframe 73,335 hrs · 16,780 cycles

NR 1 ENGINE OUTBOARD CORE COWL IS CHAFED. REMOVED AND REPLACED NR 1 ENGINE OUTBOARD CORE COWL IAW B767 AMM 71-11-06. ADJUSTED CORE COWL LATCHES IAW B767 AMM 71-11-0, ACFT WAS GROUNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 73,335 hrs · 16,780 cycles

SEVERAL POCKETS OF CORROSION ON EXTERNAL SURFACE OF LEFT KEEL CHORD. REMOVED CORROSION ON EXTERNAL SURFACE OF LEFT KEEL BEAMS, COMPLIED WITH REA B653-60395-MR. SHOT PEEN PER BOEING 767 SOPM 20-10-031, ACFT WAS GROUNDED.

Part: WARNING SYSTEM — INTERMITTENT (COCKPIT) · airframe 7,208 hrs · 6,283 cycles

EMERGENCY DOORS LIGHT ILLUM INTERMITTENT. NO EICAS MSG DISPLAYED. INSPECTED OVERWING DOOR AND WIRING NO PROBLEMS NOTED PER B767 WDM 52-71-12. PERFORMED BITE TEST OF PSEU IAW B767 AMM 33-09-03. NO FAULTS FOUND, ACFT WAS GROUNDED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 72,004 hrs · 16,262 cycles

PREVIOUS REPAIR AT LEFT FUSELAGE STATION 1439 AT S-36L AND S-39L NEAR DENTS. REMOVED REPAIR TRIMMED OUT SKIN AND INSTALLED AN EXTERNAL DOUBLERS PER REA B653-59754MR, ACFT WAS GROUNDED.

Part: ANGLE — CHAFED (RT PYLON) · airframe 72,004 hrs · 16,262 cycles

RIGHT PYLON STRUCTURE JUST AFT OF NOSE COWL CHAFE PAD ON PYLON CHAFED. FABRICATED - 134 ANGLE IAW DWG 311T1510 USING .050 2024-0 PO#0011149. FABRICATED 133 ANGLE IAW DWG 311T1510 USING .050 2024-0 PO# 0011149, ACFT WAS GROUNDED.

Part: SWIVEL FITTING — CHAFED (RT MLG) · airframe 72,004 hrs · 16,262 cycles

RIGHT WING MAIN LANDING GEAR SUPPORT, SIDE STRUT SWIVEL FITTING CHAFED, CHAFING AT THE BEARING PAD COMMON TO THE OUTBOARD LUG. PERFORMED LOCAL BENDING MINIMUM REMAINING THICKNESS WAS .301 WORK ACCOMPLISHED PER REA NO, B657-59762-MR.

Part: SWIVEL FITTING — CHAFED (LT MLG) · airframe 72,004 hrs · 16,262 cycles

LEFT LANDING GEAR SUPPORT, SIDE STRUT SWIVEL FITTING AFT LANDING GEAR SIDE STRUT SWIVEL FITTING CHAFED. PERFORMED LOCAL BLENDING MINIMUM REMAINING THICKNESS WAS .308", AREA 2" X 2" WORK ACCOMPLISHED ON REA NO. B657-59761-MR, AIRCRAFT WAS GROUNDED.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 72,004 hrs · 16,262 cycles

FUSELAGE SECTION 48 TOOLING DAMAGE ON LOWER FITTING SPLICE. BLENDED DAMAGE 1.50 LONG, .075 WIDE, .010 DEEP PER REA B653-59755-MR, ACFT WAS GROUNDED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 72,004 hrs · 16,262 cycles

GOUGE IN LEFT FORWARD FUSELAGE SKIN AT STA 246 S-21L. REMOVED DAMAGE AND REPAIRED IAW REA B653-59747-MR, ACFT WAS GROUNDED.

Part: STRUCTURE — CHAFED (RT WING) · airframe 72,004 hrs · 16,262 cycles

RT WING MAIN LANDING GEAR SUPPORT SIDE BRACE SWIVEL HAS CHAFING DAMAGE. BLENDED AT OUTBOARD SIDE WHERE PANEL SUPPORT ATTACHES. WORK ACCOMPLISHED PER REAB657-59746MR, ACFT WAS GROUNDED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 72,004 hrs · 16,262 cycles

FUSELAGE SKIN AT FS 650 BLD AROUND DRAIN PLUG OPENING IS CORRODED. REMOVED CORROSION, BLENDED AREA WITHIN LIMITS IAW REA B653-59738, ACFT WAS GROUNDED.

Part: FITTING — DAMAGED (RT WING) · airframe 72,004 hrs · 16,262 cycles

RIGHT WING BACK UP FITTING AT RWS 385 HAS MULTIPLE TOOLING MARKS. BLENDED AREAS IAW B767 SRM 57-20-00 AND B657-59720-MR, ACFT WAS GROUNDED.

Part: SUPPORT BRACKET — CRACKED (RT PYLON) · airframe 72,004 hrs · 16,262 cycles

RIGHT PYLON RT SIDE, AFT CORE COWL FAIRING SUPPORT BRACKET CRACKED. LOCATED JUST FORWARD OF EXHAUST CONE SEAL. WELDED IAW ABX PROCESS STANDARDS MANUAL CHAPTER 900-7, ACFT WAS GROUNDED.

Part: SKIN — GOUGED (FUSELAGE) · airframe 72,004 hrs · 16,262 cycles

LOWER SKIN IN AFT ACCESSORY FWD OF 1809 BULKHEAD BETWEEN S39L AND S37L HAS A GOUGE. CLEANED UP GOUGE AT FWD OF FS 1809 S39L TO S38L ALODINE, PRIMED AND PAINTED IAW ABX AIR REA B653-59739, ACFT WAS GROUNDED.

Part: FITTING — CHAFED (RT PYLON) · airframe 72,004 hrs · 16,262 cycles

RIGHT PYLON WING SIDE FITTING CHAFED ACCESS PNL 447AL. REPAIRED ON REA B654-59729-MR, ACFT WAS GROUNDED.

Part: CHANNEL — CRACKED (LT PYLON) · airframe 72,004 hrs · 16,262 cycles

LEFT PYLON PNL 447 ELX ACCESS CUTOUT LWR FWD "U" CHANNEL CRACKED. REMOVED AND REPLACED BEAM UNDER NR 2 PYLON PANEL 447ELX IAW B767 SRM 51-40-02, ACFT WAS GROUNDED.

Part: BEAM — CRACKED (LT PYLON) · airframe 72,004 hrs · 16,262 cycles

LEFT INBD PYLON BEAM BELOW HYD BAY DOOR IS CRACKED AT FWD LATCH FITTING INSIDE. REMOVED & REPLACED BEAM IAW B767-200 SRM 51-40-02, ACFT WAS GROUNDED.

Part: SUPPORT FITTING — DAMAGED (LT WING) · airframe 72,004 hrs · 16,262 cycles

LEFT WING RIB 8 ENGINE SUPPORT FITTING AT LWS 375 HAS SEVERAL TOOLING MARKS ON UPPER INBD SIDE. BLENDED AREA IAW B767 SRM 57-20-00 AND REA B657-59730-MR, ACFT WAS GROUNDED.

Part: SENSOR — OUT OF ADJUST (ENTRY DOOR) · airframe 71,473 hrs · 16,043 cycles

EICAS LEFT FORWARD ENTRY DOOR ON LANDING OVERHEAD DISCRETE LITE "ENTRY DOOR". WITH DOOR OPERATED TO CLOSED, FOUND "FAR" ON S194 OUT OF ADJUSTMENT WITH SLIGHTEST MOTION OF DOOR PER B767 AMM 52-11-11 ADJUSTED S194 IAW B767 AMM 52-11-00-5, AWG.

Part: CDU — BURNED (LEFT) · airframe 70,697 hrs · 15,811 cycles

SMOKE IN COCKPIT ON TAKEOFF. LOST TOP ENGINE EICAS DISPLAY AND LEFT FMC. EMERGENCY RETURN TO OVERWIEGHT LANDING. CHECKED MAIN CARGO FOR SMOKE/FIRE, NONE FOUND. CHECKED MAIN ELECTRICAL COMPARTMENT FOR SMOKE/FIRE, NONE FOUND. CHECKED CAPTAINS AND COPILOTS FMC CDU. FOUND CAPTAINS CDU BURNED. REPLACED IAW 34-61-02. CHECKED OK. REPLACED UPPER EICAS SCREEN IAW 31-40-01, CHECKED OK. RAN BOTH ENGINES SEPARATELY IAW AMM CHECKING FOR EVIDENCE OF SMOKE, CHECKED ALL COCKPIT INSTRUMENTS IAW AMM 20-60-04 ALL CHECKED OK. OVERWEIGHT INSPECTION PERFORMED PHASE I OPTION A NO DEFECTS NOTED IAW 5-51-35 PG 202.

Part: INDICATION SYS — MALFUNCTIONED (COCKPIT) · airframe 67,528 hrs · 14,966 cycles

ACCESS DOORS LIGHT ILLUMINATED INTERMITTENTLY EICAS MESSAGE "FWD ACCESS DOOR" DISPLAYED INTERMITTENTLY. DEFERRED FWD ACCESS DOOR INDICATION IAW MEL 52-71-1-1.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 37,417 hrs · 14,939 cycles

FWD LOWER CARGO DOOR HAS CORROSION ON INTERIOR FRAME BELOW FWD HINGE. REMOVED AND REPLACED DOOR BEAM.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 67,417 hrs · 14,939 cycles

AFT LOWER CARGO DOOR FRAME UNDER FWD VENT IS CORRODED AROUND THREE NUT PLATES. BLENDED CORRODED AREA AND FOUND TO BE OUT OF LIMITS IAW B767-200 SRM 52-30-02. REMOVED CORRODED T-CAP AND REPLACED WITH NEW ONE IAW B767-200 SRM 51-40-02. REPLACED ALC PANEL FOR INTERIOR DOOR AND RECONNECTED CONNECTOR BRACKET PLATE IAW B767-200 SRM 51-40-02.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 67,417 hrs · 14,939 cycles

THE LBL NOSE WHEEL WELL VERTICAL CHORD AT STA 287 IS CRACKED LOCATED 11.5 INCHES BELOW CEILING PANEL. REPAIRED NOSE WW LBL 25 VERTICAL CHORD AT STA 287 IAW B767 SRM 51-70-12 FIG 1.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 67,417 hrs · 14,939 cycles

THE RBL 25, NOSE W/W VERTICAL CHORD AT STA 287 IS CRACKED. LOCATED 11.75 INCHES BETWEEN CEILING PANEL. REPAIRED NOSE W/W RBL 25 VERTICAL CHORD AT STA 287 IAW B767 SRM 51-70-12 FIG 1.

Part: MOUNT — CORRODED (NR 1 ENGINE) · corrosion level 2 · airframe 67,417 hrs · 14,939 cycles

NR 1 AFT ENG MOUNT HAS AREAS OF CORROSION, WHERE MOUNT ATTACHES TO THE ENGINE. REMOVED AND REPLACED NR 1 ENG AFT MOUNT AND MOUNT BOLTS IAW AMM 71-00-02 PAR 3.

Part: MOUNT — CORRODED (NR 1 ENGINE)

DURING A MX INSP EVENT, FOUND NR 1 AFT ENGINE MOUNT HAD AREAS OF CORROSION WHERE MOUNT ATTACHED TO THE ENGINE. R & R NR1 ENGINE AFT MOUNT AND MOUNT BOLTS IAW MM.

Part: DOUBLER — BROKEN (RT WING) · airframe 67,417 hrs · 14,939 cycles

PANEL 621ZB RT LEADING EDGE HAS TWO DOUBLERS BROKEN AND MISSING. REMOVED AND REPLACED TWO DOUBLERS ON PANEL 621AZB IAW BOEING DRAWING 114T2.

Part: PANEL — BROKEN (ZONE 600)

(ABXR) DURING A MX INSP EVENT, FOUND PANEL 621ZB , RT L/E HAD (2) DOUBLERS BROKEN AND MISSING. REMOVED (2) DOUBLERS ON PANEL 621ZB IAW DWG 114T2400.

Part: HYDRAULIC LINE — FAILED (HYD SYSTEM)

JFK - FLT 133 - ON DEPARTURE, RIGHT HYDRAULIC SYSTEM WAS LOST AT BOUT 5000 FEET RIGHT HYDRAULIC QUANTITY SHOWED .12 RF HYDRAULIC PRIM PUMP PRESSURE LIGHT ILLUMINATED. RIGHT ENGINE HYDRAULIC PUMP PRESSURE LINE FAILED. REMOVED AND REPLACED PRESSURE LINE. REMOVED AND REPLACED HYDRAULIC PUMP AND CASE DRAIN AND PRESSURE FILTERS LEAK AND OPS CHECK OK. (M)

Part: LIGHT — INOPERATIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, RIGHT MID GALLEY FLOOR EMERGENCY ESCAPE LIGHTING INOPERATIVE. REPLACED RIGHT MID GALLEY FLOOR EMERGENCY ESCAPE LIGHTING ASSEMBLY. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

BOS - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTS AT SEAT 11B FOUND INOPERATIVE. RECONNECTED CONNECTOR FOUND ON INBOARD SIDE OF SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CHARGER — INOPERATIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY PATH LIGHTING RIGHT ROWS 10-17 INOPERATIVE. REPLACED RIGHT CONTROL CHARGER MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — DELAMINATED (ELEVATOR)

AFW - RIGHT OUTBOARD ELEVATOR LOWER SKIN HAS MULTIPLE LAYERS OF DELAMANATION FS 137.5-141.25 AND 160.25-162.0 AS SHOWN ON SKETCH. REQUEST APPROVAL TO CONTINUE SERVICE. TAP TEST AREA FOR DELAMINATIONS. (M)

Part: SKIN — DAMAGED (FUSELAGE)

AFW - ACCOMPLISH REPAIR TO FUSELAGE SIN AT STATION 432. REPAIR SKIN PER REF (A). FABRICATED DOUBLER. SHIMMED STRINGER. FINISHED ALL REPAIR PARTS AND INSTALLED. (M)

Part: LIGHT — INOPERATIVE (L1 DOOR)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LINE — LEAKING (NR 2 ENGINE)

BWI - FLT 174 - EN ROUTE RDU-LGW, DETECTED RIGHT SIDE HYDRAULIC SYSTEM FAILURE. DIVERTED BWI AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT SIDE ENGINE HYDRAULIC PUMP PRESSURE INE. SERVICED RIGHT HYDRAULIC SYSTEM. RAN BOTH ENGINES. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PIN — BROKEN (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR PIN AT SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 24B INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 28B INOPERATIVE. RESECURED EMERGENCY EIT LIGHT CONNECTOR AT SEAT 28B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FAN — DEFECTIVE (ACM BAY)

DEN - FLT 22 - EN ROUTE LAX-FJK, DETECTED STRONG ELECTRICAL SMELL IN CABIN AND COCKPIT. DIVERTED DEN AND LANDED WITHOUT INCIDENT. REPLACED LEFT SIDE RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DISCONNECTED (SEAT 31)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 31H INOPERATIVE. RECONNECTED EMERGENCY EXIT SEAT PATH LIGHT CONNECTOR AT SEAT 31H. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — BROKEN (SEAT 17)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 17H INOPERATIVE. REPAIRED BROKEN WIRE AT SEAT 17H. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 23H INOPERATIVE. RELOCKED EMERGENCY EXIT SEAT LIGHT CONNECTOR AT SEAT 23H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: FITTING — CORRODED (BS 632)

AFW - FRAME SPLICE FITTING AT STA 632 RBL 48 HAD GOUGE BLENDED BEYOND SRM LIMITS. REPAIRED IAW MRB 767-1553. TST: 4,172 HOURS. CYCLES: 673. (X)

Part: SLIDE — DEFECTIVE (CABIN)

SFO - AT GATE, RIGHT HAND OVERWING SLIDE WAS INADVERTENTLY DEPLOYED AND DEPLOYMENT WAS SUCCESSFUL. REPLACED RIGHT HAND OVERWING SLIDE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT RIGHT SIDE OF MAIN CABIN WOULD NOT EXTINGUISH. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT PAX SEAT 22J CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRAP — CORRODED (BS 615)

AFW - FORWARD CARGO OF FAILSAFE STRAP AT STA 615 RBL 45 HAD GOUGE BLENDED BEYOND SRM LIMITS. REPAIRED IAW MRB 767-1552. TST: 4,172 HOURS. CYCLES, 673. (X)

Part: GENERATOR — DEFECTIVE (RT ENGINE)

SFO - FLT 682 - AFTER TAKEOFF SFO CLIMBING THROUGH 4000FT MSL, ELECTRICAL ODOR NOTED IN CABIN. AT 8000 FT MSL, RIGHT GENERATOR TRIPPED OFF. AIRCRAFT RETURNED TO SFO AND LANDED WITHOUT INCIDENT. REPLACED RIGHT INTERGRATED DRIVE GENERATOR (IDG). ACCOMPLISHED GROUND ENGINE RUN WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO ODOR NOTED. (M)

Part: LIGHT — DEFECTIVE (NLG)

LHR - FLT 108 - DURING APPROACH TO LHR WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR GREEN LIGHT FAILED TO ILLUMINATE. ACCOMPLISHED GO AROUND AND ABNORMAL PROCEDURES. AIRCRAFT LANDED LHR WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR GREEN INDICATION LIGHT DIODE MODULE AND LENS CARRIER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TEAR STRAPS — DAMAGED (BS 1540-1562)

AFW - FOUND TEAR STRAPS DAMAGED BEYOND SRM LIMITS. MANUFACTURED .080 2.2A-T3 BARE DOUBLER, INSTALLED USING FILLER BETWEEN DOUBLER AND TEAR STRAPS PER ENGINEERING MRB 767-1265. (M)

Part: FLOOR BEAM — CORRODED (BS 850-870)

AFW - FOUND AND BLENDED CORROSION IN 2 AREA OF THE UPPER SURFACE OF THE CABIN FLOOR BEAMS. THE BLENDOUTS EXCEEDED SRM ALLOWABLE LIMITS. CUT EACH FLOOR BEAM OF STATION 843.5 AND 876.8. SPLICED NEW SECTIONS OF FLOOR BEAM. ACCOMPLISHED PER APPROVED ENGINEERING INSTRUCTIONS OF MRB 767-1264. (M)

Part: FLOOR BEAM — GOUGED (BS 855)

AFW - FOUND AND BLENDED GOUGE ON THE UPPER SURFACE OF THE MAIN CABIN FLOOR BEAM. BLEND EXCEEDS SRM MAX ALLOWABLE LIMITS. ROTO PEENED, ALODINED AND PRIMED APPROVED BY ENGINEERING PER MRB 767-1270. (M)

Part: DOOR SILL — CORRODED (BS 615.5)

AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF FWD CARGO DOOR LOWER MAIN SILL INNER CHORD. THE BLENDOUT EXCEEDED SRM MAX ALLOWABLE LIMITS. ROTO PEENED AREA, INSTALLED FILLER FABRICATED FROM 7075-T6 ALUMINUM. ALODINED AND PRIMED AREA. APPROVED BY ENGINEERING PER MRB 767-1269. CHORD WILL BE REPLACED ON OR BEFORE NEXT MBV. (M)

Part: SKIN — CORRODED (CTR WING)

AFW - FOUND AND REMOVED HEAVY CORROSION ON CENTER WING UPPER SKIN AT AFT DRAIN LOCATIONS STA 955 LBL 71 AND RBL 7L. ALSO, THE LOWER CHORD TO FLOOR BEAM T-EXTRUSION WAS CUT AND REMOVED. REINSTALLED T-CHORD WITH 'I' EXTRUSION ON EACH SIDE OF THE CHORD WITH 5 FASTENERS ON EACH SIDE OF THE CUT. CORRODED AREAS WERE CLEANED, SHOT PEENED, ALODINED AND PRIMED. APPROVED BY ENGINEERING PER MRB 767-1268. (M)

Part: HOUSING — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY LIGHT AT PASSENGER SEAT 28B FOUND INOPERATIVE. REPLACED EMERGENCY LIGHT HOUSING AT PASSENGER SEAT 28B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, RIGHT AFT DOOR EMERGENCY EXIT BULKHEAD LIGHT INOPERATIVE. REPLACED RIGHT AFT EMERGENCY EXIT BULKHEAD LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT 24 A/B INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR PIN AT 24 A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)