N798AX

Part: STRIKER — INOPERATIVE (COCKPIT DOOR) · airframe 65,617 hrs · 48,006 cycles

THE FLIGHT DECK DOOR WILL NOT RELEASE ELECTRICALLY DURING THE CREW'S PREFLIGHT INSPECTION. THE DOOR CIRCUIT BREAKER OPENS. THE AIRPLANE WAS REMOVED FROM SERVICE, GROUNDED, UNTIL THE DOOR'S SECURITY SYSTEM WAS DEFERRED. 3 DAYS LATER, THE AIRPLANE WAS REMOVED FROM SERVICE, GROUNDED, WHILE THE ELECTRIC STRIKE WAS REPLACED AND MISSING SHIMS WERE INSTALLED. THE CAUSE FOR THE ELECTRIC STRIKE BECOMING INOPERATIVE IS UNKNOWN.

Part: LOCK — FAILED (COCKPIT DOOR) · airframe 65,350 hrs · 47,887 cycles

FLIGHT DECK DOOR LOCK CIRCUIT BREAKER TRIPPED. THERE WAS A BURNING ODOR IN THE VICINITY OF THE FLIGHT DECK DOOR. THE FLIGHT DECK DOOR LOCK WAS REPLACED. THE CAUSE OF THE ODOR WAS NOT FOUND.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 64,504 hrs · 47,479 cycles

LEFT WING LE CORROSION ON RIB AT LES 436. REMOVED LT WING TAI DUCT, CORROSION OUT OF LIMITS ON RIB. R & R RIB IAW SRM 51-40-02 PARA 7 & 4B. REINSTALLED TAI DUCT IAW MM 20-11-00, LEAK CHECKED GOOD IAW MM 3071-00. CORRODED LEVEL 2, PN 114T2200-17, PART NAME RIB, SN N/A, FS & BS LT WING LE. ACFT WAS GNDED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,504 hrs · 47,479 cycles

STATION 883.5, LBL 89 LT SIDE FRAME INNER CHORD CRACKED 1/4" AT TRANSITION RAD II. IAW WS02568 FIG 1 SH 2 FOR LOCATION. INNER CHORD CRACK WILL BE REPAIRED ON JC EA 53000049-101. CRACKED LENGTH .25", PN 145T1004-1, PART NAME, INNER CHORD, SN NSN, BS LOCATION FROM 883.5 TO 883.5, STRINGER & WS LOCATION FROM LBL 89 TO LBL 89. ACFT WAS GNDED.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 64,504 hrs · 47,479 cycles

RIGHT OVERWING EXIT CUT OUT FWD SIDE HAS CORROSION. REPAIRED CORRODED AREA AT RT OVERWING EXIT CUT OUT FORWARD SIDE, BETWEEN STATION 859 - 862, STRINGER 16R - 17R IAW REA B653-61943-MR. CORRODED, PN 145T28320-10, PART NAME UPPER BEAR STRAP, SN NSN, FS & BS LOCATION FROM FS 859.5 - 862.5, STRINGER & WS LOCATION, FROM STRINGER 16 TO 17. ACFT WAS GNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,504 hrs · 47,479 cycles

STATION 676, AFT STRINGER 19L, LOWER HAT FLANGE CRACKED, AT 4 SPLICE FITTING FLANGE FASTENER LOCATIONS. REPAIR IAW NEA53100137-201 STEP 27 B B 2 & ENGINEERING. COMPLETED M-289, REPAIRED STRINGER 19L TO STATION 676 IAW ENGINEERING SKETCH ES 02821. CRACKED 4", PN 143T3001-17, SN NA, PART NAME: STRINGER, EXACT FS & BS LOCATION ON ACFT FROM 676 TO 681, EXACT STRINGER & WS LOCATION ON ACFT FROM 19L. ACFT WAS GNDED.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 64,504 hrs · 47,479 cycles

STATION 676, STRINGER 4L SPLICE HAS 3/4" CRACK ON VERTICAL LEG FWD SIDE OF FRAME. CONTACT ENGINEERING FOR REPAIR. COMPLETE M 289, REF NEA53100137-201. R & R SPLICE IAW B767 SRM 51-40-02 REA B653-61924MR. CRACKED LENGTH .650, PN 368-53-00-95387, SN N/A, PART NAME SPLICE FITTING, EXACT FS & BS LOCATION ON ACFT, FROM STATION 676, EXACT STRINGER & WS LOCATION ON ACFT FROM STRINGER 14L. ACFT WAS GNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,504 hrs · 47,479 cycles

STATION 676 AFT STRINGER 24L, UPPER HAT FLANGE CRACKED, APPROX 5". REPAIR IAW NEA 53100137-201 STEP 27 B B 2 & ENGINEERING. COMPLETED M-289, REPAIRED 524L IAW SRM 53-00-03 & NEA5310037-201 STEP 27B. CRACKED LENGTH 4.75", PN 143T3001-32, PART NAME STRINGER 24L, SN MSM. SN, FS LOCATION FROM 676 TO 681, STRINGER LOCATION FROM 24L TO 24L. ACFT WAS GNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,504 hrs · 47,479 cycles

STATION 676, AFT STRINGER 8L, UPPER HAT FLANGE CRACKED APPROX 4", LOWER HAT FLANGE CRACKED APPROX 5 1/2". REPAIR IAW NEA53100137-201 STEP 16 B B 2 & ENGINEERING. COMPLETE M-289 IAW NEA53100137-201. PERFORMED REPAIR IAW ENGINEERING SKETCH E502821 FIG 7. INSTALLED STRINGER & REPAIR SPLICE IAW SRM 51-40-02 & 53-00-03. CRACKED 5.5", PN 143T3001-6, PART NAME STRINGER 8L, SN:NSN, BS LOCATION: FROM 676 - 681, STRINGER LOCATION FROM 8L TO 8L. ACFT WAS GNDED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,504 hrs · 47,479 cycles

STATION 883.5, RBL 89 RT SIDE FRAME INNER CHORD CRACKED 1/4" AT TRANSITION RADII. EF ES02568 FIG 1 SH 2 FOR LOCATION. REPAIR WILL BE ACCOMPLISHED & DOCUMENTED ON JC EA 53000050-101. CRACKED LENTH .25", PN 145T1004-2, PART NAME, INNER CHORD, SNS NSN, FS & BS LOCATION FROM FS 883.5, STRINGER & WS LOCATION FROM RBL 89. ACFT GNDED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,504 hrs · 47,479 cycles

FLOOR SUPPORT AT STATION 610, APPROX RBL 20 CORRODED. R & R SUPPORT ANGLE FROM STATION 615 - 532. INSTALLED SUPPORT CLIP IAW SRM 51-40-02 FIG 12. CORRODED LEVEL 2, PN 143T5000-36AX, SN NA, PART NAME SUPPORT, EXACT FS & BS LOCATION ON ACFT FROM STATION 615 TO 632. EXACT STRINGER & WS LOCATION ON ACFT FROM RBL 16.4 TO RBL 16.4. AIRCRAFT WAS GROUNDED.

Part: BEAM — CORRODED (LT WING) · corrosion level 2 · airframe 64,504 hrs · 47,479 cycles

NUMBER 8 SUPPORT 123 BEAM, C FASTENER ONE EACH SHOWS CRACK INDICATION & CORROSION IN BOTTOM. REQUEST TECHNICAL ENGINEERING ASSISTANCE, REPAIRED HOLE ON THE NR 8 FLAP SUPPORT 1 - 3 BEAM IAW REA CO57-61926-MR. CORRODED LEVEL 2, PN 113T1313-8, PART NAME 1-3 BEAM, SN ABXV716, WS LOCATION FROM 798 TO 798. ACFT WAS GNDED.

Part: BEAM — GOUGED (LT WING) · airframe 64,504 hrs · 47,479 cycles

NUMBER 2 FLAP SUPPORT 1-3, BEAM HAS A GOUGE AROUND FASTENER HOLE. REPAIRED HOLE ON THE NR 2, 1 - 3 BEAM FOR THE NR 2 FLAP SUPPORT IAW REA CO57-61933-MR. PN 113T1314-15, PART NAME 1 - 3 BEAM. SN ABXV654, WS LOCATION, 616.2 - 616.2. ACFT WAS GNDED.

Part: RIB — CORRODED (LE SLAT) · corrosion level 2 · airframe 64,504 hrs · 47,479 cycles

NUMBER 5 SLAT UPPER RIB ON INBD SIDE OF TELESCOPING DUCT CORRODED. R & R NR 5 SLAT UPPER RIB ON INBD SIDE OF TELESCOPING DUCT IAW DWG 114T2202 & SRM 51-40-02. CORRODED LEVEL 2, PN 114T2202-23, PART NAME RIB, SN NSN, WS LOCATION, FROM 456 TO 456. ACFT WAS GNDED.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 64,504 hrs · 47,479 cycles

LEFT WING LE CORROSION IN TWO PLACES ON RIB AT LES 779. R & R RIB IAW REA B657-61902 & SRM 51-40-02. CORRODED LEVEL 2, PN 114T2217-15, SN N/A, PART NAME RIB, EXACT STRINGER & WS LOCATION ON ACFT FROM WS 779. ACFT WAS GNDED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,504 hrs · 47,479 cycles

LOWER FRAME CORRODED, AT STATION 742L, BETWEEN STRINGER 34L & 36L, IN THREE PLACES. BLENDED CORROSION, SHEAR TIE OUT OF LIMITS, TO BE REPAIRED ON NON-ROUTINE 0822. BLENDED WEB STATION 742L, STRINGER 34 - 35L. ORIGINAL MT .032, REMOVED .003, REMAIN .029 WITHIN LIMITS IAW SRM 53-00-07, NO CORROSION FOUND. CORRODED LEVEL 2, PN IAW DWG 143T1214, PART NAME CHORD, WEB SHEAR TIE, EXACT FS & BS LOCATION ON ACFT, FROM STATION 742L TO BL 21 - 26L. ACFT WAS GNDED.

Part: SUPPORT — CORRODED (RT MLG TRUNNION) · corrosion level 2 · airframe 64,504 hrs · 47,479 cycles

REFERENCE CARRY OVER ITEM 62398-001, PERMANENT TRUNNION SUPPORT RE. PN 112T1711-8, PART NAME, SUPPORT ASSEMBLY, SN NSN, CORRODED LEVEL 2, EXACT STRINGER & WS LOC ON ACFT, RT TE WS310 TO WS310. ACFT WAS GNDED.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 64,504 hrs · 47,479 cycles

NUMBER 8 FLAP SUPPORT, OTBD SPAR FITTING HAS PITTING IN CRANK ARM BUSHING BORE. REPAIRED IAW REA B657-61911-MR. LEVEL 2 PN 113T1345-20, PART NAME, RIB ASSEMBLY, SN NSN, STRINGER & WS LOCATION FROM, WS 798 - 798. ACFT WAS GNDED.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,504 hrs · 47,479 cycles

FORWARD NLG BAY FWD BULKHEAD FOUND CORRODED DOUBLER. R & R DOUBLER IN NLG BAY IAW SRM 51-40-02. FABRICATED FROM SRM 53-10-14 FIGURE 1 DWG 141T290 METAL 2024-T3-090 PO 1473909. CORRODED LEVEL 2, PN 141T2912-2, SN NSN, PART NAME STRAP, EXACT FS BS LOCATION ON ACFT, FROM 169 TO 169, EXACT STRINGER & WS LOCATION ON ACFT, FROM LBL 9 - LBL 11. ACFT WAS GNDED.

Part: WEB — CORRODED (LT WING) · corrosion level 2 · airframe 64,504 hrs · 47,479 cycles

LEFT WING LE SHIM, CORRODED AT LES 582, FRONT INBD CORNER OF BAY. FOUND CORROSION TO BE ON NOSE BEAM, FOUND CORROSION TO BE OUT OF LIMITS. REMOVED NOSE BEAM & FABRICATED NEW NOSE BEAM FROM 7075-T6 050 IAW DWG 114T2300 & SAMPLE PO 0069430. INSTALLED NEW NOSE BEAM IAW SRM 51-40-02 46 & 51-40-02 7D & 51-40-0258. CORRODED LEVEL 2, PN 114T2300-135, PART NAME WEB, SN N/A, FS & BS LOCATION, FROM OSS 585 - 607. ACFT WAS GNDED. .

Part: STRUT — CORRODED (RT WING) · corrosion level 3 · airframe 61,133 hrs · 45,807 cycles

NUMBER 8 SLAT OTBD AUXILIARY TRACK OTBD LOWER PANEL ATTACH STRUT CORRODED AROUND NUTPLATE. REMOVED DMG STRUT, FABRICATED NEW STRUT IAW REA B657-60902 & REINSTALLED STRUT IAW 200 SRM 51-40-02 - COMPLETED SRM 51-70-13 ON DMG HOLES. SDR INFO PN 114T2204-16, PART NAME STRUT, SN NSN, CORRODED LEVEL 3, EXACT FS & BS LOCATION ON ACFT WS 500 RT, EXACT WS LOCATION ON ACFT WS 500 RT. ACFT WAS GROUNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 61,133 hrs · 45,807 cycles

STRINGER CRACKED AT STATION 676 STRINGER 6L. REMOVED DAMAGED STRINGER, FABRICATED & INSTALLED STRINGER & REPAIR SPLICE IAW REA653-60886, SRM 51-40-02 & 53-00-03. SDR INFO CRACKED .750, PN 143T3001-6, PART NAME STRINGER, SN NSN, FUSELAGE STATION LOCATION 676 TO 710, STRINGER LOCATION 6L. ACFT WAS GROUNDED.

Part: RIB — CORRODED (LT WING) · airframe 61,133 hrs · 45,807 cycles

NUMBER 8 SLAT INBD AUXILIARY TRACK OTBD LOWER PANEL ATTACH STRUT CORRODED AROUND NUTPLATE. R & R NR 8 SLAT INBD AUXILIARY TRACK ATTACH STRUT IAW SRM 51-40-02, REA NR B657- 60897 FOR PART FABRICATION. SDR INFO PN 114T2201-24, AIR LOAD RIB, SN NSN, CORRODED, LOCATION LES 442. ACFT WAS GROUNDED.

Part: SUPPORT BEAM — CORRODED (RT WING) · airframe 61,133 hrs · 45,807 cycles

WING TE ANGEL 661CB AFT ATTACH CHANNEL CORRODED AROUND NUTPLATE. REMOVED PN 113T1944-44 SUPPORT BEAM IAW SRM 51-40-02 & INSTALLED FABRICATED SUPPORT BEAM IAW REA B657-60904 & B767 SRM 51-40-02. SDR INFO CORRODED, PN 113T944-44, PART NAME PANEL SUPPORT BEAM, SN NSN, WS LOCATION 508 - 534. ACFT WAS GROUNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 61,133 hrs · 45,807 cycles

CRACKED STRINGER AT STATION 676 STRINGER 11L. REMOVED DAMAGED STRINGER. FABRICATED & INSTALLED REPAIR IAW REA 653-60886 & SRM 51-40-02. PN 143T3001-7, PART NAME STRINGER, CRACKED .800, SN NSN, EXACT FUSELAGE ON ACFT 676L TO 710L, EXACT STRINGER LOCATION ON ACFT 11L. ACFT WAS GROUNDED.

Part: RIB — CORRODED (LT WING) · airframe 61,133 hrs · 45,807 cycles

NUMBER 9 SLAT OTBD AUXILIARY TRACK OTBD LOWER PANEL ATTACH STRUT CORRODED AROUND NUTPLATE. R & R NR 9 SLAT OTBD AUXILIARY TRACK OTBD LOWER PANEL ATTACH STRUT IAW SRM 51-40-2. SDR PN 114T2111-2, SN N/A, AIR LOAD RIB CORRODED, RWS AT 630. ACFT WAS GROUNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 61,133 hrs · 45,807 cycles

CRACKED STRINGER AT STATION 676, STRINGER 12L. R & R DAMAGED STRINGER 12L SECTION AT FS 676 IAW REA B653- 60886 REPAIR DATED 03/04/2014. SDR INFO PN 143T3001-8, PART NAME STRINGER, SN NSN, CRACKED 3 INCHES, EXACT LOCATION ON ACFT 676L TO 710L, EXACT STRINGER LOCATION ON ACFT STRINGER 12L. ACFT WAS GROUNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 61,133 hrs · 45,807 cycles

CRACKED STRINGER AT STATION 654 S17L. REMOVED DAMAGED STRINGER. FABRICATED REPAIR & INSTALLED IAW REA B653-60886 & B767 SRM CH 51-40-02. SDR INFO PN 143T3001-10, PART NAME STRINGER, CRACKED 1 INCH, EXACT FS ON ACFT 676L TO 710L, EXACT LOCATION ON ACFT 17L. ACFT WAS GROUNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 61,133 hrs · 45,807 cycles

CRACKED STRINGER AT STATION 676 S7L. R & R DAMAGE STRINGER 7L AT FUSELAGE 676 STATION IAW REA B653-601886 REV IP DATED 3-4-14. SDR INFO CRACKED 2 INCHES, PN 143T8001-96, PART NAME STRINGER & SPLICE, EXACT FS & BS LOCATION FROM STATION 676 TO 678, EXACT STR & WS LOCATION FROM STRINGER 7. ACFT WAS GROUNDED.

Part: SKIN PANEL — CORRODED (LE SLAT) · airframe 61,133 hrs · 45,807 cycles

SLAT PANEL 625 FT HAS SMALL SPOT OF CORROSION ON LE. REMOVED CORROSION FOUND TO BE OUT OF LIMITS OF SRM. FABRICATED NEW PANEL IAW REA B627-60900 HT 7075-0 IAW 5602 REV AF. PN114T4157-6, SN NSN - SKIN, CORRODED FROM OSS 933 TO OSS 948. ACFT WAS GNDED.

Part: WEB — CORRODED (RT WING) · airframe 61,133 hrs · 45,807 cycles

CLOSE OUT WEB ON INSIDE OF LE AT NR 9 SLAT CORRODED AT LE STATION 612. R & R CLOSE OUT WEB ON INSIDE LE AT NR 9 SLAT IAW B767 SRM 51-40-02. PN 114T2300, PART NAME NOSE BEAM, CORRODED, STRINGER & WING STATION LOCATION ON ACFT LE STATION 602 TO LE STATION 620 RT WING. ACFT WAS GROUNDED.

Part: ATTACH FITTING — CORRODED (LT WING) · airframe 61,133 hrs · 45,807 cycles

NUMBER 9 SLAT OTBD AUXILIARY TRACK INBD LOWER PANEL ATTACH STRUT CORRODED AROUND NUTPLATES. R & R SLAT OTBD AUXILIARY TRACK INBD LOWER PANEL ATTACH STRUT IAW SRM 51-10-02. SDR INFO CORRODED, PN 114T2210-20, SN N/A, PART NAME LE STRUT, STR & WS LOCATION FROM LES 624. ACFT WAS GROUNDED.

Part: RIB — CORRODED (RT WING) · airframe 61,133 hrs · 45,807 cycles

NUMBER 9 SLAT OTBD AUXILIARY TRACK OTBD LOWER PANEL ATTACH STRUT CORRODED AROUND NUTPLATE. R & R NR 9 SLAT OTBD AUXILIARY TRACK OTBD LOWER PANEL ATTACH STRUT IAW SRM 51-40-2. SDR PN 114T2111-2, SN NA, AIR LOAD RIB CORRODED, RWS AT 630. ACFT WAS GROUNDED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,133 hrs · 45,807 cycles

STATION 266 BACK SIDE OF FLOOR BEAM VERTICAL STRAP CRACKED LT SIDE FWD ACCESSORY. REMOVED DAMAGED ANGLE INSTALLED NEW ANGLE PN 141T5198 IAW 51-40-02. SDR PN 141T5198, SN NSN, PART NAME ANGLE BRACKET, CRACKED 1/2 INCHES. FUSELAGE STATION & BODY STATION LOCATION ON ACFT STATION 266 TO LBL 15. ACFT WAS GROUNDED.

Part: SKIN — DAMAGED (ZONE 100) · airframe 60,529 hrs · 45,498 cycles

FUSELAGE SKIN DAMAGED BS 434, STRINGERS 31-32R. SKIN REPAIRED IAW COI59981-001 AND REA B653-607-24-MR ACFT WAS GROUNDED.

Part: TERMINAL — BROKEN (EMERGENCY LIGHTS) · airframe 58,455 hrs · 44,527 cycles

DURING S/C FOUND EMERGENCY LIGHTS PARTIALLY WORKING. T/S EMERGENCY LIGHTS SYSTEM FOR LEFT EXIT/THRESHOLD SIGN FOUND BROKEN TERMINAL AT PIN 1, REPAIRED TERMINAL IAW WDM 33-51-14. OPS CHECK NORMAL PER RIGHT EXIT SIGN, DOOR LIGHT (L298), EXTERIOR REAR R1 LIGHT FOUND LOOSE GND AT PIN 2, RETIGHTENED GND & PERFORMED OPS CHECK. OPS CHECK OK IAW AMM 35-51-00, ACFT WAS GROUNDED.

Part: STRINGER — CRACKED (LT WING) · airframe 58,227 hrs · 44,417 cycles

LEFT WING STRINGER AT 16U STA 616.2 HAS A CRACK 5 INCHES LONG. REPAIRED LEFT WING & 16U AT WS 616.2 IAW B767 SRM 57-00-03 AND REA B657-59899MR, ACFT WAS GROUNDED.

Part: STRINGER — CRACKED (RT WING) · airframe 58,227 hrs · 44,417 cycles

RIGHT WING U-15 STRINGER CRACKED AT RIB 17 WS 616.20. REMOVED CRACKED SECTION OF STRINGER AND INSTALLED REPAIR IAW REA B657-59898-MR AND SRM 57-00-03 FIG 201 REPAIR 1, R-19A SHEET NO 45. ACFT WAS GROUNDED.

Part: BEARING — WORN (NR 5 SPOILER) · airframe 58,227 hrs · 44,417 cycles

RIGHT WING WBL 220.5, NR 5 SPOILER I/B BEARING LOOSE / WORN. REPLACED NR 5 SPOILER I/B BEARING IAW SOPM 20-30-03. REFERENCE TO REA 46966REA09. ACFT WAS GROUNDED.

Part: SPAR — CORRODED (TE FLAP) · airframe 58,227 hrs · 44,417 cycles

FLAP MID SPAR WEB UPPER CORD STR 7 IS CORRODED AT LBL 38 JUST I/B OF RIB 2 VERTICAL FLANGE. REMOVED CORROSION AS REQUIRED IAW B767 SRM 55-10-03 AND REA B655-59827-MR, ACFT WAS GROUNDED.

Part: MOUNT — CORRODED (NR 2 ENGINE) · airframe 58,227 hrs · 44,417 cycles

NR 2 ENGINE AFT MOUNT CORRODED. NR 2 ENGINE REMOVED IAW JC 7010 AFT MOUNT REMOVED, INSTALLED SERVICEABLE AFT MOUNT IAW B767 AMM 71-21-02-4. REINSTALL NR 2 ENG IAW J/C 7010. NR 2 ENG NAC STA 298. AFT MOUNT CORROSION, NO CRACK.

Part: ANGLE — CRACKED (LT PYLON) · airframe 58,227 hrs · 44,417 cycles

ANGLE BRACKET CRACKED ON I/B SIDE & O/B SIDE BROKEN BELOW HYD BAY DOORS 1ST LATCH, ABOVE EXHAUST NOZZLE. REPLACED CRACKED ANGLE BRACKET P/N 313T1380-31 IAW B767 SRM 51-40-02, ACFT WAS GROUNDED.

Part: DOUBLER — CORRODED (RT WING) · airframe 58,227 hrs · 44,417 cycles

LIGHT CORROSION INSIDE RT WING OUTBOARD FLAP BOX AT TRAILING EDGE OUTBOARD END RIB. REMOVED AND REPLACED DOUBLER INSIDE RT WING OUTBOARD FLAP BOX AT TRAILING EDGE OUTBOARD END RIB IAW B767 SRM 51-40-02 RT OUTBOARD FLAP, ACFT WAS GROUNDED.

Part: SPAR — CORRODED (TE FLAP) · airframe 58,227 hrs · 44,417 cycles

RIGHT WING INBOARD FLAP MID SPAR WEB UPPER CORD IS CORRODED INSIDE RIGHT INBOARD MAIN FLAP AT WBL 97. REPAIRED CORRODED CORD IAW B767 SRM 51-70-12 FIG 1, ACFT WAS GROUNDED.

Part: PANEL — MISSING (LT WING) · airframe 54,899 hrs · 42,902 cycles

AIRCRAFT EXPERIENCED A PART DEPARTING THE AIRCRAFT EVENT. CREW REPORTED HEARING A LOUD BANG AT 12,000 FT. COMPOSITE PANEL P/N 561QB TRAILING EDGE PANEL JUST FORWARD OF LT AILERON HAD 75 SCREWS MISSING OF 104. PANEL MEASURES 14 X 46 AND IS COMPLETELY MISSING. NO DAMAGE TO AILERON OR ANY OTHER AIRCRAFT PART. INSTALLED MISSING PANEL, INSPECTED AREA AND FOUND NO DAMAGE. PANEL INSTALLED IAW SRM 51-10-2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 54,899 hrs · 42,902 cycles

PERFORMED OPEN HOLE HFEC ON STA 1809.5 RT SPLICE FITTING. TWO CRACKS FOUND IN AREA 2 REF EA 5380002-002 ESO1222. REMOVED AND REPLACED SPLICE FITTING IAW 767 SRM 51-40-02.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 54,899 hrs · 42,902 cycles

NWW AFT LT VERTICAL CHORD CRACKED. REPAIRED CRACK ON NWW VERTICAL CHORD IAW BOEING 767 SRM 51-70-12.

Part: WINDOW — MALFUNCTIONED (COCKPIT) · airframe 53,316 hrs · 42,200 cycles

LEFT SIDE OF CAPTAIN'S INSTRUMENT PANEL PRODUCING A STRONG BURNING ODOR, NO SMOKE OR VAPOR SEEN. LT 2 & RT 2 WINDOWS REPLACED.

Part: ACTUATOR — DEFECTIVE (CAPTAIN SEAT) · airframe 51,944 hrs · 41,562 cycles

CAPTAIN'S SEAT DID NOT MAINTAIN POSITION DURING LANDING, SLID FORWARD 4+ INCHES. REPLACED CAPTAIN'S SEAT HORIZONTAL ACTUATOR ASSY IAW WEBBER CMM 25-10-28. OPS CHECKED GOOD.

Part: ENGINE — FAILED (RIGHT) · airframe 51,836 hrs · 41,516 cycles

AT APPROXIMATELY 600 FEET ON TAKEOFF, RIGHT ENGINE COMPRESSOR STALLED. EGT EXCEEDANCE OF 1053 DEGREES WAS RECORDED. ENGINE FAILED ON FINAL. REPLACED RIGHT ENGINE IAW JOB CARD 7010.

Part: INDICATOR — BURNED (COCKPIT) · airframe 48,567 hrs · 40,418 cycles

STA: JFK, MAINTENANCE SMELLED ELECTRICAL SMOKE IN COCKPIT. CO-PILOT EADI BLANK. INSPECTED AND FOUND F/O'S EADI DAMAGED. REMOVED AND REPLACED F/O'S EADI IAW B767 AMM 34-22-34. OPS CHECKED GOOD.

Part: SERVO — DEFECTIVE (YAW DAMPER) · airframe 46,366 hrs · 39,728 cycles

EXPERIENCED UNCOMMANDED RUDDER INPUTS ALL PHASES OF FLIGHT WITH AUTO PILOT ENGAGED AND OFF AS WELL. GAINED ACCESS TO RUDDER YAW DAMPERS AND INSPECTED ACTUATORS. FOUND ACTUATOR LEAKING FROM SERVO RUDDER. REMOVED AND REPLACED ACTUATOR IAW B767 MM 22-21-02.4. FUNCTION AND LEAK CHECKED GOOD. ALL LEAKAGE AND FITTINGS LOOKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,436 hrs · 39,463 cycles

LEFT INTERIOR EMERGENCY LIGHT ABOVE DOOR IS INOP. T/S AND FOUND M735 PWR SUPPLY CHARGER INOP SWAPPED M735 AND M736, NOW CHECK OK M736 SPARE INOP. PRIMARY PWR SUPPLY CHARGER M735, OPS CHECK GOOD. DEFERRED DI NR 48990 DEFERRED PER GMM 01-07-04 FOR MAINT TRACKING MBCB. PLACARD INSTALLED CODE 10 CLEAR DI 48990. REPLACED SPARE EMERGENCY LIGHT PWR SUPPLY CHARGER IAW AMM 33-51-03-2 EMERGENCY LIGHT TEST GOOD IAW AMM 33-51-00-5.