N922DX

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 48,241 hrs · 32,095 cycles

DAMAGE FOUND ON THE DORSAL FIN SKIN, FWD OF ACCESS PANEL, AT FASTENER HOLES BY BSS 52. REMOVED THE DAMAGE AND REPAIRED IAW SRM 55-30-05, FIG 20, SHEET 3. AND APPLIED PROTECTIVE COATINGS.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 48,231 hrs · 32,091 cycles

DAMAGE ON DORSAL FIN SKIN FWD OF ACCESS PANEL AT FASTENER HOLES BY STA 2FS-52. REMOVED NUT PLATE STRIP AND BACKING PLATE. TRIMMED DAMAGE PER MD 90 SRM 55-30-05. FABRICATED REPAIR DOUBLER FROM 7075-0.050, FILLER .040 7075-0 AND SPLICE .050 7075-0. INSTALLED REPAIR IAW MD 90 SRM 55-30-05. REPAIR COMPLETE. (LP#0612926)

Part: SKATE ANGLE — CRACKED · airframe 48,199 hrs · 32,076 cycles

RIGHT SKATE ANGLE WAS CRACKED AT THE BASE OF THE VERTICAL STAB, UNDER THE LEADING EDGE. REMOVED AND REPLACED THE ANGLE.

Part: SHEAR TIE — CRACKED (BS 1494) · airframe 48,199 hrs · 32,076 cycles

CRACKED SHEAR TIE AT BS 1494 OTBD OF LEFT DORSAL FITTING. REMOVED AND REPLACED THE SHEAR TIE IAW DWG 9953016-29.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 47,462 hrs · 31,649 cycles

ROW 27 LEFT 10" OF PHOTO LUMINESCENT STRIP MISSING. REPLACED PHOTO LUM STRIP OK FOR SVC.

Part: LANYARD — LOOSE (EVAC SLIDE) · airframe 47,142 hrs · 31,461 cycles

R1 DOOR SLIDE LANYARD LOOSE. REINSTALLED LANYARD PER MM. OPERATION CHECKS GOOD.

Part: STARTER — FIRE (APU) · airframe 46,942 hrs · 31,333 cycles

DURING GROUND OPERATION, ACS ALERTED MAINTENANCE TO SMOKE FROM APU AREA. MAINTENANCE OPENED LT APU ACCESS DOOR AND FOUND APU STARTER ON FIRE. CLOSED ACCESS AND BLEW NR 1 FIRE BOTTLE. APU REMOVED AND COMPARTMENT INSPECTED AND CLEANED. NEW APU INSTALLED. A/C WIRING INSPECTION AND STARTER RELAY REPLACEMENT IN PROGRESS.

Part: OIL SYSTEM — EMPTY (NR 2 ENGINE) · airframe 46,010 hrs · 30,777 cycles

PERFORMED AN AIR TURN BACK TO DEPARTURE DUE TO A NR 2 ENGINE OIL QUANTITY INDICATION OF ZERO. IFSD IAW QRH DUE TO LOSING OIL QUANTITY AND PRESSURE. ENGINE CHANGED.

Part: ACM — OVERSERVICED · airframe 45,701 hrs · 30,602 cycles

DIVERTED, DUE TO REPORT OF SMOKE ODOR IN CABIN. SMOKE DISSIPATED BUT UNABLE TO DETERMINE CAUSE. MAINTENANCE FOUND EVIDENCE OF OIL CONTAMINATION IN RIGHT COALESCER BAG. TROUBLESHOT AND FOUND BOTH ACM'S OVERSERVICED. DRAINED AND SERVICED TO PROPER LEVEL. REPLACED COALESCER BAGS AND PERFORMED DUCT BURNOUT. NO ODOR OR SMOKE NOTED.

Part: SENSOR — FAILED (CABIN TEMP) · airframe 45,711 hrs · 30,608 cycles

WITH BOTH PACKS OPERATING AT 25000FT, LEFT PACK FULL HOT IN AUTO MODE, CABIN SUPPLY TEMP STOPPED AT 80. ODOR OF BURNED RUBBER. PACK TRIPPED. TROUBLESHOT AND REMOVED AND REPLACED FLIGHT COMPARTMENT TEMP SENSOR. PERFORMED DUCT BURNOUT. OPERATION CHECKED GOOD.

Part: ACCESS PANEL — CORRODED (WING) · airframe 45,616 hrs · 30,558 cycles

CORROSION ON COUNTERSINK ON FUEL ACCESS PANEL. FOUND TO BE OUT OF LIMITS AND REPLACED IAW SRM 57-00-04.

Part: STRUCTURE — CORRODED (BS 943-962) · airframe 45,616 hrs · 30,558 cycles

CORROSION ON UPPER SURFACE OF THE STRUCTURE BETWEEN BS 943 - 962, LBL 44 - 54. REPAIRED COMPLIED WITH ERA 558080-14AD, REV O.

Part: BULKHEAD — CORRODED (BS 994) · airframe 45,616 hrs · 30,558 cycles

CORROSION ON SKIN AT FORWARD PRESSURE BULKHEAD, BS 994 BELOW SLANT PANEL LBL 25 TO 60 AT MAIN LANDING GEAR WHEEL WELL. REPAIRED IAW ERA 558080-14AD, REV O.

Part: WEB — CORRODED (VENTRAL STAIR) · airframe 45,616 hrs · 30,558 cycles

CORROSION ON WEB AT THE RIGHT SIDE OF STEP NR 11 AT VENTRAL STAIR. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 51-11-01.

Part: CARGO TRACK — CORRODED (BS 1268-1307) · airframe 45,616 hrs · 30,558 cycles

CORROSION ON CARGO TRACK BS 1268 - 1307 IN THE AFT CARGO BAY. REPLACED IAW SRM 51-10-03, 51-30-01, AND 51-30-05.

Part: FLOOR SUPPORT — CRACKED (BS 1288-1344) · airframe 45,616 hrs · 30,558 cycles

CRACKED FLOOR SUPPORT ON BS 1328, 1344, AND 1288 IN THE AFT CARGO COMPARTMENT. REPLACED IAW ERA 412247-14.

Part: ACCESS PANEL — CORRODED · airframe 45,616 hrs · 30,558 cycles

CORROSION ON FUEL TANK ACCESS PANEL 520CB. REPLACED THE ACCESS PANEL.

Part: SPAR — DAMAGED (RT STAB) · airframe 45,616 hrs · 30,558 cycles

DISCREPANT AREA FOUND AT RIGHT STABILIZER UPPER REAR SPAR AFT BARREL NUT HOLE. FOUND TO BE OUT OF LIMITS. REPAIRED IAW ERA 531273-14AD, REV A.

Part: TEE FITTING — CRACKED (BS 1055) · airframe 45,616 hrs · 30,558 cycles

CRACK ON TEE FITTING ON AFT MAIN LANDING GEAR DOOR FRAME, BS 1055, LBL 60. REPLACED THE TEE FITTING IAW SRM 51-30-01, 51-30-02, 51-30-05, 51-10-05 AND DWG 5936395, REV BF.

Part: BEAM — CRACKED (NLG DOOR FRAME) · airframe 45,616 hrs · 30,558 cycles

CRACKED LEFT DOOR FRAME BEAM OF NOSE LANDING GEAR,BS 41 TO 69. REPAIRED IAW SRM 53-90-01.

Part: BUSHING — CORRODED (RT NACELLE) · airframe 45,616 hrs · 30,558 cycles

CORROSION ON AFT CONE BOLT FITTING SUPPORT BUSHINGS AT RIGHT PYLON. REMOVED AND REPLACED THE BUSHINGS IAW CMM 71-20-14.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 45,616 hrs · 30,558 cycles

CRACK ON FORWARD EDGE BEAM EDGE AT FORWARD SERVICE DOOR. REPLACED IAW SRM 51-30-02 AND 51-30-05.

Part: SUPPORT — CORRODED (BS 994) · airframe 45,616 hrs · 30,558 cycles

CORROSION ON FITTING SUPPORT AT LEFT MAIN LANDING GEAR TRAPEZOIDAL PANEL, BS 994, LBL 60, Z=-10. FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 51-30-01 AND 51-10-03.

Part: SUPPORT — CORRODED (BS 994) · airframe 45,616 hrs · 30,558 cycles

CORROSION ON FITTING SUPPORT AT RIGHT HAND MAIN LANDING GEAR TRAPEZOIDAL PANELS, BS 994, LBL 60, Z=-10. FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 51-10-05, 51-30-01 AND 51-10-03.

Part: SKIN — CORRODED (FUSELAGE) · airframe 45,616 hrs · 30,558 cycles

CORROSION BELOW PRODUCTION DOUBLERS AT MID CARGO COMPARTMENT DOOR. REPAIRED IAW ERA 558092-14, REV O AND ETI 90-17-038 REV O. (LP# 0013408)

Part: DOUBLER — WORN (CARGO DOOR) · airframe 45,616 hrs · 30,558 cycles

WEAR ON FORWARD AND AFT LOWER DOUBLERS AT MID CARGO DOOR. REPLACED DOUBLERS IAW SRM 51-30-02.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 45,616 hrs · 30,558 cycles

CORROSION ON FUEL TANK PANEL 520GB. REPAIRED IAW SRM 57-00-04. (LP# 0012851)

Part: ACCESS PANEL — DAMAGED (NOT REPORTED) · airframe 45,616 hrs · 30,558 cycles

ELONGATED HOLES ON FUEL TANK ACCESS PANEL, 620DB. REPAIRED IAW SRM 57-00-04.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 45,616 hrs · 30,558 cycles

CRACKS ON SKIN AROUND OF HANDLE AT AFT CARGO COMPARTMENT DOOR. REPAIRED IAW ERA 558083-14, REV O AND ETI 90-17-033, REV 3.

Part: SKIN — NICKED (FUSELAGE) · airframe 45,616 hrs · 30,558 cycles

NICK ON RIGHT HAND EXTERNAL FUSELAGE SKIN, STA 1542 CANT PROJECTIONS L17R. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 51-31-02 AND 53-31-02.

Part: ACCESS PANEL — CORRODED (WING) · airframe 45,616 hrs · 30,558 cycles

CORROSION ON COUNTERSINK OF FUEL PANEL 620CT AND 520CT. REPLACED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,616 hrs · 30,558 cycles

CRACK ON FRAME STA 1458 BETWEEN LONGERON 1 AT AFT ACCESSORY COMPARTMENT. REPAIRED IAW SRM 53-10-02 AND 51-30-05.

Part: DOOR — CRACKED (CABIN) · airframe 45,616 hrs · 30,558 cycles

CRACKS ON FORWARD AND AFT UPPER CORNERS OF L1 DOOR. REPAIRED IAW SRM 52-10-02.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 45,616 hrs · 30,558 cycles

CORROSION ON LOWER DOOR JAMB FROM STA 693 TO 750, MID CARGO COMPARTMENT. REPLACED IAW SRM 53-60-02.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,616 hrs · 30,558 cycles

CRACKED LEFT HAND FLOORBEAM AT STA 984 AT X=54 TO 60. REPAIRED IAW SRM 51-30-02, 51-30-05, 51-30-01 51-30-08 AND 51-10-03.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 45,616 hrs · 30,558 cycles

CRACKED INTERCOSTAL BETWEEN BEAM NR 4 AND 5 OF L1 DOOR. REPLACED IAW SRM 51-30-02 AND 51-30-05.

Part: ACCESS PANEL — CORRODED (WING) · airframe 45,616 hrs · 30,558 cycles

CORROSION ON FUEL ACCESS PANEL 620AT. FOUND TO BE OUT OF LIMITS. REPLACED.

Part: CHANNEL — CORRODED (BS 200-215) · airframe 45,616 hrs · 30,558 cycles

CORROSION ON CHANNEL BS 200 - 215, RLB 54.

Part: CUSP WEB — CORRODED (BS 750) · airframe 45,616 hrs · 30,558 cycles

CORROSION ON THE CUSP WEB BS 750, LBL 48. REPAIRED IAW SRM 51-30-02 AND 51-11-01.

Part: CUSP WEB — CRACKED (BS 439) · airframe 45,616 hrs · 30,558 cycles

CRACK ON THE CUSP WEB BS 439. REPAIRED IAW SRM 53-20-02.

Part: CUSP WEB — CORRODED (BS 943-962) · airframe 45,616 hrs · 30,558 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER ON THE CUSP WEB, BS 943 TO 962, RBL 54 TO 60. THE DOUBLER WAS REPLACED IAW SRM 53-20-02.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 45,616 hrs · 30,558 cycles

CRACKED INNER SUPPORT FORWARD EDGE ON BEAM 5 AT MID CARGO COMPARTMENT DOOR. REPLACED IAW SRM 51-30-05.

Part: STRUCTURE — CRACKED (CARGO DOOR SKIN) · airframe 45,616 hrs · 30,558 cycles

CRACK ON PREVIOUS REPAIR AROUND HANDLE OF MID CARGO COMPARTMENT DOOR. REPAIR WAS REPLACED IAW SRM 52-30-01.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 45,616 hrs · 30,558 cycles

CRACKS ON OUTER SKIN AROUND HANDLE ON THE FORWARD CARGO COMPARTMENT DOOR. REPAIRED IAW SRM 52-30-01.

Part: FLOOR SUPPORT — CORRODED · airframe 45,616 hrs · 30,558 cycles

CORROSION OUT OF LIMITS ON FLOOR SUPPORT. REPLACED IAW SRM 51-30-02, 51-30-05, 51-10-03.

Part: BEAM — CRACKED (L1 DOOR) · airframe 45,616 hrs · 30,558 cycles

CRACKED NR 1 BEAM MAIN ENTRY DOOR L1. REPAIRED IAW SRM 52-10-02.

Part: ANGLE — CRACKED (RT OVERWING EXIT) · airframe 45,616 hrs · 30,558 cycles

CRACK ANGLE ON STOP FITTING, NR 1 RIGHT AFT OVERWING EXIT DOOR. REPLACED IAW SRM 51-30-05 AND 51-30-02.

Part: CUSP WEB — CORRODED (BS 389) · airframe 45,616 hrs · 30,558 cycles

CORROSION ON CUSP WEB, BS 389, RBL 49. REPAIRED IAW SRM 53-20-02.

Part: WEB — CORRODED (BS 170-180) · airframe 45,616 hrs · 30,558 cycles

CORROSION ON MEMBRANE LOWER SURFACE BETWEEN BS 170 - 180, RBL 54 TO 60. REPAIRED IAW SRM 51-30-02, AND 51-3.0-05.

Part: FITTING — CRACKED (EMERGENCY EXIT) · airframe 45,616 hrs · 30,558 cycles

CRACKED CLIP ON STOP FITTING 12 LEFT HAND FORWARD OVERWING EXIT DOOR. REPLACED IAW SRM 51-30-05 AND 51-30-02.

Part: FLOORBEAM — CORRODED (BS 180) · airframe 45,616 hrs · 30,558 cycles

CORROSION ON FLOORBEAM BS 180 BETWEEN LBL 17 TO 38. REPLACED IAW SRM 51-30-02, 51-10-05, 51-30-05, AND 51-10-03.

Part: JACKSCREW — GOUGED · airframe 44,395 hrs · 29,903 cycles

HORIZONTAL JACK SCREW ATTACH POINTS HAS GOUGES ON ATTACH BOLT BORE FACES. REPAIRED IAW PRI/ERA 552082-14, REV O.

Part: CATWALK — OUT OF ADJUST · airframe 44,132 hrs · 29,735 cycles

FLIGHT ATTENDANT AND SEVERAL PASSENGERS HEARD LOUD UNUSUAL NOISE FROM TAIL COMPARTMENT. MAINTENANCE FOUND CATWALK HANGING UP ON FORWARD UPPER PANEL AND THEN FALLING TO THE FLOOR WITH A LOUD CLANG. ADJUSTED CATWALK PER MM. OPERATION CHECKS OK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,514 hrs · 29,362 cycles

CORROSION ON FLOOR SUPPORT, STA 180, RBL 24. R & R SAME IAW SRM 53-00-01.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 43,514 hrs · 29,362 cycles

CORROSION ON LONGERON 29R, STA 162-166 IN ELECTRONIC EQUIPMENT COMPARTMENT. R & R IAW SRM 53-00-01 AND DWG 5911401.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,514 hrs · 29,362 cycles

CORROSION SEAT TRACK RT SIDE, RBL 22, STA 198. R & R SEAT TRACK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,514 hrs · 29,362 cycles

CORROSION ON FLOORBOARD SUPPORT LBL 44, STA 160-200. REPLACED FLOOR SUPPORT IAW DWG 9936534.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,464 hrs · 29,341 cycles

SKIN CRACK CANTED FRAME STA 1531, RT SIDE UP FROM AIR STAIRS CUTOUT.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 43,445 hrs · 29,330 cycles

FLOORBEAM CORRODED, BS 200, LBL 4- RBL4. R & R SUPPORT IAW SRM 51-30-02.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 43,445 hrs · 29,330 cycles

FLOORBEAM CORRODED, BS 200, LBL 10-14. REPLACED SUPPORT IAW DWG 9936534.

Part: FLOOR SUPPORT — CORRODED (BS 180-200) · airframe 43,445 hrs · 29,330 cycles

FLOOR SUPPORT AT R1 DOOR OPENING FROM BS 180-200 CORRODED. R & R SUPPORT IAW DWG 9936534.

Part: FLOOR SUPPORT — CORRODED (BS 180-200) · airframe 43,445 hrs · 29,330 cycles

FLOORBOARD SUPPORT AT BS 180-200, RBL 8 CORRODED. REPLACED SUPPORT IAW SRM 51-30-02.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 43,445 hrs · 29,330 cycles

FLOORBEAM AT BS 200, RBL 44-54 CORRODED. R & R SUPPORT IAW DWG 9936534.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,445 hrs · 29,330 cycles

CORROSION ON WEB, BS 201, RBL 45. REPAIRED IAW SRM 51-11-01.

Part: MOUNT — CORRODED (GALLEY) · airframe 43,445 hrs · 29,330 cycles

OTBD AFT MOUNT ON G1 GALLEY IS CORRODED. REPLACED FITTING IAW CMM 25-30-14, FIG 10, IB 40613.

Part: FLOOR PANEL — CORRODED (BS 180) · airframe 43,445 hrs · 29,330 cycles

CORROSION ON FLOOR PAN, BS 180, RBL 44 CORNER. REPAIRED IAW SRM 53-20-02.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 43,445 hrs · 29,330 cycles

FLOOR SUPPORT, BS 160-200, LBL 8, CORRODED. REPLACED THE FLOOR SUPPORT IAW DWG 9936534.

Part: CUSP WEB — CORRODED (BS 200) · airframe 43,445 hrs · 29,330 cycles

CUSP WEB, BS 200, RBL 10, CORRODED. REPAIRED IAW PRI/ERA 547709-14, REV O.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 43,445 hrs · 29,330 cycles

CORROSION ON FLOORBEAM, BS 200, RBL 18-44. R & R FLOORBEAM IAW SRM 51-00-00.

Part: WEB — CORRODED (BS 201) · airframe 43,445 hrs · 29,330 cycles

CORROSION ON WEB, STA 201, RBL 7. REPAIRED IAW SRM 51-11-01.

Part: FLOOR SUPPORT — CORRODED (BS 180-200) · airframe 43,445 hrs · 29,330 cycles

CORROSION ON FLOOR SUPPORT, BS 180-200, RBL 44. REPLACED SUPPORT IAW DWG 9936534.

Part: SEAT TRACK — CORRODED (BS 195) · airframe 43,445 hrs · 29,330 cycles

CORROSION ON SEAT TRACK RT SIDE RBL 44, STA 195. REPAIRED IAW SRM 53-10-00.

Part: SEAT TRACK — CORRODED (BS 200) · airframe 43,445 hrs · 29,330 cycles

LEFT CENTER SEAT TRACK CORRODED, BS 200. REPLACED IAW SRM 53-10-01.

Part: CRANK ASSY — CORRODED (LT SPOILER) · airframe 43,445 hrs · 29,330 cycles

LEFT GROUND SPOILER CRANK HAS CORROSION IN BORES. REPAIRED IAW SRM 57-00-01.

Part: FRAME — CRACKED (BS 1520) · airframe 43,445 hrs · 29,330 cycles

CRACK ON CANTED B-FRAME AFT WEB, BS 1520. REPAIRED IAW SRM 53-10-03.

Part: FRAME — WORN (BS 1437) · airframe 43,445 hrs · 29,330 cycles

FRAME WEB, FORWARD SIDE HAS DEEP WEAR MARKS, BS 1437, NEAR L5L. REPAIRED IAW SRM 53-00-01.

Part: LONGERON — CORRODED (BS 160-167) · airframe 43,573 hrs · 29,404 cycles

CORROSION ON LONGERON 29L, BS 160-167. REMOVED AND REPLACED THE LONGERON IAW SRM 53-00-01.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 43,514 hrs · 29,362 cycles

CORROSION ON LONGERON CHANNEL 30, STA 160-162, ELECTRICAL EQUIPMENT COMPARTMENT. R & R IAW SRM 53-00-01 AND DWG 5911401.

Part: FLOOR SUPPORT — CORRODED (BS 254) · airframe 43,445 hrs · 29,330 cycles

FLOOR SUPPORT CORRODED, BS 254. R & R FLOOR SUPPORT IAW SRM 51-30-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,353 hrs · 29,276 cycles

WHILE REPLACING EMERGENCY LIGHT BATTERY PACKS, FOUND 1 BATTERY PACK NOT CHARGING. R & R IAW MM. OPERATION CHECKS GOOD. OK FOR SERVICE.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 43,207 hrs · 29,200 cycles

DAMAGE TO RT LOWER HORIZONTAL STABILIZER SKIN PANEL.

Part: ELECTRICAL SYS — POWER LOSS · airframe 38,147 hrs · 26,054 cycles

PERFORMED AN AIR TURN BACK DUE TO ELECTRICAL POWER LOSS AFTER TAKEOFF. LT GENERATOR ON DEFERRAL AT TIME OF EVENT. TROUBLESHOT IAW FIM. FOUND CURRENT LIMITERS F1-23, F1-24 AND F1-25 ALL BLOWN. REPLACED CURRENT LIMITER, EPCU, RT GENERATOR, AND RIGHT BUSS TIE RELAYS, B6-609 AND B-611. RAN BOTH ENGINES AT IDLE AND TAKEOFF POWER . TRANSFERRED POWER SEVERAL TIMES BETWEEN LT, RT AND APU BUSSES. SYSTEM CHECKED GOOD. ALSO PERFORMED VISUAL INSPECTION OF FEEDER CABLES ON RT ENGINE. NTF.

Part: STRUCTURE — DAMAGED (HORIZONTAL STAB) · airframe 38,079 hrs · 26,011 cycles

DAMAGE FOUND ON THE RT LOWER HORIZONTAL STABILIZER PLANK JUST AFT OF THE FRONT SPAR. REPAIR COMPLETE IAW ERA 526487-14, REV O.

Part: SKIN — CORRODED (BS 1394) · airframe 38,077 hrs · 26,009 cycles

FOUND EVIDENCE OF CORROSION AT LAP JOINT, FWD OF RT APU DOOR, APPROXIMATELY BS 1394 BETWEEN L24 -25R. COMPLIED WITH ERA 525661-14, REV O.

Part: LONGERON — CORRODED (BS 1318-1402) · airframe 38,077 hrs · 26,009 cycles

MULTIPLE SPOTS OF CORROSION ON LONGERON 28R AT BS 1318 - 1402. R & R LONGERON IAW DWG 5936667 AD ERA 1463600-14, REV O, SECT I.

Part: LONGERON — CORRODED (BS 1318-1402) · airframe 38,077 hrs · 26,009 cycles

MULTIPLE SPOTS OF CORROSION ON LONGERON 27R BS 1318 - 1402. R & R LONGERON IAW DWG 5936667 AND ERA 525752-14, REV O, SECTION I.

Part: LONGERON — CORRODED (BS 1307) · airframe 38,077 hrs · 26,009 cycles

CORROSION ON LONGERON 30 FORWARD OF BS 1307. R & R THE LONGERON IAW DWG 5936667 AND ERA 525752-14, REV O., SECT I.

Part: TEE FITTING — CORRODED (AFT BULKHEAD) · airframe 38,077 hrs · 26,009 cycles

CORROSION ON AFT PRESSURE BULKHEAD TEE FITTING LOWER FORWARD FLANGE LOWER SURFACE BETWEEN LONGERON 27R AND 28R. ACCOMPLISHED ERA 525970-14, REV O, SECTION I.

Part: LONGERON — CORRODED (BS 1290-1307) · airframe 38,077 hrs · 26,009 cycles

CORROSION ON LONGERON 29L BETWEEN FS 1290-1307. R & R THE LONGERON IAW DWG 5936667 AND ERA 52752-14, REV O. SECTION I.

Part: TEE FITTING — CORRODED (BS 1395 BULKHEAD) · airframe 38,077 hrs · 26,009 cycles

CORROSION ON AFT PRESSURE BULKHEAD TEE FITTING, BS 1395, LOWER HORIZONTAL SURFACE BETWEEN LONGERON 26R - 26L. R & R IAW ERA 525970-14, REV O.

Part: LONGERON — CORRODED (BS 1318-1402) · airframe 38,077 hrs · 26,009 cycles

MULTIPLE SPOTS OF CORROSION LONGERON 29R FROM SPLICE BS 1318 AFT BS 1402. R & R LONGERON IAW DWG 5936667 AND ERA 525752-14, REV O.

Part: BEAM — DAMAGED (AFT CARGO DOOR) · airframe 38,077 hrs · 26,009 cycles

AFT CARGO DOOR BEAM, FOUND OUT OF LIMITS AND R & R IAW DWG 591104.

Part: ATTACH FITTING — CORRODED (TAIL CONE) · airframe 38,077 hrs · 26,009 cycles

FUSELAGE TAILCON ATTACH FRAME HAS MILD CORROSION ON AFT FACE AT 6 O'CLOCK POSITION FROM LBL 14 TO RBL 14. REPAIRED IAW ERA 526342-14, REV O.

Part: SKIN — STRETCHED (BS 1402) · airframe 38,077 hrs · 26,009 cycles

LOWER FUSELAGE EXTERNAL SKIN STRETCHED AT FORWAD SIDE OF AFT PRESSURE BULKHEAD FS 1402. R & R BELLY SKIN IAW DWG 593667 AND ERA 525752-14 REV O.

Part: SKIN — DAMAGED (BS 1318) · airframe 38,077 hrs · 26,009 cycles

SKIN DAMAGED BS 1318, L26L - 26R. REPAIRED IAW ERA 525752-14, SECTION 1.

Part: FRAME — CORRODED (BS 1364) · airframe 38,077 hrs · 26,009 cycles

FRAME BS 1364, CORRODED BETWEEN LONGERON 29L AND 29R AT AFT SIDE OF FRAME. REPAIRED IAW SRM 51-70-01.

Part: FRAME — CORRODED (BS 1328) · airframe 38,077 hrs · 26,009 cycles

CORROSION AFT OF FRAME BS 1328 BETWEEN L29-30L. REPAIRED IAW SRM 51-70-01.

Part: SKIN — CRACKED (BS 1475) · airframe 38,077 hrs · 26,009 cycles

SKIN CRACKED AT BS 1475 BETWEEN L1 AND L2R. REPAIRED IAW ERA 525798-14, REV O.

Part: FRAME — CHAFED (BS 1458) · airframe 38,077 hrs · 26,009 cycles

FRAME BS 1458 CHAFED THROUGH AT L7L. REPAIRED IAW SRM 53-10-02.

Part: FRAME — CHAFED (BS 1458) · airframe 38,077 hrs · 26,009 cycles

TAIL INTERIOR FRAME, BS 1458, IS CHAFED THROUGH AT LONGERON 7L. REPAIRED IAW SRM 53-10-02.

Part: SHEAR TIE — CRACKED (BS 1475) · airframe 38,077 hrs · 26,009 cycles

FRAME TO SKIN SHEAR TIE CRACKED AT BS 1475, L2L AFT SIDE. REMOVED CRACKED SHEAR TIE AND REPLACED IAW ERA 525829-14, REV O.

Part: SKIN — CRACKED (BS 1475) · airframe 38,077 hrs · 26,009 cycles

SKIN CRACKED FROM FASTENER AT BS 1475 JUST OUTBOARD OF SKATE ANGLE LEFT HAND SIDE. REPAIRED IAW PRI 525829-14, REV O.

Part: DOOR FRAME — CORRODED (BS 1212) · airframe 38,077 hrs · 26,009 cycles

C3 CARGO DOOR CUT OUT LOWER FORWARD CORNER BS 1212, FITTING CORRODED. REMOVED AND REPLACED FITTING IAW DWG 5936469.

Part: INTERCOSTAL — CORRODED (BS 1212) · airframe 38,077 hrs · 26,009 cycles

INTERCOSTAL CORROSION L28-29R, BS 1212. REMOVED AND REPLACED INTERCOSTAL PER DWG 5930483.

Part: FRAME — CRACKED (BS 962) · airframe 38,077 hrs · 26,009 cycles

FRAME, BS 962 CRACKED IN RADIUS AT CUSP LINE. REMOVED AND REPLACED OVERWING FRAME, BS 962, IAW DWG SR90530027.

Part: INTERCOSTAL — CORRODED (BS 1259) · airframe 38,077 hrs · 26,009 cycles

INTERCOSTAL CORROSION L28-29R, BS 1259. REMOVED AND REPLACED INTERCOSTAL IAW DWG 5930483.

Part: INTERCOSTAL — CORRODED (BS 1231) · airframe 38,077 hrs · 26,009 cycles

INTERCOSTAL CORRODED L28-29R, BS 1231. REMOVED AND REPLACED INTERCOSTAL IAW DWG 5930483.

Part: INTERCOSTAL — CORRODED (BS 1268) · airframe 38,077 hrs · 26,009 cycles

INTERCOSTAL CORROSION L28-29R, BS 1268. REMOVED AND REPLACED INTERCOSAL IAW DWG 5930483.

Part: FITTING — UNKNOWN (BS 1268) · airframe 38,077 hrs · 26,009 cycles

C3 DOOR CORNER FITTING LOWER AFT BS 1268 OUTBOARD OF L28R. REMOVED AND REPLACED FITTING IAW DWG 5936469.

Part: INTERCOSTAL — CORRODED (BS 1250) · airframe 38,077 hrs · 26,009 cycles

INTERCOSTAL CORRODED ON L28-29R, BS 1250. REMOVED AND REPLACED INTERCOSTAL IAW DWG 5930483.

Part: INTERCOSTAL — CORRODED (BS 1222) · airframe 38,077 hrs · 26,009 cycles

INTERCOSTAL CORRODED L28-29R, BS 1222. REMOVED AND REPLACED INTERCOSTAL IAW DWG 5930483.

Part: SHEAR TIE — CORRODED (BS 1193) · airframe 38,077 hrs · 26,009 cycles

CORROSION ON SHEAR TIE AT BS 1193 L27R FORWARD SIDE. FABRICATED AND INSTALLED NEW SHEAR TIE SECTION AND STRAP IAW SRM 51-10-04 AND 53-10-02.

Part: STRUCTURE — CRACKED (CATWALK) · airframe 38,077 hrs · 26,009 cycles

CATWALK EMERGENCY WALKWAY CRACKED AT BOTH FORWARD SIDES. FABRICATED AND INSTALLED DOUBLERS IAW SRM 53-00-02 AND ERA 489806-14MA.

Part: LONGERON — CORRODED (BS 1290-1307) · airframe 38,077 hrs · 26,009 cycles

CORROSION ON LONGERON 29L BETWEEN FS 1290-1307. REMOVED AND REPLACED LONGERON IAW DWG 5936667-517 AND ERA 5252752-14.

Part: LONGERON — CORRODED (BS 1307) · airframe 38,077 hrs · 26,009 cycles

CORROSION ON LONGERON 29L AFT OF FS 1307. REMOVED AND REPLACED LONGERON IAW PRI 525752-14, REV O, FROM BS 1296 - 1395. COMPLETED REMOVAL AND REPLACEMENT IAW DWG 5936667-517 AND ERA 525752-14.

Part: SKIN — CRACKED (BS 1475) · airframe 38,077 hrs · 26,009 cycles

CRACK WAS FOUND COMMON TO LONGERON 2R JUST AFT OF BS 1475 IAW ERA 525798-14, SECT II.

Part: BOTTLE — LOW PRESSURE (TAILCONE SLIDE) · airframe 36,327 hrs · 24,894 cycles

DURING SERVICE CHECK, MX FOUND TAILCONE SLIDE BOTTLE PRESSURE BELOW GREEN BAND. R & R TAIL CONE EVACUATION SLIDE IAW WC 2500-4332.

Part: PIN — OUT OF POSITION (CONNECTOR) · airframe 34,641 hrs · 23,992 cycles

EMERGENCY LIGHT INOPERATIVE. FOUND PIN 1 ON CONNECTOR P1-2300 PUSHED BACK. RESET PIN. OPS CHECKED NORMAL.

Part: GIRT BAR — DETACHED (R1 DOOR SLIDE) · airframe 32,623 hrs · 22,875 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE 1R DOOR GIRT BAR WAS NOT ATTACHED TO THE EMERGENCY EVACUATION SLIDE. MAINTENANCE HAS RE-ATTACHED THE GIRT BAR TO THE SLIDE.

Part: LIGHT — MISSING (CABIN) · airframe 32,437 hrs · 22,771 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND EMERGENCY FLOOR PATH LIGHTING MISSING AT SEAT 26B. REMOVED AND REPLACED MISSING EMERGENCY FLOOR PATH LIGHT PER MAINTENANCE MANUAL. OPERATION CHECKS GOOD.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 30,743 hrs · 21,925 cycles

DURING CHECK, MAINTENANCE FOUND LEFT AFT LAVATORY MISSING 7 INCHES OF EMERGENCY PATHWAY GLOW STRIP LIGHT. MAINTENANCE FORWARD TO MCO/PLACARD PER MEL 33-51-01B. MAINTENANCE IN ATL REPLACED MISSING STRIP PER EA 02-477506-03 ME07. (2011-D0903)

Part: LIGHT — MISSING (L2 DOOR) · airframe 30,743 hrs · 21,925 cycles

DURING CHECK, MAINTENANCE FOUND 7 INCH STRIP OF EMERGENCY PATHWAY GLOW STRIP LIGHT FORWARD OF L2 DOOR, FORWARD OF PARTITION, MISSING. MAINTENANCE FORWARD TO MCO/PLACARD PER MEL 33-51-01B.

Part: FRAME — CORRODED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

AFT CARGO FRAME L29L STA 1288 CORRODED. SPICED IN NEW SECTION OF FRAME IAW SRM 53-10-02 VOL I.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

FUSELAGE EXTERNAL SKIN STA 237-256 STR 28L - 29R CORROED UNDER TCAS ANTENNA DOUBLER. REPAIRED EXTERNAL SKIN PER ERA 491199-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

SKIN HAS TOOLING DAMAGE STA 1520 9R. REPAIRED IAW ERA 491204-14 ORIG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

FWD CARGO INTERIOR SKIN CORRODED AT STA 427 - 2. REPAIRED IAW SRM 53-30-02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

CABIN STA 1350 BL 0 LBL 14 FRAME CORRODED. REPLACED TOP CAP OF FRAME IAW SRM 5300.

Part: BEAM — CORRODED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

AFT CARGO BAY STA 1240 29R CORRODED ON BEAM. REPAIRED PER ERA 490980-4.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

AFT CARGO LONG 29R CORRODED STA 1204. REPAIRED IAW ERA 491205-14 ORIG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

SKIN UNDER RUB STRIP STA 1136-1174 CORRODED L28R TO L28L. REPAIRED PER ERA 489831-14.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

LONGERON 29R AT STA 1320 CORRODED. REMOVED AND REPLACED IAW SRM.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

STA 1288 +7 L30 CORRODED. REMOVED AND REPLACED SPLICE IAW 5310.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

FWD CARGO L30 CORRODED. REMOVED AND REPLACED STA 209-229 53-10-01,

Part: LONGERON — CORRODED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

STA 1344 LONG 27R CORRODED. REPAIRED IAW SRM 5310.

Part: STRAP — CRACKED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

DOUBLER UNDER CANTED BLKHD STA 1520 CRACKED BETWEEN 1 AND L1. REPAIRED DORSAL EXTERNAL ANGLE IAW ERA 488954-14 ORIG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 30,355 hrs · 21,721 cycles

FWD CARGO R CARGO TRACK CORRODED STA 522 TO 427. REPAIRED IAW SRM 53-40-01 VOL I FIG 7.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

DOUBLER CORRODED UNDER BODY WEAR STRIP STA 1136-1174 28R AND 28L. REPAIRED IAW ERA 489831-14 ORIG.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

STA 1250-1260 LONGERON SPLICE L30 CORRODED. REMOVED AND REPLACED SPICE IAW SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 30,355 hrs · 21,721 cycles

MID CARGO STA 579-598 TRACK CORRODED. REPAIRED IAW SRM 53-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

SEAT TRACK CORRODED FROM 233 TO 236 RT I/B. REMOVED AND REPLACED RT I/B SEAT TRACK FROM 196 TO 256+9 IAW SRM 53-40-01 VOL I AN DRAWING 5930547.

Part: SKATE ANGLE — CRACKED (VERTICAL STAB) · airframe 30,355 hrs · 21,721 cycles

VERT STAB SKATE ANGLE CRACKED AFT 2 I/B HOLES. REPAIRED IAW ERA 488954-14.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

FWD CARGO PIT LONGERON 30 IS CORRODED STA 229. REPLACED DAMAGE SECTION IAW SRM 53-10-01 VIL I FIG 7.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

CENTER CARGO LONGERON 30 STA 842 CORRODED AT FASTENERS. REPAIRED IAW ERA 489821-14 ORIG.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

LONGERON 30 SPICE CORRODED STA 484-503. REMOVED AND REPLACED SPICE IAW SRM 5300.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

LONGERON 30 CORRODED AT SPLICE. REMOVED AND REPLACED LONGERON PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

FWD CARGO LONGERON SPLICE 29R STA 229 CORRODED. REMOVED AND REPLACED LONGERON SPICE 29R AT STA 229.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,355 hrs · 21,721 cycles

STA 237-256 SKIN CORRODED L28-29 TCAS ANTENNA DOUBLER. REPAIRED PER ERA 491199-14

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 30,336 hrs · 21,711 cycles

HMV2 SHEAR TIE STA 1269 L30-L29R CORRODED. REPLACED SHEAR TIE PER SRM 51-30-02

Part: LONGERON — CORRODED (FUSELAGE) · airframe 30,336 hrs · 21,711 cycles

HMV2 L29L LONGERON CORRODED STA 1395. REPLACED LONGERON PER SRM 51-30-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 30,336 hrs · 21,711 cycles

HMV2 L29R FITTING CORRODED STA 1395. REPLACED FITTING PER SRM 51-10-05.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 30,336 hrs · 21,711 cycles

HMV2 MID CARGO STA 532-865 LT CARGO TRACK CORRODED. REPLACED TRACK PER SRM 53-40-01.

Part: RUB STRIP — CORRODED (LT WING) · airframe 30,336 hrs · 21,711 cycles

HMV2 UPPER FUEL PANEL CUT OUT NR 520 FT HAS SURFACE CORROSION ON EXTERIOR RIM. REPLACED RUB STRIP PER 57-10-05.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 30,336 hrs · 21,711 cycles

HMV2 MID CARGO STA 750 FLOOR SUPPORT ANGLE CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-30-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 30,336 hrs · 21,711 cycles

HMV2 MID CARGO DOOR CUT OUT LWR AFT CORNER FITTING CORRODED. REPLACED FITTING PER SRM 51-10-04.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 30,336 hrs · 21,711 cycles

HMV2 AFT PRESS BULK HEAD CORROSION ON L28R. REPLACED L28R PER SRM 51-30-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,336 hrs · 21,711 cycles

HMV2 FWD CARGO COMP BS 332 LONGERON28L-28R FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-30-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,336 hrs · 21,711 cycles

HMV2 AFT CARGO FLOOR SUPPORT STA 1212-1269 ABOVE L29R CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-30-01.

Part: RUB STRIP — CORRODED (LT WING) · airframe 30,336 hrs · 21,711 cycles

HMV2 LT WING UPPER FUEL PANEL CUT OUT NR 520AT HAS SURFACE CORROSION ON EXTERNAL RIM. REPLACED RUB STRIP PER SRM 57-10-05.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,336 hrs · 21,711 cycles

HMV2 AFT AIRSTAIR AT STA 1520 BULKHEAD BETWEEN LONGERONS 2L-2R CRACKED. REPAIR PER ERA487592-14 REV ORIG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 30,336 hrs · 21,711 cycles

HMV2 FWD CARGO Z ANGLE CORRODED STA 427-446. REPLACED Z ANGLE PER SRM 53-40-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,336 hrs · 21,711 cycles

HMV2 FWD CARGO FLOOR SUPPORT CORRODED STA 427-465. REPLACED Z ANGLE PER SRM 53-40-01.

Part: SKIN — CORRODED (AFT CARGO DOOR) · airframe 25,496 hrs · 17,852 cycles

CORROSION ON Y1193-Y1269 L28 RT OF AFT CARGO DOOR SRM 53-60-02 VOL I FIG 9.

Part: PAN — CORRODED (FWD CARGO DOOR) · airframe 25,496 hrs · 17,852 cycles

FORWARD CARGO DOOR JAMB PAN CORROSION REPAIR. REPAIRED PER MESSAGE 1-723032321-1/1-723032321-2.

Part: FORMER — CORRODED (FUSELAGE) · airframe 25,496 hrs · 17,852 cycles

CHINA EASTERN AIRLINES PERFORMED TASK CARD 65061155, CORROSION ON FORMER Y1288 L29-R29 OF AFT CARGO COMPARTMENT SRM 53-10-03 VOL III, FIG 1 SRM 53-10-02 VOL I FIG 3.

Part: BEAM — CORRODED (AFT CARGO DOOR) · airframe 25,496 hrs · 17,852 cycles

CORROSION ON PLATE BETWEEN Y1212-Y1269 OF AFT CARGO DOOR BEAM SRM 53-60-02 VOL I FIG 9.

Part: FORMER — CORRODED (FUSELAGE) · airframe 25,496 hrs · 17,852 cycles

CHINA EASTERN AIRLINES PERFORMED TASK CARD 65061150, CORROSION ON FORMER Y1269 L29-R29 OF AFT CARGO COMPARTMENT SRM 53-10-03 VOL III, FIG 1 SRM 53-10-02 VOL I FIG 3.

Part: SKIN — CORRODED (MID CARGO DOOR) · airframe 25,496 hrs · 17,852 cycles

CORROSION ON Y693-Y750 L28 RT OF MID CARGO DOOR SRM 53-60-02 VOL I, FIG 9.

Part: FORMER — CORRODED (FUSELAGE) · airframe 25,496 hrs · 17,852 cycles

CHINA EASTER AIRLINES PERFORMED TASK CARD 65061153, CORROSION ON FORMER Y1212 L29-R29 OF AFT CARGO COMPARTMENT SRM 53-10-03 VOL III, FIG 1 SRM 53-10-02 VOL I FIG 3.

Part: PAN — CRACKED (LT MLG DOOR) · airframe 25,496 hrs · 17,852 cycles

LEFT MAIN LANDING GEAR DOOR PAN CRACK REPAIR. REPAIRED PER BOEING MESSAGE 1-691375741-2.

Part: SKIN — DENTED (RT SLAT) · airframe 24,807 hrs · 17,409 cycles

CSTA XIS=12.290 OF RT NR 0 SLAT DENT REPAIR. REPAIRED PER MESSAGE 1-432640761-3.