N982DL

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 68,197 hrs · 49,190 cycles

LEFT ENGINE ANTI-ICE VALVE CIRCUIT BREAKER TRIPPED WITH ODOR AND SMALL AMOUNT OF SMOKE. DISCONNECTED THE VALVES FROM B1-43, MEGGED WIRES FROM B1-43 TO PL809. ALL GOOD IAW WDM 75-11-00. REPLACED THE CIRCUIT BREAKER B1-43. FOUND COWL ANTI ICE VALVE BAD.

Part: LIFE RAFT — LOW PRESSURE (CABIN) · airframe 68,043 hrs · 49,082 cycles

FWD LT LIFE RAFT PRESSURE LESS THAN 3000PSI. REMOVED AND REPLACED LIFE RAFT ASSY PER AMM 25-62-02.

Part: LANYARD — NO TEST (TAILCONE SLIDE) · airframe 68,043 hrs · 49,082 cycles

TAILCONE SLIDE LANYARD FAILS SNAP PULL TEST. REPLACED THE LANYARD. A CCOMPLISHED A PULL TEST IAW AMDS 5350-4644.

Part: SLIDE — CRACKED (SERVICE DOOR) · airframe 68,043 hrs · 49,082 cycles

AFT SERVICE DOOR SLIDE IS CRACKED. REPLACED THE SLIDE WILL BE ACCOMPLISHED ON AMDS CARD 2561-4002.

Part: ATTACH FITTING — CRACKED (LT WING) · airframe 68,043 hrs · 49,082 cycles

LEFT WING GROUND SPOILER ACTUATOR ATTACH FITTING CRACKED AT INBOARD FORWARD CORNER. REPLACED SPOILER ATTACH FITTING IAW DWG 5936832, AND SRM 51-30-00.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 67,164 hrs · 48,449 cycles

ROW 23DE SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. FOUND A WIRE BROKEN AT SEAT CONNECTOR. TERMINATED THE CONTACT PIN IAW SWPM 20-90-03. CHECKED GOOD.

Part: SLIDE — NOT REPORTED (TAILCONE) · airframe 66,773 hrs · 48,163 cycles

TAIL SLIDE UNSERVICEABLE. REMOVED AND REPLACED TAILCONE SLIDE IAW AMDS 2561-4001.

Part: NUT — LOOSE (AXLE) · airframe 66,137 hrs · 47,675 cycles

CREW REPORTED THAT THE AIRCRAFT WAS SHAKING VIOLENTLY WHEN BRAKES WERE APPLIED MAKING IT DIFFICULT TO STOP. MAINTENANCE FOUND AXLE NUTS ABOUT 1/2 TURN LOOSE. TORQUED ALL MAIN AXLE NUTS. NO FURTHER ISSUES NOTED.

Part: CONTROL UNIT — MALFUNCTIONED (ANTI SKID SYS) · airframe 65,779 hrs · 47,420 cycles

RT OTBD ANTI-SKID MESSAGE WHEN GEAR LOWERED. EMERGENCY WAS DECLARED IAW MCC NOTIFICATION. THE ANTISKID CONTROL UNIT WAS REPLACED WITH SUCCESSFUL CHECK OUTS.

Part: VANE — DAMAGED (LT WING TE FLAP) · airframe 65,254 hrs · 47,029 cycles

LEFT INBD FLAP OTBD FIXED VANE HAS DAMAGE BEYOND SRM LIMITS. REPLACED FLAP FIXED VANE IAW AMM 27-51. OPERATION OF FLAP AND VANE CKS GOOD.

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 64,822 hrs · 46,736 cycles

CREW DISCOVERED THAT A LED FLOOR PROXIMITY LIGHT IN THE GALLEY WAS INOPERATIVE. MAINTENANCE R & R THE LIGHT ASSEMBLY AND THE LIGHT CHECKED OK.

Part: HYDRAULIC SYSTEM — LEAKING (APU BAY) · airframe 64,255 hrs · 46,353 cycles

DURING CLIMB BOTH AFT LAVATORY SMOKE DETECTORS ALERTED AND F/A REPORTED SMELLING AND SEEING SMOKE. AFTER 1 MINUTE THE SMOKE DETECTORS SILENCED AND THE SMOKE DISSIPATED. CREW ELECTED TO RETURN TO DEPARTURE. MAINTENANCE FOUND HYDRAULIC FLUID DRIPPING FROM DRAIN JUST FORWARD OF APU INLET AND CONTAMINATING THE APU. SOURCE OF LEAK WAS FOUND TO BE THE RT MLG RETRACT ACTUATOR AND THE AFT AIR STAIR ACTUATOR. REPLACED BOTH ACTUATORS AND ACCOMPLISHED A MINI-DUCT BURNOUT.

Part: CUSP WEB — CORRODED (BS 1208-1249) · corrosion level 2 · airframe 66,783 hrs · 48,172 cycles

CABIN BS 1208 - 1249 LBL 60 CUSP WEB UPPER AND LWR SURFACES HAS AREAS OF CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW ER/A 511165-14MA REV B. REPLACED THE CUSP WEB IAW SRM 51-30-01 AND SRM 51-30-02.

Part: FLOOR SUPPORT — CORRODED (BS 160-195) · corrosion level 2 · airframe 66,783 hrs · 48,172 cycles

FLOOR SUPPORT CORRODED ON UPPER SURFACE BS 160 TO 195. REMOVE CORROSION. REPLACED THE FLOOR SUPPORT IAW SRM 51-20-0 AND 51-30-01.

Part: SKIN — CORRODED (BS 288) · corrosion level 2 · airframe 66,783 hrs · 48,172 cycles

UPON REMOVAL OF ANTENNA ON LOWER FUSELAGE AT BS 288, FOUND THE FUSELAGE SKIN UNDER ANTENNA TO BE CORRODED. REMOVED CORROSION, STRINGERS 29 AND 30L. FOUND TO BE OUT OF LIMITS IAW SRM 53-01-1 PAR D CONDITION 2. REPAIRED IAW ER/A 535864-14 REV ORIG. SECTION 1.

Part: CUSP WEB — CORRODED (BS 946-965) · corrosion level 2 · airframe 63,132 hrs · 45,567 cycles

CORROSION ON MAIN CABIN RT FLOOR CUSP WEB BETWEEN BS 946 - 965, RBL 58 ACCOMPLISHED ERA 534456-14, REV ORIGINAL SECTION 1 PERMANENT REPAIR ON MAIN CABIN RT FLOOR CUSP WEB.

Part: CUSP WEB — CORRODED (BS 1193-1212) · corrosion level 2 · airframe 66,783 hrs · 48,172 cycles

CUSP WEB BS 1193 - 1212, X -54 CORRODED. REPAIRED PER ER/A 534449-14.

Part: CUSP WEB — CORRODED (BS 864-886) · corrosion level 2 · airframe 63,132 hrs · 45,567 cycles

RT FWD OVERWING EXIT AREA BETWEEN BS 864 - 886 CUSP WEB HAS CORROSION AT SECOND LIGHTING HOLE. ACCOMPLISHED ERA 534456-14, REV ORIGINAL SECTION 1.

Part: CUSP WEB — CORRODED (BS 927-946) · corrosion level 2 · airframe 63,132 hrs · 45,567 cycles

CORROSION ON MAIN CABIN RT FLOOR CUSP WEB BETWEEN BS 927 - 946, RBL 58. ACCOMPLISHED ERA 534456-14, REV ORIGINAL SECTION 1 PERMANENT REPAIR ON MAIN CABIN RT FLOOR CUSP WEB BETWEEN FS 864 AND FS 965, RBL 58.

Part: CUSP WEB — CORRODED (BS 886-905) · corrosion level 2 · airframe 63,132 hrs · 45,567 cycles

RT FWD OVERWING EXIT AREA. BETWEEN BS 886-905 CUSP WEB HAS CORROSION AT SECOND LIGHTING HOLE. ACCOMPLISHED ERA 534456-14, REV ORIGINAL SECTION 1.

Part: LONGERON — CORRODED (BS 1337) · airframe 63,132 hrs · 45,567 cycles

CORROSION ON LONGERON 18L BS 1337. FOUND OUT OF LIMITS. CUT-OUT SECTION OF LONGERON AND REPAIRED IAW ERA 534442-14, REV ORIGINAL SECTION I.

Part: ANGLE — CORRODED (BS 198) · corrosion level 2 · airframe 63,132 hrs · 45,567 cycles

CORROSION ON R1 DOOR CUTOUT LOWER AFT WEB BS 198. RT UPPER ANGLE WAS FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE SECTION OF RT UPPER ANGLE AND INSTALLED A REPAIR IAW SRM 53-05, FIG 55 AND ERA 521188-14, REV ORIGINAL SECTION I.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,776 hrs · 48,166 cycles

AFT CARGO COMPT, CORROSION ON FWD & AFT SIDE OF T-SHAPED SHEAR TIE ATTACHED TO LOWER FRAME AT STA 1231, BETWEEN STR 26R & 27R. CORROSION OUT OF LIMITS IAW SRM 53-01 FIG 1 PG 8 ORIGINAL THICKNESS IS .063" MATERIAL LOSS L= 1.0",W= .50", D= .063". REPLACED AFT CARGO T-SHAPED SHEAR TIE ATTACHED TO LOWER FRAME AT STA 1231 BETWEEN STR 26R AND 27R IAW SRM 51-30-2.

Part: SKIN — DAMAGED (BS 236) · airframe 63,132 hrs · 45,567 cycles

FUSELAGE SKIN, BS 236, S-17L & S-18L DENTED AND GOUGED. REPAIRED IAW ERA 534432-14.

Part: CUSP WEB — CORRODED (BS 702-712) · corrosion level 2 · airframe 66,776 hrs · 48,166 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 702 AND 712, RBL 58. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW ER/A 511165-14MA REV B ORIG L . REPLACED THE CUSP WEB IAW SRM 51-30-1 PG 1.

Part: WEB — CORRODED (BS 826-845) · corrosion level 2 · airframe 66,776 hrs · 48,166 cycles

RIGHT CREASE BEAM WEB UPPER AND LOWER SURFACE HAS CORROSION INCLUDING LOWER SURFACE SECTION BETWEEN BS 826 AND 845. CUT OUT DAMAGE AREA IAW SRM 53-05 FIG 131A-1 HFEC PER NDTSPM 06-10-01.001 NO CRACKS NOTED, FABRICATED, LOCATED, AND INSTALLED ALL REPAIR IAW SRM 53-05 FIG 131A-1.

Part: LONGERON — CRACKED (BS 1240) · corrosion level 2 · airframe 63,132 hrs · 45,567 cycles

CORROSION ON LONGERON 22R APPROXIMATELY STA 1240 AFT CARGO. REMOVED CORROSION AT LONGERON, 22R FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1, CUT OUT DAMAGE SECTION AT LONGERON, 22R STA 1241-1260 IAW SRM 53-02, FIG 18. LP 1931285.

Part: FLOOR SUPPORT — CORRODED (BS 195-199) · corrosion level 2 · airframe 66,776 hrs · 48,166 cycles

CORROSION ON MAIN CABIN FLOOR SUPPORT BETWEEN BS 195-199, RBL-53. REPLACED THE FLOOR SUPPORT IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 66,776 hrs · 48,166 cycles

CORROSION ON MAIN CABIN FLOORBEAM BS 200 RBL 46 TO 49. REPLACED FLOORBEAM IAW SRM 51-30-2 .

Part: CUSP WEB — CORRODED (BS 1231-1250) · corrosion level 2 · airframe 66,776 hrs · 48,166 cycles

CUSP WEB CORRODED BETWEEN BS 1231 AND 1250 RBL 59. FOUND TO BE OUT OF LIMITS IAW ER/A 511165-14MA REV B. FABRICATED, LOCATED, DRILLED, AND INSTALLED A REPAIR IAW SRM 53-05 FIG 131A-1.

Part: CUSP WEB — CORRODED (BS 1250) · corrosion level 2 · airframe 66,776 hrs · 48,166 cycles

CABIN BS 1250 LBL 46-60 CUSP WEB CORRODED. REMOVED CORROSION IAW SRM 51-30-01 AND ER/A 511165-14MA REV B HFEC PER NDTSPM 06-10-01.001 NO CRACKS NOTED. FOUND TO BE OUT OF LIMITS IAW ER/A 5116-14MA REV B FABRICATED, LOCATED, AND INSTALLED REPAIR IAW SRM 53-05 FIG 131A-1.

Part: WEB — CORRODED (BS 200) · corrosion level 2 · airframe 66,776 hrs · 48,166 cycles

CORROSION ON MAIN CABIN SUB FLOOR WEB AT BS 200 RBL 56. THE WEB WAS FOUND OUT OF LIMITS IAW SRM 53-01 FIG 1, REMOVED, FABRICATED, AND INSTALLED A NEW WEB IAW SRM 53-14-1, SRM 51-30-8.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 66,823 hrs · 48,205 cycles

CORROSION ON MAIN CABIN RT FLOOR CUSP WEB AT STA 651, RBL 58. WEB REPLACED.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 66,823 hrs · 48,205 cycles

CABIN STA 298 LBL 60 CUSP WEB LWR SKIN HAS CORROSION. REPAIRED CUSP WEB.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 66,823 hrs · 48,205 cycles

CORROSION ON MAIN CABIN RT FLOOR CUSP WEB BETWEEN STA 674 AND 693, RBL 58. REPLACED WEB.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 66,823 hrs · 48,205 cycles

CORROSION ON MAIN CABIN RT FLOOR CUSP WEB BETWEEN STA 541 AND STA 560, RBL 58. REMOVED CORROSION ON MAIN CABIN CUSP WEB AT STA 541 RBL 58 AND STA 560 RBL 58 PER ERA.

Part: LONGERON SPLICE — DAMAGED (BS 1401-1418) · airframe 63,132 hrs · 45,567 cycles

TAIL COMPARTMENT FS1401-1418 L8R LONGERON SPLICE GOUGED RECURRING DAMAGE, PREVIOUS REWORK AREA. REMOVED SPLICE, FABRICATED, AND REPLACED IAW DAC SRM 51-30-1, PAR 6 , 53-02, FIG 18.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,823 hrs · 48,205 cycles

CORROSION ON FUSELAGE FRAME AT AFT CARGO COMPARTMENT STA 1250, BETWEEN LONGERON 28R AND 28L. REMOVED FRAME AND INSTALLED NEW FRAME.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 66,823 hrs · 48,205 cycles

CABIN STA 1136-1178 LBL 46-53 CUSP WEB UPPER SKIN HAS CORROSION AND CHAFING. FABRICATED AND INSTALLED REPAIR PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 66,884 hrs · 48,251 cycles

CORROSION ON A CABIN FLOOR SUPPORT AT STA 200 RBL-20 AND RBL-36 AND 1EA ELONGATED HOLE AT RBL-15. REMOVED AND REPLACED FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 66,884 hrs · 48,251 cycles

CORROSION ON MAIN CABIN FLOOR SUPPORT BETWEEN STA 148 - 200 LBL-7. REMOVED AND REPLACED FLOOR SUPPORT BETWEEN STA 148-200 LBL 7.

Part: FLOOR SUPPORT — CORRODED (BS 186-194) · airframe 66,884 hrs · 48,251 cycles

FLOOR SUPPORT HAS CORROSION AROUND ATTACH TAB ON UPPER SURFACE 8 INCHES INBD OF THE L1 DOOR THESHOLD, BS 186 - 194. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM.

Part: CUSP WEB — CORRODED (BS 1003-1022) · airframe 66,884 hrs · 48,251 cycles

CORROSION ON CUSP WEB, BS 1003 - 1022, RBL 58. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED THE CUSP WEB IAW SRM.

Part: FRAME — CORRODED (BS 1219) · airframe 66,884 hrs · 48,251 cycles

CORROSION ON FUSELAGE FRAME LOWER SECTION ATTACHED TO SKIN BS 1219 , BETWEEN LONGERONS 29L AND 29R. CORROSION OUT OF LIMITS. REMOVED AND REPLACED THE FRAME IAW SRM.

Part: CUSP WEB — CORRODED (BS 522-541) · airframe 66,884 hrs · 48,251 cycles

CORROSION ON MAIN CABIN CUSP WEB, BS 522 - 541, RBL 58. CORROSION OUT OF LIMITS. REPLACED THE CUSP WEB.

Part: CUSP WEB — CORRODED (BS 1179) · airframe 66,884 hrs · 48,251 cycles

CABIN BS 1179, LBL 50, CUSP WEB UPPER SKIN HAS CORROSION. CORROSION OUT OF LIMITS, CUSP WEB REPLACED.

Part: CUSP WEB — CORRODED (BS 597) · airframe 66,884 hrs · 48,251 cycles

CORROSION ON MAIN CABIN CUSP WEB BS 597, RBL 58. CORROSION OUT OF LIMITS. REPLACED THE CUSP WEB.

Part: CUSP WEB — CORRODED (BS 560-579) · airframe 66,884 hrs · 48,251 cycles

CORROSION ON MAIN CABIN CUSP WEB, BS 560 - 579 , RBL 58. CORROSION FOUND TO BE OUT OF LIMITS. REPLACED THE WEB CUSP.

Part: CUSP WEB — CORRODED (BS 484-503) · airframe 66,884 hrs · 48,251 cycles

CORROSION ON CUSP WEB BETWEEN BS 484 - 503 , RBL 58. REPAIRED THE CUSP WEB IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 148-200) · airframe 66,884 hrs · 48,251 cycles

CORROSION ON MAIN CABIN FLOOR SUPPORT BETWEEN BS 148 - 200, RBL 7. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM.

Part: CUSP WEB — CORRODED (BS 560-579) · airframe 66,884 hrs · 48,251 cycles

BS 560 - 579, LBL 60, WEB LOWER SKIN HAS CORROSION. REPAIRED THE CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (BS 475) · airframe 66,884 hrs · 48,251 cycles

CABIN BS 475 LBL 60 CUSP WEB LOWER SKIN HAS CORROSION. REPAIRED IAW SRM.

Part: CUSP WEB — CORRODED (BS 446-465) · airframe 66,884 hrs · 48,251 cycles

BS 446 - 465, LBL 60, CUSP WEB UPPER AND LOWER SKIN CORRODED. REPAIRED THE CUSP WEB IAW SRM.

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 63,132 hrs · 45,567 cycles

FORWARD CARGO BAY AFT JAMB IS CORRODED. CORROSION NOTED ON -21 REPAIR ANGLE , 0.013 MATERIAL LOSS IS OUT OF LIMITS AND WAS R & R PART AND INSTALLED IAW SRM 53-05, FIG 44. LP 1911442.

Part: CUSP WEB — CORRODED (BS 579-598) · corrosion level 2 · airframe 66,860 hrs · 48,234 cycles

CUSP WEB BS 579 - 598 LBL 60 HAS CORROSION. REPAIRED IAW SRM 53-05 , FIG 131A-13.

Part: LANYARD — FRAYED (L2 DOOR SLIDE) · airframe 62,444 hrs · 45,113 cycles

DURING CHECK, MAINTENANCE FOUND THE 2L DOOR SLIDE LANYARD TO BE FRAYED. MAINTENANCE R & R THE LANYARD.

Part: SKIN — UNKNOWN (AFT LAV PAN) · airframe 62,384 hrs · 45,075 cycles

SKIN, AFT LAV PAN SURROUND BS 1310 -1321 AND L-22L. REPAIRED IAW ERA 521818-14.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,906 hrs · 43,453 cycles

DURING CHECK, NOTED FUSELAGE SKIN BELOW AFT LAVATORY PANEL PILLOWED WITH CORROSION. REPAIRED IAW ER/A 521814-14.

Part: FRAME — CRACKED (UNKNOWN) · airframe 59,906 hrs · 43,453 cycles

CRACKED, LOCATION: AT 2 LOCATIONS AT 8 & 9 O`CLOCK POSITIONS M, RII: Y, REMOVED FRAME AND STARTED PICKING UP HOLES ON NEW FRAME. FRAME INSTALLED EXCEPT FOR, SLIDE ATTACH ANGLE, PN 9911843-5 WORK WITH CARD NR 67. INSTALLED ORIGINAL SERVICEABLE SLIDE ATTACH ANGLE IAW SRM 51-30.

Part: WEB — CRACKED (BS 1485) · airframe 59,906 hrs · 43,453 cycles

DURING CHECK, WEB CRACKED AT BS 1485. REPAIRED IAW ER/A 521787-14.

Part: FITTING — WORN (TAILCONE) · airframe 59,906 hrs · 43,453 cycles

DURING CHECK IN MSP, NOTED THE TAIL CONE RELEASE BAYONET FITTINGS WERE WORN INSIDE OF CASTING AND LOOSE ON FRAME STA 1510 AT 4:30 AND AT 7:30 POS. REPLACED TAILCONE LATCH ASSY AT STA1510 AT 4:30 AND 7:30 POSITIONS. REQUIRED INSPECTION COMPLETED.

Part: BEAM — CRACKED · airframe 59,906 hrs · 43,453 cycles

DURING C-CHECK, A CRACK WAS FOUND COMMON TO BEAM WHICH SEVERED 90 PERCENT OF THE BEAM CROSS SECTION. REPAIRED IAW ER/A 521795-14.

Part: DOOR — UNKNOWN (FWD, MID, AFT) · airframe 59,383 hrs · 43,094 cycles

FWD, MID, AFT CARGO DOORS REPAIRED IAW AA 5230-01159.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,918 hrs · 42,757 cycles

DURING ROUTINE LINE INSPECTION, THE SEAT MOUNTED EMERGENCY PATH LIGHT AT ROW 21D WAS NOTED TO BE INOPERATIVE. A SEAT CONNECTOR PLUG WAS REPLACED AND THE SYSTEM CHECKED NORMALLY.

Part: SIGN — MISSING (CABIN) · airframe 58,512 hrs · 42,501 cycles

DURING LINE CHECK, THE CEILING MOUNTED EXIT IDENTIFIER/SIGN WAS NOTED TO BE MISSING AT THE AFT LT DOOR POSITION. NEW INSERTS FOR THE ATTACH BRACKET WERE INSTALLED AND THE EXIT SIGN WAS REPLACED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,008 hrs · 42,183 cycles

DURING SERVICE CHECK, THE AFT OVER WING EMERGENCY EXIT SIGNS WERE FOUND TO BE INOPERATIVE. REPLACED AFT OVER WING EMERGENCY EXIT SIGN BATTERY PACKS IAW AMM 33-53 AND OPS CHECKED NORMALLY.

Part: SKIN — CRACKED (BS 1437) · airframe 56,185 hrs · 40,960 cycles

DURING PSV, THE RT CROWN FUSELAGE SKIN BS 1437 BETWEEN LONGERON 2R-3R JUST BELOW VERTICAL STAB ATTACH ANGLE WAS FOUND TO BE CRACKED WITH A 1 INCH DIAMETER CUTOUT REQUIRED TO REMOVE CRACK. REPAIR ACCOMPLISHED PER ERA 504954-14

Part: DEPRESSOR — CORRODED (FWD CARGO DOOR) · corrosion level 2 · airframe 56,185 hrs · 40,960 cycles

FOUND CORROSION FWD CARGO SEAL DEPRESSOR SPLICE AT BS 380. REMOVED AND REPLACED SPLICE PER DWG 5910142.

Part: SKIN — UNKNOWN (H.S. UPPER) · airframe 56,182 hrs · 40,959 cycles

HS UPPER CENTER SKIN PANEL REPAIRED IAW AA 5510-01086.

Part: LUG — UNKNOWN (HS HINGE) · airframe 56,182 hrs · 40,959 cycles

HS HINGE RIB PIVOT BEARING LUG REPAIRED IAW AA 5500-01011.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,520 hrs · 40,538 cycles

DURING LINE CHECK, MAINTENANCE FOUND BOTH OVERWING EMERGENCY EXIT SIGNS TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,189 hrs · 40,343 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY ESCAPE LIGHTING IN ROW 3CD WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPERATIONAL CHECK WAS GOOD.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 53,246 hrs · 39,104 cycles

DURING LINE CHECK, MX FOUND EMERGENCY ESCAPE PATHWAY LIGHTS INOPERATIVE FROM ROWS 24-30. MX FOUND WIRING HARNESS AT ROW 29E CHAFING AGAINST SEAT FRAME AND REPAIRED HARNESS IAW SWPM. ALSO REPLACED FUSE AT BATTERY PACK B5-211. OPS CHECKS GOOD. ACFT IS OK FOR SERVICE.

Part: FUSE — FAILED (EMERGENCY LIGHT) · airframe 53,200 hrs · 39,075 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATHWAY LIGHTS ROW 24-30 AND OVERWING EXIT LIGHTS INOPERATIVE. MAINTENANCE TROUBLESHOT AND FOUND OPEN FUSE AT BATTERY PACKS B5-211 AND B5-212. MAINTENANCE REMOVED AND REPLACE FUSE. OPERATION OF LIGHTS CHECKED OKAY.

Part: SPAR — CRACKED (WING) · airframe 53,049 hrs · 38,966 cycles

WING REAR SPAR CRACKING AT XRS 164. REPAIRED IAW AA 5710-01110.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,965 hrs · 38,911 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATH LIGHTS AT ROWS 24-30DE TO BE INOPERATIVE. MAINTENANCE FOUND BLOWN FUSE IN AFT CABIN BATTERY PACK AND BAD LIGHT ASSEMBLY AT 29DE. MAINTENANCE REPLACED FUSE AND LIGHT ASSEMBLY. LIGHTS AT ROW 24-30DE NOW OPERATE NORMALLY.

Part: HOUSING — UNKNOWN (NLG / HOUSING) · airframe 51,815 hrs · 38,220 cycles

NLG HOUSING ASSY REPAIRED IAW ERA 485660-14.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 51,800 hrs · 38,211 cycles

DURING LINE CHECK MX FOUND EMERGENCY PATH LIGHTS FROM ROW 24-30 INOPERATIVE. MX REPAIRED BROKEN WIRE AT SEAT 30D AND LIGHT HARNESS. ALSO REPLACED POWER SUPPLY B5-211. OPERATION OF LIGHTS NOW CHECK OK.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 51,201 hrs · 37,822 cycles

MX FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT 27DE TO BE INOPERATIVE. MX FOUND A BROKEN WIRE IN THE HARNESS AND REPLACED IT. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE. (DLM88101578)

Part: PLATE — CORRODED (WING) · corrosion level 2 · airframe 48,945 hrs · 36,398 cycles

FUEL TANK PLATE 1414 HAS LEVEL 2 CORROSION. PLATE REPLACED.

Part: PLATE — CORRODED (WING) · corrosion level 2 · airframe 48,945 hrs · 36,398 cycles

FUEL TANK PLATE 1436 HAS LEVEL 2 CORROSION. REPLACED PLATE IAW AMM 28.

Part: PULLEY BRACKET — CORRODED (SPOILER) · airframe 48,943 hrs · 36,396 cycles

RIGHT WING O/B SPOILER PULLEY BRACKET CORRODED LEVEL 2. REPLACED BRACKET IAW AMM 27-60-00-501.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

AFT CARGO FS 1212 LEFT LONGERON 29 TO RIGHT LONGERON 29 FRAME SUPPORT CORRODED. REPLACED SUPPORT IAW SRM 51-30-5.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

FWD CARGO UPPER JAMB AT CUTOUT FWD DOOR HINGE BRACKET ANGLE AT AFT SIDE HAS CORROSION. REPLACED ANGLE IAW SRM 51-30-5.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

AFT CARGO FS 1231 LONGERON 28 LEFT TO LONGERON 28 RIGHT FRAME SUPPORT CORRODED. REPLACED SUPPORT IAW 51-30-02.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

AFT CARGO FS 1155 FRAME SUPPORT LONGERON 28 LEFT TO 29 LEFT CORRODED. REPAIRED SUPPORT IAW SRM 53-03.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,943 hrs · 36,396 cycles

AFT CARGO FS 1174 LONGERON 25L HAS LEVEL 2 CORROSION. REPLACED LONGERON IAW 51-30-5.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

FS 1380 LONGERON 28R UPPER FRAME SUPPORT AT FWD INTERCOSTAL CRACKED. REPLACED IAW SRM 51-10-4, 51-30-2, 51-30-3, 51-10-2.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

FRAME SUPPORT AT FS 1250 LONG 18 LEFT CORRODED. REPLACED FRAME IAW 51-10-4.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

R1 DOOR THRESHOLD FLOOR PANEL HAS CORROSION. REPLACED PANEL IAW SRM 51-10-4.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

CUSP WEB CORRODED AT FS 712 AND 731 LEFT. REPAIRED IAW DRD 53-05D FIG 827D.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

FS 1117 ATTACH ANGLE HAS CORROSION. REPLACED ANGLE IAW SRM 51-30-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

AFT CARGO FLOOR SUPPORT CORRODED FS 1322 LONGERON 27 LEFT AND LONGERON 27 RIGHT. REPAIRED IAW SRM 53-01 FIG 1.

Part: CARGO TRACK — CORRODED (CARGO TRACK) · airframe 48,943 hrs · 36,396 cycles

AFT CARGO FS 1222-1322 LEFT SIDE TIE DOWN TRACK LEVEL 2 CORROSION. REMOVED AND REPLACED TRACK IAW SRM 51-10-04.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

AFT CARGO STA 1147 BETWEEN LT LONG 29 AND RT LONG 29, FRAME SUPPORT HAS CORROSION ON FWD AND AFT SIDE (TASK 57-53301). FRAME SUPPORT CORROSION IS OUT OF LIMITS. REPLACED SUPPORT ON NRC M00/101 1758N01492.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

CUSP WEB FS 826-845 LEFT SIDE CONTAINS LEVEL 2 CORROSION. REPAIRED IAW ER/A 398191-14MA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

AFT CARGO STA 1147, BETWEEN LEFT LONGERON 29 AND RIGHT LONGERON 29, FRAME SUPPORT HAS CORROSION ON FWD AND AFT SIDE (TASK 57-53301). FRAME SUPPORT CORROSION OUT OF LIMITS. REPLACED FRAME SUPPORT ON NRC M00/101 1758N01492.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 48,943 hrs · 36,396 cycles

SEAT TRACK FS 218-389 RBL 52 LEVEL 2 CORROSION. REPAIRED IAW ER/A 398191-14MA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

AFT CARGO INTERCOSTAL AT FS 1212 AND 1220 RT LONG 29 AND 30 CORRODED. REPAIRED IAW DAC DRE 5936071 AND SRM 51-10-03.

Part: PLATE — CORRODED (FUEL TANK) · airframe 48,943 hrs · 36,396 cycles

FUEL TANK PLATE 1460 HAS CORROSION ON MATING SURFACES. REPLACED PANEL IAW AMM 28-00-00.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

AFT CARGO, BETWEEN STA 1212 AND 1220, RIGHT LONGERON 29 AND 30, INTERCOSTAL HAS CORROSION (CPCP 57-533011). REMOVED AND REPLACED WITH NEW ANGLE.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

AFT CARGO LONGERON 30 FS 1308 CORRODED. REMOVED AND REPLACED SPLICE PER SRM 51-10-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

SEAT TRACK FS 236 TO 370 CORRODED. REPLACED SEAT TRACK IAW 51-30-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

CUSP WEB FS 256 RBL 46 CONTAINS LEVEL 2 CORROSION. REPAIRED IAW SRM 53-05D.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

RIGHT CUSP WEB HAS CORROSION BETWEEN FS 590 AND 579. REPAIRED IAW ER/A 398191-14MA.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

CUSP WEB AT FS 731-750 RIGHT CONTAINS LEVEL 2 CORROSION. REPAIRED IAW SRM 53-05D.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 48,943 hrs · 36,396 cycles

CUSP WEB AT FS 712-721 RIGHT CONTAINS LEVEL 2 CORROSION. REPAIRED IAW SRM 53-05D.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,943 hrs · 36,396 cycles

CUSP WEB AT FS 655-674 RIGHT HAS LEVEL 2 CORROSION. REPAIRED IAW ER/A 318191-14 MA.

Part: BOTTLE — FULL (RT MLG WW) · airframe 42,090 hrs · 32,051 cycles

F/A REPORTED SMOKE/SMELL IN AFT CABIN AFTER TAKEOFF. FOUND OVERFLOW BOTTLE IN RT WHEEL WELL OVERFLOWING AND SKYDROL STREAKED DOWN BELLY TO THE APU INLET. CLEANED SKYDROL FROM WHEEL WELL, BELLY AND APU INLET. PERFORMED DUCT BURNOUT. REPLACED BAGS. OK FOR SERVICE.

Part: RELAY — FAILED (TRIM SYSTEM) · airframe 37,870 hrs · 29,068 cycles

AFTER T/O HIGH SPEED TRIM MOTORS WOULD NOT WORK ON BOTH YOKES, ALSO SLOW SPEED TRIM INTERMITTENT. AUTO-PILOT TRIM ALSO WOULD NOT WORK. REPLACED BRAKE RELAY.

Part: GENERATOR — FAILED (NR 2 ENGINE) · airframe 35,113 hrs · 27,113 cycles

DURING T/O RIGHT GENERATOR FAILED, ACCOMPANIED BY AC CROSSTIE LOCKOUT. REPLACED RT GENERATOR AND CSD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 29,360 hrs · 23,041 cycles

ON INSPECTION FOUND EMERGENCY FLASHLIGHT ABOVE F/C FLIGHT ATTENDANT SEAT NOT TESTING. REPLACED BATTERY PACK PER MM, OPN OF FLASHER NORMAL. REPLACED STRAP.

Part: LANYARD — BROKEN (L1 DOOR)

AT DEPARTURE TIME, F/A FOUND LANYARD BROKEN ON L-1 DOOR SLIDE GIRT BAR. REPLACED LANYARD ASSY.

Part: SKIN — DENTED (BS 237)

FUSELAGE SKIN FOUND DENTED AT APPROX FS 237 ABOVE L17L. REPAIRED PER ERA 331137-14.

Part: SKIN — CORRODED (BS 774)

CORROSION WAS FOUND ON THE FUSELAGE SKIN UNDER THE RT RUB STRIP AT 2 LOCATIONS; APPROX. FS771 AND FS775, NEAR L28R. REPAIRED PER ERA 331145-14.

Part: SKIN — DENTED (BS 237)

FUSELAGE SKIN DENTED AT FS237 BETWEEN L18L AND L19L. REPAIRED PER ERA 331131-14.

Part: SKIN — DENTED (BS 219)

FUSELAGE SKIN DENTED AT FS 219 BETWEEN L18L AND L19L. REPAIRED PER ERA 331133-14.

Part: FRAME — CRACKED (BS 1418)

FS 1418 FOUND CRACKED AT L2R. TYPICAL LOCATION FOR EARLIER AC BUT FACTORY/PRODUCTION MOD WAS TO PREVENT PROBLEM. WILL REPAIR SAME WAY AS REPAIR FOR EARLIER AC. REPAIR PER ERA 331142-14.

Part: BALLAST — FAILED (CABIN)

STRONG ELECTRICAL SMELL THROUGH OUT ALL OF A/C AFTER T/O. PAX AT 26D REPORTED SMOKE FROM CEILING SIDEWALL AREA IN FRONT OF HIM. FOUND BALLAST AT 21DE INOP. INSP AREA AND REPLACED BALLAST. OPERATED ALL FANS AND FOUND CABIN RECIRC FAN INOP. FWD TO MCO/PLAC PER MEL 21-00-43. CKD PWR AND FOUND OPEN SUSP DIODE R7-91.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY FLOOR TRACK LIGHT WOULD NOT TEST. REPLACED FWD POWER SUPPLY AND AFT BATTERY PACK, CKS GOOD.

Part: APU — FAILED (APU COMP)

AFTER T/O CREW REPORTED, SMOKE IN CABIN WITH A VERY BAD ODOR. FLT RETURNED TO COS. FOUND OIL LEAKING FROM APU CHIP DETECTOR. OIL BEING INJECTED INTO THE INTAKE. REPLACED CHIP DETECTOR.

Part: LINE — NOT SECURED (TAIL COMPARTMENT)

LOSS OF RIGHT HYDRAULIC SYSTEM IN-FLIGHT. GEAR EXTENSION HANDLE NOT STOWED AT GATE. FOUND LOOSE B-NUT ON RIGHT ENGINE HYDRAULIC PUMP PRESSURE LINE INSIDE TAIL COMPARTMENT JUST INBOARD OF PYLON. TIGHTENED SAME. RAN ENGINES - LEAK CHECKS GOOD. SERVICED HYDRAULICS.

Part: STRUT — REQD SERVICE (NLG)

ON TAKEOFF, GEAR RETRACTION LANDING GEAR LIGHTS INDICATED AN UNSAFE NOSE GEAR. EXTENDED GEAR, GOT THREE DOWN AND LOCKED. RETURNED TO AIRPORT. LOUD NOISE ACCOMPANIED UNSAFE INDICATION AS THOUGH GEAR DOOR NOT CLOSED. SWUNG NOSE GEAR. ALL INDICATION IS GOOD. FOUND NOSE STRUT PNEUMATIC CHRG UNDERSERVICED. VERIFIED PROPER FLUID LEVEL. SERVICED PNEUMATIC CHRG PROPERLY. RAN STRUT ENTIRE LENGTH SEVERAL TIMES. SWUNG GEAR. RETURNED TO SERVICE.

Part: STRUT — REQD SERVICE (NLG)

NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED DFW. C/A - FOUND NOSE GEAR FROZEN WITH WATER IN STRUT. DRAINED AND RESERVICED. SWUNG GEAR, OPERATION NORMAL.

Part: CLIP — CRACKED (KEEL BEAM)

FOUND DURING D-2 LETTER CHECK - KEEL BEAM AFT CROSSOVER RIB ATTACH CLIP CRACKED. REPAIRED PER SRM 53-05, FIG 101.

Part: WINDSHIELD — CRACKED (FLIGHT DECK)

DURING CRUISE, CAPTAIN'S L-1 WINDSHIELD OVERHEATED AND CRACKED. LANDED BOS. REPLACED WINDSHIELD AND CONTROLLER OPERATION NORMAL.