N919DL

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,027 hrs · 57,646 cycles

EMERGENCY LIGHTS OVERWING INOPERATIVE. R & R THE BATTERIES IN B5105 IAW AMM 33-53. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,485 hrs · 57,188 cycles

BOTH FWD OVERWING LIGHTED EXIT SIGNS INOPERATIVE. . INSTALLED NEW BATTERIES IAW AMM 33-53-00/401. ALL CHECKED OK.

Part: CONNECTOR — FAILED (DISPLAY) · airframe 75,236 hrs · 56,993 cycles

DIVERTED DUE TO NR 1 ENGINE OIL PRESSURE HIGH. NR 1 THROTTLE AT IDLE WITH OIL PRESSURE IN RANGE. MAINTENANCE REPLACED THE SYSTEMS DISPLAY PANEL, PLUG P1-813, OIL PRESSURE TRANSMITTER. TAKEOFF POWER RUNS CONFIRMED OIL PRESSURE NOW NORMAL.

Part: DOOR FRAME — CORRODED (BS 1154-1211) · corrosion level 2 · airframe 75,188 hrs · 56,961 cycles

CORROSION ON THE LOWER DOOR FRAME BEAM BS 1154 TO 1211. CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26, 21 AND 14. FOUNE WITHIN LIMITS IAW SRM 53-05, FIG 123, AND NDT SPM 04-00-07, FIG 3 PAR 5, SHEET 1-2.

Part: SPRING — FAILED (CAPTAIN'S SEAT) · airframe 74,243 hrs · 56,251 cycles

DURING TAKEOFF ROLL AND AFTER ROTATION, THE CAPTAIN'S SEAT ROLLED BACK TO THE FULL AFT POSITION. REPLACED LOCK RETURN SPRING.

Part: SPAR CAP — CRACKED (RT WING) · airframe 73,194 hrs · 55,462 cycles

RT WING REAR SPAR LOWER CAP PER W/C 5710-0110-05A SHOWS A CRACK INDICATION AT 6:30 POSITION TOTAL LENGTH OF CRACK TO BE DETERMINED AFTER DISASSEMBLY PER W/C 57-10-0110-05B. HFEC INSPECTION WAS ACCOMPLISHED ON RH WING REAR SPAR LOWER CAP ONE CRACK WAS FOUND (LENGTH 0.880 IN) PER W/C 5710-0110-05B EQUIPMENT PHASEC 3D C/N 1381 EXP: 20-OCT-16 AND THE REPAIR WAS PERFORMED PER AMDS CARD 5710-0110-06 BOEING DRAWING J060271-510 REV. T AND ER/A 550317-14 AD REV. ORIG. (LP8295892)

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 73,194 hrs · 55,462 cycles

CORROSION ON RIGHT HEATER BLANKET SKIN AROUND THE FUEL ACCESS 1410C. HEATER BLANKET PANEL WAS REPLACED AND SYSTEM OPS TEST WAS PERFORMED IAW AMM 30-80-02.

Part: SPAR CAP — CRACKED (RT WING) · airframe 73,194 hrs · 55,462 cycles

HFEC INSPECTION OF RT WING REAR SPAR LOWER CAP IAW W/C 5710-0110-05A SHOW A CRACK INDICATION AT 6:30 POSITION. REPAIRED IAW CARD 5710-01110-06, DRAWING J060271-510 REV. T, AND ER/A 550317-14 AD REV. ORG.

Part: ACCESS PANEL — PUNCTURED (LT WING) · airframe 73,194 hrs · 55,462 cycles

HIDDEN DAMAGE: PUNCTURE ON SECONDARY ACCESS COVER 3070-100, LT WING. SECONDARY ACCESS COVER NR 3070-100 AT LT WING WAS EVALUATED AND IT WAS FOUND OUT OF LIMITS, SECONDARY ACCESS COVER NR 3070-100 WAS REPLACED IAW ERA 530866-14AD MA, REV ORIGINAL.

Part: BEAM — CRACKED (FUSELAGE) · airframe 73,194 hrs · 55,462 cycles

INITIAL: CRACKED BEAM 1, FORWARD EDGE, APPROXIMATELY STA Y=172 AT FORWARD SERVICE DOOR. DAMAGED BEAM NR 1WAS REPLACED IAW SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 72,378 hrs · 54,859 cycles

EMERGENCY LIGHT OUT SEAT 29ED. RECONNECTED WIRE CLIP CONNECTOR AT ROW 29ED. OPS CHECKED GOOD. OK FOR SERVICE.

Part: PIN — BACKED OUT (L1 DOOR SLIDE) · airframe 71,502 hrs · 54,253 cycles

DURING INSPECTION, FOUND L1 DOOR SLIDE DEPLOYMENT PINS OUT. REPLACED 1L DOOR SLIDE AND COMPLIED WITH REQUIRED INSPECTIONS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,687 hrs · 52,955 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY CEILING LIGHTS FROM ROWS 23-25 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,293 hrs · 52,707 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT THE FORWARD OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: SLEEVE — WORN (TAILCONE RELEASE) · airframe 68,410 hrs · 52,112 cycles

MAINTENANCE DISCOVERED THAT THE KEVLAR SLEEVE OVER THE RELEASE CABLE FOR THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: FLOORBEAM — CORRODED (BS 427) · airframe 68,410 hrs · 52,112 cycles

CORROSION ON UPPER SURFACE FLOORBEAM AT BS 427 FWD CARGO BAY. REPLACED FLOORBEAM IAW SRM 51-30-2, 51-10-4.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,259 hrs · 51,295 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR THE AFT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,474 hrs · 49,352 cycles

DURING LINE MX CHECK, THE OVERWING EMERGENCY EXIT IDENTIFIER LIGHTS WERE FOUND TO BE INOPERATIVE. THE POWER SUPPLY BATTERIES WERE REPLACED AND THE EMERGENCY LIGHTS OPERATION CHECKED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,218 hrs · 49,193 cycles

FLIGHT DISCOVERED THAT THE EMERGENCY LIGHTS IN THE COCKPIT HAD BECOME INOPERATIVE. MX REPLACED THE ASSOCIATED BATTERY PACK AND THE LIGHTS RETURNED TO NORMAL OPERATION.

Part: STRUCTURE — STUCK (CATWALK) · airframe 63,407 hrs · 48,595 cycles

MX FOUND THE AFT STAIRWAY CATWALK BINDING IN THE HALF-WAY UP POSITION DURING TROUBLESHOOTING.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 62,813 hrs · 48,159 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 34D IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 62,139 hrs · 47,672 cycles

DURING HMV A CRACKED STOP FITTING WAS FOUND ON STA Y=636 AT BEAM NR 5 AND CRACKED PAN BELOW SAME STOP FITTING. AT MID CARGO COMPARTMENT DOOR CRACKED PAN WAS REPAIRED IAW MD88 SRM 52-05 FIG 50 AND THE STOP FITTING WAS REPLACED.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 62,139 hrs · 47,672 cycles

DURING HMV CORROSION WAS FOUND ON REPAIR DOUBLER STA Y=636-655 BETWEEN PROJECTION OF LONG 29RT AND 30 AT MID CARGO COMPARTMENT. CORROSION ON REPAIR DOUBLER STA Y=636-655. DOUBLER REPAIR INSTALLED IAW DC9/MD80 SRM 51-30-02 AND 51-30-05 AND ERA 455102-14 REV ORIG. REPLACE REPAIR DOUBLER IAW ERA 455102-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,139 hrs · 47,672 cycles

DURING HMV LIGHTNING STRIKES WERE FOUND ON WINDOWS BELT FRAMES SKIN AT UPPER AFT CORNER STA 461 AND 1094 AT FUSELAGE SKIN. DOUBLER REPAIR INSTALLED IAW ERA501075-14 REV.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,139 hrs · 47,672 cycles

DURING HMV CORROSION WAS FOUND ON EXTERNAL FUSELAGE SKIN FROM STA Y=731 TO Y=807 BETWEEN LONG 16RT AND 21RT. FUSELAGE SKIN WAS BLENDED OUT AND WITHIN LIMITS REF MD88 SRM 53-04 PARA 57.

Part: BEAM — CORRODED (FUSELAGE) · airframe 62,139 hrs · 47,672 cycles

DURING HMV CORROSION WAS FOUND ON AFT CARGO COMPARTMENT LWR DOORJAMB BEAM LWR CAP BTW STA Y=1155 TO Y=1212. BLEND OUT BEAM AND LESS THAN 25% REMOVED SO BEAM WAS REPAIRED IAW MD88 SRM 53-05 FIG 123 SHEET 2 SECTION C-C.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,139 hrs · 47,672 cycles

DURING HMV CORROSION WAS FOUND ON EXTERNAL FUSELAGE SKIN FROM STA Y=1060 TO Y=1131 BETWEEN LONGS 18LT AND 30 REF MD88 SRM 53-04D PARA 57 FOR REPAIR. BLENDED AREA, WITHIN LIMITS IAW DC9/MD80 SRM 53-04 PAR 57.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,139 hrs · 47,672 cycles

DURING HMV CORROSION WAS FOUND BELOW SETTLEMENT AREA OF RUBSTRIP FRON STA Y=726 TO Y=788 BETWEEN LONG 16RT TO 21RT. REF MD88 SRM 53-04D PARA 57 FOR REPAIR. BLENDED AREA WITHIN LIMITS IAW DC9/MD80 SRM 53-04 PAR 57.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,139 hrs · 47,672 cycles

DURING HMV CORROSION WAS FOUND BELOW SETTLEMENT AREA OF RUBSTRIP FROM STA Y=799 TO Y=830 BETWEEN LONG 26LT TO 30 REF MD88 SRM 53-04D PARA 57 FOR REPAIR. BLENDED ARE WITHIN LIMITS IAW DC9/MD80 SRM 53-04 PAR 57.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,139 hrs · 47,672 cycles

DURING HMV CORROSION WAS FOUND BELOW SETTLEMENT AREA OF RUB STRIP FROM STA Y=758 TO Y=830 BTW LONG 26RT TO 30RT REF MD88 SRM 53-04D PARA 57 FOR REPAIR. BLENDED AREA WITHIN LIMITS IAW SG 09530014 PAR 5A AND SRM 53-04 PAR 57.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,139 hrs · 47,672 cycles

DURING HMV CORROSION WAS FOUND BELOW SETTLEMENT AREA OF RUBSTRIP FROM STA Y=1071 TO Y=1136 BETWEEN LONG 20LT TO 30LT REF MD88 SRM 53-04D PARA 57 FOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,139 hrs · 47,672 cycles

DURING HMV CORROSION WAS FOUND BELOW SETTLEMENT AREA OF RUB STRIP FROM STA Y=995 TO Y=1032 LONG 18RT REF MD88 SRM 53-04D PARA 57 FOR REPAIR. BLENDED AREA WITHIN LIMITS IAW SG 09530014 PAR 5A AND DC9/MD80 SRM 53-04 PAR 57.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,139 hrs · 47,672 cycles

DURING HMV CORROSION WAS FOUND ON OUTER FUSELAGE SKIN AT RUBSTRIP AREA FROM STA Y=728 BTW LONGS 23RT TO 24RT AND STA Y=757-826 LONG 27RT TO 30 REF MD88 SRM 53-04D PARA 57 FOR REPAIR. BLENDED AREA WITHIN LIMITS, IAW SG 09530014 PAR 5A AND SRM 5-04 PAR 57.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,139 hrs · 47,672 cycles

DURING HMV CORROSION WAS FOUND BELOW SETTLEMENT AREA OF RUB STRIP FROM STA Y=1060 TO Y=1136 BETWEEN LONG 26RT TO 30 REF MD88 SRM 53-04D PARA 57 FOR REPAIR. BLENDED AREA WITHIN LIMITS IAW DC9/MD80 SRM 53-04 PAR 57.

Part: TEE FITTING — DAMAGED (FUSELAGE) · airframe 62,139 hrs · 47,672 cycles

DRILL MARKS WERE FOUND ON AFT PRESSURE BULKHEAD TEE LOWER SECTION STAY=1338 BTW PROJECTION OF LONGERON 29L-29R AT AFT CARGO COMPARTMENT REF MD 88 SRM 53-03 FIG 37 FOR REPAIR (NRC TO241646). NEW SECTION OF TEE AND REPAIR PARTS INSTALLED IAW DC9/MD88 SRM 53-03D FIG 37.

Part: PLATE — CORRODED (LT WING) · airframe 62,139 hrs · 47,672 cycles

DURING HMV CORROSION WAS FOUND BELOW SETTLEMENT RUB STRIP AREA ON FUEL ACCESS PLATE NBR 1335C UPPER LT WING WILL BE ATTENDED WITH AN ERA. CORR ON SETTLEMENT AREA FUEL ACCESS 1335C REPAIR ACCOMPLISHED IAW ERA 501079-14 REV ORIG.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 62,139 hrs · 47,672 cycles

DURING HMV LIGHTNING STRIKE WAS FOUND ON RT WINDOW BELT FRAME AT FWD UPPER CORNER BETWEEN STA Y=845 TO Y=864. LIGHTNING STRIKE RT WINDOW BELT FRAME. REPAIR PERFORMED IAW ERA 501072-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,139 hrs · 47,672 cycles

LIGHTNING STRIKES ON WINDOW BELT FRAME SKIN AT LWR AFT CORNER EDGE STA Y=479,888,742-745. LIGHTNING STRIKE TO WINDOW BELT STA 421, 479, 888, 742-745 BLENDOUT REWORK ACCOMPLISHED IAW ERA 501075-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,139 hrs · 47,672 cycles

LIGHTNING STRIKE ON LT WINDOW BELT FRAME SKIN AT AFT LWR EDGE STA Y=518 AT FUSELAGE SKIN. BLENDOUT REWORK ACCOMPLISHED IAW ERA 501075-14 REV ORIG.

Part: SPAR — CORRODED (HORIZ STAB) · airframe 62,139 hrs · 47,672 cycles

DURING HMV CORROSION WAS FOUND ON BARREL NUT HOLES NR 1 AND 4 FROM FWD SPAR TO REAR SPAR STA XH=27 RT HORIZONTAL STAB ERA WAS ISSUED FOR BARREL NUT HOLES CORROSION ON HORIZONTAL STAB BARREL NUT HOLES CORROSION REMOVED AND BUSHING REPAIR INSTALLED AT 1 AND 4 HOLES IAW ERA 500117-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,139 hrs · 47,672 cycles

LIGHTNING STRIKES ON WINDOW BELT FRAME SKIN AT FWD LOWER CORNER STA Y=931,469. BLENDOUT REWORK ACCOMPLISHED IAW ERA 501075-14 REV ORIG.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,236 hrs · 47,003 cycles

DURING SERVICE CHECK MAINTENANCE FOUND OVERHEAD EMERGENCY LIGHTS INOP IN COCKPIT, R1, AND R2 DOORS. MAINTENANCE REPLACED BATTERIES PER AMM 33-53. OPERATION OF LIGHTS NOW CHECKS GOOD.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 61,014 hrs · 46,844 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHTS FROM ROW 27 AFT INOPERATIVE. MAINTENANCE REPLACED LIGHT CONNECTOR DUE TO PULLED WIRE. OPERATION OF LIGHTS NOW CHECKS OK.

Part: PIN — PULLED (EVAC SLIDE) · airframe 60,862 hrs · 46,733 cycles

MAINTENANCE FOUND THE L1 DOOR SLIDE PIN PULLED WHILE PERFORMING MAINTENANCE ON SLIDE. MAINTENANCE CONTINUED WITH REMOVAL, REPLACEMENT, AND CHECK OF THE L1 DOOR SLIDE PER MAINTENANCE MANUAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 60,120 hrs · 46,199 cycles

DURING SERVICE CHECK MAINTENANCE FOUND EMERGENCY PATHWAY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD AND AFT SEATING POWER SUPPLIES AND ONE BATTERY PACK. OPERATION CHECKS GOOD AND THE AIRCRAFT OKAY FOR SERVICE.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 59,722 hrs · 45,959 cycles

LIGHTNING STRIKE AT FS 506 LONGERON 1. REPAIRED IAW ERA 32223-14.

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 59,648 hrs · 45,911 cycles

LOWER FIXED L/E NUMEROUS HOLES WORN. REPAIRED IAW SRM 55-03D, FIG 30.

Part: LIGHT — MISWIRED (COCKPIT) · airframe 59,246 hrs · 45,678 cycles

CREW NOTED EMERGENCY LIGHTS IN OVERHEAD COCKPIT PANEL REMAIN ON WITH SWITCH IN OFF POSITION. MX FOUND WHEN THE L1 ENTRY LIGHT SWITCH IS TURNED OFF AT PANEL, EMERGENCY LIGHTS WILL EXTINGUISH. ALSO FOUND WRONG BULBS INSTALLED IN ALL 3 POSITIONS. VERIFIED WIRES ARE CORRECT TO POWER SUPPLY. FOUND BAD GROUND AT L2-152 RT FWD GALLEY LIGHT PANEL. MX FOUND FWD SERVICE ENTRY LIGHT ASSY MIS-WIRED. WIRES WERE CORRECTED IAW WM 33-23-11 AND 33-51-12. OPS OF LIGHTS NOW CHECKS GOOD. MCO PLACARD REMOVED.

Part: LIGHT — INOPERATIVE (SEAT 23D) · airframe 58,882 hrs · 45,423 cycles

DURING LINE CHECK MX FOUND EMERGENCY LIGHTS AT SEAT 23D INOPERATIVE. MX REPLACED THE LIGHT ASSY AT 23D. OPERATION OF LIGHTS NOW CHECK OK.

Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHTS) · airframe 58,475 hrs · 45,149 cycles

|MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHTING AT SEAT25DE TO BE INOPERATIVE. MAINTENANCE FOUND THE WIRE HARNESS BROKEN AT THE PLUG. MAINTENANCE REPAIRED THE HARNESS. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 58,075 hrs · 44,875 cycles

MX FOUND THE SEAT 13D EMERGENCY LIGHT TO BE INOPERATIVE. (SAV EMPLOYEE NR 225052) MX REPLACED THE SEAT HARNESS. (DLM88101575)

Part: BRACKET — CRACKED (LT WING) · airframe 55,519 hrs · 43,132 cycles

BRACKET ON I/B SIDE OF LT WING L/E FORMER AT APPROXIMATELY XRS 416 IS CRACKED.

Part: LINE — LOOSE (APU OIL SYS) · airframe 54,215 hrs · 42,348 cycles

ON DEPARTURE WITH TAKEOFF POWER SELECTED CREW NOTICED SLIGHT ODOR IN COCKPIT SMELLED LIKE OVERHEATED DUCTS NOT ELECTRICAL, BRAKE OR TIRES. AFTER LANDING PASSENGERS TOLD F/A THAT THEY SAW HAZE AND ODOR IN AFT CABIN. AFTER TAKEOFF ODOR DISSIPATED AFTER 1 MINUTE FROM INITIAL OBSERVATION. FOUND LOOSE UNION ON APU OIL PRESSURE SWITCH THAT CONTAMINATED APU INLET WITH OIL-TIGHTENED LINE AND CLEANED APU INLET IN WASH RACK. PERFORMED OPN 5089 DUCT BURNOUT AND CHANGED COALESCER BAGS. LEAK AND OPS CHECKS GOOD.

Part: HYDRAULIC SYSTEM — OVERSERVICED · airframe 50,011 hrs · 39,630 cycles

DESCENDING THROUGH 1900 GOT LT HYD PRESS LOW MESSAGE ON OAP. PRESS INDICATED ZERO QTY 19. TURNED OFF ENG PUMP. OM GND PRESSURE VARIED BETWEEN ZERO AND 3000 WITH NO PUMPS ON QTY VARIED BETWEEN 11-19. INSPECTED AIRCRAFT NO LEAKS FOUND. FOUND HYD SYSTEM OVERSERVICED BLEED SYSTEM OF AIR AND FLUID TO NORMAL.OPERATED FLIGHT CONTROL WITH HYD ALL CK'S NML. HYD QTY AND PRESSURE CK'D GOOD. NO HISTORY AIRCRAFT OK FOR SERVICE.

Part: TIRE — SEPARATED (NLG) · airframe 47,717 hrs · 38,166 cycles

FOUND LEFT NOSE TIRE RECAP CAME OFF ON TAKEOFF. FOUND LEFT NOSE TIRE CAP SEPARATED. REPLACED LEFT NOSE WHEEL ASSY PER M/M.

Part: SKIN — DENTED (BS 434-484 L29LR) · airframe 47,646 hrs · 38,116 cycles

THE FUSELAGE SKIN IS DENTED AT STA 434-484 BETWEEN L-29L AND L-29R. DAMAGED SKIN WAS CUT OUT AND A DOUBLER WAS INSTALLED.

Part: SKIN — CORRODED (FS 655-674 L28L) · airframe 47,646 hrs · 38,116 cycles

THE NR 2 CARGO DOOR CUTOUT DOUBLER IS CORRODED BETWEEN STA 655-674 AND L-28L TO L-30. THE CORRODED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.

Part: SKIN — GOUGED (RT WING) · airframe 47,646 hrs · 38,116 cycles

THE RIGHT WING LOWER SKIN AND INBOARD FLAP WEDGE SKIN ARE DAMAGED. THE DAMAGED SKIN WAS CUT OUT AND A NEW SECTION OF SKIN WAS SPLICED IN.

Part: FITTING — CORRODED (MLG) · airframe 47,646 hrs · 38,116 cycles

CORROSION WAS FOUND IN MLG RETRACT ACTUATOR SUPPORT FITTING BORES. CORROSION WAS REMOVED AND OVERSIZED BUSHINGS WERE INSTALLED, REF AD 2004-25-14.

Part: RELAY — FAILED (MLG) · airframe 46,972 hrs · 37,627 cycles

UPON LANDING GEAR EXTENSION, ALL GEAR NORMAL, BUT COULD NOT EXTINGUISH THE GEAR HORN AT FLAPS 28 AND 40. REPLACED R2-295 RELAY.

Part: SENSOR — MALFUNCTIONED (AFT STAIRWAY) · airframe 46,506 hrs · 37,279 cycles

AFT STAIRWAY DOOR MESSAGE ILLUMINATED WHEN POWER ADVANCED FOR TAKEOFF. MESSAGE REMAINED ILLUMINATED UNTIL CLEARING RUNWAY. MAX SPEED AT RTO 25 KTS. CLEANED AND LUBED ROLLERS AND SWITCHES.

Part: ACTUATOR — BYPASSING (NGL STEERING) · airframe 46,503 hrs · 37,277 cycles

AFTER TAKEOFF, NOSE GEAR DID NOT RAISE. LOUD VIBRATION FELT IN NOSE GEAR, BUT IT DID NOT RAISE. NOSE LANDING GEAR INDICATOR ON CENTER CONSOLE REMAINED EXTENDED. FOUND STEERING ACTUATOR BYPASSING FLUID. REPLACED SAME.

Part: LANDING GEAR — UNDERSERVICED (NOSE) · airframe 44,590 hrs · 35,900 cycles

CREW REPORTS NOSE GEAR UNSAFE LIGHT ON AFTER TAKEOFF. SERVICED NOSE STRUT, SWUNG GEAR.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 44,538 hrs · 35,857 cycles

CORROSION ON C2 CARGO BIN DOOR JAMB BEAM FOUND DURING MTC VISIT. REMOVED CORROSION FROM C2 BIN DOOR JAMB BEAM AND WAS FOUND TO BE OUT OF LIMITS PER SRM 53-05D FIG 63 SECTION E-E SHEET 2 AND WAS REPAIRED IAW SRM 53-05D FIG 63.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 44,538 hrs · 35,857 cycles

CORROSION ON C3 CARGO BIN DOOR JAMB BEAM FOUND DURING MTC VISIT. REPLACED C3 CARGO BIN DOOR JAMB BEAM PER DOUGLAS DRAWING 5936038.

Part: TIRE — DAMAGED (NR 3 MLG) · airframe 44,232 hrs · 35,637 cycles

NR 3 MAIN TIRE HAS FOD DAMAGE. REPLACED NR 3 MAIN TIRE.

Part: HOSE — LEAKING (COCKPIT) · airframe 42,755 hrs · 34,640 cycles

CAPT`S O2 MASK HAS LEAK IN HOSE 6 INCHES BELOW MASK. REPLACED MASK/HOSE ASSY.

Part: FIRE BOTTLE — DISCHARGED (TAIL COMPT) · airframe 42,138 hrs · 34,218 cycles

NR 2 FIRE BOTTLED DISCHARGED DURING T/S ENGINE RUN DUE TO AUG VALVE LEAK. REMOVED AND REPLACED LT ENGINE NR 2 AGENT BOTTLE. FOUND FLEX LINE FOR APU AGENT BAD. REPLACED SAME ALL WORK DONE PERM/M

Part: VALVE — LEAKING (TAIL) · airframe 42,138 hrs · 34,218 cycles

TAIL COMPT OVERHEAT LIGHT CAME ON AT 10000 FT. CONT TO CYCLETHE REST OF FLIGHT. LIGHT EXT ON THE GROUND. FOUND LEAKS AT LT AUG VALVE AND LT HEAT EXCHANGER. THIGHTENED CLAMPS, PERFORMED HIGH POWER ENGINE RUN WITH BOTHENGINES NO LEAKS NOTED.

Part: CSD — UNDERSERVICED (NR 1 ENGINE) · airframe 41,154 hrs · 33,502 cycles

LEFT CSD OVERTEMP IN FLIGHT. GENERATOR TURNED OFF AND TEMP DROPPED. SERVICED CSD.

Part: RADOME — CRUSHED (FORWARD) · airframe 41,079 hrs · 33,443 cycles

BIRD STRIKE ON APPROACH RWY19R APPROX 400 FT AGL 126 KTS REPLACED RADOME WITH PART BORROWED FROM A/A

Part: WIRE — BROKEN (CABIN) · airframe 38,772 hrs · 31,766 cycles

EMERGENCY TRACK LIGHTING AT ROW 30 INOP. REPAIRED BROKEN WIRING, OPERATIONAL CHECKS OK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,545 hrs · 30,858 cycles

THE FUSELAGE SKIN AT THE FORWARD ENTRY DOOR CUTOUT WAS CRACKED IN THE LOWER AFT CORNER. THE DAMAGED SKIN WAS REMOVED AND A REPAIR INSTALLED PER S/B MD80-53-253. THE ORIGINAL REPAIR WAS CLASSIFIED AS MINOR, BUT RECLASSIFIED DUE TO DAMAGE FINDINGS PER 09-069085-12AD, REF AD 98-17-06, 09-069085-12AD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,458 hrs · 30,054 cycles

ON LO FOUND SEAT EMERGENCY LIGHT INOP. REPLACED BATTERIES. CHECKS GOOD.

Part: SKIN — DENT (BS 313 - 351)

THREE DENTS WERE FOUND IN THE FUSELAGE SKIN FROM FS 313 TO 351 BETWEEN L21R AND L22R. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333828-14.

Part: RETRACT MECH — MALFUNCTIONED (LANDING GEAR)

ON RETRACTION DURING T/O, ALL GEAR DID NOT RETRACT AND NOSE SNUBBER DID NOT STOP WHEEL ROTATION. JACKED A/C PER M/M T/S GEAR EXT AND RETRACTION INDICATIONS NORMAL. CKD STRUT EXT OK. NOSE SNUBBERS CKD GOOD PER M/M 32-10-00.

Part: COALESCER BAG — CONTAMINATED (CABIN)

DURING T/O AT APPROX 100 FT, SMOKE SMELL DETECTED IN CBN STRONG NEAR ROW 10 AFT GALLEY, HAD SCORCHED SMELL W/HINT OF RUBBE. INSPECTED WHEEL WELLS APU GALLEYS CBN, RAN PACKS ALL CKS OK. CHANGED WATER BAGS ON BOTH SIDES, BORESCOPE NR 2 ENGINE.

Part: LIGHT — BROKEN (CABIN)

EMERGENCY FLOOR PATH LIGHT AT SEAT 17 BROKEN. REPLACED LAMP, CKS OK.