N930DN

Part: PANEL — MISSING (NR 1 PYLON) · airframe 44,929 hrs · 31,043 cycles

PANEL MISSING ON THE NR 1 ENGINE PYLON. INSTALLED A REPLACEMENT PANEL IAW AMM 20-10. OK FOR SERVICE.

Part: LANYARD — DETACHED (EVAC SLIDE) · airframe 43,021 hrs · 29,945 cycles

GIRT BAR LANYARD DETACHED FROM EMERGENCY SLIDE PACK L1 DOOR. SECURED LANYARD. OPERATION CHECKS GOOD.

Part: DOOR FRAME — DENTED (L1 DOOR) · airframe 42,494 hrs · 29,682 cycles

SMALL DENT IN L1 DOOR FRAME. STRAIGHTENED LOWER EDGE IAW SRM 52-01-01.

Part: WIRE — ARCED · airframe 41,986 hrs · 29,372 cycles

DIVERTED DUE TO A STRAKE ICE FAULT ON EOAP DURING FLIGHT, WITH ICING CONDITIONS FORECASTED. MAINTENANCE REMOVED AND REPLACED THE RIGHT STRAKE WITH NO HELP. MAINTENANCE FOUND AND CONFIRMED THE RIGHT STRAKE CONNECTOR INSIDE THE FUSELAGE, BEHIND RIGHT RADIO RACK, WITH THREE WIRES DAMAGED FROM ARCING AND DETTACHED FROM THE CONNECTOR PINS. MAINTENANCE REPAIRED THE WIRING, AND PERFORMED AN OPERATIONAL TEST OF THE STRAKE ICE PROTECTION SYSTEM. THE TEST PASSED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (LP# 9490500)

Part: SLIDE — MALFUNCTIONED (TAILCONE) · airframe 41,782 hrs · 29,251 cycles

TAIL CONE SLIDE UNFOLDED WHEN REMOVED FOR TAIL CONE FUNCTION. INSTALLED TAIL CONE SLIDE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,838 hrs · 29,277 cycles

EMERGENCY EXIT SIGNS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT STA 740. OPERATIONAL TEST CHECK GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,502 hrs · 29,080 cycles

CANTED FRAME, STA 1520, WEB CRACKED AT UPPER LEFT CORNER OF CUT OUT. REPAIRED IAW ERA 52770-14.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 41,440 hrs · 29,035 cycles

PHOTO LUMINESCENT STRIP MISSING AT 27B. REPLACED STRIP IAW MM. PLACARD REMOVED.

Part: ACTUATOR — FAILED (SPOILERS) · airframe 41,232 hrs · 28,901 cycles

UN-COMMANDED MOVEMENT OF SPOILER HANDLE ON TAKE-OFF. PERFORMED OPERATIONAL TEST OF THE GROUND SPOILER AUTOMATIC ACTUATOR PER MM. REMOVED AND REPLACED GROUND SPOILER ACTUATOR. OPERATION CHECKS GOOD.

Part: HINGE FITTING — DAMAGED (LT HORIZ STAB) · airframe 40,437 hrs · 28,425 cycles

HORIZONTAL STABILIZER AT LT VERTICAL STABILIZER HINGE ATTACH FITTINGS, PITTED WITH MATERIAL LOSS ON OUTER AND INNER SURFACE. ALSO ON INNER BUSHING BORES.

Part: SPAR — CRACKED (LT HORIZ STAB) · airframe 40,437 hrs · 28,425 cycles

NR 4 HORIZONTAL STABILIZER LT SIDE AFT REAR SPAR UPPER AFT BARREL NUT HOLE CORRODED, CRACK INDICATION. REMOVED HORIZONTAL STABILIZER UNSERVICEABLE.

Part: HINGE FITTING — DAMAGED (RT HORIZ STAB) · airframe 40,437 hrs · 28,425 cycles

HORIZONTAL STABILIZER RT HINGE FITTINGS PITTED WITH MATERIAL LOSS ON OUTER AND INNER SURFACE. CORROSION CONTAINED. FABRICATED AND INSTALLED IAW SRM 55-30-05.

Part: ATTACH FITTING — CORRODED (LT MLG) · airframe 40,192 hrs · 28,281 cycles

LEFT MLG AFT ATTACH FITTING, FORWARD LUG, HAS PITTING ON AFT FACE OF BUSHING. REPLACED SPACER IAW DWG 5935812.

Part: DOOR FRAME — DAMAGED (NLG) · airframe 40,192 hrs · 28,281 cycles

NLG OPENING AFT RT SIDE FRAME DAMAGED. INSTALLED NEW FRAME IAW DWG 5913421.

Part: BUSHING — CORRODED (LT MLG) · airframe 40,192 hrs · 28,281 cycles

LEFT MLG FIXED BRACE OTBD ATTACH POINT AFT FACE BUSHING HAS PITTING. INSTALLED BUSHINGS IAW DWG 5935812.

Part: BUSHING — DAMAGED (LT MLG) · airframe 40,192 hrs · 28,281 cycles

LEFT MLG, FORWARD FITTING, FORWARD LUG BUSHING HAS DAMAGE ON AFT FACE. REPLACED SPACER IAW DWG 5935812.

Part: LANYARD — UNSECURE (L1 DOOR SLIDE) · airframe 40,064 hrs · 28,203 cycles

L1 DOOR SLIDE LANYARD HANGING. FOUND SLIDE HAD BEEN ACTIVATED AND DAMAGED. R & R SLIDE IAW WC 2561-4641.

Part: SKIN — DAMAGED (BS 1098-1136) · airframe 38,474 hrs · 27,218 cycles

ELONGATED HOLES ON EXTERNAL FUSELAGE SKIN FROM BS 1098 TO 1136 BETWEEN LONGERONS 18 - 19R. REPAIRED IAW ERA 537809-14, REV O.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 520BT. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 520FT. REPLACED THE ACCESS PANEL.

Part: WIRE — BROKEN (DOOR SLIDE) · airframe 38,474 hrs · 27,218 cycles

BROKEN WIRES ON LANYARDS OF R1 AND L2 DOOR SLIDES. R & R LANYARDS.

Part: DOOR FRAME — CRACKED (NLG WW) · airframe 38,474 hrs · 27,218 cycles

CRACK ON DOOR JAMB BELOW ANGLE AT NLG WHEEL WELL. CRACK WAS STOPPED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 AND 51-30-02.

Part: FRAME SPLICE — CORRODED (BS 1503) · airframe 38,474 hrs · 27,218 cycles

CORROSION ON FRAME SPLICE, BS 1503, LONGERON 22 - 24L. REPAIRED IAW ETI 90-15-075 AND ERA 537814-14, REV O.

Part: FRAME — WORN (BS 1437) · airframe 38,474 hrs · 27,218 cycles

WEAR ON FRAME, BS 1437. R & R WEB SECTION IAW DWG9912246.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 38,474 hrs · 27,218 cycles

CORROSION ON HORIZONTAL STAB LT BARREL NUT HOLE NR 24. R & R IAW ERA 5377990-14, REV O.

Part: DOOR FRAME — CRACKED (NLG WW) · airframe 38,474 hrs · 27,218 cycles

CRACK ON NLG WHEEL WELL DOOR JAMB BEAM, BS Y=46 AND Y=17. REPAIRED IAW SRM 53-90-01.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 38,474 hrs · 27,218 cycles

CORROSION ON HORIZONTAL STAB LT BARREL NUT HOLE, NR 10. REPAIRED IAW ERA 537790-14, REV O.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 620MB. REPLACED THE ACCESS PANEL.

Part: ANGLE — CRACKED (NLG WW) · airframe 38,474 hrs · 27,218 cycles

CRACK ON ANGLES AT BS 110, X=-7 AND -10, Z=-301, NOSE WHEEL WELL. REPLACED ANGLES IAW ERA 5912616, REV CK AND SRM 51-30-08.

Part: SKIN — WORN (ACCESSORY BAY) · airframe 38,474 hrs · 27,218 cycles

WEAR ON STRIP LT/RT FORWARD SIDE LOWER SKIN AT AFT ACCESSORY COMPARTMENT. DAMAGE REMOVED. FABRICATED AND INSTALLED DOUBLERS IAW SRM 53-00-01, FIG 6 AND 51-30-20.

Part: RUB STRIP — WORN (SLAT PANEL) · airframe 38,474 hrs · 27,218 cycles

EXCESSIVE WEAR ON RUB STRIP SLAT PANEL NR 1 AND NR 2 INBD SIDE RT WING. REMOVED, FABRICATED AND INSTALLED NEW IAW SRM 51-30-02, 51-10-05.

Part: SKIN — DAMAGED (BS 427-434) · airframe 38,474 hrs · 27,218 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN BS 427-434 BETWEEN LONGERON 29-30R. EXCESSIVE DAMAGE. REPAIRED IAW SRM 53-30-02, 51-30-02, 51-10-03.

Part: SKIN — PUNCTURED (ACCESSORY DOOR) · airframe 38,474 hrs · 27,218 cycles

PUNCTURED SKIN ON FORWARD ACCESSORY COMPARTMENT DOOR LATERAL EDGE. REPAIRED IAW SRM 57-00-01.

Part: INTERCOSTAL — CRACKED (BS 1542-1554) · airframe 38,474 hrs · 27,218 cycles

CRACK ON INTERCOSTAL BETWEEN BS 1542-1554 LONGERON 24R. REMOVED AND REPAIRED THE INTERCOSTAL IAW SRM 51-10-01 AND DWG 9910087.

Part: SUPPORT BRACKET — CORRODED (R1 DOOR SLIDE) · airframe 38,474 hrs · 27,218 cycles

CORROSION ON RT EVACUATION SLIDE FITTING SUPPORT BRACKETS, 2 EA. EXCESSIVE DAMAGE. R & R FITTINGS IAW SRM 51-10-05, 51-10-03, 51-30-02 AND DWG 3936190.

Part: SKIN — DAMAGED (BS 178) · airframe 38,474 hrs · 27,218 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN, BS 178, BETWEEN STRINGERS 28 - 29L. REPAIRED IAW SRM 53-31-02, PARA 3C.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 520EB. REPLACED THE ACCESS PANEL.

Part: SEAT TRACK — CORRODED (BS 1281-1320) · airframe 38,474 hrs · 27,218 cycles

CORROSION ON SEAT TRACK BS 1281-1320. CUTOUT DAMAGE. PLUG WAS INSTALLED IAW SRM 53-40-01, 51-10-03.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 620EB. REPLACED THE ACCESS PANEL.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 38,474 hrs · 27,218 cycles

CRACKED LEFT INBD L/E PANEL RIB OF HORIZONTAL STABILIZER. REPAIRED IAW SRM 55-00-01.

Part: SKIN — DENTED (BS 223) · airframe 38,474 hrs · 27,218 cycles

DENT ON FUSELAGE SKIN, BS 223 BETWEEN LONGERONS 17 - 18L. REPAIRED IAW SRM 53-30-01, 51-30-02, 51-30-05 AND 51-10-03.

Part: CUSP WEB — DENTED (BS 994-1003) · airframe 38,474 hrs · 27,218 cycles

CORROSION ON LT CUSP WEB FROM BS 994 - 1003. REPAIRED IAW SRM 53-20-02.

Part: ANGLE — CRACKED (BS 883) · airframe 38,474 hrs · 27,218 cycles

CRACK ON ANGLE AT WING BOX STRUCTURE AT BS 883, X=-41 AND Z=-9. REPAIRED IAW ERA 498192-14MA, REV A.

Part: SUPPORT FITTING — CORRODED (LT WING TE FLAP) · airframe 38,474 hrs · 27,218 cycles

CORROSION ON LT FLAP SUPPORT FITTING HINGE INTERNAL STRUCTURE XW=154. REPAIRED IAW ERA 537789-14, REV O.

Part: WEB — CRACKED (HORIZONTAL STAB) · airframe 38,474 hrs · 27,218 cycles

CRACK ON WEB ABOVE FITTING BS XH 7.235 AT LT HORIZONTAL STAB INBD L/E. REPAIRED IAW SRM 51-00-02.

Part: CUSP WEB — CORRODED (BS 757) · airframe 38,474 hrs · 27,218 cycles

CORROSION ON LT CUSP WEB MEMBRANE SURFACE, BS 757, X=60. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-20-02.

Part: SKIN — DAMAGED (RUDDER TAB) · airframe 38,474 hrs · 27,218 cycles

DAMAGED METALLIC COVER ON RUDDER TAB. REPAIRED IAW SRM 55-41-01. WEIGHT AND BALANCE IAW SRM 55-40-01.

Part: CUSP WEB — CRACKED (BS 1119-1121) · airframe 38,474 hrs · 27,218 cycles

THREE CRACKS FOUND ON RT CUSP WEB BETWEEN BS 1119-1121, X=-60. REPAIRED IAW SRM 53-20-02, FIG 15, 51-30-01, 51-30-03, 51-30-05 AND 51-10-03.

Part: SKIN — DAMAGED (BS 712-731) · airframe 38,474 hrs · 27,218 cycles

SCRATCH ON WINDOW BELT FRAME ON AFT UPPER CORNER BETWEEN 712-731. REPAIRED IAW ERA 537779-14, REV O.

Part: PAN — CRACKED (CARGO DOORWAY) · airframe 38,474 hrs · 27,218 cycles

CRACKED OUTER PAN AFT EDGE BETWEEN BEAM 1-2 AT MID CARGO DOOR. REPAIRED IAW SRM 52-30-02.

Part: SEAT TRACK — WORN (BS 200-256) · airframe 38,474 hrs · 27,218 cycles

CORROSION ON RT SEAT TRACK, BS 200-256, X -22. R & R THE SEAT TRACK IAW SRM 51-10-05, 51-30-0, 51-30-05 AND 51-10-03.

Part: SEAT TRACK — CORRODED (BS 200) · airframe 38,474 hrs · 27,218 cycles

CORROSION ON LT SEAT TRACK, BS 200, X=44. REPLACED SEAT TRACK BS 200-300, X=44 IAW SRM 51-30-05, 51-20-03.

Part: BEAM — CRACKED (FUSELAGE) · airframe 38,474 hrs · 27,218 cycles

CRACKED INNER PAN PROJECTION BEAM NR 5 AT FORWARD CARGO DOOR FORWARD EDGE. REPAIRED IAW SRM 52-30-02.

Part: SEAT TRACK — CORRODED (BS 218-322) · airframe 38,474 hrs · 27,218 cycles

CORROSION ON LT SEAT TRACK, BS 237-313, X=22. REPLACED SEAT TRACK BS 218-322 IAW SRM 51-30-01 AND 51-30-05.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 620DB. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 620QB. REPLACED ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 520LB. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 520PB. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 520CB. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 620GB. REPLACED THE ACCESS PANEL.

Part: SEAT TRACK — CORRODED (BS 200-256) · airframe 38,474 hrs · 27,218 cycles

CORROSION ON RT SEAT TRACK, BS X=-44, BETWEEN BS 200-256. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-40-01.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 620PB. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 520HB. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 620HB. REPLACED ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 520DB. REPLACED ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 620LB. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 520QB. REPLACED THE ACCESS PANEL.

Part: FLOORBEAM — CORRODED (BS 180) · airframe 38,474 hrs · 27,218 cycles

CORROSION ON FLOORBEAM AT BS 180 BETWEEN X 7 AND X -40. TASK 53-037-02. R & R THE FLOORBEAM IAW SRM 51-30-02, 51-30-05 AND 51-10-03.

Part: ANGLE — CRACKED (BS 962) · airframe 38,474 hrs · 27,218 cycles

CRACK ON ANGLE OF WING BOX INTERNAL STRUCTURE AT BS 962, X=42 AND Z=-8. REMOVED AND INSTALLED NEW ANGLE IAW DWG 9923417, REV B AND SRM 51-30-05.

Part: LONGERON — CRACKED (BS 984) · airframe 38,474 hrs · 27,218 cycles

CRACKED LONGERON 6R, BS 984. REPAIRED IAW SRM 51-10-01, 51-10-03 AND 51-30-05.

Part: FLOOR SUPPORT — CRACKED (BS 520-522) · airframe 38,474 hrs · 27,218 cycles

CRACKS AND ELONGATED HOLES ON FORWARD CARGO FLOOR SUPPORT, BS 520-522 BETWEEN LONGERONS 28R-28L. R & R FLOOR SUPPORT IAW DWG 5936592-16 AND SRM 51-30-02, 51-10-03.

Part: SKIN — DAMAGED (BS 712-731) · airframe 38,474 hrs · 27,218 cycles

LEFT WINDOW BELT PANEL BETWEEN FS 712 AND FS 731 HAD A SCRATCH BLENDED OUT ON A TIME LIMITED BASIS. ACCOMPLISH ERA 537779-14.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 620AT. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 620JB. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 520DT. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 620DT. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 520JB. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 520GB. REPLACED THE ACCESS PANEL.

Part: CUSP WEB — DAMAGED (BS 883) · airframe 38,474 hrs · 27,218 cycles

TOOL DAMAGE ON LT CUSP WEB MEMBRANE SURFACE, BS 883 BETWEEN LBL 44 AND 54. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-00-01, 51-10-03, 51-30-02 AND ERA 511165-14MA.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 620CB. REPLACED THE ACCESS PANEL.

Part: BEAM — CRACKED (PAX DOOR) · airframe 38,474 hrs · 27,218 cycles

CRACKS ON BEAM NR 1 FORWARD AND AFT EDGE OF FORWARD ENTRY DOOR. REPAIRED IAW SRM 52-10-02.

Part: HOUSING — WORN (CARGO DOOR) · airframe 38,474 hrs · 27,218 cycles

WEAR ON EXTERNAL HOUSING AT MID CARGO DOOR. REPLACED IAW SRM 51-30-00 AND 51-30-05.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 520CT. REPLACED THE ACCESS PANEL.

Part: CUSP WEB — CRACKED (BS 864) · airframe 38,474 hrs · 27,218 cycles

CRACK ON RT CUSP WEB, BS 864 X=-60. REPAIRED IAW SRM 53-20-02, FIG 19.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,340 hrs · 28,977 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 620CT. REPLACED THE ACCESS PANEL.

Part: CUSP WEB — DAMAGED (BS 541) · airframe 38,474 hrs · 27,218 cycles

LT CUSP WEB ON DAMAGED ON REPAIR, BS 541 AND X=60. REMOVED, FABRICATED AND INSTALLED REPAIR IAW SRM 51-30-02, 51-10-05 AND 53-20-02.

Part: FLOOR PANEL — PUNCTURED (BS 182-198) · airframe 38,474 hrs · 27,218 cycles

FLOOR PANEL PUNCTURED RBL 8 AND BS 182 - 198. REPAIRED IAW SRM 53-00-01, 51-10-3, PARA 14 AND 21 AND 51-30-02.

Part: COVER — DAMAGED (NOT REPORTED) · airframe 38,474 hrs · 27,218 cycles

DAMAGE DUST COVER ON EYEBOLT AT XET 83.580, R & R.

Part: BOTTLE — LOW PRESSURE (TAILCONE) · airframe 38,474 hrs · 27,218 cycles

LOW PRESSURE ON TAILCONE JETTISON BOTTLE. SERVICED NITROGEN CYLINDER. CHECKS OK.

Part: CABLE — MISROUTED (L1 DOOR SLIDE) · airframe 37,185 hrs · 26,449 cycles

L1 DOOR SLIDE CABLE ROUTED INCORRECTLY. R & R SLIDE IAW AMM 25-61-01.

Part: UNKNOWN — UNKNOWN (HORIZONTAL STAB) · airframe 37,170 hrs · 26,440 cycles

REPAIR AFT INBD CORNER OF RT HORIZONTAL STABILIZER. REPAIRED IAW PRI/ERA 531273-14AD.

Part: LONGERON — CRACKED (BS 1475) · airframe 37,170 hrs · 26,440 cycles

LONGERON 2R IS CRACKED AT HAT FLANGE, AFT SIDE OF B-FRAME, BA 1475. ACCOMPLISHED REPAIR IAW ERA 533633-14, REV O.

Part: LONGERON — CRACKED (BS 1475) · airframe 37,170 hrs · 26,440 cycles

LONGERON 2L IS CRACKED AT HAT FLANGE AFT SIDE OF B-FRAME AT BS 1475. ACCOMPLISHED REPAIR IAW PRI/ERA 533635-14, REV O.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 40,951 hrs · 28,729 cycles

DURING C-CHECK, A CRACK WAS FOUND COMMON TO L-2R ON AFT END OF STA 1475. ERA 533633-14 ISSUED AND C/W FOR SPLICE TO LONGERON L-2R, LP 1846105.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 37,170 hrs · 26,440 cycles

AFT CARGO COMPARTMENT DOOR LOWER SILL CORRODED. REPAIRED IAW SRM 53-60-02.

Part: ATTACH FITTING — CRACKED (VERTICAL STAB) · airframe 37,170 hrs · 26,440 cycles

LEFT VERTICAL FIN ATTACH ANGEL HAS 1" LONG CRACK IN RADIUS, NEAR FIN AFT SPAR. COMPLIED WITH PRI/ERA 533587-14, REV O.

Part: NONE — NONE (NONE) · airframe 37,251 hrs · 26,492 cycles

ERA 533588, SECTION I ISSUED FOR REPAIR TO C2 BEAM.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 37,170 hrs · 26,440 cycles

MID CARGO COMPARTMENT LOWER DOOR SILL CORRODED. BLENDED AND REPAIRED IAW SRM 53-60-02 AND ERA 533588-14, REV O.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 37,170 hrs · 26,440 cycles

LEFT VERTICAL FIN ATTACH ANGLE HAS LONG CRACK IN RADIUS, NEAR FIN AFT SPAR. REMOVED DAMAGE AND INSTALLED DOUBLER IAW PRI/ERA 533587-14, REV O.

Part: DOOR — OBSTRUCTED (COCKPIT) · airframe 37,005 hrs · 26,340 cycles

COCKPIT DOOR JAMMED IN FLIGHT. MAINTENANCE FOUND D-RING FOR EMERGENCY EGRESS, NOT STOWED IN LATCHES. D-RING WAS JAMMED IN THE DOOR HINGE. REMOVED AND STOWED THE D-RING IN PLACE. OPS CHECKED GOOD.

Part: ACTUATOR — FAILED (OUTFLOW VALVE) · airframe 36,203 hrs · 25,822 cycles

PERFORMED AN AIR TURNBACK DUE TO AN AUTO INOP LIGHT ON PRESSURIZATION PANEL, WHILE CLIMBING THROUGH 10K. CABIN ALTITUDE ALSO NEAR 10K AND CLIMBING. SWITCHED TO MANUAL ON CONTROL WHEEL, BUT WHEEL WOULD NOT ROLL. WE WERE UNABLE TO REGAIN CONTROL OF CABIN ALTITUDE. REPLACED THE OUTFLOW VALVE ACTUATOR ASSY. OPS CHECK OF OUTFLOW VALVE ACTUATOR ASSEMBLY GOOD.

Part: WIRE — DETACHED (EMERGENCY LIGHT) · airframe 35,668 hrs · 25,488 cycles

AFT STAIRWELL FIRST HORIZONTAL EMERGENCY EXIT PATHWAY LIGHT ASSEMBLY INOPERATIVE. CONNECTED WIRES TO LIGHT ASSY AT QUICK DISCONNECT. OPS CHECKED GOOD.

Part: STRUCTURE — SCRATCHED (L1 DOOR) · airframe 35,409 hrs · 25,324 cycles

L1 DOOR HAS LARGE SCRAPE AT LOWER LEFT. REPAIRED DOOR EDGE IAW SRM 52-01-01. OK FOR SERVICE.

Part: CABLE — BROKEN (PAX DOOR) · airframe 34,840 hrs · 24,953 cycles

1 OF 2 ALUMINUM HANDLE CABLES BROKE OFF OF THE FLIGHT DECK DOOR. R & R FLIGHT DECK DOOR AND DOOR HANDLE RELEASE HANDLE IAW AMM.

Part: CABLE — BROKEN (GIRT BAR) · airframe 33,960 hrs · 24,407 cycles

FOUND L1 DOOR GIRT BAR CABLE BROKEN. REMOVED AND REPLACED CABLE ASSEMBLY. OPS CHECKED OK IAW AMM.

Part: WEB — DAMAGED (MLG WW) · airframe 32,875 hrs · 23,754 cycles

NLG OVERSTEER DCA. DAMAGE TO NLG WHEEL WELL AT APPROX BS 95. REPAIRED IAW ERA 92-515901.

Part: TRUNNION — DAMAGED (NLG) · airframe 32,905 hrs · 23,773 cycles

FOUND LT NLG WHEEL WELL, FORWARD OF LEFT TRUNION FITTING, GOUGED/CRACKED. REMOVED DAMAGED AREA. COMPLIED WITH PRI 515901-14, REV 4 AND REV 5. FABRICATED, TREAT, PRIMED AND INSTALLED INNER AND OUTER DOUBLER IAW PRI 515901-14, REV 6.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 32,296 hrs · 23,422 cycles

DURING CHECK, ERA 512588-14AD ISSUED FOR SKIN CRACK ON RT UPPER HORIZONTAL STABILIZER INBD AFT CORNER. ACCOMPLISH ERA 512588-14AD SECTION II EVERY 250 FLIGHT CYCLES. SECTION III NOT TO EXCEED 4000 FLIGHT CYCLES.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 32,296 hrs · 23,422 cycles

AFT UPPER SKIN PANEL CRACKED ON RT HORIZONTAL STABILIZER. CONFIRMED WITH HFEC. STOP DRILLED CRACK ACCOMPLISHED REPAIR IAW ERA 512588-14AD RII QC1981.

Part: FLAP — PUNCTURED (LT WING) · airframe 29,942 hrs · 22,127 cycles

MAINTENANCE FOUND SMALL PUNCTURE IN LEFT WING INBOARD FLAP 30 INCHES FORWARD OF TRAILING EDGE AND 44 INCHES OUTBOARD OF FUSELAGE. COMPLIED WITH ERA 502781-14 REV 0 TEMPORARY REPAIR.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,818 hrs · 22,056 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB 22J2. OPS CHECKED GOOD.

Part: CUSP WEB — CORRODED (BS 750-773) · airframe 29,618 hrs · 21,950 cycles

MAIN CABIN LEFT CUSP WEB HAS CORROSION BETWEEN BS 750-773. REMOVED CORROSION IN MAIN CABIN AT LT CUSP WEB IAW SRM VOL 2 51-10-03 PG 46-49 AND MD90 SRM VOL1 53-00-01. FOUND OUT OF LIMITS IAW SRM 53-00-01 VOL 1 FIG 3. REMOVED AND REPLACED FILLER AND DOUBLER IAW SRM 53-20-02 FIG 6 SH 1 AND ER/A 501651-14 REV ORIG. DURING HMV AT SAA/SAT.

Part: CUSP WEB — CORRODED (BS 750-773) · airframe 29,618 hrs · 21,950 cycles

MAIN CABIN LEFT CUSP WEB HAS CORROSION BETWEEN BS 750-773. REMOVED CORROSION IN MAIN CABIN AT LT CUSP WEB BETWEEN STA 750-773 IAW SRM VOL2 51-10-03 PG 46-49 AND SRM VOL1 53-00-01. FOUND OUT OF LIMITS IAW SRM 53-00-01 VOL 1 FIG 3. REMOVED AND REPLACED FILLER AND DOUBLER IAW SRM 53-20-02 FIG 6 SH 1 AND ER/A 501651-14 REV ORIG.

Part: SLIDE — DISCONNECTED (L1 DOOR) · airframe 29,617 hrs · 21,949 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND L1 DOOR SLIDE PACK PINS OUT OF POSITION. MAINTENANCE REMOVED AND REPLACED SLIDE PER AMM.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,500 hrs · 21,878 cycles

ON INSPECTION, FOUND DENT AT STATION 234, 34 INCHES AFT OF L1 DOOR AND 24 INCHES UP FROM LOWER LIP OF DOOR. PERFORMED INSPECTION PER ERA500280-14. PERMANENT REPAIR PER ERA 500280-14. DUPLICATE WRITE-UP ON DELTA LOG 959383001.

Part: CABLE — DISCONNECTED (TAILCONE) · airframe 29,361 hrs · 21,809 cycles

DURING SERVICE CHECK, FAA FOUND RIGHT TAIL CONE SLIDE JETTISON CABLE DISCONNECTED AT BOX. MAINTENANCE RECONNECTED CABLE TO THE FORWARD RIGHT HOLD DOWN STRAP AND WALKWAY CLIP PER AMM.

Part: SPAR — CRACKED (WING) · airframe 29,360 hrs · 21,808 cycles

WING REAR SPAR CRACKED. REPAIRED IAW AA 5710-01119.

Part: BEAM — CORRODED (CARGO DOOR FRAME) · airframe 29,355 hrs · 21,806 cycles

AFT CARGO DOOR FRAME BEAM, L28R, CORRODED. REPAIRED IAW ERA 398119-14.