N935DN

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 45,952 hrs · 28,857 cycles

EXTERIOR EMERGENCY LIGHTS WERE INOPERATIVE. FOUND WIRES L1594J18 AND L1598B18 SHORTING TO GROUND WITH EACH OTHER AT PRESSURE SEAL. REPAIRED THE WIRING IAW WDM 33-51-13 691460. FOUND WIRE AT L2-664 CHAFED AT THE LIGHT ASSY L1594H18. REPAIRED THE TERMINAL END AND NO SHORTS FOUND. 28V GOOD AT TERMINAL 2 OF S3-329. INSTALLED A NEW POWER SUPPLY ASSY B5-125 AND NO POWER AT S3-329 TERMINAL 2 AGAIN. FOUND SHORT AT PRESSURE SEAL OF LIGHT ASSY B5-125. REMOVED BAD SECTION OF WIRE L1594H18 AND INSTALLED NEW LIGHT ASSY AND NEW POWER SUPPLY B5-125. OVER WING EMERGENCY LIGHTS NOW OP NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,490 hrs · 28,581 cycles

L1 DOOR UPPER EXIT EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE POWER SUPPLY.

Part: DUCT — CRACKED · airframe 45,278 hrs · 28,459 cycles

STRONG ACRID FUMES STARTED DURING TAKEOFF. CABIN TEMP WAS IN MANUAL IAW MEL BUT TEMP INDICATED COOL. FUMES SEEMED TO DISSIPATE AFTER TURNING OFF RIGHT PACK. CHANGED COALESER SOCK ON THE RT SIDE. FOUND CRACKED DUCT RT SIDE DOWN STREAM OF TEMP CONTROLLER VALVE. DUCT HAD 5" OPEN CRACK & RT WATER SEPERATOR FOUND PLUGGED. REMOVED AND REPLACED DUCT ASSY.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 45,225 hrs · 28,429 cycles

WHILE PERFORMING AMDS CARD 5510-01073-02, FOUND A DAMAGED UPPER BOLT OF THE RIGHT SIDE INBOARD ELEVATOR HINGE. ATTEMPTING TO REMOVE BOLT FOR INSPECTION. DUE TO SKIN CRACKS IN HORIZONTAL STABILIZER, COMPLETE STAB ASSEMBLY WAS REPLACED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,073 hrs · 28,336 cycles

DURING A SERVICE CHECK, FOUND OVERWING EMERGENCY EXIT EXTERNAL LIGHTS INOPERATIVE. REPLACED THE POWER SUPPLY B5-125 IAW AMM 33-51-03. LIGHTS OPS CHECKED NORMAL. OK FOR SERVICE.

Part: ELECTRICAL SYS — FAILED · airframe 44,371 hrs · 27,911 cycles

EXPERIENCED A TOTAL LOSS OF ELECTRICAL POWER WHILE BEING VECTORED FOR APPROACH. MAINTENANCE TROUBLESHOT AND FOUND OHMS FROM GENERATOR TO CEU T-1 270 M OHMS, T-2 157 M OHMS AND T-3 OL. REMOVED AND REPLACED RIGHT COTA AND CEU IAW MM. REMOVED AND REPLACED EPCU, LEFT CEU, COTA AND HARNESS. OPERATION CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,220 hrs · 27,813 cycles

ONE EMERGENCY LIGHT FAILED TO ILLUMINATE AT ROW 17. REPLACED THE LAMPS IAW AMM 33-51. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BRAKE — DAMAGED (LT MLG) · airframe 43,488 hrs · 27,380 cycles

AFTER UNEVENTFUL LANDING AND RUNWAY CROSSING, FLIGHT CREW FELT A BUMP AND SHORT LIVED DECELERATION THEN RELEASE. BRAKE INDICATIONS APPEARED NORMAL. THE CREW WAS ADVISED BY TOWER THAT THE LT MLG BRAKE WAS SMOKING HEAVILY. STOPPED ON THE TAXIWAY AND THE PARKING BRAKE OPERATED NORMALLY. THE RIGHT BRAKE TEMP NEVER EXCEEDED 350. PERFORMED HIGH ENERGY STOP INSPECTION. FOUND NR 2 BRAKE DAMAGED. REPLACED NR 2 TIRE AND BRAKE ASSEMBLIES. AIRCRAFT OKAY FOR SERVICE.

Part: LANYARD — DETACHED (R1 DOOR) · airframe 43,315 hrs · 27,290 cycles

LANYARD ON R1 DOOR FELL OUT OF ACCESS DOOR. REATTACHED. OPERATION CHECKS GOOD.

Part: CABLE — FRAYED (TAILCONE RELEASE) · airframe 43,056 hrs · 27,144 cycles

TAIL CONE LATCH RELEASE CABLE RUN 547 HAS SEVERAL BROKEN STRANDS . REMOVED & REPLACED, OPS CHECKED GOOD.

Part: FRAME — CRACKED (BS 1520) · airframe 43,032 hrs · 27,128 cycles

CRACKS ON CANTED FRAME, BS 1520 DOUBLER AT FASTENER HOLE. REMOVED AND REPLACED THE DOUBLER IAW DWG 9953015, AND SRM 51-3.0-02, AND 51-30-05.

Part: FRAME — CRACKED (BS 1520) · airframe 43,032 hrs · 27,128 cycles

AFT ACCESSORY COMPARTMENT FRAME BS 1520 LEFT SIDE OF STRINGER 2R CRACKED. INSTALLED A NEW FRAME IAW SRM 51-30-02, AND 51-30-05.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,056 hrs · 27,144 cycles

OVER WING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECKED GOOD.

Part: PANEL — CRACKED (VERTICAL STAB) · airframe 43,032 hrs · 27,128 cycles

VERTICAL STABILIZER LOWER AFT CORNER IS CRACKED AT PANEL 370BL. REPAIRED IAW ERA 555250-14, REV O.

Part: FRAME — CRACKED (BS 45) · airframe 43,032 hrs · 27,128 cycles

NOSE WHEEL WELL, BS 45 LEFT FRAME CRACKED. REPAIRED IAW SRM 53-90-01.

Part: FRAME — CRACKED (BS 45) · airframe 43,032 hrs · 27,128 cycles

CRACK ON RIGHT FRAME BS 45, IN THE NOSE WHEEL WELL. REMOVED AND REPLACED THE FRAME IAW DWG 9910088, REV CJ, SRM 51-30-02, AND 51-30-05.

Part: STRAP — CRACKED (BS 1520) · airframe 43,032 hrs · 27,128 cycles

STRAP AT FRAME, BS 1520 INBOARD OF LONGERON 3R IS CRACKED. FABRICATED AND INSTALLED NEW STRAP IAW DWG 9911839, REV DP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,032 hrs · 27,128 cycles

FUSELAGE SKIN CRACK AT NOSE STRUT DOOR AFT HINGE RIGHT HAND SIDE. IN WORK/FIXED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,032 hrs · 27,128 cycles

FUSELAGE SKIN CRACKED AT NOSE STRUT DOOR AFT HINGE LEFT HAND SIDE. FIXED/IN WORK.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 42,197 hrs · 26,667 cycles

RIGHT FUEL SWITCH RED FIRE WARNING ON FUEL SWITCH, ILLUMINATED AFTER PLACING SWITCH TO ON DURING ENGINE START. REMAINED ILLUMINATED. MAINTENANCE RESET RIGHT ENGINE FIRE HANDLE AND PROBLEM RESOLVED. PERFORMED ENGINE FIRE WARNING SYSTEM TEST IAW MM. OPERATION CHECKS GOOD.

Part: DOOR FRAME — CRACKED (RT MLG) · airframe 42,182 hrs · 26,661 cycles

RIGHT MAIN LANDING GEAR DOOR FRAME CRACKED. REMOVED, FABRICATED AND INSTALLED NEW DOOR FRAME IAW DWG 5930584.

Part: ENGINE — FAULTED (NR 1) · airframe 41,216 hrs · 26,112 cycles

ON SHORT FINAL, NR 1 EGT GAUGE BEGAN FLASHING AND INDICATED 699. EPR GAUGES DID NOT MATCH. LANDING WAS NORMAL. AFTER SHUTDOWN, EGT=708 WITH LT ENG SYS FAIL MESSAGE. POST FLIGHT INSPECTION, NR 1 ENGINE HAS SMOKE RISING FROM COWL. MAINTENANCE OPENED COWLS AND THRUST REVERSER. COMPLETED BSI OF NR 1 ENGINE HT SECTION. NO RESTRICTIVE DAMAGE FOUND. INSPECTED VSV ACTUATORS AND VANES. NO FAULT NOTED. NR 1 ENGINE REMOVED AND REPLACED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,496 hrs · 25,704 cycles

L2 DOOR EMERGENCY EXIT LIGHT FORWARD OF DOOR IS INOPERATIVE. R & R BATTERY POWER SUPPLY. NO HELP. CHANGED BATTERY. OPERATION CHECKS OK.

Part: PIN — DISLODGED (L1 DOOR SLIDE) · airframe 40,180 hrs · 25,506 cycles

L1 DOOR SLIDE PINS DISLODGED. R & R SLIDE.

Part: HARNESS — DAMAGED (TAILCONE SLIDE) · airframe 39,956 hrs · 25,380 cycles

AFT TAIL CONE SLIDE HARNESS DAMAGED. INSTALLED NEW TAIL CONE SLIDE HARNESS IAW AMDS.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 39,821 hrs · 25,309 cycles

AFT STAIRS EMERGENCY SIDEWALL LIGHT INOPERATIVE. FOUND WIRE BROKEN AT QUICK DISCONNECT. REPAIRED IAW SWPM. OPERATION CHECKS OK.

Part: ANGLE — CORRODED (RT WING TE FLAP) · airframe 37,917 hrs · 24,139 cycles

CORROSION ON ANGLES LOCATED ON RT WING OTBD FLAP INNER STRUCTURE, XRS 164. FLAP AND VANES WERE R & R .

Part: SKIN — CORRODED (RT WING) · airframe 37,899 hrs · 24,127 cycles

CORROSION ON RT WING UPPER SKIN STA XRS=240. REPAIRED IAW ERA 534378-14 AD, REV O. LP 1976805.

Part: STRUCTURE — CORRODED (WING) · airframe 37,899 hrs · 24,127 cycles

CORROSION ON FIXED L/E AFT LOWER EDGE STA XRS=240. REPAIRED IAW ETI90-15052, REV 1 AND ERA 534406-14, REV O.

Part: CLEVIS — CORRODED (TAILCONE RELEASE) · airframe 37,899 hrs · 24,127 cycles

THREE RUSTED CLEVIS`S, ON CABLE SUPPORT AT TAILCONE RELEASE SYSTEM. R & R AND ADJUSTED CLEVIS ON CABLE SUPPORT AT TAILCONE RELEASE IAW AMM. LP 1965257.

Part: SKIN — CRACKED (BS 1484) · airframe 37,899 hrs · 24,127 cycles

CRACKED OUTER SKIN, BS 1484, BETWEEN LONGERON 2R-3R. REPAIRED IAW SRM 51-10-3, 51-30-02, 51-30-05, AND ERA 534366-14, REV O.

Part: DOOR FRAME — CRACKED (RT MLG) · airframe 37,899 hrs · 24,127 cycles

CRACKED FORMER ON RT FORWARD MLG DOOR JAMB, BS 1006, X=-56. R & R FORMER IAW SRM 51-30-02, 51-30-05, AND 51-10-05. LP 1961928.

Part: SEAT TRACK — CORRODED (BS 235-238) · corrosion level 2 · airframe 37,899 hrs · 24,127 cycles

CORROSION ON SEAT TRACK, BS 235-238, X=-44. FOUND TO BE OUT OF LIMITS. R & R THE SEAT TRACK IAW SRM 53-40-01.

Part: FRAME — CRACKED (BS 294) · airframe 37,899 hrs · 24,127 cycles

CRACKED FRAME, BS 294, LONGERON 6L AT INNER FUSELAGE STRUCTURE. REPAIRED IAW ERA 534382-14, REV O.

Part: SPAR CAP — CORRODED (RT WING) · corrosion level 2 · airframe 37,899 hrs · 24,127 cycles

CORROSION ON LOWER CAP, BS XRS 531 AND 544 AT RT WING FRONT SPAR. REPAIRED IAW ETI 90-15-044 R1 AND ERA 534381-14, REV O.

Part: SUPPORT — CRACKED (BS 1079-1098) · airframe 37,899 hrs · 24,127 cycles

CRACK ON KEEL BEAM AFT SUPPORT BETWEEN BS 1079 - 1098, LONGERON 30. SUPPORT WAS REPLACED IAW SRM 51-30-05. LP 1961920.

Part: SEAT TRACK — CORRODED (BS 856-902) · airframe 37,899 hrs · 24,127 cycles

CORROSION ON SEAT TRACK, BS 856-874 AND 883-902, X=54. TASK 53-211-02. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 53-40-01 AND 51-10-03.

Part: FORMER — CRACKED (DOOR FRAME) · airframe 37,899 hrs · 24,127 cycles

CRACKED FORMER ON LT MLG FORWARD DOOR JAMB, BS 997 X=7. R & R FORMER IAW SRM 51-30-02, 51-30-01, 51-30-05, 51-10-03.

Part: SKIN — DAMAGED (RUDDER) · airframe 37,899 hrs · 24,127 cycles

METALLIZED COVER ON RUDDER TAB DAMAGED. REPAIRED IAW SRM 55-41-01.

Part: PIN — OUT OF POSITION (L1 DOOR SLIDE) · airframe 37,899 hrs · 24,127 cycles

THE SECURITY PIN FOR L1 DOOR SLIDE WAS OUT OF POSITION. R & R SLIDE.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 37,899 hrs · 24,127 cycles

CORROSION ON HORIZONTAL STABILIZER BARREL NUT NR 10. REMOVED BARREL NUT AND NEW BUSHING FABRICATED AND INSTALLED IAW SRM 55-10-03.

Part: FORMER — CRACKED (BS 994) · airframe 37,899 hrs · 24,127 cycles

CRACKED FORMER, BS 994, C=7, KEEL BEAM FORWARD EDGE. REMOVED, FABRICATED AND INSTALLED NEW FORMER IAW SRM 51-30-02, 51-30-05, 51-10-05, AND 51-10-03.

Part: CUSP WEB — CORRODED (BS 935-947) · corrosion level 2 · airframe 37,899 hrs · 24,127 cycles

CORROSION ON LT CUSP WEB, BS 935-947, X= 54 - 60. REPAIRED IAW SRM 53-20-02, FIG 26.

Part: BEAM — CRACKED (PAX DOOR) · airframe 37,899 hrs · 24,127 cycles

CRACK ON FORWARD EDGE BEAM NR 4 AT FORWARD SERVICE DOOR R1. R & R BEAM IAW SRM 51-10-05, 51-10-03, 51-30-01, 51-30-02, 51-30-04, 51-30-05 AND DWG 9911582, REV T.

Part: SEAT TRACK — CORRODED (BS 470-526) · corrosion level 2 · airframe 37,899 hrs · 24,127 cycles

CORROSION ON RIGHT SEAT TRACK BS 470-526, X=54. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-40-01.

Part: FLOORBEAM — CORRODED (BS 256) · corrosion level 2 · airframe 37,899 hrs · 24,127 cycles

CORROSION ON FLOORBEAM BS 256 BETWEEN X=22 - -22. FLOORBEAM WAS R & R IAW SRM 51-30-01 AND 51-10-03.

Part: SUPPORT — BROKEN (BS 561-674) · airframe 37,899 hrs · 24,127 cycles

RT SLANT SUPPORTS BROKEN, BS 561, 655 AND 674. REPLACED IAW SRM 412241-14MA, REV C.

Part: CUSP WEB — CORRODED (BS 910-913) · corrosion level 2 · airframe 37,899 hrs · 24,127 cycles

CORROSION ON RT CUSP WEB, BS 910-913, X= 54-60. TASK 53-211-02. REMOVED CORROSION IAW SRM 53-20-02 AND 51-10-03.

Part: FLOORBEAM — CORRODED (BS 522) · airframe 37,899 hrs · 24,127 cycles

CORROSION ON FLOORBEAM BS 522 BETWEEN LONGERON 28R AND 28L. R & R THE FLOORBEAM IAW SRM 51-30-02, 51-10-05, 51-10-03.

Part: SKIN — CORRODED (BS 1117-1193) · airframe 37,899 hrs · 24,127 cycles

CORROSION ON LT OUTER SKIN, BS 1117-1193, BETWEEN LONGERONS 18-30L. CORROSION WAS REMOVED IAW SRM 51-10-03 AND 53-30-01.

Part: CUSP WEB — CORRODED (BS 902-947) · airframe 37,899 hrs · 24,127 cycles

RT CUSP WEB CORRODED, BS 902-947, X=44-54. AREA OUT OF LIMITS, REPAIRED WITH NRC 98.

Part: LONGERON — CRACKED (BS 1475) · airframe 37,899 hrs · 24,127 cycles

CRACKED LONGERON END OF LONGERON 2R AND 2L, BS 1475 AT AFT ACCESSORY COMPARTMENT. R & R IAW SRM 51-30-05 AND 51-10-03. LP 1945580.

Part: NUT — CORRODED (BS 511-521) · corrosion level 2 · airframe 37,899 hrs · 24,127 cycles

CORROSION ON CHANNEL NUTS BETWEEN BS 511-521 FIXED L/E INNER STRUCTURE RT WING. CHANNEL NUTS WERE REPLACED IAW SRM 51-30-02. LP 1945567.

Part: ARM — CORRODED (SPOILER) · airframe 41,699 hrs · 26,397 cycles

CORROSION ON REACTION ARM OF RIGHT OUTBOARD FLIGHT SPOILER. REPLACED THE ARM.

Part: BEAM — CRACKED (L1 DOOR) · airframe 37,899 hrs · 24,127 cycles

CRACK ON AFT EDGE BEAM L1 DOOR. REPAIRED IAW SRM 52-10-02, FIG 5.

Part: CARGO TRACK — CORRODED (BS 1277-1307) · airframe 37,899 hrs · 24,127 cycles

CORROSION ON LEFT CARGO TRACK, BS 1277-1307. R & R CARGO TRACK IAW SRM 51-30-05, 51-10-03 AND 51-10-05.

Part: HINGE FITTING — CORRODED (TE FLAP) · airframe 41,699 hrs · 26,397 cycles

CORROSION ON FLAP HINGE FORWARD FITTING XRS 264, LEFT WING. REPLACED THE FITTING.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,699 hrs · 26,397 cycles

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

Part: LONGERON — CRACKED (BS 1053) · airframe 37,899 hrs · 24,127 cycles

CRACKED LONGERON 20L, BS 1053. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-10-01, 51-30-05.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,699 hrs · 26,397 cycles

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

Part: SEAT TRACK — CORRODED (BS 237-256) · airframe 37,899 hrs · 24,127 cycles

CORROSION ON LEFT SEAT TRACK, BS 237-256, RBL 22. FOUND OUT OF LIMITS. R & R THE SEAT TRACK IAW SRM 53-40-01, 51-40-014, 51-10-03, 51-30-01 AND 51-30-05.

Part: SPLICE — CRACKED (RT WING) · airframe 37,899 hrs · 24,127 cycles

CRACKED INNER SPLICE, STA 160 AT FIXED L/E INNER STRUCTURE RT WING. SPLICE WAS REMOVED, FABRICATED AND INSTALLED IAW SRM 57-30-01, 51-10-03 AND 51-30-02.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,699 hrs · 26,397 cycles

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

Part: RIB — CRACKED (VERTICAL STAB) · airframe 37,899 hrs · 24,127 cycles

CRACKED RIB TO ATTACH DOUBLER AT DORSAL FIN L/E, Y=1778. RIB WAS REMOVED, FABRICATED AND INSTALLED IAW SRM 51-30-02 AND 51-10-05. LP 1941655.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 37,899 hrs · 24,127 cycles

CRACKED DOUBLER ON DORSAL FIN LOWER SECTION BS 1474, AT VERTICAL STABILIZER. REMOVED DOUBLER. FABRICATED AND INSTALLED NEW DOUBLER IAW SRM 51-30-02 AND DWG 5910242, REV BV. LP 1941709.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 37,899 hrs · 24,127 cycles

CRACK ON LT ANGLE TO ATTACH VERTICAL STABILIZER INTERNAL BETWEEN, STA 1458-1486, LONGERON 1L - 2L. ANGLE WAS REMOVED, FABRICATED AND INSTALLED IAW SRM 51-30-02 AND 51-30-05. LP 1942004.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 37,899 hrs · 24,127 cycles

CRACK ON RT ANGLE TO ATTACH INTERNAL VERTICAL STABILIZER BETWEEN FS 1458-1486, LONGERON 1R-2R. ANGLE WAS REMOVED, FABRICATED AND INSTALLED IAW SRM 51-30-02 AND 51-30-05. LP 1942008.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,690 hrs · 26,392 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF ACCESS PANEL 620AT. FOUND OUT OF LIMITS. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,699 hrs · 26,397 cycles

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

Part: SEAT TRACK — CORRODED (BS 1281-1282) · airframe 37,899 hrs · 24,127 cycles

CORROSION ON SEAT TRACK, BS 1281-1282, X=22. REPAIRED IAW SRM 53-40-01, FIG 2, PARA 6.

Part: SEAT TRACK — CORRODED (BS 1281-1282) · airframe 37,899 hrs · 24,127 cycles

CORROSION ON SEAT TRACK, BS 1281-1282, X=22. REPAIRED IAW SRM 53-40-01.

Part: SEAT TRACK — CORRODED (BS 921-923) · corrosion level 2 · airframe 37,899 hrs · 24,127 cycles

CORROSION ON SEAT TRACK, BS 921-923, X=44. REPAIRED THE SEAT TRACK IAW SRM 53-40-01, FIG 2, PARA 6.

Part: SEAT TRACK — CORRODED (BS 290-295) · corrosion level 2 · airframe 37,899 hrs · 24,127 cycles

CORROSION ON SEAT TRACK, BS 290-295, X=54. REPAIRED THE SEAT TRACK IAW SRM 53-40-01, FIG 2, 51-10-03, 51-10-05 AND 51-30-01.

Part: SEAT TRACK — CORRODED (BS 1053-1054) · airframe 37,899 hrs · 24,127 cycles

CORROSION ON SEAT TRACK, BS 1053-1054, X=54. PLUG WAS ADJUSTED AND INSTALLED IAW SRM 53-40-01 AND 51-30-01. LP 1939133.

Part: SEAT TRACK — CORRODED (BS 200-242) · airframe 37,899 hrs · 24,127 cycles

CORROSION ON RT SEAT TRACK BS 200-242. REPLACED SEAT TRACK IAW SRM 53-40-01.

Part: SEAT TRACK — CORRODED (BS 1264-1270) · airframe 37,899 hrs · 24,127 cycles

CORROSION ON SEAT TRACK, BS 1264-1270, X=54. REPAIRED IAW SRM 53-40-01, 51-10-03 AND 51-30-01.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 37,899 hrs · 24,127 cycles

CORROSION ON FLOOR SUPPORT FS 160-200. R & R FLOOR SUPPORT IAW SRM 51-30-02, 51-10-03, 51-10-05 AND 53-10-01.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 37,899 hrs · 24,127 cycles

CORROSION ON FLOOR SUPPORT BS 160-200. R & R THE FLOOR SUPPORT IAW SRM 51-30-02, 51-10-03, 51-10-05 AND 53-10-01.

Part: WEB — CRACKED (BS 1412) · airframe 37,899 hrs · 24,127 cycles

CRACKED WEB BEHIND CONTOL CABLES PULLEY, BS 1412, X=16. DAMAGE ON WEB WAS REWORKED IAW SRM 51-30-02, 53-00-01 AND 51-10-03, 51-30-05.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,690 hrs · 26,392 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 520LB. FOUND OUT OF LIMITS. REPLACED THE ACCESS PANEL.

Part: PAN — CRACKED (CARGO DOOR) · airframe 37,899 hrs · 24,127 cycles

CRACK ON MID CARGO COMPARTMENT DOOR INNER PAN BELOW FORWARD ANGLE BETWEEN 1 AND 2. REPAIRED IAW SRM 52-30-02, FIG 3. LP 1933267.

Part: HINGE — CORRODED (ELEVATOR) · airframe 37,899 hrs · 24,127 cycles

CORROSION ON HINGE NR 6 OF RT ELEVATOR LOCATED ON RT HORIZONTAL STABILIZER REAR SPAR. REWORKED AREA. FOUND TO BE OUT OF LIMITS. REPAIR BUSHING FABRICATED AND INSTALLED IAW CMM AND SRM 51-10-03, PARA 21. LP 1933288.

Part: ACCESS PANEL — CORRODED (WING) · airframe 41,690 hrs · 26,392 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 520CB. FOUND OUT OF LIMITS. REPLACED THE ACCESS PANEL.

Part: WEB — PUNCTURED (BS 168) · airframe 37,899 hrs · 24,127 cycles

PUNCTURES ON WEBS OCCURRED DURING MAINTENANCE STA 168, X=15 AND 177, X=12, CABIN FLOOR STRUCTURE. REPAIRED IAW SRM 53-00-01, FIG 6, 51-10-03, PAR 14-21 AND 51-30-02. LP 1931563.

Part: BEAM — CRACKED (CARGO DOORWAY) · airframe 37,899 hrs · 24,127 cycles

FORWARD STOP FITTING PROJECTION BEAM 5 AND AFT STOP FITTING PROJECTION BEAM 3 AT FORWARD CARGO DOOR CRACKED. HFEC 5. NO CRACKS FOUND. NR 3 STOP FITTING WAS REPLACED IAW SRM 51-30-01 AND 51-30-05. LP 1928677.

Part: WEB — CRACKED (BS 215-218) · airframe 37,899 hrs · 24,127 cycles

CRACK ON DIAPHRAGM BETWEEN BS 215-218 X=54-44, PASSENGER CABIN FLOOR STRUCTURE LT SIDE. REPAIRED IAW SRM 51-11-01.

Part: FLOOR SUPPORT — CORRODED (BS 1022) · airframe 37,899 hrs · 24,127 cycles

CRACK ON FLOOR SUPPORT, BS 1022, X=33. R & R FLOOR SUPPORT IAW SRM 51-30-05.

Part: SKIN — DENTED (BS 351-361) · airframe 37,899 hrs · 24,127 cycles

DENT ON FUSELAGE SKIN BETWEEN FS 351-361, LONGERON 28R. INSPECTED. NO CRACKS FOUND. CONDITION 1A AND DC.

Part: SKIN — DENTED (BS 332-351) · airframe 37,899 hrs · 24,127 cycles

DENT ON FUSELAGE SKIN BETWEEN BS 332-351, LONGERON 24 - 25R. INSPECTED. NO CRACKS FOUND.

Part: PIN — UNSECURE (L1 DOOR SLIDE) · airframe 37,073 hrs · 23,631 cycles

L1 DOOR SLIDE LOOSE. FOUND RETAINING PIN PULLED. R & R L1 SLIDE IAW AMM.

Part: PIN — DETACHED (DOOR SLIDE) · airframe 35,715 hrs · 22,735 cycles

PARACHUTE PINS ON FORWARD SERVICE DOOR SLIDE ARE DETACHED. R & R FORWARD SERVICE DOOR SLIDE IAW AMDS 2561-4641.

Part: FRAME — CRACKED (BS 1531) · airframe 34,620 hrs · 22,083 cycles

CANTED FRAME WEB, BS 1531, RBL 20 FORWARD SIDE CRACKED. CUT OUT CRACK. INSTALLED REPAIR ERA 522695-14, REV O.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 34,620 hrs · 22,083 cycles

TAILCONE RELEASE BOTTLE ATTACH CABLE FRAYED. R & R TAILCONE RELEASE BOTTLE CABLE IAW AMM.

Part: GUIDE — DAMAGED (TAILCONE RELEASE) · airframe 34,620 hrs · 22,083 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND TAILCONE EXTERIOR EMREGENCY EXIT PULL HANDLE ANGLE BROKEN. R & R ANGLE GUIDE ON TAILCONE EXTERIOR EMERGENCY EXIT PULL HANDLE. OPS CHECKED GOOD IAW AMDS 5352-7116, STEP 5, A-1-A.

Part: HANDLE — BROKEN (TAILCONE RELEASE) · airframe 34,620 hrs · 22,083 cycles

EXTERIOR TAILCONE PULL RELEASE HANDLE BROKEN. REPAIR ACCOMPLISHED ON NR 124.

Part: SKIN — CRACKED (BS 1542) · airframe 34,620 hrs · 22,083 cycles

FUSELAGE EXTERIOR SKIN CRACKED AT CANTED FRAME BS 1542. STOP DRILLED CRACK. INSTALLED DOUBLER IAW SRM 53-00-01, FIG 4.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,215 hrs · 21,828 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND AFT EMERGENCY LIGHTS IN TAIL COMPARTMENT INOPERATIVE. R & R POWER SUPPLY AND BATTERY IAW AMM. OPS CHECKED GOOD.

Part: COALESCER BAG — CONTAMINATED · airframe 33,736 hrs · 21,517 cycles

PRIOR TO TOP OF DECENT, CABIN EMERGENCY LIGHT ILLUMINATED. LIGHT BEGAN FLICKERING FOLLOWED BY SMOKE COMING FROM FROM THAT AREA. DIVERTED, MX FOUND CEILING PANELS FULL OF WATER . WATER SEPERATOR DRAIN LINES CLEAR. DRIED OVERHEAD AREA AND LIGHT ASSEMBLIES. REPLACED COELESCER BAGS. RAN PACKS , CYLCLED ALL LIGHTS. ALL OPS CHECK NORMAL. INSPECTED LIGHT ASSEMBLIES . NO SIGNS OF BURNING OR ARCING. ACFT OK FOR SERVICE.

Part: TERMINAL — DAMAGED (EMERGENCY LIGHT) · airframe 33,254 hrs · 21,229 cycles

EXTERIOR EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK AND CONTROLLER IAW AMM 33-51-03. REPAIRED DAMAGED TERMINAL. OPS CHECKED GOOD.

Part: CONTROLLER — FAILED (A/C PACK) · airframe 33,059 hrs · 21,119 cycles

DECLARED MEDICAL EMERGENCY ON FINAL. RT PACK UNABLE TO COOL ACFT. MULTIPLE PEOPLE BECAME ILL ON FLIGHT AND ONE PASSENGER PASSED OUT DUE TO CABIN BECOMING UNCOMFORTABLY HOT. MX TROUBLESHOT AND REMOVED AND REPLACED PACK AUTO TEMPERATURE CONTROLLER AND ANTICIPATOR. RAN PACKS, CHECKS NORMAL. PRESSURIZED ACFT TO 7PSID, MAINTAINED 42F. RAN PACK WITH ENGINE AT CRUISE POWER WITH NO TROUBLE NOTED.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,981 hrs · 21,080 cycles

DURING SERVICE CHECK, TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. R & R POWER SUPPLY AND BATTERY IAW AMM. OPS CHECKS GOOD.

Part: CONTROL PANEL — INOPERATIVE (SMOKE DETECTION) · airframe 32,267 hrs · 20,674 cycles

PERFORMED AN AIR TURN BACK. AT CRUISE, FL 310, ALL FAIL LIGHTS ILLUMINATED ON THE OVERHEAD CARGO DETECTION ANNUNCIATOR PANEL. NO AURAL INDICATION. SMOKE DETECTOR LOOP LIGHT ON CAPTAINS FORWARD PANEL. EMERGENCY DECLARED, REPLACED THE CARGO CONTROL SMOKE DETECTOR PANEL IAW AMM. OPERATION CHECKS OK.

Part: CABLE — OUT OF RIG (TAIL) · airframe 31,182 hrs · 20,118 cycles

DURING INSPECTION AND RIG CHECK OF CATWALK, MX FOUND CABLE TENSIONS LOW. ADJUSTED LIFT CABLE TENSIONS IAW AMM. OPS CHECKS GOOD.

Part: SKIN — DAMAGED (BS 313-712) · airframe 29,946 hrs · 19,429 cycles

FUSELAGE SKIN LIGHTNING STRIKE LT WINDOW BELT BS 313-712. REPAIRED IAW ERA 500853-14.

Part: NONE — NONE (NONE) · airframe 29,946 hrs · 19,429 cycles

FUSELAGE SKIN REPAIR DOCUMENTATION, STA 1475 L3L-3R REPAIRED IAW ERA 500855-14__LOG PAGE 0637754

Part: SKIN — UNKNOWN (BS 522, L21-22R) · airframe 29,943 hrs · 19,427 cycles

FUSELAGE SKIN REPAIR INSPECTION STA 522, L21-22R. REPAIRED IAW ERA 500852-14

Part: SKIN — UNKNOWN (BS 229-275) · airframe 29,943 hrs · 19,427 cycles

FUSELAGE SKIN DEPRESSION INSPECTION BS 229-275, L11-15L. REPAIRED IAW ERA 500854-14

Part: SKIN — DENTED (FUSELAGE) · airframe 29,943 hrs · 19,427 cycles

DENT LEFT SIDE OF FUSELAGE EXTERNAL STA 237 AND L17. CUT OUT DAMAGED AREA AND REPAIRED SKIN BY INSTALLING REPAIR DOUBLER AND FILLER PER MD90 SRM 53-31-02 FIG 2.

Part: SKIN — CRACKED (RUDDER) · airframe 29,943 hrs · 19,427 cycles

RUDDER SKIN CRACKED AT NR 3 HINGE CUTOUT RT SIDE. REPAIRED RUDDER SKIN AT NR 3 HINGE CUTOUT PER MD 90 SRM 55-41-01 PAGES 111 AND 112 AND PERFORMED WEIGHT AND BALANCE USING CHECK WEIGHT METHOD WITHIN LIMITS PER MD90 SRM 55-40-01.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 29,943 hrs · 19,427 cycles

FIXED ELT DEACTIVATION APPROX STA 1374. REMOVED ELT ANTENNA AND REPAIR WAS ACCOMPLISHED ON FUSELAGE PER SRM 53-30-01, 53-31-03 REF EA 02-477733-03 REV D ME 04 OPN 0401.

Part: SUPPORT FITTING — DAMAGED (LT MLG) · airframe 29,943 hrs · 19,427 cycles

INSPECT AND REPLACE LT MLG ACTUATOR SUPPORT FITTING. DAMAGE FOUND PER STEPS 5 & 6 PER EA02-093855-03AD REV A. AAR N/R 838261 GENERATED FOR BEARING BORE AND BUSHING BORE. INSTALLED NEW SUPPORT BEARING, BUSHING, AND FITTING PER EA 02-093855-03AD REV A OPN 0101.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,943 hrs · 19,427 cycles

FIXED ELT DEACTIVATION APPROX STA 1374. REMOVED ELT ANTENNA AND REPAIR WAS ACCOMPLISHED ON FUSELAGE PER SRM 53-30-01 REF ERA 02-477733-03 REV D ME04 OPN 0401. REF AAR N/R 838287.

Part: FITTING — CORRODED (RT MLG) · airframe 29,943 hrs · 19,427 cycles

ITEM INSPECT MLG RETRACT ACTUATOR FITTING REF EA 02-093855-03AD REV A.OPN 0201 ME02 E -151.

Part: SPAR CAP — UNKNOWN (VERTICAL STAB) · airframe 29,942 hrs · 19,426 cycles

VERTICAL STABILIZER L/E FRONT SPAR CAP REPAIRED IAW AA 5530-01044.

Part: STOP FITTING — UNKNOWN (CARGO DOOR) · airframe 29,942 hrs · 19,426 cycles

CARGO DOOR STOP PAD FITTINGS REPAIRED IAW AA 5230-01136.

Part: JACKSCREW — UNKNOWN (HORIZONTAL STAB) · airframe 29,942 hrs · 19,426 cycles

HORIZONTAL STABILIZER JACKSCREW ASSY, REPAIRED IAW AA 2740-01071.

Part: RIB — UNKNOWN (HORIZONTAL STAB) · airframe 29,942 hrs · 19,426 cycles

HORIZONTAL STABILIZER HINGE RIB PIVOT BEARING LUG REPAIRED IAW AA 5510-01083.

Part: SUPPORT FITTING — UNKNOWN (MLG ACTUATOR) · airframe 29,942 hrs · 19,426 cycles

MLG ACTUATOR SUPPORT FITTING REPAIRED IAW AA 5740-01140.

Part: FRAME — UNKNOWN (BS 883 - BS96) · airframe 29,942 hrs · 19,426 cycles

BS 883-BS962 OVERWING FRAMES REPAIRED IAW AA 5310-01375.

Part: SPAR — CRACKED (WING) · airframe 29,942 hrs · 19,426 cycles

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

Part: SUPPORT FITTING — UNKNOWN (PYLON) · airframe 29,942 hrs · 19,426 cycles

PYLON AFT SUPPORT FITTING UPPER FASTENERS REPAIRED IAW AA 5440-01069.

Part: SKIN — UNKNOWN (HORIZONTAL STAB) · airframe 29,942 hrs · 19,426 cycles

HORIZONTAL STABILIZER UPPER CENTER SKIN PANEL REPAIRED IAW AA 5510-01085.

Part: CLAMP — MISSING (NR 1 ENGINE) · airframe 29,939 hrs · 19,425 cycles

NR 1 ENGINE SHUTDOWN ON IT'S OWN DURING MAINTENANCE FERRY FLT MZJ TO ATL. FLIGHT CREW RETURNED AIRCRAFT TO MZJ. MAINTENANCE FOUND A CLAMP WAS MISSING ON THE COWL ANTI ICE VALVE ALLOWING HOT AIR TO BLOW ON THE EEC AND THE ANTI ICE VALVE. MAINTENANCE REPLACED THE ANTI ICE VALVE, EEC, AND DUCT CLAMP (RC NOTIFIED OF EVENT BY MCC. NO LOG PAGE AT THIS TIME.)

Part: SKIN — CRACKED (CARGO DOOR) · airframe 29,938 hrs · 19,424 cycles

DEFORMATION AND CRACK ON FWD CARGO DOOR INNER SKIN PANEL, NEAR DOOR LOCK HOOK. REPIARED IAW SRM 52.

Part: SKIN — CRACKED (BS 1475) · airframe 29,938 hrs · 19,424 cycles

CRACK REPAIR ON TAIL SKIN AT STA 1475, STR 2L AND 3L. REPAIRED IAW SRM 55.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 29,938 hrs · 19,424 cycles

CRACK REPAIR ON LEFT DORSAL FIN ATTACH ANGLE IAW SRM 53

Part: BEAM — UNKNOWN (BS 693-750) · airframe 29,938 hrs · 19,424 cycles

CORROSION REPAIR ON MID CARGO DOOR JAMB BEAM AT STA 693-750. REPAIRED IAW SRM 53.

Part: SKIN — DAMAGED (BS 389-446) · airframe 29,938 hrs · 19,424 cycles

LIGHTNING STRIKES ON RT WINDOW BELT AT BS 389-446. REPAIRED IAW SRM 53.

Part: SKIN — DAMAGED (BS 313-712) · airframe 29,938 hrs · 19,424 cycles

LIGHNING STRIKES ON LT WINDOW BELT AT BS 313-712. REPAIRED IAW SRM 53.

Part: BEAM — UNKNOWN (BS 1211-1269) · airframe 29,938 hrs · 19,424 cycles

CORROSION REPAIR ON AFT CARGO DOOR JAMB BEAM AT STA 1211-1269REPAIRED IAW SRM 53

Part: SKIN — DENTED (BS 229-275) · airframe 29,938 hrs · 19,424 cycles

DENT ON SKIN AT STA 229-275, L11-15LHREPAIRED IAW SRM 53

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 29,938 hrs · 19,424 cycles

AFT CARGO DOORWAY LOWER JAMB BEAM CORRODED. REPAIRED IAW ERA 398119-14