N937DN

Part: ACCESS PANEL — CRACKED (NOT REPORTED) · airframe 44,919 hrs · 36,582 cycles

CRACK AT LEADING EDGE OF FUEL ACCESS PANEL. REPAIRED PER ERA 560110-14.

Part: PIN — DISCONNECTED (EMERGENCY LIGHT) · airframe 44,554 hrs · 36,375 cycles

EMERGENCY LIGHT INOPERATIVE ROW 32. TROUBLESHOT. FOUND PIN DISCONNECTED FROM SPLICE. CONNECTED PIN. OPERATION CHECKED GOOD.

Part: BOTTLE — OUT OF LIMITS (L1 DOOR SLIDE) · airframe 44,314 hrs · 36,243 cycles

L1 DOOR SLIDE BOTTLE PRESSURE IS OUT OF LIMITS. REMOVED AND REPLACED THE SLIDE.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 45,081 hrs · 36,681 cycles

LEFT HORIZONTAL STABILIZER UPPER, AFT SPAR NR 1 AND 2 BARREL NUT BORES WERE FOUND WITH CORROSION. REPAIRED IAW ER/A 549961.

Part: AMPLIFIER — MALFUNCTIONED (FIRE DETECTION) · airframe 42,342 hrs · 35,119 cycles

PERFORMED A DIVERSION DUE TO AN RT ENG FIRE, T-HANDLE RED LIGHT WITH AURAL WARNING "FIRE RIGHT ENGINE" AND RT ENG FIRE DET FAULT EOAP MESSAGE IN CRUISE. MAINTENANCE TROUBLESHOT PER FIM. ALL FIRE LOOP DETECTOR ELEMENTS RESISTANCE CHECKS WERE NORMAL. THE NACELLE OUTBOARD FIRE DETECTOR WAS REMOVED AND REPLACED DUE TO BEING IN POOR CONDITION. THE TECHNICIANS APPLIED POWER TO THE AIRCRAFT AND FOUND AMBER LOOP A & B FAULT LIGHTS ON THE RIGHT ENGINE. MAINTENANCE CONTINUED A DETAILED INSPECTION OF THE RIGHT ENGINE FIRE DETECTION SYSTEM. NO OBVIOUS DAMAGE WAS FOUND. THE NR 2 RIGHT ENGINE FIRE DETECTOR AMPLIFIER WAS REMOVED AND REPLACED PER AMM. THE APU AND RIGHT ENGINE WERE STARTED AND OPERATED ABOVE IDLE POWER. NO FIRE DETECTION SYSTEM FAULTS WERE FOUND AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (BS 962) · airframe 41,793 hrs · 34,829 cycles

UPPER RADIUS OF THE FRAME TAB IS DAMAGED BS 962, RT OF THE OVERWING FRAME. REPAIRED IAW ERA 547722-14, REV O.

Part: STRAP — MISROUTED (TAILCONE) · airframe 41,793 hrs · 34,829 cycles

TAILCONE SLIDE CONNECTION STRAP ROUTED INCORRECTLY. ROUTED STRAP CORRECTLY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,015 hrs · 34,336 cycles

BOTH FORWARD CABIN OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK IAW MM. OPS CHECKS OK.

Part: PANEL — CRACKED (TAILCONE) · airframe 39,053 hrs · 33,154 cycles

DURING A TAILCONE DROP, TAILCONE LOWER T/E PANEL WAS CRACKED AND DENTED. COMPLIED WITH ERA 463180-14MA PERMANENT REPAIR.

Part: UNKNOWN — SMOKE (CABIN) · airframe 38,282 hrs · 32,682 cycles

AFTER LANDING, WHITE/GREY SMOKE FIRST CLASS BACK TO MID CABIN. DIMINSHED VISABILITY. TROUBLESHOT. NO TROUBLE FOUND. R & R COALESCER BAGS AND PERFORMED DUCT BURNOUT. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,802 hrs · 32,394 cycles

AFT TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED THE LAMPS . OPS CHECKED GOOD.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 35,851 hrs · 31,111 cycles

HORIZONTAL STAB SKIN CRACKED. REPAIRED IAW ERA 523708-14AD, SECTION I.

Part: BATTERY PACK — DISCONNECTED (EMERGENCY LIGHTS) · airframe 35,836 hrs · 31,104 cycles

DURING SERVICE CHECK, FOUND TAIL COMPARTMENT UPPER EMERGENCY LIGHTS INOPERATIVE. MX FOUND BATTERY PACK B5-239 DISCONNECTED. RECONNECTED. OPS CHECKED GOOD.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 32,339 hrs · 29,099 cycles

MID CARGO BAY DOOR LOWER FRAME HAS SEVERAL SPOTS OF CORROSION, BS 693-750. REMOVED DAMAGED AREA. DRILLED AND INSTALLED NEW FRAME IAW SRM 51-30-05, 51-10-05, 51-30-02 AND DWG 5930481. ACFT OK FOR SERVICE.

Part: SKIN — DAMAGED (BS 313 L4L) · airframe 32,339 hrs · 29,099 cycles

LIGHTNING STRIKE ON SKIN AT BS 313 L4L. REPAIR ACCOMPLISHED PER DWG SG09530001.

Part: SKIN — DAMAGED (BS 294 L4L) · airframe 32,339 hrs · 29,099 cycles

LIGHTNING STRIKE ON SKIN AT BS 294, L4L. REPAIR ACCOMPLISHED PER DWG SG0953000.

Part: SKIN — DAMAGED (BS 256 L5-6L) · airframe 32,339 hrs · 29,099 cycles

LIGHTNING STRIKE ON SKIN AT BS 256, L5-6L. REPAIR ACCOMPLISHED PER DWG SG09530001.

Part: CHANNEL — DAMAGED (FUSELAGE) · airframe 32,339 hrs · 29,099 cycles

RIGHT WHEEL WELL CUTOUT FORWARD FRAME CHANNEL INBOARD END HAS PIECE BROKEN OFF STA 1003 LBL 10. FABRICATED REPAIR ANGLES AND INSTALLED REPAIR AT RIGHT WHEEL WELL CUTOUT FRAME STA 1003 LBL 10 PER SRM 53-60-02 FIG 6 VOL 1, SRM 51-30-05 VOL 2 AND SRM 51-30-02 VOL 2.

Part: CHANNEL — DAMAGED (FUSELAGE) · airframe 32,339 hrs · 29,099 cycles

LEFT WHEEL WELL CUTOUT, FORWARD FRAME CHANNEL INBOARD END HAS PREVIOUS STOP DRILL BUT AREA IS KNIFED EDGED STA 1003 RBL 10. REMOVED PREVIOUS REPAIR ANGLE (CRACKED), DEBURRED STOP DRILL, FABRICATED AND INSTALLED NEW REPAIR ANGLES PER SRM 53-60-02 FIG 6 VOL AND SRM 51-10-01 PAR 3 VOL 2.

Part: SEAT TRACK — DAMAGED (BS 856-1080) · airframe 32,339 hrs · 29,099 cycles

SEAT TRACK LBL 54.5 FROM BS 856 TO 1080 SPLICE HAS SEVERAL GOUGES AND EXPOSED BARE METAL IN SEVERAL PLACES. REMOVED AND REPLACED SEAT TRACK SECTION PER SRM 53-40-01 FIG 3 VOL I AND 51-30-01 VOL 2.

Part: SKIN — CORRODED (BS 826 L28R) · airframe 32,339 hrs · 29,099 cycles

RIGHT FUSELAGE AT BS 826, L28R SKIN HAS CORROSION. CUTOUT DAMAGED AREA PER SRM 53-31-03 VOL 1. FABRICATED DOUBLER, FILLER AND FOUR FINGER DOUBLERS. INSTALLED FILLER, DOUBLER REPAIR AND FOUR FINGER DOUBLERS PER SRM 51-30-02 AND 51-30-05.

Part: SEAT TRACK — DAMAGED (BS 588-617) · airframe 32,339 hrs · 29,099 cycles

SEAT TRACK AT LBL 22, FROM STA 588 TO FR STA 856 SPLICE HAS SEVERAL GOUGES AND EXPOSED BARE METAL, SEVERAL LOCATIONS. BLENDED GOUGES AT LBL 22 STA 588 TO 856 FROM STA 617 TO 856 WITHIN LIMITS. FROM STA 588 TO 617, SEAT TRACK OUT OF LIMITS PER SRM 53-40-01 FIG 4. LOCATED AND DRILLED NEW SEAT TRACK AT STA 588 TO 647 PER SRM 51-10-05 FIG 1, 53-40-01, FIG6. INSTALLED SEAT TRACK.

Part: SLIDE — NO TEST (TAILCONE) · airframe 32,339 hrs · 29,099 cycles

TAILCONE SLIDE FAILED TO DEPLOY DURING TEST. FOUND SNAP ON SLIDE COVER STRAP WORN. INSTALLED NEW STUD MFG MS 27983-3N. TAILCONE DEPLOYMENT SUCCESSFUL. SLIDE DEPLOYS CORRECTLY. REMOVED AND REPLACED SLIDE.

Part: BOTTLE — DISCHARGED (TAILCONE) · airframe 32,339 hrs · 29,099 cycles

TAILCONE DISCHARGE BOTTLE PRESSURE LOW. SERVICED TAILCONE DISCHARGE BOTTLE PER AMM. CHECKED GOOD.