N557CM

Part: FIRE BOTTLE — DISCHARGED (CARGO BAY) · airframe 77,347 hrs · 28,136 cycles

ENROUTE FLIGHT ATN531, CREW REPORTS-MSG DISPLAY NR 1 LOWER CARGO FIRE EXTINGUISHER BOTTLE DISCHARGED. POST LANDING, MAINTENANCE VERIFIED BOTTLE DISCHARGED. FIRE BOTTLE RECHARGED. INITIATED DEFERRAL MAINTENANCE ITEM 54132 CAT C.BY ELECTRICAL METHOD BOTTLE WILL BE VERIFIED TO BE FULLY CHARGED EACH DAY DEFERRAL REMAINS ACTIVE. WORK IN PROGRESS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 75,764 hrs · 26,943 cycles

LEFT EXTERIOR EMERGENCY ESCAPE LIGHT INOPERATIVE. RELAMPED LEFT EXTERIOR EMERGENCY ESCAPE LIGHT IAW AMM 33-51-06. OPERATIONAL CHECK SATISFACTORY. FAULT NOT DUPLICATED. AIRCRAFT RELEASED TO SERVICE.

Part: SKIN — CRACKED (THRUST REVERSER) · airframe 75,676 hrs · 26,896 cycles

NR 1 ENGINE OUTBOARD COWL LOWER BIFURCATION SKIN IS CRACKED AND DELAMINATED. IAW 757 SRM 54-31-01 CRACK AND DELAMINATION ARE OUT OF LIMITS. #1 ENGINE OUTBOARD THRUST REVERSER COWL WAS REMOVED AND REPLACED IAW 757 AMM 78-31-01. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT WAS RELEASED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 75,040 hrs · 26,568 cycles

LOWER FLASHLIGHT UNDER SUPERNUMERARY SEAT NOT RECEIVING POWER. DEFERRED IAW MEL 25-63-04-01. DEFERRED MX ITEM 47254 INITIATED. NO FLY DATE 05 17 2016. R & R EMER FLASHLIGHT IAW AMM 25-64-00. OPERATIONAL CHECKED SATISFACTORY. DMI CLEARED & ACFT RELEASED TO SERVICE.

Part: SKIN — DENTED (BS 560) · airframe 75,036 hrs · 26,566 cycles

RIGHT FUSELAGE HAS A DENT FORWARD OF THE FORWARD CARGO DOOR BS 560, STR 24R GM014. MECHANCICALLY MEASURED DENTED AREA AT EXTERNAL FUSELAGE SKIN, FOUND TO BE WITHIN 2" OF FORWARD LOWER CARGO DOOR CUTOUT AND OUT OF LIMITS IAW SRM 757-200, CHAPTER 53-00-01, FIGURE 101, DETAIL III. ACCOMPLISHED ATI EO 52-757-5455, REV IR. ACCOMPLISH REPETITIVE INSPECTIONS AT EVERY A-CHECK AND PERFORMED PERMANENT REPAIR AT NEXT C-CHECK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 73,631 hrs · 25,778 cycles

RIGHT ESCAPE ROPE EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED RT EXTERIOR ESCAPE ROPE EMER LIGHT IAW AMM 33-51-09 301. OPERATIONAL CHECK SATISFACTORY.

Part: SUPPORT ANGLE — CRACKED (NR 2 NACELLE) · airframe 72,895 hrs · 25,396 cycles

NUMBER 2 NACELLE INSIDE PANEL 445AR-BR, OTBD OF DIAGONAL BRACE FWD ATTACH POINT. SUPPORT ANGLE AT FWD CHORD, CRACKED AT FASTENER HOLE TO EDGE. CRACK APPROX 1/4 INCH VERIFIED BY HFEC. CRACK LENGTH .6 INCHES, LOCATION NAC STATION 206.00 TO N/A. PART NAME BRACKET, PART NUMBER 313N353-24, SN N/A. SUPPORT ANGLE WAS R & R IAW SRM 51-40-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,895 hrs · 25,396 cycles

STATION 654 & 2 STRINGER 11L CRACKED 1/2 INCH. R & R CRACKED STRINGER SECTION IAW SERVICE BULLETIN 368-53-041 & SRM 53-00-03-B67.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 71,741 hrs · 24,607 cycles

BS 1681, FRAME LOWER SHEAR TIE CORRODED ON AFT SIDE BETWEEN STRINGER 29R TO 29L. REPAIRED ON FAS WO 21197 NR 34087.

Part: SKIN — DENTED (L3 DOOR) · airframe 71,741 hrs · 24,607 cycles

L3 DOOR SKIN HAS A DENT BETWEEN STR 15-16L. REPAIRED ON FAS WO 21197.

Part: SKIN — DENTED (ZONE 200) · airframe 71,741 hrs · 24,607 cycles

AT BS 405 BETWEEN STR 15 - 16L SKIN IS DENTED. REPAIRED FAS WO 21197.

Part: SKIN — CORRODED (ZONE 500) · airframe 71,741 hrs · 24,607 cycles

LT WING UPPER SURFACE HAS AREA OF CORROSION AT REAR SPAR 35" OTBD OF FUSELAGE BS 1060. REPAIRED ON FAS WO 21197, NR 33916.

Part: FRAME — DAMAGED (ZONE 200) · airframe 71,741 hrs · 24,607 cycles

BS 418, STR 8R, FRAME HAS EXISTING .1875 HOLE WITH NO ED. REPAIRED ON FAS WO 21197.

Part: SKIN — DENTED (ZONE 100) · airframe 71,741 hrs · 24,607 cycles

FUSELAGE SKIN DENTED, BS 600 STR 28 TO 29L. REPAIRED ON FAS WO 21197.

Part: FRAME — CRACKED (ZONE 200) · airframe 71,741 hrs · 24,607 cycles

FUSELAGE INTERIOR FRAME CRACKED AT BS 1640, STRINGER 14R. REPAIRED ON FAS WO 21197.

Part: SKIN — DENTED (ZONE 200) · airframe 71,741 hrs · 24,607 cycles

LT SIDE OF FUSELAGE SKIN HAS SEVERAL DENTS BS 1681 TO 1720, STRINGER 14L TO STRINGER 20L. REPAIRED ON FAS WO 21197 NR 33876.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 71,741 hrs · 24,607 cycles

AFT PIT BILGE AREA, INTERCOSTAL LOWER ANGLE HAS CORROSION AT BS 1475, RBL14. REPAIRED ON FAS WO 21197.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 71,741 hrs · 23,687 cycles

LEFT WING UPPER SURFACE SKIN HAS AREA OF CORROSION AT BS 1003, 4 INCHES OTBD OF FUSELAGE. REPAIRED ON FAS WO 21197.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 71,741 hrs · 24,607 cycles

AFT PIT BILGE AREA, SHEAR TIE AT BS 1440 RBL 3 HAS CORROSION ON FWD SIDE. REPAIRED ON FAS WO 21197.

Part: SKIN — DENTED (ZONE 100) · airframe 71,741 hrs · 24,607 cycles

LOWER FUSELAGE SKIN HAS A DENT AT BS 1654 BETWEEN STRINGER 27L AND 28L. REPAIRED ON FAS WO 21197, NR 33846.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 71,741 hrs · 24,607 cycles

MAIN CABIN SEAT TRACK AT LBL 45, BS 874 TO 900 HAS SEVERAL GOUGES ON UPPER SURFACE. REPAIRED ON FAS WO 21197 N34204.

Part: SKIN — DENTED (ZONE 100) · airframe 71,741 hrs · 24,607 cycles

LOWER FUSELAGE SKIN HAS A DENT AT BS 1780 JUST BELOW STR 26L. REPAIRED ON FAS WO 21197 NR 33849.

Part: SKIN — DENTED (BS 725) · airframe 71,741 hrs · 24,607 cycles

RIGHT SIDE OF FUSELAGE SKIN HAS A DENT AT BS 725 BETWEEN STRINGERS 20R AND 21R. REPAIRED ON FAS WO 21197, NR 33865.

Part: TEAR STRAP — DAMAGED (ZONE 200) · airframe 71,741 hrs · 24,607 cycles

SCRIBE LINE ON TEAR STRAP AT BS 660 BETWEEN STR 8L-10L. REPAIRED ON FAS WO 21197, NR34183.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 71,741 hrs · 24,607 cycles

CORROSION ON SHEAR TIE AT BS 820 BETWEEN STR 28L-28R. REPAIRED ON FAS WO 21197.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 71,741 hrs · 24,607 cycles

FWD PIT-CORROSION ON SHEAR TIE AT BS 800 BETWEEN STR 28L-28R. REPAIRED ON FAS WO 21197.

Part: SHEAR TIE — CORRODED (BS 800) · corrosion level 2 · airframe 71,741 hrs · 24,607 cycles

FWD PIT-- CORROSION ON SHEAR TIE AT STA 800 BETWEEN STR 28L-28R. REPAIRED ON FAS WO 21197 NR 24261.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 71,741 hrs · 24,607 cycles

FLOORBEAM AT BS 395 RBL 51 HAS CORROSION ON UPPER FLANGE. REPAIRED ON FAS WO 21197.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 71,741 hrs · 24,607 cycles

MAIN CABIN SEAT TRACK HAS DAMAGED UPPER LUG AT BS 1190, RBL 24. REPAIRED ON FAS WO 21197 NR 34194.

Part: STRINGER — CRACKED (ZONE 200) · airframe 71,741 hrs · 24,607 cycles

STRINGER 2L CRACKED AT BS 336. REPAIRED ON FAS WO 21197.

Part: SKIN — DENTED (ZONE 100) · airframe 71,741 hrs · 24,607 cycles

LOWER FUSELAGE SKIN HAS A DENT AT BS 592 BETWEEN STRINGER 26 TO 27L. REPAIRED ON FAS WO 21197.