N617AM

Part: STRUCTURE — CORRODED (ZONE 200) · corrosion level 2 · airframe 69,212 hrs · 24,920 cycles

CORROSION ON OUTER CHORD STATION 1640 LEFT BUTTLINE 65. CUT OUT DAMAGED SECTION AND INSTALLED DOUBLER REPAIR PER EA B757-53-022750.

Part: FLOOR SUPPORT — CORRODED (BS 1639-1641) · corrosion level 2 · airframe 69,212 hrs · 24,920 cycles

FLOOR SUPPORT STRUCTURE CORRODED AT STATION 1640. INSTALLED TEE CAP PER EA B757-53-022722 AND BOEING LOR5L53005 DRAWING REPAIR 4 AND FIGURE 1 REPAIR SKETCH.

Part: STRUCTURE — CORRODED (BS 1640-1680) · corrosion level 2 · airframe 69,212 hrs · 24,920 cycles

LEFT NUMBER 4 ENTRY DOOR GUTTER BOX STRUCTURE CORRODED FROM STATIONS 1640 TO 1680. REMOVED AND REPLACED 2 GUTTER BOXES FOR THE LEFT NUMBER 4 ENTRY DOOR, FRAME STATIONS 1640 TO 1680 PER SRM 51-10-02-0G.

Part: FLOOR SUPPORT — CORRODED (ZONE 250) · corrosion level 2 · airframe 69,212 hrs · 24,920 cycles

FLOORBOARD SUPPORT AT CENTER LINE, STATIONS 1660 TO 1680 CORRODED. REPLACED FLOORBOARD SUPPORT PER SRM 51-10-02-0G AND AARD 51-00-05-1, REPAIR 1.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 69,212 hrs · 24,920 cycles

CORROSION TO NUT CLIP HOLE ON FLOORBEAM AT BS 365, RIGHT BUTTLINE 27. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-51-2R 3.

Part: FLOOR PANEL — CORRODED (BS 1681-1720) · corrosion level 2 · airframe 69,212 hrs · 24,920 cycles

CORROSION ON AFT PRESSURE DECK FROM BS 1681 TO 1720. REPLACED AFT PRESSURE DECK SRM 51-10-02-0G.

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 69,212 hrs · 24,920 cycles

FLOORBEAM AT STATION 1681 CORRODED. REPLACEDFLOORBEAM PER SRM 51-10-02-0G.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 69,212 hrs · 24,920 cycles

FRAME FORWARD OF LEFT 4 DOOR STATION 1646.3 AT FLOOR LEVEL AT LEFT BUTTLINE 63 HAS DAMAGE TO A FASTENER HOLE. INSTALLED REPAIR DOUBLER PER THE SRM 51-70-13-0G.

Part: SUPPORT — CORRODED (BS 1640-1680) · corrosion level 2 · airframe 69,212 hrs · 24,920 cycles

RIGHT NUMBER 4 DOOR GUTTER BOX STRUCTURE CORRODED FROM STATIONS 1640 TO 1680. INSTALLED FORWARD GUTTER SUPPORT AND INSTALLED AFT GUTTER SUPPORT ON RIGHT NUMBER 4 DOOR THRESHOLD PER SRM 51-10-02-0G, 51-40-02-0G AND AARD 51-00-05-1, REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,212 hrs · 24,920 cycles

MAIN CABIN FLOOR SUPPORT STRUCTURE EXFOLIATED (BLOWN OUT), AT CENTER LINE FUSELAGE STATIONS 1640 TO 1660. INSTALLED FLOOR SUPPORT AT STATIONS 1640 AND 1660 BEAM PER SRM 51-10-02-0G AND AARD 51-10-05-1, REPAIR 1.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,212 hrs · 24,920 cycles

RIGHT NUMBER 4 DOOR THRESHOLD SUPPORT STRUCTURE CORRODED, STATIONS 1640 TO 1680. INSTALLED THRESHOLD SUPPORT STRUCTURE PER SRM 51-10-02-0G AND AARD 51-00-05-1 REPAIR 1, WITH FASTENERS PER SRM 51-40-02-0G.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,212 hrs · 24,920 cycles

CORROSION ON U-CHANNEL IN THRESHOLD OF RIGHT NUMBER 1 ENTRY DOOR, FRAME STATIONS 324 TO 377. INSTALLED NEW U-CHANNEL AT THE RIGHT NUMBER 1 SERVICE/PASSENGER DOOR PER SRM 51-109-02-0G, AND AARD 51-00-05-1, REPAIR 1.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,212 hrs · 24,920 cycles

FLOORBOARD CREASE ANGLE SUPPORT CORRODED AT STATION 365 AND RIGHT BUTTLINE 64. INSTALLED NEW CREASE ANGLE PER SRM 51-10-02-0G AND AARD 51-00-05-1, REPAIR 1.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 69,212 hrs · 24,920 cycles

FORWARD CARGO DOOR, OUTER SKIN HAS STATIC DISCHARGE WITH MATERIAL LOSS AROUND IT, 12 INCHES AFT OF HANDLE CUTOUT. CUT AND REMOVED DAMAGED AREA PER SRM 52-30-01-2R 4 AND INSTALLED DOUBLER PER SRM 52-30-01.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 69,212 hrs · 24,920 cycles

FORWARD CARGO DOOR, OUTER SKIN HAS STATIC DISCHARGE BURN WITH MATERIAL LOSS AROUND IT, 2 INCHES AFT OF HANDLE CUTOUT. INSTALLED DOUBLER AND FILLER PER SRM 52-30-01.

Part: STRUCTURE — CRACKED (R2 DOOR) · airframe 69,212 hrs · 24,920 cycles

R-2 DOOR DAMAGED/CRACKED AT UPPER HINGE CUTOUT, MKD. R-2 DOOR, INSTALLED REPAIR DOUBLER ON UPPER HINGE CUT OUT PER SRM 52-10-02-2R REPAIR 1 AND EA COMP-52-022490.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,212 hrs · 24,920 cycles

TOP L-ANGLE AT BUTTLINE 0, BETWEEN STATIONS 1200 AND 1220 IS CRACKED AT THE 3RD FROM AFT NUT CLIP HOLE, MRT NO. 035846. INSTALLED NEW L-ANGLE PER AARD SRM 51-10-02-0G AND AARD 51-10-05-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,212 hrs · 24,920 cycles

IN THE AFT CARGO, BELOW THE CABIN FLOOR THE INTERCOSTAL WEB HAS 3 CRACKS BETWEEN STATIONS 1200 AND 1220. INSTALLED NEW INTERCOSTAL PER AARD SRM 51-10-02-0G AND AARD 51-10-05-1.

Part: SKIN — CRACKED (L2 DOOR) · airframe 69,212 hrs · 24,920 cycles

L2 DOOR CRACKED AT UPPER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 52-10-02-2R REPAIR 1 AND EA COMP-52-022491.

Part: TIE DOWN — CORRODED (LAVATORY) · corrosion level 2 · airframe 69,212 hrs · 24,920 cycles

LEFT AFT LAVATORY AFT OUTBOARD TIEDOWN CORRODED. REMOVED AND REPLACED WITH NEW TIEDOWN PER AARD 51-10-05-1, REPAIR 1 AND SRM 51-10-02-9G.

Part: TIE DOWN — CORRODED (LAVATORY) · corrosion level 2 · airframe 69,212 hrs · 24,920 cycles

LEFT AFT LAVATORY AFT INBOARD TIEDOWN CORRODED. INSTALLED NEW TIEDOWN PER SRM 51-10-02-9G AND AARD 51-10-05-1, REPAIR 1.

Part: TIE DOWN — CORRODED (LAVATORY) · corrosion level 2 · airframe 69,212 hrs · 24,920 cycles

LEFT AFT LAVATORY FORWARD OUTBOARD TIEDOWN CORRODED. REMOVED AND REPLACED WITH NEW TIEDOWN PER SRM 51-10-02-9G AND AARD 51-10-05-1, REPAIR 1.

Part: TIE DOWN — CORRODED (LAVATORY) · corrosion level 2 · airframe 69,212 hrs · 24,920 cycles

LEFT AFT LAVATORY FORWARD INBOARD TIEDOWN CORRODED. REMOVED AND REPLACED WITH NEW TIEDOWN PER SRM 51-10-02-9G AND AARD 51-10-05-1, REPAIR 1.

Part: KEELBEAM — CORRODED (RT MLG WW) · corrosion level 2 · airframe 70,106 hrs · 25,257 cycles

CORROSION FOUND AT RIGHT WHEEL WELL KEEL BEAM LOWER CHORD. REMOVED CORROSION AND PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION FOR FASTENER HOLDS WITH NO FINDINGS. BLENDED AREA HAD SEVERAL AREAS OUTSIDE OF SRM LIMITS. REPAIRED IN ACCORDANCE WITH SRM 5340 AND ENGINEERING AUTHORIZATION B757-53-022639.

Part: PUMP — BROKEN (LT ENGINE) · airframe 67,787 hrs · 24,398 cycles

BAQ - INFLIGHT VVI-MIA. CREW REPORTED LEFT ENGINE LOW PRESSURE PUMP MESSAGE WITH A LOSS OF ENGINE POWER. LEFT ENGINE WAS SHUTDOWN (SINGLE ENGINE TIME 20 MINS). EMERGENCY DECLARED FLIGHT DIVERTED BAQ LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE LOW PRESSURE FUEL PUMP THAT WAS BROKEN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,696 hrs · 24,371 cycles

SEAT 3E EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED LAMP FOR SEAT 3E EMERGENCY PATH LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,694 hrs · 23,623 cycles

EMERGENCY LIGHT ABOVE SEATS 24DEF INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT ABOVE SEAT 24DEF. OPS CHECKS NORMAL.

Part: PAN — CRACKED (FUSELAGE) · airframe 65,270 hrs · 23,481 cycles

LEFT DITCHING PAN AT STATION 1155 CRACKED. INSTALLED DITCHING PAN AND FASTNERS AT STATION 1155 LEFT PER SRM 51-10-02-0G PARAGRAPH 8.

Part: SLAT — CORRODED (LT WING) · corrosion level 2 · airframe 65,270 hrs · 23,481 cycles

LEFT WING: THERE IS CORROSION ON THE NUMBER 1 SLAT AT THE OUTBOARD END. INSTALLED DOUBLER PER AARD 57-43-01.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 65,270 hrs · 23,481 cycles

CABIN FLOOBOARD SUPPORT/INTERCOSTAL UPPER ANGLE CRACKED STATIONS 1520 TO 1540. REPLACED UPPER WEB ANGLE AS PER SRM 51-10-02-G8.

Part: RELAY — DEFECTIVE (TE FLAP) · airframe 64,961 hrs · 23,371 cycles

MIA - CREW REPORTED TRAILING EDGE FLAP DISAGREE AND FLAP ISOLATION VALVE STATUS MESSAGE. EMERGENCY DECLARED LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED FIM 25-51-00, NO FAULTS NOTED. REPLACED DEPRESSURIZATION RELAY AS A PRECAUTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: IDG — FAULTY (RT ENGINE) · airframe 64,564 hrs · 23,226 cycles

SJU - INFLIGHT MIA-UVF. CREW REPORTED RIGHT ENGINE GENERATOR DRIVE FAILED IN FLIGHT. FLIGHT DIVERTED SJU LANDED WITHOUT INCIDENT. RIGHT INTEGRATED DRIVE GENERATOR WAS PLACARD AND FLIGHT CONTINUED. REPLACED RIGHT INTEGRATED DRIVE GENERATOR AT LGA. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,415 hrs · 22,806 cycles

EMERGENCY LIGHT AT SEAT 15D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 15D. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,415 hrs · 22,806 cycles

CENTER COACH SEAT EMERGENCY LIGHTS INOPERATIVE. REPLACED CENTER COACH EMERGENCY LIGHT BATTERY PACK M1800. OPS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 63,415 hrs · 22,806 cycles

CENTER COACH SEAT EMERGENCY LIGHTS INOPERATIVE. REPLACED CENTER COACH EMERGENCY LIGHT CHARGER M1800. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,355 hrs · 22,783 cycles

EMERGENCY LIGHTS FROM SEATS 9DEF TO 13DEF INOPERATIVE. REPLACED BATTERY PACK ABOVE CEILING PANEL AT SEAT 9DEF, OPS CHECKS NORMAL.

Part: RELAY — FAILED (CABIN) · airframe 61,921 hrs · 22,263 cycles

BTV - INFLIGHT BOS-ORD. CREW REPORTED STRONG ELECTRICAL ODOR IN COCKPIT AND CABIN. EMERGENCY DECLARED LANDED BTV WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RECIRCULATION FAN HAD OVERHEATED. REPLACED RECIRCULATION FAN AND RELAY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,332 hrs

ORD - SEAT MOUNTED EMERGENCY LIGHTS FOR ROWS 1 TO 6 INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 1 TO 6.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,310 hrs

BOS - MID CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER IN MID CABIN LEFT NUMBER 2 DOOR.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT ROW 11DEF BULL NOSE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 11DEF BULL NOSE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT EXIT PLACARD DAMAGED AT RIGHT AFT OVERWING. REPLACED EMERGENCY LIGHT EXIT PLACARD AT RIGHT AFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 58,777 hrs

JFK EMERGENCY LIGHT AT SEAT 34A MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 34A. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: LENS — MISINSTALLED (EMERGENCY LIGHT) · airframe 58,777 hrs

JFK SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 9A WRONG COLOR. REPLACED LENS FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 9A. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,437 hrs · 58,437 cycles

JFK - EMERGENCY LIGHTS AT MID COACH CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT 20D FOR EMERGENCY LIGHTS AT MID COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,437 hrs · 58,437 cycles

JFK - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT 2A FOR EMERGENCY LIGHTS AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: CONNECTOR — DEFECTIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 29D INOPERATIVE. REPLACED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 29D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,321 hrs

LAX - EMERGENCY LIGHTS AT SEAT 9D AND 15D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT 9D AND 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,893 hrs

MIA - LEFT AFT EMERGENCY LIGHT AT AFT LEFT LAVATORY INOPERATIVE. REPLACED LAMP FOR LEFT AFT EMERGENCY LIGHT AT AFT LEFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,893 hrs

MIA - EXTERIOR EMERGENCY LIGHT AT FORWARD LEFT OVERWING DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT FORWARD LEFT OVERWING DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OVEN — SMOKE (CABIN)

VVI INFLIGHT 922/27JAN - CREW REPORTED SMOKE IN CABIN. TURNED OFF RIGHT AIR RECIRCULATION FAN AND SMOKE DISSIPATED. INSPECTED AND CLEANED AFT GALLEY NUMBER TWO OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — MISWIRED (CABIN)

TUL - EMERGENCY EXIT LIGHTS AT LEFT NUMBER 2 DOOR INOPERATIVE. FOUND WIRING TO LEFT NUMBER 2 DOOR FORWARD LIGHT (L752) WIRED INCORRECTLY TO BATTERY PACK M10799. CORRECTED WIRING AT PLUG ON BATTERY PACK M10799 PER WIRING DIAGRAM 33 51 21 AND 24. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — DETERIORATED (CABIN)

DFW - EMERGENCY LIGHT EXIT MARKER DECAL AT LEFT HAND FORWARD OVERWING EXIT IS DETERIORATED. REPLACED EMERGENCY LIGHT EXIT MARKER DECAL FOR LEFT HAND FORWARD OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

FOUND SEAT MOUNTED EMERGENCY PATH LIGHTING AT 22D INOPERATIVE. REPAIRED CONNECTOR UNDER SEAT 22F. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT MODULE INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT MODULE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — LOOSE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN MID CABIN INOPERATIVE. RECONNECTED LOOSE JUMPER WIRES ON TRACK LIGHT STRIPS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — CHAFED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD CABIN EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING WIRES IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS ILLUMINATED WITH SWITCH OFF. REPLACED EMERGENCY FLOOR PATH LIGHTING CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SERVO — LEAKING (YAW DAMPER)

DFW - FLT 731 - AFTER TAKEOFF DFW DURING CLIMB-OUT, CENTER HYDRAULIC SYSTEM INDICATED FLUID LOSS FOLLOWED BY LOSS OF PRESSURE INDICATION. AIRCRAFT RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED YAW DAMPER SERVO AND SEALING PLATE. SERVICED CENTER HYDRAULIC SYSTEM. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. (M)

Part: SKIN — PUNCTURED (LT MLG DOOR)

AFW - FOUND LEFT MAIN LANDING GEAR DOOR OUTER SURFACE HAS PUNCTURE IN CRITICAL AREA. PER MRB 757-828. (M)