N19638

Part: STRINGER — CORRODED (FUSELAGE) · airframe 35,170 hrs · 18,398 cycles

SUPPORT TASK FWD BAG BIN STRINGER 28R END FITTING STA 482B HAS CORROSION IN OUTBD FLANGE. REPAIRED STRINGER 28R REF ECRA 5311-01507.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 35,170 hrs · 18,398 cycles

SUPPORT TASK,VERTICAL STABILIZER L/E HAS A BIRD STRIKE APPROX 41 INCHES FROM LOWER END CUT OUT DAMAGED SECTION OF LEADING EDGE, FABRICATED DOUBLER AND FILLER. INSTALLED REPAIR REF SRM 55-30-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,170 hrs · 18,398 cycles

SUPPORT TASK - CORR ON FWD SIDE OF FRAME AT STA 482B O/B OF STR 28RT. INSTALLED NEW SKIN CLIP (SHEAR TIE) REF SRM 51-40-2.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,170 hrs · 18,398 cycles

SKIN BLENDED OVER FRAME AT STA 380 JUST ABOVE STR 17 LT INSTALLED REPAIR PER ECRA 5331-01535 NEED TO RE-INSPECT BEFORE THE ACCUMULATION OF 78398 TOTAL FLY CYCLES PER ECRA 5331-01535 PART 2 REF DIP # 007353. INTERIM REPAIR ACCOMPLISHED PER ECRA 5331-01535, PART 1. BEFORE THE ACCUMULATION OF 78,398 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM AN INSPECTION PER PART 2 OF ECRA 5331-01535. PLANNING TO CONTACT ENGINEERING AFTER ACCUMULATION OF 71,000 TOTAL FLIGHT CYCLES BUT BEFORE 72,000 TOTAL FLIGHT CYCLES FOR INSP DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,170 hrs · 18,398 cycles

SUPPORT TASK STEP 20 OF EA 5330-03736 OP 3 HOLE 11 HAS CRACK INDICATION INSTALLED REPAIR PER ECRA 5330-04070 NEED TO RE-INSPECT BEFORE THE ACCUMULATION OF 73398 TOTAL FLT CYCLES PER ECRA 5330-04070 PART 2 REF DIP 007371. REPAIR HOLE PER ECRA 5330-04070 PRIOR TO ACCUMULATION OF. PRIOR TO THE ACCUMULATION OF 73,398 TOTAL AIRCRAFT 73.398 FLT CYCLES PERFORM AN INSPECTION PER PART 2 OF ECRA 5330-04070 PLANNING TO CONTACT ENG AFTER 66,000 TTL FLT CYC BUT BEFORE 67,000 TTL FLT CYC FOR INSPECTION DETAILS.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 35,170 hrs · 18,398 cycles

SUPPORT TASK - REMOVE L-1 LOWER HINGE FITTING TO FACILITATE OTHER MAINTENANCE. REMOVED AND REPLACE LWR HINGE FITTING REF SRM 51-40-02.

Part: SKIN — DENTED (CARGO DOOR) · airframe 35,170 hrs · 18,398 cycles

SUPPORT TASK - FWD CARGO DOOR SKIN IS DENTED 12 INCHES FROM TOP OF DOOR & 22 INCHES FROM FWD EDGE DENT MEASURED 1.9 X 3 X .066 A/Y=28 INSTALLED REPAIR PER SRM 52-00-01 FIG 201 PEPAIR 3. FCBS EVALUATED AS CAT A REPAIR PER SRM 51-00-04.

Part: SKIN — CRACKED (LE SLAT) · airframe 35,170 hrs · 18,398 cycles

SUPPORT TASK - NR 1 SLAT CRACKED AT NR 2 AUX-TRACK FROM I/B, MARKED. CUT AND REMOVED DAMAGED SKIN, FABRICATED FILLER AND SPLICE PLATE. TREATED, PRIMED INSTALLED REPAIR PARTS REF SRM 57-43-01 REPAIR 6.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,170 hrs · 18,398 cycles

SUPPORT TASK - WHEN PERFORMED EA 5310-04437 OP 2 INSP FOUND CRACKED FRAME AT STA 360 BETWEEN STR 8L & 9L. INSTALLED REPAIR ON FRAME AT STA 360 BETWEEN STR 8L AND 9L REF ECRA 5311-01506.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 32,578 hrs · 17,076 cycles

AFT EMERGENCY INBOARD FLASHLIGHT, LEFT SIDE GALLEY INOPERATIVE. REPLACED BATTERY, LED FLASHES WITHIN SERVICEABLE LIMITS.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 29,135 hrs · 15,267 cycles

AIR CONDITIONING SUPPORT BRACKET CRACKED AT RIGHTHAND FRAME STATION 747 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING SUPPORT BRACKET AT RIGHTHAND FRAME STATION 747 BETWEEN S-8 AND S-9 PER EA 5310-04498.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 29,135 hrs · 15,267 cycles

AIR CONDITIONING SUPPORT BRACKET CRACKED AT RIGHTHAND FRAME STATION 787 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING SUPPORT BRACKET AT RIGHTHAND FRAME STATION 787 BETWEEN S-8 AND S-9 PER EA5310-04498.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 29,135 hrs · 15,267 cycles

AIR CONDITIONING SUPPORT BRACKET CRACKED AT LEFTHAND FRAME STATION 440 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING SUPPORT BRACKET AT LEFTHAND FRAME STATION 440 BETWEEN S-8 AND S-9 PER EA 5310-04498.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 29,135 hrs · 15,267 cycles

AIR CONDITIONING SUPPORT BRACKET CRACKED AT LEFTHAND FRAME STATION 827 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING SUPPORT BRACKET AT LEFTHAND FRAME STATION 827 BETWEEN S-8 AND S-9 PER EA5310-04498.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 29,135 hrs · 15,267 cycles

AIR CONDITIONING SUPPORT BRACKET CRACKED AT LEFTHAND FRAME STATION 747 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING SUPPORT BRACKET AT LEFTHAND FRAME STATION 747 BETWEEN S-8 AND S-9 PER EA 5310-04498.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 29,135 hrs · 15,267 cycles

AIR CONDITIONING SUPPORT BRACKET CRACKED AT RIGHTHAND FRAME STATION 380 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING SUPPORT BRACKET AT RIGHTHAND FRAME STATION 380 BETWEEN S-8 AND S-9 PER EA 5310-04498.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 29,135 hrs · 15,267 cycles

AIR CONDITIONING SUPPORT BRACKET CRACKED AT RIGHTHAND FRAME STATION 867 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING SUPPORT BRACKET AT RIGHTHAND FRAME STATION 867 BETWEEN S-8 AND S-9 PER EA5310-04498.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 29,135 hrs · 15,267 cycles

AIR CONDITIONING SUPPORT BRACKET CRACKED AT LEFTHAND FRAME STATION 867 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING SUPPORT BRACKET AT LEFTHAND FRAME STATION 867 BETWEEN S-8 AND S-9 PER EA 5310-04498.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 29,135 hrs · 15,267 cycles

AIR CONDITIONING SUPPORT BRACKET CRACKED AT LEFTHAND FRAME STATION 787 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING SUPPORT BRACKET AT LEFTHAND FRAME STATION 787 BETWEEN S-8 AND S-9 PER EA 5310-04498.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 29,135 hrs · 15,267 cycles

AIR CONDITIONING SUPPORT BRACKET CRACKED AT RIGHTHAND FRAME STATION 827 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING SUPPORT BRACKET AT RIGHTHAND FRAME STATION 827 BETWEEN S-8 AND S-9 PER EA5310-04498.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 29,135 hrs · 15,267 cycles

AIR CONDITIONING SUPPORT BRACKET CRACKED AT LEFTHAND FRAME STATION 907 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING SUPPORT BRACKET AT LEFTHAND FRAME STATION 907 BETWEEN S-8 AND S-9 PER EA 5310-04498.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 29,135 hrs · 15,267 cycles

AIR CONDITIONING SUPPORT BRACKET CRACKED AT RIGHTHAND FRAME STATION 400 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING SUPPORT BRACKET AT RIGHTHAND FRAME STATION 440 BETWEEN S-8 AND S-9 PER EA 5310-04498.

Part: SUPPORT BRACKET — CRACKED (RUDDER PEDAL) · airframe 29,135 hrs · 15,267 cycles

FIRST OFFICER RUDDER PEDAL ASSY, SUPPORT SHAFT BRACKET CRACKED. FABRICATED NEW 69-15295-3 RUDDER PEDDLE BRACKET PER BAC DWG 69-15295.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 29,135 hrs · 15,267 cycles

L-1 DOOR FWD GIRT BAR ATTACH MOUNT AT CABIN FLOOR FOUND CORRODED. REMOVED DAMAGED GIRT BAR ATTACH MOUNT IAW B737 SRM 51-40-02. LOCATED AND DRILLED SERVICEABLE ATTACH FITTING IAW B737 SRM 51-40-02. INSTALLED GIRT BAR FITTING ATTACH MOUNT IAW B737 SRM 51-40-02, L-1 DOOR FWD.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 29,135 hrs · 15,267 cycles

L-1 DOOR AFT GIRT BAR ATTACH MOUNT FOUND CORRODED AT CABIN FLOOR. REMOVED DAMAGED GIRT BAR ATTACH MOUNT IAW B737 SRM 51-40-02. LOCATED AND DRILLED SERVICEABLE MOUNT FITTING IAW B737 SRM 51-40-02. INSTALLED L-1 GIRT BAR AFT FITTING IAW B737 SRM 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 29,135 hrs · 15,267 cycles

AFT CARGO, AT STATION 847 & 4" STRINGER 24R TIE CLIP CORRODED. REMOVED CORRODED STRINGER CHANNEL PER B737 SRM 51-40-02, FABRICATED NEW STRINGER TIE CLIP CHANNEL AT STATION 847+4 STR 24R, TREATED AND INSTALLED STRINGER TIE CLIP CHANNEL AT STATION 847 + 4 STR 24R IAW B737 SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,135 hrs · 15,267 cycles

BS 616 INBOARD CHORD AT RBL 66 IS CRACKED. REPAIRED CRACKED CHORD AT BS 616 IAW ECRA 5311-01158 AND B737-500 SRM 51-40-02.

Part: ANGLE — CORRODED (CARGO BAY) · airframe 29,135 hrs · 15,267 cycles

FWD CARGO FWD RIGHT Z-ANGLE (FWD OF DOOR) HAS CORROSION ON BOTTOM SIDE AT NUT PLATE. REMOVED AND INSTALLED FWD CARGO FWD RIGHT Z-ANGLE FWD OF DOOR PER SRM 53-00-04 AND SRM 51-40-02.

Part: SILL — CORRODED (FUSELAGE) · airframe 29,135 hrs · 15,267 cycles

AFT CARGO DOOR SILL WEB IS CORRODED. REMOVED AND REPLACED CARGO DOOR SILL WEB REF 737-500 SRM 51-40-02.

Part: ANGLE — CRACKED (RT NACELLE) · airframe 29,135 hrs · 15,267 cycles

RIGHT ENGINE PYLON VERTICAL ANGLE AFT SIDE OF PANEL OPENING NR 5858R CRACKED. INSTALLED SUPPORT ASSY 313A1380-214 AND PYLON PANEL 15852R IAW B737 SRM 51-40-02.

Part: ANGLE — CORRODED (L2 DOOR) · airframe 29,135 hrs · 15,267 cycles

L-2 DOOR Z-ANGLE HAS SEVERAL AREAS OF CORROSION STA 951 TO 986.5+12. CORROSION AT L-2 DOOR DETERMINED TO BE BEYOND ALLOWABLE LIMITS PER 737-500 SRM 53-60-15 FIG 101. REMOVED AND REPLACED L-2 DOOR Z-ANGLE, REF 737-500 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,135 hrs · 15,267 cycles

AFT CABIN STATION 927 BL 0, CORROSION AT CLIP NUT HOLE. BLENDED CORROSION, DAMAGE FOUND TO BE OUT OF LIMITS PER 737-500 SRM 53-60-51 FIG 101. REPAIRED FLOORBEAM AT BS 927 BL-0 PER 737-500 SRM REFS, 53-60-51 FIG 201 REPAIR 3, AND 51-70-11 FIG 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,135 hrs · 15,267 cycles

RIGHT SIDE FRAME 907 BETWEEN S-8 AND S-9 AC BRACKET HOLE CRACKED. REPAIRED RIGHT FRAME AT STATION 907 BETWEEN S-8 AND S-9 AC BRACKET PER EA5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,135 hrs · 15,267 cycles

LEFT SIDE STA 400 BETWEEN S-8 AND AC BRACKET FASTENER HOLE CRACKED. REPAIRED LEFT FRAME 400 BETWEEN S-8 AND S-9 PER EA 5310-04498, OP 02.

Part: SLIDE — LOW (R-1 DOOR) · airframe 22,499 hrs · 11,837 cycles

THE R-1 DOOR EMERGENCY ESCAPE SLIDE WAS FOUND TO HAVE LOW PRESSURE. THE R-1 DOOR SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-35.

Part: MOUNT — CORRODED (LAVATORY) · airframe 16,814 hrs · 8,835 cycles

INSPECTION FOUND FORWARD LAV MOUNT CORRODED AT DOOR THRESHOLD AFT CORNER. THE AFT CORNER MOUNT WAS REPLACED IAW ECRA 2540-01436.

Part: ISOLATOR — CRACKED (NR 2 ENGINE) · airframe 16,814 hrs · 8,835 cycles

INSPECTION FOUND A 1 INCH CRACK IN RIGHT ENGINE AFT ISOLATOR ELASTOMER. THE NR 2 ENGINE AFT MOUNT WAS REMOVED AND REPLACED IAW MM 54-42-11.

Part: SUPPORT — GOUGED (NR 1 FLAP TRACK) · airframe 16,814 hrs · 8,835 cycles

INSPECTION FOUND NR 1 FLAP TRACK FAIRING SUPPORT GOUGED AT I/B HINGE LUG. A NEW TRACK FAIRING SUPPORT WAS INSTALLED IAW MM 27-51-71.

Part: MOUNT — CORRODED (GALLEY) · airframe 16,814 hrs · 8,835 cycles

INSPECTION FOUND RT AFT GALLEY FLOOR MOUNT CORRODED. THE FLOOR MOUNT WAS REPLACED IAW ECRA 2540-01305.

Part: ARM — GOUGED (RT WING TE FLAP) · airframe 16,814 hrs · 8,835 cycles

INSPECTION FOUND FAIRING SUPPORT ARM GOUGED AT RIGHT O/B MID FLAP CARRIAGE.REPLACED ARM IAW MM 27-51-34.

Part: ANGLE — CORRODED (R-2 DOOR) · airframe 16,814 hrs · 8,835 cycles

INSPECTION FOUND R-2 DOOR THRESHOLD Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: ANGLE — GOUGED (VERTICAL STAB) · airframe 16,814 hrs · 8,835 cycles

INSPECTION FOUND L-ANGLE AT LT VERTICAL STABILIZER BOTTOM INSIDE PANEL 9507 GOUGED. THE GOUGED SECTION OF L-ANGLE WAS REMOVED AND REPLACED IAW ECRA 5380-01013.