N949FD

Part: WARNING MESSAGE — ILLUMINATED (ZONE 800) · airframe 59,689 hrs · 31,129 cycles

ON TAKEOFF AT 70 KTS MAIN CARGO DOOR WARNING WITH EICAS MSG. MASTER WARNING HORN SOUNDED. REJECTED TAKEOFF & MESSAGE CLEARED, SECOND ATTEMPT WAS GOOD WITH NO INDICATIONS PRESENT. ENTERED PER CA 219512 AMM: 52-32-00-5-0 AMM: 05-51-14-14-2 PERFORMED OPS CHECK OF MCD PER AMM 52-32-00-5-0, OPS CHECK NORMAL. NO DAMAGE OR EVIDANCE OF POSSABLE HIGH ENERGY STOP PER AMM 05-51-14-14-2. OK FOR SERVICE.

Part: GUST LOCK — DAMAGED (ZONE 800) · airframe 59,608 hrs · 31,054 cycles

L-1 DOOR GUST LOCK BROKEN NOT ALLOWING DOOR TO SHUT PROPERLY. REMOVED BROKEN GUST LOCK COLLAR AND INSTALLED NEW COLLAR S/N 25-0009 PN 140N6008-1 REF INCLUDED MANUAL, NEWER COLLAR IS A FAULTY INSTALLED, SEVERE WEATHER INTERFERED WITH COMPLETION, ITEM NEEDS TO BE REPLACED. RE POSITION HOLD OPEN LOCK COLLAR AS NEEDED REF M/M 52-11-08-8 OPS CK NORMAL ACFT OK FOR SERVICE

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 59,568 hrs · 31,031 cycles

WHEN CONFIGURING FOR APPROACH, SELECTED FLAPS 1. GOT TRAILING EDGE FLAPS DISAGREE EICAS AND ANNUNCIATOR. FLAPS DID NOT MOVE. FLAP LEVER WAS FIRMLY IN THE FLAPS 1 DETENT. REFERENCED THE QRH AND PUT THE FLAPS TO 20 USING THE ALT FLAPS SWITCH. LANDED WITH FLAPS 20. ***EMERGENCY DECLARED*** SHGN 15MAY25 06:07 MEM FIM: 27-51-00-815-804 AMM: 27-51-00-5 WHILE TROUBLESHOOTING, FSEU #1 AND #3 HAD NO FAULTS. FSEU #2 (-32) HAD THE "ALT ARM DISAG" LED DISPLAYED. CONTINUED TROUBLESHOOTING PER BLOCK 26, SHEET 11 OF B757 FIM 27-51-00-815-804. CYCLED FLAPS PER B757 AMM 27-51-00-5 WITHOUT ANY FAULTS. THE FORWARD CARGO DOOR AND E5 DOOR PANEL ARE OPEN FOR CONTINUED TROUBLESHOOTING PURPOSES. FACT 15MAY25 08:01 MEM NO FAILED LRU'S DURING BITE CHECK OF FESU #3. FESU #1 INDICATED A FLAP DISAGREE AND FESU #2 HAD A FLAP SYSTEM FAULT FOR NO MOTION. INSPECTED ALL FLAP TRANSMISSIONS OF BOTH L/H & R/H WINGS. FOUND L/H WING INBOARD FLAP, INBOARD TRANSMISSION OVERLOAD INDICATOR TRIPPED. DRAINED AND RESERVICED TO FULL, 16OZ. NO LEAKS NOTED. RESET INDICATOR. FOUND L/H WING OUTBOARD FLAP, OUTBOARD TRANSMISSION OVERLOAD INDICATOR TRIPPED. RESERVICED TO FULL, 2 OZ. NO LEAKS NOTED. RESET INDICATOR. CYCLED FLAPS THROUGH FULL TRAVEL WITH NO DEFECTS NOTED. ALL OPS CHECKS GOOD. A/C OK FOR SERVICE. THE FORWARD CARGO DOOR AND E5 DOOR PANEL ARE CLOSED.

Part: SLIDE — FAULTED (ZONE 800) · airframe 59,437 hrs · 30,940 cycles

L1 DOOR SLIDE PRESSURE OUTSIDE OF GREEN BAND. RELEASED FOR SERVICE PER MEL : 52-11-01-A CATEGORY : B EXPIRATION : 04FEB25 "MEL 52-11-01-A: L1 DOOR SLIDE INOP MEL: 52-11-01-A. AMM 25-66-01-4 , REMOVED AND REPLACED L1 DOOR SLIDE. OSD: 2/3/2025

Part: GUST LOCK — STUCK (ZONE 800) · airframe 59,257 hrs · 30,809 cycles

L1 DOOR LOCK WILL NOT DISENGAGE. RELEASED FOR SERVICE PER MEL : 52-11-01-A. FOUND GUSTLOCK STUCK AND WHEN PULLING HARD ENOUGH HEARD POP SOUND AND DOOR WILL NOW OPEN AND SHUT BUT GUST LOCK DOES NOT WORK. REPLACED THE BROKEN HOLD OPEN LOCK COLLAR. WITH REF TO AMM 52-11-08-8. OPS CHECK GOOD.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 59,040 hrs · 30,649 cycles

DURING SERVICE CHECK FOUND CENTER EMERGENCY EXIT LIGHT AND R/H EMERGENCY EXIT LIGHT WOULD NOT TEST. PREMATURE REMOVAL/INSTALLATION OFF MPN: 2013-1ASMI POS: 1 SRL: 9021 ON MPN: 2013-1A CPN: 3301128 SRL: 18133 TAG NBR: 7G8138 AMM: 33-51-07-2 REMOVED AND REPLACED FWD EMERGENCY POWER SUPPLY BATTERY IAW ABOVE REF. OPS CHK SERVICEABLE. OK TO CONTINUE.

Part: FLAP — DAMAGED (ZONE 600) · airframe 58,387 hrs · 30,194 cycles

AT THE TIME OF AIRCRAFT INSPECTION, FOUND EXISTING FLUSH REPAIR ON INBOARD FLAP LOWER SURFACE TRAILING EDGE AREA APPROXIMATELY 6 INCHES FROM OUTBOARD EDGE OF FLAP. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. VISUALLY INSPECTED REPAIR IAW ATTACHMENT "B" OF E.O. F-5100-7-5001. REPAIR IS INSTALLED IAW SRM 57-53-01-2R FIG 201. CATEGORY A REPAIR. CLASSIFIED AS A MAJOR REPAIR IAW GMM 6- 2-100. THIS REPAIR IS FOR FEDEX TRACKING PURPOSES.

Part: LOCK — DAMAGED (N/A) · airframe 57,601 hrs · 29,629 cycles

L1 DOOR GUST LOCK BROKEN. REMOVED AND REPLACED L1 DOOR GUST LOCK REF AMM: 52-11-08-4-0. OPS CHECK GOOD.

Part: SKIN — DELAMINATED (LT MLG DOOR) · airframe 57,596 hrs · 29,625 cycles

LANDING GEAR - BODY GEAR AND DOORS - LH MLG DOOR LH HEAT SHIELD ASSY DELAMINATI COMPLY WITH E..A. F-3212-T0367771 REV NO. POS. P1. COMPLIED WITH EA F-3212-T0367771 P1 BY REPAIR ON PN 149N6023-7 HEAT SHIELD DELAMINATION ON SKIN.

Part: NONE — NONE (N/A) · airframe 57,596 hrs · 29,625 cycles

MDIS 949 53-21 0303 04MAR22 OAK OPEN U RAMP REPORTED PUNCHER HOLE IN FLOOR LOWER FWD PIT 5 FEET AFT OF DOOR CENTERLINE OF FLOOR MEASURES 1/8 INCH ROUND. OIL 04MAR22 08:56 OAK U NO RESTRICTION REF : SR 57-53-01 RAMP REPORTED PUNCHER HOLE IN FLOOR LOWER FWD PIT 5 FEET AFT OF DOOR CENTERLINE OF FLOOR MEASURES 1/8 INCH ROUND. . C/7307684 ENT BY: 720201 RPT BY:720201 OILS 04MAR22 08:56 OAK U OIL REFERENCE: SR 57-53-01 TERMINATING ACTION REQUIRED AT OR BEFORE: SPC :

Part: NONE — NONE (N/A) · airframe 57,596 hrs · 29,625 cycles

MDIS 949 53-21 0305 04MAR22 LAS OPEN U RAMP REPORTED 1/4" HOLE IN THE FLOOR FWD COMPARTMENT STA 720 OIL 04MAR22 12:14 LAS U NO RESTRICTION REF : AMM SR57-53-001 RAMP REPORTED 1/4" HOLE IN THE FLOOR FWD COMPARTMENT STA 720 C/W PER SR57-53-01 C/7307701 OILS 04MAR22 12:14 LAS U OIL REFERENCE: AMM SR57-53-001 TERMINATING ACTION REQUIRED AT OR BEFORE: SPC :

Part: PLATE — DAMAGED · airframe 57,596 hrs · 29,625 cycles

MDIS 949 53-21 0306 04MAR22 LAS OPEN U RAMP REPORTED 1/4" HOLE (STA1540) AFT COMPARTMENT OIL IAW SRM 57-53-001 RAMP REPORTED 1/4" HOLE (STA1540) AFT COMPARTMENT C/W PER SR57-53-01 OILS SRM 57-53-001 TERMINATING ACTION REQUIRED AT OR BEFORE: SPC :

Part: NONE — NONE (N/A) · airframe 57,596 hrs · 29,625 cycles

MDIS 949 25-50 0015 12OCT21 DAY OPEN U 1/4" CUT IN FLOOR AFT CARGO @ STA 1380 JUST INBD OF DOOR CUTOUT. OIL 12OCT21 15:42 DAY U NO RESTRICTION REF : SR57-53-001 1/4" CUT IN FLOOR AFT CARGO @ STA 1380 JUST INBD OF DOOR CUTOUT. TEMP REPAIRED PER DRAWING SR57-53-001 MUST HAVE PERM REPAIR NLT NEXT B CHECK C/7289576 OILS 12OCT21 15:42 DAY U OIL REFERENCE: SR57-53-001 TERMINATING ACTION REQUIRED AT OR BEFORE: SPC :

Part: NONE — NONE (N/A) · airframe 57,548 hrs · 29,590 cycles

SLIDE LIGHT DOES NOT ILLUMINATE WHEN LEFT FWD ENTRY DOOR IS ARMED. CLEANED GIRT BAR PROXIMITY SENSORS. SLIDE LIGHT OPS CHECK GOOD REF 757 AMM 25-66-11-2.

Part: ADC — FAILED (RIGHT) · airframe 56,985 hrs · 29,165 cycles

EICAS MX MESSAGE- STAB TRIM REMOVED AND REPLACED RIGHT AIR DATA COMPUTER IAW 34-12-01-4.

Part: ADC — FAILED (RIGHT) · airframe 56,985 hrs · 29,165 cycles

EICAS MX MESSAGE- RUDDER RATIO REMOVED AND REPLACED RIGHT AIR DATA COMPUTER IAW B757 AMM 34-12--00-5

Part: ADC — FAILED (RIGHT) · airframe 56,985 hrs · 29,165 cycles

EICAS MX MESSAGE- ELV ASYM REMOVED AND REPLACE RIGHT AIR DATA COMPUTER IAW B757 AMM 34-12-01-4

Part: FLOORBEAM — CORRODED (BS 377 LBL25-58) · corrosion level 2 · airframe 56,984 hrs · 29,164 cycles

LH NOSE TUNNEL, MAIN CABIN FLOOR BEAM, FLOOR BOARD ATTACH FASTENER HOLE IS CORRODED AT STA 377.7 AT APPROX LBL24 ACCOMPLISHED FEDEX EA # F-5310-TO333967-P2 FUSELAGE - MAINFRAME - EXFOLIATION CORROSION ON FLOOR BEAM AT STA 377.7, LBL 24.75 - 58.22

Part: PANEL — CRACKED (RT WING TE) · airframe 56,984 hrs · 29,164 cycles

R.WING T/E PANEL 661CB IS CRACKED REPAIR IAW FEDEX EA F-5750-T0362146 - WINGS - FLIGHT SURFACES - RH AILERON, ACTUATOR AFT FAIRINGS, WS 726, GOUGE DAMAGE

Part: STRUCTURE — CRACKED (BS 1100) · airframe 56,984 hrs · 29,164 cycles

RMLG W/W APPROX. STA 1100 WING TO BODY SUB-STRUCTURAL CLIP IS CRACKED AT APPROX. RBL60 REMOVED AND REPLACED CLIP PER DWG # 149N7552 REV U

Part: ATTACH ANGLE — CRACKED (BS 1060) · airframe 56,984 hrs · 29,164 cycles

RMLG W\W FWD EDGE BULB SEAL RETAINER ATTACH ANGLE IS CRACKED AT APPROX. BL60 REMOVED AND REPLACED BRACKET PER DWG # 149N7550 REV;AE

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 56,984 hrs · 29,164 cycles

LEFT WING ,I/B FLAP, I/B LOWER SURFACE HAS CORROSION REMOVED AND REPLACED LOWER PANEL PER DWG # 113N2402 REV G

Part: FRAME — CRACKED (BS 1640 S14L) · airframe 56,984 hrs · 29,164 cycles

LEFT SIDE STATION 1640, FUSELAGE FRAME WEB SHOWS 2 EA CRACK INDICATIONS ON THE UPPER AND LOWER INBOARD HOLES. CRACKS NOTED ONLY IN THE FRAME LAYER ACCOMPLISHED FEDEX EA# F-5310-T0361898-P1: FUSELAGE - MAINFRAME - FRAME WEB STA 1640 S14L - CRACK INDICATION

Part: LANDING — CRACKED (BS 1200) · airframe 56,984 hrs · 29,164 cycles

PANEL 197KL HYD ACCESS PANEL LATCH LANDING IS MISSING AND ATTACH BRACKET IS CRACKED REMOVED AND REPLACED TEE CLIP PER FEDEX EA # F-5320-T0362153-P1

Part: FRAME — CRACKED (BS 1640 S14R) · airframe 56,984 hrs · 29,164 cycles

RIGHT SIDE STATION 1640 FUSELAGE FRAME WEB SHOWS 2 EA CRACKI INDICATIONS ON THE UPPER AND LOWER INBOARD HOLES. CRACKS NOTED ONLY IN THE FRAME LAYER ACCOMPLISHED FEDEX EA# F-5310-T0361899-P1: FUSELAGE MAINFRAME - FRAME WEB STA 1640 S14R - CRACK INDICATION

Part: GIRT BAR — FAILED INSP (R1 DOOR) · airframe 56,984 hrs · 29,164 cycles

R1DOOR GIRT BAR LEAF SPRING FAILED CHECK REMOVED AND REPLACED R1 DOOR EVAC SLIDE GIRT BAR PER FEDEX B757 AMM 25-66-10-2

Part: WEDGE — DELAMINATED (NR 7 SLAT) · airframe 56,984 hrs · 29,164 cycles

DISBOND INDICATION FOUND ON #7 SLAT T/E WEDGE LOWER I/B SIDE ORDERED AND RECEIVED #7 SLAT IAW B757 IPC 27-81-02-04A ITEM 010

Part: SKIN — CORRODED (NR 1 NACELLE) · airframe 56,984 hrs · 29,164 cycles

#1 PYLON I/B FWD HINGE PANEL LANDING IS EXFOLIATED REPAIRED DAMAGE IAW FEDEX EA # F-5430-T0362060 NACELLES/PYLONS - SKIN/PLATES/PANELS - #1 PYLON INBD SKIN PANEL, PP STA 120, INNER SURFACE, CORROSION REPAIR.

Part: SKIN — DELAMINATED (LT WING LE) · airframe 56,984 hrs · 29,164 cycles

LEFT WING I/B FIXED L/E UPPER PANEL P/N 114N1604-7 BETWEEN ISS201-ISS213 IS DELAMINATED RECEIVED NEW PANEL PN 114N1604-11.LOCATED AND DRILLED PANEL AND INSTALLED PER BAC DWG #114N1601 REV E

Part: SKIN — CRACKED (RT WING LE) · airframe 56,984 hrs · 29,164 cycles

RW L/E UPPER SURFACE IS CRACKED JUST AFT OF #8 SLAT INBD END. REPAIRED RW L/E UPPER SURFACE CRACKED AREA AFT OF #8 SLAT IAW BOEING 757 SRM 51-70- 07-0G PARAGRAPH 5.A FIG 5 AND B757 SRM 57-41-01 FIG 201 TABLE 4

Part: SKIN — CRACKED (LT WING LE) · airframe 56,984 hrs · 29,164 cycles

LH WING FIXED L/E CRACKED AT FSS 428. REPAIRED LH WING FIXED LEADING CRACK AT FSS 428 IAW B757 SRM 57-41-01-2R REPAIR 1 TABLE 4 AND SRM 51-70-07-0G PARA 5.A FIG 5

Part: WINDOW — CRACKED (COCKPIT) · airframe 56,451 hrs · 28,804 cycles

FO FWD RT WINDOW STARTED TO SPARK, THEN SHATTERED. QRH FOLLOWED. REMOVED AND REPLACED R1 WINDOW, IAW B757 AMM 56-11-01-4. UP TO STEP E23. NEXT STEP TO BE ACCOMPLIED IS E24, FINISHED INSTALLATION OF F/O FWD RT WINDOW, PER AMM 56-11-01-4 AND FINAL TORQUE OF BOLTS PLACED ON OIL, REF WRI 56-10/9218. ALSO REPLACED F/O FWD WINDOW CONTROLLER, PER AMM 30-41-01-4 AS PRECAUTIONARY.

Part: SLIDE — DETACHED (L1 DOOR) · airframe 56,347 hrs · 28,730 cycles

WHEN TRYING TO ENTER THE A/C L1 DOOR WOULD NOT OPEN. FOUND DOOR SLIDE HAD DISPLACED CAUSING THE GIRT TO JAM THE DOOR. REINSTALLED L1 DOOR ESCAPE SLIDE. OPS CHECK NORMAL, REF: B757 AMM 25-66-01-4. MANUFACTURER: AIR CRUISERS, MPN: D30654-122, MSN: 1912. OK FOR SERVICE.

Part: SPAR — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 55,440 hrs · 28,101 cycles

RH WING O/B MAIN FLAP FWD SPAR LOWER CHORD FOUND HEAVY CORROSION. PERFORMED THE REPAIR ON RH WING O/B MAIN FLAP FWD SPAR LOWER CHORD AT WBL 493- WBL 545 PER FEDEX EA # F-5750-T0347068 P1, TITLE: WING - FLIGHT SURFACES - EXFOLIATION CORROSION C/T RH WING OUTBOARD MAIN FLAP FRONT SPAR LOWER CHORD BETWEEN WBL 493 AND WBL 545.THIS REPAIR WAS CATEGROY B AND WAS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: SPAR — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 55,440 hrs · 28,101 cycles

LH WING O/B MAIN FLAP FWD SPAR LOWER CHORD FOUND HEAVY CORROSION AT WBL 361- WBL 390. PERFORMED THE REPAIR ON LH WING O/B MAIN FLAP FWD SPAR LOWER CHORD AT WBL 361- WBL 390 PER FEDEX EA # F-5750-T0346997 P1, TITLE: WING - FLIGHT SURFACES - EXFOLIATION CORROSION C/T LH WING OUTBOARD MAIN FLAP FRONT SPAR LOWER CHORD BETWEEN WBL 361 AND WBL 390.THIS REPAIR WAS CATEGROY B AND WAS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: SENSOR — MALFUNCTIONED (AC BAY) · airframe 54,804 hrs · 27,738 cycles

LEFT PACK OFF THEN INOP, PERFORMED PHASE 1S. PERFORMED V LIST. EMER DESCENT. DIVERTED TO HKG. RT ENGINE BLEED OFF AFTER DEPARTURE COMPLIED WITH CHECKLIST. REPLACED COMPRESSOR OUTLET SENSOR PER AMM 21-51-06-4.

Part: UNKNOWN — ODOR (CSABIN) · airframe 54,799 hrs · 27,735 cycles

STRONG BURNING SMELL DEVELOPED IN COURIER COMPARTMENT AFTER COURIER HEATER SELECTED TO "HIGH" POSITION. TURNED OFF COURIER HEAT AND SMELL DISSIPATED, EVENTUALLY. OPENED THE COURIER AERA CEILING PANEL, DETAIL VISUALLY INSPECTED THE AIR FLOW DUCT AND WIRING, NO ABNORMAL FOUND. OPERATIONAL TEST OF ZONE TEMPERATURE CONTROL SYSTEM SATISFIED PER AMM 21-61-00-5. RUN APU PER JRH AND OPERATE BOTH PACKS FOR 30 MINUTES, NO BURNING SMELL FOUND. ITEM CLOSED, A/C RELEASED FOR SERVICE.

Part: CIRCUIT CARD — MALFUNCTIONED (SMOKE DETECTOR) · airframe 54,676 hrs · 27,674 cycles

EN ROUTE, RED FWD CARGO FIRE EICAS ILLUMINATED. DECLARED EMERGENCY. EXECUTED QRH PROCEDURES INCLUDING DISCHARGE OF FIRE BOTTLE 1. RED EICAS FLICKERED AT TIMES AND EVENTUALLY EXTINGUISHED. DISCHARGED FIRE BOTTLE 2 IAW QRH PROCEDURE. TROUBLESHOT IAW FIM 26-16, FAULT TREE 805, NO RED FIRE CARGO MESSAGES, ONLY EICAS STATUS MESSAGE FWD CARGO DETECTOR 1 AND FWD CARGO DETECTOR 2. OPENED FWD CARGO DOOR WITH ASSIST BY FIRE DEPARTMENT PERSONAL. CONFIRMED NO CARGO LOADED IN FWD CARGO COMPARTMENT AND NO SIGN OF FIRE OCCURED. CARRIED OUT LOWER CARGO COMPARTMENT SMOKE DETECTION BITE PROCEDURE PER FIM 26-16 FT 802. TEST SATISFACTORY AND FWD CARGO DETECTOR 1 AND 2 NOT SHOWING ON STATUS PAGE. REMOVED AND REPLACED THE NR 6 AFOLTS CARD M10427 IAW AMM 26-10-01-4. TEST PASSED. REMOVED AND REPLACED THE NR 1 LOWER FWD CARGO SMOKE DETECTOR AS A PRECAUTION IAW AMM 26-16-01-2.TEST PASSED.

Part: FLOORBEAM — CORRODED (BS 377) · airframe 53,786 hrs · 27,290 cycles

MAIN DECK BS 377.7, LBL 24.75 - 58.22, FLOORBEAM CORRODED. REPAIRED THE FLOORBEAM IAW EA F-5310- T0333967 P1. MAJOR REPAIR IAW GMM 6-2-100.

Part: SKIN — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 518 hrs · 26,261 cycles

RIGHT ELEVATOR OTBD END CONDUCTIVE SKIN PLATE HAS CORROSION ON LOWER SURFACE. REMOVED, FABRICATED AND INSTALLATION CONDUCTIVE SKIN PLATE. IAW DWG 183N2003 REV G AND REV AM AND SRM 51-40-02.

Part: SKIN — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 518 hrs · 26,261 cycles

RIGHT ELEVATOR OTBD END CONDUCTIVE SKIN PLATE HAS CORROSION ON UPPER SURFACE. REMOVED, FABRICATED AND INSTALLATION CONDUCTIVE SKIN PLATE (FRAME) IAW DWG 183N2007 REV B, AND REV AM AND SRM 51-40-02.

Part: SKIN — GOUGED (NR 2 NACELLE) · airframe 518 hrs · 26,261 cycles

NR 2 PYLON AFT LOWER SKIN GOUGED AT SEAL ATTACH AREA. REPAIRED IAW EA F-5480-146471 REV A PART 2.

Part: LEAF SPRING — BROKEN (GIRT BAR) · airframe 517 hrs · 26,208 cycles

FOUND LEAF SPRING ON L1 GIRT BAR BROKEN. R & R GIRT BAR IAW AMM 25-66-10-2.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 50,632 hrs · 25,236 cycles

FL 350, RT FWD WINDOW CRACKED WITH VISIBLE ARCING IN LOWER LEFT CORNER. REMOVED AND REPLACED WINDSHIELD IAW AMM 56-11-01-4.

Part: WIRE — OUT OF POSITION (EMERGENCY LIGHT) · airframe 49,500 hrs · 24,438 cycles

EMERGENCY EXITS LIGHTS SWITCH, LIGHTS WHEN COVER IS CLOSED LT SWITCH IS IN OFF POSITION WITH "UNARMED" LIGHT ILLUMINATED. FOUND ARM SWITCH POSITIONING RETAINER WIRE IN WRONG POSITION. REPOSITION WIRE ON ARM SWITCH AND EMERGENCY LIGHTS OPS CHECKED GOOD WHEN SWITCH IS PLACED IN THE ARMED POSITION IAW MM 33-51-00-0. ACFT OK FOR SERVICE. FINAL CLOSED.

Part: COLLAR — BROKEN (DOOR HOLD OPEN) · airframe 49,204 hrs · 24,238 cycles

ON WALKAROUND INSP FOUND L1 DOOR HOLD OPEN LOCK DISCONNECTED FROM TORQUE SHAFT. INSTALLED DOOR BOTTLE SAFTEY PIN IN OVERHEAD. REMOVED PANEL AND SEAL 221AL AND FOUND DOOR HOLD OPEN LOCK COLLAR BROKE IN 2 PIECES. R & R BROKEN HOLD OPEN LOCK COLLAR IAW 52-11-08-8, CHECKED GOOD, OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,050 hrs · 24,146 cycles

DOOR SLIDE LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,659 hrs · 23,904 cycles

RT EMERGENCY EXIT LIGHTS DO NOT TEST. R & R BATTERY PACKS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,477 hrs · 23,797 cycles

EMERGENCY LIGHTS INOPERATIVE. PERFORMED ADJUSTMENT & TEST ON EMERGENCY LIGHTS IAW AMM 33-51-00-5. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,501 hrs · 23,810 cycles

EMERGENCY LIGHTS INOPERATIVE. RELEASED FOR SERVICE IAW MEL: 33-51-01-01. PERFORMED ADJUSTMENT & TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00-5. OPS CHECKED GOOD.

Part: FAIRING — GOUGED (NR 1 STRUT) · airframe 48,330 hrs · 23,691 cycles

NR 1 STRUT AFT FAIRING STRUCTURE LOWER PAN EXTERNAL SKIN OTBD SIDE FOUND GOUGED AT PP STA 259.0. GOUGED SKIN REPAIRED IAW EA F-5480-146470 ( LT PYLON AFT FAIRING PAN GOUGE REPAIR). REPAIR IS CLASSIFIED AS MAJOR.

Part: FAIRING — GOUGED (ZONE 400) · airframe 48,330 hrs · 23,691 cycles

NR 2 STRUT AFT FAIRING STRUCTURE LOWER PAN EXTERNAL SKIN INBD SIDE FOUND WITH PUNCTURE HOLE AT PP STA 259.0. DAMAGED SKIN ON NR 2 STRUT AFT FAIRING LOWER PAN REPAIRED IAW EA F-5480-146471. REPAIR IS CLASSIFIED AS MAJOR.

Part: FAIRING — GOUGED (ZONE 400) · airframe 48,330 hrs · 23,691 cycles

1 STRUT AFT FAIRING STRUCTURE LOWER PAN EXTERNAL SKIN INBD SIDE FOUND WITH GOUGE MARK AT PP STA 259.0. GOUGE REPAIR CARRIED OUT IAW EA F-5480-146470. REPAIR IS CLASSIFIED AS MAJOR.

Part: FAIRING — GOUGED (ZONE 400) · airframe 48,330 hrs · 23,691 cycles

2 STRUT AFT FAIRING STRUCTURE LOWER PAN EXTERNAL SKIN OTBD SIDE FOUND WITH PUNCTURE HOLE AT PP STA 259.0. GOUGED SKIN REPAIRED IAW EA F-5480-164671. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — NICKED (ZONE 100) · airframe 48,330 hrs · 23,691 cycles

FWD LWR CARGO DOOR CONTROL PANEL P43 CENTER CUTOUT AREA LWR SIDE HAS NICK ON INNER SKIN SURFACE. REPAIR CARRIED OUT AS PER E.A. F-5330-152504. REPAIR IS CLASSIFIED AS MINOR.

Part: SKIN — DENTED (ZONE 100) · airframe 48,330 hrs · 23,691 cycles

FUSELAGE EXTERIOR SKIN WITH DENT AT BS 1701 (8 IN) TO BS 1720, BETWEEN STR 20L TO STR 21L. REPAIR TO DENT CARRIED OUT IAW EA F-5330-150715, PART 1, DENT IN FUSELAGE SKIN BETWEEN BS 1700 TO 1720 AND S20L TO S21L. REPAIR IS CLASSIFIED AS MAJOR.

Part: STRINGER — DAMAGED (BS 1844 S23L) · airframe 48,330 hrs · 23,691 cycles

INTERIOR AFT COMPARTMENT EMPENNAGE AREA AT BS 1844 STR 23L, THERE ARE 2 ELONGATED HOLES. REPAIR CARRIED OUT AS PER E.A. F-5310-146491. REPAIR IS CLASSIFIED AS MAJOR.

Part: STRINGER — DAMAGED (BS 1844 S27R) · airframe 48,330 hrs · 23,691 cycles

AFT COMPARTMENT EMPENNAGE AREA AT BS 1844, STR 27R THERE ARE 2 ELONGATED HOLES. REPAIRED AS PER SRM 51-40-05 REV. 102. REPAIR IS CLASSIFIED AS MAJOR.

Part: FRAME — DENTED (ZONE 100) · airframe 48,330 hrs · 23,691 cycles

FWD LWR CARGO COMP. FRAME AT STA 660 HAS DENT ABOVE STR S24R. DENTED FRAME REPAIRED IAW EA F-5310-146476 PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — CORRODED (BS 1380) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

AFT LWR CARGO NR 2 DOOR LWR SILL GUARD AREA REMOVAL OF LWR SILL PLATE FOR MX, ACCESS FOUND CORROSION ON EXTERIOR SKIN SURFACE STA 1380, WL 143.0- WL 147.0. REPAIR CARRIED OUT AS PER E.A. F-5330-146495 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: STRINGER — DAMAGED (BS 1844 S27L) · airframe 48,330 hrs · 23,691 cycles

AFT COMPARTMENT EMPENNAGE AREA AT BS1844, STR 27L THERE ARE 2 ELONGATED HOLES. REPAIR CARRIED OUT AS PER E.A. F-5310-146491. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 1650-1681) · airframe 48,330 hrs · 23,691 cycles

FUSELAGE EXTERIOR SKIN AT BS 1650-1681 AT STR S17 TO S19 LT. THERE ARE NUMEROUS SCRATCHES WITH STICKER 4331, ALL BELOW THE L4 DOOR. REPAIR CARRIED OUT AS PER E.A. F-5330-146481 PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (ZONE 300) · airframe 48,330 hrs · 23,691 cycles

FUSELAGE TAILCONE EXTERIOR SKIN LOWER WITH EXTERNAL DOUBLER REPAIR AT BS 1720 TO 1743.85 BETWEEN STR 27R TO STR 28R. REPAIR DOUBLER REPLACED IAW SRM 58-00-01, FIG 201, REV 102. REPAIR IS CLASSIFIED AS MAJOR.

Part: SHIM — LOOSE (ZONE 400) · airframe 48,330 hrs · 23,691 cycles

EXISTING REPAIR THE LT WING OTBD NACELLE FITTING HAS SHIM MIGRATION BETWEEN THE WING SURFACE. EA F-5740-146462, PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CORRODED (ZONE 600) · airframe 48,330 hrs · 23,691 cycles

WING, RT FALSE WORK PANEL (COMPOSITE) OVER RT U/C BAY, FWD EDGE (AT REAR SPAR), 8 PULLED RIVETS. REPAIR CARRIED OUT IAW EA F-5730-146480. RT WING UPPER AFT SKIN CORROSION BLEND REPAIR). REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (BS 1280) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

AFT LWR CARGO COMP TIE DOWN FITTING LT AT STA 1280 HAS CORROSION. REPAIR CARRIED OUT AS PER E.A. F-5340-146489. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (BS 800) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

FWD LWR CARGO COMP TIE DOWN FITTING RT AT STA 800 HAS CORROSION. REPAIR CARRIED OUT AS PER E.A F-5340-146490. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

AFT LWR CARGO COMP TIE DOWN FITTING LT AT STA 1240 HAS CORROSION. TIEDOWN FITTING CORROSION REPAIR CARRIED OUT AS PER E.A. F-5340-146489. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (BS 1620) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

AFT LWR COMP TIE DOWN FITTING RT AT STA 1620 HAS CORROSION. REPAIR CARRIED OUT AS PER E.A. F-5340-146489. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

AFT LWR CARGO COMP TIE DOWN FITTING LT AT STA 1560 HAS CORROSION. REPAIR CARRIED OUT AS PER E.A. F-5340-146489.

Part: FITTING — CORRODED (BS 1620) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

AFT LWR CARGO COMP TIE DOWN FITTING LT AT STA 1620 HAS CORROSION. REPAIR CARRIED OUT AS PER E.A. F-5340-146489. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (BS 1520) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

AFT LWR CARGO COMP TIE DOWN FITTING RT AT STA 1520 HAS CORROSION. REPAIR CARRIED OUT AS PER E.A. F-5340-146489. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

AFT LWR CARGO COMP TIE DOWN FITTING LT AT STA 1440 HAS CORROSION. REPAIR CARRIED OUT AS PER E.A. F-5340-146489. REPAIR]. REPAIR IS CLASSIFIED A MAJOR.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

FWD LWR CARGO COMP TIE DOWN FITTING RT AT STA 839 HAS CORROSION. REPAIR ON TIE DOWN FITTING CARRIED OUT AS PER E.A. F-5340-146490. REPAIR CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (BS 740) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

FWD LWR CARGO COMP TIE DOWN FITTING RT AT STA 740 HAS CORROSION. REPAIR CARRIED OUT AS PER E.A. F-5340-146490. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (BS 1600) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

AFT LWR CARGO COMP TIE DOWN FITTING RT AT STA 1600 HAS CORROSION. REPAIR CARRIED OUT AS PER E.A F-5340-146489. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (BS 1260) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

AFT LWR CARGO COMP TIEDOWN FITTING LT AT STA 1260 HAS CORROSION. REPAIR CARRIED OUT AS PER E.A. F-5340-146489. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (BS 1220) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

AFT LWR CARGO COMP TIE DOWN FITTING RT AT STA 1220 HAS CORROSION. REPAIR CARRIED OUT ON TIE DOWN FITTING AS PER E.A. F-5340-146489. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (BS 720) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

FWD LWR CARGO COMP TIE DOWN FITTING RT AT STA 720 HAS CORROSION. REPAIR CARRIED OUT AS PER E.A. F-5340-146490. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (BS 1340) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

AFT LWR CARGO COMP TIE DOWN FITTING RT AT STA 1340 HAS CORROSION. REPAIR CARRIED OUT AS PER E.A. F-5340-146489. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

FWD LWR CARGO COMP TIE DOWN FITTING RT AT STA 520 HAS CORROSION. REPAIR CARRIED OUT ON TIE DOWN FITTING AS PER E.A. F-5340-146490. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (BS 1560) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

AFT LWR CARGO COMP TIE DOWN FITTING RT AT STA 1560 HAS CORROSION. REPAIRED AS PER E.A. F-5340-146489. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (BS 820) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

FWD LWR CARGO COMP TIE DOWN FITTING LT AT STA 820 HAS CORROSION. REPAIR CARRIED OUT AS PER E.A. F-5340-146490. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (BS 1300) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

AFT LWR CARGO COMP TIE DOWN FITTING LT AT STA 1300 HAS CORROSION. REPAIR CARRIED OUT ON TIEDOWN FITTING AS PER E.A. F-5340-146489. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (BS 1300) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

AFT LWR CARGO COMP TIE DOWN FITTING RT AT STA 1300 HAS CORROSION. REPAIR CARRIED OUT AS PER E.A. F-5340-146489. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

AFT LWR CARGO COMP TIE DOWN FITTING LT AT STA 1600 HAS CORROSION. REPAIRED AS PER E.A. F-5340-146489.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

FWD LWR CARGO COMP TIE DOWN FITTING RH AT STA 820 HAS CORROSION. REPAIR CARRIED OUT AS PER E.A. F-5340-146490. REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

AFT LWR CARGO COMP TIE DOWN FITTING LT AT STA 1540 HAS CORROSION. REPAIR CARRIED OUT ON TIEDOWN FITTING AS PER E.A. F-5340-146489.

Part: TORQUE TUBE — CORRODED (ZONE 500) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

LEFT WING AFT INBD FLAP, TORQUE TUBE EVIDENCE OF CORROSION ON INTERNAL BORE OF TUBE AND BETWEEN TUBE AND BUSHING AT INBD END. R & R LT INBD FLAP TORQUE TUBE AND FAILSAFE TUBE IAW CMM 57-53-43, REV 103. REPAIR IS CLASSIFIED AS MINOR.

Part: BEAM — DENTED (CARGO DOOR) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

AFT LWR CARGO NR 2 DOOR LWR AFT CORNER EDGE BEAM HAS DENT/DAMAGE. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 102 AND E.A. F-5230-146488. REPAIR IS CLASSIFIED AS MAJOR.

Part: BEAM — DENTED (CARGO DOOR) · airframe 48,330 hrs · 23,691 cycles

AFT LWR CARGO NR 2 DOOR, LWR DOOR FWD CORNER EDGE BEAM HAS DENT/DAMAGE. REMOVED AND REPAIRED IAW SRM 51-40-02 REV. 102 AND E.A. F-5230-150713. REPAIR IS CLASSIFIED AS MAJOR.

Part: BEAM — DAMAGED (CARGO DOOR) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

FWD LWR CARGO COMP NR1 DOOR LWR DOOR CTR EDGE BEAM HAS DENT/DAMAGE. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 102 AND E.A. F-5230-146487. REPAIR IS CLASSIFIED AS MAJOR.

Part: FRAME — UNKNOWN (ZONE 100) · airframe 48,330 hrs · 23,691 cycles

EXISTING REPAIR AT BS 1520 BETWEEN STR 22R AND 26R THERE IS DOUBLER REPAIR ON THE INTERIOR FRAME AT THE SPLICE JOINT. REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SKIN — DENTED (ZONE 100) · airframe 48,330 hrs · 23,691 cycles

FUSELAGE EXTERIOR WITH DENT AT BS 1661 (2 IN) TO BS 1681.8 BETWEEN STR 27 TO STR 26L. DENT IS WITHIN LIMITS IAW SRM 53-00-01. COMPLIED EA F-5330-150714, DENT IN FUSELAGE SKIN BETWEEN BS 1661 TO 1681 AND S26L TO S27L. REPAIR IS CLASSIFIED AS MAJOR.

Part: BEAM — DENTED (CARGO DOOR) · airframe 48,330 hrs · 23,691 cycles

AFT LWR CARGO NR2 DOOR, LOWER DOOR EDGE BEAM CTR SECTION HAS DENT/DAMAGE. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 102 AND E.A. F-5230-146488. REPAIR IS CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (ZONE 200) · airframe 48,330 hrs · 23,691 cycles

CREASE BEAM STA 755 - 990, RBL 60, HAS CORROSION APPROX 1" CIRCULAR AT STA 755 AND APPROX. 1" CIRCULAR AT STA 790. REPAIR CARRIED OUT ON CREASE BEAM AS PER E.A. F-5310-150708 PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (BS 761) · airframe 48,330 hrs · 23,691 cycles

CABIN, CREASE BEAM AT STA 761 LT HAS CORROSION. REPAIR CARRIED OUT AS PER E.A. F-5310-150709 PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: FRAME — GOUGED (BS 1280 S11-16L) · airframe 48,330 hrs · 23,691 cycles

CABIN - FUSELAGE FRAME AT BSTA 1280 BETWEEN STR 11L-16L HAS 6 GOUGE MARKS. DAMAGE REPAIRED AS PER E.A. F-5310-146477 PART 1 REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CORRODED (BS 720) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

CABIN SEAT TRACK BS 720 RBL 45.5 I/B UPPER FLANGE HAS CORROSION. REPAIR ACCOMPLISHED AS PER E.A. F-5320-149249 PART 1

Part: SEAT TRACK — MISINSTALLED (ZONE 200) · airframe 48,330 hrs · 23,691 cycles

CABIN SEAT TRACK AT STN 680 TO STN 780 LBL 24.75 MISMATCHED IN HEIGHT. REPAIR ACCOMPLISHED AS PER E.A. F-5320-149249 PART 1.

Part: SEAT TRACK — MISINSTALLED (ZONE 200) · airframe 48,330 hrs · 23,691 cycles

CABIN SEAT TRACK AT STN 640 TO STN 780, RBL 45 MISMATCH IN HEIGHT. REPAIR CARRIED OUT AS PER E.A. F-5320-149249 PART 1 [ SEAT TRACK HEGIHT DIFFERENCE REWORK AND CORROSION FOUND BETWEEN BS 640 TO BS 780, LBL 45.50 TO RBL 45.50]. THIS IS A MAJOR ALTERATION.

Part: SEAT TRACK — CORRODED (BS 700-720) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

CABIN SEAT TRACK BS 700-720, RBL 24.75, FLANGE HAS CORROSION. REPAIR ACCOMPLISHED AS PER E.A. F-5320-149249 PART 1

Part: SEAT TRACK — MISINSTALLED (BS 680-780) · airframe 48,330 hrs · 23,691 cycles

CABIN, SEAT TRACK AT BS 680 TO 780 LBL 45 IS MIS-MATCHED IN HEIGHT. REPAIR ACCOMPLISHED AS PER E.A. F-5320-149249 PART 1.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

CABIN SEAT TRACK BS 720 RBL 24.75 HAS CORROSION ON UPPER FLANGE, OTBD SIDE. REPAIR ACCOMPLISHED AS PER E.A. F-5320-149249 PART 1.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

CABIN SEAT TRACK BS 725 RBL 45.5 HAS CORROSION ON UPPER FLANGE OTBD SIDE.

Part: SEAT TRACK — MISINSTALLED (ZONE 200) · airframe 48,330 hrs · 23,691 cycles

SEAT TRACK AT BS 640 TO 780 RBL 24.75 MIS-MATCH IN HEIGHT. REPAIR ACCOMPLISHED PER E.A F-5320-149249 PART 1.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

CABIN SEAT TRACK BSTA 700 RBL 24.75 HAS CORROSION ON UPPER OTBD FLANGE. REPAIR ACCOMPLISHED AS PER E.A. F-5320-149249 PART 1

Part: SHIM — LOOSE (ZONE 400) · airframe 48,330 hrs · 23,691 cycles

NR2 PYLON MID BULKHEAD UPPER LINK FITTING AT PP STA 174.30 FOUND WITH SHIMS MIGRATION. RECTIFIED IAW SRM 54-50-90, REV 102. REPAIR 6. REPAIR IS CLASSIFIED AS MAJOR.

Part: BUSHING — LOOSE (ZONE 400) · airframe 48,330 hrs · 23,691 cycles

NR 2 PYLON STRUT TO DIAGONAL BRACE LOWER SPAR FITTING BUSHING FOUND WITH MIGRATION. REPAIR CARRIED OUT IAW SRM 54-50-90, REPAIR 5, REV 102. REPAIR IS CLASSIFIED AS MAJOR.

Part: SHIM — LOOSE (ZONE 400) · airframe 48,330 hrs · 23,691 cycles

NR1 PYLON MID BULKHEAD RT FWD SIDE LOWER FLANGE AT PP STA 174.30 FOUND WITH SHIMS MIGRATION. RECTIFIED IAW SRM 54-50-90, REV 102. REPAIR IS CLASSIFIED AS MAJOR.

Part: DOOR FRAME — CORRODED (BS 687) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

CABIN -FWD L2 DOOR FRAME B STA 687, WL 208.1 - WL 212 HAS CORROSION. REPAIR ACCOMPLISHED AS PER E.A. F-5310-150703 PART 1[CORROSION BLENDOUTS AT BS 690 BETWEEN WL 208.1 AND 212 FORWARD OF L2 DOOR. REPAIR IS CLASSIFIED AS MAJOR.

Part: DOOR FRAME — CORRODED (ZONE 800) · airframe 48,330 hrs · 23,691 cycles

R4 FWD DOOR FRAME REVEAL AT B STA 1645 HAS CORROSION FROM APPROX WL 208.5 - WL 211.5. REPAIR CARRIED OUT IAW EA F-5310-150704, PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: SHIM — LOOSE (ZONE 400) · airframe 48,330 hrs · 23,691 cycles

NR1 PYLON MID BULKHEAD LT AFT SIDE LOWER FLANGE AT PP STA 174.30 FOUND WITH SHIMS MIGRAGTION. RECTIFIED IAW SRM 54-50-90, REV 102. REPAIR 7. REPAIR IS CLASSIFIED AS MAJOR.

Part: SHIM — MIGRATED (ZONE 400) · airframe 48,330 hrs · 23,691 cycles

RT WING BETWEEN OTBD NAC FITTING AND LOWER WING SKIN FOUND WITH SHIMS MIGRATION AT WS 303.5. REPAIRED IAW EA F-5740-146463 PART 1.

Part: DOOR FRAME — GOUGED (BS 1645) · airframe 48,330 hrs · 23,691 cycles

CABIN - R4 FWD DOOR FRAME REVEAL BSTA 1645 HAS A GOUGE APPROX. .2500" X .2500 AT WL 219. REPAIR ACCOMPLISHED AS PER E.A. F-5310-150704 PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: SHIM — LOOSE (ZONE 400) · airframe 48,330 hrs · 23,691 cycles

NR2 PYLON MID BULKHEAD RT FWD SIDE LOWER FLANGE AT PP STA 174.30 FOUND WITH SHIMS MIGRATION. REPAIRED IAW SRM 54-50-90, REV 102, REPAIR 7. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — CRACKED (LT WING) · airframe 48,330 hrs · 23,691 cycles

LT WING L/E NOSE SKIN AT NACELLE AT ISS 280 FOUND WITH 1.0" CRACK. CRACKED NOSE SKIN ON LT WING R & R IAW SRM 51-40-02 REV 102. REPAIR IS CLASSIFIED AS MINOR.

Part: SKIN — DAMAGED (APU BAY DOOR) · airframe 48,330 hrs · 23,691 cycles

APU RT DOOR EXTERNAL SKIN LOWER FWD CORNER HAS DAMAGE. REPAIR CARRIED OUT IAW EA F-5240-145356. REPAIR IS CLASSIFIED AS MINOR.

Part: DECK PLATE — CORRODED (BS 1714-1717) · airframe 48,330 hrs · 23,691 cycles

AFT SHEAR DECK HAS CORROSION - BSTA 1717-1714 AND RBL 22- RBL 26. AFT DECK PLATE BETWEEN STA 1681 AND STA 1720, LBL 60 TO RBL 60, REMOVED AND REPLACED IAW SRM 51-40-02 REV. 102. REPAIR IS CLASSIFIED AS MAJOR.

Part: FLOORBEAM — DAMAGED (BS 1280) · airframe 48,330 hrs · 23,691 cycles

CABIN FLOORBEAM BSTA 1280, FOUND DOUBLER CUT DUE TO EXISTING REPAIR, ON UPPER CHORD FWD LOWER SURFACE. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 102. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (BS 1620-1640) · airframe 48,330 hrs · 23,691 cycles

SEAT TRACK BS 1620-1640 RBL 45.5 HAS DAMAGE TO THE CROWN. REMOVED AND REPLACED WITH FABRICATED PART IAW SRM 51-40-02 REV. 102. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 48,330 hrs · 23,691 cycles

SEAT TRACK BS 1060-1080 RBL 45.75 HAS DAMAGE TO THE CROWN AND CHANNEL AREAS. R & R IAW SRM 51-40-02 REV.102. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (BS 1540-1560) · airframe 48,330 hrs · 23,691 cycles

SEAT TRACK BSTA 1540-1560 RBL 24.75 HAS DAMAGE TO THE CROWN AREA. DAMAGED SEAT TRACK BETWEEN STA 1540 AND STA 1640 REMOVED AND REPLACED WITH FABRICATED TRACK IAW SRM 51-40-02 REV. 102. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (BS 940-960) · airframe 48,330 hrs · 23,691 cycles

CABIN - SEAT TRACK B STA 940-960, LBL 45.5 HAS DAMAGE TO CROWN AND CHANNEL. REMOVED AND REPLACED WITH FABRICATED PART IAW SRM 51-40-02 REV. 102. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 48,330 hrs · 23,691 cycles

CABIN - SEAT TRACK B STA 900-920, LBL 24.75 HAS DAMAGE TO CROWN AND CHANNEL. DAMAGED CROWN ON SEAT TRACK BETWEEN STA 900 AND STA 1075. REMOVED AND REPLACED IAW SRM 51-400-02, REV 102. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (BS 960-1010) · airframe 48,330 hrs · 23,691 cycles

CABIN - SEAT TRACK BSTA 960-1010 RBL 24.75 HAS DAMAGE TO CROWN AND CHANNEL. REMOVED AND REPLACED WITH FABRICATED PART IAW SRM 51-40-02 REV. 102. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 48,330 hrs · 23,691 cycles

CABIN - SEAT TRACK B STA 1420-1440, RBL 24.75 HAS DAMAGE AT CROWN AREA. DAMAGED SEAT TRACK REMOVED AND REPLACED IAW SRM 51-40-02 REV. 102. REPAIR IS CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 48,330 hrs · 23,691 cycles

CABIN - FLOORBEAM STA 760, RBL 50 HAS CORROSION. REMOVED AND REPLACED WITH FABRICATED FLOORBEAM IAW SRM 51-40-02, REV 102. REPAIR IS CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,330 hrs · 23,691 cycles

FLOORBEAM UPPER CHORD HAS CORROSION STA 1640 RT RBL 54. FLOORBEAM AT STA 1640 REMOVED AND REPLACED IAW SRM 51-40-02 REV 102. REPAIR IS CLASSIFIED AS MAJOR.