N140UP

Part: ATTACH ANGLE — BROKEN (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

FR 79 +Y1589.5 AFT SEAT TRACK ATTACHMENT ANGLE IS CRACKED THROUGH THE BOTTOM AFT FASTENER HOLE ON SEAT TRACK ATTACHMENT POINT. INSTALLED ANGLE WITH FASTENERS IAW SRM 51-40-21.

Part: HYDRAULIC SYSTEM — LEAKING (ZONE 100) · airframe 27,603 hrs · 17,055 cycles

FWD CARGO COMPARTMENT CENTER BILLIAGE AREA INSULATION SATURATED WITH SKYDROLL. CLEANED UNDER FWD CARGO BILLIAGE AREA FROM FR27 TO FR37 WITH 1/4 GAL IAW AMM 12-21-12/201.TREATED FOR CORROSION 2 IAW SRM 51-23-20. REPLACEED 50 FT OF INSULATION IAW AMM 25-50-21/401.

Part: BRACKET — CORRODED (ZONE 100) · airframe 27,603 hrs · 17,055 cycles

FORWARD CARGO COMPARTMENT, CENTER CEILING SUPPORT AT FRAME 26 HAS CORROSION. INSTALLED CENTER CEILING SUPPORT AT FRAME 26 FASTENERS P/N: MS20426AD5 (30EA) BATCH: 0004233090, P/N: MS20426AD 3 (36EA) BATCH: 0004410248, P/N: ABS0330-01A (18EA) BATCH: 004416794 I.A.W A300-600 SRM 51-40-21.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 27,603 hrs · 17,055 cycles

FORWARD CARGO COMPARTMENT, LEFT CEILING SUPPORT AT FRAME 26 HAS CORROSION. INSTALLED NEW PART CEILING SUPPORT FROM FORWARD CARGO COMPARTMENT, LEFT CEILING SUPPORT AT FRAME 26 IAW A300-600 SRM 51-40-21.

Part: ANGLE — CRACKED (ZONE 500) · airframe 27,603 hrs · 17,055 cycles

KRUGER FLAP I/B REINFORCING ANGLE HAS A CRACK. INSTALLED REINFORCING ANGLE AND BRACKET AT KRUGER FLAP I/B IAW A300-600, SRM 51-40-21.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

FR80 -Y1221.2 AFT FLOOR STRUCTURE HAS A CRACK. INSTALLED PROFILE T AT FR80 -Y1221.2 APPLIED IAW A300-600, SRM 51-40-21.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MAIN CARGO FLOOR STRUCTURE BETWEEN FRAMES 13-14, Y1552 HAS CORROSION AT 2 EA FASTENR HOLES INSTALLED NEW FLOOR SUPPORT IAW A300-600 SRM 51-40-21 USING RETAINED HARDWARE.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MAIN CARGO FLOOR STRUCTURE BETWEEN FRAMES 14-15, Y953 HAS CORROSION AROUND 2 EA FASTENER HOLES INSTALLED NEW SUPPORT IAW A300 SRM 51-40-21.

Part: ANGLE — GOUGED (ZONE 100) · airframe 27,603 hrs · 17,055 cycles

BULK CARGO SCUFF PLATE INSERT FASTENER HOLE HAS VISUAL DAMAGED ON INSIDE ANGLE INSTALLED NEW ANGLE PN UP-F5347569820800 IAW SRM A300-600 51-40-21.

Part: ATTACH BRACKET — CRACKED (ZONE 100) · airframe 27,603 hrs · 17,055 cycles

FWD E&E BAY SUSPECTED CRACK ON L/H VERTICAL INTERCOSTAL ATTACH BRACKET. (OTBD OF LADDER FROM E&E BAY TO FLIGHT DECK) REMOVED ANGLE AT E&E BAY ON L/H VERTICAL INTERCOSTAL IAW A300-600, SRM 51-40-21.FABRICATED NEW ANGLE IAW A300-600, SRM 53-12-15, PAGE 18 AND GMM 09-08-01-03.INSTALLED NEW ANGLE AT FWD E&E BAY SUSPECTED CRACK ON L/H VERTICAL INTERCOSTAL ATTACH BRACKET OTBD OF LADDER FROM E&E BAY TO FLIGHT DECK IAW A300-600, SRM 51-40-21

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MAJOR REPAIR. MDC FLOOR STRUCTURE SEAT TRACK WITH CORROSION BTWN FR 27 THROUGH FR 29 AT Y1456. COMPLIED WITH ACCOMPLISH PERMANENT REPAIR PER SRM REV. 42 CHAPTER 53-10-16-201 PARAGRAPH 4 FIGURE 201.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MAJOR REPAIR, MDC FLOOR STRUCTURE SEAT TRACK WITH CORROSION BTWN FR 28 THROUGH FR 31 AT Y1959. INSTALLED 3(EA) FLOORBOARD PANELS IAW AMM 53-10-23/0401 WITH RETAINED HARDWARE. INSTALLED 2(EA) FWD CARGO SIDEWALL PANEL IAW AMM 25-54-10/201.

Part: SUPPORT — CRACKED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MDC FLOOR STRUCTURE, R/H SIDE REINFORCEMENT SUPPORT CRACKED AT FR 38.2 AND -Y2462. 21-50 INSTALLED NEW SUPPORT ON MDC FLOOR STRUCTURE, R/H SIDE REINFORCEMENT AT FR 38.2 AND -Y2462. I.A.W A300-600 SRM 51-40-21

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MDC FLOOR STRUCTURE, L/H SIDE REINFORCEMENT SUPPORT CRACKED BTWN FR 37 AND FR38 AT Y2462. 21-53.REMOVED REINFORCEMENT SUPPORT AT MCD FLOOR STRUCTURE BTWN FR 37 AND FR 38, Y 2462 LH I.A.W. A300-600 SRM 51-40-21.LOCATED AND DRILLED REINFORCEMENT SUPPORT STRUCTURE AT THE MDC FLOOR STRUCTURE BTWN FR37 AND FR38. I.A.W AIRBUS 300-600 SRM 51-40-44-001.INSTALLED REINFORCEMENT SUPPORT STRUCTURE AT THE MDC FLOOR BTWN FR37 AND FR38 I.A.W SRM 51-4021-001

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

FAULT-Z200-INT MAI CARGO FLOOR PANEL 251HM EDGE CRACKED.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

FAULT-Z200-INT MAIN CARGO FLOOR PANEL 252ZG HAS COMPOSITE DAMAGE AT EDGE.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MAIN CARGO FLOOR PANEL 251LG HAS COMPOSITE DAMAGE TO EDGE.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MAIN CARGO FLOOR PANEL 251XJ HS EXPOSED COMPOSITE IN MULTIPLE LOCATION.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 27,603 hrs · 17,055 cycles

MAIN CARGO FLOOR PANEL 251BN HAS EXPOSED COMPOSITE.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 27,603 hrs · 17,055 cycles

MAIN CARGO FLOOR PANEL 251EN HAS COMPOSITE DAMAGE AT CORNERS.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MAIN CARGO FLOOR PANEL 252FJ CRACKED.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MAIN CARGO FLOOR PANEL 251LJ HAS COMPOSITE DAMAGE AROUND FASTENER HOLE.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MAIN CARGO FLOOR PANEL 252LJ CRACKED. MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

FAULT-INT-Z200- MDC FLOOR PANEL 252DN WITH COMPOSITE MATERIAL EXPOSURE AT UPPER FACE. DOT 21-15.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MAJOR REPAIR, MCD FLOOR PANEL231KJ IS DELAMINATING IN SEVERAL AREAS. FABRICATED FLOOR PANEL 231KJ, I.A.W. SREO-16407-REQ001 (APPX B).

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 27,614 hrs · 17,062 cycles

MAJOR REPAIR, MAIN CARGO DECK FLOOR STRUCTURE BETWEEN FRAMES 73 AND 74, -Y2127.5 HAS CORROSION. COMPLIED WITH REMOVED AND REPLACED SEAT TRACK PER DWR SPECS AND SRM REQUIREMENTS

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MAIN CARGO DECK FLOOR STRUCTURE BETWEEN FRAMES 74 AND 75, Y2127.5 HAS A CRACK ON Z CHANNEL VERIFIED STEP # 16 OF EA # 300-5318-27-A4081 OF PRELIMINARY 2 WERE RII

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 27,614 hrs · 17,062 cycles

MAJOR REPAIR, MAIN CARGO DECK FLOOR STRUCTURE BETWEEN FRAMES 74 AND 75, Y2127.5 HAS A CRACK ON Z CHANNEL. VERIFIED ACCOMPLISHMENT OF PERMANENT REPAIR IAW EA 300-5318-27-A4081, REV. -.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MAIN CARGO DECK FLOOR STRUCTURE BETWEEN FRAMES 73 AND 74, -Y2127.5 HAS CORROSION REMOVE AND REPLACE SEAT TRACK P/N: A53279221211 PER DWG SPECS AND SRM REQUIREMENTS.<BR><BR>THIS IS A MINOR REPAIR PER GMM 05.04

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 27,609 hrs · 17,059 cycles

MAJOR REPAIR. MAIN DECK FLOOR STRUCTURE BETWEEN FRAME 79-80 AT Y0 HAS CORROSION. COMPLIED WITH REPAIR SEAT TRACK, IAW SRM 53-10-16-201 PARAGRAPH 4 FIGURE 201 (REV. 42).

Part: PROFILE — CRACKED (ZONE 200) · airframe 27,614 hrs · 17,062 cycles

MAJOR REPAIR, MAIN DECK FLOOR STRUCTURE AT FRAME 79, -Y1580.5 HAS A CRACK THROUGH FASTENER HOLE COMPLIED WITH EO-94650-REQ1 AND VT-MAE EA 300-5318-27-A4086, REV. -.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

COMP MAIN CARGO FLOOR PANEL 262DM HAS COMPOSITE DAMAGE.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MAIN DECK FLOOR STRUCTURE AT FRAME 79, -Y1580.5 HAS A CRACK THROUGH FASTENER HOLE OUT OF SEQUENCE PRELIMINARY 1 STEP#12 E.A.#. 300-5318-27-A4086 OK TO INSTALL GIVEN

Part: SUPPORT — BROKEN (ZONE 200) · airframe 27,614 hrs · 17,062 cycles

FR 75, BTW Y1221.2 AND Y1580.5, CLS ADAPTER WITH CORROSION. INSTALLED ADAPTER CLS AT THE MDC, FR 75 BTW Y1221.2 AND Y1580.5. I.A.W AIRBUS SRM 51-40-21-001.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MDC FLOOR, FR 80, BTW Y1221.2 AND Y1580.5, AFT FLOOR STRUCTURE WITH CRACK. INSTALLED PROFILE T AT FR80 Y1221.2 APPLIED IAW A300-600, SRM 51-40-21.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MDC FLOOR 261DM, CRACK ON L/H AFT CORNER.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001.

Part: PROFILE — CRACKED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MAJOR REPAIR, MDC, BTW FR 78 AND FR 79, Y2127.5, Z PROFILE WITH CRACK COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94651-REQ1 AND VT-MAE EA 300-5318-27-A4088, REV. -.

Part: SKIN — CRACKED (ZONE 600 FLAP) · airframe 27,603 hrs · 17,055 cycles

RT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 13. COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94787-REQ1 AND VT-MAE EA 300-5750-27-A4063, REV. -.

Part: RIB — CRACKED (ZONE 500 FLAP) · airframe 27,603 hrs · 17,055 cycles

MAJOR REPAIR, LEFT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 27. CIRCLED IN RED. COMPLIED WITH ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-94788-REQ1 AND VT-MAE EA 300-5750-27-A4064, REV. -.

Part: SKIN — CRACKED (ZONE 600 FLAP) · airframe 27,603 hrs · 17,055 cycles

RT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 27. COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94787-REQ1 AND VT-MAE EA 300-5750-27-A4063, REV. -.

Part: SKIN — CRACKED (ZONE 600 FLAP) · airframe 27,603 hrs · 17,055 cycles

RT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 26. COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94787-REQ1 AND VT-MAE EA 300-5750-27-A4063, REV. -.

Part: ADAPTER — CORRODED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MAJOR REPAIR, MDC FR28 Y0 RH CLS ADAPTER HAS CORROSION INSIDE DOT 5612-35 COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94687-REQ1 AND VT-MAE EA 300-5314-27-A4053 REV. -.

Part: ADAPTER — CORRODED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MDC FR27 Y0 LH CLS ADAPTER HAS CORROSION DOT 5612-36 INSTALLED NEW CLS ADAPTER IAW A300-600 SRM 51-40-21.

Part: RIB — CRACKED (ZONE 500 FLAP) · airframe 27,603 hrs · 17,055 cycles

MAJOR REPAIR, LEFT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 26. COMPLIED WITH ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-94788-REQ1 AND VT-MAE EA 300-5750-27-A4064, REV. -.

Part: ADAPTER — CORRODED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MDC FR27 Y0 LH CLS ADAPTER HAS CORROSION DOT 5612-37 INSTALLED NEW CLS ADAPTER IAW SRM 51-40-21.

Part: ADAPTER — CORRODED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MDC FR28 Y0 LH CLS ADAPTER HAS CORROSION ON FLANGE AND INSIDE DOT 5612-34 COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94687-REQ1 AND VT-MAE EA 300-5314-27-A4053 REV. -

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

MAJOR REPAIR, MDC FR28 Y0 SEAT TRACK HAS CORROSION. COMPLIED WITH ACCOMPLISH PERMANENT REPAIR, SEAT TRACK PER SRM 53-10-16-201 PARAGRAPH 4 FIGURE 201.

Part: ADAPTER — WORN (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

CLS ADAPTER AT FR57.1 Y0 LH HAS CORROSION. COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94652-REQ1 AND VT-MAE EA 300-5316-27-A4065 REV. - .

Part: ADAPTER — CORRODED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

CLS ADAPTER AT FR71 IB OF Y1580 HAS CORROSION. REMOVED AND REPLACED CLS ADAPTER IAW PRODUCTION DRAWING REQUIREMENTS AND SRM CHAPTER 51 REQUIREMENTS.

Part: STOP FITTING — GOUGED (ZONE 800) · airframe 27,603 hrs · 17,055 cycles

FWD CREW DOOR STOP ( FROM FWD FACE OF THE DOOR ) NR 5 FROM LOWER APPEAR TO HAVE GOUGES .

Part: STOP FITTING — GOUGED (ZONE 800) · airframe 27,614 hrs · 17,062 cycles

FWD CREW DOOR STOP ( FROM FWD FACE OF THE DOOR ) # 7 FROM LOWER APPEAR TO HAVE GOUGES . 89-831 REMOVED AND REPLACED FWD CREW DOOR STOP ( FROM FWD FACE OF THE DOOR ) # 7 FROM LOWER IAW A300/600 AMM 52-10-31/401.

Part: ADAPTER — CORRODED (ZONE 200) · airframe 27,605 hrs · 17,056 cycles

CLS ADAPTER AT FR43 Y0 LH HAS CORROSION. COMPLIED WITH EO-94969-REQ1 AND VT-MAE EA 300-5315-27-A4057 REV.-.

Part: STOP FITTING — GOUGED (ZONE 800) · airframe 27,603 hrs · 17,055 cycles

FWD CREW DOOR STOP ( FROM FWD FACE OF THE DOOR ) NR 7 FROM LOWER APPEAR TO HAVE GOUGES .

Part: ADAPTER — CORRODED · airframe 27,603 hrs · 17,055 cycles

CLS ADAPTER AT FR38.1 RT OTBD IS BROKEN. COMPLIED WITH REMOVED AND REPLACED CLS ADAPTER IAW PRODUCTION DWR REQUIREMENTS AND SRM CHAPTER 51 REQUIREMENTS

Part: ADAPTER — WORN (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

CLS ADAPTER AT FR62 Y0 LH HAS WEAR DOT 5612-16 COMPLIED ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94688-REQ1 AND VT-MAE EA 300-5317-27-A4067 REV. - .

Part: ADAPTER — BROKEN (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

CLS ADAPTER AT FR34 RH OB IS BROKEN. COMPLIED WITH REMOVE AND REPLACE 1(EA) CLS ADAPTER P/N B53774136204 PER PRODUCTION DRAWING REQUIREMENTS AND A300-600F SRM CHAPTER 51 REQUIREMENTS

Part: STOP FITTING — GOUGED (ZONE 800) · airframe 27,614 hrs · 17,062 cycles

FWD CREW DOOR STOP ( FROM FWD FACE OF THE DOOR ) # 6 FROM LOWER APPEAR TO HAVE GOUGES . 89-830 CLEANED AREA AT FWD CREW DOOR STOPS (FROM FWD FACE OF THE DOOR) # 6, AFTHER FURTHER EVALUATION AND REMOVED DAMAGE, ORIGINAL THICKNESS 0.135", REMOVED THICKNESS 0.003", REMAINING THICKNESS 0.132". MAX REWORK 5% FOUND WITHIN LIMITS. IAW A300-600, SRM 52-11-00, FIG 101, TABLE 102, DAMAGE CODE L.

Part: STOP FITTING — GOUGED (ZONE 800) · airframe 27,603 hrs · 17,055 cycles

FWD CREW DOOR STOP ( FROM FWD FACE OF THE DOOR ) NR 6 FROM LOWER APPEAR TO HAVE GOUGES.

Part: STOP FITTING — GOUGED (ZONE 800) · airframe 27,614 hrs · 17,062 cycles

FWD CREW DOOR STOP ( FROM FWD FACE OF THE DOOR ) # 8 FROM LOWER APPEAR TO HAVE GOUGES . 89-832 REMOVED AND REPLACED ADJUSTABLE BOLT FOR DOOR FITTING IAW A300 AMM 52-10-31/401 STEP 2B(2) AND 2D(2). ADJUSTED FWD PASSENGER/CREW DOORS STOP FITTINGS IAW A300 AMM 52-10-11/501, GAP CHECK GOOD.

Part: ADAPTER — CORRODED (ZONE 200) · airframe 27,605 hrs · 17,056 cycles

CLS ADAPTER AT FR40 Y0 RH HAS CORROSION. .COMPLIED WITH EO-94969-REQ1 AND VT-MAE EA 300-5315-27-A4057 REV.-. CASS FEEDBACK REPORT COMPLETED AND FORWARDED TO [email protected]. JOB COMPLETE

Part: ADAPTER — WORN (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

ADAPTER AT FR56 Y0 RH HAS CORROSION COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94652-REQ1 AND VT-MAE EA 300-5316-27-A4065 REV. - .

Part: STOP FITTING — GOUGED (ZONE 800) · airframe 27,614 hrs · 17,062 cycles

FWD CREW DOOR STOP ( FROM FWD FACE OF THE DOOR ) # 5 FROM LOWER APPEAR TO HAVE GOUGES . 89-829 REMOVED AND REPLACED FWD CREW DOOR STOP ( FROM FWD FACE OF THE DOOR ) # 5 FROM LOWER IAW A300/600 AMM 52-10-31/401.

Part: ADAPTER — CRACKED (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

CLS ADAPTER AT FR38.1 LH OB IS BROKEN DOT 5612-28 COMPLIED WITH REMOVE AND REPLACE 1(EA) CLS ADAPTER P/N B53774136204 PER PRODUCTION DRAWING REQUIREMENTS AND A300-600F SRM CHAPTER 51 REQUIREMENTS

Part: ADAPTER — BROKEN (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

CLS ADAPTER AT FR38 LH OB IS BROKEN. COMPLIED WITH REMOVE AND REPLACED 1(EA) CLS ADAPTER P/N B53774136204 PER PRODUCTION DRAWING REQUIREMENTS AND SRM CHAPTER 51 REQIREMENTS.

Part: ADAPTER — BROKEN (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

CLS ADAPTER AT FR37 RH OB IS BROKEN. COMPLIED WITH REMOVED AND REPLACE 1(EA) CLS ADAPTER P/N B53774136204 PER PRODUCTION DRAWING REQUIREMENTS AND A300-600F SRM CHAPTER 51 REQUIREMENTS

Part: STOP FITTING — GOUGED (ZONE 800) · airframe 27,603 hrs · 17,055 cycles

FWD CREW DOOR STOP ( FROM FWD FACE OF THE DOOR ) # 8 FROM LOWER APPEAR TO HAVE GOUGES . 89-832 APPROVED.

Part: ADAPTER — WORN (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

CLS ADAPTER AT FR57.1 Y0 RH HAS CORROSION. COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94652-REQ1 AND VT-MAE EA 300-5316-27-A4065 REV. - .

Part: ADAPTER — WORN (ZONE 200) · airframe 27,603 hrs · 17,055 cycles

CLS ADAPTER AT FR54.2 Y0 RH HAS WEAR DOT 5612-15 COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94652-REQ1 AND VT-MAE EA 300-5316-27-A4065 REV. - .

Part: SUPPORT — CRACKED (ZONE 100) · airframe 27,614 hrs · 17,062 cycles

AFT CARGO FR 54 VERTICAL SUPPORT AT Y953 LH IS CRACKED INSTALLED VERTICAL SUPPORT AT AFT CARGO FR 54 Y953 LH APPLIED IAW A300-600, SRM 51-40-21.

Part: SUPPORT — CORRODED (CEILING) · airframe 27,603 hrs · 17,055 cycles

FAULT - STR - Z100 - AFT CARGO FR 54.2 CENTER HORIZONTAL CEILING SUPPORT IS CORRODED AT FASTENER HOLES INSTALLED CEILING SUPPORT AT AFT CARGO FR54.2 IAW A300-600 SRM 51-40-21.

Part: SUPPORT — CORRODED (CEILING) · airframe 27,603 hrs · 17,055 cycles

FAULT - STR - Z100 - AFT CARGO FR 54.2 RH HORIZONTAL CEILING SUPPORT IS CORRODED AT FASTENER HOLES INSTALLED CEILING SUPPORT AT AFT CARGO FR54.2 R/H. IAW A300-600 SRM 51-40-21.

Part: SEAL — CRACKED (ZONE 800) · airframe 27,603 hrs · 17,055 cycles

AFT CARGO FR 65 RH DOOR LANDING UPPER CORNER IS CRACKED INSTALLATION OF SECTION CEILING ANGLE SUPPORT. JOB COMPLETE.

Part: VERTICAL SUPPORT — CRACKED (ZONE 100) · airframe 27,603 hrs · 17,055 cycles

AFT CARGO FR 54 VERTICAL SUPPORT AT Y0 IS CRACKED VERIFIED STEP 13 C/W, TASK IS COMPLETE

Part: VERTICAL SUPPORT — CRACKED (ZONE 100) · airframe 27,603 hrs · 17,055 cycles

AFT CARGO FR 54 VERTICAL SUPPORT AT Y-1959 IS CRACKED VERIFIED STEP 14 C/W, TASK IS COMPLETE.

Part: VERTICAL SUPPORT — CRACKED (ZONE 100) · airframe 27,603 hrs · 17,055 cycles

AFT CARGO FR 54 VERTICAL SUPPORT AT Y953 RH IS CRACKED VERIFIED STEP 13 C/W, TASK IS COMPLETE.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 27,614 hrs · 17,062 cycles

AFT CARGO FR 54 VERTICAL SUPPORT AT Y-1959 IS CRACKED INSTALLED VERTICAL SUPPORT AT AFT CARGO FR 54 Y-1959 APPLIED IAW A300-600, SRM 51-40-21.

Part: VERTICAL SUPPORT — CRACKED (ZONE 100) · airframe 27,614 hrs · 17,062 cycles

AFT CARGO FR 54 VERTICAL SUPPORT AT Y953 RH IS CRACKED INSTALLED VERTICAL SUPPORT AT AFT CARGO FR 54 Y953 RH APPLIED IAW A300-600, SRM 51-40-21.

Part: ANGLE — CRACKED (ZONE 100) · airframe 27,603 hrs · 17,055 cycles

AFT CARGO FR 54 VERTICAL SUPPORT AT Y-953 IS CRACKED. INSTALED NEW PART IAW SRM 51-40-21.

Part: VERTICAL SUPPORT — CRACKED (ZONE 100) · airframe 27,603 hrs · 17,055 cycles

AFT CARGO FR 54 VERTICAL SUPPORT AT Y953 LH IS CRACKED VERIFIED STEP14 C/W, TASK IS COMPLETE.

Part: SUPPORT — CORRODED (CEILING) · airframe 27,603 hrs · 17,055 cycles

FAULT - STR - Z100 - AFT CARGO FR 54.2 LH HORIZONTAL CEILING SUPPORT IS CORRODED AT FASTENER HOLES INSTALLED CEILING SUPPORT AT AFT CARGO FR54.2 L/H. IAW A300-600 SRM 51-40-21.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 27,603 hrs · 17,055 cycles

AFT CARGO FR 62 CENTER HORIZONTAL CEILING SUPPORT IS CORRODED AT FASTENER HOLES INSTALLED CEILING SUPPORT ON AFT CARGO FR 62 IAW SRM 51-40-21.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 27,603 hrs · 17,055 cycles

AFT CARGO FR 54 VERTICAL SUPPORT AT Y1959 IS CRACKED.REMOVED SUPPORT AT AFT CARGO FR 54 VERTICAL Y 1959 IAW - SRM 51-40-21.LOCATED AND DRILL SUPPORT AT AFT CARGO FR54 Y 1959 IAW SRM 51-40-21.INSTALED NEW PART P/N: A5341076522200 IAW SRM 51-40-21.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 27,614 hrs · 17,062 cycles

AFT CARGO FR 54 VERTICAL SUPPORT AT Y0 IS CRACKED INSTALLED VERTICAL SUPPORT AT AFT CARGO FR 54 Y 0 APPLIED IAW A300-600, SRM 51-40-21.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 27,603 hrs · 17,055 cycles

AFT CARGO FR 54 CENTER HORIZONTAL CEILING SUPPORT IS CORRODED AT ATTACHING POINT. INSTALLED EXTRUSION SUPPORT STRUCTURE AT THE FR54 IN THE AFT CARGO PIT IAW SRM 51-40-21-001. REVIEWED

Part: SKIN — DENTED (ZONE 100) · airframe 27,603 hrs · 17,055 cycles

MAJOR REPAIR, LEFT SIDE FUSELAGE SKIN DENT REPAIR BETWEEN FR0-FR1 REQUIRES PERMANENT REPAIR. COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IAW EO-79250-REQ1 AND VT-MAE EA 300-5311-27-A4048, REV. -.

Part: SKIN — DENTED (ZONE 100) · airframe 27,623 hrs · 17,065 cycles

MAJOR REPAIR, DENT WITH GAUGE FWD OF TAIL STAND ON RIGHT HAND SIDE. ACCOMPLISHED REPAIR DAMAGE IAW SRM 53-10-12-201, PARAGRAPH 11 AND FIGURE 208 (SHEET 1).

Part: INDICATION SYS — FAULTED (ZONE 800) · airframe 27,115 hrs · 16,778 cycles

REF. MEL 52-11-01-2-4. MAIN ENTRY DOOR/SLIDE INOP "CREW SIGN OFF" VERIFIED MAIN ENTRY DOOR (L1) CLOSED, AND LOCKED. MEL/ DMP 52-11-01-2-4.

Part: INDICATION SYS — FAULTED (ZONE 800) · airframe 27,115 hrs · 16,778 cycles

AFTER DIS-ARMING CABIN DOOR AND PUSHING TEST BUTTON. DOOR SHOWS DISARMED UNTIL THE DOOR IS OPENED. WARNING IS CONTINUOUS. DOOR SHOWS SLIDE ARMED AFTER OPENING DOOR.SLIDE DIDN€™T DEPLOY INSTALLED NEW SLIDE W/REF TO AMM 25-61-21/401. OPS NORMAL.

Part: WINDOW — FIRE (ZONE 200) · airframe 26,936 hrs · 16,675 cycles

DURING CLIMBOUT NOTICED/HEARD A WHEEZING NOISE: FOLLOWED BY ARCING-SMALL FLAMES IN LOWER CORNER OF FO€™SWINDOW: A CRACK FROM THAT CORNER TO MIDWAY DEVELOPED- AFTER LEVELING OFF AT 14,000 THE CRACK DOUB ACCOMPLISHED AMM 56-11-11/401 F, ATB

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 26,267 hrs · 16,269 cycles

HOLE FOUND IN MAIN CARGO FLOOR AT 4R. REMOVED THE NO-SLIP MATERIAL FROM THE SURFACE OF THE FLOOR PANEL. SECURED THE LOWER PATCH WITH EPOXY ADHESIVE IN THE HOLE LOCATEDIN THE LOWER SKIN PER A300-600F SRM 51-77-10-201

Part: SIGN — INOPERATIVE (DOOR) · airframe 25,323 hrs · 15,665 cycles

INSPECTION TYPE:NACREW DOOR EXIT SIGN EMERGENCY LIGHT INOP OPENED SAFETIED AND TAGGED CIRCUIT BREAKERS E28M 22VU AND P80 M 132VU FOR REMOVAL / INSTALLATION OF EXIT MODULE REF AMM 33-51-13-0401REMOVED AND REPLACED DOOR EXIT SIGN MODULE PER A300 AMM 33-51-13-0401 REMOVED SAFTEY CLIPS AND TAGS AND CLOSED CIRCUIT BREAKERS 21WL AND 65WL ACCOMPLIHSED EMERGENCY LIGHT TEST PER A300 AMM 33-51-13-4010 OPS TEST OK A300 IPC : 33-51-04-098-040

Part: COVER — LOOSE (L1 DOOR SLIDE) · airframe 25,284 hrs · 15,639 cycles

L1 DOOR SLIDE PACK COVER LOOSE. REMOVED SLIDE, SLIDE COVER, & GIRT BAR IAW AMM 25 61 21. REMOVED & REPLACED L1 DOOR ESCAPE SLIDE IAW AMM 25-61-21.

Part: PANEL — INOPERATIVE (CABIN) · airframe 24,943 hrs · 15,427 cycles

INSPECTION TYPE:NAEMER EXT LT PANEL ABOVE CREW ENTRY DOOR IS FALLING OFF.RESECURED EMERGENCY EXIT LT PANEL IN REF TO AMM 33-50-00.

Part: DAMPER — UNSERVICEABLE (L-1 DOOR) · airframe 24,778 hrs · 15,317 cycles

INSPECTION TYPE:N/A*MAJOR REPAIR* EMERGENCY DOOR DAMPNER WILL NOT HOLD PRESSUEREMOVED AND REPLACE WITH SERVICEABLE UNIT AMM 52-10-14-0401

Part: FITTING — CRACKED (NOT REPORTED) · airframe 24,723 hrs · 15,284 cycles

INSPECTION TYPE:CK1HOLE 9 CRACK INDICATION IN FR21 FORK FITTINGREPAIRED PER EA 300-5231-27-A3131

Part: FITTING — CORRODED (NOT REPORTED) · airframe 24,723 hrs · 15,284 cycles

INSPECTION TYPE:CK1CHOLE 5 CORROSION INDICATION IN FR22A FORK FITTINGREPAIRED PER EA 300-5231-27-A3131

Part: FITTING — CRACKED (FR 47) · airframe 24,723 hrs · 15,284 cycles

INSPECTION TYPE:CK1CCRACK INDICATION AT FR47 UPPER RADIUS 3MMREPEAT INSPECTIONS AT 1400 FC INTERVALS PER EO A300-5310-18290-R

Part: NONE — NONE (FUSELAGE) · airframe 23,030 hrs · 14,357 cycles

INSPECTION TYPE:N/A**ATB**EMERG DEC'D**FIRE DEPT USED**THERMAL CAMERAS USED** A/C LANDED W/OUT INCIDENT**RCVD AFT COMP LOOP FAULT ECAM MSG. RAN CHECKLIST AND THEN RCVD CARGO COMPT SMOKE WARNING LAND ASAP, BACK TO DFW.PLACARDED LOWER AFT CARGO AGENT BOTTLES INOP IAW MEL 26-16-02-2 PFM BOX VERIFIED EMPTY DMP COMPLIED WITH. REPLACED BOTH FWD & AFT LWR CARGO PIT FIRE EXTINGUISHER BOTTLES IAW A300 AMM 26-23-11 OPERATIONAL RESTORED. THIS CLEARS M764098 ESR 26-23-02-07.

Part: LIGHT — NONE (CABIN) · airframe 22,860 hrs · 14,245 cycles

INSPECTION TYPE:N/A"EMER EXIT LIGHTS" WERE ON INTERMITTENTLY IN ARM POSITION.SECOND TIME ITEM INTERMITTENT. R&R EPSU IAW MM 33-51-14 NO HELP. R&R CONTACTOR FIN 1XX IAW MM 24-42-11 NO HELP. R&R EMER LT CTL SWITCH FIN 22WL IAW MM 33-51-03 OPS. CK GOOD IAW MM 33-51-00. REF. MM 36-11-00

Part: LIGHT — ILLUMINATED (CABIN) · airframe 22,841 hrs · 14,231 cycles

INSPECTION TYPE:N/AAFTER TAKEOFF CREW NOTICED EMPERGENCY EXIT LGIHT ING ILLUMINATED WHIE IN ARM POTION ALLOTHER ELECTRICAL INDICATIONS NORMLA EXIT LIGHTING LATER TURNED OFF ON ITS OWNPERFORMED OPS CK OF EMERGENCY LIGHT SYS. REFERECING TO AMM 33 51 00. NO DEFECTS NOTED AT THIS TIME OK FOR CONTINUED SVC.

Part: POWER SUPPLY — INOPERATIVE (EVACUATION SLIDE) · airframe 22,787 hrs · 14,199 cycles

EVAC SLIDE WARNING LIGHT INOP. EVAC SLIDE WARNING LIGHT INOP IAW MEL 52 73 01 1 PLACKARDS INSTALLED.R/R AUTONOMOUS STANDBY POWER SUPPLY UNIT (70WN) IAW AMM 52-73-18-0401. INSTALLED 2 NEW BATTERIES AS WELL. OPS CK GOOD. THIS CLEARS M755587

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: SEG EMERGENCY EXIT LIGHT ASSEMBLY ABOVE L-1 DOOR CONNECTOR CONTRACTS WILL OT LOCK IN PLACE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY PN 10-0984-1 SN 3014 IAW AMM 33-51-13-0401.

Part: ANGLE — CRACKED (NR 1 NACELLE) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: A300 NR 1 PYLON AT LT SIDE AT RIB 4 AREA HAS A CRACK STRUCTURAL NGLE LOCATED AT AREA INSIDE ACCESS PANEL 413CL CUT OUT. REPAIRED NR 1 PYLON ON VT MAE TRAVELER T2/1534571 IAW SRM 54-50-00.

Part: SUPPORT — CORRODED (CEILING LINER) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:A300CEILING LINER SUPPORTS 3 EA ATTACHED TO THE LOWER AFT SECTION OF FLOOR BEAM 54.2 CORRODED IN SEVERAL PLACES2 EA CEILING LINER SUPPORTS CORRODED OUT OF LIMITS REMOVED FABRICATED NEW SUPPORTS AND REPLACED IAW SRM ONE EACH FOUND TO BE IN LIMITS AND TREATED PRIME AND PAINTED IAW SRM 51-73-11 & 51-40-21.

Part: FLOOR PANEL — DAMAGED (COCKPIT) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGFLIGHT DECK FLOOR PANEL #211JPREMOVED AND REPLACE IAW AMM 53-11-21

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:A300PNL 251XJ DAMAGEDFABBED IAW SRM A300-5320-40552-B

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:A300PNL 231LG DAMAGEDFABBED IAW ARM SREO A300-5320-40552-B

Part: PANEL — DAMAGED (MAIN CARGO FLOOR) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: A300 MCD FLOOR PANEL 241KF IS DAMAGED. SREO A300-5320-42722.

Part: INTERCOSTAL — CRACKED (RT WING SPOILER) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGINTER COSTAL AND SUPPORT FOUND CRACKED DURING SKIN REPAIR AFT OF #3 SPOILER REMOVED AND REPLACED INTER COASTAL AND SUPPORT IAW SRM 51-40-21

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGAFT CATGO COMPARTMENT FLOOR BOARD #152KG-CORNER DAMAGED AS MAKEDSRO A300-5320-42722

Part: FLOOR PANEL — DAMAGED (AFT CARGO COMPT) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: SEG AFT CARGO COMPARTMENT FLOOR BOARD 152UF-CORNER DAMAGE, AS MARKEDS REO A300-532-4272F.

Part: FLOOR PANEL — DAMAGED (AFT CARGO COMPT) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: SEG AFT CARGO COMPARTMENT FLOOR BOARD 152QI E EACH CORNERS ARE DAMAGED, AS MARKED, SREO A300-5320-42722.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGAFT CARGO COMPARTMENT FLOOR BOARD #152TF CONMER DAMAGED AS MAKEDSREO A300-5320-42700

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGAFT CARGO COMPARTMENT FLOOR BOARD #151LG CONER DAMAGED AS MARKEDSREO A300-5320-42722

Part: MOUNT FITTING — CORRODED (L-1 DOOR CLOSET) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:A300CLOSET MOUNT FITTING HAS SEVERE EXFOLIATIONREMOVED AND REPLACED MOUNT FITTING IAW CMM 25-24-07

Part: FLOOR PANEL — DAMAGED (LWR CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:A300PNL 131RG DAMAGEDFABBED PER SREO A300-5320-16407-

Part: FLOOR PANEL — DAMAGED (MAIN CARGO COMPT) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: SEGMAIN CARGO DECK COMPARTMENT DOOR PANEL 252ZL IS DAMAGED AND BROKEN SREO A300-5320-42722.

Part: FLOOR PANEL — DAMAGED (LWR CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:A300PNL 132FE IS DAMAGEDFABBED PE SREO A300-5320-16407-E

Part: FLOOR PANEL — DAMAGED (LWR CARGO) · airframe 22,125 hrs · 13,778 cycles

PNL 132QG HAS DAMAGEFABBED PER SREO A300-5320-16407-E

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: A300 PANEL 131AH HAS AREAS WITH DAMAGED COMPOSITES REO A300-5320-42722.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: C FWD CABIN JUST AFT OF COCKPIT CTR FLOOR HAS LOWER SURFACE DAMAGE AS MARKED. SREO A300-5320-42722.

Part: FLOOR PANEL — DAMAGED (LWR CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:A300PNL 131GE IS BROKENFABBED PER SREO A300-5320-16407-E

Part: FLOOR PANEL — DAMAGED (E/E BAY) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGFWD E/E BAY FLOOR PANEL #121EF IS DAMAGED AT CUTOUTSREO A300-42722

Part: FLOOR PANEL — DAMAGED (LWR CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:A300PNL 132MG DAMAGEDFABBED PER SREO A300 5320-16407-E

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: A300 PANEL 132AH HAS EXPOSED COMPOSITE HONEY COMB ON EDGE OF PANELS REO A300-5320-42722.

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:A300PNL 252XJ DAMAGEDFABBED IAW SREO A300-5320-40552-B

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: A300 PANEL 132PG HAS DAMAGED COMPOSITE IN SEVERAL AREAS SREO A300-5320-42722.

Part: CARGO TRACK — DAMAGED (FR 65) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEG AFT MAIN DECK CARGO COUPT LH SEAT TRACK AT Y1959 AT FR65 AREA HAS (1EA) ENLARGED FASTERNER HOLE.REPAIRED SEAT TRACK IAW A300 SRM 53-10-16

Part: BULKHEAD — CRACKED (NR 1 INLET) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:A300#1 ENGINE INLET COWL AFT BULKHEAD CRACKED AT I/B PT2 PROBE SENSOR ATTACH POINTREPAIRED BULKHEAD IAW P&W SRM 54-10-00 REPAIR 14

Part: BULKHEAD — CRACKED (NR 1 INLET) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:A300#1 ENGINE INLET COWL AFT BULKHEAD CRACKED AT O/B PT2 PROBE SENSOR ATTACH POINTREPAIRED BULKHEAD IAW P& W SRM 54-10-00 REPAIR 14

Part: FLOOR PANEL — DAMAGED (LWR CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:A300PNL 131BH DAMAGEDFABBED PER SREO A300-5320-16407-E

Part: FLOORBEAM — CRACKED (MAIN CABIN FR42B) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: SEG MAIN CABIN FLOOR BEAM STUB TRACK AT FR 42 LT AND RT OF BLO SUSPECTED CRACKS. REMOVED SCORE MARKED IAW SRM 53-10-16. INSTALLED STUB TRACK IAW SRM 51-40-21.

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGPNL 251NJ DAMAGEDFABBED IAW SREO A300-5320-40552-B

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGPNL 251WJ DAMAGEDFABBED AW SREO A300-5320-40552-B

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: A300 PNL 252VJ BROKEN. FABBED IAW SREO A300-5320-40552-B.

Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: NA MAIN FLOOR PANEL NR 231PH IS BROKEN SREO A300-5320-42722.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:A300MAIN DECK CARGO COMPT. FLOOR PANEL 251FJ IS DAMAGED AND BROKEN REPAIRED IAW SERO A300-5320-42722

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGPNL 251UJ BROKENFABBED IAW A300-5320-40552-B

Part: WEB — CORRODED (MAIN DECK) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGMAIN CARBIN FLOOR WEB UNDER PANEL 231MJ HAS SERVEALS ARAS WITH CORRSIONREMOVED AND REPLACED ADAPTER IAW A300 SRM 51-40-21

Part: FLOOR PANEL — DAMAGED (MAIN CABIN DECK) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: SEG PNL 252FJ DAMAGED. FABBED IAW SREO A300-5320-40552-B.

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGMAIN DECK CARGO COMP. FLOOR PANEL 252HM IS DAMAGED AND BROKENSREO A300-5320-42722

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGPNL 251BN DAMAGEDFABBED IAW SREO A300-5320-40552-B

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGPNL 251LJ DAMAGEDFABBED IAW SREO A300-40552-B

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGPNL 251PG DAMAGEDFABBED IAW SREO A300-5320-40552-B

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:A300PNL 251LG DAMAGEDFABBED IAW SREO A300-5320-40552-B

Part: SEAT TRACK — DAMAGED (MAIN DECK) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGAFT MAIN CARGO DEACK SEAT TRACK AT -450 HAS AN ENGLAGED AND ADAMGED FASTENER HOLE BETWEEN FR 73 AND 74PER SRM 53-10-16 FIGURR 202

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: C RT WING I/B FLAP UPPER SKIN L SHAPED REPAIR DOUBLER HAS A CHAFFE MARK. REMOVED AND REPLACED DOUBLER IAW SRM 57-50-00 FIG 205 RCD NR 184819.

Part: SEAT TRACK — CORRODED (FR79-80) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:A300AFT MAIN CARGO COMPT. DECK LH SEAT TRACK LOCATED AT Y1137. 1 BETWEEN FRAMES 79 TO 80 HAS CORROSION LOCATED AT AREA BETWEEN FLOOR PANEL 261HM AND 261FMREPAIRED IAW SRM 53-10-16 FIG 201

Part: CARGO TRACK — CORRODED (FR79-80) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGAFT MAIN CARGO COMPT DECK LH SEAT TRACK LOCTED A TO BETWEEN FRAMES 79-80 HAS CORROSION LOCATED AT AREA BETWEEN FLOOR PANELS 26EM AND 262EM.REPAIRED IAW SRM 5-10-16 FIG 201.

Part: INTERCOSTAL — BENT (FRAMES 86-87) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGTHS COMPARTMENT R/H LOWER INTER COSTAL BETWEEN FR86 AN DFR87 BENT DOT #54-02REMOVED A D REPLACED NEW PAT IAW A300 SRM 51-40-21.

Part: FLOOR PANEL — DAMAGED (LWR CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:A300PNL 161HF DAMAGEDFABBED PER SREO A300-5320-16407-E

Part: ANGLE — CRACKED (LT PACK RAM AIR) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: SEG EXTERNAL LOWER FUSELAGE HAS FAIRING SUPPORT CLIP CRACKED AHEAD OF LT PACK AIR. REMOVED AND REPLACED FAIRING SUPPORT PN A5341042621601, IAW A300 SRM 51-40-21.

Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGMAIN CABIN FLOOR PNL 232HL BROKEN AS MARKEDSREO A300-5320-42722

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: A300 MAIN CABIN FLOOR PANEL NR 231KJ BROKEN AND MISSING EDGE FILL VARIOUS SPOTS SREO A300-5320-42722.

Part: WEB — CORRODED (MAIN DECK) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SGEMAIN CABIN FLOOR SUPPORT WEB AND TRACK FLOOR FR 22 TP FR27 BO TO 8 LH AND RH SPOTS OF CORROSIO AN DBARE METALREMOVED AND REPLACED SUPPORT WEB PER SRM 51-74-10 & 51-40-21.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGMAIN CABIN FLLOR PANEL 232QH HAS DAMAED AS MARKEDSREO A300-5320-42722

Part: STRUCTURE — GOUGED (THRUST REVERSER) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:A300#2 ENG LH T/R HAS CHAFFED/GOUGED AREAREMOVED AND REPLACED TRAILING EDGE IAW A300 SRM 51-40-21 AND 51-40-44

Part: FLOOR PANEL — DAMAGED (BULK CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: SEG PANEL 162HF HAS DMAGE AT EDGE, AS MARKED, SREO A300-5320-72722.

Part: FLOOR PANEL — DAMAGED (LWR CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGPANEL 162HF CRACKEDFABBED PER SREO A300-5320-16407-E

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: SEG MAIN CABIN RT OB FLOOR PANEL 232EF HAS CORROSION ON SEAT TACK OB FWD CORNER. COMPLIED WITH A300 SRM 53-10-15 AND 53-10-16.

Part: SUPPORT ANGLE — CRACKED (WING TE) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:A300LH WING FIXED TRAILING EDGE SUPPORT ANGLE CROCKEDREMOVED AND REPLACED IAW SRM 51-40-21

Part: FLOOR PANEL — DAMAGED (BULK CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: SEG PANEL 162HF HAS DAMAGE AT ECENTER CUT-OUT SREO A300-5320-42722.

Part: FLOOR PANEL — DENTED (BULK CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: SEG PANEL 161LF DENTED, AS MARKED. SREO A300-5320-42722.

Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGMAIN CABIN FLOOR PANEL 231 NJ IS BROKEN AS MARKEDSREO A300-5320-42722

Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGMAIN CABIN FLOOR PANEL 232SG BROKEN AS MAKEDSREO A300-5320-42722

Part: FLOOR PANEL — DAMAGED (BULK CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: SEG PANEL 161MF HAS SEPARATION AT (2) CORNERS. SREO A300-5320-42722.

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGPNL 152RF DAMAGEDFABBED PER SREO A300-5320-16407-E

Part: FITTING — CRACKED (THRUST REVERSER) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: SEG NR 1 ENG LT, TR HAS A CRACKED AND DAMAGED CIRCUMFERENTIAL FITTING M AT AFT UPPER CORNER. REMOVED AND REPLACED FITTING IAW A300-600 SRM 51-40-21.

Part: ATTACH BRACKET — CRACKED (FAIRING) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: SEG FAIRING 485 ALIB ATTACH BRACKET FOR FORWARD RIB HAS CRACK AT LOWER PORTION. R & R FAIRING PER ACCESS 104 WORK CARD AND IPC 54-54-06-020.

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGPNL 151KG DAMAGEDFABBED PER SRRO A300-5320-16404-E

Part: ROLLER — WORN (RT WING FLAP) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGRH WING OUTBOARD FLAP UPPER L/E SURFACE ROLLER WEAR PLATES ARE GOUGED/WORNREMOVED AND REPLACED STRIP ROLLER IAW A300 SRM 51-40-21.

Part: WEB — CRACKED (NACELLE) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGPANEL 413 BL 92) CRACKS ON INTERIOR WEB BELOW SEAL RETAINERREPAIRED PANEL PER SRM 54-52-51 FIG 204

Part: ACCESS PANEL — CORRODED (RT NACELLE) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGPANEL 414ER HAS (10 AREA OF CORRORION OF FAUGEREMOVED CORROSION IAW A300 SRM 51-74-10. FOUND TO BE IN LIMITS IAW A3000 SRM 54-52-71.

Part: HINGE FITTING — CHAFED (RT NACELLE) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: A300 NR 1 ENGINE RT FAN COWL AFT HINGE FITTING HAS CHAFF MARKS. REMOVED AND REPLACED HINGE FITTING IAW SRM 51-40-21.

Part: SKIN — CRACKED (RT WING TE) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGRH WING T/E UPPER SURFACE OF SKIN JUST FWD OF #5 SPOILER HAS MULTIPLE LOSSE RIVERS AND APPROX 3 INCH SKIN CRACK.REPAIRED IAW A300 SRM 57-51-12 FIG 207

Part: SKIN — DAMAGED (NR 3 SPOILER) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: SEG RT WING T/E UPPER SURFACE SKIN JUST FWD OF NR 3 SPOILER HAS MULTIPLE LOOSE FASTENER AND APPROX. 3 INCH CRACK AS MARKED. REPAIRED IAW SRM 57-51-12 FIG 207.

Part: HINGE FITTING — CHAFED (LT NACELLE) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: A300 NR 1 ENGINE LT FAN HINGE FITTING HAS CHAFF MARKS. REMOVED AND REPLACED HINGE FITTING IAW SRM 51-40-21.

Part: PANEL — CRACKED (NR 1 NACELLE) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: C PANEL 413BL 4 CRACKS AT VENT CUT OUTS REPAIRED IAW SRM 54-52-51 VTMAE T21/1534548.

Part: ATTACH BRACKET — CHAFED (FUSELAGE) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: C PANEL 147CZ HAS 1EA ATTACH BRACKET CHAFFED. REMOVED AND REPLACED FITTING IAW SRM 51-40-21.

Part: WINDOW FRAME — CORRODED (COCKPIT WINDOW) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE:SEGRH FWD FUSLEAGE UNCROUS REUTED FASTENERS BENEATH RH DLIDING A D AFT FIXED COCKPIT WINDOWS AN DABOVE TOP FWD CORUES OF SLIDING WINDOWREMOVED CORROSIN OAW A300 SRM 51-74-10

Part: SKIN — DENTED (FUSELAGE) · airframe 22,125 hrs · 13,778 cycles

INSPECTION TYPE: SEG LT EXTERNAL FORWARD SKIN HAD 2 DENTS FORWARD OF FR1 DENT MEASURES 4.9 WIDE BY 8.5 LONG BY .385 DEEP THE 2ND DENT MEASURES 4.3 LONG BY 3.8 WIDE BY .070 DEEP. BOTH DENTS WERE DEEMED OUT OF LIMITS AND NEEDED A PERMANENT REPAIR. REPAIRED LT FORWARD EXTERNAL SKIN IAW EA NR 300-5311-27-A2535 STEPS 1 THROUGH 20. REPAIR IS CONSIDERED TEMPORARY AND ACCEPTABLE BUT NEEDS TO EB REPLACED A T 3300 FC.

Part: WARNING LIGHT — INOPERATIVE (DOOR SLIDE) · airframe 21,563 hrs · 13,468 cycles

SLIDE RAFT RELEASE WARNING SYS LIGHT INOP. DEFERRED SLIDE RAFT RELEASE WARNIG LIGHT, PER MEL 52-73-01-1 PLACARD INSTALLED. RELEASE WARNING LIGHT TEST GOOD, REF AMM 52-71-11. THIS CLOSES M720000.

Part: HYDRAULIC LINE — CHAFED (HYDRAULIC SYS) · airframe 19,641 hrs · 12,300 cycles

INSPECTION TYPE:N/A EMERGENCY DECLARED - SHORTLY AFTER TAKE OFF, HYD YELLOW SYS LO PRESS, FOLLOWED BY YELLOW RSVR LO LEVEL.DURING TROUBLE SHOOTING FOUND YELLOW HYD LINE CHAFED AND LEAKING BY RT MLG AFT MOUNT. REMOVED AND REPLACED 4 HYD LINES DUE TO POSSIBLE FURTHER CHAFING IN REFERENCE TO AMM 20-23-11. LEAK CHECK GOOD AT THIS TIME. REFERENCE ML 207320-1 FOR POSSIBLE STARVATION/CAVITATION OF ENG PUMP.

Part: WARNING MESSAGE — FALSE ACTIVATION (#1 ENGINE) · airframe 19,554 hrs · 12,248 cycles

ON SHUTDOWN, RECEIVED AN EPR MODE #1 ENGINE FAULT. ALONG WITH ECAM ENG #1 FAIL & OIL PRESSURE LOW LIGHT ON CENTER INSTRUMENT PANEL.ACCOMPLISHED FADEC GRND TEST PER TSM 73-21-04 NO RETRIEVABLE FAULTS. ACCOMPLISHED ENG RUN IAW AMM 71-00-00 ALL PERAMETERS. NORMAL. ENG. SHUTDOWN NORMAL. NO DEFECTS NOTED.

Part: BLOCKER DOOR — DAMAGED (THRUST REVERSER) · airframe 19,212 hrs · 12,049 cycles

#2 ENG INBOUND #3 BLOCKER DOOR DAMAGED.REPLACED BLOCKER DOOR REF AMM 78-32-13-0401.OPS CHECK OK.

Part: PLATE — CRACKED (NR 2 PYLON) · airframe 18,584 hrs · 11,725 cycles

INSPECTION TYPE:12YR, NR 2 ENG PYLON HAS A CRACKED FISH PLATE O/B FWD CORNER OF PRE COOLER AREA. INSTALLED NEW FISH PLATE IAW SRM 51-40-21.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 18,584 hrs · 11,725 cycles

INSPECTION TYPE:12YR, NR 2 PYLON AFT LOWER FAIRING AFT SKIN IS CRACKED AT BOTTOM CORNER. REPAIRED IAW SREO EO NR A300-5450-21297-1.

Part: COVER — CRACKED (E&E BAY) · airframe 18,584 hrs · 11,725 cycles

INSPECTION TYPE:12YR, E&E COMPARTMENT RT SIDE STRUCTURE FOR BATTERY RACK COVER CRACKED AT AFT I/B SIDE. INSTALLED NEW BATTERY RACK COVER PER SRM 51-40-21.

Part: WEB — CRACKED (LT WING) · airframe 18,584 hrs · 11,725 cycles

INSPECTION TYPE:12YR, LT WING ROOT INTERNAL L/E WEB CRACKED. REMOVED AND REPLACED LT WING KRUEGER FLAP WELL RIB REINFORCEMENT ANGLE IAW SRM 51-40-21 AB DWG 57241993.

Part: FITTING — CRACKED (FUSELAGE) · airframe 18,584 hrs · 11,725 cycles

INSPECTION TYPE:12YR, LEFT WTB SUPPORT RIB CRACKED AT FR 47. REMOVED AND REPLACED FITTING AT FR 47 LT IAW SRM 51-40-21, DWG A53510059.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 18,584 hrs · 11,725 cycles

INSPECTION TYPE:12YR, FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT STA 38.2 AT RBL 41 CLIP CRACKED. REMOVED AND REPLACED NEW UPPER FRAME SUPPORT IAW SRM 51-40-21.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 18,584 hrs · 11,725 cycles

INSPECTION TYPE:12YR, FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT STA 38.2 AT RBL22. REMOVED AND REPLACED NEW UPPER FRAME SUPPORT IAW SRM 51-40-21.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 18,584 hrs · 11,725 cycles

INSPECTION TYPE:12YR, FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT STA 38.2 AT LBL41 CLIP CRACKED. REMOVED AND REPLACED NEW UPPER FRAME SUPPORT IAW SRM 51-40-21.

Part: FRAME ANGLE — CRACKED (FRAME 38.2) · airframe 18,584 hrs · 11,725 cycles

FWD CARGO BAY AFT BULKHEAD UPPER FRAME SUPPORT FRAME 38.2, LBL 22 ANGLE WAS CRACKED. REMOVED AND REPLACED THE FRAME ANGLE IAW SRM 51-40-21.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 18,584 hrs · 11,725 cycles

INSPECTION TYPE:12YR, FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT STA 38.2 AT LBL41 CLIP CRACKED. REMOVED AND REPLACED NEW UPPER FRAME SUPPORT IAW SRM 51-40-21.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 18,584 hrs · 11,725 cycles

INSPECTION TYPE:12YR, AFT CARGO COMPARTMENT FWP BULKHEAD UPPER PANEL SUPPORT BRAKET FR54 AT LBL36 CRACKED. REMOVED AND REPLACED NEW SUPPORT BRAKET IAW SRM 51-40-21.

Part: SUPPORT BRACKET — CRACKED (FRAME 54) · airframe 18,584 hrs · 11,725 cycles

AFT CARGO BAY FWD BULKHEAD UPPER PANEL SUPPORT BRAKET FRAME 54, BL 0 WAS CRACKED. REMOVED AND REPLACED THE SUPPORT BRAKET IAW SRM 51-40-21.

Part: SUPPORT BRACKET — CRACKED (FRAME 54) · airframe 18,584 hrs · 11,725 cycles

AFT CARGO BAY FWD BULKHEAD UPPER PANEL SUPPORT BRACKET AT FRAME 54, LBL 40. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-40-21.

Part: SUPPORT BRACKET — CRACKED (FRAME 54) · airframe 18,584 hrs · 11,725 cycles

AFT CARGO BAY FWD BULKHEAR UPPER PANEL SUPPORT BRACKET AT FRAME 54, RBL 40 WAS CRACKED. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-40-21.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 18,584 hrs · 11,725 cycles

INSPECTION TYPE:12YR, AFT CARGO COMPARTMENT FWD BULKHEAD UPPER PANEL SUPPORT BRACKET FR54 AT RBL 36 CRACKED. REMOVED AND REPLACED CRACKED BRACKET IAW SRM 51-40-21.

Part: DOOR — UNKNOWN (ARMING MECH) · airframe 18,510 hrs · 11,689 cycles

CREW ENTRY DOOR WILL NOT DISARM. PERFORMED A FWD EMERGENCY ESCAPE SLIDE RELEASE MECHANISM TEST IAW AMM 52-10-30-0501. OPS CHECKED NORMAL

Part: INDICATOR — INOPERATIVE (AIRSPEED) · airframe 17,681 hrs · 11,205 cycles

INSPECTION TYPE:N/AON CLIMBOUT, F/O'S PRIMARY AIRSPEED INDICATOR SHOWED 30 KTS LESS THAN CPTS PRIMARY AND BOTH STANDBY'S. ECAM CAUTION=NAV ADC IAS DISCREPANCY, IAS/STDBY IAS X CHECK, AP/FD USE VALID SIDE, ADC INST SWITCH AS REQ'DT/S PER TSM 34-10-00-BLOCK 301 FIG 110 AND 112 REMOVED AND REPLACED ADC 2 (1FL2) PER AMM 34-11-34-0401. OPS CK NORMAL EFF SOURCE REF: IPC 34-11-08-02-130A

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 17,662 hrs · 11,195 cycles

INSPECTION TYPE:N/ALAVATORY FWD UPPER LIGHT ASSY HAS BROKEN LENS COVER. RELAMPED AND REPLACED LENS REF MM 33-51-00.

Part: SKIN — DAMAGED (FRAMES 79-80) · airframe 16,966 hrs · 10,755 cycles

DAMAGE TO PLATING ON SKIN AT FRAME 79 -80 AT STRINGER S43R. REPAIRED IAW EO A300-5330-64273A.

Part: STRINGER — DAMAGED (FRAMES 79-80) · airframe 16,966 hrs · 10,755 cycles

STRINGER 43R DAMAGED BETWEEN FRAMES 79-80. REPAIRED IAW EO A300-5310-64274A.

Part: WEB — CRACKED (NR 2 NACELLE) · airframe 15,649 hrs · 9,914 cycles

INSPECTION TYPE:5YR, NR 2 ENGINE INLET INBD WEB 15 CRACKED. R & R WEB IAW SRM 54-10-00.

Part: CEILING PANEL — DAMAGED (FWD CARGO BAY) · airframe 15,649 hrs · 9,914 cycles

INSPECTION TYPE: 5YR,FWD PIT PANEL 132LC CEILING PANEL DAMAGED. REPAIRED THE PANEL IAW EO A300-2550-29554-C.

Part: STIFFENER — CRACKED (AFT CARGO BAY) · airframe 15,649 hrs · 9,914 cycles

INSPECTION TYPE:5YR, AREA FORWARD IF AFT CARGO COMPARTMENT. LT SIDE VERTICAL STIFFNER, CRACKED FR 54-LBL 77. R & R SUPPORT BRACKET IAW DWG A53410765 AND SRM 51-40-21.

Part: FITTING — CRACKED (FRAME 46) · airframe 15,649 hrs · 9,914 cycles

INSPECTION TYPE: 1C2C, AIR CONDITIONING COMPARTMENT, LEFT FRAME FITTING CRACKED, FRAME 46, STR 36L. REPAIR IAW EO A300-5310-46789-C.

Part: STIFFENER — CRACKED (FRAME 54) · airframe 15,649 hrs · 9,914 cycles

INSPECTION TYPE:5YR, AREA FORWARD OF AFT CARGO COMPARTMENT, RT SIDE VERTICAL STIFFENER CRACKED FRAME 54, RBL 77. R & R IAW SRM 51-40-21 AND DWG A53410765.

Part: FLOOR PANEL — DAMAGED (FWD CARGO BAY) · airframe 15,649 hrs · 9,914 cycles

INSPECTION TYPE:1C2C, FWD CARGO FLOOR PANEL 132PG HAS EDGE DAMAGE. REPAIRED THE FLOOR PANEL IAW SREO A300-5320-42721-F.

Part: FLOOR PANEL — DAMAGED (FWD CARGO BAY) · airframe 15,649 hrs · 9,914 cycles

INSPECTION TYPE:1C2C, FWD PIT FLOOR PANEL 132MG HAS EDGE DAMAGE. REPAIRED FLOOR PANEL 132MG IAW SREO A300-5320-42721-F.

Part: FLOOR PANEL — DAMAGED (FWD CARGO BAY) · airframe 15,649 hrs · 9,914 cycles

INSPECTION TYPE:1C2C, FWD CARGO FLOOR PANEL 132AH HAS EDGE DAMAGE. REPAIRED THE FLOOR PANEL IAW SREO A300-5320-42721-F.

Part: FLOOR PANEL — DAMAGED (FWD CARGO BAY) · airframe 15,649 hrs · 9,914 cycles

INSPECTION TYPE: 1C2C, FWD CARGO BAY FLOOR PANEL132QG HAS EDGE DAMAGE. REPAIRED THE FLOOR PANEL 132QG IAW SREO A300-5320-42721-F.

Part: CROSSBEAM — CRACKED (FRAME 79) · airframe 15,649 hrs · 9,914 cycles

INSPECTION TYPE:1C2C, MAIN CABIN FLOOR CROSSBEAM LT AT FR 79, Y1580 IS CRACKED. REPAIRED IAW EO A300-5310-59934-B.

Part: FLOOR PANEL — DAMAGED (E & E BAY) · airframe 15,649 hrs · 9,914 cycles

INSPECTION TYPE: 5YR, ELECTRONIC EQUIPMENT COMPARTMENT FLOOR PANEL HAS 2 INSERTS. PULLED OUT AND EDGE DAMAGE REPAIRED PANEL IAW SRM 51-77-10, 51-77-11.

Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 15,649 hrs · 9,914 cycles

INSPECTION TYPE: 1C2C, MAIN CABIN FLOOR CROSSBEAM RT AT FRAME 79-Y1580 IS CRACKED. REPAIRED IAW EO A300-5310-59934-B.

Part: LINER — CRACKED (AFT CARGO DOOR) · airframe 15,649 hrs · 9,913 cycles

INSPECTION TYPE: 5YR, AFT PIT DOOR LINER CRACKED 3 PLACES. REPAIRED LINER IAW EO A300-2550-43367-B.

Part: CEILING PANEL — GOUGED (AFT CARGO) · airframe 15,649 hrs · 9,913 cycles

INSPECTION TYPE:5YR, PARTS RACK, AFT PIT CEILING PANEL 151RC IS GOUGES. REPAIRED PANEL IAW AMM 25-00-00-0801.

Part: GAUGE — UNSERVICEABLE (SLIDE PRESSURE)

UNABLE TO SEE SLIDE PRESSURE GAUGE. DEFERRED IAW MEL 52-11-01-4. PLACARD INSTALLED. VISUALLY INSPECTED MAIN CREW ENTRY DOOR ESCAPE SLIDE PRESSURE. PRESSURE GAUGE VISIBLE. PRESSURE IN GREEN BAND. CHECKED GOOD IAW MM 25-61-20, PARA 1.C. THIS CLEARS ITEM M543400.

Part: FLOOR PANEL — DAMAGED (FRAME 29)

MAIN CARGO DECK FLOOR PANEL 3R, FRAME 29, HAS TWO HOLES 1 X .5 AND 1.25 X .25. FABRICATED A NEW FLOOR PANEL IAW EO 5320-40552-B.

Part: CONNECTOR — DIRTY (DOOR SLIDE)

CREW ENTRY DOOR SLIDE ARMED WARNING LIGHT INOPERATIVE. BUZZER OK. CLEANED AND SECURED CONNECTIONS. OPS CHECKED NORMAL IAW AMM 57-3-11-0401.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 13,254 hrs · 8,298 cycles

1C INSPECTION, LARGE DENT ON LOWER SURFACE OF RT MID FLAP BETWEEN RIB 17A AND RIB 18 AND REAR SPAR AND T/E. REPAIRED RT MID FLAP LOWER SURFACE BETWEEN RIB 17A AND RIB 18 AND REAR SPAR AND T/E REF STASA EA 300-5753-01-A4869, REV IR AND EO A300-575 0-51968-A.

Part: SWITCH — DIRTY (L1 DOOR)

L1 DOOR ARMED ALARM KEEPS SOUNDING (DOOR DISARMED). CLEANED PUSH TO TEST SWITCH. NO DEFECTS NOTED IAW 25 61 20 00.

Part: SWITCH — INTERMITTENT (EMERGENCY LIGHTS)

EMERGENCY LIGHT SWITCH INTERMITTENT. REPLACED 22WL IAW ESPM 20-45-21. TESTED OK IAW MM 33-51-00-05.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

INTERIOR EMERGENCY LIGHT TEST FAILS. REPLACED POWER SUPPLY UNIT AND TESTED GOOD IAW MM 33-51-14-04.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

INTERIOR EMERGENCY LIGHT FAILS OPS TEST. R & R EMERGENCY LIGHT POWER SUPPLY UNIT IAW AMM 33-51-14-04. OPS CHECKED NORMAL.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 242GF IS CRACKED. ACCOMPLISHED REPAIR ON FLOORBOARD NR 242GF IAW EO A300-5320-42721-A, PARA 6A.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 252VJ DAMAGED. FABRICATED MAIN CABIN FLOORBOARD 252VJ IAW EO A300-5320-40552-A, APPENDIX B.

Part: FLOOR PANEL — DAMAGED (FWD CARGO BAY) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, FWD CARGO COMPT FLOOR PANEL 132AH HAS DAMAGED LOWER SKIN. REPAIRED FWD CARGO COMPT FLOOR PANEL 132AH IAW EO A300-5320-16407-E.

Part: FLOOR PANEL — CRACKED · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, COURIER COMPT FLOOR PANEL 222NG IS CRACKED. REPAIRED FLOOR PANEL 222NG IAW EO A300-5320-42721-A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 232TG IS DAMAGED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 232TG IAW EO A300-5320-42721-A PARA 6A.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 231RG IS DAMAGED. FABRICATED MAIN CABIN FLOORBOARD NR 231RG IAW EO A300-5320-40552-A, APPENDIX B.

Part: CLEVIS — CORRODED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN CLEVIS ADAPTER AT FR 25 BL 0 CORRODED. R & R CLEVIS ADAPTER IAW SRM 51-40-21.

Part: CLEVIS — CORRODED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN CLEVIS ADAPTER CORRODED AT FR 23 BL 0 INBD SIDE. R & R CLEVIS ADAPTER IAW SRM 51-40-21, PARA 6 AND 7.

Part: FLOOR PANEL — PUNCTURED (MAIN DECK) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MDCC FLOOR PANEL 231KJ IS PUNCTURED AND HAS AREAS OF FLUID INTRUSION. FABRICATED NEW FLOOR PANEL 231KJ IAW EO A300-5320-10552-A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 242KF IS CRACKED AT LOWER SURFACE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 242KF IAW EO A300-5320-42721-A, PARA 6A.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 232XG IS DELAMINATED. FABRICATED MAIN CABIN FLOORBOARD NR 232XG IAW EO A300-5320-40552-A, APPENDIX B.

Part: FLOOR PANEL — BROKEN (FWD CARGO BAY) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, FWD CARGO COMPT FLOOR PANEL 132PG IS BROKEN. FABRICATED NEW FWD CARGO COMPT FLOOR PANEL 132PG IAW EO A300-5320-16407-E.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 231XG IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 231XG IAW EO A300-5320-42721-A PARA. 6A.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 251UJ IS PUNCTURED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 251UJ IAW EO A3005320-42721-A PARA 6A.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 241VM IS BROKEN/ PUNCTURED. FABRICATED MAIN CABIN FLOORBOARD NR 241VM IAW EO A300-5320-40552-A, APPENDIX B.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK AT -Y1959 BETWEEN FR 30 AND FR 31 IS CORRODED. ACCOMPLISHED REPAIR IAW SRM 53-10-16, FIG 201.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 252MG IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 252MG IAW EO A300-5320-42721-A PARA 6A.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK IS CORRODED AT STA -Y1137 BETWEEN FR 79 AND FR 80. ACCOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR MAIN CABIN FLOORBOARD NR 242VM IS DELAMINATED AT EDGE ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 242VM EO A300-5320-42721-A, PARA 6A.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 242BN IS PUNCTURED AT LOWER SURFACE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 242BN IAW EO A300-5320-42721-A PARA 6A.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK IS CORRODED AT Y0 BETWEEN FR 79 AND FR 80. ACCOMPLISHEED REPAIR IAW SRM 53-10-16, FIG 201.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 242BQ IS CRACKED AT EDGE. FABRICATED MAIN CABIN FLOORBOARD NR242BQ IAW EO A300-5320-40552-A, APPENDIX B.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK IS CORRODED AT Y450 BETWEEN FR 79 AND FR 80. ACCOMPLISHED REPAIR IAW SRM 53-10-16, FIG 201.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 241LT LOWER SURFACE IS CRACKED ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 241LT IAW EO A300-5320-42721-A PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 242LT IS CRACKED AT LOWER SURFACE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 242LT IAW EO A300-5320-42721-A PARA. 6A.

Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MDCC FLOOR PANEL 241ZG IS BROKEN. FABRICATED NEW FLOOR PANEL 241ZG IAW EO A300-5320-10552-A.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 241HP IS DELAMINATED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 241HP EO A300-5320-42721-A PARA 6A.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 251DF IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 251DF IAW EO A300-5320-42721-A PARA 6A.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 252AN IS DELAMINATED AT LOWER AFT INBD CORNER. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 252AN IAW EO A300-5320-42721-A PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 242LJ IS CRACKED AT EDGE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 242LJ IAW EO A300-5320-42722-A AND EO A300-5320-42721-A PARA 6A.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 241BF UNDER SURFACE IS PUNCTURED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 241BF IAW EO A300-5320-42721-A, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 252ZG IS CRACKED AT LOWER SURFACE ON INBD FWD SIDE. FABRICATED MAIN CABIN FLOORBOARD NR 252ZG IAW EO A300-5320-40552-A, APPENDIX B.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 261RF IS PUNCTURED ON LOWER SURFACE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 261RF IAW EO A300-5320-42721-A, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CARGO) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, AFT CARGO COMPARTMENT FLOORBOARD NR 151LG IS CRACKED. FABRICATED AFT CARGO COMPARTMENT FLOORBOARD NR 151LG IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 242AQ IS CRACKED AT EDGE. FABRICATED MAIN CABIN FLOORBOARD NR 242AQ IAW EO A300-5320-40552-A, APPENDIX B.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 241ZH IS PUNCTURED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 241ZH IAW EO A300-5320-42722-A PARA 6A.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 241YK UNDERSURFACE IS PUNCTURED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD 241YK IAW EO A300-5320-42721-A, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 252LJ IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 252LJ IAW EO A300-5320-42721-A PARA 6A.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 251GJ IS DAMAGED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 251GJ IAW EO A300-5320-42721-A PARA 6A.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 241KF LOWER SURFACE IS PUNCTURED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 241KF IAW EO A300-5320-42721-A PARA. 6A.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK IS CORRODED AT STA -Y794 FR 79 AND FR 80. ACCOMPLISHED REPAIR IAW SRM 53-10-16 FIG 201

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 251JF IS DAMAGED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 251JF IAW EO A300-5320-42721-A PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR MAIN CABIN FLOORBOARD NR 252WG IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 252WG IAW EO A300-5320-42721-A, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 252XG IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 252XG IAW EO A300-5320-42721-A PARA 6A.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 252TJ HAS DELAMINATION ON LOWER SURFACE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 252TJ IAW EO A300-5320-42721-A PARA 6A.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK IS CORRODED AT Y1137.1 BETWEEN FR 79 FR 80. ACCOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK AT Y1137 BETWEEN FR 79 AND FR 80 IAW SRM 53-10-16, FIG 201.

Part: FLOORBOARD — BROKEN (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 241TN IS BROKEN. FABRICATED MAIN CABIN FLOORBOARD NR 241TN IAW EO A300-5320-40552-A, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 252VF IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR252VF EO A300-5320-42721-A PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 242CN IS CRACKED AT EDGE FABRICATED MAIN CABIN FLOORBOARD NR 242CN IAW EO A300-5320-40552-A, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 242MN IS CRACKED AT EDGE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 242MN IAW EO A300-5320-42721-A, PARA 6A

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 262RF IS CRACKED AT LOWER CENTER AREA. FABRICATED MAIN CABIN FLOORBOARD NR 262RF IAW EO A300-5320-40552-A APPENDIX B PARA, 6A.

Part: FLOORBOARD — BROKEN (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR MAIN CABIN FLOORBOARD NR 252CH IS BROKEN AT AFT INBD CORNER. FABRICATED MAIN CABIN FLOORBOARD NR 252CH IAW EO A300-5320-40522-A, APPENDIX B.

Part: FLOORBOARD — BROKEN (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 251WG IS BROKEN AT CORNER. FABRICATED MAIN CABIN FLOORBOARD NR 251WG IAW EO A300-5320-40552-A, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 262DM IS CRACKED AT LOWER SURFACE. FABRICATED MAIN CABIN FLOORBOARD NR 262DM IAW EO A300-5320-40552-A, APPENDIX B.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK IS CORRODED AT STA -Y450 BETWEEN FR 79 AND FR 80. ACCOMPLISHED REPAIR IAW SRM 53-10-16, FIG 201

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 241YH IS CRACKED AND PUNCTURED ON LOWER SURFACE. FABRICATED MAIN CABIN FLOORBOARD NR 241YH IAW EO APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 242TN IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 242TN IAW OE A300-5320-42721-A PARA. 6A.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 241EF IS DELAMINATED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 241EF IAW EO A300-5320-42721-A, PARA 6A.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK IS CORRODED AT Y794.3 BETWEEN FR 79 AND FR 80. ACCOMPLISHED REPAIR IAW SRM 53-10-16, FIG 201.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR MAIN CABIN FLOORBOARD NR 262RF IS CRACKED AT LOWER CENTER AREA. FABRICATED MAIN CABIN FLOORBOARD NR 262RF IAW EO A300-5320-40552-A, APPENDIX B PARA, 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 252UJ IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 252UJ IAW EO A300-5320-42721-A, PARA 6A.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 241XG IS DELAMINATED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 241XG IAW EO A300-5320-42721-A, PARA 6A.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 251EN IS DAMAGED AT EDGE. FABRICATED MAIN CABIN FLOORBOARD NR 251EN IAW EO A300-5320-40552-A, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 252XJ LOWER FACESHEET IS DAMAGED AND CENTER OF BOARD IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 252XJ IAW EO A300-5320-42721-A PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 242NN LOWER SURFACE IS CRACKED. FABRICATED MAIN CABIN FLOORBOARD NR 242NN IAW EO A300-5320-40552-A, APPENDIX B.

Part: FLOORBOARD — BROKEN (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR251BN FWD CORNER IS BROKEN. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR251BN IAW EO, PARA 6A.

Part: FITTING — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, FRAME 12A RT FITTING IS CRACKED. ACCOMPLISHED REPAIR ON FR 12A RT FITTING IAW EO A300-5310-23539-C, APPENDIX E.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN SUPERNUMARY FLOORBOARD NR 221SF IS PUNCTURED AT LOWER SURFACE. ACCOMPLISHED REPAIR ON MAIN CABIN SUPERNUMARY FLOORBOARD NR 221SF IAW EO A300-5320-42721-A PARA. 6A.

Part: FLOORBOARD — CORRODED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, FWD CREW ENTRANCE DOOR FLOORBOARD NR 221FF IS CORRODED AT LOWER SURFACE FWD INBD CORNER. ACCOMPLISHED REPAIR IAW EO A300-5320-44957-A.

Part: FLOORBOARD — BROKEN (FWD CARGO) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, FWD CARGO FLOORBOARD NR 132MG HAS THE HONEYCOMB BROKEN OUT ON THE SIDE. FABRICATED FWD CARGO FLOORBOARD NR 132MG IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOORBOARD — BROKEN (FWD CARGO) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, FWD CARGO FLOORBOARD NR 132QG HAS A CORNER BROKE OUT OF THE HONEYCOMB. FABRICATED FWD CARGO FLOORBOARD NR 132QG IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOORBOARD — BROKEN (FWD CARGO) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, FWD CARGO FLOORBOARD NR 132FE THE HONEYCOMB IS BROKEN OUT ON THE SIDE AND CRACKED IN THE MIDDLE. FABRICATED FWD CARGO FLOORBOARD NR 132FE IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 252ZF IS CRACKED AND DELAMINATED AT LT EDGE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR252ZF IAW EO A300-5320-42721-A PARA 6A.

Part: FLOOR PANEL — CRACKED (MAIN DECK) · airframe 11,296 hrs · 7,019 cycles

INSPECTION TYPE:10YR, MDCC FLOOR PANEL 231LG IS CRACKED. FABRICATED NEW FLOOR PANEL 231LG IAW EO A300-5320-40552-A.

Part: PROCESSING UNIT — INOPERATIVE (MLG)

ATB, LANDING GEAR WILL NOT RETRACT. R & R PROX DETECTOR PROCESSING UNIT IN REF TO AMM 32-31-71-04. PERFORMED GEAR RETRACTION TEST SYS 1/ SYS 2. CKS GOOD IN REF TO AMM 32-31-00-05. THIS CLEARS M456798.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 10,774 hrs · 6,691 cycles

INSPECTION TYPE:10YR, LT OTBD FLAP LWR SKIN HAS EXTERNAL DENT WITH FILLER BUT NO EXTERNAL DOUBLER INSTALLED AT RIB 3A AND RIB 4 TRAILING EDGED. ACCOMPLISHED REPAIR ON LT OTBD FLAP T/E LWR SKIN AT RIB 3A AND RIB 4 IAW EO A300-5750-25611-F, APPENDIX A.

Part: SKIN — DENTED (FUSELAGE) · airframe 10,774 hrs · 6,691 cycles

INSPECTION TYPE:4C, EXTERIOR FUSELAGE SKIN DENTED BETWEEN FR66-FR67 AND STR 50R-55R. REPAIRED EXTERIOR FUSELAGE SKIN BETWEEN FR66-FR67 AND STR 50R-55R IAW STA-SA EA 300-5330-01-A3022 AND EO A300-5330-42250-A.

Part: SKIN — GOUGED (FUSELAGE) · airframe 10,774 hrs · 6,691 cycles

INSPECTION TYPE:4C, FUSELAGE EXTERIOR SKIN EXISTING REPAIR DOUBLER IS GOUGED AT FR85 BETWEEN STR 42L AND STR 43R. REPAIRED FUSELAGE EXTERIOR SKIN AT FR85 BETWEEN STR 42L AND STR 43R IAW STA-SA EA 300-5330-01-A3021 AND EO A300-5330-42248-A.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 10,774 hrs · 6,691 cycles

INSPECTION TYPE:4C, RT WING INBD FLAP UPPER SURFACE HAS EXISTING REPAIR DOUBLER WITH GOUGES BETWEEN STGR 2.1- 2.2 AND RIB 15-17. REPAIRED RT WING INBD FLAP UPPER SURFACE BETWEEN STGR 2.1 - 2.2 AND RIB 15 - 17 IAW STA-SA EA 300-5330-01-A3017 AND EO A300-5750-42264-A.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 10,774 hrs · 6,691 cycles

INSPECTION TYPE:10YR, REPAIR VALIDATION SURVEY, REPAIR OF MAIN CARGO FLOORBOARD NR 252DN HAS A PUNCTURE. FABRICATED MAIN CABIN FLOORBOARD NR 252DN IAW EO A300-5320-16407-E, APPENDIX B.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 10,774 hrs · 6,691 cycles

INSPECTION TYPE:4C, REPAIR RECORD VALIDATION SURVEY. REPAIR OF AFT BULK CARGO FLOOR PANEL 161GF. FABRICATED NEW BULK CARGO FLOOR PANEL 161GF IAW EO A300-5320-16407-E APPENDIX A/D.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 10,774 hrs · 6,691 cycles

INSPECTION TYPE:4C, REPAIR RECORD VALIDATION SURVEY. REPAIR OF BULK CARGO FLOOR PANEL 161HF. FABRICATED NEW BULK CARGO FLOOR PANEL 161HF IAW EO A300-5320-16407-E.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 10,774 hrs · 6,691 cycles

INSPECTION TYPE:4C, DAMAGED MAIN CARGO FLOOR PANEL 232WG. FABRICATED NEW MAIN CARGO FLOOR PANEL 232WG IAW EO A300-5320-16407-E.

Part: SLAT SYSTEM — INOPERATIVE (NR 1 & 2)

SLATS SYS 1&2 FAULT/SLATS STUCK, TRIED CYCLING THE FLAPS 3 TIMES, LANDING WITH FLAPS ONLY. EMERGENCY DECLARED RESET FLAP/SLAT CONT'L UNITS. OPER FLAP/SLATS WITH REF TO MM 27-81- 00-05, RAN SLAT/FLAP SYS 6 TIMES WITH NO DEFECTS. ACFT OK FOR CONT'D SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

F/O'S GLARESHIELD EMERGENCY LIGHTS INOP. RELAMPED. OPS CHECK FWD IAW TC 0050 PS CHECK STEP 16.

Part: SLIDE — INOPERATIVE (CREW DOOR)

CREW ENTRY DOOR SLIDE INOP. SLIDE PRESSURE INDICATOR IN RED ZONE. DEFERRED 413258. REMOVED AND REPLACED CREW ESCAPE SLIDE W/REF TO MM 25-61-2-04. THIS CLEARS M413258. PLACARD REMOVED.

Part: HOOK AND LOOP — DEFECTIVE (ESCAPE ROPE)

INSPECTION TYPE:N/A F/O'S ESCAPE ROPE COVER FALLING OFF. REPLACED VELCRO. OPS CHECK GOOD AMM 25-61-13-04.

Part: SLIDE — DISENGAGED (GIRT BAR)

INSPECTION TYPE:N/A FWD ENTRY DOOR SLIDE DIFFICULT TO DISARM. FOUND FWD SLIDER FROM GIRT BAR DISENGAGED FROM LINKAGE GUIDES. PROPERLY ENGAGED SLIDERS WITH LINKAGE GUIDES PER AMM 25-61-21-04. EMERGENCY DISARM HANDLE OPERATES NORMALLY WITH NO DEFECTS NOTED.

Part: INDICATOR — UNSERVICEABLE (ESCAPE SLIDE)

PRESSURE GAUGE ON ESCAPE SLIDE IS UNREADABLE. DEFERRED CABIN DOOR SLIDE PER MEL 52-11-01-03. PERFORMED DMP 52-11-01-03. CHECKED LEDGE ABILITY OF DOOR SLIDE PRESSURE GAUGE. OK FOR SERVICE AS PER MM 25-61-20-06.

Part: BOTTLE — LOW (ESCAPE SLIDE)

ON PREFLIGHT, FOUND MAIN CABIN DOOR EMERGENCY SLIDE PRESSURE LOW. NEEDLE IS WITHIN THE TEMPERATURE COMPENSATED GREEN SCALE. NO PROBLEM NOTED.

Part: FLOORBOARD — CRACKED (MAIN CARGO BAY) · airframe 7,921 hrs · 4,930 cycles

INSPECTION TYPE:1/3C MAIN CARGO DECK FLOORBOARD 241TN CRACKED. REPAIRED MAIN CARGO DECK FLOORBOARD 241TN REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOORBOARD — DAMAGED (MAIN CARGO BAY) · airframe 7,921 hrs · 4,930 cycles

INSPECTION TYPE:1C3C MAIN CARGO DECK FLOORBOARD 241XK HAS FIELD REPAIR. REPAIRED MAIN CARGO DECK FLOORBOARD 241XK REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOORBOARD — DAMAGED (MAIN CARGO BAY) · airframe 7,921 hrs · 4,930 cycles

INSPECTION TYPE:1C3C MAIN CARGO DECK FLOORBOARD 251BN HAS FIELD REPAIR. REPAIRED MAIN CARGO FLOORBOARD 251BN REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOORBOARD — DAMAGED (MAIN CARGO BAY) · airframe 7,921 hrs · 4,930 cycles

INSPECTION TYPE:1/3C MAIN CARGO DECK FLOORBOARD 242DQ AFT HALF HAS FIELD REPAIR. REPAIRED MAIN CARGO DECK FLOORBOARD 242DQ REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOORBOARD — DAMAGED (MAIN CARGO BAY) · airframe 7,921 hrs · 4,930 cycles

INSPECTION TYPE:1C3C MAIN CARGO DECK FLOORBOARD 242CQ FWD HALF HAS FIELD REPAIR. REPAIRED MAIN DECK FLOORBOARD 242CQ REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOORBOARD — DAMAGED (MAIN CARGO BAY) · airframe 7,921 hrs · 4,930 cycles

INSPECTION TYPE:1C3C MAIN CARGO DECK FLOORBOARD 252NM HAS FIELD REPAIR. REPAIRED MAIN CARGO DECK FLOORBOARD 252NM REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOORBOARD — DAMAGED (MAIN CARGO BAY) · airframe 7,921 hrs · 4,930 cycles

INSPECTION TYPE:1C3C MAIN CARGO DECK FLOORBOARD 242LJ HAS A FIELD REPAIR. REPAIRED MAIN CARGO FLOORBOARD 242LJ REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOORBOARD — DAMAGED (MAIN CARGO BAY) · airframe 7,921 hrs · 4,930 cycles

INSPECTION TYPE:1C3C MAIN CARGO DECK FLOORBOARD 241DQ HAS FIELD REPAIR. REPAIRED MAIN CARGO DECK FLOORBOARD 241DQ REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOORBOARD — DAMAGED (MAIN CARGO BAY) · airframe 7,921 hrs · 4,930 cycles

INSPECTION TYPE:1C3C MAIN CARGO DECK FLOORBOARD 241EF HAS FIELD REPAIR. REPAIRED MAIN CARGO FLOORBOARD 241EF REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: SKIN — CHAFED (TE FLAP) · airframe 7,921 hrs · 4,930 cycles

INSPECTION TYPE:1C3C LT WING CENTER FLAP UPPER MID SECTION REPAIR DOUBLER CHAFED. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER ON LT WING CENTER FLAP UPPER MID SECTION REF A300-600 SRM 57-50-00 FIG 205 AND SRM 57-50-00.

Part: GIRT BAR — DETACHED (FUSELAGE)

EMERGENCY SLIDE GIRT BAR BECAME DETACHED AT FORWARD POINT. DEFERRED SLIDE PER MM 52-11-01-3. SECURED GIRT BAR UNDER DOOR WITH SAFETY WIRE. FORWARD SLIDER IN PFM BOX. REINSTALLED DOOR SLIDE REF MM 25-61-21. OPS CHECKS GOOD. THIS CLEARS D363555.

Part: HANDLE — MALFUNCTIONED (CO-PILOT WINDOW)

ON TAXI OUT, CO-PILOTS WINDOW SAFE INDICATION POPPED UP TO UNSAFE. THE RED UNSAFE INDICATOR WILL NOT STOW. RESEATED OUTSIDE EMERGENCY ESCAPE SLIDE HANDLE WINDOW. CKS GOOD.

Part: HANDLE — STICKING (PAX DOOR)

WHEN DISARMING MAIN ENTRANCE DOOR ITS HANDLE HANGS UP STARTING AT THE GREEN DISARM BAND. REPEAT WRITE UP. CLEANED AND LUBED FLOOR FITTING FOR GIRT BAR. PERFORMED FUNCTIONAL TEST FWD ENTRY DOOR SLIDE MECHANISM AS PER MM 52-10-30-05. CKS GOOD.

Part: LEVER — STICKING (PAX DOOR)

CREW ENTRY DOOR ARMING LEVER CATCHES APPROX 2" FROM THE DISARMED POSITION WHEN MOVING LEVER FROM ARMED TO DISARMED. C/W FUNCTIONAL TEST NOTED TO OPERATE NORMAL IN REF TO AMM 52-10-30. OK FOR SERVICE.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS)

SUPERNUMERARY EMERGENCY LIGHTS "TEST" FUNCTION INOP. EMERG LIGHTS OPERATE NORMALLY. REMOVED AND REPLACED POWER SUPPLY UNIT AS PER M/M 33-51-14. OPS CHECK GOOD.

Part: VALVE — FAILED (APU)

APU AUTO SHUTDOWN IN FLIGHT. REMOVED AND REPLACED APU GEARBOX SHUTTLE VALVE AND PRESS SHUTOFF VALVE IAW MM 49-26-14-4 AND 49-26-13-4. RAN APU NO SMELL OF OIL IN PACKS. CHECKED APU OIL LEVEL. NO SERVICING REQUIRED. PLACARD REMOVED. APU OPS CKD GOOD. SHUTTLE VLV P/N 3616848-2, S/N 0341 ON.

Part: LIGHT — NO TEST (FWD ENTRY DOOR)

EMERGENCY EXIT LIGHTS WON'T TEST PROPERLY. RELAMPED WITH SERVICEABLE LAMPS 2 IN FWD ENTRY DOOR EMERGENCY EXIT MODULE LIGHT ASSY. OPS CHECKS NORMAL PER A-300-600 AMM 33-51-13-4.

Part: BULKHEAD — CRACKED (NR 2 NACELLE)

NR 2 ENG LT INLET COWL AFT BULKHEAD WEB CRACKED AT STATIC LPORT LINE UNION TO EEC. REPAIRED BULKHEAD WEB AS PER EO A300-7110-20525.

Part: CONTROL SYSTEM — INOPERATIVE (LE SLATS)

ALL SLATS WILL NOT EXTEND ON APPROACH. LUBRICATED L/E SLATS AS REQUIRED PER A300 MM 12-22-27-0 SLATS SEEM TO OPERATE WITH LESS NOISE AND RESISTANCE.

Part: SKIN PANEL — CRACKED (RT WING TE)

RT WING T/E OUTER SHROUD BOX INNER SKIN PANEL CRACKED. R & R PANEL ASSY IAW EO A300-5720-21353. DMI CLOSED.