N291FE

ATA 5321

Part: FLOOR PANEL — GOUGED (ZONE 100) · airframe 2,577 hrs · 1,301 cycles

DURING HMV1 LFC LSY4 LST MAINT FOUND THE MAIN CARGO COMP. AT STA 470 & LBL 77.5 FLOOR PANEL 231EFF HAS PUNCTURE ON SURFACE SKIN REPAIRED FLOORBOARD AT MAIN CARGO COMPARTMENT AT STA 470 & LBL 77.5 FLOOR PANEL 231EFF P/N (143T5875-6) IN REF. TO SRM 53-00-50-SR FIG. 201 REPAIR 1 SHEET 1. THIS IS A MAJOR REPAIR. (THIS IS A CORRECTED SDR FOR 24-1475)

ATA 5321

Part: FLOORBOARD — GOUGED (ZONE 200) · airframe 2,577 hrs · 1,301 cycles

DURING HMV1 LFC LSY4 LST MAINT FOUND THE MAIN CARGO COMPÏ¿½T FLOORBOARD STA (APPROX) 1390 LEFT SIDE (LBL 77.5) MOST OUTBOARD HAS SEVERAL PUNCTURES 26. CORRECTIVE ACTION 0000491350 : FLORES, LUIS R - 10-OCT-2024 02:18 REPAIRED FLOORBOARD MAIN CARGO COMPARTMENT AT STA 1390 LEFT SIDE PANEL 251VFF P/N (146T5869-28) IN REF. TO SRM 53-00-50-SR FIG. 201 SHEET 1. THIS IS CLASSIFIED AS MAJOR REPAIR. (NOTE: THIS IS A CORECTION FOR SDR 24-1474)

ATA 5754

Part: WEDGE — DENTED (NR 2 SLAT) · airframe 2,576 hrs · 1,300 cycles

MX DISCOVERED DENT DAMAGE TO NR 2 SLAT TE WEDGE. DISCOVERED THAT DAMAGE IS OUT OF LIMITS IAW SRM 57-43-02-1A ALL DENTS MUCH LESS THAN 0.120" IN DEPTH. A FEW DENTS SLIGHTLY LESS THAN 1" FROM EDGE, REQ A REPAIR. ALL DENTS FOUND SMOOTH, FREE OF SHARP CREASES, GOUGES, OR CRACKS & NO DEBONDS OR DELAM. SOME DENTS WERE FOUND TO BE ACCEPTABLE AS-IS. DENTS NUMBERED 231, 232, 241, 243, 384, & 425, 426 WILL REQ REPIR IAW SRM 51-70-10, REP 2 OR REP 4. EA H-5750-T0380783 REV A WHICH PROVIDES INSTRUCTIONS TO FILL ALL DENTS THAT ARE DEEPER THAN 0.003 INCH WITH A A/Y < 30 IAW SRM 51-70-01. REPAIRS ACCOMPLISHED IAW SRM.

ATA 5754

Part: SKIN — DENTED (NR 3 SLAT) · airframe 2,576 hrs · 1,300 cycles

NUMBER #3 SLAT HAS NUMEROUS NUMBER OF SMALL HAIL DAMAGE TO UPPER SURFACE #3 SLAT DISCREPANCY ADDRESSED ON WO 89208 SEQ. 11, EA H-5750-T0380693P1. TITLE: WING - FLIGHT SURFACES - NUMBER 3 SLAT TRAILING EDGE WEDGE DENTS DUE TO HAIL STORM. MAJOR REPAIR

ATA 5754

Part: SKIN — DENTED (NR 1 SLAT) · airframe 2,576 hrs · 1,300 cycles

NUMBER #1 SLAT HAS NUMEROUS NUMBER OF SMALL HAIL DAMAGE TO UPPER SURFACE. #1 SLAT DISCREPANCY ADDRESSED ON WO 89208 SEQ. 13, EA H-5750-T0380689P1. TITLE: WING - FLIGHT SURFACES - NUMBER 1 SLAT TRAILING EDGE WEDGE DENTS DUE TO HAIL STORM. MAJOR REPAIR

ATA 5754

Part: SKIN — DENTED (NR 2 SLAT) · airframe 2,576 hrs · 1,300 cycles

NUMBER #2 SLAT HAS NUMEROUS NUMBER OF SMALL HAIL DAMAGE TO UPPER SURFACE NR 4 #2 SLAT DISCREPANCY ADDRESSED ON WO 89208 SEQ. 19, EA H-5750-T0380783P1. TITLE: WING - FLIGHT SURFACES - NUMBER 2 SLAT TRAILING EDGE WEDGE DENTS DUE TO HAIL STORM. MAJOR REPAIR

ATA 5754

Part: WEDGE — DENTED (NR 6 SLAT TE) · airframe 2,576 hrs · 1,300 cycles

DURING CURRENT HMV VISIT IN IND ON N291FE, MX DIS DENT DMG TO THE SUBJECT # 6 SLAT TRAILING EDGE WEDGE. THIS TYPE OF DAMAGE IS MOST LIKELY CAUSED BY HAIL WHILE IN SVC .MX MAPPED ALL THE DENTS ON THE WEDGE AND DIS THAT THE DMG IS OUTSIDE OF THE DMG LIMITS PER B767-300F SRM 57-43-02-1A DUE TO DISTANCES BETWEEN THE DENTS AT SEVERAL LOCATIONS. NOTE 'K' REQ MIN DISTANCE OF 1.75 MULTIPLIED BY THE DIAMETER OF THE LARGEST DENT. ALL DENTS HAVE A/Y VALUES OVER 10 AND ALL DENTS ARE MUCH LESS THAN 0.120" IN DEPTH. THERE WERE A FEW DENTS SLIGHTLY LESS THAN 1 INCH FROM THE EDGE. ALL DENTS WERE FOUND SMOOTH, FREE FROM SHARP CREASES, GOUGES, OR CRACKS AND NO DISBONDS OR DELAM. DENT #113 WAS A LARGER DENT AND REQUIRES AN EXTERNAL DBLR REPAIR. THE DATA WAS SENT TO BOEING FOR ANALYSIS. ALL OTHER DENTS WERE FOUND TO BE STRUCTURALLY ACCEPTABLE AS-IS WITHOUT REINFORCED REP. BOEING MESSAGES FED-FED-24-0715-06B CONTAINS THE MAPPING AND STATEMENTS FROM BOEING STATING THAT THE DENTS ARE STRUCTURALLY ACCEPTABLE STRUCTURALLY ACCEPTABLE AS A PERMANENT REPAIR PER 767-300F SRM 51-00-06. DENTS DEEPER THAN 0.003 INCH WITH A A/Y < 30 WILL BE FILLED PER 767-300F SRM 51-70-01. DENT #113 REQ A METAL BOND REPAIR WHICH IS REINFORCING REPAIR TO PRIMARY STRUCTURE AND CONSIDERED MAJOR PER GMM 6-2-100. ISSUED EA H-5750-T0380784

ATA 5754

Part: SKIN — DENTED (NR 11 SLAT) · airframe 2,576 hrs · 1,300 cycles

NUMBER #11 SLAT HAS NUMEROUS NUMBER OF SMALL HAIL DAMAGE TO UPPER SURFACE. #11 SLAT DISCREPANCY ADDRESSED ON WO 89208 SEQ. 14, EA H-5750-T0380787P1. TITLE: WING - FLIGHT SURFACES - NUMBER 11 SLAT TRAILING EDGE WEDGE DENTS DUE TO HAIL STORM. MAJOR REPAIR

ATA 5754

Part: SKIN — DENTED (NR 6 SLAT) · airframe 2,576 hrs · 1,300 cycles

NUMBER #6 SLAT HAS NUMEROUS NUMBER OF SMALL HAIL DAMAGE TO UPPER SURFACE. #6 SLAT DISCREPANCY ADDRESSED ON WO 89208 SEQ. 16, EA H-5750-T0380784P1. TITLE: WING - FLIGHT SURFACES - NUMBER 6 SLAT TRAILING EDGE WEDGE DENTS DUE TO HAIL STORM. MAJOR REPAIR

ATA 5754

Part: WEDGE — DENTED (NR 11 SLAT) · airframe 2,576 hrs · 1,300 cycles

DURING CURRENT HMV VISIT IN IND ON N291FE, MAINTENANCE DISCOVERED DENT DAMAGE TO THE SUBJECT NUMBER 11 SLAT TRAILING EDGE WEDGE. THIS TYPE OF DAMAGE IS MOST LIKELY CAUSED BY HAIL WHILE IN SERVICE. MAINTENANCE MAPPED ALL THE DENTS ON THE WEDGE AND DISCOVERED THAT THE DAMAGE IS OUTSIDE OF THE ALLOWABLE DAMAGE LIMITS PER B767-300F SRM 57-43-02-1A DUE TO DISTANCES BETWEEN THE DENTS AT SEVERAL LOCATIONS. S PER B767-300F SRM 57-43-02-1A DUE TO DISTANCES BETWEEN THE DENTS AT SEVERAL LOCATIONS. NOTE 'K' REQUIRED MINIMUM DISTANCE OF 1.75 MULTIPLIED BY THE DIAMETER OF THE LARGEST DENT. ALL DENTS HAVE A/Y VALUES OVER 10 AND ALL DENTS ARE MUCH LESS THAN 0.12-INCH IN DEPTH. THERE WERE A FEW DENTS SLIGHTLY LESS THAN 1-INCH FROM THE EDGE. ALL DENTS WERE FOUND SMOOTH, FREE FROM SHARP CREASES, GOUGES, OR CRACKS AND NO DISBONDS OR DELAMINATION. ENG CREATED EA H-5750-T03800787 FROM THE FOLLOWING: THE DATA WAS SENT TO BOEING FOR ANALYSIS. DENT LOCATION #105 WILL BE PERMANENTLY REPAIRED PER SRM 57-43- 02-2R, REPAIR 1 AND SRM 51-70-10. 10 DENTS WILL BE FILLED PER SRM 51-70-01 REQUIREMENTS. REST OF THE DENTS WERE FOUND TO BE STRUCTURALLY ACCEPTABLE AS-IS WITHOUT REINFORCED REPAIRS. THIS EA ALSO PROVIDES INSTRUCTIONS TO FILL ALL DENTS THAT ARE DEEPER THAN 0.003 INCH WITH A A/Y < 30 PER 767-300F SRM 51-70-01. (CAT A)

ATA 5754

Part: WEDGE — DENTED (NR 1 SLAT) · airframe 2,576 hrs · 1,300 cycles

DURING CURRENT HMV VISIT IN IND ON N291FE, MAINTENANCE DISCOVERED DENT DAMAGE TO THE SUBJECT NUMBER 1 SLAT TRAILING EDGE WEDGE. THIS TYPE OF DAMAGE IS MOST LIKELY CAUSED BY HAIL WHILE IN SERVICE. MAINTENANCE MAPPED ALL THE DENTS ON THE WEDGE AND DISCOVERED THAT THE DAMAGE IS OUTSIDE OF THE ALLOWABLE DAMAGE LIMITS PER B767-300F SRM 57-43-02-1A DUE TO DISTANCES BETWEEN THE DENTS AT SEVERAL LOCATIONS.S PER B767-300F SRM 57-43-02-1A DUE TO DISTANCES BETWEEN THE DENTS AT SEVERAL LOCATIONS. NOTE 'K' REQUIRED MINIMUM DISTANCE OF 1.75 MULTIPLIED BY THE DIAMETER OF THE LARGEST DENT. ALL DENTS HAVE A/Y VALUES OVER 10 AND ALL DENTS ARE MUCH LESS THAN 0.12-INCH IN DEPTH. THERE WERE A FEW DENTS SLIGHTLY LESS THAN 1-INCH FROM THE EDGE. ALL DENTS WERE FOUND SMOOTH, FREE FROM SHARP CREASES, GOUGES, OR CRACKS AND NO DISBONDS OR DELAMINATION. ENG CREATED EA H-5750-T03800689 FROM THE FOLLOWING DATA SENT TO BOEING FOR ANALYSIS. DENT LOCATION #608 WILL BE PERMANENTLY REPAIRED PER SRM 57-43-02-2R, REPAIR 1 & SRM 51-70-10. 10 DENTS WILL BE FILLED IAW SRM 51-70-01 REQUIREMENTS. REST OF THE DENTS WERE FOUND TO BE STRUCTURALLY ACCEPTABLE AS-IS WITHOUT REINFORCED REPAIRS. THIS EA ALSO PROVIDES INSTRUCTIONS TO FILL ALL DENTS THAT ARE DEEPER THAN 0.003 INCH WITH A A/Y < 30 PER SRM 51-70-01.

ATA 5754

Part: WEDGE — DENTED (NR 3 SLAT) · airframe 2,576 hrs · 1,300 cycles

DURING CURRENT HMV VISIT IN IND ON N291FE, MAINTENANCE DISCOVERED DENT DAMAGE TO THE SUBJECT NUMBER 3 SLAT TRAILING EDGE WEDGE. THIS TYPE OF DAMAGE IS MOST LIKELY CAUSED BY HAIL WHILE IN SERVICE. MAINTENANCE MAPPED ALL THE DENTS ON THE WEDGE AND DISCOVERED THAT THE DAMAGE IS OUTSIDE OF THE ALLOWABLE DAMAGE LIMITS PER B767-300F SRM 57-43-02-1A DUE TO DISTANCES BETWEEN THE DENTS AT SEVERAL LOCATIONS.S PER B767-300F SRM 57-43-02-1A DUE TO DISTANCES BETWEEN THE DENTS AT SEVERAL LOCATIONS. NOTE 'K' REQUIRED MINIMUM DISTANCE OF 1.75 MULTIPLIED BY THE DIAMETER OF THE LARGEST DENT. ALL DENTS HAVE A/Y VALUES OVER 10 AND ALL DENTS ARE MUCH LESS THAN 0.12-INCH IN DEPTH. THERE WERE A FEW DENTS SLIGHTLY LESS THAN 1-INCH FROM THE EDGE. ALL DENTS WERE FOUND SMOOTH, FREE FROM SHARP CREASES, GOUGES, OR CRACKS AND NO DISBONDS OR DELAMINATION. ENG CREATED EA H-5750-T03800693 REV B FROM THE FOLLOWING: THE DATA WAS SENT TO BOEING FOR ANALYSIS. DENT LOCATION #608 WILL BE PERMANENTLY REPAIRED PER SRM 57-43- 02-2R, REPAIR 1 AND SRM 51-70-10. 10 DENTS WILL BE FILLED PER SRM 51-70-01 REQUIREMENTS. REST OF THE DENTS WERE FOUND TO BE STRUCTURALLY ACCEPTABLE AS-IS WITHOUT REINFORCED REPAIRS. THIS EA ALSO PROVIDES INSTRUCTIONS TO FILL ALL DENTS THAT ARE DEEPER THAN 0.003 INCH WITH A A/Y < 30 PER 767-300F SRM 51-70-01.

ATA 5542

Part: SKIN — DAMAGED (RUDDER) · airframe 2,576 hrs · 1,300 cycles

RUDDER, LH SIDE APPROXIMATELY 56" FROM TRAILING EDGE AND 75" FROM THE BOTTOM, SKIN HAS DAMAGE. MARKED WITH RED GREASE PEN AND YELLOW STICKER. REPAIRED, TREATED, AND PAINTED RUDDER SKIN DAMAGE AT L/H SIDE APPROXIMATELY 56" FROM TRAILING EDGE AND 75" FROM THE BOTTOM OF RUDDER, REPAIR MATERIAL PLYS AND PAINT REMOVED IS THE SAME WEIGHT AS MATERIAL PLYS AND PAINT READDED TO REPAIR, NO WEIGHT ADDED TO RUDDER, NO WEIGHT AND BALANCE NEEDED. IN REF. TO B767 SRM 55-40-01- 2R FIG.201 SHEET 2., SRM 51-10-06-0G, SRM 51-60-03-0G, AMM 51-21-00-07. SEE JPF FOR OTHER WORK ACCOMPLISHED. THIS IS A MAJOR REPAIR.