N188FE

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 6,156 hrs · 3,039 cycles

MAIN DECK CARGO, SECT.43, B.S 636, NEXT TO MDC DOOR REAR FRAME,(231O) DELAMINATED FLOOR PANEL. MAIN DECK CARGO, SECT. 43, BS 636, NEXT TO MDC DOOR REAR FRAME FLOOR PANEL 231EFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 89 APR 15/2024

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 5,768 hrs · 2,833 cycles

L/H WING INBD FLAP LEADING EDGE OTBD POSITION CAP PANEL #555DB IS DELAMINATED, MPN 113T2201-413G. REPAIRED, INSTALLED, AND SEALED L/H WING INBD FLAP LEADING EDGE OTBD POSITION CAP PANEL #555DB IS DELAMINATED, MPN 113T2201-413G. IAW E.A. # H-5750-T0378910 A. REF B767 SRM 57-53-01-2R TABLE 1 REPAIR1, SRM 51-70-17-0G DETAIL II, AMM 51-21-00-7, SRM 51-40-02-0G, SRM 51-20-05-0G. MAJOR REPAIR

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 5,768 hrs · 2,833 cycles

L/H WING INBOARD FLAP ASSY - THE FORE FLAP LEADING EDGE OUTBOARD POSITION CAP PANEL # 555DB IS DELAMINATED, MPN 113T2201-413G. REPAIRED L/H WING INBOARD FLAP ASSY, FORE FLAP LEADING EDGE OUTBOARD POSITION CAP PANEL # 555DB, MPN 113T2201-413G. IAW E.A. # H-5750-T0378910, REF B767 SRM 57-53-01-2R TABLE 1 REPAIR 1, SRM 51-70-17-0G DETAIL II, AMM 51-21-00-7.

Part: BRAKE — FAILED (MLG) · airframe 4,958 hrs · 2,440 cycles

UPON GEAR RETRACTION ON TAKEOFF IN IND WE GOT A BRAKE TEMP LIGHT ON CLIMB OUT. THE #6 BRAKE CONTINUED TO CLIMB AND PEAKED AT 7. WE RAN QRH PROCEDURES AND EXTENDED THE GEAR TO COOL THE BRAKE. UPON LANDING IN PHX THE #6 BRAKE INDICATOR WAS THE FIRST ONE TO SHOW ANY RIDE IN TEMP. IT WAS AT A 3 ALMOST IMMEDIATELY AFTER TURNING OFF THE RUNWAY. BY THE TIME WE WERE IN THE CHOCKS AFTER A SHORT TAXI THE INDICATOR SHOWED 7. ALL OTHER INDICATORS APPEARED NORMAL. REMOVED #6 MAIN WHEEL ASSY.REF M/M B767 32-45-01-4. FOUND #6 BRAKE ASSY. LOCKED UP. UPON FREEING #6 BRAKE IT IS STILL EXTREMELY DIFFICULT TO ROTATE INSTALLED NEW BRAKE ASSY. PER 767 M.M. 32-41-08-4-4. OPS AND LEAK CHECK NORMAL. DUE TO #6 BRAKE DRAGGING ALSO REMOVED AND REPLACED #6 TIRE AND WHEEL ASSY. PER 767 M.M. 32-45-01-4. A/C OK FOR SERVICE

Part: NONE — NONE (N/A) · airframe 2,553 hrs · 1,242 cycles

LH WING LE AT STA OSS441 FORMER CRACKED P/N 114T2170-5 C/W WITH EA H-5720-T0368062P1

Part: ROD — DIRTY (NLG) · airframe 68,537 hrs · 50,295 cycles

DURING TEST FLIGHT WITH GEAR HANDLE UP NOSE GEAR RED LIGHT AND RED DOORS LIGHT STAYED ON. *S/D* CLEANED DIRT FROM AND LUBRICATED NLG DOOR SWITCH ACTUATOR RODS. JACKED NOSE AND SWUNG GEAR. NLG FUNCTIONALLY TESTED GOOD. SERVICED NLG STRUT. WORK DONE PER MM 32-61-000-15, 07-11-000-2, 12-15-025-2.

Part: ACCESSORY UNIT — FAILED (MLG) · airframe 68,537 hrs · 50,295 cycles

DURING TEST FLIGHT, HAD NO LEFT MAIN GEAR INDICATION. PERFORMED GOOD RING OUT PER FED EX WDM 32-64-02, 32-64-01. REPLACED LANDING GEAR ACCESSORY UNIT AND PERFORMED GOOD FUNCTIONAL TEST PER FED EX MM 20-10-017-2, 32-09-111-5.

Part: SKIN — DAMAGED (BS 480) · airframe 68,537 hrs · 50,294 cycles

REWORK REQUIRED, FROM NR01182. ACCOMPLISH REPAIR PER FEDEX ENGINEERING, BS 480, STR 26L-27L. *S/D* COMPLIED WITH FED EX EA 7-5330-95353, FOUND TO BE A MAJOR REPAIR.

Part: REPAIR — IMPROPER (FUSELAGE) · airframe 68,537 hrs · 50,294 cycles

REPAIR AT BS 694, STR 19R REQUIRES ENGINEERING DISPOSITION IAW EO 7-5100-7- 5000 PT1. ACCOMPLISHED REPAIR AT BS 694 STR 19R PER FED EX E.A. 7-5330-91416.

Part: RIB — MISLOCATED (ELEVATOR HINGE) · airframe 68,537 hrs · 50,294 cycles

WHILE WORKING CARD N01365, FOUND RT NR 5 ELEVATOR HINGE RIB MISLOCATED. REMOVED AND REPLACED RT NR 5 ELEVATOR HINGE RIB PER EA 7-5510-91413.

Part: FITTING — CORRODED (TRUNNION) · airframe 68,537 hrs · 50,294 cycles

LEFT MLG FWD TRUNNION SUPPORT FITTING O/B FLANGE, O/B SURFACE HAS SURFACE CORROSION BETWEEN -THROUGH PIN- AND LWR PORK CHOP FITTING BOLT HOLE LOCATIONS. REPAIRED L/H MLG FWD TRUNNION SUPPORT FITTING PER FED EX EA 7-5710-91408.

Part: RIB — DAMAGED (HORIZONTAL STAB) · airframe 68,537 hrs · 50,294 cycles

DURING INSPECTION OF THE LT HORIZ STAB ELEVATOR RIB AT ELEV STA 136.5, FOUND TO HAVE EXISTING REPAIRS ON THE LOWER IB AND OB FLANGES OF THE RIB AT THE TRAILING EDGE BEAM. RIB REQUIRES REPLACEMENT PER FEDEX EO 7-5510-7-5001 PT 1. REPAIRED PER S.B. 727-55A0091

Part: REPAIR — UNKNOWN (BS 480) · airframe 68,537 hrs · 50,294 cycles

REPAIR AT BS 480 STR 26L TO 27L REQUIRES ENGINEERING DISPOSITION PER EO 7- 5100-7-5000 P3. COMPLIED WITH FED-EX EA 7-5330-95353. FOUND TO BE MAJOR REPAIR

Part: FRAME — DAMAGED (BS 520) · airframe 68,537 hrs · 50,294 cycles

FUSELAGE, MAIN FRAME FORWARD CARGO DOOR FORWARD FRAME REPLACEMENT AD'S 90-06-09 AND 98-11-03 R1 (LOG BOOK ENTRY REQUIRED). REPAIRED PER E.A. 7-5310-93709

Part: STRINGER — UNKNOWN (BS 384-396) · airframe 68,537 hrs · 50,294 cycles

STR 25R REQUIRES ENGINEERING DISPOSITION PER EO 7-5100-7-5000 PT1. COMPLIED WITH E.A. 7-5330-91409

Part: FAILSAFE — CRACKED (BS 990) · airframe 68,537 hrs · 50,294 cycles

N01348 BS 990 FRAME IS CRACKED TWO PLACES AT STRINGER 25 LT. REPAIRED PER SRM 51-40-3

Part: SUPPORT — CORRODED (BS 1107) · airframe 68,537 hrs · 50,294 cycles

CORROSION AFT CARGO BAY CEILING SUPPORT BS 1107 RBL 6 WL 200. REPAIRED PER SRM 53-10-1

Part: SKIN — CRACKED (BS 1352) · airframe 68,537 hrs · 50,294 cycles

BS 1352 RT SKIN CRACK AT RAIN GUTTER LOCATION. REPAIRED PER SRM 54-30-2

Part: SKIN — DAMAGED (BS 1081) · airframe 68,537 hrs · 50,294 cycles

FOUND MATERIAL LOSS EXCEEDS 10 PERCENT BS 1081 STR 10R. REPAIRED PER E.O. 7-5330-7-2313 PT 5

Part: SKIN — DAMAGED (BS 361) · airframe 68,537 hrs · 50,294 cycles

FOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 361 STR 19. REPAIRED PER E.O. 7-5330-7-2319 PT 5

Part: SKIN — DAMAGED (BS 261) · airframe 68,537 hrs · 50,294 cycles

FOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 261 STR 14R. REPAIRED PER E.O. 7-5330-7-2319 PT 5

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 68,537 hrs · 50,294 cycles

FOUND FORWARD CARGO DOOR HAS MULTIPLE SCRATCHES ON EXTERIOR SKIN IN THE UNPAINTED AREA. REPAIRED PER E.A. 7-5230-91411.

Part: FAILSAFE — CRACKED (BS 1010) · airframe 68,537 hrs · 50,294 cycles

BS 1010 FRAME IS CRACKED AT STRINGER 25 LEFT. REPAIRED PER SRM 51-40-3

Part: SKIN — DAMAGED (BS 361) · airframe 68,537 hrs · 50,294 cycles

FOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 361 STR 10L. REPAIRED PER E.O. 7-5330-7-2319 PT 5

Part: SKIN — DAMAGED (BS 1081) · airframe 68,537 hrs · 50,294 cycles

FOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 1081 STR 10L. REPAIRED PER E.O. 7-5330-7-2313F PT 5

Part: FLOORBEAM — CORRODED (BS 1130) · airframe 68,537 hrs · 50,294 cycles

FOUND CORROSION (C53-224-01) ON MAIN CARGO DECK FLOORBEAM UPPER AND LOWER FLANGE AT BS 1130 BETWEEN RBL 25 AND RBL 45, WL 208. REPAIRED MAIN DECK FLOORBEAM UPPER FLANGE AT BS 1130, RBL 45, WL 208 REF SRM 53-10- 8 FIG 10.

Part: FAILSAFE — CRACKED (BS 990) · airframe 68,537 hrs · 50,294 cycles

BS 990 FRAME IS CRACKED AT STRINGER 25 RIGHT. REPAIRED PER SRM 51-40-3

Part: SHEAR TIE — CORRODED (BS 990) · airframe 68,537 hrs · 50,294 cycles

CORROSION ON SHEAR TIE BS 990 LBL 3 WL 148. REPAIRED PER SRM 53-10-2

Part: SKIN — DAMAGED (BS 361) · airframe 68,537 hrs · 50,294 cycles

FOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 361 STR 10R. REPAIRED PER E.O. 7-5330-7-2319 PT 5

Part: FRAME — DAMAGED (BS 890) · airframe 68,537 hrs · 50,294 cycles

UPPER LOBE INTERIOR FRAME HAS MACH DAMAGE AND OPEN HOLES BS 890 STR 9L. [OPEN]

Part: FLOORBEAM — CORRODED (BS 480) · airframe 68,537 hrs · 50,294 cycles

BS 480 FLOORBEAM UPPER CHORD CORRODED AT RBL 48, WL 208. [OPEN]

Part: INTERCOSTAL — CRACKED (BS 660) · airframe 68,537 hrs · 50,294 cycles

N01148 CRACK BS 660 STR 2L UPPER INTERCOSTAL EXTENSION. [OPEN]

Part: SKIN — CRACKED (BS 591) · airframe 68,537 hrs · 50,294 cycles

CRACK IN FUSELAGE OUTER SKIN STA 591 STR 15R FWD UPPER CORNER OF WING L/E ILLUMINATION LIGHT CUT OUT. REPAIRED PER FED EX EA 7-5330-95384.

Part: FRAME — DAMAGED (BS 990) · airframe 68,537 hrs · 50,294 cycles

N00737 FRAME BS 990 BTWN STR 22 LT- 24 LT DAMAGED. [OPEN]

Part: FRAME — DENTED (BS 1030) · airframe 68,537 hrs · 50,294 cycles

AFT CARGO BAY FRAME BS 1030 BETWEEN STR 26 LT AND 27 LT DENTED. FABRICATED DOUBLER CAP AT BS 1030 BTWN STR 26 AND 27 L/H USING 7075T6 .071 M590750 PER SRM 51-40-3. INSTALLED DOUBLER CAP AT BS 1030 BETWEEN STR 26 AND STR 27 LT PER SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 1130) · airframe 68,537 hrs · 50,294 cycles

AFT CARGO COMP SHEAR TIE IS CORRODED BS 1130 RBL 8 WL 152. REPAIRED PER SRM 53-10-4.

Part: FLOORBEAM — CRACKED (BS 295) · airframe 68,537 hrs · 50,294 cycles

N00474 E&E BAY FLOORBEAM WEB BS 295 LBL 30 WL 200 CRACK EXTENDING UP FROM STOP DRILL. STOP DRILLED CRACK AND REPAIRED WEB AT CRACK IN E&E BAY FLOORBEAM WEB BS 295 LBL 30 WL 200 IAW SRM 51-10-1 AND SRM 51-40-2

Part: SKIN — CRACKED (BS 235-245) · airframe 68,537 hrs · 50,294 cycles

FOUND EXTERNAL SKIN CRACKED AT F/O'S NR 5 WINDOW CUT OUT AT UPPER AFT FASTENER HOLE. INSTALLED REPAIR DOUBLER F/O'S NR 5 WINDOW CUT OUT UPPER AFT CORNER IAW SRM 53-30-3.

Part: SHEAR WEB — CRACKED (BS 805-825) · airframe 68,537 hrs · 50,294 cycles

WHILE WORKING CARD N00368 FOUND SHEAR WEB 8-5-825, RBL 65-70, WL 208 TO BE CRACKED. SHEAR WEB BS 805-825 RBL 65-70 W/L 208 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED IAW SRM 51-30-2. SRM 51-30-5, SRM 51-10-2.

Part: SKIN — DENTED (BS 465) · airframe 68,537 hrs · 50,294 cycles

FOUND BS 465 STR 19L HAS A DENT. REPAIRED STR 19L AT BS 465 PER SRM 51-30-2 AND 53-10-3.

Part: SKIN — GOUGED (BS 368) · airframe 68,537 hrs · 50,294 cycles

FOUND GOUGE IN SKIN AT STR 20L BS 368. REPAIRED GOUGE IN SKIN AT STR 20L BS 368 PER SRM 53-30-3 FIG 3.

Part: STRINGER CLIP — GOUGED (BS 380) · airframe 68,537 hrs · 50,294 cycles

FOUND MAIN CARGO COMPARTMENT STRINGER CLIP GOUGED BS 380 STR 6R. REMOVED AND REPLACED MAIN CARGO COMPARTMENT STRINGER CLIP BS 380, STR 6R IAW SRM 51-30-2.

Part: SHEAR TIE — DAMAGED (BS 620) · airframe 68,537 hrs · 50,294 cycles

FOUND BS 620 STR 25 LT DAMAGE AROUND FASTENER ON SHEAR TIE THROUGH SKIN. REMOVED AND REPLACED SHEAR TIE AT BS 620 STR 25 LH IAW SRM 51-10-2, 51-20, AND SRM 51-30-2.

Part: STRINGER — CRACKED (BS 480) · airframe 68,537 hrs · 50,294 cycles

FOUND UPPER LOBE INTERIOR STRINGER IS CRACKED BS 480 STR 16R. REMOVED AND REPLACED WITH NEW STR. SECTION IAW SRM 53-30-2 AND SRM 53-10-4.

Part: STRINGER CLIP — DAMAGED (BS 440) · airframe 68,537 hrs · 50,294 cycles

FOUND MAIN CARGO DECK STRINGER CLIP IS DAMAGED AT BS 440, STR 8L. REMOVED AND REPLACED MAIN CARGO DECK STRINGER CLIP BS 440 STR 8L IAW SRM 51-30-2.

Part: STRINGER — DAMAGED (BS 782) · airframe 68,537 hrs · 50,294 cycles

UPPER LOBE INTERIOR SIDE OF STRINGER IS DAMAGED BS 782 STR 4L. REPAIRED STRINGER AT B.S. 782 STR 4L PER SRM 53-10-1.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 68,537 hrs · 50,294 cycles

CORROSION BS 328 FLOORBEAM AT FASTENER HOLES. CORROSION ON FLOORBEAM AT B.S. 328 LBL 22 WAS OUT OF LIMITS REPAIRED FLOORBEAM PER FED EX EA 7-5310-91401.

Part: WEB — GOUGED (BS 640) · airframe 68,537 hrs · 50,294 cycles

HAYES MOD WEB GOUGED AT BS 640L AT STR 12L AND 14L.

Part: FLOOR PANEL — CORRODED (BS 1150) · airframe 68,537 hrs · 50,294 cycles

CORROSION ON MAIN CARGO DECK FLOOR PANEL WEB AT BS 1150, RBL 60, WL 208. CUT OUT DAMAGE FLOOR WEB AT BS 1150, RBL 60, WL 208 AND INSTALLED REPAIR DOUBLER PER SRM 51-40-2.

Part: WEB — GOUGED (BS 620) · airframe 68,537 hrs · 50,294 cycles

HAYES MOD WEB GOUGED AT 9 PLACES BETWEEN STR 5L AND STR 13L BS 620. REPAIRED GOUGES STR 5L AND 13L, BS 620 HAYES MOD WEB PER SRM 53-10-2, 51-40-2, 51-30- 2.

Part: WEB — CRACKED (BS 344) · airframe 68,537 hrs · 50,294 cycles

WHILE WORKING N01046 FOUND WEB AT BS 344 LBL 32 CRACKED. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-02 ON WEB AT BS 344 LBL 32.

Part: FLOORBEAM — CORRODED (BS 344) · airframe 68,537 hrs · 50,294 cycles

CORROSION BS 344 FLOORBEAM LBL 55 TO RBL 10. REPAIRED BS 344 FLOORBEAM LBL 55 TO RBL 10 PER FED-EX DWG SR 27-53-007.

Part: FLOORBEAM — CORRODED (BS 360) · airframe 68,537 hrs · 50,294 cycles

CORROSION BS 360 FLOORBEAM BL 0. REJECTED BECAUSE CORROSION AND BARE METAL STILL PRESENT ON BOTTOM SIDE OF UPPER CHORD AND BL 0. REPAIRED PER SRM 53-10-8.

Part: STRINGER CLIP — GOUGED (BS 380) · airframe 68,537 hrs · 50,294 cycles

MAIN CARGO COMPARTMENT STRINGER CLIP GOUGED BS 380 STR 5R. REMOVED AND REPLACED MAIN CARGO COMPARTMENT CLIP BS 380 STR 5R IAW SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 1110) · airframe 68,537 hrs · 50,294 cycles

AFT CARGO COMP SHEAR TIE IS CORRODED BS 1110 RBL 8 WL 150.

Part: FRAME — CRACKED (BS 826) · airframe 68,537 hrs · 50,294 cycles

STA 826 LBL 47 FRAME WEB SUPPORT CRACKED. REMOVED CRACKED FRAME WEB SUPPORT BS 826, LBL 47, INSTALLED NEW SUPPORT IAW SRM 51-30-2, 51-30-5, AND 51-10-2.

Part: FLOORBEAM — CORRODED (BS 1110) · airframe 68,537 hrs · 50,294 cycles

CORROSION AFT CARGO BAY FLOORBEAM LWR CHORD BS 1110 RBL 4 - 24 WL 200. CUT OUT DAMAGE ON LWR FLANGE OF BS 1110 FLOORBEAM RBL 2-RBL 26. FABRICATED AND INSTALLED REPAIR IAW FEDEX SR DRAWING SR 27-53-034E.

Part: STRINGER — CRACKED (BS 503-509) · airframe 68,537 hrs · 50,294 cycles

UPPER LOCE INTERIOR STRINGER IS CRACKED AT 6 EA FASTENER LOCATIONS BS 503-509 STR 16R. REMOVED AND REPLACED CRACKED STR. IAW SRM 51-30-2 AND SRM 53-10-2.

Part: SPLICE — CRACKED (BS 680) · airframe 68,537 hrs · 50,294 cycles

STR 15L END SPLICE/CLIP IS CRACKED AT AFT FASTENER BS 680. REMOVED DAMAGED CLIP AT STR 5L, BS 680 AND INSTALLED IAW SRM 51-30-2.

Part: FRAME — CRACKED (BS 804) · airframe 68,537 hrs · 50,294 cycles

UPPER LOBE INTERIOR FRAME IS CRACKED BS 804 RBL 68, WL 210.5. REMOVED AND REPLACED FRAME PER SRM 51-30-02.

Part: SHEAR TIE — CORRODED (BS 1030) · airframe 68,537 hrs · 50,294 cycles

CORROSION ON SHEAR TIE BS 1030 RBL 3 WL 148. REMOVED CORROSION ON SHEAR TIE FOUND TO BE OUT OF LIMTIS. INSTALLED NEW SHEAR TIE, ALL WORK DONE IAW SRM 53-10-1, 53-10-4, 51-30-2.

Part: SHEAR TIE — CORRODED (BS 1030) · airframe 68,537 hrs · 50,294 cycles

CORROSION ON SHEAR TIE BS 1030 RBL 10 WL 148. REMOVED CORROSION ON SHEAR TIE FOUND TO BE OUT OF LIMITS. INSTALLED NEW SHEAR TIE, ALL WORK DONE IAW SRM 53-10-1, 53-10-4 & 51-30-2.

Part: SHEAR TIE — CORRODED (BS 1030) · airframe 68,537 hrs · 50,294 cycles

CORROSION ON SHEAR TIE BS 1030 LBL 10.

Part: SHEAR TIE — CORRODED (BS 990) · airframe 68,537 hrs · 50,294 cycles

FOUND CORROSION ON SHEAR TIE BS 990 LBL 10 WL 148. REPAIRED SHEAR TIE AT BS 990, LBL 10 PER SRM 53-10-4.

Part: STRINGER CLIP — DAMAGED (BS 700) · airframe 68,537 hrs · 50,294 cycles

STRINGER CLIP HAS MECHANICAL DAMAGE BS 700 STR 4L. REPLACED STRINGER CLIP AT BS 700, STR 4L PER SRM 51-30-2.

Part: STRINGER CLIP — MISSING (BS 600) · airframe 68,537 hrs · 50,294 cycles

STRINGER CLIP MISSING AT BS 600 STR 4R. INSTALLED STRINGER CLP AT BS 600 STR 4R PER SRM 51-30-2.

Part: FRAME — CORRODED (BS 760) · corrosion level 2 · airframe 68,537 hrs · 50,294 cycles

WHILE WORKING FEDEX WORK CARD 7-5310-7-3367 B4 PT1 FOUND LT 760 FRAME CORRODED LBL 65 WL 205. REMOVED AND REPLACED L/H 760 FRAME IAW SRM 51-30-2, 51-30-5, 51-10-2.

Part: FRAME — CORRODED (BS 460) · airframe 68,537 hrs · 50,294 cycles

E & E BAY CORROSION ON FRAME SPLICE ANGLE AFT SIDE BS 460 STR 26L. REMOVED CORROSION ON FRAME SPLICE FOUND TO BE OUT OF LIMITS. FABRICATED NEW SPLICE ANGLE & INSTALLED ALL WORK DONE IAW SRM 53-10-1, 51-40-04, 51-30-2.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 68,266 hrs · 50,097 cycles

DURING B-CHECK, STIFFENER FITTING BELOW "S" DUCT CRACKED AND FRAMING STRUCTURE FOR "S" DUCT CORRODED, BOTH AT BS 1342 BOTH ON RT SIDE REF EA NR7-5310-87123 FOR FERRY FLT APPROVAL.

Part: WARNING LIGHT — FALSE INDICATION (CARGO DOOR) · airframe 67,819 hrs · 49,734 cycles

MAIN CARGO DOOR LIGHT CAME ON DURING CLIMBOUT PASSING 15,000 FT MSL AT 310 KAUS, CHECKLIST ACCOMPLISHED, RETURNED TO AUS. AFTER AIRCRAFT BLOCK IN, OPENED MAIN CARGO DOOR. FOUND AFT THRESHOLD LOCK DOWN, WITH RED LIGHT ON. LOCKED THRESHOLD LOCK. CHECKED DOOR SWITCHES; CHECKED GOOD. CLOSED MAIN CARGO DOOR, WARNING LIGHT WENT OUT. PRECAUTIONARY PRESSURIZED AIRCRAFT TO 3.5 PSI ON GROUND. WARNING LIGHT DID NOT COME ON. NO LEAKS NOTED ON OUTSIDE OF MCD. MAIN CARGO DOOR WARNING SYSTEM OPS CHECKS NORMAL. AIRCRAFT PRESSURIZED PER 727 JRH CH 7. OKAY FOR SERVICE.

Part: ACCESS PANEL — BENT (CARGO DOOR) · airframe 67,819 hrs · 49,734 cycles

MAIN CARGO DOOR LIGHT CAME ON PASSING 15,000 FT AT 310 KNOTS. REPEAT WRITE-UP, APPROX CABIN PRESSURE 4.5 PSI. CHECKLIST ACCOMPLISHED, RETURNED TO AUS. OPENED MAIN CARGO DOOR, INSPECTED ALL SWITCHES ON MAIN CARGO DOOR, LATCH SWITCHES, LOCK TUBE SWITCHES, FOUND ACCESS PANEL ON LOWER AFT MAIN CARGO DOOR BENT IN AND MAKING CONTACT WITH THE TARGETS ON THE AFT TWO LATCH SWITCHES. STRAIGHTENED ACCESS PANEL AND FOUND BOTH TARGETS ON AFT TWO SWITCHES BENT AND OUT OF ADJUSTMENT. ADJUSTED BOTH TARGETS AND SWITCHES PER 727-100 MM CHAPTER 52-34-009-5. CLOSED CARGO DOOR, DOOR WARNING SYSTEM OPS CHECK'S NORMAL. OK FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (FIRE PROTECTION) · airframe 67,446 hrs · 49,439 cycles

WITH LEFT A/C PACK OPERATING THE LOWER AFT BODY OVERHEAT LIGHT ILLUM AFTER AT LEAST 30 MINS OF PACK OPS. AFTER TURNING OFF LT PACK, THE LIGHT EXTINGUISHED WITHIN 2 MINS. TURNED RT PACK ON, THE LIGHT CAME BACK ON AFTER 5 MINS. CHECKED AFT AIRSTAIR AREA FOR LEAKS, NONE FOUND. NO LEAKS IN WHEEL WELL AREAS. NO LEAKS IN KEEL BEAM AREA. RAN PACKS FOR 1.5 HRS WITH ENGINES RUNNING. NO LEAKS OR PROBLEMS FOUND. NO LEAKS OR OTHER PROBLEMS FOUND IN AFT BELLY AREAS. FIRE LOOPS IN KEEL BEAM AND AFT AIRSTAIRS CHECK OK. A/C OK FOR SERVICE.

Part: SWITCH — FAILED (ZONE 700) · airframe 67,356 hrs · 49,359 cycles

UPON LOWERING GEAR FOR LANDING, GREEN GEAR NOSE LIGHT DID NOT ILLUMINATE (TESTED OK). NO AMBER GEAR LIGHT. CYCLED GEAR AND NOSE GEAR LIGHT ILLUMINATED ON SECOND EXTENSION OF GEAR. REMOVED AND REPLACED NOSE LANDING GEAR LOCK SWITCH PER 727 MM 32-61-021-4. PERFORMED ADJUSTMENT/TEST PER 727 MM 32-61-021-5. OPS CHECKED NORMAL. A/C OK FOR SERVICE.

Part: SWITCH — CORRODED (ZONE 700) · airframe 67,338 hrs · 49,344 cycles

DURING FIRST FLIGHT GEAR EXTENSION GOT NO GREEN NOSE GEAR INDICATOR (NO RED ONE EIGHTER) LIGHTS CHECKED GOOD, LONG AFTER OTHER MAIN GEAR INDICATION ON S/O PANEL, A PRESSURE WAS NORMAL. AFTER RECYCLING GEAR GOT NORMAL GEAR IND. LANDED UNEVENTFULLY. FOUND WATER AND CORROSION ON POSITION SWITCH ELECTRICAL CONNECTOR. REMOVED CORROSION AND WATER, OPS CHECKED IAW B727-100 M/M 32-61-021-5. ALL CHECKS GOOD AT THIS TIME.

Part: COMPRESSOR — STALLED (NR 3 ENGINE) · airframe 67,337 hrs · 49,343 cycles

RIGHT AFTER ROTATION AND LIFT OFF, NR 3 ENGINE HAD 3 LARGE COMPRESSOR STALLS WITH EPR DROP TO 1.2/1.4. RAMP PERSONNEL SAW FLAMES OUT REAR OF ENGINE. SHUT DOWN NR 3 ENGINE IAW QRH AND COMPLIED WITH REMAINING QRH PROCEDURES. UNEVENTFUL LANDING. R&R'D NR 3 ENGINE PER ENGINE CHANGE WORK CARD 70T0501-03 UP TO ITEM 6. J. COMPLETED ENGINE CHANGE WORK CARD 70T0501-03 AND ENGINE RUN WORK CARD 70T0301-03. ALL SYSTEMS OPS CHECK NORMAL.

Part: POSITION SWITCH — FAULTY (NLG) · airframe 67,251 hrs · 49,279 cycles

INFLIGHT, NO NOSE GEAR DOWN INDICATION. (GREEN LIGHTS). REPLACED BOTH BULBS NO EFFECT. CYCLED GEAR, TESTED BULBS, DID NOT WORK, REPLACED BOTH BULBS, AGAIN A VERY WEAK LIGHT, GOOD INDICATION, WENT TO BRIGHT, WORKED. BACK TO DIM AND WAS INTERMITTENT, LANDING NORMAL IN ALL RESPECTS. REMOVED AND REPLACE THE NOSE GEAR POSITION SWITCH IAW MM 32-61-021-4. CLEANED CONNECTOR PLUG. OPS CHECKED NORMAL. AIRCRAFT OK FOR SERVICE.

Part: DUCT — BLOWN (NR 3 STARTER) · airframe 67,211 hrs · 49,237 cycles

AFTER TAKEOFF NR 3 ENGINE HAD FIRE INDICATOR, IAW FLIGHT MANUAL QRM SHUTDOWN ENGINE, FIRELIGHT EXTINGUISHED BY ITSELF AND TESTED GOOD. NO ABNORMAL ENGINE INDICATIONS WERE NOTED. AFTER ENGINE SHUTDOWN WINDMILLED FOR APPROXIMATELY 10 MIN. NR 3 OIL PRESS APPROX 10 PSI (WINDMILLING). OPENED NR 3 ENGINE COWLING. FOUND SUPPLY DUCT (1ST ELBOW) OFF OF STARTER, BLOWN. REMOVED AND REPLACED THE NR 3 ENGINE STARTER SUPPLY DUCT IAW MM, LEAK CHECK OK. INSPECTION NR 3 ENGINE MAIN OIL STRAINER AND CHIP DETECTORS AS REQUIRED FOR ENGINE WINDMILLING CONDITION IAW MM. NO CONTAMINATION FOUND. REMOVED AND REPLACED NR 3 ENGINE MAIN OIL FILTER IAW MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,966 hrs · 48,150 cycles

DURING ROUTINE INSP, THE SHEAR TIE CLIP AT BS 990, STR 4L & 6L FOUND CRACKED. REMOVED AND REPLACED FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.

Part: LIGHT — INOPERATIVE (ESCAPE SLIDE) · airframe 65,966 hrs · 48,150 cycles

DURING ROUTINE INSP, FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE LIGHT FOUND INOP. REMOVED BROKEN WIRE AND REPLACED LIGHT BULB PER IAW FEDEX MM 33-50-21.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,966 hrs · 48,150 cycles

DURING ROUTINE INSP, BS 1130 FLOORBEAM FOUND CORRODED BETWEEN NR 5 & 6 SEAT TRACKS. REPAIRED PER IAW DALFORT AERO, LP XEA X1-53-707 REV 1.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 65,966 hrs · 48,150 cycles

DURING ROUTINE INSP NR 4 SEAT TRACK FOUND CORRODED BETWEEN BS 460 - 480. REMOVED AND REPLACED, FAB PER IAW BAC 727 SRM 53-10-5 & 51-30-2.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,966 hrs · 48,150 cycles

DURING ROUTINE INSP, STR 30 FOUND CORRODED BETWEEN BS 1020 - 1030. CUT OUT DAMAGE AREA, FAB, AND INSTALLED PER IAW BAC 727 SRM 53-10-3.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,966 hrs · 48,150 cycles

DURING ROUTINE INSP, SHEAR TIE CLIP AT BS 1050, STR 6L FOUND CRACKED. REMOVED AND REPLACED, FAB PER IAW BAC 7S7 SRM 51-20-1, 51-30-2.

Part: SKIN — CHAFED (LT TE FLAP) · airframe 65,966 hrs · 48,150 cycles

DURING ROUTINE INSP, LEFT O/B MIDFLAP FOUND CHAFED AT LWR SKIN ACCESS PNL. REMOVED AND REPLACED, FAB PER IAW BAC 727 SRM 57-50-4.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 65,966 hrs · 48,150 cycles

DURING ROUTINE INSP, NR 6 SEAT TRACK FOUND CORRODED BETWEEN BS 813 - 817. REMOVED AND REPLACED, FAB PER IAW BAC 727 SRM 53-10-5 & 51-30-2.

Part: SUPPORT FITTING — CRACKED (LT NR 3 AILERON) · airframe 65,966 hrs · 48,150 cycles

DURING ROUTINE INSP, LEFT O/B AILERON NR 3 ATTACHMENT SUPPORT FOUND CRACKED. REMOVED AND REPLACED PER IAW BAC 727 SRM 51-30-2.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 65,966 hrs · 48,150 cycles

DURING ROUTINE INSP, BS 1130 FLOORBEAM FOUND CORRODED BETWEEN NR 6 & 7. REPAIRED PER IAW DALFORT AERO, LP XEA X1-53-707 REV 1.

Part: FAN — FAILED (COCKKPIT)

LIGHT SMOKE FUMES IN COCKPIT WHICH DISAPPEARED WHEN GASPER FAN WAS TURNED OFF. REMOVED AND REPLACED GASPER FAN.

Part: FRAME — CORRODED (BS 950)

WHILE WORKING NR 0562, FOUND CORROSION ON BS 950 MAIN FRAME AT RBL 30 WL 144. REMOVED CORROSION ON BS 950 MAIN FRAME AT RBL 30 WL 144 AND REPAIRED PER FEDEX EA 7-5310-25935.

Part: KEEL BEAM — CORROSION (BS 1126-1129)

WHILE WORKING NR 0079, DISCOVERED CORROSION ON RT KEEL BEAM BS 1126 TO 1129 STR 29R TO BE OUT OF LIMITS, REQUIRES REPLACEMENT FROM BS 950 TO 1060. REMOVED CORRODED KEEL BEAM AND INSTALLED NEW KEEL BEAM FROM BS 950 TO 1086 STR 29R IAW FEDEX EA 7-5310-25936.

Part: SPAR — CORRODED (BS 920)

CORROSION (C53-132-02-1/2), WING CENTER SECTION BS 920 LOWER SPAR CHORD RBL 34 TO 44. REMOVED CORROSION ON STA 870 LOWER SPAR CHORD. FOUND CHORD IS OUT OF LIMITS PER FEDEX 727 SRM 75-10-1. REMOVED AND REPLACED STA 870 LOWER CHORD PER EWO NR 95-3133 (EA NR 7-5710-25916).

Part: CHORD — CORRODED (BS 950)

WHILE WORKING NR 0562, FOUND CORROSION AT BS 950 CHORD AT STR 26R. REMOVED AND REPLACED LOWER SKIN FORWARD CHORD AT BS 950 STR 26R AS PER DRAWING 65-16336.

Part: SKIN — CORRODED (BS 320-360)

WHILE WORKING NR 0559, FOUND SIDE SKIN CORROSION AT BS 320 TO 360 WL 160, BS 328 TO 332 RBL 17 FROM WL 145 TO 160, BS 280 RBL 17 FROM WL 145 AND CRACKED SHEAR TIE AT BS 325 RBL 17 TO 22. COMPLIED WITH EA 7-5310-25937.

Part: SKIN — CORRODED (BS 950-1183)

CORROSION (71C905-00), BS 950 TO 1183, STR 26L AND 26R ON EXTERIOR SKIN. COMPLIED WITH EA 7-5310-25938 (FEDEX EA), AT BS 950 TO 958, STR 28 TO 30L. REMOVED CORROSION ON REMAINDER OF SKIN FROM BS 950 TO 1183, STR 26 LT AND RT FOUND TO BE WITHIN LIMITS AS PER FEDEX SRM 53-30-1.

Part: SPAR — CORROSION (BS 870 UPPER)

CORROSION (C53-132-02-1/2), DETERIORATED FINISH, WING CENTER SECTION BS 870 UPPER SPAR CHORD, ENTIRE LENGTH. REMOVED CORROSION ON STA 870 UPPER SPAR CHORD, FOUND CHORD TO BE OUT OF LIMITS PER FEDEX 727 SRM (57-10-1). REMOVED AND REPLACED STA 870 UPPER CHORD PER EWO 95-3134 AND EA 7-5710-25916.

Part: STRAP — CORRODED (BS 950)

WHILE WORKING NR 0562, FOUND CORROSION ON STRAP ON BS 950 MAIN FRAME RBL 19 TO 55 WL 144 TO 146. REMOVED AND REPLACED STRAP BS 950 RBL 19 TO 55 WL 144 TO 164 IAW FEDEX ES 7-5310-25935.

Part: STRAP — CRACKED (BS 1110)

WHILE WORKING NR 0562, FOUND REINFORCING STRAP CRACKED BS 1110 RBL 32 WL 132. REPAIRED REINFORCING STRAP AT BS 1110 RBL 32 WL 153 IAW FEDEX SRM 51-40-4.

Part: STRINGER — CRACKED (BS 440-455)

WHILE WORKING NR 0081, DISCOVERED CRACKED STR AT BS 440 PLUS 15 STR 23R. ACCESSED AND REPAIRED STR AT BS 440 PLUS 15 STR 23R PER FEDEX SRM 53-10-3. INSTALLED AND LEAK CHECKED OXYGEN CYLINDERS.

Part: CHORD — CORRODED (BS 312-350)

SEVERAL AREAS OF CORROSION ON UPPER LT NOSE CHORD BS 312 TO 350, LBL 13 WL 169. WILL REQUIRE REMOVAL OF DOGHOUSE FLOOR, STIFFENER BRACKETS AND COOLING DUCT FOR ACCESS. REMOVED AND REPLACED LT NOSE CHORD BS 312 TO 350, LBL 13 WL 169, INSTALLED FASTENERS PER BAC DRAWING NR 65-18415.

Part: KEEL BEAM — CORRODED (BS 1126-1129)

WHILE WORKING NR 0079, DISCOVERED CORROSION ON RT KEEL BEAM BS 1126 TO 1129, STR 29R TO BE OUT OF LIMITS.

Part: STRINGER — CORRODED (BS 385)

CORROSION ON STR 26R STA 385 RT, E-BAY. REMOVED DAMAGED AREA OF STR 26R FROM BS 377 TO 393 AND REPAIRED PER FEDEX SRM 53-10-3. ALODINED AND PRIMED ALL EFFECTED AREAS.

Part: KEEL BEAM — CRACKED (BS 1077-1085)

LT/KEEL BEAM IS CRACKED AND CORRODED FROM BS 1077 TO 1085. REPAIRED LT/KEEL BEAM THAT WAS CRACKED AND CORRODED FROM BS 1077 TO 1085 AS PER ENGINEERING EO 7-5310-7-2356 REV C PART 4. UPON FASTENER INSTALLATION FOUND STR 29L TO HAVE DRILL START OUT OF LIMITS. REMOVED AND REPLACED STR SECTION PER FEDEX SRM 53-10-3.

Part: SHEAR TIE — CORROSION (BS 1070)

WHILE WORKING KEEL BEAM NR0389, FOUND CORROSION ON THE SHEAR TIE AT BS 1070 BETWEEN STR 29 AND STR 28L AFTER REMOVING SEAL FOR ACCESS OF AREA. CORROSION FOUND TO BE OUT OF LIMITS, REMOVED SHEAR TIE, FABRICATED SHEAR TIE, DOUBLER, AND FILLER, ALODINED, PRIMED AND PAINTED AS REQ, SEALED PARTS, REPAIRED SHEAR TIE PER FEDEX SRM 53-10-4.

Part: FRAME — DAMAGED HOLE (BS 990)

HOLE ON BS 990 RT FRAME ON THE I/B SIDE OF STR 27R IS NOT INSPECTABLE DUE TO GEOMETRIC CONFIGURATION, FIG 8 SHAPED. REPAIRED HOLE IN BS 990 RT FRAME ON I/B SIDE OF STR 27R PER FEDEX SRM 51-40-3 FIG 1.

Part: FRAME — DAMAGE HOLE (BS 1010)

HOLE ON BS 1010 RT FRAME ON THE I/B SIDE OF STR 27R IS NOT INSPECTABLE DUE TO GEOMETRIC CONFIGURATION, FIG 8 SHAPED. REPAIRED HOLE IN BS 1010 RT FRAME ON I/B SIDE OF STR 27R PER FEDEX SRM 51-40-3 FIG 1.

Part: FRAME — CRACKED (BS 970)

HOLE ON BS 970, RT FRAME ON THE INBOARD SIDE OF STR 27R IS NOT INSPECTABLE DUE TO GEOMETRIC CONFIGURATION (FIGURED AND SHAPED). CUT OUT DAMAGE ON UPPER FLANGE OF FRAME AT STR 27R, BS 970, RT AREA. CUT OUT WAS .50 INCH BY 1 INCH. FABRICATED REPAIR PART AND INSTALLED AS PER FEDEX SRM 51-40-3.

Part: FLOOR BEAM — CORROSION (BS 600)

CORROSION (72C235-02) AND BARE METAL ON TOP CHORD AND WEB OF THE BS 600 FLOOR BEAM RBL 2-55 AND LBL 2-48, WL 202-208. REMOVED CORROSION AT BS 600, RBL 2-55 AND LBL 2-43, WL 202-208, RBL 11 - 41 WERE FOUND TO BE OUT OF LIMITS. ORIGINAL MATERIAL THICKNESS WAS .125 INCH. MATERIAL REMOVED WAS .040 INCH AT RBL 41 AND 100 PERCENT AT RBL 11. REPAIRED BOTH AREAS PER FEDEX SRM 53-10-8 - ALODINED AND PRIMED ALL BARE METAL.

Part: FRAME — CRACKED (BS 1090)

HFEC INSP EXHIBITS CRACK EMANATING FROM HOLE ON BS 1090 FRAME, O/B SIDE UPPER OF STR 27L. REPAIRED CRACKED FRAME AT BS 1090, O/B SIDE UPPER OF STR 27L PER FEDEX SRM 51-40-3 FIG 1.

Part: FLOOR BEAM — CORROSION (BS 720)

CORROSION (72C235-02), ON TOP CHORD AND WEB OF BS 720 FLOORBEAM, RBL 13 TO 22, 47.5 TO 55, WL 206 TO 208.

Part: FRAME — CRACKED (BS 1050)

WHILE WORKING ON EO 7-5310-7-2354E1, A CRACK WAS FOUND ON FRAME AT TOOLING HOLE LOCATED AT BS 1050, LBL 22.5 ABOVE STR 27L. REPAIRED CRACK FOUND ON FRAME AT TOOLING HOLE LOCATED AT BS 1050, LBL 22.5 ABOVE STR 27L AS PER FEDEX SRM 51-40-3.

Part: SKIN — DENTED (BS 227)

DENT IN SKIN AT NOSE ACCESS DOOR, BS 227 RBL 5. REPAIRED DENT PER FEDEX SRM 53-30-3, AT BS 227 RBL 5 FUSELAGE SKIN.

Part: FLOOR BEAM — CORRODED (BS 328)

CORROSION ON FLOOR BEAM STA 328, WL 208, LBL 18 - 45. REMOVED CORROSION AND TREATED BS 328, WL 208, LBL 45. FOUND CORROSION AT BS 328, WL 208, LBL 18 OUT OF LIMITS. REMOVED DAMAGED AREA AND INSTALLED REPAIR. ALL PER FEDEX SRM 53-10-8, 53-10-1, 53-10-2.

Part: SKIN — GOUGED (NR 6 LE SLAT)

THE NR 6 SLAT L/E HAS SMALL GOUGES APPROX 28 INCHES FROM O/B END. REMOVED DAMAGE, FABRICATED REPAIR AND INSTALLED ON NR 6 SLAT L/E APPROX 28 INCHES FROM O/B END IAW FEDEX SRM 57-50-1, 57-50-3, DWG 65-17302.

Part: SKIN — LIGHTNING STRIKE (BS 360-480)

THERE ARE 24 LIGHTNING STRIKES ON SKIN, BS 360 TO 480 STR 23 TO 26R. REMOVED DAMAGE AND REPAIRED PER FEDEX SRM 53-30-3.

Part: NOSE CHORD — CORROSION (BS 294.5)

CORROSION EMANATING FROM BULGING LEVELING COMPOUND ON LOWER RT NOSE CHORD, BS 294.5 PLUS 17 RBL 17 WL 145. REMOVED AND REPLACED RT NOSE CHORD, BS 284.5 PLUS 17 TO 351 RBL 17 WL 145 IAW BAC DRAWING NR 6515724.

Part: FLOOR SUPPORT — CORRODED (BS 277-295)

CORRODED INTERCOSTAL STA 277 TO 295 RBL 13 WL 208. REMOVED AND REPLACED INTERCOSTAL FLOOR SUPPORT, STA 277 TO 295 RBL 13 WL 208.

Part: FLOOR PANEL — CORROSION (BS 312)

CORROSION AROUND FLOOR PANEL FASTENER HOLE AT STA 312 LBL 45 WL 208. REPAIRED PER FEDEX SRM 53-10-8 FIG 7.

Part: FLOOR BEAM — CORRODED (BS 344)

CORROSION AROUND FLOOR PANEL FASTENER HOLES AT FLOORBEAM STA 344 WL 208 RBL 19 LBL 55. CORROSION FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-02. REMOVED AND REPLACED 344 BEAM UPPER CHORD FROM SKIN TO SKIN PER FEDEX DRAWING NR SR 8753-007.

Part: SKIN — DELAMINATED (LT TE AFT FLAP)

THE L/W I/B AFT FLAP HAS AREA OF DELAMINATION ON LOWER SURFACE, APPROX 70 INCHES FROM I/B END ON FRONT SPAR. REPAIRED L/W I/B AFT FLAP LOWER SURFACE IAW FEDEX SRM 51-40-6.

Part: FLOORBEAM — CORRODED (BS 660)

CORROSION (72C235-02), AROUND FASTENER HOLE ON BS 660 FLOORBEAM RBL 19 WL 208. REMOVED DAMAGE AT BS 660 FLOORBEAM RBL 19 WL 208 AND INSTALLED REPAIR PER FEDEX SRM 53-10-08 FIG 8. REMOVED .046 MATERIAL FROM ORIGINAL .125 THICKNESS FLANGE, FOUND TO BE OUT OF LIMITS PER FEDEX SRM 57-10-01.

Part: SHEAR TIE — CRACKED (BS 312)

FOUND CRACKED SHEAR TIE STA 312L BETWEEN STR 22 TO 23L, DOG HOUSE. REMOVED CRACKED SHEAR TIE AT BS 312 BETWEEN STR 22 TO 23L AND INSTALLED REPLACEMENT SHEAR TIE WET WITH SEALANT.

Part: CLIP — MIS MFG (BS 400)

THERE IS NO RADIUS AT STR CLIP CUTOUT, BS 400 STR 5R. REMOVED AND REPLACED STR CLIP AT BS 400 STR 5R.

Part: FRAME — CRACKED (BS 1070)

HFEC INSP EXHIBITS CRACK EMITTING FROM HOLE ON BS 1070 FRAME ON THE O/B SIDE UPPER OF STR 27L. REPAIRED CRACK IN FRAME AT BS 1070 O/B SIDE OF STR 27L, WORK DONE IAW PER FEDEX SRM 51-40-3.

Part: CLIP — MIS MFG (BS 420)

THERE IS NO RADIUS AT STR CLIP CUTOUT, BS 420 STR 5 TO 6R. REMOVED AND REPLACED STR CLIPS AT BS 420 STR 5 TO 6R.