N244FE

Part: RECEIVER — FAILED (VOR) · airframe 44,301 hrs · 34,873 cycles

VOR'S CHECKED GOOD ON PREFLIGHT. DURING CLIMBOUT BOTH VOR'S SHOWED A 30 DEGREE SPLIT ON VOR STA COULD NOT CTR EITHER CDI ON VOR STATION. TRIED ANOTHER VOR STA, SAME SITUATION. BOTH RMI'S HAD VOR NEEDLES 30 - 40 ' SPLIT. COMPASS SYS MATCHED. HAD TO RELY ON ATC HEADINGS TO RETURN TO FIELD. FOUND NR1 VOR SYS LAGS BEHIND NR2 SYS. R & R NR1 VOR/ILS RCVER IAW 34-31-001-5. CHECKS OK.

Part: FLOORBEAM — CORRODED (BS 312) · airframe 43,596 hrs · 34,294 cycles

MAIN CABIN FLOORBEAM BS 312, LBL 6 IS EXFOLIATED ON AFT LIP OF UPPER CHORD. CUT OUT DAMAGED AREA 2 BY 1 INCH IAW DWG NR SR27-53-017 REV A. FABRICATED 2 REPAIR ANGLES AND REPAIR FILLER IAW DWG NR SR27-53-017 REV A. HEAT TREATED REPAIR ANGLES FROM TO T6 IAW FAS ENGINEERING REPORT NR 2 37153-801 REV A. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND DWG NR: SR27-53-017 REV A.

Part: STRINGER — CORRODED (BS 950E-950F) · airframe 43,596 hrs · 34,294 cycles

ART PIT STR 27L CORRODED IN CHANNEL BETWEEN BS 950E-950F. REMOVED CORROSION IAW SRM 51-10-6. UT INSPECTED AREA FOUND OUT OF LIMITS. CUT OUT DAMAGE AREA IAW SRM 53-10-3 FIG 1. FABRICATED REPAIR PARTS AND 2 SPLICES IAW SRM 53-10-2 FIG 9. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: STRINGER — CORRODED (BS 970-990) · airframe 43,596 hrs · 34,294 cycles

AFT PIT STR 27L CORRODED IN CHANNEL BETWEEN BS 970-990. REMOVED CORROSION IAW SRM 51-10-6. INSPECTED AREA AND FOUND OUT OF LIMITS IAW SRM 53-10-1. FIG 1. CUT OUT DAMAGED AREA IAW SRM 53-10-3, FIG. 1. FABRICATED STRINGER, & SPLICERS IAW SRM 53-10-3 FIG. 1. AND 53-10-2 FIG 9. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 1110) · airframe 43,596 hrs · 34,294 cycles

MAIN CABIN FUSELAGE SEAT TRACK AT BS 1110, LBL 24 IS CORRODED. REMOVED CORRODED SECTION OF SEAT TRACK IAW 51-30-2 FABRICATED NEW SECTION IAW DRAWING 53FX976 REV B. TREATED & PRIMED SECTION IAW SRM 51-10-2 INSTALLED SEAT TRACK SECTION IAW SRM 51-30-2

Part: STRINGER — CORRODED (BS 720B S26L) · corrosion level 2 · airframe 43,596 hrs · 34,294 cycles

FWD PIT CORROSION ON STR 26 L STA 720B. CUT OUT DAMAGE AREA IAW SRM 53-10 3 FIG 1. FABRICATED REPAIR PART AND 2 SPLICES IAW SRM 53-10-2 FIG 1 AND 53-10-2 FIG 9. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: STRINGER — CORRODED (BS 700-720) · corrosion level 2 · airframe 43,596 hrs · 34,294 cycles

FWD PIT - CORROSION ON STR 26 L BETWEEN STA 700 AND 720. CUT OUT DAMAGE AREA IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER AND 1 SPLICE IAW SRM 53-10-2 FIG 9. TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED REPAIR PARTS IAW B727 SRM 51-30-2.

Part: SKIN — CORRODED (RT WING) · airframe 43,596 hrs · 34,294 cycles

RT WING LEADING EDGE HAS BULGING SEALANT AND CORROSION AT WS 510 UPPER SURFACE ABOVE SPAR. FABRICATED REPAIR FILLERS & DOUBLER IAW B727 SRM 57-30-4 FIG 6. TREATED & PRIMED PARTS & AREA IAW SRM 51-10-2. FLAP SHOT PEEN AREA IAW EA 7-5710-127964. INSTALLED REPAIRS, STIFFENERS, CHANNELS, RIBS, SEALS & RETAINERS, IAW SRM 57-30-4 FIG 6, 51-30-2 & EA 7-5710-127964. CLOSED FUEL PANELS & LEAK CHECKED IAW MM 28-11-021-4 & 28-11-000-6.

Part: SKIN — DAMAGED (ZONE 100) · airframe 43,596 hrs · 34,294 cycles

FUSELAGE SKIN AT STA 300 STRINGER 21LT IS GOUGED BLENDED OUT DAMAGED AREA IAW SRM 51-10-1, FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1 FIG 1 AND 2, CUT OUT DAMAGED AREA IAW SRM 51-10-1, FABRICATED REPAIR DOUBLER IAW SRM 53-30-3 FIG 1 AND 53-30-2 FIG 2, TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2, INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 43,596 hrs · 34,294 cycles

RIGHT FOREFLAP, INBOARD WBL 124, CRACK ON SKIN ABOVE CARRIAGE ATTACH FITTING CUT OUT DAMAGED AREA IAW SRM 51-10-1, FABRICATED REPAIR DOUBLER & FILLER IAW SRM 57-50-2 FIG 4 AND 57-50-2 FIG 1, TREATED AND PRIMED IAW SRM 51-10-2 INSTALLED REPAIR IAW SRM 51-30-2

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 43,596 hrs · 34,294 cycles

LEFT HAND FORE FLAP OUTBD WBL 348 CRACK ON SKIN ABOVE CARRIAGE ATTACH FITTING. TRIMMED OUT CRACKED AREA IAW SRM 57-50-4 FIG 1 AND 51-10-1. FABRICATED REPAIR DOUBLER, TREATED, PRIMED, AND INSTALLED DOUBLER AT LEFT HAND FOREFLAP O/B WBL 348 IAW SRM 57-50-4 FIG 1, 51-10-2, AND 51-30-2.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 43,596 hrs · 34,294 cycles

LEFT WING OUTBD T/E FOREFLAP HAS GOUGE EXTERNAL DOUBLER FROM PREVIOUS REPAIR, INBD END. REMOVED DAMAGED REPAIR IAW SRM 51-30-2. FABRICATED NEW DOUBLER IAW SRM 57-50-4 FIG 1. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED NEW DOUBLER AT LT. WING O/B T/E FOREFLAP IAW SRM 57-50-4 FIG 1 AND 51-30-2.

Part: STRUCTURE — CRACKED (LT WING TE FLAP) · airframe 43,596 hrs · 34,294 cycles

LEFT WING INBOARD MID-FLAP LOWER CHORD CRACKED WBL 124. DISPLACED SKIN, REMOVED SEAL, AND SEAL RETAINER FOR ACCESS IAW SRM 51-30-2. CUTOUT DAMAGE AND REPAIRED IAW SRM 51-40-4 FIG 3 AND 57-50-2 FIG 5. TREATED, PRIMED AND INSTALLED REPAIR IAW SRM 51-10-2 AND 51-40-4 FIG 3. REINSTALLED SKIN, SEAL, AND RETAINER IAW SRM 51-30-2.

Part: FLOORBEAM — CRACKED (BS 760) · airframe 43,596 hrs · 34,294 cycles

WING CENTER SECTION OVERWING FLOORBEAM TEE CRACKED BS 760.9 LBL 45. REMOVED CRACKED TEE IAW SRM 51-30-2, FABRICATED NEW ANGLE IAW SRM 53-10-2 FIG 7 AND 51-30-5, TREATED AND PRIMED NEW TEE IAW SRM 51-10-2, INSTALLED NEW TEE IAW SRM 53-10-2 AND 51-30-2

Part: SUPPORT BRACKET — CORRODED (BS 1175-1183) · airframe 43,596 hrs · 34,294 cycles

AFT CARGO COMPARTMENT LBL 17.8 VERTICAL BEAM SUPPORT BRACKET HAS CORROSION AT UPPER SIDE STA 1183. REMOVED VERTICAL BEAM SUPPORT BRACKET IAW SRM 51-30-2. FABRICATED NEW SUPPORT BRACKET(FITTING) IAW DRAWING 65-19608. TREATED AND PRIMED NEW FITTING IAW SRM 51-10-2. INSTALLED NEW AFT CARGO COMPARTMENT LBL 17.8 VERTICAL BEAM SUPPORT BRACKET(FITTING) STA 1183 IAW B727 SRM 51-30-2 AND DRAWING 65-19608.

Part: FLOORBEAM — CRACKED (BS 760) · airframe 43,596 hrs · 34,294 cycles

WING CENTER SECTION OVERWING FLOORBEAM TEE FITTING CRACKED BS 760.9 RBL45. REMOVED TEE FITTING IAW SRM 51-30-2. FABRICATED NEW TEE FITTING IAW SRM 51-30- 5 AND PF SRM 53-10-2 FIG 7A. LOCATED, DRILLED, TREATED, AND PRIMED NEW FITTING IAW SRM 51-30-5 AND 51-10-2. INSTALLED WING CENTER SECTION OVERWING FLOORBEAM TEE FITTING BS 760.9 RBL 45 IAW SRM 51-30-2.

Part: STRINGER — CORRODED (BS 950E S29R) · airframe 43,596 hrs · 34,294 cycles

CORROSION ON STRINGER 29R AT STA 950E AFT PIT. REMOVED CORROSION AND FOUND OUT OF LIMITS, FABRICATED REPAIR STRAP AND INSTALLED IAW DWG SR27-53-023 REV A.

Part: ANGLE — CRACKED (RT WING TE FLAP) · airframe 43,596 hrs · 34,294 cycles

RIGHT WING INBOARD MID-FLAP LOWER TRAILING EDGE ANGLE IS CRACKED AT WBL 90. OPENED LOWER INNER SKIN IAW SRM 51-30-2. REMOVED 3EA LOWER INBD SEAL RETAINERS IAW SRM 51-30-2. REMOVED CRACKED LOWER INBD ANGLE IAW SRM 51- 30-2. FABRICATED NEW ANGLE IAW SRM 57-50-2 FIG 5. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW ANGLE IAW SRM 51-30-2. REINSTALLED RETAINERS IAW SRM 51-30-2. CLOSED LOWER INNER SKIN PANEL IAW SRM 51-30-2.

Part: SKIN — CORRODED (BS 680 S27L) · airframe 43,596 hrs · 34,294 cycles

CORROSION UNDER SEALANT ON FUSELAGE SKIN STA 680 S27L. REMOVED CORROSION AND FOUND OUT OF LIMITS SRM 51-10-6 AND 53-30-1 FIG.1 REMOVED TRANSITION PANELS FOR ACCESS IAW SRM 51-30-2. CUT OUT SKIN SECTION IAW SRM 53-30-3 FIG.12 AND REPAIRED IAW SRM 53-30-3 FIG. 12 AND 53-30-2 FIG. 2. REINSTALLED TRASITION PANELS IN FOWARD PIT IAW SRM 51-30-2.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 43,596 hrs · 34,294 cycles

RIGHT FORE FLAP, INBOARD, WBL 224, CRACK ON SKIN ABOVE CARRIAGE ATTACH FITTING CUT OUT DAMAGED AREA OF SKIN IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER MATERIAL USED 2024 T3 0.063" PO NR 9008130 DIM 5 1/2 INCH BY 4 3/8 INCH IAW SRM 57-50-2 FIG 4 AND 57-50-4 FIG 1. TREATED AND PRIMED REPAIR DOUBLER IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 ON RT INBD FORE FLAP.

Part: SPAR — CORRODED (BS 740) · corrosion level 2 · airframe 43,596 hrs · 34,294 cycles

LT LWR FWD CTR TANK SPAR CORRODED AT STA 744 LBL 20 TO LBL 30. DISPLACED SEAL AT BS 740, OPENED FUEL PANELS NR 7540 AND 7340 FOR ACCESS IAW SRM 51-30-2, MM 51-30-011-4 AND 28-11-021-4, REMOVED SEAL RETAINER , CORNER FITTINGS AND PANELS NR 3445, 6402R AND 6302L FOR ACCESS IAW SRM 51-30-2, DISPLACE CENTER TANK AND WEB AND REMOVED LWR SPAR IAW SRM 51-30-2, LOCATED, DRILLED, COLD WORKED HOLES AND INSTALLED NEW SPAR IAW SRM 51-30-2 AND EA-7-5710-127965, REINSTALLED ALL PREVIOUSLY REMOVED PARTS AT LT LWR FWD CTR TANK IAW SRM 51-30-2 AND MM 28-11-021-4.

Part: SKIN — CORRODED (BS 1166) · airframe 43,596 hrs · 34,294 cycles

SKIN BULGE AND BROKEN FASTENER STA 1166 STR 21L. FOUND CORROSION ON AFT LAV TRIPLER OUT OF LIMITS, REMOVED TRIPLER, FABRICATED NEW TRIPLER AND INSTALLED IAW DWG 65-54583, SRM 51-30-2 AND 51-30-5.

Part: SKIN — CORRODED (CARGO DOOR) · airframe 43,596 hrs · 34,294 cycles

SKIN BULGE IN C-3 DOOR SKIN AFT UPPER CORNER. REMOVED DAMAGED SKIN, FABRICATED NEW SKIN, TREATED, PRIMED AND INSTALLED NEW C3 DOOR EXTERIOR SKIN IAW EA NR 7-5230-126820 AND SRM'S 51-30-2, 51-30-5, AND 51-10-2.

Part: SKIN — DENTED (BS 664-678) · airframe 43,596 hrs · 34,294 cycles

PROTRUDING DENT STA 675 STR 23R. UPON EVALUATION DETERMINED PROTRUDING DENT IS OIL CANNING IAW B727SRM 53-30-1 FIG 1, REMOVED PREVIOUS REPAIR, AND CUT OUT DAMAGE AREA, 2 DAMAGE AREAS DIM (3 1/2 INCHES BY 3 3/8 INCH) AND (2 INCH BY 2 INCH) IAW B727 SRM 53-30-3 FIG 1. FAB DOUBLER MAT USED 2024-T3 .050 INCH PO NR 9008328 DIM (18 INCH BY 14 INCH) IAW B727 SRM 53-30-3 FIG 1, 53-30-2 FIG 2. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 51-30-2.

Part: SPAR — CRACKED (LT WING) · airframe 43,596 hrs · 34,294 cycles

LEFT WING TRAILING EDGE FALSE SPAR LOWER CHORD IS CRACKED AT WBL 118. REPAIRED RT WING T/E FALSE SPAR LOWER CHORD ANGLE IAW DRAWING SR27-57-038 REV C.

Part: FLOORBEAM — CORRODED (BS 312) · airframe 43,596 hrs · 34,294 cycles

FLOORBEAM HAS PITTING CORROSION STA 312 LBL45.

Part: FLOOR SUPPORT — CORRODED (BS 312-344) · airframe 43,596 hrs · 34,294 cycles

FWD LAV AREA, CORROSION ON FLOOR SUPPORT ANGLE BS 312 TO 344 LBL 45. REMOVED CORROSION IAW SRM 51-10-6 AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1. REMOVED FLOOR SUPPORT IAW SRM 51-30-2. CUT OUT DAMAGED AREA AND REPAIRED FLOOR SUPPORT IAW SRM 51-40-4 FIG 3. HEAT TREATED REPAIR ANGLES IAW ENGINEERING REPORT 2-37153-801 REV. A. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS AT FWD LAV AREA FLOOR SUPPORT ANGLE STA 312-344, LBL 45 IAW SRM 51-40-4, FIG 3.

Part: STRINGER — CORRODED (BS 1170-1183) · airframe 43,596 hrs · 34,294 cycles

AFT PIT - STR 22L IS CORRODED FROM BS 1170 TO 1183. CUT-OUT DAMAGED STRINGER SECTION AND FABRICATED STRINGER REPAIR FILLER AND 2 SPLICES AND INSTALLED IAW SRM 53-10-3, 53-10-2 AND 51-10-2.

Part: SPAR — CRACKED (RT WING) · airframe 43,596 hrs · 34,294 cycles

RIGHT WING TRAILING EDGE FALSE SPAR LOWER CHORD IS CRACKED AT WBL 118. REPAIRED RT. WING T/E FALSE SPAR LOWER CHORD IAW DRAWING SR27-57-038 REV. C (STD REWORK DRAWING INBD SPOILER SUPT. BEAM CRACK REPAIR).

Part: BRACKET — CRACKED (BS 640 S3-4L) · airframe 43,596 hrs · 34,294 cycles

CRACKED BRACKET AT MAIN CARGO DOOR UPPER SILL STA 640 BETWEEN STR 3L AND 4L. REMOVED CRACKED FITTING IAW SRM 51-30-2 FABRICATED NEW FITTING IAW DRAWING 53FX1280 REV E TREATED & PPRIMED NEW FITTING IAW SRM 51-10-2 & INSTALLED NEW MAIN CARGO DOOR UPPER SILL BRACKET IAW SRM 51-30-2 & DRAWING 53FX1285 REV E.

Part: SKIN — DENTED (BS 410 S21R) · airframe 43,596 hrs · 34,294 cycles

SKIN DENTED STA 410 STR 21R. EVALUATED DENTS AND FOUND OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA IAW SRM 53-30-3. FABRICATED DOUBLER IAW SRM 53-30-3 FIG 3 AND 53-30-2 FIG 2. TREATED AND PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED REPAIR IAW SRM 53-30-3 FIG 3 AND 51-30-2.

Part: SKIN — DENTED (E/E DOOR) · airframe 43,596 hrs · 34,294 cycles

SEVERAL DENTS IN E/E DOOR SKIN. REMOVED E/E DOOR IAW MM 52-40-001-4, REMOVED SKIN IAW SRM 51-30-2, FABRICATED NEW SKIN IAW SRM 52-40-4 FIG 2 AND 51-30-8, TREATED AND PRIMED SKIN IAW SRM 51-10-2, OPENED INNER SKIN TO FOM IAW SRM 51-30-2, INSTALLED NEW SKIN IAW SRM 51-30-2, INSTALLED INNER SKIN IAW SRM 51-30-2, INSTALLED E/E DOOR IAW MM 52-40-001-4.

Part: SKIN — DENTED (EMERGENCY HATCH) · airframe 43,596 hrs · 34,294 cycles

RT AFT OVERWING EMERGENCY HATCH HAS DENT AT PREVIOUS REPAIR DOUBLER, TOP OF DOOR AT VENT CUT OUT, EXTERIOR SKIN. REMOVED PREVIOUS REPAIR AT RT AFT OVERWING EMERGENCY HATCH IAW SRM 51-30-2. FABRICATED NEW REPAIR DOUBLE IAW SRM 52-20-01 FIG 1 AND 52-00-03 FIG 3. ALODINED AND PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW SRM 52-00-03 FIG 3.

Part: SKIN — MISREPAIRED (100) · corrosion level 2 · airframe 43,596 hrs · 34,294 cycles

IMPROPER FASTENERS IN REPAIR AT STA 1180 STR 21L REMOVED AFT LAV DOOR, PAN, PREVIOUS REPAIR & STRINGER FITTINGS 21 & 22LT IAW SRM 51-30-2 FOR ACCESS, CUT OUT SKIN SECTION AND REPAIRED IAW SRM 53-30-03 FIGURE 12. REINSTALLED AFT LAV DOOR & PAN STRINGER FITTINGS 21 LT & 22 LT IAW 51-30-2 AT STA 1180 STRINGERS 20LT & 26LT

Part: SEAL — FAILED (CARGO DOOR) · airframe 42,373 hrs · 33,322 cycles

AT FL250, CABIN ALT HORN WENT OFF. RAN QRH REGAINED PRESS WITH CARGO OUTFLOW CLOSED. MECHANIC STATED LOWER CARGO DOOR SEAL FAILURE. FOUND THE LWR FWD CARGO DOOR SEAL ON THE LOWER EDGE PUSHED UNDER. LEFT SEAL AS IT WAS FOUND FOR FURTHER EVALUATION. SECURED DOOR SEAL AS NEEDED IAW SMP. PRESSURIZED A/C WITH RIGHT HAND PACK ONLY TO 3.0 PSI, NO DEFECTS NOTED, NO LEAKS FOUND ON DOORS. ACCOMPLISHED EXCESSIVE CABIN PRESSURE LEAKAGE TEST IAW B727 JRH. FOUND TO BE WELL WITHIN LIMITS PER TEST AND PG 8-29, FIGURE 6. OK FOR SERVICE.

Part: LANDING GEAR — FAILED · airframe 41,802 hrs · 32,874 cycles

LANDING GEAR FAILED TO RETRACT NORMALLY. FOLLOWED QRH PROCEDURE TEST 1: INTERMITTENT HORN SOUNDED WHEN RETRACTING FLAPS FROM 5' TO 2'. UNABLE TO TEST WING ANTI-ICE DUE TO SYSTEM OPERATING ALREADY. NOSEWHEEL STEERING ALIGNMENT APPEARED NORMAL. QRH STATES STRUTS NOT EXTENDED. RETURNED FOR NORMAL LANDING.

Part: FRAME — CORRODED (BS 1142 S25-27R) · airframe 41,737 hrs · 32,813 cycles

DURING ACCOMPLISHMENT OF C CHECK MX, AAR AIRCRAFT SERVICES, IND CORROSION WAS FOUND COMMON TO THE FORWARD SIDE OF THE AFT FRAME AT THE NR 3 CARGO DOORWAY AT STA 1142.7 BETWEEN STRINGERS 25R AND 27R (RBL 26). THE DAMAGE WAS BLENDED TO A 20:1 RATIO AND VERIFIED TO BE CRACK FREE. THE DEEPEST NOTED DAMAGE WAS .026" (32% MAT'L LOSS). THERE ARE NO SRM REPAIRS FOR THIS FRAME, DATA WAS SUBMITTED TO BOEING FOR REPAIR, FRAMES ARE SUBJECT OF REFERENCE INSPECTIONS BUT THIS REPAIR IS NOT A DEVIATION TO THIS AD. REPAIR ACCOMPLISHED ON EA 7-5310-106952.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 41,737 hrs · 32,813 cycles

PREVIOUSLY INSTALLED REPAIR INSTALLED ON THE LT OTBD FORE FLAP 10" FROM INBD END HAS GOUGE ON DOUBLER, WITH DEPTH OF DAMAGE AT .040". REMOVED DAMAGED DOUBLER AND INSTALLED NEW DOUBLER REF SRM 57-50-4 FIG 1 PG 2. THIS IS A MAJOR REPAIR ON WO NR 34160 SNRM NR N01238.

Part: SKIN — MISREPAIRED (BS 680-710) · airframe 41,737 hrs · 32,813 cycles

REPAIR LOCATED AT 680-700 STR 27L-28L FOUND NOT TO BE INSTALLED USING APPROVED DATA. FILLER DOES NOT PICK UP 2 ADDITIONAL ROWS BEFORE BUTT SPLICE. REMOVED AND REPLACED DOUBLER FILLER ADDED ADDITIONAL ROWS. INSTALLED REPAIR BETWEEN STA 680-710, STR 27L-25R REF SRM 53-30-3 PG 14B FIG 3A. WORK ACCOMPLISHED ON WO#34610, SNRM N00747.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 41,737 hrs · 32,813 cycles

LT PASSENGER DOOR, LOWER HINGE CUTOUT DOUBLER, HAS INCORRECT FASTENER SIZE, ACCORDING TO SB 727-53A-0198 FIG 5 COMPLIED WITH FED EX EO NR 7-5330-7-2345 PT3. INSTALLED EXTERNAL DOUBLER REPAIR REF SB727-53AO0198 R3.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 41,737 hrs · 32,813 cycles

LT FWD CABIN FLOORBEAM UPPER CAP IS CORRODED AT STA 480, LBL 27-LBL32. CLASSIFIED AS A MAJOR REPAIR ON WO 34610, SNRM # N00525. REMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS REF SRM 51-10-1. CUT OUT DAMAGED SECTION OF BEAM, FABRICATED REPAIR PARTS, TREAT AND PRIME PARTS. REINSTALLED FASTENERS AND REPAIR PARTS WET WITH SEALANT REF SRM 53-10-8 PG 2A FIG 1.

Part: SKIN — GOUGED (FORE FLAP) · airframe 41,737 hrs · 32,813 cycles

PREVIOUSLY INSTALLED REPAIR ON LT OTBD FORE FLAP 10" FROM INBD END HAS GOUGE ON DOUBLER REMOVED DAMAGED DOUBLER AND INSTALLED NEW DOUBLER REF SRM 57-50-4 FIG PG 1. THIS REPAIR CLASSIFIED AS MAJOR ON WO NR 34610, SNRM NR N01238.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 41,737 hrs · 32,813 cycles

CABIN FLOOR STRUCTURE CORROSION ON UPPER SURFACE OF BEAM STA 950, LBL 38-46 STR 17L. REMOVED CORRODED SECTION OF BS 950 AND REPAIRED REF EA NR 7-5310-109942 CLASSIFIED AS A MAJOR REPAIR ON WO NR 34610, SNRM # N00520.

Part: DEPRESSOR — WORN (ZONE 800) · airframe 41,737 hrs · 32,813 cycles

AFT PIT NR 2 DOOR LWR SEAL DEPRESSOR HAS LIGHT WEAR. REMOVED AND REPLACED SEAL DEPRESSOR REF SRM 51-30-02.

Part: FRAME — DAMAGED (BS 360) · airframe 41,737 hrs · 32,813 cycles

LT FOWARD CABIN, FRAME WEB BETWEEN STR 3L AND 4L HAS (7 EA.) UNPLUGGED HOLES. REMOVED DAMAGED AND REPAIRED WITH A FORMED SECTION REPAIR REF. SRM 51-40-03 PG 1-6.

Part: SKIN — UNKNOWN (ZONE 100) · airframe 41,737 hrs · 32,813 cycles

REPAIR LOCATED AT STA 720D-720E AT STR 18L-19L FOUND NOT TO BE INSTALLED USING APPROVED DATA. REMOVED EXISTING DOUBLER, FABRICATED NEW DOUBLER, ADDING ADITIONAL FASTENERS TO THE REPAIR. REF SRM 53-30-03 PG 76-82 AND DETAIL 3. THIS IS CLASSIFIED AS A MAJOR REPAIR ON W/O NR 34610 N00719.

Part: STRINGER — CRACKED (VERTICAL STAB) · airframe 41,737 hrs · 32,813 cycles

LT VERTICAL STAB INTERIOR STRINGER 9L IS CRACKED AT INSPAR RIB CHORDS AT FIN STA 157.2. REMOVED DAMAGE AND REPAIRED REF SRM 51-40-4 FIGURE 3, PAGES 14-17. CLASSIFIED AS A MAJOR REPAIR ON WO 34160, SNRM NR N00685.

Part: REPAIR — MISINSTALLED (FUSLEAGE) · airframe 41,737 hrs · 32,813 cycles

FOUND FLUSH REPAIR LOCATED AT APPROX STA 227.8, LBL 12, UPPER FUSELAGE ABOVE CAPT'S WINDOW. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING NON-CONFORMING DOUBLER AND INSTALLED NEW REPAIR REF EA 7-5310-99336. FUSELAGE MAIN FRAME SKIN REPAIR. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 680-620) · airframe 41,737 hrs · 32,813 cycles

LT FWD CABIN SEAT TRACK BEAM IS CORRODED FROM STA 580 - STA 620 LBL 45 REMOVED CORRODED SECTION OF SEAT TRACK AND REPLACED, REF SRM 53-10-1 FIGURE 3, SRM 53-10-2 FIGURE 7A.

Part: SKIN — UNKNOWN (BS 1343) · airframe 41,737 hrs · 32,813 cycles

FOUND EXTERNAL REPAIR AT APPROX STA 1343 RT SIDE NR 2 NACELLE SKIN (STR 9R-S10R). REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACOMPLISHED USING FAA APPROVED DATA. REPAIRED AREA WITH A SINGLE DOUBLER TYPE REPAIR REF SRM 51-40-2 FIGURE 1 PAGE 3.

Part: SKIN — MISREPAIRED · airframe 41,737 hrs · 32,813 cycles

REPAIR LOCATED AT STA 1030-1039 BETWEEN S26R-27R INSIDE AFT PIT FOUND NOT TO BE INSTALLED USING FAA APPROVED DATA. REF SNRM # 00574 AND SRM 53-30-3 FIG 2 DOES NOT HAVE REQUIRED NUMBER OF FASTENERS. REMOVED REPAIR DOUBLER STA 1030-1039 BETWEEN STR 26R AND S27R. FABRICATED AND INSTALLED INTERNAL DOUBLER REF EA 7-5330-106944, FIG 2 AND SRM 53-30-3 FIG 4.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 41,737 hrs · 32,813 cycles

REPAIR LOCATED AT APPROX STA 294-312, STR 10L-11L FOUND NOT TO BE INSTALLED USING APPROVED DATA. REFERENCE BOEING SB 727-53A0198 AND SNRM NR N00375, THERE ARE INSUFFICIENT FASTENERS IN REPAIR. FABRICATED REPAIR DOUBLER, CAD PLATED, PRIME AND PAINTED REF BOEING SB-727-53A0198 AND INSTALLED.

Part: SKIN — MISREPAIRED · airframe 41,737 hrs · 32,813 cycles

REPAIR LOCATED AT STA 720-720A, BETWEEN STR 28R-29R FOUND NOT TO BE INSTALLED USING APPROVED DATA. REF SNRM NR N00696 AND SRM 53-30-3 FIG 13, DAMAGE CLEAN OUT. EXCEEDS LIMITATIONS OF THIS SRM REPAIR (FIGURE 13). REMOVED REJECTED REPAIR AND REPLACED WITH EXTERNAL SKIN REPAIR REF SRM 53-30-03 FIG 1 PG 8. TREATED, PRIMED, SEALED AND TOP COATED REPAIR AREA, REF SRM 51-10-2, 51-20-4, AND MM 51-20-151-7.

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 41,737 hrs · 32,813 cycles

EXTERNAL REPAIR LOCATED AT APPROX 29 INCHES FROM AFT END AND 48" FROM BOTTOM END ON THE FWD LOWER CARGO DOOR FOUND NOT TO BE INSTALLED USING FAA APPROVED DATA. REF SNRM NR N00567 AND SRM 52-00-3 FIG 3 - FIG 4. INCORRECT FASTENER SPACING, DAMAGE REMOVAL CANNOT BE VERIFIED. ADDED FASTENERS TO EXISTING DOUBLER TO CONFORM TO SRM 52-00-03 FIG 3.

Part: SEAT TRACK — CORRODED (BS 620-628) · airframe 41,737 hrs · 32,813 cycles

LT CABIN SEAT TRACK BEAM IS CORRODED AT STA 620-628 LBL 1. REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK AND INSTALLED REF SRM 51-30-02 (N00537).

Part: FLOORBEAM — CORRODED (BS 620) · airframe 41,737 hrs · 32,813 cycles

LT FWD CABIN FLOORBEAM UPPER CAP CORRODED FOM STA 620 LBL 1- LBL 24. REMOVED CORROSION AND REPAIRED DAMAGED AREA REF SRM53-10-8 FIG 1 (N00533).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,737 hrs · 32,813 cycles

CABIN LT SIDE STA 990-1070 LBL 45.5 SEAT TRACK HAS CORROSION AND EXFOLIATION ON O/B FLANGE REMOVED DAMAGED SEAT TRACK AND REPLACED WITH NEW TRACK REF SRM 53-10-5 PG1-5

Part: FRAME — CRACKED (BS 804 S14R) · airframe 41,737 hrs · 32,813 cycles

CABIN FUSELAGE FRAME AT STA 804 STR 14R, CRACKING OUT OF FASTENER HOLE AFT SIDE OF FRAME. CUTOUT AND REMOVED DAMAGED PORTION OF FRAME CHORD, HFEC INSPECTED THE CUTOUT TO VERIFY NO CRACKS. FABRICATED FILLER AND REPAIR ANGLE. INSTALLED REPAIR PARTS WET WITH SEALANT REF SRM 51-40-3 FIG 1 (N00505).

Part: SKIN — MISREPAIRED (BS 400-420) · airframe 41,737 hrs · 32,813 cycles

AGING A/C INSP, REPAIR LOCATED AT STA 400-420, STR 16L-17L FOUND NOT TO BE INSTALLED USING APPROVED DATA REF SNRM NR N00371 AND SRM 53-30-3 FIG 3. REPAIR ENDS ON A STRINGER. REMOVED REPAIR, FABRICATED AND INSTALLED NEW REPAIR REF SRM53-30-3 FIG 3.

Part: SKIN — MISREPAIRED (BS 1090-1110) · airframe 41,737 hrs · 32,813 cycles

AGING A/C INSPECTION REPAIR LOCATED AT STA 1090-1110, STR 29L-29R FOUND NOT TO BE INSTALLED USING APPROVED DATA, REF SNRM NR N00081 AND SRM 53-30-3 FIG 3 REPAIR DOES NOT HAVE REQUIRED NUMBER OF FASTENER ROWS FWD AND AFT. REMOVED PREVIOUS REPAIR, VERIFIED MATERIAL, MANUFACTURED DOUBLER AND FILLER, TREATED, PRIMED, AND INSTALLED REPAIR REF SRM 53-30-3 FIG 3.

Part: SKIN — DAMAGED (BS 227-227) · airframe 41,737 hrs · 32,813 cycles

LIGHTNING STRIKE ON FWD LOWER FUSELAGE BLENDED OUT OF LIMITS REF SNRM N00292 AT STA 226 13 INCH BELOW STR 26L. CUT OUT DAMAGED AREA, VERIFIED MATERIAL. FABRICATED DOUBLER, ALODINED, PRIMED, PAINTED, EDGE SEALED DOUBLER. REF SRM 53-30-3, AND SRM 51-10-7 FIG 13A PG 74C-74F.

Part: SEAT TRACK — CORRODED (BS 546-547) · airframe 41,737 hrs · 32,813 cycles

LT FWD CABIN SEAT TRACK BEAM IS CORRODED AT STA 546 LBL 24. REMOVED SEAT TRACK AND INSTALLED NEW TRACK REF SRM 51-30-5, AND SRM 51-30-2. (N00527)

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 41,737 hrs · 32,813 cycles

MAIN CARGO COMPT SEAT TRACK HAS A CRACK AND CORROSION AT FASTENER HOLE, APPROX AT BS 693 LBL 24 REMOVED SEAT TRACK FROM STA 690-740 LBL24 REF SRM 51-30-2. VERIFIED MATERIAL FOR NEW SEAT TRACK REF SRM 53-10-2 PG 13. FABRICATED NEW SEAT TRACK REF DWG NR 2902 AND GMM 7-0-1001 PAGES 1-2. TREATED SEAT TRACK REF MM 51-20-021-7 PAGES 1-3. PRIMED SEAT TRACK REF MM 51-20-031-7 PAGES 1-3. INSTALLED NEW SEAT TRACK AT STA 690-740 LBL 24. REF SRM 51-30-2 PAGES 8/14. PICKED UP HOLES FOR FLOORBOARDS REF SRM 51-20-1 PG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: WARNING HORN — FALSE ACTIVATION (CARGO FIRE) · airframe 41,163 hrs · 32,349 cycles

MAIN CARGO SMOKE POSITION 3 ILLUMINATED INTERMITTANTLY ACCOMPANIED BY FIRE BELL AT 35,000 FT CONTINUED FOR APPROX 5 MIN AND QUIT JUST PRIOR TO LANDING. PTT GOT A FLASHING POSITION 3 AND STEADY ALL OTHERS. PERFORMED CARGO SMOKE DETECTOR TEST WITH NO FAULTS. A/C CARGO WAS UNLOADED & INSPECTED. POSITION NR 4 HAD 90 LBS OF DRY ICE, SUSPECT SOURCE OF SMOKE INDICATION NR 3 SMOKE DETECTOR REMOVED AND REPLACED PRECAUTIONARY PER M/M 26-16-011-4. OPS CHECK NORMAL.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 40,619 hrs · 31,906 cycles

FLOORBEAM AT STA 620 RBL 0-24.5 HAS CORROSION ON UPPER CAP. REMOVED DAMAGED AREA IAW SRM 53-10-8. FAB REPAIR PARTS, T-ANGLE, SUPPORT ANGLE, STRAP, IAW SRM 53-10-3 FG 3 PG 18. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED PARTS IAW SRM 53-10-8 FIG 3 PG 18.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 39,624 hrs · 31,083 cycles

FLOORBEAM AND SHEAR WEB STA 1130, RBL 19 (TOP CHORD) EXFOLIATED. INSTALLED SEAT TRACK, 2 STRAPS AND T-CHORD IAW SRM 51-30-2. INSTALLED REPAIR IAW SRM 53-10-8.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 39,624 hrs · 31,083 cycles

FWD CARGO COMPT BILGE AREA HAS A CORRODED SHEAR TIE FS 520, STR 26L - 27L. INSTALLED NEW SHEAR TIE IAW SRM 51-30-2.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 39,624 hrs · 31,083 cycles

AFT LWR CARGO COMPT INTERCOSTAL INBOARD OF STR 26L, BETWEEN FS 1140 TO 1166, UPPER AND LWR FLANGES CORRODED. INSTALLED FABRICATED FLANGES OF INTERCOSTAL IAW SRM 51-30-2. INSTALLED FABRICATED DOUBLER AT STA 1140 -1166, STR 26L IAW SRM 51-30-2.

Part: FRAME — DENTED (ZONE 100) · airframe 39,624 hrs · 31,083 cycles

AFT LWR CARGO COMPT FRAME 1010 UPPER FLANGE DENTED AT STR 26L. REPLACED FRAME IAW B727 SRM 51-40-3 FIG 1.

Part: CONTROL CABLE — OUT OF POSITION (HORIZ STAB) · airframe 39,354 hrs · 30,872 cycles

AFTER LANDING, STABILIZER INOP IN BOTH CRUISE AND STAB MODE MANUAL HAND CRANK SHOWS NO RESISTANCE AS IF CABLE IS BROKEN. TROUBLESHOT TO STAB TRIM CABLES BEING OFF UPPER DRUM AND BOUND UP UNDERNEATH IT. REMOVED UPPER AND LOWER, LEFT AND RIGHT JACK SCREW ACCESS PANELS. CUT AND BLOCKED CABLES (TO THE BULKHEAD FORWARD OF JACKSCREW). REMOVED BOUND UP CABLE FROM AROUND BOTTOM OF DRUM. CRUISE AND STAB TRIM MOTOR C/B'S ARE PULLED AND TAGGED. REMOVED AND REPLACED STAB TRIM CABLES. COMPLETED INSTALLATION AND RIG OF STAB TRIM CABLES. ADJUSTED CHAIN TENSION AND INDICATOR PER B727-200 MM 27-40-000.

Part: MOTOR — FAILED (T/E FLAP) · airframe 38,358 hrs · 30,112 cycles

COMPLETE LOSS OF SYSTEM A HYDRAULIC FLUID JUST PRIOR TO FLAP EXTENSION. SPOILERS HAD BEEN USED JUST PRIOR TO LOSS. REPLACED RIGHT OUTBOARD FLAP MOTOR IAW MM, SERVICED HYDRAULIC SYSTEM TO FULL LEVEL. OPERATED FLAPS UP AND DOWN SEVERAL TIMES, ALL INDICATIONS NORMAL.

Part: TIE — CORRODED (STABILIZERS) · corrosion level 2 · airframe 32,537 hrs · 29,470 cycles

N 1259 VERT STAB TENSION TIE FITTING RH AFT VERTICAL BOLT HOLE CORRODED. R&R TIE PER MM 55-30-051-4.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 32,537 hrs · 29,470 cycles

VERT STAB TENSION TIE FITTING LT AFT VERTICAL BOLT HOLE CORRODED. REMOVED AND REPLACED TIE PER MM 55-30-051-4.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,537 hrs · 29,470 cycles

COCKPIT FLOOR PANEL SUPPORT ANGLE CORRODED BS 266, LBL 10 TO 12, WL 207. REMOVED AND REPLACED ANGLE PER SRM 51-10-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE LOWER) · airframe 32,537 hrs · 29,470 cycles

N 1322 INTERCOSTAL CRACKED BETWEEN BS 720C AT STR 26L. R&R INTERCOSTAL PER SRM 51-20-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE LOWER) · airframe 32,537 hrs · 29,470 cycles

N 1306 INTERCOSTAL CRACKED AT BS 950 AT STR 29R. R&R INTERCOSTAL PER SRM 51-20-1.

Part: SKIN — CRACKED (FUSELAGE TOP) · airframe 32,537 hrs · 29,470 cycles

N 1228 6 FASTENER HOLES CRACKED FOR MCD UPR HINGE ON FUSELAGE BETWEEN 480 & 620, STR 2L & 3L. R&R PER EO 7-5230-7-5000.

Part: ANGLE — CORRODED (FUSELAGE LOWER) · corrosion level 2 · airframe 32,537 hrs · 29,470 cycles

N 848 BAGGAGE BIN WALL SUPPORT ANGLE CORRODED AT BS 720D BETWEEN STR 24L & 25L. R&R ANGLE PER SRM 51-30-2.

Part: TRACK — CORRODED (FUSELAGE TOP) · airframe 32,537 hrs · 29,470 cycles

N 973 #7 CARGO TRACK CRACKED BETWEEN BS 690 AND 700. R&R TRACK PER SRM 53-10-5.

Part: STRINGER — CORRODED (FUSELAGE LOWER) · corrosion level 2 · airframe 32,537 hrs · 29,470 cycles

N 815 STR 28L CORRODED AT BS 540. R&R STRINGER PER SRM 51-10-3.

Part: FITTING — CORRODED (LAND GEAR) · corrosion level 2 · airframe 32,537 hrs · 29,470 cycles

N 600 SUPPORT FITTING FOR NOSE LG DOOR ACTUATOR RODS CORRODED. R&R FITING PER SRM 51-30-2.

Part: STRINGER — CORRODED (FUSELAGE LOWER) · corrosion level 2 · airframe 32,537 hrs · 29,470 cycles

N 813 STR 28R CORRODED AT BS 400 TO 500. R&R STR PER SRM 51-10-3.

Part: STRINGER — CORRODED (FUSELAGE LOWER) · corrosion level 2 · airframe 32,537 hrs · 29,470 cycles

N 593 CORROSION ON STR 28R, BS 1065 TO 1070. R&R STRINGER PER SRM 53-10-3.

Part: SHEAR TIE — CRACKED (FUSELAGE LOWER) · airframe 32,537 hrs · 29,470 cycles

N 507 SHEAR TIE CRACKED AT BS 1168, STR 29R. R&R SHEAR TIE PER SRM 53-10-4.

Part: STRINGER — CORRODED (FUSELAGE LOWER) · corrosion level 2 · airframe 32,537 hrs · 29,470 cycles

N 507 CORROSION ON STR 29R AT BS 1168. R&R STRINGER PER SRM 53-10-3.

Part: SEAT TRACK — CRACKED (FUSELAGE TOP) · airframe 32,537 hrs · 29,470 cycles

N 414 SEAT TRACK #4 CRACKED AT BS 400. R&R TRACK PER SRM 53-10-5.

Part: SKIN — CRACKED (RT MLG DOOR) · airframe 32,537 hrs · 29,470 cycles

RT MLG WING DOOR SKIN CRACKED AT HINGE CUTOUT. REMOVED AND REPLACED DOOR PER EO 7-5280-7-4301.

Part: INTERCOSTAL — CRACKED (FUSELAGE LOWER) · airframe 32,537 hrs · 29,470 cycles

N 412 CRACKED INTERCOSTAL BS 550 AT STR 27L. R&R INTERCOSTAL PER SRM 51-40-3.

Part: ANGLE — CORRODED (FUSELAGE LOWER) · corrosion level 2 · airframe 32,537 hrs · 29,470 cycles

N 424 WALL SUPPORT ANGLE CORRODED BS 1166 AT WL 178. R&R ANGLE PER SRM 51-30-2.

Part: SHEAR TIE — CORRODED (FUSELAGE LOWER) · corrosion level 2 · airframe 32,537 hrs · 29,470 cycles

N 408 CORROSION ON SHEAR TIE BS 720A BETWEEN STR 25R AND 26R. R&R SHEAR TIE PER SRM 51-30-2.

Part: INTERCOSTAL — CRACKED (FUSELAGE LOWER) · airframe 32,537 hrs · 29,470 cycles

N 411 CRACKED INTERCOSTAL BS 540 TO 560 AT STR 25L. R&R INTERCOSTAL PER SRM 51-40-3.

Part: BELTFRAME — CORRODED (FUSELAGE LOWER) · corrosion level 2 · airframe 32,537 hrs · 29,470 cycles

N 592 CORROSION ON BELT FRAME BS 1050 BETWEEN STR 27R & 28R. R&R BELTFRAME PER SRM 53-10-4.

Part: INTERCOSTAL — CRACKED (FUSELAGE LOWER) · airframe 32,537 hrs · 29,470 cycles

N 522 INTERCOSTAL CRACKED AT BS 970 BETWEEN STR 26R AND 27R. R&R INTERCOSTAL PER SRM 51-30-2.

Part: STEP — CORRODED (FUSELAGE LOWER) · corrosion level 2 · airframe 32,537 hrs · 29,470 cycles

N 258 CORROSION ON #5 AIRSTAIR STEP. R&R STEP PER SR 27-52-003 & SRM 51-30-2.

Part: SLAT — CRACKED (LEFT WING) · airframe 32,537 hrs · 29,470 cycles

N 246 #4 LEAD EDGE SLAT HAS 3 CRACKED RIBS BETWEEN WS 383.5 AND 436.5. R&R SLAT PER MM 27-81-811-4.

Part: DOOR — CRACKED (LT MLG) · airframe 32,537 hrs · 29,470 cycles

LT MLG STRUT DOOR CRACKED AT AFT HINGE CUTOUT. REMOVED AND REPLACED DOOR PER EO 7-5280-7-4301.

Part: ACTUATOR — RUPTURED (NR 1 SLAT)

COMPLETE LOSS OF SYS A HYD FLUID ON T/O. PER EMERGENCY AND ABNORMAL PROC HDBK CK LIST, 1 AND 2 ENG FLUID SHUTOFF SWITCHES CLOSED. NR 1 LEAD EDGE SLAT ACTUATOR FAILED WHILE EXTENDED. *S/D* REPLACED NR 1 SLAT ACTUATOR PER MM 27-81-32. LEAK AND OPS CK NORM.

Part: DRIVE UNIT — FAILED (LT TE FLAP)

TOTAL LOSS OF A SYS QUANT ON SHORT FINAL. REPLACED CASE DRAIN FILTERS PER MM 29-11-041, I/B FLAP DRIVE UNIT HYD MTR PER MM 27-51-062-4, A SYS HYD PRESS FILTER PER MM 29-11-062-3. ENGINE DRIVEN HYD PUMPS OPER NORM.

Part: FLOORBEAM — CORRODED (BS 680-700)

NR 0300 004, CORROSION AT NUT PLATE HOLES BETWEEN BLOWOUT PANEL TRIM AND TENSION STRAPS AND BETWEEN BS 680 TO 700, RBL 25 AND 45 WL 200. *S/D* REMOVED DAMAGED TEAR STRAPS. FABRICATED NEW TEAR STRAPS AND INSTALLED AT RBL 25 AND RBL 45 BETWEEN BS 680 TO 700, WL 200. ALL WORK DONE IAW FED-EX SRM 53-30-4. REMOVED DAMAGE ON FLOORBEAM, FABRICATED REPAIR PARTS AND INSTALLED IAW FED-EX SRM 53-10-8.

Part: SHEAR TIE — CORRODED (BS 700)

NR 0609 005, CORROSION ON SHEAR TIE AT BS 700 IN BETWEEN STR 25 AND STR 26 RT, WL 155. *S/D* REMOVED DAMAGED SHEAR TIE AND INSTALLED NEW SHEAR TIE AT BS 700 BETWEEN STR 25 AND STR 26 RT, WL 155, IAW FED-EX SRM 51-302, 51-20-01, 51-10-02, M/M 51-20-151.

Part: FLOORBEAM — CORRODED (BS 344)

NR 0465 002 CORROSION (53-224-01) ON BS 344 FLOORBEAM BETWEEN RBL 12 AND LBL 55, WL 208. REMOVED UPPER CHORD ON FLOORBEAM AT BS 344, RBL 4 - LBL 65, WL 208 AND FABRICATED NEW UPPER CHORD AND SPLICE ANGLES PER FED-EX DRAWING SR 27-53-007. INSTALLED FASTENERS PER FED-EX SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 1130)

NR 0167 001 CORROSION ON FLOORBEAM BS 1130, RBL 54 TO LBL 54 UNDER NUTPLATE CLIPS WL 200. REMOVED DAMAGED PART AT BS 1130. FABRICATED REPAIR PARTS ALODINED, PRIMED, DRILLED, PAINTED AND INSTALLED PER FED-EX EA NR 7-5310-32960 AT BS 1130, RBL 54 TO LBL 54.

Part: MIDFLAP — DELAMINATED (LT TE FLAP)

NR 0345 003 L/W INBOARD MIDFLAP TIE WEDGE CORRODED IN SEVERAL PLACES ON UPPER SURFACE. REPAIRED CORRODED AREAS ON UPPER SURFACE OF LT WING INBOARD MIDFLAP TIE IAW FED-EX SRM 51-40-6.