N241FE

Part: STRINGER SPLICE — CORRODED (BS 1000) · airframe 54,318 hrs · 41,731 cycles

AFT PIT CORROSION ON STRINGER SPLICE AT BS 1000, STRINGER 29 RT. REMOVED STRINGER SPLICE FOR CORROSION REMOVAL IAW SRM 51-30-2. FABRICATED NEW SPLICE IAW SRM 51-20-2. FIGURE 1 & 51-30-5. INSTALLED NEW STR. SPLICE IAW SRM 51-30-2. APPLIED LEVELING COMPOUND IAW SRM 51-20-3. MAJOR

Part: SPAR — CRACKED (ZONE 600) · airframe 54,318 hrs · 41,731 cycles

RIGHT WING T/E FALSE SPAR CHORD ANGLE CRACKED. REMOVED & REINSTALLED TORQUE BOX FITTING TO ACCESS WEB, CUT-OUT DAMAGED AREA. FABRICATED NEW WEB, FABRICTATED NEW CHORD SECTION, FABRICATED 2 ANGLES, FABRICATED 2 RADIUS FILLER, AND FABRICATED NEW DOUBLER. HEAT TREATED ANGLES AS REQUIRED TO T6 CONDITION IAW FAS ENGINEERING REPORT 2-37153-801 REV A. TREATED/PRIMED AND INSTALLED ALL PARTS ALL IAW SRM 51-30-2 & DWG SR 27-57-038 REV C.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 54,318 hrs · 41,731 cycles

FOUND SHEAR TIE CORROSION BS 680 STR 28R TO 28L. CUT-OUT DAMAGED AREA IAW SRM 53-10-4 FIG 15. FABRICATED REPAIR PARTS IAW SRM 53-10-4 FIG 15 AND TREATED AND PRIMED IAW SRM 51-10-2 AND INSTALLED PARTS IAW SRM 53-10-4 FIG 15 AT SHEAR TIE STA 680 STR 28L - 28R.

Part: SPAR — CRACKED (LT WING) · airframe 54,318 hrs · 41,731 cycles

LT WING T/E FALSE SPAR LOWER CHORD ANGLE CRACKED, WBL 118. REMOVED DAMAGED SECTION OF FALSE SPAR IAW DWG SR27-57-038. FABRICATED NEW SPAR SECTION, WEB, 2 SUPPORT ANGLES, STRAP, DOUBLER, ALL IAW DWG SR 27-57-038 REV. C. INSTALLED ALL REPAIR PARTS IAW SR 27-57-038 REV. C.

Part: SKIN — DENTED (BS 712-720) · airframe 54,318 hrs · 41,731 cycles

DENT EXTERIOR FUSELAGE STA 712 TO STA 720 6 INCH BETWEEN STR 18R TO STR 19R. CUT OUT DAMAGED AREA, FABRICATED NEW SKIN AND REPAIR DOUBLER. TREATED, PRIMED & INSTALLED NEW PARTS ALL IAW SRM 53-30-3 FIG (12), 51-30-2 & 51-10-2.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 54,318 hrs · 41,731 cycles

NON-COMPLIANT REPAIR AT BS 533-543 STR 25R-26R. REMOVED EXISTING REPAIR AND FABRICATED NEW DOUBLER REPAIR, TREATED, PRIMED, & INSTALLED NEW DOUBLER REPAIR ALL IAW SRM 51-30-2, 53-30-3 FIG (1) & 51-10-2.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 54,318 hrs · 41,731 cycles

FWD PIT STRINGER 28L CORRODED BS 490. REMOVED FASTENERS AND CUT-OUT DAMAGED AND FABRICATED STRINGER FILLER. FABRICATED NEW SPLICE. TREATED, PRIMED & INSTALLED NEW PARTS ALL IAW 53-10-3 FIG (1), 51-30- 2, AND 51-10-2.

Part: REGULATOR — FAILED (A/C PACK) · airframe 53,513 hrs · 41,090 cycles

DURING CLIMB-OUT WITH ENG ANTI ICE OPEN, WHEN RT PACK WAS TURNED ON, RIGHT PSI MAXED OUT TO 110 PSI. WHEN RT PACK WAS SWITCHED OFF, ENG 3 STRUT OVHT LIGHT ILLUM FOR APPROX 20 SEC. NR 3 PWR LEVER WAS REDUCED AND LIGHT WENT OUT. CYCLING THE PACK BACK ON PSI REMAINED 20 PSI HIGHER THAN THE LEFT SIDE AT 50 PERCENT POWER SETTING. REMOVED AND REPLACED NR 3 HIGH PRESS REGULATOR PER AMM 36-12-051-4. RAN ENG PER JRH AND LEAK CK OF HIGH PRESSURE REGULATOR IS GOOD. NO LEAKS NOTED. PERFORMED HI-PRESS BLEED CONT SYS CK. CK OK PER 727 JRH 8-17. CK'D STRUT O/H LOOPS. NO DEFECTS NOTED. TEST SYS RUN OK.

Part: SWITCH — DAMAGED · airframe 53,479 hrs · 41,057 cycles

AFT AIRSTAIR AMBER WARNING LIGHT ILLUMINATED IN FLIGHT WHILE CRUISING AT FL 350. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 21JAN08 "MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT - INOP." REMOVED AND REPLACED AFT AIRSTAIRS UPPER HANDLE SWITCH S395 USING S/M/P REF AMM CHAPTER 20. PERFORMED ADJ/TEST REF AMM 52-70-001-5. OPS CHECKS NORMAL.

Part: RIB — MISALIGNED (ZONE 600) · airframe 53,144 hrs · 40,787 cycles

COMPLY WITH EA NR 7-5710-110754 WING, (AD 90-06-09: 94-07-08: 98-11-03) RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS. COMPLIED WITH EA NR 7-5710-110754 WING, (AD 90-06-09: 94-07-08: 98-11-03) RBL 70.5 RIB UPPER REPAIR DEVIATIONS.

Part: RIB — MISALIGNED (ZONE 600) · airframe 53,144 hrs · 40,787 cycles

WING RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS EA NR 7-5710-110754. COMPLIED WITH EA NR 7-5710-110754 WING, AD 90-06-09: 94-07-08: 98-11-03) RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS.

Part: RIB — DAMAGED (ZONE 600) · airframe 53,144 hrs · 40,787 cycles

COMPLY WITH EA 7-5710-110753, RT SIDE ONLY, WINGS- (AD 90-06-09 AND AD 94-07-08) MAIN FRAME, RIB UPPER CHORD REPAIR EO 7-5710-7-2308 PART 2. COMPLIED WITH EA 7-5710-110753 RT SIDE IAW SB 727-57-0112.

Part: RIB — CRACKED (ZONE 600) · airframe 53,121 hrs · 40,768 cycles

RIGHT RIB CHORD UPPER VERTICAL FLANGE HOLE AT STATION 760.95. LOWER FWD HOLE (B), RELEVANT CRACK INDICATION NOTED AT THE 9 O`CLOCK POSITION LOOKING I/B. MADE TEMPORARY REPAIR PER ENGINEERING AND AIRCRAFT WAS FERRIED TO VENDOR FOR PERMANENT REPAIR.

Part: STRINGER — CRACKED (VERTICAL STAB) · airframe 52,783 hrs · 40,493 cycles

VERTICAL STAB INTERIOR, STR 9 LT IS CRACKED AT RIB STA 110.4 REPAIRED PER FED EX EA 7-5530-100611.

Part: SKIN — CORRODED (LT WING) · airframe 52,783 hrs · 40,493 cycles

CORROSION LEFT WING UPPER SKIN AT BUTT SPLICE 42" OTBD OF NR 4 SLAT INBD EDGE. REPAIRED PER FED EX EA 7-5730-105911.

Part: FITTING — CORRODED (TE FLAPS) · airframe 52,783 hrs · 40,493 cycles

WHILE WORKING CARD N00533, FOUND CORROSION ON NR 5 K-FLAP CENTER HINGE FITTING (A/C SIDE) IB LUG, I/B FACE. REPAIRED NR 5 K-FLAP CENTER HINGE FITTING IAW FED EX EA 7-5710-100605.

Part: SHEAR TIE — CORRODED (BS 1148) · airframe 52,783 hrs · 40,493 cycles

FOUND CORROSION BETWEEN SHEAR TIE AND FRAME BS 1148, STR 28 LT - 30 LT. REPAIRED SHEAR TIE PER SRM 53-10-4 FIG 14.

Part: FLAP TRACK — CORRODED (TE FLAPS) · airframe 52,783 hrs · 40,493 cycles

RT WING LWR SURFACE AT NR 7 FLAP TRACK HAS CORROSION AT FWD TRACK MOUNTING BRACKET. REPAIRED PER FED EX EA 7-5710-100604.

Part: FLAP TRACK — CORRODED (TE FLAPS) · airframe 52,783 hrs · 40,493 cycles

NR 7 FLAP TRACK HAS CORROSION AT AFT MOUNTING HOLES. REMOVED AND REPLACED NR 7 FLAP TRACK IAW FED EX W/C 27X5709-03.

Part: SEAT TRACK — CORRODED (BS 740-760) · airframe 52,783 hrs · 40,493 cycles

EXPANSION LINK, BS 740-760, LBL 45 CORRODED AROUND FWD ATTACH BOLT. REMOVED AND REPLACED EXPANSION LINK BS 740-760 LBL 45 IAW SRM 53-10-1.

Part: ANGLE — CORRODED (SPOILER) · airframe 52,783 hrs · 40,493 cycles

FOUND CORROSION ON UPPER SPOILER BEAM ANGLE FROM NR 5 TO NR 6 SPOILER ACTUATORS. REMOVED DAMAGE ON UPPER SPOILER BEAM ANGLE FROM NR 5 TO NR 6 SPOILER ACTUATORS AND REPAIRED IAW SRM 51-40-4.

Part: SKIN — UNKNOWN (HORIZ STAB) · airframe 52,783 hrs · 40,493 cycles

RT STAB UPPER SURFACE, STA APPROX 4" FROM I/B END T/E, EXTERNAL 3" DOUBLERS, REQUIRES EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF THE REPAIR IS IN ACCORDANCE WITH FAA, APPROVED DATA. REMOVED EXISTING REPAIR ON RT HORIZ STAB UPPER SURFACE AND REPAIRED IAW SRM 51-30-2 AND 55-20-3.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,783 hrs · 40,493 cycles

FOUND DENT IN FRAME STA 600 BETWEEN STR 24L - 25L. REMOVED DAMAGE IN FRAME STA 600 BETWEEN STR 24L - 25L AND REPAIRED IAW SRM 51-30-2.

Part: DEPRESSOR — DAMAGED (CARGO DOOR) · airframe 52,783 hrs · 40,493 cycles

AFT NR 2 CARGO DOOR LWR CENTER SEAL DEPRESSOR CHAFED. REMOVED AND REPLACED AFT NO. 2 CARGO DOOR CNTR SEAL DEPRESSORE IAW SRM 51-30-5.

Part: DEPRESSOR — DAMAGED (CARGO DOOR) · airframe 52,783 hrs · 40,493 cycles

AFT NR 2 CARGO DOOR LWR FWD CORNER SEAL DEPRESSOR DAMAGED. REMOVED AND REPLACED AFT NO. 2 CARGO DOOR LWR FWD SEAL DEPRESSOR IAW SRM 51- 30-5.

Part: SKIN — BULGED (CARGO DOOR) · airframe 52,783 hrs · 40,493 cycles

AFT NR 2 CARGO DOOR SKIN BULGING AROUND 8 CUPPED FASTENERS 1-2 INCHES FROM AFT EDGE 8-10 INCHES FROM BOTTOM. CUT OUT DAMAGE AREA LWR AFT CORNER, FABRICATED SKIN DOUBLER AND FILLER INSTALLED REPAIR ALODINED & PRIMED. REINSTALLED LEVELING COMPOUND PER SRM 52-00- 2, SRM 52-00-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,783 hrs · 40,493 cycles

CORROSION ON FLOORBEAM UPPER CHORD BS 380 RBL 50 WL 208. REMOVED DAMAGE AREA OF UPPER CHORDS AT BS 380 RBL 50 AND REPAIRED IAW SRM 53-10-8.

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 52,783 hrs · 40,493 cycles

NR 2 CARGO DOOR, EXTERNAL SKIN, FWD LWR CORNER, DOUBLER REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF THE REPAIR IS IN ACCORDANCE WITH FAA, APPROVED DATA. COMING DOUBLER REPAIR ON NR 2 CARGO DOOR SKIN WAS NOT IN COMPLIANCE WITH FAA APPROVED DATA. REMOVED REPAIR AND REMOVED DAMAGED AREA OF SKIN. FABRICATED REPAIR DOUBLER AND REPAIR PARTS. INSTALLED REPAIR IAW SRM 52-00-3, 51-40-3, AND 51-30-2.

Part: FRAME — DENTED (BS 680) · airframe 52,783 hrs · 40,493 cycles

FRAME FLANGE DENTED STA 680 STR 23L - 25L. REMOVED DAMAGE ON FRAME BS 680 STR 23L-25L AND IAW SRM 51-40-3.

Part: FLOORBEAM — DAMAGED (BS 870) · airframe 52,783 hrs · 40,493 cycles

DRILL START IN UPPER CHORD OF BS 870 FLOORBEAM AT LBL 50, WL 208. REPAIRED BS 870 FLOORBEAM AT LBL 50, WL 208 IAW FED EX EA 7-5310- 105909.

Part: FRAME — DAMAGED (BS 520) · airframe 52,783 hrs · 40,493 cycles

FWD CARGO COMPARTMENT, DAMAGE TO STA 520 FRAME BETWEEN STR 22L AND 25L. REMOVED DAMAGE ON FRAME BS 520 BETWEEN STR 22L AND 25L AND REPAIRED IAW SRM 53- 10-1.

Part: SHEAR TIE — CORRODED (BS 1148) · airframe 52,783 hrs · 40,493 cycles

AFT CARGO BAY CORROSION ON SHEAR TIE BS 1148 LBL 3. REMOVED AND REPLACED SHEAR TIE BS 1148 LBL 3 IAW SRM 53-10-4.

Part: SHEAR TIE — CORRODED (BS 1148) · airframe 52,783 hrs · 40,493 cycles

AFT CARGO BAY CORROSION ON SHEAR TIE BS 1148 LBL 16. REMOVED AND REPLACED SHEAR TIE AT BS 1148 LBL 16 IAW SRM 53-10-4.

Part: SHEAR TIE — CORRODED (BS 1148) · airframe 52,783 hrs · 40,493 cycles

AFT CARGO BAY CORROSION ON SHEAR TIE BS 1148 LBL 10. REMOVED AND REPLACED SHEAR TIE BS 1148 LBL 10 IAW SRM 53-10-4.

Part: SHEAR WEB — DENTED (FUSELAGE) · airframe 52,783 hrs · 40,493 cycles

FOUND DENT IN SHEAR WEB AT BS 1137, RBL 26, WL 208. REPAIRED PER SRM 51-40-2 FIG 1.

Part: SHEAR WEB — DAMAGED (BS 1130-1176) · airframe 52,783 hrs · 40,493 cycles

WHILE WORKING N01197 FOUND LT SHEAR WEB AT BS 1130 - 1176, LBL 25 - LBL 65, WL 208 TO HAVE NUMEROUS MISDRILLED AND DOUBLE HOLES. REMOVED AND REPLACED LEFT SHEAR WEB AT BS 1130 - BS 1176, LBL 25 - LBL 65 WL 208 PER SRM 51-30-2.

Part: CREASE BEAM — DAMAGED (BS 720E-720F) · airframe 52,783 hrs · 40,493 cycles

FOUND CREASE BEAM TO BE MISDRILLED AT BS 720F AND 720E LBL 63, WL 208. REMOVED DAMAGE CREASE BEAM AT BS 720F TO 720E LBL 63 WL 208 AND REPAIRED IAW SRM 51-30-5, 51-30-6, AND 51-30-8.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,783 hrs · 40,493 cycles

FOUND CORROSION ON CREASE BEAM WEB AT BS 720C PLUS 11" AND 720C PLUS 18", LBL 65, WL 208. REMOVED DAMAGE ON CREASE BEAM AT 720C PLUS 11 TO 720C PLUS 18, LBL 65, WL 208 AND REPAIRED IAW SRM 51-30-2.

Part: SPAR — DAMAGED (WS 212) · airframe 52,783 hrs · 40,493 cycles

SHEARED FASTENER HEAD IN RT WING UPPER REAR SPAR VERTICAL FLANGE AT WS 212. REPAIRED PER FED EX EA 7-5710-100602.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 52,783 hrs · 40,493 cycles

WHILE WORKING 1176 CHORD, FOUND AFT CENTER SHEAR WEB FROM BS 1148 - BS 1176, LBL 25 - RBL 25, WL 208 TO HAVE NUMEROUS DOUBLE HOLES AND TO BE CRACKED. FABRICATED NEW WEB PER SRM 51-0-2.

Part: STIFFENER — CORRODED (LT WING) · airframe 52,783 hrs · 40,493 cycles

WHILE WORKING ON THE L/W UPPER SKIN CORROSION AT THE FRONT SPAR WING LBL 348, FOUND THE TEE CLIP COMMON TO THE UPPER SPAR CHORD AND WSTA 410 RIB FD STIFFENER CORRODED. REMOVED AND REPLACED TEE CLIP AT L/W STA 410 IAW SRM 51-30-5, 561-30-6, 51-30-2.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,783 hrs · 40,493 cycles

FRAME FLANGE DENTED STA 660 STR 23L - 25L. DENT ON FRAME FLANGE BS 660 STR 23L - 25L FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE OF FRAME LOCATED DRILLED NEW FRAME SECTION ALODINED, PRIMED AND INSTALLED SRM 53-10-1, SRM 51-40-3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,783 hrs · 40,493 cycles

OUTER CHORD OF FRAME CRACKED STA 804.5 STR 14R. REMOVED AND REPLACED OUTER CHORD OF FRAME 804.5 STR 14R IAW SRM 51-30-5, 51-30-2.

Part: STIFFENER — CORRODED (LT WING) · airframe 52,783 hrs · 40,493 cycles

WHILE WORKING ON THE L/W UPPER SKIN CORROSION AT THE FRONT SPAR WING LBL 348, FOUND THE TEE CLIP COMMON TO THE UPPER SPAR CHORD AND WSTA 357 RIB FWD STIFFENER CRACKED. REMOVED AND REPLACED TEE CLIP AT L/W STE 357 IAW SRM 51-30-5, 51-30-6, 51-30-2.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,783 hrs · 40,493 cycles

FOUND STR 16L IS CRACKED AT BS 644. REMOVED DAMAGED AREA, LOCATED AND DRILLED REPAIR PARTS AND INSTALLED IAW SRM 53-10-3.

Part: SKIN — DAMAGED (E/E BAY DOOR) · airframe 52,783 hrs · 40,493 cycles

E/E BAY DOOR OUTER SKIN DAMAGED ALL AROUND OUTER EDGE, AFT LT, OUT OF LIMITS. REMOVED AN AREA APX 3" BY 16" FROM AFT LT EDGE SKIN OF E/E BAY DOOR. FABRICATED FILLER FROM 2024-T3 .040, LOT 707522 AND PATCH FROM 2024-T3, 050, LOT NR 715012 PER SRM 52-00-3, FIG 1. ALODINED AND PRIMED PER SRM 51-10-2, INSTALLED PER SRM 51-30-2.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,783 hrs · 40,493 cycles

FOUND CORROSION ON CREASE BEAM WEB BS 720D - BS 720E, STR 17L. REMOVED DAMAGED CREASE BEAM WEB BS 720D-720E, STR 17L AND REPAIRED IAW SRM 51-10-2.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,783 hrs · 40,493 cycles

FOUND CORROSION C53-111-01, ON FRAME SHEAR TIE STA 720A BETWEEN STR 27L - 28L. REMOVED SHEAR TIE FABRICATED NEW SHEAR TIE ALODINIED AND PAINTED PARTS INSTALLED WET WITH SEALANT PER SRM 51-10-1, SRM 53-10-4, SRM 51-30-2, SRM 51-20-4 AT STA 720A BETWEEN STR 27L - 28L.

Part: FLOORBEAM — DAMAGED (BS 720F) · airframe 52,783 hrs · 40,493 cycles

WHILE WORKING N01184 , FOUND TOP CHORD OF FLOORBEAM TO BE MISDRILLED AT BS 720F, LBL 63, WL 208. ACCESSED CREASE BEAM STIFFNER, SEAT TRACK BS 720B TO 740 LBL 25 - LBL 65 AND FLOORBEAM WEB IAW SRM 51-30-2 AND REINSTALLED UPON COMPLETION OF REPAIR IAW SRM 51-30-2. CUT OUT DAMAGE SECTION OF FLOOR BEAM, FABRICATED REPAIR PARTS AND INSTALLED IAW FED EX DWG SR27-53-034 REINSTALLATION OF CREASE BEAM ACCOMPLISHED ON CUST CARD N01409 THIS IS A MAJOR REPAIR.

Part: FRAME — MISREPAIRED (BS 950F) · airframe 52,783 hrs · 40,493 cycles

LT INTERIOR FUSELAGE, FRAME REPAIR STA 950F, STRINGER 5L, REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF THE REPAIR IS IN ACCORDANCE WITH FAA, APPROVED DATA. EVALUATED REPAIR ON FRAME BS 750F STR 5L REPAIR DOES NOT COMPLY WITH FAA APPROVED DATA. REPAIRED PER SRM 53-10-4 FIG 1 FAA APPROVED DATA. THIS IS A MAJOR REPAIR.

Part: FRAME — DENTED (BS 520) · airframe 52,783 hrs · 40,493 cycles

FOUND DENT ON FRAME AT BS 520 STR 126R.

Part: SKIN — CORRODED (BS 760) · airframe 52,783 hrs · 40,493 cycles

FOUND WING UPPER CENTER SKIN AT STA 760 , RBL 45-51, WL 204 CORRODED. REPAIRED PER FED EX EA 7-5710-100612.

Part: SKIN — GOUGED (BS 538 S25R) · airframe 52,783 hrs · 40,493 cycles

WHILE WORKING CUSTOMER CARD NR N00224, FOUND OUT OF LIMITS GOUGE IN EXTERIOR SKIN BS 538 1.5 INCH BELOW STR 25 RT. REMOVED DAMAGE IN EXTERNAL SKIN BS 538 BELOW STR 25R AND REPAIRED IAW SRM 53-30-3 FIG 1.

Part: SKIN — CORRODED (WING) · airframe 52,783 hrs · 40,493 cycles

CORROSION ON WING LOWER SKIN SURFACE, AT NR 2 AFT FLAP TRACK MOUNT. REMOVED CORROSION ON WING LWR SURFACE AT NR 2 FLAP TRACK MOUNT AND REPAIRED IAW FED EX EA 7-5710-100598.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 52,783 hrs · 40,493 cycles

NR 2 FLAP TRACK, AFT MOUNT HOLE IS CORRODED. REMOVED AND REPLACED NR 2 FLAP TRACK IAW FED EX W/C 27X5706-03.

Part: CREASE BEAM — CORRODED (BS 720E-720F) · airframe 52,783 hrs · 40,493 cycles

FOUND CORROSION ON CREASE BEAM WEB BS 720E PLUS 2" TO 720F LBL 65 TO 70. REMOVED AND REPLACED CREASE BEAM WEB STA 720E TO 720F LBL 65 TO 70 PER SRM 51-30- 2, 51-30-5, 51-30-6, 51-10-2 AND MM 51-20-151-7.

Part: FRAME — DAMAGED (BS 580) · airframe 52,783 hrs · 40,493 cycles

FOUND FWD CARGO COMPARTMENT, DAMAGE TO STA 580 FRAME BETWEEN STR 22L AND 25L. REMOVED DAMAGE ON FRAME BS 580 STR 22L TO 25L AND REPAIRED IAW SRM 53-10-1, 51-40-3.

Part: FLOORBEAM — CORRODED (BS 1110) · airframe 52,783 hrs · 40,493 cycles

FOUND CORROSION ON BS 1110 FLOORBEAM UPPER FLANGE LBL 6-23 WL 208. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND REPAIRED IAW SRM 53-10-8 FIG 5.

Part: STRUCTURE — MISINSTALLED (BS 1176) · airframe 52,783 hrs · 40,493 cycles

MISDRILLED HOLE ON REINFORCEMENT CHORD BS 1176 RBL 23 WL 208. REMOVED AND REPLACED BS 1176 REINFORCEMENT CHORD FROM LBL 65 TO RBL 65, WL 208 PER SRM 51-30-2, 53-10-1.

Part: FRAME — DAMAGED (BS 930) · airframe 52,783 hrs · 40,493 cycles

L/H INTERIOR FUSELAGE, FRAME REPAIR STA. 930 STRINGER 5L, REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF THE REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA. REPAIRED FRAME AT BS 930, STR 5L PER SRM 51-40-3.

Part: FRAME — DAMAGED (BS 560 S22-25L) · airframe 52,783 hrs · 40,493 cycles

FWD CARGO COMPARTMENT, DAMAGE TO STA 560 FRAME BETWEEN STR 22L AND 25L. REPAIRED FRAME IAW SRM 51-40-3.

Part: FLOORBEAM — CORRODED (BS 1110) · airframe 52,783 hrs · 40,493 cycles

FOUND CORROSION ON BS 1110 FLOORBEAM LOWER FLANGE AT NUT PLATE HOLE LBL 40 WL 200. REPAIRED BS 1110 FLOORBEAM AT LBL 40, WL 200 PER SRM 53-10-8 FIG 8.

Part: SKIN — DELAMINATED (AIR STAIR) · airframe 52,783 hrs · 40,493 cycles

AFT AIR STAIRS, EXTERIOR SKIN AFT RT CORNER BENT AND DELAMINATING. REPAIRED EXTERIOR SKIN AT RT CORNER OF AFT AIRSTAIR PER SRM 51-40-2.

Part: STRINGER CLIP — CRACKED (BS 420 S3R) · airframe 52,783 hrs · 40,493 cycles

FOUND CRACKED STR CLIP AT BS 420 STR 3R. REMOVED & REPLACED CRACKED STR CLIP AT BS 420 STR 3R PER SRM 51-30-2.

Part: STRINGER CLIP — CRACKED (BS 720B S16R) · airframe 52,783 hrs · 40,493 cycles

FOUND CRACKED STR CLIP AT BS 720B STR 16R. REMOVED & REPLACED CRACKED STR CLIP AT BS 720B STR 16R IAW SRM 51-30-2.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 52,783 hrs · 40,493 cycles

FOUND CRACK IN NR 3 DOOR FWD FRAME ABOVE LOWER CROSS BEAM IN THE RADIUS. REPLACED DOOR NR 3 PER MM 52-35-051-4.

Part: STRINGER CLIP — CRACKED (BS 680 S9R) · airframe 52,783 hrs · 40,493 cycles

FOUND CRACKED STR CLIP AT BS 680 STR 9R. REMOVED & REPLACED CRACKED STR CLIP AT BS 680 STR 9 RT IAW SRM 51-30-2.

Part: STRINGER CLIP — CRACKED (BS 680 S9R) · airframe 52,783 hrs · 40,493 cycles

FOUND CRACKED STR CLIP AT BS 680 STR 9R. REMOVED & REPLACED STR CLIP AT BS 680 STR 9RT IAW SRM 51-30-2.

Part: STRINGER CLIP — BENT (BS 680 S2L) · airframe 52,783 hrs · 40,493 cycles

FOUND BENT STR CLIP AT BS 680 STR 2L. REMOVED & REPLACED BENT STR CLIP AT BS 680 STR 2L IAW SRM 51-30-2.

Part: LINK — CORRODED (BS 740-760) · airframe 52,783 hrs · 40,493 cycles

EXPANSION LINK, BS 740-760, BL 0, CORRODED AROUND FWD ATTACH BOLT. REMOVED AND REPLACED EXPANSION LINK PER SRM 51-30-2.

Part: STRINGER CLIP — CRACKED (BS 848 S4L) · airframe 52,783 hrs · 40,493 cycles

FOUND STRINGER CLIP CRACKED STA 848.95 STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2, 51-30-5.

Part: STRINGER CLIP — CRACKED (BS 783 S4L) · airframe 52,783 hrs · 40,493 cycles

FOUND STRINGER CLIP CRACKED STA 783.95 STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2, 51-30-5.

Part: STRINGER CLIP — CRACKED (BS 783 S5L) · airframe 52,783 hrs · 40,493 cycles

FOUND STRINGER CLIP CRACKED STA 783.95 STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2, 51-30-5.

Part: FLOORBEAM — CORRODED (BS 312) · airframe 52,783 hrs · 40,493 cycles

FOUND CORROSION ON FLOORBEAM UPPER TEE BS 312 LBL 4. REPARIED BS 312 FLOORBEAM AT LBL 4 PER SRM 53-10-8.

Part: STRINGER CLIP — CRACKED (BS 804 S5L) · airframe 52,783 hrs · 40,493 cycles

STRINGER CLIP CRACKED STA 804.5 STR 5L . REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2, 51-30-5.

Part: FLOORBEAM — CORRODED (BS 760-848) · airframe 52,783 hrs · 40,493 cycles

FOUND CORROSION ON LONGITUDINAL FLOORBEAM AROUND NUTPLATE HOLES, LBL 25, BS 760 THROUGH 848, WL 208. REPLACED LONGITUDINAL FLOOR BEAM IAW SRM 53-10-1, 51-30-5 AND 51-30-2.

Part: FLOORBEAM — CORRODED (BS 782) · airframe 52,783 hrs · 40,493 cycles

FOUND LONGITUDINAL FLOORBEAM CORRODED AT NUTPLATE HOLE, RBL 45, BS 782, WL 208. LONGITUDINAL FLOORBEAM WAS REPLACED ON N01170.

Part: FLOORBEAM — CORRODED (BS 832-848) · airframe 52,783 hrs · 40,493 cycles

FOUND LONGITUDINAL FLOORBEAM CORRODED AT NUTPLATE HOLES, RBL 45, BS 823 - 848, WL 208. FOUND CORROSION OUT OF LIMITS ON FLOOR BEAM IAW SRM 53-10-1 FIG 8 AND SRM 51-10-6. REMOVED AND REPLACED BEAM IAW SRM 51-30-2 AND SRM 51-30-5.

Part: STRINGER — GOUGED (BS 565 S1) · airframe 52,783 hrs · 40,493 cycles

GOUGE ON STR 1 BS 565. REPAIRED STRINGER 1 AT BS 565 PER SRM 53-10-3 FIG 3.

Part: STRINGER — GOUGED (BS 565 S1) · airframe 52,783 hrs · 40,493 cycles

FOUND GOUGE ON STR 1 BS 565. REPAIRED STRINGER 1 AT BS 565 PER SRM 53-10-3 FIG 3.

Part: FLOORBEAM — CORRODED (BS 680) · airframe 52,783 hrs · 40,493 cycles

FOUND CORROSION ON FLOORBEAM UPPER TEE AND LOWER SURFACE STA 680 RBL 3-21. REPAIRED FLOOR BEAM UPPER CHORD AT STA 680 PER SRM 53-10-8.

Part: FRAME — DENTED (BS 1030 S25-26R) · airframe 52,783 hrs · 40,493 cycles

FOUND AFT CARGO BAY DENT ON FRAME AT BS 1030 BETWEEN STR 25R AND STR 26R. REMOVED DAMAGE, FABRICATED DOUBLER AND INSTALLED PER SRM 51-40-3.

Part: FRAME — DENTED (BS 1110 S25-26L) · airframe 52,783 hrs · 40,493 cycles

FOUND AFT CARGO BAY DENT ON FRAME AT BS 1110 BETWEEN STR 25L AND STR 26L. REPAIRED FRAME AT BS 1110 BETWEEN STR 25L AND STR 26L PER SRM 51-40-3.

Part: FRAME — DENTED (BS 990 S25-26L) · airframe 52,783 hrs · 40,493 cycles

AFT CARGO BAY DENT ON FRAME AT BS 990 BETWEEN STR 25L AND STR 26L. REPAIRED FRAME BS 990 BETWEEN STR 25L - 26L PER SRM 51-40-3.

Part: FRAME — DENTED (BS 1050 S23R) · airframe 52,783 hrs · 40,493 cycles

FOUND DENT AFT CARGO BAY ON FRAME AT BS 1050 STR 23R. REMOVED DAMAGE REPAIREDWITH FASTENER PER SRM 53-10-1, SRM 51-30-2.

Part: FRAME — DENTED (BS 950D S25L) · airframe 52,783 hrs · 40,493 cycles

FOUND AFT CARGO BAY DENT ON FRAME AT BS 950D STR 25L. REMOVED DAMAGE ON FRAME BS 950F STR 26L AND REPAIRED IAW SRM 53-10-1, 51-40-3.

Part: FRAME — DENTED (BS 1070 S25R) · airframe 52,783 hrs · 40,493 cycles

FOUND AFT CARGO BAY DENT ON FRAME AT BS 1070 BETWEEN STR 25R. REMOVED DAMAGE ON FRAME BS 1070 AT STR 25R AND REPAIRED IAW SRM 51-40-3

Part: FRAME — DENTED (BS 950B) · airframe 52,783 hrs · 40,493 cycles

FOUND AFT CARGO BAY DENT ON FRAME AT BS 950B STR 26R. REPARIED FRAME AT BS 950B, STR 26R PER SRM 51-40-3.

Part: FRAME — DENTED (BS 1050 S25-26L) · airframe 52,783 hrs · 40,493 cycles

AFT CARGO BAY DENT ON FRAME AT BS 1050 BETWEEN STR 25L AND STR 26L. REMOVED DAMAGE ON FRAME AFT CARGO BAY BS 1050 BETWEEN STR 25L AND 26L AND REPAIRED IAW SRM 51-30-5, 51-40-3.

Part: CONNECTOR — DAMAGED (COCKPIT) · airframe 52,302 hrs · 40,090 cycles

HAD OVER VOLTAGE SYS 1 UNDER VOLTS SYS 1, OVER EXCITED SYS 1, UNDEREXCITED SYS 1, IF EXTINGUISH LIGHTS, WARNING LIGHTS PANEL WILL NOT OPERATE CORRECTLY. ONLY APU AND APU BLEED LIGHTS WILL TEST. INSPECTED NR 1 GCU FOUND ELECTRICAL RECEPTACLE AND GCU PINS BURNT. UPON INSPECTION AS TO THE ROOT CAUSE OF THIS DISCREPANCY. MX DISCOVERED SMOKE IN THE E/E COMPARTMENT DUE TO THE GCU BOX BEING FRIED. AUXILIARY GENERATOR PANEL TEST AND RESET CHECKS GOOD.

Part: ENGINE — FAILED (NR 3) · airframe 51,805 hrs · 39,661 cycles

DURING CLIMBOUT S/O NOTICED RT MANIFOLD DROP TO ZERO. THIS WAS FOLLOWED BY NR 3 STRUT OVERHEAT LIGHT & ACRID SMELL. FOLLOWED QRH TO NR 3 ENGINE SHUTDOWN & EMERGENCY RETURN TO ONT. 20 MIN ENGINE WINDMILLING. STRUT EXTINGUISHED AFTER ABOUT 3 MINUTES. (OPEN)

Part: POWER UNIT — LEAKING (T/E FLAP) · airframe 51,634 hrs · 39,519 cycles

DURING FLAP RETRACTION INDICATORS SHOWED SPLIT FLAP W/INBOARDS REMAINING AT 2 DEG W/FLAP UP. AFTER RUNNING QRH AND INBOARDS GOING TO FULL UP, HYD A SYSTEM INDICATED 0 QTY. RAN QRH AGAIN W/ALTERNATE FLAPS SYSTEM AND MANUAL GEAR EXTENSION PROCEDURES. WHEN ARRIVING AT A/C NOTICED HYD FLUID COMING FROM LT WHEEL-WELL AREA, OPENED GEAR DOORS AND FLAP DRIVE MOTOR WAS DUMPING FLUID. REMOVED AND REPLACED FLAP POWER UNIT HYDRAULIC MOTOR IN ACCORDANCE WITH 727-200 MM REF NR 27-51-062-4. SERVICED HYDRO, CYCLED FLAPS SEVERAL TIMES AND INDICATIONS FOLLOWED CORRECTLY. OPS CHK GOOD. NO LEAKS NOTED.

Part: BRACKET — GOUGED (SPOILER) · airframe 50,770 hrs · 38,870 cycles

WINGS - SPOILERS - SPOILER DOWN STOP BRACKET GOUGE REPAIR. COMPLIED WITH EA 7-5740-77411. BLENDED GOUGE, HFEC NO CRACKS NOTED.

Part: RIB — DAMAGED (WING) · airframe 50,770 hrs · 38,870 cycles

COMPLY WITH EA 7-5720-77412 WING - SPOILER DOWN STOP RIB REPAIR. COMPLIED WITH EA 7-5720-77412. WORKED IN CONJUNCTION WITH EA 7-5720-77423.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,770 hrs · 38,870 cycles

FWD PIT - STA 715 FLOOR SUPPORT R3 - EXFOLIATED AT NUT PLATE HOLES. FABRICATED NEW FLOOR SUPPORT IAW SRM 51-40-4, INSTALLED IAW SRM 51-30-2, ON NON ROUTINE N00637 AT MAE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,770 hrs · 38,870 cycles

AFT CARGO COMPT HAS A CORRODED SHEAR TIE AT FS 970 STR 28L - 29L. FABRICATED SHEAR TIE ON TRAVELER T4/432278 & FABRICATED FLOOR SUPPORT ON TRAVELER T4/430988. REPAIRED & INSTALLED SHEAR TIE AT FS 970 STR 28L - 29L IAW SRM B727 SRM 53-10-4 PAGE 46.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,770 hrs · 38,870 cycles

FWD PIT - STA 715 - FLOOR SUPPORT L2 EXFOLIATED AT NUT PLATE HOLES. FABBED NEW FLOOR SUPPORT ON TRAVELER T4/430748 & INSTALLED REPAIR IAW SRM 51-40-4 AND 51-30-2, ON NON ROUTINE N00641 AT MAE.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,770 hrs · 38,870 cycles

RIGHT MLG W/W - CRACK IN STR 18 AT APPROX STA 908. STOP DRILLED CRACK AS PER SRM 53-10-1 FIG 1. FABRICATED REPAIR ANGLES ON MAE TRAVELER T4/428590. INSTALLED REPAIR ANGLES IAW SRM 51-30-2, ON NON ROUTINE N00097.

Part: SUPPORT ANGLE — CRACKED (NR 5 SPOILER) · airframe 50,770 hrs · 38,870 cycles

NR 5 SPOILER ACTUATOR I/B SUPPORT ANGLE HAS A CRACK. REMOVED AND REPLACED NR 5 SPOILER ACTUATOR I/B SUPPORT ANGLE IAW SRM 51-30-2, ON NON ROUTINE N00606.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,770 hrs · 38,870 cycles

FWD PIT - STA 720E - 720F, STR 27L EXFOLIATED. CUT OUT STRINGER DAMAGE IAW SRM 53-10-3 FIG 1, FABRICATED NEW SECTION STRINGER & REPAIR SPLICES FROM MAT BAC 1498-147, BATCH 32659 & BAC 1498-131 BATCH 54832 IAW SRM 53-10-3. INSTALLED STRINGER & SPLICES IAW SRM 53-10-3 FIG 1.

Part: TRANSITION PANEL — CORRODED (CARGO BAY) · airframe 50,770 hrs · 38,870 cycles

FWD PIT - LT TRANS PANEL STR 675 - 2 NUT PLATE HOLES EXFOLIATED. REMOVED & REPLACED TRANS ANGLE IAW SRM 51-30-2. ORIGINAL TRANS ANGLE .050. REMOVED .050 IAW SRM 51-10-6. REMAINING .000 OUT OF LIMITS IAW SRM 53-10-1 FIG 1 PG 2. FABRICATED NEW TRANS ANGLE FROM 7075-T6 .050C BATCH 8R00071001 IAW SRM 51-20-1 AND SRM 51-30-5. TREATED AND PRIMED BARE METAL IAW SRM 51-10-2.

Part: HINGE — WORN (MAIN CARGO DOOR) · airframe 50,770 hrs · 38,870 cycles

COMPLY WITH EA 7-5210-77407; DOORS - MAIN CARGO DOOR HINGE WEAR REPAIR P/N B27-53-070-03. COMPLIED WITH EA 7-5210-77407. MAIN CARGO DOOR HINGE REPAIR P/N B27-53-070-03.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 50,770 hrs · 38,870 cycles

AFT CARGO COMPT FS 1147 - 1164 STR 27L - STR 28L INTERCOSTAL HAS LIGHT CORROSION AND MISSING NUT PLATES ON LWR SURFACE OF CHORD. REMOVED CORROSION IAW SRM 51-10-6, OUT OF LIMITS IAW SRM 53-10-1, REMOVED ANGLE IAW SRM 51-30-2. FABRICATED NEW ANGLE IAW SRM 51-20-1, MATERIAL ID 04091 7075-T6 .050C BATCH 8R00071001. INSTALLED NEW ANGLE IAW SRM 51-30-2. INSTALLED NUT PLATES IAW SRM 51-30-2.

Part: CLIP — CORRODED (FUSELAGE) · airframe 50,770 hrs · 38,870 cycles

FWD PIT - STA 720D, FRAME FOR BULKHEAD PANEL, BOTTOM SIDE CLIP CORRODED RBL 4. REMOVED CLIP IAW SRM 51-30-2, FABRICATED NEW CLIP IAW SRM 51-20-1, MAE MATERIAL ID 04074,7075-T6 .032 BATCH 671070, INSTALLED NEW CLIP IAW SRM 51-30-2, AT MAE.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 50,770 hrs · 38,870 cycles

RIGHT MLG DOOR FORWARD HINGE SEAL SUPPORT THE AFT BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET, FABBED FROM 2024-T3 .040 BATCH 744347 AT MAE ON N/R N00389.

Part: SWITCH — FAULTY (RT MLG) · airframe 49,268 hrs · 37,734 cycles

DURING GEAR RETRACTION DURING TAKEOFF A RED DOOR WARNING LIGHT ON THE GEAR WARNING PANEL AND ASSOCIATED RIGHT GEAR DOOR LIGHT ON SECOND OFFICERS PANEL ILLUMINATED AFTER PLACING THE GEAR HANDLE TO THE OFF POSITION. QRH WAS REFERENCED. LIGHT WENT OUT AFTER PLACING HANDLE TO UP POSITION. REMOVED AND REPLACED THE RT GEAR DOOR WARNING SWITCH PER M/M 32-62 011-4. ACCOMPLISHED GEAR SWING OPS CK NORMAL FOR SERVICE.

Part: SWITCH — FAULTY (COCKPIT) · airframe 49,181 hrs · 37,670 cycles

DURING INITIAL TAKEOFF, AS FLAPS WERE BROUGHT FROM 5' TO 2' THE L/E FLAP INDICATOR REMAINED AMBER (DID NOT SHOW GREEN). L/E FLAPS POSITION TEST ON S/O PANEL INDICATED 2, 3, 5, 6 & 7 STILL EXTENDED (IN GREEN). QRH (RED TABS) PROCEDURE ACCOMPLISHED. UNEVENTFUL LANDING BACK AT SAN. PILOTS REPORTED NO ABNORMAL ROLLING TENDENCIES DURING ENTIRE FLIGHT. CYCLED L/E TEST SWITCH S1010. NR 5 SLAT INDICATION, OPS CHECKS OK. RAN L/E DEVICES SEVERAL TIMES. ALL CHECKS OK PER M/M 27-82-011-4.

Part: RIB — CRACKED (L/E SLAT) · airframe 48,659 hrs · 37,249 cycles

NR 3 SLAT INBD RIB CRACKED. R&R RIB PER SRM 57-50-3.

Part: RIB — CRACKED (RIGHT WING)

N 241 #7 SLAT OUTBD RIB CRACKED. R&R RIB PER SRM 57-50-3.

Part: STEP — CRACKED (AIRSTAIRS) · airframe 48,659 hrs · 37,249 cycles

TOP AIRSTAIR STEP CRACKED AT BS 1183-1190. R&R STEP PER SRM 51-10-1.

Part: RIB — CRACKED (AILERON) · airframe 48,659 hrs · 37,249 cycles

LEFT WING OUTBOARD AILERON NR 5 RIB CRACKED. REMOVED AND REPLACED AILERON PER MM 27-10-031-2.

Part: RIB — CRACKED (RT WING) · airframe 48,659 hrs · 37,249 cycles

RT WING LEAD EDGE RIB CRACKED WS 510, WBL 415. R&R RIB PER SRM 51-40-2.

Part: RIB — CRACKED (LEFT WING) · airframe 48,659 hrs · 37,249 cycles

N 567 LEFT WING OUTBOARD AILERON #6 RIB CRACKED. R&R AILERON PER MM 27-10-031-2.

Part: BRACKET — CRACKED (FUSELAGE LOWER) · airframe 48,659 hrs · 37,249 cycles

N 1391 BRACKET CRACKED UNDER #4 CARGO TRACK AT BS 950A, BL0, WL 207. R&R BRACKET PER SRM 51-30-2.

Part: TIE CLIP — CRACKED (FUSELAGE TOP) · airframe 48,659 hrs · 37,249 cycles

N 945 STRINGER TIE CLIP CRACKED AT BS 950E, STR 6R. R&R CLIP PER SRM 51-30-2.

Part: FLOORBEAM — CORRODED (FUSELAGE TOP) · airframe 48,659 hrs · 37,249 cycles

N 1289 UPPER CHORD OF FLOORBEAM CORRODED AT BS 340, RBL 2-8, WL 208.1. R&R FLOORBEAM PER SRM 53-10-8.

Part: GUSSET — CRACKED (FUSELAGE LOWER) · airframe 48,659 hrs · 37,249 cycles

N 1361 GUSSET CRACKED AT BS 950F, RBL 20, WL 146. R&R GUSSET PER SRM 51-40-3.

Part: ANGLE — CORRODED (FUSELAGE TOP) · airframe 48,659 hrs · 37,249 cycles

N 1089 "Z" ANGLE CORRODED AT BS 340, RBL 18-40. R&R ANGLE PER SRM 51-30-2.

Part: STEP — CRACKED (FUSELAGE LOWER) · airframe 48,659 hrs · 37,249 cycles

N 284 AIRSTAIRS STEP #12 CRACKED AT BS 1293-1303, RBL 14.25 TO LBL 14.25. R&R STEP PER SRM 51-10-1.

Part: STEP — CORRODED (FUSELAGE LOWER) · airframe 48,659 hrs · 37,249 cycles

N 282 AIRSTAIRS STEP #11 CORRODED BS 1283-1293, RBL 14.25-LBL 14.25. R&R STEP PER SRM 51-10-1.

Part: TRACK — CORRODED (FUSELAGE TOP)

N 1390 #2 CARGO TRACK CORRODED BS 340-380, LBL 45.5, WL 210. R&R TRACK PER SRM 53-10-5.

Part: FLOORBEAM — CORRODED (FUSELAGE TOP) · airframe 48,659 hrs · 37,249 cycles

N 1288 UPPER CHORD OF FLOORBEAM CORRODED BS 340, RBL 40-55, WL 208.1. R&R FLOORBEAM PER SRM 53-10-8.

Part: SKIN — CORRODED (FUSELAGE LOWER) · airframe 48,659 hrs · 37,249 cycles

N 906 CORROSION ON FUSELAGE SKIN AT BS 720D, STR 27R. R&R SKIN PER SRM 53-30-3.

Part: STEP — CRACKED (FUSELAGE LOWER) · airframe 48,659 hrs · 37,249 cycles

N 280 AIRSTAIRS STEP #4 CRACKED BS 1203-1213, RBL 14.25-LBL 14.25. R&R STEP PER SRM 51-10-1.

Part: TRACK — CORRODED (FUSELAGE TOP) · airframe 48,659 hrs · 37,249 cycles

N 1320 #6 CARGO TRACK CORRODED AND GOUGED BS 560-660, RBL 45.5. R&R TRACK PER SRM 53-10-5.

Part: STEP — CRACKED (FUSELAGE LOWER) · airframe 48,659 hrs · 37,249 cycles

N 281 AIRSTAIRS STEP #10 CRACKED AT BS 1273-1283, RBL 14.25-LBL 14.25. R&R STEP PER SRM 51-10-1.

Part: CLIP — CRACKED (FUSELAGE TOP) · airframe 48,659 hrs · 37,249 cycles

N 946 STRINGER TIE CLIP CRACKED BS 970, STR 4L. R&R CLIP PER SRM 51-30-2.

Part: TIE CLIP — CRACKED (FUSELAGE TOP) · airframe 48,659 hrs · 37,249 cycles

N 947 STRINGER TIE CLIP CRACKED AT BS 1070, STR 5L. R&R CLIP PER SRM 51-30-2.

Part: STEP — CORRODED (FUSELAGE LOWER) · airframe 48,659 hrs · 37,249 cycles

N 285 AIRSTAIRS STEP #13 CORRODED AT BS 1303-1313, RBL 14.25 TO LBL 14.25. R&R STEP PER SRM 51-10-1.

Part: TRACK — CORRODED (FUSELAGE TOP) · airframe 48,659 hrs · 37,249 cycles

N 1438 CORROSION ON #2 CARGO TRACK BS 480, LBL 45.5, WL 210. R&R PER SRM 53-10-5.

Part: BRACKET — CRACKED (FUSELAGE LOWER) · airframe 48,659 hrs · 37,249 cycles

N 311 SUPPORT BRACKET CRACKED FOR FUSELAGE FAIRING BS 720E, STR 28L. ** S/D ** COMING

Part: ANGLE — CRACKED (FUSELAGE LOWER)

N 730 FLOOR TO BULKHEAD ANGLE CRACKED AT BS 480, RBL 18, STR 27R. R&R ANGLE PER SRM 51-30-2.

Part: SKIN — CORRODED (FUSELAGE LOWER) · airframe 48,659 hrs · 37,249 cycles

N 87 CORROSION & CRACK IN LOWER SKIN AT BS 727C, STR 27R. R&R SKIN PER SRM 53-30-3 & STR PER SRM 53-10-3.

Part: CYLINDER — CRACKED (LAND GEAR) · airframe 48,659 hrs · 37,249 cycles

N 491 CHICKEN WIRE CRACKS ON CHROME OF RMG INNER CYLINDER. R&R PER E.A. 7-3210-60399.

Part: GUSSET — CRACKED (FUSELAGE LOWER)

N 733 FLOOR SUPPORT GUSSET CRACKED BS 480, STR 28L. R&R GUSSET PER SRM 51-30-2.

Part: INDICATOR — FROZEN (ALTIMETER)

00-337 AT ROTATION 1XT OFF AIRSPEED DROPPED TO 0 ALT FROZE & VSI CENTERED. ** S/D ** COMING

Part: ENGINE — SPARKS (RIGHT)

ATA: 05-50 98-0098, AFTER TAKEOFF FROM PHL 9L- TOWER REPORTED THAT SEVERAL AIRCRAFT SAW SPARKS FROM RIGHT SIDE OF AIRCRAFT. RETURNED TO PHL FOR INSPECTION. ALL AIRCRAFT SYSTEMS NORMAL, ENGINE PARAMETERS NORMAL, NO PRESSURE PROBLEMS. INSPECTED ALL 3 ENGINE INLETS AND EXHAUSTS NO DEFECTS FOUND. INSPECTED AIRCRAFT AND GEAR ALL CHECKS GOOD. OK FOR SERVICE.

Part: OIL TEMP BULB — INOPERATIVE (NR 3 ENGINE)

NR 3 OIL TEMPERATURE GAUGE INOPERATIVE. NEEDLE HANGS STRAIGHT DOWN TWITCHES OCCASIONALLY. REMOVED AND REPLACED NR 3 OIL TEMPERATURE BULB PER MAINTENANCE MANUAL 79-32-01.

Part: SWITCH — INOPERATIVE (RT MLG)

ON GEAR RETRACTION ENGINEERS PANEL DID NOT INDICATE AN AMBER RIGHT GEAR DOOR LIGHT DURING SEQUENCE. LANDING GEAR FRONT PANEL SHOWED CORRECT LIGHT SEQUENCE AND EXTINGUISHED RED LIGHT GEAR DOOR LIGHT. MAKING SURE RIGHT GEAR DOORS WERE UP. THE LANDING GEAR WAS EXTENDED AND RETRACTED WITH THE SAME RESULTS, NO AMBER RIGHT GEAR DOOR LIGHT ON FLIGHT ENGINEER'S PANEL. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOOR SWITCH PER MAINTENANCE MANUAL 727-200 32-62-11. SYSTEM CHECKS GOOD OK FOR SERVICE.

Part: BEAM — CORRODED (NR 4 FLAP TRACK)

NR 0673 011, CORROSION IN I/B HOLE IN GEAR BEAM FOR NR 4 FLAP TRACK ATTACH. REMOVED CORROSION, EDDY CHECKED HOLE, INSTALLED BUSHING PER EA 7-5710-28983 DATED 2/10/97.

Part: STRINGER — CRACKED (BS 720)

NR 0693 009, ICE LIGHT RT SIDE STA 720B FWD STRINGER END CRACKED. INSTALLED NEW SECTION OF STRINGER AT STA 720B, STR 15R FWD OF LIGHT PER SRM 53-10-3.

Part: BEAM — CORRODED (NR 4 FLAP TRACK)

NR 0674 12, CORROSION IN GEAR BEAM AT O/B BOLT HOLE NR 4 FLAP TRACK ATTACH HOLE. REMOVED CORROSION, EDDY CHECKED HOLE, INSTALLED NEW BUSHING AND SPECIAL WASHER PER EA 7-5710-28983 DATED 2/10/97.

Part: FLOORBEAM — CORRODED (BS 1070)

NR 0785 010, STA 1070 RBL 50, FLOORBEAM HAS CORROSION AROUND NUTCLIP HOLE. REPAIRED FLOORBEAM WITH DOUBLERS, CUTOUT DAMAGED AREA AND REPLACED WITH FILLER PER SRM 53-10-8.

Part: STRINGER — CRACKED (BS 720)

NR 0714 012, STR 15L CRACKED AT STA 720B AND 5, FWD OF EXTERIOR LIGHT HOUSING. INSTALLED STR U-CHANNEL REPAIR PER SRM 53-10-3.

Part: STRINGER — CRACKED (BS 460-480)

NR 0056 008, STR 21L HAS DOUBLE AND TRIPLE DRILLED HOLES IN SIDE OF STR BETWEEN STA 460 AND 480. REPAIRED STR 21L IAW SRM 53-10-3 FIG 1.

Part: SKIN — CORRODED (FUSELAGE)

NR 1078 005, LOWER FUSELAGE CORROSION ON AND AROUND ALL FASTENERS ON KEEL BEAM ABOVE BLOW OUT DOOR. CORROSION REMOVED, PUT THICKNESS OUT OF EXCEPTABLE LIMITS. REPAIRED DAMAGED AREA BY INSTALLING DOUBLER PER SRM 51-40-2.

Part: STRINGER — CRACKED (BS 720)

NR 0715 013 STR 15L IS CRACKED AT STA 720B AND 15, AFT OF EXTERIOR LIGHT FIXTURE. STOP DRILLED CRACK IAW SRM 51-10-01. REPAIRED STR 15L IAW SRM 53-10-3.

Part: SUPPORT — CORRODED (COCKPIT)

NR 1038 015, COCKPIT FLIGHT ENG'S SEAT AFT TRACK SUPPORT BEAM UNDER FLOOR PNL CORRODED. INSTALLED NEW SEAT TRACK SUPPORT BEAM PER SRM 51-10-1.

Part: FLOORBEAM — CORRODED (BS 1130)

NR 0782 011, STA 1130 RBL 60 FLOORBEAM HAS CORROSION AND PIECE OF FLOORBEAM GROUND OFF BELOW SEAT TRACK. REMOVED CORROSION, TREATED AND PRIMED AREA, INSTALLED ANGLE REPAIR PER EA 7-5310-28980 DATED 2-4-97.

Part: STRINGER — CRACKED (BS 620-640)

LOWER FWD CARGO STRINGER 25L CRACKED AND DAMAGED BETWEEN STA 620 TO 640. STOPPED DRILLED CRACKS AND ROUTED OUT DAMAGE. CONFIRMED BY DYE-PENETRANT INSPECTION. INSTALLED STRINGER U-CHANNEL REPAIR DOUBLER PER SRM 53-10-3.

Part: DOUBLER — CORRODED (BS 520-540)

NR 1068 006, LOWER FWD CARGO LEVELING COMPOUND IS RAISING UP O/B SIDE OF STR 27R STA 520 TO 540. CORROSION FOUND UNDER LEVELING COMPOUND. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. INSTALLED DOUBLER PER SRM 53-30-3.

Part: FLOORBEAM — CORRODED (BS 344)

NR 0379 001, UPPER LOBE STA 344 FLOORBEAM CORRODED AT CLIP NUTS HOLES, LBL 35 TO LBL 40. REMOVED CORRODED SECTION OF FLOORBEAM AND INSTALLED REPAIR PER DRAWING SR 27-53-007.

Part: STRINGER — CRACKED (BS 1040)

NR 0328 002, FUSE STRINGER 3L BENT AND CRACKED IN UPPER LEG AT FUSE STA 1040. CRACK LENGTH APPROX 0.312. STRAIGHTENED STRINGER AND STOP DRILLED ENDS OF CRACK, CONFIRMED BY DYE PENETRANT INSP. INSTALLED REPAIR DOUBLER TO STRINGER 3L UPPER LEG PER SRM 53-10-3.

Part: STIFFENER — CORRODED (FSS 260)

MCM - LT WING FRONT SPAR STIFFENER CORRODED AND EXFOLIATED UNDER HYD LINE CLAMP STANDOFFS. LOCATED JUST OUTBD OF BOOST PUMP PRESSURE SWITCHES APPROX. FRONT SPAR STA 260. REMOVED HYD LINES LT WING F.O.M. INSTALLED SPAR STIFFENER REF EA 7-5710-3813 REV A. CLOSED FUEL TANK, LEAK CK OK.