N286SC

Part: SKIN — DENTED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

(FOTR) DENT ON LT FUSELAGE SKIN BS 1319 STR 9L. REPAIRED ON FASI WO 20006. N/R 02095- R & R PREVIOUS REPAIR TO LT FUSELAGE SKIN AT STA 1319 STR 9L IAW SRM 53-30-3 FIG 1, REV 102. MATERIAL USED: 2024-T3, 0.063", DIM: 9.250" X 8.750".

Part: SKIN — DEBONDED (AILERON TAB) · airframe 57,864 hrs · 41,947 cycles

RT WING INBD AILERON TAB LOWER SURFACE DISBONDED 22 INCHES FROM OTBD END. REPAIRED ON FASI WO 20006, N/R 02059. REPAIRED RT WING INBD AILERON TAB AT WBL 280 BY HOT BONDING REPAIR IAW B727 SRM 51-40-20, REV 102. MATERIAL USED: FILLER- 2024-T3, 0.010, DIM: 4.0 BY 4.50, DOUBLER- 2024-T3, 0.010, DIM: 6.0 BY 7.50, CUT OUT DIM: 4.0 BY 4.50. WEIGHT OF TAB AFTER REPAIR IS 5.740 LBS, WITHIN LIMITS.

Part: STRUCTURE — CRACKED (RT WING TE FLAP) · airframe 57,864 hrs · 41,947 cycles

RT WING INBD MID FLAP LOWER T/E CHORD CRACKED WBL 100. REPAIRED ON FASI WO 20006, N/R 02054. REMOVED AND REPLACED RT WING INBD MID-FLAP LOWER T/E CHORD SECTION AT WS 100.0 IAW B727 SRM 51-30-5 AND 57-50-2, FIG 5, REV 102. MATERIAL USED: BAC1503-10046 7075-T-6, DIM: 29.0 LONG.

Part: SKIN — DEBONDED (NR 9 SPOILER) · airframe 57,864 hrs · 41,947 cycles

RT WING NR 9 SPOILER LOWER SURFACE HAS DISBONDED DOUBLER JUST AFT OF ACTUATOR ATTACH FITTING. REPAIRED ON FASI WO 20006, N/R 02033. REPAIRED RT WING NR 9 SPOILER LOWER SURFACE AT WBL 113 BY HOT BY 8.0.

Part: SKIN — PUNCTURED (ZONE 300) · airframe 57,864 hrs · 41,947 cycles

RT ELEVATOR LOWER SKIN WORN THRU AT ELEV STA 78 NEAR CENTER OF ELEVATOR. REPAIRED ON FASI WO 20006, N/R 02028. INSTALLED REPAIR DOUBLER ON RIGHT ELEVATOR LOWER SURFACE AT ELEV STA 78, IAW B727 SRM 55-20-3 FIG 4, REV 102. MATERIAL USED: 2024-T3, DIM; 4.325 BY 3.0 BY 0.032. NEW ELEVATOR MOMENT IS 120.9 IN LBS, IS WITHIN LIMIT IAW B727 SRM 51-80.

Part: SKIN — DEBONDED (AFT FLAP) · airframe 57,864 hrs · 41,947 cycles

LT INBD AFT FLAP LOWER SURFACE HAS DISBONDED AREA AT WBL 135. REPAIRED ON ASI WO 20006, N/R 02031. INSTALLED HOT BONDED REPAIR TO LEFT INBD AFT FLAP LOWER SURFACE AT WBL 135 IAW B727 SRM 51-40-20, PARA 20 AND 51-40-23, REV 102. MATERIAL USED: CORE; 5052-4.4-3/16, 2 DIA., DOUBLER; 7075-T6, 0.016 DIM.; 5 DIA.

Part: FRAME — DAMAGED (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

UPPER CABIN FRAME DAMAGED AT BS 380 STR 5L. REPAIRED ON FASI WO 20006. N/R 02027. INSTALLED REPAIR ANGLE TO FUSELAGE FRAME AT BS 380, STR 5L IAW B727 SRM 53-10-4 FIG 1, REV 102. MATERIAL USED; 7075-O, HEAT TREATED TO T-6 CONDITION. DIM.; 11 BY 1 BY 0.063.

Part: STRINGER CLIP — PUNCTURED (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

FRAME TO STR. BRACKET HAS HOLE IN RADIUS AT STA. 672 STR. 13L. REPAIRED ON FASI W/O NR 20006, N/R 02020- R & R SUPPORT ANGLE AT STA 672 STR 13L IAW SRM 51-30-2, REV 102 AND DWG AE4899 DATED 6/29/92.

Part: SKIN — DEBONDED (AILERON TAB) · airframe 57,864 hrs · 41,947 cycles

RT OTBD AILERON TAB, UPPER SURFACE INBD END HAS AREA OF DISBOND. REPAIRED ON FASI WO 20006. N/R 02023, INSTALLED HOT BONDED REPAIR TO RT OTBD AILERON TAB UPPER SURFACE AT INBD END IAW SRM 51-40-20 PARA 20, REV 102. MATERIAL USED: CORE; 5052-44-3/16 DIM. 13" X 3", DOUBLER; 2024-T3, DIM. 14.5" X 4.5" X 0.012". TAB WEIGHT IS 3.89LBS AFTER REPAIR, IS WITHIN LIMITS IAW SRM 51-80-0.

Part: SKIN — DELAMINATED (ZONE 600) · airframe 57,864 hrs · 41,947 cycles

RT WING OTBD AFT FLAP IS DELAMINATED AT STA WBL 338. REPAIRED ON FASI W/O NR 20006, N/R 2011 INSTALLED HOT BONDED REPAIR TO RT WING OTBD AFT FLAP AT WBL 228 IAW SRM 51-40-20 PARA 7 AND PARA 20 REV 102. MATERIAL USED: 7075-T7, 0.012". DIM ; FILLER; 1" X 4", DOUBLER; 2" X 6".

Part: SKIN — GOUGED (NR 4 SLAT) · airframe 57,864 hrs · 41,947 cycles

LT WING NR 4 SLAT OTBD END GOUGED. REPAIRED ON W/O NR 20006, N/R 02016- R & R LT WING NR4 SLAT OTBD RIB IAW SRM 51-30-2, REV 102 WITH PN 65-17286-13.

Part: SKIN — DELAMINATED (RT AILERON) · airframe 57,864 hrs · 41,947 cycles

RT OTBD AILERON T/E WEDGE HAS AREA OF DISBOND ON UPPER SURFACE. REPAIRED ON FASI W/O NR 20006, NR 02012 - INSTALLED HOT BONDED REPAIR TO RT WING OTBD AILERON T/E WEDGE UPPER SURFACE IAW SRM 51-40-20 PARA 8 AND PARA 20 REV 102. MATERIAL USED: 2024 T3, 0.012". DIM FILLER; 3" X 1", DOUBLER; 5" X 2". AILERON REBALANCE IAW SRM 51-80-4.

Part: SKIN — PUNCTURED (RT FORE FLAP) · airframe 57,864 hrs · 41,947 cycles

RT WING OTBD FORE FLAP HAS SEVERAL GOUGES. REPAIRED ON FASI W/0 NR 20006, N/R 02021" INSTALLED REPAIR DOUBLER TO RT WING OTBD FORE FLAP AT WS 465 IAW SRM 57-50-2 FIG 4 AND 57-50-4 FIG 1, REV 102. MATERIAL USED; 2024-T3, DIM.; 3.5" X 3.75" X 0.063".

Part: WEDGE — DELAMINATED (RT AILERON) · airframe 57,864 hrs · 41,947 cycles

RT AILERON OTBD T/E WEDGE HAS AREA OF DISBOND ON UPPER INBD END. REPAIRED ON FASI W/O NR 20006, N/R 02013. INSTALLED HOT BONDED REPAIR TO RIGHT WING OTBD AILERON TRAILING EDGE WEDGE UPPER OTBD END IAW B727 SRM 51-40-20 PARA. 8 AND PARA 20 REV 102. MATERIAL USED: 2024 T3, 0.012 DIM FILLER; 1 BY 1, DOUBLER; 2 BY 2. AILERON REBALANCE PER B727 SRM 51-80-4.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 57,864 hrs · 41,947 cycles

RT WING INBD FLAP LOWER SURFACE IS DENTED AT WS 135. REPAIRED ON FASI W/O 20006, N/R 01992, INSTALLED HOT BONDED REPAIR TO LOWER SURFACE OF RT INBD AFT FLAP AT WS 135 IAW SRM 51-40-20 PARA 7, PARA 8 AND PARA 20, REV 102. MATERIAL USED: 7075-T6, 0.016". DIM; FILLER; 10.50" X 8.0", DOUBLER; 13.60" X 9.5".

Part: FRAME — DENTED (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

STA 720A STR 16R FRAME IS DENTED. REPAIRED ON FASI W/O NR 20006, NR 01965. INSTALLED REPAIR DOUBLER TO FRAME AT BS 720A, STR 16R, DUE TO DENT, IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

STA 600 STR 16L SHEAR TIE CRACKED. REPAIRED ON FASI W/O NR 20006, NR 01971, REPLACED CRACKED SHEAR TIE AND DOUBLER AT BS 680, STR 16L IAW B727 SRM 53-20-2 FIG 3 AND 53-10-4 FIG 11, REV 102. MATERIAL USED: 7075-O, HEAT TREATED TO T6 CONDITION. DIM.; DOUBLER; 6 BY 5 BY 0.050, SHEAR TIE; 6 BY 21 BY 0.050.

Part: WEB — CRACKED (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

LT SIDE OF FUSELAGE INTERIOR WEB CRACKED JUST ABOVE NR 2 ENG "S" DUCT AT BS 1303. REPAIRED ON FASI W/O NR 20006, N/R 01976. INSTALLED REPAIR DOUBLER TO CRACKED WEB ABOVE NR 2 ENGINE S DUCT AT BS 1303 IAW B727 SRM 51-40-2, FIG 1, REV 102. MATERIAL USED: DOUBLER 7075-T6, DIM 5 BY 4.5 BY 0.032.

Part: DOUBLER — CRACKED (L1 DOOR HINGE) · airframe 57,864 hrs · 41,947 cycles

L1 DOOR UPPER HINGE SKIN DOUBLER CRACKED LOWER CORNER. REPAIRED ON FASI W/O NR 20006, N/R 01972. REPLACED EXTERNAL DOUBLER AT LEFT FORWARD ENTRY DOOR UPPER HINGE CUTOUT AT BS 303 IAW S/B 727-53A0198 REV. 3 DUE TO CRACK. MATERIAL USED: 3011/2 HD STAINLESS STEEL, DIM. 16.5 BY 7.5 BY 0.063.

Part: FRAME — GOUGED (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

LEFT UPPER CABIN FRAME GOUGED AT BS 670 BETWEEN STR 5L AND 6L. REPAIRED ON FASI W/O 20006, N/R 01962. REMOVED AND REPLACED FUSELAGE FRAME AT BS 670 BETWEEN STR 4L TO STR 14L WITH P/N AE2330-11 IAW AEI DRAWING AE4899 CHANGE H DATED 06/29/1992, DUE TO GOUGING .

Part: STRINGER CLIP — CRACKED (BS 700 S16L) · airframe 57,864 hrs · 41,947 cycles

STA 700 STR. 16L STR CLIP CRACKED. REPAIRED ON FASI W/O NR 20006,NR 01969. REPLACED CRACKED STRINGER CLIPS AT BS 700 STR 16L IAW DRAWING NR 66-11809 REV B AND B727 SRM 51-30-2 REV 102. MATERIAL USED; 7075-T6, DIM.; 4.6 BY 3.1 BY 0.040.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 57,864 hrs · 41,947 cycles

AFT AIRSTAIR AT BS 1323 CENTER STRINGER AT LOWER END CORRODED. REPAIRED ON FSAI W/O NR 20006, N/R 01984. REPAIRED STRINGER AT AFT STAIRS STA 1323 IAW B727 SRM 53-10-3 FIG 1 AND 52-10-1 FIG 3, REV 102. MATERIAL USED: STRINGER; BAC1498-138 7075-T62, DIM: 12.0, CHANNEL; BAC1493-412, DIM: 12.0, ANGLES; 2 EACH- BAC1498-95 7075-T62, DIM: 12.0. CUT OUT DIM: 12.0.

Part: FRAME — BENT (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

STA 420 FRAME BENT AT STR 7R. REPAIRED ON FASI W/O NR 20006, NR 01862. INSTALLED REPAIR DOUBLER TO FRAME AT BS 420, STR 7R, DUE TO DENT, IAW B727 SRM 53-10-2 FIG 3 AND 53-10-4 FIG 2, REV 102. MATERIAL USED: DOUBLER 7075-O, HEAT TREATED TO T6 CONDITION. DIM.; 8.25 BY 3.5 BY 0.063.

Part: STRUCTURE — PUNCTURED (ZONE 600) · airframe 57,864 hrs · 41,947 cycles

RT INBD AFT FLAP LOWER SURFACE IS PUNCTURED NEAR INBD END. REPAIRED ON FASI W/O NR 20006, NR 01850. INSTALLED HOT BONDED REPAIR TO RIGHT INBD AFT FLAP LOWER SURFACE AT WBL 75 IAW B727 SRM 51-40-20 PARA 20, REV 102. MATERIAL USED: 2024-T3, 0.012 THICK, 3 DIAMETER.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

AFT PIT HAS A CRACK AT INTERCOSTAL STR 23L BETWEEN BS 950D TO 950E. REPAIRED ON FASI W/O NR20006, NR01798. R & R CRACKED INTERCOSTAL BETWEEN BS 950D TO BS 950E, STR 23L IAW SRM 51-20-1 FIG 1 REV 102 AND DWG NR 65-56125. MATERIAL USED: 7075-T6, DIM.; 19.5 X 4 X 0.063.

Part: FRAME — DENTED (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

MAIN CABIN FRAME BS.400 FLANGE IS DENTED AT STR 6R. REPAIRED ON FASI W/O 20006,NR 01841 INSTALLED REPAIR DOUBLER TO FRAME AT BS 400, STR 6R, DUE TO DENT, IAW SRM 53-10-2 FIG 3 AND 53-10-4 FIG 2, REV 102. MATERIAL USED: DOUBLER 7075-O, HEAT TREATED TO T6 CONDITION. DIM.; 9 X 4 0.063.

Part: FRAME — DENTED (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

MAIN CABIN FRAME BS 280 FLANGE IS DENTED AT STR 6R. REPAIRED ON FASI W/ONR 20006, NR 01842. INTALLED REPAIR DOUBLER TO FRAME AT BS 380, STR 6R, DUE TO DENT, IAW B727 SRM 53-10-2 FIG 3 AND 53-10-4 FIG 2, REV 102. MATERIAL USED: DOUBLER 7075-O, HEAT TREATED TO T6 CONDITION, DIM.; 10.5 BY 3.25 0.063.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

STA 1070 FLOORBEAM DOUBLE DRILLED HOLE RBL.50. REPAIRED ON FASI W/O NR 20006, N/R 04858. REMOVED AND REPLACED UPPER SUPPORT FITTING AT RT LOWER TORQUE BOX WEB AT VENTRAL STAIRS STA 1263 WITH P/N 65C27137-1 IAW B727 SRM 53-10-2, REV 102.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 57,864 hrs · 41,947 cycles

LT OTBD FOREFLAP WBL 348 CRACK ON SKIN FWD OF FITTING. REPAIRED ON FASI W/O NR 20006,NR 01795 - INSTALLED REPAIR DOUBLER TO LT OTBD FOREFLAP AT WS 348 IAW SRM 57-50-4 FIG 7 REV 102. MATERIAL USED: 2024-T3, DIM.; 6 X 4 X 0.063.

Part: ANGLE — CORRODED (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

STA 1166 AT STR 17 WEB AREA CORRODED. REPAIRED ON FASI W/O NR 20006, N/R 005753. REMOVED AND REPLACED UPPER ANGLE AND LOWER CHANNEL SUPPORT AT STA 1166, STR 17R IAW B727 SRM 53-10-1-FIG. 1, 51-20-1 AND 53-10-2, REV 102. MATERIAL USED: CHANNEL; 7075-T6, 0.080, DIM: 5.625 BY 4.750, SUPPORT ANGLE; 7075-T6, 0.063, DIM: 3.0 BY 2.0.

Part: SKIN — CRACKED (ZONE 600) · airframe 57,864 hrs · 41,947 cycles

RT OTBD FORE FLAP WBL 348 CRACK ON SKIN FWD OF FITTING. REPAIRED ON FASI W/O 20006, NR 01794. INSTALLED REPAIR DOUBLER TO RT OTBD FOREFLAP AT WS 348 IAW SRM 57-50-2, FIG 4 AND 57-50-4 FIG 1 REV 102. MATERIAL USED: 2024-T3, DIM.; 5 X 3 X 0.063.

Part: WEB — CORRODED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

LT MOP SILL CORRODED UNDERSIDE STA 1130 BELOW FLOOR. REPAIRED ON FASI WO 20006, N/R 05780. REMOVED AND REPLACED WEB BETWEEN STA 1110 TO 1130 IAW B727 SRM 53-10-2 FIG 5, 51-30-5, 51-30-6 AND 51-10-1, REV 102. MATERIAL USED: 7075-T6, 0.063, DIM: 18.620 BY 7.0.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

MAIN CABIN OVERWING FLOORBEAM T-CHORD CRACKED AT BS 760 RBL.45.5. REPAIRED ON FASI W/O NR 20006, N/R 05718. REMOVED AND REPLACED MAIN CABIN FLOORBEAM T-CHORD AT STA 760.9 IAW BOEING DWG 65-16279 REV A. MATERIAL USED: BAC1506-1108, DIM: 110.0 L.

Part: SKIN — DELAMINATED (RT AILERON) · airframe 57,864 hrs · 41,947 cycles

RT OTBD AILERON T/E WEDGE PUNCTURED ON LOWER SURFACE. REPAIRED ON FASI W/O NR 20006, NR 01778 - INSTALLED HOT BONDED REPAIR DOUBLER TO RT OTBD AILERON TAB IAW SRM 51-40-20 PARA 7, 20 AND 22, REV 102. MATERIAL USED: 2024-T3, 0.012” THICK, DIM.; 3 X 3. CALCULATED WEIGHT AND BALANCE ACCOMPLISHED.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

CABIN AREA STA 700, STRINGER 7L FRAME TO STRINGER BRACKET IS CRACKED. REPAIRED ON FASI WO 20006. N/R 05633- R & R STRINGER TO FRAME CLIP AT STR 7L, STA 700 IAW DWG 65-45313 REV E AND SRM 51-30-2. MATERIAL USED: 7075-T6, 0.032", DIM: 3.60" X 1.80".

Part: STRINGER — CRACKED (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

CABIN AREA STA 720C AFT OF LIGHT HSG, STRINGER 15L IS CRACKED. REPAIRED ON FASI WO20006. N/R 05629- REPAIRED STR 15L AT STA 720C IAW SRM 53-10-3 FIG 5 AND 51-30-2. MATERIAL USED: CHANNEL; 7075-T6, 0.040", DIM: 6.0" X 0.750", RADIUS FILLER; 7075-T6, 0.080", DIM: 6.0" X 0.750", FILLER; 7075-T6, 0.040", DIM: 3.50" X 0.750" AND 2.50" X 0.750".

Part: STRINGER CLIP — GOUGED (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

STR TIE CLIP GOUGED STA 440 STR 4R. REPAIRED ON FASI WO 20006, N/R 05649. REMOVED AND REPLACED STRINGER TO FRAME CLIP AT STR 4R, STA 440 IAW BOEING DWG 65-45313 REV E AND B727 SRM 51-30-2. MATERIAL USED: 7075-T6, 0.032, DIM: 3.60 BY 1.80.

Part: SKIN — CRACKED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

FUSELAGE STA 1096 AT STRINGER 1 FIRST FAIRING FASTENER RT SKIN HAS CRACKS. REPAIRED ON FASI WO 20006, N/R 05661. REPAIRED FUSELAGE SKIN AT STA 1096, STR 1 IAW BOEING S/B 727-53A0204 REV 3. MATERIAL USED: 2024-T3, 0.063, DIM: 13.50 BY 11.25. CUT OUT DIM: 3.0 BY 1.0.

Part: SKIN — DELAMINATED (AILERON TAB) · airframe 57,864 hrs · 41,947 cycles

LT INBD AILERON TAB HAS DELAMINATION LOWER SURFACE CENTER. REPAIRED ON FASI WO 20006, N/R 05666. INSTALLED HOT BONDED REPAIR TO LT WING INBD AILERON TAB LOWER SURFACE AT WBL 275 IAW B727 SRM 51-40-20, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.012, DIM: 7.0 BY 4.50, FILLER- 2024-T3, 0.012, DIM: 4.0 BY 3.0. WEIGHT OF TAB: 5.500 LBS WITHIN LIMITS.

Part: PANEL — DELAMINATED (NR 6 SPOILER) · airframe 57,864 hrs · 41,947 cycles

NR 6 SPOILER PANEL LOWER SKIN DOUBLER BELOW ACTUATOR ATTACH FITTING IS DISBONDED. REPAIRED ON FASI WO 20006, N/R 05683. INSTALLED BONDED REPAIR TO NR 6 SPOILER PANEL LOWER SKIN DOUBLER BELOW ACTUATOR ATTACH FITTING AT WBL 110 IAW B727 SRM 51-40-20. MATERIAL USED: CORE; PED 3.1 3/16 5052N4, FILLER; 7075-T6, 0.025, DIM: 7.50 INCH 3.0, DOUBLER; 7075-T6, 0.032, DIM: 9.50 BY 5.50.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

STR TIE CLIP CRACK STA 460 STR 2R. REPAIRED ON FASI WO 20006 N/R 05647. REMOVED AND REPLACED STRINGER TO FRAME CLIP AT STR 2R, STA 460 IAW BOEING DWG 65-45313 REV E AND B727 SRM 51-30-2. MATERIAL USED: 7075-T6, 0.032, DIM: 3.60 BY 1.80.

Part: SKIN — DELAMINATED (AILERON TAB) · airframe 57,864 hrs · 41,947 cycles

LT INBD AILERON TAB LOWER SURFACE INBD HAS DELAMINATION. REPAIRED ON FASI WO 20006, N/R 05664. INSTALLED HOT BONDED REPAIR TO LT WING INBD AILERON TAB LOWER SURFACE AT WBL 250 BY IAW B727 SRM 51-40-20, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.012, DIM: 12.0 BY 6.0, FILLER- 2024-T3, 0.012, DIM: 5.0 BY 5.0. WEIGHT OF TAB: 5.460 LBS WITHIN LIMITS.

Part: SKIN — DELAMINATED (LT AILERON TAB) · airframe 57,864 hrs · 41,947 cycles

LT IB AILERON TAB LOWER SURFACE OTBD HAS DELAMINATION AREA-MARKED. REPAIRED ON FASI WO 20006. N/R 05665- INSTALLED HOT BONDED REPAIR TO LT WING INBD AILERON TAB LOWER SURFACE AT WBL 295 IAW SRM 51-40-20, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.012", DIM: 7.0" X 8.0", FILLER- 2024-T3, 0.01", DIM: 5.5" X 6.5". WEIGHT OF TAB: 5.440 LBS. WITHIN LIMITS.

Part: STRINGER — CRACKED (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

CABIN AREA STA 720B FWD OF LIGHT HOUSING, STRINGER 15L IS CRACKED. REPAIRED ON FASI WO 20006. N/R 05630- REPAIRED STR 15L AT STA 720B IAW SRM 53-10-3 FIG 5 AND 51-30-2. MATERIAL USED: ANGLE; 7075-T6, 0.040", DIM: 6.0".

Part: FRAME — DAMAGED (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

STA 970 FRAME DOUBLER DRILLED BELOW STR 7R. REPAIRED ON FASI WO20006 N/R 05548. REPAIRED FRAME AT STA 970 BETWEEN STR 7R AND 8R IAW B727 SRM 53-10-2 FIG 5 AND 53-10-4 FIG 2, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, DIM: 8.0 BY 3.375. CUT OUT DIM: 1.125 BY 1.0.

Part: FRAME — DENTED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

FWD CARGO COMPT FRAME BS 680 HAS 4 DENTS IN THE UPPER FLANGE BETWEEN STR 23R-25R, WEB IS BENT. REPAIRED ON FASI WO20006, N/R 05599. REPAIRED FRAME AT STA 680 BETWEEN STR 23R AND 25R IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.050, DIM: 24.750 BY 3.750. CUT OUT DIM: 1.0 BY 4.0 AND 1.0 BY 2.0.

Part: FRAME — PUNCTURED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

AFT PIT FRAME PUNCTURED STR 27L BS 1130. REPAIRED ON FASI WO 20006, N/R 05443. REPAIRED AFT CARGO COMPARTMENT FRAME AT STR 27L, STA 1130 IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: ANGLE DOUBLER; 7075-T6, 0.063, DIM: 12.25 BY 4.125. CUT OUT DIM: 1.50 BY 1.0.

Part: FRAME — DENTED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

AFT PIT FRAME DENTED AT BS 1030 JUST ABOVE STR 27L. REPAIRED ON FASI WO20006 N/R 05562. REPAIRED FRAME AT STA 1030 BETWEEN STR 26L AND 27L IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, DIM: 11.50 BY 4.20. CUT OUT DIM: 1.875 BY 1.0.

Part: FRAME — DENTED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

FWD CARGO COMPT FRAME BS 660 HAS 4 DENTS IN THE UPPER FLANGE BETWEEN STR 23R-25R. REPAIRED ON FASI WO20006, N/R 05598. REPAIRED FRAME AT STA 660 BETWEEN STR 23R AND 25R IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.050, DIM: 25.875 BY 3.750. CUT OUT DIM: 3.0 BY 1.0 AND 3.0 BY 1.250.

Part: FRAME — DENTED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

AFT PIT RT FRAME BS 950C IS DENTED, BETWEEN STR 26R AND SR 25R. REPAIRED ON FASI W/O NR 20006, N/R 05451. REPAIRED AFT CARGO COMPARTMENT FRAME AT STA 950C BETWEEN STR 25R AND 26R IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, DIM: 13.375 BY 3.90. CUT OUT DIM, 4.750 BY 1.0.

Part: FRAME — DAMAGED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

MISDRILLED HOLE ON UPPER FLANGE OF BS 1050 FRAME BETWEEN STR 27L-28L. REPAIRED ON FASI WO NR 20006, N/R 05495. REPAIRED FRAME AT STA 1050 BETWEEN STR 27L AND 28L IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, DIM: 18.60 BY 4.125. CUT OUT DIM: 1.250 BY 1.0.

Part: FRAME — DENTED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

AFT PIT HAS FRAME DENTED AT BS 1010 BETWEEN STR 26L AND 25L. REPAIRED ON FASI WO NR 20006 N/R 05458. REPAIRED AFT CARGO COMPARTMENT FRAME AT STA 1010 BETWEEN STR 25L AND 26L IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, DIM: 6.0 BY 12.0. CUT OUT DIM: 1.50 BY 1.0.

Part: FRAME — DENTED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

UPPER FLANGE OF AFT PIT FRAME DENTED AT BS950F STR 25L-27L. REPAIRED ON FASI W/O 20006 REPAIRED AFT CARGO COMPARTMENT FRAME AT STA 950F BETWEEN STR 25L AND 27L IAW SRM 53-10-2 FIG. 5 AND 51-40-3 FIG. 1, REV. 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, DIM: 20.750 X 4.50. CUT OUT DIM: 3.125 X 1.0.

Part: FRAME — DENTED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

FWD CARGO COMPT FRAME BS 500 HAS DENT IN UPPER FLANGE ABOVE STR 23R. REPAIRED ON FASI WO20006, N/R 05585. REPAIRED FRAME AT STA 500 BETWEEN STR 22R AND 23R IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, DIM: 9.0 BY 4.0. CUT OUT DIM: 1.0 BY 1.0.

Part: FRAME — DENTED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

FWD CARGO COMPT, FRAME BS 520 HAS 2 DENTS IN UPPER FLANGE ABOVE STR 24R. REPAIRED ON FASI WO20006, N/R 05586. REPAIRED FRAME AT STA 520 BETWEEN STR 23R AND 24R IAW B727 SRM 51-30-5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.050, DIM: 13.0 BY 4.375. CUT OUT DIM: 1.0 BY 2.0 AND 1.0 BY 1.0.

Part: FRAME — DENTED (BS 720A S24-25L) · airframe 57,864 hrs · 41,947 cycles

FWD CARGO COPT FRAME 720A HAS 2 DENTS IN THE UPPER FLANGE BETWEEN STR 24L-25L. REPAIRED ON FASI WO20006. N/R 05604- REPAIRED FRAME AT STA 720A BETWEEN STR 24L AND 25L IAW SRM 51-30-2 AND 51-40-3 FIG. 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.050", DIM: 3.750" X 17.50". CUT OUT DIM: 7.250" X 1.250".

Part: FRAME — DAMAGED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

2 MISDRILLED HOLES ON UPPER FLANGE OF BS 1090 FRAME BETWEEN STR 27R-28R. REPAIRED ON FASI WO NR 20006, N/R 05500. REPAIRED FRAME AT STA 1090 BETWEEN STR 27R AND 28R IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, DIM: 7.0 BY 15.0. CUT OUT DIM: 1.375 BY 1.0 AND 1.0 AND 1.0.

Part: FRAME — DAMAGED (ZONE 500) · airframe 57,864 hrs · 41,947 cycles

MISDRILLED HOLE ON UPPER FLANGE OF BS 1070 FRAME BETWEEN STR 27R-28R. REPAIRED ON FASI WO NR 20006, N/R 05501. REPAIRED FRAME AT STA 1070 BETWEEN STR 27R AND 28R IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, DIM: 11.0 BY 6.0. CUT OUT DIM: 1.0 BY 1.0.

Part: FRAME — DAMAGED (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

STA 950F RIVET HEAD NOT FLUSH STR 7R, REPAIRED ON FASI WO20006, N/R 05542. REPAIRED FRAME AT STA 950F STR 7R IAW B727 SRM 53-10-2 FIG 5 AND 53-10-4 FIG 2, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.071, DIM: 11.750 BY 3.50, FILLER; 7075-T6, 0.071, DIM: 2.750 BY 1.0. CUT OUT DIM: 2.750 BY 1.0.

Part: FRAME — DAMAGED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

MISDRILLED HOLE ON UPPER FLANGE OF BS 1130 FRAME BETWEEN STR 27R-28R. REPAIRED ON FASI WO NR 20006, N/R 05498. REPAIRED FRAME AT STA 1130 BETWEEN STR 27R AND 28R IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, DIM: 11.50 BY 5.125. CUT OUT DIM: 1.875 BY 1.0.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

AFT PIT FRAME SHEAR TIE HAS SURFACE CORROSION BETWEEN STR 30 AND 28R. REPAIRED ON FASI WO 20006, N/R 05442. REMOVED AND REPLACED AFT CARGO COMPARTMENT FRAME SHEAR TIE AND DRAIN MAST SUPPORT CHANNEL AT STA 1148 BETWEEN STR 28R AND STR 30 IAW B727 SRM 53-10-4 FIG 15, 51-10-3, AND 51-20-1 FIG 7, REV 102. MATERIAL USED: SHEAR TIE DOUBLER; 7075-T6, 0.063, DIM: 3.0 BY 4.0, DRAIN MAST SUPPORT CHANNEL; 2024-T3, 0.063, DIM: 18.50 BY 4.750.

Part: FRAME — DENTED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

AFT PIT HAS FRAME DENTED AT BS 970 BETWEEN STR 26L AND 25L. REPAIRED ON FASI WO NR 20006, N/R 05457. REPAIRED AFT CARGO COMPARTMENT FRAME AT STA 970 BETWEEN STR 25L AND 26L IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, DIM: 10.70 BY 4.0. CUT OUT DIM: 1.50 BY 1.0.

Part: FRAME — DAMAGED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

2 MISDRILLED HOLES ON UPPER FLANGE OF BS 1110 FRAME BETWEEN STR 27R-28R. REPAIRED ON FASI WO NR 20006, N/R 05499. REPAIRED FRAME AT STA 1110 BETWEEN STR 27R AND 28R IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, DIM: 12.0 BY 6.0. CUT OUT DIM: 1.375 BY 1.0.

Part: FRAME — DENTED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

AFT PIT FRAME BS 1090 IS DENTED, JUST ABOVE STR 26L. REPAIRED ON FASI WO NR 20006 N/R 05460. REPAIRED AFT CARGO COMPARTMENT FRAME AT STA 1090 BETWEEN STR 25L AND 26L IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, DIM: 21.50 BY 5.250. CUT OUT DIM: 3.0 BY 1.0.

Part: FRAME — DENTED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

AFT PIT FRAME IS DENTED AT BS 950C BETWEEN ST 25L-26L. REPAIRED ON FASI WO20006, N/R 05554. REPAIRED AFT CARGO COMPARTMENT FRAME AT STA 950C BETWEEN STR 25L AND 26L IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, DIM: 10.90 BY 4.0. CUT OUT DIM: 2.0 BY 1.0.

Part: FRAME — DENTED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

FWD CARGO COMPT FRAME BS 680 UPPER FLANGE IS DENTED AND WEB IS BENT BETWEEN STR 23L-24L. REPAIRED ON FASI WO20006. N/R 05600- REPAIRED FRAME AT STA 680 BETWEEN STR 23L AND 24L IAW B727 SRM 53-10-2 FIG. 3 AND 51-40-3 FIG. 1, REV. 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, DIM: 14.50" X 5.0". CUT OUT DIM: 5.375" X 1.50" AND 1.0" X 2.0".

Part: SKIN — DELAMINATED (AILERON TAB) · airframe 57,864 hrs · 41,947 cycles

RT WING INBD AILERON TAB UPPER SURFACE OTBD EDGE IS DELAMINATED. REPAIRED ON ASI WO 20006, N/R 05340. REPAIRED RT WING INBD AILERON TAB UPPER SURFACE AT WBL 295.0 BY HOT BONDING REPAIR IAW B727 SRM 51-40-20, REV 102. MATERIAL USED: DOUBLERS; 2024-T3, 0.012, DIM: 8.0 BY 5.0 AND 10.0 BY 6.50, FILLERS; 2024-T3, 0.012, DIM: 7.0 BY 1.50 AND 1.0 DIA., CORE; 3/16 5052, DIM: 8.0 BY 5.0. WEIGHT OF TAB 5.695 LBS WITHIN LIMITS.

Part: SKIN PANEL — CRACKED (NR 11 SPOILER) · airframe 57,864 hrs · 41,947 cycles

NR 11 SPOILER 3RD HINGE CUTOUT IS CRACKED AT WS 466. REPAIRED ON FASI WO 20006, N/R 05352. REPAIRED NR 11 SPOILER 3RD HINGE CUTOUT AT WS 466 IAW B727 SRM 57-30-4 FIG 10, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.071, DIM: 6.0 BY 4.50.

Part: SEAL DEPRESSOR — DENTED (CARGO DOOR) · airframe 57,864 hrs · 41,947 cycles

C1 DOOR FWD LOWER CORNER, SEAL DEPRESSOR IS DENTED. REPAIRED ON FASI WO 20006, N/R 05353. REMOVED AND REPLACED SEAL DEPRESSOR AT FORWARD DOOR FWD LOWER CORNER AT STA 560 WITH P/N 65-57146-4 IAW B 727 SRM 51-30-2, REV 102.

Part: SKIN — CRACKED (LT WING) · airframe 57,864 hrs · 41,947 cycles

LT WING STA 474 SLAT TRACK CUTOUT UPPER L/E CUTOUT IS CRACKED IN THE RADIUS. REPAIRED ON FASI WO 20006, N/R 05293. REPAIRED LT WING LEADING EDGE AT SLAT TRACK CUTOUT AT WS 474 IAW B727 SRM 57-30-4 FIG 11, REV 102. MATERIAL USED: DOUBLER- 2024-T3, 0.063, DIM: 9.0 BY 8.0.

Part: SKIN — GOUGED (RT ELEVATOR) · airframe 57,864 hrs · 41,947 cycles

RT ELEVATOR UPPER SKIN GOUGED AT ELEVATOR STA 118. REPAIRED ON FASI WO 20006, N/R 05097- REPAIRED RT ELEVATOR UPPER SKIN AT ELEV STA 118 IAW SRM 55-20-3 FIG, 4 AND 55-20-2 FIG 1, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.032", DIM: 7.375" X 4.125", FILLER; 2024-T3, 0.012", DIM: 2.875" X 1.250". CUT OUT DIM: 2.875" X 1.250". ACCOMPLISHED WEIGHT AND BALANCE, NEW MOMENT 120.9 IN. LBS. WITHIN LIMITS.

Part: HINGE BRACKET — CRACKED (NR 14 SPOILER) · airframe 57,864 hrs · 41,947 cycles

RT WING NR 14 SPOILER OTBD HINGE BRACKET IS CRACKED. REPAIRED ON FASI WO 2000. N/R 05306- R & R RT WING NR 14 SPOILER HINGE BRACKET IAW SRM 51-20-1 FIG 7, REV 102 AND DWG 65-21657 REV E MATERIAL USED: 7075-T6, 0.080", DIM: 4.0" X 3.0".

Part: SKIN — PUNCTURED (ELEVATOR) · airframe 57,864 hrs · 41,947 cycles

(FOTR) RT ELEVATOR UPPER SKIN PUNCTURED AT ELEV STA 67. REPAIRED ON FASI W/O NR 20006, 05267- REPAIRED RT ELEVATOR UPPER SKIN AT ELEV STA 67 IAW SRM 55-20-3 FIG, 4 AND 55-20-2 FIG. 1, REV. 102. MATERIAL USED: DOUBLER; 2024-T3, 0.032", DIM: 4.625" X 4.125". CUT OUT DIM: 0.250" DIA. ACCOMPLISHED WEIGHT AND BALANCE, NEW MOMENT IS 120.9 IN LBS WITHIN LIMITS.

Part: SKIN — CRACKED (ZONE 500) · airframe 57,864 hrs · 41,947 cycles

LT WING, STA 549, UPPER L/E SLAT TRACK CUTOUT IS CRACKED IN UPPER RADIUS. REPAIRED ON FASI WO 20006. N/R 05289- REPAIRED LT WING UPPER L/E SLAT TRACK CUTOUT AT WS 549 IAW SRM 57-30-4 FIG 11, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.063", DIM: 9.50" X 10.0", TAPERED SHIMS (2 EA); 2024-T3, 0.050", DIM: 2.50" X 1.0" AND 1.50" X 2.0".

Part: SKIN — DELAMINATED (NR 9 SPOILER) · airframe 57,864 hrs · 41,947 cycles

RT WING NR 9 SPOILER T/E IS DELAMINATED. REPAIRED ON FASI WO 20006. N/R 05307- INSTALLED BONDED REPAIR DOUBLER TO RT WING NR 9 SPOILER T/E AT WBL 130.0 IAW SRM 51-40-20, REV 102. MATERIAL USED: FILLER; 7075-T6, 0.020", DIM: 2.0" X 50.0", DOUBLER; 7075-T6, 0.020", DIM: 4.0" X 50.0".

Part: SKIN — CRACKED (ZONE 600) · airframe 57,864 hrs · 41,947 cycles

NR 11 SPOILER 2ND HINGE CUTOUT IS CRACKED AT WS 460. REPAIRED ON FASI WO 20006. N/R 05351- REPAIRED NR11 SPOILER 2ND HINGE CUTOUT AT WS 460 IAW SRM 57-30-4 FIG 10, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.071", DIM: 6.0" X 4.50".

Part: SKIN — CHAFED (ZONE 500) · airframe 57,864 hrs · 41,947 cycles

LT WING STA 574 UPPER LE SURFACE HAS A DEEPLY CHAFED AREA 13" IN LENGTH. REPAIRED ON FASI WO 20006. N/R 05287- REPAIRED LT WING UPPER L/E SURFACE AT STA 574 IAW SRM 57-30-4 FIG 4, REV 102 MATERIAL USED: DOUBLER; 2024-T3, 0.050", DIM: 10.90", 4.10". FILLER; 2024-T3, 0.040", DIM: 7.0" X 0.870".

Part: SKIN — DENTED (ZONE 500) · airframe 57,864 hrs · 41,947 cycles

LT INBD AFT FLAP INBD LOWER SURFACE HAS 2 LARGE SHALLOW DENTS. REPAIRED ON FASI WO 20006. N/R 05171- REPAIRED LT WING INBD AFT FLAP LOWER SURFACE AT WBL 86.0 BY HOT BONDING REPAIR IAW SRM 51-40-20, REV. 102. MATERIAL USED: DOUBLER; 2024-T3, 0.020", DIM: 11.50" X 9.50", CORE; 5052-44-3/16, DIM: 10.0" X 8.0". CUT OUT DIM: 10.0" X 8.0".

Part: BRACKET — CRACKED (KREUGER FLAP) · airframe 57,864 hrs · 41,947 cycles

RT WING FIXED L/E NR 5 KREUGER FLAP ACTUAOR BRACKET OTBD SIDE IS CRACKED. REPAIRED ON FASI WO 20006, N/R 04963. REPAIRED RT WING L/E NR 5 KRUEGER FLAP ACTUATOR ATTACH BRACKET AT OTBD SIDE IAW B727 SRM 57-10-2 FIG 3, REV 102 AND BOEING DWG 65-16269 SH 4, REV C. MATERIAL USED: 2024-T3, 0.063, DIM: 9.250 BY 6.250.

Part: SKIN — CRACKED (NR 4 K FLAP) · airframe 57,864 hrs · 41,947 cycles

RT WING FIXED L/E NR 4 KREUGER FLAP CUTOUT INBD FWD EDGE DOUBLER IS CRACKED. REPAIRED ON FASI WO 20006, N/R 04955. REPAIRED RT WING FIXED L/E NR 4 KRUEGER FLAP CUTOUT EDGE DOUBLER AT FWD INBD CORNER IAW B727 SRM 51-40-4 FIG 1 AND 57-20-2 FIG 1, REV 102. MATERIAL USED: ANGLE- BAC1503-100046, DIM: 6.250 BY 1.875.

Part: SKIN — DELAMINATED (RT WING AILERON) · airframe 57,864 hrs · 41,947 cycles

RT WING AILERON OTBD T/E WEDGE IS DELAMINATED AT OTBD END. REPAIRED ON FASI WO 20006. N/R 05044- REPAIRED RT WING OTBD T/E WEDGE BY HOT BONDING REPAIR IAW SRM 51-40-20, REV 102, CUT OUT, AND FILLER DIM: 1.0" X 1.0", 3.0" X 1.0", AND 4.0" X 1.0". MATERIAL USED: 2024-T3, 0.012". REBALANCED AILERON, NEW MOMENT 1.27 " LBS WITHIN LIMITS.

Part: SPAR — DAMAGED (ZONE 300) · airframe 57,864 hrs · 41,947 cycles

C/W AD2008-17-14 SB 727-55-0089 ELEVATOR REAR SPAR AT THE TAB HINGE LOC. IAW PARA (A) REPLACEMENT OF THE ELEVATOR REAR SPAR AND SUPPORT FITTING IAW PART 2 OF S/B 727-55-0089 REV 1 (RT). REPAIRED ON FASI WO 20006. N/R 05222- R & R ELEVATOR REAR SPAR AND SUPPORT FITTINGS AT RT SIDE WITH KIT PN: 65C37663-2 IAW S/B 727-55-0089 REV 1, DATED 3/2/2000. ACCOMPLISHED WEIGHT AND BALANCE, NEW MOMENT 120.9 IN. LBS WITHIN LIMITS.

Part: SEAL DEPRESSOR — DENTED (CARGO DOOR) · airframe 57,864 hrs · 41,947 cycles

C1 DOOR AFT LOWER CORNER OF SEAL DEPRESSOR HAS 2 DENTS. REPAIRED ON FASI WO 20006, N/R 05211. REMOVED AND REPLACED SEAL DEPRESSOR P/N 65-57146-3 AT C1 DOOR AFT LOWER CORNER, STA 620 IAW B727 SRM 51-30-2 AND 51-30-05, REV 102.

Part: SKIN — CRACKED (NR 8 SLAT) · airframe 57,864 hrs · 41,947 cycles

RT WING NR 8 SLAT TE HAS 2 CRACKS COMING FROM SCREW HOLE SLAT STA 407.5. REPAIRED ON FASI WO 20006. N/R 05029- INSTALLED DOUBLER REPAIR TO RT WING NR 8 SLAT T/E AT SLAT STA 407.5 IAW SRM 57-50-3 FIG 10, REV 102 MATERIAL USED: DOUBLER- 7075-T6’ 0.125", DIM: 8.0" X 3.250".

Part: STRUCTURE — DAMAGED (NR 6 SLAT) · airframe 57,864 hrs · 41,947 cycles

RT WING NR 6 SLAT T/E IS DAMAGED AT SLAT STA 168. REPAIRED ON FASI WO 20006, N/R 04979. INSTALLED DOUBLER REPAIR TO RT WING NR 6 SLAT T/E AT SLAT STA 168.0 IAW B727 SRM 57-50-1 FIG 2, 57-50-3 FIG 10 AND 51-30-8 FIG 4, REV 102. CUTOUT DIM: 7.0 BY 0.50. MATERIAL USED: 7075-T6, 0.125, DIM.: 3.375 BY 9.0.

Part: SKIN — CRACKED (NR 6 SLAT) · airframe 57,864 hrs · 41,947 cycles

RT WING FIXED L/E NR 6 SLAT OTBD HOOK SEAL CUTOUT AFT SIDE IS CRACKED. REPAIRED ON FASI WO 20006. N/R 04981- REPAIRED RT WING FIXED L/E AT NR 6 SLAT OTBD HOOK SEAL CUT-OUT AFT SIDE AT STA 530.0 IAW SRM 57-30-4 FIG. 9 AND 51-10-1, REV 102. CUT- OUT DIM: 8.50" X 2.0". MATERIAL USED: DOUBLER; 301HD, 0.025", DIM: 4.50" X 8.50", FILLER STRIP; 301HD, 0.032", DIM: 8.50" X 2.0", BACK STRAPS (2 EACH) ; 2024-T3, 0.063", DIM: 1.0" X 3.50".

Part: SKIN — DEBONDED (NR 6 SPOILER) · airframe 57,864 hrs · 41,947 cycles

NR 6 SPOILER PANEL LOWER IB SKIN DOUBLER & HINGE FITTING IS DISBONDED. REPAIRED ON FASI WO 20006. N/R 05307- INSTALLED BONDED REPAIR DOUBLER TO RT WING NR 9 SPOILER T/E AT WBL 130.0 IAW SRM 51-40-20, REV 102. MATERIAL USED: FILLER; 7075-T6, 0.020", DIM: 2.0" X 50.0", DOUBLER; 7075-T6, 0.020", DIM: 4.0" X 50.0".

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 57,864 hrs · 41,947 cycles

RT WING OTBD AFT FLAP IS DELAMINATED STA WBL 348. REPAIRED ON FASI WO 20006, N/R 05046. REPAIRED RT WING OTBD AFT FLAP AT WBL 348.0 BY HOT BONDING REPAIR IAW B727 SRM 51-40-20, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.012, DIM: 2.0 BY 6.0, FILLER; 7075-T6, 0.012, DIM: 1.0 BY 4.0. CUT OUT DIM: 1.0 BY 4.0.

Part: SKIN — DELAMINATED (AFT FLAP) · airframe 57,864 hrs · 41,947 cycles

RT WING INBD AFT FLAP UPPER SURFACE IS DELAMINATED STA130. REPAIRED ON FASI WO 20006, N/R 05051. REPAIRED RT WING INBD AFT FLAP UPPER SURFACE AT WBL 130.0 BY HOT BONDING REPAIR IAW B727 SRM 51-40-20, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.016, DIM: 14.0 BY 5.750, FILLER; 7075-T6, 0.012, DIM: 11.0 BY 4.250. CUT OUT DIM: 11.0 BY 4.250.

Part: SKIN — TORN (NR 6 SLAT) · airframe 57,864 hrs · 41,947 cycles

RT WING FIXED L/E NR 6 SLAT INBD HOOK SEAL CUTOUT AFT SIDE HAS 2 MISSING FASTENERS. REPAIRED ON FASI WO 2000654. N/R 04980- REPAIRED RT WING FIXED L/E AT NR 6 SLAT INBD HOOK SEAL CUTOUT AFT SIDE AT STA 519 IAW SRM 57-30-4 FIG 9, REV 102. MATERIAL USED: DOUBLER; 301.5 HD, 0.025", DIM: 8.750" X 5.50", FILLER; 301.5 HD, 0.032", DIM: 8.750" X 2.0". CUT OUT DIM: 0.60" X 0.60".

Part: BRACKET — CRACKED (NR 5 K FLAP) · airframe 57,864 hrs · 41,947 cycles

RT WING FIXED L/E NR 5 KREUGER FLAP ACTUATOR BRACKET INBD SIDE IS CRACKED. REPAIRED ON FASI WO 20006, N/R 04962. REPAIRED RT WING L/E NR 5 KRUEGER FLAP ACTUATOR ATTACH BRACKET AT INBD SIDE IAW B727 SRM 57-10-2 FIG 3, REV 102 AND BOEING DWG 65-16269 SH 4, REV C . MATERIAL USED: 2024-T3, 0.063, DIM: 9.250 BY 6.250.

Part: FRAME — CRACKED (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

MAIN CARGO AREA, BS 480, BETWEEN STR 16L-17L, CRACKED FRAME. REPAIRED ON FASI WO 20006, N/R 05059. REPAIRED FRAME AT STA 480 BETWEEN STR 16L AND 17L IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3, REV 102. MATERIAL USED: 7075-T6, 0.050, DIM: 9.0 BY 3. CUT OUT DIM: 5.0 BY 0.750.

Part: SKIN — GOUGED (FORE FLAP) · airframe 57,864 hrs · 41,947 cycles

RT WING INBD FORE FLAP OB LOWER SKIN IS GOUGED. REPAIRED ON FASI WO 20006. N/R 05049- REPAIRED RT WING INBD FORE FLAP OTBD LOWER SKIN AT STA 240.0 IAW SRM 57-50-4 FIG 1, REV. 102. MATERIAL USED: DOUBLER; 2024-T3, 0.063", DIM: 5.250" X 4.125".

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 57,864 hrs · 41,947 cycles

RT WING AFT IB FLAP LOWER SURFACE HAS GRAVEL DAMAGE AT INBD END. REPAIRED ON FASI WO 20006. N/R 05050- REPAIRED RT WING AFT INBD FLAP LOWER SURFACE AT WBL 115.0 BY HOT BONDING REPAIR IAW SRM 51-40-20 AND 57-50-2 FIG 3, REV 102. MATERIAL USED: DOUBLER- 7075-T6, 0.016", DIM: 4" DIA. CUT OUT DIM: 0.50" DIA.

Part: SKIN — DELAMINATED (NR 5 SPOILER) · airframe 57,864 hrs · 41,947 cycles

NR 5 SPOILER PANEL AFT EDGE SKIN IS DELAMINATED. REPAIRED ON FASI WO 20006, N/R 05164. REPAIRED NR 5 SPOILER PANEL AFT EDGE AT WBL 217.0 BY HOT BONDING REPAIR IAW B727 SRM 51-40-20 AND 57-50-2 FIG 9, REV 102. MATERIAL USED DOUBLER; 7075-T6, 0.025, DIM: 45.0 BY 8.0, FILLER; 7075-T6, 0.025, DIM: 41.0 BY 4.0. CUT OUT DIM: 41.0 BY 4.0.

Part: ANGLE — CRACKED (LT WING TE FLAP) · airframe 57,864 hrs · 41,947 cycles

LT IB MIDFLAP LOWER AFT CLOSE OUT CHORD ANGLE AT ACTUATOR ROD CUTOUT HAS ONE CORNER CRACKED. REPAIRED ON FASI WO 20006. N/R 05170- R & R LT INBD MID FLAP LOWER AFT CLOSEOUT CHORD ANGLE AT ACTUATOR ROD CUT OUT AT WBL 108 IAW SRM 57-50-2 FIG. 5 AND 51-40-4 FIG. 1, REV 102. MATERIAL USED: ANGLE; BAC 1503-100046, DIM: 48.0" L.

Part: SEAL DEPRESSOR — CRACKED (CARGO DOOR) · airframe 57,864 hrs · 41,947 cycles

C2 DOOR FWD SEAL DEPRESSOR IS CRACKED BETWEEN 1ST DOORSTOP AND LOWER ROLLER. REPAIRED ON FASI WO 20006, N/R 04915. REPAIRED C-2 DOOR FWD SEAL DEPRESSOR BETWEEN 1ST DOOR STOP AND LOWER ROLLER STA 950E IAW B727 SRM 51-10-2, REV 102. MATERIAL USED: FORMED ANGLE AND DOUBLER- 7075-T6, 0.050, DIM: 6.0 BY 1.80. REMOVED AND REPLACED LOWER FWD CORNER SEAL DEPRESSOR ON C-2 DOOR WITH P/N 65-59947-501 IAW B727 SRM 51-20-01.

Part: SKIN — CRACKED (NR 6 SLAT) · airframe 57,864 hrs · 41,947 cycles

RT WING NR 6 SLAT LOWER SKIN COMMON TO TRACK IS CRACKED IN 2 PLACES SLAT SLAT STA 216. REPAIRED ON FASI WO 20006. N/R 04982- INSTALLED DOUBLER REPAIR TO RT WING NR 6 SLAT LOWER SKIN AT SLAT STA 216.0 IAW SRM 57-50-3 FIG 1, REV 102. MATERIAL USED: 2024-T3, 0.080", DIM: 5.0" X 7.0".

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 57,864 hrs · 41,947 cycles

LT OB FORE FLAP UPPER OB LE WBL 485 HAS A DEEP CHAFED AREA ON THE REPAIR DOUBLER. REPAIRED ON FASI WO 20006. N/R 05184- R & R PREVIOUS DOUBLER AT LT WING OTBD FORE FLAP OTBD L/E AT WBL 485.0 IAW SRM 57-50-4 FIG 1, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.050", DIM: 6.0" X 4.250". CUT OUT DIM: 11.0" X 4.250".

Part: SKIN — DAMAGED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

AFT AIRSTAIR RT T/E PREVIOUS REPAIR BENT AT AFT EDGE. REPAIRED ON FASI W/O NR 20006, N/R 04771. REMOVED AND REPLACED PREVIOUS REPAIR TO AFT AIRSTAIR RT T/E AT STA 1342 IAW B727 SRM 52-10-2 FIG 4, REV 102. MATERIAL USED SKIN; 2024-T3, 0.040, DIM: 42.0 BY 38.50, SPLICE; 2024-T3, 0.040, DIM: 4.50 BY 42.0. CUTOUT DIM: 42.0 38.50.

Part: NOSE COWL — CHAFED (ZONE 400) · airframe 57,864 hrs · 41,947 cycles

NR 3 ENGINE AFT T/E FROM 2-3 O`CLOCK POSITION CHAFED AND HOLE WORN THRU AS MARKED A NOSE COWL. REPAIRED ON FASI WO 20006, N/R 04879. REPAIRED NR 3 ENGINE NOSE COWL T/E FROM 2 TO 3 O’CLOCK POSITION IAW B727 SRM 54-10-3 FIG 3, REV 102. MATERIAL USED: ANGLE- 2024-T3, 0.063, DIM: 20.0 BY 2.250, FILLERS; 2 EACH- 2024-T3, 0.050, DIM: 3.125 BY 0.750 AND 1.50 BY 0.750. CUT OUT DIM: 3.125 BY 0.750 AND 1.50 BY 0.750.

Part: SKIN — CRACKED (ZONE 700) · airframe 57,864 hrs · 41,947 cycles

LT MLG WING DOOR AT AFT HINGE AREA, SKIN IS CRACKED AFT OF SEAL RETAINER. REPAIRED ON FASI WO 20006, N/R 04905. REMOVED AND REPLACED PREVIOUS REPAIR TO LT MLG WING DOOR AT AFT HINGE AREA WBL 124 IAW S/B 727-32-318 FIG 4, REV IR. MATERIAL USED: DOUBLER; 2024-T3, 0.050, DIM: 14.250 BY 7.750, FILLER; 2024-T3, 0.050, DIM: 10.50 BY 5.0, SKIN; 2024-T3, 0.050, DIM: 6.250 BY 4.50. CUT OUT DIM: 5.0 BY 4.0.

Part: WEB — CRACKED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

VENTRAL STAIRS, RT LOWER TORQUE BOX WEB, LIGHTNING HOLE IS CRACKED AT BA 1323. REPAIRED ON FASI WO 20006. 44. N/R 04860. REPAIRED RT LOWER TORQUE BOX WEB AT STA 1323 IAW B727 SRM 53-10-2, FIG 6 AND 51-40-2, FIG 1, REV 102. MATERIAL USED: 7075-T6, 0.032, DIM: 1.50 BY 4.0. CUT OUT DIM: 0.50 BY 0.750.

Part: WEB — CRACKED (BS 1223) · airframe 57,864 hrs · 41,947 cycles

VENTRAL STAIRS, LT LOWER TORQUE BOX, LIGHTNING HOLE IS CRACKED AT BS 1223. REPAIRED ON FASI WO 20006, N/R 0485. REPAIRED LT LOWER TORQUE BOX WEB AT STA 1223 IAW B727 SRM 53-10-2, FIG 6 AND 51-40-2, FIG 1, REV 102. MATERIAL USED: 7075-T6, 0.032, DIM: 1.50 BY 4.0. CUT OUT DIM: 0.125 BY 0.50.

Part: SUPPORT FITTING — DAMAGED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

VENTRAL STAIRS, TR LOWER TORQUE BOX, BS 1263 UPPER SUPPORT FITTING HAS HOLE DRILLED INTO RADIUS. REPAIRED ON FASI WO 20006, N/R 04858. REMOVED AND REPLACED UPPER SUPPORT FITTING AT RT LOWER TORQUE BOX WEB AT VENTRAL STAIRS STA 1263 WITH P/N 65C27137-1 IAW B727 SRM 53-10-2, REV 102.

Part: NOSE COWL — GOUGED (ZONE 400) · airframe 57,864 hrs · 41,947 cycles

NR 3 ENGINE NOSE COWL AT 4 O`CLOCK POSITION T/E GOUGED. REPAIRED ON FASI WO 20006, N/R 04888. REPAIRED NR 3 ENGINE NOSE COWL T/E AT 4 O’CLOCK POSITION IAW B727 SRM 54-10-3 FIG 3, REV 102. MATERIAL USED: ANGLE; 2024-T3, 0.063, DIM: 10.0 BY 2.0, FILLER; 2024-T3, 0.050, DIM: 1.50 BY 0.750, SHIM; 2024-T3, 0.050, DIM: 1.0 BY 1.125. CUT OUT DIM: 1.50 BY 0.750.

Part: DEPRESSOR — CHAFED (C2 DOOR SEAL) · airframe 57,864 hrs · 41,947 cycles

C2 DOOR LOWER SEAL DEPRESSOR IS CHAFED AT FWD END. REPAIRED ON FASI WO 2000, N/R 04913. REMOVED AND REPLACED C-2 DOOR LOWER SEAL DEPRESSOR AT STA 950F WITH P/N 65-60234-501 IAW B727 SRM 51-30-2, REV 102.

Part: ANGLE — CORRODED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

NOSE WHEEL WELL INSIDE WEB BOX AT BOTTOM OF VERTICAL SUPPORT, ANGLE CORRODED AND CRACKED BS 294.5. REPAIRED ON FASI WO 20006, N/R 04757. REMOVED AND REPLACED TEE ANGLE ON BOTTOM OF VERTICAL SUPPORT AT STA 294.5 BETWEEN STR 25L AND 26L WITH P/N 65-16312-145 IAW B727 SRM 51-30-2, REV 102.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

AFT PIT INTERCOSTAL IS CRACKED BETWEEN BS 950-950A BETWEEN STR 21R-20R. REPAIRED ON FASI WO 20006, N/R 04763. REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 950 AND 950A AND BETWEEN STR 20R AND 21R IAW B727 SRM 53-10-2 FIG 2 AND 53-10-2 FIG 5, REV 102. MATERIAL USED: 7075-T6, 0.080, DIM: 19.0 BY 6.750.

Part: SKIN — BULGED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

RT FUSELAGE SKIN HAS SKIN SURFACE BULGE AT BS 350 ABOVE SR 21R. REPAIRED ON FASI WO 20006, N/R 04713. REMOVED AND REPLACED JACK PAD STRAP STIFFENER AT STA 350.0 BETWEEN STR 20R AND 21R WITH P/N 65-22589-8 IAW B727 SRM 51-30-5 AND 51-10-1, REV 102.

Part: STIFFENER — CORRODED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

(FOTR) CORROSION AT 227.8 BULKHEAD, BL 0 SKIN INTERIOR, JUST AFT OF EQUIPMENT BAY ACCESS DOOR. REPAIRED ON FASI WO 20006. N/R 04709- R & R DAMAGED STIFFENER AT BL 0 STA 227.8 IAW SRM 51-30-2, 53-10-1 FIG. 1, REV 102 AND DWG 69-15768. MATERIAL USED: 7075-T6, 0.063", DIM.; 9.0" X 7.9".

Part: SKIN — DENTED (ZONE 200) · airframe 57,864 hrs · 41,947 cycles

DENT ON LT FUSELAGE SKIN BS 1319 STR 9L. REPAIRED ON FASI WO 20006, N/R 04658. INSTALLED REPAIR DOUBLER AT BS 1319 AND STR 9L IAW B727 SRM 53-30-2 FIG 2, REV 102. MATERIAL USED: 7075-T6, DIM 8.625 BY 9.25 BY 0.063.

Part: SKIN — DENTED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

(FOTR) DENT ON RT FUSELAGE SKIN AT BS 1100 ABOVE STR 19R. REPAIRED ON FASI WO 20006. N/R 04642 INSTALLED REPAIR DOUBLER AT BS 1100 ABOVE STR 19R, IAW SRM 53-30-3 FIG 3, REV 102 MATERIAL USED: 2024-T3 DIM. 12.25" X 9" X 0.071".

Part: HINGE — CRACKED (CARGO DOOR) · airframe 57,864 hrs · 41,947 cycles

EXT FUSELAGE MCD AFT MOST SEGMENT FUSELAGE SIDE HAS 2ND AFT LOBE CRACKED. REPAIRED ON FASI WO 20006. R & R MAIN CARGO DOOR AFT HINGE SECTION WITH PN MS20001-16-7200 AT STA 620 IAW B727 FREIGHTER MM, CH 52, FIG 5201B, REV. G.

Part: SKIN — DENTED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

(FOTR) DENT AT L FUSELAGE SKIN AT BS 356 BELOW STR 24L. REPAIRED ON FASI WO 20006. REPAIRED LT FUSELAGE SKIN AT STA 356.0 BETWEEN STR 24L AND 25L IAW DWG AJ07-53-102 REV. IR. 8110-3 DATED 02/12/2010 ISSUED. REWORKED LOWER SKIN LAP SEAM AND CUT OUT DAMAGED SECTION (1.0" X 1.50") OF UPPER SKIN LAP SEAM. MATERIAL USED: DOUBLER; 2024-T3, 0.080", DIM: 8.10" X 11.70", FILLER; 2024-T3, 0.071", DIM: 1.50" X 1.0", FILLERS; 3 EACH- 2024-T3, 0.071", DIM: 6.40" X 11.0".

Part: SKIN — DENTED (ZONE 100) · airframe 57,864 hrs · 41,947 cycles

MULTIPLE DENTS AT RT FUSELAGE SKIN SURFACE, PREVIOUS REPAIR DOUBLER AT BS 345.2 STR 24R. REPAIRED ON FASI WO 20006, N/R 04712. REMOVED PREVIOUS REPAIR DOUBLERS ON RT FUSELAGE SKIN AT STA 345 STR 24R AND INSTALLED ONE REPAIR DOUBLER FROM STA 321 TO 340, STR 22R TO 24R IAW COTNEY AEROSPACE DWG AJ07-53-101 REV IR 8110-3 DATED 02/12/2010 ISSUED. MATERIAL USED: DOUBLER; 2024-T3, 0.063, DIM.; 18.50 BY 19.250, FILLERS; 2 EACH, 2024-T3, 0.040, DIM: 1.0 BY 1.0 AND 1.0 BY 2.750.

Part: SWITCH — DEFECTIVE (ZONE 600) · airframe 57,716 hrs · 41,851 cycles

DURING CLIMB OPERATION, WHILE RETRACTING THE FLAP FROM FLAPS 5 TO FLAPS 2. THE L/E FLAP AMBER LIGHT ILLUMINATED, FLIGHT ENGINEERS FLAP DISPLAY INDICATED NR 6 FLAP OUT. ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED AND THE NR 6 L/E FLAP POSITION SWITCH WAS REMOVED AND REPLACED. OPS CHECK GOOD, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.

Part: TRANSMITTER — UNSERVICEABLE (EPR) · airframe 57,556 hrs · 41,671 cycles

FLT 740 FROM TOL TO RDU. DURING TAKEOFF ROLL THE # THREE EPR CIRCUIT BREAKER POPPED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE BLOCKS. INSPECTED ENGINE INLET AND EXHAUST, NO DEFECTS WERE NOTED. REMOVED AND REPLACED EPR TRANSMITTER, OPS CHECK GOOD. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SENSOR — MALFUNCTIONED (STALL WARNING) · airframe 56,989 hrs · 41,251 cycles

FLT 1705 FROM MSP TO TOL. AFTER LIFT OFF THE STALL WARNING STICK SHAKER CAME ON. AIRCRAFT RETURNED TO MSP WHERE IT LANDED WITH OUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED. THE ANGLE OF ATTACK SENSOR AND THE STALL WARNING MODULE WAS REMOVED AND REPLACED. OPERATIONAL CHECKS WERE PERFORMED AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACCESSORY UNIT — MALFUNCTIONED (MLG) · airframe 55,756 hrs · 40,553 cycles

FLT 706 FROM TOL TO MSP, AFTER TAKEOFF FROM TOL ,THE LANDING GEAR HANDLE WOULD NOT RAISE TO THE UP POSITION. THE AIRCRAFT RETURNED TO TOL WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE LANDING GEAR ACCESSORY UNIT WAS AT FAULT. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT AND OPERATIONALLY CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (FIRE WARNING) · airframe 55,252 hrs · 40,284 cycles

FLT 738 FROM TOL TO SLW - DURING CRUISE OPERATION THE LOWER CARGO FIRE WARNING CAME ON. AIRCRAFT DIVERTED TO EVV, EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED, LOWER CARGO COMPARTMENT WAS EMPTY NO DEFECTS WERE NOTED. REMOVED AND REPLACED CENTRAL CONTROL UNIT OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Part: RADOME — LIGHTNING STRIKE (FUSELAGE) · airframe 52,737 hrs · 38,483 cycles

FLT 716 FROM TOL TO MEM, DURING CRUISE OPERATION, AIRCRAFT FLEW THROUGH HEAVY WEATHER. DIVERTED TO BNA AND LANDED WITHOUT INCIDENT. ON POST FLIGHT FOUND LARGE HOLE IN RADOME APPROXIMATELY ONE FOOT IN DIAMETER. AFTER INSPECTION, DETERMINED TO BE LIGHTNING STRIKE. REPLACED RADOME AND PERFORMED LIGHTNING STRIKE INSPECTION. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: VOLT REGULATOR — INOPERATIVE (NR 2 GENERATOR) · airframe 52,514 hrs · 38,369 cycles

FLT 738 FROM MMIO TO MGDL. AFTER V1, NR 2 GENERATOR 3 LIGHT TRIP. COULD NOT RE-ESTABLISH BUS TIE BREAKER. RETURNED TO MMIO AND LANDED WITHOUT FURTHER INCIDENT. PLACED NR 2 GENERATOR/CSD ON MEL. AIRCRAFT RETURNED TO SERVICE. ON 3/13/05, REMOVED AND REPLACED VOLTAGE REGULATOR AND GENERATOR CONTROL PANEL. OPS CHECK GOOD. MEL CLEARED.

Part: CONNECTOR — LOOSE (NR 2 GENERATOR) · airframe 52,070 hrs · 38,134 cycles

FLT 737 FROM GDL TO MTY, ON TAKEOFF ROLL, NR 2 GENERATOR SHOWED UNDERVOLTAGE WITH ASSOCIATED THREE LIGHT TRIP. ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. DEFERRED NR 2 GENERATOR UNDER MEL 24-1. AIRCRAFT RETURNED TO SERVICE. TWO LEGS LATER IN TOL, CLEANED AND RESECURED CONNECTORS ON NR 2 LOAD CONTROLLER AND GENERATOR PROTECTION PANEL. OPS CHECK GOOD. MEL CLEARED. AIRCRAFT RETURNED TO SERVICE.

Part: BOLT — MISLOCATED (DOWNLOCK) · airframe 51,455 hrs · 37,754 cycles

ON WALK AROUND IN KDEN, FOUND THE LT MAIN GEAR BOLT DOWNLOCK LINK PIVOT IMPROPERLY INSTALLED AS PER BOEING IPC 32-10-01-04. A SPECIAL MAINTENANCE FERRY FLIGHT WAS ISSUED ON 6-14-2004 FROM KDEN TO KTOL. PRIOR TO FLIGHT, A VISUAL INSPECTION WAS PERFORMED IN THE LEFT HAND MAIN LANDING GEAR DOWNLOCK LINK ASSEMBLY. ON JUNE 15, 2004 THE AIRCRAFT WAS FERRIED FROM KDEN TO KTOL AND LANDED WITHOUT INCIDENT. UPON ARRIVAL IN KTOL, THE AIRCRAFT WAS INSPECTED AND CLEARED BY REPOSITIONING THE LT MAIN GEAR DOWN LOCK BOLT TO ITS ORIGINAL CONFIGURATION IAW BOEING IPC 32-10-01-04 AND B727 MM 32-13-01 AND THE AIRCRAFT RETURNED TO SERVICE.

Part: ACCESSORY UNIT — DEFECTIVE (MLG) · airframe 50,462 hrs · 37,228 cycles

FLT 711 FROM DEN TO TOL. ON TOUCHDOWN IN TOL, THE LT, RT & NOSE RED GEAR UNSAFE LIGHTS CAME ON IN CONJUNCTION WITH THE THREE LIGHTS. INITIATED GO AROUND, RECYCLE GEAR AND GREEN LIGHTS CAME ON. AGAIN ON TOUCHDOWN, THE THREE RED GEAR UNSAFE LIGHTS CAME ON. RECYCLED GEAR AND DID A FLY BY AND THE TOWER CONFIRMED THE GEAR DOWN AND AIRCRAFT LANDED WITHOUT INCIDENT IN TOL. OPERATIONAL CHECKS WERE ACCOMPLISHED AND REPLACED THE LANDING GEAR ACCESSORY UNIT IAW MM 32-09-122 AND THE AIRCRAFT RETURNED TO SERVICE.

Part: SENSOR — DEFECTIVE (OVERHEAT) · airframe 49,863 hrs · 36,916 cycles

FLT 707 FROM PHX TO TOL. THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED DURING FLIGHT. FOLLOWED ALL CCIA PROCEDURES AND THE LOWER BODY OVERHEAT LIGHT REMAIN ON. ADVISED CCIA FLIGHT FOLLOWING AND ATC IN PHX OF THE PROBLEM AND AIR TURN BACK TO PHX. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED SYSTEM AND REMOVED AND REPLACED THE FORWARD AFT BODY (KEELBEAM) OVERHEAT SENSOR IAW MM 26-10. AIRCRAFT RETURNED TO SERVICE.

Part: INDICATOR — DEFECTIVE (TE FLAP) · airframe 49,532 hrs · 36,787 cycles

FLT 723 FROM ROC TO TOL. AFTER DEPARTURE, DURING FLAP RETRACTION THE OUTBOARD FLAP INDICATOR INDICATED ASYMMETRY BETWEEN THE FLAP FIVE DEGREE AND TWO DEGREE POSITION. ACCOMPLISHED THE APPROPRIATE CHECKLIST AND RETURNED TO ROC AND AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND THE OUTBOARD FLAP POSITION INDICATOR WAS REPLACED. OPERATIONAL CHECKS WERE ACCOMPLISHED IAW MM 27-52-21 AND THE AIRCRAFT RETURNED TO SERVICE.

Part: BEAM — CRACKED (BS 1183)

DURING A HEAVY MAINTENANCE CHECK, A CRACKED DOUBLER WAS FOUND AT BS 1183 PRESSURE WEB AT THE 6 O'CLOCK POSITION ON THE LEFT VERTICAL I BEAM ON THE BOTTOM. REMOVED AND REPLACED THE VERTICAL STIFFENER.

Part: BATTERY PACK — DISCHARGED (R1 SLIDE)

DURING A HEAVY MAINTENANCE CHECK, THE R1 SLIDE LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE BATTERY PACK IAW MM 335022, OPERATIONALLY CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (LT EMER EXIT)

DURING A SCHEDULED MAINTENANCE CHECK, THE LEFT FORWARD AND AFT EMERGENCY OVERWING EXIT IDENTIFIERS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW MM 335022, OPERATIONALLY CHECKS GOOD.

Part: BEAM — CRACKED (BS 1183)

DURING A HEAVY MAINTENANCE CHECK, THE I BEAM IN THE AFT PIT AT BL 0 OF 1183 BULKHEAD WAS FOUND TO EXHIBIT CORROSION ON THE LOWER LEFT SIDE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. I BEAM TO BE REPLACED.

Part: BEAM — CRACKED (BS 740)

DURING A HEAVY MAINTENANCE CHECK, A CREASE BEAM WAS FOUND CRACKED AT LEFT FS 740 SIDE. FABRICATED A NEW ATTACH Z-ANGLE OUT OF 7075 T6 .040 PER B727 SRM 51-20-1. FABRICATED REPAIR ANGLES OUT OF 7075 T6 .063 IAW BAC 727 SRM 51-40-4. INSTALLED REPAIR ANGLES AND Z-ANGLES.

Part: FLOORBEAM — CRACKED (BS 760.95)

DURING A HEAVY MAINTENANCE CHECK, A FLOORBEAM WAS FOUND CRACKED AT RBL 55 FS 760.95. FABRICATED, TREATED AND INSTALLED A REPAIR DOUBLER IAW B727 SRM 51402 AND 51201, 51302.

Part: FRAME — CRACKED (BS 950F)

DURING A HEAVY MAINTENANCE CHECK IN THE AFT CARGO COMPARTMENT AT FS 950F WL 203 RBL 55. THE FUSELAGE SKIN FRAME WAS FOUND CRACKED FWD OF THE DOOR WARNING SWITCH ON THE SECONDARY LIP FLANGE. FOUND SEAL DEPRESSOR DAMAGED BEYOND REPAIR. FABRICATED A NEW SEAL DEPRESSOR IAW B727 SRM 51201. ALODINED, PRIMED AND INSTALLED SEAL DEPRESSOR. INSTALLED SEAL RETAINER IAW B727 SRM 51-30-2.

Part: SWITCH — INOP (LANDING GEAR)

UPON GEAR RETRACTION, GEAR WARNING HORN SOUNDED. PULLED AURAL WARNING CIRCUIT BREAKER TO SILENCE HORN. RESET CIRCUIT BREAKER BEFORE GEAR EXTENSION, GEAR WARNING HORN CAME ON AND THEN WENT OUT WHEN ALL GEAR SHOWED DOWN AND LOCKED. REMOVED AND REPLACED FLAP SWITCH S294 IAW MM 312612. LANDING GEAR WARNING SYSTEM OPERATIONALLY CHECKS GOOD PER MM 326101.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A LINE MAINTENANCE CHECK, THE FORWARD OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE ASSOCIATED BATTERY PACK AND ALL EMERGENCY LIGHTS CHECK GOOD.

Part: LIGHTS — INOPERATIVE (AFT AIRSTAIR)

DURING A LINE MAINTENANCE CHECK, TWO AFT AIRSTAIR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. RELAMPED 2 AIRSTAIR LIGHTS AND OPERATIONALLY CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (ROW 5)

DURING A LINE MAINTENANCE CHECK, THE FORWARD AISLE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AT THE CENTER AISLE ROW 5. SYSTEM OPERATIONALLY CHECKS GOOD.

Part: LIGHT — INOP (ROW 3)

DURING A LINE MAINTENANCE CHECK, AN EMERGENCY LIGHT WAS FOUND TO BE OUT AT LOCATION SEAT ROW 3 IN THE FLOOR TRACK LIGHTING. REPAIRED FLOOR TRACK LIGHT AT SEAT ROW 3. SYSTEM OPERATIONALLY CHECKS GOOD.

Part: LIGHT — INOPERATIVE (ROW 3)

DURING A LINE MAINTENANCE CHECK, AN EMERGENCY FLOOR TRACK LIGHT WAS FOUND TO BE INOPERATIVE AT SEAT ROW 3. REPAIRED FLOOR TRACK LIGHT AT SEAT ROW 3, OPERATIONALLY CHECKS NORMAL.

Part: ANGLE — CORRODED (BS 1070)

DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON CABIN FLOOR SUPPORT ANGLE AT STATION 1070 RBL 30. REMOVED CORROSION FROM SUPPORT ANGLE IAW B727 SRM 511006. CORROSION FOUND TO BE OUT OF LIMITS IAW B727 SRM 531001. FABRICATED NEW PART FROM 44871, 7075 T6. TREATED AND PRIMED IAW B727 SRM 511006. INSTALLED IAW SRM 513001.

Part: ANGLE — CORRODED (BS 1130-1140)

DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT ANGLE BETWEEN STATIONS 1130 AND 1140 LBL 10 ON CABIN FLOOR STRUCTURE. REMOVED CORROSION FROM SUPPORT ANGLE IAW B727 SRM 511001. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW B727 SRM 531001. FABRICATED PART FROM 215584171, 7075 T6. TREATED AND PRIMED IAW B727 SRM 511006. INSTALLED IAW SRM B727 513002.

Part: FLOORBEAM — CORRODED (BS 1050)

DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON UPPER FLOORBEAM STATION 1050 RBL 33. CORROSION OUT OF LIMITS IAW SRM B727 53-10-1. CUT OUT DAMAGED AREA IAW SRM B727 531008. REPAIRED UPPER CHORD FROM BAC 1505100617. REPAIRED SUPPORT ANGLES FROM BAC 14902785. REPAIRED SUPPORT ANGLE FROM BAC 14902831 AND 14902831. FABRICATED NEW STRAPS FROM 7075 T6 .080 AND .051. TREATED PRIMED IAW SRM B727 511001. INSTALLED IAW SRM B727 513002.

Part: ANGLE — CORRODED (BS 1130-1140)

DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND BETWEEN STATIONS 1130 AND 1140 RBL 15 ON CABIN FLOOR SUPPORT ANGLE. REMOVED CORROSION FROM SUPPORT ANGLE IAW B727 SRM 511001. CORROSION FOUND TO BE OUT LIMITS IAW B727 SRM 531001. FABRICATED PART FROM 215584171, 7075 T6511. TREATED AND PRIMED IAW B727 SRM 511006. INSTALLED IAW SRM B727 513002.

Part: ANGLE — CORRODED (BS 1030-1050)

DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON SEAT TRACK SUPPORT ANGLE BETWEEN STATIONS 1030 AND 1050 RBL 44 IN CABIN FLOOR STRUCTURE. REMOVED CORROSION FROM SUPPORT ANGLE IAW B727 SRM 511006. CORROSION FOUND TO BE OUT OF LIMITS IAW B727 SRM 531001. FABRICATED PART FROM 44871, 7075 T6511. TREATED AND PRIMED IAW B727 SRM 511006. INSTALLED IAW SRM B727 513001.

Part: SEAT TRACK — CORRODED (BS 1030-1050)

DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON SEAT TRACK BETWEEN STATIONS 1030 AND 1050 RBL 56 IN CABIN FLOOR STRUCTURE. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW SRM B727 531001. REMOVED SEAT TRACK IAW SRM B727 513002. FABRICATED NEW SEAT TRACK IAW SRM B727 531003. TREATED AND PRIMED IAW SRM B727 511006. INSTALLED SEAT TRACK IAW SRM B727 513001.

Part: SEAT TRACK — CORRODED (BS 1050-1070)

DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON SEAT TRACK BETWEEN STATIONS 1050 AND 1070 RBL 46 IN CABIN FLOOR STRUCTURE. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM B727 531001. REMOVED SEAT TRACK IAW SRM B727 513002. FABRICATED NEW SEAT TRACK IAW SRM B727 531003. TREATED AND PRIMED IAW SRM B727 511006. INSTALLED IAW SRM B727 513001.

Part: ANGLE — CORRODED (BS 1050-1070)

DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT ANGLE BETWEEN STATIONS 1050 AND 1070 LBL 27 ON CABIN FLOOR STRUCTURE. REMOVED CORROSION FROM SUPPORT ANGLE IAW B727 SRM 511001. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW B727 SRM 531001. FABRICATED PART FROM 215584171, 7075 T6. TREATED AND PRIMED IAW B727 SRM 511006. INSTALLED IAW SRM B727513002.

Part: FLOORBEAM — CORRODED (BS 1110)

DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND AROUND A .25 DIA HOLE IN T-CAP OF FLOORBEAM AT STATION 1110 RBL 15. CORROSION WAS TO BE OUT OF LIMITS IAW B727 SRM 511001. CUT OUT DAMAGED AREA IAW B727 SRM 531008. FABRICATED UPPER CHORD FROM BAC 1505100617. FABRICATED NEW SUPPORT ANGLES FROM BAC 14902785. FABRICATED SUPPORT ANGLES FROM BAC 14902831. FABRICATED REINFORCEMENT STRAP FROM 7075 T6 .080. FABRICATED REINFORCEMENT STRAP FROM 7075 T6 .051. TREATED AND PRIMED IAW B727 SRM 511001 MM 512002. INSTALLED IAW B727 SRM 513002.

Part: ANGLE — CORRODED (BS 1090-1110)

DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND BETWEEN STATIONS 1090 AND 1110 LBL 15 ON CABIN FLOOR SUPPORT ANGLE. REMOVED CORROSION FROM SUPPORT ANGLE IAW B727 SRM 511001. CORROSION FOUND TO BE OUT LIMITS IAW B727 SRM 531001. FABRICATED PART FROM 44871, 7075 T6511. TREATED AND PRIMED IAW B727 SRM 511006. INSTALLED IAW SRM B727 513002.

Part: FLOORBEAM — CORRODED (BS 1110)

DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND AT STATION 1110 ON T-CAP OF FLOORBEAM AT BL 0. CORROSION WAS TO BE OUT OF LIMITS IAW B727 SRM 511001. CUT OUT DAMAGED AREA IAW B727 SRM 531008. FABRICATED UPPER CHORD FROM BAC 1505100617. FABRICATED NEW SUPPORT ANGLES FROM BAC 14902785. FABRICATED SUPPORT ANGLES FROM BAC 14902831. FABRICATED REINFORCEMENT STRAP FROM 7075 T6 .080. FABRICATED REINFORCEMENT STRAP FROM 7075 T6 .051. TREATED AND PRIMED IAW B727 SRM 511001 MM 512002. INSTALLED IAW B727 SRM 513002.

Part: ANGLE — CORRODED (BS 1090-1110)

DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND BETWEEN STATIONS 1090 AND 1110 RBL 5 ON CABIN FLOOR SUPPORT ANGLE. REMOVED CORROSION FROM SUPPORT ANGLE IAW B727 SRM 511001. CORROSION FOUND TO BE OUT LIMITS IAW B727 SRM 531001. FABRICATED PART FROM 44871, 7075 T6511. TREATED AND PRIMED IAW B727 SRM 511006. INSTALLED IAW SRM B727 513002.

Part: ANGLE — CORRODED (BS 1050-1070)

DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON SEAT TRACK SUPPORT ANGLE BETWEEN STATIONS 1050 AND 1070 RBL 20 IN CABIN FLOOR STRUCTURE. REMOVED CORROSION FROM SUPPORT ANGLE IAW B727 SRM 511001. CORROSION FOUND TO BE OUT OF LIMITS IAW B727 SRM 531001. FABRICATED NEW PART FROM 215584171, 7075 T6. TREATED AND PRIMED IAW B727 SRM 511006. INSTALLED IAW SRM B727 513001.

Part: SEAT TRACK — CORRODED (BS 1070)

DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON SEAT TRACK AT STATION 1070 RBL 24 IN CABIN FLOOR STRUCTURE. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM B727 531001. REMOVED SEAT TRACK IAW SRM B727 513002. FABRICATED NEW SEAT TRACK IAW SRM B727 531003. TREATED AND PRIMED IAW SRM B727 511006. INSTALLED IAW SRM B727 513001.

Part: ANGLE — CORRODED (BS 1030-1050)

DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT ANGLE BETWEEN STATIONS 1030 AND 1050 RBL 24 IN CABIN FLOOR STRUCTURE. REMOVED CORROSION FROM SUPPORT ANGLE IAW B727 SRM 511001. CORROSION FOUND TO BE OUT OF LIMITS IAW B727 SRM 531001. FABRICATED PART FROM 2155841701 7075 T6. TREATED AND PRIMED IAW B727 SRM 511006. INSTALLED IAW SRM B727 513002.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A LINE MAINTENANCE CHECK, THE EMERGENCY EVACUATION SLIDE LIGHTS WERE FOUND TO BE INOPERATIVE AT DOOR L1 AND R1. REMOVED AND REPLACED THE BATTERY PACK FOR THE EVACUATION SLIDE LIGHTS AT DOORS L1 AND R1.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A LINE MAINTENANCE CHECK, THE EMERGENCY EVACUATION SLIDE LIGHTS WERE FOUND TO BE INOPERATIVE AT DOOR L2 AND R2. REMOVED AND REPLACED THE BATTERY PACK FOR THE EVACUATION SLIDE LIGHTS AT DOORS L2 AND R2.

Part: LINE — RUPTURED (ELEVATOR)

AFTER DEPARTURE LOSS OF A SYSTEM HYDRAULIC QUANTITY UPON GEAR RETRACTION. PERFORMED ALL COM PROCEDURES AND DUMPED FUEL. RETURNED TO MSP. FOUND RUPTURED LINE ON ELEVATOR ACCESSORY. REMOVED AND REPLACED LINE WITH FOLLOWING LEAK AND OPERATIONAL CHECKS GOOD.

Part: KEEL BEAM — CRACKED (BS 870)

DURING A SCHEDULED MAINTENANCE CHECK, A CRACK WAS LOCATED ON THE VERTICAL KEEL BEAM CHORD AT BS 870, APPROXIMATE RBL 3.5. DURING REMOVAL AND REPLACEMENT OF THE CRACKED CHORD NO ADJACENT STRUCTURE WAS FOUND DAMAGED.

Part: STRAP — OUT OF POSITION (2R DOOR)

AIR RETURN DUE TO DOOR STRAP NOISE FROM DOOR 2R. REMOVED DOOR STRAP FROM DOOR AND INSPECTED DOOR SKIN AND NR 3 ENGINE C1 AND C2 DISCS FOR DAMAGE. NO DAMAGE FOUND AND OPS CHECK OK.

Part: SUPPORT — CORRODED (BS 344)

DURING HEAVY MAINTENANCE VISIT, FOUND THE FLOOR SUPPORT CHANNEL AT STATION 344, RBL 50 - 62.5 CORRODED OUT OF LIMITS. REMOVED, FABRICATED, AND INSTALLED NEW CHANNEL IAW SRM 51-30-2, 51-20-2, 51-10-1 AND DRAWING 65-26173.

Part: SEAT TRACK — CORRODED (BS 344-380)

DURING HEAVY MAINTENANCE VISIT, FOUND THE SEAT TRACK AT STATION 344-380, RBL 44 CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 344-360)

DURING HEAVY MAINTENANCE VISIT, FOUND THE SEAT TRACK AT STATION 344-360, LBL 22 CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW SRM 51-30-2, 53-10-5, AND 51-10-2.

Part: FLOORBEAM — CORRODED (BS 344)

DURING HEAVY MAINTENANCE VISIT, FOUND THE FLOORBEAM UPPER CAP CORRODED BEYOND LIMITS AT STATION 344, RBL 68 - LBL 52. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT CAP IAW SRM 51-10-1, AND 51-10-2.

Part: SUPPORT — CORRODED (BS 950)

DURING HEAVY MAINTENANCE VISIT, FOUND THE FLOORBOARD SUPPORT CHANNEL IN THE AFT CARGO PIT DENTED AT STATION 950F, RBL 11. REMOVED, FABRICATED, AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-30-02, 53-10-2, AND 51-30-2.

Part: SUPPORT — CORRODED (BS 950-990)

DURING HEAVY MAINTENANCE VISIT, FOUND FLOORBOARD SUPPORT CHANNEL IN THE AFT CARGO PIT DENTED AND PUNCTURED FROM STATION 950E TO 990. REMOVED, FABRICATED AND INSTALLED NEW SUPPORT CHANNEL IAW SRM 53-10-2 AND 51-30-01.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

THE L-2 DOOR OVERHEAD EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK, OPS CHECKED NORMAL PER B727 MAINTENANCE MANUAL 33-50-01.

Part: BATTERY PACK — DISCHARGED (CABIN)

THE EMERGENCY LIGHT AT DOOR 2L WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, LIGHT TESTED GOOD.

Part: BATTERIES — DISCHARGED (CABIN)

THE L-2 DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERIES, LIGHT OPS CHECKED NORMAL.

Part: LAMP — FAILED (AFT AIRSTAIR)

THE AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. RELAMPED LIGHT, LIGHT TESTED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

THE L-2 DOOR FIXED EXIT SIGN AND AREA LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, LIGHT OPS CHECKED GOOD.

Part: CONNECTOR — LOOSE (LAV SMOKE DET)

ALL THREE LAV SMOKE DETECTORS FAILED TO TEST. RECONNECTED CANNON PLUGS IN ACCORDANCE WITH 20-60-06, ALL OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (CABIN)

FOUND RIGHT AFT SERVICE DOOR EMERGENCY LIGHT INOP. CLEANED SOCKET, RELAMPED FIXTURE AND OPS CHECKED GOOD.

Part: SWITCH WIRE — FAILED (NLG)

ON RETRACTION, NOSE GEAR DISAGREE LIGHT REMAINED ON WITH ALL OTHER INDICATIONS NORMAL. LIGHT EXTINGUISHED WHEN GEAR CYCLED DOWN. FOUND WIRE-C BROKEN AT S96 NOSE LANDING GEAR LOCK SWITCH. REPAIRED WIRE, OPS CHECKED GOOD IN ACCORDANCE WITH 32-60-2.

Part: BATTERIES — DISCHARGED (CABIN)

FOUND CEILING MOUNTED EMERGENCY AREA LIGHT IN FORWARD CABIN INOP. REMOVED AND REPLACED BATTERIES FOR AREA LIGHT IN ACCORDANCE WITH MM 33-50-81 AND OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

THE AFT AIRSTAIR EMERGENCY EXIT AREA LIGHT WAS FOUND FLICKERING AND DIM. REMOVED AND REPLACED AFT AIRSTAIR LIGHT ASSEMBLY. PERFORMED OPS CHECK, NEW LIGHT OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (L2 DOOR)

FOUND L2 OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED THE POWER SUPPLY (P/N 9005-42), (S/N 19440) AND THE BATTERY PACK (P/N 9008-3-5A), (S/N 10000), OPS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (AIRSTAIR)

FOUND AFT AIRSTAIR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES AND OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP ON LINE CHECK. REMOVED AND REPLACED RIGHT OVERWING BATTERY PACK. EMERGENCY LIGHTS OPS CHECK GOOD.

Part: LAMP — FAILED (CABIN)

FOUND RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOP ON LINE CHECK. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIGHT LAMP. EMERGENCY LIGHTS OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (OVHD PANEL)

FOUND EMERGENCY LIGHTS DISARM AMBER LIGHT INOP. REMOVED AND REPLACED LAMP, OPS CHECK GOOD.

Part: SMOKE DETECTOR — INOPERATIVE (LT AFT LAV)

THE AFT LEFT LAVATORY SMOKE DETECTOR WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED SMOKE DETECTOR AND UNIT CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (AFT AIRSTAIR)

THE AFT AIRSTAIR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERIES IN AFT AIRSTAIR EMERGENCY EXIT LIGHT AND LIGHT CHECKED GOOD.

Part: ANGLE — CRACKED (BS 1010)

DURING HEAVY MAINTENANCE VISIT, FOUND AFT CARGO SUPPORT ANGLE CRACKED AT STATION 1010, STRINGERS 26L TO 28L. FABRICATED AND INSTALLED REPAIR ANGLE IAW B727 SRM 53-10-04.

Part: FIRE CONNECTOR — LOOSE (NR 1 ENGINE)

DURING EN ROUTE CLIMB, THE NUMBER 1 ENGINE FIRE DETECTION LIGHT FLICKERED ON AND OFF. FOUND FIRE LOOP CONNECTOR D1926 CERAMIC INSULATION DAMAGED, REPLACED CONNECTOR. INSPECTED LOOPS AND ATTACHING WIRING AND FOUND NO OTHER DISCREPANCIES. PERFORMED SYSTEM TEST IAW MM 26-11-01 PAGE 501-502, OPS CHECKED GOOD.

Part: FIRE WIRE — OUT OF POSITION (NR 1 ENGINE)

DURING EN ROUTE CLIMB, THE NUMBER 1 ENGINE FIRE DETECTION LIGHT FLICKERED ON AND OFF, LASTED A FEW SECONDS THEN WENT OFF AND STAYED OFF. ALL ENGINE INDICATIONS READ NORMAL. FOUND FORWARD PLUG CONNECTOR STRAIN RELIEF RUBBING WIRE. REROUTED WIRING FOR BETTER RELIEF AND RAN ENGINE AT FULL POWER AND HALF POWER WITH NO DEFECTS NOTED.

Part: FIRE LOOP — OIL CAKED (NR 1 ENGINE)

THE NUMBER 1 ENGINE FIRE WARNING LIGHT ILLUMINATED AND BELL RANG DURING GROUND OPERATIONS. ALL ENGINE INDICATIONS WERE NORMAL. THE ENGINE WAS SHUTDOWN. DURING INSPECTION TWO CONNECTORS FOR FIRE LOOP IN STUB WING WERE FOUND OIL CAKED CAUSING FALSE FIRE INDICATION. CLEANED CONNECTORS AND SYSTEM CHECKED GOOD IAW MM 26-11-01, RAN ENGINE AT TAKEOFF POWER AND SYSTEM TESTED GOOD.

Part: DRIVE MOTOR — LEAKING (TE FLAPS)

DURING CLIMBOUT AT 13,000 FEET, THE NUMBER 1 A-SYSTEM HYDRAULIC PUMP \LO PRESS\ LIGHT ILLUMINATED AND THE A-SYSTEM QUANTITY DROPPED RAPIDLY. THE OUTBOARD FLAP DRIVE MOTOR SEAL WAS FOUND BLOWN OUT. REMOVED AND REPLACED THE MOTOR PER MM 27-57-62.

Part: FLAP DRIVE MOTOR — LEAKING (OTBD FLAP DRIVE)

AFTER ENGINE START AND TAXI THE A-SYSTEM HYDRAULIC QUANTITY DROPPED FROM FULL TO 2 GALLONS. THE OUTBOARD FLAP DRIVE MOTOR WAS FOUND LEAKING WITH THE ENGINES RUNNING AND FLAPS IN THE DOWN POSITION. REMOVED AND REPLACED THE FLAP DRIVE MOTOR PER MM 27-51-62. OPERATIONS TESTED GOOD WITH NO LEAKS NOTED.

Part: OIL PRESS SWITCH — LEAKING (NR 3 ENGINE)

WHILE EN ROUTE THE NR 3 ENGINE OIL QUANTITY BEGAN TO DECREASE. THE ENGINE WAS SHUTDOWN, AND ALL INDICATIONS WERE NORMAL. A LEAK WAS FOUND AT THE LOW OIL PRESSURE SWITCH AND THE UNION BELOW THE SWITCH. THE SWITCH AND PACKINGS AT THE UNION WERE REPLACED, AND THE ENGINE LEAK CHECKED GOOD.

Part: EEL LAMP — FAILED (L-2 DOOR)

FOUND THE L-2 EMERGENCY SLIDE LIGHT INOPERATIVE. RELAMPED THE L-2 DOOR EMERGENCY SLIDE LIGHT. OPS CHECKED GOOD.

Part: APU — FAILED (AFT FUS)

WHILE AIRCRAFT WAS TAXIING, THE CABIN FILLED WITH SMOKE. MAINTENANCE FOUND THE APU INTERNALLY FAILED CAUSING SMOKE, IT WAS THEN INTRODUCED INTO THE CABIN THOUGH THE AIRCRAFT PACKS. THE APU WAS REMOVED AND REPLACED AND OPERATIONS CHECKED NORMAL.

Part: CONTROL CABLE — OUT OF ADJ (NLG DOOR)

NOSE GEAR DOOR LIGHT ON WITH GEAR DOOR CLOSED. FOUND FORWARD NOSE GEAR DOORS CABLE BELOW TENSION LIMITS. ADJUSTED GEAR DOORS CABLE PER 32-22-01, PAGE 501. OPS CHECK GOOD.

Part: WARNING SWITCH — INTERMITTENT (NOSE GEAR DOORS)

NOSE GEAR DOOR LIGHT STAYED ON AFTER TAKEOFF. DUMPED 17, 500 LBS OF FUEL AND RETURNED TO ORD. FOUND INTERMITTENT NOSE GEAR DOOR WARNING SWITCH. REMOVED AND REPLACED NOSE GEAR DOOR WARNING SWITCHES. GEAR DOOR WARNING SYSTEM OPS CHECK GOOD IAW 727 MM 32-62-11.

Part: EEL POWER PACK — FAILED (AFT AIRSTAIR)

MSP - DURING LINE CHECK FOUND AFT AIRSTAIR EMERGENCY OVERHEAD LIGHT INOPERATIVE. REMOVED AND REPLACED AFT AIRSTAIR EMERGENCY LIGHT POWER PACK, IAW MM 33-50-61 AND OPS CHECKED GOOD. (W)

Part: EEL BATTERIES — DISCHARGED (AFT AIRSTAIR)

MSP - AFT AIRSTAIR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES. OPERATIONAL CHECK PER B727 MM 33-50-00. (W)