N492FE

Part: ENGINE — MALFUNCTIONED (NR 3) · airframe 41,972 hrs · 28,876 cycles

AFTER STANDARD POWER SET AND BRAKE RELEASE HEARD LOUD BANG FOLLOWED BY EPR ON NR 3 GOING TO ZERO, DISCONTINUED TAKEOFF AND TAXIED CLEAR. ON TAXI BACK SAW IDLE NUMBERS ON NR 3 OF N1-26 EGT-410 N2-53 (IE LOWER N1 AND HIGHER EGT). ENGINE SHUTDOWN ON TAXI BACK. R & R NR 3 ENGINE IAW WC 70T0001-03, AND 70T0301-03. LEAK CHECKED, IDLE CHECKED, FLIGHT IDLE CHECKED, PART POWER, AND MAX POWER ASSURANCE COMPLIED WITH IAW JRH WITH NO DISCREPANCIES NOTED.

Part: ACTUATOR — LEAKING (TE FLAP) · airframe 41,716 hrs · 28,671 cycles

LOSS OF ALL SYS A HYD ASSOCIATED WITH LED FLAP MALFUNCTION NR 4 L/E FLAP. COMPLETED ALL QRH APPROPRIATE CHECKLISTS AND QRH PROCEDURES. REMOVED AND REPLACED NR 4 LEADING EDGE FLAP ACTUATOR

Part: LEVER — BINDING (THRUST) · airframe 41,532 hrs · 28,513 cycles

FLIGHT TEST-DURING LEVEL OFF AND RETARDING THE THRUST LEVERS, THE NR 3 THRUST LEVER WOULD NOT RETARD PAST THE 12 O'CLOCK POSITION. ATTEMPTED SEVERAL TIMES TO RETARD BUT NO JOY. THE NR 3 THRUST LEVER WOULD MOVE FWD BUT NOT FWD IDLE. AFTER 5 MINUTES OR SO THE THRUST LEVER WOULD MOVE TO IDLE. INSPECTED NR 3 ENG POWER LEVER CONTROL CABLE QUADRANT INSIDE NR 3 PYLON, NO DEFECTS NOTED IAW AMM 76-11-021-2. INSPECTED THRUST LEVER PEDESTRAL & CABLE RUN IAW AMM 76-11-000-6, NO DEFECTS FOUND. INSPECTED RT AFT AIRSTAIR AREA FOUND NR 3 ENG THROTTLE LEVER LOWER PULLEY AT 1183 BULKHEAD DIRTY & EXCESSIVE GREASE BUILD UP, CLEANED IAW BSOPM 20-30-03 & AMM 12-20-001-2, NR 3 ENG CONTROL SYST OPS CHECKED NORMAL IAW AMM 76-11-000-5-0.

Part: FLOORBEAM — CORRODED (BS 950C) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

CORROSION ON STA 950C FLOORBEAM UPPER FLANGE UPPER SURFACE, LBL 30. CUT OUT CORRODED AREA IAW SRM 53-10-8 FIG 3, FABRICATED REPAIR PARTS UPPER CHORD, 2 SUPPORT ANGLES, AND 2 REINFORCEMENT STRAPS IAW SRM 53-10-8 FIG 3 AND 53-10-2 FIG 7. INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 690-720C) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

CORROSION SEAT TRACK FLANGE BETWEEN STA 690 TO 720C, RBL 25. REMOVED SEAT TRACK SECTION IAW SRM 51-30-5, FIG 1. FABRICATED SEAT TRACK , SPLICE, ANGLES, & STRAP IAW SRM 53-10-5, FIG 1 AND 51-30-5. INSTALLED SEAT TRACK SECTION AND SPLICE IAW SRM 51-30-2 AND 53-10-5, FIG 1.

Part: SEAT TRACK — CORRODED (BS 950) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

CORROSION ON SEAT TRACK FLANGE STA 870 TO 950, 10" RBL 45. REMOVED SEAT TRACK SECTION AT BS 870 TO 950 10" RBL 45, FABRICATED NEW SECTION FROM BAC 1520-792 7178T6511, AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53- 10-2 FIG 7, 51-30-5, 51-10-1, 51-10-2, AND 51-30-2.

Part: INTERCOSTAL — CRACKED (BS 870) · airframe 41,528 hrs · 28,504 cycles

MAIN CABIN HAS INTERCOSTAL CRACKED AT RADIUS BS 870 RBL 45. REMOVED INTERCOSTAL AT BS 870 RBL 45.0 IAW B727 SRM 51-30-2. FABRICATED INTERCOSTAL FROM PM50-550101-7075T6511 IAW DWG 65-18745 AND SRM 51-20-1, 51-30-5, AND 51-10-1. INSTALLED INTERCOSTAL IAW SRM 51-30-2.

Part: BULKHEAD — MISREPAIRED (BS 1183) · airframe 41,528 hrs · 28,504 cycles

REPAIR AT BS 1183 BULKHEAD LBL 50 WL 223.67 FOUND DURING WC 7-5100-7-5005 PT2 REPAIR IDENTIFICATION, CLASSIFICATION, AND TRACKING TO BE NON CONFORMING. REMOVED REPAIR AT BS 1183 BULKHEAD LBL 50 WL 223.67, FABRICATED NEW REPAIR AND FILLER. INSTALLED REPAIR DOUBLER IAW EA 7-5310-123576.

Part: FLOORBEAM — CORRODED (BS 440) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

CORROSION FLOORBEAM TOP TEE CAP MAIN CABIN STA 440, LBL 25-45. CUT OUT DAMAGED AREA IAW SRM, REV 103, 53-10-8 FIG 8. FABRICATED ANGLES AND FILLER IAW SRM 53-10-8 FIG 8. LOCATED AND DRILLED PARTS IAW SRM 51-30-5, INSTALLED REPAIR ANGLES AND FILLER IAW SRM 53-10-8 FIG 8.

Part: SEAT TRACK — CORRODED (BS 950) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

CORROSION LBL 25 SEAT TRACK STA 950 TO 950, 10". REMOVED CORRODED SEAT TRACK, FABRICATED NEW TRACK, AND INSTALLED IAW SRM 53-10-2 FIG 7, 51-30-5, 51-10-1, 51-10-2, AND 51-30-2.

Part: FLOORBEAM — CORRODED (BS 380) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

CORROSION FLOORBEAM TOP TEE CAP MAIN CABIN STA 380, LBL 45 TO LBL 25. CUT OUT DAMAGED AREA IAW SRM 53-10-8 FIG 8. FABRICATED 2 REPAIR ANGLES AND FILLER IAW SRM 53-10-8. INSTALLED 2 REPAIR ANGLES AND FILLER IAW SRM 53-10-8 FIG 8 REV. 103.

Part: STRINGER — CRACKED (BS 500 S27R) · airframe 41,528 hrs · 28,504 cycles

STRINGER CRACKED AT BS 500, STR 27R. CUT OUT DAMAGED AREA DIM 17 1/4" LONG IAW SRM 53-10-3 FIG 1 FABRICATED HAT SECTION, 2 EACH CHANNELS, 4 ANGLES & 4 EACH STRAPS IAW SRM 53-10-3 FIG 1 DETAIL 11 AND 53-10-2. INSTALLED STRINGER AND REPAIR PARTS IAW SRM 51-30-2 AND 53-10-3 FIG 1 REV 103.

Part: SKIN — CRACKED (NR 3 INLET) · airframe 41,528 hrs · 28,504 cycles

# 3 ENGINE INLET COWL AFT EDGE HAS TORN SKIN AT 4 O'CLOCK POSITION. CUT OUT DAMAGED SKIN, IAW SRM 54-30-3, FIG 5. FABRICATED REPAIR DOUBLER , AND FILLER IAW SRM 54-30-3, FIG 5. INSTALLED REPAIR DOUBLER IAW SRM 54-30-3, FIG 5 AND 51-30-2, REV 103.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

CORROSION LBL 45, SEAT TRACK IN NUMEROUS AREAS, STA 950, 10" TO STA 1130. REMOVED OLD TRACK, FABRICATED, AND INSTALLED NEW SECTION IAW SRM`S 53-10-2 FIG 7, 51-30-5, 51-10-1, 51-10-2, AND 51-30-2.

Part: FRAME — GOUGED (BS 1030 S1-2L) · airframe 41,528 hrs · 28,504 cycles

GOUGES AFT SIDE OF FRAME WEB STA 1030, BETWEEN S1-2L. CUT OUT DAMAGED AREA, FABRICATED WEB REPAIR AND INSTALLED WEB REPAIR IAW SRM 53-10-4 FIG 1, 51-30-2, 51-10-2 AND 51-30-5 REV 103

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 41,528 hrs · 28,504 cycles

RT HORIZONTAL STABILIZER HAS A DENT IN LOWER SKIN AT APPROX STAB STA 72.08, APPROX 30" AFT OF L/E SPAR WEB. CUT OUT DAMAGED AREA DIM 3 1/2" X 8" IAW SRM 55-10-3 FIG 4. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 55-10-3 FIG 4. INSTALLED DOUBLER AND FILLER IAW SRM 55-10-3 FIG 4 REV. 103.

Part: SEAT TRACK — CORRODED (BS 950-950C) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

CORROSION BL 0 SEAT TRACK STA 950-950C REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK, AND INSTALLED IAW SRM 53-10-2 FIG 7A, SRM 51-30-5, 51-10-1, 51-10-2, AND 51-30-2.

Part: FRAME — DAMAGED (BS 1148) · airframe 41,528 hrs · 28,504 cycles

AFT PIT- DAMAGE ON UPPER FLANGE OF FRAME AT BS 1148 RBL30. BLENDED DAMAGE ON BS 1148 RBL 30 IAW SRM 51-10-1 FOUND TO OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED AREA IAW SRM 51-40-3 FIG 1. FABRICATED REPAIR DOUBLER 10" X 5" FROM .071" 7075 O IAW SRM 51-40-3 FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 51-40-3 FIG 1 REV 103

Part: SEAT TRACK — CORRODED (BS 1010-1130) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

CORROSION BL 0 SEAT TRACK, BS 1010-1130. REMOVED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK SECTION, INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A, AND SRM 51-30-5, 51-10-1, 51-10-2, AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 950C-950F) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

CORROSION BL 0 SEAT TRACK STA 950C-950F. REMOVED SEAT TRACK SECTION, FABRICATED NEW SECTION, AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A AND SRM 51-30-5, 51-10-1, 51-10-2, AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 950-950A) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

CORROSION LBL 25 SEAT TRACK STA 950, 10" TO 950A. REMOVED SEAT TRACK, FABRICATED & INSTALLED NEW SEAT TRACK IAW SRM 53-10-2 FIG 7 AND 51-30-5.

Part: SEAT TRACK — CORRODED (BS 950) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

CORROSION RBL 25 SEAT TRACK STA 950 . REMOVED SEAT TRACK SECTION AT BS 870 TO 950 + 10" RBL 25, FABRICATED NEW SECTION AND INSTALLED IAW SRM 53-10-2 FIG 7, 51-30-5, 51-10-1, 51-10-2, AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 950-950E) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

CORROSION RBL 25, SEAT TRACK STA 950, 10" TO 950E. REMOVED & FABRICATED NEW SEAT TRACK SECTION, ANGLES, & STRAPS AND INSTALLED IAW SRM 53-10-5 FIG 1, 51-30-2, 51-30-5, AND 51-10-2.

Part: SKIN — CORRODED (BS 502) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

FWD PIT BILGE AREA LOWER SKIN HAS AREA OF CORROSION AT BS 502, RBL 17. CUT OUT DAMAGED AREA, DIMENSION 7" X 6" IAW SRM 53-30-3 FIG 24. FABRICATED REPAIR DOUBLER, STRUCTURAL FILLER AND FILLERS IAW SRM 53-30-3 FIG 24 AND 53-30-2 FIG 2. INSTALLED REPAIR DOUBLER, STRUCTURAL FILLER AND FILLERS IAW SRM 51-30-2 AND 53-30-3 FIG 24, REV 103.

Part: SHEAR TIE — CORRODED (BS 540) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

FWD PIT BILGE AREA HAS CORRODED SHEAR TIE AT BS 540, LBL 2 TO RBL 5. CUT OUT DAMAGED LOWER FLANGE OF SHEAR TIE IAW SRM 53-10-4. FIG 15 FABRICATED. REPAIR DOUBLER FROM 7075 T6 .050" DIM 5" X 3.2500" AND RADIUS FILLER FROM 7075 T6 .063", DIM 5" X .8750" IAW SRM 53-10-4, FIG 15. INSTALLED REPAIR DOUBLER AND RADIUS FILLER IAW SRM 51-30-2, REV 103 AND 53-10-4, FIG 15.

Part: FRAME — CORRODED (BS 720B S24L) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

FWD PIT LT SIDE, BS 720B FRAME HAS AREA OF CORROSION JUST BELOW STRINGER 24L. CUT OUT DAMAGED CHORD IAW SRM 51-40-4 FIG 2 LOCATED AND DRILLED NEW FRAME, FABRICATED REPAIR ANGLES, AND RADIUS FILLER IAW SRM 51-40-4 FIG 2 INSTALLED NEW FRAME, 3 EACH REPAIR ANGLES AND RADIUS FILLER IAW SRM 51-40-4 FIG 2 AND 51-30-2 REV 103.

Part: FRAME — CORRODED (BS 720C) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

FWD PIT LT SIDE BS 720C FRAME HAS AREA OF CORROSION JUST BELOW STR 24L. CUT OUT DAMAGED FRAME IAW SRM 51-40-4 FIG 2 LOCATED AND DRILLED REPAIR FRAME SECTION, FABRICATED REPAIR ANGLE 1 AND 2 AND REPAIR ANGLE 3. FABRICATED REPAIR RADIUS FILLER IAW SRM 51-40-4 FIG 2 INSTALLED FRAME REPAIR ANGLES AND RADIUS FILLER IAW SRM 51-30-2 AND 51-40-4 FIG 2 REV 103.

Part: FLOORBEAM — CORRODED (BS 560) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

CORROSION TOP TEE CAP FLOORBEAM MAIN CABIN STA 560 BL0 TO LBL 25. CUT OUT DAMAGE IAW SRM 53-10-8 FIG 3. LOCATED AND DRILLED NEW UPPER TEE, AND 4 SUPPORT ANGLES AND 4 REINFORCEMENT STRAPS IAW SRM 53-10-8 FIG 3. INSTALLED TEE, SUPPORT ANGLES AND STRAPS IAW SRM 53-10-8 FIG 3 REV. 103.

Part: TORQUE BOX — CRACKED (BS 1233) · airframe 41,528 hrs · 28,504 cycles

AFT AIRTSTAIRS AREA , LIGHTING HOLE IS CRACKED AT RT LOWER TORQUE BOX, BS 1233. CUT OUT DAMAGED AREA OF WEB, DIM 1/2" X 1/2" IAW SRM 51-40-2 FIG 1 AND 51-10-1. FABRICATED DOUBLER FROM 7075 T-6 .032" DIM 6" X 2" IAW SRM 51-40-2 FIG 1 AND 53-10- 2 FIG 6. INSTALLED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1 AND 51-30-2 REV. 103.

Part: SKIN — GOUGED (BS 620 S8-10L) · airframe 41,528 hrs · 28,504 cycles

INNER SURROUND SKIN GOUGED STA 620, STR 8L TO 10L. REMOVED MCD INNER SKIN AT STA 620 STR 8L TO 10L, FABRICATED NEW INNER SKIN FROM 2024T3 0.125", AND INSTALLED NEW INNER SKIN IAW SRM 53-10-2 FIG 3A, SRM 51-30-5, 51-10-1, 51-10-2, AND 51-30-2.

Part: STRINGER — DAMAGED (BS 420-440) · airframe 41,528 hrs · 28,504 cycles

EVALUATE PREVIOUS STRINGER REPAIR AT STR 8L BETWEEN BS 420 AND 440. CUT OUT DAMAGED AREA IAW SRM 53-10-3 FIG 3, FABRICATED STRINGER SECTION FROM BAC 1498-139 AND REPAIR PLATE 1 (2EA) FROM 2024T3 0.125", PLATE 2 (4EA) FROM 2024T3 0.056", AND PLATE 3 (4EA) FROM 2024T3 0.071" IAW SRM 53-10-3 FIG 3. INSTALLED STR SECTION AND STR REPAIR IAW SRM 53-10-3 FIG 3 AT STR 8L BETWEEN BS 411 TO BS 429.

Part: SEAT TRACK — CORRODED (BS 1010-1050) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

CABIN SEAT TRACK HAS SURFACE CORROSION ON FLANGE RBL 45.5 BETWEEN BS 1010 AND 1050. REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK SECTION, AND INSTALLED IAW SRM 53-10-2 FIG 7, 51-30-5, 51-10-1, 51-10-2, AND 51-30-2 REV 103.

Part: SKIN — GOUGED (BS 620 S4-10L) · airframe 41,528 hrs · 28,504 cycles

INNER SURROUND SKIN GOUGED STA 620, STR 4L TO 10L. FABRICATED NEW INNER SKIN FROM 2024T3 0.125", AND INSTALLED NEW INNER SKIN AT AFT SECTION STA 600 TO 640 STR 4L TO 10L IAW SRM 53-10-2 FIG 3A, SRM 51-30-5, 51-10-1, 51-10- 2, AND 51-30-2.

Part: SKIN — GOUGED (ZONE 100) · airframe 41,528 hrs · 28,504 cycles

C-2 DOOR IS GOUGED ON PREVIOUS REPAIR AROUND FASTENER HEADS. REMOVED PREVIOUS REPAIR DOUBLER IAW SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER USING 2024 T-3 .080" X 6.8750" X 4" IAW SRM 52-00-3, FIG 3. INSTALLED NEW REPAIR DOUBLER IAW SRM 52-00-3, FIG 3 AND 51-30-2, REV 103, AND EA NR 7-5230-143940.

Part: SKIN — GOUGED (BS 620 S12-16L) · airframe 41,528 hrs · 28,504 cycles

INNER SURROUND SKIN GOUGED STA 620, STR 12L TO 16L. FABRICATED INNER SKIN AND DOUBLER REPAIR FROM 2024T3 0.125", AND INSTALLED INNER SKIN AND DOUBLER REPAIR PER EA 7-5330-143933.

Part: SKIN — GOUGED (BS 480 S4-10L) · airframe 41,528 hrs · 28,504 cycles

INNER SURROUND SKIN GOUGED STA 480, STR 4L TO 10L. FABRICATED NEW INNER SKIN FROM 2024T3 0.125", AND INSTALLED NEW INNER SKIN IAW SRM 53-10-2 FIG 3A, SRM 51-30-5, 51-10-1, 51-10-2, AND 51-30-2.

Part: FLOORBEAM — CORRODED (BS 950) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

CORROSION ON UPPER SURFACE OF UPPER FLANGE STA 950, FLOORBEAM TOP STRAP, LBL 25 TO LBL 45. REMOVED UPPER TEE CHORD AT STA 950 LBL 63.5 TO RBL 63.5, FABRICATED NEW TEE CHORD FROM BAC 1505-100405 7075T6, AND INSTALLED NEW UPPER TEE CHORD AT STA 950 IAW DWG 65-16338 REV B AND SRM 51-30-2.

Part: WEB — BUCKLED (HORIZONTAL STAB) · airframe 41,528 hrs · 28,504 cycles

WEB BUCKLED AT LIGHTNING HOLE - RT HORIZ STABILIZER INTERIOR BOX RIB, APPROX STAB L/E 100.63. CUT OUT DAMAGED AREA OF WEB DIM 1/4" X 1" IAW SRM 55-10-4 FIG 2 REV 103. FABRICATED WEB LIGHTNING HOLE DOUBLER FROM 2024 T3 .032" DIM 9.75" X 13.25" IAW SRM 55-10-4 FIG 2 AND 55-10-2 FIG 2 INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 REV 103

Part: SEAT TRACK — CORRODED (BS 370-480) · airframe 41,528 hrs · 28,504 cycles

SEAT TRACK CORRODED STA 370-480 LBL 45. REMOVED SEAT TRACK SECTION, FABRICATED SEAT TRACK, AND INSTALLED NEW SECTION IAW SRM 53-10-2, FIG 7, SRM 51-30-5, SRM 51-10-1, SRM 51-10-2, AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 690-740) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

SEAT TRACK CORRODED STA 690-740 LBL 45. REMOVED SEAT TRACK IAW SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK. FABRICATED SPLICER AND 2 EA ANGLES AND SPLICE PLATE IAW SRM 53-10-3, FIG 1 AND 51-30-5 TREAT AND PRIMED IAW SRM 51-10-2. INSTALLED NEW SEAT TRACK AND SPLICE ANGLES AND PLATE IAW SRM 51-30-2, REV 103.

Part: SEAT TRACK — CORRODED (BS 480-690) · airframe 41,528 hrs · 28,504 cycles

SEAT TRACK CORRODED STA 480-690 LBL 45. REMOVED SEAT TRACK, LOCATED AND DRILLED 2 EA SEAT TRACK SECTIONS FROM BAC 1520-792 7178-T6511 DIM 150" AND 60" IN LENGTH AND SPLICES FROM BAC 1503-100122 7178 T6511 DIM ( 2 EA ) 14" X 13.5" AND SPLICE STRAP FROM 7075 T6 .250" DIM 7.125" X 2" IAW SRM 53-10-5, FIG 1. INSTALLED NEW SEAT TRACK SECTION AND SPLICES IAW SRM 51-30-2, REV 103.

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

SEAT TRACK CORRODED STA 480-690 LBL 25. REMOVED SEAT TRACK AT BS 480 TO 690, LBL 25, FABRICATED NEW SEAT TRACK FROM BAC 1520-792 7178T6511, SPLICES FROM BAC 1503-100122 7178T6511, AND STRAPS FROM 7075T6, 0.250", AND INSTALLED SEAT TRACK SECTIONS, SPLICES, AND STRAPS REPAIR IAW SRM 53-10-2, FIG 7 AND 53-10-5, FIG 1.

Part: SEAT TRACK — CORRODED (BS 480-640) · airframe 41,528 hrs · 28,504 cycles

SEAT TRACK CORRODED STA 480-640 BL 0. REMOVED SEAT TRACK IAW SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK SECTION, MATERIAL USED BAC 1520-792 7178 T-6511 DIM 120" IN LENGTH IAW SRM 51-30-5 AND SRM 53-10-2 FIG 7A. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2 REV. 103.

Part: SEAT TRACK — CORRODED (BS 690) · airframe 41,528 hrs · 28,504 cycles

SEAT TRACK CORRODED, STA 690, RBL 45. REMOVED SEAT TRACK SECTION STA 480 TO 690 RBL 45, FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 7178T6511 DIM. 209.5" LONG, AND INSTALLED NEW SEAT TRACK SECTION AT BS 480 TO 690, RBL 45 IAW SRM 53-10-2 FIG 7, 51-30-5, 51-10-1, 51-10-2, AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 360-480) · airframe 41,528 hrs · 28,504 cycles

SEAT TRACK CORRODED STA 360-480, LBL 25. REMOVED SEAT TRACK SECTION BS 344 TO BS 480 LBL 25 IAW SRM 51-30-2. REMOVED SPLICE PLATE BS 460-500, LBL 25 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 7178 T6511 DIM 135.75" LONG INSTALLED SEAT TRACK SECTION AND SPLICE PLATE IAW SRM 51-30-2 AND 53-10-2, FIG 7, REV 103.

Part: SEAT TRACK — CORRODED (BS 698) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

SEAT TRACK CORRODED, STA 698, BL 0. REMOVED SEAT TRACK SECTION AT BS 600 TO 720 BL 0 IAW SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK SECTION FROM BAC 1520-792 7178 T6511 DIM 120" IN LENGTH IAW SRM 51-30-5 AND SRM 53-10-2 FIG 7A. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2 REV. 103.

Part: SEAT TRACK — CORRODED (BS 480-670) · airframe 41,528 hrs · 28,504 cycles

SEAT TRACK CORRODED, STA 480-670, RBL 25. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED 2 EA SEAT TRACK SECTIONS FROM BAC1520-792 7178 T6511, AND BAC 1520-792 7178 T6511, AND SPLICER REPAIR TO STA 630, 2EA ANGLES MAT USED BAC 1503-100122-7178, T6511. STRAP 7075-T6 .250" IAW SRM 53-10-5, FIG 1 53-10-2, FIG 7. INSTALLED SEAT TRACK SECTION AND SPLICE IAW SRM 53-10-5 FIG 1 & 51-30-2.

Part: SEAT TRACK — CORRODED (BS 690-740) · airframe 41,528 hrs · 28,504 cycles

SEAT TRACK CORRODED STA 690-740 RBL 45. REMOVED SEAT TRACK SECTION STA 690 TO 740, FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 7178T6511 DIM 172" LONG, SPLICE REPAIR FROM BAC 1503-100122 7178T6 DIM 15" LONG (2EA), AND STRAP PLATE FROM 7075T6 0.250" DIM 8.25" X 2", INSTALLED SEAT TRACK SECTION AT STA 690 TO 740 RBL 45 IAW SRM 53-10-5, FIG 1 AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 720-740) · corrosion level 2 · airframe 41,528 hrs · 28,504 cycles

SEAT TRACK CORRODED, STA 720-740, BL 0. REMOVED SEAT TRACK IAW SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK, MATERIAL USED BAC 1520-792 7178 T6511 DIM 141 1/2" IAW SRM 51-30-5 AND FEDEX P-F SRM 53-10-2 FIG 7A. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2 REV. 103.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,253 hrs · 28,277 cycles

EMERGENCY LIGHTS GO DIM IN 30 SECONDS. REPLACED BATTERIES COCKPIT O/H EMERGENCY LIGHT PACK IAW MM 33-50-101-2-0. OPS CKS GOOD.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 41,253 hrs · 28,277 cycles

EXTERNAL L1 DOOR LOWER EMERGENCY LIGHT INOP. RELAMPED ESCAPE SLIDE LIGHT, NO HELP. R & I EMERGENCY ESCAPE SLIDE LIGHT BATTERY & POWER SUPPLY IAW MM 33-50-051-2-0 . OPS CK'S NORMAL. PREMATURE REMOVAL/INSTALLATION. RELAMPED ESCAPE SLIDE LIGHT, NO HELP.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,253 hrs · 28,277 cycles

COCKPIT O/H DOOR EMERGENCY LIGHTS GO DIM AFTER 30 SEC. REPLACED BATTERIES O/H COCKPIT DOOR EMERGENCY LIGHT PACK IAW MM 33-50-101-2-0 . OPS CK'S NORMAL. REPLACED BATTERIES O/H COCKPIT DOOR EMERGENCY LIGHT PACK IAW MM 33-50-101-2-0. OPS CKS NORMAL. (CLOSED)

Part: LINE — LEAKING (HYD SYSTEM) · airframe 40,499 hrs · 27,694 cycles

LOST SYS "A" HYDRAULICS WHEN MOVING FLAPS FROM 2 DEG TO 5 DEG. HYD SYS "A" PUMP LIGHTS DID NOT ILLUMINATE. KEPT POSITIVE PRESSURE. FOUND 5/8 INCH LINE TO A SYS PRESSURE MODULE LEAKING. IPC REF 29-15-00-01G ITEM 280 LINE FROM NR 1 ENG "A" PUMP TO MODULE. QTY 1 HYD TUBE MSN 1125584. REPAIRED HYD LEAK WITH TEMPORARY FLEX LINE IAW AMM 20-10-005-8. INSTALLED HOSE. SERVICED HYD SYS "A" IAW B727 AMM 12-1 2-000-2. RAN NR 1 ENG PER JRH, "A" SYS HYD SYS OPS AND LEAKS GOOD.

Part: PRESSURE SWITCH — MALFUNCTIONED (ENGINE) · airframe 40,252 hrs · 27,517 cycles

NR 1 ENGINE SHUT DOWN IN FLIGHT DUE TO LOW PRESSURE/FILTER BYPASS LIGHT. COMPLIED WITH QRH ENGINE WINDMILLED 2 MIN PRIOR TO SHUT DOWN. OIL PRESSURE AT APPROX 40 PSI. FOUND FAULTY LOW OIL PRESS SWITCH, REMOVED AND REPLACED SWITCH IAW MM 79-34-001-4, ALSO CLEANED CONNECTORS ON LOW OIL PRESS SWITCH AND FILT BYPASS PRESS DIFF SWITCH RAN ENGINE AND PERFORMED LEAK CHECK OF SWITCHES, NO LEAKS NOTED AND LIGHT IS OPERATING NORMALLY AT THIS TIME.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 40,141 hrs · 27,406 cycles

TEST FLIGHT, LOST ALL HYD SYS A FLUID UPON RAISING LANDING GEAR. REMOVED AND REPLACED LT MLG ACTUATOR LWR HYD HOSE IAW MM 32-32-000-4. LEAK CHECK GOOD IAW MM 32-32-000-5. PART IS TRACKING LEVEL 0. CLOSED FINAL.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 40,141 hrs · 27,406 cycles

TEST FLIGHT, LOST ALL HYD SYS A FLUID UPON RAISING LANDING GEAR. REMOVED AND REPLACED LMLG ACTUATOR LOWER HYDRAULIC HOSE IAW MM 32-32-000-4. LEAK CHECK GOOD IAW MM 32-32-000-5.

Part: SUPPORT BEAM — CRACKED (SPOILER) · airframe 40,141 hrs · 27,405 cycles

LWR SIDE OF I/B SPOILER FITTING HAS MISSING AND LOOSE FASTENERS EVALUATED AND FOUND CRACK ON SPOILER SUPPORT BEAM. REPAIRED I/B SPOILER SUPPORT BEAM CRACK AT SPOILER FITTING AREA IAW FEDEX DRAWING NR: SR27-57-038 REV "C".

Part: BEAM — CRACKED (RT WING) · airframe 40,141 hrs · 27,405 cycles

RT WING T/E "J " BEAM IS CRACKED AT WBL 118 REMOVED T/E PANEL FOR ACCESS IAW SRM 51-30-2. REMOVED "J" BEAM AS REQUIRED BY SRM 51-30-2. FABRICATED NEW "J" BEAM IAW DRAWIING NR 65-21655-10 REV "J". TREATED AND PRIMED AFFECTED PARTS IAW SRM 51-10- 2. INSTALLED NEW "J" BEAM AND T/E PANEL IAW SRM 51-30-2 AND DRAWING NR 65-21655-10 REV "J".

Part: SKIN — DAMAGED (BS 480-490) · airframe 40,141 hrs · 27,405 cycles

FUSELAGE LT, STATIC PORTS AREA HAS WORN AROUND EDGES AND POSITIVE STEP HEIGHT IS ON MAX LIMITS (0.006 INCH). REMOVED FASTENERS FROM AREA IAW SRM 51-30-2. FABRICATED DOUBLER AND TRIPLER IAW EA NR 7-5330-117032. TREATED AND PRIMED DOUBLER AND TRIPLER AND AFFECTED AREA IAW SRM 51-10-2. INSTALLED REPAIR WASHERS IAW SRM 51-30-8. INSTALLED DOUBLER AND TRIPLER IAW EA NR 7-5330-117032. TRIMMED OUT STATIC PORT HOLES AND SPOT FACE ORIGINAL SKIN IAW EA NR 7-5330-117032.

Part: FLOORBEAM — DAMAGED (BS 328) · airframe 40,141 hrs · 27,405 cycles

TOOL MARK AT FLOOR SUPPORT MAIN CABIN STA 328 TOP OF FRAME APROX 11" FROM I/B EDGE OF LWR SILL. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. CUTOUT DAMAGE AREA DIM 9 1/2 PER 2 INCH IAW B727 SRM 53-10-8 FIG 9. FABRICATED FILLER MAT USED 7075T6 0.071 AND 04 EA ANGLES MAT USED 7075T6 0.071 AND 02 EA SHIMS IAW B727 SRM 53-10-8 FIG 9. TREATED AND PRIMED AFFECTED PARTS IAW B727 SRM 51-10-2. INSTALLED ALL REPAIR PARTS IAW B727 SRM 51-30-2.

Part: SKIN — CRACKED (NR 1 SLAT) · airframe 40,141 hrs · 27,405 cycles

NR 1 SLAT TRAILING EDGE IS GOUGED AND CRACKED AT I/B HOOK WS 716 TRIMMED OUT DAMAGED AREA DIM 1/2 PER 1/2 IAW SRM 57-50-3 FIG 10. FABRICATED REPAIR DOUBLER MAT USED 7075T6 0.125, DIM 4 INCH PER 3 1/2 INCH IAW SRM 57-50-3 FIG 10. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR PART IAW SRM 51-30-2.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 40,141 hrs · 27,405 cycles

LT WING O/B FORE FLAP I/B SEQUENCE CARRIAGE HAS ELONGATED BOLT HOLES AT AFT END WBL 348 REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER IAW SRM 57-50-2 FIG 4, 57-50-4 FIG 7. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.

Part: SKIN — CRACKED (BS 1214) · airframe 40,141 hrs · 27,405 cycles

CRACK TAIL SKID CUTOUT EXTERIOR SKIN STA 1214 TRIMMED OUT DAMAGED AREA DIM 1/4 PER 1/2 INCH IAW B727 SRM 53-10-3 FIG 1. FABRICATED REPAIR DOUBLER MAT USED 2024T3 0.050 IAW B727 SRM 53-30-2 FIG 3 AND 53-30-3 FIG 1. TREATED AND PRIMED AREA AND REPAIR PART IAW B727 SRM 51-10-2. INSTALLED COUNTERSINK WASHER IAW B727 SRM 51-30-8. INSTALLED REPAIR DOUBLER IAW B727 SRM 51-30-2.

Part: SKIN — CORRODED (BS 662 S28L) · corrosion level 2 · airframe 40,141 hrs · 27,405 cycles

FWD CARGO COMPARTMENT, SKIN UNDER STRINGER 28L IS CORRODED AT STA 662 JUST I/B OF EXISTING REPAIR CUTOUT. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-10-6 AND 53-30-1 FIG 1. REMOVED EXISTING REPAIR IAW SRM 51-30-2. CUTOUT DAMAGED AREA DIM 5" PER 1 3/4' AND FABRICATED NEW DOUBLER IAW SRM 53-30-3 FIG 1. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER AT FWD CARGO COMPARTMENT SKIN STRINGER 28L , STA 662 IAW SRM 53-30-3 FIG 1 AND 51-30-2.

Part: STRINGER — CORRODED (BS 720D) · corrosion level 2 · airframe 40,141 hrs · 27,405 cycles

FWD CARGO COMPARTMENT, STRINGER 27R CORRODED JUST FWD OF STA 720D APPROX 12 INCHES. REMOVED WEB IAW SRM 51-30-2. REMOVED DAMAGED AREA OF STRINGER IAW SRM 53-10-3. FABRICATED STRINGER SECTION AND 2 SPLICES IAW SRM 53-10-3 FIG 1. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 53-10-3 FIG 1. REINSTALLED WEB IAW SRM 51-30-2.

Part: STRINGER — CORRODED (BS 690 S27R) · corrosion level 2 · airframe 40,141 hrs · 27,405 cycles

FWD CARGO COMPARTMENT, CORROSION ON STR AT BS 690, STR 27R. REMOVED CORROSION IAW SRM 51-10-6 AND FOUND OUT OF LIMITS IAW SRM 53-10-1. CUTOUT DAMAGED AREA DIM 11" AND FABRICATED NEW STRINGER SECTION AND 02 EA SPLICES IAW SRM 53-10-2 FIG 9 AND 53-10-3 FIG 1. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS AT FWD PIT STRINGER 27R AT STA 690 IAW SRM 53-10-3 FIG1.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 40,141 hrs · 27,405 cycles

CRACK ON DOUBLER AT RIGHT O/B FORE FLAP BY O/B TRUCK ATTACH FITTING AT WS 629. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED REPAIR PARTS, IAW SRM 57-50-4 FIG 7 AND 457-50-2 FIG 4. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: STRINGER — CORRODED (BS 720D S27R) · corrosion level 2 · airframe 40,141 hrs · 27,405 cycles

FWD CARGO COMPARTMENT, STRINGER 27R CORRODED JUST FWD OF STA 720D APPROX 12 INCHES. REMOVED WEB IAW SRM 51-30-2. CUTOUT DAMAGED AREA OF STRINGER IAW SRM 53-10-3. FABRICATED STRINGER SECTION AND 2 SPLICES IAW SRM 53-10-3 FIG1. TREATED AND PRIMED REPAIR PARTS AND AREA IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 53-10-3 FIG 1. REINSTALLED WEB IAW SRM 51-30-2.

Part: SKIN — CRACKED (BS 720C-720D) · airframe 40,141 hrs · 27,405 cycles

CRACK AT FUSELAGE SKIN FWD OF STA 720D AND O/B OF STR 27R ABOVE RT RAM AIR DUCT REMOVED CTR FAIRING AT STA 720D, AIR DUCT AND 2 SUPPORT BRACKETS FOR ACCESS IAW SRM 51-30-2. CUT OUT DAMAGED AREA DIM 4" PER 3". FABRICATED REPAIR DOUBLER AND 2 REPAIR FILLERS IAW SRM 53-30-3 FIG 1 AND 53-30-2 FIG 3. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 53-30-1 FIG 1. REINSTALLED REMOVED PARTS IAW SRM 51-30-2.

Part: STRINGER — CORRODED (BS 1010-1039) · corrosion level 2 · airframe 40,141 hrs · 27,405 cycles

CORROSION INSIDE CHANNEL AND AT ATTACHING RIVETS STR 27L STA 1010 TO STA 1039 CUT OUT DAMAGED SECTION IAW SRM 53-10-31 FIG 1. FABRICATED 2 STRINGER SECTIONS AND 3 SPLICE SECTIONS IAW SRM 53-10-3 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED 2 STRINGERS AND 3 SPLICES IAW SRM 51-30-2.

Part: SKIN — CORRODED (BS 720D S30L) · corrosion level 2 · airframe 40,141 hrs · 27,405 cycles

FUSELAGE SKIN HAS CORROSION BY CARGO HEAT OUTFLOW VALVE FLANGE AT STA 720D AND STR 30 REMOVED CENTER FAIRING AT STA 720D AIR DUCT AND 02 EA SUPPORT BRACKETS FOR ACCESS IAW SRM 51-30-2. CUTOUT DAMAGED AREA DIM 4 INCH PER 3 INCH. FABRICATED REPAIR DOUBLER AND 2 REPAIR FILLERS IAW SRM 53-30-3 FIG 1, AND 53-30-2 FIG 3. TREATED AND PRIMED PARTS AND AREA IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 53-30-1 FIG 1. REINSTALLED REMOVED PARTS FOR ACCESS IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 380-420) · corrosion level 2 · airframe 40,141 hrs · 27,405 cycles

MAIN CARGO COMPARTMENT, CORROSION ON SEAT TRACK RBL 45 STA 380 STA 420 REMOVED 9G BULKHEAD AND ATTACHMENT PARTS FOR ACCESS IAW SRM 51-30-2 AND VENTURA SRM. REMOVED FLOOR PANELS IAW SRM 53-20-012. REMOVED DAMAGED SEAT TRACK AND FABRICATED NEW SEAT TRACK AND INSTALLED IAW SRM 53-10-2 FIG 7, P-F SRM 53-10-2 FIG 7A AND SRM 51-30-2. REINSTALLED 9G BULKHEAD AND ATTACHMENT PARTS, FLOOR PANELS IAW SRM 51-30-2.

Part: SKIN — DAMAGED (BS 1010 S22-23L) · airframe 40,141 hrs · 27,405 cycles

FUSELAGE LT SIDE SKIN BULGE AT STA 1030 AND STA 1010 AND STR 22L - STR 23L CUTOUT DAMAGED AREA DIM 8" PER 4 3/4" IAW SRM 53-30-3 FIG 3. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3 AND 53-30-2 FIG 2. TREATED AND PRIMED DOUBLER AND AREA IAW SRM 51-10-2. INSTALLED REPAIR WASHER AND REPAIR PARTS IAW SRM 51-30-8 AND 51-30-2.

Part: SKIN — CORRODED (BS 720F-740) · corrosion level 2 · airframe 40,141 hrs · 27,405 cycles

FWD CARGO COMPARTMENT, STR 26R IS CORRODED BETWEEN STA 720F AND STA 740 WITH EXFOLIATION REMOVED RT PACK CHECK VALVE AND DUCT IAW FEDEX MM 21-20-004 AND SRM 51-30-2. CUTOUT DAMAGED AREA DIM 10 1/2 INCH LONG. FABRICATED REPAIR FILLER FROM BAC1498-147 AND REPAIR SPLICE FROM BAC1498-131 IAW B727 SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-10-3 NAD 51-30-2. REINSTALLED RT PACK CHECK VALVE AND DUCT IAW B727 MM 21-20-004 AND SRM 51-30-2. LEAK AND OPS CHECKS GOOD.

Part: SKIN — CORRODED (BS 660-680) · corrosion level 2 · airframe 40,141 hrs · 27,405 cycles

FWD CARGO COMPARTMENT, FUSE SKIN IS CORRODED STR 28L FROM STA 660 TO STA 680 WITH EXFOLIATION CUTOUT DAMAGED AREA DIM 12.9 INCH AND FABRICATED REPAIR FILLER AND 2 REPAIR SPLICES IAW SRM 53-10-3 FIG 1. TREATED AND PRIMED REPAIR PARTS AND AREA IAW SRM 51-10-2. INSTALLED REPAIR PARTS AT STRINGER 28L BTW STA 660 NAD STA 680 IAW B727 SRM 53-10-3 FIG 1 AND SRM 51-30-2.

Part: SPAR — CRACKED (RT WING TE FLAP) · airframe 40,141 hrs · 27,405 cycles

RT WING O/B MID FLAP AFT SPAR, UPPER CHORD IS CRACKED AT WBL 332 REMOVED AND REPLACED RT O/B MIDFLAP ASSY IAW FX B727-200 MM 27-51-011-4. OPS CHECK GOOD IAW FX B727-200 MM 27-51-011-4 AND 27-51-000-5.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 40,141 hrs · 27,405 cycles

LT WING O/B FORE FLAP L/E REPAIR DOUBLER IS CHAFED (DAMAGED) AT WS 440 REMOVED PREVIOUS REPAIR DOUBLER IAW SRM 51-30-2. FABRICATED NEW DOUBLER IAW SRM 57-50-2 FIG 4 AND SRM 57-50-4 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.

Part: SKIN — DENTED (BS 1130 S21-22L) · airframe 40,141 hrs · 27,405 cycles

FUSELAGE LT SIDE DENT AT FWD OF STA 1130 STR 22L AND STR 21L CUTOUT DAMAGE AREA DIM CUTOUT 4 3/4 INCH PER 2 7/8 IAW SRM 53-30-3 FIG 3. FABRICATED DOUBLER REPAIR & FILLER IAW SRM 53-30-2 FIG 2, 53-30-3 FIG 3. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR WASHERS IAW SRM 51-30-8. INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 40,015 hrs · 27,287 cycles

ON SHORT FINAL AT EWR ALL 3 CREW MEMBERS COULD SEE AND SMELL SMOKE IN COCKPIT. ONLY LEFT PACK WAS ON AT THE TIME, WITH NR 1 AND NR 3 BLEEDS OPEN. RAN LT PACK WITH APU BLEED, NO SMELL OR SMOKE PRESENT. RAN NR 1 WITH LT PACK, NO SMELL. INSPECTED LEFT ACM FOR PROPER OIL LEVEL AND FOUND ALL INDICATIONS OF LT PACK TO BE NORMAL. WHILE T/S NOTICED WEATHER IND C/B POPPED, C/B WILL NOT RESET.

Part: WARNING LIGHT — ILLUMINATED · airframe 39,667 hrs · 27,011 cycles

AFTER T/O AMBER AFT AIRSTAIR LIGHT ILLUMINATED. RAN QRH. AFTER LANDING LIGHT WENT OUT. REPLACED THE AFT AIRSTAIR SWITCH ACTUATOR PER 727-200 MM 52-62-001-5, 52-70-001-5,OPS C. REPLACED ACTUATOR. COMPLIED WITH MTSI 52-62-9902.

Part: WARNING LIGHT — FALSE ACTIVATION (AIRSTAIR DOOR) · airframe 39,558 hrs · 26,925 cycles

AFT AIRSTAIR LIGHT ILLUMINATED IN FLIGHT AT FL330. LIGHT WENT OUT AT 10000 FT ENGINE ANTI-ICE WAS OPEN WHEN AFT AIRSTAIR LIGHT WAS ON. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C . 10-30-07

Part: PANEL — MISSING (NR 1 PYLON) · airframe 38,239 hrs · 25,866 cycles

FOUND NR 1 PYLON FWD BLOWOUT PANEL MISSING AFTER TEST FLIGHT. REPLACED MISSING PANEL AND CORRECTED DUCT LEAK AT PRE-COOLER.

Part: PANEL — MISSING (NR 1 NACELLE) · airframe 38,239 hrs · 25,866 cycles

NR 1 ENGINE PYLON MISSING FWD BLOWOUT PANEL. INSTALLED NEW BLOW OUT PANEL IN NR 1 ENGINE PYLON PANEL NR 5402 IAW FED EX MM 54-30-011-8.

Part: SWITCH — OUT OF ADJUST (PAX DOOR) · airframe 38,239 hrs · 25,866 cycles

FWD ENTRY DOOR LIGHT CAME ON DURING FLIGHT. ADJUSTED FWD ENTRY DOOR WARNING SWITCH REF MM 52-70-001-5. SWITCH FUNCTIONAL, TESTED OK. PRESSURIZED AIRCRAFT TO SIMULATE FLIGHT LOADS AT 5.5. PSI, SWITCH OPERATION REMAINED NORMAL.

Part: STRUCTURE — NICKED (RUDDER) · airframe 38,235 hrs · 25,857 cycles

UPPER RUDDER TRAILING EDGE HAS NUMEROUS NICKS RIGHT HAND. REMOVED AND REPLACED FAIRING STRIP RT SIDE PER FED EX EA 7-5540-99063.

Part: STRUCTURE — DENTED (RUDDER) · airframe 38,235 hrs · 25,857 cycles

UPPER RUDDER TRAILING EDGE DENTED LEFT HAND LOWER 6 INCHES FROM BOTTOM. *S/D* REMOVED AND REPLACED FAIRING STRIP LOWER LT SIDE PER FED EX EA 7-5540-99063.

Part: STRUCTURE — NICKED (RUDDER) · airframe 38,235 hrs · 25,857 cycles

UPPER RUDDER TRAILING EDGE HAS NUMEROUS NICKS LEFT HAND. *S/D* REMOVED AND REPLACED FAIRING STRIP UPPER LT SIDE PER FED EX EA 7-5540-99063.

Part: FLOORBEAM — DAMAGED (BS 1130) · airframe 38,235 hrs · 25,857 cycles

AFT CARGO BAY BS 1130 FLOORBEAM VERTICAL WEB CUT INTO A BL 0 VERTICAL ATTACH BRACKET. REPAIRED PER FED EX EA 7-5310-99474.

Part: SPAR — CHAFED (VERTICAL STAB) · airframe 38,235 hrs · 25,857 cycles

VERTICAL STAB JACKSCREW COMPARTMENT LWR MID SPAR CHORD CHAFED JUST FWD OF STAB SLIDING SEAL, FIN STA 230, RT SIDE. *S/D* REPAIRED PER FED EX EA 7-5330-96617.

Part: ATTACH FITTING — CORRODED (NR 8 FLAP TRACK) · airframe 38,235 hrs · 25,857 cycles

NR 8 FLAP TRACK FWD FITTING IS CORRODED. *S/D* REPAIRED PER FED EX EA 7-5710-96574.

Part: SPAR — CHAFED (VERTICAL STAB) · airframe 38,235 hrs · 25,857 cycles

VERTICAL STAB JACKSCREW COMPARTMENT LWR MID SPAR CHORD CHAFED JUST FWD OF STAB SLIDING SEAL, FIN STA 230, LT SIDE. *S/D* REPAIRED PER FED EX EA 7-5530-96617.

Part: ATTACH FITTING — CORRODED (NR 1 FLAP TRACK) · airframe 38,235 hrs · 25,857 cycles

NR 1 FLAP TRACK FWD FITTING I/B FACE IS CORRODED. *S/D* REPAIRED PER FED EX EA 7-5710-7-96574.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,235 hrs · 25,857 cycles

EXTERNAL DOUBLER REPAIR APPROX 12.75 X 26.75 INCHES, RT FUSELAGE STA 1010 STRINGER 26R TO 26L REPAIR REQUIRES EVALUATION FOR MAJOR MINER DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. *S/D* REPAIRED PER FED EX EA 7-5330-96615.

Part: SKIN — CORRODED (BS 680 S27R) · airframe 38,235 hrs · 25,857 cycles

FOUND BS 680 ABOVE STR 27 RT FUSELAGE SKIN BUT SPLICE IS CORRODED INSIDE FWD CARGO BAY. REPAIRED SKIN AT BS 680, AT STA 27RT PER FED EX EA 7-5310-99057.

Part: SKIN — GOUGED · airframe 38,235 hrs · 25,857 cycles

REWORK ON N00140 REQUIRED. LWR LOBE EXTERNAL SKIN, SKIN AFT OF FWD CARGO DOOR HAS GRAVEL GOUGES BETWEEN STR 23R AND 25R. REWORK REQUIRED BECAUSE BLENDING EXTENDS OVER FASTENERS AND FASTENER HOLES. THIS IS NOT ALLOWED PER SRM 53-30-1. *S/D* REPAIRED PER FED EX EA 7-5330-98568.

Part: SKIN — DENTED (RUDDER) · airframe 38,235 hrs · 25,857 cycles

WHILE WORKING LWR RUDDER CARD N01322 FOUND DENT AT 2 INCHES FROM LOWER END AT RT CENTER SKIN AREA. *S/D* REPAIRED LOWER RUDDER PER SRM 55-40-1.

Part: SKIN — DENTED (BS 1344) · airframe 38,235 hrs · 25,857 cycles

DENT IN EXTERNAL FUSELAGE SKIN IN LEFT HAND UPPER TORQUE BOX AT BS 1344 JUST BELOW VERTICAL STABILIZER. *S/D* INSTALLED REPAIR DOUBLER IAW SRM 53-30-3.

Part: SHEAR TIE — CORRODED (BS 1166) · airframe 38,235 hrs · 25,857 cycles

AFT CARGO BAY SHEAR TIE IS CORRODED BS 1166 RBL 3. *S/D* REMOVED AND REPLACED SHEAR TIE BS 1166, RBL 3 IAW SRM 53-10-4 FIG 13.

Part: BEAM — DAMAGED (LT MLG ATTACH) · airframe 38,235 hrs · 25,857 cycles

WHILE WORKING N01478, FOUND MECHANICAL DAMAGE AROUND UPPER I/B BRACKET ATTACH FASTENER ON FWD FACE OF LT MLG BEAM, JUST AFT OF THE MAIN GEAR STRUT. *S/D* REPAIRED PER FED EX EA 7-5710-96608.

Part: FLOORBEAM — MISDRILLED (BS 720D) · airframe 38,235 hrs · 25,857 cycles

WHILE WORKING ON ATTACHING L-ANGLE FOUND FLOOR BEAM AT BS 720D,WL 208, LBL 64 WITH MISDRILLED HOLE. REMOVED DAMAGE ON FLOORBEAM BS 720D, WL 208, LBL 64 AND REPAIRED IAW FED-EX SR 27-53-034.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,235 hrs · 25,857 cycles

EXTERNAL DOUBLER REPAIR APPROX 8.5" BY 6.5", FUSELAGE STA 365 WL 218. REPAIR REQUIRES EVALUATION FOR MAJOR MINER DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED PER SRM 53-30-3, SRM 51-30-2 MAJOR REPAIR.

Part: REPAIR — NONE · airframe 38,235 hrs · 25,857 cycles

N01048 LOWER FWD CARGO COMP. FLOOR FRAME REPAIR FUSELAGE STA. 560 LBL 5. REPAIR REQUIRES EVALUATION FOR MAJOR MINER DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ** SD ** COMING REPAIRED FRAME PWR SRM 51-40-3.

Part: WEB — CORRODED (BS 720C) · airframe 38,235 hrs · 25,857 cycles

CORROSION ON WEB BS 720C PLUS 13 LBL 67 WL 208. REMOVED AND REPLACED WEB PER SRM 53-10-02.

Part: REPAIR — NONE (FUSLEAGE) · airframe 38,235 hrs · 25,857 cycles

EXTERNAL DOUBLER REPAIR LEFT HORIZONTAL STAB UPPER T/E PANEL, APPROX 4 X 4 INCHES. REPAIR REQUIRES EVALUATION FOR MAJOR MINER DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.

Part: SKIN — PUNCTURED (BS 680) · airframe 38,235 hrs · 25,857 cycles

WHILE WORKING FEDEX CARD N01048 FOUND SKIN PUNCTURE BS 680 PLUS 10 INCHES ABOVE STR 25L. *S/D* REMOVED DAMAGE FROM SKIN BS 680 PLUS 10 INCHES ABOVE STR 25L, FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-3, FIG 1.

Part: FLOORBEAM — MAINT ERROR (BS 400) · airframe 38,235 hrs · 25,857 cycles

DOUBLE HOLE BS 400 RBL 12.5 WL 208. *S/D* REMOVED DAMAGED AREA ON FLOORBEAM UPPER CHORD 8.5 INCHES LONG BY 1 INCH WIDE. FABRICATED & INSTALLED REPAIR IAW SRM 51-30-2, 53-10-8.

Part: BEAM — CRACKED (SPOILER) · airframe 38,235 hrs · 25,857 cycles

CRACK AT LEFT SPOILER BEAM, I/B END. *S/D* REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED SAME IAW FED EX EA 7-5710- 96597.

Part: WEB — CORRODED (BS 720E) · airframe 38,235 hrs · 25,857 cycles

CORROSION ON WEB BS 720E 4 RBL 66 WL 208. REMOVED AND REPLACED WEB AT BS 720E 4 RBL 66 WL 208 IAW SRM 51-30-2.

Part: CREASE BEAM — MISDRILLED (BS 720E) · airframe 38,235 hrs · 25,857 cycles

WHILE WORKING ON ATTACHING L-ANGLE FOUND CREASE BEAM WEB AT BS 720E, WL 208, LBL 64 WITH MISSED DRILLED HOLE. *S/D* REMOVED AND REPLACED CREASE BEAM WEB BS 720D TO 720E, LBL 64, WL 208 IAW SRM 51-30-2.

Part: CREASE BEAM — MISDRILLED (BS 720F) · airframe 38,235 hrs · 25,857 cycles

WHILE WORKING ON ATTACHING L-ANGLE FOUND CREASE BEAM WEB AT BS 720F, WL 208, LBL 64 WITH MISDRILLED HOLE. *S/D* REMOVED AND REPLACED CREASE BEAM WEB AT BS 720E TO 720F, LBL 64, WL 208 IAW SRM 51-30-2.

Part: CREASE BEAM — MISDRILLED (N/A) · airframe 38,235 hrs · 25,857 cycles

WHILE WORKING ON ATTACHING L-ANGLE FOUND CREASE BEAM WEB AT BS 720F 16, WL 208, LBL 64 WITH MISDRILLED HOLE. *S/D* REMOVED AND REPLACED CREASE BEAM WEB AT BS 720F TO 740, LBL 64, WL 208 IAW SRM 51-30-02.

Part: SILL — CORRODED (BS 600) · airframe 38,235 hrs · 25,857 cycles

WEB AT FWD CARGO DOOR SILL BS 600, BELOW FLOOR SUPPORT HAS CORROSION. *S/D* REMOVED AND REPLACED WEB AT FWD CARGO DOOR SILL BS 600 BELOW FLOOR SUPPORT IAW SRM 51-30-2, 51-20-1.

Part: STRINGER CLIP — DAMAGED (BS 1090) · airframe 38,235 hrs · 25,857 cycles

STRINGER CLIP AT BS 1090 AT STR 1 IS MISSING ALL FASTENERS COMMON TO FRAME. INSTALLED FASTENERS IN STR CLIP PER SRM 51-30-2.

Part: STRINGER — TOOL DAMAGE (BS 1090) · airframe 38,235 hrs · 25,857 cycles

REWORK REQUIRED DUE TO DRILL STARTS IN WEB OF STR AT STR CLIP INSTALLED AT BS 1090 STR 1. REPAIRED PER FED EX EA 7-5310-96616.

Part: REPAIR — MISINSTALLED (FUSELAGE) · airframe 38,235 hrs · 25,857 cycles

EXTERNAL DOUBLER REPAIR APPROX 7 X 6 INCH STA 1223 AFT OF PNEUMATIC SERVICE PANEL. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. *S/D* EVALUATED REPAIR DOUBLER AND FOUND TO BE NOT ACCORDING TO THE SRM. REMOVED OLD REPAIR. FABRICATED NEW REPAIR DOUBLER. ALODINED, PRIMED AND INSTALLED THE NEW REPAIR DOUBLER IAW ER 06-1172 & FED EX EA 7-5330-96590 (PART 1).

Part: REPAIR — MISINSTALLED (FUSELAGE) · airframe 38,235 hrs · 25,857 cycles

EXTERNAL UPPER FUSELAGE LEFT SIDE STA 393 WL 272 CIRCULAR DENT APPROX 1 X 1 INCH. REPAIR REQUIRES EVALUATION FOR MAJOR MINER DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. CIRCULAR DENT APPROX 1 X 1 INCH STA 393 WL 272 WAS NOT IAW APPROVED DATA. CUT OUT DAMAGED AREA & FABRICATED & INSTALLED REPAIR DOUBLER IAW FED-EX EA 7-5330-98580. THIS IS A MAJOR REPAIR.

Part: FLOORBEAM — DAMAGED (BS 950A) · airframe 38,235 hrs · 25,857 cycles

FLOORBEAM BS 950A, HAS MECHANICAL DAMAGE AT WL 207, LBL 1 (AFT SIDE OF VERTICAL FLANGE). REPAIRED BS 950A FLOORBEAM, WL 207, LBL 1 PER FED EX EA 7-5310-98584.

Part: SKIN — GOUGED (BS 460-560) · airframe 38,235 hrs · 25,857 cycles

EXTERNAL LWR LOBE SKIN BS 460 TO 560 BETWEEN STR 23R & 25R, SKIN HAS NUMEROUS GOUGES. *S/D* ACCOMPLISHED FED EX EA 7-5330-98569.

Part: REPAIR — MISINSTALLED (FRAME) · airframe 38,235 hrs · 25,857 cycles

LOWER FWD CARGO COMP FLOOR FRAME REPAIR FUSELAGE STA 580 RBL 3. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. *S/D* EVALUATED FRAME REPAIR AT STR 580, RBL 3. REPAIR FOUND NOT IN ACCORDANCE WITH SRM 51-10-1. REPAIRED FRAME IAW SRM 51-40-3.

Part: SUPPORT FITTING — CORRODED (NLG) · airframe 38,235 hrs · 25,857 cycles

NLG LEFT UPPER HALF TRUNNION RACE SUPPORT FITTING HAS CORROSION AND GOUGED IN BORE. *S/D* LEFT NLG UPPER HALF TRUNNION RACE SUPPORT FITTING RE-WORKED ON OSS WORK ORDER 26594 IAW SRM 53-40-01.

Part: SUPPORT FITTING — CORRODED (NLG) · airframe 38,235 hrs · 25,857 cycles

RIGHT NLG TRUNNION SUPPORT ASSY, UPPER AND LOWER FITTING BEARING RACE BORES HAVE CORROSION. *S/D* CORROSION RIGHT NLG UPPER AND LOWER TRUNNION FITTING BEARING RACES RE-WORKED ON OSS WORK ORDER 26594 IAW SRM 53-40-01.

Part: SHEAR TIE — CORRODED (BS 950C) · airframe 38,235 hrs · 25,857 cycles

AFT CARGO BAY, CORROSION ON SHEAR TIE BS 950C BETWEEN LEFT KEEL BEAM AND LBL 0.

Part: REPAIR — UNKNOWN (BS 1050) · airframe 38,235 hrs · 25,857 cycles

EXTERNAL DOUBLER REPAIR APPROX 8 X 12 INCHES. LT AFT FUSELAGE STA 1050 STRINGER 19L TO 20L. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ALL WORK ACCOMPLISHED IAW FED EX EA 7-5330-96607.

Part: FAILSAFE — DAMAGED (BS 950C) · airframe 38,235 hrs · 25,857 cycles

FOUND FAIL SAFE SEVERED AT BS 950C FRAME, BL 0.

Part: FLOORBEAM — CORRODED (BS 720) · airframe 38,235 hrs · 25,857 cycles

CORROSION ON FLOORBEAM LWR FLANGE BS 720 LBL30-RBL37. REPLACED WITH NEW FLOOR BEAM PER SRM 51-10-2, SRM 51-30-5 & 51-30-2.

Part: SHEAR TIE — CORRODED (BS 720) · airframe 38,235 hrs · 25,857 cycles

BS 720 STR 28 LT TO STR 28 RT FRAME TO SKIN ATTACH STRUCTURE IS CORRODED. *S/D* REMOVED AND REPLACED FRAME TO SKIN ATTACH STRUCTURE STA 720 STR 28L TO STR 28R IAW SRM 53-10-4 AND SRM 51-30-2.

Part: ANGLE — DAMAGED (BS 870) · airframe 38,235 hrs · 25,857 cycles

MAIN WHEEL WELL RBL-8 BS-870 WL-150 CORNER ANGLE ON AFT SIDE OF BS 870 DAMAGED. REPARIED DAMAGED ANGLE PER SRM 51-30-2.

Part: FRAME — DENTED (BS 1010) · airframe 38,235 hrs · 25,857 cycles

BS 1010, STR 25 - STR 26L FRAME AT BS 1010, STR 25L-26L IS DENTED. REPAIRED FRAME WITH DOUBLER PER SRM 51-40-3.

Part: STRINGER CLIP — CRACKED (BS 400) · airframe 38,235 hrs · 25,857 cycles

STA 400 STR 7L, STR CLIP IS CRACKED. REMOVED AND REPLACED CRACKED STRINGER CLIP BS 400 STR 7L PER SRM 51-30-2. ITEM INSPECTED NOT ACCEPTED, SEE N01412 MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 950D) · airframe 38,235 hrs · 25,857 cycles

AFT CARGO BAY, CORROSION IN AND AROUND NUT PLATE HOLES ON LWR CHORD OF BS 950D FLOORBEAM, BL 0 - LBL 45, WL 200. *S/D* REPAIRED BS 950D FLOORBEAM LWR CHORD BL 0 - LBL 45 IAW SRM 53-10-8 FIG 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,235 hrs · 25,857 cycles

AFT CARGO BAY, CORROSION ON BS 1148 FLOORBEAM LWR CHORD AT NUT PLATE HOLES RBL 25 - LBL 45, WL 200. *S/D* REPAIRED BS 1148 FLOORBEAM LWR CHORD RBL 3 - RBL 20 AND LBL 1 - LBL 32 IAW SRM 53-10-8 FIG 2.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 38,235 hrs · 25,857 cycles

EXISTING EXTERNAL REPAIR AT BS 393 WL 228 APPROX 16.5 X 9.5 INCH REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED PER EA 7-5330-98567

Part: STRINGER CLIP — DAMAGED (BS 400) · airframe 38,235 hrs · 25,857 cycles

STRINGER CLIP AT BS 400 STR 7 LT HAS MECHANICAL DAMAGE. REMOVED AND REPLACED STRINGER CLIP AT BS 400 STR 7 LT PER SRM 51-30-2, 51-30-5, 51-30- 6.

Part: SHEAR TIE — DAMAGED (BS 1148) · airframe 38,235 hrs · 25,857 cycles

TRANSFERED FROM CARD N01315, ITEM 7 OF JPF. UPON INSTALLATION OF FASTENERS FOUND DAMAGE ON AFT SIDE OF SHEAR TIE. REMOVED & REPLACED SHEAR TIE, BS 1148 BETWEEN STR 25R & 26R PER SRM 51-30-2.

Part: UNKNOWN — MISDRILLED (BS 600) · airframe 38,235 hrs · 25,857 cycles

BS 600 STR 18 LT HAS ONE DRILL START AND ONE MISSING FASTENER. *S/D* CUT OUT DAMAGED STR 18 LT BS 651 - 670, REPAIRED STR PER SRM 53-10-3.

Part: SHEAR TIE — CORRODED (BS 700) · corrosion level 2 · airframe 38,235 hrs · 25,857 cycles

BS 700 STR 28 RT SHEAR TIE IS CORRODED. *S/D* REPLACED SHEAR TIE AT BS 700 STR 28 RT IAW SRM 51-30-2 AND 51-30-5.

Part: SHEAR TIE — CORRODED (BS 680) · airframe 38,235 hrs · 25,857 cycles

BS 680 BETWEEN STR 28RT AND STR 28LT SHEAR TIE IS CORRODED. *S/D* REPAIRED SHEAR TIE BS 680 BETWEEN STR 28 RT AND STR 28 LT IAW SRM 53-10-4.

Part: SHEAR TIE — CORRODED (BS 1050) · airframe 38,235 hrs · 25,857 cycles

CORROSION ON SHEAR TIE BS 1050, STR 26L - 27L. *S/D* REMOVED AND REPLACED SHEAR TIE IAW SRM 51-30-2 AND SRM 51-10-2.

Part: FLOORBEAM — CORRODED (BS 1130) · airframe 38,235 hrs · 25,857 cycles

AFT CARGO BAY, CORROSION ON BS 1130 FLOORBEAM LWR CHORD AT NUT PLATE HOLES RBL 65 - LBL 65, WL 200. REPAIRED DAMAGED AFT CARGO BAY FLOORBEAM, BS 1130, LOWER CHORD, RBL 45 TO LBL 45, WL 200 PER FED-EX EA 7-5310-99474

Part: SKIN — TOOL DAMAGE (BS 365) · airframe 38,235 hrs · 25,857 cycles

FOUND STA 365 ABOVE STR 5R (2) DRILL STARTS ON INTERIOR SKIN.

Part: SKIN — CHAFED (BS 720D) · airframe 38,235 hrs · 25,857 cycles

FOUND CHAFING ON EXTERNAL FUSELAGE SKIN LAP STR 19R BS 720D PLUS 13. REPAIRED CHAFING ON EXTERNAL FUSELAGE SKIN LAP STR 19R BS 720D PLUS 13 IAW SRM 53-30-3.

Part: SKIN — TOOL DAMAGE (BS 365) · airframe 38,235 hrs · 25,857 cycles

FOUND STA 365 ABOVE STR 3R, DRILL START ON INTERIOR SKIN.

Part: STRUCTURE — DAMAGED (RUDDER) · airframe 38,235 hrs · 25,857 cycles

FOUND LOWER RUDDER RT, T/E HAS SEVERAL AREAS OF NICK DAMAGE. REPAIRED PER FED EX EA 7-5530-96603.

Part: SUPPORT FITTING — CRACKED (BS 600) · airframe 38,235 hrs · 25,857 cycles

FOUND FITTING AT FWD CARGO DOOR SILL BS 600, BELOW FLOOR SUPPORT IS CRACKED.

Part: FRAME — DAMAGED (BS 660) · airframe 38,235 hrs · 25,857 cycles

FOUND BS 660 ABOVE STR 26 LT FRAME HAS DOUBLED HOLE. REPAIRED FRAME IAW SRM 51-40-03.

Part: FLOORBEAM — CORRODED (BS 1070) · airframe 38,235 hrs · 25,857 cycles

FOUND BS 1070 FLOORBEAM IS CORRODED AT NUT PLATE HOLES LBL 65 - RBL 65, WL 201. REPAIRED OUT OF LIMITS AREA AT STA 1070 W/L 201 RBL 48 IAW SRM 53-10-8, ALL OTHER AREAS FOUND TO BE IN LIMITS IAW SRM 53-10-1.

Part: TEE FITTING — CORRODED (BS 740) · airframe 38,235 hrs · 25,857 cycles

FOUND TEE FITTING CORRODED STA 740 RBL 4 CORROSION ON LOWER EDGE OF BULKHEAD. REPLACED BULKHEAD LOWER CHORD PER SRM 51-30-5 AND 51-30-2.

Part: SUPPORT FITTING — CORRODED (BS 607) · airframe 38,235 hrs · 25,857 cycles

WHILE WORKING N01255 FOUND SUPPORT FITTING CORRODED AT FWD CARGO DOOR THRESHOLD BS 607.

Part: WEB — CORRODED (BS 720A-720B) · corrosion level 2 · airframe 38,235 hrs · 25,857 cycles

FOUND CORROSION ON WEB BS 720A-720B LBL 67 WL 208. REMOVED CORROSION ON WEB ON 720A-B BY 8"X4"X .007". FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED, ALODINED, PRIMED, AND INSTALLED IAW SRM 53-10-1, SRM 53-30-02 SRM 51-10-2 USING LOT# 664728 7075-T6. MINOR REPAIR

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 38,235 hrs · 25,857 cycles

STA 400 STR 8L, DRILL STARTS ON FRAME WEB. DRILL STARTS STA 400 STR 8L ON FRAME WEB FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE, INSTALLED REPAIR ON FRAME REF SRM 53-10-4 FOUND TO BE A MAJOR REPAIR.

Part: DOUBLER — UNKNOWN (FUSELAGE) · airframe 38,235 hrs · 25,857 cycles

EXTERNAL DOUBLER REPAIR APPROX 9 X 9 INCH, LT LWR FUSELAGE STA 680 TO 690 STRINGER 28L REPAIR REQUIRES EVALUATION FOR MAJOR MINER DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED & REPLACED REPAIR DOUBLER PER SRM 53-30-3.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 38,235 hrs · 25,857 cycles

EXISTING DOUBLER REPAIR APPROX 11" BY 19", RT LWR FUSELAGE STA 680 TO 692 STRINGER 27R TO 28R REPAIR REQUIRES EVALUATION FOR MAJOR MINER DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED REPAIR DOUBLER PER SRM 53-30-3.

Part: SUPPORT FITTING — GOUGED (LT WING) · airframe 38,235 hrs · 25,857 cycles

LEFT WING FORWARD TRUNNION SUPPORT FITTING INBOARD LUG IS GOUGED. LEFT WING FWD TRUNNION SUPPORT FITTING INBOARD LUG BLENDED, GOUGE IS WITHIN LIMITS PER FED EX EA 7-5710-96571.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 38,235 hrs · 25,857 cycles

BS 990 FRAME HAS A FIGURE 8 HOLE AT STR 5 RT. REPAIRED FRAME AT BS 990 IAW SRM 53-10-4.

Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 38,235 hrs · 25,857 cycles

WHILE WORKING CUST CARD N01118 DISCOVERED DBL DRILLED HOLES IN FLOORBEAM UPPER CHORD AT BS 740 LBL 45 WL 208. FLOOR BEAM UPPER CHORD AT BS 740 LBL 45 WL 208 REPAIRED IAW SRM 53-10-4

Part: FLOORBEAM — TOOL DAMAGE (BS 720F) · airframe 38,235 hrs · 25,857 cycles

TOOLING DAMAGE ON FLOORBEAM BS 720F BBL0 WL 207. REPAIRED FLOOR BEAM AT 720F BL 0 WL 207 PER FED EX EA 7-5310-99423.

Part: STRINGER CLIP — DAMAGED (BS 540) · airframe 38,235 hrs · 25,857 cycles

STA 540 STR 7R, OPEN HOLES IN STRINGER CLIP. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-2.

Part: FRAME — DENTED (BS 700) · airframe 38,235 hrs · 25,857 cycles

FRAME DENTED TWO PLACES BS 700 STR 22-25R. REPAIRED BS 700 FRAME IN TWO PLACES BETWEEN STR 22R - 23R AND BETWEEN S24R AND S25R IAW SRM 51-40-3.

Part: BULKHEAD — GOUGED (BS 178) · airframe 38,235 hrs · 25,857 cycles

BS 178 BULKHEAD FWD SURFACE, GOUGES JUST INBOARD OF NR 2 RADOME ALIGNMENT AND ATTACH PAD. REPAIRED BS 178 BULKHEAD FWD SURFACE IAW SRM 53-10-1.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 38,235 hrs · 25,857 cycles

CRACK INDICATION IN STRINGER CLIP AT BS 970, STRINGER 9 LEFT. REMOVED CRACKED STR CLIP BS 970, STR 9 LT, INSTALLED NEW CLIP IAW SRM 51-30-2.

Part: CREASE BEAM — CORRODED (BS 743) · airframe 38,235 hrs · 25,857 cycles

WHILE WORKING CORROSION REMOVAL ON CREASE BEAM WEB FOUND THE ATTACHING ANGLE WITH SEVERAL MISDRILLED HOLES AT BS 743 LBL 64 WL 208 . REPAIRED PER SRM 51-30-2. (CLOSED)

Part: BULKHEAD — GOUGED (BS 178) · airframe 38,235 hrs · 25,857 cycles

BS 178 BULKHEAD FWD SURFACE, GOUGES JUST INBOARD OF NR 4 RADOME ALIGNMENT AND ATTACH PAD. REPAIRED BS 178 BULKHEAD IAW MM 51-20-0007.

Part: SKIN — CHAFED (BS 720D) · airframe 38,235 hrs · 25,857 cycles

N01158 CHAFING ON EXTERNAL FUSELAGE SKIN LAP STR 19L BS 720D 10 TO 13.P REPAIRED SKIN AT BS 770D PLUS 10" - 13" STR 19L IAW SRM 53-30-3 FIG 5.

Part: BULKHEAD — GOUGED (BS 178) · airframe 38,235 hrs · 25,857 cycles

BS 178 BULKHEAD FWD SURFACE, GOUGES JUST INBOARD OF NR 3 RADOME ALIGNMENT AND ATTACH PAD. REPAIRED BS 178 BULKHEAD IAW MM 51-20-0007.

Part: CREASE BEAM — CRACKED (BS 460) · airframe 38,235 hrs · 25,857 cycles

WEB CRACKED BS 460 LBL 69 WL 208. *S/D* REMOVED CREASE BEAM WEB AT BS 460, LBL 69, WL 208 AND INSTALLED NEW CREASE BEAM WEB P/N HFAB53-SW-011 AT BS 460, LBL 69, WL 208 IAW SRM 51-30-2.

Part: WEB — CORRODED (BS 720C) · airframe 38,235 hrs · 25,857 cycles

CORROSION ON WEB BS 720C PLUS 6 RBL 68 WL 208. *S/D* REMOVED AND REPLACED SHEAR WEB BS 720C-D RBL 68, WL 208 IAW SRM 51-30-2.

Part: STRINGER CLIP — CRACKED (BS 950B) · airframe 38,235 hrs · 25,857 cycles

CRACKED STRINGER CLIP AT BS 950B, STRINGER 9 LEFT. REPLACED STRINGER CLIPS PER SRM 51-30-2.

Part: ATTACH FITTING — CORRODED (BS 227) · airframe 38,235 hrs · 25,857 cycles

MAGNESIUM ATTACH FITTING ON BS 227.8 BULKHEAD, LBL 10, 6 INCHES BELOW PRESSURE DECK IS CORRODED IN UPPER POCKET. *S/D* REMOVED AND REPLACED FITTING PER SRM 51-30-2.

Part: FRAME — MISINSTALLED (BS 1010) · airframe 38,235 hrs · 25,857 cycles

BS 1010 FRAME HAS FASTENERS WITH INSUFFICIENT SPACING AT STRINGER 5 RIGHT. FABRICATED AND INSTALLED FRAME REPAIR BS 1010 STR 5R IAW SRM 53-10-4.

Part: FRAME — DENTED · airframe 38,235 hrs · 25,857 cycles

FRAME DENTED B/S 660 STR 23-25 RT. REPAIRED FRAME BS 660 STR 23-25 RT IAW SRM 51-40-3.

Part: STRINGER CLIP — CRACKED (BS 950B) · airframe 38,235 hrs · 25,857 cycles

CRACKED STRINGER CLIP AT BS 950B, STRINGER 8 RT.

Part: FRAME — DENTED (BS 560) · airframe 38,235 hrs · 25,857 cycles

FRAME DENTED THREE PLACES STA 560 STR 23-24 LT. REMOVED DAMAGE ON FRAME STA 560 STR 23L TO 24L AND REPAIRED IAW SRM 51-40-3 AND SRM 51-30-02

Part: STRINGER CLIP — CRACKED (BS 950C) · airframe 38,235 hrs · 25,857 cycles

CRACKED STRINGER CLIP AT BS 950C, STRINGER 5 RIGHT. REMOVED CRACKED STRINGER CLIP AND INSTALLED A REPLACEMENT PER SRM 51-30-2. WORK ACCOMPLISHED AT BS 950C RT FOUND TO BE A MINOR REPAIR.

Part: FRAME — DENTED (BS 540) · airframe 38,235 hrs · 25,857 cycles

FRAME DENTED TWO PLACES STA 540 STR 23 AND 24 LT. FOUND DENTED FRAME TO BE OUT OF LIMITS REMOVED DAMAGED AREA FABRICATED REPAIR PARTS ALODINED & PRIMED & INSTALLED ALL WORK DONE IAW SRM 51-40-03, 51-30-2, M/M 51- 20-021-7, 51-20-151-7.

Part: FRAME — DENTED (BS 600) · airframe 38,235 hrs · 25,857 cycles

FRAME DENTED THREE PLACES STA 600 STR 24 LT. REMOVED DAMAGE ON FRAME BS 600 STR 24L AND REPAIRED IAW SRM 51-40-03 AND SRM 51- 30-02.

Part: FASTENER — MISSING (STRINGER CLIP) · airframe 38,235 hrs · 25,857 cycles

STA 400 STR 115L, MISSING FASTENERS IN STRINGER CLIP. INSTALLED NEW FASTENERS IN STRINGER CLIP AT STA 400 STR 15L IAW SRM 51-30-2.

Part: STRINGER — CRACKED (BS 720B) · airframe 38,235 hrs · 25,857 cycles

STA 720B PLUS 3, STR 15L CRACKED ON END. REMOVED DAMAGE AND INSTALLED REPAIR PARTS PER SRM 53-10-3

Part: STRINGER — CRACKED (BS 720B) · airframe 38,235 hrs · 25,857 cycles

STA 720B PLUS 3 STR 15R CRACKED ON END. REMOVED DAMAGE AND INSTALLED REPAIR PARTS PER SRM 53-10-3.

Part: TRUNNION — MISDRILLED (NLG) · airframe 38,235 hrs · 25,857 cycles

NLG RT TRUNNION SUPPORT FITTING FWD LOWER HOLE HAS MISDRILLED HOLE. REPAIRED NLG RT TRUNNION SUPPORT FITTING IAW FED EX EA 7-5310-96601.

Part: SKIN — CHAFED (BS 980-990) · airframe 38,235 hrs · 25,857 cycles

EXTERNAL FUSELAGE, BS 980-990, S24L, SKIN CHAFED BY FAIRING. REPAIRED SKIN CHAFF AT BS 980-990 S24L IAW SRM 53-30-1, 53-30-3.

Part: FLOORBEAM — CORRODED (BS 720) · airframe 38,235 hrs · 25,857 cycles

N00441 CORROSION (C53-111-01) ON FLOORBEAM LWR FLANGE BS 720 LBL30-RBL37. ** SD ** COMING ALL WORK TO BE DONE ON CUSTOMER ID #N01427

Part: FRAME — DENTED (BS 680) · airframe 38,235 hrs · 25,857 cycles

FRAME DENTED BS 680 STR 25 RIGHT. REPAIRED FRAME AT BS 680 STR 25RT IAW SRM 51-40-3.

Part: FLANGE — CORRODED (BS 312-328) · airframe 38,235 hrs · 25,857 cycles

CORROSION E-BAY RT MID CHORD FOR NWW HOR. FLANGE LWR SURFACE STA 312 - 328 RBL 16 WL 168 AND ON VERTICAL FLANGE STA 302 RBL 15 WL 170. REMOVED AND REPLACED NOSE WHEEL WELL R/H MID CHORD IAW SRM 51-30-2, 51-30-5.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 38,235 hrs · 25,857 cycles

AFT LOWER CARGO DOOR OUTER SKIN IS GOUGED ON LOWER EDGE. REPAIRED AFT LWR CARGO DOOR SKIN IAW SRM 52-00-3.

Part: FRAME — DENTED (BS 1030) · airframe 38,235 hrs · 25,857 cycles

AFT CARGO BAY FRAME IS DENTED AT BS 1030, ABOVE STR 26R. REPAIRED FRAME BS 1030 ABOVE STR 26R IAW SRM 51-40-3.

Part: BULKHEAD — CRACKED (BS 870) · airframe 38,235 hrs · 25,857 cycles

RIGHT HAND MLG BAY BS 870 BULKHEAD IS CRACKED AT APU LOAD CONTROL VALVE AND DUCT PENETRATION. REPAIRED CRACK IAW EA 7-5310-96606.

Part: SKIN — CHAFED (BS 874) · airframe 38,235 hrs · 25,857 cycles

UPON REMOVAL OF APU FOUND RT DELTA KEEL BEAM SKIN CHAFED AT BS 874 INBOARD OF APU FLOW CONTROL VALVE. REMOVED AND REPLACED R/H DELTA BEAM SKIN AT BS 874 I/B OF APU FLOW CONTROL IAW SRM 53-30-01, SRM 53-10-02 AND SRM 53-30-02.

Part: ACCESSORY UNIT — MALFUNCTIONED (MLG) · airframe 37,796 hrs · 25,530 cycles

AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RAISE PAST THE OFF POSITION. JACKED A/C REF 727 MM 07-11-000-2, ATTEMPTED TO RETRACT LANDING GEAR BUT UNABLE TO RAISE THE HANDLE PAST THE OFF POSITION WITHOUT PULLING THE OVERIDE. REMOVED AND REPLACED THE LANDING GEAR ACCY UNIT REF 727 MM 32-09-121-4, OPS CHK GOOD, OK FOR SERVICE.

Part: ACCESSORY UNIT — MALFUNCTIONED (MLG) · airframe 37,790 hrs · 25,523 cycles

AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RAISE PAST THE OFF POSITION. JACKED A/C REF 727 MM 07-11-000-2, ATTEMPTED TO RETRACT LANDING GEAR BUT WE WERE UNABLE TO RAISE THE HANDLE PAST THE OFF POSITION WITHOUT PULLING THE OVERIDE. REMOVED AND REPLACED THE LANDING GEAR ACCY UNIT REF 727 MM 32-09-121-4, OPS CHK GOOD, OK FOR SERVICE.

Part: OVERHEAT LOOP — INOPERATIVE (KEELBEAM) · airframe 36,069 hrs · 24,210 cycles

LOWER AFT BODY OVERHEAT LIGHT ON IN CRUISE FLIGHT (35,000) OVERHEAT SELECTOR SWITCH UTILIZED = KEELBEAM LIGHT STAYED ON. COMPLETED QRH PROCEDURE. RIGHT PACK AND NR 3 BLEED CLOSED. LIGHT EXTINGUISHED. REMOVED AND REPLACED KEELBEAM LOOP PER MM 26-14-001-2. OPS CK NORMAL, NO LEAKS NOTED IN AREA. PART- KEEL BEAM LOOP P/N 35548-4-255.

Part: WARNING LIGHT — ACTIVATED (OVERHEAT SYS) · airframe 36,206 hrs · 24,316 cycles

LOWER AFT BODY OVERHEAT LIGHT AT CRUISE. FOLLOWED QRH- RIGHT PACK SECURED, RIGHT (NR 3) BLEED SECURED, LIGHT WENT OUT. RAN ALL 3 ENGINES AT 40 PERCENT N1 FOR APPROX 25 MINUTES (WITH AIRSTAIRS RETRACTED) NO LEAKS DETECTED AND COULD NOT GET LIGHT. OK FOR CONTINUED SERVICE. REQUEST CREW TO ISOLATE WITH BODY OVERHEAT SELECTOR ROTARY SWITCH IF PROBLEM REOCCURS ENT BY: 102445 RPT BY: 102445.

Part: WARNING LIGHT — FALSE ACTIVATION (ZONE 200) · airframe 36,001 hrs · 24,156 cycles

DURING CRUISE GOT LOWER AFT BODY OVERHEAT LIGHT. ENGINE ANTI-ICE WAS OPEN. RED TABS COMPLETED DETERMINED NR 2 ENG ANTI-ICE WAS CAUSE OF OVERHEAT LIGHT. WHEN NR 2 ENGINE ANTI-ICE CLOSED DUCT TEMP DECREASED BELOW 50 DEGREES C OVERHEAT LIGHT WENT OUT. RAN ENGINE NR 2 JRH CHAPTER 5 AND PERFORMED OPERATIONAL CHECK IAW MM 30-21- 011-4 AND 30-21-031-4. OPERATIONAL CHECK GOOD. REPOSITIONED LOOP TO COMPLY WITH MM 26-14-001-2.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,970 hrs · 24,123 cycles

N00586 CORROSION (C53-113-01) FWD CARGO STA 720B LBL 2 ON FRAME SHEAR TIE. CORROSION ON FWD CARGO STA 720B, LBL 2, SHEAR TIE WAS FOUND OUT OF LIMITS. REMOVED AND REPAIRED ACTUATOR PANEL AND SPLITER TO ACCESS. REMOVED DAMAGED SHEAR TIE. FABRICATED REPAIR PARTS AND INSTALLED. REINSTALLED REPAIRED ACTUATOR PANEL AND SPLITER IAW SRM 51-30-2, 53-10-4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,970 hrs · 24,123 cycles

N00801 FRAME AT BS 640, LBL 3, WL 155 IS CRACKED ON UPPER FLANGE IN RADIUS. CUTOUT CRACKED PORTION OF FRAME IN AREA OF 2.2 INCHES X 1.8 INCHES. FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER ON FRAME BS 640, LBL 3, W/L 155 IAW SRM 51-40-3 FIG 1 AND 51-30-2 STEPS 4 AND 7.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,970 hrs · 24,123 cycles

N00606 CORROSION (C53-132-02-1) ON UPR SURFACE HORIZONTAL FLANGE BS 744, LBL 8, WL 159 ABOVE DELTA BEAM FWD OF PANEL 3209L IN AIR CONDITIONING BEAY. REMOVED CORROSION AREA 3 INCHES X 1 INCH X .021 INCH FROM ORIGINAL .100 INCH FOUND OUT OF LIMITS IAW SRM 53-10-1. REPLACED STIFFENER ON UPPER SURFACE HORIZONTAL FLANGE BS 744, LBL 10 TO RBL 10, WL 159 ABOVE DELTA BEAM IAW SRM 51-10-1 AND 51-30-02, 51-30-04 AND 51-30- 5.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,970 hrs · 24,123 cycles

CORROSION (C53-100-01) IN RT MLG WHEEL WELL ON UPPER SURFACE OF STRINGER 18A SHELF FROM BS 900 TO BS 940.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,970 hrs · 24,123 cycles

CORROSION (C53-113-01) STA 660, LBL 4 - RBL 4 ON FRAME SHEAR TIE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,970 hrs · 24,123 cycles

CORROSION (C53-113-01) FWD CARGO STA 640, RBL 4 - LBL 4 OF FRAME SHEAR TIE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,970 hrs · 24,123 cycles

CORROSION (C53-113-01) FWD CARGO STA 660, RBL 6 IN STR 28R. REMOVED CORROSION AND REPAIRED STR 28 RT AT BS 660 PER SRM 53-10-1, 53-10-3, FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,970 hrs · 24,123 cycles

CORROSION (C53-224-06) TOP OF FLOORBEAM BS 328, LBL 40, WL 208.

Part: SKIN — CORRODED (FUSELAGE) · airframe 35,970 hrs · 24,123 cycles

CORROSION ON INTERIOR SIDE OF SKIN AT BS 664, RBL 4 TO LBL 4.

Part: COOLER — LEAKING (BLEED AIR) · airframe 35,261 hrs · 23,573 cycles

ENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. NO PACK TAKEOFF, ALL BLEED AIR SWITCHES CLOSED, 0 PSI MANIFOLD PRESSURE PRIOR TO TAKEOFF. LIGHT WENT OUT AS THRUST LEVERS RETARDED AND NR 1 BLEED AIR VALVE WAS OPENED. OVERHEAT SYSTEM TESTED GOOD. LIGHT REMAINED OUT FOR REMAINDER OF FLIGHT. ABNORMAL PROCEDURES COMPLETED. REMOVED AND REPLACED NR 1 PRECOOLER IAW 36-11-051-4. LEAK AND OP CHECKS GOOD.

Part: ADC — FAILED (COCKPIT) · airframe 35,195 hrs · 23,525 cycles

CAPTAINS AIRSPEED AND ALTIMETER AND VERTICAL SPEED INDICATOR FAILED ON ROTATION WITH WINDSHEAR WARNINGS. REPLACED CADC IAW MM. OPS CHECK GOOD. CAT STATUS DOWNGRADED TO CHK II, CHK II. OVERALL CAT STATUS IS NOT II.

Part: OVERHEAT LOOP — OUT OF POSITION (NR 1 ENGINE)

DURING CLIMBOUT NR 1 ENG STRUT OVERHEAT LIGHT ILLUM. NO LEAKS FOUND WITH ENG. REPOSITIONED OVERHEAT LOOP.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUM AFT T/O. *S/D* TIGHTENED LOOSE CLAMPS IN STUB WING. REF 36-00-001-2. RAN ENG PER JET RUN HDBK CHPT 5, NO LEAKS NOTED. OK FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR)

AFT DEPARTURE AT HRL, MAIN CARGO DOOR LIGHT CAME ON.

Part: LINE — LEAKING (B HYD SYS)

BOTH B-SYS PUMP LOW PRESS LIGHTS ON 2ND OFF PANEL AND ALL 3 SYS-B FLT CONTROL LIGHT ON FWD PANEL ILLUM IN FLT. *S/D* INSTALLED TUBE ASSY PACK AND UNION PER B727 MM 20-10-005-4. LEAK CHECK OK, B CHECK OK.

Part: HEAT VALVE — MALFUNCTION (NR 1 ENGINE)

97-0254 - NR 1 ENGINE OIL TEMPERATURE IN YELLOW BAND DUE TO FUEL HEAT VALVE STUCK OPEN. SHUTDOWN ENGINE, AFTER 15 MINUTES TEMPERATURE AT 125C MAX TEMPERATURE 130C LESS THAN 5 MINUTES. WINDMILL 50 MINUTES. PULLED OIL FILTER, FOUND CLEAN. INSTALLED NEW FILTER, MOTORED ENGINE NO LEAKS NOTED. REPLACED FUEL DE-ICING VALVE PER MAINTENANCE MANUAL 73-14-11. CANNON PLUG TO THE VALVE IS BAD AND NEEDS TO BE CHANGED. THE VALVE REMAINS DEFERRED PLUG REMOVED, BAGGED AND TIED BACK. VALVE IS WIRED IN THE CLOSED POSITION. CIRCUIT BREAKER OPENED AND COLLARED.

Part: CONNECTOR — DIRTY (LT MLG DOOR)

ON GEAR RETRACTION, RED DOOR LIGHT ON FIRST OFFICER'S PANEL AND LEFT GEAR DOOR LIGHT ON SECOND OFICER'S PANEL. RECYCLED GEAR, LIGHT WENT OUT. *S/D* FOUND LEFT MAIN GEAR DOOR SWITCH SECURE. CLEANED CONNECTOR AND PINS, REINSTALLED. DOOR LIGHTS CHECK NORMAL ON BOTH PANELS PER MAINTENANCE MANUAL 32-62-0.

Part: ANTI-ICE DUCT — FAILED (NR 1 ENGINE)

APPROXIMATELY 1 MINUTE AFTER SETTING TAKEOFF POWER NR 1 FIRE WARNING SOUNDED. WARNING EXTINGUISHED WHEN THROTTLE WAS RETARDED. SUSPECT BLEED AIR LEAK. SEE PREVIOUS WRITE UP. INSPECTED ENGINE FOR BLEED AIR LEAK AND DISCREPANCIES ASSOCIATED. FOUND NR 1 ENGINE ISOLATORS UPPER AND LOWER DAMAGED FROM LEAKING AIR. REMOVED AND REPLACED ISOLATORS PER MAINTENANCE MANUAL 71-21-1. REMOVED AND REPLACED NR 1 ENGINE TO FACILITATE OTHER MAINTENANCE PER WORK CARD 70T0001. FOUND ANTI-ICE DUCT BLOWN. REMOVED AND REPLACED DUCT, DETECTED NO LEAKS.

Part: CONNECTOR — DIRTY (NR 1 ENGINE)

IN CRUISE AT FLIGHT LEVEL 310 NR 1 FIRE WARNING SOUNDED. WARNING EXTINGUISHED IMMEDIATELY WHEN THROTTLE WAS RETARTDED. OPERATED NR 1 ENGINE AT IDLE AS PER AIRCRAFT FLIGHT MANUAL FOR DESCENT AND LANDING AT DFW. PARAMETERS WHEN WARNING OCCURRED AS FOLLOWS EPR 1.94, N1 88 PERCENT, EGT 480, N2 88 PERCENT. CONFIRMED FIRE DETECTION PROBLEM WITH NR 1 ENGINE. CHECK NR 1 ENGINE FIRE LOOP. FOUND CONNECTION AT LOOP CANNON PLUG LOOSE AND DIRTY. CLEANED PLUG AND POSITIONED FIRE LOOP. GROUND OPERATIONAL CHECK GOOD.

Part: SMOKE DETECTOR — FAILED (CARGO COMPT)

AT 6,000 FT MAIN CARGO SMOKE ALARM 2 ILLUMINATED WITH ACCOMPANYING FRONT COCKPIT FIRE WARNING LIGHT. COMPLIED WITH RED TABS AND TURNED SMOKE CONTROL ON. LIGHT EXTINGUISHED BUT REAPPEARED WITH ALARM, 1 MIN LATER LIGHT/ALARM EXTINGUISHED BY ITSELF. NO SMOKE OR FUMES IN FLIGHT. INSPECTED AREA, FOUND NO EVIDENCE OF SMOKE. MADE SURE LINE WAS CLEAR FROM UPPER CARGO TO SMOKE DETECTOR, CHANGED NR 2 SMOKE DETECTOR AND OPS CHECKS GOOD.

Part: AIR DISTR — ODOR (CARGO COMPT)

FAINT SMELL IN CABIN BECAME A VERY HEAVY PAINT SMELL, SO MUCH SO THAT NORMAL BREATHING IN CARGO AREA WAS DIFFICULT. PAINT SMELL WAS VERY NOTICEABLE IN COCKPIT. DONNED OXYGEN AND DIVERTED TO TYS. SOURCE OF HEAVY SMELL SEEMED TO BE EMANATING FROM NORMAL CARGO CANS. GROUND CREW COMMENTED ON STRENGTH OF ODORS WHEN FIRST ENTERING THE AIRCRAFT. THE FUMES DID NOT COME FROM THE DANGEROUS GOODS. WET INK ON PAMPHLETS IN 3R AND 4 CAUSED THE ODOR. THESE WERE DOWN LOADED AND SHIPPED VIA GROUND TO DESTINATION.

Part: STRINGER — DAMAGED (BS 1072-1090)

UPPER LOBE BS 1072 TO 1090 STR 7R DAMAGE TO STRINGER INSIDE U-CHANNEL ABOVE SKIN RIVETS. INSTALLED REPAIR DOUBLER IAW BOEING SRM 53-10-3.

Part: STRINGER — DAMAGED (BS 757-759)

BS 757 TO 759 STR 7L DAMAGE INSIDE STRINGER ABOVE RIVETS THROUGH SKIN. REPLACED STR PER SRM 53-10-3.

Part: STRINGER — DAMAGED (BS 882-889)

UPPER LOBE BS 882 TO 889 STR 7R DAMAGED TO STR INSIDE U-CHANNEL ABOVE SKIN RIVETS. REMOVE DAMAGED STR 7R FROM BS 872 TO 898, FABRICATED PARTS 1, 2, 3 AND 4. DRILLED AND INSTALLED PER SRM 53-10-3 FIG 3.

Part: STRINGER — DAMAGED (BS 885-888)

UPPER LOBE BS 885 TO 888 STR 7L, DAMAGE TO STRINGER INSIDE U-CHANNEL. REMOVED FASTENERS, CUT OUT DAMAGED AREA, FABRICATED FILLER, REPAIRED PARTS 1, 2, 3. LOCATED AND DRILLED ALL HOLES, TREATED AND PRIMED ALL PARTS AND INSTALLED PER SRM 53-10-3 PAGES 5 TO 8 FIG 3.