N257FE

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 59,191 hrs · 37,906 cycles

ACFT HAS BEEN INVOLVED IN AN ACFT STRIKE, THE RT SIDE OF THE VERTICAL STABILIZER HAS SUSTAINED DAMAGE. INITIAL INSPECTION SHOWS NUMEROUS RIBS AND STIFFENERS BROKEN INTERNAL TO VERTICAL FIN. ALSO, HAS DAMAGED HYD LINES INTERNAL OF STAB, OUTER DAMAGE INCLUDES TORN SKIN, SEVERAL PUNCTURES AND 3 PUNCTURE HOLES TO THE LOWER RUDDER ON RT SIDE. REPAIRED DAMAGED AREA AS REQUIRED REF EA 7-5530-1541-18.

Part: PANEL — UNSECURE (E/E BAY) · airframe 59,186 hrs · 37,899 cycles

IN FLIGHT, ACFT WOULD NOT PRESSURIZE IN AUTO, STANDBY OR MANUAL MODE. WITH ACFT AT 10000 FT PRESSURE CONTROLLER WOULD HOLD ABOUT 7000 FT CABIN ALTITUDE IN MANUAL WITH OUTFLOW VALVE FULLY CLOSED OR IN STANDBY MODE. DURING PRESSURIZATION CHECK, FOUND AIR LEAKING IN NOSE TRUNION AREA OF NOSE WHEEL WELL. INSPECTION FOUND ACCESS PANELS 3514, 3515, 3622 LEFT OPENED INSIDE LT AND RT OF NOSE TUNNEL IN FWD E/E COMPARTMENT. SECURED PANELS AND RECHECKED ACFT. PRESSURIZATION IAW MM 21-31-000-2. OPS AND LEAK CHECKS GOOD. ACFT. HOLDS NORMAL PRESSURIZATION, OK FOR SERVICE. SECURED PANELS CLOSED THAT WERE OPENED IN FWD AND AFT BAGGAGE COMPARTMENTS OPENED TO F.O.M. FINAL CLOSED.

Part: OXYGEN MASK — FAILED (SECOND OBSERVER) · airframe 59,104 hrs · 37,831 cycles

SECOND OBSERVER OXYGEN MASK FAILED PREFLIGHT CHECK. THE FLOW INDICATOR SHOWED RED DURING TEST. REPLACED SECOND OBSERVER`S OXYGEN MASK, OP CHECKED NORMAL IAW 35-12-000-4.

Part: SLIDE — UNWANTED DEPLOY (CARGO) · airframe 58,987 hrs · 37,742 cycles

FORWARD CARGO SLIDE DEPLOYED FROM DOOR BEING OPENED EXTERNALLY. STOWED SLIDE AS REQUIRED IN REF TO AMM 25-60-015-2. ACFT IS OK FOR SERVICE.

Part: OIL SYSTEM — LEAKING (NR 3 ENGINE) · airframe 58,863 hrs · 37,627 cycles

45 MIN AFTER TAKEOFF NR 3 ENG HAD LOST APPROX 1 GAL DOWN TO 1.5 GALS FROM 2.6 GAL AT TAKEOFF. OIL PRESSURE & TEMP WERE NORMAL ON NR 3. LANDED WITH GAL 1.25 GAL / 42 PSI PRESS / 10C OIL TEMP. ENT BY: 152952 RPT BY: 434068 SHGN 28MAR12 23:57 MEM U OPENED NR 3 ENGINE AND FOUND ABOUT 1 QT OF OIL IN COWLING. INSPECTED TAIL PIPE AND IT WAS CLEAN AND DRY. COULD NOT TELL WHERE LEAK WAS COMING FROM. ADDED 5 QTS OF OIL IAW MM REF 12-13-001-2-0. ENGINE NEEDS TO BE RAN TO INSPECT FOR LEAKS. AWAITING TRANSLOAD TO RUN ENGINE. REPLACED #3 ENGINE PER WC70T0001-03,WC70T000303, WC70T0301-03. OPS CHECKED GOOD. OK FOR SERVICE.

Part: STRINGER — CORRODED (BS 540 S28L) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

STRINGER 28L CORRODED BS 540. CUT OUT DAMAGED STRINGER DIM 17 AND 1/4 INCHES LONG IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER REPAIR PARTS IAW SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9. INSTALLED STRINGER REPAIR PARTS IAW SRM 51-30-2 AND 53-10-3 FIG 1.

Part: SKIN — DENTED (BS 360 S19R) · airframe 58,584 hrs · 37,359 cycles

DENT AT FRAME 360 AT STRINGER 19, RT SIDE OF EXTERIOR SURFACE. CUT OUT DAMAGED AREA, FABRICATED 3EA REPAIR FILLERS, REPAIR DOULBER, AND STRUCTURAL FILLER, AND INSTALLED 3EA REPAIR FILLERS, REPAIR DOUBLER, AND STRUCTURAL FILLER AT FRAME BS 360 STR 19R EXTERIOR FUSELAGE IAW SRM 51-30-2 AND EA 7-5330-136798.

Part: SKIN — CORRODED (BS 550) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

CORROSION UNDER ANTENNA STRUCTUAL DOUBLER STA.550 BETWEEN STR 28 RIGHT AND 28 LEFT REMOVED ANTENNA STRUCTURAL DOUBLER STA 550 BETWEEN STR 28R TO 28L IAW SRM 51-30-2. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-30-01 FIG 1. FABRICATED REPAIR DOUBLER IAW EA 7-5330-154102. INSTALLED REPAIR DOUBLER AND ANTENNA STRUCTURAL DOUBLER IAW SRM 51-30-2 AND EA 7-5330-154102.

Part: FLOORBEAM — CRACKED (BS 900) · airframe 58,584 hrs · 37,359 cycles

FLOORBEAM HAS CRACK AT LOWER FWD RADIUS BL 0, CRACK DOES NOT EXTEND. BEYOND SECOND FASTENER EITHER SIDE OF BL 0. STOP DRILLED CRACK IN BS 900 FLOORBEAM LWR FWD RADIUS AT BL 0 IAW EO 7-5300-7-2309 G PT 3. FABRICATED REPAIR ANGLE, 2 FILLERS, AND 2 RADIUS FILLERS IAW EO 7-5300-7-2309 G PT 3. INSTALLED REPAIR PARTS IAW EO 7-5300-7-2309 G PT 3.

Part: STRUCTURE — CRACKED (RT WING TE FLAP) · airframe 58,584 hrs · 37,359 cycles

RT WING INBD MID FLAP T/E CHORD CRACKED AT INBD CABLE CONTROL DRUM CUTOUT. CUT OUT DAMAGE TRAILING EDGE CHORD RIGHTHAND WING INBOARD MID FLAP IAW SRM 51-40-4 FIG 3. FABIRCATED LOCATED AND DRILLED NEW CHORD AND SPLICE IAW 51-40-4 FIG 3 AND 57-50-2. INSTALLED CHORD AND SPLICE IAW SRM 51-30-2.

Part: FRAME — CRACKED (BS 760.95) · airframe 58,584 hrs · 37,359 cycles

RT FRAME BS 760.95, CRACK IN 2ND HOLE ABOVE FLOOR AND CRACK IN 3RD HOLE ABOVE FLOOR. REPAIRED RT FRAME BS 760.95 IAW FED EX EO 7-5310-7-3367 PT9.

Part: FRAME — CRACKED (BS 760.95) · airframe 58,584 hrs · 37,359 cycles

RIGHT FRAME, BS 760.95 CRACK IN WEB PILOT HOLE. REPAIRED RT FRAME BS 760.95 IAW EO 7-5310-7-3367 PT 9.

Part: STRUCTURE — DAMAGED (LT WING TE FLAP) · airframe 58,584 hrs · 37,359 cycles

LT WING OTBD MID FLAP INBD T/E IS CHIPPED. FOUND TO BE UNREPAIRABLE IAW SRM 57-50-1 FIG 3. REMOVED AND REPLACED LT O/B MID FLAP ASSEMBLY IAW AMM 27-51-011-4-0.

Part: SEAT TRACK — CORRODED (BS 1140-1180) · airframe 58,584 hrs · 37,359 cycles

SURFACE CORROSION ON SEAT TRACK BL 0 BS 1140 TO 1180. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK IAW SRM 53-10-2, FIG 7A. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 1170) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

SURFACE CORROSION ON SEAT TRACK, RBL 26, BS 1170. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED, LOCATED, AND DRILLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 1110) · airframe 58,584 hrs · 37,359 cycles

MAIN CABIN BS 1110 FLOORBEAM HAS CORROSION ON UPPER SURFACE BETWEEN BL0 AND LBL26. CUT OUT DAMAGED AREA IAW SRM 53-10-8 FIG. 3, FABRICATED REPAIR PARTS IAW SRM 53-10-8 FIG. 3, AND INSTALLED REPAIR PARTS IAW B727 51-30-2.

Part: SEAT TRACK — CORRODED (BS 772-850) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

MULTIPLE AREAS OF CORROSION ON SEAT TRACK FLANGES LBL 26, BS 772-850. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1. REMOVED SEAT TRACK IAW SRM 51-30-2 FABRICATED NEW SEAT TRACK IAW SRM REV 103 51-30-5 AND 53-10-2 FIG 7. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2

Part: SEAT TRACK — CORRODED (BS 370-480) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

CORROSION SEAT TRACK FLANGE STA 370-480, LBL 24. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A & SRM 53-10-2 FIG 7, INSTALLED SEAT TRACK SECTION IAW SRM 51-30-2 & 51-10-2.

Part: SKIN — DAMAGED (BS 265 S4R) · airframe 58,584 hrs · 37,359 cycles

RT SIDE OF FUSELAGE HAS LIGHTING STRIKE DAMAGE AT BS 265 BELOW STR 4R. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS, AND INSTALLED DOUBLER IAW SRM 53-30-3 FIG. 3 AND 53-30-2 FIG. 1.

Part: SEAT TRACK — CORRODED (BS 780-870) · airframe 58,584 hrs · 37,359 cycles

MULTIPLE AREAS OF CORROSION ON SEAT TRACK FLANGE LBL 50 BS 780-870. REMOVED DAMAGED SEAT TRACK IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK IAW SRM 53-10-2 FIG 7 AND 51-30-5. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 344-390) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

CORROSION SEAT TRACK FLANGE BS 344-390, RBL 25. REMOVED SEAT TRACK SECTION AFTER FOUND OUT OF LIMITS IAW SRM 51-30-2 & SRM REPORT 2489, FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A, INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 480-550) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

CORROSION SEAT TRACK FLANGE STA 480 - 550, RBL 45. REMOVED SEAT TRACK SECTION AND SPLICE PARTS AFTER FOUND OUT OF LIMITS IAW SRMR 2489 & SRM 51-30-2. FABRICATED NEW SEAT SECTION AND SPLICE PARTS IAW SRM 53-10-2 FIG 7A & SRM 53-10-5 FIG 1. INSTALLED NEW SEAT TRACK SECTION & SPLICE PARTS IAW SRM 51-30-2.

Part: FRAME SPLICE — CRACKED (BS 930 S14R) · airframe 58,584 hrs · 37,359 cycles

CABIN FRAME SPLICE AT BS 930, STR 14R HAS CRACK INDICATING AT SPLICE. CUT OUT DAMAGED AREA IAW SRM 53-10-4 FIG 1. FABRICATED REPAIR PARTS IAW SRM 53-10 4 FIG 1. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 53-10-4 FIG 1

Part: SKIN — DAMAGED (BS 580 S7R) · airframe 58,584 hrs · 37,359 cycles

RT SIDE OF FUSELAGE HAS LIGHTNING STRIKE DAMAGE AT BS 580, STRINGER 7R. CUT OUT DAMAGED AREA OF FUSELAGE SKIN IAW SRM REV.103 53-30-3 FIG 3. FABRICATED REPAIR DOUBLER IAW SRM 53-30-3 FIG 3 AND 53-30-2 FIG. 2. INSTALLED REPAIR DOUBLER IAW SRM 53-30-3 FIG 3.

Part: SEAT TRACK — CORRODED (BS 480-498) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

CORROSION SEAT TRACK SPLICE PLATE BS 480-498, LBL 45. FOUND SEAT TRACK SPLICE AND SEAT TRACK SECTION OUT OF LIMITS IAW SRM REPORT 2489. REMOVED SEAT TRACK SECTION AND SPLICE PARTS IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK SECTION AND SPLICE ANGLES, AND SPLICE PLATE IAW SRM 53-10-5 FIG 1 & P -F SRM 53-10-2 FIG 7A. INSTALLED NEW SEAT TRACK & SPLICE PARTS IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 480-600) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

CORROSION SEAT TRACK FLANGE STA 480-600, BL 0. REMOVED OUT OF LIMITS SEAT TRACK IAW SRM 51-30-2 AND SRM 2489. FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A AND SRM 51-30-5. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2.

Part: STRINGER — CORRODED (BS 510 S28L) · airframe 58,584 hrs · 37,359 cycles

STR 28L AT BS 510 HAS CORROSION INSIDE HAT CHANNEL. CUT OUT DAMAGED AREA IAW SRM 53-10-1 FIG 1. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-3 FIG 1 AND 53-30-2.

Part: SEAT TRACK — CORRODED (BS 480-500) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

CABIN SEAT TRACK AT LBL 24 IS CORRODED ON LWR SURFACE BTWN BS 480-500. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK SECTION AND 2 EA. REPAIR SPLICE ANGLES AND STRAP IAW SRM 53-10-2 FIG 7A, SRM 53-10-5 FIG 1 & 51-30-5. INSTALLED NEW SEAT TRACK SECTION AND SPLICE PARTS IAW SRM 51-30-2.

Part: SKIN — CORRODED (BS 510) · airframe 58,584 hrs · 37,359 cycles

BS 510 BL 0 IN FWD CARGO BAY FUSELAGE SKIN HAS CORROSION AROUND ANTENNA DOUBLER. REMOVED ANTENNA STRUCTURAL DOUBLER BS 510, BL 0 IAW SRM 51-30-2. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-30-01, FIG 1, FABRICATED REPAIR DOUBLER IAW EA 7-5330-154103. INSTALLED REPAIR PARTS AND ANTENNA STRUCTURAL DOUBLER IAW SRM 51-30-2 AND EA 7-5330-154130.

Part: STRINGER — CORRODED (BS 510 S28L) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

STR 28L AT BS 510 HAS CORROSION INSIDE HAT CHANNEL. CUT OUT DAMAGED AREA IAW SRM 53-10-1 FIG.1. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-3 FIG.1 AND 53-30-2.

Part: FRAME — DENTED (BS 500 S24-25R) · airframe 58,584 hrs · 37,359 cycles

BS 500 FRAME DENTED BTWN STR 24R-25R AT UPPER FLANGE. FOUND AREA DENTED AND OUT OF LIMITS IAW SRM 53-10-1 FIGURE 1. TRIMMED OUT DAMAGE, FABRICATED REPAIR FILLER AND REPAIR DOUBLER SPLICE AND INSTALLED IAW EA 7-5310-152426.

Part: BEAM — MISINSTALLED (BS 1183) · airframe 58,584 hrs · 37,359 cycles

AFT PIT BS 1183 VERTICAL BEAM LBL 17.8 SEVERAL FASTENERS HAVE LOW SPACING. TRIMMED OFF BEAM AFT FLANGE AND WEB, FABRICATED REPAIR PARTS, TREATED, PRIMED AND INSTALLED IAW EA 7-5310-136787.

Part: SEAT TRACK — CORRODED (BS 383-480) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

CORROSION SEAT TRACK FLANGE STA 383 - 480, LBL 45. REMOVED SEAT TRACK AND SPLICE PARTS AND WEB FOR ACCESS IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A, SRM 51-30-5 & 53-10-2 FIG 7, TREATED AND PRIMED, AND INSTALLED SEAT TRACK SECTION AND REINSTALLED SPLICE PARTS AND WEB IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 950D) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

SURFACE CORROSION ON FLOORBEAM BS 950D, LBL 20. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG. 1. CUTOUT DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW SRM 53-10-8 FIG 8.

Part: SEAT TRACK — CORRODED (BS 600-720) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

CORROSION SEAT TRACK FLANGE STA 600 - 720, BL 0. REMOVED OUT OF LIMITS SEAT TRACK IAW SRM REPORT 2489 AND SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A AND SRM 51-30-5. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.

Part: SKIN — DAMAGED (BS 690 S7R) · airframe 58,584 hrs · 37,359 cycles

RT SIDE OF FUSELAGE HAS LIGHTNING STRIKE DAMAGE AT BS 690, STRINGER 7R. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED DOUBLER IAW SRM 51-30-4 FIG. 6 AND 53-30-3 FIG. 1

Part: SEAT TRACK — CORRODED (BS 380-480) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

CORROSION SEAT TRACK FLANGE STA 380 - 480, RBL 45. REMOVED SEAT TRACK SECTION AND FABRICATED NEW SEAT TRACK SECTION AND INSTALLED IAW SRM 51-30-2 AND SRM 53-10-2 FIG 7A.

Part: SEAT TRACK — CORRODED (BS 480-530) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

CORROSION SEAT TRACK FLANGE STA 480 - STA 530, RBL 25. REMOVED SEAT TRACK & SPLICE SECTION IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK AND SPLICE ANGLES AND SPLICE STRAP IAW SRM 53-10-2 FIG 7A & SRM 53-10-5 FIG 1 AND INSTALLED NEW SEAT TRACK AND SPLICE PARTS IAW SRM 51-30-2

Part: KEELBEAM — CRACKED (BS 880) · airframe 58,584 hrs · 37,359 cycles

LT KEEL BEAM IS CRACKED AT SECOND FASTENER BS 880 LBL 6. REPAIRED LT KEELBEAM BS 880 LBL6 IAW EA 7-5310-152421.

Part: FLOORBEAM — CORRODED (BS 950F) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

SURFACE CORROSION TOP OF FLOORBEAM, BS 950F, LBL 18. CUTOUT DAMAGED AREA IAW SRM 53-10-8 FIG 3 AND FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-8 FIG 3.

Part: STRUCTURE — CORRODED (BS 930) · airframe 58,584 hrs · 37,359 cycles

SURFACE CORROSION AROUND FASTENERS LOWER SIDE OF FLOORBEAM TOP TEE , BS 930, RBL 60. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1, FIG 4, FABRICATED REPAIR ANGLES IAW EA 7-5310-154104, AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND EA 7-5310-154104.

Part: FLOORBEAM — CORRODED (BS 950) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

SURFACE CORROSION ON TOP OF FLOORBEAM BS 950, RBL 50. REMOVED UPPER TEE CAP IAW SRM 51-30-2. FABRICATED NEW TEE CAP IAW SRM 53-10-2 FIGURE 7 AND SRM 51-30-5. INSTALLED TEE CAP IAW SRM 51-30- 2 AND SRM 51-30-5.

Part: SKIN — DAMAGED (BS 198 S13R) · airframe 58,584 hrs · 37,359 cycles

RT SIDE OF FUSELAGE HAS LIGHTNING STRIKE DAMAGE AT BS 198, STR 13 R. CUTOUT DAMAGED AREA IAW SRM 53-30-3 FIG 13, FABRICATED DOUBLERS & FILLERS IAW SRM 53-30-3 FIG 13 & 53-30-2 FIG 1. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AT RT SIDE OF FUSELAGE AT BS 198 AND SRM 53-30-3 FIG 13.

Part: SEAT TRACK — CORRODED (BS 870-950) · airframe 58,584 hrs · 37,359 cycles

SURFACE CORROSION ON SEAT TRACK RBL 26, BS 870 AND 950. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 3 AND REMOVED SEAT TRACK SECTION IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7 & SRM 51-30-5, AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 950) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

SURFACE CORROSION ON FLOORBEAM, LOWER SIDE LBL58, BS 950. FLOORBEAM REPLACED ON NR NOO538.

Part: SKIN — DAMAGED (BS 950 S26L) · airframe 58,584 hrs · 37,359 cycles

LT SIDE OF FUSELAGE SKIN IS DENTED AND CHAFED AT LAP SEAM BS 950, PLUS 10", STRINGER 26L. CUT OUT DAMAGE AREA IAW SRM 53-30-3 FIG.14. FABRICATED REPAIR PARTS DOUBLER AND STRUCTURAL FILLER IAW SRM 53-30-3 FIG.14 AND 53-30-2 FIG.2. INSTALLED DOUBLER AND STRUCTURAL FILLER IAW SRM 51-30-2

Part: FLOORBEAM — CORRODED (BS 380) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

CORROSION TOP TEE CAP FLOORBEAM STA 380, RBL 25 - RBL 45. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG. 4B. FABRICATED REPAIR PARTS AND REPAIRED TOP TEE CAP OF FLOORBEAM BS 380 IAW SRM 53-10-8 FIG. 3 AND 51-30-2.

Part: FLOORBEAM — CORRODED (BS 620) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

CORROSION TOP TEE ON FLOORBEAM STA 620, LBL 45 - 25. CUT OUT DAMAGE IAW SRM 53-10-8 FIG.3. FABRICATED REPAIR PARTS IAW SRM 53-10-8 FIG.3. INSTALLED ALL REPAIR PARTS IAW SRM 51-30-2

Part: SEAT TRACK — CORRODED (BS 500) · corrosion level 2 · airframe 58,584 hrs · 37,359 cycles

CORROSION SEAT TRACK SPLICE PLATE M/C STA 480 - STA 500, LBL 24. REMOVED SEAT TRACK SPLICE PLATE & FOUND OUT OF LIMITS IAW SRM 51-30-2, FABRICATED NEW SPLICE PLATE IAW SRM 53-10-2 FIG 7A AND 51-30-5, INSTALLED NEW SPLICE PLATE IAW SRM 51-30-2.

Part: KEELBEAM — CRACKED (BS 880) · airframe 58,584 hrs · 37,359 cycles

RT KEELBEAM IS CRACKED AT SECOND HAND, THIRD FASTENER, BS 880, RBL 6. REPAIRED RT KEELBEAM AT BS 880 RBL 6 IAW EA 7-5310-152421.

Part: FRAME — DAMAGED (BS 783.95) · airframe 58,584 hrs · 37,359 cycles

RT FRAME BS 783.95, SECOND AND THIRD HOLE ABOVE FLOOR HAVE DOUBLE DRILLED HOLES. REPAIRED RIGHT HAND FRAME BS 783.95 IAW EA 7-5310-152422.

Part: FRAME — DAMAGED (BS 1130 S27-28L) · airframe 58,584 hrs · 37,359 cycles

AFT PIT BS1130 FRAME UPPER FLANGE HAS TRIPLE DRILLED HOLE BETWEEN STR 27L AND 28L. CUT OUT DAMAGED AREA IAW SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR IAW SRM 51-40-3 FIG 1. INSTALLED FRAME REPAIR IAW SRM 51-30-2 AND 51-40-3 FIG 1.

Part: FRAME — PUNCTURED (BS 1070 S27L) · airframe 58,584 hrs · 37,359 cycles

AFT PIT BS 1070 FRAME IS PUNCTURED IN UPPER FLANGE ABOVE STR 27L. CUT OUT DAMAGE AREA IAW SRM 51-40-3 FIG 1. FABRICATED REPAIR PARTS IAW SRM 51-40-3 FIG 1. INSTALLED REPAIR PARTS AND FITTING IAW SRM 51-30-2

Part: CONTROL PANEL — FAILED (AUTOPILOT) · airframe 57,715 hrs · 36,613 cycles

ON CLIMBOUT "STAB OUT OF TRIM LIGHT" LIGHT ON CONTINUOUSLY WITH AUTOPILOT ON. AUTOPILOT WOULD NOT TRIM OR HOLD ALTITUDE. RAN " STABILIZER OUT OF TRIM LIGHT REMAINING ILLUMINATED" CHECKLIST TWICE. AUTOPILOT WOULD NOT ENGAGE PROPERLY WITH A/P DISCONNECTED, ALL TRIM SEEMED TO WORK PROPERLY. MADE DESCENT AND LANDING WITH A/P DISENGAGED. AACFT WAS IN SERVO "A" AT THE TIME. RELEASED FOR SERVICE IAW MEL: 22-01-11-A. REMOVED AND REPLACED A/P MODE CONTROL PANEL IAW MM 22-11-181-4. PERFROMED A/P RTS CKS IAW MM 22-11-008-5. NO DISCREPANCIES NOTED. A/P SERVO "A" REMAINS NOT II. SERVO "B" IS CK II.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 57,580 hrs · 36,509 cycles

ON INITIAL TAKEOFF ROTATION THE DFFERENTIAL PRESSURE MOMENTARILY STUCK AT ZERO AND THEN JUMPED TO 3.6 PSID WHILE THE CABIN ALTITUDE CONTINUED TO CLIMB NORMALLY. HOWEVER PASSING 15000 FT CABIN ALTITUDE EXCEEDED 5600 FT WHICH WAS SET IN CABIN ALTITUDE WINDOW. DIFFERENTIAL PRESSURE STOPPED AT 5.9 PSID WHILE CABIN ALTITUDE CONTINUED TO CLIMB. AFTER LEVELING OFF AT 25000 FT CONSULTED QRH RED TABS AND STARTED A DESCENT. ON TAXI IN VERY LITTLE AIRFLOW FELT FROM THE EYEBALL OUTLETS WITH THE GASPER FAN SWITCH ON. R&R CPC PER AMM 21-31-010-4 OPS CHK GOOD PER 21-31-000-2.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,182 hrs · 36,205 cycles

DENT STA 1180 STR 17R. FOUND DENT OUT OF LIMITS, CUT OUT DAMAGED SKIN DIMS 3.2 INCH X 3.0 INCH, FABRICATED REPAIR DOUBLER USING 2024-T3 .090 DIMS 10.5 INCH X 8.750 INCH AND FILLER USING 2024-T3 .080 DIMS 3.2 INCH X 3.0 INCH, INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3A.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 57,182 hrs · 36,205 cycles

FWD CARGO COMPT STRINGER 28L IS CORRODED FROM BS 600-620. CUTOUT DAMAGED STRINGER. FABRICATED STRINGER REPAIR FILLER, REPAIR SPLICE. CUTOUT DAMAGED SKIN & FABRICATED REPAIR DOUBLER. INSTALLED REPAIR PARTS IAW SRM 53-10-3, 53-10-2, 53-30-2 AND 51-30-2.

Part: SKIN — DENTED (BS 390) · airframe 57,182 hrs · 36,205 cycles

DENT STA 390 STR 8L. DENT FOUND TO BE OUT OF LIMITS, REWORKED DENT TO ORIGINAL CONTOUR IAW SRM 51-40- 1 HFEC INSPECTED IAW NDTM 51-00-00 WITH NO DEFECTS NOTED.

Part: SKIN — BULGED (BS 650) · corrosion level 2 · airframe 57,182 hrs · 36,205 cycles

SKIN BULGE STA 650 STR 29R. CUT OUT STR DAMAGE AND REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-30-1. CUTOUT DAMAGED SKIN, FABRICATED REPAIR DOUBLER , FABRICATED STR REPAIR AND SPLICE, INSTALLED REPAIR PARTS IAW SRM 51-30-2, 53-30-3 AND 53-10-3.

Part: VALVE — FAILED (CABIN PRESSURE) · airframe 56,801 hrs · 35,920 cycles

CABIN PRESSURE WOULD NOT HOLD WITH ACFT AT 240. DESCENT TO 200 HELPED FOR ABOUT 1 HOUR, THEN CABIN CREAPED UP TO 9500'. FURTHER DESCENT TO 18000 ALLOWED CABIN TO HOLD STEADY. MAINTENANCE ACTIONS, REPLACED RT PACK VALVE.

Part: HOSE — LEAKING (NR 1 OVERHEAT) · airframe 56,652 hrs · 35,810 cycles

ENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT COMPLIED WITH QRH. AIRCRAFT INCURRED A MAINTENANCE FLIGHT DIVERSION INTO ATL. FLIGHT CREW ADVISED, THAT, THE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED AT APPROXIMATELY 10,000 FT, DURING CLIMB-OUT WITH AN EPR 1.95 INDICATION DISPLAYED, ENGINE NR 1 STRUT OVERHEAT LIGHT 'EXTINGUISHED' WHEN THROTTLE WAS RETARDED. R&R MODULATING SHUTOFF VALVE SENSE LINE. NR 1 ENGINE REQUIRES LEAK CHECK RUN OF SENSE LINES AND INSTALLATION OF STRUT PANELS. RAN NR 1 ENGINE AT 75% N1 FOR A DURATION OF 40+ MINS - RAN WITH BLEEDS OPEN. ALL CHECKED GOOD - NO LEAKS FOUND - A/C RETURNED TO SERVICE.

Part: PUMP — CRACKED (HYD SYSTEM) · airframe 56,167 hrs · 35,418 cycles

APPROX 30 SECS AFTER GOING TO FLAPS 30. TOTAL LOSS OF A HYDRAULIC SYSTEM. ALTERNATE FLAP SYSTEM USED TO RAISE FLAPS TO 15. GPWS SYSTEM INHIBITED. PER CREW DEBRIEF, BOTH HYDRAULIC PUMPS WERE SHUT OFF IMMEDIATELY AFTER PRESSURE LOSS. FOUND NR 1 ENG DRIVEN HYD PUMP CRACKED. REMOVED AND REPLACED NR 1 ENG DRIVEN HYDRO PUMP AND HYD CASE DRAIN. FILTER MANIFOLD ASSY REF M/M 29-11-033-4 AND M/M 29-11-041-2. SERV HYDRO.

Part: HYDRAULIC LINE — BROKEN (HYDRAULIC SYSTEM) · airframe 55,575 hrs · 34,920 cycles

TOTAL LOSS OF HYD SYS A IN FLT FOUND A SYS HYD RETURN LINE BROKEN JUST O/B OF NR 3 SPOILER, ADDED MPN 65-17840-492, CPN 0029943 QTY 1 TUBE AY MSN 1018327 MANUFACTURE HYD LINE O/B OF NR 3 SPOILER REF 727-200 MM 20-10-005-8. INSTALLED SAME. NEEDS LEAK CK. INSPECTION REMOVED AND REPLACED BOTH NR 1 AND NR 2 ENG CASE DRAIN FILTERS PER MM 29-11-041, CASE DRAIN FILTERS LEAK CK GOOD. PERF LEAK CK OF LINE. NO LEAKS NOTED. EXERCISED ALL DOORS, FLT CTLS ETC AND SERV HYD. OPS CK/LEAK CK IS GOOD. SWUNG GEAR, REQUIRED SERV AND TOPPED OFF HYD FLUID. SERVICED HYD SYS, RAN NR 1 AND NR 2 ENGS, CKD CASE DRAIN FILTERS, NO LEAKS NOTED. PER JRH AND SMP.

Part: HYDRAULIC LINE — BROKEN (HYDRAULIC SYS) · airframe 55,331 hrs · 34,742 cycles

EN ROUTE TO KFNT SYS A HYDRAULIC FLUID WENT TO ZERO QUANTITY. ALONG W/ 2 SYS A LOW PRESSURE LIGHTS. HYDRAULIC SYSTEM LEAK OR LOSS PROCEDURES ACCOMPLISHED IAW QRH. FOUND NR 2 SPOILER HYD RETURN LINE BROKEN. REMOVED AND REPLACED BOTH NR 1 AND NR 2 HYDRAULIC CASE DRAIN FILTERS IAW M/M 29-11-041-2. REMOVED AND REPLACED BOTH A SYSTEM PRESSURE FILTERS IAW M/M 29-11-062-3. SERVICED HYDRAULIC SYSTEM BACK TO FULL IAW M/M 12-12-000-2 PER M/M 29-11-000-1.

Part: HYDRAULIC LINE — BROKEN (HYDRAULIC SYS) · airframe 55,331 hrs · 34,742 cycles

EN ROUTE TO KFNT SYS A HYDRAULIC FLUID WENT TO ZERO QUANTITY. ALONG W/ 2 SYS A LOW PRESSURE LIGHTS. HYDRAULIC SYSTEM LEAK OR LOSS PROCEDURES ACCOMPLISHED IAW QRH. FOUND NR 2 SPOILER HYD RETURN LINE BROKEN.

Part: REPAIR — MISINSTALLED (FUSELAGE) · airframe 55,246 hrs · 34,657 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA. 500, STR 29L IS NOT CONFORMED TO FAA APPROVED DATA. REMOVED EXISTING REPAIR, FABRICATED REPAIR DOUBLER IAW SRM 53-30-3, FIGURE 3 AND REINSTALLED REPAIR DOUBLER IAW SRM 53-30-3 FIG 3 AND SRM 51-30-2. REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: INDICATION SYS — OUT OF RIG (DOORS) · airframe 54,898 hrs · 34,361 cycles

LIGHT ILLUMINATED, PASSING 16K MSL (MCD A LIGHT WAS OUT AND TESTED GOOD). DESCENDED TO 10K MSL. LIGHT EXTINGUISHED AT 12K MSL, BULB TESTED GOOD. RELEASED FOR SERVICE PER MEL/CDL: 52-15-01 CATEGORY: C EXP: 26DEC05 "MEL 52-15-01: MCD WARN LIGHT SYS B INOP. VERIFY DOOR CLOSED AND LOCKED PRIOR TO EACH BLOCK OUT." FOUND MCD 'B' LIGHT RIGGED OUT OF SEQ WITH 'A' (PREMATURE TO INDICATE), ADJ CONTACT, IND NORMAL AND IN SEQ WITH SW 'A'.

Part: ROLLER — DAMAGED (AIRSTAIR) · airframe 54,427 hrs · 33,961 cycles

DURING LANDING ROLLOUT, AFT AIRSTAIR EXTENDED. REMOVED AND REPLACED AFT RT SIDE ROLLER BECAUSE ROLLER DOES NOT TURN. REPLACED MAIN BEARING AS PER 727-200 M/M 52-62-001-1, T/S DOOR OPS CKED OK. OK FOR FLT.

Part: RIB — CRACKED (NR 4 SPOILER) · airframe 53,152 hrs · 32,979 cycles

LT WING AFT SPAR, NR 4 SPOILER ACTUATOR INBOARD SUPPORT RIB IS CRACKED. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-30-2. RECEIVED NEW FABRICATED SUPPORT ANGLE P/N FX65-24608 -7, ON TRAVELER T2/385523. LOCATED & DRILLED NEW PART IAW SRM 51-20-1. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-30-2 & 51-20-4. LEAK CHECK TO BE DONE ON TANK CLOSE CARD N00826.

Part: FITTING — GOUGED (NR 1 SLAT) · airframe 53,152 hrs · 32,979 cycles

WINGS BASIC- REWORK OF SLIGHT GOUGE IN L/E SLAT ACTUATOR FITTING. COMPLIED WITH ALL ASPECTS OF EA 7-5740-73855.

Part: FITTING — CHAFED (ZONE 800) · airframe 53,152 hrs · 32,979 cycles

COMPLY WITH EA 7-5340-73853 FUSELAGE FITTINGS MAIN CARGO DOOR UPPER JAMB LIFT FITTING GOUGES. COMPLIED WITH EA7-5340-73853 DATED 11/20/03 FUSELAGE FITTINGS MAIN CARGO DOOR UPPER JAMB LIFT FITTING GOUGES.

Part: DUCT — BLOWN (NR 1 ENGINE) · airframe 52,391 hrs · 32,363 cycles

DURING CLIMBOUT WITH STANDARD TAKEOFF POWER SET, NR 1 ENGINE FIRELIGHT ILLUMINATED WITH HORN ON. SHUT DOWN ENGINE IAW WITH CHECKLIST. REMOVED AND REPLACED MAIN OIL STRAINER DUE TO INFLIGHT SHUT DOWN OF NR 1 ENGINE. ENGINE WINDMILLED FOR APPROXIMATELY 10 MINUTES. WORK DONE IAW AMM. LEAK CHECKED GOOD. REMOVED AND REPLACED 13TH STAGE SADDLE DUCT IAW AMM. LEAK CHECKED GOOD. AWAITING UPPER ENGINE COWL. INSTALLED UPPER ENGINE COWLING IAW AMM. OK FOR SERVICE.

Part: DUCT — KINKED (E/E BAY)

NO RACK COOLING LIGHT ILLUM. REPOSITIONED KINKED DUCT PER MM 21-58-001.

Part: OVERHEAT LOOP — MALFUNCTIONED (OVERHEAT SYS)

LWR AFT BODY O/H LIGHT ISOLATED LEAK BETWEEN BLD VLV AND PACK VLV. REMOVED AND REPLACED FIRE DETECTOR PER MM 26-14-000-5. OPS CHECK GOOD ON GROUND.

Part: DOOR — MALFUNCTIONED (NLG)

RED DOOR LIGHTS AND S/O AMBER NOSE GEAR DOOR LIGHT REMAINED ILLUM'D AFTER GEAR RETRACTION W/HANDLE UP. CREW FELT/HEARD NOSE GEAR DOOR NOT FULLY CLOSED. ACCOMPLISHED RED TABS. AFTER GEAR WAS RECYCLED CREW FELT/HEARD SUBSTANTIALLY LESS NOISE AIRSPEED LIMITED TO 270 KNOTS OR LESS. LIGHT WENT OUT AT 6000 MSL 190 KNOTS.

Part: VALVE — FAILED (MLG DOOR)

DURING GEAR RETRACT RED DOORS LIGHT AND AMBER GEAR DOOR LIGHT (2ND OFF PNL) REMAIN ILLUM. RECYCLED GEAR. *S/D* REMOVED AND REPLACED NOSE SCHRADER VALVE AND RESERVICE PER MM 12-15-025-2. CHECKED 6 HRS LATER, NO LEAKS AND PRESSURE THE SAME.

Part: WHEEL — MISSING (RT MLG)

98-302 - RIGHT OUTBD WHEEL AND ASSEMBLY MISSING. REMOVED AND REPLACED RIGHT MAIN LAND GEAR ASSY PER MM 32-11-0 PG 401-601 AND FEDEX A/C MAINTENANCE WORK CD 32T/502. OK FOR SERVICE.

Part: AIR DATA COMP — FAILED (E/E COMP)

AIR DATA COMPUTER NR 1 CIRCUIT BREAKER POPPED ON TAKEOFF ROLL, CONTINUED TO TROUBLESHOOT PROBLEM IN AIR. CIRCUIT BREAKER WOULD NOT RESET. RETURNED TO SDF FOR MAINTENANCE TO WORK. REMOVED AND REPLACED AIR DATA COMPUTER PER MAINTENANCE MANUAL 34-12-0 PAGES 8 AND 9. OPERATIONAL CHECK OK, PERFORMED PITOT/STATIC LOW RANGE PER MAINTENANCE MANUAL 34-11-0 PAGES 503 AND 504.

Part: AIR DATA COMP — FAILED (E/E COMPT)

98-0011 - ON CLIMB-OUT (APPROX 2000FT) CAPTAIN LOST AIRSPEED, ALTIMETER, GPWS. SUSPECTED NR 1 AIR DATA COMPUTER FAILURE. ALL CIRCUIT BREAKERS CHECK, NONE TRIPPED. RED TABS COMPLIED WITH. REMOVED AND REPLACED NR 1 AIR DATA COMPUTER. PERFORMED LOW LEVEL LEAK OF CAPTAINS'S PITOT/STATIC SYSTEM. LEAK CHECKS GOOD. AIR DATA COMPUTER FUNCTION TEST IS GOOD. ALTIMETER ALERT AND GPWS CHECK GOOD.

Part: AIR DATA COMP — FAILED (E/E COMPT)

98-0010 - NR 1 AIR DATA COMPUTER CIRCUIT BREAKER TRIPPED ON CLIMB-OUT, EFFECTING CAPTAIN'S AIRSPEED, ALTIMETER, GPWS. RESET CIRCUIT BREAKER TRIPPED AGAIN. REMOVED AND REPLACED NR 1 AIR DATA COMPUTER. SYSTEM OPERATIONAL AND LEAK CHECKS GOOD.

Part: FUEL PUMP — MALFUNCTION (NR 1/3)

AFTER T/O, THE NR 1 CSD RISE TEMP WAS PEGGED OFF SCALE HIGH. THEN NOTICED NR 1 CSD LO PRESS LIGHT FLICK EVERY 5-15 SEC. NR 1 GEN OUTPUT NORM BUSSES WERE IN PARALLEL OPER. THEN NR 1 ENG ROLL BK AND BEGAN TO SURGE. DISCONNECTED NR 1 CSD JUST AS WE BEGAN TO RUN THE LO PRESS CSD LIGHT CK LIST THE NR 1 ENG BEGAN TO ROLL BK AND SURGE FOLLOW BY NR 3 ENG ROLL BK AND SURG, WENT TO TANK TO ENG AND ALL PUMPS ON. THROT NR 1 AND 3 RETARD AND EMER DESCENT BEGAN NR 3 STAB AT IDLE. REINSTALL B/S PLUG AND IGN PLUG. FUEL FILTERS REMOVED AND INSP. REMOVED AND REPLACED NR 1 AND 3 MAIN FUEL PUMPS PER PWA M/M 73-11-1 PG 401. OPS AND LK CK OF 1 AND 3 ENG GOOD.

Part: CIRCUIT BREAKER — TRIPPED (AIR DATA COMP)

ON TAKEOFF ROLL, CAPTAINS AIR SPEED AND ALTIMETER FAILED. AFTER AIRCRAFT WAS LOADED IN RAIN SHOWERS. NR 1 AIR DATA COMPUTER CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER AND RAN OPERATIONAL CHECK PER MAINTENANCE MANUAL 34-12-0 PAGE 509, OPERATIONAL CHECK GOOD. LOWER ELECTRICAL COMPARTMENT WAS CHECKED FOR WATER BEFORE DEPARTURE AND WAS FOUND TO BE DRY. AIRCRAFT DOWN GRADED TO CHECK CAT 2.

Part: FLOOR BEAM — CORRODED (BS 344)

FLOOR BEAM UPPER CHORD UPPER SURFACE CORRODED AT STA 344 BL ZERO - LBL 60. REMOVED CORROSION ON UPPER CHORD SURFACE - BEYOND LIMITS PER SRM 51-10-6. REMOVED AND REPLACED TOP TEE ANGLE PER SRM 51-10-1. FLOOR BEAM REPAIRED USING FEDEX END DRAWING SR 27-53-007.

Part: FLOOR BEAM — CORRODED (BS 870)

FLOOR BEAM UPPER CHORD UPPER SURFACE CORRODED STA 870, LB 25 - 45, WL 208. REMOVED CORROSION, INSTALLED REPAIR DOUBLER PER 53-10-07-02.

Part: STRINGER — CRACKED (BS 720)

UPPER LOBE, BL 9, 720C, STR 15L CRACKED. REMOVED DAMAGE AND INSTALLED STR SPLICE PER SRM 53-10-3.

Part: SUPPORT — CORRODED (BS 758-848)

SEAT TRACK SUPPORT UPPER CHORD UPPER SURFACE CORRODED STA 758-848, LBL 45. REMOVED AND REPLACED SEAT TRACK SUPPORT PER SRM 51-10-01, STA 758 - 848.

Part: TR SWITCH — FAILED (NR 1 ENGINE)

AFTER T/O, ENG NR 1 REVERSER OPERATING LIGHT CAME ON NR 1 ENGINE, SHUTDOWN AS PER PROCEDURE. A/C RELEASED FOR SERV PER MEL 78-2A. CHECKED WIRING HARNESS AT SWITCH FOR CONDITION, FOUND GOOD. CHECKED SW ADJ, WITHIN LIMITS. DURING T/S HAD NR 1 T/R OPS LIGHT GLOW DIM FOR SEVERAL SECONDS AND EXTINGUISH, WHILE NOTHING AROUND SW WAS TOUCHED. SUSPECT EITHER INTERNAL FAILURE OF SW (P/N B27-78-064-01) OR LIGHT SOCKET (10-61803-78). REPLACED NR 1 T/R SW, OPS CHECK GOOD.

Part: CADC — MALFUNCTIONED (LEFT)

AFTER TAKEOFF, THE CAPTAIN'S AIRSPEED AND ALT FLAGS CAME IN VIEW. PROBABLE CASE FAILURE. THE AIR DATA CMPTR CB WAS POPPED AND WOULD NOT RESET. REMOVED AND REPLACED AIR DATA COMPUTER PER MM 34-12-01. OPS CHECK GOOD, NEEDS PITOT STATIC CK. A/C DOWNGRADED TO NOT CAT 2, CKA AND CKB W. NOLTE 16114 PERFORM PITOT STATIC CHECK. IAW MM 34-11, OPS CK NORMAL NOTE INITIAL ROOT CAUSE WET E & E COMPARTMENT SR 13661.