N208UP

Part: SKIN — GOUGED (FUSELAGE) · airframe 27,444 hrs · 20,985 cycles

INSPECTION TYPE:C, GOUGED SKIN AT BS 187 WL 160 LBL 7. REPAIRED PER SRM 53-30-3.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 27,444 hrs · 20,985 cycles

INSPECTION TYPE:C WHILE WORKING CUSTOMER CARD 140368, FOUND UPPER SURFACE OF THE BS 312 FLOORBEAM CORRODED RBL 47 - 50 WL 208. REMOVED FABRICATED AND INSTALLED UPPER CHORD BS 312 RBL 27 - 64 WL 208 PER SRM 53-10-8.

Part: BATTERY — INOPERATIVE (COCKPIT)

INSPECTION TYPE:P/F, COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERIES AS REQUIRED. LIGHT OPS CHECK GOOD.

Part: FLOORBEAM — CORRODED (BS 1130)

INSPECTION TYPE:SI, CORROSION (C53-111-01.00-03) ON LOWER CHORD OF BS 1130 FLOORBEAM AT NUT CLIP HOLES BL 0-RBL 50, WL 201. REPAIRED FLOORBEAM PER ER NR 99-5650.

Part: SEAT TRACK — CORRODED (BS 630-638)

INSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 630 TO BS 638 RBL 45. REPLACED PER SRM 51-10-1.

Part: SEAT TRACK — CORRODED (BS 705)

INSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 705 TO BS 708 RBL 95 WL 208. REPLACED TRACK PER SRM 51-10-1.

Part: SHEAR TIE — CORRODED (BS 720)

INSPECTION TYPE:SI, SHEAR TIE CORRODED BS 720 FRAME BETWEEN 25 AND 26 RT. REMOVED AND REPLACED SHEAR TIE PER SRM 51-30-2 PG 2.

Part: SEAT TRACK — CORRODED (BS 690)

INSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 690 LBL 45, WL 208. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10-5 PG 4.

Part: STRINGER — CORRODED (BS 720 & 1270)

INSPECTION TYPE:SI, CORROSIN AND TOOLING DAMAGE ON STRINGER 7 LT BS 720B AND 1270+18. REMOVED CORROSION DAMAGE, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. PERFORMED STRINGER REPAIR PER SRM 53-10-3.

Part: TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE:SI, CORROSION (C57-581-06.00-04) ON NR 5 FLAP TRACK AT SPOILER BEAM PAD FWD ATTACH LUG AND INSIDE L/G BEAM ATTACH HOLES. REMOVED NR 5 FLAP TRACK PER MM 27-51-31. REMOVED ATTACH HARDWARE ON NR 5 FLAP TRACK PER SRM 51-30-2. RECEIVED REPLACEMENT FLAP TRACK, INSTALLED ON TC C57-581-04-4D. REINSTALLED ATTACHING HARDWARE ON NR 5 FLAP TRACK PER SRM 51-30-2.

Part: TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE:SI, CORROSION (C57-581-06.00-03) ON NR 1 FLAP TRACK IN REAR SPAR MAIN BOLT HOLE. REMOVED NR 1 FLAP TRACK, ROUTED TO CSD, RECEIVED NEW FLAP TRACK AND INSTALLED IAW 27-51-31.

Part: FRAME — DENTED (BS 680)

INSPECTION TYPE:SI, DENTED I/B FLANGE ON FRAME AT BS 680, LBL 34, STR 24 IN FWD CARGO BAY. THE DENT ON FRAME OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS, ALODINED AND PRIMED THE REPAIR PARTS. INSTALLED REPAIR PARTS, ALL WORK ACCOMPLISHED PER SRM 51-40-3, 51-20-1 AND MM 51-20-21.

Part: SEAT TRACK — CORRODED (BS 1031)

INSPECTION TYPE:SI, SEAT TRACK CORRODED AND DAMAGED TSS 1029 TO BS 1031 RBL 24 WL 208. AFTER REMOVAL OF CORROSION, FOUND THE SEAT TRACK TO GO BEYOND ALLOWABLE LIMITS PER SRM 53-10-1. FABRICATED NEW SEAT TRACK, ALODINED, PRIMED AND PAINTED AND INSTALLED SEAT TRACK, ALL WORK ACCOMPLISHED IAW SRM 53-10-5, 51-30-2, MM 51-20-151.

Part: SHEAR TIE — CORRODED (BS 1130)

INSPECTION TYPE:SI, CORROSION ON SHEAR TIE BS 1130 RBL 5 WL 148. REPLACED PER SRM 51-10-2, SRM 51-10-1.

Part: KEEL BEAM — CORRODED (BS 760)

INSPECTION TYPE:SI, CORROSION ON KEEL BEAM AT BS 760, RBL 7, LBL 7 WL 148. REPLACED PER SRM 51-10-1.

Part: TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE:SI, CORROSION (C57-581-06.00-04) ON NR 7 FLAP TRACK IN REAR SPAR MAIN BOLT HOLE. REMOVED AND REPLACED NR 7 FLAP TRACK.

Part: SKIN — CORRODED (CARGO DOOR)

INSPECTION TYPE:SI, CORROSION (C53-111-02.00-02) EMINATING FROM UNDER 3 RIVNUTS ON INNER SKIN OF AFT CARGO DOOR 11 FROM BOTTOM OF DOOR AFT OF FWD FRAME 10, 18 AND 35. CORROSION REMOVAL FOUND TO BE OUT OF LIMITS ON INNER SKIN OF AFT CARGO DOOR AT 35 FROM FWD FRAME AND 11 ABOVE BOTTOM OF DOOR. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS, PER SRM 51-10-6, 51-10-2, 51-30-2 AND 52-00-02.

Part: FRAME — CORRODED (BS 560)

INSPECTION TYPE:SI, CORROSION (C53-224-01.00-01) ON FRAME BS 560 WL 215 RBL 64. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. COMPLETE STANDARD FORMED SECTION REPAIR PER SRM 51-40-03, SRM 51-10-2 AND SRM 51-40-3.

Part: SEAT TRACK — CORRODED (BS 444-457)

INSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 444 TO BS 457 LBL 45. SEAT TRACK FLANGE FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED NEW SEAT TRACK PER SRM 53-10-5. INSTALLED NEW SEAT TRACK PER MM SRM 53-10-5.

Part: FRAME — CRACKED (BS 540)

INSPECTION TYPE:SI, POSSIBLE CRACK AT FASTENER HOLE IN FRAME BS 540 WL 215 RBL 64. REMOVED DAMAGED AREA IN FRAME, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-40-3, 51-30-2, 51-10-2.

Part: FLOORBEAM — CORRODED (BS 950)

INSPECTION TYPE:SI, CORROSION ON FRAME BS 950, WL 207.5, LBL 55. REMOVED CORROSION AND TREATED AREA PER SRM 51-20-00.

Part: FRAME — CORRODED (BS 930)

INSPECTION TYPE:SI, CORROSION ON FRAME BS 930, WL 207.5, LBL 66. REMOVED CORROSION AND TREATED AREA PER SRM 51-20-00.

Part: FRAME — CORRODED (BS 939)

INSPECTION TYPE:SI, CORROSION ON 940 FRAME WL 207.5 LBL 67 AT BS 939. REMOVED CORROSION AND TREATED AREA PER SRM 51-20-00.

Part: SEAT TRACK — CORRODED (BS 826)

INSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 826, LBL 26, WL 208. REMOVED CORROSION 2 X 4 X 0.001 WITHIN LIMITS PER SRM 53-10-1, ALODINED AND PRIMED.

Part: SEAT TRACK — CORRODED (BS 806)

INSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 806, LBL 26, WL 208. REMOVED CORROSION AND TREATED AREA PER MM 51-20-00.

Part: SEAT TRACK — CORRODED (BS 848)

INSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 848, WL 208, LBL 26. REMOVED CORROSION TREATED AND PAINTED AREA PER MM 51-20-00.

Part: SHEAR TIE — CORRODED (BS 720)

INSPECTION TYPE:SI CORROSION ON SHEAR TIE FWD SIDE BS 720E FRAME BETWEEN STR 26 AND 27 LEFT CORROSION ON SHEAR TIE FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED SHEAR TIE PER 53-10-4 SRM REPAIRED SHEAR TIE PER SRM 53-10-4.

Part: SHEAR TIE — CORRODED (BS 720)

INSPECTION TYPE:SI, CORROSION (C53-111-01.00-03) ON SHEAR TIES FWD AND AFT SIDE BS 720A FRAME BETWEEN STR 25 AND 26 RT CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. INSTALLED NEW PART PER SRM 51-30-2 PG 2 AND 3.

Part: SHEAR TIE — CORRODED (BS 720)

INSPECTION TYPE:SI CORROSION ON FWD FACE OF FRAME AND SHEAR TIE BS 720F BETWEEN STR 27 AND 28 RT. BLENDED CORROSION ON FRAME, FOUND TO BE IN LIMITS PER SRM 53-10-1. SHEAR TIE FOUND TO BE OUT OF LIMITS PER 53-10-1 SRM. REPAIRED SHEAR TIE PER SRM 53-10-4.

Part: FLAP TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE:SI CORROSION (C57-581-06.00-04) ON NR 6 FLAP TRACK AT SPOILER BEAM PAD AND HOLES AND AT FORWARD LUG AND REAR SPAR MOUNT HOLES. REMOVED NR 6 FLAP TRACK, REMOVED HARDWARE, SENT TO OVERHAUL FACILITY. RECEIVED OVERHAULED FLAP TRACK, INSTALLED HARDWARE AND INSTALLED OVERHAULED FLAP TRACK ONTO AIRCRAFT PER SRM 51-30-02, AND OHM 20-50-03.

Part: FLAP TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE:SI CORROSION (C57-581-06.00-03) ON NR 3 FLAP TRACK AT SPOILER BEAM MOUNT PAD AND HOLES AND AT REAR SPAR MOUNT HOLES. REMOVED NR 3 FLAP TRACK, REMOVED HARDWARE, SENT FLAP TRACK OUT TO OVERHAUL FACILITY. RECEIVED OVERHAULED FLAP TRACK AND INSTALLED HARDWARE. ALL WORK IAW SRM 51-30-02 AND OHM 57-40-01, OHM 20-50-03 INSTALLED FLAP TRACK ONTO AIRCRAFT.

Part: VALVE — MALFUNCTIONED (NR 1 ENGINE)

INSPECTION TYPE:N/A ON TAKEOFF ABOVE 80 KTS T6 NR 1 ENGINE OIL PRESSURE WENT ABOVE THE RED LINE TO 65 PSI. WHEN THRUST WAS REDUCED TO CLIMB POWER, T6 OIL PRESS REMAINED ABOVE THE RED LINE UNTIL POWER WAS REDUCED BELOW 1.5 EPR. OIL PRESS REMAINED BELOW THE THE RED LINE UNTIL BLOCK TURN BACK WAS ACCOMPLISHED. REPLACED THE OIL PRESSURE TRANSMITTER AND OIL PRESSURE RELIEF VALVE PER MM 79-30-86 AND 79-33-00. RAN NR 1 ENGINE T/O POWER PER MM 71-00-86 OIL PRESS REMAINED WITHIN OIL PRESS LIMITS OF 45-55 PSI.

Part: CLAMP — LOOSE (NR 3 ENGINE)

INSPECTION TYPE:N/A, NR 3 STRUT OVERHEAT LIGHT LIGHT WENT OUT AFTER 15-20 SECONDS. UNABLE TO COMPLETE CHECK LIST DUE TO NR 1 ENGINE SHUTDOWN AND CLOSE PROX TO LANDING. NR 3 PRECOOLER CLAMP LEAKING. TIGHTENED CLAMP, RAN ENGINE NO DEFECTS PER M/M 36-10-10 & 71-00-00.

Part: COMPRESSOR — STALLED (NR 1 ENGINE)

INSPECTION TYPE:N/A, JUST AFTER T/O PASSING 4,800 FT, NR 1 ENG HAD SEVERE VIBRATION AND EGT CLIMBED IMMEDIATELY TO 800 C WITH THRUST LEVER RETARDED TO FLT IDLE AND EGT CONTINUED TO CLIMB. LOUD BANG (COMPRESSOR STALL) ACCOMPANIED LOSS OF THRUST. REMOVED AND REPLACED NR 1 ENG.

Part: DUCT — BROKEN (NR 1 ENGINE)

INSPECTION TYPE:N/A, FIRE WARNING ON NR 1 ENGINE AFTER TAKEOFF ON CLIMBOUT. SECURED ENGINE IAW PROCEDURE. FIRE WARNING LIGHT/BELL WENT OUT WHEN POWER REDUCED. FOUND FUEL DEICING HEATER DUCT BROKEN. REMOVED AND REPLACED MANIFOLD AND RAN ENGINES. OPS CK AND LK CK GOOD PER MM 71-00-00.

Part: COMPRESSOR — STALLED (NR 3 ENGINE)

COMPRESSOR STALL PASSING FL270. MAX TEMP 620 DEGREES. ALL OTHER LIMITS NORMAL. DID SHUT DOWN OF NR 3 ENGINE. REMOVED AND REPLACED THE NR 3 ENGINE.

Part: BATTERY — DISCHARGED (COCKPIT)

INSPECTION TYPE-N/A, PREFLIGHT COCKPIT EMER EXIT LIGHT CAME OUT OF ASSEMBLY ABOVE DOOR. INSTALLED NEW BATTS AND REPLACED ASSEMBLY, OPS CHECK OK.

Part: SEAT TRACK — CRACKED (BS 514)

INSPECTION TYPE:C SEAT TRACK CRACKED BS 514 AND ELONGATED TEETH AT BS 526, RBL 25 WL 208. REPLACED SEAT TRACK BS 480 TO 530 PER SRM 53-10-5.

Part: WEB — CORRODED (BS 720-725)

INSPECTION TYPE:C WHILE WORKING TC NO CL2-224-03 DISCOVERED CORROSION AT BS 720E TO 725F LBL 65-70 WL 208. REMOVED, FABRICATED AND INSTALLED NEW SHEAR WEB IAW SRM 51-20-01, 51-30-05, 51-30-07, MM 51-20-151.

Part: ACTUATOR — FAILED (SPOILER)

A/C STARTED TO VIBRATE CLIMBING THROUGH FL 250 AT 280 KTS LEVELED AT FL 260 AT MAINTAINED 270 KTS EXCERCISED SPEEDBRAKE LEVER BUT VIBRATION CONTINUED WHEN ABOVE 280 KTS, VIBRATION TO DIMISH IN TURNS. REMOVED AND REPLACED OUTBOARD FLIGHT SPOILER NR 3 ACTUATOR IN REF TO MM 27-61-81. OP CK OK FOR SERVICE AT THIS TIME P/N ON 21450-11, SN OFF 355227A P/N OFF 21450-14 SN OFF 419826.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, TURNING ON NO SMOKING SWT ILLUMINATED THE EMERGENCY LTS ABOVE THE COCKPIT DOOR AND THE FWD ENTRY. REPLACED BOTH EMERGENCY LT ASSYS AND PERFORMED FUNCTIONAL CHECK.

Part: COVER — FELL OFF (PAX DOOR)

INSPECTION TYPE-N/A, EMERG EXIT LIGHT OVER MAIN DOOR COVER FELL OFF. RESECURED COVER F/EMER LIGHT, CKS NORMAL.

Part: LIGHT — FELL OFF (PAX DOOR)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS ABOVE FORWARD ENTRY DOOR FELL OFF. REINSTALLED AS REQUIRED.

Part: SHEAR TIE — CORRODED (BS 990)

INSPECTION TYPE-C, CORROSION ON SHEAR TIE AFT SIDE OF FRAME BS 990 RBL 10 WL 137. REMOVED CORRODED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE IAW SRM 51-30-02, 51-40-03, CORRODED PART OUT OF LIMITS PER SRM 53-10-1.

Part: NOSE CHORD — CORRODED (BS 294.5-297)

INSPECTION TYPE-C, CORROSION ON UPPER NOSE CHORD BS 294.5 TO 297 LBL 14 WL 175 ON LOWER SURFACE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. INSTALLED NEW CHORD IAW SRM 51-10-1, 51-30-2.

Part: SKIN PATCH — DISBONDED (LT TE FOREFLAP)

INSPECTION TYPE-C, L/W INBOARD FOREFLAP HAS A LARGE PREVIOUS REPAIR DISBONDED UPPER SURFACE MID SPAN. REMOVED PREVIOUS REPAIR, INSTALLED A NEW REPAIR IAW SRM 51-40-6.

Part: SKIN — DELAMINATION (NR 10 SPOILER)

INSPECTION TYPE-C, NR 10 SPOILER HAS DELAMINATION AT THE UPPER SURFACE LEFT HAND CORNER. REMOVED DAMAGE, REPAIRED IAW SRM 51-40-6.

Part: LIGHTS — DIM (CABIN)

EMERGENCY EXIT LIGHT ABOVE FWD ENTRY DOOR PARTIALLY LIT. REMOVED AND REINSTALLED EXIT LIGHT ASSY. OPS CHK GOOD.

Part: INDICATION SYST — MALFUNCTIONED (LANDING GEAR)

CREW REPORTED, ON GEAR RETRACTION RED NOSE GEAR LIGHT REMAINED ILLUMINATED. CYCLED GEAR, NORMAL DOOR INDICATION EXTENSION AND RETRACTION. THREE GROUND LIGHTS ON EXTENSION AND NO RED LIGHT ON RETRACTION. RED NOSE LIGHT CAME BACK ON AND FLUCTUATED IN INTENSITY. OCCASIONALLY GROUND NOSE LIGHT CAME ON DIM AND WENT OUT WHILE RED LIGHT STAYED ON.

Part: BEAM — CORRODED (BS 1040-1060)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C53-224-06.00-1), LBL 65, STA 1040 TO 1060 WL 208.2 AT NUTPLATES FOR DOOR SILL AT CREASE BEAM. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED CREASE BEAM, INSTALLED NEW CREASE BEAM, SEALED AND PAINTED PER SRM 51-10-1, 51-30-2 AND 51-10-2.

Part: EEL — DIM (CABIN)

EMERGENCY EXIT LIGHTS ARE DIM WITH SWITCH IN OFF POS. TRANSFERRED TO NRC 374590.

Part: EEL BATTERIES — DISCHARGED (CABIN)

WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERIES, OPS CHECK GOOD.