N207UP

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A COCKPIT EMERG EXIT LIGHT INTERMITTENT, OFF WHEN SHOULD BE ON OR ON W HEN SHOULD BE OFF CLEANED CONTACTS, REINSTALLED, OP CHECKS GOOD

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A COCKPIT EMERGENCY EXIT LIGHT INTERMITTENT- OFF WHEN SHOULD BE ON, OR ON WHEN SHOULD BE OFF. CLEANED CONTACTS. REINSTALLED. OPS CK NORMAL PER MM 33-50-01.

Part: ACTUATOR — INOPERATIVE (TE FLAPS)

INSPECTION TYPE:N/A ON T/O RFD, FLAPS HUNG AT GREATER THAN 2 DEG (IN BLACK BAND) L/E FLAP LIGHT RED CHRISTMAS TREE INDICATES LEP 5, 6 FAILED TO RETRACT, AMBER LIGHTS. RECYCLED, NO HELP. AIR TURNBACK RFD, GROUND TEST IN RFD INBOARD FLAPS LAGGING BEHIND OUTBOARD''S BADLY. REMOVED AND REPLACED NR 6 L/E SLAT ACTUATOR.

Part: COUPLER — FAILED (SPOILERS)

INSPECTION TYPE:N/A, PILOT REPORT A/C ROLLED 30 DEGREE DURING FLIGHT UNABLE TO TRIM AIRCRAFT UNTIL SYS A OUTBOARD SPOILERS SECURED. *S/D* PERFORMED ILLEG AND OPS CK OF SPOILER SYS W/R/T MM 27-61-00 PERFORMED RIG AND OPS CK OF ILLEG SYS W/R/T 27-10-00, NO DEFECTS NOTED AT THIS TIME. FOUND LOWER ILLEG COUPLER BAD, REMOVED AND REPLACED W/R/T MM 22-11-131 (P/N 4080952-901) (S/N 77100)

Part: STRINGER — CRACKED (FUSELAGE) · airframe 27,549 hrs · 21,265 cycles

INSPECTION TYPE:C, BS 500 - 503 STR 6L CRACKED AND 2 DOUBLE HOLES. REMOVED DAMAGED SECTION OF STR 6L, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-3, 51-30-2.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 27,549 hrs · 21,265 cycles

INSPECTION TYPE:SI, WHILE WORKING CUST CARD NR 159636 FOUND STR L/R CRACKED IN RADIUS AT BS 680. REMOVED DAMAGED SECTION OF STRINGER, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-3.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 27,549 hrs · 21,265 cycles

INSPECTION TYPE:C WHILE WORKING CUST CARD 159636, FOUND STR 1 CRACKED ON INNER FLANGE CORNER AT BS 660. REPAIRED CRACKED STRINGER IAW SRM 53-10-03.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 27,549 hrs · 21,265 cycles

INSPECTION TYPE:C WHILE WORKING CARD NR 159523 FOUND 1 INCH CRACK IN RADIUS OF STR 9L BS 500 WL 268, LBL 66. EVALUATED CRACK, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SECTION OF STRINGER SECTION BS 480 - 507 STR 9L WL 268. FABRICATED NEW STRNGER SECTION USING BAC5300 REFERENCE MATERIAL BAC1498-140 7075T6 BACK. DRILLED NEW SECTION AND INSTALLED IAW SRM 51-30-2, SRM 51-30-5.

Part: SEAT TRACK — CRACKED (BS 522)

INSPECTION TYPE:C CRACKED SEAT TRACK AT BS 522, LBL 25, WL 206. REMOVED DAMAGED SECTION INSTALLED NEW SECTION, FABRICATED SPLICES AND REPAIR EXTRUSIONS, WORK DONE IAW SRM 51-30-2, 53-10-5 AND 51-20-4.

Part: SEAT TRACK — CRACKED (FUSELAGE)

INSPECTION TYPE:C CRACKED SEAT TRACK AT BS 522, LBL 45, WL 206. REMOVED DAMAGED SECTION, INSTALLED NEW SECTION, FABRICATED AND INSTALLED FABRICATED ANGLES AND STRAPS WORK DONE IAW SRM'S 53-10-5 51-30-2 AND 51-20-4.

Part: ANGLE — CORRODED (BS 304)

INSPECTION TYPE:C CORROSION (C53-111-03.00-01) ON L ANGLE AT BS 304, WL 150, RBL 20 (BELOW DOG HOUSE FLOOR). REMOVED, FABRICATED AND INSTALLED NEW ANGLE, WORK DONE IAW SRM 53-10-2, 51-30-2 AND SRM 51-40-2.

Part: ANGLE — CRACKED (FUSELAGE)

INSPECTION TYPE:C JACK STAND COMPARTMENT SURROUNDING STRUCTURE IS CRACKED AND DENTED LBL 11 TO LBL 17. REMOVED CRACKED ANGLE. FABRICATED AND INSTALLED NEW ANGLE. WORK DONE IAW SRM'S 51-30-2, 53-10-1, 51-30-5 AND 51-10-2.

Part: FUEL PUMP — FAILED (NR 1 ENGINE)

INSPECTION TYPE-N/A, CLIMBING OUT OF 700 FT AGL NR 1 ENGINE FAILED. CHECKLIST RUN ENGINE WAS IN RESTART ENVELOPE, RESTART ATTEMPT UNSUCCESSFUL OIL PRESS AND INDICATIONS NORMAL. REMOVED AND REPLACED NR 1 FUEL CONTROL AND FUEL PUMP PER MM 73-21-1 AND 73-11-1, RUN CK GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT)

COCKPIT EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE WHEN TESTED FROM PILOT'S OVERHEAD PANEL. INSTALLED FRESHLY SERVICED BATTERIES IN REPLACEMENT COCKPIT EMERG EXIT LIGHT ASSY AND INSTALLED AND TESTED LIGHT, IAW MM 33-50-101, TEST GOOD, PN ON-OFF 10-0067-9. SN OFF 28163 SN ON 12740.

Part: FLAP TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE-SI, CORROSION (C57-581-05.00-04) NR 8 FLAP TRACK CENTER AFT MOUNT HOLE HAS CORROSION. REMOVED CORROSION IN MOUNT HOLE PER UPS EO NR 727-57-1963.

Part: FLAP TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE-SI, CORROSION (C57-581-05.00-04) NR 7 FLAP TRACK FORWARD MOUNT CENTER HOLE IS CORRODED. REMOVED CORROSION IN MOUNT HOLE PER UPS EO NR 727-57-1964.

Part: FLAP TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE-C, CORROSION (C57-581-05.00-04) NR 7 FLAP TRACK AFT CENTER MOUNT HOLE HAS CORROSION. REMOVED CORROSION ON MOUNT HOLE PER UPS EO NO 727-57-1964.

Part: TRACK — CORRODED (BS 740-755)

INSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON EXPANSION LINK LBL 45 BS 740 TO 755 WL 207 TO 208. REMOVED CORROSION ON EXPANSION LINK FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED EXPANSION LINK/TRACK PER SRM 51-30-4.

Part: SEAT TRACK — CORRODED (BS 990-1005)

INSPECTION TYPE-SI, THE SEAT TRACK AT RBL 55 HAS CORROSION AROUND NUT PLATE HOLES BETWEEN BS 990 TO 1005 WL 208. REMOVED AND REPLACED SEAT TRACK SECTION BS 990 TO 1010 IAW SRM 51-30-2 53-10-01, 51-10-02.

Part: BOTTLE PIN — CORRODED (RT WING/FUS)

INSPECTION TYPE-SI, RT WING AFT BOTTLE PIN CORRODED. REPLACED BOTTLE PIN PER 727 MM 57-41-01.

Part: BRACKET — CORROSION (BS 720)

INSPECTION TYPE-SI, CORROSION (C53-224-01.00-01) ON FRAME AND BRACKET AT BS 720C STR 7 LT FRAME WITHIN LIMITS, BRACKET OUT OF LIMITS. REMOVED CORROSION ON FRAME, FABRICATED AND INSTALLED NEW BRACKET IAW SRM 51-20-1, 51-10-6, 51-10-02, 51-30-2.

Part: SEAT TRACK — CORRODED (BS 870-960)

INSPECTION TYPE-C, CORROSION ON SEAT TRACK FLANGE, AS MARKED, IN MAIN DECK BS 870 TO 960 RBL 45 WL 208. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPLACED WITH NEWLY FABRICATED ITEM PER SRM 53-10-5, 51-30-2 AND 51-30-0.

Part: TUBE ASSY — CHAFED (B-HYD SYST)

INSPECTION TYPE-N/A, ON TAKEOFF ALL B-HYDRAULIC SYSTEM LOW PRESS INDICATOR LIGHTS ILLUM. CIRCUIT BREAKERS FOR B-SYSTEM PUMPS AND INDICATOR WERE CYCLED OFF FOR TWO MINUTES AND BACK ON. LOW PRESS LIGHTS REMAINED ON. REPLACED CHAFED B-SYS HYD RETURN LINE IN HYD SERVICE BAY PER MM 20-10-5. SERVICED SKYDROL PER 12-12-00, LK CK GOOD. REPLACED CASE DRAIN FILTERS ON SEG CK 13.

Part: FRAME — CRACKED (AFT SERVICE DOOR)

INSPECTION TYPE-C, RIGHT HAND AFT SERVICE DOOR FORWARD FRAME LOWER HINGE CUTOUT UPPER I/B CORNER IS CRACKED .35 LONG. REMOVED AND REPLACED AFT SERVICE DOOR FORWARD FRAME IAW SRM 51-10-1, 51-10-2, MM 51-20-151, 52-14-00.

Part: SHEAR TIE — CORRODED (BS 950)

INSPECTION TYPE-C, CORROSION ON SHEAR TIE AT BS 950E PLUS 3 WL 149 RBL 9. MECHANICALLY REMOVED CORROSION FROM SHEAR TIE AT BS 950E PLUS 3 WL 149 RBL 9. REWORKED DEEMED OUT OF LIMITS IAW SRM 53-10-1, REPAIRED SHEAR TIE/FRAME IAW SRM 53-10-4.

Part: BULLNOSE — CORRODED (NR 4 LE FLAP)

INSPECTION TYPE-C, CORROSION ON NR 4 K-FLAP BULLNOSE OUTBOARD BONDING JUMPER ATTACH POINT. MECHANICALLY REMOVED CORROSION ON NR 4 K-FLAP BULLNOSE OUTBOARD BONDING JUMPER ATTACH POINT. REWORKED DEEMED OUT OF LIMITS IAW SRM ADDENDUM B727-5740-3980A. REPAIRED AREA IAW TRAMCO EWO 96-2517 N/A.

Part: RIB — CRACKED (NR 5 LE SLAT)

INSPECTION TYPE-C, WHILE WORKING WINGS 162 FOUND CRACKED RIB ON NR 5 SLAT O/B OF ROD END DUE TO OTHER DAMAGE TO NR 5 SLAT. THE SLAT IS BEING REPLACED ON NRC 607692 AND INSTALLED ON NRC 607694.

Part: FRAME — CORRODED (BS 970)

INSPECTION TYPE-C, CORROSION ON SHEAR TIE AT BS 970 FRAME RBL 8 WL 149. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, CUT OUT DAMAGE AND REPLACED PER SRM 53-10-4.

Part: SHEAR TIE — CORRODED (BS 720)

INSPECTION TYPE-C, CORROSION ON AFT SIDE OF SHEAR TIE AT BS 720C WL 149 RBL 10. MECHANICALLY REMOVED CORROSION IAW SRM 51-10-6, REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPLACED SHEAR TIE IAW SRM 51-20-1, 51-30-2 AND MM 51-20-151.

Part: LINE — FAILED (B-HYD SYSTEM)

CREW REPORTED, AFTER GEAR EXT, LOSS OF B-SYSTEM PRESSURE AND LOW PRESSURE LIGHTS CAME ON. B-SYS PRESS ZERO AND QUANTITY DECREASED FROM 3 TO 1.9, RAN APPROVED CHECKLIST, LOST B-SYS. REPLACED NR 2 PUMP PRESSURE LINE WITH TEMPORARY FLEX LINE BETWEEN B-PUMP AND B-SYS MODULE PACKAGE. NO LEAKS NOTED, OPS CHECK OK (DEFFERAL NR D-106432).

Part: LIGHT — INOPERATIVE (CABIN)

YHM - MAINTENANCE REPORTED, L 1 EMERGENCY EXIT LIGHT WILL NOT TEST. LIGHT ASSY REMOVED AND REPLACED AND OPS CHECKED GOOD AS PER MM 33-50-01.

Part: BATTERY PACK — DISCHARGED (FLIGHT DECK)

MAINT REPORTED, FLIGHT DECK EMERGENCY EXIT LIGHT DIM DUE TEST. FOUND COCKPIT DOOR EMERGENCY LIGHT ASSY BAD. REMOVED AND REPLACED LIGHT ASSY AND BATTERIES IAW MM 33-50-101 PAR 1 TO 3 PAGE 202 TO 203, GND OPS GOOD.

Part: FRAME — CRACKED (FS 840)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND BOX FRAME UPPER WEB AT STA 840 RBL 65 CRACKED. REPLACED IAW SRM 51-30-2, M/M 51-20-151, 51-20-21.