N17614

Part: WIRE HARNESS — SHORTED (COCKPIT) · airframe 45,858 hrs · 24,464 cycles

F/O SIDE WINDOW SHORTHED OUT DURING T/O. FOUND SHORTHED WIRE BUNDLE (COILED HARNESS) ON F/O SIDE AT WINDOW BASE. REMOVED AND REPLACED COILED HARNESS FOR WINDOW HEAT CONTROL ON F/O SLIDE WINDOW IN REF TO WDM 30-41-11 AND OPS CHECKED IN REF TO AMM 56-12-11-404-007.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,314 hrs · 22,510 cycles

SUPPORT TASK, FWD ENTRY DOOR CUTOUT AREA, HOLE CRACK INDICATION AT STA 302.9 THIRD FASTENER BELOW WL 236.68 (REF EA 5330-03736 CIRCLE NOTE 3 FIG 5 LAST LWR HOLE). INSTALLED REPAIR DOUBLERS IN REF ECRA 5330-04031. INITIATED DIP AS FOLLOW;" BEFORE ACCUMULATION 77,510 TOTAL A/C FLT. CYCLE, PERFORM IN SPT. PER PART 2 OF ECAR 5330-04031. PLANNING CONTACT ENG AFTER ACCUMULATION OF 70K FLT CYCLE BUT BEFORE 71K FLT CYCLE. INTERIM REPAIR ACCOMPLISHED PER ECRU 5330-04031, PART 1. BEFORE THE ACCUMULATION OF 77,510 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM AN INSPECTION PER PART 2 OF ECRU 5330-04031. PLANNING TO CONTACT ENGINEERING AFTER ACCUMULATION OF 70,000 TOTAL FLIGHT CYCLES BUT BEFORE 71,000 TOTAL FLT CYCLES FOR IMPS DETAILS. 1) INIT: AFTER 70,000 BUT BEFORE 71,000 TOTAL A/C F/C & 2) T/A: W/I 77150 TOTAL A/C F/C.

Part: FRAME — CORRODED (FUSELAGE) · airframe 42,314 hrs · 22,510 cycles

FRAME STA 380 AT S28R HAS CORROSION. REPAIRED PER ECRA 5311-01495 PART 1 REF NR LP 9717663 FOR DIP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,314 hrs · 22,510 cycles

SUPPORT TASK FORWARD ENTRY DOOR UPPER HINGE CUTOUT, CRACK INDICATION AT LOWER, MOST FORWARD HOLE OF LWR FITTING LEG. FIG 4 CIRCLE NOTE 7 OF EA 5330-03736 REV B, REPAIRED PER ECRA 5330-04032.

Part: SKIN — CRACKED (L2 DOOR) · airframe 42,314 hrs · 22,510 cycles

L2 DOOR INNER SKIN IS CRACKED AT UPPER SECTION AT CENTER LIGHTENING HOLE. FABRICATED AND INSTALLED REPAIR DOUBLER PER ECRA 5210-02156.

Part: WEB — WORN (RT WING) · airframe 42,314 hrs · 22,510 cycles

RIGHT WING AT APPROX RSS 500 HAS A WORN AREA ON I/B SIDE OF WEB ABOUT 3 INCHES AFT OF AILERON CABLE GROMMET. INSTALLED DOUBLERS REPAIR REF ECRA 5720-02138 PART 1. INITIATED DIP AS FOLLOW; "ACCOMPLISH PERMANENT REPAIR BEFORE 6-7-2012. PLANNING TO CONTACT ENGINEERING AFTER 4-07-2012 BUT BEFORE 5-07-2012 FOR A PERMANENT REPAIR". ACCOMPLISH A PERMANENT REPAIR BEFORE JUNE 7. 2012, REF EC/RA 5720-02138. PLANNING TO CONTACT ENGINEERING AFTER APRIL 07, 2012 BUT BEFORE MAY 07, 2012 FOR A PERMANENT REPAIR. DIP CNTL NR D 05516. 1) INIT: AFTER 04-07-2012 BUT BEFORE 05-07-2012 & 2) T/A: DUE 07 JUN 2012.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,314 hrs · 22,510 cycles

ABB ALL FLOORBEAMS UNDER STRAP BETWEEN STA 767 & 787 CORRODED. REPAIRED PER ECRA 5320-01990. COMPLETED AND ATTACHED FORM 44.00 08.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,314 hrs · 22,510 cycles

SUPPORT TASK - STA 270 CORROSION AROUND SEVERAL FASTENER HOLES ON FLOOR SUPPORT STRUCTURE AT NLG DOWN LOCK VIEWER APPROXIMATELY BETWEEN LBL 6 TO LBL 9. REPAIRED PER ECRA 5311-01497.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 42,314 hrs · 22,510 cycles

SUPPORT TASK, CRACK IN STR SPLICE CHANNEL AT STR 14L JUST FWD OF FRAME STA 360. REMOVED AND REPLACED STR SPLICE CHANNEL AT STR 14L STA 360 REF ECRA 5311-01496.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,314 hrs · 22,510 cycles

DENT ON BOTTOM OF FWD FUSELAGE AT STATION 197 AND A FEW INCHES RIGHT OF CENTER LINE REF ECRA 5331-01463. INSP DENT PER ECRA PART 1 STEP 1-5. NO DEF C/W ECRA 5331-01463 REV B PART 1A. PLACED ON DIP C/N 00814. ACCOMPLISH EC FOR WORK PERFORMED. DIP REMAINS RA 5331-01463 PART 1A AFTER 1 FLT CYCLE & NOT TO EXCEED 3 FLT CYCLE. INSPECT PART 2 AT INTERVALS NOT TO EXCEED 50 FLT CYCLE AND REPAIR PER PART 3 ON OR BEFORE 01/31/2010. PERFORMED HFEC INSPECTION OF SKIN, NO CRACKS NOTED IN DAMAGED AREA PER ECRA 5331-01463 PART 2. PERFORMED HFEC INSPECTION OF AFFECTED AREA IAW ECRA 5331-01463 REV B PART 2 NO FURTHER DEFECTS NOTED DIP REMAINS INSPECTED PER ECRA 5331-01463B PART 2. NO CRACK INDICATIONS PRESENT. DIP REMAINS INSPECTED AREA PER ECRA 5331-01463B PART 2. NO DISCREPANCY NOTED. PERFORMED HFEC REF ECRA PART 2.5331-01463. NO DEFECTS NOTED AT THIS TIME. DIP REMAINS PERFORMED HFEC INSPECTION AT FUSELAGE STA 197 REF ECRA 5331-0146 3 NO DEFECTS NOTED AT THIS TIME DIPS REMAINS INSPECTED DENT PER ECRA 5331-01463 REV B, PART 2. NO CRACK INDICATIONS NOTED. DIP REMAINS. PERFORMED HFEC AT DENT FUSELAGE STA 197 NO DEFECTS NOTED DIP REMAINS INSPECTED AREA PER PART 2 OF ECRA 5331-01463. NO DEFECTS NOTED AT THIS TIME. DIP REMAINS. PERFORMED HFEC INSPECTION PER PART 2 OF EC/RA 5331-01463. NO DEFECTS NOTED. DIP REMAINS. PERFORMED HFEC INSPECTION PER ECRA 5331-01463 PART 2. NO CRACKS NOTED IN DAMAGE AREA. DIP REMAINS WPB QC 791 INSPECTED PER EC.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 42,314 hrs · 22,510 cycles

SUPPORT TASK, L-1 DOOR FUSELAGE OPENING AFT SIDE STR 15 INTERCOSTAL FWD ATTACH CLIP STA 348.2 CRACKED IN RADIUS I/B SIDE. REMOVED AND REPLACED ATTACH CLIP STA 348.2 STR 15L REF ECRA 5311-01496.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 42,314 hrs · 22,510 cycles

L-1 DOOR SURROUND STRUCTURE HAS CRACK ON STR 11 SUPPORT AT STA 360. REMOVED AND REPLACED SUPPORT ANGLE AT STR 11L STA 360 REF ECRA 5311-01496.

Part: FITTING — CORRODED (FUSELAGE) · airframe 42,314 hrs · 22,510 cycles

ABB SKIN CLIP CORRODED STA 727C BETWEEN STR-26 RT. & 27 RT. REMOVED DAMAGED SHEAR TIE AND INSTALLED REPAIR REF SRM 53-00-07 FIG 201 REPAIR 4.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 42,314 hrs · 22,510 cycles

EVIDENCE OF RUST BETWEEN NR 7 FLAP TRACK AND LWR SURFACE OF REAR SPAR REMOVED NR 7 FLAP TRACK ASSY. ROTABLE PARTS CHANGE WAS INDICATED - 24-5753-9-9001 TRACK, FLAP, OB OFF 24-5753-9-9001 1614 ON. REMOVED NR 7 FLAP TRACK. INSTALLED NEW SERVICEABLE FLAP TRACK. REF M/M 27-51-49-404-006. ROTABLE PARTS CHANGE WAS INDICATED - 0927618 TRACK, FLAP, O/B OFF 0000 ON 24-5753-9-9001 1961.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 42,314 hrs · 22,510 cycles

RT WING NR 8 FLAP TRACK AFT ATTACH POINT EMITTING RUST. REMOVED NR 8 FLAP TRACK. INSTALLED NEW SERVICEABLE FLAP TRACK REF M/M 27-51-49-404-006.

Part: FITTING — CORRODED (FUSELAGE) · airframe 42,314 hrs · 22,510 cycles

ABB STA 747 BETWEEN STR 26 RT.& 27 RT SKIN CLIP CORRODED. REMOVED SHEAR TIE AND INSTALLED REPAIR REF SRM 53-00-07 FIG 20 1.

Part: SEAT TRACK — CORRODED (BS 787-887) · airframe 42,314 hrs · 22,510 cycles

LT OTBD SEAT TRACK HAS CORROSION FROM STA 787 TO STA 887. REPAIRED LT OTBD SEAT TRACK BETWEEN STA 787-807, REF SRM 53-00-52, REPAIR 4, PAGE 201, SHEET 1-4, AND STA 807-927 REF SRM 53-00-52 REPAIR 3, PAGE 201, SHEET 1-4, ATTACH FROM 44.008 PAGE 1-2 AND ECRA 5310-05192.

Part: ANGLE — CORRODED (STA 349) · airframe 42,314 hrs · 22,510 cycles

L1 DOOR LT ANGLE, STA 349 JUST AFT OF DRAIN AND ON UNDER SIDE HAS CORROSION. R & R LT ANGLE REF SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,314 hrs · 22,510 cycles

RIGHT O/B SEAT TRACK HAS CORROSION STA 695 FOUND OUT OF LIMITS. CUT & REMOVED SEAT TRACK, FABRICATED NEW TRACK, APPLIED PROTECTIVE COATING, PRIMED & INSTALLED REF SRM 53 -00-52.

Part: TRANSITION PANEL — CORRODED (BS 727-947.5) · airframe 42,314 hrs · 22,510 cycles

ABB LT TRANSITION PANEL CORRODED FROM 727C TO 947.5. REMOVED AND INSTALLED FABRICATED TRANSITION PANEL FROM STA 727- STA 947.5 IN REF TO SRM 53-60-53 AND SRM 53-30-53.

Part: STOP FITTING — CRACKED (R1 DOOR) · airframe 42,314 hrs · 22,510 cycles

R-1 DOOR LOWER AFT STOP FITTING, INTERIOR LEG CRACKED THROUGH HI-LOK HOLE (MARKED). VERIFIED WITH HFEC P/N OF FITTING 65-51647-501. REMOVED CRACKED FRAME REINFORCEMENT, FABRICATED, ALODINED AND PRIMED NEW FRAME REINFORCEMENT AND INSTALLED REF BAC DRAWING 69-69854 AND SRM 51-40-02.

Part: FITTING — CORRODED (TE FLAP) · airframe 42,314 hrs · 22,510 cycles

NR 3 MID FLAP O/B TORQUE TUBE HOUSING HAS CORROSION. REMOVED AND INSTALLED NEW FITTING PER SRM 51-40-02 PARAGRAPH 7 AND 51-20-02 PARAGRAPH 8.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,314 hrs · 22,510 cycles

MAIN FRAME CRACKED AT STA 616 BELOW STR 17 RT. INSTALLED REPAIR PER ECRA 5311-01158.

Part: FRAME — CRACKED (STA 380) · airframe 42,314 hrs · 22,510 cycles

PAX CABIN HAS CRACKED FRAME STA 380 BETWEEN STR 8R AND 9R. REPAIRED FRAME PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,314 hrs · 22,510 cycles

PAX CABIN HAS CRACKED FRAME STA 867 BETWEEN STA 8R AND 9R. REPAIRED CRACKED FRAME AT STA 867 BETWEEN STR 8R AND 9R REF EA 5310-04498 OP 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,314 hrs · 22,510 cycles

RIGHT FRAME CRACKED STA 842 BETWEEN STR 8-9 FRAME WAS CRACKED DURING PSU RAIL BLOCK REMOVAL. REPAIRED RT FRAME AT STA 482 BETWEEN STR8-9 REF EA 5310-04498 OP2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,314 hrs · 22,510 cycles

LEFT FRAME CRACKED STA 482 BETWEEN STR 8&9. REPAIRED LT FRAME AT STR 482 BETWEEN STR 8&9 REF EA5310-04498 OP2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,314 hrs · 22,510 cycles

LEFT FRAME STA 440 BETWEEN STR 8 &9 CRACKED. REPAIRED FRAME STA 440 LT BETWEEN STR 8&9 LT PER EA 5310-04498 OP2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,314 hrs · 22,510 cycles

PAX CABIN HAS CRACKED FRAME STA 440 BETWEEN STR 8R AND 9R. INSTALLED REPAIR ANGLES, REF EA5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,314 hrs · 22,510 cycles

PAX CABIN HAS CRACKED FRAME STA 787 BETWEEN STR 8R AND 9R. INSTALLED REPAIR ANGLES REF EA5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,314 hrs · 22,510 cycles

SUPPORT TASK LT FUSELAGE FRAME CRACKED BETWEEN STR 8&9 STA 400. INSTALLED REPAIR ANGLES A&B PER EA 5310-04498.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 42,182 hrs · 22,443 cycles

AFT RT EMERGENCY FLASHLIGHT INDICATOR DOES NOT FLASH. REMOVED AND REPLACED AFT RT EMERGENCY FLASHLIGHT BATTERY. OPS CHECK GOOD.

Part: CIRCUIT BREAKER — TRIPPED (LANDING GEAR) · airframe 41,784 hrs · 22,230 cycles

AT FLIGHT IDLE ONLY THE NOSE GEAR RED LIGHT IS ILLUMINATED NOT THE MAIN GEARS. FOUND AIR/GND RELAY C/B OUT (PG-3, ROW 17C) AS DIRECTED BY MAINTENANCE, RESET C/B (CONT L/P 8331803) RESET C/B AND TROUBLESHOT PER AMM 32-61-00/101. LANDING GEAR LEVER WAS CYCLED SEVERAL TIMES. NO DEFECTS WERE NOTED. ALL INDICATIONS NORMAL. C/B REMAINED SET. A/C OK TO CONTINUE.

Part: CABLE — FRAYED (GIRT BAR) · airframe 41,422 hrs · 22,029 cycles

L2 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR LATCH CABLE HAS BROKEN STRANDS (FCD 2561-01189). REMOVED AND REPLACED L2 EMERGENCY ESCAPE SLIDE CABLE IAW 737AMM 25-61-35-402-007.

Part: CABLE ASSY — FRAYED (L2 DOOR) · airframe 41,256 hrs · 21,950 cycles

L2 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR LATCH CABLE HAS BROKEN STRANDS (FCD 2561-01189). REMOVED AND REPLACED L2 EMERGENCY ESCAPE SLIDE CABLE IAW 737 AMM 25-61-35-402-007.

Part: CABLE ASSY — FRAYED (R2 DOOR) · airframe 41,256 hrs · 21,950 cycles

R2 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR LATCH CABLE HAS BROKEN STRANDS (FCD 2561-01189). REMOVED AND REPLACED R2 DOOR EMERGENCY ESCAPE SLIDE CABLE IAW 737 AMM 25-61-35-402-007.

Part: UPLOCK ACTUATOR — MALFUNCTIONED (RT MLG) · airframe 41,198 hrs · 21,922 cycles

RIGHT MAIN GEAR UNSAFE AFTER TAKEOFF, AIRCRAFT DESCENDED TO LOWER ALT, AS THROTTLES ADVANCED RIGHT MAIN GEAR FREE FELL DOWN. EXECUTED UNSAFE GEAR INDICATION CHECK LIST, GEAR DOWN 3-GREEN, AIR RETURN ACCOMPLISHED. CYCLED LANDING GEAR SEVERAL TIMES, NO FAULTS NOTED. REMOVED AND REPLACED RIGHT MAIN UPLOCK ACTUATOR IAW MM 32-32-41 AS A PRECAUTION. REF TO NR 4335180 FOR OPS AND LEAK CHECK. ROTABLE PARTS CHANGE WAS INDICATED - TT 1178238, S/N OFF 08091 IPC REFERENCE 32-32-41-01.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 34,853 hrs · 18,645 cycles

THE EMERGENCY EXIT LIGHTS AT SEATS 20-25 WERE FOUND INOPERATIVE. THE CHARGER AND BATTERY PACK WAS REMOVED AND REPLACED, OPERATIONAL CHECKS WERE GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,282 hrs · 17,281 cycles

INSPECTION FOUND THE EMERGENCY ESCAPE AISLE PATH LIGHTING INOPERATIVE AT ROWS 15-21. THE BATTERY PACK AND POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-51-51.

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 31,648 hrs · 16,944 cycles

INSPECTION FOUND THE EMERGENCY EXIT LIGHTS OUT ON SEAT ROWS 7-14ABC. MAINTENANCE FOUND A POWER WIRE SHORTED TO SEAT TRACK AT SEAT 7ABC. THE WIRE WAS REPAIRED IAW SRM 20-11-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,089 hrs · 16,139 cycles

FLOORBEAM CORRODED AT STA 986.5, RBL43. INSTALLED DOUBLER PER ECRA 5321-01209.

Part: FLOORBEAM — CORRODED (FUSLEAGE) · airframe 30,089 hrs · 16,139 cycles

FLOORBEAM CORRODED AT STA 986.5, LBL 43. INSTALLED DOUBLER PER ECRA 5321-01210.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,792 hrs · 15,980 cycles

INSPECTION FOUND CABIN FLOORBEAM CORRODED AT FASTENER HOLE OF FORWARD FLANGE OF UPPER CHORD, STA 986, LBL 43. A REPAIR WAS INSTALLED IAW ECRA 5321-01210.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,792 hrs · 15,980 cycles

INSPECTION FOUND CABIN FLOORBEAM FORWARD FLANGE OF UPPER CHORD FASTENER HOLE CORRODED AT STA 986, RBL 43 TO RBL 44. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01209.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,792 hrs · 15,980 cycles

INSPECTION FOUND CABIN FLOORBEAM CORRODED AT AFT FLANGE OF UPPER CHORD, STA 986, LBL 14 TO LBL 18. THE CORRODED AREA WAS CUT OUT AND ANGLES WERE INSTALLED IAW SRM 53-60-51.

Part: CIRCUIT BREAKER — FAILED (NR 1 ENGINE) · airframe 25,984 hrs · 13,969 cycles

A HEAVY ELECTRICAL ODOR WAS NOTICED IN THE CABIN WHILE EN ROUTE TO DCA. THE ODOR WAS ACCOMPANIED BY FAILURE OF CABIN LIGHTS, OVEN, AND AUTOPILOT AND THE NR 1 ENGINE GENERATOR BUS OFF LIGHT, AND RIGHT EQUIP COOLING SUPPLY OFF LIGHT ILLUMINATED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 TRANSFORMER RECTIFIER (TR) C/B POPPED. THE NR 1 TR CIRCUIT BREAKER WAS REMOVED AND REPLACED. THE NR 1 TRANSFORMER RECTIFIER WAS REMOVED AND REPLACED IAW MM 24-21-31. ALL OPERATIONAL CHECKS WERE NORMAL.

Part: MEGAPHONE — INOPERATIVE (CABIN)

THE AFT MEGAPHONE WAS FOUND INOPERATIVE. THE MEGAPHONE WAS REPLACED.

Part: LIGHT — INOPERATIVE (L2 DOOR)

INSPECTION FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT L-2 DOOR. THE EXIT LIGHT ASSEMBLY WAS REPLACED IAW MM 33-51-11.

Part: CIRCUIT BREAKER — TRIPPED (LANDING GEAR)

THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. THE GEAR HANDLE WOULD NOT RAISE BEYOND THE OFF POSITION. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LANDING GEAR LATCH AND WARNING CIRCUIT BREAKER POPPED. THE CIRCUIT BREAKER WAS RESET. ALL THREE LANDING GEAR WERE SWUNG IAW MM 07-11-11 AND OPERATION CHECKED GOOD.

Part: SKIN — PUNCTURED (BS 967-1016)

INSPECTION FOUND A PUNCTURE IN THE FUSELAGE SKIN CAUSED BY GROUND DAMAGE. THE PUNCTURE WAS LOCATED AT BS 967 TO 1016, STRINGER 21 TO 25R. THE AREA WAS REPAIRED IAW ECRA 5330-02616.

Part: CARBON SEAL — LEAKING (NR 2 ENGINE GB)

THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AND OIL QUANTITY INDICATED ZERO WHILE ON APPROACH. THE NR 2 ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE STARTER PAD CARBON SEAL LEAKING. THE STARTER PAD CARBON SEAL WAS REPLACED IAW MM 72-60-00 AND LEAK CHECKS WERE GOOD.

Part: RETRACT MECH — LACK OF LUBE (TE FLAPS)

YHE FLAPS WOULD NOT EXTEND BEYOND 15 DEGREES DURING APPROACH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTH OUTBOARD FLAP'S JACKSCREW GIMBALS DRY OF LUBRICATION. THE GIMBALS WERE LUBRICATED AND OPERATION OF THE FLAPS CHECKED GOOD.