N205AU

Part: SKIN — CRACKED (BS 245)

DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED A 3 INCH CRACK IN NOSE WHEEL WELL SKIN, BS 245.6 TO 248.6, WL 168.5. A .125 INCH CRACK AT RIVET, BS 244.1, W 165.5, AND A .125 INCH CRACK AT BS 243.1, WL 164.3. MAINTENANCE REPAIRED DAMAGED AREAS PER SRM 51-40-2. (M)

Part: GCU — FAILED (NR 1 GEN)

PHX - FLT 429 - DURING DESCENT INTO PHX, FLIGHT CREW REPORTED NR 1 GENERATOR OFF BUS LIGHT ILLUMINATED FOLLOWED BY THE SMELL OF ELECTRICAL SMOKE WITH A SMALL AMOUNT OF VISIBLE SMOKE NOTICED. COMPLIED WITH SMOKE REMOVAL CHECKLIST AND SMOKE DISSIPATED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED GENERATOR CONTROL UNIT AND CHECKED OK. (M)

Part: ANGLE — CORRODED (BS 353)

PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON MAIN EQUIPMENT BAY RIGHT INTERCOSTAL LOWER OUTBOARD SUPPORT ANGLE AT BS 353, RBL 12, WL 146. MAINTENANCE REPAIRED PER EO 98-0502. (M)

Part: DOUBLER — CORRODED (BS 270)

PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON INNER MOUNTING DOUBLER FOR FORWARD LAVATORY DRAIN TUBE, BS 270, STRINGER 23R. MAINTENANCE REMOVED DAMAGED DOUBLER, FABRICATED REPLACMENT PART AND REPAIRED PER SRM 51-20-4, 51-30-2 AND 53-10-1. (M)

Part: SHEAR TIE — CRACKED (BS 294)

PAE - DURING C-CHECK INSPECTION, REPORTED 1.8 INCH CRACK IN SHEAR TIE AT BS 294 BETWEEN STRINGER 12L AND 14L. MAINTENANCE FABRICATED NEW SHEAR TIE AND REPAIRED PER SRM 51-10-2 AND 51-30-2. (M)

Part: SKIN — CRACKED (FUSELAGE)

PAE - DURING C-CHECK INSPECTION, REPORTED CRACK IN FORWARD ENTRY DOOR OUTER SKIN, LOWER HINGE CUTOUT, UPPER AFT CORNER. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SB 737-52-1096 AND SRM 51-30-2. (M)

Part: FRAME — CRACKED (CARGO DOORWAY)

PAE - DURING C-CHECK INSPECTION, REPORTED CRACK IN FORWARD CARGO DOOR UPPER AFT FRAME. MAINTENANCE REMOVED DAMAGED FRAME. FABRICATED REPLACEMENT PART AND REPAIRED PER SRM 51-30-2. (M)

Part: FRAME — CORRODED (BS 360)

PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON FRAME AND SHEAR TIE AT BS 360, RBL 8-13, BETWEEN STRINGER 27R AND 28R. MAINTENANCE REMOVED DAMAGED AREA (6 INCH BY 4 INCH BY .006 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND 53-10-4. (M)

Part: SKIN — CRACKED (LT WING)

PAE - DURING C-CHECK, INSPECTION REPORTED 1 INCH CRACK IN SKIN ABOVE NR 1 ENGINE PYLON, LEFT WING LEADING EDGE. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND 57-30-04. (M)

Part: INTERCOSTAL — CRACKED (BS 294)

PAE - DURING C-CHECK INSPECTION, REPORTED CRACK ON INTERCOSTAL, AFT SIDE AT BS 294.5 STRINGER 7L. MAINTENANCE REMOVED INTERCOSTAL, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND 53-10-3 FIG 2. (M)

Part: SPLICE — CRACKED (BS 727)

PAE - DURING C-CHECK INSPECTION, REPORTED CRACK IN BS 727 BULKHEAD TO FLOORBEAM SUPPORT SPLICE AFT FLANGE, LBL 25, WL 202. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-1, 51-10-2, 51-20-1 AND 51-30-2. (M)

Part: SKIN — CRACKED (BS 949)

PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN AFT SERVICE DOOR SKIN ABOVE LOWER HINGE CUTOUT AT BS 949, STRINGER 14R, WL 220. MAINTENANCE REMOVED DAMAGED AREA, 1.5 INCH BY 2.5 INCH. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 52-00-3. (M)

Part: FRAME — CRACKED (CARGO DOOR)

PAE - DURING C-CHECK INSPECTION REPORTED CRACK IN FORWARD CARGO DOOR LOWER FORWARD FRAME IN OUTBOARD RADIUS OF LATCH ARM. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SB 737-52-1100 AND MM 52-31-0. CYCLES: 2,451. (X)

Part: SKIN — CRACKED (WING)

PAE - DURING C-CHECK INSPECTION, REPORTED CRACK ABOVE NR 2 LEADNG EDGE PYLON. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM'S 51-10-1, 51-30-2, AND 57-30-4. CYCLES: 2,451.0. (X)

Part: STRINGER — CRACKED (BS 294)

PAE - DURING C-CHECK, INSPECTION REPORTED CRACK 1 INCH ABOVE STRINGER 12L, BS 294.5. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2, 51-30-2, 51-40-3, FIG 1 AND 53-10-4. (M)

Part: STRINGER — CRACKED (BS 295)

PAE - DURING C-CHECK INSPECTION, REPORTED CRACK IN CROWN OF STRINGER 7L, BS 295. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND 53-10-3, FIG 1. (M)

Part: SKIN — CORRODED (BS 353-356)

PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON INTERNAL SKIN AT BS 353-356, RBL 3. MAINTENANCE REPAIRED SKIN PER SRM 53-30-3, FIG 28. (M)

Part: SKIN — CRACKED (LT WING)

DEN - PRIOR TO DEPARTURE, MAINTENANCE REPORTED ONE .25 INCH CRACK IN LEFT WING LEADING EGE SKIN AT WBL 165.0. MAINTENANCE REPAIRED DAMAGED AREA PER SRM 57-30-4, PAGE 4. (M)

Part: WIRE — LOOSE (CABIN)

PHX - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 4 A, B, C INOPERATIVE. MAINTENANCE REPAIRED WIRING AND SECURED WIRING HARNESS AND SYSTEM CHECKED OK. (M)

Part: LINE — FAILED ('A' HYD SYSTEM)

SFO - ON INBOUND FLIGHT TO SFO, FLIGHT CREW REPORTED LOSS OF 'A' SYSTEM HYDRAULIC PRESSURE AND FLUID. USED ALTERNATE FLAP SYSTEM AND AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE 'A' SYSTEM HYDRAULIC PRESSURE LINE IN AFT FLAP WELL, BOTH 'A' SYSTEM HYDRAULIC PUMPS (NR 1 P/N 65075-01, S/N 184104AK, NR 2 P/N 65075-06, S/N 183975), NR 1 AND NR 2 ENGINE PUMP CASE DRAIN FILTERS. 'A' SYSTEM HYDRAULIC RETURN FILTER. PERFORMED LEAK AND OPERATIONAL CHECK AND SYSTEM CHECKED OK. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED AFT RT EMERGENCY EXIT LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. REPLACED LIGHT ASSEMBLY AND CHECKED OK. (M)

Part: CONTROL PANEL — FAILED (AUTOPILOT)

OMA - UPON ARRIVAL, FLIGHT CREW REPORTED ELECTRICAL ODOR IN COCKPIT. REPLACED AUTOPILOT CONTROL PANEL AND CHECKED OK. (M)

Part: LINE — FAILED (NR 2 ENGINE)

AIR TURN BACK. UPON ROTATION, FLIGHT CREW REPORTED LOSS OF 'A' SYSTEM HYDRAULI CS AND DECLARED AN EMERGENCY. AIRCRAFT LEFT RUNWAY UPON LANDING AND GOT STUCK IN THE MUD. PASSENGERS WERE EVACUATED. REPLACED NR 2 ENGINE HYDRAULIC PRESSURE LINE IN PYLON AND BOTH ENGINE HYDRAULIC PUMPS PERFORMED REQUIRED INSPECTIONS PER MM AND SYSTEM CHECKED OK. (M)

Part: WIRE — BROKEN (CABIN)

DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 4L INOPERATIVE. MAINTENANCE SPLICED BROKEN WIRE UNDER SEAT WITH BUTT CONNECTOR AND SECURED WIRE ROUTING UNDER SEAT FRAME. SYSTEM CHECKED OKAY. AIRFRAME TOTAL TIME: 72,075.1 HRS. (X)

Part: WIRE — FAILED (CABIN)

DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 7A INOPERATIVE. MAINTENANCE INSTALLED NEW BUTT SPLICE SYSTEM CHECKED OKAY. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

DEN - FLT 18 - UPON ARRIVAL, FLIGHT CREW REPORTED FORWARD SECTION OF FLOOR PROXIMITY LIGHTING INOPERATIVE. REPLACED BATTERY PACK AND SYSTEM CHECKED OK. (M)

Part: BULB — FAILED (CABIN)

DEN - UPON ARRIVAL, FLIGHT CREW REPORTED L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED LAMP AND CHECKED OK. (M)

Part: SKIN — CRACKED (PAX DOORWAY)

PAE - A .5 INCH CRACK IN THE UPPER FORWARD CORNER OF THE FORWARD ENTRY DOOR CUTOUT SKIN. WHILE ACCOMPLISHING EA 53-737-023 INADVERTENTLY OVERSIZED 34 HOLES ABOVE ALLOWABLE LIMITS IN BOEING SB 737-53-1163. REPAIRED DAMAGED HOLES IAW TRAMCO EWO 97-0140 BY OVERSIZING AND INSTALLING FREEZE PLUGS, REPLACING, DAMAGED SUB-STRUCTURE AND DOOR STOP FITTINGS, AND INSTALLING A THICKER AND LARGER REPAIR DOUBLER. WORK ACCOMPLISHED IAW TRAMCO EWO 97-0140, BOEING DRAWING 65C36941-5, SRM 51-10-01, 51-10-2, 51-30-2. REF WORK ORDERS 214932 DOORS 51, INTERIOR 264. (M)

Part: SKIN — DENTED (BS 360-440)

FUSELAGE DENTS BETWEEN BS 360 AND 409. REMOVED SKIN FROM BS 360 TO 440, STRINGER 19R TO 24R. FABRICATED AND INSTALLED REPLACEMENT SKIN AND REPAIR IAW EWO 97-0080. REF WORK ORDER 214932 FUSELAGE 153/7-133 AND SRM. (M)

Part: SKATE ANGLE — CRACKED (VERT STAB)

RIGHT VERTICAL STAB AFT MOUNT LUG INBOARD SKATE ANGLE CRACKED. REMOVED RIGHT VERTICAL STAB AFT MOUNTING LUG INBOARD SKATE ANGLE. FABRICATED REPAIR ANGLE FROM MATERIAL OF 7075-0 .071 AND HEAT TREATED BY GIDDENS INDUSTRIES, INC TO 7075-T6, PO NR 1ML212756. INSTALLED SKATE ANGLE IAW DRAWING 65-53744, SRM 51-30-2 ADN SRM 51-10-2. CRACK WAS .5 INCHES LONG. (M)

Part: SKIN — CRACKED (SERVICE DOOR)

PAE - FORWARD SERVICE DOOR LOWER HINGE CUTOUT UPPER CORNER IS CRACKED .125 INCH IN LENGTH. REPAIRED CRACK BY STOP DRILLING AND INSTALLING EXTERNAL DOUBLER IAW TRAMCO EWO 97-0094. (M)

Part: BRACKET — CORRODED (BS 982)

PAE - FOUND CORROSION (C53-107-01) ON AFT AIRSTAIR HINGE SUPPORT BRACKET AT BS 982, LBL 40, WL 208. REMOVED CORROSION FROM AFT AIRSTAIR HINGE SUPPORT BRACKET IAW SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. FABRICATED FLOOR SUPPORT PLATE AND FILLER STRAP FROM SHEET STOCK OF 7075-T6 .140 AND 7075-T6 .125 AND INSTALLED FABRICATED REPAIR PARTS IAW SRM 51-10-1, 51-30-2, 53-10-1 AND DRAWING NR 65-67393 AT BS 982, LBL 40, WL 208. (M)

Part: FLOOR BEAM — CORRODED (BS 277)

PAE - FLOOR BEAM UPPER CHORD AT BS 277 HAS TWO .625 INCH DIAMETER HOLES AT LBL 17 AND LBL 24, WL 208. CORROSION WAS DISCOVERED AT BS 277 LBL 17, LBL 20, AND LBL 25 WL 208. REMOVED CORROSION ON FLOOR BEAM FOUND TO BE OUT OF LIMITS, IAW 53-10-1, REPAIRED FLOOR BEAM BS 277 LBL 17 TO LBL 25 WL 208 IAW SRM 53-10-9. (M)

Part: SEAT TRACK — CORRODED (BS 344-360)

PAE - WHILE WORKING INTERIOR 00171, FOUND CORROSION ON SEAT TRACK AT RBL 25, BS 344-BS 360. REMOVED CORROSION ON SEAT TRACK AT RBL 25, BS 344-BS 360, WL 208, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED SEAT TRACK FROM BS 344-BS 360, FABRICATED SEAT TRACK SECTION AND INSTALLED. ALL WORK PERFORMED IAW SRM 53-10-5. (M)

Part: STRINGER — CRACKED (BS 500)

PAE - AT STATION 500B PLUS 2.5, STRINGER 16L IS CRACKED, LENGTH OF CRACK .25 INCH. CUTOUT DAMAGED AREA AND REPAIRED PER TRAMCO EWO NR 97-0115 AND BOEING SB 737-53-1145. WORK ACCOMPLISHED ON TRAMCO WORK ORDER NR INTERIOR 262. (M)

Part: FLOOR BEAM — CORRODED (BS 360)

PAE - FOUND CORROSION (C53-107-02) ON FLOOR BEAM UPPER CHORD, BS 360, RBL 1 TO LBL 11, WL 208.1. FOUND CORROSION BEYOND LIMITS. REMOVED BS 360, WL 208.1 CHORD FROM LBL 13 TO RBL 15. FABRICATED AND INSTALLED REPAIR. ALL WORK DONE IAW SRM 53-10-1, 53-10-9, 51-20, 51-10 AND MM 51-21. (M)

Part: FLOOR BEAM — CORRODED (BS 344)

PAE - FOUND CORROSION (C53-107-02) ON FLOOR BEAM UPPER CHORD BS 344, RBL 9 TO LBL 65. FOUND CORROSION BEYOND LIMITS PER SRM 52-10-1. REMOVED CHORD FROM LBL 65 TO RBL 65. FABRICATED AND INSTALLED NEW CHORD. ALL WORK PERFORMED IAW SRM 51-10-6, 53-10-2, 53-10-9. (M)

Part: FLOOR BEAM — CORRODED (BS 328)

PAE - FOUND CORROSION (C53-107-02) ON FLOOR BEAM UPPER CHORD BS 328, RBL 60 - LBL 30, WL 208.1. REMOVED CORROSION ON FLOOR BEAM UPPER CHORD BS 328. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED UPPER CHORD AND REPAIR ANGLES FROM 7075-T6 .090 T-ANGLE EXTRUSION PER SRM 53-10-9. INSTALLED FABRICATED UPPER CHORD AND REPAIR ANGLE PARTS WITH HI-LOCKS BACB30PN6-3 AND BACB30PM6-5 PER SRM 53-10-9. (M)

Part: SEAT TRACK — CORRODED (BS 344-360)

FOUND CORROSION (C53-107-01), ON SEAT TRACK BS 344-360, LBL 45, WL 208. BLENDED OUT CORROSION AT BS 344-360, LBL 45, WL 208. BLENDED OUT CORROSION AT BS 344-360, LBL 45, WL 208 IN AN AREA 6 INCH BY 1 INCH BY .020 INCH. ORIGINAL THICKNESS . 270 INCH OF SEAT TRACK. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND INSTALLED FABRICATED SEAT TRACK (FABRICATED FROM 7178-T6 STOCK EXTRUSION P/N BAC 1520-7920) IAW SRM 51-30-2. (M)

Part: ACCESS DOOR — CRACKED (APU COMPT)

APU ACCESS DOOR MOST AFT RIB RIGHT CORNER CRACKED. STOP DRILLED CRACK END USING .125 INCH DRILL, CRACK WAS FOUND TO BE 2 INCHES IN LENGTH. REMOVED DAMAGED AREA AND INSTALLED FABRICATED REPAIR PARTS FROM STOCK MATERIAL OF 2024-T3 .050 IAW SRM 51-10-1, 52-40-1 AND SRM 51-30-2. (M)

Part: SKIN — GOUGED (FUSELAGE)

PAE - AFT CARGO DOOR EXTERNAL SKIN GOUGED 28 INCH FROM FWD EDGE. BLENDED GOUGED AREA IN EXTERNAL SKIN OF AFT CARGO DOOR 28 INCH IN FROM FORWARD EDGE AND 21 INCH DOWN FROM EDGE. DAMAGED AREA FOUND TO BE OUT LIMITS IAW SRM 52-00-2. REMOVED, FABRICATED DOUBLER (2024-T3 .071 INCH) AND FILLER (7075-T6 .032) AND INSTALLED REPAIR PARTS IAW SRM 52-30-2. (M)

Part: FLOOR BEAM — CORRODED (BS 294)

PAE - FOUND CORROSION (C53-107-02) ON FLOOR BEAM UPPER CHORD BS 294, LBL 21 TO RBL 60, WL 208.1. REMOVED CORROSION ON FLOOR BEAM UPPER CHORD BS 294, LBL 21 TO RBL 60, WL 208.1 IAW SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED UPPER CHORD FROM LBL 60 TO RBL 60 AND INSTALLED FABRICATED FLOOR BEAM UPPER CHORD AND SPLICE ANGLES MADE OF STOCK MATERIAL OF 7075-T6 .063 INCH IAW SRM 53-10-9. (M)

Part: SKIN — DENTED (CARGO DOOR)

PAE - FORWARD CARGO DOOR EXTERNAL SKIN DENTED 18-20 INCHES DOWN FROM TOP EDGE AND 15-16 INCHES IN FROM AFT EDGE. DENT IN FORWARD CARGO DOOR EXTERNAL SKIN 18-20 INCHES DOWN FROM TOP EDGE AND 15-16 INCHES IN FROM AFT EDGE. FOUND TO BE OUT OF LIMITS IAW SRM 52-00-2. REMOVED DAMAGED AREA AND INSTALLED FABRICATED DOUBLER MADE FROM STOCK SHEET OF 2024-T3 .071 MATERIAL IAW SRM 52-30-2. (M)

Part: SKIN — DENTED (BS 388.5)

PAE - DENT ON SKIN AT BS 388.5, 4 INCH ABOVE STRINGER 19L. REMOVED DAMAGED SKIN ON BS 388.5, 4 INCHES ABOVE STRINGER 19L. FABRICATED THE DOUBLER FROM 2024-T3 .050 MATERIAL. SEALED AND INSTALLED WITH RIVETS PER SRM 53-30-3. (M)

Part: SKIN — DENTED (BS 875-879)

PAE - DENT IN SKIN AT BS 875-879, BETWEEN STRINGER 17R-18R. FOUND DENT TO BE OUT OF LIMITS IAW SRM 53-30-01. CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER FROM 2024-T3 .063 SHEET STOCK. DOUBLER INSTALLED WET SEALANT. ALL WORK DONE IAW SRM 53-30-3 FIG 1 AT BS 875-879 BETWEEN STRINGER 17R AND 18R. (M)

Part: SKIN — DELAMINATED (RT TE FORE FLAP)

PAE - RIGHT WING OUTBOARD FOREFLAP HAS AREA OF DELAMINATION ON UPPER SURFACE MID-SECTION. REPAIRED RIGHT WING FOREFLAP UPPER SURFACE MID-SECTION PER SRM 51-40-6. FABRICATED AND INSTALLED DOUBLERS, USING 2024-T3 .016 MATERIAL. (M)

Part: SKIN — DISBONDED (RT TE FOREFLAP)

PAE - RIGHT WING OUTBOARD FORE FLAP HAS AREA OF DISBOND ON UPPER INBOARD END. REPAIRED RIGHT WING OUTBOARD FORE FLAP UPPER INBOARD END IAW SRM 51-40-6. FABRICATED AND INSTALLED DOUBLERS, USING 2024-T3 .010 MATERIAL. (M)

Part: FRAME — GOUGED (BS 328)

PAE - BS 328 STRINGER 28L FRAME IS GOUGED GREATER THAN 50 PERCENT AT FASTENER COMMON TO FRAME AND STRINGER. REMOVED DAMAGED SECTION OF FRAME AT BS 328 STRINGER 28L. FABRICATED REPAIR ANGLE AND FILLER, TREATED REPAIR PARTS AND INSTALLED IAW SRM 51-40-03. (M)

Part: SKIN — CRACKED (BS 784-786)

FLT 93 - DEN - DURING WALK AROUND, MAINTENANCE REPORTED A 2 INCH CRACK IN THE FUSELAGE SKIN AT STATION 784 TO 786, .5 INCH ABOVE STRINGER 24L. MAINTENANCE STOP DRILLED CRACK AND INSTALLED TYPICAL REPAIR PER BOEING SRM 53-30-3. (M)

Part: CHORD — CRACKED (BS 727)

DURING SERVICE CHECK, INSPECTION REPORTD A .5 INCH CRACK IN OUTER CHORD AT STATION 727, STRINGER 25R. REPAIRED PER BOEING TELEX FRO-DEN-96-0090RR AND SRM 51-40-4, FIG 1. (M)

Part: SKIN — CRACKED (FUSELAGE)

DURING SERVICE CEHCK, INSPECTION REPORTED A .5 INCH CRACK IN THE UPPER FORWARD CORNER OF THE FORWARD ENTRY DOOR CUTOUT. REPAIRED PER BOEING TELEX FRO-DEN-96-0085RR AND SRM 51-10-1. (M)

Part: CONTROL SYSTEM — STIFF (ELEVATOR)

UPON ARRIVAL, FLIGHT CREW REPORTED ELEVATOR STIFF, ESPECIALLY DURING FLARE. MAINTENANCE CHECKED ALL FLIGHT CONTROLS FOR MOVEMENT AND POSITION PER MM AND FOUND OK. PERFORMED TEST FLIGHT AND CHECK OK. (M)

Part: CONTROLS SYSTEMS — STIFF (ELEVATOR)

DEN - UPON ARRIVAL, FLIGHT CREW REPORTED ELEVATOR STIFF, ESPECIALLY DURING FLARE. MAINTENANCE CHECKED ALL FLIGHT CONTROLS FOR MOVEMENT AND POSITION PER MM AND FUOND OK. PERFORMED TEST FLIGHT AND CHECKED OK. (M)

Part: VALVE — FAILED (A HYD SYSTEM)

DEN - FLT 546 - AFTER TOUCHDOWN, FLIGHT CREW REPORTED A-SYSTEM HYDRAULIC PRESSURE FLUCTUATING AND LOSS OF NOSE WHEEL STEERING. TOWED AIRCRAFT TO GATE. REPLACED LEFT HYDRAULIC SHUT OFF VALVE, CASE DRAIN FILTER AND PRESSURE FILTER AND SYSTEM CHECKED OKAY. TOTAL TIME AIRFRAME, 69,487.3 HRS.

Part: CORNER — CRACKED (SERVICE DOOR)

DEN - DURING AN A-3 CHECK, MAINTENANCE REPORTED A CRACK IN THE FORWARD SERVICE DOOR (R-1). CRACK WAS APPROXIMATELY 1.25 INCHES IN LENGTH AND WAS LOCATED IN THE LOWER FORWARD CORNER. REPAIRED CRACK PER SB 737-52-1070.

Part: SWITCH — MALFUNCTION (GEAR HANDLE)

DEN - UPON ARRIVAL, FLIGHT CREW REPORTED LANDING GEAR UNSAFE (INTRANSIT) LIGHTS ILLUMINATED WITH GEAR HANDLE UP. MAINTENANCE REPLACED THE LANDING GEAR HANDLE MICROSWITCH AND CHECKED OK. (M)