N904UP

Part: SENSOR — DIRTY (TE FLAP SYSTEM) · airframe 15,870 hrs · 9,747 cycles

FLAPS FAIL CAS MESSAGE ILLUMINATED AFTER TAKE-OFF. FLAPS AT 15* SETTING. FOLLOWED CHECKLIST AND DIVERTED TO ALTERNATE AIRPORT. LANDING WAS UNEVENTFUL. MAINTENANCE REMOVED THE FLAP HANDLE AND CLEANED OPTICAL SENSOR AND SETTING SWITCHES WITH COMPRESSED AIR, IAW AMM. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: PIN — BROKEN (TILLER) · airframe 15,599 hrs · 9,601 cycles

AFTER TAXIING ABOUT TWO MILES, WITH MULTIPLE TURNS, SOMETHING IN THE STEERING BROKE. USE OF THE RUDDER AND DIFFERENTIAL BREAKING TO PULL OFF THE TAXIWAY. AIRCRAFT WAS TOWED BACK TO THE FBO. MAINTENANCE REPLACED STEERING TILLER PIN. OPS AND TAXI CHECKS PERFORMED WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — OVERTEMP (MASTER) · airframe 15,529 hrs · 9,961 cycles

DURING CRUISE FLIGHT AT FL430, WE EXPERIENCED A MASTER WARNING FOR A NR 1 BATTERY OVER TEMPERATURE. THE TEMPERATURE WAS INDICATING 63 DEGREES C. THE EMERGENCY PROCEDURE CHECKLIST WAS PERFORMED. THE TEMPERATURE CONTINUED TO CLIMB OVER AN APPROXIMATELY A 10 MINUTE PERIOD TO 65 DEGREES CELSIUS. AT THAT TIME, A CREW DECISION WAS MADE TO DIVERT. MAINTENANCE REPLACED THE LEFT AIRCRAFT MAIN BATTERY. OPERATIONAL CHECKS PERFORMED WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: CIRCUIT BOARD — FAILED (BLEED SYS) · airframe 14,992 hrs · 9,234 cycles

LEFT STAB BLEED LEAK WARNING ANNUNCIATOR ILLUMINATED DURING FLIGHT. ANNUNCIATOR WENT AWAY WITH POWER REDUCED BUT CAME BACK AFTER POWER APPLIED. FOLLOWED CHECKLIST, DECLARED AND EMERGENCY. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE BLEAD THE LEFT BLEAD AIR MONITO PCB. GROUND CHECKS WERE GOOD. AIRCRAFT RELEASED FOR OPERATIONAL CHECK FLIGHT.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS BOTH NOT WORKING. REMOVED AND REPLACED BATTERIES. OPS CK GOOD.

Part: LIGHT — DISCHARGED (COCKPIT)

INSPECTION TYPE:PFLT COCKPIT EMERGENCY LIGHT ABOVE DOOR VERY DIM. REMOVED AND REPLACED BATTERIES, OPS CHECK OK AS PER MM 33-50-01.

Part: WARNING SYSTEM — INOPERATIVE (COCKPIT)

COMPT SHOWS-TD DELAY FOR FIRE WARNING BELL INDICATOR INOP COCKPIT FIRE BELL WILL NOT SOUND WITH THE ENG FIRE DETECTION PANEL TEST SWITCH IN A,B,OR A/B THIS APPLIES TO ACTUATING EITHER THE ENG TEST SWITCH OR WHEEL WELL TEST SWITCH. CLEANED AND RESECURED WIRING AT TB 224 56 AND 57. TEST VOLTAGE, OK SYSTEM OK PER 26-11-02.

Part: STRAP — UNSERVICEABLE (ENTRY DOOR)

INSPECTION TYPE:IN FWD ENTRY DOOR HANDLE STRAP IS NOT LONG ENOUGH TO ENGAGE VELCRO PAD WHEN LOOPED AROUND THE DOOR HANDLE. REMOVED FWD ENTRY DOOR HANDLE STRAP AS PER EO B727-2560-12064. OK FOR SERVICE.

Part: SWITCH — OUT OF ADJ (MLG)

INSPECTION TYPE:N/A ATB-AIR/GROUND SAFETY SENSOR FAILED IN GROUND ILLEG BUT LANDING GEAR RETRACTED NORMALLY. REPOSITION MAIN GEAR SAFETY SWITCH ILLEG AND PERFORMED SWITCH OPS CHECK AS PER B727 M/M 32-0211. NO DEFECTS NOTED.

Part: PRESSURE PANEL — CRACKED (NLG WW)

INSPECTION TYPE:C, NOSE WHEEL WELL RT SIDEWALL BS 264.3 WL 154 LWR OF AFT ACCESS DOOR CRACK INDICATION ALONG ROW OF RIVET HEADS. CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-2 & 51-10-1. INSTALLED DOUBLER REPAIR AS PER B727 SRM 51-40-2 MAT USED 2024-T3.050 30, .5 X 27.5.

Part: PRESSURE PANEL — CRACKED (NLG WW)

INSPECTION TYPE:C, NOSE WHEEL WELL RT SIDE WALL BS 259.5 FWD OF AFT ACCESS DOOR CRACK INDICATION ALONG ROW OF RIVET HEADS. CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-2, INSTALLED DOUBLER. REPAIR PER SRM 51-40-20.

Part: PRESSURE PANEL — CRACKED (NLG WW)

INSPECTION TYPE:C, NOSE WHEEL WELL RT SIDEWALL BS 248 LWR OF FWD ACCESS DOOR CRACK INDICATION AROUND FASTENER HEAD. CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-2 & 51-10-1. INSTALLED DOUBLER REPAIR AS PER B727 SRM 51-40-2.

Part: PRESSURE PANEL — CRACKED (NLG WW)

INSPECTION TYPE:C, NOSE WHEEL WELL BS 227.8 FWD WALL BL 0 CRACK INDICATION AROUND ROW OF FASTENER HEADS. CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-2 & 51-10-1, INSTALLED DOUBLER REPAIR AS PER B727 51-40-2.

Part: PANEL — CRACKED (NLG WW)

INSPECTION TYPE:C, NOSE WHEEL WELL LT SIDEWALL LOWER CHORD COVER PANEL SHOWS CRACK INDICATION 2 AROUND RIVET HEADS. REMOVED PANEL AND MADE NEW PER SAMPLE AND INSTALLED AS PER B727 SRM 51-30-2.

Part: ANGLE — CORRODED (AFT AIRSTAIR)

INSPECTION TYPE:C-CK, AFT AIRSTAIR SUPPORT ANGLE CORROSION UNDER 4TH STEP FROM TOP. REMOVED AND REPLACED CHORD SUPPORT ANGLE ON AFT AIRSTAIRS.

Part: BRACKET — CRACKED (FUSELAGE)

INSPECTION TYPE:C-CK, TAIL SKID COMPT, 2 UPPER SUPPORT RODS AFT ATTACH BRACKETS, LT AND RT CRACKED. REMOVED AND REPLACED BOTH LT AND RT ATTACH BRACKETS FOR TAIL SKID UPPER SUPPORT RODS.

Part: ATTACH ANGLE — CRACKED (RT MLG WW)

INSPECTION TYPE:C-CK RT MLG W/W UPPER O/B SIDE, FS 910, MLG UPLOCK SUPPORT FRAME FWD O/B ATTACH ANGLE CRACKED IN THE O/B RADIUS APPROX 6 INCHES BELOW PRESSURE DECK. REPAIRED RIGHT MLG W/W UPPER O/B SIDE FS 910 MLG UPLOCK SUPPORT FRAME.

Part: PRESSURE PANEL — CRACKED (NLG WW)

INSPECTION TYPE:C-CK, NOSE W/W LT SIDEWALL CRACK INDICATION ALONG ROW OF RIVETS HEADS. CUT OUT DAMAGE AREA AND INSTALLED DOUBLER.

Part: PRESSURE PANEL — CRACKED (NLG WW)

INSPECTION TYPE:C-CK, NOSE W/W LT SIDEWALL, CRACK INDICATION ALONG VERTICAL ROW OF RIVETS HEADS. CUT OUT DAMAGE AREA AND INSTALLED DOUBLER.

Part: PANEL — CRACKED (RT WING)

INSPECTION TYPE:C-CK, RT WING T/E TOP PANEL HAS 2 CRACKS BY NR 10 SPOILER O/B HINGE. STOP DRILLED CRACKS AT RT WING T/E PANEL, ACCOMPLISHED HFEC INSP. NO CRACKS EXTENDED BEYOND STOP DRILLED HOLES. REMOVED NR 10 SPOILER O/B SUPPORT BRACKET. REMOVED AND REPLACED CRACKED ANGLE AND RT WING, INSTALLED, REPAIRED,TREATED AND PRIMED. INSTALLED NR 10 SPOILER O/B SUPPORT BRACKET AT RT WING T/E.

Part: FIRE DETECTOR — MALFUNCTIONED (CARGO HOLD)

INSPECTION TYPE:N/A P-WRITE UP, LOWER CARGO FIRE DETECTOR AMBER LIGHT. *S/D* GROUND CKS SATISFACTORY AT THIS TIME IAW MM 26-18-01.

Part: LIGHT — MALFUNCTIONED (COCKPIT)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT AT REAR OF COCKPIT ILLUMINATED DURING CLIMB AND WOULD NOT TURN OFF. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSY, TEST GOOD.

Part: SEAL — BROKEN (OXYGEN GENERATOR)

FWD LAV AVIOX OXYGEN GENERATOR HAS INCORRECT EQUIPMENT DUE STICKER. STICKER INDICATES DUE AT 'C' OR 'D' CHECK SHOULD BE A MONTH AND YEAR. FURTHER INSPECTION REVEALED TRIGGERING MECHANISM FOR GENERATOR ACTUATED, HOWEVER GENERATOR CANISTER WAS NOT BREACHED. INSTALLED NEW AVIOX 02 GENERATOR IAW SCOTT MAINT INSTRUCTIONS. THIS CLEARS D184996 INOP STICKER REMOVED P/N ON 802501 S/N TAG303142.

Part: BATTERY PACK — DISCHARGED (CABIN)

FWD ENTRY DOOR EMERGENCY LIGHT DOES NOT ILLUMINATE. REPLACED BATTERY PACK ON EMERGENCY LIGHT. OPS CHECK GOOD.

Part: QUADRANT — CORRODED (RUDDER CONTROL)

INSPECTION TYPE-SI, AFT RUDDER CONTROL QUADRANT AREAS OF CORROSION AROUND FASTENERS. CORROSION REWORK OUT OF LIMITS. REMOVED OVER .75 OF THICKNESS. REMOVED AND REPLACED AFT RUDDER QUADRANT IAW MM 27-20-71.

Part: RIB — CRACKED (NR 3 SLAT)

INSPECTION TYPE-SI, WHILE WORKING CARD NR 465869 FOUND L/W NR 3 SLAT O/B TRACK O/B TRACK RIB CRACKED. INSTALLED NEW RIB AT O/B TRACK STATION PER 727 SRM 51-30-2.

Part: FITTING — CORRODED (NR 1 FLAP TRACK)

INSPECTION TYPE-SI, NR 1 FLAP TRACK FWD FITTING IS CORRODED AROUND MOUNT HOLE. REPLACED FITTING PER SRM 51-10-1, NEW FITTING SETUP AND MACHINED PER BOEING DRAWING 65-17357.

Part: SEAT TRACK — CORRODED (BS 675-680)

INSPECTION TYPE-SI, CORROSION ON CARGO TRACK IN WELL OF TRACK AT BS 675 TO 680, WL 155, RBL 15. REMOVED DAMAGED SECTION OF CARGO TRACK, FABRICATED AND INSTALLED REPLACEMENT SECTION IAW SRM 53-10-5.

Part: BEAM — CORRODED (BS 765-825)

INSPECTION TYPE-SI, CORROSION ON LONGITUDINAL BEAM LBL 25, WL 208, BS 765 TO 825. REMOVED AND REPLACED UPPER CHORD OF LONGITUDINAL BEAM IAW SRM 51-30-2, 51-20-1, 51-30-5.

Part: BULKHEAD SKIN — CRACKED (BS 178)

INSPECTION TYPE-SI, BS 178 BULKHEAD IS CRACKED AROUND FASTENERS AT BS 10, WL 235. REMOVED DAMAGED AREA .5 X 3 ENCOMPASSING 3 CRACKS. REPAIRED BS 178 AT LBL 10, WL 235, PER 727 SRM 53-10-9 AND SRM 51-30-2.

Part: SUPPORT — CORRODED (BS 328)

INSPECTION TYPE-SI, CORROSION ON FLOOR SUPPORT BS 328 TO 344, LBL 29, WL 208. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-2.

Part: BEAM — CRACKED (CARGO DOOR)

INSPECTION TYPE-SI, FORWARD CARGO DOOR NR 3 BEAM IS CRACKED IN OUTBD RADIUS 12 INCHES AFT FROM FORWARD EDGE OF DOOR, 16 INCHES DOWN FROM TOP EDGE OF DOOR. REMOVED AND REPLACED DOOR IAW MM ON SEPARATE NRC NR 465118.

Part: SEAT TRACK — CORRODED (BS 861)

INSPECTION TYPE-SI, CORROSION AROUND NUT PLATES BS 861, RBL 24, WL 208. REMOVED AND REPLACED SECTION OF SEAT TRACK AND EXPANSION LINK IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 730)

INSPECTION TYPE-SI, WHILE WORKING CUST ID 2-224-22B FOUND CORROSION ON SEAT TRACK INBD FLANGE STA 730, LBL 65, WL 208. REMOVED DAMAGED SECTION OF SEAT TACK AND SPLICED IN NEW SECTION IAW SRM 53-10-5.

Part: STRINGER — CRACKED (BS 485)

INSPECTION TYPE-SI, CRACKED STRINGER 24 RT BS 485, WL 165, RBL 35. STOP DRILLED ENDS AT CRACK AND INSTALLED REPAIR DOUBLERS OVER DAMAGED SECTION IAW SRM 53-10-3.

Part: STRINGER — CRACKED (BS 887)

INSPECTION TYPE-SI, CRACK AT STR 14 LT BS 887 LBL 70 WL 229. REPAIRED CRACKED STR 14 LT AT STA 887, LBL 70, WL 229 IAW SRM 51-40-4.

Part: CORE — CORROSION (NR 7 SPOILER)

INSPECTION TYPE-SI, WATER ENTRAPMENT NOTED IN LT WING NR 7 SPOILER I/B END FROM LEADING EDGE AFT 12 INCHES (X-RAY FILM VIEW NR 8). FURTHER INVESTIGATION REQUIRED. REMOVED 24 X 9 OF LOWER SURFACE SKIN AND 5 X 11.8 DAMAGED CORE CLEANED, DRIED AND REPAIRED IAW SRM 51-40-6.

Part: RIB — CRACKED (WS 629)

INSPECTION TYPE-SI ,RWS 629 RIB IS CRACKED IN RADIUS AT S-11 LOWER ATTACH BOLT HOLE. REPAIRED 629 RIB (RWS) IAW UPS EO B727-5710-1325H.

Part: BULLNOSE — CORRODED (NR 2 LE FLAP)

INSPECTION TYPE-SI, L/W NR 2 K-FLAP BULLNOSE I/B MOUNT LUG CORRODED AROUND I/B FASTENER. REMOVED CORRODED BULLNOSE, CORROSION OUT OF LIMITS, INSTALLED SERVICABLE BULLNOSE IAW MM 27-81-01.

Part: STRINGER — CRACKED (WS 629)

INSPECTION TYPE-SI, WHILE WORKING NRC 465706 WINGS 329, FOUND STRINGER 14 TAB TO BE CRACKED AT R/W STA 629.0. REPAIRED STR 14 AT RWS 629.0 IAW UPS EO B727-5710-0314F.

Part: WEB — CORRODED (BS 307-314)

INSPECTION TYPE-SI, CORROSION ON VERTICAL WEB OF DOGHOUSE BS 307 TO 314, LBL 13.5, WL 157 TO 161. CUT OUT DAMAGED AREA OF WEB AND INSTALLED DOUBLER IAW SRM 53-10-9, 51-40-2.

Part: FITTING — CORRODED (BS 365)

INSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON STRINGER TIE OF STR 26 LT BS 365. REMOVED AND REPLACED STRINGER TIE IAW SRM 51-30-2, 53-10-1, 51-30-4.

Part: FRAME — CORRODED (BS 680)

INSPECTION TYPE-SI, CORROSION BS 680 FRAME LBL 24 WL 154 UPPER FLANGE. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER PER SRM 51-40-3, HEAT TREATED AND THEN INSTALLED PER SRM 51-20-04 SRM 53-10-2 AND SRM 51-40-3.

Part: FITTING — CORRODED (LT AILERON)

INSPECTION TYPE:SI, I/B CENTER HINGE FITTING ON AILERON SIDE IS CORRODED ON O/B AILERON L/W. REMOVED AND REPLACED L/W O/B AILERON CENTER HINGE FITTING AILERON SIDE IAW SRM 51-30-2 AND 51-30-5.

Part: STRINGER — CORRODED (BS 730-735)

INSPECTION TYPE:SI, CORROSION ON STRINGER 23L BS 730 TO 735 WL 155. REMOVED FASTENERS AND CUT STRINGER AT BS 712. INSTALLED STRINGER REPAIR PER SRM 53-10-3 FROM BS 712 TO 726, 726 TO 740 CORROSION FOUND WITHIN LIMITS.

Part: ANGLE — CORRODED (BS 868)

INSPECTION TYPE:SI, CORROSION ON OUTBD SIDE OF INBD EXPANSION LINK STA 868, LBL 35, WL 161. REMOVED AND REPLACED EXPANSION LINK ATTACH ANGLES IAW SRM 51-30-2.

Part: STIFFENER — CORRODED (BS 294)

INSPECTION TYPE:SI, CORROSION ON VERTICAL STIFFENER AT STA 294, RBL 5, WL 193 ON STIFFENER STRAP. REMOVED AND REPLACED STRAP ON STIFFENER IAW SRM 51-30-2.

Part: WEB — CORRODED (BS 243-251)

INSPECTION TYPE:S, CORROSION (C53-111-01.00-01) ON NOSE WHEELWELL PRESSURE WEB BS 243-251, LBL 235, WL 168-172 (AREA MARKED). REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 51-10-02. REPAIRED PER SRM 53-10-9, 51-10-02.

Part: RIB — CRACKED (NR 3 LE SLAT)

INSPECTION TYPE-SI, WHILE WORKING CARD NR 465720 FOUND CRACKED RIB ON L/W NR 3 SLAT AT SLAT STA 128 TO 950. REMOVED CRACKED RIB, REPLACED WITH NEW RIB IAW SRM 51-30-2.

Part: STRINGER — CORRODED (BS 575)

INSPECTION TYPE:SI, CORROSION ON STR 21 RT, BS 575, WL 178. REMOVED DAMAGED SECTION OF STRINGER AND SPLICED IN REPAIR SECTION IAW SRM 53-10-3.

Part: FRAME — CORRODED (BS 243)

INSPECTION TYPE:SI, CORROSION (C53-111-01.00-01) AROUND FASTENERS ON FRAME BS 243, RBL 25, WL 166. CORROSION OUT OF LIMITS. REMOVED CORROSION, FABRICATED FILLER AND DOUBLER, INSTALLED IAW SRM 51-40-2, 51-10-2, 51-20-151.

Part: INTERCOSTAL — CORRODED (BS 211-220)

INSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON INTERCOSTAL BS 211.8 TO 219.8, LBL 25, WL 176. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REPLACED INTERCOSTAL STA 211.8 TO 219.8, LBL 25, WL 176 IAW SRM 51-20-1, 51-30-2, 51-10-3.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION TYPE:SI, CORROSION (C53-224-01.05-01) ON TOP OF BS 312 FLOORBEAM, LBL 3, WL 208. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 DAMAGED AREA REMOVED AND STANDARD REPAIR PERFORMED IAW WITH SRM 53-10-08 AND SRM 51-30-7.

Part: FLOORBEAM — CORRODED (BS 420)

INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) AND GOUGE ON BS 420 FLOORBEAM LBL 19, RBL 56, WL 208. CORROSION FOUND OUT OF LIMITS PER SRM 53-10-1. COMPLETED STANDARD UPPER CHORD REPAIR PER SRM 53-10-8, SRM 51-30-2 AND 51-10-2.

Part: FLOORBEAM — CORRODED (BS 480)

INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) AND BARE METAL ON FLOORBEAM BS 480, LBL 45 TO 59, WL 208. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. COMPLETED STANDARD UPPER CHORD SPLICE PER SRM 53-10-8, FIG 5, SRM 51-30-2 AND MM 51-20-21.

Part: FLOORBEAM — CORRODED (BS 400)

INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) ON FLOORBEAM BS 400, LBL 25, WL 208, UPPER FLANGE. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 51-10-1. COMPLETED STANDARD T-CHORD REPAIR PER SRM 53-10-8, SRM 51-30-2 AND MM 51-20-31.

Part: FRAME — CORRODED (BS 251)

INSPECTION TYPE-SI, CORROSION AROUND FASTENERS ON FRAME BS 251 RBL 24 WL 162. REMOVED DAMAGED SECTION AND INSTALLED FILLER AND DOUBLER IAW SRM 51-10-2, 51-40-2 AND MM 51-20-15.

Part: STRINGER — CORRODED (BS 352-358)

INSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON STR 23L BS 352 TO 358. CORROSION FOUND OUT OF LIMITS PER SRM 53-10-1. REPLACED STRINGER WITH NEW ITEM PER SRM 51-10-1 AND 51-30-2.

Part: STIFFENER — CORRODED (BS 301)

INSPECTION TYPE-SI, CORROSION (C53-111-01.05-01) ON STIFFENER OF NOSE WHEEL WELL TOP PANEL BS 301 LBL 7, RLB 12, WL 184. CORROSION OUT OF LIMITS PER SRM 51-10-6. REPLACED PART WITH NEW ITEM PER SRM 51-30-2.

Part: FRAME — CORRODED (BS 329)

INSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON FRAME BS 328, RBL 43, WL 169 (AREA MARKED). CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, INSTALLED STANDARD FRAME DOUBLER REPAIR IAW SRM 51-40-3, AND SRM 51-30-2.

Part: STRINGER — CORRODED (BS 370-380)

INSPECTION TYPE-SI, CORROSION ON STR 26 LT BS 370 TO 380. REMOVED DAMAGED SECTION, INSTALLED NEW STRINGER AND STRINGER SPLICE PER SRM 53-10-3 WITH FASTENER BS 360 TO 380.

Part: SEAT TRACK — CORRODED (BS 1010-1110)

INSPECTION TYPE-SI, CORROSION (44-53-12) IN SEAT TRACK WELL AND AROUND NUT PLATES BS 1010 TO 1110, RBL 62, WL 208. CORROSION FOUND OUT OF LIMITS PER SRM 51-30-2, REPLACED SEAT TRACK WITH NEW ITEM PER SRM 51-30-2, SRM 51-10-2 AND SRM 51-20-151.

Part: SEAT TRACK — CORRODED (BS 970-1110)

INSPECTION TYPE-SI, CORROSION (44-53-12) IN SEAT TRACK WELL BS 970 TO 1110 RBL 25, WL 208 CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED NEW TRACK AND SPLICE PER 53-10-5, INSTALLED PER SRM 51-30-2.

Part: INTERCOSTAL — CORRODED (BS 211.8)

INSPECTION TYPE:SI, CORROSION (C53-111-01.00-01) ON INTERCOSTAL BS 211.8, RBL 25, WL 176. CORROSION OUT OF LIMITS. REMOVED INTERCOSTAL, FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-20-1, 51-10-3.

Part: STRINGER — CORRODED (BS 492-497)

INSPECTION TYPE:SI, CORROSION (SDN 53-111-01.00-02) ON STR 25 LT BS 492-497 WL 160. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. CUT OUT DAMAGED SECTION AND COMPLETED STANDARD REPAIR IAW SRM 53-10-3.

Part: BATTERIES — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHT DENT STAYED ILLUMINATED WHEN SWITCH IS TURNED ON. REPLACED BATTERIES OP'S CK'D OK.

Part: COALASCER BAG — DIRTY (CABIN)

ON TAKEOFF, NOTICED A STRONG ODOR. RAN AIRCONDITIONING SMOKE CHECKLIST, ODOR DID NOT DECREASE. RETURNED TO IAD. PERFORMED TAKEOFF POWER CK PER MM 71-00-58. NO ODOR NOTICED, CHANGED WATER SEPARATOR BAGS LT/RT PACK. NO OIL FOUND IN DUCTS, OLD BAGS IN GOOD SHAPE. ALL PACK INTAKES CLEAR. UNABLE TO DUPLICATE.

Part: WEB — CRACKED (FS 251.6)

INSPECTION TYPE-C, NLG WHEEL WELL LEFT SIDE WEB IS CRACKED AT FS 251.6. REMOVED, FABRICATED AND INSTALLED WEB PER SRM 51-40-2 AND 51-30-2.

Part: ACTUATOR RIBS — CRACKED (NR 3 SLAT)

INSPECTION TYPE-C, NR 3 SLAT INBD AND OTBD ACTUATOR ATTACH RIBS ARE CRACKED. REMOVED, FABRICATED AND INSTALLED RIBS PER SRM 57-50-2, 51-30-2 AND BOEING DWG 65-17240.

Part: SUPPORT CHANNEL — CRACKED (NR 3 SLAT)

INSPECTION TYPE-C, NR 3 SLAT ACTUATOR SUPPORT CHANNEL BETWEEN I/B AND O/B ACTUATOR. REMOVED, FABRICATED AND INSTALLED CHANNEL PER DWG 65-17294 AND SRM 51-30-2.

Part: SKIN — CRACKED (FS 850-870)

INSPECTION TYPE-C, MAIN CABIN FS 850 TO 870 BL 0 TO LBL 45 CENTER TANK UPPER PRESSURE SKIN HAS CORROSION. REMOVED AND AREA NOTED WAS SUBMITTED TO ENG FOR REPAIR. FLAP PEENING DAMAGE AREA PER DHC SK 904-400-AND BOEING M/M 20-10-3. ALODINE AND PRIMED STRUCTURE AND REINSTALLED FASTENERS PER SK 904-400 AND SRM 51-20-4.

Part: SEAT TRACK — CRACKED (BS 740-760)

INSPECTION TYPE-C, SEAT TRACK AT BS 740 TO 760 LBL 44.5 IS CORRODED AND CRACKED. REMOVED AND REPAIRED TRACK PER SRM 51-30-2.

Part: K-FLAP — CRACKED (NR 1 LE FLAP)

INSPECTION TYPE-C, NR 1 K-FLAP 6 INCHES O/B OF I/B HINGE, WEB L/E INSIDE HAS A 3 INCH CRACK. REMOVED, FABRICATED REPLACEMENT PART AND INSTALLED IAW 57-10-2 AND 51-30-2.

Part: INNER WEB — CRACKED (NR 3 SLAT)

INSPECTION TYPE-C, NR 3 SLAT INNER WEB AT ACTUATOR CRACKED ON BOTH SIDES. STOP DRILLED CRACKS PER SRM 51-10-1, FABRICATED AND INSTALLED WEB REPAIR PER SRM 51-40-3 AND 57-50-1.

Part: WEB — CRACKED (BS 1263-1270)

INSPECTION TYPE-C, THE RT LWR TORQUE BOX I/B WEB AT STA 1263 TO 1270 HAS 4 CRACKS AT RIVET HOLE AND 3 CRACKS PAST STOOP DRILLS. REPAIRED I/B TORQUE BOX WEB AND INSTALLED THE 65-17510-313 AND 65-175 10-314.

Part: SWTCH — DEFECTIVE (RT MLG)

WHEN GEAR LOWERED FOR LANDING, RIGHT MAIN GREEN LIGHT DID NOT ILLUMINATE, WARNING HORN SOUNDED WHEN FLAPS SELECTED TO 30 DEGREES. RECYCLED GEAR PER AMO PROCEDURE. NO CHANGE. ACCOMPLISHED ALTERNATE EXTENSION PROCEDURE, REMOVED AND REPLACED GEAR GREEN LIGHT SWITCH RT. PERFORMED OPERATIONAL CHECK OF LANDING GEAR WITH PLANE ON JACKS. OPERATIONAL INDICATION NORMAL.

Part: CONNECTOR — CHAFED (NR 3 ENGINE)

INSPECTION TYPE N/A, ENG 3 STRUT OVERHEAT LIGHT CAME ON JUST PRIOR TO LANDING. EXTINGUISHED AFTER ENGINE WAS SHUT DOWN. ENGINE SHUTDOWN DURING LANDING ROLL. *S/D* REPAIRED CHAFED WIRE AT FIRE WALL. REMOVED AND REPLACED CONNECTOR ON START STRUT, CONNECTOR ON START STRUT OVERHEAT 1OO DEG IN AFT AIRSTAIR AREA AND OPS CK NORMAL.

Part: SEAL — LOOSE (LT WINDSHIELD)

CREW REPORTED, LOUD FLAPPING SOUND HEARD AT 15,000 FT MSL 280 KTS AT TOP OF CAPT'S WINDSHIELD. REQUESTED PRIORITY LANDING, DECLARED EMERGENCY AND LANDED. AFTER SLOWING ASAP, FLAPPING SOUND WAS TOP OUTSIDE SEAL ON NEW WINDOW INSTALLED ON 2/20 IN SDF, DEFERRED AERO DYNAMIC SEAL. INSTALLED MYLAR TAPE.

Part: BEAM — CORRODED (FS 344)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION AROUND THE FASTENER ON THE NOSE LANDING GEAR DRAG BRACE SUPPORT BEAM AFT FLANGE AT THE RIGHT HAND OUTBOARD SIDE STATION 344 AND WL 198.5. MAINTENANCE REMOVED AND REPAIRED THE FORWARD DRAG BRACE SUPPORT BEAM IAW UPS EO 727-53-1573.

Part: FITTING — CRACKED (FS 870)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACKS IN THE LEFT HAND TERMINAL FITTING AT STATION 870. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW UPS EO 727-5310-6913.

Part: CHORD — CORRODED (FS 740)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE CHORD AT STATION 740, WL 170 AND LBL 24 AND RBL 33. MAINTENANCE REMOVED AND REPLACED THE CHORD PER SRM 51-10-1, 51-10-2, 51-20-4 AND 51-30-2.

Part: FRAME — CORRODED (FS 760)

WHILE IN C- CHECK, MAINTENANCE FOUND CORROSION ON THE FRAME AT STATION 760, LBL 60-66 AND WL 209-213. MAINTENANCE REMOVED AND REPAIRED THE AREA IAW UPS EO 727-53-1574.

Part: STIFFENER — CORRODED (FS 870)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE VERTICAL STIFFENER AT STATION 870 AND LBL 44. MAINTENANCE REMOVED THE DAMAGED STIFFENER AND REPLACED WITH A NEW STIFFENER PER SRM 51-30-2.

Part: SKIN — CRACKED (FS 740)

WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE LOWER FUEL CELL SKIN AT STATION 740, LBL 18 TO LBL 24 AND WL 169. MAINTENANCE REPAIRED THE CRACK IAW UPS EO 727-5710-6914A.

Part: STIFFENER — CORRODED (FS 870)

WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK AND CORROSION ON THE STIFFENER ON THE WING CENTER SECTION REAR WEB AT STATION 870 AND LBL 33. MAINTENANCE REMOVED THE DAMAGED STIFFENER AND REPLACED WITH A NEW STIFFENER PER SRM 51-30-2.

Part: CHORD — CORRODED (FS 740)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE LOWER 740 CHORD AT RBL 55, LBL 55 AND WL 165. MAINTENANCE REMOVED AND REPLACED THE LOWER CHORD IAW UPS EO 727-5710-6911A.

Part: SKIN — CORRODED (FS 870)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE LOWER SURFACE OF THE UPPER FUEL CELL SKIN AT STATION 870 FROM LBL 65 TO RBL 65. MAINTENANCE REMOVED CORROSION, BLENDED AREAS, INSTALLED FILLER WASHERS, FLAP PEENED EFFECTED AREAS, ALODINED AND PRIMED AND RETURNED AIRCRAFT TO NORMAL PER SRM 51-10-2 AND MM 51-20-151.

Part: STRINGER — CRACKED (FS 742)

WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN STRINGER 17L AT STATION 742 AND WL 208. MAINTENANCE REMOVED THE CRACK AND REPAIRED THE STRINGER PER UPS 727-52-1580.

Part: SPAR CHORD — CORROSION (FS 870)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE CENTER WING TANK UPPER SPAR CHORD AT STATION 870 AND LBL 37 TO 40. MAINTENANCE FABRICATED AND INSTALLED REPAIR PER SRM 51-10-7, 51-30-2 AND 51-10-2.

Part: K FLAP — CORRODED (NR 5 LE FLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE NUMBER 5 K-FLAP AND BULLNOSE. MAINTENANCE REMOVED AND REPLACE WITH A NEW K-FLAP AND BULLNOSE IAW OHM 20-50-01 AND MM 27-81-01.

Part: RIB CHORD — CRACKED (FS 759)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACKS IN THE RIB CHORD ON THE RIGHT HAND SIDE AT 12 AND 6 O'CLOCK POSITION AT STATION 759, BL 70.5. MAINTENANCE REPAIRED THE CRACKS IAW UPS EO 727-5710-1271G.

Part: SKIN — CORRODED (FS 857)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON TOP OF FUSELAGE FUEL CELL SKIN AT STATION 857 TO 870, RBL 60 TO 65 AND WL 190. MAINTENANCE BLENDED AREA PER UPS EO 727-57-1350.

Part: EXPANSION LINK — CORRODED (FS 740)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE EXPANSION LINK AT STATION 740, WBL 168 AND RBL 13. MAINTENANCE REMOVED AND REPLACED THE EXPANSION LINK PER SRM 51-30-2 AND 51-10-1.

Part: STRINGER — CORRODED (FS 860)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 18A ON THE RIGHT HAND LOWER VERTICAL FLANGE AT STATION 860 TO 865. MAINTENANCE REMOVED THE CORROSION AND REPAIRED IAW UPS EO 727-53-1575.

Part: CHORD — CORRODED (FS 870)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE VERTICAL FLANGE OF THE LOWER CHORD AT STATION 870, WL 160, LBL 27 AND RBL 25. MAINTENANCE REMOVED THE CORRODED CHORD, FABRICATED NEW CHORD AND INSTALLED IAW UPS EO 727-5710-6912A.

Part: RIB CHORD — CRACKED (BL 70.5)

WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIB UPPER CHORD AT BL 70.5. MAINTENANCE REPAIRED AND MODIFIED THE CHORD IAW UPS EO 727-5710-1271G.

Part: RIB — CRACKED (LT HORIZ STAB)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON LT HORIZONTAL STAB, NR 4 T/E SUPPORT RIB ON LWR T/E BEAM AFT O/B ATTACH BOLT. REPLACED PER SRM 51-30-2, 51-10-2, MM 27-30-05.

Part: SKIN — CRACKED (LT AILERON)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON UPPER SKIN ON LT WING LWR O/B AILERON, O/B EDGE ON SKIN DOUBLER. REPAIRED PER SRM 57-50-05.

Part: CHORD — CORRODED (25 G BEAM)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON 25 G-BEAM CHORD FILLER PLATE. REPLACED 25G BEAM PER SRM 53-10-8, 51-10-01, 51-10-02, 51-30-2, MM 51-20-121.

Part: SPAR — CRACKED (LT AILERON)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON LT WING O/B AILERON, AFT SPAR. INSTALLED REPAIRED PER SRM 51-40-3, 57-50-2.

Part: SKIN — OIL-CANNED (LT ELEVATOR)

WHILE IN 'C' CHECK, MAINTENANCE FOUND OIL-CANNED UPPER SKIN PANEL ON LT ELEVATOR, STA 173.2-209.96. REPLACED PER SRM 51-30-2, 51-80-7.

Part: FLAP — CORRODED (RT WING)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON NR 6 K-FLAP JUST O/B OF THE DATA PLATE. INSTALLED REPAIR PER UPS EO FILE NR 727-57-1340.