N233SW

Part: FRAME — GOUGED (FRM 35) · airframe 44,643 hrs · 61,164 cycles

REMOVED DAMAGED AREA ON FRAME 35 BETWEEN STRINGERS 3 AND 4R IAW SRM 51-40-02, AND 53-00-04, REV 58. INSTALLED A REPAIRED DOUBLER IAW SRM 53-00-04, REV 58.

Part: SHEAR TIE — CRACKED (FRAME 44) · airframe 44,643 hrs · 61,164 cycles

REMOVED CRACKED SHEAR TIE AND MATCH DRILLED NEW SHEAR TIE IAW SRM 51-40-02, 51-25-00 REV 58. INSTALLED NEW SHEAR TIE IAW SRM 51-40-02 REV 58. TREATED AND APPLIED TOP COAT IAW CPM 51-21-04, REV 10.

Part: TRIM TAB — RUSTED (LT ELEVATOR) · airframe 44,643 hrs · 61,164 cycles

LEFT ELEVATOR TRIM TAB CORRODED. R & R THE TRIM TAB OUTBOARD 2 HINGE FITTING IAW AMM 20-10-01-2 REV 43.

Part: FLAP — CRACKED (NACELLE) · airframe 44,643 hrs · 61,164 cycles

FLAP CRACKED. R & R 18 FASTENERS PER EMB120 SRM 51-40-02 REV 58.

Part: COVER PLATE — CORRODED (CARGO THRESHOLD) · airframe 44,643 hrs · 61,164 cycles

REMOVAL AND INSTALLATION OF CARGO DOOR THRESHOLD COVER PLATE COMPLETE (PER ETD 2019-120-062528). PN: 120-16200-001 LOWER CARGO DOOR BEAM

Part: TRUNNION — DAMAGED (MLG) · airframe 44,643 hrs · 61,164 cycles

TRUNNION DAMAGED. INSTALLED A NEW LT MLG WELDED TRUNNION LUG ASSY IAW CMM 32-12-01 REV 15.

Part: FRAME — DAMAGED (FRM 30) · airframe 44,643 hrs · 61,164 cycles

REMOVED DAMAGED FRAME AND MATCH DRILLED NEW FRAME IAW SRM 51-40-02 REV 58. INSTALLED A NEW FRAME 30 SEGMENT IAW SRM 51-40-02 REV 58.

Part: DOUBLER — CRACKED (DOOR) · airframe 44,643 hrs · 61,164 cycles

DOUBLER CRACKED. MATCH DRILLED AND INSTALLED NEW DOUBLER IAW SRM 54-30-01, REV 58.

Part: DOUBLER — CORRODED (STAB) · airframe 44,643 hrs · 61,164 cycles

DOUBLER CORROED. MATCH DRILLED REPAIR PARTS IAW SRM 51-70-04, AND 51-40-02, REV 58. INSTALLED DOUBLER AND FILLER IAW STEP 2 OF ETD 2019-120-055992 AND SRM 51-40-02, REV 58. REMOVED REPAIRED DOUBLER IAW SRM 51-40-02, REV 58, CONFIRMED AFFECTED AREA CRACK FREE IAW STEP 2 OF ETD 2019-120-055992. REINSTALLED DOUBLER AND FILLER IAW STEP 2 OF ETD 2019-120-055992 AND SRM 51-40-02, REV 58.

Part: PLATE — CRACKED (NOT REPORTED) · airframe 44,643 hrs · 61,164 cycles

PLATE CRACKED. REMOVED DOOR STOP PLATE, MATCH DRILLED NEW PART AND INSTALLED IAW SRM 51-40-02, AND 51-25-00 REV 58.

Part: SHEAR TIE — CRACKED (FRAME 44) · airframe 44,643 hrs · 61,164 cycles

REMOVED CRACKED SHEAR TIE AND MATCH DRILLED NEW SHEAR TIE IAW SRM 51-40-02, 51-25-00 REV 58. INSTALLED NEW SHEAR TIE IAW SRM 51-40-02 REV 58. TREATED AND APPLIED TOP COAT IAW CPM 51-21-04 REV 10.

Part: SUPPORT CHANNEL — CRACKED (COWLING) · airframe 44,643 hrs · 61,164 cycles

SUPPORT CHANNEL CRACKED. MATCH DRILLED NEW HALF FRAME TO COWLING STRUCTURE IAW SRM 51-25-00 REV 58. MATCH DRILLED LATCH PIN GUIDE ASSY'S AND DOOR HOLD OPEN ROD PINS AND INSTALLED ON NEW HALF FRAME IAW AMM 20-10-01-2, REV 43, SRM 51-40-02-PR, AND 51-25-00-PR REV 58. INSTALLED NEW HALF FRAME IAW SRM 51-40-02-PR REV 58.

Part: DOOR — DAMAGED (NOT REPORTED) · airframe 44,643 hrs · 61,164 cycles

DOOR CHAFED. BLENDED CHAFFING IAW CPM 51-14-00. CONFIRMED AFFECTED AREA CRACK FREE IAW NDIM 51-00-03 REV 3. TREATED, PRIMED, AND APPLIED TOP COAT IAW COM 51-21-03 REV DATE 6/30/17.

Part: RIB — CHAFED (STAB) · airframe 44,643 hrs · 61,164 cycles

RIB FLANGE CHAFED AND CORRODED. REMOVED CORROSION AND CHAFFING IAW CPM 51-14-00 REV DATE 6/30/17. MATCH DRILLED NEW LEADING EDGE RIB FLANGE IAW SBM 51-5-00 REV 58. INSTALLED THE RIB FLANGE IAW SRM 51-40-02 REV 58. APPLIED PRIMER AND TOP COAT IAW CPM 512106 REV 6/30/17.

Part: FLOOR SUPPORT — CORRODED (FRAMES 15A-16A) · airframe 44,643 hrs · 61,164 cycles

UPPER SURFACE OF LH FLOOR BOARD ATTACH ANGLE BETWEEN FRAMES 15A - 16A WAS FOUND TO HAVE CORROSION. REMOVED FLOOR SILL (REF. SRM 51-40-02 REV 58). INSTALLED NEW FLOOR SILL (REF. SRM 51-40-02 REV 58). PN: 120-05802-001 SILL

Part: SKIN — GOUGED (FRAMES 39-40) · airframe 44,643 hrs · 61,164 cycles

SKIN GOUGED BETWEEN FRAMES 39-40, STRINGERS 18-19L. FABRICATED A DOUBLER AND FILLER SHIM AND APPLIED ALODINE AND EPOXY PRIMER TO DOUBLER AND SHIM PARTS IAW SRM 50-00-01 REV 58. APPLIED EDGE SEAL AND TOP COAT IAW SRM 51-22-00.

Part: SUPPORT — BURNED (NACELLE) · airframe 44,643 hrs · 61,164 cycles

FABRICATED REPAIR PARTS AND INSTALLED REPAIR IAW ETD 2019-120-045306 AND SRM 54-30-02 REV 58.

Part: FLOORBEAM — CORRODED (NOT REPORTED) · airframe 44,643 hrs · 61,164 cycles

FLOORBEAM CORRODED. MATCH DRILLED BEAM CAP AND INSTALLED LT FLOOR BEAM UPPER SURFACE AND BRACKET, RIB IAW SRM 51-40-02 REV 58. APPLIED SURFACE PROTECTION IAW CPM 51-21-00 REV 10.

Part: PANEL — CHAFED (NACELLE) · airframe 44,643 hrs · 61,164 cycles

PANEL CHAFED. REMOVED DAMAGED SEAL RING, MATCH DRILLED NEW PART, INSTALLED NEW SEAL RING (REF. EMB120 SRM 51-40-02 REV 58, EMB120 SRM 51-25-00 REV 58, EMB120 SRM 51-40-02 REV 58). LOCATED AND DRILLED NEW PNL 429AT (PER EMB120 SRM 51-40-04 REV 58).

Part: PAN — CRACKED (ZONE 800) · airframe 44,643 hrs · 61,164 cycles

PAN CRACKED. INSTALLED REINFORCING ANGLE IAW SRM 52-10-02 REV 58.

Part: SKIN — DAMAGED (TAILCONE) · airframe 44,643 hrs · 61,164 cycles

TAILCONE SKIN DAMAGED. FABRICATED A DOUBLER AND MATCH DRILLED REPAIR PARTS IAW ETD 209-120-046706, AND SRM 53-31-17, REV 58. INSTALLED THE REPAIRED DOUBLER AND FILLER IAW ETD 2019-120-046706, REV A.

Part: SKIN — DENTED (NOT REPORTED) · airframe 44,643 hrs · 61,164 cycles

REWORKED DENT IAW SRM 51-7400 REV 58. CONFIRMED AFFECTED AREA CRACK FREE IAW NDIM 51-00-03 REV 3. TREATED, PRIMED, AND APPLIED TOPCOAT IAW CPM 51-21-04 REV 10.

Part: SHEAR TIE — CRACKED (RT WING) · airframe 44,643 hrs · 61,164 cycles

RT WING SHEAR TIE CRACKED. MATCH DRILL NEW SHEAR CLIP IAW SRM 51-40-02 REV 58. INSTALLED CLIP WITH SEALANT IAW SRM 51-40-02 REV 58. APPLIED TOP COAT IAW CPM 51-21-06 REV 6/30/17.

Part: FITTING — CHAFED (ZONE 700) · airframe 44,643 hrs · 61,164 cycles

FITTING CHAFED. BLENDED CHAFFING (IAW EMB120 CPM 51-14-00).

Part: INTERCOSTAL — DAMAGED (NOT REPORTED) · airframe 44,643 hrs · 61,164 cycles

INTERCOSTAL DAMAGED, REMOVED DAMAGE IAW EPM 51-14-00. CONFIRMED AFFECTED AREA CRACK FREE IAW NDIM 51-00-03 REV 3. TREATED AND PRIMED AFFECTED AREA IAW CPM 51-21-04.

Part: BEARING — CORRODED (RUDDER HINGE) · airframe 44,643 hrs · 61,164 cycles

RUDDER HINGE BEARING CORRODED. R & R THE RUDDER LOWER HINGE BEARING IAW MM 20-40-03, REV 43.

Part: HINGE FITTING — CORRODED (RUDDER) · airframe 44,643 hrs · 61,164 cycles

RUDDER HINGE FITTING CORRODED. LOCATED AND DRILLED NEW HINGE FITTING IAW SRM 51-40-04 REV 58. APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO HOLES IAW CRM 51-21-07 REV 4.

Part: SHEAR TIE — CORRODED (FRAME 19) · airframe 44,643 hrs · 61,164 cycles

SHEAR TIE CORROED. REMOVED FR 19 SEGMENT FROM STR 1R-15R AND 2 DOUBLERS IAW SRM 51-40-02 REV 58. INSTALLED NEW FRAME AND 2 DOUBLERS IAW SRM 51-40-02 REV 08.

Part: SHEAR TIE — CRACKED (NOT REPORTED) · airframe 44,643 hrs · 61,164 cycles

SHEAR TIE FOUND DAMAGED. REMOVED AND REPLACED THE DAMAGED SHEAR TIE IAW SRM 51-40-02, REV 58. TREATED, PRIMED AND APPLIED TOP COAT TO FASTENERS IAW CPM 51-21-04 REV 10.

Part: SHEAR TIE — CRACKED (FRAME 44) · airframe 44,643 hrs · 61,164 cycles

SHEAR TIE CRACKED AT FRAME 44, BETWEEN STRINGERS 1 & 2. REMOVED AND REPLACED THE DAMAGED SHEAR TIE IAW SPM 51-40-02. TREATED AND APPLIED TOP COAT TO FASTENERS IAW CPM 51-21-04 REV 10.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 44,643 hrs · 61,164 cycles

FLOOR BEAM SEGMENT CORRODED . INSTALLED A NEW FLOOR BEAM SEGMENT IAW SRM 51-40-02 REV 58.

Part: DOOR — CHAFED (OVERWING EXIT) · airframe 44,643 hrs · 61,164 cycles

OVERWING EXIT WAS CHAFED. REMOVED CHAFE DAMAGE IAW CPM 51-14-00. TREATED, PRIMED AND APPLIED TOP COAT TO AFFECTED AREA IAW CPM 51-21-04.

Part: COVER — CORRODED (RUDDER HINGE) · airframe 44,643 hrs · 61,164 cycles

RUDDER HINGE COVER CORROED. CLEANED, PREPARED A NEW UPPER HINGE PANEL AND APPLIED PRIMER IAW CPM 51-21-04, AND 51-21-05. APPLIED TOP COAT IAW CPM 51-21-06.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-18) · airframe 44,643 hrs · 61,164 cycles

REMOVED FLOOR BEAM UPPER SURFACE (REF. SRM 51-25-00). INSTALLED NEW FLOOR BEAM AT FRAMES 17 - 18 (REF. SRM 51-40-02 REV 58). PN: 120-05805-603 BUTT STRAP REPLACES 120-05805-003

Part: COWLING — CRACKED (NACELLE) · airframe 44,643 hrs · 61,164 cycles

FABRICATED, LOCATED, AND DRILLED REPAIR DOUBLER (PER EMB120 SRM 51-40-04 REV 58 AND ETD 2019-120-067917). INSTALLED REPAIR DOUBLER (PER EMB120 SRM 51-40-02 REV 58 AND ETC 2019-120-067917). PN: 120-37974-001 RH INTERMEDIATE COWL SHIM

Part: FLOORBEAM — CORRODED (NOT REPORTED) · airframe 44,643 hrs · 61,164 cycles

FLOORBEAM CORRODED. MATCH DRILLED NEW BUTT STRAP AND INSTALLED BUTT STRAP IAW SRM 51-40-02 REV 58.

Part: FRAME — GOUGED (FRM 19) · airframe 44,643 hrs · 61,164 cycles

BLENDED A GOUGE ON THE AFT SIDE OF FRAME 19 IAW CPM 51-14-02 REV 10. CONFIRMED CRACK FREE IN AFFECTED AREA IAW NDIM 51-00-03 REV 3. TREATED AND PRIMED AFFECTED AREA IAW CPM 51-21-04 REV 4.

Part: SUPPORT — CRACKED (FRAME 44) · airframe 44,643 hrs · 61,164 cycles

SUPPORT CRACKED. REMOVED AND REPLACED THE SUPPORT AND MATCH DRILLED NEW SUPPORT IAW SRM 51-40-02 REV 58).

Part: SHEAR TIE — CRACKED (FRAME 16) · airframe 44,643 hrs · 61,164 cycles

SHEAR TIE CRACKED AT FRAME 16, STRINGER 15R. FABRICATED A NEW SUPPORT IAW DRAWING 120-09850 REV E AND SRM 51-30-01 REV 58. LOCATED AND MATCH DRILLED IAW SRM 51-40-04 REV 58. INSTALLED NEW SUPPORT / SHEAR TIE LESS FASTENERS THRU SKIN IAW SRM 51-40-02 REV 58. APPLIED SURFACE PROTECTION TO EXTERIOR SKIN IAW CPM 51-21-05 REV 10.

Part: SKIN — DAMAGED (NACELLE) · airframe 44,643 hrs · 61,164 cycles

CUT REPLACEMENT INNER PAN REPAIR SECTION (PER ETD 2019-120-050341). MATCH DRILLED AND TRIMMED DOUBLER REPAIR (IAW EMB120 ETD 2019-120-050341 REV A). INSTALLED REPAIR (PER EMB120 ETD 2019-120-050341 REV A). PN: 120-25601-029 DOOR SKIN, 120-25601-005 INNER SKIN

Part: RELAY — BURNED (PITOT HEAT) · airframe 44,301 hrs · 60,985 cycles

IN CRUISE, PILOT NOTICED A SMELL LIKE BURNING WIRE AND SMOKE WAS VISIBLE IN THE COCKPIT. DE-ICE LIGHT FAIL INDICATION ILLUMINATED AND THE NR 2 PITOT STATIC CIRCUIT BREAKER POPPED. AIRCRAFT DIVERTED TO THE NEAREST AIRPORT AND LANDED WITHOUT INCIDENT. MX TROUBLE SHOT THE ISSUE AND FOUND THE POWER FEED WIRES FOR THE NR 2 PITOT TUBE HEATER RELAY BURNT. R&R RELAYS AND RELAY SOCKETS K0092, K0093, K0092 & KX0093. R&R NR 2 PITOT TUBE HEAT CIRCUIT BREAKER CB0234. R&R CURRENT SENSORS T0030 & T0031. INSPECTED ELECTRICAL CONNECTIONS A NR 2 AND AUX PITOT PROBES. REPLACED DAMAGED WIRING AT RELAYS. PERFORMED OPERATIONAL CHECK OF PITOT HEAT SYSTEM WITH NO DEFECTS NOTED. ALL WORK PERFORMED IAW WM 20-50-00 & MM 30-31-00.

Part: AHRS — INOPERATIVE · airframe 41,882 hrs · 59,535 cycles

DIVERTED TO PSP WITH AN ATTITUDE DISPLAY LIGHT THAT ILLUMINATED FOLLOWED BY F/O ATTITUDE INDICATOR TUMBLING. HEADING FLAG DISPLAYED, AUTOPILOT AND FLIGHT DIRECTOR INOPERATOR. R & R FOS AHRS.

Part: HANDLE — FAILED (MLG) · airframe 41,379 hrs · 58,830 cycles

GEAR WARNING AT 900 DURING LANDING. REPLACED GEAR HANDLE ASSEMBLY AND MLG CONTROL MODULE.

Part: SWITCH — DIRTY (MLG) · airframe 41,199 hrs · 58,585 cycles

WHEN THE GEAR WAS EXTENDED ALL GEAR LIGHTS WERE IN THE GREEN. RECEIVED A GEAR WARNING LIGHT. AFTER LANDING ALL GEAR DOORS WERE FOUND OPEN. CLEANED MICROSWITCHES ON POWER LEVERS AND LUBED THE SELECTOR VALVES, OPS CHECKED GOOD.

Part: SIGN — UNSECURE (EMERGENCY LIGHT) · airframe 41,001 hrs · 58,313 cycles

EMERGENCY EXIT SIGN AT 9C NOT SECURE. RESECURED EXIT SIGN.

Part: ACTUATOR — FAILED (LT MLG) · airframe 40,959 hrs · 58,259 cycles

DURING GEAR RETRACTION, LEFT MAIN GEAR DISAGREEMENT LIGHT WOULDN'T EXTINGUISH. CYCLED GEAR, LIGHT WENT OUT. PASSED FUNCTIONAL FLIGHT. R & R LT MLG UPLOCK - UNLOCKING ACTUATOR AND ADJUSTED UPLOCK LINK IAW AMM.

Part: CONTROL MODULE — FAILED (MLG) · airframe 40,945 hrs · 58,235 cycles

AFTER TAKEOFF, RETRACTED LANDING GEAR AND HAD A LT MAIN GEAR DISAGREEMENT. RAN QRH AND GEAR RETRACTED NORMALLY. R & R LANDING GEAR RELAY BOX AND REPLACED LANDING GEAR CONTROL MODULE IAW AMM. CHECKED GAPS OF LT MLG DOWNLOCK PROXIMITY SENSORS IAW AMM. CYCLED SEVERAL TIMES, NO DISAGREEMENT. OPS CHECK GOOD AT THIS TIME, PN: 120-38594-001, SN ON: 120135, SN OFF: 120127, PN: 120-61110-001, SN ON: 505060, SN OFF: 241867-315

Part: ACTUATOR — FAILED (MLG) · airframe 40,745 hrs · 57,955 cycles

LEFT MAIN GEAR WOULD NOT RETRACT AFTER TAKEOFF. RECEIVED LT MAIN GEAR DISAGREE LIGHTS. REPLACED LT MLG ACTUATOR AND REPLACED LT MLG RETRACT ACTUATOR ROD, BRACKET AND ATTACH PIN IAW AMM AND CMM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 40,656 hrs · 57,838 cycles

SHEET METAL CRACKED IN BOTH AFT CORNERS UNDER OBSERVER SEAT AREA. C CHECK INSTALLED DOUBLERS TO LT & RT CORNER CLIPS BELOW OBSERVERS SEAT IAW SRM.

Part: DOOR — CRACKED (HYDRUALIC BAY) · airframe 40,656 hrs · 57,838 cycles

RT HYD BAY DOOR HAS A CRACK BY OTBD HINGE. C CHECK NEW DOOR FIT ON RT NACELLE HYD BAY IAW EA.

Part: CLEAT — CRACKED (RT WING) · airframe 40,656 hrs · 57,838 cycles

RT WING NR 5 FUEL PANEL AREA HAS CRACKED UPPER SKIN CLEAT ON INBD SIDE. C CHECK REPLACED SKIN CLEAT, PN 120-17062-613, AT RIB INBD OF LT NR 5 FUEL CELL ACCESS PANEL IAW SRM.

Part: CLEAT — CRACKED (RT WING) · airframe 40,656 hrs · 57,838 cycles

RT WING NR 5 FUEL PANEL AREA HAS CRACKED UPPER SKIN CLEAT BY FUEL PROBE. C CHECK REPLACED UPPER SKIN CLEAT, PN 120-17063-609, OTBD OF RT NR 5 FUEL CELL ACCESS PANEL IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 40,656 hrs · 57,838 cycles

FRAME 36 IN THE CTR OF THE BELLY OVER THE APU BLEED LINE THE OUTER SKIN SHOWS SIGNS OF CORROSION. C CHECK REPAIRED LOWER CTR BELLY SKIN AT FRAME 36 IAW ETD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 40,656 hrs · 57,838 cycles

FRAME 31 IN THE CTR OF THE BELLY OVER THE APU BLEED LINE THE OUTER SKIN SHOWS SIGNS OF CORROSION. C CHECK REPAIRED CTR BELLY SKIN AT FRAME 31 IAW ETD.

Part: SENSOR — FAILED (WOW) · airframe 40,462 hrs · 57,595 cycles

ELEC CAUTION ON MAP & BOTH IDLE UNLOCK LIGHTS ON & NOSE WHEEL STEERING WAS NOT WORKING NO INDICATION LIGHTS. HAD TO USE DIFFERENTIAL POWER BRAKING TO THE GATE. FLT 6302 REPLACED RT WOW SENSOR & HARNESS IAW AMM. OPERATIONS CHECKED GOOD.

Part: CIRCUIT BREAKER — FAILED (ELECTRICAL SYS) · airframe 40,340 hrs · 57,418 cycles

ON CLIMB OUT NR 2 INVERTER INOPERATIVE LIGHT ILLUMINATED, RETURN TO FIELD. FLT 1352 REPLACED CIRCUIT BREAKER 0414 IAW AMM 0-13-03.

Part: RELAY — FAILED (ELECTRICAL SYS) · airframe 40,340 hrs · 57,418 cycles

ON TAKEOFF THE NR 2 INVERTER INOPERATIVE LIGHT ILLUMINATED, RETURNED TO FIELD. FLT 6286 REPLACED INVERTER 2 RELAYS K0008 & K0004 IAW EMB MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,560 hrs · 56,364 cycles

EMERGENCY EXIT LIGHT UNDER FA JUMP SEAT BURNED OUT. FLT#6286 RELAMPED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,430 hrs · 56,183 cycles

FORWARD FLOOR EMERGENCY LIGHTS DO NOT ILLUMINATE. REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK, PN: D366-04-001, SN ON: 632, SN OFF: 1164.

Part: SOLENOID VALVE — FAILED (LANDING GEAR) · airframe 39,370 hrs · 56,091 cycles

LEFT MLG WOULD NOT RETRACT. ATTEMPTED TO CYCLE THE GEAR BUT WOULD NOT RETRACT. REPLACED LANDING GEAR SOLENOID VALVE AND GEAR HANDLE MODULE ASSY IAW AMM. PN: 18190-003, SN ON: 758, SNOFF: 845, SNON: 120-38594-501, SNON: 120343, SNOFF: 190451-306.

Part: PLACARD — DETACHED (EMERGENCY EXIT) · airframe 39,100 hrs · 55,713 cycles

EMERGENCY EXIT PLACARD 6C FELL OUT. (FLT 5510) RE-INSTALLED EMERGENCY EXIT PLACARD AT 6C, OPS CHECK GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 38,537 hrs · 54,893 cycles

ONE RED FLOOR LEVEL EMERGENCY LIGHT MISSING NEAR MAIN CABIN DOOR. (FLT 5373) INSTALLED ONE FLOOR LEVEL RED EMERGENCY LIGHT AT MAIN CABIN DOOR.

Part: FUSE — FAILED (CABIN) · airframe 38,309 hrs · 54,581 cycles

FORWARD FLOOR EMERGENCY LIGHTS INOPERATIVE. (SERVICE) REPLACED FUSE.

Part: AILERON — OUT OF ADJUST (WING) · airframe 38,250 hrs · 54,496 cycles

DURING DESCENT AIRCRAFT STARTED UNCOMMANDED LEFT TURN. UPON DISCONNECTING AUTOPILOT, AIRCRAFT CONTINUED LEFT TURN. (FLT 5615) INSPECTED ALL FLIGHT CONTROL CABLE ROUTING AND TENSIONS. ADJUSTED AILERON, AILERON TRIM TENSIONS. ALSO RT AILERON TAB WAS ADJUSTED.

Part: APU — FAULTY (APU BAY) · airframe 38,219 hrs · 54,454 cycles

FUEL SMELL IN THE FLIGHT DECK WHEN THE APU IS ON. (FLT 5458) REPLACED APU ASSEMBLY IN REFERENCE TO AMM.

Part: WIRE — BROKEN (CABIN) · airframe 37,993 hrs · 54,141 cycles

EMERGENCY EXIT SIGN ABOVE SEAT 9B DOES NOT ILLUMINATE. (FLT 5349) REPAIRED BROKEN WIRE WITH A SERVICEABLE SPLICE.

Part: INDICATOR — FAILED (COCKPIT) · airframe 37,609 hrs · 53,586 cycles

T6 CLIMBED RAPIDLY AND RECEIVED A T6 WARNING ON THE LEFT ENGINE. THE T6 CONTINUED TO CLIMB AND DID A PRECAUTIONARY ENGINE SHUTDOWN. (FLT 5607) REPLACED T6 INDICATION. P/N: SEL-OC19EG S/N OFF: 215.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,357 hrs · 53,261 cycles

ONE WHITE EMERGENCY FLOOR LIGHT AT 3A IS BURNED OUT. (FLT 5547) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,320 hrs · 53,209 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 7 IS OUT. (FLT 5566) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,289 hrs · 53,163 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 9 IS OUT. (FLT 6752) RELAMPED EMERGENCY LIGHT.

Part: SKIN — CORRODED (FUSELAGE) · airframe 37,148 hrs · 52,971 cycles

CORROSION FOUND AT FRAME 37 AND STRINGER 21R AND TITANIUM STRAP IS LIFTED. (C-CHECK) REPAIRED AREA OF CORROSION ON FUSELAGE SKIN AT FRAME 37 AND STRINGER 21R IN REFERENCE TO ETD.

Part: SIGN — MISSING (CABIN) · airframe 36,650 hrs · 52,294 cycles

EXIT SIGN AT 9B IS MISSING. (FLT 6254) REPLACED EMERGENCY EXIT SIGN AT SEAT 9B.

Part: CONTROL SWITCH — FAILED (MCD) · airframe 35,864 hrs · 51,212 cycles

MCD WOULD NOT OPEN. (FLT 5323) REPLACED MAIN CABIN DOOR CONTROL SWITCH AT F/A'S CONTROL PANEL.

Part: BALLAST — FAILED (CABIN) · airframe 35,719 hrs · 51,001 cycles

SMOKE SMELL IN CABIN. (FLT 5371) GALLEY LIGHT BALLAST BURNED UP WHEN IT FAILED. REPLACED AFT GALLEY LIGHT BALLAST.

Part: HANDLE — LACK OF LUBE (CABIN DOOR) · airframe 35,670 hrs · 50,935 cycles

MAIN CABIN DOOR INNER HANDLE DIFFICULT TO OPERATE. (FLT 5315) LUBRICATED MAIN CABIN DOOR HANDLE ASSEMBLY.

Part: WIRE — BROKEN (CABIN) · airframe 34,592 hrs · 49,522 cycles

FORWARD EMERGENCY EXIT LIGHT IS OUT. (SERVICE) REPAIRED BROKEN WIRES AT FORWARD EMERGENCY LIGHT.

Part: SIGN — MISSING (CABIN) · airframe 34,160 hrs · 48,925 cycles

EXIT SIGN BELOW F/A'S JUMPSEAT FELL OFF. (FLT 6281) REPLACED EXIT SIGN BELOW F/A'S JUMPSEAT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 34,134 hrs · 48,887 cycles

OVERHEAD CEILING EMERGENCY LIGHT ABOVE ROW 3 INOPERATIVE . (FLR 6315) 315 ) RELAMPED EMERGENCY LIGHT.

Part: STOP FITTING — OUT OF ADJUST (CABIN DOOR) · airframe 33,862 hrs · 48,516 cycles

F/A REPORTS MAIN CABIN DOOR HARD TO OPEN. (FLT 6226) RE-SHIMMED BOTH FORWARD AND AFT UPPER MOST BACK STOPS.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 33,803 hrs · 48,434 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. (FLT 6287) ADJUSTED AND LUBRICATED FORWARD DOOR ASSEMBLY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,803 hrs · 48,434 cycles

SEVERAL EMERGENCY LIGHTS AND SIGNS AT FRONT OF CABIN DO NOT ILLUMINATE. (FLT 6373) REPLACED FORWARD ELBP.

Part: HANDLE — LACK OF LUBE (CABIN DOOR) · airframe 32,734 hrs · 46,941 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6227) APPLIED LUBE TO MAIN CABIN DOOR HANDLE INSIDE AND OUTSIDE PIVOT POINTS.

Part: LIGHT — LOOSE (CABIN) · airframe 32,617 hrs · 46,778 cycles

ROW SIX OVERHEAD EMERGENCY EXIT LIGHT INOP. RE-SEATED LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,512 hrs · 46,634 cycles

AFT EMERGENCY LIGHT INOP. (FLT 6195) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,512 hrs · 46,634 cycles

FLOOR EMERGENCY LIGHTS FROM ROW 6 AND AFT STAY ON WITH SWITCH IN OFF POSITION. (FLT 6505) REPLACED AFT ELBP P/N D366-04-001, S/N ON 1089, S/N OFF 1260/08-96.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,512 hrs · 46,634 cycles

ONE RED AND ONE WHITE FLOOR EMERGENCY LIGHT INOP. (FLT 6553) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,512 hrs · 46,634 cycles

FLOOR EMERGENCY LIGHT INOP. (FLT 5801) RELAMPED EMERGENCY LIGHT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,464 hrs · 46,569 cycles

EMERGENCY LIGHTS CAME ON DURING TAXI OUT, WOULD NOT TURN OFF. (FLT 6645) REPLACED OVERWING EMERGENCY LIGHT BATTERY.

Part: WIRE — BROKEN (CABIN) · airframe 32,271 hrs · 46,285 cycles

NR 3 LIGHT ON LEFT SIDE OF FLOOR LEVEL ILLUMINATION TRACK LIGHTING INOP. (FLT 5758) REPAIRED BROKEN WIRE.

Part: LIGHT — MISSING (CABIN) · airframe 32,219 hrs · 46,206 cycles

ONE RED EMERGENCY LIGHT AT ROW 1 IS MISSING. (FLT 5803) REPLACED LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,219 hrs · 46,206 cycles

ONE WHITE FLOOR LEVEL EMERGENCY LIGHT INOP. (FLT 5767) REPLACED LIGHT ASSEMBLY.

Part: DUCT — BLOWN (BLEED AIR SYS) · airframe 31,748 hrs · 45,506 cycles

RIGHT ENGINE OVERTORQUED ON CLIMB OUT DUE TO BLOWN DUCT. (FLT 6847)REPLACED BLEED DUCT AND RIGHT ENGINE PROP.

Part: FUSE — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 31,697 hrs · 45,445 cycles

AFT THIRD OF FLOOR LEVEL EMERGENCY LIGHTS INOP. (FLT 5803) RESET FUSES.

Part: WIRE — BURNED (CABIN) · airframe 31,364 hrs · 44,971 cycles

WIRE AT RCCB BURNED. (SVC CHECK) REPAIRED WIRING.

Part: WIRE — BROKEN (CABIN) · airframe 31,086 hrs · 44,583 cycles

FORWARD MOST RED EMERGENCY TRACK LIGHT INOP. (FLT 6236) REPAIRED WIRE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,986 hrs · 44,433 cycles

ONE OF THE RED FLOOR LEVEL EMERGENCY LIGHTS INOP. (FLT 6311)RELAMPED.

Part: WIRE — BROKEN (CABIN) · airframe 30,709 hrs · 44,052 cycles

FORWARD FLOOR EMERGENCY LIGHT INOP. (FLT 6179) REPAIRED BROKEN WIRE.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 30,649 hrs · 43,967 cycles

FLT 5972 - EXIT SIGN AT ROW 9 IS BROKEN. REPLACED SIGN.

Part: LAMP — LOOSE (EMERGENCY LIGHT) · airframe 30,517 hrs · 43,791 cycles

FLT 6206 - FORWARD FLOOR LEVEL EMERGENCY LIGHT INOP. RESECURED LAMP.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 30,298 hrs · 43,480 cycles

FLT 5540 - EMERGENCY LIGHT INOP SEAT 2A. RESEATED WIRE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 30,206 hrs · 43,362 cycles

FLT 5472 - OVERHEAD EMERGENCY LIGHT AT ROW 9 INOP. RELAMPED.

Part: SPAR CAP — CRACKED (LT WING) · airframe 30,338 hrs · 43,530 cycles

LEFT WING INBOARD UPPER AUXILIARY SPAR CAP IS CRACKED (C CHECK). REPAIRED PER EMB DIRECTIVE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,338 hrs · 43,530 cycles

CORROSION FOUND BEYOND LIMITS AT FRAME 38 INTERNAL SKIN BETWEEN STRINGERS 21L AND 21R (C CHECK). REPAIRED PER EMBRAER DER.

Part: FRAME — CRACKED (LT NACELLE) · airframe 30,338 hrs · 43,530 cycles

LEFT NACELLE POWER & CONDITION LEVER PULLEY QUADRANT SUPPORT FRAME IS CRACKED (C CHECK). REPLACED PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,338 hrs · 43,530 cycles

LOWER FUSELAGE CENTER SKIN SUPPORT AT FRAME 30 CORRODED (C CHECK). REPAIRED PER EMBRAER INSTRUCTIONS.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 29,039 hrs · 41,834 cycles

EMERGENCY EXIT SIGN AT ROW 6 IS BROKEN. FLIGHT 5576. REPLACED EXIT SIGN AT ROW 6.

Part: OIL COOLER — LEAKING (RT ENGINE) · airframe 28,079 hrs · 40,550 cycles

FLT 5557 - RIGHT ENGINE OIL PRESSURE DROPPED ON TAKEOFF. REPLACED OIL COOLER IAW EMB 79-21-01. OPS AND LEAK CHECKS GOOD.

Part: LENS — CRACKED (EMERGENCY LIGHTS) · airframe 26,657 hrs · 38,554 cycles

EMERGENCY EXIT SIGN LENS IS CRACKED, FLIGHT NR 5658. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. OPS CHECK GOOD.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 26,359 hrs · 38,165 cycles

FLT 5792 - EMERGENCY "EXIT" SIGN ABOVE ROW 9 DOES NOT ILLUMINATE RECONNECTED WIRE ON EXIT SIGN. OPS CHECK GOOD.

Part: RIB — CRACKED (PAX DOOR) · airframe 26,359 hrs · 38,165 cycles

PAX DOOR MID SECTION FORWARD INTERNAL RIB IS CRACKED. REPLACED PAX DOOR INTERNAL RIB IAW SRM 120 51-10-02 PG 3 SEC 3A.

Part: RIB — CRACKED (PAX DOOR) · airframe 26,359 hrs · 38,165 cycles

PAX DOOR MID SECTION AFT INTERNAL RIB IS CRACKED, DISCOVERED AT C-CHECK. REPLACED PAX DOOR INTERNAL RIB IAW SRM 120 51-100-02 PG 3 SEC 3A.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 26,359 hrs · 38,165 cycles

EXFOLIATING CORROSION FOUND ON PROFILE OF RIGHT SIDE CROSSBEAM MEMBER FORWARD OF CARGO DOOR, DISCOVERED AT C-CHECK. REPAIRED RIGHT SIDE OF CROSSBEAM IAW EMB 120 SRM 51-10-02 PG 3 SEC 3A, P/N 120-04449-001.

Part: TORQUE TUBE — CORRODED (PAX DOOR) · airframe 26,359 hrs · 38,165 cycles

PAX DOOR TORQUE TUBE AFT BEARING BOSS HAS CORROSION, DISCOVERED AT C-CHECK. REPLACED PAX DOOR TORQUE TUBE AFT BEARING BOSS IAW EMB 120 MM 52-11-05.

Part: ROD END — CORRODED (RT ELEVATOR) · airframe 26,359 hrs · 38,165 cycles

RIGHT LOWER ROD END BEARING ON THE ELEVATOR QUADRANT IS CORRODED, DISCOVERED AT C-CHECK. REPLACED RIGHT LOWER ROD END ON ELEVATOR QUADRANT IAW EMB 120 MM 27-31-04, PN RA4MK7-J.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 25,600 hrs · 37,048 cycles

FOUND FORWARD CABIN EMERGENCY LIGHT FAILED. REPLACED FORWARD EMERGENCY BATTERY PACK. OPERATIONAL CHECKS GOOD, SN OFF 222.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,017 hrs · 36,210 cycles

NO EMERGENCY LIGHT AFT OF ROW 8. REPLACED CENTER FUSE AND AFT ELBP. OPERATIONAL CHECKS GOOD.

Part: SOCKET — DEFECTIVE (CABIN) · airframe 24,305 hrs · 35,143 cycles

FORWARD RED EMERGENCY LIGHT INOP. INSTALLED NEW LIGHT SOCKET. OPERATIONAL CHECKS GOOD.

Part: WINDSHIELD — DEFECTIVE (COCKPIT) · airframe 24,024 hrs · 34,699 cycles

WINDSHIELD HEAT CAUSES BURNING SMELL IN COCKPIT. REPLACED LEFT WINDSHIELD ASSEMBLY IAW EMB 120 MM 56-10-00 AND RII 56-200-1000. OPERATIONAL CHECKS GOOD, PN NP-151311-1, SN/OFF 0412H3933.

Part: WIRE — BURNED (NLG WW) · airframe 23,966 hrs · 34,637 cycles

FRIED WIRES FOR TAXI LIGHTS IN NOSE WHEEL AREA. REPLACED DAMAGED WIRES TO RIGHT TAXI LIGHT. OPERATIONAL CHECKS GOOD.

Part: WIRE — BROKEN (EMERGENCY EXIT) · airframe 23,615 hrs · 34,115 cycles

FOUND EXIT ROW SIGN IN OVERHEAD BIN INOP. REPAIRED WIRE W220-1052-22W IAW WM 33-50-00. OPERATIONAL CHECK GOOD.

Part: SERVO — MALFUNCTIONED (ELEVATOR) · airframe 22,742 hrs · 32,806 cycles

SLIGHT RESISTANCE AND RUBBING SOUND FROM CAPT SIDE WHEN YOKE IS EXERCISED FWD AND AFT. REPLACED ELEVATOR SERVO IAW MM 22-10-05. OPERATIONAL CHECK GOOD.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,434 hrs · 32,317 cycles

ONE RED LIGHT INOP IN FLOOR LEVEL LIGHTING OVER ROW 6. REPLACED LIGHT SOCKET ON FLOOR LIGHTING AT ROW 6. OPERATIONAL CHECK GOOD.

Part: GROUND WIRE — LOOSE (EXIT SIGN) · airframe 22,128 hrs · 31,836 cycles

EMERGENCY EXIT SIGN OVER ROW 9 IS INTERMITTENT. SECURED LOOSE GROUND WIRE AT ROW 9 EXIT SIGN. OPERATIONAL CHECK GOOD.

Part: RELAY — BURNED (APU) · airframe 19,812 hrs · 28,318 cycles

PILOT'S COMPLAIN OF BURNED ODOR IN COCKPIT. REMOVED AND REPLACED APU FEEDER PROTECTION RELAY IAW SRM 20-40-00 AND MM 24-52-00 FIG 7. OPERATIONAL CHECK GOOD.

Part: CONTROL HANDLE — MALFUNCTIONED (TE FLAPS) · airframe 19,407 hrs · 27,694 cycles

WHEN ON APPROACH, SELECTED FLAPS 25 GOT CONTROL FAULT. REPLACED FLAP HANDLE. OPS CHECK GOOD. P/N ON 120-54207-615, S/N OFF 120338.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 19,324 hrs · 27,579 cycles

COCKPIT LEFT SIDE FRAME 12 SUPPORT AFT/MIDDLE OF DV WINDOW FRAME. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED COCKPIT LEFT SIDE FRAME 12 SUPPORT AFT/MIDDLE OF DV WINDOW FRAME WITH A SERVICEABLE UNIT IAW SRM 51-10-02, 51-40-00.

Part: SKIN — CRACKED (RT NACELLE) · airframe 19,358 hrs · 27,630 cycles

RIGHT NACELLE FLAP UPPER SKIN TO RIB CLIP CRACKED AT RIVET. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED RIGHT NACELLE FLAP UPPER SKIN TO RIB CLIP WITH A SERVICEABLE UNIT IAW SRM 51-10-02, 51-40-00.

Part: CLIP — CRACKED (RT NACELLE) · airframe 19,324 hrs · 27,579 cycles

RIGHT WING OUTBOARD OF NACELLE 1ST FUEL PANEL OUTBOARD MIDDLE LOWER CLIP CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SHEAR TIE RIGHT WING (MIDDLE LOWER). NO LEAKS NOTED.

Part: CONTROL PANEL — MALFUNCTIONED (AUTO PILOT) · airframe 19,209 hrs · 27,373 cycles

AFTER LANDING, AUTOPILOT KEPT RE-ENGAGING ITSELF, WOULD RE-ENGAGE ON BOTH SIDES REPEATEDLY. REPLACED AUTOPILOT CONTROL PANEL. OPS CHECK GOOD ON BOTH SIDE AUTOPILOT.

Part: SELECTOR — MALFUNCTIONED (TE FLAPS) · airframe 19,209 hrs · 27,373 cycles

CONTROL FAULT WHEN FLAPS SELECTED FROM 25 DEGREES TO 45 DEGREES WITH NO COMMAND BARS. REPLACED FLAP CONTROL HANDLE WITH SERVICEABLE UNIT. OPS CHECKS GOOD.

Part: ACTUATOR — MALFUNCTIONED (ELEVATOR TRIM) · airframe 19,044 hrs · 27,122 cycles

IN CRUISE, NOTICED ELEVATOR TRIM SNAPBACK WITH AUTOPILOT ENGAGED, FL 230 AND -31 DEGREES C. DISCONNECTED AUTOPILOT, MANUALLY ATTEMPTED TO MOVE TRIM, UNABLE TO MOVE TRIM. REGAINED TRIM CONTROL AT 4000 FT AND + 6 DEGREES. REPLACED RIGHT AND LEFT ELEVATOR TRIM TAB ACTUATORS IAW EMB 120 MM 27-32-02. OPS CHECK GOOD. P/N: 5299-1, S/N ON: 633, S/N OFF: 728, S/N ON: 938, S/N OFF: 535.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 18,531 hrs · 26,354 cycles

FLAP CONTROL FAULT INDICATION OCCURED WHEN GOING FROM 25 TO 45 DEGREE FLAP COULD NOT RESET. REPLACED FCU WITH SERVICEABLE UNIT. OPS CHECK GOOD.

Part: CONTROL HANDLE — FAULTY (COCKPIT) · airframe 18,221 hrs · 25,852 cycles

ON APPROACH, WHEN SELECTING FLAPS 45 GOT CONTROL FAULT. REPLACED FLAP CONTROL LEVER ASSY IAW MM 27-50-00. OPS CHECK OK

Part: CONTROL LEVER — MALFUNCTIONED (COCKPIT) · airframe 18,041 hrs · 25,529 cycles

FLAPS WILL NOT EXTEND PAST 25 DEGREE SETTING EVEN WHEN 45 DEGREE IS SELECTED.FLAP SELECTOR WOULD NOT SLIDE SMOOTHLY INTO 45 DEGREE DETENT. REPLACED FLAP SELECTOR LEVER. OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,905 hrs · 25,338 cycles

NUMEROUS FLOOR EMERGENCY LIGHTS (REAR ROWS) DO NOT ILLUMINATE ON TEST AND EMERGENCY LIGHT SIGNS AT ROW 9 DO NOT ILLUMINATE ON TEST.REMOVED AND REPLACED AFT EMERGENCY LIGHT BATTERY IAW MM 33-00-00. OPS CHECK GOOD.

Part: WIRE — CHAFED (NR 1 ENG OIL) · airframe 17,900 hrs · 25,332 cycles

ABORTED TAKEOFF FOR AURAL WARNING ''OIL'' WITH LIGHT FLASHING ON MAP (OIL PRESS). PERFORMED AURAL WARNING RESET AND STATIC RUN UP. STILL RECEIVED ''OIL'' AURAL WARNING. FOUND AND REPAIRED A CHAFED WIRE ON NR 1 ENGINE OIL PRESSURE SWITCH. GROUND RUN UP OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,151 hrs · 24,204 cycles

LEFT FORWARD OUTBOARD EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY WITH NEW ASSEMBLY IAW 33-52-01. OPS CHECK GOOD.

Part: ACTUATOR — FROZEN (ELEVATOR TRIM) · airframe 17,151 hrs · 24,204 cycles

ELEVATOR TRIM FROZE IN FLIGHT AT 24,000 FT -31C DEGREES. AFTER DESCENDING TO ABOUT 12,000 FT WITH OAT AT -5C DEGREES IT RETURNED TO NORMAL. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR TRIM ACTUATORS IAW MM 27-32-02. CABLES TENSIONED IAW MM 27-00-01. OPS CHECK GOOD.

Part: MOTOR — FAILED (WINDSHIELDWIPER) · airframe 17,151 hrs · 24,204 cycles

AFTER TAKEOFF THE RIGHT WINDSHIELD WIPER WOULD NOT PARK. RETURNED TO RDD DUE TO WIPER BOUNCING ON WINDSHIELD. REPLACED RIGHT WINDSHIELD WIPER MOTOR ASSEMBLY. OPS CHECK GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 17,151 hrs · 24,204 cycles

ROW 6C EMERGENCY EXIT LIGHT FIXTURE IS BROKEN. INSTALLED SERVICEABLE LIGHT FIXTURE. OPS CHECK GOOD.

Part: INDICATOR — FAILED (COCKPIT) · airframe 15,906 hrs · 22,295 cycles

ON TAKEOFF ROLL, PAST 80 KIAS, THE NR 2 TORQUE GAUGE INDICATION WENT TO ZERO. ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED RIGHT TORQUE INDICATOR. RAN THE ENGINE TO 100 PERCENT TORQUE FOR 1 MIN. NO FAULTS FOUND. OPS CHECK GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 15,630 hrs · 21,862 cycles

LEFT FRAME 9 IS CRACKED FORWARD OF THE DIRECT VISION WINDOW POST. REPAIRED CRACK BY COMPLIANCE WITH SB 120-53-0073.

Part: FUEL CONTROL — FAULTY (APU) · airframe 13,967 hrs · 19,410 cycles

UPON LIFT OFF FROM PDX, STRONG FUEL SMELL NOTED IN CABIN AND FLIGHT DECK. APU BLEED WAS POWERING BOTH PACKS. INSPECTED APU AND BLEED SYSTEM. NO FAULTS NOTED. REMOVED AND REPLACED APU FUEL CONTROL UNIT. OPS CHECK GOOD IAW ALLIED SIGNAL MM 49-00-00. P/N: 3882730-9, S/N ON: A1124, S/N OFF: 15683.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 13,639 hrs · 18,938 cycles

COMPLETE LOSS OF BLUE SYSTEM HYDRAULICS AT SBP, COMPLIED WITH QRH. RETURNED TO LAX AND LANDED FLAPS 0 DEGREES. INSPECTED AND FOUND T6 CAP SCREWS OF RIGHT NACELLE ACTUATOR LOCK PIN SOLENOID SHEARED OFF. INSTALLED SERVICEABLE RIGHT NACELLE FLAP ACTUATOR IAW MM 27-50-00, SEE RII 27-307. CYCLED FLAPS NUMEROUS TIMES, OPS CHECKS GOOD. NO LEAKS NOTED.

Part: POTENTIOMETER — INOPERATIVE (NLG) · airframe 13,214 hrs · 18,331 cycles

AIRCRAFT WANTED TO VEER RIGHT DURING TAXI. AFTER ROTATION THE PEDAL STEER INOP LIGHT ILLUMINATED. RETURNED TO SEA. AFTER LANDING THE AIRCRAFT WANTED TO VEER RIGHT WHEN NOSE WHEEL TILLER WAS APPLIED. REPLACED NOSE WHEEL FEEDBACK POT WIDTH A SERVICEABLE UNIT IAW MM 32-50-05. OPS CHECKS GOOD AT THIS TIME. (S/N ON: 191) (S/N OFF: 257) (P/N ON/OFF: 20500-000-02).

Part: SWITCH — OUT OF ADJ (CARGO DOOR) · airframe 12,958 hrs · 17,999 cycles

ABORT TAKEOFF AT 90 KNOTS FOR CARGO DOOR WARNING. RETURNED TO GATE. ADJUSTED FORWARD CARGO DOOR MICROSWITCH IAW MM 52-30-00. OPS CHECK GOOD.

Part: SEAL — LOOSE (CARGO DOOR) · airframe 12,844 hrs · 17,857 cycles

COMPLETE LOSS OF CABIN PRESSURIZATION AT 25,000 FEET. MASKS DEPLOYED. PERFORMED RAPID DESCENT TO SAFE ALTITUDE AND LANDED IN LAX. FOUND LOWER AFT PORTION OF CARGO DOOR SEAL POPPED OUT OF POSITION. REINSTALLED SEAL BACK INTO RETAINER AND CHECKED SECURITY. PRESSURIZED AIRCRAFT TO 7.0 PSI FOR 10 MINUTES AND CHECKED FOR LEAKS. OPS CHECK GOOD.

Part: SERVO — FAILED (ELEVATOR) · airframe 12,243 hrs · 17,001 cycles

AUTO PILOT DOES NOT CATCH ALTITUDE, BOTH SIDES. REPLACED ELEVATOR SVO-65 IAW MM 27-10-05 AND TESTED AUTOPILOT WITH PITOT STATIC TESTER AND NAV 401L, OPS CHECK GOOD IAW MM 22-10-00. PLACARDS REMOVED. P/N ON 622-5734-002, S/N ON 451, S/N OFF 3856.

Part: TRANSMITTER — FAILED (NR 5 TANK) · airframe 12,137 hrs · 16,843 cycles

RIGHT FUEL GAUGE DROP 1000 LBS IN 5 MINUTES WHILE IN HOLDING PATTERN FOR MRY. REMOVED AND REPLACED NUMBER FIVE TANK UNIT FUEL TRANSMITTER AND NUMBER SIX IAW MM 28-41-01. P/N ON: 20028-0000-0105, S/N: 458, S/N OFF: 402, P/N ON: 20025-0000-0106, S/N: 844, S/N OFF: 0390.

Part: ACTUATOR — FROZEN (STABILIZER TRIM) · airframe 10,899 hrs · 15,131 cycles

ELEVATOR TRIM WILL NOT MOVE, (FROZEN) AT 26,000 FEET AT 27 DEG, DID NOT FREE UP UNTIL DESCENT TO LOWER WARMER ALTITUDE 5 DEG. REPLACED RIGHT STABILIZER TRIM ACTUATOR WITH SERVICEABLE UNIT. REPLACED LEFT STABILIZER TRIM ACTUATOR WITH SERVICEABLE UNIT. ALL WORK PERFORMED IAW MM 27320 0RT (P/N 5299) (S/N 535) ON, (S/N 695LT) OFF, (P/N 5299) (S/N 731) ON, (S/N 616) OFF.

Part: COMPUTER — FAILED (NR 1 AHRS)

CAPTAINS AHRS COMPUTER FAILED. DIVERTED FROM LAX. REPLACED NR 1 AHRS COMPUTER. OPS CHECK GOOD.

Part: INVERTER — FAILED (NR 2)

NUMBER TWO INVERTER FAILED IN FLIGHT. DIVERTED FROM YUM TO PSP. REMOVED AND REPLACED NUMBER TWO INVERTER, OPS CHECK NORMAL.

Part: SEAL — FAILED (CARGO DOOR)

CARGO DOOR SEAL BLEW OUT IN FLIGHT. RETURNED TO SFO. REPAIRED CARGO DOOR SEAL AT BOTTOM AFT. OPS CHECKS GOOD.

Part: STRAP — CORRODED (CABIN)

CORROSION ON AFT BUTT STRAP BETWEEN FRAME 40 AND 41. REMOVED AFT CENTER BUTT STRAP. REMOVED CORROSION ON BUTT STRAPS BETWEEN FRAME 40 AND 41. SPLICED IN NEW BUTT STRAP, PRIMED AND PAINTED IAW SRM 51-40-00.