N880EA

Part: NONE — INTERMITTENT · airframe 55,842 hrs · 61,490 cycles

DE-ICE PRESS LIGHT ILLUMINATED DE-ICE BOOTS CEASED OPERATION REMOVED AND REPLACED DE-ICE PRESS CAUTION LT. PRESSURE SWITCH. RAN ENGINES OPS CHECKED GOOD

Part: FLOOR SUPPORT — CORRODED (BS 182) · corrosion level 2 · airframe 54,634 hrs · 60,010 cycles

AT STATION X182 AT W/L Z100 ANGLE FLOOR SUPPORT FOUND CORRODED REPLACED ANGLE SRM 51-4205

Part: SKIN — DENTED (BS 201 S20R) · airframe 54,634 hrs · 60,010 cycles

PERMANENT REPAIR FOR DENT RH FUSE 85310016 X182 -X201 STR 20S. REPAIRED RD8-53-16442

Part: STRUCTURE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 54,634 hrs

PASSENGER DOOR SHELL FWD AND AFT SIDE EDGES HAVE CORROSION REPAIRED IAW SRM 51-42-05.

Part: SEAT TRACK — CORRODED (BS 564-597) · corrosion level 2 · airframe 54,634 hrs · 60,010 cycles

CORROSION FOUND OUT OF LIMITS ON LH INBD SEAT TRACK STA 564.5 - 597 REPAIRED RD8-53-1599

Part: FLOORBEAM — CRACKED (CABIN) · airframe 54,634 hrs · 60,010 cycles

STA X255 BELOW SERVICE DOOR LOWER CUT OUT FLOOR BEAM CRACKED REPAIRED SRM 51-42-05

Part: SKIN — DAMAGED (BS 202 S21R) · airframe 54,634 hrs · 60,010 cycles

EXTERNAL FUSELAGE RH SIDE STA X202 STR 21S SKIN NICKED REPAIRED RD8-53-4940

Part: THRESHOLD — CORRODED (EMERGENCY EXIT) · corrosion level 2 · airframe 54,634 hrs · 60,010 cycles

STA X243 FWD EMERGENCY DOOR CUT OUT EDGE X2 CLEETS AND THRESHOLD PLATE CORREODED. REPAIRED SRM 51-42-05

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,634 hrs · 60,010 cycles

RH EXT SKIN EDGE OF Y12 AND X115 RIVET LOOSE REPAIRED WITH RD 8-53-5099

Part: SKIN — DAMAGED (BS 201 S23R) · airframe 54,634 hrs · 60,010 cycles

DAMAGE ON THE RH FUSE FWD OF THE RH EMERGENCY EXIT 1" AVOVE 23 FWD STA X201 REPAIRED RD8-53-17031

Part: THRESHOLD — CORRODED (PAX DOOR) · corrosion level 2 · airframe 54,634 hrs · 60,010 cycles

UNDERFLOOR CABIN PAX DOOR THRESHOLD CORROSION FOUND, REPAIRED SRM 51-42-05

Part: SKIN — DENTED (BS 202 S23R) · airframe 54,634 hrs · 60,010 cycles

R/H FUSELAGE, DENT FOUND ABOVE STR 23S AND FWD OF FR STA X 202.75. REPAIRED BY INSTALLING EXTERNAL PATCH IAW ECO 008.53-21.03

Part: DOOR — GOUGED (EMERGENCY EXIT) · airframe 54,634 hrs · 60,010 cycles

NICK ON R/H EMERGENCY EXIT DOOR TYPE 2, 2.50" FROM FWD EDGE AND 25.00" FROM LOWER EDGE. REPAIRED IAW ECO 008.52-21.01. NO ICA

Part: SKIN — DENTED (RUDDER) · airframe 50,709 hrs · 55,350 cycles

MULTIPLE DENTS ON FORE RUDDER. REPAIRED IAW RD 8-55-3616

Part: SKIN — DENTED (BS 270-312) · airframe 53,760 hrs · 59,185 cycles

LARGE DENT UNDER R/H FUSELAGE ICE SHIELD

Part: SKIN — DENTED (FUSELAGE) · airframe 53,645 hrs · 59,059 cycles

DENT WITH SCRATCHES IN FUSELAGE SKIN 85311825-101 BEYOND MFG. LIMITS 2.0X1.6X0.11 SCRATCHES MAX DEPTH OF 0.01

Part: FIREWALL — DAMAGED (ZONE 400) · airframe 53,307 hrs · 58,608 cycles

#1 ENGINE FIREWALL CHAFED BY FIRE LOOP BRACKET. FIRE LOOP BRACKET MOUNTING HOLES IN FIREWALL ELONGATED.

Part: CONTROL UNIT — INOPERATIVE · airframe 53,027 hrs · 58,202 cycles

ON APPROACH AFTER GEAR WAS DOWN MOMENTARY GEAR WARNING HORN SOUNDED W/GEAR UNSAFE LIGHT (MOMENTARY 1 SEC OR LESS). HAPPENED TWO TIMES.

Part: HYDRAULIC LINE — LEAKING (ZONE 200) · airframe 51,989 hrs · 56,943 cycles

HAZE, POSSIBLE ELECTRICAL SMOKE IN THE CABIN, CAUSED RETURN FROM DEICE TO GATE. TURNED OUT TO BE HYDRAULIC LEAK IN HYDRAULIC LINE.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 51,845 hrs · 56,770 cycles

AFT MOST EMERGENCY LIGHT INOP.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · corrosion level 2 · airframe 50,548 hrs · 55,157 cycles

PAX DOOR SHELL LOWER ATTACHMENT POINTS CORRODED. ATTACHMENT FITTINGS REPAIRED IAW RD 8-52-647.

Part: BRACKET — DAMAGED (PAX DOOR STAIR) · corrosion level 2 · airframe 50,548 hrs · 55,157 cycles

PAX DOOR STAIR LOWER FWD ATTACHMENT BRACKET TO SHELL WAS FOURN CRACKED AND CORRODED. REPLACED THE BRACKET.

Part: SEAT TRACK — CORRODED (BS 182-264) · airframe 50,548 hrs · 55,157 cycles

CORROSION FOUND ON THE RIGHT INBD SEAT TRACK FROM BS 182 - 264. THE CORRIOSION WAS REMOVED, AND FOUND WITHIN LIMITS.

Part: SEAT TRACK — CORRODED (BS 264-377) · airframe 50,548 hrs · 55,157 cycles

CORROSION FOUND ON THE RT INBD SEAT TRACK FROM BS 264 - 377. CORROSION REMOVED AND WITHIN LIMITS.

Part: STEP — CORRODED (PAX DOOR) · corrosion level 2 · airframe 50,548 hrs · 55,157 cycles

AIRSTAIR DOOR STEEP NOSING STEP CORRODED ON STEPS 1,3 & 4. PARTS REPLACED.

Part: FITTING — CORRODED (BS 210) · corrosion level 2 · airframe 50,548 hrs · 55,157 cycles

CORROSION FOUND ON THE TOP OF LAVATORY CASTING AT BS 210, BETWEEN STRINGERS 25 - 27R. THE FITTING WAS REPLACED.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · corrosion level 2 · airframe 50,548 hrs · 55,157 cycles

RIGHT FWD EMERGENCY EXIT DOOR FOUND CORRODED ON THE LOWER FRAME. REPLACED THE FRAME.

Part: HINGE ARM — CORRODED (PAX DOOR) · corrosion level 2 · airframe 50,548 hrs · 55,157 cycles

PAX DOOR HINGE ARMS CORRODED OUT OF LIMITS. BOTH HINGE ARMS REPLACED.

Part: THRESHOLD — CORRODED (PAX DOOR) · corrosion level 2 · airframe 50,548 hrs · 55,157 cycles

CORROSION FOUND ON PAX DOOR THRESHOLD. THE THRESHOLD WAS REPLACED.

Part: BRACKET — CORRODED (PAX DOOR STAIR) · corrosion level 2 · airframe 50,548 hrs · 55,157 cycles

PAX DOOR STAIR, AFT UPPER BRACKET WAS FOUND CORRODED. REPLACED THE BRACKET.

Part: PLATE — CORRODED (AIRSTAIR) · corrosion level 2 · airframe 50,548 hrs · 55,157 cycles

PAX DOOR STRAIRCASE FWD AND AFT BACKING PLATED CORRODED. REPLACED THE PLATE.

Part: INDICATION SYS — ACTIVATED (COCKPIT) · airframe 50,597 hrs · 55,202 cycles

AUTOMATED ENGINE MONITORING SYSTEM HAS REPORTED OVER-TEMPERATURE IN DEPARTURE OUT OF YYC. EXCEEDED 816C FOR 104 SECONDS.

Part: WIRE HARNESS — CHAFED (INDICATOR) · airframe 50,548 hrs · 55,157 cycles

LEFT WING FSL-13 FAILED A FUNCTIONAL CHECK, WS 225 & 243. WIRE FOUND CHAFED IN THE CONDUIT. REPLACED WITH NEW INDICATOR HARNESS IAW AMM.

Part: SKIN — DAMAGED (RT ELEVAOTR) · airframe 50,548 hrs · 55,157 cycles

RT ELEVATOR ASSEMBLY TRAILING EDGE TOP SKIN AT STATIC DISCHARGE ATTACHMENT DAMAGED. REPAIRED IAW RD8-55- 064, D8-55-3182, AND ECO 008.55-18.03.

Part: SEAT TRACK — CORRODED (BS 182-302) · airframe 50,548 hrs · 55,157 cycles

CORROSION FOUND ON LEFT INBOARD SEAT TRACK FROM BS 182 - 302. LEFT INBOARD SEAT TRACK WAS REPLACED IAW RD8-53-3074.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 50,548 hrs · 55,157 cycles

PERMANENT REPAIR FOR MULTIPLE DAMAGES ON FUSELAGE SKIN PANEL P/N 85320106 BETWEEN FUSELAGE STATIONS X202.75 - X370.80 AND STRINGERS 29P - 29S. THE REPAIR CONSISTS OF BLENDING THE DAMAGE TO THE LIMITS SHOWN IN RD8-53-14531, ENSURING THE REPAIR AREA IS CRACK AND DIS-BOND FREE (NONE PERMITTED), LEAVING THE DENT AS IS, INSTALLING PLUG RIVETS AND APPLYING CORROSION INHIBITING COMPOUNDS. ALL WORK IS DONE IN ACCORDANCE WITH RD8-53-14531 ISSUE 3 DATED 02 APRIL 2018 AND ECO 008.53-18.23 DATED 05 APRIL 2018.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 50,548 hrs · 55,157 cycles

PERMANENT REPAIR FOR DAMAGE ON THE LEFT HAND SIDE CENTER FUSELAGE SKIN PANEL(P/N 85320251) LOCATED BETWEEN FUSELAGE STATIONS X291.40 - X354.35 AND STRINGERS 26P - 29P. THE PERMANENT REPAIR CONSISTS OF LEAVING THE DAMAGE SPECIFIED IN RD8-53-15651, INSPECTING REWORK AREA FOR CRACKING AND DIS-BONDING (NO INDICATIONS PERMITTED), FABRICATING AND INSTALLING AN EXTERNAL REPAIR DOUBLER AND RE-PROTECTING REPAIR WITH CORROSION INHIBITING COMPOUNDS. ALL WORK IS DONE IN ACCORDANCE WITH RD8-53-15651 DATED 05 APRIL 2018 AND ECO 008.52-18.26 DATED 05 APRIL 2018.

Part: SKIN — DAMAGED (BS 202.75-222) · airframe 50,548 hrs · 55,157 cycles

FUSELAGE SKIN BS 202.75 - 222, STRINGERS 30P - 31P DAMGED. REPAIRED IAW RD8-53-15633 AND ECO 008.53-18.10.

Part: SKIN — DENTED (BS 291.4-312.25) · airframe 50,548 hrs · 55,157 cycles

CENTER FUSELAGE LOWER SKIN DENTED BETWEEN BS 291.4 - 312.35, STRINGERS 29P - 32P. REPAIRED IAW RD8-53-15632, AND ECO 008.53-18.18.

Part: PANEL — DAMAGED (BS 123-136.8) · airframe 50,548 hrs · 55,157 cycles

SKIN BETWEEN BS 123 - 136.8, STRINGERS 30P - 32P DAMAGED. REPAIRED IAW RD8-53-15627, AND ECO 008.53-18.17.

Part: SKIN — CORRODED (BS 136-151) · airframe 50,548 hrs · 55,157 cycles

SKIN CORRODED BETWEEN BS 136.8 - 151.6, STRINGERS 29P - 31S, REPAIRED IAW RD8-53-15630, AND ECO 008.53-18.16.

Part: SKIN — DAMAGED (BS 136-151) · airframe 50,548 hrs · 55,157 cycles

FUSELAGE SKIN PANEL DAMAGED BETWEEN BS 136.80 - 151.60, STRINGERS 31S - 32S. REPAIRED IAW RD8-53-15610, AND ECO 008.53-18.11.

Part: SKIN — SCRATCHED (BS 424-488) · airframe 50,548 hrs · 55,157 cycles

BOTTOM FUSELAGE SKIN PANEL SCRATCHED BETWEEN BS 424.124 - 488.50, STRINGERS 30P - 29S. REPAIRED IAW RD8-53-15623, AND ECO 008.53-18.14.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 50,548 hrs · 55,157 cycles

DENT AND CREASE DAMAGE TO THE RIGHT HAND FUSELAGE SKIN PANEL ASSEMBLY BETWEEN STATION X405.735 TO X424.124 AND STRINGERS 21S TO 22S. RD CALLS FOR A PERMANENT REPAIR FOR THE DENT AND CREASE DAMAGE TO RIGHT SKIN PANEL ASSEMBLY (PART NUMBER 85320266) BETWEEN X405.735 TO X424.124 AND STRINGERS 21S TO 22S. THE REPAIR CONSISTS OF REMOVING THE DAMAGE AS STATED IN RD 8-53-15588, WHICH SUPERSEDES RD 8-53-12158, INSPECTING THE REWORK AREA FOR CRACK AND DIS-BOND INDICATIONS(NONE PERMITTED), FABRICATING AND INSTALLING THE REPAIR PARTS, AND RE-PROTECTING THE REPAIR AREA BY APPLYING CORROSION INHIBITING COMPOUNDS. ALL WORK DONE IN ACCORDANCE WITH RD 8-53-15588 ISSUE 1 DATED 17 MARCH 2018 AND ECO 008.53-18.09 DATED 19 MARCH 2018. ALSO RD 8-53-15588 ISSUE 1 DATED 17 MARCH 2018 SUPERSEDES RD 8-53-12158 ISSUE 2 DATED 17 MARCH 2018.

Part: SKIN — NICKED (EMERGENCY EXIT) · airframe 50,548 hrs · 55,157 cycles

NICK DAMAGE ON THE RIGHT TYPE-III EMERGENCY EXIT SKIN FORWARD OF BS 366.05 AND BETWEEN THE WINDOW AND THE LOWER BEAM. BLENDED THE DAMAGE IAW RD8-52-1577, ISSUE 1, AND ECO 008.52-18.06.

Part: SKIN PANEL — CRACKED (VERTICAL STAB) · airframe 50,548 hrs · 55,157 cycles

CRACK AND CREASE DAMAGE TO THE VERTICAL STABILIZER LOWER FORWARD LT SKIN BETWEEN STRINGERS 20 - 22L AND BETWEEN THE FRONT SPAR AND FRAME 5. REPAIRED THE VERTICAL STABILIZER LOWER FORWARD LEFT SIDE SKIN IAW RD 8-55-3155, REVISION 1, AND ECO 008.55-18.03.

Part: SKIN — DENTED (BS 270-291) · airframe 50,548 hrs · 55,157 cycles

THREE DENTS IN THE LEFT FUSELAGE SKIN BETWEEN BS 270.5 - 291.4, STRINGERS 8P - 11P. REPAIRED THE SKIIN IAW RD8-53-13551 REVISION 4 AND EC0 008.53-18.08.

Part: SENSOR — SMOKE (COCKPIT TEMP) · airframe 48,541 hrs · 52,441 cycles

SMOKE IN COCKPIT COMING FROM COCKPIT TEMP SENSOR.

Part: HYDRAULIC LINE — LEAKING (NLG) · airframe 47,969 hrs · 51,775 cycles

NR 2 HYD ISO VLV CAUTION LIGHT ILLUMINATED IN FLIGHT. FOUND NLG GEAR UP LINE TO NOSE GEAR DOORS LEAKING. INSTALLED TEMP HOSE ASSY

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 47,862 hrs · 51,661 cycles

RIGHT EXIT & OVERHEAD EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY IN EMERGENCY LIGHT POWER SUPPLY 3351 PS2 & ALL EMERGENCY LIGHTS OPS CHECKED OK

Part: ACM — LEAKING (AC BAY) · airframe 46,490 hrs · 50,081 cycles

BURNING SMELL & SMOKING HAZE SEEN COMING FROM GASPER WITH HEAT IN MANUAL AT FULL HOT. STOPPED WHEN HEAT WAS TURNED OFF. R & R ACM DUE TO LEAKING OIL INTERNALLY. OPERATIONS CHECKED CABIN HEAT SYS IAW MM 21-60-01. CHECKS GOOD, OK FOR SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 46,014 hrs · 49,548 cycles

MULTIPLE DENTS & BLENDS ON BELLY SKIN BEYOND MANUFACTURES LIMITS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,014 hrs · 49,548 cycles

LEFT INBD SEAT TRACK IN CARGO AREA CORRODED BEYOND LIMITS.

Part: SCOOP — ABNORMAL (RAM AIR) · airframe 46,014 hrs · 49,548 cycles

RAM AIR SCOOP HAS A HOLE IN IT.

Part: STRUCTURE — DAMAGED · airframe 46,014 hrs · 49,548 cycles

TWO DENTS & SCRATCHES BEYOND MFG SRM LIMITS.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 46,014 hrs · 49,548 cycles

PASSENGER DOOR THRESHOLD CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,014 hrs · 49,548 cycles

LEFT INBD FWD SEAT TRACK CORRODED BEYOND LIMITS.

Part: SMOKE DETECTOR — FALSE ACTIVATION (ZONE 200) · airframe 45,761 hrs · 49,308 cycles

SMOKE WARNING LIGHT ILLUMINATED IN FLIGHT. R & R NR 1 OVERHEAD SMOKE DETECTOR.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 45,292 hrs · 48,870 cycles

CREASE & DENT DAMAGE X167.0, -X182.0 & STRINGER 30S - 32S.

Part: EEC — DEFECTIVE (NR 1 ENGINE) · airframe 44,291 hrs · 47,815 cycles

NR 1 ENGINE SHUTDOWN. TORQUE FLUCTUATIONS +/- 20% WITH NR 1 ENGINE MANUAL CAUTION LIGHT GOING ON AND OFF. NR 1 ENGINE EEC REMOVED AND REPLACED, GROUND RUN OPS CHECKED GOOD IAW PSM 1-8-2ER TABLE 5-1

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 43,338 hrs · 46,723 cycles

SMOKE LIGHT FLICKERED IN FLIGHT. R & R CARGO COMPARTMENT NR 2 SMOKE DETECTOR MOUNTED ON LT BULKHEAD IAW DHC-8 MM 26-12-01. OPERATIONS CHECKED GOOD. OK FOR SERVICE.

Part: GENERATOR — FAILED (NR 2 AC) · airframe 43,132 hrs · 46,505 cycles

RIGHT AC BUSS FAILED IN FLIGHT. R & R NR 2 AC GENERATOR IAW MM 24-21-01 AND OPS CHECKED GOOD.

Part: GCU — DEFECTIVE (RT AC) · airframe 43,121 hrs · 46,496 cycles

RT AC BUSS CAUTION LIGHT AND ASSOCIATED CAUTION LIGHTS ILLUMINATED WHEN SELECTING PROP HEAT. R & R RT GCU IAW AMM 24-21-00. GROUND RUN AND SYSTEM CHECK SATISFACTORY.

Part: PIN — BACKED OUT (CONNECTOR) · airframe 41,914 hrs · 45,265 cycles

SMOKE WARNING LIGHT INTERMITTENT. FOUND PIN 9 ON CONTROL AMPLIFIER CONNECTOR 2612-P1 RECESSED. REINSERTED PIN IN CONNECTOR & GND TESTED GOOD IAW -8 MM 26-12-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,903 hrs · 45,252 cycles

EMERGENCY EXIT LIGHT ABOVE AIR STAIR INOPERATIVE. R & R ALL EMERGENCY BATTERY PACKS IAW DHC-8 MM 33-51-00. OPERATIONS CHECKED GOOD, OK FOR SERVICE.

Part: SMOKE DETECTOR — INTERMITTENT (CARGO BAY) · airframe 41,872 hrs · 45,215 cycles

MOMENTARY SMOKE WARNING LIGHT, 3 - 4 FLASHES PER WARNING. FLIGHT ATTENDANT VERIFY NO SMOKE OR SMELL NOTED IN BAG COMPARTMENT. R & R NR 2 CARGO SMOKE DETECTOR IAW PSM 1-8-2 CH 26-12-00 & OPERATIONS CHECKED GOOD.

Part: WIRE HARNESS — CHAFED (SMOKE DETECTOR) · airframe 41,678 hrs · 44,995 cycles

SMOKE CAUTION LIGHT ILLUMINATED. REPAIRED CHAFFED WIRES AT NR 2 SMOKE DETECTOR & OPERATIONS CHECKED GOOD.