N113DQ

Part: ENGINE — ODOR (RIGHT) · airframe 15,261 hrs · 7,045 cycles

DIV TO DTW DUE TO DIRTY SOCK SMELL ON TAKEOFF THAT DISSIPATED. CORRECTIVE ACTION: T/S PER WORKCARDS FOUND SOURCE OF ODOR COMING FROM RIGHT ENGINE. C/W AMDS WC 0550-6001 AND 0550-2003. ODOR DOES NOT PERSIST. (LP# 7675577, 1288692)

Part: REU — FAULTED (RUDDER) · airframe 14,274 hrs · 6,591 cycles

SHIP 8113 - MISC - DECLARED EMERGENCY DUE TO "RUDDER FAIL" WARNING MESSAGE ON FINAL. CORRECTIVE ACTION: REPLACED AFT REU-1 AND CLEARED THE LATCHED MESSAGES. (LP# 6754140)

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,782 hrs · 6,382 cycles

***CORROSION*** ON FWD CARGO COMPARTMENT DOOR LOWER SILL FASTENER HOLES, BETWEEN FR-24 AND FR-29. WORK ACCOMPLISHED ON ER/A 625727-14 REV-ORIGINAL SECTION 1-2-3. (LP# 0936112)

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 13,782 hrs · 6,382 cycles

L2 DOOR EMERGENCY OPENING ASSIST MEANS PRESSURE LOW (RED RANGE). SERVICED L2 EMERGENCY DOOR OPENING ASSIST IAW A220 AMP BD500- A-J52-12-08-01AAA-214B-A. (LP# 0936752)

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,782 hrs · 6,382 cycles

***CORROSION*** FWD CARGO DOOR CUTOUT, UNDER SCUFF PLATES, AT HOLES 80U AND 20OL (MARKED). WORK ACCOMPLISHED ON ER/A 625727-14 REV-ORIGINAL. SECTION 1-2-3 ASSOCIATED ER/A 14-625727 ADDED FOR AC 8113. (LP# 0936219)

Part: SKIN — DAMAGED · airframe 13,782 hrs · 6,382 cycles

WHILE ACCESSING FOR CUSTOMER CARD 4430-01020-01D VIASAT MOD INSTALL FOUND 4 EXTRA FASTENER HOLES AND 1 EXTRA CUT OUT. REPAIRED EXTRA FASTENER HOLES AND CUT OUT AT VIASAT MOD AREA PER ER/A 625610-14 REV ORIGINAL. REFERENCE LOGPAGE 0930834 FOR REPAIR SERVICE LIMIT. (LP# 0933642)

Part: SKIN — NOT REPORTED (ZONE 200) · airframe 13,826 hrs · 6,399 cycles

DTE / MONITOR INSPECTION LOG REF. ER/A 625610-14; A220-100 / FUSELAGE / SKIN, CROWN, REAR / BTW STR 1R & STR 4R / BTW FR62 & FR68 / WIFI VIASAT INSTL / PLUGGED HOLES. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. REPAIR APPROVAL IS LIMITED TO 12 MONTHS FROM REPAIR ISSUE DATE OF 22APR25. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEER: DAMAGE TOLERANCE EVALUATION IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA AC 120-93. ASSOCIATED ER/A 14-625610 ADDED FOR AC 8113. (LP# 0930834)

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,782 hrs · 6,381 cycles

WHILE ACCOMPLISHING DVI OF DOUBLER EDGE AROUND WASTE BOX CUT-OUT , FOUND CORROSION ON AFT INBOARD CORNER. (REF CC# 171-0784323) . REMOVED AND REPLACED WASTE BOX CUT-OUT DOUBLER. IAW BOMBARDIER DWG C01342100 REV-T AND A220 ASRP BD500-A-J51-42-21-00AAA-078A-A. (LP# 0925285)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,782 hrs · 6,381 cycles

CORRODED SEAT TRACK AT FR 53 RBL 23 WL 147 HAS MULTIPLE SPOTS. REMOVED AND REPLACED SEAT TRACK RBL 23, FR 51 TO FR 61 WL 147 IAW A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND ASRP BD500- A-J51-40-00-01AAA-652A-A & DWG: C01335810 REV C. (LP# 0921110)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,782 hrs · 6,381 cycles

CORRODED SEAT TRACK BETWEEN FR 68+69 RBL 44 WL 147. REMOVED AND REPLACED SEAT TRACK BETWEEN FR61 TO FR 74 RBL 44 WL 147 IAW A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND DWG BOMBARDIER PL C01342724 REV-C. (LP# 0920334)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,782 hrs · 6,381 cycles

CORRODED SEAT TRACK BETWEEN FR 55+56 LBL 23 WL 147. REMOVED AND INSTALLED NEW SEAT TRACK P/N C01335891 PO 1029740 ON FR 51 TO FR 61 LBL 23 WL 147 PER A220 ASRP BD500-A-J51-42-21- 00AAA-078A-A AND DWG PL C01335810 REV-C, PL C01334800 REV-K AND PL C01303000 REV-G. (LP# 0919670)

Part: SEAT SPRING — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,782 hrs · 6,381 cycles

SEAT TRACK AT FR 74 LBL 23 WL 147 CORRODED. REMOVED AND REPLACED SEAT TRACK LBL23 FR61 TO FR 75 IAW A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND DWG BOMBARDIER C0134270 REV E. (LP# 0904709)

Part: SEAT SPRING — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,782 hrs · 6,381 cycles

SEAT TRACK BETWEEN FR 65+67 RBL 23 WL 147 CORRODED. REMOVED SEAT TRACK DAMAGED AND INSTALLED NEW SEAT TRACK BTW FR 61-74 RBL 23 WL 147 PER A220 ASRP BD500-A-J51-42-20-00AAA- 078A-A AND BOMBARDIER PL C01342701 REV E. (LP# 0902721)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,782 hrs · 6,381 cycles

SEAT TRACK BETWEEN FR 69+70 RBL 23 WL 147 CORRODED. CORROSION REMOVAL FOUND TO BE OUT OF LIMITS, SEAT TRACK REPLACED FROM FR 61-74 RBL 23 WL 147 ON CUSTOMER CARD 00153. (LP# 0902710)

Part: SEAT SPRING — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,782 hrs · 6,381 cycles

SEAT TRACK AT FR 71 RBL 23 WL 147 UNDER FITTING. CORROSION REMOVAL FOUND TO BE OUT OF LIMITS, SEAT TRACK REPLACED FROM FR 61-74 RBL 23 WL 147 ON CUSTOMER CARD 00153. (LP# 0902712)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,782 hrs · 6,381 cycles

SEAT TRACK BETWEEN FR 72+74 RBL 23 WL 147 CORRODED. CORROSION REMOVAL FOUND TO BE OUT OF LIMITS, SEAT TRACK REPLACED FROM FR 61-74 RBL 23 WL 147 ON CUSTOMER CARD 00153. (LP# 0902707)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,782 hrs · 6,381 cycles

***CORROSION*** SEAT TRACK FROM FR 72+74 LBL 44 WL 147 . REMOVED AND REPLACED SEAT TRACK FROM FR 61-4" TO FR 74+5 LBL WL 14 7 IAW DWG BOMBARDIER PL C01342701 REV E AND A220 ASRP BD500-A-J 51-42-20-00AAA-078A-A. UPDATING CORROSION LEVEL 2; CORROSION LEVEL CHANGED FROM: 1 TO: 2. (LP# 0882613)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,782 hrs · 6,381 cycles

***CORROSION*** SEAT TRACK AT FR 20 RBL 23 IS CORRODED . REPLACED SEAT TRACK RBL23 FR 20 TO FR 30 IAW A220 ASRP BD500- A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG:C02312600 REV E, DWG :C01735610 REV B, DWG:C01712000 REV A. (LP# 0876752)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,782 hrs · 6,381 cycles

***CORROSION*** SEAT TRACK BETWEEN FR 54+55 RBL 44 WL 147 . REMOVED AND REPLACED SEAT TRACK AT STA FR 57+6 TO FR 52 RBL 44 WL 147 PER BOMBARDIER DWG C01303000 REV: G. CORRECTION LINE 03: REV: G AND A220 ASRP 500A-A-J51-42-21-00AAA-078A-A. (LP# 0870065)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,782 hrs · 6,381 cycles

SEAT TRACK FR20 RBL44 WL 147 HAS CORROSION. UPON EVALUATED DAMAGED ON SEAT TRACK AT FR=20, RBL=44, WL= 147 AS FOLLOW: TOP CROWN ORIGINAL THICK= 0.145", REMAINING THICK= 0.073" MATERIAL LOSS= 0.072" BOTTOM CROWN ORIGINAL THICK= 0.180" REMAINING THICK 0.152" THEREFORE IT'S OUT LIMITS IAW A220 ASRP BD500-A-J53-21-44-00AAA-661A-A, REMOVED AND REPLACED SEAT TRACK FROM RBL=44 BTW FR=20 TO FR=30+9 IAW BOMBARDIER DWG# C02312600 REV:E AND C01712000 REV-A. (LP# 0859322)

Part: SLAT TRACK — CORRODED (ZONE 500) · airframe 12,540 hrs · 5,803 cycles

LH SLAT TRACK NBR 5 UPPER SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01028-02A. PERFORMED EDDY CURRENT INSPECTION PER ANDTP 51-01-20-01AAA- 353A-A. NO DEFECTS NOTED.

Part: SLAT TRACK — CORRODED (ZONE 500) · airframe 12,540 hrs · 5,803 cycles

LH SLAT TRACK NBR 10 LWR INB FWD SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01028-02A. PERFORMED EDDY CURRENT INSPECTION IAW ANDTP51-01-20-01AAA-353A-A .

Part: SIGN — MISSING (FWD GALLEY) · airframe 11,569 hrs · 5,384 cycles

FWD GALLEY EMERGENCY EXIT SIGN MISSING. REPLACED MISSING EMERGENCY EXIT SIGN PER A220 AMP 33-52. OPS CK GOOD. A/C OK FOR SERVICE. (LP# 5798708)

Part: LINE — DAMAGED (FUEL SYSTEM) · airframe 11,445 hrs · 5,324 cycles

LH WING FUEL TANK, PER AMDS 2820-01281-07A STEPS 5 FOUND ITEM C TUBE PER#C01633381-001 HAS A SCRATCH WITHIN 0.050 NEAR COUPLING OUT OF LIMITS LOG-PAGE UPDATED @ 06APR24 1334 UTC 02 CORR BY RAMDAN 01738681 IAH 06APR24 ATA 2821 RII: N ENTR 01738681 W REPLACED FUEL TUBE PN C01633381-001 PER AMDS 2820-01281-07A & A220 0500-A-J28-21-80-07AAA-720A-A CDCCL COMPLIED WITH. ASSOCIATED AA 2820-01281 ADDED FOR AC 8113. (LP# 0280376)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

RH SLAT TRACK #3 UPPER FWD HAS EVIDENCE OF CORROSION AND HAS NO EVIDENCE OF PREVIOUS REWORK. REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FLIGHT. REPAIRED R/H SLAT TRACK NBR 3 UPPER FWD SURFACE PER ERA 607872- 14AD REV C + PRI REV 0 & 1. (LP# 0135768)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

RH SLAT TRACK #7 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND NO EVIDENCE OF REWORK. REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FLIGHT. REPAIRED R/H SLAT TRACK NBR 7 UPPER FWD SURFACE PER ERA 607872- 14AD REV C + PRI REV 0 & 1. (LP# 0135807)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

RH SLAT TRACK #5 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND NO EVIDENCE OF REWORK. REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FLIGHT. REPAIRED R/H SLAT TRACK NBR 5 UPPER FORWARD SURFACE PER ERA 607872-14AD REV C + PRI REV 0 & 1. (LP# 0135799)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

RH SLAT TRACK #9 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND EVIDENCE OF PREVIOUS REWORK. REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FLIGHT. REPAIRED R/H SLAT TRACK NBR 9 UPPER FORWARD SURFACE PER ERA 607872-14AD REV C + PRI REV 0 & 1. (LP# 0135814)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

RH SLAT TRACK #1 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND HAS EVIDENCE OF PREVIOUS REWORK. REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FLIGHT. REPAIRED R/H SLAT TRACK NBR 1 LOWER AFT SURFACE PER ERA 607872- 14AD REV C + PRI REV 0 & 1. (LP# 0135751)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

RH SLAT TRACK #10 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND HAS EVIDENCE OF PREVIOUS REWORK. REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FLIGHT.REPAIRED R/H SLAT TRACK NBR 10 UPPER AFT SURFACE PER ERA 607872- 14AD REV C + PRI REV 0 & 1. (LP# 0135817)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

RH SLAT TRACK #8 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND EVIDENCE OF PREVIOUS REWORK. REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FLIGHT. REPAIRED R/H SLAT TRACK NBR 8 LOWER AFT SURFACE PER ERA 607872- 14AD REV C + PRI REV 0 & 1. (LP# 0135810)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

L/H SLAT TRACK NBR 8 LOWER SURFACE FWD HAS EVIDENCE OF CORROSION + HAS EVIDENCE OF PREVIOUS REWORK REF AA5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQD. BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 8 LOWER SURFACE FWD PER ER/A 607871- 14AD REV C + PRI REV 0 + 1. (LP# 0134796)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

L/H SLAT TRACK NBR 1 LOWER SURFACE FWD HAS EVIDENCE OF CORROSION + NO EVIDENCE OF PREVIOUS REWORK REF AA5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQD. BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 1 LOWER SURFACE FWD PER ER/A 607871- 14AD REV C + PRI REV 0 + 1. (LP# 0134764)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

L/H SLAT TRACK NBR 1 UPPER SURFACE FWD HAS EVIDENCE OF CORROSION + HAS NO EVIDENCE OF PREVIOUS REWORK REF AA5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQD. BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 1 UPPER SURFACE FWD PER ER/A 607871- 14AD REV C + PRI REV 0 + 1. (LP# 0134742)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

RH SLAT TRACK #5 LOWER AFT HAS EVIDENCE OF CORROSION AND EVIDENCE OF PREVIOUS REWORK. REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FLIGHT. REPAIRED R/H SLAT TRACK NBR 5 LOWER AFT SURFACE PER ERA 607872- 14AD REV C + PRI REV 0 & 1. (LP# 0135792)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

L/H SLAT TRACK NBR 5 LOWER SURFACE FWD HAS EVIDENCE OF CORROSION AT 2 LOCATIONS + NO EVIDENCE OF PREVIOUS REWORK REF AA5742- 01028-02A LIASON ENGINEERING SUPPORT WILL BE REQD. BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 5 LOWER SURFACE FWD PER ER/A 607871- 14AD REV C + PRI REV 0 + 1. (LP# 0134793)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

L/H SLAT TRACK NBR 8 UPPER SURFACE FWD HAS EVIDENCE OF CORROSION + HAS NO EVIDENCE OF PREVIOUS REWORK REF AA5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQD. BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 8 UPPER SURFACE FWD PER ER/A 607871- 14AD REV C + PRI REV 0 + 1. (LP# 0134762)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

L/H SLAT TRACK NBR 5 UPPER SURFACE AFT HAS EVIDENCE OF CORROSION + HAS EVIDENCE OF PREVIOUS REWORK REF AA5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQD. BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 5 UPPER SURFACE AFT PER ER/A 607871- 14AD REV C + PRI REV 0 + 1. (LP# 0134759)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

RH SLAT TRACK #8 LOWER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND EVIDENCE OF PREVIOUS REWORK. REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FLIGHT. REPAIRED R/H SLAT TRACK NBR 8 LOWER FORWARD SURFACE PER ERA 607872-14AD REV C + PRI REV 0 & 1. (LP# 0135812)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

RH SLAT TRACK # 4 LOWER AFT HAS EVIDENCE OF CORROSION AND HAS EVIDENCE OF PREVIOUS REWORK. REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FLIGHT. REPAIRED R/H SLAT TRACK NBR 4 LOWER AFT SURFACE PER ERA 607872- 14AD REV C + PRI REV 0 & 1. (LP# 0135771)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

L/H SLAT TRACK NBR 2 LOWER SURFACE FWD HAS EVIDENCE OF CORROSION + NO EVIDENCE OF PREVIOUS REWORK REF AA5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQD. BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 2 LOWER SURFACE FWD PER ER/A 607871- 14AD REV C + PRI REV 0 + 1. (LP# 0134769)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

L/H SLAT TRACK NBR 3 UPPER SURFACE FWD HAS EVIDENCE OF CORROSION + HAS NO EVIDENCE OF PREVIOUS REWORK REF AA5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQD. BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 3 UPPER SURFACE FWD PER ER/A 607871- 14AD REV C + PRI REV 0 + 1. (LP# 0134757)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

RH SLAT TRACK #8 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND EVIDENCE OF REWORK. REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FLIGHT. REPAIRED R/H SLAT TRACK NBR 8 UPPER AFT SURFACE PER ERA 607872- 14AD REV C + PRI REV 0 & 1. (LP# 0135809)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

RH SLAT TRACK #7 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND HAS EVIDENCE OF REWORK. REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FLIGHT. REPAIRED R/H SLAT TRACK NBR 7 UPPER AFT SURFACE PER ERA 607872- 14AD REV C + PRI REV 0 & 1. (LP# 0135804)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

RH SLAT TRACK #3 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND HAS EVIDENCE OF PREVIOUS REWORK. REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FLIGHT. REPAIRED R/H SLAT TRACK NBR 3 LOWER AFT SURFACE PER ERA 607872- 14AD REV C + PRI REV 0 & 1. (LP# 0135765)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

RH SLAT TRACK #5 LOWER FORWARD HAS EVIDENCE OF CORROSION AND HAS EVIDENCE OF PREVIOUS REWORK. REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FLIGHT. REPAIRED R/H SLAT TRACK NBR 5 LOWER FORWARD SURFACE PER ERA 607872-14AD REV C + PRI REV 0 & 1. (LP# 0135777)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

L/H SLAT TRACK NBR 10 LOWER SURFACE FWD HAS EVIDENCE OF CORROSION + NO EVIDENCE OF PREVIOUS REWORK REF AA5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQD. BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 10 LOWER SURFACE FWD PER ER/A 607871 -14AD REV C + PRI REV 0 + 1. (LP# 0134799)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

L/H SLAT TRACK NBR 3 LOWER SURFACE FWD HAS EVIDENCE OF CORROSION + NO EVIDENCE OF PREVIOUS REWORK REF AA5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQD. BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 3 LOWER SURFACE FWD PER ER/A 607871- 14AD REV C + PRI REV 0 + 1. (LP# 0134787)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

L/H SLAT TRACK NBR 4 LOWER SURFACE FWD HAS EVIDENCE OF CORROSION + NO EVIDENCE OF PREVIOUS REWORK REF AA5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQD. BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 4 LOWER SURFACE FWD PER ER/A 607871- 14AD REV C + PRI REV 0 + 1. (LP# 0134790)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

L/H SLAT TRACK NBR 2 UPPER SURFACE FWD HAS EVIDENCE OF CORROSION + HAS NO EVIDENCE OF PREVIOUS REWORK REF AA5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQD. BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 2 UPPER SURFACE FWD PER ER/A 607871- 14AD REV C + PRI REV 0 + 1. (LP# 0134745)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

RH SLAT TRACK #2 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND HAS EVIDENCE OF PREVIOUS REWORK. REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FLIGHT. REPAIRED R/H SLAT TRACK NBR 2 LOWER AFT SURFACE PER ERA 607872- 14AD REV C + PRI REV 0 & 1. (LP# 0135760)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,747 hrs · 5,017 cycles

RH SLAT TRACK #6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND NO EVIDENCE OF PREVIOUS REWORK. REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FLIGHT. REPAIRED R/H SLAT TRACK NBR 6 UPPER AFT SURFACE PER ERA 607872- 14AD REV C + PRI REV 0 & 1. (LP# 0135802)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 9,488 hrs · 4,472 cycles

SHIP 8113 - DIV - TO PIT DUE TO RUBBER SMELL WITH CABIN LIGHTS FLICKERING. CORRECTIVE ACTION: ACCOMPLISHED SMOKE AND FUME WORKCARDS, REPLACED CABIN MANAGEMENT SYSTEM ZONE BOX 1. R/R BOTH RECIRCULATION FILTERS. (LP# 4484997)

Part: PROTECTOR — ERODED (ZONE 300) · airframe 13,782 hrs · 6,381 cycles

RT HORIZONTAL STABILIZER TIP EROSION PROTECTOR MATERIAL MISSING. REPETITIVE INSPECTION REQUIRED EVERY 150 FH. REPAIR REQUIRED WITHIN 8500 FH. REFER TO A220 ASRP 55-12-86-01AAA-662A-A. PAIN REPAIR REQUIRED PRIOR TO EROSION TAPE APPLICATION. REFER TO IRREG LOG 4484986 FOR PAINT MON LOG. (LP# 4484985 )

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 9,205 hrs · 4,333 cycles

PER AMDS 5742-01028-02B. RH WING SLAT TRACK #4 HAS CORROSION ON UPPER FORWARD SURFACE. THIS HAS BEEN PREVIOUSLY REWORKED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 005-0001:5742-01028-02B/004 00011 REPAIRED TRACK PER AMDS 5742-01028-02B AND ER/A 607872-14AD REV A AND PRI 607872-14B REV 0. (LP# 2859008)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 9,205 hrs · 4,333 cycles

PER AMDS 5742-01028-02A. LH WING SLAT TRACK #5 HAS CORROSION ON LOWER AFT AND FORWARD SURFACE, AND UPPER AFT SURFACE. THIS HAS BEEN PREVIOUSLY REWORKED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 006-0001:5742-01028-02A/001 00004 REPAIRED TRACK PER AMDS 5742-01028-02B AND ER/A 607871-14AD REV. A AND PRI607871-14AD REV A. (LP# 2858692)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 9,205 hrs · 4,333 cycles

PER AMDS 5742-01028-02A. LH WING SLAT TRACK #11 HAS CORROSION ON UPPER AFT SURFACE. NO PREVIOUS REWORK NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 006-0001:5742-01028-02A/004 00007 REPAIRED TRACK PER AMDS 5742-01028-02A AND ER/A 607871-14AD REV A AND PRI 607871-14AD REV 0. (LP# 2858712)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 9,205 hrs · 4,333 cycles

PER AMDS 5742-01028-02B. RH WING SLAT TRACK #2 HAS CORROSION ON LOWER AFT SURFACE. THIS HAS BEEN PREVIOUSLY REWORKED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 005-0001:5742-01028-02B/002 00009 REPAIRED TRACK PER AMDS 5742-01028-02B AND ER/A 607872-14AD REV A AND PRI 607872-14B REV 0. (LP# 2859000)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 9,205 hrs · 4,333 cycles

PER AMDS 5742-01028-02B. RH WING SLAT TRACK #6 HAS CORROSION ON LOWER FORWARD SURFACE. THIS HAS BEEN PREVIOUSLY REWORKED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 005-0001:5742-01028-02B/006 00013 REPAIRED TRACK PER AMDS 5742-01028-02B AND ER/A 607872-14AD REV A AND PRI 607872-14B REV 0. (LP# 2859013)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 9,205 hrs · 4,333 cycles

PER AMDS 5742-01028-02B. RH WING SLAT TRACK #11 HAS DAMAGE ON LOWER AFT SURFACE. THIS HAS BEEN PREVIOUSLY REWORKED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 005-0001:5742-01028-02B/007 00014 REPAIRED TRACK PER AMDS 5742-01028-02B AND ER/A 607872-14AD REV A AND PRI 607872-14B REV 0. (LP# 2859016)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 9,205 hrs · 4,333 cycles

PER AMDS 5742-01028-02B. RH WING SLAT TRACK #1 HAS CORROSION AND DAMAGE ON LOWER AFT SURFACE. NO PREVIOUS REWORK NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 005-0001:5742-01028-02B/001 00008 REPAIRED TRACK PER AMDS 5742-01028-02B AND ER/A 607872-14AD REV A AND PRI 607872-14B REV 0. (LP# 2858998)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 9,205 hrs · 4,333 cycles

PER AMDS 5742-01028-02A. LH WING SLAT TRACK #8 HAS CORROSION ON LOWER FORWARD SURFACE, AND UPPER AFT SURFACE. THIS HAS BEEN PREVIOUSLY REWORKED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 006-0001:5742-01028-02A/003 00006 REPAIRED TRACK PER AMDS 5742-01028-02A AND ER/A 607871-14AD REV A AND PRI 607871-14AD REV 0. (LP# 2858708)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 9,205 hrs · 4,333 cycles

PER AMDS 5742-01028-02B. RH WING SLAT TRACK #8 HAS CORROSION ON LOWER AFT SURFACE. HAS PREVIOUS REWORK. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 005-0001:5742-01028-02B/008 00017 REPAIRED TRACK PER AMDS 5742-01028-02B AND ER/A 607872-14AD REV A AND PRI 607872-14B REV 0. (LP# 2859021)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 9,205 hrs · 4,333 cycles

PER AMDS 5742-01028-02B. RH WING SLAT TRACK #3 HAS DAMAGE ON LOWER AFT SURFACE. NO PREVIOUS REWORK NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 005-0001:5742-01028-02B/003 00010 REPAIRED TRACK PER AMDS 5742-01028-02B AND ER/A 607872-14AD REV A AND PRI 607872-14B REV 0. (LP# 2859006)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 9,205 hrs · 4,333 cycles

PER AMDS 5742-01028-02A. LH WING SLAT TRACK #6 HAS CORROSION ON UPPER AFT SURFACE. THIS HAS BEEN PREVIOUSLY REWORKED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 006-0001:5742-01028-02A/002 00005 REPAIRED TRACK PER AMDS 5742-01028-02A AND ER/A 607871-14AD REV A AND PRI 607871-14AD REV 0. (LP# 2858702)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 9,205 hrs · 4,333 cycles

PER AMDS 5742-01028-02B. RH WING SLAT TRACK #5 HAS CORROSION ON LOWER AFT AND LOWER FORWARD SURFACE. THIS HAS BEEN PREVIOUSLY REWORKED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 005-0001:5742-01028-02B/005 00012 REPAIRED TRACK PER AMDS 5742-01028-02B AND ER/A 607872-14AD REV A AND PRI 607872-14B REV 0. (LP# 2859011)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 8,706 hrs · 4,109 cycles

ERA607872-14AD SECTION I ISSUED FOR CORROSION TO RH WING SLAT TRACKS. FOLLOW ON ACTION REQUIRED. ACCOMPLISHED ERA 607872-14AD REV O SECTION I, R/H SLAT TRACK CORROSION BLENDING (TIME LIMITED REPAIR) RII STEP 3 WAS ACCOMPLISHED ON LOG 2714772 N/R 23. (LP# 2713652)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 8,706 hrs · 4,109 cycles

ERA607871-14AD SECTION I ISSUED FOR CORROSION AND WEAR TO L WING SLAT TRACKS 1-10. FOLLOW ON ACTION REQUIRED. ACCOMPLISHED ERA 60781-14AD REV O SECTION I, L/H SLAT TRACK CORROSION BLENDING (TIME LIMITED REPAIR) RII STEP 3 WAS ACCOMPLISHED ON LOG 2714780 N/R 22. (LP#2713584)

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 7,708 hrs · 3,649 cycles

LAVATORY SMOKE MASTER WARNING DURING CRUISE. WARNING LASTED ONE MINUTE. F/A CONFRIMED AFT LAV AC RIGHT FIRE WARNING. NO SMOKE VISABLE AND NO SMOKE ODOR AFTER INSPECTING LAV. WARNING WENT AWAY ON ITS OWN. FOUND BOTH AFT LAV SMOKE DETECTORS FAILED, NOT TESTING. PULLED & RESET AFT LAV SMOKE DETECTORS CIRCUIT BREAKERS. ALL LAV SMOKE DETECTORS OPS TESTED GOOD IAW AMP 26-16-01. A/C OK FOR SERVICE.

Part: DOOR — DENTED · airframe 6,171 hrs · 2,911 cycles

FWD CARGO DOOR 5 INCHES FROM LEADING EDGE. ON BOTTOM OF DOOR DENT 2 INCHES BY 13/16 AND .10. PERFORMED VISUAL INSPECTION OF FWD CARGO DOOR IAW AIRBUS A220 ANDTP 51-10-01-01AAA-018A-A. NO VISUAL DEFECTS NOTED. J.MORAN 413164. C/W ERA#600099-14 REV ORIG SECTION 1 STEPS 1,3,4,5,6. J.MORAN 413164. PERFORMED HFEC INSPECTION PER ERA 600099-14 ORIG , STEP 2 NO DEFECTS NOTED 913913. THIS ERA 600099-14 REV ORIG IS APPROVED PER P.S. 900-5-1 N04. THIS ITEM IS PLACED ON MONITOR WITH PERMANENT REPAIR AT 1,700HRS OR 365 DAYS. (LP#8727922)

Part: SKIN — DAMAGED · airframe 6,011 hrs · 2,844 cycles

FUSELAGE SKIN DAMAGED BETWEEN FR3 AND FR4. SKIN REPAIRED IN MSP DURING C CHECK W/REF. TO ERA 582205-14, REV . C, REFERENCE LOG PAGE 5841746. THIS REPAIR SHOULD HAVE BEEN CLASSIFIED AS A MAJOR REPAIR AND THERFORE SDR RECORDABLE. THIS LOG IS TO IDENTIFY IT AS SUCH. (LP# 2251562)

Part: SKIN — NONE · airframe 6,238 hrs · 2,941 cycles

ERA 582205-14 REV C SECTION IV ISSUED FOR PERMANENT REPAIR TO LH NOSE SKIN DENT. REF LOGPAGE 5841746FOR ORIGINAL DEFERRAL FOLLOW ON ACTION REQUIRED. ACCOMPLISH SECTION VI WITHIN 10 DAYS OF SECTION IV COMPLETION AND ACCOMPLISH SECTION VII WITHIN 30 DAYS OF SECTION IV COMPLETION. SECTION VI REQUIRES RVSM INSPECTION USING HANDSCAN700 SCANNER. PER AMP 51-10-00-01AAA-310E-A ASSOCIATED ER/A 00-582205 ADDED FOR AC 8113. (LP#2249153)

Part: HINGE — CRACKED · airframe 5,995 hrs · 2,836 cycles

LH HORIZONTAL STABILIZER - #2 HINGE RIB IS CRACKED AT THE AFT END. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0255:2021-2053-LH/ 004 00131 COMPLIED WITH PRI 599462-14 REV 0, AND ER/A 599462-14 REV ORIGINAL. (LP# 2247586)

Part: WASTE BOX — CORRODED · corrosion level 2 · airframe 5,995 hrs · 2,836 cycles

LAV WASTE BOX HAS CORROSION AT AFT RIGHT DOOR FLANGE. -M- SUMMARY SEE NR FOR ADDITIONAL INFORMATION 023-0001:5327-01014-01 /001 00192 COMPLIED WITH PRI 599478-14AD REV 0, PRI 599478-14AD REV 1, AND ER/A 599478-14AD REV ORIGINAL. (LP# 2247525)

Part: REPAIR — INSTALLED · airframe 5,995 hrs · 2,836 cycles

ERA 599478-14AD ISSUED FOR CORROSION FINDING TO AFT WASTE BOX CORROSION INSPECTION PER EM 5327-01014-01. FOLLOW ON ACTION REQUIRED. ACCOMPLISH SECTION II PRIOR TO 8500 FH FROM SECTION I ACCOMPLISH MENT ASSOCIATED AA 5327-01014 ADDED FOR AC 8113 ASSOCIATED ER/A 00-599478 ADDED FOR AC 8113. (LP# 2240977)

Part: BLEED VALVE — FAILED · airframe 5,974 hrs · 2,823 cycles

SHIP 8113 -ATB- DUE TO LEFT BLEED FAILURE DURING CLIMB. CORRECTIVE ACTION: PLACED LEFT BLEED ON MEL, COMPLIED WITH NO GO ODI PROCEDURES; REPLACED LT PRSOV. (LP# 8861636)

Part: DOOR — LOW PRESSURE (CABIN) · airframe 2,352 hrs · 1,089 cycles

AFT LEFT PASSENGER DOOR EOAM IN YELLOW. SERVICED AFT LEFT PAX DOOR PER A220 AMP 52-12 EAOM IW NOW GREEN. EAOM VERIFIED ARMED AND SAFETIED RII COMPLETE (LP6912725)

Part: HOSE — UNSECURE (LT ENGINE) · airframe 2,305 hrs · 1,068 cycles

DOING WORKCARD 2620-01223-01A FOUND TORQUE SEAL CRACKED ON LEFT ENGINE FIREX HOSE PYLON CONNECTOR. RESECURRED HOSE PER A220 WORKCARD 2620-01223-01A. OK FOR SERVICE. (LP5372597)

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 2,000 hrs · 927 cycles

AT CRUISE ALTITUDE LAV SMOKE WARNING ON EICAS AND LAV SMOKE 2C ON CMS. VISUAL INSPECTION REVELED NO SMOKE AND WARNING STOPPED AFTER 30 SEC. LAV SMOKE WARNIG RESET PER BD500 SOLUTION ID# 2-37498. A/C OK FOR SERVICE. (LP# 6516956)

Part: LOUVER — DAMAGED (BODY FAIRING) · airframe 1,927 hrs · 889 cycles

ON WALK AROUND FOUND RT FWD WTBF LOUVER MISSING PIECES. REMOVED AND REPLACED R FWD WTBF LOUVER PER AMP J53-82.

Part: LONGERON — CRACKED · airframe 1,494 hrs · 690 cycles

R/H WTBF LONGERON CRACKED. REMOVD R/H WTBF LONGERON. INSTALLED SERVICEABLE L/ H WTBF LONGERON WITH HI-LOKS IAW A220 ASRP 51-42-20. SECURITY CHECKS GOOD. A/C OK FOR SERVICE. (LP#1373124)

Part: LONGERON — CRACKED · airframe 1,494 hrs · 690 cycles

L/H WTBF LONGERON CRACKED. REMOVED L/H WTBF LONGERON. MIP. (302615) INSTALLED SERVICEABLE L /H WTBF LONGERON WITH HI-LOKS IAW A220 ASRP 51-42-20. SECURITY CHECKS GOOD. A/C OK FOR SERVICE. (LP# 1373129)

Part: WARNING MESSAGE — ILLUMINATED · airframe 205 hrs · 94 cycles

DURING APPROACH INTO LGA, OBSERVED A "FMS OEI PERF ACTIVE" MASTER CAUTION MESSAGE , THEN OBSERVED LEFT ENGINE N1 ROLLING BACK AND EGT DECREASING. ABOUT 1 MIN LATER ENGINE RECOVERED TO NORMAL, LEFT GEN NEVER FELL OUT AND ALL OTHER IND NORMAL (0223/ JFK). REF LOG # 112237, PERFORMED POWER ASSURANCE TEST AND POWER ACCELERATION AND DECELERATION PER AMP BD500-1-J71-00-00-01AAA- 320A-A AND BD500-A-J71-00-00-01AAA-320B-A, ALL PARAMETERS NML. PER A220 EFIM SOLUTION NUMBERS 1-10333 AND 1-10334, CHECKED FOR ANY MOISTURE OR BLOCKAGE IN THE P2/T2 CONNECTIONS AND EEC CONECTIONS BLEW COMPRESSED AIR INTO LINES TO ENSURE THEY WERE CLEAR, RAN EEC SYSTEM TEST , NO FAULTS, ALSO RAN A/T OPERATIONAL TEST PER BD500 AMP TASK BD500-A-J71-00-00-01AAA- 320B-A, RAN AT IDLE FOR 15 MINUTES, THEN 5 MINUTES AT 79% N1, THEN ALLOWED 15 MIN TO COOL, ALL PARAMETERS NML THEN RAN POWER ACC AND DECELERAION TEST PER AMP BD500-A-J71-00-00-01AAA-320A-A, BOOSTED TO MAX T.O FOR 30 SECS, PARAMETERS NORMAL, THEN ALLOWED ENG TO WARM TO TARGET N1 FOR 15 MINS, BOOSTED N1 TO MAX-TOOK 6.4 SEC, THEN BACK TO IDLE TOOK 7.9 SECS, ENG PARAMETERS WITHIN LIMITS (957782). C/W ERA 579025-14 REV ORIG PERMANENT REPAIR INSTRUCTIONS STEP 1-9, ACCOMPLISHED NO 2 ENGINE POWER ASSURANCE TEST PER AMP TASK BD500-A-J71-00-00-01AAA-320B-A AND NO 2 ENGINE POWER ACCELERATION AND DECELERATION TEST PER AMP BD500-A-J71- 00-00-01AAA-321A-A. ALL PARAMETERS NORMAL, NO ABNORMALITIES NOTED, OKAY FOR SVC. (LP#5120993)