N600QX

Part: RIB — BENT (LT WING) · airframe 38,997 hrs · 29,612 cycles

LEFT WING TE RIB AT WS 260 WAS BENT. COMPLIED WITH EC/TC SNIEO CC670-17000 S02.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 38,318 hrs · 28,987 cycles

FOUND HYDRAULIC LINE MOUNTING BRACKET ON AFT SIDE AT FS 797 RBL 18 IS CRACKED. FABRICATED BRACKET IAW SH670-75544 S01 AND EC/TC SH670-75544 S01.

Part: INTERCOSTAL — CHAFED (BS 725) · airframe 38,318 hrs · 28,987 cycles

INTERCOSTAL AT BS 725 ON BETWEEN LBL 27 AND LBL 36 IS FOULING ON HYDRAULIC LINE ON BOTTOM INBOARD SIDE. REPAIRED INTERCOSTAL IAW BOMBARDIER REO 670-53-41-353 REV-- DATED 2018-01-16 AND EXPRESS JET EC/TC REO 670-53-41-353.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,318 hrs · 28,987 cycles

RBL 9 FLOORBEAM AT FS 684.00 HAS CORROSION ON TOP SIDE. REPAIRED IAW REO 670-53-31-428 REV A DATED 2018-01-09 AND EC/TC REO 670-53-31-428.

Part: POST — CRACKED (BS 693) · airframe 38,318 hrs · 28,987 cycles

BS 693, LBL 18, VERTICAL POST HAS TWO CRACK INDICATIONS NOTED IN THE VERTICAL SURFACE RADIUS AT TOP FASTENERS. REMOVED AND REPLACED THE POST IAW SRMS 51-40-11-001-001-A01 AND SB670BA 53-042.

Part: POST — CRACKED (BS 693) · airframe 38,318 hrs · 28,987 cycles

BS 693, LBL 9 VERTICAL POST HAS TWO CRACK INDICATIONS NOTED IN THE VERTICAL FLANGE RADIUS AT TOP FASTENERS. REMOVED AND REPLACED THE POST IAW SRM 51-40-06-001-001-A01, 51-40-11-001-001-A01, AND S/B 670SH-53-042.

Part: FITTING — CORRODED (FUSELAGE) · airframe 37,259 hrs · 27,889 cycles

DURING PREP TO JACK AIRCRAFT THE NOSE JACK PAD BROKE CAUSING DAMAGE TO AC EXTERNAL SKIN AT NLG JACK FITTING OUTBOARD OF STR 27R. COMPLIED WITH REO 670-53-11-1278 AND EC/TC REO 670-53-11-1278 FOR REPAIR OF NLG JACKING FITTING.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 35,542 hrs · 26,565 cycles

LEFT AFT EXTERIOR EMERGENCY LIGHT LENS CRACKED. REMOVED & REPLACED THE LENS & OPS CHECKED GOOD IAW AMM 33-51-15.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 35,534 hrs · 26,559 cycles

LEFT AFT EXTERIOR EMERGENCY LIGHT LENS CRACKED.

Part: POWER SUPPLY — INTERMITTENT (EMERGENCY LIGHTS) · airframe 35,461 hrs · 26,507 cycles

EMERGENCY LIGHTS INTERMITTENTLY FLASHING. REMOVED AND REPLACED RELAY K135 ON PCB-5 JB 11 IAW AMM 20-42-00. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHECK FAILED FOR OVERHEAD LIGHTS ABOVE EMERGENCY ROW. REMOVED AND REPLACED ESPU 3 IAW AMM 33-51-17 WITH PART IAW SUPPLEMENT 33-51-17 ITEM 6B. OPS CHECKED GOOD AT THIS TIME. ACFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,278 hrs · 26,353 cycles

FOUND MULTIPLE EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY ASSEMBLIES IN POSITIONS NR 1, 2, 4 IAW AMM 33-51-17 AND AIPC 33-51-17, FIG 1, ITEM 6. OPS CHECK GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,080 hrs · 26,201 cycles

SEVERAL EMERGENCY LIGHTS INOPERATIVE IN CABIN AND EXTERIOR. REMOVED & INSTALLED SERVICABLE EPSU BATTERY PACK AND CHARGER IAW AMM 33-51-17-000-801 A01 & 33-51-17-000-802 A01 & 33-51-17-400-801 A01 & 33-51-17-400-802 A02. OPS CHECK GOOD.

Part: LINK — CRACKED (WING-BODY) · airframe 35,080 hrs · 26,201 cycles

CRACK FOUND AT LT LOWER SPA LINK BEARING DURING SPAN LINK INSP REF W/O 630639. REPAIRED BY REPLACING WING/FUSELAGE PICK-UP LINKS IAW SB601BA-57-016.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 35,080 hrs · 26,201 cycles

CABIN CEILING PANEL 253CLC EMERGENCY LIGHT CONNECTOR HAS 1 BROKEN WIRE. REMOVED DAMAGED PIN FROM CONNECTOR IAW ESPM 20-26-00. CRIMPED NEW PIN AND INSTALLED IN SERVICABLE CONNECTOR IAW ESPM 20-16-00 AND 20-26-00. PERFORMED OPS TEST OF THE EMERGENCY LIGHTS, OPS TEST CHECKED GOOD AT PANEL 253CLC.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 35,080 hrs · 26,201 cycles

RT WEB AT FS 280 CORRODED. REMOVED CORROSION DAMAGE IAW SRM 51-21-06-001-001 A01 CORROSION FOUND UNDER FASTENER HEADS. COMPLIED WITH EC/TC REO 670-53-11-1142 AND REO 670-53-11-1142.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 35,080 hrs · 26,201 cycles

FLOORBEAM CORRODED . REMOVED CORROSION DAMAGE IAW SRM 51-21-06-001-001 A01. R & R 280 CROSSBEAM IAW SRM 53-11-41-201-003-A01.

Part: DOOR — LACK OF LUBE (GALLEY) · airframe 35,080 hrs · 26,201 cycles

FWD GALLEY SERVICE DOOR FAILED FUNCTIONAL CHECK AT 50 LBS FORCE TO OPEN DOOR. MAX ALLOWED 35 LBS. LUBRICATED GALLEY SERVICE DOOR REF AMM TASK 12-20-52-640-801 A01. COMPLIED WITH FUNCTIONAL TEST OF THE GALLEY SERVICE DOOR REF AMM TASK 52-41-00-720-801 A01 FUNCTIONAL TEST GOOD.

Part: FRAME — CORRODED (BS 349) · airframe 35,080 hrs · 26,201 cycles

FRAME 349.00 CORRODED AFT SIDE BETWEEN INTERCOSTALS LBL2 & RBL2. REMOVED CORROSION DAMAGE IAW SRM 51-21-06-001-001-A01. COMPLIED WITH REPAIR EA 26-2016-091, REV A COMPLIED ALL STEP OF EC/TC EA 26-2016-091, REV A.

Part: FRAME — CORRODED (BS 333) · airframe 35,080 hrs · 26,201 cycles

FRAME 333.00, CORRODED AFT SIDE BETWEEN STR 25LT-25RT. REMOVED CORROSION DAMAGE IAW SRM 51-21-06-001-001-A01. COMPLIED WITH PERMANENT REPAIR IAW EA 32-2016-055 & STEP A COMPLIED WITH EA 32-2016-055.

Part: FLOOR SUPPORT — CORRODED (BS 380) · airframe 35,080 hrs · 26,201 cycles

COCKPIT FLOOR PANEL 221ALF AFT SUPPORT ANGLE CORRODED AT FS 280.00. REMOVED CORROSION DAMAGE IAW SRM 51-21-06-001-001 A01. COMPLIED WITH EC/TC ROE 670-53-11-1141 AND REO 670-53-11-1141.

Part: ANGLE — CORRODED (BS 333) · airframe 35,080 hrs · 26,201 cycles

CORRODED CLIP AT FRAME 333.00, STR 27. REMOVED STR 27 CLEAT FROM FRAME STA 333.00, IAW SRM 51-42-06-001-001-A01. INSTALLED NEW CLEAT AT FS 333, STR 27 IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. COMPLIED WITH EC/TC EO 700-53-0305 PARTS FABRICATION FRAME CLEAT PN SH670-32437-1.

Part: FRAME — CORRODED (BS 319) · airframe 35,080 hrs · 26,201 cycles

FRAME 319.70 CORRODED FWD SIDE BETWEEN STRS 26RT-26LT. REMOVED CORROISON DAMAGE IAW SRM 51-21-06-001-001-A01. COMPLIED WITH PERMANENT REPAIR IAW EA 32-2016-054 & STEP A COMPLIED WITH EC/TC EA 32-2016-054.

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 35,080 hrs · 26,201 cycles

FLOOR SUPPORT BETWEEN BS 349.00 & 364.00 AT RBL 2 CORRODED RT AFT SECTION. REMOVED CORROSION IAW SRM 51-21-06-001-001 A01 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001 A01. REMOVED INTERCOSTAL BETWEEN FS 349-FS 364 AT RBL-2 IAW SRM 51-42-06-001-001 A01. INSTALLED NEW SERVICABLE INTERCOSTAL BETWEEN FS 349-FS 364 AT RBL-2 IAW SRM 51-42-06-001-001 A01.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 35,080 hrs · 26,201 cycles

INTERCOSTAL BETWEEN BS 349 & 364 AT LBL2 CORRODED LT & RT AFT SECTION. REMOVED CORROSION IAW SRM 51-21-06-001-001 A01 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001 A01. REMOVED INTERCOSTAL BETWEEN FS 349-FS 364 AT LBL-2 IAW SRM 51-42-06-001-001 A01. INSTALLED NEW SERVICABLE INTERCOSTAL BETWEEN FS 349-FS 364 AT LBL-2 IAW SRM 51-42-06-001-001 A01.

Part: DOUBLER — CORRODED (BS 295-310) · airframe 35,080 hrs · 26,201 cycles

TCAS DOUBLER CORRODED AT STR 27 BETWEEN FRAMES 295.00 & 310.00. R & R TCAS DOUBLER AT STR 27 BETWEEN FRAMES 295.00+310.00 IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 869-883) · airframe 35,080 hrs · 26,201 cycles

LBL 9 SEAT TRACK BS 869 -883 CORODDED. REMOVED THE SEAT TRACK IAW AMM 53-00--49-000-801. 836-850 INSTALLED NEW LBL9 SEAT RAIL SEGMENT FROM FS 836 TO FS 580 IAW AMM 53-00-49-400-01. COMPLIED WITH EC/TC REO 670-53-00-343, REV M.

Part: SEAT TRACK — CORRODED (BS 847-989) · airframe 35,080 hrs · 26,201 cycles

LBL 9, SEAT TRACK BS 847- 989, SEVERAL AREAS. REMOVED THE SEAT TRACK FROM IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A01. COMPLIED WITH WC/TC REO670-53-00-343 AND GREO 670-53-00-343, REV M.

Part: SEAT TRACK — CORRODED (BS 946) · airframe 35,080 hrs · 26,201 cycles

LT SIDE SEAT TRACK FS 946 CORRODED SEAVEAL AREAS. R & R IAW AMM 53-00-49-000-801-A01, 53-00-49-400-801-A01. C

Part: SEAT TRACK — CORRODED (BS 483-572) · airframe 35,080 hrs · 26,201 cycles

LT SIDE SEAT TRACK BS 483 - 572 CORRODED SEVERAL AREAS. R & R IAW AMM 53-00-49-000-801-A01, 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 675-712) · airframe 35,080 hrs · 26,201 cycles

LEFT SIDE SEAT TRACK BS 675 - 712 CORRODED SEVERAL AREAS. R & R IAW AMM 53-00-49-000-801-A01, 53-00-49-400-801-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 35,080 hrs · 26,201 cycles

FLOORBEAM BS 280 CORRODED AT LBL 14. FLOORBEAM R & R IAW SB 670BA-53-041-02.

Part: SEAT TRACK — CORRODED (BS 483-572) · airframe 35,080 hrs · 26,201 cycles

RT SIDE SEAT TRACK BS 483 -572 CORRODED SEVERAL AREAS. R & R THE SEAT TRACK IAW AMM 53-00-49-400-801-A01, 53-00-49-801-A01.

Part: SEAT TRACK — CORRODED (BS 865-915) · airframe 35,080 hrs · 26,201 cycles

RT SIDE SEAT TRACK BS 865 - 915 CORRODED SEVERAL AREAS. R & R THE SEAT TRACK IAW AMM 53-00-49-400-801-A01, 53-00-49-801-A01.

Part: ATTACH ANGLE — CRACKED · airframe 35,080 hrs · 26,201 cycles

RT VERTICAL STABILIZER TO FUSELAGE ANGLE APPEARS CRACKED. ALL STEPS OF REO 670-55-31-082 HAVE BEEN COMPLIED WITH & COMPLIED WITH ECTC REO 670-55-31-082.

Part: SEAT TRACK — CORRODED (BS 378-457) · airframe 35,080 hrs · 26,201 cycles

RT SIDE SEAT TRACK BS 378 - 457 CORRODED SEVERAL AREAS. R & R IAW AMM 53-00-49-000-801-A01, 53-00-49-400-801-A01.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 35,080 hrs · 26,201 cycles

LT WEB AT FS 280 CORRODED AT LB12. REMOVED CORROSION DAMAGE IAW SRM 51-21-06-001-001-A01 CORROSION FOUND UNDER FASTENER HEADS. COMPLIED WITH EC/TC REO 670-53-11-1142 AND REO 670-53-11-1142.

Part: SEAT TRACK — CORRODED (BS 847-1005) · airframe 35,080 hrs · 26,201 cycles

RBL9, SEAT TRACK BS 847-1005 CORRODED SEVERAL AREAS. REMOVED SEAT TRACK IAW AMM 53-00-49-000-80. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343-REV M.

Part: SEAT TRACK — CORRODED (BS 378-457) · airframe 35,080 hrs · 26,201 cycles

LT SIDE SEAT TRACK BS 378 - 457 CORRODED SEVERAL AREAS. REMOVED AND REPLACED IAW AMM 53-01-11-000-802-A01, AND AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 573-675) · airframe 35,080 hrs · 26,201 cycles

RT SIDE SEAT TRACK BS 573 - 675 CORRODED SEVERAL AREAS. R & R SEAT TRACK IAW AMM 53-00-49-400-801-A01, 53-00-49-801-A01.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 35,080 hrs · 26,201 cycles

RBL9, SEAT TRACK FS 485-581 CORRODED SEVERAL AREAS. REMOVED RBL9, SEAT TRACK FROM FS 485 TO FS 581 IAW AMM 53-00-49-000-80. INSTALLED NEW RBL9, SEAT TRACK IAW AMM 53-00-49-400-801. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV M.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 34,967 hrs · 26,108 cycles

EXTERIOR EMERGENCY LIGHT AFT OF SERVICE WILL NOT ILLUMINATE. R & R BULB FOR EXTERIOR EMERGENCY LIGHT AFT OF SERVICE DOOR. OPS CHECK GOOD IAW AMM 33-51-15-710-801-A01.

Part: LIGHT — INOPERATIVE (SEAT 10B) · airframe 33,948 hrs · 25,303 cycles

SEAT 10B, C OVERHEAD ISLE EMERGENCY LIGHT INOPERATIVE. R & R THE EMERGENCY LIGHT IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: ROLLER — UNSECURE (PAX DOOR) · airframe 33,642 hrs · 25,032 cycles

PASSENGER DOOR FAILED FUNCTIONAL TEST STEP 4A, A21. REMOVED SHIMS FROM FWD UPPER CENTERING ROLLER IAW AMM 52-11-00-720-802-A01. RETORQUED FASTENERS ON FWD UPPER CENTERING ROLLER AND PERFORMED CLEARANCE CHECK IAW AMM 20-21-00-910-801-A01 52-11-00-720-802-A01 STEP 4A, 21, CLEARANCE CHECK GOOD.

Part: DOOR SILL — CORRODED · airframe 33,642 hrs · 25,032 cycles

SERVICE DOOR SILL CAP ANGLE CORRODED. REMOVED SERVICE DOOR SILL CAP ANGLE IAW SRM 51-42-06-001-001-AO1. LOCATED & DRILLED NEW SERVICEABLE SERVICE DOOR SILL CAP ANGLE IAW SRM 51-40-11-001-001-AO1 & INSTALLED BRACKETS TO NEW DOOR SILL CAP ANGLE IAW SRM 51-42-06-001-001 A01. INSTALLED NEW SERVICE SERVICE DOOR SILL CAP ANGLE IAW SRM 51-42-06-001-001-AO1, 51-42-21-001-001-AO1 AND DWG SA670-31950.

Part: FLOORBEAM — CORRODED (BS 295) · airframe 33,642 hrs · 25,032 cycles

FLOORBEAM CORRODED BS 295 BETWEEN BL 0 & LBL 9. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REPAIRED IAW EA 32-2015-318.

Part: FLOORBEAM — CORRODED (BS 333) · airframe 33,642 hrs · 25,032 cycles

FLOORBEAM CORRODED AT BS 333 BETWEEN LBL 9 & BL 0. REMOVED CORROSION IAW SRM 51-21-06-001-001A-01. COMPLIED WITH REO 670-53-21-1207.

Part: SEAT TRACK — CORRODED (BS 677-693) · airframe 33,642 hrs · 25,032 cycles

LBL9, SEAT TRACK SEGEMENT BS 677 - 693 HAS CORROSION. REMOVED SEAT RAIL AT LBL9, FS677-693 IAW AMM 53-00-49-000-801A-01. INSTALLED NEW SEAT RAIL AT FS677-693, REF: SRM 53-00-49-400-801-A01. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 33,642 hrs · 25,032 cycles

LBL 9 SEAT TRACK SEGEMENT BS 485-581 HAS CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-00-000-801-A01 AND 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 693-699) · airframe 33,642 hrs · 25,032 cycles

RBL 9, SEAT RAIL SEGEMENT BS 699 - 693 HAS CORROSION. REMOVED SEAT RAIL AT RBL9, FS677-693 IAW AMM 53-00-49-000-801-A01. INSTALLED SERIVCABLE SEAT TRACK AT FS677-693 IAW AMM 53-00-49-400-801-A01. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 693-830) · airframe 33,642 hrs · 25,032 cycles

LBL9 SEAT TRACK SEGEMENT BS 693 - 830 HAS CORROSION. EVALUATED SEAT RAIL AT LBL9, FS 693- FS 830 FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED SEAT TRACK AT LBL9 FS 693-FS 830 IAW AMM 53-00-49-000-801-A02. REMOVED AND INSTALLED NEW SEAT TRACK AT LBL9 FS 693-FS 830 IAW AMM 53-00-49-400-801-A02, AMM 53-00-49-000-801-A02.

Part: SEAT TRACK — CORRODED (BS 693-830) · airframe 33,642 hrs · 25,032 cycles

RBL9, SEAT TRACK SEGEMENT FS 693 - 830 HAS CORROSION. REMOVED AND INSTALLED NEW SEAT TRACK RBL9, FS 693-FS 830 IAW AMM 53-00-49-400-801-A02, AMM 53-00-49-00-801-A02. EVALUATED SEAT TRACK AT RBL9, FS 693-FS 830. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01.

Part: SEAT TRACK — CORRODED (BS 385-485) · airframe 33,642 hrs · 25,032 cycles

LBL 9, SEAT TRACK SEGEMENT BS 385-485 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A01 AND AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 33,642 hrs · 25,032 cycles

LBL 9, SEAT TRACK SEGMENT BS 581-677 CORRODED. REMOVED SEAT RAIL AT LBL9, FS581-677 IAW AMM 53-00-49-000-801-A01. INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 33,642 hrs · 25,032 cycles

RBL9 SEAT TRACK SEGEMENT FS 349-485 HAS CORROSION. R & R RT FLOOR SEAT TRACK SEGMENT FS349-485 IAW AMMM 53-00-49-000-801-A01.

Part: FRAME — CORRODED (BS 549) · airframe 33,642 hrs · 25,032 cycles

BS 549 FRAME HAS CORROISON BETWEEN STRINGERS 17 & 18. COMPLIED WITH REO 670-53-31-350, REV.

Part: SEAT TRACK — CORRODED (BS 379-385) · airframe 33,642 hrs · 25,032 cycles

LBL 9, SEAT TRACK SEGMENT BS 379-385 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801A-01 AND AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 33,642 hrs · 25,032 cycles

RBL9, SEAT TRACK SEGEMENT FS 581-677 HAS CORROSION. REMOVED SEAT RAIL AT RBL9, FS581-677 IAW AMM 53-00-49-000-801-A01. INSTALLED SERVICEABLE SEAT TRACK AT FS581-677 IAW AMM 53-00-49-400-801-A01. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 785-830) · airframe 33,642 hrs · 25,032 cycles

RIGHT SIDEWALL SEAT TRACK SEGMENT BS 785-830 HAS CORROSION. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN FOR SEAT RAIL FABRICATION. REMOVED OLD SEAT RAIL AND INSTALLED NEW SEAT RAIL AT SIDEWALL RT SIDE, FS 785-830, REF: AMM 53-00-401-000-801-A01, AND 53-00-44-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 33,642 hrs · 25,032 cycles

RIGHT SIDEWALL SEAT TRACK SEGMENT BS 708-761 HAS CORROSION. R & R SEAT TRACK IAW AMM 53-0044-000-801-A01 AND 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 33,642 hrs · 25,032 cycles

RIGHT SIDEWALL SEAT TRACK SEGMENT BS 677-708 HAS CORROSION. FOUND CORROISON TO BE OUT OF LIMITS IAW SRM 53-21-101-001-A01 AND 51-21-06-001-001-A01. R & R SEAT TRACK IAW AMM 53-00-49-000-801A-01 AND 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 33,642 hrs · 25,032 cycles

LEFT SIDE WALL SEAT RAIL SEGMENT, FS 708-761 HAS CORROSION. EVALUATED DAMAGE ON SEAT TRACK AND FOUND SEAT RAIL AND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED LT SIDE SEAT RAIL BETWEEN FS 708-761 IAW AMM 53-00-49-000-801-A01. INSTALLED SERVICEABLE LT SIDE RAIL SEAT TRACK IAW AMM 53-00-49-400-801-A01, IPC REF 53-00-49, ITEM 25.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 33,642 hrs · 25,032 cycles

AFT CARGO DOOR SILL IS CORRODED. REPAIRED AFT CARGO LOWER SILL IAW REO 670-53-61-913 ECTC. FINISHED REMOVING CORROISON IAW SRM 51-21-06-001-001-A01. REPAIRED IAW SRM, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 IAW DWG MM 670-35085.

Part: SEAT TRACK — CORRODED (BS 785-830) · airframe 33,642 hrs · 25,032 cycles

LEFT SIDEWALL SEAT TRACK SEGMENT 785-830 HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-41-101-001-A01. FABRICATED NEW SEAT TRACK IAW ECTC REO 670-53-00-343, REV J COMPLIED WITH ECTC REO 670-53-00-343 & GREO 670-53-00-343, REV L. REMOVED SEAT TRACK SIDEWALL LT SIDE AT FS 785-830, REF: AMM 53-00-49-000-801-A01. INSTALLED SEAT TRACK SIDEWALL LT SIDE AT F/S 785-830, REF AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 597-661) · airframe 33,642 hrs · 25,032 cycles

LEFT SIDE WALL SEAT RAIL SEGMENT FS 597-661 HAS CORROSION. EVALUTED SEAT RAIL FS 597-661 ON 41 SIDE AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-AO1. INSTALLED NEW SEAT RAIL IAW AMM 53-00-49-400-801-AO1.

Part: DOOR SILL — CORRODED (PAX DOORWAY) · airframe 33,642 hrs · 25,032 cycles

PAX DOOR SILL ANGLE HAS CORROSION. INSTALLED NEW SERVICEABLE PAX DOOR KICK PLATE LWR ANGLE IAW DWG SH670-31875 & SRM 51-42-06-004-001-AO1 & 51-42-21-001-001-AO1. LOCATED & DRILLED NEW SERVICEABLE PAX DOOR KICK PLATE ANGLE IAW SRM 51-40-11-001-001-AO1 & DWG SH670-31875. REMOVED UPPER SILL ANGLE TO ACCESS LOWER ANGLE FOR REMOVAL/ REPLACEMENT IAW SRM 51-42-06-001-001-AO1. RE-INSTALLED UPPER SILL ANGLE TO LOWER SILL ANGLE IAW SRM 51-42-06-001-001-AO1 & DWG SH670-31875. INSTALLED NEW SERVICEABLE FWD & AFT HANDRAIL ATTACHMENT FITTINGS IAW SRM 51-42-21-001-001-AO1 & DWG SH670-31905. INSTALLED NEW FITTINGS FWD & AFT IAW SRM 51-42-21-001-001-AO1 & DWG SH670-31905. LOCATED & DRILLED NEW HANDRAIL FITTINGS FWD & AFT AT PAX DOOR SILL AREAS IAW DWG SH670-31905 & SRM 51-40-11-001-001-AO1.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 33,642 hrs · 25,032 cycles

AVIONICS FLOOR SUPPORT ANGLE CORRODED AT FS 280.00. R & R FLOOR SUPPORT ANGLE AT FS 280 IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-15-001-001-A01 AMD 51-42-21-001-01-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 33,642 hrs · 25,032 cycles

BS 280 CROSSBEAM HAS CORROSION. REMOVED CORRODED FS 280 CROSSBEAM IAW SRM 53-11-41-201-001-AO1. CUT NEW SERVICEABLE BEAM IN HALF, DRILLED & LOCATED LT & RT SIPES IAW SRM 53-11-41-201-001-AO1, DWG CC670-34175. LOCATED FASTENER HOLES IN NEW SERVICEABLE BEAM AT FS 280 AND STARTED INSTALLATION OF 280 CROSSBEAM IAW SRM 51-40-11-001-001- AO1, 57-42-21-001-001-AO1 AND 53-11-41-201-003-001. INSTALLED FS 280 CROSSBEAM IAW SRM 51-42-06-001-001-AO1, 51-42-21-001-001-AO1, 51-42-13-001-001-AO1 AND 53-11-41-201-003-001 AO1 IAW DWG CC670-34175.

Part: STRAP — CRACKED · airframe 33,642 hrs · 25,032 cycles

AFT FAIRING STRAP JOINT AT BS 939.00 CRACKED, PANEL 196DR. RECEIVED EC/TC REPAIRED AFT FAIRING STRAP JOINT AT FS 939.00 IAW EC/TC REO 670-53-82-479. REMOVED STRAP JOINT FROM PANEL 196DR TO FOM IAW SRM 51-41-02-001-001-A01. REINSTALLED STRAP JOINT TO PANEL 196DR IAW SRM 51-41-02-001-001-A01.

Part: BRACKET — GOUGED · airframe 33,642 hrs · 25,032 cycles

SUPPORT WHEEL BRACKET HAS GOUGE FROM CONTACT WITH DOOR SURROUND FITTING. RECEIVED STS EA 43-2015-006 AND COMPLIED WITH PERMANENT REPAIR. R & R TUBE AT TOP CABLE ASSEMBLY REF: AMM 52-11-13-000/400-803-AO1. COMPLIED WITH ECTC 43-2015-006.

Part: INLET — DENTED (RT ENGINE) · airframe 33,642 hrs · 25,032 cycles

RIGHT ENGINE INLET HAS A DENT AT 7 O'CLOCK POSITION. COMPLIED WITH EC/TC EA 32-2015-313 PERMANENT REPAIR REFER TO W/O 372985 N/R 00097. UPON FURTHER INVESTGATION FOUND THAT RT ENGINE INLET OTBD SKIN HAS DENT MEASURED 7.5" X 4.5" W AND .125" DEPTH IAW ACRJ 700 TR-51-0050. COMPLIED WITH STS EA 32-2015-313 DATED 07-31-2015. COMPLIED WITH ECTC EA 32-2015-313.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 33,620 hrs · 25,013 cycles

12 AB LOWER EXIT SIGN, TWO LIGHT BULBS BURNED OUT. REPLACED THE BULB IAW GMM 3-8. OPS CHECKED GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 33,562 hrs · 24,966 cycles

FLOOR LEVEL LIGHTING MISSING BETWEEN FIRST CLASS. INSTALLED LIGHT STRIPS IAW GMM 3-8.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 33,343 hrs · 24,775 cycles

LT AND RT BS 280, FLOORBEAM HAS CORROSION.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 33,338 hrs · 24,771 cycles

BS 280 FLOORBEAM CORRODED, RBL 10-16. C/W EA10-2015-062.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 33,338 hrs · 24,771 cycles

BS 280 FLOORBEAM AT LBL 10-16 CORRODED. C/W EA10-2015-061.

Part: MEGAPHONE — DAMAGED (CABIN) · airframe 30,897 hrs · 22,906 cycles

MEGAPHONE HAS A DAMAGED SCREW RETAINER. R & R THE MEGAPHONE IAW AMM 25-61-14 AND AIPC 25-61-14, FIG 1A, ITEM 5A.

Part: RETAINER — DAMAGED (CARGO DOOR) · airframe 30,613 hrs · 22,691 cycles

FWD CARGO DOOR SEAL RETAINER DAMAGED. COMPLIED WITH REO 670-52-35-127, REV. C, PERMANENT REPAIR. BLENDED OUT GOUGE DAMAGE TO A SMOOTH CONTOUR. DRESSED BACK SEAL RETAINER TO ORIGINAL CONTOUR. ALL WORK ACCOMPLISHED IAW REO 670-52-35-127, REV C. MAJOR REPAIR IAW GMM 5-3.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,094 hrs · 22,328 cycles

INTERIOR CEILING EMERGENCY LIGHT IS OUT AT 6 ABCD. REPLACED LAMP IAW AMM 33-51-09, OPS CHECKED GOOD.

Part: SKIN — DAMAGED (BS 1015-1031) · airframe 29,483 hrs · 21,873 cycles

SKIN DAMAGE FOUND BETWEEN FS 1015-1031 S25R. REPAIRED IAW REO 670-53-61-983, REV-A. REPAIR CLASSIFIED AS MAJOR.

Part: TRUNNION — CRACKED (LT MLG) · airframe 29,458 hrs · 21,855 cycles

LEFT MLG TRUNNION HAS (1EA) CRACKED FASTENER HOLE (MARKED). REPAIRED IAW REO 670-57-21-572, P2 DATED 07/27/2013. REO 670-57-21-572 IS A MAJOR REPAIR.

Part: TRUNNION — CRACKED (RT MLG) · airframe 29,458 hrs · 21,855 cycles

RT MLG TRUNNION HAS (3EA) FASTENER HOLES WITH CRACK INDICATION (MARKED). REPAIRED IAW REO 670-57-21-572, REV P2 DATED JUL 27, 2013. REO 670-57-21-572 IS A MAJOR REPAIR.

Part: RISER — CRACKED (DOOR) · airframe 29,458 hrs · 21,855 cycles

ASD FWD RISER CRACKED 1 INCH ABOVE LOWER STEP. REPAIRED IAW REO 670-52-11-718. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,458 hrs · 21,855 cycles

SKIN GASHED ABOVE FWD CARGO DOOR. REPAIRED IAW EO CL600-2C10-53-I00346. MAJOR REPAIR.

Part: SILL — CORRODED (SERVICE DOORWAY) · airframe 29,458 hrs · 21,855 cycles

SERVICE DOOR SILL CORRODED BETWEEN FS 319-349. REMOVED DOOR SILL ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW SILL ANGLE IAW SRM 51-40-11-001-001. INSTALLED SERVICE DOOR SILL ANGLE IAW SRM 51-42-06-001-001. REPAIR CLASSIFIED AS MAJOR.

Part: LINK — DAMAGED (RT WING) · airframe 29,483 hrs · 21,873 cycles

DURING INSPECTION OF RT WING, LINK WAS FOUND TO BE TOUCHING ON UPPER AND LOWER FITTING. COMPLIED WITH EC/TC SB670BA-57-016 IAW PART A SB 670BA-27-016, REV B, DEC 07/2012. REPAIR CLASSIFIED AS MAJOR.

Part: FLOOR SUPPORT — CORRODED (BS 280-319.7) · airframe 29,458 hrs · 21,855 cycles

RT CABIN FLOOR SUPPORT CORRODED FROM FS 280 TO 319.7. REPAIRED IAW SRM 51-42-06-001-001-A01, 51-42-06-001-A01. REPAIR CLASSIFIED AS MAJOR.

Part: WEB — CORRODED (BS 280) · airframe 29,458 hrs · 21,855 cycles

AFT SIDE OF LEFT WEB AT FS 280.00 CORRODED. REPAIRED IAW REO 670-53-11-594 REV .

Part: FLOORBEAM — CORRODED (BS 280) · airframe 29,458 hrs · 21,855 cycles

BS 280 FLOORBEAM CORRODED. REPAIRED IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-06-001-001, 51-42-21-001-001, 51-23-00, 51-25-06-001-001, 53-11-41-201-003-A01, 51-20-006-250-A01 AND REO 670-53-11-265. REPAIR CLASSIFIED AS MAJOR.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 29,483 hrs · 21,873 cycles

TCAS ANTENNA DOUBLER CORRODED S27 BETWEEN FRAMES 295.00 AND 310.00. REMOVED DOUBLER IAW SRM 51-42-06. DRILLED NEW DOUBLER IAW SRM 51-40-11, -001-001-A01. INSTALLED IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: WEB — CORRODED (BS 280) · airframe 29,458 hrs · 21,855 cycles

AFT SIDE OF RIGHT WEB AT FS 280 CORRODED. REPAIRED IAW REO 670-53-11-594 REV.

Part: SHIELD — WORN (WIRE HARNESS) · airframe 29,458 hrs · 21,855 cycles

RIGHT ENGINE IDG WIRES RIDING ON FIRE LOOP SUPPORT TUBE AND WEARING HOLE IN OUTER COVER OF WIRE. REPAIRED IAW REO 670-57-21-001. REPAIR CLASSIFIED AS MAJOR.

Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 29,458 hrs · 21,855 cycles

COCKPIT FLOOR SUPPORT ANGLE CORRODED. REMOVED COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. LOCATED & DRILLED NEW SERVICEABLE FLOOR SUPPORT IAW SRM 51-40-11-001-001. INSTALLED NEW FLOOR SUPPORT ANGLE IAW SRM 51-42-06 AND 51-42-21. REPAIR CLASSIFIED AS MAJOR

Part: SHIELD — TORN (WIRE HARNESS) · airframe 29,458 hrs · 21,855 cycles

IDG HARNESS SHIELDING TORN IN 3 PLACES ON LT ENG. REPAIRED IAW REO 670-24-21-001. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DENTED (BS 1031-1051) · airframe 29,483 hrs · 21,873 cycles

AFT FUSELAGE RT SIDE AT BS 1031.00 -1051.30 AND S23-26R HAS MULTIPLE DENTS AFT OF GROUND AIR CONNECTION ACCESS PANEL. REPAIRED IAW REO 670-53-61-977, DATED 8-16-13. REPAIR CLASSIFIED AS MAJOR.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 29,458 hrs · 21,855 cycles

ASD DRAG ANGLE CRACKED AFT SIDE CENTER SECTION. REPAIRED IAW SRM 51-42-06-001-001-A01, 51-40-06-001-001-A01 AND 52-11-04-201-002-A01.

Part: ACCESS PANEL — CHAFED (CHAFED) · airframe 29,458 hrs · 21,855 cycles

LEFT WING ACCESS PANEL 584EB IS CHAFED. REPAIRED IAW EO CL600-2C10-57-I00345. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: SKIN — DENTED (BS 549-565) · airframe 29,430 hrs · 21,830 cycles

DENT WITH GOUGE FOUND IN SKIN BAY ABOVE FWD CARGO DOOR BETWEEN FS 549 AND 565 S16-17L. REPAIRED IAW REO 670-53-31-294. REPAIR CLASSIFIED AS MAJOR.

Part: TAPE — WRONG PART (EMERGENCY LIGHT) · airframe 27,848 hrs · 20,683 cycles

INCORRECT FLOOR TRACK EMERGENCY LIGHT TAPE FROM ROW 4 TO ROW 17. R & R THE FLOOR TRACK EMERGENCY LIGHT TAPE FROM ROW 4 TO ROW 17 IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,848 hrs · 20,683 cycles

INTERIOR CEILING EMERGENCY LIGHT OUT AT 7ABCD. RELAMPED AND OPS CHECKED GOOD IAW AMM 33-51-00.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 27,573 hrs · 20,484 cycles

EXIT SIGN AT ROW 12 DOES NOT LIGHT UP ON THE FRONT SIDE. (AILSLE SIGN) RESET EMERGENCY LIGHT BATTERY AND FOUND LOOSE CONNECTOR PLUG. ALL CHECKS GOOD IAW AMM 33-50-00.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 27,321 hrs · 20,296 cycles

FLASHLIGHT BEHIND F/A'S SEAT ON/OFF SWITCH INOP. R & R FLASHLIGHT BY REMOVING FROM MOUNT CLIP AND INSTALL SERVICEABLE UNIT INTO MOUNT CLIPS. SDR CLOSED.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 26,479 hrs · 19,679 cycles

REF DMIL 3128461 PIECE OF PHOTOLUMINESCENT TRACK MISSING AT SEATS 12 A & B. R & R PHOTOLUMINESCENT TRACK AT SEAT 12A AND B IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: GLOWSTRIP — BROKEN (CABIN) · airframe 26,441 hrs · 19,653 cycles

GLOWSTRIP BROKEN AT SEATS 12- A+B. OPEN. R & R GLOWSTRIP IAW AMM 33-51-01. OPS CHECK GOOD.

Part: GLOWSTRIP — BROKEN (CABIN) · airframe 26,215 hrs · 19,503 cycles

A/B LUMINESCENT STRIP BROKEN. REPLACED PHOTOLUMINISCENT STRIP AT 12A/B IAW AMM 33-51-01. NO DEFECTS NOTED.

Part: IRS — MALFUNCTIONED · airframe 25,237 hrs · 18,799 cycles

IRS REVERTED IN FLIGHT TRIED TO RESET LOST ALL ATTITUDE AND HEADING INFO WAS IN STRAIGHT FLIGHT. IRS WERE MORE THAN 6 MILES OFF POSITION. EMERGENCY DECLARED AS A PRECAUTION. PREFORMED OPS CHECK OF IRS SYS IAW AMM 34-45-00. NO DEFECTS NOTED AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,989 hrs · 18,609 cycles

EXIT LIGHTS BETWEEN FIRST CLASS SEATS AND COACH C IN FRONT OF SEATS 4DC ARE NOT WORKING. TROUBLESHOT IAW FIM 33-51-00-810-804-A01. TROUBLESHOT EMERGENCY EXIT LIGHTS BETWEEN FIRST CLASS SEATS & COACH IAW FIM 33-51-00-810-804-A01. FOUND BATTERY PACK TO BE UNSERVICEABLE. R & R BATTERY PACK IAW AMM 33-51-17-000-801-A01 & 33-51-17-400-801-A01. OPS CHECKED GOOD IAW AMM 33-51-17-710-801.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,989 hrs · 18,609 cycles

COCKPIT FLOORBEAM CORRODED BEYOND LIMITS FS 280 BETWEEN LBL 9.00 AND RBL 9.00. FABRACATED ANGLES IAW REO 670-53-11-632 & DWG CC670-33292. HEAT TREATED ANGLES IAW DWG CC670-33292. LOCATED AND DRILLED ANGLE IAW 51-42-21-001-001-A01. INSTALLED IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 349-379) · airframe 24,989 hrs · 18,609 cycles

RT FLOOR SEAT TRACK BETWEEN FS 349 TO FS 379 CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SILL — CORRODED (FUSELAGE) · airframe 24,989 hrs · 18,609 cycles

AFT CARGO DOOR SILL AND ANGLE CORRODED. REPAIRED IAW REO 670-53-61-770.

Part: ANGLE — CRACKED (BS 280) · airframe 24,989 hrs · 18,609 cycles

ANGLE AT RBL 26 LWR HOLE FS 280 CRACKED. R & R WITH SERVICABLE ANGLE FROM STORES IAW SRM 51-42-21-001-A01.

Part: SILL — CORRODED (FUSELAGE) · airframe 24,989 hrs · 18,609 cycles

AFT CARGO DOOR SILL AND ANGLE CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 AND 51-42-06-001-001-A01. PERFORMED UT THICKNESS MEASUREMENT OF BLEND AREA IAW NDT INSPECTION PROCESS UT-. REPAIRED SILL IAW REO 670-53-61-770.

Part: SEAT TRACK — CORRODED (BS 825) · airframe 24,989 hrs · 18,609 cycles

LEFT SIDE SEAT TRACK AT FS 825.00 CORRODED. CORROSION FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 708) · airframe 24,989 hrs · 18,609 cycles

LEFT SIDE SEAT TRACK AT FS 708.00 CORRODED. CORROSION FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACE SEAT TRACK IAW SRM 51-41-02.

Part: WEB — CORRODED (BS 280) · airframe 24,989 hrs · 18,609 cycles

LEFT BS 280 WEB IS CORRODED. CUT, REMOVED, FABRICATED AND INSTALLED NEW WEB IAW REO 670-53-11-594.

Part: STRUCTURE — CORRODED (BS 661) · airframe 24,989 hrs · 18,609 cycles

FOUND CORROSION AT FS 661.00 AND STR 27. REPAIRED IAW SRM 51-21-06-001-001-A01.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 24,989 hrs · 18,609 cycles

BS 280 CROSSBEAM CORRODED. BLENDED .002 IN OUT .063 THICKNESS. FOUND DAMAGE TO BE WITHIN LIMITS IAW SRM 51-21-06-001-001-A01.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 24,989 hrs · 18,609 cycles

BS 280 CROSSBEAM IS CORRODED. REMOVED AND REPLACED CROSSBEAM IAW REO 670-53-11-047.

Part: WEB — CORRODED (BS 280) · airframe 24,989 hrs · 18,609 cycles

LEFT BS 280 WEB IS CORRODED. CUT, REMOVED, FABRICATED NEW WEB AND INSTALLED IAW REO 670-53-11-594.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 24,989 hrs · 18,609 cycles

CORROSION ON FLOOR PANEL SUPPORT BRACKET ON AFT SIDE FS 280. REMOVED AND REPLACE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.

Part: WIRE — DAMAGED (CABIN LIGHTS) · airframe 24,006 hrs · 17,932 cycles

F/A REPORTS LIGHTS IN OVERHEAD IN CABIN ARE INOP EG CDIL LIGHT EMERGENCY CALL LIGHT ETC. RECONNECTED WIRE AT PIN 239 IAW AMM 33-51-09. (CLOSED)

Part: ESCAPE HATCH — OUT OF ADJUST (COCKPIT) · airframe 22,929 hrs · 16,953 cycles

CREW ESCAPE HATCH IS HARD TO OPEN & CLOSE. ADJUSTED CREW ESCAPE HATCH STOP BOLTS ITEM 4A6 OF AMM 52-22-00-820-801 PG508 PF161762 8/4/10 (PB) 2. CLEARANCE CHECKS REQUIRED WITH ACFT PRESSURIZED IAW AMM 52-22-00-820-801 STOPS 4A7 THRU COMPLETION 8/4/10 PF161762 (PB) PRESSURIZED ACFT PERFORMED CLEARANCE CHECKS IAW AMM 52-22-00-820-801, CLEARING WITHIN LIMITS. (CLOSED)

Part: ACM — SMOKE (ZONE 100) · airframe 22,876 hrs · 16,908 cycles

CABIN SMOKE AT GATE. APU WAS THE POWER SOURCE. PLACED ON MEL 49-10-1B. PERFORMED GVI OF APU FOR OIL LEAKS ON EXTERIOR AND IN APU EXHAUST CONE. NO DEFECTS FOUND. C/W APU BORESCOPE S/N 99141000051 IAW AMM 49-20-00 PAGE 601-620 TASK 49-20-00-290-801. NO DEFECTS NOTED. REPLACED THE RT ACM, RAN APU AND C/W OPS TEST OF AC DISTRIBUTION SYSTEM PER AMM 21-51-00-710-801, OPS CHECK GOOD, NO CABIN SMOKE NOTED. RETURNED TO SERVICE.

Part: FADEC — MALFUNCTIONED (LT ENGINE) · airframe 20,636 hrs · 15,217 cycles

PDX - "L FADEC" CAUTION MSG. ALL ENGINE INDICATIONS NORMAL. RETURNED TO THE FIELD. LANDED BELOW MAX LANDING WEIGHT. MDC MESSAGE L FADEC FAILED SWITCH VERSION - DISAGREE SOFTWARE CHECK SUMS (A+B) DISAGREE. LABEL BIT 355A - 23 (BUILT IN TEST) FLAGGED WITH ONE. ATTEMPTED CLEAR OF MESSAGE BY MEANS OF IBIT - MESSAGE CHANGED TO FADEC FAULT 1 WITH THE SAME FAULT IN MDC. REMOVED AND REPLACED LEFT FADEC AS A PRECAUTIONARY MEASURE IAW CRJ-700 MM TASK 73-21-01-000-801 + 73-21-01-400-801. PBIT CHECK GOOD. NO MDC MESSAGES RELATED TO FADEC. RETURNED TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8 YR TASK - FWD SERVICE DOOR APERTURE HAS LITE SURFACE CORROSION AROUND THE BASE OF THE LOWER FWD DOOR STOP FITTING AT APPROX FS 325.00 STR 18R. REMOVED LWR FWD DOOR STOP FITTING FOR ACCESS TO CORROSION. REMOVED LOWER SILL ANGLE TO GAIN ACESS TO CORROSION AND REMOVED CORROSION IAW SRM 53-21-23. HFEC IAW CRJ 700 NDTM PART 1, 51-20-006, NO CRACKS NOTED. UT THICKNESS IAW CRJ 700 NDTM PART 1, 51-20-004, HIGH .063 LOW .056. INSPECTED AREA OF BLEND AND FOUND BLEND TO BE OUTSIDE ALLOWABLE LIMITS IAW SRM 53-21-23 WITH .007, REMOVED AND IS BEYOND 10 PERCENT OF THE ORIGINAL THICKNESS. MAPPED FOR ENGINEERING. ALODINED, PRIMED, AND PAINTED REWORKED AREA IAW REO 670-53-21-485 DISPOSITION STEP 3. INSTALLED LOWER SILL ANGLE TO AIRCRAFT STRUCTURE WITH SOLID RIVETS IAW CRJ 700 SRM 51-42-06. COMPLETED REO 670-53-21-485 BY APPLYING CORROSION INHIBITING COMPOUND TO AFFECTED AREA. INSTALLED LOWER FWD DOOR STOP WITH ORIGINAL HARDWARE, COMPLIED WITH ADJUSTMENT IAW CRJ 700 AMM 52-41-00-82-801-A01 1-4A(18). AREA OF BLEND FOUND WITHIN LIMITS IAW REO 670-53-21-485, COMPLETED ADJUSTMENTS IAW CRJ 700 AMM TASK 52-41-00-820-801 PARA 4A(19)-5D.

Part: PANEL — CHAFED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8 YEAR TASK - AT APPROX FS 985 WHERE PANELS 196DR AND 195DL COME TOGETHER AT AFT END THERE ARE 2 CIRCULAR CHAFES WITH DENTS AND 1 LONGITUDINAL CHAFE ABOUT 1.5 INCH LONG. REMOVED 3 RIVETS AT APPROX FS 985 AND STR 27. BLENDED DAMAGE AND MAPPED FOR ENGINEERING. UT THICKNESS CHECK OF BLENDED AREA IAW CRJ 700 NDTM PT 1, 51-20-004. HIGH .110 LOW .062. CUT OUT DAMAGE PER REO 670-53-61-501 SHT 4 STEP 1. HFEC INSP CUTOUT FOR CRACKS IAW REO 670-53-61-501 NOTE 2, NO CRACKS NOTED. FABRICATED DOUBLER AND FILLER PIECES IAW REO 670-53-61-501 AND LOCATED NEW HOLES FOR FIELD FASTENERS AS NEEDED PER SAME REO. FABRICATED DOUBLERS (ITEM 12) AND TAPERED SHIMS (ITEMS 7&8), REAMED ALL HOLES TO FINAL SIZE, COUNTERSUNK NECESSARY HOLES AND DEBURRED ALL HOLES IAW REO 670-53-61-498 NOTES 4-8. FINISHED CUT EDGE AND FABRICATED PARTS IAW REO 670-53-61-498 NOTES 3 AND 11. FILLED REDUNDANT COUNTERSINKS AS APPLICABLE IN REF REO 670-53-61-501/3. INSTALLED HI-LOKS AND COMPLETED INSTALL OF FASTENERS IN REPAIR DOUBLERS AND TAPERED SHIMS REF REO 670-53-61-501 AND REO 670-53-61-498 SHT 4 ITEMS 12,13,15, AND 16. COMPLIED WITH MOD IS670538200021 AS PER REO 670-53-61-501 SHT 4 ITEM 14, COMPLETED STEP 17 SHT 4 OF REO 670-53-61-501.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

RT OUTBOARD SEAT TRACK FROM STA FS 795-802 HAS LIGHT CORROSION ON THE TOP OF THE TRACK AND IN THE CHANNEL. BLENDED CORROSION ON RT OUTBOARD SEAT TRACK FROM FS 795 TO FS 802 TO A MAX DEPTH OF .021 INCH IN UPPER RADIUS INSIDE CHANNEL. ORIGINAL MATERIAL THICKNESS .270 INCH AND REMAINING THICKNESS FOUND TO BE .249 INCH. BLENDED AREA FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED EMERGENCY EXIT AFT PANEL (262FRW) TO FOM IAW AMM TASK 25-26-09-000-801(A01). REMOVED SIDEWALL PANEL 262 HRW TO FOM IAW AMM TASK 25-26-01-000-801 (A08). REMOVED EFFECTED SEAT TRACK IAW AMM TASK 53-00-49-000-801(A01) PARA 1-3A AND 4A(4).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

RT OUTBOARD SEAT TRACK FROM STA FS 808-811 HAS CORROSION ON THE TOP OF THE TRACK AND IN THE CHANNEL. BLENDED CORROSION ON THE RT OUTBOARD SEAT TRACK FROM FS 808-811 TO A MAX DEPTH OF.021 INCH IN LOWER RADIUS INSIDE CHANNEL. ORIGINAL MATERIAL THICKNESS .270 INCH AND REMAINING THICKNESS FOUND TO BE .249 INCH. BLENDED AREA FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED EMERGENCY EXIT AFT PANEL TO FOM (262FRW) IAW AMM 25-26-09-000-801 (A01). REMOVED SIDEWALL PANEL 262HRW TO FOM IAW AMM 25-26-01-000-801(A08). REMOVED EFFECTED SEAT TRACK IAW AMM 53-00-49-000-801 (A01) PARA 1-3A AND 4A(4).

Part: DIAPHRAGM — CRACKED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8 YR TASK - THERE IS A CRACK ON A DIAPHRAGM AT APPROX FS 8879 FOR THE SKIN WING TO FUSELAGE FAIRING AREA. MAPPED FOR ENGINEERING. REMOVED DAMAGE AND DIAPHRAGM AS PER REO 670-53-82-377 PG 3 STEPS 1 & 2. HFEC INSP CUTOUT FOR CRACKS IAW NDTM PT 1, 51-20-006 & REO 670-53-82-377 NOTE 3. NO CRACKS NOTED. BEGAN FABRICATION OF REPAIR PIECES AS PER REO 670-53-82-377 PG 3 STEP 4&5. COMPLETED FABRICATION OF REPAIR ANGLES, SHIMS AND SPACERS AS PER REO 670-53-82-377 PG 3&4. C/W REPAIR AT WING TO FUSELAGE SUPPORT AT FS 909 AS PER REO 670-53-82-377.

Part: SKIN — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8YR TASK - CORROSION ON FWD CENTER PORTION OF LAV SERVICE DOOR APERTURE. REMOVED CORROSION PER RD 8/4-53-347. REMOVED RIVETS TO FOM PER RD 8/4-53-347. HFEC INSP BLENDED AREA FOR CRACKS IAW Q400 NDTM PT 6, 51-00-01-250-801. NO CRACKS NOTED. UT THICKNESS CHECK IAW Q400 NDTM PT 1, 51-00-04. HIGH .075 LOW .044. BLENDED AREA IS .046 REMAINING THICKNESS AND OUT OF LIMITS PER RD 8/4-53-347. CUT OUT DAMAGED AREA PER RD 8/4-53-347. HFEC IAW -8 400 NDTM PT 6, 51-00-01. NO CRACKS NOTED. FABRICATED PACKERS AND BACKING PLATE, ALODINED AND PRIMED PER RD 8/4-53-347. INSTALLED TWO REPAIR PACKER AND BACKING PLATE AND COMPLIED WITH STEPS 4-11 OF RD 8/4-53-347 SHEET 9.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8 YR TASK - ON THE RT OUTBOARD SEAT TRACK AT FS 521 TO 539 THERE ARE LITE SCRATCHES AND LITE CORROSION. BLENDED AREA OF TRACK AND FOUND AREA OF BLEND TO BE OUT OF LIMITS IAW REO 670-53-00-013 WITH .047 INCH OF MATERIAL REMOVED FROM TOP LUGS OF TRACK. REMOVED SEAT TRACK FROM FS 485 TO 570 IAW CRJ AMM TASK 53-00-49-000-801 ITEM 1-4A (1). INSTALLED NEW TRACK FROM STOCK IAW CRJ AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8 YR TASK - AFT CABIN LT INBOARD SEAT TRACK HAS CORROSION CHANNEL AND ON TOP OF LUGS AT FS 967. REMOVED CORROSION ON TRACK CHANNEL AND TOP AT FS 967 LT INBOARD. MAX AMOUNT OF MATERIAL REMOVED WAS .003. BLENDED AREA IS IN LIMITS, IAW BOMBARDIER REO 670-53-00-013 NOTE 1. COMPLETED REPAIR OF SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8 YR TASK - RT INBOARD SEAT TRACK AT APPROX FS 923 IS GOUGED ON THE TOP AND INSIDE OF THE SEAT TRACK. BLENDED AREA OF DAMAGE AND FOUND BLEND TO BE WITHIN LIMITS IAW REO 670-53-00-013 WITH .012 INCH OF MATERIAL REMOVED FROM THE TOP OF TRACK AND .011" FROM INSIDE LUG. FPI BLEND AREA FOR CRACKS IAW REO 670-53-00-013, HORIZON AIR NDTM SEC 8.2. NO CRACKS NOTED. COMPLETED REPAIR OF SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8 YR TASK - ON THE RT OUTBOARD SEAT TRACK AT FS 411 THERE ARE SMALL SCRATCHES ON THE TRACK. BLENDED AREA OF DAMAGE AND FOUND TRACK TO BE WITHIN LIMITS IAW REO 670-53-00-013 WITH .007 MATERIAL REMOVED FROM TOP LUGS OF TRACK. FPI BLENDED AREA FOR CRACKS IAW REO 670-53-00-013 AND HORIZON NDTM SEC 8.2, NO CRACKS NOTED. COMPLETED REPAIR OF SEAT TRACK IAW REO 670-53-00-013 NOTE 2-9.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8 YR TASK - ON THE OUTBOARD SEAT TRACK AT FS 429 THERE ARE SMALL SCRATCHES ON THE TRACK. BLENDED AREA OF DAMAGE AND FOUND TRACK TO BE WITHIN LIMITS IAW REO 670-53-00-013 WITH .031 INCH OF MATERIAL REMOVED FROM TOP LUGS OF TRACK AND .007 INCH REMOVED FROM INSIDE TRACK. FPI BLENDED AREA FOR CRACKS IAW REO 670-53-00-013 AND HORIZON AIR NDTM SEC 8.2. NO CRACKS NOTED. COMPLETED REPAIR OF SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8 YR TASK - ON THE RT OUTBOARD SEAT TRACK AT FS 381 THERE ARE SMALL SURFACE SCRATCHES. BLENDED AREA OF DAMAGE AND FOUND TRACK TO BE WITHIN LIMITS IAW REO 670-53-00-013 WITH .015 INCH MATERIAL REMOVED FROM TOP SURFACE OF TRACK. FPI BLENDED AREA FOR CRACKS IAW REO 670-53-00-013 AND HORIZON AIR NDTM SEC 8.2, NO CRACKS NOTED. COMPLETED REPAIR OF SEAT TRACK IAW REO 670-53-00-013 NOTE 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8 YR TASK - AFT CABIN LT INBOARD SEAT TRACK HAS CORROSION IN CHANNEL AND ON TOP OF LUGS AT FS 863. REMOVED CORROSION ON TRACK CHANNEL TOP OF FS 863. LT INBOARD MAX AMOUNT OF MATERIAL REMOVED WAS .020. BLEND AREA IS IN LIMITS IAW BOMBARDIER REO 670-53-00-013. COMPLETED REPAIR OF SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8 YR TASK - AFT CABIN LT INBOARD SEAT TRACK HAS CORROSION CHANNEL AND ON TOP OF LUGS AT FS 897. REMOVED CORROSION ON TRACK CHANNEL AND TOP AT FS 897 LT INBOARD. MAX AMOUNT OF MATERIAL REMOVED WAS .012. BLENDED AREA IS IN LIMITS, IAW BOMBARDIER REO 670-53-00-013. COMPLETED REPAIR OF SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8 YR TASK - AFT CABIN LT INBOARD SEAT TRACK HAS CORROSION IN CHANNEL AND ON TOP OF LUGS AT FS 927. REMOVED CORROSION ON TRACK CHANNEL AND TOP AT FS 927 LT INBOARD. MAX AMOUNT OF MATERIAL REMOVED WAS .018. BLENDED AREA IS IN LIMITS, IAW BOMBARDIER REO 670-53-00-013 NOTE 1. COMPLETED REPAIR OF SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8 YR TASK - AFT CABIN LT INBOARD SEAT TRACK HAS CORROSION IN CHANNEL AND ON TOP OF LUGS AT FS 954. REMOVED CORROSION ON TRACK CHANNEL AND TOP AT FS 954 LT INBOARD. MAX AMOUNT OF MATERIAL REMOVED WAS .011. BLENDED AREA IS IN LIMITS, IAW BOMBARDIER REO 670-53-00-013 NOTE 1. COMPLETED REPAIR OF SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8 YR TASK - ON THE RT OUTBOARD SEAT TRACK AT FS 460 TO 466 THERE ARE AREAS OF LITE CORROSION. BLENDED AREA OF DAMAGE AND FOUND TRACK TO BE WITHIN LIMITS IAW REO 670-53-00-013 WITH .007 INCH MATERIAL REMOVED FROM TOP SURFACE OF LUGS AND .005 INCH FROM INSIDE TRACK. COMPLETED REPAIR OF SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8 YR TASK - AFT CABIN LT INBOARD SEAT TRACK HAS CORROSION CHANNEL AND ON TOP OF LUGS AT FS 913. REMOVED CORROSION ON TRACK CHANNEL AND TOP AT FS 913 LT INBOARD. MAX AMOUNT OF MATERIAL REMOVED WAS .003. BLENDED AREA IS IN LIMITS, IAW BOMBARDIER REO 670-53-00-013 NOTE 1. COMPLETED REPAIR OF SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8 YR TASK - RT INBOARD SEAT TRACKS BETWEEN FS 469.00 - 533.00, FS 534.00 - 597.00, FS 598.00 - 677.00, FS 678.00 - 693.00 SHOW SIGNS OF CORROSION IN MULTIPLE PLACES ON THE CLAW AND CHANNEL AREAS. BLENDED DEEPEST AREA OF DAMAGE AND FOUND BLENDS TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED AND REPLACED SECOND AND THIRD SEAT TRACK REF 700 AMM 53-00-49 FIG 405 39, 40, CC, BB. CLEANED, PREPPED AND ALODINED SHORT TRACK SECTION LT INBOARD RAIL. REF AMM 53-00-49 PG 458 NR 24. REF REO 670-53-00-013 NOTE 3 SHT 2 AND CRJ SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8YR TASK - ON THE LT OUTBOARD SEAT TRACK AT FS 610.00 TO FS 632.00 THERE ARE AREAS OF CORROSION. BLENDED CORROSION ON LT OUTBOARD SEAT TRACK FS 610 TO 632 IS SERVICEABLE IAW REO 670-53-00-013 NOTE 1. MAX MATERIAL REMOVED ON SURFACE IS .015. COMPLETED REPAIR ON SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8 YR TASK - RT OUTBOARD SEAT TRACK FROM STA FS 853 TO 857 HAS LITE CORROSION ON THE TOP OF THE TRACK AND IN THE CHANNEL. BLENDED CORROSION ON RT OUTBOARD SEAT TRACK FROM FS 853 - FS 857 TO A MAX DEPTH OF .007 INCH IN SEAT TRACK CHANNEL AND .002 INCH ON TOP OF SEAT TRACK LIP. BLENDED AREAS WERE FOUND TO BE WITHIN LIMITS IAW REO 670-53-00-013. COMPLETED REPAIR OF SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8YR TASK - ON THE LT OUTBOARD SEAT TRACK AT FS 557.00 TO FS 568.00 THERE ARE AREAS OF CORROSION. BLENDED OUT DAMAGE IAW REO 670-53-00-013 NOTES 1 AND 2. MEASURED AREA, FOUND TO BE WITHIN LIMITS PER REO 670-53-00-013. MAX MATERIAL REMOVED .006. COMPLETED REPAIR ON SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8YR TASK - ON THE LT OUTBOARD SEAT TRACK AT FS 643.00 TO FS 663.00 THERE ARE AREAS OF CORROSION. BLENDED CORROSION ON LT O/B SEAT TRACK FS 643 TO 663 FOUND TO BE SERVICEABLE IAW REO 670-53-00-013 NOTE 1. MAX MATERIAL REMOVED ON SURFACE IS .016. COMPLETED REPAIR ON SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8YR TASK - LT OUTBOARD SEAT TRACK FROM STA FS 699.00 TO FS 708.00 HAS CORROSION ON THE TOP OF THE TRACK AND IN THE CHANNEL. BLENDED CORROSION ON LT OUTBOARD SEAT TRACK FS 699 TO 708, FOUND TO BE SERVICEABLE IAW REO 670-53-00-013 NOTE 1. MAX MATERIAL REMOVED ON SURFACE IS .002. COMPLETED REPAIR ON SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8YR TASK - LT OUTBOARD SEAT RAIL STA 459.00 TO FS 468.00 HAS LITE CORROSION ON THE TOP OF THE RAIL. BLENDED OUT DAMAGE IAW REO 670-53-00-013 NOTES 1 AND 2. MEASURED AREA, FOUND TO BE WITHIN LIMITS PER REO 670-53-00-013. MAX MATERIAL REMOVED .003. COMPLETED REPAIR ON SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8YR TASK - LT OUTBOARD SEAT TRACK AT FS 796.00 HAS CORROSION ON THE TOP OF THE TRACK. BLENDED CORROSION ON LT OUTBOARD SEAT TRACK FS 796, MAX MATERIAL REMOVED .015 ON SURFACE FOUND TO BE SERVICEABLE IAW REO 670-53-00-013. COMPLETED REPAIR ON SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8YR TASK - LEFT FWD SEAT RAIL HAS MULTIPLE SPOTS OF CORROSION FROM STA 379.00 TO FS 457.00. BLENDED OUT DAMAGE IAW REO 670-53-00-013 NOTES 1 AND 2. MEASURED AREA, FOUND TO BE WITHIN LIMITS PER REO 670-53-00-013. MAX MATERIAL REMOVED .006. COMPLETED REPAIR ON SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8YR TASK - ON THE LT OUTBOARD SEAT TRACK AT FS 490.00 TO FS 501.00 THE SEAT TRACK IS GOUGED AND CORRODED. BLENDED OUT DAMAGE IAW REO 670-53-00-013 NOTES 1 AND 2. MEASURED AREA, FOUND TO BE WITHIN LIMITS PER REO 670-53-00-013. MAX MATERIAL REMOVED .005. COMPLETED REPAIR ON SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8 YR TASK - RT OUTBOARD SEAT TRACK FROM STA FS 813 TO 826 HAS LITE CORROSION ON THE TOP OF THE TRACK. BLENDED CORROSION ON RT OUTBOARD SEAT TRACK FROM FS 813 - FS 826 TO A MAX DEPTH OF .002 INCH ON TOP OF SEAT TRACK LIP. ORIGINAL MATERIAL THICKNESS OF SEAT TRACK LIP .370 INCH AND REMAINING THICKNESS FOUND TO BE .368 INCH. ALL WORK DONE IAW REO 670-53-00-013. FOUND TO BE IN LIMITS. COMPLETED REPAIR OF SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8YR TASK - LT OUTBOARD SEAT TRACK AT FS 810.00 HAS CORROSION ON THE TOP OF THE TRACK AND IN THE CHANNEL. BLENDED CORROSION ON LT OUTBOARD SEAT TRACK FS 810, MAX MATERIAL REMOVED IS .010 FOUND TO BE SERVICEABLE IAW 670-53-00-013. COMPLETED REPAIR ON SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8YR TASK - LT OUTBOARD SEAT TRACK FROM FS 752.00 TO FS 757.00 HAS CORROSION ON THE TOP OF THE TRACK AND IN THE CHANNEL. BLENDED CORROSION ON LT OUTBOARD SEAT TRACK FS 752 TO 757 IS SERVICEABLE IAW REO 670-53-00-013 NOTE 1. MAX MATERIAL REMOVED ON SURFACE IS .019. COMPLETED REPAIR ON SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8YR TASK - ON THE LT OUTBOARD SEAT TRACK AT FS 522.00 TO FS 536.00 THE SEAT TRACK HAS A GOUGE AND AREAS OF CORROSION. BLENDED OUT DAMAGE IAW REO 670-53-00-013 NOTES 1 AND 2. MEASURED AREA, FOUND TO BE WITHIN LIMITS PER REO 670-53-00-013. MAX MATERIAL REMOVED .012. COMPLETED REPAIR ON SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8YR TASK - LT OUTBOARD SEAT TRACK FROM FS 735.00 TO FS 740.00 HAS CORROSION ON THE TOP OF THE TRACK AND IN THE CHANNEL. BLENDED CORROSION ON LT OUTBOARD SEAT TRACK FS 735 TO 740 IS SERVICEABLE IAW REO 670-53-00-013 NOTE 1. MAX MATERIAL REMOVED ON SURFACE IS .029. COMPLETED REPAIR ON SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,622 hrs · 15,206 cycles

PDX - 8YR TASK - ON THE LT OUTBOARD SEAT TRACK AT FS 581.00 TO FS 600.00 THERE ARE AREAS OF CORROSION. BLENDED OUT DAMAGE IAW REO 670-53-00-013 NOTES 1 AND 2. MEASURED AREA, FOUND TO BE WITHIN LIMITS PER REO 670-53-00-013. MAX MATERIAL REMOVED .006. COMPLETED REPAIR ON SEAT TRACK IAW REO 670-53-00-013 NOTES 2-9.

Part: PANEL — CRACKED (CARGO DOOR) · airframe 19,992 hrs

AFT SIDE PANEL ON THE MCD IS CRACKED NEAR THE POWER ASSIST MOTOR ATTACH BRACKET & BEAM FOR GAS SPRING REF 52-11-04-001-A01. MAPPED AREA FOR ENGINEERING. REMOVED AFT COUNTER BALANCE SYS REF 52-11-17-000-802. REMOVED THE GAS SPRING BEAM REF SRM 51-42-06 FOR RIVET REMOVAL. FOUND ADDITIONAL CRACKS IN SIDE WALL SKIN 2 INCH TO LT OF ORIGINAL CRACK. MAPPED FOR ENGINEERING. CUT OUT DAMAGED AREA PER REO 670-52-11-416. HFEC INSP CUT OUT FOR CRACKS IAW NDTM PART 6, 53-00-000-250-A01. NO CRACKS NOTED & REO 670-52-11-416. FABRICATED DOUBLER FILLERS & SHIMS IAW REO 670-52-11-416. INSTALLED DOUBLER REF SRM 51-42-06, REO 670-52-11-416. RE-INSTALLED AFT PAX DOOR COUNTER BALANCE SYSTEM IAW AMM 52-11-17-400-802-A01.

Part: SUPPORT ANGLE — CRACKED (PAX DOOR) · airframe 19,992 hrs · 14,713 cycles

PDX - C5 - THE MAIN CABIN DOOR LOWER SUPPORT ANGLE FOR THE ASSIST MOTOR IS CRACKED ON THE LOWER END OF THE SUPPORT. REMOVED PAX DOOR MOTOR REF AMM 52-11-08-000-801. REMOVED SUPPORT ANGLE BY REMOVING SOLID RIVETS. MATCH DRILLED NEW LOWER SUPPORT ANGLE TO AIRCRAFT STRUCTURE IAW SRM 51-41-00. INSTALLED SUPPORT ANGLE BY INSTALLING RIVETS, WET IN LOWER SUPPORT ANGLE IAW SRM 51-42-05, 51-23-00. RE-INSTALLED PAX POWER ASSIST MOTOR IAW AMM T 52-11-08-400-801-A02 STEPS 1-4 N/A STEP 4A(1) NOT DISASSEMBLED DURING REMOVAL. COMPLETED INSTALLATION OF ASSIST MOTOR IAW AMM 52-11-08-400-801-A02 PARA 5A-E.

Part: LUG — CRACKED (HORIZONTAL STAB) · airframe 19,992 hrs · 14,713 cycles

PDX - C5 - RT OTBD HORIZONTAL STAB LUG HAS A SMALL CRACK (APPROX .125 INCH) ON UNDER SIDE OF ANTI ROTATION TAB ON AFT SIDE. FPI INSPECTED AT THE AREA IAW CRJ700 NDTM PART 1, 51-20-008 CRACK INDICATION CONFIRMED IAW CRJ 700 NDTM PART 1 51-20-006. MAPPED DAMAGE FOR ENGINEERING. REMOVED CRACK IAW TC REO 670-55-11-145/1 W/O 71869 GENERAL NOTES 1-4. HFEC LOW CRJ 700 NDTM PART 1, 51-20-006 AND REO 670-55-11-145. NO CRACKS NOTED. REPAIRED THE REQUIRED AREA BY ROTO PEENING IAW TC REO 670-55-11-145/1. COMPLETED RT OUTBOARD HORIZ STAB LUG IAW REO 670-55-11-145/1 STEPS 7-9.

Part: BULKHEAD — DAMAGED (BS 2800) · airframe 19,992 hrs · 14,713 cycles

PDX - C5 - RT WEB AT PILOTS BULKHEAD FWD OF FS2800.00 BEAM HAS CORROSION ON LOWER FLANGE P/N670-53-11-052-1. CORROSION ON WEB FOUND TO BE OUT OF LIMITS IAW REO 670-53-11-052. REMOVED OLD WEB FASTENERS IAW REO 670-53-11-052, LOCATED AND DRILLED NEW WEB IAW 670-53-11-052. INSTALLED NEW WEB IAW 670-53-11-052 AND CRJ 700 SRM 51-42-06.

Part: SKIN — DAMAGED (BS 265) · airframe 19,992 hrs · 14,713 cycles

PDX - C5 - BURNED FASTENER APPROX FS 265 2 INCHES ABOVE STRINGER 25 LT. C/W TEMP REPAIR IAW REO 670-53-00-045 REQ PERMANENT REPAIR AT NEXT SCHEDULED C CHECK. REMOVED BLIND RIVET AND INSTALL PERMANENT REPAIR IAW REO 670-53-00-045 PARA 2 STEP A.

Part: TAB — DAMAGED (HORIZONTAL STAB) · airframe 19,992 hrs · 14,713 cycles

DAMAGED LT AND RT ANTI ROTATION TABS OF THE HORIZ STAB PIVOT FITTING P/N AV670-23120, REMOVED PANELS 326CL AND 326CR. REMOVED HORIZ STAB PIVOT BOLT INNER PIN AND LT OUTER PIN, TRIMMED CHAFED LT LOCK TAB IAW TC REO 670-55-11-099 GENERAL NOTES 1-3. COMPLIED WITH EDDY CURRENT INSPECTION IAW REO 670-55-11-102/3 STEP 4. NO CRACKS NOTED. ROTO PEENED BARE AREA IAW REO 670-55-11-099 ON LT TAB. TRIMMED CHAFED RT LOCK TAB IAW TC REO 670-55-11-099 GENERAL NOTES 1-3. PRIOR TO REMOVING RT OUTER PIN INSTALLED LT OUTER PIN IAW TC REO 670-55-11-099 NOTE 6-10. RIL 0146 INSTALLATION STEPS 1-3 NOTE BOTH OUTER PINS AND INNER PIN NEW FROM STOCK. INSTALLED RT OUTER PIN IAW RIL 0146 STEP 1-3, FINISHED INSTALLING HORIZ TAB PIVOT BUSHINGS IAW RIL 0146 STEP 4-10. RE-INSTALLED PANELS 326CL AND 326CR AS REQUIRED.

Part: LUG — GOUGED (HORIZONTAL STAB) · airframe 19,992 hrs · 14,713 cycles

PDX - C5 - FOUND SMALL GOUGE IN THE AFT SIDE ANTI ROTATION LUG DURING REINSTALLATION OF PINS AND BOLTS. REMOVED LT OUTER PIN IAW RIL 0146 STEP 3 AND 4 ALL OTHER STEPS PREVIOUSLY COMPLIED WITH. ELIMINATED GOUGE ON LT AFT SIDE ANTI ROTATION LUG PER REO 670-55-11-099 STEP 3. PERFORMED HFEC INSPECTION ON BLENDED AREA IAW CRJ NDTM 51-20-006. NO CRACKS NOTED. ROTO PEENED REQUIRED AREA IAW REO 670-55-11-099 COMPLIED WITH REO 670-55-11-099 STEPS 1, 6 AND 10 (STEPS 2,6-9 PREVIOUSLY COMPLIED WITH N/R 00048 WO 71869). INSTALLED HORIZ STAB PIVOT BUSHING IAW RIL 0146 INSTALLATION PROCEDURE 1-10.

Part: LUG — DAMAGED (HORIZONTAL STAB) · airframe 19,992 hrs · 14,713 cycles

PDX - C5 - RT OTBD HORIZONTAL STAB LUG P/N AV670-23000 APPEARS TO HAVE BEEN BLENDED BELOW ANTI-ROTATION TAB ON AFT SIDE. BLENDED OUT DAMAGE TO A SMOOTH CONTOUR IAW SRM 51-12-00-001-001-A01 STEPS 1-3, 5.B(1)-(2). MAPPED FOR ENGINEERING. REMOVED DAMAGE IAW TC REO 670-55-11-145/1 W/O 71869 GENERAL NOTES 1-4. HFEC IAW NDTM PART 1 51-20-006, NO CRACKS NOTED. REPAIRED THE REQUIRED AREA BY ROTO PEENING THE AREA IAW TC REO 670-55-11-145/1. COMPLETED RT COMPLETED RT OUTER HORIZ STAB LUG IAW REO 670-55-11-145/1 STEP 7-9.

Part: ANGLE — DAMAGED (STAB TO FUSELAGE) · airframe 19,992 hrs · 14,713 cycles

LEFT SIDE CONNECTING ANGLE FOR THE VERTICAL STAB TO THE FUSELAGE IS POSSIBLY CRACKED APPROX 1 INCH AT VERTICAL STAB STRINGER DATUM 67.5 PERCENT. HFEC INSPECTED SUSPECTED CRACK IAW NDTM 51-20-006. CONFIRMED CONNECTING ANGLE IS CRACKED. DRILLED OUT FASTENERS AND CUT OUT CRACKED ANGLE REF REO 670-55-31-018. THIRD FASTENER FROM FWD EDGE BOTTOM ROW OF VERTICAL. FABRICATED PACKER AND REPAIR DOUBLER REF REO 670-55-31-018. HFEC INSPECTED AT CUTOUT FOR CRACK IAW NDTM PART 1 51-20-006. NO CRACK NOTED. REPAIRED IAW REO670-55-31-018, 670-55-31-043.

Part: SKIN — GOUGED (BS 220) · airframe 19,992 hrs · 14,713 cycles

PDX - C5 - THERE ARE SEVERAL SMALL GOUGES ON THE LT FUSELAGE SKIN AT APPROX FS 220 BETWEEN THE SECOND AND FOURTH STRINGERS FROM THE BOTTOM CENTER STRINGER. BLENDED 3 AREA IAW SRM 53-11-01. INSPECTED BLENDS AND FOUND TO BE OUT OF LIMITS IAW 53-00-01. HFEC INSP BLENDS FOR CRACKS IAW NDTM SEC 6. 53-00-000-250-A01. NO CRACKS NOTED. MAPPED FOR ENGINEERING. ETCHED ALODINED IAW SRM 51-21-16. APPLIED PRIMER AND TOPCOAT IAW SRM 51-21-16, REO 670-53-11-409/3.

Part: BEAM — CRACKED (BS 280) · airframe 19,992 hrs · 14,713 cycles

FS 280 BEAM CRACKED ON LOWER FLANGE APPROX 12 INCHES RT FROM CENTERLINE OF ACFT. HFEC INSPECTED SUSPECT CRACK IAW NDTM 51-20-006 CONFIRMED APPROX 1 INCH CRACK. REMOVED RT DRIP TRAY ATTACHING INTERCOSTALS, CAMLOC CHANNEL AND RT SECTION OF 280 BEAM. LOCATED NEW RT SIDE 280 BEAM, OUTBOARD OF CENTER SPLICE IAW SRM 51-40-11. CUT NEW BEAM SECTION AND COMPLETED DRILLING REF SRM 51-40-11. INSTALLED INBOARD INTERCOSTAL AND OUTBOARD INTERCOSTAL IAW SRM 51-42-21. INSTALLED FASTENERS AND RIVETS IN CENTER SPLICE AREA IAW REO 670-53-11-045. INSTALLED DRIP TRAY IAW SRM 51-42-06 AND 51-42-13.

Part: CHANNEL — CORRODED (BS 280) · airframe 19,992 hrs · 14,713 cycles

CAMLOCK CHANNEL ON FWD SIDE OF CENTER 280.00 BEAM IS CORRODED. CAMLOCK CHANNEL REMOVED, DRILLED UP NEW CAMLOCK CHANNEL AND DEBURRED CRJ SRM 51-42-06-001-001-A01. INSTALL NEW CAMLOCK CHANNEL AND CAMLOCKS IAW CRJ SRM 51-42-06-001-001-A01.

Part: STIFFENER — LOOSE (MLG WW) · airframe 19,992 hrs · 14,713 cycles

PDX - C5 - FWD OF RT WHEEL BIN CUTOUT AT X797.63 WEB STIFFENER FASTENERS ARE LOOSE AND HAVE CAUSED STEP WEAR. REMOVED AND REPLACED WEB STIFFENER IN RT WHEEL WELL AS PER SRM 51-40-15 AND 51-42-00.

Part: STIFFENER — LOOSE (FUSELAGE) · airframe 19,992 hrs · 14,713 cycles

FWD OF LT WHEEL BIN CUTOUT AT X797.63 WEB STIFFENER FASTENERS ARE LOOSE AND HAVE CAUSED STEP WEAR. REMOVED AND REPLACED WEB STIFFENER IN LT WHEEL WELL AS PER CRJ 700 SRM 51-40-15 AND 51-42-00.

Part: STRUCTURE — CHAFED (LT AILERON) · airframe 19,992 hrs · 14,713 cycles

LEFT WING AILERON LEADING EDGE IS CHAFED ON CENTER AND OTBD EDGE. BLENDED DAMAGED AREA REF SRM 57-61-01-101-001-A01. HFEC INSPECTED BLENDED AREA FOR CRACKS IAW NDTM PART 6, 53-00-000-250-A01. NO CRACKS NOTED. UT THICKNESS CHECK IAW NDTM PART 1, 51-20-004 HIGH .087 LOW .084 FOR CENTER HINGE POINT AREA OF AILERON. CHECKED OTBD EDGE OF AILERON SKIN FOUND MAX MATERIAL REMOVED TO BE .003. BOTH SPOTS WITHIN LIMITS REF SRM 57-61-01-101-001-A01 TABLE 2. ALODINE, PRIMED AND PAINTED AREA REF SRM 51-21-11, 51-25-16 AND 51-25-21. AREA IS LESS THAN 6 INCHES AND LESS THAN 22 PERCENT. NO ADDITIONAL INSPECTION REQUIRED.

Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 19,992 hrs · 14,713 cycles

PDX - C5 - RT FLAP OUTBOARD MOVEABLE VANE HAS CHAF ON LOWER LEADING EDGE AT WS 272.00. BLENDED AREA TO MAX DEPTH OF .014 INCH WITHIN LIMITS REF SRM 57-53-01-101-001-A01 TABLE 1. PREPPED AND RESTORED FINISH TO BLENDED AREA REF SRM 51-25-01 PG 12 PARA 2-A-G.

Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 19,992 hrs · 14,713 cycles

PDX - C5 - RT FLAP OUTBOARD MOVEABLE VANE BRACKET AT WS 220 HAS WEAR AND SHARP EDGES. REMOVED SHARP EDGES, WEAR WITHIN LIMITS REF SRM 57-53-01-101-001-A01 TABLE 2. PREPPED AND RESTORED FINISH TO AFFECTED AREA REF SRM 51-25-01 PAGE 12 PARA 2-A-G.

Part: SKIN — CORRODED (BS 437) · airframe 19,992 hrs · 14,713 cycles

PDX - C5 - THERE ARE TWO CORRODED RIVETS AT FS 437, THREE STRINGERS FROM THE BOTTOM ON THE LT SIDE OF THE FUSELAGE. REMOVED 2 RIVETS AT FS 437 STR 25L. INSPECTED AREA WITH HF EDDY CURRENT AS PER MAINTENANCE REQUEST, NO CRACKS NOTED, REF NDT MANUAL PART 01 51-20-006. INSTALLED TWO RIVETS IAW CRJ 700 SRM 51-42-06.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 19,992 hrs · 14,713 cycles

PDX - C5 - RT FLAP OUTBOARD MOVEABLE VANE HAS CHAFING ON INBOARD UPPER SURFACE AT WS 166.00. BLENDED DAMAGE TO MAX DEPTH OF .004 INCH WITHIN LIMITS REF SRM 57-53-01-101-001-A01 TABLE 1 PREPPED AND RESTORED FINISH TO BLENDED AREA REF SRM 51-25-01 PG 12 PARA 2-A-G.

Part: SKIN — DAMAGED (BS 485) · airframe 19,992 hrs · 14,713 cycles

PDX - C5 - LIGHTNING STRIKE ON FUSELAGE SKIN REQUIRES PERMANENT REPAIR AT FS 485.00 AND STRINGER 25L PER REO670-53-135/3. REMOVED FASTENERS FROM REPAIR AREA, CUT OUT DAMAGE AND DEBURRED IAW TC REO670-53-31-135/3. HFEC INSPECTED AT CUT OUT AND UNDERLYING STRUCTURE FOR CRACK IAW NDTM PART 1, 51-20-006. NO CRACKS NOTED. FABRICATED DOUBLER AND PACKER, DRILLED , COUNTERSUNK AND DEBURRED. ALODINED AND PRIMED ALL BARE METAL. INSTALLED COUNTERSINK FILLERS IAW TC REO 670-53-31-135/3. INSTALLED DOUBLER IAW TC REO670-53-31-135/3.

Part: TRANSDUCER — FAILED (WHEEL SPEED) · airframe 19,822 hrs · 14,579 cycles

PDX - AFTER BRAKE APPLICATION, NR 3 BRAKE HEATS UP MORE RAPIDLY AND HOTTER THAN NR 4 (7 VS 2); ALSO RIGHT BRAKE IS NOTICEABLY WEAKER THAN LEFT BRAKE. REMOVED AND REPLACED NR 3 MLG BRAKE ASSY, NO HELP. REMOVED AND REPLACED NR 4 MLG WHEEL SPEED TRANSDUCER. OP'S CHECKS ARE GOOD. ALL 4 BRAKE TEMPS HEAT UP EVENLY AND WITHIN LIMITS. MAINTENANCE PERFORMED IAW MTC NR R324301, AMM TASKS NR 32-44-01-000-801-A01 AND NR 32-44-01-400-801-A01. RETURNED TO SERVICE.

Part: FUSE — FAILED (BRAKES) · airframe 19,407 hrs · 14,231 cycles

PDX RT OUTBOARD BRAKE DOESN’T WORK, AIRCRAFT PULLS TO LEFT AND THE RT OUTBOARD BRAKE STAYS COLD. REPLACED RT OUTBOARD BRAKE VOLUMETRIC FUSE & NR 4 BRAKE, OPS TEST GOOD. RETURNED TO SERVICE.

Part: SPRING — BROKEN (PAX DOOR HANDLE) · airframe 16,668 hrs · 11,982 cycles

ONT - FLIGHT 2624.; AFTER TAKEOFF, THE REAR SERVICE DOOR WARNING LIGHT ILLUMINATED, THEN RECEIVED A PROX SENSOR INDICATION. HANDLE ON THE DOOR STARTED TO MOVE UP. THE REAR FLIGHT ATTENDANT WAS UNABLE TO KEEP THE HANDLE DOWN. DIVERTED TO ONT AND ACCOMPLISHED A UNEVENTFUL LANDING. NO EMERGENCY OR CFR CALLED. MAINTENANCE FOUND A BROKEN SPRING ON THE INNER HANDLE DETENT. REPLACED THE SPRING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DCU — SMOKE (NR 2) · airframe 16,661 hrs · 11,977 cycles

YEG- ON TAXI (APU POWER ON), THE CIRCUIT BREAKER FOR THE DCU 2 POPPED. SMOKE FROM THE H13 CIRCUIT BREAKER (EICAS). CIRCUIT BREAKER DID NOT POP. RECEIVED MULTIPLE FAULT STATUS MESSAGES FOR THE DCU 2 AND DCU AURAL 2 FAILURE. EVACUATED AIRCRAFT. MAINTENANCE REPLACED THE DCU NR 2 AND THE CIRCUIT BREAKERS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: HOUSING — CRACKED (E/E BAY DOOR) · airframe 15,538 hrs · 11,184 cycles

AVIONICS DOOR HANDLE HOUSING CRACKED AROUND THE SHAFT. REPLACED THE HANDLE HOUSING. OPERATIONAL CHECKS GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (CARGO DOOR) · airframe 15,445 hrs · 11,125 cycles

PDX - FLIGHT 2565 (PDX-ONT), AFTER TAKEOFF DURING CLIMB, RECEIVED A AFT CARGO DOOR WARNING MESSAGE. NO LOSS OF CABIN PRESSURE. CIRCLED FOR 30 MINUTES TO BURN OFF FUEL AND RETURNED TO PDX AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE ADJUSTED THE PX-102 PROX SENSOR IAW AMM 52-70-02-400-802-A02. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WARNING SYSTEM — FALSE ACTIVATION (CARGO DOOR) · airframe 15,248 hrs · 11,005 cycles

SEA - AT FLIGHT LEVEL 34,000, AFT CARGO DOOR WARNING ILLUMINATED FOLLOWED BY A PROX SYSTEM 2 FAULT MESSAGE. MAINTENANCE INSPECTED THE DOOR AND SURROUND WITH NO DEFECTS NOTED. OPERATIONAL CHECK OF THE AFT CARGO DOOR GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: UNKNOWN — UNKNOWN (ENGINE) · airframe 15,164 hrs · 10,945 cycles

PDX - FLIGHT 2262, AFTER ENGINE START, RT BLEED CLOSED AND LT BLEED CLOSED. MAINTENANCE PLACED ON MEL 36-12-2. 8/1. PERFORMED OPERATIONAL TEST WITH NO DEFECTS. CLEARED MEL. AIRCRAFT RETURNED TO SERVICE WITH NO PARTS REPLACED.

Part: LATCH — CRACKED (THRUST REVERSER) · airframe 14,993 hrs · 10,828 cycles

C3 OKC - NR 2 ENGINE LOWER TRANSCOWL CENTER LATCH CUTOUT CORNER IS CRACKED. REPAIRED IAW SRM 51-42-06, 51-42-13, 51-21-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 14,993 hrs · 10,828 cycles

C3 OKC - FLIGHT DECK CENTER FLOORBOARD AFT SUPPORT ANGLE HAS CORROSION ON LOWER SURFACE. REPAIRED IAW SRM 51-40-00, 51-42-06.

Part: STIFFENER — CRACKED (BS 280) · airframe 14,993 hrs · 10,828 cycles

C3 OKC - FS 280 STIFFENER AT RBL 21 CRACKED AT BOTTOM RIVET. REPAIRED IAW SRM 51-42-06, 51-25-06.

Part: FRAME — CRACKED (RT NACELLE) · airframe 14,993 hrs · 10,828 cycles

C3 OKC - RIGHT LOWER TRANS COWL CENTER FRAME CRACKED ON OUTBOARD SIDE. REPAIRED IAW REO670-54-21-814.

Part: SKIN — DENTED (FUSELAGE) · airframe 14,993 hrs · 10,828 cycles

C3 OKC - REPAIR DENT IN FUSELAGE SKIN PER REO 670-53-11-228. REPAIRED IAW REO 670-53-11-228.

Part: SKIN — CORRODED (FUSLEAGE) · airframe 14,993 hrs · 10,828 cycles

C3 OKC - FORWARD LOWER FUSELAGE SKIN UNDER LOWER ADF ANTENNA AROUND RIGHT AFT MOUNT HOLE THERE IS CORROSION. REPAIRED IAW SRM 51-21-06, 53-22-21, 51-21-11.

Part: UNKNOWN — CRACKED (BS 280) · airframe 14,993 hrs · 10,828 cycles

C3 OKC - FS 280 AT LBL 9 IS CRACKED. REPAIRED IAW REO670-53-11-045.

Part: UNKNOWN — CORRODED (BS 280) · airframe 14,993 hrs · 10,828 cycles

C3 OKC - FS 280 AT RBL 9 AFT SIDE HAS CORROSION. REPAIRED IAW SRM 51-42-06, 51-42-21.

Part: SKIN — DAMAGED (PAX DOOR) · airframe 14,993 hrs · 10,828 cycles

C3 OKC - PASSENGER DOOR EXTERNAL SKIN FORWARD UPPER CORNER HAS SEVERAL DEEP SCRATCHES. REPAIRED IAW SRM 51-12-00, 51-21-11.

Part: SKIN — CORRODED (FUSELAGE) · airframe 14,993 hrs · 10,828 cycles

C3 OKC - LOWER TCAS MOUNT SKIN HAS LIGHT CORROSION. REPAIRED IAW SRM 51-21-06, 53-00-01.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 14,993 hrs · 10,828 cycles

C3 OKC - PASSENGER DOOR LOWER EDGE MEMBER CRACKED ON FORWARD AND AFT EDGE. REPAIRED IAW REO 601R-52-11-279.

Part: SKIN — CHAFED (RT TE FLAP) · airframe 14,993 hrs · 10,828 cycles

C3 OKC - RIGHT FLAP LEADING EDGE 684EB CHAFED AT CUTOUT. REPAIRED IAW SRM 51-12-00, 51-21-11, 51-25-06, 57-52-01.

Part: PANEL — CHAFED (RT TE FLAP) · airframe 14,993 hrs · 10,828 cycles

C3 OKC - RIGHT FLAP LEADING EDGE PANEL 684JB CHAFED AT CUTOUT. REPAIRED IAW SRM 51-12-00, 51-21-11, 51-25-06, 57-52-01.

Part: PANEL — CHAFED (RT TE FLAP) · airframe 14,993 hrs · 10,828 cycles

C3 OKC - RIGHT FLAP LEADING EDGE 684GB CHAFED AT CUTOUT. REPAIRED IAW SRM 51-12-00, 51-21-11, 57-52-01.

Part: PANEL — CHAFED (LT WING) · airframe 14,993 hrs · 10,828 cycles

C3 OKC - LEFT WING PANEL 584GB CHAFED. REPAIRED IAW SRM 51-12-00, 51-25-06, 57-52-01.

Part: PANEL — CHAFED (LT WING) · airframe 14,993 hrs · 10,828 cycles

C3 OKC - LEFT WING PANEL 584JB CHAFED. REPAIRED IAW SRM 51-12-00, 57-52-01, 51-21-11.

Part: PANEL — CHAFED (LT WING) · airframe 14,993 hrs · 10,828 cycles

C3 OKC - LEFT WING PANEL 584ET CHAFED. REPAIRED IAW SRM 51-12-00, 57-52-01, 51-21-11.

Part: PANEL — CHAFED (RT TE FLAP) · airframe 14,993 hrs · 10,828 cycles

C3 OKC - RIGHT FLAP LEADING EDGE PANEL 684LB CHAFED AT CUTOUT. REPAIRED IAW SRM51-12-00, 57-52-01, 51-25-06.

Part: UNKNOWN — UNKNOWN · airframe 14,773 hrs · 10,686 cycles

OAK - INTERMITTENT FIDEEX FIRE FAULT MESSAGE. MAINTENANCE PLACED ON MEL. MEL CLEARED BY PERFORMING A OPERATIONAL CHECK WITH NO FAULTS FOUND. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: A/C PACK — MALFUNCTIONED (RIGHT) · airframe 14,493 hrs · 10,504 cycles

PDX - FLIGHT 2555, UNABLE TO CONTROL RIGHT AIR CONDITIONING PACK TEMPERATURE IN AUTO OR MANUAL POSITIONS. RETURNED TO THE GATE. MAINTENANCE PLACED THE AIR CONDITIONING PACK ON MEL 21-51-1B. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL PANEL — MALFUNCTIONED (AILERON TRIM) · airframe 14,388 hrs · 10,438 cycles

SEA- UNABLE TO TRIM THE AILERONS TO THE LEFT. MAINTENANCE REPLACED THE AILERON/RUDDER TRIM CONTROL PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (APU) · airframe 13,932 hrs · 10,148 cycles

PSP - FLIGHT 2580, AT PUSHBACK RECEIVED A APU LOAD CONTROL VALVE OPEN CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE RESET ALL CIRCUIT BREAKERS. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: FIRE LOOP — MALFUNCTIONED (RT NACELLE) · airframe 13,864 hrs · 10,096 cycles

SEA - FIRE SYSTEM FAULT STATUS MESSAGE APPEARED INTERMITTENTLY. MAINTENANCE FOUND A RIGHT ENGINE FIRE LOOP A MESSAGE IN THE MDC. PLACED ON MEL 26-00-1, RSI 268959. AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — LEAKING (ZONE 400) · airframe 13,646 hrs · 9,939 cycles

SMF - FLIGHT 2526, FUEL LEAKING FROM THE LEFT ENGINE WITH THE BOOST PUMPS ON. MAINTENANCE FOUND THE MASTER VG ACTUATOR LEAKING. REPLACED ACTUATOR IAW AMM 75-30-01-000-801-A01. OPERATIONAL CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED · airframe 13,583 hrs · 9,897 cycles

BOI - DURING CRUISE FLIGHT, THE FIRE SYSTEM FAULT CAUTION ILLUMINATED. PER THE CHECKLIST PROCEDURE, THE TEST BUTTON WAS PUSHED AND THE "OK" GREEN STATUS MESSAGE WAS DISPLAYED. MAINTENANCE CYCLED THE CIRCUIT BREAKERS N1, N2, R2 & R3. NO FAULTS RECORDED IN THE MDC. C/W GROUND TEST IAW AMM 26-10-00 PAGES 501-503. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DOOR — LACK OF LUBE (SERVICE DOOR) · airframe 13,452 hrs · 9,811 cycles

PDX- SERVICE DOOR DIFFICULT TO OPEN. MAINTENANCE CLEANED AND LUBRICATED THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DOOR — LACK OF LUBE (SERVICE DOOR) · airframe 13,444 hrs · 9,807 cycles

PDX - GALLEY SERVICE DOOR IS HARD TO OPEN. MAINTENANCE LUBRICATED THE DOOR HANDLE ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CIRCUIT BREAKER — TRIPPED (APU SYS) · airframe 12,006 hrs · 8,805 cycles

SEA - ON FLIGHT 2469 RETURN TO GATE, APU SHUTOFF VALVE FAIL. APU PUMP CAUTION MESSAGE. MAINTENANCE CYCLED BREAKERS. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: SENSOR — FAILED (SERVICE DOOR) · airframe 11,679 hrs · 8,583 cycles

SEA- FLIGHT 2484, ON PUSHBACK, "PROX SYS FAULT 2" STATUS MSG WITH ALL DOOR CLOSED. INTERROGATED MDC AND FOUND FAULT "SERVICE DOOR HL SENSOR PX38 FAILED/WIRING OPEN CIRCUIT." DEFERRED MTX PER MEL 52-70-5 RSI NR 355141 CATEGORY C EXPIRES 04-18-06. AIRCRAFT RETURNED TO SERVICE.

Part: TRANSDUCER — DIRTY (ENGINE OIL) · airframe 11,517 hrs · 8,462 cycles

FAT - ON FLIGHT 2480, RETURNED TO GATE, AFTER ENGINE START, LEFT ENGINE OIL PRESSURE INDICATED FLUCTUATION FROM 0-26 PSI FOR 60-70 SECONDS. DURING THIS TIME, THE OIL TEMPERATURE WS STABLE AT 66 DEGREES, THE OIL QUANTITY WAS STABLE AT 85 PERCENT FULL, AND NO LEFT ENGINE OIL PRESSURE WARNING MESSAGE WAS OBSERVED AFTER THIS TIME PERIOD THE OIL PRESSURE FLICKERED BACK UP TO 47 PSI AND THEN REMAINED STABLE. MAINTENANCE REMOVED CLEANED AND RESEATED NR 2 ENGINE PRESSURE TRANSDUCER. GROUND RAN, NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: PRECOOLER — CRACKED (NR 2 A/C PACK) · airframe 11,229 hrs · 8,262 cycles

BUR - ON CLIMB FOR FLIGHT 2508, RIGHT ENGINE BLEED CAUTION MESSAGE CAME ON 1 MIN AFTER T/O. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. FOUND NR 2 AIR CONDITIONING PACK PRECOOLER CRACKED CAUSING THIS DISCREPANCY. AFTER ISOLATING THIS DEFECT RAN BOTH ENGINE'S AND APU BLEED'S NO OTHER DISCREPENCIES NOTED. BLEED AIR FROM THIS CRACK WAS BLOWING UPON SENSE LOOPS. FERRIED AIRCRAFT TO PDX. REMOVED AND REPLACED RT PRECOOLER IAW CRJ 700 AMM TASK 21-53-04-400-801-A01. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL PANEL — MALFUNCTIONED (AUDIO) · airframe 11,222 hrs · 8,257 cycles

SEA - ON TAXI FOR FLIGHT 2316 LOST COM 1 AND 2 AND STANDBY TAXIING OUT. RETURNED TO THE GATE. REMOVED AND REPLACED AUDIO ELECTRONIC CONTROL UNIT AND CAPT'S AUDIO CONTROL PANEL IAW CRJ AMM TASK 23-51-01-000-801-A01 & 23-51-01-400-801-A01, 23-51-04-000-801-B01 & 23-51-01-400-801-BO1. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (APU DOOR WARNING) · airframe 11,200 hrs · 8,238 cycles

SEA - ON TAXI FOR FLIGHT 2467, APU DOOR OPEN CAUTION APU DOOR INDICATES AMBER DASHES. RETURNED TO THE GATE. PLACED ON MEL AND AIRCRAFT RETURNED TO SERVICE. ON 2/9, CHECKED ALL WIRING FROM APU ECU TO DOOR ACTUATOR AND DOOR POSITION INDICATOR, NO DEFECTS NOTED REF CRJ 700 WDM 49-15-00 SHEET 4 OF 7 PG 01-A01 C/W EO R-49-26 -A- (INSTRUCTIONS TO REMOVE THE APU INLET DOOR PADS) RE-RIGGED APU INLET DOOR AND PERFORMED FUNCTIONAL TEST OF THE INLET DOOR OF THE APU. OPS CHECK GOOD. NO DEFECTS NOTED. OPEN AND CLOSED APU INLET DOOR MANY TIMES (USING EXTERNAL AND APU GEN) COULD NOT DUPLICATE FAULT. MEL CLEARED AND AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: ECU — MALFUNCTIONED (NLG STEERING) · airframe 10,936 hrs · 8,063 cycles

BUR - FLT 2507 "STEERING INOP" CAUTION MSG DURING CRUISE. LANDED W/O INCIDENT WITH NLGE STEERING INOP. RESET PER CRJ-700/900-SL-32-019 REV B. NO FURTHER FAULTS NOTED. REPEATED THE SAME DAY ON FLT 2504. INTEROGATED MDDC DID NOT FIND ANY CURRENT NOSE WHEEL INOP CAUTION MSG. WENT TO A/C HISTORY PAGE AND FOUND MULTIPLE POSTING OF NOSE WHEEL STEERING LNWS CAT MTOGG STEERING R NWS ACT MT098 LVDT OPEN OR SHORT AND NWS ECU/ NO LA-10C-6BUS INPUT. PERFORMED CRJ 700 FIM TASK 32-51-10-7801-807-A01 FOR T/S, DID CONTINUITY CHECK OF CONNECTORS A164P2 PIN 24 TO A12P5 PIN 51 AND A164 P3 PIN 25 TO A12 P5 P[IN 52 CONTINUITY CHECKS GOOD, REMOVED AND REPLACED ECU (NWS ELEC CONTROL) IAW CRJ 700 AMM TASK 32-51-10-000-801-A01 AND

Part: STRUCTURE — UNKNOWN (CARGO DOOR) · airframe 10,870 hrs · 8,019 cycles

YYC - C3 NEW BAG DOOR ASSEMBLY DOES NOT FIT REBATE MUST BE TRIMMED TO FIT. REPAIRED IAW CRJ700 SRM 51-74-16-201-001-A01, HORIZON AIR EA R-52-254 AND REO 670-52-44-007 AND HORIZON AIR EA R-53-409.

Part: LUG — WORN (HORIZONTAL STAB) · airframe 10,870 hrs · 8,019 cycles

YYC - C3 LEFT HAND HORIZONTAL STAB PIVOT PIN ANTI ROTATION LUG WORN. REPAIRED IAW REO 670-55-11-029 AND HORIZON AIR EA R-55-40.

Part: PIN — WORN (HORIZONTAL STAB) · airframe 10,870 hrs · 8,019 cycles

YYC - C3 RIGHT HORIZONTAL STAB HINGE PIN ANTI ROTATION STOP LUG IS BEING WORN BY PIN. REPAIRED IAW REO 670-55-11-029 AND HORIZON AIR EA R-55-40.

Part: BUSHING — UNKNOWN (AILERONS) · airframe 10,870 hrs · 8,019 cycles

YYC - C3 RIGHT AILERON OUTBOARD PCU INBOARD LUG BUSHING FOUND NON CONFORM. REPLACED BUSHING IAW HORIZON AIR EA R-27-218.

Part: UNKNOWN — UNKNOWN (AILERON) · airframe 10,870 hrs · 8,019 cycles

YYC - C3 RIGHT AILERON FAILS BACKLASH TEST ON NR 3 HYDRAULIC SYSTEM. REPAIRED IAW CRJ700 SRM 27-11-00-710-001-A01.

Part: SKIN — WORN (RT ELEVATOR) · airframe 10,870 hrs · 8,019 cycles

YYC - RIGHT ELEVATOR TOP LEADING EDGE IS WORN THRU PAINT. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND SRM 51-41-02-001-001-A01.

Part: SKIN — GOUGED (BS 293) · airframe 10,870 hrs · 8,019 cycles

YYC - C3 EXTERNAL FUSELAGE, SKIN GOUGED AT FS293.0 BETWEEN STRINGER 26R AND 27. REPAIRED IAW REO 670-53-21-153 AND CRJ 700 SRM 51-25-16-001-001-A01.

Part: SKIN — WORN (LT ELEVATOR LE) · airframe 10,870 hrs · 8,019 cycles

YYC - LEFT ELEVATOR TOP LEADING EDGE IS WORN THROUGH PAINT. REPAIRED IAW CRJ 700 SRM 51-12-00-001-001-A01 AND SRM 51-41-02-001-001-A01.

Part: DOOR FRAME — NICKED (BS 349) · airframe 10,870 hrs · 8,019 cycles

YYC - C3 FUSELAGE LEFT FS349, WL89.50 HAS SKIN NICKED AT DOOR FRAME. REPAIRED IAW HORIZON AIR EA R-53-403, REO 670-53-21-151 AND CRJ SRM 51-25-16-001-001-A01.

Part: SKIN — DENTED (ESCAPE HATCH) · airframe 10,870 hrs · 8,019 cycles

YYC - C3 EMERGENCY ESCAPE HATCH OUTSIDE SKIN RIGHT HAND SIDE HAS DENT. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND SRM 57-25-16-001-001-A01

Part: FITTING — DAMAGED (ROLLER GUIDE) · airframe 10,870 hrs · 8,019 cycles

YYC - C2 RIGHT WING OUTBOARD FLAP ROLLER GUIDE FITTING HAS DAMAGE AT FLS168.98. REPAIRED IAW CRJ700 SRM 57-51-02-201-001-A01 AND SRM 51-25-16-001-001-A01.

Part: SKIN — DAMAGED (TE FLAPS) · airframe 10,870 hrs · 8,019 cycles

YYC - RIGHT HAND INBOARD FLAP BOTTOM SKIN HAS GRAVEL DAMAGE. REPAIRED IAW CRJ 700 SRM 57-01-101-001-A01.

Part: SKIN — CHAFED (BS 956) · airframe 10,870 hrs · 8,019 cycles

YYC - FUSELAGE EXTERIOR LOWER SKIN AT FS956 BETWEEN STRINGER 23R AND 24R CHAFED BY LAV SERVICED LATCH. REPAIRED IAW HORIZON AIR EA R-53-404 AND CRJ SRM 57-25-16.

Part: SEAT TRACK — GOUGED (BS 784) · airframe 10,870 hrs · 8,019 cycles

YYC - C3 INTERNAL FUSELAGE LEFT SIDE SEAT RAIL FS 784.0 - 861.0 HAS AREAS OF GOUGES. REPAIRED IAW REO 670-53-00-013, REV A. AND CRJ 700 SRM 51-21-16.

Part: SEAT TRACK — GOUGED (BS 850-985) · airframe 10,870 hrs · 8,019 cycles

YYC - C3 INTERNAL FUSELAGE RIGHT HAND FLOOR SEAT RAIL FS850.45-985.0 HAS AREAS OF GOUGES. REPAIRED IAW REO 670-53-00-013, REV A.

Part: SEAT TRACK — GOUGED (BS 850-977) · airframe 10,870 hrs · 8,019 cycles

YYC - C3 INTERIOR FUSELAGE RIGHT FLOOR SEAT RAIL FS850.45-977.0 HAS AREAS OF GOUGES. REPAIRED IAW REO 670-53-00-013 REV A.

Part: STRINGER CLIP — MISSING (BS 611) · airframe 10,870 hrs · 8,019 cycles

YYC - C3 FUSELAGE INTERIOR LEFT HAND SIDE, FS611, STRINGER 16L, MISSING ONE TIE CLIP. REPAIRED IAW CRJ700 SRM 53-31-03-991-803 AND SRM 51-42-06-001-A01.

Part: STRINGER CLIP — MISINSTALLED (BS 469) · airframe 10,870 hrs · 8,019 cycles

YYC - C3 FUSELAGE INTERIOR, STRINGER TIE CLIP HAS TWO POORLY INSTALLED RIVETS AT FS469, STRINGER 7R. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: FASTENER — MISSING (BS 319) · airframe 10,870 hrs · 8,019 cycles

YYC - C3 FUSELAGE INTERIOR RIGHT HAND SIDE FS 319.90, STRINGER 13-14 HAS MISSING LOCK FASTENER COLLAR ON FRAME. REPAIRED IAW CRJ700 SRM 51-42-21-001-001-A01.

Part: STRINGER CLIP — MISINSTALLED (BS 909) · airframe 10,870 hrs · 8,019 cycles

YYC - C3 FUSELAGE INTERIOR, STRINGER TIE CLIP AT FS909, STRINGER 6R HAS POORLY INSTALLED RIVET. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: UNKNOWN — UNKNOWN (BS 597-605) · airframe 10,870 hrs · 8,019 cycles

YYC - C3 FUSELAGE INTERIOR RIGHT SIDE FS 597-605 AT STRINGER 12R SEVEN RIVETS DUMPED. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: RETAINER — CRUSHED (E/E BAY DOOR) · airframe 10,870 hrs · 8,019 cycles

YYC - C3 AVIONICS DOOR SEAL RETAINER CRUSHED IN TWO PLACES ON BOTH FRON AND BACK EDGES. REPLACED SEAL IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: FASTENER — MISSING (BS 394) · airframe 10,870 hrs · 8,019 cycles

YYC - C3 FUSELAGE INTERIOR RIGHT SIDE FS394 BETWEEN CABIN FLOOR AND RIGHT HAND SIDE RAIL, TWO RIVETS MISSING ON FRAME TO INNER CHORD. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: FASTENER — MISINSTALLED (MLG WW) · airframe 10,870 hrs · 8,019 cycles

YYC - FUSELAGE LOWER FS822 ON LEFT SIDE OF WHEEL WELL WL500 HAS POORLY INSTALLED RIVET ON INNER GUSSET TO HORIZONTAL SUPPORT. REPAIRED IAW CRJ700 SRM 51-42-21-001-001-A01.

Part: SKIN — WORN (BS 981) · airframe 10,870 hrs · 8,019 cycles

YYC - FUSELAGE EXTERIOR LOWER SKIN AT FS 981, BLO AND LBL1.3 HAS TWO WEAR MARKS. REPAIRED IAW REO 670-53-014 AND CRJ-700 SRM 51-42-21.

Part: SKIN — CHAFED (BS 975) · airframe 10,870 hrs · 8,019 cycles

YYC - FUSELAGE EXTERIOR, LOWER SKIN AT FS 975, LBL0.75 CHAFED. REPAIRED IAW REO 670-53-00-014, REV AND CRJ700 SRM 51-21-16.

Part: SEAT TRACK — CORRODED (BS 357-763) · airframe 10,870 hrs · 8,019 cycles

YYC- RT SIDE SEAT RAIL FS 357.0-763.0 HAS AREAS OF CORROSION. BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREAS PER SRM 51-21-16 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEPS 2 AND STEPS 4 THR 8 IAW REO 670-53-00-013 REV A.

Part: SEAT TRACK — GOUGED (BS 701) · airframe 10,870 hrs · 8,019 cycles

YYC - LT FLOOR SEAT RAIL FS 701.45-836.55 PN SH670-35864-951 HAS AREAS OF GOUGES ALL DAMAGE REMOVED IAW REO 670-53-00-013 REV A STEPS 1 AND 6. REWORKED AREAS ALODINED TO CODE A044 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9 AND COMPLIED WITH STEP 2 AND STEPS 4 THRU 8.

Part: SEAT TRACK — CORRODED (BS 379) · airframe 10,870 hrs · 8,019 cycles

YYC - RT SIDE SEAT RAIL FS 379.0-483.0 HAS AREAS OF GOUGES AND CORROSION. REMOVED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINE REOWRKED AREA PER SRM 51-21-16 IAW REO 670-53-00-213 REV A STEPS 3. COMPLETED WITH STEPS 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9.

Part: SKIN — DAMAGED (BS 1015-1051) · airframe 10,870 hrs · 8,019 cycles

YYC- FUSELAGE EXTERIOR SKIN ABOVE AFT BAGGAGE DOOR HAS AREAS OF WICK FROM STA1015 TO STA 1051. STR10L TO STR RL BLENDED OUT DAMAGE IAW REO 670-53-61-224, REV STEPS 1 AND 2 PER EA R-53-407. HFEC INSP COMPLETED ON ALL BLENDED AREAS IAW CRJ 700 NDTM PT 01 51-20-006. NO CRACKS NOTED. PREPED PRIMED AND PAINTED REPAIRED AREA IAW CRJ 700 SRM 51-25-01-001-001-A01.

Part: SKIN — DAMAGED (LT WING) · airframe 10,870 hrs · 8,019 cycles

YYC - LT WING, I/B MFS SURROUND SKIN AT WS 170.83 LOOSE FASTNERS. FASTENERS REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01. TOUCH-UP IAW CRJ 700 SRM 51-25-16-001-001-A01.

Part: SEAT TRACK — GOUGED (BS 683-701) · airframe 10,870 hrs · 8,019 cycles

YYC- LT FLOOR SEAT RAIL FS 683.45-701.45 P/N SH670-33400-961 HAS AREAS OF GOUGES BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREAS PER SRM 51-21-16 IAW REO 670-53-00-013. REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013. REV A STEP 9. COMPLIED WITH STEPS 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A.

Part: SEAT TRACK — CORRODED (BS 581-683) · airframe 10,870 hrs · 8,019 cycles

YYC - RT FLOOR SEAT RAIL FS 581.0-683.0 PN SH670-33425-951 HAS AREAS OF GOUGES AND CORROSION. BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREAS PER SRM 51-21-16 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEPS 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A.

Part: SEAT TRACK — GOUGED (BS 683-701) · airframe 10,870 hrs · 8,019 cycles

YYC- RT FLOOR SEAT RAIL FS 683.45-701.45 P/N SH670-33400-961 HAS AREAS OF GOUGES BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREAS PER SRM 51-21-16. IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEPS 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A.

Part: STRINGER — CRACKED (PAX DOOR) · airframe 10,870 hrs · 8,019 cycles

YYC - PAX DOOR AFT STRINGER (STAIR SIDE) CRACKED AT HANDRAIL STOWAGE BRACKET. CUT OUT DAMAGED SIDE PANEL AND FABRICATED REPAIR PARTS IAW REO 670-52-11-104 STEPS 1, 3, 4, 5, 6, 7. HFEC INSPECTION C/O ON CUT-OUT REPAIR AREA OF PAX DOOR STAIR WEB AS REQUIRED IAW NDTM PT 1 51-20-006 NO CRACKS FOUND. REMAINING STEPS 2, AND 8 THROUGH 17 COMPLETED IAW REO 670-52-11-104.

Part: DOOR FRAME — GOUGED (BS 310) · airframe 10,870 hrs · 8,019 cycles

YYC - FUSELAGE FWD PAX DOOR SURROUND, FWD COMBING HAS GOUGES BETWEEN STR 12L TO STR 16L STA 310. BLENDED GOUGES IAW SRM TASK 53-21-23-101-001-A01 SRM 51-12-00-001-001. PG 9 PARA 7B. LPI C/O BLENDED AREA OF PAX DOOR SURROUND FWD COMBINE AS REPAIRED IAW NDTM PT 51-20-008. NO CRACKS FOUND. TREATED, PRIMED AND PAINTED IAW CRJ 700 SRM 51-25-16-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 581-689) · airframe 10,870 hrs · 8,019 cycles

YYC- INTERNAL FUSELAGE, LT FLOOR SEAT RAIL FS 581.0-689.0 PN SH670-33425-951 HAS AREAS OF CORROSION AND GOUGES. BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV STEP 1. ALODINED REWORKED AREAS PER SRM 51-21-16 IAW ROE 670-53-00-013 REV A STEP 3. COMPLIED WITH STEP 2 AND 4 THRU 8 IAW REO 670-53-00-013 REV A. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9.

Part: SKIN — DAMAGED (BS 1051) · airframe 10,870 hrs · 8,019 cycles

YYC- FUSELAGE EXTERIOR HAS WICK ON SKIN AT STA 1051, STR 12R. DAMAGE BLENDED OUT IAW CRJ 700 SRM 51-12-00-001-001-A01 BLENDED AREA WITHIN LIMITS IAW CRJ 700 SRM 53-61-01-101-004-A01. NDT FLPI CARRIED OUT IAW NDTM PART 1 51-20-008 NO CRACKS NOTED. TREATED, PRIMED AND PAINTED IAW CRJ 700 SRM 51-25-16-001-001-A01.

Part: SKIN — NICKED (BS 939) · airframe 10,870 hrs · 8,019 cycles

YYC - FUSELAGE EXTERIOR HAS NICK ON SKIN AT STA 939, STR 9L. NICK BLENDED OUT IAW CRJ 700/900 SRM TASK 53-51-01-101-002-A01 .004 MAT'R REMOVED. LPI C/O ON BLENDED SKIN REPAIR AREA AS REQUIRED IAW NDTM PT 1 51-20-008 NO CRACKS FOUND. TREATED PRIMED AND PAINTED IAW CRJ 700 SRM 51-25-16-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 485) · airframe 10,870 hrs · 8,019 cycles

YYC - LT FLOOR SEAT RAIL FS 485.0-581.0 PN SH670-33426-1 HAS AREAS OF CORROSION AND GOUGES. BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREAS PER SRM 51-21-16 IAW REO 670-53-00-013 REV STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEPS 2 AND 4 THRU 8 IAW REO 670-53-00-013 REV A.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 10,870 hrs · 8,019 cycles

YYC - AFT BAGGAGE DOOR HAS AREAS OF SCRATCHES TOP EXTERNAL SURFACE. BLENDED OUT DAMAGE IAW EA R-52-253 AND REO 670-52-31-012 REV- NDT-HFEC CARRIED OUT IAW NDTM PART 1 51-20-006. NO CRACKS NDT ON FASTENERS REPLACED IAW EA R-53-253 AND REO 670-52-31-012 REV. TREATED, PRIMED AND PAINTED IAW CRJ700 SRM 51-25-16-001-001-A01.

Part: SHROUD — BROKEN (SPOILER) · airframe 10,870 hrs · 8,019 cycles

YYC - RT WING BOTTOM TRAILING EDGE. MULTI FUNCTION SPOILER SHROUD HAS MULTIPLE BROKEN AND LOOSE FASTENERS BETWEEN WS 170.83 TO WS 231.23. FASTENERS REPLACED (MS20426T) IAW CRJ700 SRM 51-02-06-001-001-A01.

Part: BULKHEAD — CORRODED (BS 286) · airframe 10,870 hrs · 8,019 cycles

YYC - LEFT FS 286 BULKHEAD LOWER WEB HAS CORROSION ALONG THE FLOOR LINE. FUSELAGE INT LEFT FS 280 LOWER BULKHEAD CORROSION REMOVED IAW REO 670-53-11-052 REV A REPAIR NR 1 REMAINING WEB THICKNESS .037 IN AFFECTED AREA. AREA TREATED PRIMED AND PAINTED IAW SRM 51-21-163.

Part: SEAT TRACK — CORRODED (BS 784-861) · airframe 10,870 hrs · 8,019 cycles

YYC - RT SIDE SEAT RAIL FS 784.0-861.0 HAS AREAS OF GOUGES AND CORROSION. BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORK AREAS PER SRM 51-21-16 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEPS 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A.

Part: DOOR FRAME — MISREPAIRED (FUSELAGE) · airframe 10,870 hrs · 8,019 cycles

YYC - FUSELAGE AT PAX DOOR AFT FRAME AT TOP HAS OPEN HOLE. INSTALLED RIVET IAW CRJ 700 SRM 51-42-06-001-001-A01.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 10,870 hrs · 8,019 cycles

YYC - CROSS BEAM AT FS 280 HAS SPOTS OF CORROSION AROUND ANCHOR NUT HOLES. CROSS BEAM AT FS 280 CORROSION REMOVED IAW REO 670-53-11-046 REV A REMAINING THICKNESS .037 OVER BLENDED AREAS. AREA TREATED PRIMED AND PAINTED IAW SRM 51-21-16.

Part: COLLAR — MISSING (FASTENER) · airframe 10,870 hrs · 8,019 cycles

YYC - FUSELAGE INTERIOR HAS (2) MISSING LOCK FASTENER COLLARS AT FS 761, STR 16L, BELOW EXIT DOOR ON FRAME WEB. INSTALLED NEW COLLARS (2) IAW CRJ 700 SRM 51-42-21-001-001-A01 (HST79CKS).

Part: SEAT TRACK — CORRODED (BS 483-573) · airframe 10,870 hrs · 8,019 cycles

YYC - RT SIDE SEAT RAIL FS 483.0-573.0 HAS AREAS OF CORROSION. REPAIRED IAW REO 670-5-00-013, MAT'L LOSS WITHIN LIMITS OF REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREA PER SRM 51-21-16 IAW REO 670-53-00-013 REV A STEP 3. COMPLETED WITH STEPS 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9.

Part: BULKHEAD — CORRODED (BS 280) · airframe 10,870 hrs · 8,019 cycles

YYC - RIGHT FS 280 BULKHEAD LOWER WEB HAS CORROSION ALONG THE FLOOR LINE FUSELAGE INT RT FS 280 BULKHEAD LOWER WEB CORROSION REMOVED IAW REO 670-53-11-052 REV A REPAIR NR 1 REMAIN INT THICKNESS .038 OVER BLENDED AREAS. AREA TREATED PRIMED AND PAINTED IAW SRM 51-21-16.

Part: SEAT TRACK — CORRODED (BS 573-763) · airframe 10,870 hrs · 8,019 cycles

YYC - LT SIDE SEAT RAIL FS 573.0-763.0 HAS AREAS OF GOUGES AND CORROSION. BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-00-013 REV A STEP 1. ALODINED REWORKED AREA PER SRM 51-21-16 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV STEP 9. COMPLIED WITH STEPS AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A.

Part: SKIN — DAMAGED (BS 1070-1098) · airframe 10,870 hrs · 8,019 cycles

YYC - FUSELAGE EXTERIOR HAS AREAS OF WICKS ON SKIN FROM STA 1070 TO STA 1098, BETWEEN STR 12L TO 16L. BLENDED OUT DAMAGE IAW REO 670-53-61-224 REV PER EA (STEPS 1 AND 2) R-53-407. HFEC INSP COMPLETED ON ALL BLENDED AREAS IAW CRJ 700 NDTM PT 01 51-20-006. NO CRACKS NOTED. PREPPED PRIMED AND PAINTED REPAIRED AREA IAW CRJ 700 SRM 51-25-01-001-001-A01.

Part: SEAT TRACK — GOUGED (BS 701) · airframe 10,870 hrs · 8,019 cycles

YYC- RT FLOOR SEAT RAIL FS 701.45-836.55 PN SH670-35864-951 HAS AREAS OF GOUGES DAMAGE BLEND OUT WITHIN LIMITS OF REO 670-53-00-013 REV A IAW CRJ 700 SRM 51-12-00 AND 51-21-06 (STEP 1 REO 670-53-00-013 REV A) ALODINED REWORKED AREAS TO A044 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A AND COMPLETE STEPS 1-9.

Part: SKIN — DAMAGED (LT WING) · airframe 10,870 hrs · 8,019 cycles

YYC - LT WING, O/B MFS SKIN (SURROUND) AT WS 231.23 LOOSE FASTENERS. REPLACED FASTENERS (MS20426T) IAW CRJ 700 SRM 51-42-06-001-001-A01. TOUCHED UP IAW CRJ 700 SRM 51-25-16-001-001-A01.

Part: FITTING — WORN (CARGO DOORWAY) · airframe 10,870 hrs · 8,019 cycles

YYC - FUSELAGE LT FWD BAGGAGE DOOR SURROUND STRUCTURE HAS FWD UPPER FITTING WORN APPROX .010". BLENDED OUT DAMAGE IAW EA R-53-402 AND REO 670-53-31-060 REV. NDT HFEC CARRIED OUT IAW NDTM PART 1 51-20-006. NO CRACKS NOTED. TREATED, PRIMED AND PAINTED IAW CRJ 700 SRM 51-25-16-001-001-A01.

Part: BULKHEAD — DAMAGED (BS 1690) · airframe 10,870 hrs · 8,019 cycles

YYC- FORWARD SIDE OF FS 1690 HAS WEAR MARKS ON LT AND RT OUTBOARD AT 3 O'CLOCK AND 9 O'CLOCK POSITIONS. BLENDED OUT DAMAGE IAW CRJ 700 SRM 53-00-00-101-001-A01 AND CRJ 700 SRM 51-12-00-001-001-A01 PARA 7B WITHIN LIMITS LPI C/O ON BLEND REPAIR AREA AS OF BULKHEAD WEB AS REQUIRED IAW NDTM PT 1 51-20-008 NO CRACKS FOUND. TREATED AND PRIMED REWORKED AREA IAW CRJ 700 SRM 51-25-06-001-001-A01.

Part: SKIN — CRACKED (SPOILERS) · airframe 10,870 hrs · 8,019 cycles

YYC- RT WING OUTBD MULTIFUNCTION SPOILER UPPER CENTER HINGE SKIN CRACKED. SPOILER UPPER CENTER HINGE SKIN REPAIRED IAW CRJ 700 EA R-57-136 AND REO 670-57-73-011 REV STEPS 1 AND 2. NDT HFEC CARRIED OUT IAW NDTM PART 1 51-20-006 NO CRACKS NOTED. ROTARY FLAP PEENED REWORK EDGE IAW REO 670-57-73-011. TREATED, PRIMED AND PAINTED IAW CRJ 700 SRM 51-25-16-001-001-A01.

Part: VANE — DAMAGED (TE FLAPS) · airframe 10,870 hrs · 8,019 cycles

YYC - RT OUTBD FLAP VANE L/E (LOWER SURFACE) HAS LOOSE FASTENER AT WS 218. REPLACED FASTENER IAW CRJ 700 SRM 51-42-13-001-001-A01.

Part: GUIDE — WORN (LT WING TE FLAP) · airframe 10,870 hrs · 8,019 cycles

YYC - LT WING, O/B FLAP AFT GUIDE ROLLER FITTING IS WORN (RECEIVING END). BLENDED OUT DAMAGE ON ROLLER FITTING IAW CRJ700 SRM 57-51-02-201-001-A01. HEFC INSPECTION C/00N BLEND REPAIR AREA OF FITTING AS REQUIRED IAW NDTM PT 151-20-006. NO CRACKS FOUND. ROTARY FLAP PEENED REWORKED AREA IAW CRJ700 SRM TASK 57-51-02-201-011-A01 PARA 2 (2A(4)) TREATED, PRIMED AND PAINTED AREA IAW CRJ700 SRM 51-25-16-001-001-A01.

Part: SKIN — DAMAGED (BS 565) · airframe 10,870 hrs · 8,019 cycles

YYC - FUSELAGE EXTERIOR HAS SCRATCH ON SKIN AT STA 565, STR 0. SCRATCH BLENDED OUT IAW CRJ 700/900 SRM TASK 53-31-01-101-001-A01 .003 MAT REMOVED. LPI C/O ON BLEND REPAIRED AREA OF FUSELAGE SKIN AT STA 565 STR AS REQUIRED IAW NDTM PT 1 51-20-008. NO CRACKS FOUND. TREATED, PRIMED AND PAINTED BLENDED AREA IAW CRJ 700 SRM 51-25-16-001-001-A01.

Part: INTERCOSTAL — CRACKED (BS 176) · airframe 10,870 hrs · 8,019 cycles

YYC - FORWARD FUSELAGE AT ADG COMPARTMENT FLOOR INTERCOSTAL RT SIDE STA 176 HAS CRACKED LOWER FLANGE P/N CC670-33191-1 (REF SRM 53-11-43-991-802-50). REPLACED INTERCOSTAL P/N CC670-33191-1 IAW CRJ 700 SRM 51-42-06-001-001-A01.

Part: SKIN — NICKED (BS 1047) · airframe 10,870 hrs · 8,019 cycles

YYC - FUSELAGE EXTERIOR HAS NICK ON SKIN AT STA 1047, STR 19R. BLENDED OUT DAMAGE IAW CRJ 700 SRM 53-61-01-101-004-A01 AND 51-12-00-001-001-A01. NDT - FLP1 CARRIED OUT IAW NDTM PART 1 51-20-008, NO CRACKS NOTED. TRACKED, PRIMED AND PAINTED IAW CRJ SRM 51-25-16-001-001-A01.

Part: VANE — DAMAGED (RT WING FLAP) · airframe 10,870 hrs · 8,019 cycles

YYC - RT WING OUTBD FLAP - FLAP VANE, INBD UPPER L/E HAS BROKEN FASTENERS. REPLACE 6 EA RIVETS (CR3214-4-3) B/N 62151 IAW CRJ 700 SRM 51-42-13-001-001-A01.

Part: SKIN — DAMAGED (LT WING) · airframe 10,870 hrs · 8,019 cycles

YYC - LT WING, I/B MFS SURROUND AT WS 170.83 LOOSE FASTNERS. FASTENERS REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01. TOUCH-UP IAW CRJ 700 SRM 51-25-16-001-001-A01.

Part: RIVET — LOOSE (BS 549) · airframe 10,870 hrs · 8,019 cycles

YYC - FUSELAGE EXTERIOR HAS SMOKING RIVET AT STA 549, STR 0. RIVET REMOVED IAW CRJ 700/900 SRM 51-42-06-001-001-A01 PG 8 PARA 11. RIVET INSTALLED IAW CRJ 700/900 SRM 51-42-06-001-001-A01 PG 4 PARA 2B.

Part: SKIN — NICKED (BS 310) · airframe 10,870 hrs · 8,019 cycles

YYC - FUSELAGE EXTERIOR, SKIN AT FWD PAX DOOR CUTOUT, FWD EDGE HAS NICKS ON SKIN, STA 310, BETWEEN STR 13L TO STR 15L. BLEND OUT DAMAGE IAW REO 670-53-21-155 REV A STEPS 1 AND 2 PER EA NR R-53-408. HFEC COMPLETED ON BLENDED AREAS IAW CRJ NDTM PT 01 51-20-006. NO CRACK INDICATIONS NOTED. TOUCHED UP REWORKED AREA PER CRJ 700 SRM 51-21-16-001-001-A01 IAW REO 670-53-21-155 REV A STEP 4.

Part: SEAT TRACK — GOUGED (BS 836-850) · airframe 10,870 hrs · 8,019 cycles

YYC - LT FLOOR SEAT RAIL FS 836.55-850.45 PN SH670-37380-951 HAS AREAS OF GOUGES.ALODINED OUT ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREAS TO COMP A044 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEPS 2, 4, 6, 7 AND 8 OF REO 670-53-00-013 REV A.

Part: SEAT TRACK — CORRODED (BS 483-573) · airframe 10,870 hrs · 8,019 cycles

YYC - LT SIDE SEAT RAILS FS 483.0-573.0 HAS AREAS OF GOUGES AND CORROSION. BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREA PER SRM 51-21-16 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEPS 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A.

Part: FITTING — CORRODED (FUSELAGE) · airframe 10,870 hrs · 8,019 cycles

YYC- GALLEY NR 1 INB FWD FLOOR FITTING CORRODED P/N 9331091-1. REMOVED CORROSION FROM FITTING IAW CRJ 700 SRM 51-21-06-001-001-A01. NOMINAL THICKNESS OF .110, MIN REMAINING .030. REPAIR C/O IAW EA R-25-286 SECTION 1 AND REO 670-25-31-002.

Part: SEAT TRACK — CORRODED (BS 861-985) · airframe 10,870 hrs · 8,019 cycles

YYC- LT SIDE SEAT RAIL FS 861.0-985.0 HAS AREAS OF GOUGES AND CORROSION. BLENDED DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREA PER SRM 51-21-16 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEP 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A.

Part: SEAT TRACK — CORRODED (BS 379-483) · airframe 10,870 hrs · 8,019 cycles

YYC- LT SIDE SEAT RAIL FS 379.0 -483.0 HAS AREAS OF GOUGES AND CORROSION. BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREAS PER SRM 51-21-16 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEPS 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A.

Part: SEAT TRACK — CORRODED (BS 485) · airframe 10,870 hrs · 8,019 cycles

YYC - RT FLOOR SEAT RAIL FS 485.0-581.0 PN670-33426-1 HAS AREAS OF GOUGES AND CORROSION. BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREAS PER SRM 51-21-16 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEPS 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A.

Part: SEAT TRACK — CORRODED (BS 381-485) · airframe 10,870 hrs · 8,019 cycles

YYC - LT FLOOR SEAT RAIL FS 381.45-485.0 P/N SH670-32249-951 HAS AREAS OF GOUGES AND CORROSION. BLENDED OUT ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREAS PER SRM 51-21-16 IAW REO 670-53-00-013 REV A STEP 3. COMPLIED WITH STEP 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9.

Part: STRINGER — CRACKED (PAX DOOR) · airframe 10,870 hrs · 8,019 cycles

YYC- PAX DOOR FWD STRINGER CRACKED AT HANDRAIL STOWAGE BRKT (FWD STAIR SIDE) CUT OUT DAMAGED SIDE PANEL AND FABRICATED REPAIR PARTS IAW REO 670-52-11-104 STEPS 1,3,4,5,6,7. HFEC INSPECTION C/O ON CUT OUT REP AIR AREA OF PAX DOOR STAIR WEB AS REPAIRED IAW NDTM PT 151-20-006 NO CRACKS FOUND REMAINING STEPS 2 AND 8 THROUGH 17 COMPLETED IAW REO 670-52-11-104

Part: SKIN — CORRODED (BS 302) · airframe 10,870 hrs · 8,019 cycles

YYC - FUSELAGE LOWER SKIN AT FS 302 AND STR27 IS CORRODED AROUND THE LOWER TCAS ANTENNA BASE REPAIRED FUSELAGE SKIN IAW EA R-53-405 AND REO 670-53-21-153 REV - .002 MAT'L LOSS. HFEC COMPLETED ON BLENDED AREA IAW CRJ NDTM PT 1 51-20-006. NO CRACKS NOTED. TREATED IAW CRJ 700 SRM 51-21-11-001-001-A01, EA NO R-53-405 AND REO 670-53-21-153.

Part: STRINGER — CRACKED (PAX DOOR) · airframe 10,870 hrs · 8,019 cycles

YYC - PAX DOOR AFT STRINGER (STAIRSIDE) CRACKED AT BASE OF 4TH RISER. DRESSED OUT EDGE CRACK IAW 700/900 SRM FIG 53-00-00-991-804 WITHIN LIMITS. DENT LP C/O ON CUT-OUT REPAIRED AS REQUIRED IAW NDTM PT 1 51-20-008, NO CRACKS FOUND. REPROTECTED IAW CRJ 700/900 SRM 51-25-16.

Part: SEAT TRACK — CORRODED (BS 350-485) · airframe 10,870 hrs · 8,019 cycles

YYC - RT FLOOR SEAT RAIL FS 350.0-485.0 P/N SH670-32159-1 HAS AREAS ON CORROSION BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREAS PER SRM 51-21-16 IAW REO 670-53-00-01B REV A STEP 3. IDENTIFIED SEAT TRACKS IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEPS 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A.

Part: HOUSING — CRACKED (GALLEY DOOR) · airframe 10,870 hrs · 8,019 cycles

YYC - GALLEY SERV DOOR MECH HOUSING CRACKED IPC 52-41-03-01-A01 TR 52-0109. HOUSING ASSY REMOVED IAW CRJ 700 AMM 52-41-03-000-801-A01. BUSHINGS FOR INNER LEVER, LATCH CRANK AND VENT CRANK TRANSFERED TO NEW HOUSING P/N CC670-38238-5 IAW CRJ 700 AMM TASK 20-31-00-400-801-A01 PG 404. LATCH CRANK AND VENT CRANK REINSTALLED ACTUATOR SHAFT BRG TRANSFERED OVER. NEW MECH HOUSING P/N CC670-38238-1 HI-LITE INSTALLED IAW CRJ 700 SRM 51-42-21-001-001-A01 P.8 PARA 8C. DETENT ASSY INSTALLED IAW CRJ 700 AMM TASK 52-41-02-400-803-A01, UPLOCK BELL CRANK INSTALLED WITH NEW COLLAR P/N B0206011DV8 AND LATCH AND VENT RODS CONNECTION TO CRACKS, COMPLATE AND ANTENNA HANDLE INSTALLING IAW CRJ 700 AMM TASK 52-41-03-400-801-A01 PG 4

Part: SKIN — CHAFED (LT WING) · airframe 10,870 hrs · 8,019 cycles

YYC- RT WING OUTBD LEADING EDGE SKIN HAS CHAFED MARK FRO ADJACENT RIVET HEAD AT WS294. CHAFE DAMAGE BLENDED IAW CRJ 700 SRM 57-41-01-101-001-A01 AND 51-12-00-001-001-A01 REMAINING MATERIAL WITHIN LIMITS. LPI COMPLETED ON BLENDED AREA IAW CRJ 700 PT 01 51-20-008. NO CRACKS NOTED. TREATED, PRIMED AND PAINTED IAW CRJ 700 SRM 51-25-16-001-001-A01.

Part: SKIN — DAMAGED (BS 1000-1047) · airframe 10,870 hrs · 8,019 cycles

YYC - FUSELAGE EXTERIOR, AFT BAGGAGE DOOR CUTOUT HAS EDGE DAMAGE, STA 1000 AND STA 1047, BETWEEN STR14 AND 16L. BLENDED OUT DAMAGE IAW REO 6760-53-61-224 REV-PER EA R-53-407 (STEPS 1 & 2). HFEC INSP COMPLETED ON BLENDED AREA IAW CRJ 700 NDTM PT 01 51-20-006. NO CRACKS NOTED. PREPPED PRIMED AND PAINTED REPAIRED AREA IAW CRJ 700 SRM 51-25-01-001-001-A01.

Part: SKIN — DAMAGED (RT WING) · airframe 10,870 hrs · 8,019 cycles

YYC - RT WING UPPER TRAILING EDGE (JUST I/B OF MULTIFUNCTION SPOILERS) HAS LOOSE FASTENER. FASTENERS REPLACED IAW CRJ 700 SRM 51-42-00-001-001-A01 AND 51-42-21-001-001-A01.

Part: SEAL — TORN (CARGO DOOR) · airframe 10,870 hrs · 8,019 cycles

YYC- FWD BAGGAGE DOOR TOP EXTERNAL SEAL BENT OUT FROM FUSELAGE AND TORN IPC 52-35-00-01-A01-190. DEFLECTOR P/N LE 670-39630-5 REMOVED AND NEW FITTED IAW CRJ 700 LATECORE CMM 52-35-00-300-84-A01. DEFLECTOR P/N LE 670-39630-5 INSTALLED IAW CRJ 700 LATECORE CMM 52-35-00-300-804-A01.

Part: DOOR FRAME — DENTED (BS 1015) · airframe 10,870 hrs · 8,019 cycles

YYC- AFT BAGGAGE DOOR SURROUND FWD LOWER COMBING HAS AREA OF SCRATCHES AND DENTS. FS 1015. REPAIR CARRIED OUT IAW REO 670-53-61-196 REV- STEPS 1 AND 2. HFEC INSPECTION C/W. BLENDED REPAIR OF LOWER COMBING AS REQUIRED IAW NDTMP 151-20-006 NO CRACKS FOUND TOUCHED UP REWORKED AREA IAW REO 670-53-61-196 REV. AIRCRAFT PRESSURIZED IAW TASK 52-00-00-790-801 LEAK CHECK ELO. NO LEAKS FOUND. REPAIR IAW REO 670-53-61-196 C/W.

Part: BRAKE ASSY — MALFUNCTIONED (MLG) · airframe 10,728 hrs · 7,919 cycles

PDX - ON LANDING FOR FLIGHT 2481, LEFT BRAKE INEFFECTIVE ABOVE 50 KNOTS. MAINTENANCE BLED THE BRAKE SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CIRCUIT BOARD — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 10,592 hrs · 7,828 cycles

SEA - EMERGENCY LIGHTS IN THE CABIN AS WELL AS THE EMERGENCY LT ON STATUS MESSAGE KEEPS CYCLING ON AND OFF. MAINTENANCE REPLACED THE PCB-5 IN JB11. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DISPLAY — OVERHEATED (COCKPIT) · airframe 10,302 hrs · 7,633 cycles

DEN - ARRIVING AT THE AIRCRAFT IN THE MORNING FOR FLIGHT 2457, NOTICED A STRONG ELECTRICAL BURNING SMELL IN THE COCKPIT, AND THE DISPLAY TEMP WARNING WAS DISPLAYED. AIRCRAFT HAD ELECTRICAL POWER APPLIED ALL NIGHT, AND THE DISPLAY FAN HAD BEEN TURNED TO STANDBY. MAINTENANCE TURNED THE DISPLAYS TO DIM POSITION AND COOLED THE DISPLAYS WITH FANS. THE NR 1 MULTI-FUNCTION DISPLAY REMAINED BLANK. REMOVED AND REPLACED NR 1 MULTI-FUNCTION DISPLAY. OPERATIONAL CHECKS GOOD. ODOR CLEARED FROM AIRCRAFT BY OPENING EMERGENCY EXITS AND WITH CONDITIONED AND RECIRC AIR. AIRCRAFT RETURNED TO SERVICE.

Part: MANIFOLD — LEAKING (NR 2 ENG FUEL) · airframe 10,238 hrs · 7,591 cycles

PDX - NR 2 ENGINE FUEL LEAK. REPLACED THE VG SLAVE ACTUATOR WITH NO HELP. REPLACED THE HEAD-END MANIFOLD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: APU — ODOR (AFT) · airframe 10,191 hrs · 7,556 cycles

GEG - ON FLIGHT 2351 NOTICED FUEL SMELL IN CABIN. MAINTENANCE PLACED THE APU ON MEL 49-10-1B, RSI 351878. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (NLG STEERING) · airframe 10,948 hrs · 8,071 cycles

ON FLT 2453, STEERING INOP CAUTION MESSAGE AFTER ARMING THE SYSTEM. ACCOMPLISHED RESET PROCEDURE IAW MX CONTROL. MESSAGE WENT AWAY FOR APPROX 30 SECONDS. ACCOMP RESET PROCEDURE A SECOND TIME IAW MTX CONTROL AND RETURNED TO GATE. MX INTERROGATED MDC FAULT HISTORY. FOUND (NWS ECU NO NWS A BUG TO DCU) (L NWS ACT LVDT OPEN OR SHORT) (R NWS ACT LVDT OPEN OR SHORT). REMOVED AND REPLACED RT STEERING ACTUATOR/LVDT REF TASK 30-52-01-000-801 AND TASK 32-52-01-400-801-A01. LEAK CHECK OF ACTUATOR GOOD, OPS TEST IAW 30-51-00-710-801, OPS CHECK GOOD. REMOVED AND REPLACED PILOTS CONTROL HAND WHEEL, GROUND TAXI AIRCRAFT, TAXI CHECK GOOD. OPERATIONAL CHECK FLIGHT GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CHIMNEY — TORN (FWD CARGO BAY) · airframe 7,249 hrs · 5,467 cycles

DURING MAINTENANCE INSPECTION, MAINTENANCE FOUND THE FORWARD CARGO BAY CHIMNEY DAMAGED. MAINTENANCE REMOVED AND REPLACED THE CHIMNEY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 7,014 hrs · 5,288 cycles

UPPER SURFACE OF CABIN FLOOR SUPPORT CHANNEL, IMMEDIATELY AFT OF COCKPIT BULKHEAD AT FS 280.00 IS CRACKED AT TWO PLACES. REPAIRED IAW EA R-53-205 AND REO 670-53-11-042 AND REO 670-53-11-043.

Part: BULKHEAD — CORRODED (ZONE 100) · airframe 7,014 hrs · 5,288 cycles

UPPER SURFACE OF CABIN FLOOR SUPPORT CHANNEL IMMEDIATELY AFT OF COCKPIT BULKHEAD AT FS 280.00 IS CORRODED FROM LBL 22.0 TO RBL 22.00. REPAIRED IAW EA R-53-203.

Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 7,014 hrs · 5,288 cycles

AFT SUPPORT BEAM FOR COCKPIT FLOOR PANEL 221 ALF IS CORRODED ON UPPER SURFACE. REPAIRED IAW CRJ-700 SRM 51-40-11 AND SRM 51-25-06.

Part: FASTENER — SHEARED (RT TE FLAP) · airframe 7,008 hrs · 5,284 cycles

ON RIGHT HAND FLAP SHROUD (TRAILING WING BOX) BETWEEN NR 3 AND NR 4 FLAP CANOE HAS FOUR PLACES SHOWING SHEARED RIVET HEADS IN FLAP COVE. REPLACED FASTENERS PER SRM 51-42-06-001-001.

Part: BLADE — VIBRATION (RT ENGINE) · airframe 6,620 hrs · 4,961 cycles

BOI - FLIGHT 2520 ON CLIMB, RIGHT ENGINE N1 VIBRATION 1.8. REDUCED POWER/CHECKLIST, DROPPED TO 1.3. MAINTENANCE COMPLIED WITH INSPECTION OF FAN BLADES, LOOSENED STIFF BLADE. COMPLIED WITH VIBRATION CHECK, WITHIN LIMITS. PLACED ON RSI TO LUBE FAN BLADE TANGS IN NEXT 10 FLIGHT HOURS. MAINTENANCE REPLACED NR 2 ENGINE FAN BLADES IAW HORIZON AIR EO R-52-218. PERFORMED VIBRATION CHECK IAW CRJ MM TASK 71-00-00-720-806. OPERATIONAL CHECK GOOD. MAXIMUM VIBRATION .3 AT TOGA. AIRCRAFT RETURNED TO SERVICE.

Part: DUCT — LEAKING (BLEED AIR) · airframe 6,532 hrs · 4,902 cycles

BOI FLIGHT 2522 RETURN TO FIELD FOR RIGHT BLEED DUCT WARNING LIGHT - LIGHT EXTINGUISHED AT COMPLETION OF EMERGENCY CHECKLIST WHEN AIRCRAFT WAS DEPRESSURIZED. MAINTENANCE REMOVED BLEED AIR CROSSOVER DUCT IAW RT 36-0078. NO ABNORMAL INDICATIONS OR LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: IMPELLER — VIBRATION (ZONE 400) · airframe 6,288 hrs · 4,707 cycles

PDX - ON FLIGHT NUMBER 2555, ON CLIMBOUT, NR 1 FAN VIBRATION ROSE ABOVE 1.7. AFTER LERCHING AT 29,000 FT, AIRCRAFT COULD NOT MAINTAIN CRUISE SPEED WITH POWER SET TO KEEP FAN ON THE GREEN ARC. FOUND ONE BLADE TIGHT. LOOSENED AS REQUIRED. GROUND RAN AIRCRAFT WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (ZONE 200) · airframe 6,227 hrs · 4,660 cycles

PDX - AFT CARGO SMOKE DETECTOR CAUTION MESSAGE DISPLAYED, THEN WENT OUT. INSPECTED BOTH AFT CARGO SMOKE DETECTORS WITH NO DEFECTS FOUND. NO CAUTION MESSAGES DISPLAYED. AIRCRAFT RETURNED TO SERVICE.

Part: UPLOCK — DISENGAGED (ZONE 800) · airframe 6,203 hrs · 4,641 cycles

PDX - FLIGHT 2553 - UNABLE TO OPEN FORWARD GALLEY SERVICE DOOR. MAINTENANCE INSPECTED THE DOOR AND FOUND THE DOOR UPLOCK ACTUATOR INNER AND OUTER ASSEMBLIES DISENGAGED. THE ASSEMBLIES WERE RE-ENGAGED AND OPERATIONAL CHECKS WERE PERFORMED. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 6,199 hrs · 4,637 cycles

FLIGHT 2465 - THE CREW REPORTED THAT AFTER TAKE-OFF, THE GEAR FAILED TO RETRACT. THE FLIGHT CONTINUED ON TO PDX AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE WHEEL CENTERING PROX SENSORS OUT OF ADJUSTMENT. THE SENSORS WERE ADJUSTED, OPERATIONAL CHECKS WERE PERFORMED, AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BLADE — STUCK (NR 2 ENGINE) · airframe 5,950 hrs · 4,446 cycles

ON FLIGHT FROM BOI TO SJC. NR 2 ENGINE N1 VIBRATION. AIRCRAFT RETURNED TO FIELD AND MAINTENANCE FREED STUCK BLADE. NO PARTS REPLACED OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FAN BLADE — DAMAGED (NR 1 ENGINE) · airframe 5,781 hrs · 4,324 cycles

TUS FLIGHT 2505 RETURN TO FIELD: NR 1 ENGINE VIBRATION 2.4 MILS. MAINTENANCE REPLACED FAN BLADES IHI1387N, IHI1392N, IHI1399N, IHI1429N, IHI1495N, IHI1501N, IHI1683N, IHI1693N, INI1702N, IHI1735N, IHI1737N IHI1739N, IHI1741N, IHI1744N, IHI1745N, IHI1747N, IHI1748N, IHI1751N, IHI1752N, IHI1754N, IHI1758N, IHI2178N, IHI2192N, IHI2193N, IHI2778N, IHI2874N, IHI3774N, IHI5186N. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SCREEN — TORN (CARGO BAY) · airframe 5,521 hrs · 4,133 cycles

PDX - FORWARD CARGO BAY CENTER CHIMNEY SCREEN IS TORN. REMOVED AND REPLACED CHIMNEY.

Part: PIN — BACKED OUT (CONNECTOR) · airframe 5,440 hrs · 4,078 cycles

PDX - FLIGHT 2543 - WHEN SELECTING RIGHT BOOST PUMP ON, NEITHER THE RIGHT OR LEFT BOOST PUMPS TURN ON. WHEN SELECTING LEFT BOOST PUMP ON, SYSTEM OPERATES NORMALLY. MAINTENANCE INSPECTED THE FUEL SYSTEM AND FOUND AN OPEN WIRE FROM THE FUEL CONTROL PANEL TO K56 RELAY X1. RESET PIN-J OF THE CANNON PLUG AND PERFORMED AN OPERATIONAL CHECK. THE CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: VALVE — INOPERATIVE (ANTI ICE SYS) · airframe 5,276 hrs · 3,959 cycles

SMF FLIGHT 2527 RETURNED TO FIELD. RIGHT COWL ANTI ICE FAULT CAUTION MESSAGE WHEN SELECTED ON. REPLACED VALVE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — VIBRATION (ZONE 400) · airframe 5,269 hrs · 3,953 cycles

PDR FLIGHT 2553 RETURN TO FIELD - NR 1 ENGINE N1 VIBRATION 1.7 TO 1.9. COMPLIED WITH PIN LUBES AND ENGINE RUNS. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DAMAGED (PAX DOOR) · airframe 5,257 hrs · 3,942 cycles

PDX - THE MAIN CABIN DOOR FORWARD LOWER SKIN REQUIRES PERMANENT REPAIR. MAINTENANCE FABRICATED REPAIR STRAP AND FILLERS FROM 2024T3 AND INSTALLED SAME IAW EA R-52-132A AND REO 670-52-11-040.

Part: WARNING LIGHT — FALSE INDICATION (ZONE 400) · airframe 4,990 hrs · 3,737 cycles

RT COWL ANTI-ICE CAUTION MESSAGE IN FLIGHT WHEN RIGHT COWL ANTI-ICE IS SELECTED ON. SAT -38 DEGREES C. COMPLIED WITH EMERGENCY/ABNORMAL CHECKLIST AND MESSAGE REMAINED ON. CLIMBED OUT OF ICING CONDITIONS. DURING DESCENT RT COWL ANTI-ICE OPERATED NORMALLY. GROUND RAN BOTH ENGINES AND CHECKED COWL ANTI-ICE SYSTEM IAW MM 30-20-00. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — BENT (ZONE 800) · airframe 4,690 hrs · 3,521 cycles

MAIN CABIN DOOR OUTER SKIN BENT AT LOWER FORWARD CORNER. REPAIRED IAW HORIZON AIR EA R-52-132. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — DIRTY (ZONE 400) · airframe 4,398 hrs · 3,306 cycles

ON FLIGHT 2452 ABORTED TAKEOFF DUE TO LEFT THRUST REVERSER UNSAFE CAUTION MESSAGE. CLEANED HYDRAULIC FLUID RESIDUE FROM NR 1 ICV CONNECTORS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CHIMNEY — DAMAGED (CARGO BAY) · airframe 4,030 hrs · 3,032 cycles

BOI- CENTER CHIMNEY DAMAGED. REMOVED AND REPLACED DAMAGED CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 3,798 hrs · 2,866 cycles

SEA- ON FLIGHT 2423 SMOKE AFT LAVATORY MESSAGE. REMOVED AND REPLACED SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RIVET — DAMAGED (ZONE 200) · airframe 3,431 hrs · 2,597 cycles

RIVET DAMAGED AT STRINGER 8R, 4.5 INCHES AFT OF FS 724.08. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-46-06, PG 1-8.

Part: STRINGER — DAMAGED (ZONE 100) · airframe 3,431 hrs · 2,597 cycles

RIVET DAMAGED AT STRINGER 19R, 17 INCHES AFT OF FS250. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 25-42-06, PG 1-8.

Part: RIVET — DAMAGED (ZONE 200) · airframe 3,431 hrs · 2,597 cycles

RIVET DAMAGED AT FS 409, 2 INCHES ABOVE STRINGER 15R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.

Part: RIVET — DAMAGED (ZONE 200) · airframe 3,431 hrs · 2,597 cycles

RIVET DAMAGED AT FS 830.4, 2 INCHES ABOVE STRINGER 10R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.

Part: FASTENER — DAMAGED (ZONE 200) · airframe 3,431 hrs · 2,597 cycles

FASTENER DAMAGED, 3 INCHES FORWARD OF FS597 AND 2 INCHES ABOVE STRINGER 10R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-20, PG 13-22.

Part: RIVET — DAMAGED (ZONE 200) · airframe 3,431 hrs · 2,597 cycles

RIVET DAMAGED AT STRINGER 15R, 3 INCHES AFT OF FS379. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.

Part: SKIN — DAMAGED (ZONE 100) · airframe 3,431 hrs · 2,597 cycles

BURN MARK ON SKIN .2 INCHES BELOW BOTTOM EDGE OF ADG DOOR, 9 INCHES AFT OF FS169. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.

Part: RIVET — DAMAGED (ZONE 200) · airframe 3,431 hrs · 2,597 cycles

RIVET DAMAGED AT FS421, 2 INCHES BELOW STRINGER 14R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.

Part: RIVET — DAMAGED (ZONE 200) · airframe 3,431 hrs · 2,597 cycles

RIVET DAMAGED AT FS469, 3 INCHES ABOVE STRINGER 14R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.

Part: RIVET — DAMAGED (ZONE 100) · airframe 3,431 hrs · 2,597 cycles

RIVET DAMAGED AT FS295, 2 INCHES BELOW STRINGER 18R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.

Part: RIVET — DAMAGED (ZONE 100) · airframe 3,431 hrs · 2,597 cycles

RIVET DAMAGED AT .5 INCHES BELOW BOTTOM EDGE OF ADG DOOR, 15INCHES AFT OF FS169. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.

Part: RIVET — DAMAGED (ZONE 200) · airframe 3,431 hrs · 2,597 cycles

RIVET DAMAGED AT FS 953, 2 INCHES ABOVE STRINGER 12R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.

Part: RIVET — DAMAGED (ZONE 200) · airframe 3,431 hrs · 2,597 cycles

RIVET DAMAGED ON STRINGER 11R, 4 INCHES FORWARD OF FS 893. REPAIRED IAW SRM 51-25-16. PG 7 AND SRM 51-42-06, PG 1-8.

Part: RIVET — DAMAGED (ZONE 200) · airframe 3,431 hrs · 2,597 cycles

RIVET DAMAGED AT STRINGER 8R, 7 INCHES AFT OF FS645. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-03 PG 1-8.

Part: RIVET — DAMAGED (ZONE 200) · airframe 3,431 hrs · 2,597 cycles

RIVET DAMAGED AT STRINGER 12R, 4 INCHES FORWARD OF FS533. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.

Part: RIVET — DAMAGED (ZONE 200) · airframe 3,431 hrs · 2,597 cycles

RIVET DAMAGED AT FS 394, 1 INCH ABOVE STRINGER 15R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.

Part: RIVET — DAMAGED (ZONE 200) · airframe 3,431 hrs · 2,597 cycles

RIVET DAMAGED AT FS693, 4 INCHES BELOW STRINGER 8R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-03, PG 1-8.

Part: RIVET — DAMAGED (ZONE 200) · airframe 3,431 hrs · 2,597 cycles

PDX-RIVET DAMAGED AT FS 364, 3 INCHES ABOVE STRINGER 17R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.

Part: RIVET — DAMAGED (ZONE 100) · airframe 3,431 hrs · 2,597 cycles

RIVET DAMAGED AT STRINGER 18R, 6 INCHES AFT OF FS 235. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.

Part: RIVET — DAMAGED (ZONE 200) · airframe 3,431 hrs · 2,597 cycles

RIVET DAMAGED AT STRINGER 9R, 5 INCHES AFT OF FS 797. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.

Part: RIVET — DAMAGED (ZONE 200) · airframe 3,431 hrs · 2,597 cycles

RIVET DAMAGED AT STRINGER 13R, 1 INCH AFT OF FS501. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.

Part: FASTENER — DAMAGED (ZONE 200) · airframe 3,431 hrs · 2,597 cycles

FASTENER DAMAGED AT 4 INCHES AFT OF FS549 AND 7 INCHES ABOVE STRINGER 12R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-20, PG 13-22.

Part: CHIMNEY — DAMAGED (ZONE 100) · airframe 3,364 hrs · 2,547 cycles

THE FORWARD, CENTER, AND AFT SECTIONS OF THE SMOKE DETECTOR CHIMNEY ARE DAMAGED. MAINTENANCE REPLACED THE DAMAGED SECTIONS AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: STRIKER — CRACKED (ZONE 800) · airframe 3,271 hrs · 2,483 cycles

PDX-FORWARD LOWER CORNER OF PASSENGER DOOR SEAL STRIKER ON FUSELAGE HAS A GOUGE AND CRACK IN METAL. REPAIRED IAW CRJ-700 SRM 51-42-06.

Part: SKIN — DENTED (ZONE 200) · airframe 3,271 hrs · 2,483 cycles

PDX-DENT IN FUSELAGE AT STATION 349.00 MID FUSELAGE JUST AFT OF MAIN CABIN DOOR CUTOUT. REPAIRED IAW CRJ-700 SRM 53-00-01, SRM 51-12-00 AND SRM 51-25-16. HORIZON AIR EA R53-95, R53-94 AND EO 670-53-21-035.

Part: SKIN — NICKED (ZONE 800) · airframe 3,271 hrs · 2,483 cycles

PDX-TWO NICKS IN FUSELAGE SKIN EDGE ON AFT SIDE OF PASSENGER DOOR CUTOUT. REPAIRED IAW CRJ-700 SRM 51-25-16 AND SRM 51-00-01. HORIZON AIR EA R53-95, R53-93 AND EO 370-53-21-035.

Part: SKIN — CHAFED (ZONE 200) · airframe 3,271 hrs · 2,483 cycles

PDX-SKIN CHAFED AT FS319.00 ON LT SIDE, MID FUSELAGE JUST FORWARD OF CUTOUT FOR MAIN CABIN DOOR. REPAIRED IAW CRJ-700 SRM 51-25-16 AND HORIZON AIR EA R53-95 AND EO 670-53-21-035.

Part: SKIN — CORRODED (ZONE 200) · airframe 3,271 hrs · 2,483 cycles

AIRCRAFT SKIN HAS LIGHT SURFACE CORROSION AT UPPER TCAS ANTENNA MOUNT POINT.REPAIRED IAW CRJ NDT 51-20-06.

Part: SKIN — GOUGED (ZONE 200) · airframe 3,271 hrs · 2,483 cycles

PDX-GOUGE IN UPPER FUSELAGE SKIN AT FS 394.00 ON LT SIDE. REPAIRED IAW CRJ700 SRM 53-00-01, SRM 51-21-11 AND SRM 51-21-16.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 3,271 hrs · 2,483 cycles

INTERCOSTAL IMMEDIATELY FORWARD OF REAR PRESSURE BULKHEAD IS CRACKED AT HYDRUALIC LINE FEED THROUGH OF LEFT HAND SIDE. REPAIRED IAW HORIZON AIR EO R-29-07.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 3,271 hrs · 2,483 cycles

INTERCOSTAL IMMEDIATELY FORWARD OF REAR PRESSURE BULKHEAD CRACKED AT RIGHT HAND HYDRUALIC PRESSURE LINE FEED THROUGH. REPAIRED IAW HORIZON AIR EO R-29-07.

Part: SENSOR — LEAKING (ZONE 100) · airframe 2,798 hrs · 2,162 cycles

BIL-ON FLIGHT NUMBER 2483, FLUID LEAKING AT AIRCRAFT TAIL NEAR APU. REMOVED AND REPLACED PRIMARY EJECTOR SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — LEAKING (FUEL SYSTEM) · airframe 2,606 hrs · 2,035 cycles

PDX-FUEL LEAKING FROM RIGHT HAND FUEL ENGINE INLET PRESSURE SENSOR. REPLACED NR 2 RIGHT HAND FUEL ENGINE INLET PRESSURE SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SENSOR — FAILED (LT ENGINE) · airframe 2,464 hrs · 1,938 cycles

PDX- DURING FLIGHT SEA-FAT AIRCRAFT DIVERTED TO PDX DUE TO: AT CRUISE POWER FLIGHT LEVEL 370 NOTED LEFT ENGINE TEMPERATURE IN RED AT 164 DEGREES FLUCTUATING TO 145 DEGREES. SHORTLY AFTER "LOW OIL QUANTITY" STATUS MESSAGE. REDUCED POWER ON LEFT ENGINE TO BRING TEMPERATURE INTO NORMAL RANGE. OIL PRESSURE REMAINED CONSTANT AND NORMAL THROUGHOUT. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED OIL LEVEL/TEMPERATURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CAGE — PUNCTURED (CARGO BAY) · airframe 2,449 hrs · 1,923 cycles

SEA- FORWARD CARGO SMOKE DETECTOR SCREEN HAS PUNCTURE HOLE. REMOVED AND REPLACED SMOKE DETECTION SCREEN. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — FAULTY (HORIZ STAB) · airframe 2,379 hrs · 1,867 cycles

BOI- RETURNED TO FIELD DUE TO STABILIZER TRIM, MACH TRIM CAUTION MESSAGES INFLIGHT. STABILIZER AND MACH TRIM WOULD NOT RESET. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED STABILIZER 1 ENGAGE SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — FAILED (FUEL SYSTEM) · airframe 2,311 hrs · 1,818 cycles

SJC - AFTER ENGINE START THE LEFT FUEL LOW PRESSURE CAUTION STAYED ON. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE ENGINE FUEL FEED SWITCH. OPERATIONAL AND LEAKS CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — LEAKING (FUEL SYSTEM) · airframe 2,259 hrs · 1,782 cycles

BOI-FUEL LEAK AT CENTER SECTION. REMOVED AND REPLACED ENGINE FUEL FEED SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BRACKET — MISINSTALLED (FUEL SYSTEM) · airframe 2,188 hrs · 1,720 cycles

PDX- BRACKET NUMBER IS INSTALLED IN THE REVERSE POSITION. REPARIED IAW HORIZON AIR EO R-28-82 "A".

Part: WARNING SYSTEM — ACTIVATED (NR 1 HYD SYS) · airframe 2,113 hrs · 1,670 cycles

LGB - EMERGENCY CHECKLIST WAS PERFORMED WHEN THE CREW RECEIVED A MESSAGE THAT THE NR 1 HYDRAULIC SYSTEM FAILED DUE TO FLUID LOSS. THE ELECTRIC HYDRAULIC PUMP WAS ACTIVATED AND REMAINED IN OPERATION FOR ABOUT .5 HOUR, AT WHICH TIME IT FAILED DUE TO FLUID LOSS. THE NR 1 HYDRAULIC SYSTEM WAS SECURED AND THE AICRAFT LANDED WITHOUT INCIDENT. AIRCRAFT DOWN FOR MAINTENANCE.

Part: CAGE — DAMAGED (CARGO BAY) · airframe 1,973 hrs · 1,560 cycles

BOI- FORWARD CARGO CENTER CHIMNEY IS TORN AND BENT. REPLACED CHIMNEY WITH SERVICEABLE ONE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CHAFED (LT WING) · airframe 1,545 hrs · 1,264 cycles

CKB - LEFT HAND SIDE LEADING EDGE CHAFED AND INBOARD LOWER SIDE OF MID SLAT, INBOARD CHAFED AT WS 199.66. REPAIRED IAW WVAC EO 610R-57-4033 AND HORIZON AIR EA R-57-05.

Part: CAGE — DAMAGED (CARGO BAY) · airframe 1,450 hrs · 1,198 cycles

PDX- FORWARD CARGO BAY CHIMNEY ASSEMBLY AT TOP OF DOOR OPENING HAS SCREEN DAMAGE. MESH IS PULLED AWAY ON OUTBOARD SIDE. REMOVED AND REPLACED FORWARD CARGO BAY CHIMNEY ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 682 hrs · 616 cycles

SEA - SYSTEM ONE HYDRAULIC LOW PRESS CAUTION LIGHT CAME ON AND NUMBER ONE HYDRAULIC SYSTEM QUANTITY SHOWS ZERO IN FLIGHT. CREW PERFORMED EMERGENCY/ABNORMAL CHECKLIST. FOUND LEFT ENGINE DRIVEN HYDRAULIC PUMP LEAKING. REPLACED THE NUMBER ONE HYDRAULIC PUMP. OPERATIONAL CHECK AND LEAK CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.