N608QX

Part: SUPPORT — CORRODED (BS 879-909) · airframe 36,165 hrs · 26,758 cycles

AFT FUSELAGE FAIRING SUPPORT, RBL 18 CORRODED AROUND SCREW HOLES BOTTOM SIDE BS 879 & 909. REPLACED FAIRING SUPPORT IAW SRM REQUIREMENTS.

Part: SKIN — CORRODED (E/E BAY DOOR) · airframe 36,164 hrs · 26,757 cycles

DURING C-CHECK, THE AVIONICS BAY DOOR OPENING INNER SURFACE HAD SEVERAL AREAS OF CORROSION AT SEAL INTERFACE, FOUND TO BE OUT OF LIMITS. REPAIRED THE DOOR IAW REO 670-53-21-242.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 36,164 hrs · 26,757 cycles

DURING C-CHECK, THE RT INTERCOSTAL STRINGER 27R WAS CORRODED BETWEEN BS 349 TO 364. REPLACED IAW SRM.

Part: SEAT TRACK — CORRODED (BS 715-746) · airframe 36,165 hrs · 26,758 cycles

SEAT TRACK AT BS 715 TO 746 CORRODED. REPAIRED THE SEAT TRACK IAW AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 681-708) · airframe 36,165 hrs · 26,758 cycles

SEAT TRACK, BS 681 TO 708 CORRODED. REPAIRED THE SEAT TRACK IAW AMM 53-00-49-400-801-A01, & SRM 51-41-04-001-001-A01.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 36,165 hrs · 26,758 cycles

PAX DOOR LOWER SILL FLOOR SUPPORT ANGLE CORRODED. REPAIRED IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 842-860) · airframe 36,165 hrs · 26,758 cycles

SEAT TRACK, BS 842 TO 860 CORRODED. REPAIRED THE SEAT TRACK IAW AMM 53-00-49-400-801-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 36,165 hrs · 26,758 cycles

BS 280 FLOORBEAM HAS CORROSION AROUND FASTENER HOLES. REPAIRED IAW SRM 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 850-877) · airframe 36,165 hrs · 26,758 cycles

SEAT TRACK, RBL 9, BS 850.75 TO 877 CORRODED. REPAIRED THE SEAT TRACK IAW AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 938-953) · airframe 36,165 hrs · 26,758 cycles

SEAT TRACK, BS 938 TO 953 CORRODED. REPAIRED THE SEAT TRACK IAW AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 581-645) · airframe 36,165 hrs · 26,758 cycles

SEAT TRACK, BS 581 TO 645 CORRODED. REPAIRED THE SEAT TRACK IAW AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 583-677) · airframe 36,165 hrs · 26,758 cycles

SEAT TRACK, RBL 9 BS 583 TO 677 CORRODED. REPAIRED THE SEAT TRACK IAW AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 505-580) · airframe 36,165 hrs · 26,758 cycles

SEAT TRACK, LBL 9, BS 505 TO 580 CORRODED. REPAIRED THE SEAT TRACK IAW AMM 53-00-49-400-801-A01

Part: SEAT TRACK — CORRODED (BS 686-693) · airframe 36,165 hrs · 26,758 cycles

SEAT TRACK, LBL 9, BS 686 TO 693 CORRODED. REPAIRED THE SEAT TRACK IAW AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 836-850) · airframe 36,165 hrs · 26,758 cycles

RT SEAT TRACK AT RBL 9, BS 836.55 TO 850.45 CORRODED. REPLACED THE SEAT TRACK SECTION IAW SRM AND AMM REQUIREMENTS.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,165 hrs · 26,758 cycles

PAX DOOR INTERCOSTAL AT AFT FORMER CORRODED AT THE PROXIMITY SWITCH BRACKET. REPAIRED IAW SRM REQUIREMENTS.

Part: SEAT TRACK — CORRODED (BS 701-836) · airframe 36,165 hrs · 26,758 cycles

SEAT TRACK, LBL 9, BS 701.45 TO 836.55 CORRODED. REPLACED THE SEAT TRACK SECTION IAW SRM AND AMM REQUIREMENTS.

Part: SEAT TRACK — CORRODED (BS 850-988) · airframe 36,165 hrs · 26,758 cycles

SEAT TRACK, LBL 9, BS 850.45 TO 988 CORRODED. REPLACED THE SEAT TRACK SECTION IAW SRM AND AMM REQUIREMENTS.

Part: SPACER — CORRODED (ZONE 100) · airframe 36,165 hrs · 26,758 cycles

RAD ALT ANTENNA NR 2 MOUNTING PLATE CORRODED. FABRICATED NEW SPACER PLATES IAW DWG AF670-70326 REV --. REMOVED AND INSTALLED NEW PLATES IAW SRM REQUIREMENTS AND EC/TC EA 30-2017-006, REV 0.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 36,165 hrs · 26,758 cycles

PASSENGER DOOR LOWER SILL FLOOR SUPPORT ANGLE CORRODED. REPLACED FLOOR SUPPORT ANGLE IAW SRM REQUIREMENTS.

Part: SUPPORT FRAME — CORRODED (BS 939) · airframe 36,165 hrs · 26,758 cycles

AFT FUSELAGE FAIRING SUPPORT FARME AT BS 939 CORRODED ALONG BOTTOM SIDE OF LOWER ANGLE. REPLACED LOWER SUPPORT FRAME IAW EA 40-2016-387, REV -, AND SRM REQUIREMENTS.

Part: SEAT TRACK — CORRODED (BS 707-708) · airframe 36,165 hrs · 26,758 cycles

RT SIDE SEAT TRACK BETWEEN APPROXIMATELY BS 707 TO 708 CORRODED. REPLACED THE SEAT TRACK SECTION IAW SRM AND AMM.

Part: WEB — CORRODED (PAX DOOR) · airframe 36,165 hrs · 26,758 cycles

PASSENGER DOOR FWD WEB HAS MULTIPLE AREAS OF OUT OF LIMITS CORROSION. WEB REPLACED PER SRM, AMM, AND CMM.

Part: SEAT TRACK — CORRODED (BS 400-473) · airframe 36,165 hrs · 26,758 cycles

LT SIDE SEAT TRACK SECTION AT APPROXIMATELY BS 400 TO 473 CORRODED. REPLACED THE SEAT TRACK SECTION IAW SRM AND AMM.

Part: ATTACH ANGLE — CORRODED (FWD CARGO BAY) · airframe 36,165 hrs · 26,758 cycles

FWD CARGO BAY CARGO TRACK ATTACH ANGLE CORRODED. REPAIRED EA 25-2016-333, REV-, AND DRAWING SH670-33573.

Part: SEAT TRACK — CORRODED (BS 517-568) · airframe 36,165 hrs · 26,758 cycles

RT SIDE SEAT TRACK SECTION AT APPROXIMATELY BS 517 TO 568 CORRODED. REPLACED SEAT TRACK SECTION IAW SRM AND AMM.

Part: SEAT TRACK — CORRODED (BS 581-683) · airframe 36,165 hrs · 26,758 cycles

SEAT TRACK LBL 9, BS 581 TO 683 CORRODED. REPLACED THE SEAT TRACK SECTION IAW SRM AND AMM.

Part: SEAT TRACK — CORRODED (BS 904-936) · airframe 36,165 hrs · 26,758 cycles

RT SEAT TRACK SECTION BS 904 TO 936 CORRODED. REPLACED THE SEAT TRACK SECTION IAW SRM AND AMM.

Part: SEAT TRACK — CORRODED (BS 865-916) · airframe 36,165 hrs · 26,758 cycles

LT SIDE SEAT TRACK SECTION BS 865 TO 916 CORRODED. REPLACED SEAT TRACK SECTION PER SRM AND AMM.

Part: SEAT TRACK — CORRODED (BS 688-693) · airframe 36,165 hrs · 26,758 cycles

SEAT TRACK SECTION RBL 9, BS 688 TO 693 CORRODED. REPLACED THE SEAT TRACK SECTION IAW SRM AND AMM.

Part: SEAT TRACK — CORRODED (BS 842-858) · airframe 36,165 hrs · 26,758 cycles

RT SIDE SEAT TRACK SECTION BS 842 TO 858 CORRODED. REPLACED SEAT TRACK SECTION IAW SRM AND AMM.

Part: SEAT TRACK — CORRODED (BS 722-761) · airframe 36,165 hrs · 26,758 cycles

LT SIDE SEAT TRACK SECTION BS 722 TO 761 CORRODED. REPLACED SEAT TRACK SECTION IAW SRM AND AMM.

Part: SEAT TRACK — CORRODED (BS 500-586) · airframe 36,165 hrs · 26,758 cycles

LT SIDE SEAT TRACK BS 500 TO 586 CORRODED. REPLACED THE SEAT TRACK SECTION IAW SRM AND AMM.

Part: SEAT TRACK — CORRODED (BS 785-828) · airframe 36,165 hrs · 26,758 cycles

LT SIDE SEAT TRACK SECTION BS 785 TO 828 CORRODED. REPLACED SEAT TRACK SECTION IAW SRM AND AMM.

Part: ATTACH ANGLE — CORRODED (PAX DOOR) · airframe 36,164 hrs · 26,757 cycles

DURING C-CHECK THE PAX DOOR LOWER ATTACHMENT ANGLE FOR BOTTOM STEP CORRODED. REPLACED PER SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,164 hrs · 26,757 cycles

DURING C-CHECK SEAT TRACK RBL 9 FS 349 TO FS 469 CORRODED. REPLACED SEAT TRACK PER SRM.

Part: SEAT TRACK — CORRODED (BS 785-829) · airframe 36,165 hrs · 26,758 cycles

RT SIDE SEAT TRACK SECTION BS 785 TO 829 CORRODED. REPLACED SEAT TRACK SECTION IAW SRM AND AMM.

Part: SEAT TRACK — CORRODED (BS 486-566) · airframe 36,165 hrs · 26,758 cycles

SEAT TRACK, RBL 9, BS 486 TO 566 CORRODED. REPLACED THE SEAT TRACK SECTION IAW SRM AND AMM.

Part: SEAT TRACK — CORRODED (BS 580-645) · airframe 36,165 hrs · 26,758 cycles

SEAT TRACK SECTION, LT SIDE BS 580 TO 645 CORRODED. REPLACED THE SEAT TRACK SECTION IAW SRM AND AMM REQUIREMENTS.

Part: FRAME — CORRODED (BS 349) · airframe 36,164 hrs · 26,575 cycles

DURING C-CHECK, THE FUSELAGE FRAME AT BS 349 WAS FOUND CORRODED AT STRINGER 27L. THE FRAME WAS REPLACED IAW SRM.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 36,164 hrs · 26,757 cycles

DURING C-CHECK, THE INTERCOSTAL STRINGER 27L WAS CORRODED BEYOND LIMITS. REPLACED IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,164 hrs · 26,757 cycles

DURING C-CHECK STR 25L WAS CORRODED BETWEEN FS319 AND FS333. PART REPLACED PER SRM REQUIREMENTS.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 36,164 hrs · 26,757 cycles

DURING C-CHECK THE TCAS ANTENNA DOUBLER FOUND CORRODED BETWEEN FS 295 AND FS 310. REPLACED DOUBLER PER SRM REQUIREMENTS.

Part: LONGERON — CORRODED (BS 349-364) · airframe 36,164 hrs · 26,757 cycles

DURING C-CHECK, THE LONGERON WAS CORRODED BETWEEN BS 349 TO 364, STRINGER 25R. REPLACED IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,164 hrs · 26,757 cycles

DURING C-CHECK FRAME 319 WAS CORRODED BETWEEN STR 27 AND 26L. REPLACED FRAME SECTION PER EC/TC REO 670-53-21-799 REV A.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,164 hrs · 26,757 cycles

DURING C-CHECK STR 25R WAS CORRODED BETWEEN FS280 TO FS295. REPLACED STRINGER 25R FS295 TO FS333 PER SRM REQUIREMENTS.

Part: ANGLE — CORRODED (ZONE 100) · airframe 36,164 hrs · 26,757 cycles

DURING C-CHECK THE FLOOR PANEL ANGLE CORRODED AT FS 280 ABOVE STR 27. REPLACED PER SRM REQUIREMENTS.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 35,519 hrs · 26,205 cycles

CABIN EMERGENCY LIGHTS CEILING AT ROW 15 INOPERATIVE. REPAIRED CONNECTOR AT ROW 15 EMERGENCY FLOOD LIGHT IAW ESPM 20-26-03. OPS CHECKED GOOD.

Part: SUPPORT — DAMAGED · airframe 35,336 hrs · 26,061 cycles

LIGHTNING STRIKE DAMAGE TO END FRAME SUPPORT FOR VERTICAL AFT FAIRING ATTACHMENT. BLENDED OUT LIGHTNING STRIKE DAMAGE ON BULLET FAIRING AFT FRAME IAW SRM 51-12-00. PERFORMED ULTRASONIC THICKNESS CHECK OF BLENDED AREA INSIDE THE FLANGE COMMON TO REWORKED AREA IAW NDTM 51-00-001. REMAINING THICKNESS IS: 0..053". THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: BRACKET — DAMAGED (VERTICAL STAB) · airframe 35,336 hrs · 26,061 cycles

LIGHTNING STRIKE DAMAGE TO VERTICAL STABILIZER AFT FRAME CONDUIT BRACKET. BLENDED OUT LIGHTNING STRIKE DAMAGE ON AFT FRAME CONDUIT BRACKET IAW SRM 51-12-00. PERFORMED EDDY CURRENT INSPECTION OF BLENDED AREA ON AFT FRAME CONDUIT BRACKET IAW NDTM 51-20-006, PART 1. NO CRACKS NOTED AT THIS TIME. RESTORED FINISH A010, REF REO 670-55-32-188. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: MEGAPHONE — DAMAGED (CABIN) · airframe 34,534 hrs · 25,434 cycles

MEGAPHONE DAMAGED. R & R MEGAPHONE IAW AMM 25-61-14.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 34,213 hrs · 25,170 cycles

GALLEY FWD LOWER EXIT SIGN HAD ONE BULB BURNED OUT. R & R LOWER EXIT SIGN LIGHT BULB IAW AMM 33-51-05. OPS CHECKED GOOD.

Part: FRAME — CRACKED (BS 220) · airframe 33,408 hrs · 24,526 cycles

RT FS 220, FRAME HAS AN INDICATION NOTED AT FASTENER HOLE INBD OF LIGHTING HOLE BELOW STG 13A .800" LONG. FAILED NDT INSPECTION. REMOVED RT FS 220, UPPER FRAME SECTOR IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW RT FS 220 UPPER FRAME SECTOR, PN CC670-34146-6 IAW SRM 51-40-11-001-001-A01, REV 30, JUN 25,2013. INSTALLED NEW RT FS 220 UPPER FRAME SECTOR, PN CC670-34146-6 IAW SRM'S 51-42-06-001-001-A01 AND 51-42-21-001-001-A01, REV 30 JUN 25,2013.

Part: FRAME — CRACKED (BS 220) · airframe 33,404 hrs · 24,519 cycles

LEFT FS 220 FRAME HAS AN INDICATION NOTED AT FASTENER HOLE INBD OF LIGHTING HOLE BELOW STR 13A .800" LONGERON FAILED NDT INSPECTION. REMOVED LT FS 220 UPPER FRAME SECTOR IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. LOCATED & DRILLED SERVICEABLE FRAME PN CC670-34146-1 IAW SRM 51-40-11-001-001-A01, REV 30, DATED JUN 25/2013. INSTALLED NEW SERVICEABLE FS 220 UPPER FRAME SECTOR PN CC670-34146-1 IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01 BOTH AT REV 30, DATED JUN 25/2013.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 31,450 hrs · 23,028 cycles

EMERGENCY LIGHTS INOPERATIVE. GATE RETURN. ALLOWED AMPLE TIME FOR EMERGENCY LIGHTS BATTERY PACKS TO CHARGE, PERFORMED OPS CHECK IAW AMM 33-51-00. ALL CHECKS GOOD.

Part: SUPPORT BRACKET — DAMAGED · airframe 31,297 hrs · 22,911 cycles

WHILE REMOVING AND REPLACING EXTERNAL POWER SUPPORT BRACKET, STRINGER 23 WAS DAMAGED AT FASTENER HOLES. COMPLETED STRINGER 23R INSTALLATION AND COMPLIED WITH REO 670-53-11-939. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: SEAT TRACK — CORRODED (BS 861-696) · airframe 31,297 hrs · 22,911 cycles

RT SIDE SEAT TRACK BS 861-969 IS CORRODED. R & R SEAT TRACK IAW AMM 53-00-49, TASK 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 675-713) · airframe 31,295 hrs · 22,910 cycles

SEAT TRACK BS 675-713 CORRODED. FABRICATED NEW SEAT TRACK IAW ECTC REO 670-53-00-343. REMOVED SEAT TRACK IAW AMM 53-00-49 TASK 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SKIN — DENTED (RT NACELLE) · airframe 31,295 hrs · 22,910 cycles

RT FAN COWL UPPER FWD CORNER, SKIN DENT. FABRICATED AND INSTALLED REPAIR DOUBLER ANGLE IAW SRM 51-14-00-201-004-A01. PERMANENT & MAJOR REPAIR.

Part: SKIN — CORRODED · airframe 31,295 hrs · 22,910 cycles

DURING REMOVAL OF ADF ANTENNA FOUND SIX SPOTS OF CORROSION ON SKIN. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION ON FUSELAGE SKIN IAW BSC NDT PROGRAM MANUAL SECTION IAW SRM 53-31-01-101-003-A01. FOUND TO BE SATISFACTORY.

Part: SUPPORT — BROKEN (SEAT) · airframe 31,295 hrs · 22,910 cycles

PILOT SEAT BACK SUPPORT BROKEN, THIS REPAIR IS CLASSIFIED AS A REPAIR IAW SOP 5702. R & R SEAT BACK SUPPORT SHROUDS IAW CMM 25-14-10-390-806/808-A01.

Part: ANGLE — CORRODED (THRESHOLD) · airframe 31,295 hrs · 22,910 cycles

ASD THRESHOLD FLOOR SUPPORT THRESHOLD UPPER ANGLE CORRODED. REMOVED ASD THRESHOLD FLOOR SUPPORT MID CAP ANGLE AS REQUIRED IAW REF SRM 51-41-02-001-001-A01. INSTALLED NEW ASD THRESHOLD FLOOR SUPPORT MID ANGLE IAW SRM 51-41-02-001-001-A01 AND DWG SH670-31810 & SH670-31825.

Part: SKIN — CRACKED (LT WING) · airframe 31,295 hrs · 22,910 cycles

DURING EDDY CURRENT INSPECTION OF LT WING LOWER PLANK AND TRUMION HOLES CRACK INDICATIONS IN 1EA FASTENER HOLE. REPAIRED IAW REO 670-57-21-694, REV P2.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 31,295 hrs · 22,910 cycles

FLOOR SUPPORT BETWEEN BS 280-319.7 CORRODED AT NUMEROUS LOCATIONS, RT SIDE. REMOVED CORROSION AND FOUND TO BE BEYOND LIMITS IAW SRM 51-21-06-001-001-A01, 53-00-00-101-001-A01 AND REO 670-53-00-350. COMPLIED WITH REO 670-53-00-390.

Part: SEAT TRACK — CORRODED (BS 364-485) · airframe 31,295 hrs · 22,910 cycles

FLOOR SEAT TRACK CORRODED, RBL9 BS 364 - 485. FOUND OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. REMOVED CORRODED SEAT TRACK & INSTALLED NEW IAW AMM 53-00-49-000-801 & AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 31,295 hrs · 22,910 cycles

FLOOR SEAT TRACK RBL9, BS 349-485 CORRODED . FOUND OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. REMOVED AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 669-713) · airframe 31,295 hrs · 22,910 cycles

LT SIDEWALL SEAT TRACK CORRODED AT FS 669.4 - 713. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801. COMPLIED WITH EC/TC REO 670-53-00 AND GREO 670-53-00-343, REV E.

Part: SEAT TRACK — CORRODED (BS 784-861) · airframe 31,295 hrs · 22,910 cycles

LEFT SIDEWALL SEAT TRACK CORRODED AT BS 784 - 861. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED SEAT TRACK. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 713-763) · airframe 31,295 hrs · 22,910 cycles

LT SIDEWALL SEAT TRACK CORRODED AT FS 713 - 763. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED SEAT TRACK. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801. RECEIVED AND COMPLIED WITH EC/TC REO 670-53-00 AND GREO 670-53-00-343-REV E.

Part: HINGE — GOUGED (PAX DOOR) · airframe 31,295 hrs · 22,910 cycles

ASD HINGE, FUSELAGE, HAS A GOUGE ON 5TH LUG GOING AFT. RECEIVED AND COMPLIED WITH ECTC REO 670-53-21-582, TYPE 1. REPAIRED PASSENGER DOOR HINGE FUSELAGE SIDE IAW REO 670-53-21-582, REV A. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 31,280 hrs · 22,895 cycles

COCKPIT FLOORBEAM ANGLE BS 280 CRACKED. REMOVED FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED & TRANSFERRED MOUNTING HOLES ON NEW FLOORBEAM ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED IAW SRM 51-42-06-001-001-A01, & DWG CC670-33052.

Part: TRUNNION — GOUGED (RT MLG) · airframe 31,295 hrs · 22,910 cycles

MINOR TOOL DAMAGE FOUND ON OTBD OF RT TRUNNION FITTING INSIDE ACCESS PANEL 642AT. BLENDED TOOLING DAMAGE ON RT TRUNNION FITTING INSIDE ACCESS PANEL 642AT. RECEIVED ECTC REO 670-57-21-696 REO 670-57-21-696 HAS ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCOMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. COMPLIED WITH REO 670-57-21-696.

Part: TRUNNION — GOUGED (LT MLG) · airframe 31,295 hrs · 22,910 cycles

MINOR TOOLING MARK FOUND ON OTBD SIDE OF LT TRUNION FITTING INSIDE ACCESS PANEL 542AT. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. BLENDED DAMAGE ON LT TRUNNION FITTING INSIDE ACCESS PANEL 542AT. RECEIVED REO 670-57-21-697. REO 670-57-21-697 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. COMPLIED WITH REO 670-57-21-697.

Part: SEAT TRACK — CORRODED (BS 830-969) · airframe 31,295 hrs · 22,910 cycles

SEAT TRACK AT LBL 9, BS 830.49 - 969 CORRODED. EVALUATED CORROSION FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED THEN INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.

Part: SKIN — CHAFED (RT NACELLE) · airframe 31,293 hrs · 22,909 cycles

RIGHT ENGINE LOWER CORE COWL INNER SKIN IS CHAFED. RECEIVED EC/TC REO 670-54-23-959: COMPLIED WITH REPAIR OF THE FWD CORE COWL IAW REO 670-54-23-959. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED ACDC FIRESHIELD. INSTALLED NEW ACOC FIRESHIELD IAW SRM 54-23-00-201-001-A01.

Part: SEAT TRACK — CORRODED (BS 693) · airframe 31,293 hrs · 22,909 cycles

CORROSION ON RT SEAT TRACK AT BS 693. FOUND TO BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED SEAT TRACK. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-000-801 53-00-49-400-801.

Part: DOOR — CHAFED (ICE BREAKER) · airframe 31,293 hrs · 22,909 cycles

ASD ICE BREAKER DOOR CHAFED BY ICE BREAKER CABLE. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. COMPLIED WITH ECTC REO 670-52-11-238. REPAIR AT THE DAMAGE ON THE PRESSURE VENT FLAP ON THE PAX DOOR IS COMPLETED IAW 670-52-11-238 AND MEETS WITH ALL IT'S REQUIREMENTS.

Part: SEAT TRACK — CORRODED (BS 676) · airframe 31,280 hrs · 22,895 cycles

CORROSION ON SEAT TRACK AT BS 676. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: SKIN — GOUGED (BS 969-985) · airframe 31,293 hrs · 22,909 cycles

REPAIR DOUBLER HAS SCREW DAMAGE BETWEEN FS 969-985, STR 27. RECEIVED REO 670-53-00-410 P1. COMPLIED WITH REO 670-53-00-410 P1.

Part: SEAT TRACK — CORRODED (BS 669-977) · airframe 31,295 hrs · 22,910 cycles

PAX CABIN RT SIDE WALL SEAT TRACKS FROM BS 669.4 - 977 HAS CORROSION AND CORRODED SCREWS. RT SIDE PAX SEAT TRACK FS 784 CORRODED OUT OF LIMITS IAW SRM 53-41-101-001-A01 IAW REPLACEMENT PART ON ORDER. INSTALLED RT SIDE SEAT TRACK AT FS 784-847 IAW AMM 53-00-49, TASK 53-00-49-400-801. RT SIDE SEAT TRACK FS713-FS763 CORRODED OUT OF LIMITS IAW SRM 53-41-51-101-001-A01 REQ REPLACEMENT. INSTALLED RT SIDE SEAT RAIL FS713-FS763 IAW 53-00-49-400-801 AMM AS REQUIRED. REMOVED SEAT TRACK AT FS784-847 RT IAW AMM 53-00-49, TASK 53-00-49-000-801. INSTALLED SEAT TRACK RT SIDE FS 784-847 IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 379-669) · airframe 31,295 hrs · 22,910 cycles

LEFT CABIN SIDE WALL SEAT TRACKS FROM BS 379 - 669.4 HAS SURFACE CORROSION, CORRODED SCREWS, AT REAR ARE MARKED. BLENDED LT CABIN SIDE WALL SEND TRACK FROM FS 379.00 TO FS 669.40 FOUND TO BE OUT OF LIMITS IAW SRM 53-31-51-101-001-A01, 53-21-49-101-001-A01. REMOVED SEAT TRACK REQUIRE REPLACEMENT IAW AMM 53-00-49-000-801. INSTALLED SIDE WALL SEAT TACK FS 379.00 TO FS 669.00. INSTALLED LT CABIN SIDEWALL SEAT TRACK FS 379.00 TO FS 669.00 IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CRACKED (BS 830-969) · airframe 31,295 hrs · 22,910 cycles

SEAT TRACK AT RBL 9, BS 830.49 - 969 HAS CORROSION. EVALUATED CORROSION FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-41-19-101-001-A01. REMOVED SEAT TRACK AT RBL9, FS83049-969.00 IAW AMM 53-00-49-0000-801. INSTALLED SERVICEABLE SEAT TRACK AT RBL9 FS830 49-969.00 IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 379-669) · airframe 31,295 hrs · 22,910 cycles

RIGHT CABIN SIDE WALL SEAT TRACKS FROM BS 379 - 669.40 HAS SURFACE CORROSION, CORRODED SCREWS, AREAS ARE MARKED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED RT FWD SIDE SEAT TRACK AT FS 379- FS 483 IAW AMM 53-00-45-400-801.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 31,293 hrs · 22,909 cycles

COCKPIT FLOOR SUPPORT ANGLE AT FS 280, LT SIDE CRACKED. REMOVED COCKPIT FLOOR SUPPORT ANGLE AT FS 280 LT SIDE, REF SRM 51-42-06-001-001-A01 RECEIVED SERVICABLE ANGLE PN CC670-33199-4 LOCATED & TRANSFERRED MOUNTING HOLES AS NEEDED, REF SRM 51-40-11-001-001-A01. INSTALLED COCKPIT FLOOR SUPPORT ANGLE LT REF: SRM 51-42-06-001-001-A01, DWG: CC670-33052.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 31,293 hrs · 22,909 cycles

GALLEY SERVICE DOOR SILL LOWER ANGLE HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-21-23-101-002. REMOVED SERVICE DOOR SILL LOWER ANGLE AND LOCATED HOLES IN REPLACEMENT LOWER SILL ANGLE IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01. INSTALLED LOWER SILL ANGLE IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 633) · airframe 31,280 hrs · 22,895 cycles

CORROSION ON LEFT SEAT TRACK AT FS 633. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: CLEAT — CORRODED (SERVICE DOOR) · airframe 31,293 hrs · 22,909 cycles

SERVICE DOOR CLEATS HAS CORROSION. REMOVED CORROSION ON SERVICE DOOR CLEAT IAW SRM 51-21-06-001-001-A01 CORROSION OUT OF LIMITS IAW SRM 53-21-23-101-002. REMOVED CLEAT IAW SRM 51-42-20-001-001-A01. INSTALLED SERVICABLE REPLACEMENT CLEAT IAW SRM 51-42-20-001-001-A01.

Part: ANGLE — CORRODED · airframe 31,293 hrs · 22,909 cycles

RIGHT GUSSET PLATE ANGLE CORRODED. REMOVED CORROSION ON RT GUSSET PLATE AS NEEDED REF SRM 51-21-06-001-001. ORIGINAL MAT 0.063," REMOVED 0.011 "REMAINING MAT. 0.052 "FOUND TO BE OUT OF LIMITS REF SRM 53-00-00-101-001. R & R OUT OF LIMITS RT GUSSET PLATE ANGLE. REF DWG CC670-33467-2. R & R RT GUSSET PLATE ANGLE PICKED UP NEW HOLES COMMON TO NEW PLATE, PN CC213-0070-4 WET INSTALLED NEW FASTERNERS REF SRM 51-42-06-001-001 & 51-42-10-001-001 AND DWG CC670-33052.

Part: WEB — CORRODED (BS 280) · airframe 31,293 hrs · 22,909 cycles

LEFT LOWER WEB AT FS 280 CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-21-06-001-001-A01 AND SRM TR 51-12-00-991-807. REMOVED LOWER WEB AND DOUBLER STRAP IAW SRM 51-42-21-001-001-A01, 51-42-13-001-001-A01, 51-42-00-001-001-A01. INSTALLED LOWER WEB IAW REO 670-53-11-594. COMPLIED WITH EC/TC REO 670-53-11-594 AND GREO 670-53-11-594.

Part: PLATE — CORRODED (BS 280) · airframe 31,293 hrs · 22,909 cycles

LEFT BS 280 SUPPORT GUSSET PLATE CORRODED. REMOVED CORROSION ON LT LOWER SUPPORT GUSSET PLATE AS NEEDED REF SRM 51-21-06-001-001-A01. ORIGINAL MAT 0.053" REMOVED 0.010 "REMAINING MAT. 0.053 "FOUND TO BE OUT OF LIMITS REF CRJ700 SRM 53-00-00-101-001. R & R OUT OF LIMITS RT LT LOWER SUPPORT COVER GUSSET PLATE, REF DWG CC670-33467-2. R & R LT LOWER SUPPORT GUSSET PLATE. PICKED UP NEW HOLES COMMON TO NEW PLATE, PN CC670-33467-2 WET INSTALLED FASTENERS REF SRM 51-42-06-001-001 & 51-42-10-001-001 AND DWG CC670-33052.

Part: PLATE — CORRODED (BS 280) · airframe 31,293 hrs · 22,909 cycles

RIGHT BS 280 LOWER SUPPORT GUSSET PLATE CORRODED. REMOVED CORROSION AT RT 280 COVER SUPPORT GUSSET PLATE AS NEEDED REF SRM 51-21-06-001-001-A01. ORIGINAL MAT 0.050" REMOVED 0.010 "MATERIAL REMAINING 0.040 "FOUND TO BE OUT OF LIMITS, REF SRM 53-00-00-101-001-A01. R & R OUT OF LIMITS RT COVER GUSSET PLATE, REF DWG CC670-33467-2. R & R LT LOWER GUSSET PLATE PICKED UP NEW HOLES COMMON TO NEW PLATE P/N CC670-33467-1 WET INSTALLED FASTERNERS, REF SRM 51-42-06-001-001 & 51-42-10-001-001 AND DWG CC670-33052.

Part: WEB — CORRODED (BS 280) · airframe 31,293 hrs · 22,909 cycles

RIGHT LOWER WEB AT FS 280 CORRODED. REMOVED CORROSION IAW SRM TR 51-12-00 AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001-A01 AND TR 51-12-00-997-807. REMOVED RT LOWER WEB AND DOUBLER IAW SRM 51-42-06, 51-42-13 AND 51-42-21. INSTALLED WEB IAW REO 670-53-11-594.

Part: SKIN — DENTED (RT FAN COWL) · airframe 31,297 hrs · 22,911 cycles

RT FAN COWL UPPER FWD CORNER, SKIN DENT. COMPLIED WITH PERMANENT REPAIR OF RT FAN COWL UPPER FWD CORNER SKIN IAW SRM 54-14-00. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REPAIR IAW SRM 54-14-00-201-001-A01. COMPLIED WITH SRM 54-14-00-201-004 MODE REPAIR ANGLE AND DOUBLER.

Part: FLOOR PANEL — CRACKED (BS 193) · airframe 31,293 hrs · 22,909 cycles

FWD EQUIPMENT COMPARTMENT FLOOR CRACKED AT FS 193.00, RT SIDE NEXT TO ADG STOW PUMP. INSTALLED REPAIR PARTS IAW REO 670-53-11-509. COMPLIED WITH EC/TC REO 670-53-11-509 AND GREO 670-53-11-509.

Part: FLOOR PANEL — CRACKED (BS 193) · airframe 31,293 hrs · 22,909 cycles

FWD EQUIPMENT COMPARTMENT FLOOR CRACKED LT SIDE AT FS 193.00. INSTALLED REPAIR PARTS IAW REO 670-53-11-509. COMPLIED WITH EC/TC REO 670-53-11-509 AND GREO 670-53-11-509. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: RETAINER — CRUSHED (CARGO DOOR SEAL) · airframe 31,293 hrs · 22,909 cycles

FWD BAGGAGE BAY DOOR SEAL RETAINER CRUSHED AT LOWER AFT CORNER. REMOVED DOOR SEAL RETAINER FROM FWD BAGGAGE BAY DOOR IAW AMM 52-35-07-000-802. INSTALLED FORWARD BAGGAGE BAY DOOR SEAL RETAINER IAW AMM 52-35-07-400-802.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 31,148 hrs · 22,802 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHTED SIGN INOPERATIVE. REPLACED LAMP. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 31,148 hrs · 22,802 cycles

AFT EMERGENCY CEILING FLOOD LIGHT INOPERATIVE. REPLACED LAMP. OPS CHECKED GOOD.

Part: SENSOR — FAILED (ENGINE OIL) · airframe 31,063 hrs · 22,747 cycles

AT LT ENG OIL TEMP STARTED TO CLIMB RAPIDLY TO 249C. NEVER RECEIVED MASTER WARNING OR CAUTION, ONLY RED TEMPERATURE ON EICAS, FOLLOWED QRH & SHUTDOWN LT ENGINE, ENROUTE, ACFT DIVERTED DUE TO MAINTENANCE EMERGENCY ACTIONS. R & R OIL LEVEL/TEMP SENSOR IAW AMM 79-31-01. ACFT RAN AT CLIMB SETTING FOR 20 MIN ALL, CKS GOOD AT THIS TIME.

Part: LIGHT — UNKNOWN (CABIN) · airframe 30,746 hrs · 22,522 cycles

EMERGENCY LIGHT SYSTEM WILL NOT EXTINGUISH. OPS CHECKED EMERGENCY LIGHT IAW AMM 33-51-00 OP'S CHECKED GOOD. ACFT OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 29,315 hrs · 21,490 cycles

AFT F/A FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT IAW AMM 25-61-02.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 26,327 hrs · 19,356 cycles

SEAT TRACK BETWEEN FS 349-485 RBL 9.0 IS CORRODED. RECEIVED ECTC COMPLIED WITH ECTC REO 670-53-00-343 AND GENERIC REO 670-53-00-343 REV B. RII FOUND TO BE SATISFACTORY.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 26,327 hrs · 19,356 cycles

LEFT CABIN FLOOR SEAT TRACK BETWEEN FS 349-485 LBL 9.0 IS CORRODED. COMPLIED WITH EC/TC REO 670-53-00-343 AND GENERIC REO 670-53-00-343, REV B. RII FOUND TO BE SATIFACTORY.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 26,327 hrs · 19,356 cycles

LEFT CABIN FLOOR SEAT TRACK BETWEEN FS 581- 677, LBL 9.0 IS CORRODED. REPAIRED IAW EC/TC REO 670-53-00-343 AND GENERIC REO 670-53-00-343 REV B.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 26,327 hrs · 19,356 cycles

LEFT CABIN FLOOR SEAT TRACK BETWEEN FS 485 - 581 LBL 9.0 IS CORRODED. COMPLIED WITH EC/TC REO 670-53-00-343 AND GENERIC REO 670-53-00-343, REV B.

Part: SEAT TRACK — CORRODED (BS 483-573) · airframe 26,327 hrs · 19,356 cycles

LEFT SIDWALL SEAT TRACK HAS CORRODED HARDWARE AND CORROSION ON SEAT TRACK AT FS 483 - 573. COMPLIED WITH EC/TC REO 670-53-00-343 AND GENERIC REO 670-53-00-343, REV B. R & R CORRODED HARDWARE AS NECCESARY IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 713-763) · airframe 26,327 hrs · 19,356 cycles

RT SIDE WALL SEAT TRACK HAS ERRODED HARDWARE AND CORROSION ON SEAT TRACK AT FS 713- 763. REMOVED AND REPLACED IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 573-675) · airframe 26,327 hrs · 19,356 cycles

LT SIDE WALL SEAT TRACK HAS CORRODED HARDWARE AND CORROSION ON SEAT TRACK AT FS 573-675. R & R CORRODED HARDWARE IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 785-830) · airframe 26,327 hrs · 19,356 cycles

RIGHT SEAT TRACK BETWEEN FS 785-830 CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, FOUND OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 863-909) · airframe 26,327 hrs · 19,356 cycles

LEFT SEAT TRACK BETWEEN FS 863-909 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, MATERIAL THICKNESS ORIGINAL .370". REMOVED .004" REMAINING .366" WITH IN TOLERANCE IAW SRM 53-51-49-101.

Part: SEAT TRACK — CORRODED (BS 909-977) · airframe 26,327 hrs · 19,356 cycles

RIGHT SEAT TRACK BETWEEN FS 909-977 CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 ORIGINAL THICKNESS .370" MATERIAL. REMOVED .005 MATERIAL REMAINING .565", FOUND WITHIN LIMITS IAW SRM 53-51-49-101-001-A01.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 26,327 hrs · 19,356 cycles

RT CABIN SEAT TRACK BETWEEN FS 581-677 RBL 9.0 CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 26,327 hrs · 19,356 cycles

RIGHT CABIN FLOOR SEAT TRACK BETWEEN FS 349 - 485, RBL 9.0 CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED SEAT TRACK IAW REO 670-53-00-343, STEPS 1-4. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 785-830) · airframe 26,327 hrs · 19,356 cycles

LEFT SEAT TRACK BETWEEN FS 785-830 CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-001-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED SEAT TRACK IAW REO670-53-00-343. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 26,327 hrs · 19,356 cycles

LEFT CABIN SEAT TRACK BETWEEN FS 581-677 LBL 9.0 CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, FOUND OUT OF LIMITS IAW SRM 53-31-49-100-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343. SEAT TRACK INSTALLED IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 26,327 hrs · 19,356 cycles

LEFT CABIN SEAT TRACK BETWEEN FS 349 - 485, LBL 9.0 CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED SEAT TRACK SECTION IAW STEPS 1, 2, 4 OF REO 670-53-00-343. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 26,327 hrs · 19,356 cycles

RIGHT CABIN SEAT TRACK BETWEEN FS 485-581, RBL 9.0 CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND OUT OF LIMITS IAW 51-21-06-001-001-01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRCATED NEW FLOOR SEAT TRACK IAW REO 670-53-00-343. INSTALLED SERVICEABLE FLOOR SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 830-863) · airframe 26,327 hrs · 19,356 cycles

LEFT SEAT TRACK BETWEEN FS 830-863 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, ORIGINAL MATERIAL .370", REMOVED .005", REMAINING .365" WITH IN TOLERANCE IAW SRM 53-41-49-101-001-A01.

Part: SEAT TRACK — CORRODED (BS 348-581) · airframe 26,327 hrs · 19,356 cycles

LEFT CABIN SEAT TRACK BETWEEN FS 348-581, LBL 9.0 CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, FOUND OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 573-675) · airframe 26,327 hrs · 19,356 cycles

LEFT SEAT TRACK HAS CORRODED HARDWARE AND CORROSION ON SEAT TRACK AT FS 573 - 675. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343 STEPS 1,2, & 4. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 713-763) · airframe 26,327 hrs · 19,356 cycles

RIGHT SEAT TRACK HAS CORRODED HARDWARE AND CORROSION ON SEAT TRACK AT FS 713 - 763. REMOVED CORROSION IAW SRM 57-21-06-001-001-A01 OUT OF LIMITS IAW SRM 51-41-49-101-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW REO 670-33-00-343. INSTALLED SEAT TRACK IAW 53-00-49-400-801.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 26,327 hrs · 19,356 cycles

CORROSION DAMAGE ON INTERCOSTAL BETWEEN FS 349 AND 364 FRAMES JUST LEFT OF STR 27. CORROSION IN NO DAMAGE ALLOWED AREA, REMOVED INTERCOSTAL IAW SRM 51-42-06-001-001. DRILLED NEW INTERCOSTAL AND INSTALLED IAW SRM 51-42-06-001-001-A01.

Part: WEB — CORRODED (BS 280) · airframe 26,327 hrs · 19,356 cycles

RIGHT BS 280 WEB CORRODED. REPAIRED IAW REO 670-53-11-594, STEPS 1-12. PERFORMED EDDY CURRENT INSPECTION IAW REO 670-53-11-594 AND NDTM 57-20-006-250-A01. NO INDICATIONS NOTED.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 26,327 hrs · 19,356 cycles

FS 280 FLOORBEAM CORRODED. REMOVED AND REPLACED FLOORBEAM IAW REO-670-53-11-047.

Part: SEAT TRACK — CORRODED (BS 379-843) · airframe 26,327 hrs · 19,356 cycles

RIGHT SIDEWALL SEAT TRACK HAS CORRODED HARDWARE AND CORROSION ON TRACK AT FS 379 - 843. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 ORIGINAL .370" REMOVED .007" MATERIAL REMAINING .363" WITHIN LIMITS IAW SRM 53-21-49-404-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 26,327 hrs · 19,356 cycles

FWD ANGLE OF FS 280 FLOORBEAM CORRODED. R & R IAW SRM 51-42-06-001-001-A01 AND DWG CC670-33052.

Part: WEB — CORRODED (BS 280) · airframe 26,327 hrs · 19,356 cycles

LEFT BS 280 WEB CORRODED. REPAIRED IAW REO 670-53-11-594, STEPS 1-12. PERFORMED EDDY CURRENT INSPECTION IAW REO 670-53-11-594 AND NDTM 51-20-006-250-A01. NO INDICATIONS NOTED.

Part: SEAT TRACK — CORRODED (BS 483-573) · airframe 26,327 hrs · 19,356 cycles

RIGHT SIDE SEAT TRACK HAS CORRODED HARDWARE AND CORROSION ON SEAT TRACK AT FS 483 - 573. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, ORIGINAL MATERIAL .370" MATERIAL REMOVED .011" MATERIAL REMAINING .359" WITHIN LIMITS IAW 53-31-49-101-001-A01.

Part: ANGLE — CRACKED (BS 280 BULKHEAD) · airframe 26,327 hrs · 19,356 cycles

VERTICAL ANGLE AT LBL 26 ON BS 280 BULKHEAD IS CRACKED. R & R IAW SRM 51-42-06-001-001-A01 AND DWG CC670-34010.

Part: SEAT TRACK — CORRODED (BS 675-713) · airframe 26,327 hrs · 19,356 cycles

RIGHT SEAT TRACK HAS CORRODED HARDWARE AND CORROSION ON SEAT TRACK AT FS 675 - 713. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. ORIGINAL THICKNESS .370" MATERIAL REMOVED .014 MATERIAL REMAINING .356" WITHIN LIMITS IAW SRM 53-41-49-101-001-A01.

Part: INTERCOSTAL — CORRODED (BS 364 S26R) · airframe 26,327 hrs · 19,356 cycles

INTERCOSTAL FS 364 HAS CORROSION DAMAGE AT S26R JUST FWD OF MAIN AVIONICS DOOR CUT OUT. BLENDED CORROSION, ORIGINAL THICKNESS IS .080, MATERIAL REMOVED IS .001 REF SRM 51-21-06-001-001. FOUND TO BE IN LIMITS REF SRM 53-21-23-001-001. APPLIED ALODINE PRIMER & PAINT TO BLENDED AREA REF SRM 51-21-06-001-001.

Part: SEAT TRACK — CORRODED (BS 675-713) · airframe 26,327 hrs · 19,356 cycles

LEFT SIDEWALL SEAT TRACK HAS CORRODED HARDWARE AND CORROSION AT FS 675 - 713. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS .370" MATERIAL REMOVED .009" REMAINING .031" WITHIN LIMITS IAW SRM 53-41-49-101-001-A01.

Part: SEAT TRACK — CORRODED (BS 713-763) · airframe 26,327 hrs · 19,356 cycles

LEFT SIDEWALL SEAT TRACK HAS CORRODED HARDWARE AND CORROSION AT FS 713 - 763. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-001-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343, STEPS 1 THRU 4. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-301.

Part: ANGLE — CRACKED (BS 280 BULKHEAD) · airframe 26,327 hrs · 19,356 cycles

VERTICAL ANGLE AT RBL 26 ON BS 280 BULKHEAD IS CRACKED. R & R IAW SRM 51-42-06-001-001-A01 AND DWG CC670-34010.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 26,327 hrs · 19,356 cycles

CORROSION DAMAGE ON INTERCOSTAL BETWEEN FS 349 AND 364 FRAMES S27R. CORROSION ON INTERCOSTAL IN A NO DAMAGE AREA. REMOVED INTERCOSTAL IAW SRM 53-21-23-001-001 & 51-42-06-001-001. DRILLED NEW INTERCOSTAL AND INSTALLED INTERCOSTAL IAW SRM 51-42-06-01-001-A01.

Part: SEAT TRACK — CORRODED (BS 379-483) · airframe 26,327 hrs · 19,356 cycles

LEFT SEAT TRACK HAS CORRODED HARDWARE AND CORROSION ON SEAT TRACK AT FS 379 - 483. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. ORIGINAL .370" REMOVED .012" REMAINING MATERIAL .358" WITHIN LIMITS IAW SRM 53-41-49-101-001-A01.

Part: SEAT TRACK — CORRODED (BS 483-573) · airframe 26,327 hrs · 19,356 cycles

LEFT SIDEWALL SEAT TRACK HAS CORRODED HARDWARE AND CORROSION ON SEAT TRACK AT FS 483 - 573. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW REP 670-53-00-343. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A01.

Part: DOOR — NO TEST (SERVICE) · airframe 26,327 hrs · 19,356 cycles

SERVICE DOOR FAILED FUNCTIONAL CHECK (51LBS). PERFORMED FUNCTIONAL CHECK OF SERVICE DOOR IAW AMM 52-41-00-720-801 COULD NOT DUPLICATE DISCREPANCY TOTAL FORCE TO COMPLETE OPENING OF SERVICE DOOR WAS 30 LBS WITHIN SERVICABLE LIMITS.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 26,327 hrs · 19,356 cycles

LOWER 280, FRAME AFT SIDE FLOOR SUPPORT ANGLE HAS 3 EA CORRODED NUTPLATES. REPLACED SUPPORT ANGLE AND 3EA NUTPLATES ALL WORK IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: GROMMET — DAMAGED (RT MLG WW) · airframe 26,327 hrs · 19,356 cycles

RT WHEEL BIN PANEL 174CZ HAS 1 BAD GROMMET, DB161718 02/19/12. R & R 1EA GROMMENT AND 7EA STUDS IAW SRM 51-44-11-001-001-A01. FOUND STEPS TO BE DAMAGED (ROUNDED OFF).

Part: GROMMET — DAMAGED (RT MLG WW) · airframe 26,327 hrs · 19,356 cycles

RIGHT WHEEL, BIN PANEL 174BZ HAS 3 EA BAD GROMMETS. R & R 3EA GROMMETS AND REINSTALLED STUDS IAW SRM 51-44-11-001-001-A01. UPON FURTHER INVESTIGATION FOUND 2EA BAD GROMMETS MISSING STUDS. R & R 2EA GROMMENTS AND STUDS IAW SRM 51-44-11-001-001-A01.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 25,933 hrs · 19,082 cycles

PAX DOOR FWD DRAG ANGLE CRACKED. WORK COMPLETED IAW ITEM: 1/ CONFIRMED 2.500 CRACK AT PAX DOOR FWD SIDE WITH HFEC INSP IAW NDTM 51-20-006 PART 1.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,120 hrs · 18,526 cycles

NR 5 CABIN CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED NR 5 CABIN EMERGENCY LIGHT IAW AMM 33-51-09. OPS CHECK GOOD. RELAMPED NR 5 CABIN EMERGENCY LIGHT IAW AMM 33-51-09. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,541 hrs · 18,118 cycles

EMERGENCY CEILING LIGHTS INOPERATIVE. REPLACED LIGHTS IAW AMM 33-51-09-000-801 AND AMM 33-51-09-400-801.

Part: LIGHT — INOPERATIVE (LT WING) · airframe 24,541 hrs · 18,118 cycles

LT WING FWD EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED BULB IAW AMM TASK 20-21-00-910-801. OPS CHECKED GOOD IAW AMM 33-51-15-710-801.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 23,803 hrs · 17,610 cycles

2.5" OF CABIN FLOOR PHOTOLUMINESCENT STRIP MISSING AT ROW 1. INSTALLED MISSING PHOTOLUMINESCENT STRIP IAW AMM 33-51-01.

Part: STOP FITTING — OUT OF ADJUST (EMERGENCY EXIT) · airframe 23,411 hrs · 17,307 cycles

BOTH OVERWING EMERGENCY EXITS HARD TO OPEN. RESOLVED ON W/O: 181004 TASKCARD: N/R-00008. ADJUSTED LT OVERWING EMERGENCY EXIT STOP SCREWS IAW CRJ 700 AMM 52-21-00. OPS CHECK GOOD ITEM. ADJUSTED LT OVERWING EMERGENCY EXIT STOP SCREWS IAW CRJ 700 AMM 52-21-00. OPS CHECK GOOD. RII COMPLIED WITH PER GMM 3-3. ALL WORK FOUND SATISFACTORY.

Part: DOOR — UNSERVICEABLE (EMERGENCY EXIT) · airframe 23,411 hrs · 17,307 cycles

RT OVERWING EMERGENCY EXIT HARD TO OPEN. RESOLVED ON W/O: 181004 TASKCARD: N/R-00009. REMOVED AND REPLACED THE RT WING OVERWING EMERGENCY EXIT DOOR IAW CRJ 700 AMM 52-21-00. ADJUSTMENT AND FUNCTIONAL TEST GOOD IAW CRJ 700 AMM 52-21-00. RII INSPECTION C/W PER GMM 3-3. RESULTS SATISFACTORY. REMOVED AND REPLACED THE RT WING OVERWING EMERGENCY EXIT DOOR IAW CRJ 700 AMM 52-21-00. ADJUSTMENT AND FUNCTIONAL TEST GOOD IAW CRJ 700 AMM 52-21-00. RII INSPECTION C/W PER GMM 3-3. RESULTS SATISFACTORY.

Part: RESERVOIR — FAILED (HYD SYSTEM) · airframe 22,521 hrs · 16,525 cycles

HYD NR 3 HIGH TEMP CAUTION MESSAGE RAN CHECK LIST WITH 3A OFF 3B ON TEMP WENT FROM 98C-96C THEN STARTED TO CLIMB- TURNED 3B OFF AND TEMP FELL STEADILY. ALSO NR 3 HYD QUANTITY WENT FROM 65 PERCENT TO 100 PERCENT WHEN THE HYD 3 PUMPS WERE TURNED OFF. TURNED ON 3B FOR LANDING AND PRESS=0. COMPLETED HYD 3 LO PRESS. RETURNED TO FIELD. LANDING UNEVENTFUL. R & R THE NR 3 HYD RESEVOIR IAW TASKS 29-12-30-000-801 AND 29-12-30-400-801. PERFORMED INSP CHECK AFTER DEPLOYMENT OF LANDING GEAR ALT EXTENSION IAW 05-51-31-210-801. PERFORMED INSPECTION AFTER HYD SYS OVERHEAT IAW 05-51-15-210-801. OPS TEST GOOD. LEAKAGE TEST GOOD.

Part: SERVO — BINDING (AILERONS) · airframe 22,352 hrs · 16,396 cycles

ON SHORT FINAL, AT 500 AGL, HARD RT UNCOMMANDED V ROLL REQUIRING PILOT TO OVER POWER WITH HIGH CONTROL PRESSURE. AILERON TRIM INDICATOR ALWAYS NEUTRAL. AUTOPILOT OFF AT THE TIME, ACFT BEING HAND FLOWN. LANDING UNEVENTFUL. PERFORMED GVI OF ROLL CONTROL SYS/CABLES AND REPLACED THE AILERON SERVO. OPS CKS GOOD. NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: WINDOW — FAILED (COCKPIT) · airframe 21,869 hrs · 16,040 cycles

PDX - LT SIDE WINDOW PANEL SHATTERED DURING CLIMB AT APPROX 36000 FT FOLLOWED BY L WINDOW HEAT CAUTION MESSAGE. OVERWEIGHT LANDING PERFORMED WEIGHT 69000 DESCENT RATE 400FPM. LANDING UNEVENTFUL. WINDOW REPLACED AND VISUAL INSPECTION MADE OF THE AIRCRAFTS WINDOW MOUNTING STRUCTURE NO DEFECTS OVERWEIGHT LANDING INSPECTION OK AND WITHIN LIMITS. RETURNED TO SERVICE.

Part: SKIN — CORRODED (PAX DOOR) · airframe 21,413 hrs · 15,701 cycles

C5 CHECK - PAX DOOR, INNER SKIN HAS CORROSION BETWEEN FS 311.75 AND FS 318.5. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS, SENT FOR ENGINEERING REO. PERFORMED LPI IAW NDTM LPI 51-20-08, NO CRACKS NOTED AT THIS TIME. TREATED, PRIMED, AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. ALL WORK PERFORMED IAW REO 670-52-11-469.

Part: SKIN — CHAFED (BS 977) · airframe 21,412 hrs · 15,701 cycles

C5 CHECK - 2 BELLY SKINS CHAFED IN 3 LOCATIONS AT FS 977.0 BLENDED DAMAGE ON BELLY SKIN FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-014. PERFORMED LPI IAW NDTM LPI 51-20-08. SENT FOR ENGINEERING REO. TREATED IAW SRM 51-21-11-001-001-A01, PRIMED IAW SRM 51-25-06-001-001-A01, APPLIED TOP COAT AND CORROSION INHIBITOR IAW SRM 51-25-16-001-001-A01 AND 51-21-11-001-001-A01. ALL WORK IN CONFORMITY WITH REO 670-53-00-235.

Part: SKIN — CORRODED (PAX DOOR) · airframe 21,413 hrs · 15,701 cycles

RFD - C5 CHECK -PAX DOOR INNER SKIN HAS CORROSION BEHIND HINGE AREA FROM FS 318.75 - 347.25. BLENDED ALL CORROSION FROM PAX DOOR, AND FOUND TO BE WITHIN LIMITS IAW SRM 52-11-01-101-001-A01. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-01-001-001-A01.

Part: PANEL — CHAFED (NR 3 SLAT) · airframe 21,413 hrs · 15,701 cycles

RFD -C5 CHECK - RT NR 3 SLAT PANEL HAS A CHAFE ON THE UPPER T/E. REMOVED DAMAGE IAW SRM 51-12-00-001-001-A01. BLEND IS WITHIN LIMITS IAW SRM 57-42-01-101-001-A01. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01 AND 51-25-01-001-001-A01.

Part: PANEL — CHAFED (NR 2 SLAT) · airframe 21,413 hrs · 15,701 cycles

C5 CHECK - RT NR 2 SLAT PANEL HAS 2 CHAFES ON UPPER T/E. REMOVED DAMAGE IAW SRM 51-12-00-001-001-A01. BLEND WITHIN LIMITS IAW SRM 57-42-01-101-001-A01. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01 AND 51-25-01-001-001-A01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 20,567 hrs · 15,049 cycles

RFD - 8 YEAR TASK - FOUND CORROSION ON PAX DOOR MID CAP ANGLE. REMOVED MID CAP ANGLE FROM A/C, AFTER BLENDING CORROSION FOUND TO BE CORRODED TO LIMITS IAW CRJ 700 SRM 53-21-23. LOCATED FASTENER HOLES IN NEW MID CAP ANGLE IAW CRJ 700 SRM 51-40-11. REINSTALLED NECESSARY BRACKETS AND NUT PLATES IAW CRJ 700 SRM 51-42-06, 51-45-00 AND 51-40-02. INSTALLED PAX DOOR MID CAP ANGLE IAW CRJ 700 SRM 51-42-06. INSTALLED PROXIMITY SENSOR IAW CRJ 700 AMM 52-70-04, PERFORMED OPS CHECK IAW CRJ 700 AMM 52-11-00-710-801.

Part: SILL — CORRODED (FUSELAGE) · airframe 20,567 hrs · 15,049 cycles

RFD - 8 YEAR TASK - CORROSION ON GALLEY SERVICE DOOR. REMOVED 2 DOOR STOP FITTINGS AND 2 BRACKETS FROM LOWER SILL TO EXPOSE CORROSION FOR EVAL AT FS 325 TO FS 331, FS 338 TO FS 344 INBOARD 2 INCHES OF SILL IAW CRJ 700 SRM 51-11-00. REMOVED RIVETS TO GAIN ACCESS TO REMOVE CORROSION. MEASURE TO BE OUT OF LIMITS, DEEPEST .014 REMOVED. SUBMITTED TO ENGINEERING. PERFORMED EDDY CURRENT INSPECTION, NO DEFECT NOTED IAW NDTM 51-20-06. REMOVED .014 OF CORROSION FER REO 670-53-21-490. ALUMINUM PREPPED AND ALODINED IAW CRJ 700 SRM 51-21-11. PRIMED REPAIR AREA IAW CRJ 700 SRM 51-25-06. INSTALLED FASTENERS ON SERVICE DOOR SILL REPAIR AREA. INSTALLED THRESHOLD BRACKETS IAW CRJ 700 REO 670-53-21-490 AND CRJ 700 SRM 51-42-20. TREATED FITTING IAW CRJ 7000 AMM 51-21-01, PRIMED FITTINGS IAW CRJ 700 SRM 51-21-11. PAINTED FITTINGS AND DOOR SILL IAW CRJ 700 SRM 51-25-00. INSTALLED LOWER DOOR STOPS IAW CRJ 700 SRM 51-41-02. INSTALLED NEW BOLTS IAW CRJ 700 AMM 20-21-00. PERFORMED RIG CHECK, ALL PROCEDURES DONE IAW CRJ 700 AMM 52-41-00.

Part: BEAM — CORRODED (FUSELAGE) · airframe 20,567 hrs · 15,049 cycles

RFD - 8 YEAR TASK - CORROSION FOUND ON 280.00 BEAM AT LBL 6, RBL 6 AND 9. REMOVED RT & LT DRIP PANS AFT OF 280 BEAM, REMOVED INTERCOSTALS AT RBL 9, 27 IAW CRJ 700 SRM 51-42-21 AND 51-42-13, REO 670-53-11-041. DISCONNECTED INST AIR LT AND RT IAW CRJ 700 AMM 20-30-00. CORROSION FOUND TO BE TO LIMITS. REMOVED HI LITES, COLLARS, RIVETS AND ALL HARDWARE RELEVANT TO FS 280 BEAM REPLACEMENT IAW REO 670-53-11-047. REMOVED LT AND RT AILERON PULLEY AT FS 280. REMOVED LT AND RT FS 280 BEAMS. ALL WORK DONE IAW REO 670-53-11-047. CUT NEW BEAM P/N CC670-34175-7 IAW REO 670-53-11-047. PERFORMED LPI ON CUT LINE REO 670-53-11-047, SHT 3 NUMBER 2. NO CRACKS NOTED. LOCATED HOLES IN NEW BEAMS IAW CRJ 700 SRM 51-40-06, 51-40-11. INSTALLED LT AND RT 280 BEAM IAW CRJ 700 SRM 51-42-21, 51-42-06, 51-42-13 AND REO 670-53-11-047. INSTALLED SPLICE DOUBLERS AND PARTIALLY INSTALLED FWD ANGLE TO 280 BEAM IAW REO 670-53-11-047. INSTALLED LED LIGHT ON FWD ANGLE OF 280 BEAM IAW CRJ 700 SRM 51-42-13. INSTALLED INTERCOSTAL AT RBL 9 IAW CRJ 700 SRM 51-42-20. FINISHED INSTALL OF FWD ANGLE AT 280 BEAM IAW CRJ SRM 51-42-20, 51-42-06. INSTALLED 280 BEAM IAW REO 670-53-11-047. INSTALLED FLOORBOARD NUT PLATES IAW REO 670-53-11-047, INSTALLED LT AND RT DRIP PAN IAW SRM 51-42-11. APPLIED CORROSION INHIBITOR IAW SRM 51-21-00. INSTALLED PULLEYS ON LT AND RT SIDES FOR AILERON CABLES IAW CRJ 700 AMM 27-11-00. RECONNECTED INSTRUMENT AIR IAW CRJ AMM 20-30-00. LEAK CHECKED SYSTEMS IAW TASK CARD 34-11-00-790-801.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 20,567 hrs · 15,049 cycles

RFD - 8 YEAR TASK - CORROSION FOUND ON SUPPORT ANGLE BEHIND MID CAP ANGLE ON PAX DOOR FRAME AT STR 18L. BLENDED CORROSION FROM UNDER MID CAP ANGLE IAW CRJ 700 SRM 51-21-06. REMOVED .024 ON UPPER FLANGE REMOVED .7X.2 FROM AFT SIDE OF PROX SENSOR CUTOUT, FOUND TO BE CORRODED TO LIMITS IAW CRJ 700 SRM 53-21-23. PERFORMED EDDY CURRENT INSPECTION ON KICK PLATE ANGLE PAX DOOR SILL. NO CRACKS OR CORROSION FOUND AT THIS TIME IAW NDTM 51-20-06. EDDY CURRENT COMPLIED WITH 51-20-06 REO 670-53-21-491. TREATED AREA WITH ALUM PREP 33 AND ALODINE IAW CRJ 700 SRM 51-21-11-001-001-A01. APPLIED PRIMER IAW CRJ 700 SRM 51-25-06-001-001-A01. INSTALLED NUT PLATES ON FRAME UNDER MID CAP ANGLE IAW CRJ 700 SRM 51-42-06-001-001-A01. INSTALLED SOLID RIVETS IN SUPPORT ANGLE PAINTED RIVETS IAW CRJ 700 SRM 51-42-06 AND 51-25-06. APPLIED CORROSION INHIBITING COMPOUND ON SUPPORT ANGLE AND DOOR FRAME IAW REO 670-53-21-491.

Part: SILL — CORRODED (FUSLEAGE) · airframe 20,567 hrs · 15,049 cycles

RFD - 8 YEAR TASK - CORROSION ON AFT CARGO DOOR SILL FROM FS 1000 TO 1047. REMOVED CORROSION FROM LOWER SILL OF AFT BAGGAGE BAY DOOR SURROUND STRUCTURE BETWEEN FS 1000 AND 10047 AT BL 72. MAX MATERIAL REMOVED WAS .004 WITH ALL ORIGINAL MATERIAL THICKNESS OF .063 BLEND FOUND OUT OF LIMITS PER CRJ 700 SRM 53-61-23. REMOVED SOLID RIVETS AT BLEND LOCATION TO FOM CORROSION REMOVAL IAW CRJ 700 SRM 51-42-06. PERFORMED EDDY CURRENT INSPECTION ON SILL. NO CRACKS OR CORROSION NOTED IAW NDTM 51-20-006. TREATED METAL IAW CRJ 700 SRM 51-21-11, PRIMED IAW CRJ 700 51-26-06. PRIOR TO TREATMENT INSTALLED RIVETS IAW CRJ 700 SRM 51-42-15. PAINTED LOWER SILL OF AFT BAGGAGE BAY DOOR IAW CRJ 700 SRM 51-25-00. APPLIED AV 8 TO AFT BAG DOOR SILL IAW CRJ 700 SRM 51-21-11-001-001-A01.

Part: SKIN — CHAFED (AILERON) · airframe 20,597 hrs · 15,049 cycles

RFD - 8 YEAR TASK - CHAFING DAMAGE FOUND ON RT AILERON. REMOVED FASTENERS FROM LEADING EDGE SKIN. REMOVED LEADING EDGE SKIN FROM AILERON, CLEANED AND PREPPED FOR NEW SKIN. RECEIVED NEW SKIN, LOCATED, DRILLED AND COUNTERSUNK FOR FASTENERS, INSTALLED USING HI LOKS / COLLARS AND SOLID RIVETS IAW CRJ 700 SRM 51-42-06 AND 51-42-22.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,567 hrs · 15,049 cycles

RFD - 8 YR TASK - CORROSION ON RT FLOOR SEAT TRACK AT FS L153.00. STARTED BLENDING CORROSION ON SEAT TRACK ON INNER AND TOP SURFACE. TOP SURFACE HAS BEEN BLENDED .005, TOP SURFACE IS WITHIN LIMITS ALLOWED .035. INNER SURFACE STILL HAS PITS, IT HAS BEEN BLENDED .020 STILL WITHIN LIMITS ALLOWED .035 IAW CRJ 700 53-31-4. REMOVED AN ADDITIONAL .013 FROM INNER SURFACE, TOTAL REMOVED IS .033, FOUND TO BE WITHIN LIMITS ALLOWABLE .035 IAW REO 670-53-00-013. TREATED BLENDED AREA, DOCUMENTED RED # ON REPAIRED AREA OF SEAT TRACK IAW CRJ 700 REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,567 hrs · 15,049 cycles

ROCKFORD - 8 YR TASK - CORROSION ON RT FLOOR SEAT TRACK AT FS 629.00. STARTED BLENDING CORROSION ON SEAT TRACK TOP SURFACE, HAS BEEN BLENDED .004, IS WITHIN LIMITS ALLOWED .025 TO BE REMOVED. STARTED BLENDING INNER SURFACE THERE ARE STILL SOME PITS, REMOVED .025 FROM INNER SURFACE, STILL WITHIN LIMITS ALLOWED .035 IAW CRJ 700 53-31-49. REMOVED AN ADDITIONAL .009 FROM INNER SURFACE TOTAL REMOVED IS .034 FOUND TO BE WITHIN LIMITS ALLOWABLE .035 IAW CRJ 700 SRM 53-31-49. TREATED BLENDED AREA DOCUMENTED RED # ON REPAIRED AREA. DOCUMENTED RED # ON REPAIRED AREA OF SEAT TRACK IAW REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,567 hrs · 15,049 cycles

ROCKFORD - 8 YR TASK - CORROSION ON LT FLOOR SEAT TRACK. BLENDED CORROSION ON SEAT TRACK TOP SURFACE, BLENDED .006 WITHIN LIMITS ALLOWED .025. BLENDED INNER SURFACE .027 REMOVED IS STILL WITHIN LIMITS ALLOWED .035 IAW CRJ 700 53-31-49. ON INNER SURFACE MAX DEPT IS .027, MAX LIMIT IS .035 IAW CRJ 700 SRM 53-31-49, PREPPED AND ALODINED AREA IAW CRJ 700 SRM 51-21-16. IDENTIFIED SEAT TRACK REO 670-53-00-013 IAW CRJ SRM 53-31-49.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 20,567 hrs · 15,049 cycles

RFD - 8 YEAR TASK - CORROSION FOUND ON 280.00 BULKHEAD WEB AT LBL 10 AND RBL 11. BLENDED MINOR CORROSION ON FS 280 LT BULKHEAD WEB AT LBL 10. BLENDED .003 MATERIAL FROM AREA WITH A MAXIMUM BLEND ALLOWED OF .005 IN THE POCKET AREA AT THIS LOCATION. BLEND IS WITHIN LIMITS IAW BOMBARDIER REO 670-53-11-052. RT FS 280 BULKHEAD WEB LOWER, CORRODED BEYOND LIMITS IAW REO 670-53-11-052. REMOVED RT FS 280 BULKHEAD WEB IAW CRJ 700 SRM 51-42-21, 51-42-13 AND 51-42-06. LOCATED HOLES IN NEW WEB IAW CRJ 700 SRM 51-40-11. TREATED AND EPOXY PRIMED LT WEB IAW BOMBARDIER REO 670-53-11-052. INSTALLED NEW RT WEB IAW REO 670-53-11-052 FIG 2. APPLIED TOP COAT TO LT AND RT WEBS AT 280.00 IAW CRJ 700 REO 670-53-11-052.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 20,450 hrs · 14,958 cycles

SEA - GLD UNSAFE CAUTION MSG. NOTE: RWY 34C, ABORTED T/O AT 60 KTS. CONSTRUCTION EQUIPMENT LOCATED NEAR 34C ON 34R. RETURNED TO GATE. PERFORMED OPS TEST OF THE GLD'S OPS TEST GOOD REF CRJ 700 AMM TASK 27-61-00-710-801-A01 PERFORMED CAT III OPERATIONAL TEST OF THE RAD ALT IAW MTC R344401 OPS TEST GOOD. NO DEFECTS NOTED. A/C REMAINS CAT III FLIGHT DECK PLACARD REFLECTS CAT III. RETURNED TO SERVICE. COULD NOT DUPLICATE. NO PARTS REPLACED.

Part: FIRE WARNING — FALSE ACTIVATION · airframe 19,996 hrs · 14,610 cycles

INTERMITTENT "FIRE SYS FAULT" STATUS MESSAGE. PLACED ON MEL 26-00-1. RETURNED TO SERVICE.

Part: VANE — GOUGED (TE FLAP) · airframe 19,906 hrs · 14,547 cycles

THE LEFT OUTBOARD FLAP MOST OUTBOARD BUTE DOOR GUIDE RAIL HAS GOUGE ON THE LEADING EDGE AT THE TOP AND THE MIDDLE OF THE RAIL. REMOVED OUTBOARD FLAP VANE FROM FLAP. REMOVED OUTBOARD MOST VANE RIB END GUIDE RAIL BY REMOVING OUTBOARD MOST VANE L/E. INSTALLED OUTBOARD VANE RIB END GUIDE RAIL . INSTALLED LEADING EDGE OVERLAPPING RIB END. INSTALLED OUTBOARD FLAP VANE TO FLAPS.

Part: PANEL — CHAFED (TE FLAP) · airframe 19,906 hrs · 14,547 cycles

PDX - 20K - RT FLAP PANEL 684EB HAS CHAF. BLENDED OUT DAMAGE IAW CRJ SRM 57-52-02 PG 102 AND FOUND TO BE WITHIN LIMITS. ORIGINAL THICKNESS .100 REMAINING IS .085 OK FOR SERVICE. FPI BLENDED AREA FOR CRACKS IAW SRM 51-12-00-001-001-A01 PAGE 10, PAR 7B(4), AND CRJ NDTM PART 1, 51-20-008. NO CRACKS NOTED. ETCHED, ALODINED AND PRIMED AFFECTED AREA.

Part: PANEL — CHAFED (TE FLAP) · airframe 19,906 hrs · 14,547 cycles

PDX - 20K - LT FLAP PANEL 584LB HAS CHAFE. BLENDED OUT AND FOUND TO BE WITHIN LIMITS MAX MATERIAL REMOVED .008. ETCHED AND ALODINED AFFECTED AREA REF DAMAGE IAW CRJ 700 SRM 57-52-01-101-001-A01. FPI IAW CRJ 700 PART 1, 51-20-008, NO CRACKS NOTED. PRIMED AND PAINTED AFFECTED AREAS.

Part: PANEL — CHAFED (TE FLAP) · airframe 19,906 hrs · 14,547 cycles

PDX - 20K - RT FLAP PANEL 684BB HAS CHAF ON SHORT CURVE PANEL APPROX .010. BLENDED OUT DAMAGE IAW CRJ 700 SRM 57-52-02 PG 102. DAMAGE IS WITHIN LIMITS AND OK FOR CONTINUED SERVICE. ORIGINAL THICKNESS .100 MATERIAL REMAINING IS .085.

Part: PANEL — CHAFED (TE FLAP) · airframe 19,906 hrs · 14,547 cycles

PDX - 20K - LT FLAP PANEL 584GB HAS CHAF. BLENDED OUT AND FOUND TO BE WITHIN LIMITS MAX MATERIAL REMOVED .011. ETCHED AND ALODINED AFFECTED AREA REF DAMAGE IAW CRJ 700 SRM 57-52-01-101-001-A01. FPI IAW CRJ 700 PART 1, 51-20-008, NO CRACKS NOTED. PRIMED AND PAINTED AFFECTED AREAS.

Part: PANEL — CHAFED (TE FLAP) · airframe 19,906 hrs · 14,547 cycles

PDX - 20K - LT FLAP PANEL 584JB HAS CHAF. BLENDED OUT DAMAGE AND FOUND TO BE WITHIN LIMITS. MAX MATERIAL REMOVED .010. ETCHED AND ALODINED AFFECTED AREA REF DAMAGE IAW CRJ 700 SRM 57-52-01-101-001-A01. FPI IAW CRJ 700 PART 1, 51-20-008, NO CRACKS NOTED. PRIMED AND PAINTED AFFECTED AREAS.

Part: PANEL — CHAFED (TE FLAP) · airframe 19,906 hrs · 14,547 cycles

PDX - 20K - RT WING FLAP PANEL 684JB HAS CHAF. BLENDED OUT DAMAGE IAW CRJ SRM 57-52-02 PG 102 AND FOUND TO BE WITHIN LIMITS. MAX MATERIAL REMOVED .007 ETCHED, ALODINED AFFECTED AREA REF SRM 51-12-00-001-001-A01. FPI IAW CRJ 700 PART 1 51-20-008. NO CRACKS NOTED. PRIMED AND PAINTED AFFECTED AREA.

Part: PANEL — CHAFED (TE FLAP) · airframe 19,906 hrs · 14,547 cycles

PDX - 20K - LT FLAP PANEL 584EB HAS CHAF APPROX .020. BLENDED OUT DAMAGE IAW CRJ 700 SRM 57-52-02 PG 102. DAMAGE IS WITHIN LIMITS AND OK FOR CONTINUED SERVICE. ORIGINAL THICKNESS .100 MATERIAL REMAINING IS .078. PERFORMED FPI OF PANEL 584EB BLEND FOR CRACKS IAW CRJ 700 NDTM PART 01, 51-20-008. NO CRACKS NOTED. ETCHED, ALODINED AND PRIMED AFFECTED AREA.

Part: PANEL — CHAFED (TE FLAP) · airframe 19,906 hrs · 14,547 cycles

PDX - 20K - RT FLAP PANEL 684AB HAS CHAF. BLENDED OUT DAMAGE IAW CRJ SRM 57-52-02 PG 102 AND FOUND TO BE WITHIN LIMITS. ORIGINAL THICKNESS .100 REMAINING IS .088 OK FOR SERVICE. FPI BLENDED AREA FOR CRACKS IAW SRM 51-12-00-001-001-A01 PAGE 10, PAR 7B(4), AND CRJ NDTM PART 1, 51-20-008. NO CRACKS NOTED. ETCHED, ALODINED AND PRIMED AFFECTED AREA.

Part: PANEL — CHAFED (TE FLAP) · airframe 19,906 hrs · 14,547 cycles

PDX - 20K - RT WING FLAP PANEL 684LB IS CHAFED. BLENDED OUT DAMAGE AND FOUND TO BE WITHIN LIMITS. MAX MATERIAL REMOVED .006 ETCHED, ALODINED AFFECTED AREA REF SRM 57-52-01-101-001-A01. FPI IAW CRJ 700 NDTM PART I 51-20-008, NO CRACKS NOTED. PRIMED AND PAINTED AFFECTED AREA.

Part: WARNING MESSAGE — ILLUMINATED · airframe 19,792 hrs · 14,456 cycles

SEA- GLD UNSAFE CAUTION MSG ON TAKEOFF ROLL ABORTED AT 75 KTS, DEPARTED ON RUNWAY 34C AT P1. PERFORMED OPS TEST OF RADIO ALTIMETER IAW RIL 84-34-018 AND TC R344401. OPS TEST GOOD, NO MESSAGES NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: ALTIMETER — MALFUNCTIONED · airframe 19,789 hrs · 14,452 cycles

SEA - GLD UNSAFE CAUTION MSG ON TAKEOFF ROLL ABORTED AT 75 KTS, DEPARTED ON RUNWAY 34C AT P1. PLACED RADIO ALTIMETER SYSTEM ON MEL 34-44-1. RETURNED TO SERVICE. PERFORMED OPS TEST OF RADIO ALTIMETER IAW RIL 84-34-018 AND TC R344401. OPS TEST GOOD, NO MESSAGES NOTED ACFT IS NOW CATII PLACARD REFLECTS CATII. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WARNING MESSAGE — ILLUMINATED · airframe 19,786 hrs · 14,449 cycles

SEA - DURING T/O GLD UNSAFE CAUTION MSG ILLUMINATED. TAKEOFF ABORTED JUST BELOW 60 KTS. PERFORMED FIM TASK 27-64-00-810-803-A01. OPS TESTED GROUND LIFT DUMPING MANUAL ARM AND DISARM, CHECKS GOOD. OPS TESTED RADIO ALTIMETER, CHECKS GOOD. C/W SPOST 1 AND 2 OF SSCU'S, NO FAULTS FOUND. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: HANDLE — BROKEN (CARGO DOOR)

GROUND AGENT REPORTS MCD OUTER HANDLE BROKE OFF. FERRIED, RREMOVED AND REPLACED MCD OUTER HANDLE IAW T/C SB670BA-52-030, WO 68578. OPS TEST GOOD GROUND VALVE REACTIVATED. PREFORMED OPS TEST OF GROUND VALVE IAW AMM TASK 21-24-18-710-801-A01. OPS TEST GOOD. (K)

Part: WARNING SYSTEM — ACTIVATED (FIRE WARNING) · airframe 17,771 hrs · 12,681 cycles

PDX - FLIGHT 2621, FIRE SYSTEM FAULT MESSAGE RECEIVED. PLACED ON MEL 26-00-1. RETURNED TO SERVICE. (S)

Part: LIGHT — SMOKE (COCKPIT) · airframe 17,482 hrs · 12,446 cycles

PDX - FLIGHT 2508 - F/O NOTICED PUFF OF SMOKE WHEN STOWING MAP LIGHT. DEACTIVATED BY PULLING C/B. PLACED ON MEL 33-11-1. RETURNED TO SERVICE. (A)

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 17,042 hrs · 12,132 cycles

PFD C4 CHECK FOUND LIGHT CORROSION ON 280 CROSSBEAM. REMOVED LIGHT CORROSION ON 280 CROSSBEAM. REMOVED .002 INCH WITHIN LIMITS IAW REO 670-53-11-046. PRIMED EXPOSED AERAS IAW SRM 51-25-06 APPLIED TOPCOAT PAINT IAW SRM 51-25-16.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 17,042 hrs · 12,132 cycles

RFD C4 CHECK MINOR CORROSION ON PAX DOOR MID CAP ANGLE. REMOVED CORROSION ON PAX MID CAP ANGLE. REMOVED .002 INCH WITHIN LIMITS. IAW SRM 53-21-23. TREATED EXPOSED METAL AREAS IAW SRM 51-21-11 APPLIED EPOXY PRIMER TO AERA IAW SRM 51-25-06 APPLIED TOPCOAT IAW SRM 51-25-16.

Part: ANGLE — CORRODED (FUSELAGE)

PFD C4 CHECK FORWARD ANGLE FOUND TO BE CORRODED AT FS 280. REMOVED FORWARD ANGLE AT FS 280 IAW 51-42-06. LOCATED HOLES ON NEW ANGLE FWD AT FS 280 IAW SRM 51-40-11. INSTALL FWD ANGLE IAW SRM 51-42-06. PRIMED RIVETS IAW SRM 51-25-06 AND APPLIED PAINT TO RIVETS IAW SRM 51-25-16.

Part: PANEL — CHAFED (WING) · airframe 17,042 hrs · 12,132 cycles

RFD C4 CHECK PANEL 584HT HAS CHAFFING. BLENDED PANEL 584HT FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 57-52-02. REMOVED .004 MATERIAL FROM PANEL 584HT IAW CRJ 700 SRM 57-52-02. PRIMED PANEL 584HT IAW CRJ 700 SRM 51-25-06, PAINTED PANEL WITH 8003/B707 PAINT IAW CRJ 700 SRM 51-25-01.

Part: PANEL — CHAFED (WING) · airframe 17,042 hrs · 12,132 cycles

RFD C4 CHECK PANEL 584ET HAS CHAFFING. BLENDED PANEL 584ET FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 57-52-02. REMOVED .005 MATERIAL FROM PANEL 584ET IAW CRJ 700 SRM 57-52-02. PRIMED PANEL 584ET IAW CRJ 700 SRM 51-25-06, PAINTED PANEL WITH 8003/B707 IAW CRJ 700 SRM 51-25-01.

Part: SEAL — DAMAGED (PAX DOOR) · airframe 16,907 hrs · 12,040 cycles

FLT 2569 - AFTER DEPARTURE, THE MAIN CABIN DOOR STARTED SQUEALING. NO PRESSURIZATION PROBLEMS OR DOOR WARNINGS. SQUEAL BECAME LOUDER AND IT WAS DECIDED TO DIVERT TO PDX. MAINTENANCE REPLACED THE DOOR SEAL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SENSOR — MALFUNCTIONED (ACM INLET TEMP) · airframe 16,127 hrs · 11,457 cycles

GEG - FLIGHT 2599 - LEFT BLEED CAUTION ILLUMINATED. WENT OFF AFTER SELECTING PACK TO OFF. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE PACK INLET TEMP SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — ODOR (CABIN) · airframe 16,070 hrs · 11,417 cycles

SEAT 4A PSU LENS COVER FELL OFF AND NOTICED A BURNED ODOR COMING FROM THE LIGHT AREA. MAINTENANCE INSPECTED AREA AND NOTICED NO EVIDENCE OF BURNS OR SMOKE. REINSTALLED THE LIGHT COVER. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: FIRE LOOP — ILLUMINATED · airframe 16,007 hrs · 11,369 cycles

PSP- FLIGHT 2625 - FIRE SYSTEM FAULT MESSAGE RECEIVED. MAINTENANCE PLACED ON MEL 26-00-1. REPLACED FIRE LOOP "A" AT THE RIGHT ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (RT A/C PACK) · airframe 15,392 hrs · 10,966 cycles

FAT - ON FLIGHT 2544, DURING TAXI, RECEIVED R PACK FAULT STATUS MESSAGE. RETURNED TO GATE. MAINTENANCE CYCLED AIRCRAFT POWER AND FOUND NO CURRENT FAULTS IN MDC. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 14,372 hrs · 10,301 cycles

DEN - FLIGHT 4331 - ON POWER UP OF AIRCRAFT, FIRE DETECTOR IN LAVATORY ALARM IS ON. MAINTENANCE REPLACED THE LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: VALVE — MALFUNCTIONED (ANTI ICE SYSTEM) · airframe 13,877 hrs · 9,971 cycles

PDX - FLIGHT 2506 - RETURNED TO THE FIELD AFTER A LEFT ENGINE ANTI-ICE CAUTION MESSAGE. UNEVENTFUL LANDING. REPLACED THE COWL ANTI-ICE VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — UNKNOWN (PITCH FEEL) · airframe 13,797 hrs · 9,920 cycles

PDX - FLIGHT 2565 (PDX-ONT) PITCH FEEL CAUTION MESSAGE IN CRUISE FLIGHT. LANDED WITHOUT INCIDENT WITH REDUCED FLAP SETTING. MAINTENANCE COMPLIED WITH SSCU RESET IAW CRJ700-705-900-SL-27-052 SERVICE LETTER. OPERATIONAL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: IRS — FAILED (NR 2) · airframe 13,170 hrs · 9,493 cycles

DEN - FLIGHT 4340, RECEIVED A YAW DAMPER INOP STATUS MESSAGE, PITCH FEEL FAULT STATUS MESSAGE, AUTOPILOT FAILURE, AND PFD AND MFD FAILURES (RED X) ON FO SIDE. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE NR 2 INERITAL REFERENCE SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ANGLE — CRACKED (THRUST REVERSER) · airframe 12,390 hrs · 8,988 cycles

C3 PDX - DURING INSPECTION FOR PART ROB, FOUND RIGHT ENGINE TRANS COWL AIR PATH CLOSING ANGLE CRACKED AT OUTBOARD END. REPAIRED IAW MM 78-33-01.

Part: ANGLE — CRACKED (THRUST REVERSER) · airframe 12,390 hrs · 8,988 cycles

C3 PDX - DURING INSPECTION FOR PART ROB, FOUND LEFT ENGINE UPPER TRANS COWL AIR PATH CLOSING ANGLE CRACKED AT OUTBOARD END. REPAIRED IAW MM 78-33-01.

Part: VANE — CRACKED (TE FLAPS) · airframe 12,390 hrs · 8,988 cycles

C3 PDX - SUSPECTED CRACK ON UPPER SURFACE OF RIGHT OUTBOARD FLAP VANE AT FS79.46. REPAIRED IAW SRM 57-53-01, AND SRM 51-42-21.

Part: STRUCTURE — DAMAGED (SPOILERS) · airframe 12,390 hrs · 8,988 cycles

C3 PDX - RIGHT WING LOWER TRAILING EDGE AT WS 170 INBOARD OF THE MULTI-FUNCTION SPOILER HAS SEVERAL FASTENERS WITH BUCK TAILS BROKEN. REPAIRED IAW SRM 51-42-06.

Part: SILL — CHAFED (FUSELAGE) · airframe 12,390 hrs · 8,988 cycles

C3 PDX - CHAFE AT AFT BAGGAGE DOOR LEVER SILL. REPAIRED IAW REO 670-53-61-283.

Part: BRACKET — DAMAGED (RT WING) · airframe 12,390 hrs · 8,988 cycles

C3 PDX - RIGHT WING SHROUD BRACKET AT STATION WING 140.0 HAS ELONGATED FASTENER HOLE. REPAIRED IAW REO 670-57-51-106 AND SRM 51-21-16.

Part: SKIN — CORRODED (FUSELAGE) · airframe 12,390 hrs · 8,988 cycles

C3 PDX - UPPER TCAS ANTENNA SKIN HAS LIGHT CORROSION AROUND BOLT HOLES. REPAIRED IAW REO 670-53-21-215 AND SRM 51-21-06.

Part: PANEL — CHAFED (WING) · airframe 12,390 hrs · 8,988 cycles

C3 PDX - PANEL 622CB HAS CHAFE ON INBOARD FLANGE OF CUTOUT. REPAIRED IAW SRM 57-41-01, AND REO 670-57-41-104.

Part: RADOME — CHAFED (BS 169) · airframe 12,389 hrs · 8,987 cycles

C3 PDX - AT FS 169.00 BOTH THE RIGHT AND LEFT SPACERS ON THE RADOME ARE CHAFING ON THE BULKHEAD. REPAIRED IAW SRM 51-25-01 AND 53-81-80.

Part: SILL — CHAFED (FUSELAGE) · airframe 12,389 hrs · 8,987 cycles

C3 PDX - CHAFE AT AFT BAGGAGE DOOR LOWER SILL JUST 6" AFT OF FORWARD LOWER CORNER. REPAIRED IAW SRM 51-12-00 AND REO 670-53-61-281.

Part: DOOR FRAME — CORRODED (E/E BAY) · airframe 12,389 hrs · 8,987 cycles

C3 PDX -THE INSIDE APERTURE FOR THE AVIONICS DOOR HAS LIGHT CORROSION FROM DOOR SEAL. REPAIRED IAW SRM 51-21-06, 53-21-01, 51-20-006, AND REO 670-53-21-217.

Part: SKIN PANEL — NICKED (LT WING) · airframe 12,389 hrs · 8,987 cycles

C3 PDX - LEFT WING INBOARD FIXED LEADING EDGE PANEL 521AT HAS 2 NICKS. REPAIRED IAW SRM 57-41-01 AND SRM 51-21-11.

Part: SKIN — CHAFED (RT AILERON) · airframe 12,389 hrs · 8,987 cycles

C3 PDX - CHAFING FOUND ON RIGHT AILERON LEADING EDGE TOP SURFACE JUST INBOARD OF OUTBOARD WING. REPAIRED IAW SRM 57-61-01, SRM 51-42-06, SRM 51-21-11 AND SRM 51-41-27.

Part: SKIN — DAMAGED (LT AILERONS) · airframe 12,389 hrs · 8,987 cycles

C3 PDX - CHAFING DAMAGE FOUND ON LEADING EDGE OF LEFT AILERON UPPER SURFACE. REPAIRED IAW SRM 57-61-01, 51-40-11, 51-42-20, 51-40-10, AND 51-42-27.

Part: SKIN — DAMAGED (LT AILERON) · airframe 12,389 hrs · 8,987 cycles

C3 PDX - CHAFE DAMAGE FOUND ON LEADING EDGE OF LEFT AILERON UPPER SURFACE. REPAIRED IAW SRM 57-61-01, 51-42-20, 51-40-10, AND 51-42-27.

Part: VANE — CHAFED (LT TE FLAP) · airframe 12,389 hrs · 8,987 cycles

C3 PDX - LEFT OUTBOARD FLAP VANE LOWER SURFACE LEADING EDGE HAS CHAFE AT WS 282 OUTBOARD END. REPAIRED IAW SRM 57-53-01 AND SRM 51-25-06.

Part: SKIN — CHAFED (RT AILERON) · airframe 12,389 hrs · 8,987 cycles

C3 PDX - MINOR CHAFING FOUND ON RIGHT AILERON LEADING EDGE LOWER SURFACE. REPAIRED IAW SRM 57-61-01, SRM 51-20-0004, AND SRM 51-21-11, SRM 51-25-06.

Part: RETAINER — DAMAGED (E/E BAY) · airframe 12,389 hrs · 8,987 cycles

C3 PDX - AVIONICS ACCESS DOOR SEAL RETAINER HAS IMPACT DAMAGE IN FOUR PLACES, 2 FORWARD AND 2 AFT. THE SEAL HAS ALSO BEEN DAMAGED. REPAIRED IAW AMM 52-42-07 AND AMM 52-42-27.

Part: SKIN — GOUGED (RWS 180) · airframe 12,389 hrs · 8,987 cycles

C3 PDX - GOUGE IN RIGHT WING FIXED LEADING EDGE AT WS 180 BETWEEN INBOARD AND MID SLAT. REPAIRED IAW SRM 51-21-11 AND SRM 51-20-006, SRM 57-41-01.

Part: RIB — MISDRILLED (RT WING) · airframe 12,389 hrs · 8,987 cycles

C3 PDX - RIGHT WING LEADING EDGE 622AR AT WS 91.0 ON BOTTOM SIDE 4 RIVETS HAVE BEEN MISDRILLED THRU INNER SUPPORT RIBS. REPAIRED IAW REO 670-57-41-102.

Part: SKIN — CHAFED (LT WING) · airframe 12,389 hrs · 8,987 cycles

C3 PDX - LEFT WING FIXED LEADING EDGE 522RL CHAFED IN 5 PLACES JUST BELOW CENTER LINE OF LEADING EDGE. REPAIRED IAW SRM 57-41-01 AND SRM 51-25-01.

Part: ATTACH FITTING — CORRODED (W-F FAIRING) · airframe 12,389 hrs · 8,987 cycles

C3 PDX - FORWARD AREA OF LOWER WING TO FUSELAGE FAIRING HAS SIGNS OF CORROSION AT ATTACH POINTS, PANEL 191AB. REPAIRED IAW SRM 51-21-06.

Part: SKIN — NICKED (LT WING SLAT) · airframe 12,389 hrs · 8,987 cycles

C3 PDX - LEFT WING INBOARD SLAT HAS 2 NICKS. REPAIRED IAW SRM 57-42-01 AND SRM 51-20-00.

Part: SKIN — NICKED (LT WING SLAT) · airframe 12,389 hrs · 8,987 cycles

C3 PDX - LEFT WING CENTER SLAT LOWER SURFACE HAS 1" LINE OF SMALL NICKS. REPAIRED IAW SRM 57-42-01 AND SRM 51-20-006.

Part: SKIN — GOUGED (RT WING) · airframe 12,389 hrs · 8,987 cycles

C3 PDX - GOUGES ON RIGHT WING LEADING EDGE PANEL 621AT. REPAIRED IAW SRM 57-41-01 AND SRM 51-20-004, SRM 51-20-006.

Part: SKIN — CORRODED (BS 1000) · airframe 12,389 hrs · 8,987 cycles

C3 PDX -THERE IS SURFACE CORROSION ON THE BOTTOM OF THE FUSELAGE AT FS 1000.00 AND 10" LEFT OF THE FUEL DRAIN PIPE. REPAIRED IAW SRM 53-61-01 AND 51-25-06.

Part: STATUS MESSAGE — ILLUMINATED · airframe 12,047 hrs · 8,752 cycles

PDX - FIRE SYSTEM FAULT STATUS MESSAGE DISPLAYED. MAINTENANCE PLACED SYSTEM ON MEL 26-00-1 (RSI 278427). AIRCRAFT RETURNED TO SERVICE.

Part: ODOR — DETECTED (COCKPIT) · airframe 11,870 hrs · 8,630 cycles

PDX - OIL ODOR IN CABIN AND COCKPIT, ODOR DISSIPATES WHEN THE APU IS SHUT DOWN. MAINTENANCE PERFORMED A DETAILED INSPECTION OF THE APU INCLUDING THE DUCT AND OIL SYSTEMS, NO DEFECTS NOTED. GROUND RUN ON ENGINES AT HIGH POWER FOR 20 MINUTES AND VARIOUS SETTINGS FOR 20 MINUTES. RAN BETWEEN APU AIR AND ENGINE BLEED AIR. NO DEFECTS OR ODORS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: ODOR — DETECTED (CABIN) · airframe 11,862 hrs · 8,625 cycles

PDX - STRONG ODOR OF OIL IN THE CABIN WHILE ON THE GROUND, IMPROVES AFTER APU IS SHUT DOWN. MAINTENANCE COULD NOT DUPLICATE ODOR. APU OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: TARGET — LOOSE (MLG) · airframe 11,029 hrs · 8,072 cycles

PDX - ON FLIGHT 2525, AIRCRAFT RETURNED TO FIELD. NOSE DOOR OPEN MASTER WARNING. MAINTENANCE RESECURED LT NOSE LANDING GEAR TARGET. PERFORMED OPERATIONAL TEST OF THE LANDING GEAR, TEST GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: PRESSURE SWITCH — MALFUNCTIONED (HYD SYSTEM) · airframe 10,318 hrs · 7,629 cycles

DEN - ON TAXI FOR FLIGHT 4325 RECEIVED HYD PUMP 1B CAUTION MSG. RETURNED TO THE GATE. FOUND HYD PUMP 1B LOW PRESSURE SWITCH INTERMITTENT WITH PUMP 1B AND NR 1 ENG DRIVEN PUMP 1A OFF HYD PRESSURE INDICATED 2900 PSI WITH HYD PUMP 1B CAUT MSG CYCLED HYD PUMP 1B SWITCH AND DISCONNECTED AND RECONNECTED LOW PRESSURE SWITCH, WITH NR 1B PUMP SELECTED TO ON EICAS SHOWS GREEN WITH NO CAUTION MSG RESCHEDULED IAW MEL 29-34-1. 12/22 REMOVED AND REPLACED NR 1 PUMP PRESSURE SWITCH IAW CRJ 700 AMM 29-34-01-000-801-A01 AND 29-34-01-400-801-A01, OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SENSOR — FAILED (NR 1 A/C PACK) · airframe 10,309 hrs · 7,623 cycles

DAY- ON TAXI OUT ON FLIGHT 4192 RETURNED TO THE GATE WITH A LEFT AIR CONDITIONING PACK MESSAGE. PLACED ON MEL 21-51-4B. 12/26 REMOVED AND REPLACED NR 1 PACK. DISCHARGE TEMP SENSOR AND NR 1 PACK, DISCHARGE PRESSURE SENSOR IAW CRJ 700 AMM 21-51-22-000-801-A01/21-51-22-400-801-A01, AMM 21-51-24-000-801-A01/21-51-24-400-801-A01. PERFORMED AN OPS AND LEAK CHECK OF SYSTEM, CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: MOTOR — MALFUNCTIONED (PAX DOOR) · airframe 9,752 hrs · 7,263 cycles

DEN - MAIN CABIN DOOR HARD TO CLOSE AND OPEN. MAINTENANCE FOUND THE POWER ASSIST CABLE OFF THE ROLLER AND THE CABLE DAMAGED. REPLACED THE POWER ASSIST MOTOR AND CABLE ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RADIO — MALFUNCTIONED (ZONE 200) · airframe 8,750 hrs · 6,545 cycles

DEN - ON FLT 4333, RETURNED TO FIELD, RADIO TUNING UNIT 1 STUCK ON TX AND THEN CLEARED, THEN UNABLE TO TX. REMOVED AND REPLACED NR 1 RADIO TUNING UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CHIMNEY — DAMAGED (FWD CARGO) · airframe 7,847 hrs · 5,879 cycles

PDX - MAINTENANCE FOUND THE FORWARD CARGO BAY CHIMNEY DAMAGED AND REPLACED THE SAME. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PAN — CRACKED (ZONE 200) · airframe 7,565 hrs · 5,663 cycles

PDX - RIGHT HAND STUB WING PRESSURE PAN HAS TWO CRACKS WHERE THE NR 2 PRESSURE HYDRAULIC LINE PASSES THROUGH. REPAIRED IAW SRM 51-42-06-001-0001-A01, SRM 51-23-00 AND SRM 51-42-06.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,565 hrs · 5,663 cycles

PDX - LEFT HAND OUTBOARD SEAT TRACK HAS CORROSION AT STATION 738 TO 756. REPLACED IAW CRJ AMM 53-00-49.

Part: BEAM — CRACKED (FUSELAGE) · airframe 7,565 hrs · 5,663 cycles

PDX - BEAM 280 IS CRACKED AND CORRODED. REPAIRED IAW REO 670-53-11-045.

Part: SKIN — CRACKED (ZONE 800) · airframe 7,565 hrs · 5,663 cycles

PDX - MAIN CABIN DOOR, AFT ATTACHMENT ANGLE STEP ASSEMBLY TO INNER DOOR SKIN HAS CRACK NEXT TO PULLEY ASSEMBLY. REPAIED IAW REO 670-52-11-072, SHEET 2, NOTE 5 AND CRJ 700 AMM TASK 52-11-08-400-801-A01.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 7,565 hrs · 5,663 cycles

PDX - LEFT HAND LOWER WEB OF BULKHEAD AT STATION 280 HAS CORROSION. REPLACED IAW CRJ SRM 51-42-06 AND SRM 51-42-13.

Part: WEB — CORRODED (ZONE 100) · airframe 7,431 hrs · 5,522 cycles

PDX RIGHT HAND LOWER WEB AT STATION 280 HAS CORROSION. REPLACED IAW SRM 51-42-06, 51-42-13.

Part: TRU — FAILED (ZONE 200) · airframe 6,149 hrs · 4,610 cycles

DEN - FLIGHT 4093 - BURNED WIRE ODOR COMING FROM NR 2 RIGHT OUTBOARD TRU. REMOVED AND REPLACED NR 2 RIGHT HAND TRU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: TIRE — SEPARATED (NR 3) · airframe 5,795 hrs · 4,359 cycles

THE CREW RETURNED TO FIELD WHEN AFTER TAKE-OFF THE NR 3 MAIN TIRE RECAP CAME OFF. THIS SDR WILL REMAIN IN AN OPEN STATUS PENDING COMPLETION OF MAINTENANCE. THE NUMBER 3 MAIN TIRE WAS REPLACED WITH NEW. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NOTE: THIS TIRE WAS AT RECAP LEVEL 1. RECAPPED TIRES ARE NO LONGER BEING.

Part: EJECTOR — CRACKED (LEFT) · airframe 5,475 hrs · 4,141 cycles

BOI - FLIGHT 4276 - THE CREW REPORTED THAT THE LEFT FUEL TANK WAS LEAKING INTO THE CENTER TANK AND RECEIVED A FUEL IMBALANCE CAUTION MESSAGE. MAINTENANCE INSPECTED THE SYSTEM AND FOUND THE LEFT PRIMARY EJECTOR CRACKED. THE EJECTOR WAS REPLACED AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SCREEN — TORN (CARGO BAY) · airframe 4,940 hrs · 3,786 cycles

PDX- CENTER CHIMNEY IN FORWARD CARGO BAY HAS TORN SCREEN. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — UNSECURE (ZONE 800) · airframe 4,501 hrs · 3,458 cycles

BOI- ON FLIGHT 2571 GPU PLUG-IN DOOR UNSECURED IN FLIGHT. AIRCRAFT RETURNED TO FIELD. INSPECTED GPU DOOR AND SECURED DOOR. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CHIMNEY — TORN (ZONE 200) · airframe 4,219 hrs · 3,256 cycles

FORWARD CARGO BAY CHIMNEY ABOVE DOOR HAS A TORN SCREEN. REMOVED AND REPLACED CHIMNEY.

Part: SKIN — CHAFED (RT WING) · airframe 3,698 hrs · 2,862 cycles

PDX - RIGHT HAND WING BOTTOM TRAILING EDGE CHAFED. REPAIRED IAW MFG EA R-57-38 AND REO 670-57-51-012.

Part: SCREW — UNSECURE (TCAS ANTENNA) · airframe 3,698 hrs · 2,862 cycles

PDX - LOWER TCAS ANTENNA FORWARD RIGHT HAND NUTPLATE SCREW SPINS. REPAIRED IAW TR 34-0051, TASK 34-43-07-400-801-A01, PARAGRAPH A THROUGH D.

Part: SMOKE DETECTOR — MALFUNCTIONED (ZONE 200) · airframe 3,573 hrs · 2,768 cycles

AFT LAVATORY SMOKE DETECTOR MESSAGE. TESTED AND FOUND TO BE GOOD FOR SERVICE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FAN — FAILED (CABIN AIR) · airframe 3,257 hrs · 2,538 cycles

PDX-ON FLIGHT NUMBER 2449, FAINT ODOR OF BURNING PLASTIC IN COCKPIT AND CABIN. RECIRCULATING FAN CIRCUIT BREAKER POPPED. TURNED OFF RECIRCULATING FAN, ODOR DISAPPEARED. PLACED ON RSI 326845.

Part: CHIMNEY — TORN (ZONE 100) · airframe 3,243 hrs · 2,530 cycles

BOI- SCREEN TORN ON CENTER CHIMNEY OF FORWARD CARGO COMPARTMENT. INSTALLED NEW CHIMNEY AS REQUIRED. AIRCRAFT RETURNED TO SERVICE.

Part: STRUCTURE — CRACKED (ZONE 600) · airframe 2,957 hrs · 2,323 cycles

CKB - RIGHT HAND WING CRACK FOUND ON STRUCTURE UNDER INBOARD FLIGHT SPOILER. REPAIRED IAW RD 670-57-51-00-4 AND HORIZON AIR EA R-53-77.

Part: BULKHEAD — CRACKED (ZONE 200) · airframe 2,957 hrs · 2,323 cycles

FOUND TWO CRACKS BY LPI IN AFT PRESSURE BULKHEAD. REPAIRED IAW CRJ 700 MM TACK 51-23-00-390-810-A01 AND RO R-29-07.

Part: RIVET — LOOSE (ZONE 600) · airframe 2,957 hrs · 2,323 cycles

CKB - RIGHT HAND WING FLAP GUIDE VANES HAVE SOME LOOSE RIVETS. REPAIRED IAW CRJ 700 SRM 51-42-13.

Part: STRINGER — DAMAGED (ZONE 200) · airframe 2,957 hrs · 2,323 cycles

PDX - AT STRINGER 0 OF FS 333 LEFT HAND AND RIGHT HAND SIDES TOP EXISTING HOLE FALLS OUT INTO RADIUS OF ANGLE P/N SH670-31810-985 AND SH670-31810-987. REPAIRED IAW HORIZON AIR EA R-53-75A.

Part: BLADE — MISSING (ZONE 400) · airframe 641 hrs · 539 cycles

NR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND ONE BLADE MISSING. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECKED GOOD. AIRCRAFT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THAT MODIFICATION TO THE HPT1 DAMPNER (ALONG WITH RE-WORK OF THE ACCELERATOR) IS THE CORRECTIVE ACTION FOR THE REMOVED ENGINE. A PLAN HAS BEEN DEVISED TO INCORPORATE THIS MOD IN THE NEXT FEW QUARTERS.

Part: SWITCH — FAILED (FUEL SYSTEM) · airframe 2,776 hrs · 2,195 cycles

PDX ON FLIGHT 2474- LEFT FUEL LOW PRESSURE CAUTION MESSAGE WHEN LEFT BOOST PUMP SELECTED. REMOVED AND REPLACED ENGINE PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — FAILED (FUEL SYSTEM) · airframe 2,761 hrs · 2,185 cycles

BOI ON FLIGHT 2551- RIGHT FUEL LOW PRESSURE CAUTION MESSAGE AFTER ENGINE START. REMOVED AND REPLACED NR 2 ENGINE INLET PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 2,593 hrs · 2,063 cycles

PDX- FIRE SYSTEM FAULT STATUS MESSAGE. REMOVED AND REPLACED FORWARD BAGGAGE SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (FIRE DETECTION) · airframe 2,569 hrs · 2,046 cycles

MFR ON FLIGHT 2540- FIRE SYSTEM FAULT STATUS MESSAGE EN ROUTE. CYCLED SHIPS POWER, FIRE SYSTEM CHECKED OK. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CAGE — TORN (CARGO BAY) · airframe 2,552 hrs · 2,034 cycles

TUS ON FLIGHT 2535- FORWARD BAGGAGE COMPARTMENT CHIMNEY HAS ONE INCH TEAR. REPAIRED IAW HORIZON AIR EO 670-53-32-001. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — FAILED (FUEL SYSTEM) · airframe 2,537 hrs · 2,021 cycles

PDX- FUEL LEAKING FROM NR 1 ENGINE FUEL INLET PRESSURE SENSOR IN LEFT HAND WHEEL WELL. REMOVED AND REPLACED NR 1 PRIMARY EJECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BRACKET — BROKEN (PAX DOOR) · airframe 2,499 hrs · 1,995 cycles

PDX- MAIN CABIN DOOR SUPPORT WHEEL BRACKET IS BROKEN. REPAIRED IAW CRJ MM TASK 52-11-13-710-801-A01.

Part: CONTROL PANEL — MALFUNCTIONED (FUEL SYSTEM) · airframe 2,119 hrs · 1,721 cycles

SEA- AIRCRAFT FUELER REPORTED SMOKE FROM SPR CONTROL PANEL WHEN POWER SWITCH SELECTED ON. PANEL SMELLED OF BURNT ELECTRONIC COMPONENTS. REMOVED AND REPLACED REFUEL/DEFUEL PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PRESSURE SWITCH — LEAKING (FUEL SYSTEM) · airframe 1,944 hrs · 1,583 cycles

PDX - CREW REPORTS FUEL LEAK AT CENTER FUEL TANK DURING PREFLIGHT. MAINTENANCE INSPECTED AND REPLACED THE LEFT PRIMARY EJECTOR PRESSURE SENSOR. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CAGE — DAMAGED (CARGO BAY) · airframe 1,282 hrs · 1,039 cycles

PDX- DAMAGE FOUND TO THE SCREEN OF FORWARD BAGGAGE BAY CHIMNEY ASSEMBLY AT CENTER SMOKE DETECTOR. REMOVED AND REPLACED FORWARD CARGO SMOKE DETECTOR PROTECTIVE COVERING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SENSE LINE — BROKEN (FUEL TANK) · airframe 985 hrs · 821 cycles

FAT-RIGHT MAIN EJECTOR CAUTION MESSAGE AT 22,000 FEET DESCENDING, TANK AT 80 POUNDS INCREASED TO 220 POUNDS THEN DECREASED TO 70 POUNDS. BOTH BOOST PUMPS WERE OPERATING. REMOVED FUEL PANEL 611AB, FOUND PRIMARY EJECTOR SENSOR LINE BROKEN AT B-NUT. REMOVED AND REPLACED SENSOR LINE WITH NEW. CLOSED PANEL 611AB. GROUND RAN BOTH ENGINES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PRESSURE SWITCH — LEAKING (FUEL SYSTEM) · airframe 991 hrs · 817 cycles

MFR - FUEL LEAKING FROM CENTER FUSELAGE FORWARD WING AREA. MAINTENANCE REPLACED THE PRIMARY EJECTOR PRESSURE SENSOR. OPERATIONAL AND LEAKS CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: HINGE — DAMAGED (PAX DOOR) · airframe 263 hrs · 221 cycles

PDX - THE FORWARD PASSENGER DOOR HINGE IS DAMAGED. REPAIRED IAW EA 12-53-09.