N616QX

Part: SKIN — DAMAGED (RT WING LE) · airframe 36,051 hrs · 27,820 cycles

DISCOVERED SURFACE DAMAGE TO THE LEADING EDGE PANEL 622AR AT FASTENER HOLE BOTTOM INBD END OF THE PANEL. REPAIRED THE DAMAGE IAW EA 45-2018-127, AND EC/TC EA 45-2018-127.

Part: BUSHING — WORN (LT PYLON) · airframe 36,051 hrs · 27,820 cycles

LEFT ENGINE PYLON TIE-BAR ATTACH BUSHINGS AND BEARINGS WORN. REPLACED THE BUSHING AND BEARINGS IAW REO 670-54-22-002, REV NC, AND EC/TC REO 670-54-22-002.

Part: SUPPORT — CRACKED (BS 909) · airframe 36,051 hrs · 27,820 cycles

PANEL 195DL SUPPORT STRUCTURE WAS CRACKED AT BS 909. REPAIRED FAIRING SUPPORT IAW REO 670-53-82-478, REV K, AND EC/TC REO 670-53-82-478, REV A.

Part: WEB — CRACKED (BS 193) · airframe 36,051 hrs · 27,820 cycles

FORWARD EQUIPMENT COMPARTMENT, LT FLOOR WEB HAD A .500 INCH CRACK AT BS 193. REPAIRED IAW REO 670-53-11-509, REV D, AND EC/TC REO 670-53-11-509, REV C.

Part: TRIPLER — CHAFED (BS 985) · airframe 36,051 hrs · 27,820 cycles

TRIPLER AT BS 985, BL 0 WAS CHAFED. REPAIRED TRIPLER IAW REO 670-53-00-552 REV -, AND EC/TC REO 670-53-00-552.

Part: MOUNT — CORRODED (BS 295) · airframe 36,051 hrs · 27,820 cycles

GALLEY MOUNT FITTING AT BS 295, RBL 9 HAD MINOR CORROSION. REMOVED AND REPLACED THE MOUNT FITTING IAW SRM 51-42-21-001-001-A01.

Part: ANGLE — CORRODED (BS 280) · airframe 36,051 hrs · 27,820 cycles

BS 280, FORWARD J SPLICE, JUST BELOW FLOOR WAS CORRODED BETWEEN LBL 12 TO RBL 12. REMOVED AND REPLACED THE J-ANGLE IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: CHANNEL — CRACKED (CGO DOOR AREA) · airframe 36,051 hrs · 27,820 cycles

AFT CARGO DOOR SURROUND STRUCTURE, AFT LOWER C CHANNEL WAS CRACKED. REPLACED THE C CHANNEL IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 549) · airframe 34,455 hrs · 26,263 cycles

LBL 9 AND RBL 9 FLOORBEAM INNER FLANGE IS CORRODED AT BS 549. REPAIRED THE FLOORBEAM IAW REO 670-53-31-425, REV-, AND REO 670-53-31-425.

Part: FRAME — CORRODED (BS 364) · airframe 34,455 hrs · 26,263 cycles

FRAME SECTOR, BS 364 IS CORRODED BETWEEN STRINGERS 25R TO 26R. REPAIRED THE FRAME IAW SRM 53-21-23-201-008-A01.

Part: DIAPHRAGM — CORRODED (BS 333-349) · airframe 34,455 hrs · 26,263 cycles

DRAIN MAST DIAPHRAGM DOUBLER IS CORRODED BETWEEN STRINGERS 24R TO 25R, BS 333 TO 349. REMOVED AND REPLACED DRAIN MAST DIAPHRAGM DOUBLER IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 34,455 hrs · 26,263 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED IN PREVIOUS REPAIR. REPAIRED THE DRAG ANGLE IAW SRM 52-11-04-201-002-A01, TYPE 2 REPAIR.

Part: FRAME — CORRODED (BS 333) · airframe 34,455 hrs · 26,263 cycles

FRAME SECTOR BS 333 IS CORRODED BETWEEN STRINGERS 26R TO 26L. REPAIRED THE FRAME IAW REO 670-53-21-799, REV A, AND REO 670-53-21-799 03.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 34,455 hrs · 26,263 cycles

STRINGER SPLICE 25R IS CORRODED AT BS 333. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (BS 333-349) · airframe 34,455 hrs · 26,263 cycles

STRINGER 26R IS CORRODED BETWEEN BS 333 - 349. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 34,455 hrs · 26,263 cycles

STRINGER SPLICE 26R IS CORRODED AT BS 333. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 34,455 hrs · 26,263 cycles

STRINGER SPLICE 26L IS CORRODED AT BS 333. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (BS 333-349) · airframe 34,455 hrs · 26,263 cycles

STRINGER 25R IS CORRODED BETWEEN BS 349 TO 333. REMOVED AND REPLACED IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: FRAME — CORRODED (BS 364) · airframe 34,455 hrs · 26,263 cycles

FRAME, BS 364 IS CORRODED BETWEEN STRINGERS 25R TO 26R. REPAIRED THE FRAME IAW SRM 53-21-23-201-008-A01.

Part: STRINGER — CORRODED (BS 333-349) · airframe 34,455 hrs · 26,263 cycles

STRINGER 26L IS CORRODED BETWEEN BS 349 TO 333. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 34,455 hrs · 26,263 cycles

STRINGER SPLICE 27 IS CORRODED AT BS 333. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 34,455 hrs · 26,263 cycles

SEAT TRACK SEGMENT NR 1 AT RBL 9 IS CORRODED BETWEEN BS 349 TO 485. REMOVED AND INSTALLED A FABRICATED SEAT TRACK IAW REO 670-53-00-343, REV M, AND REO 670-53-00-343, REV K.

Part: SEAT TRACK — CORRODED (BS 677-761.85) · corrosion level 2 · airframe 34,455 hrs · 26,263 cycles

RIGHT SIDE SEAT TRACK AT BS 677 TO 761.85, HAS SEVERAL AREAS OF CORROSION. REMOVED AND INSTALLED A FABRICATED SEAT TRACK IAW REO 670-53-00-343, REV M, AND REO 670-53-00-343, REV K,

Part: ANGLE — CORRODED (BS 280 FLOORBEAM) · corrosion level 2 · airframe 34,455 hrs · 26,263 cycles

FLOORBEAM ANGLE IS CORRODED AT BS 280. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 53-00-00-101-101-A01, 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01

Part: SEAT TRACK — CORRODED (BS 785-863) · corrosion level 2 · airframe 34,455 hrs · 26,263 cycles

LEFT SIDE SEAT TRACK AT BS 785 TO 863 HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-343, REV M, AND REO 670-53-00-343, REV K.

Part: STIFFENER — CRACKED (BS 202.75) · airframe 34,455 hrs · 26,263 cycles

FOUND THE BS 202.75 FORWARD SIDE BULKHEAD, RBL 30 STIFFENER HAS A CRACK INDICATION NOTED AT THE TOP PORTION INBOARD RADIUS APPROX. .150 INCH LONG AT 70% FSH. FAILED NDT INSPECTION. REPAIRED THE STIFFENER IAW SRM 53-11-10-201-005-A01.

Part: STIFFENER — CRACKED (BS 202.75) · airframe 34,455 hrs · 26,263 cycles

FOUND THE BS 202.75 FORWARD SIDE BULKHEAD, LBL 30 STIFFENER HAS A CRACK INDICATION NOTED AT THE TOP PORTION INBOARD RADIUS APPROX. .100 INCH LONG AT 60% FSH. FAILED NDT INSPECTION. REPAIRED THE STIFFENER IAW SRM 53-11-10-201-005-A01.

Part: SEAT TRACK — CORRODED (BS 785-863) · corrosion level 2 · airframe 34,455 hrs · 26,263 cycles

RIGHT SIDE SEAT TRACK AT BS 785 TO 863 HAS SEVERAL AREAS OF CORROSION. REMOVED AND INSTALLED A FABRICATED SEAT TRACK IAW REO 670-53-00-343, REV M, AND REO 670-53-00-343, REV K.

Part: STRINGER — CORRODED (BS 280-295) · corrosion level 2 · airframe 34,455 hrs · 26,263 cycles

DURING C CHECK, STRINGER 25R WAS FOUND CORRODED BETWEEN BS 280 AND 295. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 581-693) · corrosion level 2 · airframe 34,455 hrs · 26,263 cycles

CABIN SEAT TRACK, RBL 9, BS 581 - 693 IS CORRODED AT NUMEROUS LOCATIONS. REMOVED THE SEAT TRACK AND INSTALLED A FABRICATED SEAT TRACK IAW REO 670-53-00-343, REV M, AND REO 670-53-00-343, REV K.

Part: SEAT TRACK — CORRODED (BS 863-969) · corrosion level 2 · airframe 34,455 hrs · 26,263 cycles

LEFT SEAT TRACK BS 863 TO 969 HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-343, REV M, AND REO 670-53-00-343, REV K.

Part: SKIN — CHAFED (BS 977) · airframe 34,455 hrs · 26,263 cycles

FUSELAGE SKIN IS CHAFED AT PREVIOUS REPAIR AT BS 977, STRINGER 27. COMPLIED WITH EC/TC REO 670-53-00-290 01 AND REO 670-53-00-290, REV D. COMPLIED WITH EC/TC MODSUM IS670538200021 AND MODSUM IS670538200021 REVISION C.

Part: SEAT TRACK — CORRODED (BS 581-693) · corrosion level 2 · airframe 34,455 hrs · 26,263 cycles

CABIN LEFT SEAT TRACK BS 581 TO 693 IS CORRODED AT NUMEROUS LOCATIONS, LBL 9. REMOVED THE SEAT TRACK AND INSTALLED A FABRICATED SEAT TRACK IAW REO 670-53-00-343, REV M, AND EC/TC REO 670-53-00-343, REV K,

Part: WEB — CORRODED (BS 517-581) · airframe 34,455 hrs · 26,263 cycles

RIGHT FLOOR WEB CORRODED AT BS 517, 549 AND 581. REMOVED AND REPLACED THE WEB IAW AMM 21-35-01-400-801-A01, AND SRM 51-40-11-001-001-A01.

Part: FRAME — CORRODED (BS 310) · airframe 34,455 hrs · 26,263 cycles

FRAME BS 310, IS CORRODED BETWEEN STRINGERS 26R TO 26L. REPAIRED THE FRAME IAW REO 670-53-21-799.

Part: FRAME — CORRODED (BS 295) · airframe 34,455 hrs · 26,263 cycles

FRAME SECTOR BS 295 IS CORRODED BETWEEN STRINGERS 25L TO 25R. REPAIRED THE FRAME IAW REO 670-53-21-799, REV A, AND REO 670-53-21-799.

Part: STRINGER — CORRODED (BS 280-295) · corrosion level 2 · airframe 34,455 hrs · 26,263 cycles

STRINGER 24R IS CORRODED BETWEEN BS 280 AND 295. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 477-581) · airframe 34,455 hrs · 26,263 cycles

LEFT CABIN SEAT TRACK BS 477 - 581, LBL 9 HAS NUMEROUS AREAS OF CORROSION. REMOVED AND INSTALLED A FABRICATED SEAT TRACK IAW REO 670-53-00-343, REV M, AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 477-551) · airframe 34,455 hrs · 26,263 cycles

DURING C CHECK, THE CABIN SEAT TRACK, RBL 9, BS 477 - 581 FOUND CORRODED AT NUMEROUS LOCATIONS. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 501-597) · airframe 34,455 hrs · 26,263 cycles

DURING C CHECK, THE RIGHT SIDE SEAT TRACK BS 501 - 597 HAS SEVERAL AREAS OF CORROSION. REMOVED AND INSTALLED A FABRICATED SEAT TRACK IAW REO 670-53-00-343.

Part: BRACKET — CORRODED (BS 326) · airframe 34,455 hrs · 26,263 cycles

BRACKET ATTACHING TO STRINGER 19L IS CORRODED AT BS 326. REMOVED AND REPLACED BRACKETS AND THE STRINGER IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (BS 326) · airframe 34,455 hrs · 26,263 cycles

BRACKET ATTACHING TO STRINGER 19L IS CORRODED AT BS 326. REMOVED AND REPLACED THE BRACKET AND THE STRINGER IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 379-501) · airframe 34,455 hrs · 26,263 cycles

DURING C CHECK, THE RIGHT SIDE SEAT TRACK BS 379 - 501 HAS SEVERAL AREAS OF CORROSION. REMOVED AND INSTALLED A FABRICATED SEAT TRACK IAW REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 375-485) · airframe 24,455 hrs · 26,263 cycles

LEFT SEAT TRACK SEGMENT NR 1 AT LBL 9 IS CORRODED BETWEEN BS 375 TO 485. REMOVED AND REPLACED WITH A FABRICATED SEAT TRACK IAW REO 670-53-00-343, REV M, AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 565-677) · airframe 34,455 hrs · 26,263 cycles

DURING C CHECK, LEFT SIDE SEAT TRACK BS 565 - 677 HAS SEVERAL AREAS OF CORROSION. REMOVED AND INSTALLED A FABRICATED SEAT TRACK IAW REO 670-53-00-343.

Part: PLATE — CORRODED (BS 761-785) · airframe 34,455 hrs · 26,263 cycles

OVERWING EXIT STEP PLATE HAD CORROSION. REMOVED AND REPLACED THE PLATE IAW SRM 51-41-00-001-001-A01.

Part: FRAME — CORRODED (BS 319) · airframe 34,455 hrs · 26,263 cycles

FRAME SECTOR, BS 319 IS CORRODED BETWEEN STRINGERS 19L TO 21L. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-06-001-001-A01, 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.

Part: ANCHOR FITTING — CORRODED (ZONE 100) · airframe 34,455 hrs · 26,263 cycles

ENTRANCE STORAGE COMPARTMENT, OUTBOARD FORWARD, AND AFT ANCHOR FITTINGS ARE CORRODED. REMOVED AND REPLACED THE ANCHOR FITTINGS IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01.

Part: ANCHOR FITTING — CORRODED (G1 GALLEY) · airframe 34,455 hrs · 26,263 cycles

DURING C CHECK, THE G1 GALLEY FORWARD INBOARD ANCHOR FITTING IS CORRODED. REMOVED AND REPLACED THE ANCHOR FITTING IAW SRM 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 863-969) · airframe 34,455 hrs · 26,263 cycles

DURING C CHECK, THE RIGHT SIDE SEAT TRACK, BS 863 TO 969 HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK WITH A FABRICATED SEAT TRACK IAW REO 670-53-00-343, REV M, AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 379-501) · airframe 34,455 hrs · 26,263 cycles

DURING C CHECK, THE LEFT SIDE SEAT TRACK, BS 379 - 501 HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-343.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,153 hrs · 24,973 cycles

FLOORBEAM CORRODED AT FS 1031 LBL 9. REMOVED AND REPLACED FLOORBEAM AND COMPLIED WITH EC/TC REO 670-53-61-1325, GREO 670-53-00-0029 AND EO 700-53-10-00006.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 33,153 hrs · 24,973 cycles

DURING REPLACEMENT OF AFT CARGO DOOR SILL PLATE, FOUND MID AND AFT CHORD ATTACHMENTS CORRODED OUT OF LIMITS (INTER GRANULAR). REMOVED MIDDLE AND AFT CHORDS DUE TO CORROSION OUT OF LIMITS IAW SRM 51-42-06-001-001 A01. COMPLIED WITH EO 700-53-10-00009 REV. 0 DATED 2017-01-19 AS FOLLOWS: FABRICATED INNER CHORD IAW SRM 51-24-36 AND 51-24-21. REINSTALLED MIDDLE AND AFT CHORDS IAW SRM 51-42-06-001-001 A01.

Part: DOOR SILL — CORRODED (BS 1047) · airframe 33,153 hrs · 24,973 cycles

AFT CARGO DOOR SILL FOUND HEAVILY CORRODED UNDER PANEL 281JLF. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-13-001-001-A01, 51-42-06-001-001-A01 AND DRAWING MM670-35085.

Part: FLOOR SUPPORT — CORRODED (BS 1031-1051) · airframe 33,153 hrs · 24,973 cycles

FLOOR SUPPORT HAS CORROSION DAMAGE AT BS 1031, LBL 27. REMOVED AND REPLACED THE DAMAGED FLOOR SUPPORT, BS 1031-1051, IAW SRM 53-00-41-201-001-A01, AND EC/TC EO 700-53-10-00005.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,153 hrs · 24,973 cycles

FLOORBEAM HAS CORROSION AT FS 1031 RBL 9. REMOVED CORROSION AND REPAIRED FLOORBEAM BY COMPLYING WITH EC/TC REO 670-53-61-1326 AND REO 670-53-61-1326.

Part: SEAL — CORRODED (FUSELAGE) · airframe 33,153 hrs · 24,973 cycles

SERVICE DOOR LOWER STRIKER SEAL ANGLE CORRODED AROUND SCREW HOLES. REMOVED LOWER STRIKER SEAL, DRILLED UP AND INSTALLED NEW SERVICEABLE STRIKER SEAL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 33,153 hrs · 24,973 cycles

LOWER FWD SERVICE DOOR SURROUND FITTING BRACKET HAS CORROSION. REMOVED AND REPLACED FITTING BRACKET IAW SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 33,149 hrs · 24,971 cycles

DURING C CHECK, FOUND SEAT TRACK CORRODED AT BS 581 - 677, RBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49/-400-801-A17.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,153 hrs · 24,973 cycles

LT SIDE WALL SEAT RAIL IS CORRODED AT FS 485.00-565.0. REMOVED, FABRICATED AND REPLACED WITH NEW SERVICEABLE SIDE WALL SEAT RAIL AT FS 485-565 LT SIDE IAW AMM 53-00-49-000/400-801-A17, REO 670-53-00-343 AND EC/TC REO 670-53-00-343. THIS IS A MAJOR ALTERATION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 330,153 hrs · 24,973 cycles

RIGHT SIDE WALL SEAT RAIL CORRODED AT FS613.00-677.00. REMOVED, FABRICATED AND REPLACED WITH NEW SERVICEABLE SEAT RAIL AT FSFS613.00-677.00 RT SIDE IAW AMM 53-00-49-000/400-801-A17, REO 670-53-00-343 AND EC/TC REO 670-53-00-343. THIS IS A MAJOR ALTERATION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 330,153 hrs · 24,973 cycles

LEFT SIDE WALL SEAT RAIL CORRODED AT FS677.00-761.85. REMOVED, FABRICATED AND REPLACED WITH NEW SERVICEABLE SEAT RAIL AT FS677.00-761.85 LT SIDE IAW AMM 53-00-49-000/400-801-A17, REO 670-53-00-343 REV M AND EC/TC REO 670-53-00-343. THIS IS A MAJOR ALTERATION.

Part: INTERCOSTAL — CORRODED (BS 319) · airframe 33,153 hrs · 24,973 cycles

FWD SIDE OF BS 319, STRINGER 20R IS CORRODED. INTERCOSTAL FOUND TO BE OUT OF SERVICEABLE LIMITS. REMOVED OLD INTERCOSTAL, DRILLED UP NEW AND INSTALLED SERVICEABLE INTERCOSTAL @ FS 319.0 AND STR 20R IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND BOMBARDIER DRAWING SH670-31950 REV V. THIS IS A MAJOR REPAIR.

Part: FRAME — CORRODED (BS 349) · airframe 30,519 hrs · 22,860 cycles

FRAME AT BS 349.00 CORRODED. R & R FRAME AT FS349.00 FROM STR 24R TO STR 23L IAW SRM. PERFORMED A PRESSURIZATION LEAK CHECK OF THE FASTENERS COMMON TO THE FS 349 FRAME LOWER SECTOR REPLACEMENT IAW AMM. NO LEAKS NOTED PRESSURIZATION LEAK CHECK GOOD AT THIS TIME.

Part: FRAME — CORRODED (BS 319) · airframe 30,519 hrs · 22,860 cycles

CORROSION AT FS 319.70 FRAME BETWEEN STR 25L AND STR 26R. REPLACEMENT OF FS319.70 FRAME BETWEEN STR 25L AND STR 26R IAW SRM.

Part: PLATE — CORRODED (PAX DOOR) · airframe 30,519 hrs · 22,860 cycles

PAX DOOR SURROUND STRUCTURE KICKPLATE ANGLE IS CORRODED. R & R KICKPLATE ANGLE IAW SRM.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 27,735 hrs · 20,608 cycles

F/A FLASHLIGHT BATTERY INOPERATIVE. R & R F/A FLASHLIGHT BATTERY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,195 hrs · 20,174 cycles

EMERGENCY OVERHEAD LIGHT BETWEEN 1ST AND COACH CLASS IS BURNED OUT. REPLACED LAMP.

Part: PCB — FAILED (EMERGENCY LIGHTS) · airframe 27,011 hrs · 20,046 cycles

EMERGENCY LIGHTS STATUS MESSAGE ILLUMINATED. REPLACED PCB 4 IN JB11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,183 hrs · 19,420 cycles

CABIN SEAT RAIL AT RBL 9.0 FS354.0 TO FS477.4 IS CORRODED. C-CHECK REPLACED CABIN SEAT RAIL AT RBL 9.0 FS354.0 TO FS477.4 IAW AMM.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 26,183 hrs · 19,420 cycles

FS 280 CLIPS AT LBL 11 & RBL 11 ARE CORRODED BEYOND LIMITS. C-CHECK INSTALLED NEW GUSSETS AT LBL 11 & RBL 11 AT FS 280 IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,183 hrs · 19,420 cycles

RT SIDE SEAT RAIL FROM FS716 TO FS 767 IS CORRODED IN MULTIPLE AREAS. C-CHECK REPLACED RT SIDE SEAT RAIL FROM FS716 TO FS767 IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,183 hrs · 19,420 cycles

RT SIDE SEAT RAIL FROM FS699 TO FS716 IS CORRODED IN MULTIPLE AREAS. C-CHECK REPLACED RT SIDE SEAT RAIL FROM FS699 TO FS716 IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,183 hrs · 19,420 cycles

CABIN SEAT RAIL AT RBL 9.0 FS 485.0 TO FS 581.0 HAS SEVERAL AREAS OF CORROSION. C-CHECK REPAIRED RT CABIN SEAT TRACK AT FS 485 TO FS 581 LOCATION UE, STARTING THICKNESS .371, MATERIAL REMOVED .030, REMAINING THICKNESS .341, WITHIN LIMITS IAW REO.

Part: SILL — CORRODED (FUSELAGE) · airframe 26,183 hrs · 19,420 cycles

RT FLOOR SILL FROM FS 280- FS295 CORROSION BEYOND LIMITS. C-CHECK REPLACED FLOOR SILL, PN SH670-32172-9 PO T17117/8, FROM FS 280-319 IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,183 hrs · 19,420 cycles

CABIN SEAT RAIL AT LBL 9.0 FS 581.0 TO FS 693.0 HAS SEVERAL AREAS OF CORROSION. C-CHECK REPAIRED LT FLOOR SEAT TRACK AT FS 581 TO FS 693. LOCATION UE, STARTING THICKNESS .371", MATERIAL REMOVED .020", REMAINING THICKNESS .351", IAW REO.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 26,183 hrs · 19,420 cycles

RT FS 280.00 LOWER WEB CORRODED. C-CHECK REPLACED RT FS 280 BULKHEAD WEB IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,183 hrs · 19,420 cycles

RT SIDE SEAT RAIL FROM FS785 TO FS863 IS CORRODED IN MULTIPLE AREAS. C-CHECK BLENDED CORROSION ON RT SIDE SEAT RAIL FROM FS785 TO FS863 IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,183 hrs · 19,420 cycles

LT SIDE SEAT RAIL FROM FS 708 TO FS 761 IS CORRODED IN MULTIPLE AREAS. C-CHECK REPAIRED LT SIDE SEAT TRACK AT FS 708 TO FS 761 LOCATION UE, STARTING THICKNESS .371, MATERIAL REMOVED .006, REMAINING THICKNESS .365, WITHIN LIMITS IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,183 hrs · 19,420 cycles

RT SIDE SEAT RAIL FROM FS 379 TO FS 469 IS CORRODED IN MULTIPLE AREAS. C-CHECK BLENDED CORROSION ON RT SIDE SEAT RAIL FROM FS 379 TO FS 469 IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,183 hrs · 19,420 cycles

LT SIDE SEAT RAIL FROM FS 581 TO FS669 IS CORRODED IN MULTIPLE AREAS. C-CHECK REPAIRED LT SIDE SEAT TRACK AT FS 581 TO FS 669 LOCATION UE, STARTING THICKNESS .371, MATERIAL REMOVED .030, REMAINING THICKNESS .341, WITHIN LIMITS IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,183 hrs · 19,420 cycles

RT SIDE SEAT RAIL FROM FS 469 TO FS 581 IS CORRODED IN MULTIPLE AREAS. C-CHECK BLENDED CORROSION ON RT SIDE SEAT RAIL FROM FS 469 TO FS 581 IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,183 hrs · 19,420 cycles

RT SIDE SEAT RAIL FROM FS863 TO FS977 IS CORRODED IN MULTIPLE AREAS. C-CHECK BLENDED CORROSION ON RT SIDE SEAT RAIL FROM FS863 TO FS977 IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,183 hrs · 19,420 cycles

LT SIDE SEAT RAIL FROM FS 669 TO FS708 IS CORRODED IN MULTIPLE AREAS. C-CHECK REPAIRED LT SIDE SEAT TRACK AT FS 669 TO FS 708 LOCATION UE, STARTING THICKNESS .371, MATERIAL REMOVED .022, REMAINING THICKNESS .349, IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,183 hrs · 19,420 cycles

LT SIDE SEAT RAIL FROM FS 379 TO FS 485 IS CORRODED IN MULTIPLE AREAS. C-CHECK REPAIRED LT SIDE SEAT TRACK AT FS 379 TO FS 485 LOCATION UE, STARTING THICKNESS .371, MATERIAL REMOVED .022, REMAINING THICKNESS .349, WITHIN LIMITS IAW REO.

Part: WEB — CORRODED (FUSELAGE) · airframe 26,183 hrs · 19,420 cycles

LT FS 280.00 LOWER WEB CORRODED. C-CHECK REPAIRED LT FS 280 LOWER WEB IAW REO. FASTENER REMOVAL & INSTALLATION IAW REO, REPLACEMENT OF WEB & FABRICATION OF WEB SPLICE IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,183 hrs · 19,420 cycles

LT SIDE SEAT RAIL FROM FS 785 TO FS 863 IS CORRODED IN MULTIPLE AREAS. C-CHECK REPAIRED LT SIDE SEAT TRACK AT FS 785 TO FS 863 LOCATION UE, STARTING THICKNESS .371, MATERIAL REMOVED .020, REMAINING THICKNESS .351, WITHIN LIMITS IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,183 hrs · 19,420 cycles

LT SIDE SEAT RAIL FROM FS 485 TO FS 581 IS CORRODED IN MULTIPLE AREAS. C-CHECK REPAIRED LT SIDE SEAT TRACK AT FS 485 TO FS 581 LOCATION UE, STARTING THICKNESS .371, MATERIAL REMOVED .030, REMAINING THICKNESS .341, WITHIN LIMITS IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,183 hrs · 19,420 cycles

RT SIDE SEAT RAIL FROM FS 581 TO FS 669 IS CORRODED IN MULTIPLE AREAS. C-CHECK BLENDED CORROSION ON RT SIDE SEAT RAIL FROM FS 581 TO FS 669 IAW REO.

Part: CLAMP — OUT OF ADJUST (LT MLG) · airframe 26,183 hrs · 19,420 cycles

LT MLG STRUT HYD LINE UPPER BAND CLAMP BOLT IS GOUGING GEAR DOOR. C-CHECK ADJUSTED UPPER BAND CLAMP ON LT MLG STRUT HYD LINE, REPAIRED & BLENDED DAMAGE IAW AMM & REO.

Part: CABLE — FAILED (CABIN DOOR) · airframe 25,798 hrs · 19,147 cycles

MAIN CABIN DOOR STICKS WHEN OPENING. FLT#4652 REPLACED CABLE ON PAX DOOR IAW AMM. PN 601R318127-3

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,472 hrs · 18,899 cycles

EMERGENCY OVERHEAD LIGHT ABOVE ROW 15 IS BURNED OUT. FLT#4597 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,034 hrs · 18,525 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,665 hrs · 18,253 cycles

EMERGENCY OVERHEAD LIGHT NR 2 FAILS TO ILLUMINATE. (FLT 4563) RE-INSTALLED NR 2 EMERGENCY OVERHEAD LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,595 hrs · 17,457 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 17 IS OUT. (FLT 4650) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 22,628 hrs · 16,575 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN IS INOPERATIVE. (SERVICE) RELAMPED EMERGENCY EXIT SIGN.

Part: SHOULDER BELT — FAULTY (COCKPIT) · airframe 22,383 hrs · 16,396 cycles

FIRST OFFICER'S SHOULDER HARNESS LOCKING. (SERVICE) REPLACED THE FIRST OFFICER'S SHOULDER HARNESS IN REFERENCE TO AMM. P/N: 5001-1-021-2396SW

Part: SERVO — MALFUNCTIONED (AILERON) · airframe 21,639 hrs · 15,864 cycles

THE AILERONS SEEMED TO JAM. (FLT 4497) REPLACED AILERON SERVO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 22,653 hrs · 16,593 cycles

FS 280 FLOORBEAM CRACKED. (C-CHECK) REPLACED PER SRM.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 22,653 hrs · 16,593 cycles

FORWARD SIDE OF PASSENGER DOOR STAIR STRUCTURE HAS 2 CRACKS ON STEP CORNER RADIUS BETWEEN STEPS 1 AND 2. (C-CHECK) REPAIRED IN REFERENCE TO CRJ700 SRM.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 22,653 hrs · 16,593 cycles

AFT SIDE OF PASSENGER DOOR STAIR STRUCTURE HAS 3 CRACKS IN THE CORNER RADIUS BETWEEN STEP 1&2 AND 2&3. (C-CHECK) REPAIRED PER CRJ700 SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,146 hrs · 15,503 cycles

THE 2ND TO LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4441) RELAMPED EMERGENCY LIGHT.

Part: SPHERICAL BEARIN — DAMAGED (ENGINE MOUNT) · airframe 20,808 hrs · 15,262 cycles

FORWARD YOKE LINK SPHERICAL BEARING PITTED. (ENGINE CHANGE) REPLACED RIGHT ENGINE FORWARD YOKE LINK ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,431 hrs · 15,017 cycles

EMERGENCY EXIT LIGHT AT ROW 12 IS BURNED OUT. (FLT 4685) RELAMPED EMERGENCY LIGHT.

Part: WINDOW — CRACKED (ZONE 200) · airframe 19,316 hrs · 14,231 cycles

AFTER SHUTDOWN OF ENGINES AT COMPLETION OF FLIGHT, BEFORE DEPLANING OF PASSENGERS, A FIRE ERRUPTED FROM AREA NEAR FLOOD LIGHT AND CONTROL PANEL IN THE GLARESHIELD AREA OF THE COCKPIT. FLIGHT CREW PUT OUT FIRE WITH EXTINGUISHER LOCATED IN THE COCKPIT ON LT SIDE. PASSENGERS DEPLANED WITHOUT INCIDENT. CONFIRMED A FLUID LEAK FROM THE CAPTAIN'S SIDE WINDOW (LT). REPLACED THE LT SIDE WINDOW AND ALSO THE FLOOD LIGHT THAT CAUGHT FIRE. ALSO REPLACED FIRE EXTINGUISHER SINCE IT WAS USED. PILOTS SIDE WINDOW OP'S CHECKS & LEAK CHECKS GOOD. ACFT RETURNED TO SERVICE.

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 19,283 hrs · 14,211 cycles

SLATS FAIL, CAUTION MESSAGE CAME ON WHEN FLAPS WERE SELECTED. MDC SHOWS MECHANICAL JAM. LANDING UNEVENTFUL. CLEARED CAUTION IAW FIM TASK 27-81-00-810-802-A01, INTERGRATED MDC FAULT SLAT ACTUATOR SYS / MECHANICAL JAM, PERFORMED OPS TEST OF FLAPS AND SLATS IAW AMM TASK 27-50-00-710-801-A01, NO DEFECTS NOTED, ACFT OK FOR CONTINUED SERVICE. NO PARTS REPLACED.

Part: STRIKER — CORRODED (BS 311-349)

C-CHECK. DURING INSP, FOUND CORROSION ON THE SERVICE DOOR STRIKER SEAL SCREW HOLES FROM FS 311 TO 349. BLENDED AREAS OF CORROSION. BLENDED AREAS MEASURED OUT OF LIMITS. REPLACED SERVICE DOOR STRIKER SEAL IAW SRM 51-42-06-001-001-A01. DURING INSTALL, FOUND CORROSION ON 1 WEB FLOOR CHANNEL AND 3 LOWER ANGLES. BLENDED AREAS AND BLENDED AREAS FOUND WITHIN LIMITS. PRIMED AND PAINTED AREAS.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 18,356 hrs · 13,502 cycles

C-CHECK, THE PASSENGER DOOR SURROUND STRUCTURE MID CAP ANGLE HAS CORROSION AT FS 310 TO 349 AT WL 72. REMOVED MID CAP ANGLE TO ACCESS CORROSION AREAS. BLENDED CORROSION ON THE ANGLE AND FOUND SEVERAL AREAS OF .030 DEEP BLENDS AND ONE AREA WITH A BLEND OF 0.50 MATERIAL LOSS. ANGLE IS NOW BEYOND LIMITS IAW SRM 51-21-06-001-001-A01. REPLACED WITH NEW ANGLE IAW SRM 51-40-11-001-001-A01. ADJUSTED DOOR PROXIMITY SENSOR IAW AMM 52-70-04-820-A02.

Part: SKIN — DAMAGED (LT MLG DOOR) · airframe 18,356 hrs · 13,502 cycles

C-CHECK - LT MLG DOOR HAS 10 LOOSE RIVETS IN THE OUTER SKIN. REMOVED LT MLG DOOR IAWAMM 32-12-01-000-801. REMOVED 10 RIVETS IAW SRM 51-42-06-001-001-A01 AND INSTALLED NEW RIVETS IAW SRM 51-42-06-001-001-A01. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-21-06-001-001-A01 AND 51-25-16-001-001-A01. INSTALLED DOOR IAW AMM 32-12-01-400-802-A01.

Part: SKIN — DAMAGED (RT MLG DOOR) · airframe 18,356 hrs · 13,502 cycles

C-CHECK - RT MLG DOOR HAS 5 LOOSE RIVET IN OUTER SKIN. REMOVED RT MLG DOOR IAW AMM 32-12-01-000-801. REMOVED 5 RIVETS IAW SRM 51-42-06-001-001-A01 AND INSTALLED NEW RIVETS IAW SRM 51-42-06-001-001-A01. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-21-06-001-001-A01 AND 51-25-16-001-001-A01. INSTALLED RT MLG DOOR IAW AMM 32-12-01-400-802.

Part: FITTING — CHAFED (LT MLG) · airframe 18,356 hrs · 13,502 cycles

C CHECK - LT MLG SIDE STAY FITTING HAS SMALL CHAFE. BLENDED OUT CHAFE IAW REO 670-57-11-043. BLENDED AREA IS .050" BY .050" CORNER BLEND 1.00" LENGTH. PERFORMED ECI ON LT SIDE STAY FITTING BLEND AREA. NO CRACKS NOTED AT THIS TIME, IAW NDTM ECI 51-20-006-250-A01. WORK PERFORMED IAW REO 670-57-11-043. PERFORMED ROTO PEEN ON REWORKED AREA IAW REO 670-57-11-043.

Part: SEAT TRACK — CORRODED (BS 379-469) · airframe 18,356 hrs · 13,502 cycles

C-CHECK - RT SIDEWALL SEAT TRACK FS379-FS469 HAS CORROSION AND CHAFED. BLENDED AREAS OF CORROSION IAW SRM 51-12-00-001-001-A01 AND 51-21-06-001-001-A01. SEAT TRACK FOUND TO BE BEYOND LIMITS IAW REO 670-53-00-013. REMOVED SIDE SEAT TRACK IAW AMM 53-00-49-000-801-A03. RECEIVED NEW SEAT TRACK AND PREPPED IAW SRM 51-24-36-001-001-A01, 51-40-11-001-001-A01. TREATED CUTLINES AND HOLES IAW SRM 51-21-11-001-001-A01. INSTALLED NEW TRACK IAW AMM 53-00-49-400-801-A03.

Part: SILL — CORRODED (E/E BAY DOOR) · airframe 18,356 hrs · 13,502 cycles

C CHECK - DURING INSP, FOUND LIGHT CORROSION AROUND AVIONIC BAY DOOR SILL. REMOVED CORROSION AROUND AVIONICS DOOR SILL IAW REO 670-53-21-242 REV A. PERFORMED LPI IAW NDTM LPI 51-20-008-230-A01 NO CRACKS OR CORROSION FOUND AT THIS TIME. MEASURED BLENDS AND FOUND ALL TO BE WITHIN LIMITS OF REO 670-53-21-242. TREATED AND PRIMED IAW CRJ700 SRM 51-21-11-001-001-A01 AND 51-25-01-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 349-469) · airframe 18,356 hrs · 13,502 cycles

C-CHECK - RT FWD FLOOR SEAT TRACK HAS CORROSION. BLENDED AREAS OF CORROSION FROM FS 349-469 IAW SRM 51-12-00-001-001-A01 AND 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-000-801-A03.

Part: SILL — CORRODED (CARGO BAY) · airframe 18,356 hrs · 13,502 cycles

C-CHECK - AFT BAGGAGE BAY DOOR SILL HAS EVIDENCE OF CORROSION. BLENDED AREA OF CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED ECI IAW NDTM ECI IAW 51-20-006-250-A01, NO CRACKS NOTED AT THIS TIME. ALL BLENDS WITHIN LIMITS OF REO 670-53-61-654. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-01-001-001-A01 AND 51-25-16-001-001-A01.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 18,356 hrs · 13,502 cycles

C CHECK - AFT BAGGAGE BAY DOOR LOWER COATING SCRATCH AND CHAFED. BLENDED OUT SCRATCHES AND CHAFE IAW SRM 51-12-00-001-001-A01. PERFORMED ECI IAW NDTM ECI 51-20-006-250-A01 AND RE0670-53-61-196. BLENDS FOUND WITHIN LIMITS OF REO 670-53-61-196. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-01-001-001-A01 AND 51-25-16-001-001-A01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 18,356 hrs · 13,502 cycles

C-CHECK - CORROSION FOUND ON PAX DOOR KICK PLATE ANGLE. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01 AND FOUND TO BE OUT OF LIMITS IAW 51-21-23-001-A01, PG 101. REMOVED CORRODED KICK PLATE ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED HOLES IN NEW ANGLE AND INSTALLED ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A06. INSTALLED HI LITE FASTENERS IAW SRM 51-42-21-001-001-A01. TOP COATED FASTENERS AND APPLIED CORROSION INHIBITING COMPOUND AS REQUIRED IAW 51-25-16-001-001-A01 AND 51-21-11-001-001-A01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 18,356 hrs · 13,502 cycles

C-CHECK - DURING INSP FOUND CORROSION ON SERVICE DOOR MOUNTING ANGLE UNDER MID CAP. REMOVED GALLEY SERVICE DOOR FWD LOWER FITTINGS FOR ACCESS IAW SRM 51-41-02-001-001-A01. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THIIS .063", REMAINING MATERIAL IS .060" AND WITHIN LIMITS OF SRM 53-21-23-101-002-A01. TREATED, PRIMED AND PAINTED ANGLE IAW SRM 51-21-11-001-001-A01 AND 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. APPLIED CORROSION PREVENTATIVE COMPOUND IAW SRM 51-21-00-001-001-A01.

Part: TRACK — GOUGED (CARGO DOOR) · airframe 18,356 hrs · 13,502 cycles

C-CHECK - AFT BAGGAGE BAY DOOR FWD AND AFT TRACK DAMAGED. CLEANED GOUGED IAW SRM 51-12-00-001-001-A01. FWD TRACK GOUGE MEASURES 0.3"L 0.056"W .002"D ORIGINAL THICKNESS IS .100", NO DAMAGE ALLOWED ON AFT BAGGAGE BAY STRUCTURE IAW SRM 53-61-58-101-001-A01, SENT TO MFG ENGINEERING. COLD WORKED BOTH TRACKS IAW ENGINEERING BACK TO ORIGINAL CONTOUR IAW SRM 51-24-21-001-001-A01. BLENDED OUT ANY FURTHER GOUGES IAW SRM 51-12-00-001-001-A01. FWD TRACK MEASURES .8"L .4"W .015"D AFT TRACK MEASURES .8"L .5"W .003"D. PERFORMED LPI ON BLENDED AREA NO CRACKS FOUND AT THIS TIME IAW NDTM LPI 51-20-008-230-A01. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-01-001-01-A01 AND 51-25-16-001-001-A01.

Part: SUPPORT ANGLE — CORRODED (BS 280) · airframe 18,356 hrs · 13,502 cycles

C CHECK - DURING INSP, FOUND CORROSION ON CRAWL WAY SUPPORT ANGLE AT FS 280 FOR THE AVIONICS FLOOR. REMOVED THE CRAWL WAY SUPPORT ANGLE IAW SRM 51-42-00-001-001-A01. DRILLED UP NEW SUPPORT ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED NEW SUPPORT ANGLE SRM 51-42-06-001-001-A01, 51-42-10-001-001-A01 AND 51-42-21-001-001-A01. TOPCOATED AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-25-06-001-001-A01, 51-25-16-001-001-A01 AND 51-21-11-001-001-A01.

Part: BULKHEAD — CORRODED (BS 280) · airframe 18,356 hrs · 13,502 cycles

C-CHECK - LT SIDE, FS 280 BULKHEAD WEBBING SHOWS SIGNS OF CORROSION. BLENDED CORROSION, BLEND MEASURE .030 DEEP AND EXCEED LIMITS IAW REO 670-53-11-052. WEB IS CORRODED BEYOND LIMITS IAW REO 670-53-11-052. DRILLED OFF WEB IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND REO 670-53-11-052. LOCATED FASTENER HOLES IN NEW WEB IAW REO 670-53-11-052. INSTALLED NEW WEB IAW REO 670-53-11-052. TOPCOATED AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-25-16-001-001-A01.

Part: ATTACH ANGLE — CORRODED · airframe 18,356 hrs · 13,502 cycles

C-CHECK - DURING INSP FOUND CORROSION ON ATTACHMENT ANGLE 26R FWD OF THE AVIONICS DOOR. REMOVED ATTACHMENT ANGLE IAW SRM 51-42-06-001-001-A01, STARTED BLENDING CORROSION, AFTER BLENDING FOUND BLEND TO BE BEYOND LIMITS IAW SRM 53-21-23-101-003-A01. LOCATED FASTNER HOLES IN NEW ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED NEW ANGLE IAW SRM 51-42-21-001-001-A01. TOPCOATED IAW SRM 51-25-16-001-001-A01, APPLIED CORROSION INHIBITING COMPOUND IAW 51-21-11-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 18,356 hrs · 13,502 cycles

C-CHECK - COCKPIT FLOOR SUPPORT ANGLE ON FWD SIDE OF FS 280 BEAM SHOWS SIGNS OF CORROSION. REMOVED CORRODED FLOOR SUPPORT ANGLE FOR ACCESS IAW SRM 51-42-06-001-001-A01. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. ORIGINAL THICKNESS IS .063". BLENDED .015" MATERIAL FROM ANGLE MAXIMUM BLEND ALLOWED IS .048". FOUND BLEND TO BE OUT OF LIMITS IAW SRM 53-21-43-101-001-A01. LOCATED NEW FASTENER HOLES IN NEW ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED ANGLE IAW SRM 51-42-21-001-001-A01 AND 51-23-02-001-001-A01. TOPCOATED AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-25-16-001-001-A01 AND 51-21-11-001-001-A01.

Part: FRAME — CORRODED (BS 349) · airframe 18,356 hrs · 13,502 cycles

C-CHECK - DURING INSP, FOUND CORROSION ON FRAME AT FS349 ON ATTACH ANGLE LOCATED JUST FWD OF ATTACHMENT ANGLE 26R. REMOVED RIVETS FROM ATTACH ANGLE IAW SRM 51-42-06-001-001-A01. BLENDED CORRODED AREAS ON WEB AND ATTACH FLANGE IAW SRM 51-21-06-001-001-A01. BLENDED AREA MEASURES 2.5"W 0.9"L .002"D, ORIGINAL THICKNESS IS 0.50", REMAINING MATERIAL ON WEB IS 0.48", WITHIN LIMITS OF SRM 53-21-06-101-006-A01. BLEND ON ATTACH FLANGE MEASURES 3.0"W 0.6"L .002"D, ORIGINAL THICKNESS IS 0.50", REMAINING MATERIAL IS 0.48", WITHIN LIMITS OF SRM 53-21-06-101-006-A01. TREATED, PRIMED AND PAINTED BLENDED AREAS IAW SRM51-21-11-001-001-A01, 51-21-06-001-001-A01 AND 51-25-16-001-001-A01. INSTALLED SOLID FASTENERS IAW SRM 51-42-06-001-001-A01. TOPCOATED AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-25-16-001-001-A01 AND 51-21-11-001-001-A01.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 18,356 hrs · 13,502 cycles

C CHECK - DURING INSP FOUND CHAFE MARK AND DAMAGED FASTENER ON DOUBLER FOR CONNECTOR ADJACENT TO AFT POTABLE WATER FILL PORT. REMOVED DAMAGED FASTENER IAW SRM 51-42-06-001-001-A01. BLENDED CHAFE MARK, BLEND IS WITHIN LIMITS IAW SRM 53-00-01-101-001-A01. ETCHED, ALODINED, PRIMED AND INSTALLED NEW FASTENERS IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, 51-42-06-001-001-A01. TOPCOATED IAW SRM 51-25-16-001-001-A01. APPLIED CORROSION INHIBITING COMPOUND TO AFFECTED AREAS IAW SRM 51-21-11-001-001-A01. ALL BLENDS DONE IAW SRM 51-12-00-001-001-A01.

Part: STRUCTURE — CORRODED (BS 349 S26L) · airframe 18,356 hrs · 13,502 cycles

C-CHECK - DURING INSP, FOUND CORROSION ON 4 RIVETS NEXT TO STR 26L AND FRAME 349.00. REMOVED CORRODED RIVETS IAW SRM 51-42-06-001-001-A01. INSTALLED NEW FASTENERS IAW SRM 51-42-06-001-001-A01. TOPCOATED FASTENERS AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-25-16-001-001-A01 AND 51-21-11-001-001-A01.

Part: SKIN — CHAFED (E/E BAY DOOR) · airframe 18,356 hrs · 13,502 cycles

C-CHECK - DURING INSP, FOUND GOUGES ON OUTSIDE OF AVIONICS DOOR AFT OF DOOR. BLENDED CHAFE AREA ON DOOR SKIN IAW SRM 51-12-00-001-001-A01, CHAFE MEASURES 1.3"L 1.3"W AND .002"D. ORIGINAL THICKNESS IS .100 REMAINING MATERIAL IS .098, CHAFE WITHIN LIMITS OF SRM 53-00-01-001-A01. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-24-01-001-001-A01 AND 51-25-16-001-001-A01.

Part: STRUCTURE — CHAFED (RT WING TE FLAP) · airframe 18,356 hrs · 13,502 cycles

C-CHECK - FOUND CHAFE DAMAGE TO RT INBD FLAP LOCATED AROUND INBD FLAP HINGE ARM. BLENDED 2 CHAFED AREAS IAW SRM 51-12-00-001-001-A01. ORIGINAL SKIN THICKNESS IS .063, REMAINING MATERIAL IS.055 AND .057. CHAFES ARE WITHIN LIMITS IAW SRM 57-52-01-101-001-A01. R & R 4 DAMAGED RIVETS IAW SRM 51-42-13-001-001-A01. PREPPED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-01-001-001-A01 AND 51-25-16-001-001-A01.

Part: STRINGER — DAMAGED (S19R) · airframe 18,356 hrs · 13,502 cycles

C-CHECK - OVERSIZED RIVET FOUND AT S19R BETWEEN FS 517-533. REMOVED 1 RIVET IAW SRM 51-42-06-001-001-A01. PERFORMED ECI ON BLENDED AREA AROUND, REMOVED RIVET, NO CRACKS FOUND AT THIS TIME IAW NDTM ECI 51-20-006-250-A01. WET INSTALLED SOLID FASTENER IAW REO 670-53-31-170. TOPCOATED USING IAW SRM 51-25-16-001-001-A01 AND 51-21-11-001-001-A01.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 18,356 hrs · 13,502 cycles

C-CHECK - LT SIDE FS 280 BEAM CRACKED. REMOVED DRIP PANS AND INTERCOSTALS FOR AS REQUIRED IAW SRM 51-42-13-001-001-A01 AND 51-42-21-001-001-A01. DRILLED OFF CRACKED 280 BEAM IAW SRM 51-42-06-001-001-A01. ALL WORK IAW REO 670-53-11-047. PERFORMED CUT LINE ON NEW 280 BEAM IAW REO 670-53-11-052. PERFORMED LPI ON 280 BEAM CUTLINE, NO CRACKS FOUND AT THIS TIME IAW NDTM LPI 51-20-008-230-A01, REO 670-53-11-047. LOCATED FASTENER HOLES IAW REO670-53-11-047. INSTALLED NEW BEAM IAW REO 670-53-11-047. REINSTALLED INTERCOATALS AND DRIP PAN IAW SRM 51-42-21-001-001-A01 AND 51-42-13-001-001-A01. TOPCOATED AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-25-16-001-001-A01 AND 51-21-11-001-001-A01.

Part: PAINT — CHAFED (LT WING SLAT) · airframe 18,356 hrs · 13,502 cycles

C-CHECK - LT WING SLATS NR1 & 2 SHOW EVIDENCE OF CHAFING. BLENDED AREA FOUND TO BE PAINT ONLY, WITH NO MATERIAL LOSS ON LOWER T/E SKIN, WITHIN LIMITS OF SRM 57-42-01-101-001-A01. CHAFED AREA FOUND ON WING L/E (UNDER AREA OF SLAT) BLENDED AREA IAW SRM 51-12-00-001-001-A01. MEASURED CHAFE UNDER SLAT TO BE 0.6"L X 0.50"W X .002D, WITHIN LIMITS OF SRM 57-41-01-101-001-A01. TREATED PRIMED AND PAINTED AREAS IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, 51-25-26-001-001-A02.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 18,356 hrs · 13,502 cycles

C -CHECK - FWD BAG BAY DOOR FWD/AFT CORNERS OF INNER SKIN, INBD DAMAGED. REMOVED EDGE DAMAGE FROM FWD/AFT CORNERS OF INNER SKIN ON FWD BAGGAGE BAY DOOR. BLENDED DAMAGE IAW SRM 51-12-00-001-001-A01 AND FOUND TO BE IN LIMITS IAW SRM 53-00-00-101-001-A01. TREATED AREA IAW SRM 51-21-11-001-001-A01, PRIMED AREA IAW SRM 51-21-06-001-001-A01, TOPCOATED AREA IAW SRM 51-25-16-001-001-A01.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 18,356 hrs · 13,502 cycles

C-CHECK - GOUGE ON INBD FLAP AT TOP CTR OF FLAP BY L/E. BLENDED ON GOUGE ON UPPER SKIN OF RT INBD FLAP LOCATED BETWEEN 2 RIVETS AT FLS 84.20 IAW SRM 51-12-00-001-001-A01. SCRATCH MEASURES 0.5"L X .050W X .0025"D. GOUGE IS WITHIN LIMITS OF SRM 57-52-01-101-001-A01. TREATED, PRIMED AND PAINTED BLENDED ARE IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, 51-25-26-001-001-A01.

Part: IRU — FAILED (RIGHT) · airframe 18,532 hrs · 13,500 cycles

DURING CRUISE OVER C2Q, YD2 INOP, PITCH FEEL FAULT STATUS MESSAGE CAME ON AND AUTO PILOT DISENGAGED, RAN CHECKLIST AND WAS UNABLE TO RESTORE YD2 OR AUTOPILOT. CHECK LIST REQUIRES FLAPS 20 LANDING SO HAD TO DIVERT. F/O'S ATTITUDE AND HEADING MODES ALSO FAILED. LANDING UNEVENTFUL. MDC REPORTS IRS 2 FAILED/ WIRING IRS 2/ NO R-IRS-1 BUS OUTPUT. C/W FIM TASK 34-45-01-810-813-B01, R & R NR2 INERTIAL REF UNIT IAW MTC R344501. OPS CHECK GOOD, NO CAUTIONS OR FAULTS NOTED. PERFROMED OPS CHECK OF FLIGHT CONTROL COMPUTER IAW AMM TASK 22-11-00-710-802. OPS CHECK GOOD. ALL INDICATIONS NORMAL FOR F/O & CAPTAIN, NO CAUTIONS OR FAULT MESSAGES PRESENT. RETURNED TO SERVICE.

Part: ANGLE — CRACKED (BS 280) · airframe 16,320 hrs · 11,997 cycles

CRACKED ANGLE ATTACHED TO THE 280 BEAM FS 280.00 RBL26 / WL72.50. REMOVED ACCESS PANEL AND DRILLED ANGLE FROM 280 BULKHEAD AND ATTACH ANGLES ON FWD SIDE OF BULKHEAD. FABRICATED NEW ANGLE FROM .032 7075-T6 IAW TASK CARD R-53-501. HFEC INSP BEND LINE FOR CRACKS IAW NDTM PART 6, 53-00-000-250-A01, NO CRACKS NOTED. INSTALLED ANGLE REF SRM 51-42-06.

Part: WEB — CORRODED (BS 280) · airframe 16,320 hrs · 11,997 cycles

LOWER WEB ON RT SIDE AT 280 BEAM IS CORRODED. BLENDED AWAY CORROSION IAW REO 670-53-11-052. HFEC INSPECTED IAW NDTM PART 6, 53-00-000-250-A01. NO CRACKS NOTED. UT THICKNESS CHECK IAW NDTM PART 1, 51-20-004 HIGH: .040 LOW: .027. FOUND OUT OF LIMITS IAW REO 670-53-11-052. REMOVED LOWER WEB IAW REO 670-53-11-052 AND 670-53-11-047. LOCATED ALODINED AND PRIMED NEW WEB REF REO 670-53-11-052. INSTALLED WEB AND SURROUNDING STRUCTURE IAW REO 670-53-11-052 AND SRM 51-42-06, 51-42-13 AND 51-42-21.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 16,320 hrs · 11,997 cycles

CORROSION ON TOP OF FS 280 BEAM AT RBL 10.0 TO 12.0. REMOVED FS 280 BEAM IAW REO 670-53-11-047. LOCATED, ALODINED AND PRIMED NEW REPLACEMENT RT FS 280 BEAM IAW REO 670-53-11-047 AND SRM 51-42-06, 51-42-13, AND 51-40-11. INSTALLED BEAM IAW REO-670-53-11-047 AND SRM 51-42-06, 51-42-13, 51-40-11 AND 51-42-21.

Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 16,262 hrs · 11,958 cycles

DURING GEAR RETRACTION THE NOSE GEAR INDICATOR REMAINED RED. MASTER WARNING "GEAR DISAGREE" CAME ON. RETURNED TO FIELD LANDING WEIGHT 67800LBS, RATE OF DESCENT AT TOUCHDOWN WAS 100 FPM. ADJUSTED NLG UP AND LOCKED SENSOR, PX22 IAW TASK 32-61-05-820-804. PERFORMED GEAR OPERATIONAL TEST IAW 32-30-00-710-801. OPS TEST GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 14,381 hrs · 10,498 cycles

SEA - GLD UNSAFE CAUTION MESSAGE AT TAKEOFF. ABORTED TAKEOFF AND RETURNED TO THE GATE. C/W FIM TASK 27-64-00-810-803-A01. INTERROGATED MDC FOR FAULTS, NONE FOUND. C/W OPS TEST OF THE GROUND LIFT DUMPING MANUAL ARM AND DISARM IAW AMM TASK 27-61-00-710-801-A02. OPS TEST IS GOOD. NO FURTHER DEFECTS NOTED. ACFT IS OK FOR CONTINUED SERVICE. NO PARTS REPLACED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 13,899 hrs · 10,058 cycles

PDX - C4 - UPPER TCAS ANTENNA HAS MINOR SURFACE CORROSION ON FUSELAGE SKIN AROUND NUTPLATE. BLENDED MINOR CORROSION ON FUSELAGE SKIN IAW SRM 51-12-00. BLENDED AREAS ARE WITHIN LIMITS IAW SRM 53-00-01 PG 101. SKIN IS .061", MAX REWORKED MATERIAL LOSS IS .003". FPI BLENDED AREAS FOR CRACKS IAW CRJ 700 NDTM PART 1, 51-20-008, NO CRACKS NOTED. MAPPED FOR ENGINEERING. BLEND WAS FOUND TO BE IN A "NO CHANGE ALLOWED" AREA, AS STATED IN SRM 53-21-01-101-003-AAI. BLEND WAS FOUND TO COMPLY WITH REO 670-53-21-418 STEP 1. REPLACED 2 FASTENERS AS PER STEP 2, AND FINISHED REWORKED AREA IAW STEP 4.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,899 hrs · 10,058 cycles

PDX - C4 - CRACK ON BEAM AT FS 280 ABOVE TEE FITTING IN THE UPPER RADIUS AT LBL 9.0. REMOVED LT 280 BEAM, LOCATED AND DRILLED NEW LT SECTION OF BEAM. INSTALLED BEAM IAW SRM 51-42-06 AND REO 670-53-11-265. INSTALLED DRIP TRAY AND INTERCOSTALS IAW SRM 51-42-06.

Part: SHUTOFF VALVE — FAILED (LT A/C PACK) · airframe 11,294 hrs · 8,007 cycles

RNO - FLIGHT 9851 - WITH WING AI ON AND COWL A/I ON RECEIVED A LEFT BLEED MASTER CAUTION. LEFT PACK WAS CYCLING ON AND OFF. RETURNED TO THE GATE. MAINTENANCE REPLACED THE NR 1 ENGINE PRSOV. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: STICK SHAKER — MALFUNCTIONED · airframe 11,174 hrs · 7,923 cycles

BOI - FLIGHT 2572 - APPROACHING TOP OF CLIMB RECEIVED A STALL WARNING CAUTION MESSAGE. TURNED STALL PUSHER SWITCH OFF PER CHECKLIST. MAINTENANCE FOUND ON THE MDC, NO POWER TO THE STICK PUSHER. CYCLED THE CIRCUIT BREAKER AND PERFORMED A OPERATIONAL TEST. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CONTROL UNIT — MALFUNCTIONED (FIRE DETECTION) · airframe 10,911 hrs · 7,742 cycles

DEN - FLIGHT 4324 - RECEIVED A FIRE SYSTEM FAULT MESSAGE. MAINTENANCE PLACED THE SYSTEM ON MEL 26-00-1. AIRCRAFT RETURNED TO SERVICE. REPLACED THE FIDEEX CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: HANDLE — CRACKED (E/E BAY DOOR) · airframe 10,621 hrs · 7,532 cycles

PDX - AVIONICS BAY DOOR HANDLE CRACKED. MAINTENANCE REPLACED THE HANDLE ASSEMBLY. OPERATIONAL CHECKS GOOD.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 9,940 hrs · 7,031 cycles

DEN - RECEIVED A INBOARD SPOILER CAUTION ON TAXI OUT. RETURNED TO THE GATE. MAINTENANCE REPLACED THE RIGHT INBOARD PCU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (WINDSHEAR WARN) · airframe 9,868 hrs · 6,975 cycles

DEN FLIGHT NR 4334, AFTER TAKEOFF RECEIVED A RED WINDSHEAR WARNING. AFTER RECOVERY RECEIVED "R ITT EXCEED B" MESSAGE. WENT TO "MAX THRUST" APPROXIMATELY 5-10 SECONDS. MAINTENANCE REQUESTED A RETURN TO FIELD. INTERROGATED MDC AND FOUND APR DID NOT EXCEED 5 MINUTES. NO PARTS REPLACED. AIRCRAFT K FOR CONTINUED SERVICE PER AMM 71-00-00-866-801-AA1, PAGE 248.

Part: WIRE HARNESS — MALFUNCTIONED (CARGO DOOR) · airframe 9,659 hrs · 6,820 cycles

DEN - FLIGHT 4277, RECEIVED A PROXI FAULT SYSTEM 2 MESSAGE FOR THE FORWARD CARGO DOOR. RETURNED TO THE GATE, AND MAINTENANCE PLACED THE SYSTEM ON MEL 52-70-4A. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 9,597 hrs · 6,773 cycles

OKC - MID CABIN EMERGENCY EXIT SIGN LIGHTS ARE INOP. REPLACED BATTERY PACK EPSU IAW CRJ-700 33-51-17-000-801-A01. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PCU — FAILED (SPOILERS) · airframe 9,576 hrs · 6,757 cycles

DEN - RECEIVED A INBOARD FLIGHT SPOILERS AND INBOARD SPOILERONS CAUTION MESSAGE WHEN FLIGHT SPOILERS WERE DEPLOYED IN FLIGHT. ON LANDING AFTER TOUCHDOWN, THE RIGHT INBOARD SPOILER DEPLOYED BUT THE LEFT DID NOT. MAINTENANCE INTERROGATED THE MDC AND FOUND A L IB MFS PCU FAILED PCU JAM MESSAGE. CLEARED BY SERVICE LETTER CRJ-700-SL-27-052D. NO OTHER FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: UNKNOWN — UNKNOWN · airframe 9,432 hrs · 6,658 cycles

DEN - ON TAXI OUT, RECEIVED A "L FADEC" CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE PERFORMED A ENGINE RUN AND FOUND NO DEFECTS. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: BOLT — CHAFED (HORIZONTAL STAB) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND HORIZONTAL STABILIZER MOUNT BOLT ANTI-ROTATION TAB ON RIGHT SIDE CHAFED AT AFT END. REPAIRED IAW REO670-55-11-064 AND SRM 51-21-16.

Part: SILL — DAMAGED (CARGO DOORWAY) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - LIGHT CHAFFING ON AFT CARGO DOOR FORWARD UPPER AND LOWER SILL AREAS ON AIRCRAFT WITH SEVERAL LOCATIONS OF MINOR NICKS, SCRATCHES, AND MISSING PAINT FOUND AROUND SILL. REPAIRED IAW SRM 53-00-01, 53-61-23, AND REO670-53-61-308.

Part: SKIN — CORRODED (E/E BAY DOOR) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND MAIN AVIONICS COMPARTMENT DOOR CUTOUT INTERNAL LOWER SKIN HAS LIGHT SURFACE CORROSION AROUND SKIN TO DOOR CONTACTING SURFACE. REPAIRED IAW SRM 51-21-06, 53-21-01, REO670-53-21-250, AND SRM 51-25-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,815 hrs · 6,335 cycles

C2 PDX - FLIGHT COMPARTMENT FLOOR PANEL 221ALF, AFT SUPPORT IS CORRODED ON TOP FLANGE UPPER SURFACE. REPAIRED IAW REF NON ROUTINE 00164 FOR REPLACEMENT OF FLOOR SUPPORT.

Part: SKIN — CORRODED (FUSELAGE) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - LIGHT FRETTING CORROSION ON FUSELAGE SKIN AT MOUNTING SURFACE FOR NR 2 VHF ANTENNA. REPAIRED IAW SRM 51-21-11 AND 51-21-01.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 9,815 hrs · 6,335 cycles

C2 PDX - EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON LEFT SIDE OF FUSELAGE AT FS 288 AND STRINGER 26L. REPAIRED IAW SRM 53-21-01, 51-21-06, AND 51-25-16.

Part: ATTACH FITTING — CRACKED (SEAT TRACK) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND RIGHT INBOARD CABIN SEAT RAIL ATTACH FITTING TO FS 280 BEAM IS CRACKED. REPAIRED IAW SRM 51-42-00, 51-40-11.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FLIGHT COMPARTMENT FLOOR PANEL 221ALF, AFT SUPPORT, APPEARS CRACKED AT 2 PLACES. VIEWED FROM FORWARD SIDE, ADJACENT TO CABIN SEAT TRACK. REPAIRED IAW SRM 51-42-00, 51-40-11.

Part: BOLT — CHAFED (HORIZONTAL STAB) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND HORIZONTAL STABILIZER MOUNT BOLT ANTI-ROTATION TAB ON LEFT HAND SIDE IS CHAFED AT BOTH ENDS. REPAIRED IAW REO670-55-11-064 AND SRM 51-21-16.

Part: FLOORBEAM — DAMAGED (BS 280) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - DUE TO NUMEROUS DISCREPANCIES, FS 280 FLOORBEAM REQUIRES REPLACEMENT, REF NON ROUTINE 00162, NONROUTINE 00163 AND NON ROUTINE 00171. REPLACED IAW SRM 51-42-00, 51-40-11, AND REO670-53-11-047.

Part: RIVET — DAMAGED (FUSLEAGE) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - REPLACE BURNED RIVET AT FS 437 10" BELOW WL 79.5, RHS. REPAIRED IAW SRM 51-42-06, 51-21-16, AND REO670-53-21-248.

Part: SEAT TRACK — CRACKED (FS 280) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND LEFT INBOARD CABIN SEAT RAIL ATTACH FITTING TO FS 280 BEAM IS CRACKED. REPAIRED IAW REO670-53-11-047 AND SRM 51-42-00.

Part: DOOR FRAME — DAMAGED (BS 292) · airframe 8,915 hrs · 6,355 cycles

C2 PDX - REPLACE BURNED RIVET LOCATED AT FS 292.2 12" BELOW TOP OF MAIN CABIN DOOR FRAME. REPAIRED IAW SRM 51-42-06 AND 53-21-01.

Part: SKIN — DAMAGED (BS 534 S23R) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 534 AND STRINGER 23R. REPAIRED IAW SRM 51-42-06, 53-00-01, 51-25-01.

Part: WEB — CORRODED (BS 280) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND VERTICAL WEB IS CORRODED AT FS 280 BEAM RBL 14 JUST ABOVE CABIN FLOOR LEVEL. REPAIRED IAW SRM 51-40-11, REO670-53-11-052.

Part: SKIN — LIGHTNING STRIKE (FUSLEAGE) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD JUST BELOW ADG DOOR AT FS 170. REPAIRED IAW SRM 51-42-06, 51-25-01, AND 51-40-00.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - VERTICAL WEB IS CORRODED AT STATION 280 FLOORBEAM, LBL12-LBL16 AND LBL30. REPAIRED IAW REO670-53-11-052, AND SRM 51-40-11, 51-40-02.

Part: SKIN — DAMAGED (BS 449 S24R) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 499 AND STRINGER 24R. REPAIRED IAW SRM 53-00-01, 51-40-00, AND 51-25-01.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 407 AND STRINGER 20R. REPAIRED IAW SRM 51-2-06, 51-25-01.

Part: SKIN — CHAFED (AILERONS) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - LOWER LEADING EDGE SKIN OF RIGHT AILERON IS CHAFED ALONG ENTIRE LENGTH BY THE WING TRAIL EDGE PANELS. REPAIRED IAW SRM 51-42-06 AND 51-42-21.

Part: ANGLE — CRACKED (BS 280) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND LEFT LOWER 90 DEGREE VERTICAL ANGLE IS CRACKED AT BOTTOM END THROUGH RIVET HOLES AT FS 280, LBL 25.5. REPAIRED IAW SRM 51-42-06 AND 51-42-00.

Part: SKIN — DAMAGED (BS 573 S17L) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVETHEAD ON LEFT SIDE OF FUSELAGE ABOVE FORWARD CARGO DOOR AT FS 573 AND STRINGER 17L. REPAIRED IAW SRM 53-00-01, 51-21-11, AND 51-25-01.

Part: SEAT TRACK — GOUGED (BS 510) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - RIGHT INBOARD SEAT TRACK HAS A GOUGE INSIDE THE TRACK WITH SURFACE CORROSION INSIDE AND ON TOP OF THE TRACK AT FS 510. REPAIRED IAW REO670-53-00-013.

Part: SKIN — DAMAGED (BS 942) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 942 AND STRINGER 17R. REPAIRED IAW SRM 51-42-06, 53-00-01, 51-21-11, AND 51-25-01.

Part: SKIN — DAMAGED (BS 525 S19R) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 525 AND STRINGER 19R. REPAIRED IAW SRM 53-00-01, 51-42-06, 51-25-01.

Part: SKIN — DAMAGED (BS 265) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD AT FS 265 STRINGER 23R. REPAIRED IAW SRM 51-42-06, 53-00-01, 51-21-11, 51-25-01.

Part: SKIN — DAMAGED (BS 547 S20R) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 547 AND STRINGER 20R. REPAIRED IAW SRM 51-42-06, 53-00-01, 51-25-01.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FORWARD FUSELAGE AT FS 243 AND STRINGER 22R. REPAIRED IAW SRM 51-42-06, 51-40-00, AND 51-25-01.

Part: SKIN — DAMAGED (BS 600 S17R) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 600 AND STRINGER 17R. REPAIRED IAW SRM 51-42-06, 53-00-01, AND 51-25-01.

Part: STRUCTURE — DAMAGED (BS 273 S22R) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD AT FS 273 STRINGER 22R. REPAIRED IAW SRM 51-42-06, 53-00-01, 51-21-11, 51-25-01.

Part: SEAT TRACK — GOUGED (BS 960) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND LEFT SIDE UPPER SEAT RAIL GOUGED AT FS 960.00. REPAIRED IAW REO670-53-00-013.

Part: SKIN — DAMAGED (BS 259) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD AT FS 259 STRINGER 23. REPAIRED IAW SRM 51-42-06, 53-00-01, 51-21-11, AND 51-25-01.

Part: SKIN — DAMAGED (BS 534 S19R) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 534 AND STRINGER 19R. REPAIRED IAW SRM 53-00-01, 51-42-06, 51-25-01.

Part: SKIN — DAMAGED (BS 265) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD AT FS 265 STRINGER 22R. REPAIRED IAW SRM 51-42-06, 53-00-01, 51-21-11, 51-25-01.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD JUST LEFT OF LOWER RED ANTI COLLISION LIGHT AT FS 486. REPAIRED IAW SRM 53-00-01, AND 51-21-11, 51-25-01.

Part: SKIN — DAMAGED (BS 492 S19R) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 492 AND STRINGER 19R. REPAIRED IAW SRM 51-42-06, 51-40-00, AND 51-25-01.

Part: SKIN — DAMAGED (BS 309 S22R) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD RIGHT SIDE OF FORWARD FUSELAGE AT FS 309 AND STRINGER 22R. REPAIRED IAW SRM 53-00-01, 53-21-01, AND 51-21-11.

Part: SEAT TRACK — CORRODED (BS 320-477) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND RIGHT INBOARD CABIN SEAT TRACK IS CORRODED BETWEEN FS 320 AND FS 477. REPAIRED IAW CRJ TASK 53-00-49-000-801-A03.

Part: SKIN — DAMAGED (BS 956 S17R) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 956 AND STRINGER 17R. REPAIRED IAW SRM 53-00-01, 51-42-06, 53-51-03, AND 51-25-01.

Part: SKIN — DAMAGED (BS 565) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 565 AND BETWEEN STRINGER 23R AND STRINGER 24R. REPAIRED IAW SRM 51-42-06, 53-00-01, 51-25-01, AND 51-21-11.

Part: SKIN — LIGHTNING STRIKE (FUSLEAGE) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 316 AND STRINGER 22R. REPAIRED IAW SRM 51-40-00, 51-42-06, AND 51-25-01.

Part: SKIN — DAMAGED (BS 584) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 584 AND BETWEEN STRINGER 22R AND STRINGER 23R. REPAIRED IAW SRM 51-42-06, 53-00-01, 51-21-11, AND 51-25-01.

Part: SEAT TRACK — CORRODED (BS 394-477) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND LEFT INBOARD CABIN SEAT TRACK HAS LIGHT CORROSION AT MULTIPLE LOCATIONS BETWEEN FS 394 AND FS 477. REPAIRED IAW REO670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 540) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - FOUND RIGHT INBOARD SEAT TRACK HAS SURFACE CORROSION INSIDE AND ON TOP OF THE TRACK AT FS 540. REPAIRED IAW REO670-53-00-013.

Part: RIVET — BURNED (BS 469) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - REPLACE BURNED RIVET LOCATED 10" AFT OF FS 469.6 6" BELOW WL 79.5 RTS. REPAIRED IAW SRM 51-42-06.

Part: RIVET — DAMAGED (FUSLEAGE) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - REPLACE BURNED RIVET AT FS 412.8 12" BELOW WL 79.5 RHS. REPAIRED IAW SRM 51-42-06.

Part: RIVET — BURNED (BS 469) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - REPLACE BURNED RIVET LOCATED 11" AFT OF FS 469.6 6" BELOW WL 79.5 RTS. REPAIRED IAW SRM 51-42-06.

Part: RIVET — DAMAGED (FUSELAGE) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - REPLACE BURNED RIVET AT FS 417.3 11" BELOW WL 79.5, RHS. REPAIRED IAW SRM 51-42-06.

Part: RIVET — DAMAGED (FUSLEAGE) · airframe 8,915 hrs · 6,335 cycles

C2 PDX - REPLACE BURNED RIVET AT FS 349. 13" BELOW TOP OF MAIN CABIN DOOR, AFT OF MAIN CABIN DOOR FRAME. REPAIRED IAW SRM 51-42-06.

Part: UNKNOWN — ODOR (CABIN) · airframe 8,837 hrs · 6,287 cycles

FAT- FLIGHT 4299. DURING CLIMB RECEIVED A LAV SMOKE WARNING MESSAGE. HAPPENED TWO TIMES, FOR 30 SECONDS EACH. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. NO SMOKE OR FIRE NOTICED. MAINTENANCE FOUND THE SOURCE TO BE THE APU. PLACED THE APU ON MEL 49-10-1B. RAN ENGINES FOR TWO HOURS AT ELEVATED BLEED TEMPS TO CLEAR SMELL. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 8,821 hrs · 6,276 cycles

OMA - FLIGHT 4435, RECEIVED A LAV SMOKE/FIRE WARNING MESSAGE. NO FIRE NOTED AND NO SMELL NOTED. MAINTENANCE PERFORMED A OPERATIONAL CHECK WITH NO DEFECTS, NO SMELL NOTED. PLACED SMOKE DETECTOR ON MEL. REPLACED SMOKE DETECTOR. AIRCRAFT RETURNED TO SERVICE.

Part: IGNITION LEAD — DAMAGED (RT ENGINE) · airframe 8,190 hrs · 5,844 cycles

RECEIVED A RT IGNITION FAULT STATUS MESSAGE AFTER ENGINE START. RETURNED TO THE GATE. MAINTENANCE PLACED ON MEL 74-11-1A. AIRCRAFT RETURNED TO SERVICE. MEL CLEARED BY REPLACING THE IGNITION (A) LEAD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CAUTION MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 8,182 hrs · 5,837 cycles

AFTER PUSHBACK RECEIVED A RT ENGINE BLEED CAUTION. RETURNED TO THE GATE. MAINTENANCE FOUND NO FAULTS IN THE MDC. FAULT HISTORY SHOWED A RT PRESS VALVE NO CONTROL/POSITION DISAGREE MESSAGE IN FAULT HISTORY. COMPLIED WITH FIM TASK 75-30-00-810-A01 AND PERFORMED OPERATIONAL TEST OF THE PRSOV IAW 36-12-01-710-801. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DCU — FAILED · airframe 7,988 hrs · 5,704 cycles

OMA - FLIGHT 4431, AFTER TAKEOFF HAD A ELEVATOR SPLIT CAUTION MESSAGE. RETURNED TO OMA AND ACCOMPLISHED A UNEVENTFUL LANDING. AIRCRAFT FERRIED TO DENVER FOR REPAIRS. IN DENVER, MAINTENANCE REPLACED THE DATA CONCENTRATOR UNIT (DCU). OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 7,774 hrs · 5,550 cycles

TUL- ON FLIGHT 4331, THE AFT CARGO DOOR MASTER CAUTION ILLUMINATED ALONG WITH A PROX SYSTEM 2 FAULT MESSAGE. AIRCRAFT RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE FOUND THE CARGO DOOR HANDLE NOT STOWED. RESECURED HANDLE AND OPERATED DOOR PER AMM TASK 52-31-03-710-801-A01. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SENSOR — MALFUNCTIONED (BRAKE TEMP) · airframe 7,650 hrs · 5,462 cycles

DEN - AFTER TAKEOFF FOR FLIGHT 4342 (DEN-YYC) RECEIVED A BRAKE OVERHEAT WARNING CLIMBING THROUGH 17,000 FEET. PER THE CHECKLIST, LOWERED THE LANDING GEAR AND MESSAGE WENT OUT. RESET THE BRAKE TEMPERATURE MONITORING SYSTEM. NR 4 BRAKE READ 17 AT HOTTEST POINT. RETURNED TO THE FIELD AND ACCOMPLISHED AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED LANDING GEAR AND WHEELS AND BRAKES. THERE WERE NO SIGNS OF OVERHEATING. AS A PRECAUTION, REPLACED THE NR 4 BRAKE, WHEEL, AND TEMPERATURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 7,274 hrs · 5,181 cycles

YYC - ON FLIGHT 4345 (YYC-DEN) DURING CLIMB RECEIVED A DCU 1 STATUS MESSAGE. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE COMPLIED WITH FIM TASK 31-41-00-810-804-A01. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 7,268 hrs · 5,176 cycles

OKC - FLIGHT 4184, RETURNED TO THE GATE AFTER A APU AUTO SHUTDOWN DURING ENGINE START. MAINTENANCE PERFORMED OPERATIONAL CHECK OF APU AND FOUND NO FAULTS. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: ODOR — DETECTED (CABIN) · airframe 7,249 hrs · 5,162 cycles

DEN - ON TAXI OUT FOR FLIGHT 4331, FLIGHT ATTENDANT REPORTED A EXTREME BURNING SMELL (RUBBER) THAT WAS CAUSING PEOPLE'S EYES TO WATER. RETURNED TO THE GATE. MAINTENANCE INSPECTED THE COMPUTERS IN THE AVIONICS BAY AND PERFORMED A ENGINE RUN EQUAL TO CONDITIONS AT TAXI OUT. NO DEFECTS OR ODORS WERE FOUND. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CONTROL VALVE — INOPERATIVE (LT A/C PACK FLOW) · airframe 6,371 hrs · 4,560 cycles

DEN - ON FLIGHT 4438, RETURNED TO GATE. LEFT PACK CAUTION MESSAGE. MAINTENANCE REMOVED AND REPLACED FLOW CONTROL VALVE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (COCKPIT) · airframe 5,963 hrs · 4,283 cycles

MCI - ON FLT 4197 VISIBLE SPARKS/FLAMES FROM ABOVE F/O'S GASPER VENT. DIVERTED FLT TO MCI AND ACCOMPLISHED UNEVENTFUL LANDING. NO FURTHER FIRE AND FIRE EXTINGUISHERS NOT USED. FOUND F/O FLOODLIGHT COMMON TO F/O LIGHTING CONTROL PANEL BURNED. ACCESSED AND INSPECTED WIRE RUNS COMMON TO LIGHT CIRCUIT. NO DAMAGE OR FOULING NOTED FROM LIGHT DISCONNECT PLUG TO C/B. FOUND BROKEN, ONE WIRE ON LIGHT ASSY. REMOVED FLOODLIGHT AND CAPPED DISCONNECT PLUG AND SECURED. OPS TEST OF F/O LIGHTING GOOD. PLACED F/O FLOODLIGHT ON MEL 33-11-1, RSI #356338. C/B U2 (INST FLOOD LTS) OPENED AND COLLARED. A/C RETURNED TO SERVICE. INSTALLED NEW FEEDLIGHT ASSY AT F/O LIGHTING CONTROL PANEL IAW AMM 33-11-01-400-801-A01 OPS CHECK

Part: LEVER — MALFUNCTIONED (MLG) · airframe 5,593 hrs · 4,041 cycles

DEN - AFTER LANDING GEAR EXTENSION PROX SYSTEM CAUTION MESSAGE RECEIVED. ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE INTERROGATED MDC AND FOUND L/G SELECTOR VALVE RETRACT SOLENOID LOAD ON. REMOVED/REPLACED L/G CONTROL PANEL LEVER IAW CRJ AMM 32-31-01-000/400-802-A01. PERFORMED L/G EXTENSION/RETRACTION SYSTEM CHECK IAW CRJ AMM 32-30-00-710-801. C/W QX TASK CARD R071101. ALL OPS CHECKS SATISFACTORY AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (ZONE 200) · airframe 17,682 hrs · 25,480 cycles

BOI - ON FLIGHT 4276, RETURNED TO GATE, ANTI SKID INBOARD CAUTION MESSAGE. REMOVED AND REPLACED PARKING BRAKE SHUTOFF VALVE. OPERATIONAL CHECK GOOD, MESSAGE CLEARED. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — WORN (RT WING AILERON) · airframe 4,002 hrs · 2,925 cycles

RT WING AILERON UPPER AND LOWER SKIN LEADING EDGE HAS WEAR MARKS. REPAIRED IAW CRJ 700 SRM 57-61-10-101-001-A01 AND SRM 57-52-32-400-811-A01.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 4,002 hrs · 2,925 cycles

FUSELAGE SKIN PANEL, SKIN DAMAGED AT STATION 421.00 TO 437.00, BETWEEN STRINGER 26L AND 24L. REPAIRED IAW CRJ 700 SRM 53-21-03-101-006-A01 AND SRM 51-25-01-001-001-A01.

Part: FRAME — CHAFED (ZONE 200) · airframe 4,002 hrs · 2,925 cycles

FUSELAGE STATION FORWARD SIDE OF FRAME STATION X1088 BETWEEN STRINGER 9R AND 10R HYDRAULIC LINE ATTACH CLIP BROKEN OFF AND FRAME CHAFED. REPAIRED IAW REO 670-53-61-170 AND HORIZON AIR EA R-53-337.

Part: FITTING — WORN (RT WING FLAP) · airframe 4,002 hrs · 2,925 cycles

RT WING TRAILING EDGE OUTBOARD FLAP ROLLER GUIDE FITTING HAS WEAR DAMAGE. REPAIRED IAW CRJ 700 SRM 57-51-02-201-001-A01 AND SRM 51-41-02-001-001-A01.

Part: VANE — CHAFED (RT WING FLAP) · airframe 4,002 hrs · 2,925 cycles

RT INBOARD FLAP VANE LEADING EDGE HAS CHAFED MARK. REPAIRED IAW CRJ 700 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-00-001-A01.

Part: FASTENER — LOOSE (LT WING SPOILERS) · airframe 4,002 hrs · 2,925 cycles

LT WING OUTBOARD FLIGHT SPOILERS HAVE LOOSE FASTENERS, OUTBOARD AND INBOARD SIDES. REPAIRED IAW CRJ 700 SRM 51-42-07-001-001-A01 AND SRM 51-25-01-00-001-A01.

Part: FASTENER — LOOSE (RT WING SKIN) · airframe 4,002 hrs · 2,925 cycles

RT WING UPPER SKIN TRAILING EDGE HAS LOOSE FASTENERS AT INBOARD OF MULTI-FUNCTION SPOILERS. REPAIRED IAW CRJ 700 SRM 51-42-07-001-001-A01 AND 51-25-01-001-001-A01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 4,002 hrs · 2,925 cycles

FORWARD FUSELAGE INTERIOR, FLOORBEAM AT STATION 280 IS CORRODED ALONG TOP FLANGE FROM LBL 30 TO RBL 30. REPAIRED IAW REO 670-53-11-047.

Part: SKIN — GOUGED (ZONE 100) · airframe 4,002 hrs · 2,925 cycles

EXTERNAL FUSELAGE SKIN, STATION 981.0, STRINGER 26L TO 27 HAS GOUGES IN SKIN. REPAIRED IAW HORIZON AIR EA R-53-333 AND CRJ 700 SRM 51-21-16.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 4,002 hrs · 2,925 cycles

FUSELAGE INTERIOR COCKPIT FLOORBEAM ANGLE HAS SPOTS OF CORROSION AT STATION 280, LBL 11 TO RBL 11. REPAIRED IAW CRJ 700 SRM 51-21-06-001-001-A01 AND SRM 51-21-11-001-001-A01.

Part: CHANNEL — BROKEN (FUSELAGE) · airframe 4,002 hrs · 2,925 cycles

AFT BELLY FAIRING 195DL JOINT STRAP, AFT CHANNEL HAS A BROKEN FLANGE AT AFT END OF CHANNEL. REPAIRED IAW HORIZON AIR EA R-53-333.

Part: SKIN — GOUGED (FUSELAGE) · airframe 4,002 hrs · 2,925 cycles

EXTERNAL FUSELAGE SKIN, STATION 975.0, STRINGER 27 HAS A GOUGES IN SKIN. REPAIRED IAW HORIZON AIR EA R-53-333 AND CRJ SRM 51-42-21-001-001-A01.

Part: RETAINER — BENT (CARGO DOOR SEAL) · airframe 4,002 hrs · 2,925 cycles

FORWARD BAGGAGE BAY DOOR OUTER SEAL RETAINER BENT AT 2 LOCATIONS AND GOUGED AT 2 ALONG LOWER EDGE OF DOOR. REPAIRED IAW CRJ 700 SRM 51-25-01-001-001-A01.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 2,923 hrs · 2,098 cycles

CREW FOLLOWED ABNORMAL CHECKLIST AND TURNED OFF AUTOPILOT WHEN THEY RECEIVED A MASTER CAUTION "AUTOPILOT RIGHT TRIM" MESSAGE. MAINTENANCE PERFORMED FUNCTIONAL TEST OF AILERON TRIM SYSTEM. THE FUNCTIONAL AND OPERATIONAL TESTS WERE GOOD. THE OPERATIONAL CHECK FLIGHT WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PANEL — INOPERATIVE (ZONE 200) · airframe 428 hrs · 326 cycles

PDX - RETURNED TO FIELD, FIRST OFFICER'S SPEED BUGS WILL NOT SET PROPERLY. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED AIR DATA REFERENCE PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FILTER — ODOR (APU FUEL) · airframe 360 hrs · 289 cycles

DEN FLIGHT NR 4015 DURING STARTUP, INITIALLY HAD AN APU FAULT. THAT MESSAGE WENT AWAY. STARTED APU UP AND AIRCRAFT WAS FILLED WITH A STRONG ODOR OF JET FUEL. REPLACED FUEL FILTER. PERFORMED OPERATIONAL TEST AND LEAK TEST OF APU IAW CRJ700 MM TASK 49-31-01-400-801-A01 STEP 2E. OPERATIONAL AND LEAK TEST GOOD. AIRCRAFT RETURNED TO SERVICE.