N615QX

Part: BEAM — MECHANIC ERROR (BS 743) · airframe 38,924 hrs · 29,298 cycles

REF: CO# 10065CARE JOB# 710065MOD3 OP# 3: WHILE PERFORMING SB670SH-53-042 ONE HOLE WAS MISS DRILLED ON THE LH SIDE OF THE BUMP BEAM AT FS 743 , JUST INBOARD OF LBL 36. THE MIS-DRILLED HOLE GOES THROUGH THE PRESSURE FLOOR. C/A: REPAIRED IAW EC/TC REO 670-53-41-400 AND BOMBARDIER REO 670-53-41-400, DATED 2018-09-15.

Part: RAIL — NONE (ZONE 200) · airframe 38,924 hrs · 29,298 cycles

REF: CO# 10065CARE JOB# 710065MOD5 OP# 105: TERMINAL MODULE RAIL LOCATED AT 774, RBL 27 CANNOT BE REACHED BY THE EXISTING WIRE LOOM AFTER INCORPORATIO OF SB 670SH-53-042. C/A: REPAIRED IAW EC/TC SNIEO KSH670-35829-S46 AND BOMBARDIER SNIEO KSH670-35829-S46, DATED 04/16-2014 AS WRITTEN.

Part: FRAME ANGLE — CRACKED (BS 202.75) · airframe 38,924 hrs · 29,298 cycles

REF: CO# 10065CARE JOB# 710065MOD5 OP# 95: INDICATION NOTED AT FS 202.75 BULKHEAD CAP ANGLE AFT FACE RHS BELOW STR 13R, 1.5' LONG IN LENGTH VERTICALLY. FAILS NDT INSPECTION. C/A: REPAIRED IAW EC/TC REO 670-53-11-1430 AND BOMBARDIER REO 670-53-11-1430, DATED 2018-09-19.

Part: BRACKET — CRACKED (ZONE 100) · airframe 38,924 hrs · 29,298 cycles

REF: CO 10065CARE JOB 710065MOD5 OP 99: AILERON AUTO PILOT SERVO BRACKET IS CRACKED AT FWD UPPER HOLE AT RBL 36. C/A: REPAIRED IAW EC/TC KSH670-90024-S02 AND EC/TC SH670-90000-S03.

Part: BRACKET — CRACKED (AILERONS) · airframe 38,924 hrs · 29,298 cycles

REF: CO# 10065CARE JOB# 710065MOD5 OP# 99: AILERON AUTO PILOT SERVO BRACKET IS CRACKED AT FWD UPPER HOLE AT RBL 36. C/A: REPAIRED IAW EC/TC SNIEO KSH670-90024-S02 AND EC/TC SNIEO SH670-90000-S03.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 38,924 hrs · 29,298 cycles

REF: CO 10065CARE JOB 710065MOD5 OP 95: INDICATION NOTED AT FS 202.75 BULKHEAD CAP ANGLE AFT FACE RT BELOW STR 13R, 1.5' LONG IN LENGTH VERTICALLY. FAILS NDT INSPECTION. C/A: REPAIRED IAW EC/TC REO 670-53-11-1430 AND REO 670-53-11-1430, DATED 2018-09-19.

Part: FRAME — CRACKED (BS 235) · airframe 38,924 hrs · 29,298 cycles

REF: CO# 10065CARE JOB# 710065MOD5 OP# 97: F.S. 235.00 L/H FRAME HAS VISUAL CRACK AT STRINGER 13L. C/A: REMOVED AND REPLACED L/H F.S. 235.00 FRAME UPPER FRAME SECTOR P/N CC370-34133-9 IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 38,924 hrs · 29,298 cycles

INDICATION NOTED AT FS 202.75 BULKHEAD FWD FACE AT THE TOP OF THE RBL 30.0 STIFFENER APPROXIMATELY .10" IN LENGTH, FAILS NDT. REPAIRED RBL 30.0 POST AT FS 202.75 BULKHEAD IAW SRM 53-11-10-201-005-A01.

Part: POST — CRACKED (FUSELAGE) · airframe 38,924 hrs · 29,298 cycles

LBL 27 POST IS CRACKED AT FS 693.00. DRILLED AND LOCATED LBL 27 POST AT FS 693.00 P/N SH690-35884-7 IAW SRM 51-40-11-001-001-A01. INSTALL AND REMOVAL IS DOCUMENTED ON WVAC JOB 710065MOD5 OP 5004.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,924 hrs · 29,298 cycles

FRAME AT FS 235 STR 13 RT SIDE HAS INDICATION NOTED .500 LONG FROM FASTENER HOLE TO RADIUS. REMOVED AND REPLACED FS 235 FRAME IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01 AND 51-42-21-001-001-A01.

Part: STIFFENER — CRACKED (BS 202) · airframe 37,182 hrs · 27,725 cycles

CRACK INDICATION NOTED WHILE PERFORMING A BS 202.75 INSPECTION AT BL. 0 IN BOTH FORWARD OUTBOARD RADIUS IN THE VERTICAL STIFFENER, APPROXIMATELY 1.250 INCHES LONG AND 100% FSH. FAILED NDT INSPECTION. REPAIRED THE DAMAGE IAW REO 670-53-11-1347, REV.- AND EC/TC REO 670-53-11-1347, REV 0.

Part: ANGLE — CRACKED (BS 202 BULHEAD) · airframe 37,182 hrs · 27,725 cycles

FOUND THE BS 202.75 BULKHEAD CAP ANGLE BETWEEN RBL 7.50 AND RBL 13.80 HAS A CRACK INDICATION NOTED APPROXIMATELY 1.00 INCH IN LENGTH AND 100% FSH. REPAIRED THE DAMAGE IAW REO 670-53-11-1346, REV.--, AND EC/TC REO 670-53-11-1346, REV 0.

Part: SERVO — ROUGH (ZONE 300) · airframe 35,676 hrs · 26,184 cycles

AFTER TURNING AUTO PILOT OFF TO LAND, PITCH CONTROL OF THE AIRCRAFT WAS DIFFICULT. WHILE PULLING ON THE YOKE TO PITCH UP, FELT A BUMP IN THE CONTROL COLUMN AS IF THE AUTO PILOT HAD DISCONNECTED. AT THAT POINT HAD ADEQUATE PITCH COMMAND ALTHOUGH AIRCRAFT HAS VERY HEAVY PITCH FEEL. COMPLIED WITH RIG CHECK OF ELEVATOR PCU'S, REF AMM 27-33-01. RIGGING CHECK GOOD, NO DEFECTS NOTED AT THIS TIME. REMOVED AND REPLACED ELEVATOR SERVO IAW AMM 22-11-24. PERFORMED RIG AND OPS CHECK OF ELEVATOR SERVO IAW AMM 22-11-24.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 35,674 hrs · 26,182 cycles

RT OB FLOOR SILL CORRODED AT FS 280-319. INSTALLED NEW FLOOR SILL IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. INSTALLED SPLICE AT FS 300 OB FLOOR SILL RT REFERENCE DRAWING SH670-32170 AND SRM 51-42-13-001-001-A01.

Part: ANGLE — CORRODED (BS 310-349) · airframe 35,674 hrs · 26,182 cycles

PASSENGER DOOR LOWER SILL FWD & MID CAP ANGLE CORRODED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-00-001-001-A01, 51-42-06-001-001-A01 AND 51-41-02-001-001-A01.

Part: FRAME — CORRODED (BS 485) · airframe 35,674 hrs · 26,182 cycles

FRAME FLANGE AND WEB CORRODED AT BS 485 BETWEEN STRINGERS 26L - 26R. REPAIRED IAW EC/TC EA 30-2016-370.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 35,674 hrs · 26,182 cycles

FUSELAGE SKIN IS ABRADED AT FS985 AND FS969 UNDER FAIRING 195DL STR 27 & 26L. REPAIRED SKIN PANEL, FUSELAGE FS969-977 STR 26L-26R IAW EA 32-2016-267. REPAIRED DAMAGE AT 985 IAW SRM 53-61-01-101-003-A01 AND 51-21-00-001-001-A01.

Part: ANGLE — CRACKED (ZONE 400) · airframe 35,674 hrs · 26,182 cycles

DURING C CHECK, FOUND ANGLE CRACKED IN LT PYLON, INBOARD AFT CORNER TRAILING EDGE. REPAIRED LT PYLON INBD AFT CORNER TRAILING EDGE ANGLE IAW EC/TC SNIEO MM670-37189 S01 AND SNIEO MM670-37189 S01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 35,674 hrs · 26,182 cycles

DURING C CHECK, FOUND PASSENGER DOOR LOWER SILL CORRODED. REPLACED PASSENGER DOOR LOWER SILL KICK ANGLE IAW SRM 51-40-11-001-001-A01,51-42-06-001-001-A01, AND 51-42-21-001-001-A01

Part: STRINGER — CRACKED (FUSELAGE) · airframe 35,674 hrs · 26,182 cycles

STRINGER 3L IS CRACKED AT FS280 BULKHEAD. REPAIRED STRINGER IAW EC/TC REO 670-53-21-493 REV B, REO 670-53-21-493 REV D, EC/TC SB 670BA-53-040-01 REV B AND SERVICE BULLETIN 670BA-53-040 REV C PART B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,674 hrs · 26,182 cycles

LT SIDE SEAT TRACK AT FS863-969 HAS EXFOLIATION CORROSION. FABRICATED NEW SEAT TRACK IAW EC/TC REO 670-53-00-343 AND INSTALLED IAW AMM 53-00-49-000/400-801-A03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,674 hrs · 26,182 cycles

LT SIDE SEAT TRACK AT FS785-863 HAS EXFOLIATION CORROSION. FABRICATED NEW SEAT TRACK IAW EC/TC REO 670-53-00-343 AND INSTALLED IAW AMM 53-00-49-000/400-801-A03.

Part: SEAT TRACK — CORRODED (BS 485-597) · airframe 35,674 hrs · 26,182 cycles

DURING C CHECK, FOUND THE LT SEAT TRACK FROM BS 485 - 597 HAS EXFOLIATION CORROSION. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343 AND INSTALLED IAW AMM B53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,674 hrs · 26,182 cycles

LT SIDE SEAT TRACK AT FS708-761 HAS EXFOLIATION CORROSION. FABRICATED NEW SEAT TRACK IAW EC/TC REO 670-53-00-343 AND INSTALLED IAW AMM 53-00-49-000/400-801-A03.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 35,674 hrs · 26,182 cycles

DURING C CHECK, FOUND THE LT SEAT TRACK FROM BS 379 - 485, RBL 9 HAS EXFOLIATION CORROSION. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343 AND INSTALLED IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 579-708) · airframe 35,674 hrs · 26,182 cycles

DURING C CHECK, FOUND THE LEFT SIDE SEAT TRACK, BS 579 - 708, RBL9 CORRODED BEYOND LIMITS. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343 AND INSTALLED IAW AMM 53-00-49=000/400-801-A03.

Part: SEAT TRACK — CORRODED (BS 579-708) · airframe 35,674 hrs · 26,182 cycles

DURING C CHECK, FOUND THE LT SEAT TRACK FROM BS 579 - 708, RBL 9 HAS EXFOLIATION CORROSION. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343 AND INSTALLED IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 35,674 hrs · 26,182 cycles

DURING C CHECK, FOUND THE SEAT TRACK AT BS 349 - 485, RBL 9 HAS MULTIPLE AREAS OF CORROSION. FABRICATED ANEW SEAT TRACK IAW REO 670-53-00-343 AND INSTALLED IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 708-861) · airframe 35,674 hrs · 26,182 cycles

DURING C CHECK, FOUND THE SEAT TRACK AT BS 708 - 761, STRINGER 15R CORRODED. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343 AND INSTALLED IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 35,674 hrs · 26,182 cycles

DURING C CHECK, FOUND THE SEAT TRACK AT BS 581 - 677, RBL 9 HAS MULITIPLE AREAS OF CORROSION. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343 AND INSTALLED IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 35,674 hrs · 26,182 cycles

DURING C CHECK, FOUND THE SEAT TRACK AT BS 485 - 581, RBL 9 HAS MULITIPLE AREAS OF CORROSION. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343 AND INSTALLED IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,674 hrs · 26,182 cycles

SEAT TRACK AT FS785-863 STRINGER 15R HAS MULTIPLE AREAS OF CORROSION. FABRICATED NEW SEAT TRACK IAW EC/TC REO 670-53-00-343 AND INSTALLED IAW AMM 53-00-49-400-801-A17.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 34,308 hrs · 25,065 cycles

EMERGENCY LIGHT SWITCH FOUND IN ON POSITION IN ACFT. AFTER ALLOWING APU TO RUN WITH EMERGENCY LIGHT SWITCH IN THE ARMED POSITION, NO FURTHER DEFECTS ARE NOTED, IAW MAINTENANCE, NO FURTHER ACTION REQUIRED.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 33,887 hrs · 24,738 cycles

FOWARD F/A FLASHLIGHT INOPERATIVE. INSTALLED FLASHLIGHT BATTERIES, REF AMM 25-60-00.

Part: LIGHT — MISSING (CABIN) · airframe 32,833 hrs · 23,869 cycles

PHOTOLUMINESCENT STRIP MISSING MORE THAN 6" ON WALL NEAR SERVICE DOOR. REPLACED PHOTOLUMINESCENT STRIP ON SERVICE DOOR IAW AMM 25-60-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 32,716 hrs · 23,769 cycles

ROW 15 CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED CEILING EMERGENCY LIGHT BLUB IAW AMM 33-51-09, OPS CHECKED GOOD.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 31,542 hrs · 22,879 cycles

DURING INSPECTON FOUND MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW EO 700-25-0266. NO FURTER DEFECTS NOTED.

Part: SENSOR — FAILED (RT BRAKE TEMP) · airframe 31,220 hrs · 22,646 cycles

IN FLIGHT BRAKE OVERHEAT WARNING, DIVERTED, EMERGENCY DECLARED . R & R RT OTBD BRAKE TEMP SENSOR IAW AMM 32-46-01, OPS CHECKED GOOD.

Part: STRINGER — CORRODED (BS 310-349) · airframe 30,793 hrs · 22,328 cycles

FOUND STRINGER 20R AT FS 310-349, TO BE CORRODED WITH DEEP PITTING DAMAGE. REMOVED STRINGER AT 20R FS 310-349, DUE TO DEEP PITTING CORROSION FOUND IAW SRM 51-42-06-001-001 & 51-42-21-001-01. INSTALLED FASTENERS IN STR20, FROM FS 310-FS 349 COMMON TO SKIN & STRINGER REF DWG SH670-31950 & SH 670-32-420. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. LOCATED FASTENER HOLES COMMON TO SKIN PANEL AND ATTACHING INTERCOSTAL ON SERVICABLE STRINGER IAW SRM 51-40-11-001-001-A01 AND DWG SH670-32420. INSTALLED FASTENERS IN STR 20 COMMON TO STR 20 & INTERCOSTAL REF DWG SH670-31950 & SRM 51-42-06-001-001. INSTALLED INTERCOSTAL GUSSETS FS 310 & 349 AND ATTACH CLIPS ON UPPER LOG OF INTERCOSTAL REF DWG SH670-31950 & SRM 51-42-21-001-0010.

Part: FLOOR SUPPORT — CRACKED (BS 260-280) · airframe 30,793 hrs · 22,328 cycles

FLOOR SUPPORT AT LBL11, FS280-260 IS CRACKED. REMOVED FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-AO1. LOCATED AND DRILLED SERVICABLE FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01. INSTALLED FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG CC 670-33199.

Part: FLOOR SUPPORT — CRACKED (BS 260-280) · airframe 30,793 hrs · 22,328 cycles

FLOOR SUPPORT AT RBL11, FS280-260 IS CRACKED. REMOVED FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01. LOCATED AND MATCHED DRILL SERVICEABLE FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01. INSTALLED FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG CC670-33199.

Part: SEAT TRACK — CORRODED (BS 863-985) · airframe 30,793 hrs · 22,328 cycles

RT SIDE TRACK SEGMENT BS 863 TO 985 CORRODED IN MULTIPLE AREAS. REMOVED AND REPLACED RT SEAT TRACK SEGMENT IAW AMM 53-00-49-400-801(A03) AND 53-00-49-400-801(A03).

Part: FLOORBEAM — CORRODED (BS 280) · airframe 30,793 hrs · 22,328 cycles

GUSSETS AT LBL11 AND RBL11 ON FWD SIDE 280 BEAM, ENTERING COCKPIT ARE CORRODED 2 EA. REMOVED LT AND RT GUSSETS IAW SRM 51-42-06-001-001-A01. MATCHED DRILLED NEW SERIVCABLE PARTS IAW SRM 51-40-11-001-001-A01. INSTALLED GUSSETS IAW SRM 51-42-06-001-001-A01 AND DWG CC670-33052.

Part: ANGLE — CORRODED (BS 280) · airframe 30,793 hrs · 22,328 cycles

2 EA, CLIPS CORRODED AT LBL11 AND RBL11 ON FWD SIDE 280 ENTERING COCKPIT. REMOVED 2EA CLIPS FROM RT AND LT LBL11 IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01. LOCATED FASTENER HOLES IN NEW LT AND RT CLIPS AT LBL/RBL 11, FS 280, WL 73 IAW SRM 51-40-11-001-001-A01. INSTALLED LT/RT CLIPS IAW SRM 51-42-06-001-001, 51-42-13-001-001, DWG CC670-34010.

Part: ANGLE — CRACKED (BS 280) · airframe 30,793 hrs · 22,328 cycles

ANGLE AT LBL 26.00, FS 280 IS CRACKED. R & R ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG CC670-34010.

Part: SEAT TRACK — CORRODED (BS 736) · airframe 30,785 hrs · 22,320 cycles

LEFT SIDE WALL SEAT TRACK HAS CORROSION AT BS 736. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 30,785 hrs · 22,320 cycles

INTERCOSTAL BETWEEN S26 & 27L, BS 349 - 364 CORRODED. REMOVED DAMAGED INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND SRM 51-41-21-001-001-A01. LOCATED DRILLED AND DEBURRED NEW HOLES IN NEW INTERCOSTAL IAW SRM 51-40-11-001-001-A01. INSTALLED NEW INTERCOSTAL IAW SRM 51-40-06, 51-42-21-001-001-A01 AND DWG SH670-32075.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 30,785 hrs · 22,320 cycles

SEAT TRACK SEGEMENT BS 581-677 RBL 9, CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 30,785 hrs · 22,320 cycles

SEAT TRACK SEGEMENT LBL 9 BS 581-677, CORRODED IN SEVERAL AREAS. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 397-485) · airframe 30,785 hrs · 22,320 cycles

RT SIDE SEAT TRACK SEGMENT FROM BS 397 - 485 IS CORRODED IN MULTIPLE AREAS. R & R SEAT TRACK IAW AMM TASK 53-00-49-000-801 & 53-00-49-400-801.

Part: SEAT TRACK — CORRODED · airframe 30,793 hrs · 22,328 cycles

RT SIDE SEAT TRACK SEGMENT BS 485 TO 581 CORRODED IN MULTIPLE AREAS. REMOVED AND INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 30,785 hrs · 22,320 cycles

LT SIDE SEAT TRACK SEGEMENT BS 379-485 CORRODED SEVERAL AREAS. R & R SEAT TRACK SIGMENT IAW AMM 53-00-49-40-801.

Part: SEAT TRACK — CORRODED (BS 785) · airframe 30,785 hrs · 22,320 cycles

RIGHT SIDE SEAT TRACK HAS CORROSION AT BS 785.15. FOUND OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. R & R SEAT TRACK IAW AMM TASK 53-00-49-000-801 & 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 613) · airframe 30,785 hrs · 22,320 cycles

LEFT SIDE SEAT TRACK HAS CORROSION AT BS 613. R & R INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-000-801 AND 400-801.

Part: SEAT TRACK — CORRODED (BS 736) · airframe 30,785 hrs · 22,320 cycles

RIGHT SIDE WALL SEAT TRACK HAS CORROSION AT BS 736.05. R & R SEAT TRACK IAW SRM 51-41-02-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 863 - 985) · airframe 30,785 hrs · 22,320 cycles

LEFT SIDE SEAT TRACK SEGEMENT BS 863 - 985 IN CORRODED IN MULTIPLE AREAS. R & R SEAT TRACK IAW AMM 53-00-49-400-801 & 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 30,785 hrs · 22,320 cycles

SEAT TRACK SEGEMENT BS 485-581 RBL 9, CORRODED IN SEVERAL AREAS. REPLACED SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 708) · airframe 30,785 hrs · 22,320 cycles

RIGHT SIDE WALL SEAT TRACK HAS CORROSION AT BS 708. R & R SEAT TRACK IAW AMM 53-00-49-400-801 & 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 30,785 hrs · 22,320 cycles

SEAT TRACK SEGEMENT BS 485-581 LBL 9 IS CORRODED IN SEVERAL PLACES. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 677-830) · airframe 30,785 hrs · 22,320 cycles

SEAT TRACK SEGEMENT LBL 9 BS 677-830.4 CORRODED IN SEVERAL AREAS. R & R SEAT TRACK SEGMENT IAW AMM 53-00-49-000-801, & 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 645) · airframe 30,785 hrs · 22,320 cycles

LEFT SIDE WALL SEAT TRACK CORRODED AT BS 645. REMOVED AND REPLACED SIDE SEAT TRACK IAW AMM 53-00-49-000-801 AND 400-801.

Part: SEAT TRACK — CORRODED (BS 677-830) · airframe 30,785 hrs · 22,320 cycles

SEAT TRACK SEGEMENT BS 677-830.40 RBL 9, CORRODED IN SEVERAL AREAS. R & R SEAT TRACK SEGMENT IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 30,793 hrs · 22,328 cycles

RIGHT SIDE SEAT TRACK SEGMENT BS 581 TO 677 CORRODED IN MULTIPLE AREAS. REMOVED AND REPLACED RT SIDE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 30,785 hrs · 22,320 cycles

SEAT TRACK SEGEMENT BS 349-485 RBL 9 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED SEAT TRACK IAW AMM TASK 53-00-49-000-801 AND AMM 53-00-49-400-801(A03).

Part: SEAT TRACK — CORRODED (BS 708) · airframe 30,785 hrs · 22,320 cycles

LEFT SIDE WALL SEAT TRACK HAS CORROSION AT BS 708. R & R SEAT TRACK IAW AMM 53-00-49-000-801 & 53-00-49-40-801.

Part: SEAT TRACK — CORRODED (BS 549) · airframe 30,785 hrs · 22,320 cycles

SIDE WALL SEAT TRACK HAS CORROSION ON LT SIDE AT BS 549. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 830-969) · airframe 30,785 hrs · 22,320 cycles

SEAT TRACK SEGEMENT BS 830.40-969 RBL 9, CORRODED IN SEVERAL AREAS. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 847) · airframe 30,785 hrs · 22,320 cycles

LEFT SIDE WALL SEAT TRACK HAS CORROSION AT BS 847. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 830-969) · airframe 30,785 hrs · 22,320 cycles

SEAT TRACK SEGEMENT BS 830.40-969 RBL 9, CORRODED IN SEVERAL AREAS. REPLACED SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 30,785 hrs · 22,320 cycles

CORROSION FOUND AT FS 280 LOWER AVI COMPARTMENT FLOOR SUPPORT, REMOVED, OBTAINED, LOCATED AND DRILL NEW ANGLE AND INSTALLED AT FS 280, LOWER AVI COMPARTMENT FLOOR SUPPORT ANGLE IAW AMM 51-40-11-001-001-A01, 51-42-02-06-001-001-A01, 51-42-21-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 30,785 hrs · 22,320 cycles

CORROSION FOUND AT FS 280 LT FLOORBEAM. FLOORBEAM REPAIRED IAW SB670BA-53-041.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 30,785 hrs · 22,320 cycles

CORROSION FOUND AT FS 280 R FLOORBEAM, REPAIRED IAW SB670BA-53-041.

Part: FLOOR SUPPORT — CORRODED (BS 1000-1047) · airframe 30,785 hrs · 22,320 cycles

AFT CARGO, RT CABIN FLOOR SUPPORT CORRODED SEVERAL AREAS BETWEEN FRAMES BS 1000-1047. REPAIRED IAW ECTC REO 670-53-00-390 AND REO 670-53-00-390.

Part: DOOR FRAME — CORRODED (BS 364-394) · airframe 30,785 hrs · 22,320 cycles

CORROSION FOUND AT FS 364-394, S25 LT - 25RT AVI DOOR SURROUND INSIDE. REMOVED CORROSION IAW SRM 851-21-06-001-001. BLENDED AREA IS OUT OF LIMITS IAW SRM 53-21-01-101-000801. REPAIRED IAW REO 670-53-21-242. MAJOR REPAIR.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 30,785 hrs · 22,320 cycles

LT WEB CORRODED AT BS 280. REPAIRED IAW EC/TC REO 670-53-11-594 AND GREO 670-53-11-594, REV. MAJOR REPAIR.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 30,785 hrs · 22,320 cycles

RT BULKHEAD WEB CORRODED AT BS 280. REPAIRED IAW EC/TC REO 670-53-11-594 AND GREO 670-53-11-594, REV. MAJOR REPAIR.

Part: SKIN — CORRODED (BS 501-517) · airframe 30,785 hrs · 22,320 cycles

DOUBLER SKIN CORRODED BETWEEN BS 501-517 STRINGERS 26L-26R. REMOVED CORROSION ON CHANNEL IAW SRM 51-20-06-001-001. NO DAMAGE ALLOWED INBLENDED AREA IAW SRM 53-31-01-101-003-A01. REMOVED REMAINING CORROSION IAW SRM 51-42-06-001-01 & 51-42-06-001-001. REPAIRED AREA IAW EA 32-2014-013.

Part: FRAME — CORRODED (BS 280) · airframe 30,793 hrs · 22,328 cycles

CORROSION FOUND AT FS 280 CIRCUMFERENTIAL JOINT EXTENDS FROM STRG 26LT TO 23RT. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 AT FS 280 BETWEEN STR 26L TO 26R AND BETWEEN STR 24R AND 23R.

Part: STRINGER — CORRODED (BS 310) · airframe 30,785 hrs · 22,320 cycles

CORROSION FOUND ON STRINGER 19R AT BS 310. REMOVED CORROSION AND IAW SRM 51-21-06-001-001-A01. MAJOR REPAIR.

Part: FRAME — CORRODED (BS 517) · airframe 30,785 hrs · 22,320 cycles

FRAME BS 517 CORRODED AFT FACE BETWEEN STRINGERS 26R-26L. REMOVED CORROSION IAW SRM 51-42-06-001-001, 51-21-06-001-001. BLENDED AREA IS OUT OF LIMITS IAW SRM 53-31-06-101-003-A01. REPAIRED IAW EA 25-2014-203.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 30,785 hrs · 22,320 cycles

CORROSION FOUND AT FS 349-364 AT STR 27, INTERCOSTAL. REMOVED CORROSION ON INTERCOSTAL IAW SRM 51-21-06-001-001. BLENDED AREA IS OUT OF LIMITS IAW SRM 53-21-23-101-003-A01. RECEIVED AND COMPLIED WITH EA 32-2014-008.

Part: STRINGER — CORRODED (BS 349) · airframe 30,793 hrs · 22,328 cycles

CORROSION FOUND ON STRINGER 19RT AT FS 349. CORROSION FOUND ON STGR20 ON INTERCOSTAL AND CLIP AT FS349. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. EVALUATED CORROSION OUT OF LIMIT IAW SRM 53-21-23-101-002-A01. LOCATED FASTENER HOLES IN NEW, SERVICEBLE CLEATS AT STR 20R AT FS 319, FS333 AND FS349 IAW SRM 51-40-11-001-001-A01. REMOVED INTERCOSTAL AT STR 20 BETWEEN FS 319 AND 349 AS NEEDED REF SRM 51-42-06-001-001 AND SRM 51-42-21-001-001. LOCATED, DRILLED AND INSTALLED SERVICEABLE INTERCOSTAL AT STR 20R, FS 319-349 IAW SRM 51-40-11-001-00-A01 AND DWG SH670-32004.

Part: ANGLE — CRACKED (BS 1098) · airframe 30,785 hrs · 22,320 cycles

INSIDE AFT EQUIP BAY, AN ANGLE IS CRACKED AT BS 1098.20, S24R. REMOVED CRACKED ANGLE IAW SRM 51-42-06-001-001. FABRICATED & INSTALLED NEW ANGLE IAW EO 700-53-0260.

Part: ANGLE — CRACKED (BS 1098) · airframe 30,785 hrs · 22,320 cycles

INSIDE AFT EQUIPMENT BAY, AN ANGLE IS CRACKED AT BS 1098.20, S24L. REMOVED CRACKED ANGLE IAW SRM 51-42-06-001-001. FABRICATED & INSTALLED NEW ANGLE IAW EO 700-53-0260, AT STR24R.

Part: SKIN — DENTED (FUSELAGE) · airframe 30,793 hrs · 22,328 cycles

GROUND CREW REPORTED DENT BOTTOM LT SIDE OF AFT CARGO. REPAIRED IAW EC/TC EA 12-2014-149.

Part: PLATE — CRACKED (FUELAGE) · airframe 30,785 hrs · 22,320 cycles

FWD EQUIPMENT JB6 SUPPORT PLATE CRACKED ON FWD RT SIDE CORNER. COMPLIED WITH EA 32-2014-003. COMPLIED WITH EC/TC EA32-2014-003. COMPLIED WITH EA 62-2014-003.

Part: SKIN — DENTED (BS 280) · airframe 30,793 hrs · 22,328 cycles

DENT IN FUSELAGE SKIN AT FS280 AND STR12L AND 13L FOUND ON INCOMING INSPECTION. EVALUATED DAMAGE, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01-101-001-A01. REWORKED DENT IAW ES 32-2014-005 REV A. RECEIVED AND COMPLIED WITH EA 32-2014-005 REV A DATED 7/10/2014.

Part: SEAL — DETERIORATED (APU EXHAUST) · airframe 30,785 hrs · 22,320 cycles

APU EXHAUST PIPE AFT SEAL DETERIORATED AND .2500 OF IT MISSING. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED DETERIORATED SEAL AFT ON APU EXAHAUST REF: SRM 51-42-13-001-001. REMOVED DETERIORATED AFT APU EXHAUST PIPE SEAL REF: 51-42-13-001-001. FIT AND DRILLED UP AFT APU SEAL AND BAND CLAMP IAW REO 670-49-81-006. COMPLIED WITH EC/TC REO 670-49-81-006 & REO 670-49-81-006.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 29,295 hrs · 21,212 cycles

CABIN EMERGENCY PHOTOLUMINESCENT MISSING FOR OVERWING EXIT C/D SIDE. INSTALLED GLOWSTRIP IAW AMM 33-55-01.

Part: LIGHT — MISSING (CABIN) · airframe 29,228 hrs · 21,167 cycles

SECTION OF EMERGENCY LIGHT MISSING IN FRONT OF SEAT 12C AT EMERGENCY EXIT ROW. INSTALLED EMERGENCY LIGHT IAW AMM 33-51-01M.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,592 hrs · 20,693 cycles

CABIN CEILING NR 2 EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED LAMPS . OPS CHECKED GOOD.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 28,539 hrs · 20,657 cycles

F/A DISCOVERED MISSING PHOTO LUMINESCENT STRIPS AT BOTH EMERGENCY EXIT ISLE. REINSTALLED STRIP FOUND IN STORAGE AREA BEHIND F/A'S SEAT IAW AMM 33-51-01.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,644 hrs · 20,018 cycles

NR 2 CABIN CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-09, OPS CHECKED GOOD.

Part: FLOOR SKIN — CRACKED (BS 193) · airframe 26,301 hrs · 18,996 cycles

LT SIDE OF FWD AVIONIC BAY FLOOR SKIN CRACKED AT FS 193. REPAIRED IAW GREO 670-53-11-509.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 26,300 hrs · 18,993 cycles

THREE CORRODED L ANGLES BY HINGE INNER CAVITY. REMOVED ANGLES IAW SRM 51-42-06-001-001-A01. INSTALLED NEW ANGLES IAW SRM 51-42-06-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 26,301 hrs · 18,996 cycles

AFT FLOOR SUPPORT CORRODED. REMOVED FROM SUPPORT IAW SRM 51-42-06-001-001-A01. DRILLED NEW AFT FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01. INSTALLED FLOOR SUPPORT IAW SRM 51-42-21-001-001, SRM 51-42-06-001-001-A01.

Part: ANGLE — CRACKED (BS 280) · airframe 26,300 hrs · 18,993 cycles

ON REMOVAL OF RT LOWER BS 280 WEB FOUND RBL 26 ANGLE CRACKED AT LOWER 2 FASTENER HOLES. REMOVED DAMAGED ANGLE, LOCATED & DRILLED NEW ANGLE, AND INSTALLED IAW SRM 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 830-969) · airframe 26,300 hrs · 18,993 cycles

9L SEAT TRACK SECTION FROM FS 830-969 HAS CORROSION. REMOVED CORROSION IAW 53-51-49-101-001-A01. PERFORMED LPI TYPE 1, METHOD-C ON BLEND AREAS IAW SRM 53-51-49-101-001-A01 MAC NDT INSPECTION PROCEDURE PT-1, NO INDICATIONS NOTED.

Part: SEAT TRACK — CORRODED (BS 724) · airframe 26,300 hrs · 18,993 cycles

9R SEAT TRACK SECTION HAS CORROSION AT 724. REMOVED CORROSION IAW SRM 53-41-49-101-001-A01. REMOVED .014 FROM TOP (U) LIMIT .035 .021 REMAINING. REMOVED .012 FROM CENTER (T) LIMIT .035 023 REMAINING. PERFORMED LPI, TYPE 1, METHOD-C ON BLEND AREA IAW SRM 53-31-49-101-001-A01 IAW NDT INSPECTION PROCEDURE PT-1, NO INDICATIONS NOTED.

Part: SEAT TRACK — CORRODED (BS 519-571) · airframe 26,301 hrs · 18,996 cycles

9R SEAT TRACK SECTION FROM FS 485-581 HAS CORROSION AT FS 519-571. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013 SHEET & SECTION K-K. REMOVED SEAT TRACK IAW SRM 51-41-02-0001-001-A01 AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 26,301 hrs · 18,996 cycles

9R SEAT TRACK SECTION FROM FS 349-485 HAS MULTIPLE AREAS OF CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. REPLACED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 830-969) · airframe 26,300 hrs · 18,993 cycles

9R SEAT TRACK SECTION FROM FS 830-969 HAS CORROSION AND GOUGED. REMOVED CORROSION IAW SRM 53-51-49-101-001-A01. PERFORMED LPI TYPE 1 METHOD-C ON BLEND AREA IAW SRM 53-51-49-101-001-A01 IAW MAC NDT INSPECTION PROCEDURE PT-1, NO INDICATIONS NOTED.

Part: SEAT TRACK — CORRODED (BS 601-665) · airframe 26,300 hrs · 18,993 cycles

SEAT TRACK CORRODED AT 9L AND FS 601, 613, 629, 665. REMOVED CORROSION IAW SRM 53-31-49-101-001-A01. PERFORMED LPI, TYPE 1, METHOD-C ON BLENDED AREAS IAW SRM 53-31-49-101-001A-01 IAW NDT INSPECTION PROCEDURE PT-1, NO INDICATIONS NOTED.

Part: SEAT TRACK — CORRODED (BS 364-485) · airframe 26,300 hrs · 18,993 cycles

SEAT TRACK CORRODED AT 9L FWD SECTION AT FWD END FS 364 AND 379, 420, 469, 485. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. REMOVED SEAT TRACK IAW SRM 51-41-02-001-001-A01. INSTALLED NEW SERVICEABLE TRACK IAW AMM 53-00-49-400-801.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 26,301 hrs · 18,996 cycles

BS 280 BEAM CORRODED, LT, RT AND CENTER. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-43-101-001-A01. REPAIRED IAW GREO 670-53-11-047.

Part: WEB — CORRODED (BS 280) · airframe 26,301 hrs · 18,996 cycles

RT 280 WEB CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. REPAIRED IAW GREO 670-53-11-0594.

Part: DOOR — NO TEST (EMERGENCY EXIT) · airframe 26,300 hrs · 18,993 cycles

RIGHT EMERGENCY EXIT FAILED FUNCTIONAL TEST, REQUIRES 64LBS OF FORCE. CLEANED AND LUBED RT EMERGENCY EXIT IAW AMM 12-20-52-641-802. FUNCTIONAL CHECKED IAW AMM 52-21-00-720-801.

Part: DOOR — NO TEST (EMERGENCY EXIT) · airframe 26,300 hrs · 18,993 cycles

LEFT EMERGENCY EXIT FAILED FUNCTIONAL TEST, REQUIRES 78LBS OF FORCE. CLEANED AND LUBED EMERGENCY EXIT IAW AMM 12-20-52-640-802. PERFORMED FUNCTIONAL CHECK IAW AMM 52-21-00-720-801, CHECKED GOOD .

Part: DOOR — OUT OF ADJUST (FWD SERVICE) · airframe 26,300 hrs · 18,993 cycles

FORCE TO COMPLETE THE UNLATCH CYCLE FOR THE FORWARD GALLEY SERVICE DOOR EXCEEDS ALLOWABLE LIMITS. ADJUSTED LATCH MECHANISM TO ALLOWABLE LIMITS IAW AMM 52-41-02-820-801-A01. FUNCTIONAL TEST OF THE GALLEY SERVICE DOOR COMPLY WITH IAW AMM CH 25-41-00-720-802.

Part: WEB — CORRODED (BS 280) · airframe 26,301 hrs · 18,996 cycles

LEFT BS 280 WEB CORRODED. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. REPAIRED IAW GREO 670-53-11-0594.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 26,222 hrs · 18,936 cycles

EXIT SIGN MISSING AT PAX DOOR CABIN EMERGENCY LIGHTS. INSTALLED MISSING EXIT SIGN LENS, IAW AMM 33-51-05, OPS CHECK GOOD

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 24,775 hrs · 17,895 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. INSTALLED NEW DRAG ANGLE SECTION IAW SRM TEMP, REV 52-0008 AND SRM 51-42-06, 51-42-13, AND 51-42-22.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,949 hrs · 17,330 cycles

SHORTLY AFTER TAKEOFF, THE F/A'S REPORTED MOISTURE DRIPPING FROM THE AFT CABIN GASPERS AND AN UNPLEASANT MOLD / MILDEW ODOR COULD BE SMELLED THROUGHOUT THE ENTIRE FLIGHT. ODOR MOST NOTICEABLE FWD OF ROW 1. CHECKED BOTH WATER EXTRACTERS IAW AMM 21-51-18, COULD NOT DUPLICATE ODOR. OPS CHECK GOOD. (CLOSED)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 23,368 hrs · 16,922 cycles

PAX DOOR AFT DRAG ANGLE CRACKED ABOUT MIDDLE AREA. REPAIRED IAW SRM REVISION 52-0008.

Part: SEAT TRACK — CORRODED (BS 517-736) · airframe 23,187 hrs · 16,804 cycles

LEFT SIDEWALL SEAT TRACK HAS CORROSION AT FS 736, 708, 595 AND 517. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, STEP 1-3B.

Part: SEAT TRACK — CORRODED (BS 409-813) · airframe 23,187 hrs · 16,804 cycles

RIGHT SIDEWALL SEAT TRACK HAS CORROSION AT FS 409, 435, 517, 581, 597, 708, 720, AND 813. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, STEP 1-3B.

Part: SOCKET — BROKEN (EMERGENCY LIGHT) · airframe 22,994 hrs · 16,672 cycles

CENTER EMERGENCY EXIT SIGN AFT SIDE RED LIGHT SOCKET BROKEN. REMOVED AND REPLACED CENTER EMERGENCY EXIT SIGN ASSY AFT SIDE IAW AMM 33-51-07 OPS CHECK GOOD.

Part: STEP — CORRODED (PAX DOOR) · airframe 22,906 hrs · 16,607 cycles

A4 CHECK. FOUND THE NOSE STEP (TOP) OF THE MAIN CABIN DOOR TO BE CORRODED AND CRACKED DURING THE SCHEDULED GVI INSP. R & R THE STEP.

Part: DOOR — LACK OF LUBE (SERVICE) · airframe 22,719 hrs · 16,473 cycles

RAMPER REPORTS SERVICE DOOR IS HARD TO OPEN. CLEAN & LUBED SERVICE DOOR & CYCLE THE DOOR FEW TIMES, OPS CHECK GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: HOLDER — FAILED (FLASHLIGHT) · airframe 22,476 hrs · 16,278 cycles

FLASHLIGHT BY THE MAIN CABIN DOOR CHARGING LIGHT IS NOT ON AND STRAP HOLDING LIGHT BROKE. REPLACED FLASHLIGHT AND STRAP. RETURNED TO SERVICE.

Part: SENSING ELEMENT — NO TEST (MLG OVERHEAT) · airframe 22,413 hrs · 16,230 cycles

MLG BAY OVERHEAT SYS DOES NOT TEST. REPLACED LT MLG TEMP SENSOR IAW MM 26-14-04-000/400-801 (A01), OPS CHECKS GOOD IAW AMM 26-14-00-710-801 (A01). NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 21,318 hrs · 15,408 cycles

C CHECK - FASTENER HOLES CORRODED OM BACK SIDE OF SERVICE DOOR STRIKER SEAL. REMOVED CORROSION AROUND (7) FASTENER HOLES, FOUND TO BE "NO DAMAGE ALLOWED" AREAS, BLENDS OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. PERFORMED ECI ON BACK SIDE OF SERVICE DOOR STRIKER SEAL. PERFORMED ECI ON BLENDED AREAS, NO CORROSION OR CRACKS FOUND AT THIS TIME IAW NDTM ECI 51-20-006-250-A01. SENT TO MFG FOR ENGINEERING. REMOVED PROTECTOR PLATE AND FWD/AFT DOOR STOP FITTINGS FOR ACCESS IAW AMM 53-21-23-000-801-A01 AND SRM 51-41-02-001-001-A01. REMOVED SEAL STRIKER AND LOCATED HOLES IN NEW SEAL STRIKER IAW SRM 51-42-06-001-001-A01. INSTALLED NEW SEAL STRIKER IAW SRM 51-42-06-001-001-A01. INSTALLED FWD/AFT DOOR STOPS IAW SRM 51-41-02-001-001-A01 AND INSTALLED SERVICE DOOR PROTECTOR PLATE IAW AMM 53-21-23-400-801-A01.

Part: STRINGER — CORRODED (BS 340 S26R) · airframe 21,318 hrs · 15,408 cycles

C CHECK - CORROSION ON STRINGER 26R AT FS340. REMOVED CORROSION, BLENDS FOUND TO BE OUT OF LIMITS IAW SRM 53-21-03-101-006-A01. REMOVED STRINGER 26R IAW SRM 51-42-06-001-001-A01. LOCATED FASTENER HOLES ON NEW STRINGER IAW SRM 51-40-11-001-001-A01. INSTALLED NEW STRINGER IAW SRM 51-42-06-001-001-A01. APPLIED TOPCOAT IAW SRM 51-25-16-001-001-A01. APPLIED CORROSION INHIBITING COMPOUND TO AFFECTED AREAS IAW SRM 51-21-11-001-001-A01. ALL WORK DONE IN CONFORMITY OF REO 670-53-21-584.

Part: BUTTSTRAP — CORRODED (BS 280 S26L) · airframe 21,318 hrs · 15,408 cycles

C CHECK - FOUND CORROSION ON BUTTSTRAP JUST AFT OF FS 280 BETWEEN STRINGER 26L TO 25R. REMOVED CORROSION, IAW SRM 53-21-06-001-001-A01. BLENDS FOUND TO BE WITHIN LIMITS IAW REO-53-21-584 REV A. PERFORMED ECI ON FS 280 BETWEEN STRINGER 26L TO 25R. NO CRACKS OR CORROSION FOUND AT THIS TIME IAW NDTM ECI 51-20-006-250-A01. TREATED IAW SRM 51-21-11-001-001-A01, PRIMED IAW SRM 51-25-06-001-001-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.

Part: STRINGER CLIP — CORRODED (BS 333 S26R) · airframe 21,318 hrs · 15,408 cycles

C-CHECK - FOUND CORROSION ON ATTACH ANGLE FOR STRINGER 26R AT FS 333.00. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. CORROSION FOUND TO EXCEED ALLOWABLE LIMITS IAW SRM 53-21-003-101-002-A01. REMOVED ATTACH ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED FASTENER HOLES IN NEW ATTACH ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED NEW ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. TOP COATED IAW SRM 51-25-16-001-001-A01, APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: STRINGER — CORRODED (BS 319-333) · airframe 21,318 hrs · 15,408 cycles

C CHECK - FOUND CORROSION ON S26R BETWEEN BS 319.70-333. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDS FOUND TO BE OUT LIMITS. REMOVED STRINGER IAW SRM 51-21-42-06-001-001-A01. PERFORMED CUT LINE ON NEW STRINGER IAW SRM 53-00-03-201-001-A01. PERFORMED ECI ON CUT LINE ON NEW STRINGER, NO CRACKS FOUND AT THIS TIME IAW NDTM ECI 51-20-006-250-A01. PERFORMED CUT LINE ON FRAME AT BS 319 IAW REO 670-53-21-584A. PERFORMED ECI ON CUT LINE ON FRAME AT BS 319, NO CRACKS FOUND AT THIS TIME IAW NDTM ECI 51-20-006-250-A01 AND REO 670-53-21-584A. LOCATED FASTENERS ON NEW STRINGER &, INSTALLED NEW STRINGER & REPAIR ANGLES IAW SRM 51-42-06-001-001-A01 AND 53-00-03-991-803. TREATED, PRIMED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01. FABRICATED FRAME SPLICE REPAIR ANGLE IAW REO 670-53-21-584 REV A. TREATED, PRIMED AND PAINTED AS REQUIRED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 & 51-25-16-001-001-A01. INSTALLED FRAME SPLICE REPAIR AT BS 319 IAW REO 670-53-21-584. TOP COATED IAW SRM 51-25-16-001-001-A01. APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: COWLING — CHAFED (RT NACELLE) · airframe 21,318 hrs · 15,408 cycles

C CHECK - RT ENGINE UPPER FAN COWL CHAFE UNDER T/R TRANSMISSION FLEX LINE. BLENDED CHAFED AREAS ON FAN COWL SKIN AND REINFORCING ANGLE. SENT TO MFG FOR ENGINEERING. PERFORMED ECI ON RT ENGINE UPPER FAN COWL REINFORCING ANGLE WHERE AREA WAS BLENDED. NO CRACKS FOUND AT THIS TIME IAW NDTM ECI 51-20-006-250-A01, REO 670-54-14-1016. TREATED AREAS WORKED IAW SRM 51-21-11-001-001-A01. PRIMED WORKED AREAS IAW SRM 51-21-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 349-364 S27R) · airframe 21,318 hrs · 15,408 cycles

C CHECK - CORROSION ON INTERCOSTAL 27R FROM FS349 TO 364. BLENDED CORROSION BLEND MEASURES 2.6L X .6W X .003"D, ORIGINAL MATERIAL THICKNESS .080", REMAINING MATERIAL IS .077". PERFORMED ECI ON BLENDED AREA, NO CRACKS OR CORROSION NOTED AT THIS TIME IAW NDTM ECI 51-20-006-250-A01. TREATED IAW SRM 51-21-11-001-001-A01 PRIMED IAW SRM 51-25-06-001-001-A01 AND PAINTED IAW SRM 51-25-16-001-001-A01. ALL WORK DONE IAW REO 670-53-21-584, REV A.

Part: INTERCOSTAL — CORRODED (BS 344-364 S27R) · airframe 21,318 hrs · 15,408 cycles

C CHECK - CORROSION ON INTERCOSTAL 27R FROM FS344 TO 364. BLENDED OUT CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-003-A01. SENT TO MFG FOR ENGINEERING. PERFORMED ECI ON THE BLENDED AREAS, NO CRACKS OR CORROSION FOUND AT THIS TIME IAW NDTM ECI 51-20-006-250-A01. TREATED AREAS WORKED IAW SRM 51-21-11-001-001-A01. PRIMED AND PAINTED WORKED AREAS IAW MM 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. APPLIED AV8 COMPOUND IAW SRM 51-21-11-001-001-A01. ALL WORK DONE IAW MFG REO 670-53-21-584 REV A.

Part: FRAME — CORRODED (BS 295 S19-20L) · airframe 21,318 hrs · 15,408 cycles

C CHECK - FOUND CORROSION ON FRAME AT FS 295 BETWEEN STRINGERS 19L ATO 20L. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. CORROSION REMOVED MEASURES .8L X .6W X .003 D, ORIGINAL MATERIAL IS .050" REMAINING MATERIAL IS .047". FOUND TO BE OUT OF LIMITS IAW SRM 53-21-06-101-002-A01. SENT TO MFG FOR ENGINEERING. PERFORMED ECI ON AREA BLENDED, NO CRACKS OR CORROSION FOUND AT THIS TIME IAW NDTM ECI 51-20-006-250-A01. TREATED IAW SRM 51-21-11-001-001-A01. PRIMED AND PAINTED IAW 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. APPLIED AV8 COMPOUND IAW SRM 51-21-11-001-001-A01. ALL WORK DONE IAW REO 670-53-21-584.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 21,318 hrs · 15,408 cycles

C CHECK - PAX DOOR MID CAP ANGLE CORRODED THROUGH OUT. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS .063, REMOVED .015, REMAINING MATERIAL IS .048" AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. REMOVED MIDCAP IAW SRM 51-42-06-001-001-A01. PREPARED NEW MID CAP ANGLE IAW SRM 51-40-11-001-001-A01 AND 51-21-11-001-001-A01. INSTALLED NEW ANGLE IAW SRM 51-41-02-001-001-A01. TOPCOATED IAW SRM 51-25-16-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,318 hrs · 15,408 cycles

C-CHECK. FOUND CORROSION ON FLOOR SUPPORT ANGLE AT FS 280 FOR PANEL 141 ALF. REMOVED CORROSION FROM FLOOR SUPPORT ANGLE FOUND TO BE OUT OF LIMITS. REMOVED FLOOR ANGLE IAW IAW SRM 51-42-06-001-001-A01. LOCATED FASTENER HOLES IN NEW ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED NEW ANGLE IAW SRM 51-42-21-001-001 AND 51-42-06-001-001-A01. TOPCOATED FASTENERS IAW SRM 51-25-06-001-001-A01 AND APPLIED AV8 IAW SRM 51-21-11-001-001-A01.

Part: FRAME — CORRODED (BS 310 S24-25L) · airframe 21,318 hrs · 15,408 cycles

RFD - C CHECK - FOUND CORROSION ON FRAME AT FS 310 FROM STRINGERS 25L - 24L. REMOVED CORROSION ON FRAME IAW SRM 51-21-06-001-001-A01. CORROSION BLENDED ON ATTACH FLANGE OF FRAME 310.0 IS 4.6"L X 0.6"W X .004"D, ORIGINAL MATERIAL THICKNESS IS .050" REMAINING MATERIAL IS .046" WITHIN LIMITS OF SRM 53-21-06-101-002-A01. TREATED AND ALODINED IAW SRM 51-21-11-001-001-A01. PRIMED IAW SRM 51-25-06-001-001-A01 AND TOP COATED IAW SRM 51-25-16-001-001-A01. APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: FRAME — CORRODED (BS 310 S26L/R) · airframe 21,318 hrs · 15,408 cycles

C CHECK - FOUND CORROSION ON FRAME AT FS310 FROM STRINGER 26R TO 26L. REMOVED CORROSION ON FRAME IAW SRM 51-21-06-001-001-A01. ORIGINAL THICKNESS IS .050". MAX MATERIAL REMOVED .004", REMAINING MATERIAL IS .046", WITHIN LIMITS IAW SRM 53-21-06-101-002-A01. TREATED IAW SRM 51-21-11-001-001-A01. PRIMED AND PAINTED IAW 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 21,318 hrs · 15,408 cycles

C CHECK - PAX DOOR ANGLE, KICKPLATE CORRODED LOWER. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL IS .063, REMOVED .015, REMAINING MATERIAL IS .048. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. REMOVED KICKPLATE IAW SRM 51-42-06-001-001-A01. INSPECTED FOR CORROSION AND APPLIED CORROSION PREVENTATIVE PROCEDURES IAW SRM 51-21-11-001-001-A01. APPLIED PROTECTIVE PAINT IAW SRM 51-25-00-001-001-A01. PREPARED NEW KICKPLATE ANGLE IAW SRM 511-42-06-001-001-A01. TREATED AND PRIMED HOLES IAW SRM 51-21-11-001-001-A01. INSTALLED KICKPLATE IAW SRM 51-42-06-001-001-A01. PAINTED FASTENERS IAW SRM 51-25-16-001-001-A01. APPLIED CORROSION PREVENTATIVE COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: BEAM — CRACKED (BS 280) · airframe 21,318 hrs · 15,408 cycles

C CHECK - BOTH RT AND LT 280 BEAMS CRACKED AND CORRODED. REMOVED LT AND RT 280 BEAM IAW SRM 51-42-13-001-001-A01 AND 51-42-06-001-001-A01. PREPARED NEW 280 BEAM IAW SRM 51-40-11-001-001-A01 AND REO 670-53-11-047. PERFORMED CUTLINE ON BEAM IAW REO 670-53-11-047. BLENDED LT AND RT FLOORBEAM TO PROVIDE CLEARANCE TO FACILITATE FS 280 BEAM INSTALLATION IAW REO 670-53-11-045. PERFORMED LPI ON BEAM CUTLINE, NO CRACKS NOTED AT THIS TIME. INSTALLED LT AND RT 280 BEAM IAW REO 670-53-11-047. TOP COATED ALL FASTENERS AS REQUIRED IAW SRM 51-25-16-001-001-A01. APPLIED CORROSION INHIBITING COMPOUND TO AFFECTED AREAS IAW SRM 51-21-11-001-001-A01.

Part: FRAME — CORRODED (BS 501 S22-23L) · airframe 21,318 hrs · 15,408 cycles

C CHECK - FOUND CORROSION ON FRAME FS 501 BETWEEN STRINGERS 23L TO 22L. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDED AREA ORIGINAL THICKNESS IS .050", REMAINING MATERIAL IS .047". BLEND IS WITHIN LIMITS OF SRM 53-31-06-101-003-A01. TREATED AND PRIMED IAW SRM 51-21-11-001-001-A01 AND 51-25-06-001-001-A01. PAINTED IAW SRM 51-25-16-001-001-A01 AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: FRAME — CORRODED (BS 501 S25L/R) · airframe 21,318 hrs · 15,408 cycles

C CHECK - FOUND CORROSION ON FRAME FS501 BETWEEN STRINGERS 25L TO 25R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDED AREA ORIGINAL THICKNESS IS .050", REMAINING MATERIAL IS .047". BLENDS ARE WITHIN LIMITS OF SRM 53-31-06-101-003-A01. TREATED AND PRIMED IAW SRM 51-21-11-001-001-A01 AND 51-25-06-001-001-A01. PAINTED IAW SRM 51-25-16-001-001-A01 AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: FRAME — CORRODED (BS 565 S26-27L) · airframe 21,318 hrs · 15,408 cycles

C CHECK - FOUND CORROSION ON FRAME FS565 BETWEEN STRINGERS 27 TO 26L ON BOTH FWD AND AFT SIDES OF FRAME. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDED AREA ON ATTACH ANGLE HAS ORIGINAL THICKNESS IS .050", REMAINING MATERIAL IS .048". BLEND ON WEB HAS ORIGINAL THICKNESS OF .050" AND REMAINING MATERIAL IS .048" BOTH BLENDS ARE WITHIN LIMITS OF SRM 53-31-06-101-003-A01. TREATED AND PRIME IAW SRM 51-21-11-001-001-A01 AND 51-25-06-001-001-A01. PAINTED IAW SRM 51-25-16-001-001-A01 AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: FRAME — CORRODED (BS 485 S25L-26R) · airframe 21,318 hrs · 15,408 cycles

C CHECK - FOUND CORROSION ON FRAME FS485 BETWEEN STRINGERS 26R TO 25L. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDS ARE WITHIN LIMITS OF SRM 53-31-06-101-003-A01. TREATED AND PRIMED IAW SRM 51-21-11-001-001-A01 AND 51-25-06-001-001-A01. PAINTED IAW SRM 51-25-16-001-001-A01 AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: SKIN — CORRODED (BS 517-501) · airframe 21,318 hrs · 15,408 cycles

C-CHECK, FOUND CORROSION ON DOUBLER AROUND RIVETS FROM FS 517 TO FS 501 BETWEEN STRINGERS 26L - 26R. AREA OF CORROSION IS FOUND TO BE LOCATED IN A NO DAMAGE ALLOWED AREA IAW SRM 53-31-01-101-003-A01. REMOVED CORROSION ON DOUBLER IAW SRM 51-21-06-001-001-A01. BLEND ON INNER ADF ANTENNA DOUBLER IS 12.0" LONG 4.8" WIDE AND .003" DEEP, ORIGINAL THICKNESS IS .080", REMAINING MATERIAL IS .077" OVER 20 PERCENT OF DOUBLER AREA BLENDED SENT TO MFG FOR ENGINEERING. PERFORMED ECI ON ADF ANTENNA DOUBLER WHERE CORROSION WAS REMOVED. NO CRACKS OR CORROSION FOUND AT THIS TIME IAW NDTM ECI 51-20-006-250-A01. ETCHED AFFECTED AREA AND ALODINED IAW SRM 51-21-11-001-001-A01. PRIMED AND TOP COATED IAW SRM 51-25-16-001-001-A01.

Part: FRAME — CORRODED (BS 517 S25L-26R) · airframe 21,318 hrs · 15,408 cycles

C CHECK - FOUND CORROSION ON FRAME FS 517 BETWEEN STRINGERS 25L TO 26R. BLENDED AND REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDED AREA ORIGINAL THICKNESS IS .050" DEEPEST BLEND .003" REMAINING MATERIAL IS .047" AND WITHIN LIMITS OF SRM 53-31-06-101-003-A01. TREATED AND PRIME IAW SRM 51-21-11-001-001-A01 AND 51-25-06-001-001-A01. PAINTED IAW SRM 51-25-16-001-001-A01 AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: FRAME — CORRODED (BS 549 S26-27L) · airframe 21,318 hrs · 15,408 cycles

C CHECK - FOUND CORROSION ON FRAME FS 549 BETWEEN STRINGERS 27 TO 26L. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDED AREA ORIGINAL THICKNESS IS .050", REMAINING MATERIAL IS .048". BLEND IS WITHIN LIMITS OF SRM 53-31-06-101-003-A01. TREATED AND PRIMED IAW SRM 51-21-11-001-001-A01 AND 51-25-06-001-001-A01. PAINTED IAW SRM 51-25-16-001-001-A01 AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: FRAME — CORRODED (BS 295 S25-27L) · airframe 21,318 hrs · 15,408 cycles

C-CHECK - FOUND CORROSION ON FRAME AT FS 295 FROM STRINGER 27 TO 25L. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDED 2 AREAS. ONE AT THE ATTACH FLANGE BETWEEN 25L-26L MEASURED 2.0"L X 0.6"W X .002" DEEP, SECOND BLEND ON ATTACH FLANGE BETWEEN STRINGER 27-26L AND MEASURES 2.7"L X 0.6"W X .002" DEEP. ORINGINAL THICKNESS IN BOTH AREAS IS .050" REMAINING MATERIAL IN BOTH AREAS IS .048" AND FOUND TO BE WITH IN LIMITS OF SRM 53-21-06-101-002-A01. ETCHED AND ALODINED IAW SRM 51-21-11-001-001-A01. PRIMED AND PAINTED IAW 51-25-06-001-001-A01, 51-25-16-001-001-A01.

Part: SKIN — CORRODED (BS 485-517) · airframe 21,318 hrs · 15,408 cycles

C-CHECK - LOWER FUSELAGE SKIN HAS SPOTS OF CORROSION AROUND FASTENER HOLES AT FS485 TO FS517. BLENDED CORROSION ON LOWER FUSELAGE UNDER ADF ANTENNA BETWEEN FS485-517. IAW SRM 51-21-06-001-001-A01. BLENDED AREA IS 24.0" LONG 10.5" WIDE IN A "NO DAMAGE ALLOWED AREA". 9 AREAS BLENDED, DEEPEST BLEND IS .010". ORIGINAL THICKNESS IS 0.150", REMAINING MATERIAL IS 0.140", SENT TO MFG FOR ENGINEERING. PERFORMED ECI ON FUSELAGE SKIN UNDER ADF ANTENNA WHERE CORROSION WAS REMOVED. NO CRACKS OR CORROSION FOUND AT THIS TIME IAW NDTM ECI 51-20-006-250-A01. BLENDED OUT TO SMOOTH CONTOUR AND REINSTALLED FASTENERS IAW REO 670-53-31-165. COMPLETED ALL WORK IAW REO 670-53-31-165.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 21,318 hrs · 15,408 cycles

C-CHECK - FLOOR ANGLE GOING INTO COCKPIT 221 ALF IS CORRODED. REMOVED CORRODED FLOOR ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED FASTENER HOLES IN NEW ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED FLOOR ANGLE IAW SRM 51-42-21-001-001-A01. TOP COATED ALL FASTENERS AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-25-16-001-001-A01 AND 51-21-11-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 21,318 hrs · 15,408 cycles

C-CHECK - RT SIDE SEAT TRACK HAS AREAS OF CORROSION BETWEEN FS708 AND FS761. BLENDED CORROSION ON RT SIDE SEAT TRACK. ORIGINAL THICKNESS .260, BLENDED .037, REMAINING MATERIAL .223, MAXIMUM ALLOWABLE .035. FOUND BLENDED AREA TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED RT SIDE SEAT TRACK IAW AMM 53-00-49-000-801-A03. CUT NEW BULK SEAT TRACK TO LENGTH. PREPARED FASTENER HOLES IAW SRM 51-40-11-001-001-A01. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 21,318 hrs · 15,408 cycles

C-CHECK - LT SIDE SEAT TRACK HAS AREAS OF CORROSION BETWEEN FS708 AND FS761. BLENDED CORROSION ON LT SIDE SEAT TRACK. ORIGINAL THICKNESS .260, BLENDED .040, REMAINING MATERIAL .220, MAXIMUM ALLOWABLE .035. FOUND BLENDED AREA TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED LT SIDE SEAT TRACK IAW AMM 53-00-49-000-801-A03. CUT NEW BULK SEAT TRACK TO LENGTH. PREPARED FASTENER HOLES IAW SRM 51-40-11-001-001-A01. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 814-863) · airframe 21,318 hrs · 15,408 cycles

C-CHECK - RT SIDE SEAT TRACK HAS CORROSION PRESENT BETWEEN FS814 AND FS863. BLENDED CORROSION ON RT SIDE SEAT TRACK, ORIGINAL THICKNESS .260, REMOVED .040, MAX ALLOWABLE IS .035, REMAINING MATERIAL IS .220. BLEND IS OUT OF LIMITS IAW REO 670-53-00-013. REMOVED AND INSTALLED NEW SIDEWALL SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 379) · airframe 21,318 hrs · 15,408 cycles

C CHECK - CORROSION FOUND ON SEAT TRACK LOCATED ON LBL 2700 BETWEEN FS364 AND FS379. BLENDED CORROSION ON FLOOR SEAT TRACK, ORIGINAL THICKNESS .260, REMOVED .039, MAX ALLOWABLE IS .035, REMAINING MATERIAL IS .221. BLEND IS OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK IAW IAW AMM 53-00-49-000-801-A03. CUT OUT CORRODED AREA AND SPLICED IN NEW SEAT TRACK IAW REO 670-53-00-074. PREPARED FASTENER HOLES IAW SRM 51-40-11-001-001-A01. INSTALLED SERVICEABLE SEAT TRACK AT FS376-379 AND NEW SEAT TRACK AT AT FS364-376 IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 21,318 hrs · 15,408 cycles

C-CHECK - RT FLOOR SEAT TRACK HAS CORROSION NEAR FASTENER COUNTERSINK BETWEEN FS 485-581. BLENDED CORROSION ON RT FLOOR SEAT TRACK, ORIGINAL THICKNESS .110, REMOVED .038, MAX ALLOWABLE IS .035, REMAINING MATERIAL IS .072. BLEND IS OUT OF LIMITS IAW REO 670-53-00-013. REMOVED RT FLOOR SEAT TRACK FS485 - FS581 IAW AMM 53-00-49-000-801-A03. CUT BULK MATERIAL TO LENGTH. PREPARED FASTENER HOLES ON RT FLOOR SEAT TRACK IAW SRM 51-40-11-001-001-A01. INSTALLED NEW TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 814-863) · airframe 21,318 hrs · 15,408 cycles

C-CHECK - LT SIDE SEAT TRACK HAS AREAS OF CORROSION BETWEEN FS814 AND FS863. BLENDED CORROSION ON LT SIDE SEAT TRACK. ORIGINAL THICKNESS .110, BLENDED .037, MAX ALLOWABLE .035, REMAINING MATERIAL .073. FOUND BLENDED AREA TO BE OUT OF LIMITS IAW REO 670-53-00-013. R & R LT SIDE SEAT TRACK WITH NEW TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 379-477) · airframe 21,318 hrs · 15,408 cycles

C-CHECK - LT SIDE SEAT RAIL HAS AREAS OF CORROSION BETWEEN FS379-477. BLENDED CORROSION ON LT SIDE SEAT RAIL, ORIGINAL THICKNESS .260, REMOVED .025, MAX ALLOWABLE IS .035, REMAINING MATERIAL IS .235. BLEND IS WITHIN LIMITS IAW REO 670-53-00-013. ALUMINUM PREP AND ALODINED LT SIDE SEAT TRACK IAW AMM 51-21-11.

Part: SEAT TRACK — CORRODED (BS 669-708) · airframe 21,318 hrs · 15,408 cycles

C-CHECK - LT SIDE SEAT TRACK HAS AREAS OF CORROSION BETWEEN FS669-708. BLENDED CORROSION ON LT SIDE SEAT TRACK, ORIGINAL THICKNESS .260, REMOVED .045, MAX ALLOWABLE IS .035, REMAINING MATERIAL IS .215. BLEND IS OUT OF LIMITS IAW REO 670-53-00-013. REMOVED LT SIDE SEAT TRACK IAW AMM 53-00-49-000-801-A03. CUT BULK MATERIAL TO LENGTH. PREPARED FASTENER HOLES ON RH FLOOR SEAT TRACK IAW SRM 51-40-11-001-001-A01. INSTALLED NEW TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — GOUGED (BS 893) · airframe 21,318 hrs · 15,408 cycles

C-CHECK - GOUGES ON RT SIDE SEAT TRACK AT FS 893. BLENDED GOUGES ON RT SIDE SEAT TRACK. ORIGINAL THICKNESS .260, BLENDED .015, MAX ALLOWABLE .035, REMAINING MATERIAL .245. FOUND BLENDED AREA TO BE IN LIMITS IAW REO 670-53-00-013. ALUMINUM PREPPED AND ALODINED RT SEAT TRACK IAW SRM 51-21-11-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 21,318 hrs · 15,408 cycles

C-CHECK - RT SIDE SEAT TRACK HAS CORROSION BETWEEN FS 677-708. BLENDED CORROSION ON RT SIDE SEAT TRACK, ORIGINAL THICKNESS .260. REMOVED .042 MAX ALLOWABLE IS .035, REMAINING MATERIAL IS .218. BLEND IS OUT OF LIMITS IAW REO 670-53-00-013. R & R RT SIDE SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: STRINGER — CORRODED (BS 485-501 S20L) · airframe 21,318 hrs · 15,408 cycles

RFD - C CHECK - FOUND CORROSION ON STRINGER 20L BETWEEN FS485-FS501. REMOVED CORROSION FROM STR 20L AT FS485-FS501 IAW SRM 51-21-06-001-001-A01. 2 AREAS BLENDED 1ST BLEND MEASURES .5"X.5" AND .007" DEEP, 2ND BLEND WAS 1"X 1" AND .005" DEEP. ORIGINAL MATERIAL THICKNESS IS .080". BLEND FOUND TO BE WITHIN LIMITS IAW SRM 51-31-03-101-003-A01. TREATED IAW SRM 51-21-11-001-001-A01 PRIMED IAW SRM 51-25-06-001-001-A01, PAINTED IAW SRM 51-25-16-001-001-A01. APPLIED HARDCOAT TO AREA IAW SRM 51-21-11-001-001-A01.

Part: SILL — CORRODED (FUSELAGE) · airframe 21,318 hrs · 15,408 cycles

C-CHECK - CORROSION PRESENT ON AFT BAGGAGE DOOR SILL. REMOVED CORROSION IAW 51-21-06-001-001-A01, SRM, NO DAMAGE ALLOWED IAW SRM 53-61-23-101-001-A01. PERFORMED ECI ON AFT BAGGEAGE BAY DOOR SILL BLEANDED AREA. NO CRACKS OR CORROSION FOUND AT THIS TIME IAW NDTM ECI 51-20-006-250-A01. SENT TO MFG FOR ENGINEERING. COMPLETED REPAIR IAW REO 670-53-61-612 APPLIED FINISH TO REWORKED AREAS, APPLIED CORROSION INHIBITING COMPOUND.

Part: SKIN — CHAFED (LT AILERON) · airframe 21,318 hrs · 15,408 cycles

C CHECK - LT AILERON TO L/E SKIN CHAFING DAMAGE PRESENT. BLENDED CHAFE MARKS ON LT AILERON IAW SRM 51-21-06-001-001. MAX ALLOWABLE DAMAGE 25 PERCENT. ORIGINAL THICKNESS .090", DEEPEST AREA BLENDED NO MORE THAN .007". TREATED BLENDED AREAS IAW SRM 51-21-11-001-001, PRIMED AREAS IAW SRM 51-25-06-001-001, PAINTED AREAS IAW SRM 51-25-01-001-001.

Part: SLAT SYSTEM — FAILED · airframe 20,724 hrs · 15,000 cycles

SLATS FAIL. MDC INDICATED SLAT SYS MECHANICAL JAM IN FAULT HISTORY CW OPS TEST OF THE FLAP AND SLAT SYS IAW AMM TASK 27-50-00-710-801 NO DEFECTS NOTED CW VISUAL INSP OF SLATS AND SLAT TRACK ASSYS WITH SLATS EXTENDED AND RETRACTED NO DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SKIN — CHAFED (BS 980 S27) · airframe 19,772 hrs · 14,304 cycles

CHAFE ON FUSELAGE AT FS 980. LEFT OF STRINGER 27. CHAFE APPROX 2 INCHES LONG. BLENDED AWAY DAMAGE IAW REO 670-53-00-014. HFEC INSPECTED BLENDED AREA FOR CRACKS IAW NDTM PART 6, 53-00-000-250-A01, NO CRACKS NOTED. UT THICKNESS CK IAW NDTM PART 1, 51-20-004. FOUND WITHIN LIMITS IAW REO 670-53-00-014. COMPLETED REPAIR IAW REO 670-53-00-014.

Part: SKIN — CRACKED (BS 973 S27) · airframe 19,772 hrs · 14,304 cycles

CHAFE ON LOWER FUSELAGE SKIN AT FS 973.05 INCH LEFT OF STRINGER 27. ONE INCH FWD OF PREVIOUSLY BLENDED AREA. BLENDED OUT DAMAGE IAW REO 670-53-00-014. HFEC INSPECTED BLENDED AREA FOR CRACKS IAW NDTM PART 6, 53-00-000-250-A01. NO CRACKS NOTED. UT THICKNESS CHECK IAW NDTM PART 1, 51-20-004. FOUND WITHIN LIMITS IAW REO 670-53-00-014. COMPLETED REPAIR IAW REO 670-53-00-014.

Part: MOTOR — FAILED (CABIN DOOR) · airframe 19,248 hrs · 13,906 cycles

PDX - MAIN CABIN DOOR DIFFICULT TO OPEN. FOUND MCD POWER ASSIST CABLE HANGING UP IN MOTOR ASSY. REMOVED AND REPLACED MCD POWER ASSIST MOTOR ASSY IAW CRJ-700 AMM TASK 52-11-08-000-801-A02 AND TASK 52-11-08-400-801-A02. OPS CHECK GOOD. MCD NO LONGER DIFFICULT TO OPEN. RETURNED TO SERVICE.

Part: DOOR — MALFUNCTIONED (CABIN) · airframe 19,246 hrs · 13,905 cycles

SMF - FLIGHT ATTENDANT REPORTED THAT MAIN CABIN DOOR WAS DIFFICULT TO PUSH OPEN. INSPECTED DOOR MECHANISM WITH NO DEFECTS NOTED AND C/W OPS TEST IAW AMM 52-11-00-710-801. CHECKS GOOD. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: TRANSDUCER — MALFUNCTIONED (ZONE 700) · airframe 18,479 hrs · 13,317 cycles

PDX - NR 1 BRAKE APPEARS TO BE INOP. TROUBLESHOT TO FAULTY NR 1 WHEELSPEED TRANSDUCER. REMOVED AND REPLACED NR 1 WHEELSPEED TRANSDUCER IAW CRJ-700 AMM TASKS 32-44-01-000-801-A01 AND 32-44-01-400-801-A01. OP CHECK OF ANT-SKID CONTROL UNIT PASSED. TAXIED AIRCRAFT TO CHECK BRAKES. BRAKES OPERATE NORMALLY. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,248 hrs · 13,136 cycles

YYC - WHEN FIRST ENTERING CABIN OF STATIC AIRCRAFT (APU AND AIR CONDITIONING ON) NOTICED AN ODOR OF ELECTRICAL SMOKE. THE ODOR WAS NOT VERY STRONG AND HAS DIMINISHED SOMEWHAT. CYCLED PACK ONE AT A TIME, NO CHANGE IN ODOR. INSPECTED ALL CABIN LIGHTING BALLAST. NO DEFECTS NOTED. ODOR HAS DISSIPATED. INSPECTED AVIONICS COMPARTMENT FOR ANY SIGNS. NO ODOR NOTICED AT THIS TIME. ALL CABIN LIGHTING AND SIGNS WORKING NORMAL. ACFT OK TO RETURN TO SERVICE. NO PARTS REPLACED.

Part: COMPUTER — FAILED (HGS) · airframe 17,811 hrs · 12,747 cycles

PDX- 2 APPROACH WARNINGS RWY 10R PDX. DIVERT TO SEA 1 APPROACH WARN RWY 16R SEA IN VFR CONDITIONS A3 INOP. REMOVED AND REPLACED HGS COMPUTER, HGS RETURN TO SERVICE ACCOMPLISHED IAW T/C R343201, SYSTEM TEST GOOD. AIRCRAFT UPGRADED TO CAT III STATUS, AIRCRAFT PLACARD CHANGED TO CATII STATUS. AIRCRAFT RETURNED TO SERVICE.

Part: LINE — LEAKING (FUEL SYSTEM) · airframe 17,753 hrs · 12,691 cycles

LAX - FOUND POSSIBLE FUEL LEAK AT RT INBOARD REAR SPAR, FOUND LEAK AT S46 SCAVENGE PRESS DIFFERENTIAL SENSOR, CATEGORIZED LEAK AS DRIP IAW AMM 28-11-00-790-801, NOTE 3. FOUND FUEL LEAK AT PRESSURE SENSOR ELECTRICAL CONDUIT AT THE FLAIR AT THE SENSOR. REMOVED AND REPAIRED CONDUIT, AND REINSTALLED. FINISHED CLOSE OUT OF TASK 28-42-07-400-801-A01 BY FINISHING STEPS 2. E.(5) TRU (6)(E). OPS CHECK GOOD. NO LEAKS NOTED. RETURNED TO SERVICE.

Part: RELAY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 17,749 hrs · 12,688 cycles

SEA - EMERGENCY LIGHTS COME ON AND GO OFF INTERMITTENTLY. ALL SWITCHES IN NORMAL/ARMED POSITION. REPLACED EPSU BATTERY PACKS AND RELAY IAW AMM TASKS 33-51-17-000-801-A01. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 1000-1047) · airframe 17,729 hrs · 12,672 cycles

AFT CARGO DOOR FLOORBOARD SUPPORT ADJACENT TO THE DOOR SILL HAS MULTIPLE AREA OF CORROSION AT NUTPLATES AND ALONG THE INBD OF THE SILL BETWEEN FS 1000.00 AND FS 1047.00. REMOVED AFT CARGO DOOR LOWER SILL BY REMOVING APERTURE AND DRILLING OUT RIVETS, LOCK FASTENERS AND NUTPLATES FROM STRUCTURE. REMOVED PANELS 281KLW, 281ELW AND 281MLW TO FOM. REMOVED CORROSION IAW AMM 51-21-06-001-001-A01 PARA 1-2, 3A AND3D(1),(2). HFEC INSPECTED BLENDED AREAS FOR CRACKS IAW NDTM 51-20-006. NO CRACKS NOTED. MAPPED DAMAGE FOR ENGINEERING. REMOVED CARGO HOLD DOWN INTERCOSTALS AT SILL FROM X1000 TO X1031 BY REMOVING FASTENERS. ALODINED AND PRIMED BLENDED AREAS IAW SRM 51-25-06. INSTALLED FASTENERS REMOVED IAW SRM 51-42-06 AND 51-42-21. INSPECTED AREA PER REQUEST AND FOUND BLENDED AREA TO BE PAINT REMOVAL ONLY (NO MATERIAL LOSS). COMPLETED INSTALLATION OF LOWER SILL IAW SRM 51-42-06 AND REO 670-53-61-447. REINSTALLED PANELS REMOVED. RESTORED FINISH IAW SRM 51-21-16 AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11.

Part: ADAPTER — CORRODED (FUSELAGE) · airframe 17,729 hrs · 12,672 cycles

AIRCRAFT SKIN SURFACE WHERE UPPER TCAS ANTENNA ADAPTER PLATE CONTACTS HAS LIGHT CORROSION. BLENDED CORROSION FROM UPPER SKIN IAW SRM 51-21-06-001-A01 AND PARA D. PERFORMED THICKNESS CHECK IAW CRJ NDTM 51-20-004 MAX READ .060, MINIMUM READ .056-.004 MATERIAL REMOVED. MAPPED AREA FOR ENGINEERING. HFEC IAW NDTM PART 1, 51-20-006, NO CRACKS NOTED. COMPLETE REPAIR FOUND TO BE WITHIN LIMITS IAW REO 670-53-21-435 STEP1-5.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 17,729 hrs · 12,672 cycles

PDX - C4 - FUSELAGE EXTERIOR SKIN AROUND MCD APERTURE AFT SIDE HAS GOUGE MARKS APPROX 17 INCHES UP FROM BOTTOM EDGE OF DOOR, AREA AFFECTED IS 3/4 INCH BY 1/2 INCH. BLENDED AREA OF GOUGES TO REMOVE DAMAGE AND FOUND BLENDED AREA TO BE OUT OF LIMITS IAW 53-21-01. HFEC INSP AREA IAW NDTM PART 6, 53-00-000-250-A01. NO CRACKS NOTED. UT THICKNESS CHECK IAW CRJ 700 PART 1, 51-20-004-270-A01, HIGH .135 LOW .131. MAPPED FOR ENGINEERING. INSPECTED AREA OF BLEND AND FOUND IT TO BE WITHIN LIMITS IAW REO 670-53-21-434. PREPPED, PRIMED, AND PAINTED AREA IAW CRJ SRM 51-25-01.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,729 hrs · 12,672 cycles

FS 280 FLOORBEAM HAS A CRACK ON THE TOP FLANGE AT RBL 13.00. REMOVED DRIP TRAY ON RT SIDE AT 280 FLOORBEAM IAW SRM 51-42-13. REMOVED THE RT SIDE OF THE 280 FLOORBEAM AND THE ATTACHING INTERCOSTAL IAW REO 670-53-11-047. CUT NEW SECTION OF 280 FLOORBEAM, LOCATED AND DRILLED UP HOLES, ALODINED AND PRIMED FLOORBEAM IAW REO670-53-11-047. PERFORMED HFEC OF CUTOUT IAW NDTM 51-20-006. NO CRACKS NOTED. INSTALLED REPLACEMENT FLOORBEAM RT SECTION, INSTALLED SINGLE INTERCOSTAL AND RT DRIP TRAY IAW REO 670-53-11-047.

Part: FLOORBEAM — DAMAGED (BS 280) · airframe 17,729 hrs · 12,672 cycles

FS 280.0 BEAM SPLICE AT AIRCRAFT CENTER HAS ELONGATED HOLES. LOCATED AND DRILLED NEW SPLICE PLATE. INSTALLED SPLICE PLATE IAW 51-42-06 IAW SRM 51-42-06.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 17,729 hrs · 12,672 cycles

FS 280 FLOORBEAM HAS AREAS OF CORROSION ON THE TOP FLANGE BETWEEN LBL 6.00 AND 18.00. BLENDED CORRODED AREAS PLUS 2 ADDITIONAL AREAS OUTBOARD OF THESE LOCATIONS (6.00 AND 18.00) IAW REO 670-53-11-046. FOUND REMAINING MATERIAL TO MEASURE NO LESS THAN .036 INCHES. REMOVED NUTPLATES AT CORRODED AREA AND SINGLE BLIND RIVET FOR ACCESS PER REO 670-53-11-046. .036 INCH REMAINING MATERIAL WITHIN LIMITS OF REO 670-53-11-046. FPI INSPECTED AT BLENDED AREA FOR CRACK IAW NDTM PART 1, 51-220-08 NO CRACKS NOTED. REPLACED THE NUTPLATES AND THE SINGLE BLIND RIVET THAT WERE REMOVED FOR THE CORROSION REMOVAL IAW 51-42-15. ALODINED, PRIMED AND PAINTED IAW 51-25-01 OF THE SRM.

Part: ROLL PIN — DAMAGED (SERVICE DOOR) · airframe 15,138 hrs · 10,638 cycles

SEA - FLIGHT 2536 - SERVICE DOOR WILL NOT CLOSE. MAINTENANCE REPLACED THE ROLL PIN FOR THE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED · airframe 14,981 hrs · 10,526 cycles

BOI - FLIGHT 2590 - RECEIVED A XFLOW PUMP CAUTION MESSAGE. RETURNED TO THE GATE. PLACED THE SYSTEM ON MEL 28-13-10. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED · airframe 14,931 hrs · 10,486 cycles

FLIGHT 2606. AVIONICS FAN CAUTION DURING TAXI, SELECTED ALTERNATE IAW THE CHECKLIST. AFTER TAKEOFF IT ILLUMINATED AGAIN, SELECTED NORMAL AND IT WENT OUT. DURING TAXI IN, LIGHT DID NOT COME ON. MAINTENANCE PLACED ON MEL 21-24-3. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (ANTI SKID SYS) · airframe 15,378 hrs · 10,998 cycles

PDX - ON TAXI THE ANTI-SKID RELEASES AND GRABS WHEN SLOWING THROUGH ABOUT 10 KNOTS. THE TRANSITION IS NOT SMOOTH. MAINTENANCE FOUND A MDC FAULT FOR THE ANTI-SKID CONTROL UNIT. REPLACED THE ANTI SKID CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PUMP — WARNING LIGHT (CROSSFLOW) · airframe 14,536 hrs · 10,224 cycles

GEG - ON FLIGHT 2517, RECEIVED XFLOW PUMP CAUTION MESSAGE. AIRCRAFT RETURNED TO FIELD. ACCOMPLISHED UNEVENTFUL LANDING. PLACED ON MEL IAW REF 28-13-10. AIRCRAFT RETURNED TO SERVICE.

Part: DETECTOR — FALSE INDICATION (FIRE DETECTION) · airframe 14,043 hrs · 9,906 cycles

PDX - FLIGHT 2555, ON POWER UP RECEIVED A FIRE SYSTEM FAULT MESSAGE. MAINTENANCE REPLACED THE NR 2 FORWARD SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 13,040 hrs · 9,256 cycles

PSP - FLIGHT 2580, DURING FLIGHT CONTROL CHECK THE MASTER CAUTION CAME ON FOR THE OUTBOARD SPOILERS (SPOILERONS AND FLIGHT SPOILERS). RETURNED TO THE GATE. MAINTENANCE REPLACED THE PCU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (CROSSFLOW PUMP) · airframe 12,948 hrs · 9,197 cycles

PDX - FLIGHT 2509 RETURN TO THE GATE FOR A XFLOW PUMP CAUTION ILLUMINATED WHEN THE FUEL SYSTEM IS SELECTED TO MANUAL PRIOR TO TAKEOFF. MAINTENANCE WAS UNABLE TO DUPLICATE THE PROBLEM. GROUND RAN BOTH ENGINES AND THE SYSTEM TESTED NORMALLY. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DADC — MALFUNCTIONED · airframe 12,813 hrs · 9,100 cycles

PDX - WHILE IN TURBULENCE FO'S PFD DISPLAY LOST AIRSPEED HEADING AND ALTITUDE INFORMATION. AFTER 20-30 SECONDS DISPLAY BACK TO NORMAL. MAINTENANCE REPLACED THE DADC. OPERATIONAL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE.

Part: RADOME — DAMAGED (NOSE) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - NOSE RADOME HAS EVIDENCE OF LIGHTNING STRIKE BURN THROUGH WITH DISBONDING ON INTERNAL SURFACE. REPAIRED IAW SRM 53-81-80.

Part: SKIN — DAMAGED (BS 202 S15R) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - LIGHTNING STRIKE DAMAGE ON EDGE OF SKIN AT FS 202.00 STRINGER 15R. REPAIRED IAW REO670-53-21-257.

Part: PANEL — TOOL DAMAGE (FUSELAGE) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - FUSELAGE OVERWING PANEL 172BR HAS 1 FASTENER HOLE WITH TOOLING DAMAGE. REPAIRED IAW REO670-53-82-337AND SRM 51-42-06.

Part: HINGE — DAMAGED (LT MLG DOOR) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - LEFT MAIN LANDING GEAR DOOR UPPER HINGE PANEL HAS FASTENERS WITH HEADS STRIPPED OUT. REPAIRED IAW SRM 51-42-02.

Part: SKIN — DAMAGED (BS 250 S17R) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - LIGHTNING STRIKE DAMAGE AT STRINGER 17R 4.7" FORWARD OF FS 250.00. REPAIRED IAW REO670-53-21-257 AND SRM 51-42-06.

Part: SKIN — DAMAGED (ESCAPE HATCH) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - CREW ESCAPE HATCH SKIN HAS 3 SMALL NICKS AROUND OUTER HANDLE CUTOUT RIGHT HAND SIDE. REPAIRED IAW SRM 52-00-01, 51-21-11.

Part: SKIN — CORRODED (FUSELAGE) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - UPPER TCAS ANTENNA MOUNT SKIN HAS CORROSION. REPAIRED IAW SRM 51-21-06, 53-21-01, AND 51-21-11.

Part: SKIN — DAMAGED (BS 210) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - LIGHTNING STRIKE DAMAGE AT STRINGER 15R 0.9" FORWARD OF FS 210.00. REPAIRED IAW REO670-53-21-257.

Part: PANEL — CHAFED (RT TE FLAP) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - RIGHT FLAP PANEL 684AB CHAFED ON LEADING EDGE. REPAIRED IAW SRM 57-52-01, 51-21-11.

Part: SKIN — DAMAGED (BS 302 S20R) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - SMALL NICK IN EXTERIOR FUSELAGE SKIN, RIGHT SIDE AT FS 302.00 AND STRINGER 20R. REPAIRED IAW SRM 53-21-01.

Part: SKIN — DAMAGED (BS 210) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - LIGHTNING STRIKE DAMAGE AT STRINGER 15R 2.5" FORWARD OF FS 210.00. REPAIRED IAW REO670-53-21-257.

Part: SKIN — DAMAGED (TE FLAP) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - 14 EACH, LOOSE RIVETS ON UPPER SKIN OF LEFT OUTBOARD FLAP. REPAIRED IAW REO670-57-53-05.

Part: MOUNT — CORRODED (GALLEY MOUNT) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - FORWARD GALLEY INBOARD AFT MOUNT FOOT HAS CORROSION. REPAIRED IAW CMM 25-32-97.

Part: SKIN — DAMAGED (BS 296 S16R) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - LIGHTNING STRIKE DAMAGE AT FS 296.00 4.7" DOWN OF STRINGER 16R. REPAIRED IAW REO670-53-21-257 AND SRM 51-42-06.

Part: SKIN — DAMAGED (BS 296 S16R) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - LIGHTNING STRIKE DAMAGE AT FS 296.00 3.7" DOWN OF STRINGER 16R. REPAIRED IAW REO670-53-21-257 AND SRM 51-42-06.

Part: SKIN — DAMAGED (BS 453 S15R) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - LIGHTNING STRIKE DAMAGE AT FS 453.00 2.7" DOWN OF STRINGER 15R. REPAIRED IAW REO670-53-21-257.

Part: SKIN — DAMAGED (BS 296) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - LIGHTNING STRIKE DAMAGE AT FS 296.00 2.7" DOWN OF STRINGER 16R. REPAIRED IAW REO670-53-21-257 AND SRM 51-42-06.

Part: SKIN — DAMAGED (BS 193 S16R) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - LIGHTNING STRIKE DAMAGE ON DOOR CUTOUT AT FS 193.00 6" ABOVE STRINGER 16R. REPAIRED IAW REO670-53-21-257 AND SRM 51-42-06.

Part: SKIN — DAMAGED (BS 296 S17R) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - LIGHTNING STRIKE DAMAGE AT STRINGER 17R 4.5" AFT OF FS 296.00. REPAIRED IAW REO670-53-21-257 AND SRM 51-42-06.

Part: SKIN — DAMAGED (BS 310 S16R) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - LIGHTNING STRIKE DAMAGE AT STRINGER 16R 5.5" FORWARD OF FS 310.00. REPAIRED IAW REO670-53-21-257 AND SRM 51-21-06.

Part: SKIN — DAMAGED (BS 296 S17R) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - LIGHTNING STRIKE DAMAGE AT STRINGER 17R 3.5" AFT OF FS 296.00. REPAIRED IAW REO670-53-21-257. AND SRM 51-42-06.

Part: SKIN — CORRODED (FUSELAGE) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - 2 SMALL AREAS OF SUSPECTED SURFACE CORROSION ON FUSELAGE SKIN BARE METAL/FASTENER JUST FORWARD AND BELOW PAX DOOR FUSELAGE HINGE HALF FORWARD CAP. REPAIRED IAW SRM 51-21-06 AND 51-25-06.

Part: SKIN — DAMAGED (BS 296 S17R) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - LIGHTNING STRIKE DAMAGE AT STRINGER 17R 4.7" FORWARD OF FS 296.00. REPAIRED IAW REO670-53-21-257 AND SRM 51-42-06.

Part: SKIN — DAMAGED (BS 296 S18R) · airframe 12,746 hrs · 9,062 cycles

C3 OKC-LIGHTNING STRIKE DAMAGE AT STRINGER 18R 7.5 INCH AFT OF FS 296.00. REPAIRED IAW REO670-53-21-257 AND SRM 51-42-06.

Part: ANGLE — CRACKED (BS 280) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - FS 280 AFT SIDE BETWEEN LBL 9 AND RBL 9 PREVIOUS REPAIR ANGLE HAS SUSPECT CRACK IN RADIUS. REPAIRED IAW SRM 51-42-06.

Part: SKIN — CHAFED (LT TE FLAP) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - LEFT INBOARD FLAP INNER SKIN CHAFED BY BONDING WIRE AT 2ND FROM INBOARD FLAP VANE GUIDE BEHIND PANEL 584BB. REPAIRED IAW SRM 51-21-11, 57-52-01.

Part: ACCESS PANEL — CHAFED (LT WING) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - LEFT WING INBOARD FLAP ACCESS PANEL 584LB IS CHAFED ON OUTER SURFACE BY ACTUATOR CUTOUT. REPAIRED IAW SRM 51-21-11, 57-52-01.

Part: ACCESS PANEL — CHAFED (LT WING) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - LEFT WING INBOARD FLAP ACCESS PANEL 584GB IS CHAFED ON OUTER SURFACE BY ACTUATOR CUTOUT. REPAIRED IAW SRM 51-21-11, 57-52-01.

Part: SKIN — GOUGED (NR 1 SLAT) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - LOWER AFT EDGE OF RIGHT NR 1 SLAT SKIN IS GOUGED/CHAFED BELOW INBOARD METAL WIRE CONDUIT. REPAIRED IAW SRM 53-00-01, 51-12-00.

Part: SKIN — CHAFED (RT SLAT) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - RIGHT OUTBOARD SLAT INBOARD TRAILING EDGE IS CHAFED AND HAS HIGH METAL. REPAIRED IAW SRM 57-42-01.

Part: DRAIN PAN — CRACKED (BS 280) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - FOUND FS 280 AT RBL 9 HAS A SUSPECTED CRACK COMING OUT OF FASTENER HOLE ATTACHING DRAIN PAN. REPAIRED IAW SRM 51-40-11, 51-42-06.

Part: ACCESS PANEL — CHAFED (LT WING) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - LEFT WING INBOARD FLAP ACCESS PANEL 584EB IS CHAFED ON OUTER SURFACE BY ACTUATOR CUTOUT. REPAIRED IAW SRM 57-52-01, 51-21-11, AND 51-25-06.

Part: PANEL — CORRODED (WING) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - BUTE DOOR PANEL 691JB HAS LIGHT SURFACE CORROSION IN FASTENER HOLES. REPAIRED IAW SRM 51-21-06, 51-21-11, AND 51-25-16.

Part: PANEL — CHAFED (TE FLAP) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - FLAP PANEL 684ET CHAFED ON LEADING EDGE. REPAIRED IAW SRM 51-25-16, 51-21-11.

Part: PANEL — CHAFED (RT TE FLAPS) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - RIGHT FLAP PANEL 684GB CHAFED ON LEADING EDGE. REPAIRED IAW SRM 51-25-16, 51-21-11.

Part: PANEL — GOUGED (RT WING) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - RIGHT WING LEADING EDGE PANEL 622AR IS GOUGED/CHAFED ON LEADING EDGE. REPAIRED IAW SRM 57-00-01, 51-12-00.

Part: PANEL — CORRODED (WING) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - BUTE DOOR PANEL 691KB HAS LIGHT SURFACE CORROSION IN FASTENER HOLES. REPAIRED IAW SRM 51-21-06, 51-25-16.

Part: PANEL — CHAFED (TE FLAP) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - FLAP PANEL 684EB CHAFED ON LEADING EDGE. REPAIRED IAW SRM 51-25-16, 51-21-11.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 12,746 hrs · 9,062 cycles

C3 OKC - FUSELAGE SKIN AT FORWARD EDGE OF PASSENGER DOOR CUTOUT LOWER SIDE HAS SEVERAL NICKS AND GOUGE. REPAIRED IAW SRM 53-00-01, 51-25-06.

Part: SENSOR — MALFUNCTIONED (LT A/C PACK) · airframe 12,639 hrs · 8,996 cycles

PDX - FLIGHT 2518 - LEFT AIR CONDITIONING PACK CYCLES OFF AND ON SEVERAL TIMES IN FLIGHT. LEFT PACK SELECTED OFF PER THE CHECKLIST PROCEDURE. LEFT PACK READINGS OBSERVED TO BE ERRATIC AND VARIABLE WITH PACK ON OR OFF. MAINTENANCE PLACED ON MEL 21-51-1A. 3/11. MAINTENANCE REPLACED THE LEFT PACK INLET TEMP SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CAUTION MESSAGE — FALSE ACTIVATION (FUEL LOW) · airframe 11,239 hrs · 8,069 cycles

BUR - FLIGHT 2508, ON TAXI RECEIVED A FUEL FLOW CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE COMPLIED WITH SERVICE LETTER CRJ-700/900/SL/28007. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SHUTOFF VALVE — INOPERATIVE (RT ENGINE) · airframe 9,919 hrs · 7,124 cycles

PDX - ON FLIGHT 2503, RETURNED TO GATE, RIGHT ENGINE BLEED CAUTION ON TAXI OUT. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE PRESSURE REGULATOR SHUTOFF VALVE. LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ODOR — DETECTED (CABIN) · airframe 9,841 hrs · 7,067 cycles

PDX - STRONG SMELL OF BURNING OIL IN CABIN EARLY IN FLIGHT. DISSIPATED WITHIN TIME. WITH APU, RAN AIRCRAFT BLEED AIR WITH L AND R PACKS FOR 7 HOURS AT DIFFERENT BLEED SETTINGS AND DIFFERENT TEMP AND LOAD SETTINGS. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WARNING LIGHT — ILLUMINATED (RT ENGINE) · airframe 9,693 hrs · 6,966 cycles

BOI - ON FLIGHT 4276, RETURNED TO GATE, RIGHT ENGINE BLEED MASTER CAUTION MESSAGE APPEARED DURING TAXI OUT IT WENT OFF WHEN PULLING IN TO GATE. MAINTENANCE INSPECTED DUCT, VERIFIED MDC NO CURRENT MESSAGE OR HISTORY FAULTS. GROUND RUN, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 9,378 hrs · 6,760 cycles

SEA - EMERGENCY LIGHT WILL NOT ILLUMINATE. REMOVED AND INSTALLED EMEREGENCY LIGHT BATTERIES (4) EA IAW AMM 33-51-17-000-802-A01 AND 33-51-17-400-801-A01, OPS CHECKS GOOD IAW AMM 33-51-00-710-801 AND 33-51-17-710-801. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (APU) · airframe 9,189 hrs · 6,631 cycles

GEG - ON TAXI FOR FLIGHT 4309, RECEIVED A APU BATT CHARGER STATUS MESSAGE. RETURNED TO THE GATE. APU BATTERY REPLACED ON WC 310ME2470051 DATED 01-19-06 BATTERY BAD FROM STOCK. REINSTALLED ORIGINAL BATTERY IAW AMM 24-32-03 CHECKS GOOD STATUS MESSAGE CLEARED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WARNING LIGHT — FALSE ACTIVATION (RT WING ANTIICE) · airframe 8,460 hrs · 6,145 cycles

PDX - RIGHT WING ANTI-ICE CAUTION CAME ON AFTER THE SYSTEM HAD BEEN ON 5 MINUTES. WENT OFF AFTER THE WING A/I CROSSBLEED WAS SELECTED "LEFT" AS PER THE CHECKLIST. MAINTENANCE FOUND A VALVE DISAGREE MESSAGE IN THE MDC. PERFORMED A OPERATIONAL TEST OF THE SYSTEM WITH NO DEFECTS. NO FAULTS REOCCURRED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CYLINDER — CORRODED (NLG STRUT) · airframe 8,437 hrs · 6,131 cycles

YYC - NLG OUTER CYLINDER HAS AREAS OF CORROSION. MAINTENANCE REPAIRED IAW QX EA R-32-197, REO 670-32-21-073, ASTM 1444-01 AND SCR 0008-04 REV C.

Part: FRAME — DAMAGED (THRUST REVERSER) · airframe 8,437 hrs · 6,131 cycles

YYC - RIGHT ENGINE LOWER FAN COWL HAS FRETTING DAMAGE ON FRAME JUST AFT OF CENTER LATCH APPROX NACELLE STA ESTA 155.00. MAINTENANCE REPAIRED IAW QX EA R-78-68, REO 370-78-34-460 STEPS 4 AND 5.

Part: FRAME — DAMAGED (THRUST REVERSER) · airframe 8,437 hrs · 6,131 cycles

PDX: RIGHT ENGINE UPPER FAN COWL HAS FRETTING DAMAGE ON THRUST REVERSE FIXED FRAME JUST AFT OF CENTER LATCH APPROX NACELLE STA STA 155.00. MAINTENANCE REPAIRED IAW REO 670-78-34-460 AND QX EA R-78-68.

Part: INTERCOSTAL — BROKEN (VERTICAL STAB) · airframe 8,437 hrs · 6,131 cycles

YYC - VERTICAL STAB TAIL CONE ASSY HAS A BROKEN INTERCOSTAL. MAINTENANCE REPLACED INTERCOSTAL IAW CRJ-700 SRM 51-42-27-001-001-A01.

Part: GUIDE — CHAFED (TE FLAPS) · airframe 8,737 hrs · 6,131 cycles

YYC - LEFT WING AFT SHROUD AREA AT STA 169, ON O/B FLAP ROLLER GUIDE FITTING CHAFED BY FLAP ROLLER FITTING. MAINTENANCE REPAIRED IAW REO 670-57-51-036, CRJ-700 NDTM PT 1, 51-20-006, SRM TASK 51-24-11-001-001-A01 AND FIELD P.S.18.0, CRJ 700/900 SRM 51-21-16, AND CRJ 700/900 SRM 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 739) · airframe 8,437 hrs · 6,131 cycles

YYC: FUSELAGE INT, LEFT O/B SEAT RAIL AT FS 739 HAS PITTING CORROSION ON INSIDE AND I/B FACING SURFACES. MAINTENANCE REPAIRED IAW REO 670-53-00-013 REV A.

Part: SEAT TRACK — CORRODED (BS 796) · airframe 8,437 hrs · 6,131 cycles

YYC - FUSELAGE INT, LEFT O/B SEAT RAIL AT FS 796 HAS PITTING CORROSION ON INSIDE EDGES. MAINTENANCE REPAIRED IAW REO 670-53-00-013 REV A.

Part: SEAT TRACK — CORRODED (BS 785) · airframe 8,437 hrs · 6,131 cycles

YYC - FUSELAGE INT, LEFT O/B SEAT RAIL AT FS 785 HAS PITTING CORROSION AND A TOOL MARK ON I/B FACING SURFACE. MAINTENANCE REPAIRED IAW REO 670-53-00-013 REV A.

Part: SEAT TRACK — CORRODED (BS 616) · airframe 8,437 hrs · 6,131 cycles

YYC - FUSELAGE INT, LEFT O/B SEAT RAIL AT FS 616 HAS PITTING CORROSION ON I/B FACING SURFACE. MAINTENANCE REPAIRED IAW REO 670-53-00-013 REV A.

Part: SEAT TRACK — CORRODED (BS 398) · airframe 8,437 hrs · 6,131 cycles

YYC - FUSELAGE INT, LEFT O/B SEAT RAIL AT FS 398 HAS PITTING CORROSION ON I/B FACING SURFACE. MAINTENANCE REPAIRED IAW REO 670-53-00-013 REV A.

Part: SEAT TRACK — CORRODED (BS 585) · airframe 8,437 hrs · 6,131 cycles

YYC - FUSELAGE INT, LEFT O/B SEAT RAIL AT FS 585 HAS PITTING CORROSION ON I/B FACING SURFACE. MAINTENANCE REPAIRED IAW REO 670-53-00-013 REV A.

Part: SEAT TRACK — CORRODED (BS 811) · airframe 8,437 hrs · 6,131 cycles

YYC - FUSELAGE INT, LEFT O/B SEAT RAIL AT FS 811 HAS PITTING CORROSION ON I/B FACING SURFACE. MAINTENANCE REPAIRED IAW REO 670-53-00-013 REV A.

Part: SKIN — SCRATCHED (BS 1070-1088) · airframe 8,437 hrs · 6,131 cycles

YYC - FUSELAGE INT SKIN, BETWEEN FS 1070-FS 1088 AND STR 9R-10R IS SCRATCHED. MAINTENANCE REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01, QX EA R-53-382 AND REO 670-53-61-203.

Part: SEAT TRACK — CORRODED (BS 645-661) · airframe 8,437 hrs · 6,131 cycles

YYC: FUSELAGE INT, LEFT OUTBOARD SEATRAIL AT FS 645 TO FS 661 HAS PITTING CORROSION ON INBOARD FACING SURFACE. MAINTENANCE REPAIRED IAW REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 811) · airframe 8,437 hrs · 6,131 cycles

YYC - FUSELAGE INT, RIGHT O/B SEAT RAIL AT FS 811 HAS PITTING CORROSION ON I/B FACING SURFACE. MAINTENANCE REPAIRED IAW REO 670-53-11-013 REV A.

Part: SEAT TRACK — CORRODED (BS 843) · airframe 8,437 hrs · 6,131 cycles

YYC - FUSELAGE INT, RIGHT O/B SEAT RAIL AT FS 843 HAS PITTING CORROSION ON I/B FACING SURFACE. MAINTENANCE REPAIRED IAW REO 670-53-00-013 REV A.

Part: SEAT TRACK — CORRODED (BS 796) · airframe 8,437 hrs · 6,131 cycles

YYC - FUSELAGE INT, RIGHT O/B SEAT RAIL AT FS 796 HAS PITTING CORROSION ON I/B FACING SURFACE. MAINTENANCE REPAIRED IAW REO 670-53-00-013 REV A.

Part: SEAT TRACK — CORRODED (BS 707) · airframe 8,437 hrs · 6,131 cycles

YYC - FUSELAGE INT, LEFT O/B SEAT RAIL AT FS 707 HAS PITTING CORROSION ON INSIDE SURFACE AND TWO RUSTY SCREWS. MAINTENANCE REPAIRED IAW SRM 51-41-02 AND REO 670-53-00-013 REV A.

Part: WARNING LIGHT — ILLUMINATED (FUEL SYSTEM) · airframe 5,285 hrs · 6,025 cycles

PDX - ON FLIGHT 2507, DURING TAXI OUT, RECEIVED A AUTO CROSSFLOW INHIBIT CAUTION MESSAGE. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE RESET PER THE SERVICE LETTER 28-007C. OPERATIONAL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DOOR — STIFF (ZONE 200) · airframe 7,235 hrs · 5,303 cycles

MAIN CABIN DOOR DIFFICULT TO LATCH AND OPEN. OPERATED MAIN CABIN DOOR SERVERAL TIMES. OPS CHECK NORMAL. NO DEFECTS NOTED. NO PARTS REPLACED. ACFT RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (DRAG CONTROL SYS) · airframe 7,148 hrs · 5,238 cycles

ON FINAL APPROACH DEPLOYED FLIGHT SPOILERS AND RECEIVED MASTER CAUTION "FLIGHT SPOILER DEPLOY", CAUTION WENT AWAY WHEN RETRACTED FLIGHT SPOILERS. MX INTERROGATED MDC. NO CURRENT FAULTS NOTED. COMPLIED WITH CRJ700 FIM TASK 27-61-00-810-A01. NO DEFECTS NOTED. NO PARTS REPLACED. ACFT RETURNED TO SERVICE.

Part: PUMP — LEAKING (NR 2 HYD SYS) · airframe 5,489 hrs · 4,034 cycles

FLIGHT RETURNED TO FIELD AFTER THE NR 2 HYDRAULIC SYSTEM FAILED. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 2 ENGINE DRIVEN PUMP LEAKING. A NEW PUMP WAS INSTALLED, OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULKHEAD — CRACKED (ZONE 200) · airframe 4,781 hrs · 3,480 cycles

BULKHEAD CRACKED AT BATHTUB FITTING RT SIDE OF AFT PRESSURE BULKHEAD. REPAIRED IAW REO 670-53-61-034.

Part: PAN — CRACKED (ZONE 200) · airframe 4,781 hrs · 3,480 cycles

RT PYLON PRESSURE PAN CRACKED AT AFT HYDRO, FITTING. REMOVED RT PYLON PRESSURE PAN. DRILLED UP AND INSTALLED INTERNAL DOUBLER IN NEW PAN. INSTALLED NEW PAN AND COMPLETED INSTALLATION AT FASTENERS THROUGH NEW PAN IAW SRM 51-42-06.

Part: CHIMNEY — DAMAGED (SMOKE DETECTOR) · airframe 4,499 hrs · 3,261 cycles

FORWARD BAGGAGE BAY CHIMNEY ASSEMBLY ABOVE DOOR IS DAMAGED. THE CARGO BAY CHIMNEY WAS REPLACED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (RT BLEED) · airframe 4,097 hrs · 2,962 cycles

SMF - ON FLIGHT 2494, ON CLIMBOUT, RT BLEED DUCT WARNING MESSAGE AFTER 5 SEC WARN WENT OUT AND REPLACED WITH RT BLEED DUCT CAUTION MESSAGE. C/W CHECKLIST AND MANUAL BLEED PROCEDURES. FOUND MDC TO SHOW A BLEED LEAK EVENT OCCURRED AT MT143/144 CHANNEL A & B. NO CURRENT FAULTS. SELF TEST GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (ZONE 100) · airframe 3,990 hrs · 2,876 cycles

WHEN POWER MOVED FROM TOGO TO CLIMB, RIGHT BLEED DUCT WARNING MESSAGE (RED), AFTER 5 SECONDS, WARNING OUT AND REPLACED WITH RIGHT BLEED DUCT CAUTION MESSAGE (YELLOW). COMPLIED WITH ALL CHECKLISTS. MAINTENANCE INTERROGATED MDC, NO CURRENT FAULTS. NO CURRENT CAS MESSAGES. NO PARTS REPLACED. AIRCRAFT OK FOR CONTINUED SERIVE.

Part: DEFLECTOR — BENT (CARGO DOOR) · airframe 3,902 hrs · 2,807 cycles

PDX - FORWARD BAG DOOR WIND DEFLECTOR ATTACHED TO EXTERIOR SKIN IS BENT OUTWARD INTO SLIP STREAM, WITH DOOR CLOSED. REPLACED DEFLECTOR IAW CRJ 700 SRM 51-42-06

Part: SKIN — CHAFED (PAX DOOR) · airframe 3,902 hrs · 2,807 cycles

PASSENGER DOOR INNER SKIN NEXT TO LOWER FORWARD LATCH CHAFE DAMAGE FROM UPPER FORWARD DOOR SOP. REPAIRED IAW CRJ SRM 52-11-01-101-AC1.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 3,769 hrs · 2,705 cycles

BOI - ON FLIGHT 2544 PASSENGER DOOR IS HARD TO OPEN. CLEANED AND LUBED DOOR OPEN LEVER ROLLER AND REMOVED ICE FROM DOOR SILL. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CHAFED (RT WING) · airframe 3,580 hrs · 2,563 cycles

PDX - CHAFE MARK ON RIGHT HAND WING UNDER JUNCTION OF NR 1 AND NR 2 SLATS. REPAIRED IAW HORIZON AIR EA R-57-55.

Part: FADEC — MALFUNCTIONED (LT ENGINE) · airframe 3,580 hrs · 2,563 cycles

PDX - FLIGHT 2491 AT TOP OF DESCENT, FLIGHT LEVEL 390 FT WITH INITIAL THROTTLE REDUCTION BY A THIRD, MOVED SLOW, LEFT ENGINE FLAME-OUT CAUTION MESSAGE FOR 14-15 SECONDS. NO ABNORMAL ENGINE INDICATIONS. REPLACED LEFT FADEC AS A PRECAUTIONARY MEASURE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SCREEN — TORN (CARGO BAY) · airframe 3,581 hrs · 2,563 cycles

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

Part: FIRE DETECTOR — ACTIVATED (ZONE 200) · airframe 2,908 hrs · 2,062 cycles

ON FLIGHT 2452 FIRE SYSTEM FAULT. THIS SDR IS WAITING FOR FURTHER INFORMATION.

Part: FIRE DETECTOR — FAILED (ZONE 200) · airframe 2,852 hrs · 2,029 cycles

FIRE SYSTEM FAULT STATUS MESSAGE. REMOVED AND REPLACED AFT SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 2,753 hrs · 1,952 cycles

SEA- ON FLIGHT NUMBER 2478, FIRE SYSTEM FAULT STATUS MESSAGE APPEARED FOR 20 MINUTES AND THEN EXTINGUISHED. FOUND MDC MESSAGE AFT SMOKE DETECTOR 1 FAILED WIRING NO RESPONSE TO COMMAND IN FAULT HX. REMOVED AND REPLACED SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SCREEN — TORN (CARGO BAY) · airframe 2,730 hrs · 1,935 cycles

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

Part: FIRE WARNING — INTERMITTENT (COCKPIT) · airframe 2,709 hrs · 1,919 cycles

ON FLIGHT 2502 INTERMITTENT FIRE SYSTEM FAULT. COMPLIED WITH CRJ SRM 26-15-00. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAILED (ZONE 200) · airframe 2,693 hrs · 1,908 cycles

ON FLIGHT 2547 FIRE SYSTEM FAULT STATUS MESSAGE. REMOVED AND REPLACED NR 2 AFT SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FIRE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 2,683 hrs · 1,900 cycles

PDX- FIRE SYSTEM FAULT STATUS MESSAGE. REMOVED AND REPLACED NR 1 FIRE DETECTOR IN AFT CARGO BAY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAILED (ZONE 200) · airframe 2,683 hrs · 1,900 cycles

BOI- ON FLIGHT 2430 FIRE SYSTEM FAULT STATUS MESSAGE. REMOVED AND REPLACED NR 2 AFT CARGO SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: COMPUTER — MALFUNCTIONED (ZONE 400) · airframe 2,591 hrs · 1,834 cycles

ON FLIGHT 2447 RECIEVED MOMENTARY WHITE (LEFT FADEC FAULT 1) MESSAGE FOLLOWED ABOUT ONE HOUR LATER WITH YELLOW (LEFT ENGINE FLAMEOUT) AND GREEN (LEFT AUTO IGNITION) MESSAGE UPON RETARDING THROTTLES AT TOP OF DESCENT. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED DIGITAL ENGINE COMPUTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: MECHANISM — DIRTY (PAX DOOR) · airframe 2,565 hrs · 1,814 cycles

CREW REPORTS MAIN CABIN DOOR HARD TO OPEN. CLEANED AND LUBED MATELING SURFACES. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — INTERMITTENT (ZONE 200) · airframe 2,234 hrs · 1,563 cycles

ON FLIGHT 2451 INTERMITTENT FIRE SYSTEM FAULT STATUS MESSAGE. PERFORMED FIRE SYSTEM TEST AND CHECKED ENGINE FIRE BOTTLES. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: COWLING — DAMAGED (NR 1 ENGINE) · airframe 2,028 hrs · 1,405 cycles

PDX- UPPER CORE COWL HAS FOD DAMAGE AT 12 O'CLOCK POSITION OF NR 1 ENGINE. REPAIRED IAW HORIZON AIR EA R-54-33 AND REO 670-54-23-129.

Part: PANEL — DAMAGED (ZONE 400) · airframe 2,028 hrs · 1,405 cycles

UPPER TRANS COWL HAS FOD DAMAGE AT 12 O'CLOCK POSITION OF NR 1 ENGINE. REPAIRED IAW HORIZON AIR EO R-54-33 AND REO 670-54-23-129.

Part: CARTRIDGE — FAILED (FUEL SYSTEM) · airframe 1,541 hrs · 1,061 cycles

PDX- ON FLIGHT 2493 AFTER TAKEOFF GOT A LEFT TRANSFER SHUT OFF VALVE AMBER MESSAGE. NO CENTER TANK FUEL ABNORMALITIES NOTICED. AUTO TRANSFER APPEARED EXCESSIVE BUT NO ABNORMAL IMBALANCE OR ANY FUEL LOSS NOTED. APPROXIMITLY 15 MINUTES AFTER DEPARTURE LEFT TRANSFER SHUT OFF VALVE MESSAGE WENT OUT. REMOVED AND REPLACEDLEFT HAND FUEL TRANSFER SHUT OFF VALVE CARTRIDGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CHIMNEY — DAMAGED (ZONE 100) · airframe 1,463 hrs · 1,008 cycles

BOI-CENTER CHIMNEY DAMAGED FORWARD CARGO BAY. INSTALLED NEW CENTER CHIMNEY IN FORWARD CARGO BAY IAW TASK 268100Q01 ON LINE 1 CHECK. AIRCRAFT RETURNED TO SERVICE.

Part: VALVE — FAILED (ZONE 200) · airframe 1,284 hrs · 879 cycles

PDX- ON FLIGHT 2438 OUT OF 10,000 FEET ON ARRIVAL TO PDX, RECIEVED A "APU FAULT" CAUTION MESSAGE. APU OPERATED NORMALLY. BEGAN TO RUN ABNORMAL CHECKLIST AND MESSAGE WENT OUT AFTER TWO MINUTES. REMOVED AND REPLACED DEPRIME SELINOID VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FIRE DETECTOR — INOPERATIVE (ZONE 200) · airframe 1,132 hrs · 771 cycles

PDX- ON FLIGHT NUMBER 2434, FIRE SYSTEM STATUS MESSAGE CAME ON IN FLIGHT, ALL OTHER INDICATIONS NORMAL. REMOVED AND REPLACED LOWER FIRE DETECTOR RAIL. OPERATIONAL TEST CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: COVER — DAMAGED (ZONE 200) · airframe 1,076 hrs · 734 cycles

PDX- FORWARD CARGO BAY ENTRY WAY SMOKE DETECTOR PROTECTIVE COVER IS DAMAGED. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: STRUCTURE — CHAFED (RT LE SLAT) · airframe 1,081 hrs · 737 cycles

PDX-RT SLATS CHAFING AGAINST UPPER WING SURFACE AT WS.178.00 AT INBOARD DISCONNECT SENSOR AREA. REPAIRED IAW CRJ700 SRM 51-25-26, SRM 51-00-02 AND SRM 51-25-16.

Part: WARNING LIGHT — ILLUMINATED (ZONE 100) · airframe 592 hrs · 410 cycles

SEA-ON FLIGHT NUMBER 2504, LT TRANSFER SHUT OFF VALVE CAUTION MESSAGE IN FLIGHT. USED ABNORMAL CHECKLIST. AFTER 5-10 MINUTES, CAUTION MESSAGE DISAPPEARED. MDC, LT TRANSFER VALVE COMMAND DISAGREE. COMPLIED WITH FIM TASK. NO DEFECTS NOTED. COMPLIED WITH LRU TEST OF VALVES/PUMPS. SELF TEST PASSED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: CHIMNEY — DAMAGED (ZONE 200) · airframe 566 hrs · 392 cycles

CENTER CHIMNEY ON FORWARD CARGO BAY IS TORN. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 418 hrs · 291 cycles

ONT-FIRE SYSTEM FAULT STATUS MESSAGE. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (FIRE DETECTION) · airframe 404 hrs · 284 cycles

MFR- FIRE SYSTEM FAULT STATUS MESSAGE. INTERROGATED MDC, FOUND NO FAULTS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SENSOR — FAILED (FUEL SYSTEM) · airframe 385 hrs · 270 cycles

PDX-LEFT FUEL LOW PRESSURE CAUTION LIGHT ON INFLIGHT. REMOVED AND REPLACED ENGINE FEED PRESSURE SENSOR. LEAK AND OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RETAINER — DAMAGED (PAX DOOR) · airframe 305 hrs · 211 cycles

PDX - THE MAIN CABIN DOOR SEAL RETAINER AND DOOR STRIKER ARE DAMAGED AT LOWER FORWARD CORNER. THE SEAL RETAINER WAS REPLACED AND THE CABIN DOOR SEAL STRIKER WAS REPAIRED IAW EA-R-52-67 AND THE CRJ-700 STRUCTURAL REPAIR MANUAL.

Part: CONTROL UNIT — MALFUNCTIONED (FIRE DETECTION) · airframe 100 hrs · 78 cycles

SEA- DURING DESCENT FIRE SYSTEM FAULT STATUS MESSAGE CAME ON. THE FIRE DETECTION CIRCUITS TESTED OKAY. AFTER LANDING FIRE DETECTION SYSTEM FAULT STATUS MESSAGE WENT AWAY. REMOVED AND REPLACED FIDEX CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (FIRE DETECTION) · airframe 91 hrs · 71 cycles

LAX- FIRE SYSTEM FAULT STATUS MESSAGE. COMPLIED WITH OPERATIONAL TEST OF FIDEX SYSTEM IAW 26-10-00-710-801. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.