N605QX

Part: CLEAT — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

CORRODED CLIP AT STRINGER 21 RT BETWEEN FRAMES 319.70-333.00. REMOVED AND REPLACED CLEAT P/N SH670-32695-1 IAW SRM 51-42-20-001-001-A01.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

CORRODED STRINGER 19R BETWEEN FUSELAGE STATIONS 310.00 - 319.70. REMOVED AND REPLACED STRINGER 19R IAW SRM 51-42-06-001-001 A01 AND DWG SH670-31630.

Part: RISER — CRACKED (PAX DOOR) · airframe 36,465 hrs · 27,168 cycles

UPON REMOVAL OF SEALANT, FOUND CRACK ON ASD AFT RISER PANEL AT TOP STEP. REPAIRED AFT RISER PANEL AT TOP STEP IAW SRM TR 52-0025 TASK 52-11-04-201-004-A01. THIS IS A MINOR REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

STR 20 CORRODED BETWEEN FS 295 AND FS 310. REMOVED CORROSION, REPLACED DAMAGED FASTENERS AND RESTORED FINISH PER ECTC EA 32-2017-109.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 36,465 hrs · 27,168 cycles

VERTICAL STAB RT LOWER AFT DRAG ANGLE CRACKED. REPAIRED DRAG ANGLE BY COMPLYING WITH EC/TC REO 670-55-31-097, REO 670-55-31-018, AND REO'S 670-55-31-097, 670-55-31-018.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

STR 26 RT CORRODED BTW FRAMES 280-295. REMOVED AND REPLACED STR RT 26 BTW FRAMES 280-295 IAW 51-42-06-001-001 A01, 53-21-03-001-002 A01. P/N SH670-31634-25 DRAWING SH670-31634.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

STR SPLICE CORRODED AT 25L BETWEEN FRAMES 319.70-333.00. REMOVED AND REPLACED SPLICE IAW SRM 51-42-06-001-001-A01, AND DRAWING SH670-32420.

Part: STRUCTURE — CORRODED (LE SLAT) · airframe 36,465 hrs · 27,168 cycles

RT SLAT INTERNAL STRUCTURE CORRODED WHERE TELESCOPIC DUCT ATTACHES. REPAIRED RT SLAT INTERNAL STRUCTURE IAW EA 30-2017-070 AND EC/TC EA 30-2017-070.

Part: STRAP — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

CIRCUMFERENTIAL STRAP AT FS 280 CORRODED BETWEEN STG 25R-25L. REPAIRED CIRCUMFERENTIAL STRAP IAW EA 32-2017-096 AND EC/TC EA 32-2017-096 REV 0.

Part: SEAT TRACK — CORRODED (BS 551) · airframe 36,465 hrs · 27,168 cycles

RIGHT WALL SEAT TRACK AT BS 551 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-801-A01, REO, ECTC REO 670-53-00-343, AND AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 677) · airframe 36,465 hrs · 27,168 cycles

LEFT WALL SEAT TRACK AT BS 677 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-801-A01, REO, ECTC REO 670-53-00-343, AND AMM 53-00-49-400-801-A01.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 36,465 hrs · 27,168 cycles

CRAWL WAY FLOOR SUPPORT HAS CORROSION BS 280. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-42-06-00-001-A01, 51-42-21-001-001-A01, AND DRAWING SH670-34010.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

LT WALL SEAT RAIL AT FS 615.00 IS CORRODED. REMOVED CORRODED LT WALL SEAT RAIL FS 615.00 IAW AMM 53-00-49-801-A01. FABRICATED NEW SEAT RAIL PER REO AND ECTC REO 670-53-00-343. INSTALLED NEW FABRICATED LT WALL SEAT RAIL FS 615.00 IAW AMM 53-00-49-400-801-A01. ALL DEFECTS CORRECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

RT WALL SEAT RAIL AT FS 615.00 IS CORRODED. REMOVED CORRODED LT WALL SEAT RAIL FS 615.00 IAW AMM 53-00-49-801-A01. FABRICATED NEW SEAT RAIL PER REO AND ECTC REO 670-53-00-343. INSTALLED NEW FABRICATED RT WALL SEAT RAIL FS 615.00 IAW AMM 53-00-49-400-801-A01. ALL DEFECTS CORRECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

RT FLOOR SEAT RAIL AT FS 615 IS CORRODED. REMOVED CORRODED RT FLOOR SEAT RAIL SEGMENT FROM FS 581-FS 683 IAW AMM 53-00-49-801-A01. FABRICATED NEW SEAT RAIL PER REO AND ECTC REO 670-53-00-343. INSTALLED NEW FABRICATED RT FLOOR SEAT RAIL SEGMENT FS 581-FS 683 IAW AMM 53-00-49-400-801-A01. ALL DEFECTS CORRECTED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

LEFT O/B INTERCOSTAL FS 333-364 CORRODED. REMOVED AND REPLACED CORRODED INTERCOSTAL FS 333-364 STR 25L IAW SRM 51-42-06-00-001-A01 & 51-42-21-001-001-A01. DRAWING SH670-3207 7.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

LT FLOOR SEAT RAIL AT FS 615.00 IS CORRODED. REMOVED CORRODED LT FLOOR SEAT RAIL FS 615.00 IAW AMM 53-00-49-801-A01. FABRICATED NEW SEAT RAIL PER REO AND ECTC REO 670-53-00-343. INSTALLED NEW FABRICATED LT FLOOR SEAT RAIL FS 615.00 IAW AMM 53-00-49-400-801-A01. ALL DEFECTS CORRECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

RT FLOOR SEAT RAIL AT FS 816.00-836.00 IS CORRODED. REMOVED CORRODED RT FLOOR SEAT RAIL FS 816.00-836.00 IAW AMM 53-00-49-801-A01. FABRICATED NEW SEAT RAIL PER REO AND ECTC REO 670-53-00-343. INSTALLED NEW FABRICATED RT FLOOR SEAT RAIL FS 816.00-836.00 IAW AMM 53-00-49-400-801-A01. ALL DEFECTS CORRECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

LT FLOOR SEAT RAIL AT FS 710 IS CORRODED. REMOVED AND INSTALLED SERVICEABLE LT FLOOR SEAT RAIL FROM FS 700-837 IAW AMM 53-00-49-400-801-A15. COMPLIED WITH EC/TC REO 670-53-00-343 AND GENERIC REO 670-53-00-343 REV M AS WRITTEN.

Part: RISER — CRACKED (PAX DOOR) · airframe 36,465 hrs · 27,168 cycles

UPON REMOVAL OF SEALANT, FOUND CRACK ON ASD AFT RISER PANEL AT BOTTOM STEP. REPAIRED AFT RISER PANEL AT BOTTOM STEP IAW SRM TR 52-0025 TASK 52-11-04-201-004-A01. THIS IS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

LT WALL SEAT RAIL AT FS 615 IS CORRODED. REMOVED CORRODED LT WALL SEAT RAIL FS 615 IAW AMM 53-00-49-801-A01. FABRICATED NEW SEAT RAIL PER REO AND ECTC REO 670-53-00-343. INSTALLED NEW FABRICATED LT WALL SEAT RAIL FS 615 IAW AMM 53-00-49-400-801-A01. ALL DEFECTS CORRECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

RT FLOOR SEAT RAIL AT FS 986 IS CORRODED. REMOVED CORRODED RT FLOOR SEAT RAIL FS 986 IAW AMM 53-00-49-801-A01. FABRICATED NEW SEAT RAIL PER REO AND ECTC REO 670-53-00-343. INSTALLED NEW FABRICATED RT FLOOR SEAT RAIL FS 986 IAW AMM 53-00-49-400-801-A01. ALL DEFECTS CORRECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

LT FLOOR SEAT RAIL AT FS 968 IS CORRODED. REMOVED CORRODED LT FLOOR SEAT RAIL FS 968 IAW AMM 53-00-49-801-A01. FABRICATED NEW SEAT RAIL PER REO AND ECTC REO 670-53-00-343. INSTALLED NEW FABRICATED LT FLOOR SEAT RAIL FS 968 IAW AMM 53-00-49-400-801-A01. ALL DEFECTS CORRECTED.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

PAX DOOR LOWER SILL, UPPER ANGLE CORRODED. REMOVED AND REPLACED PAX DOOR LOWER SILL UPPER ANGLE PER SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. DRW SH670-31825.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

LT WALL SEAT RAIL AT FS 583 IS CORRODED. REMOVED CORRODED LT WALL SEAT RAIL FS 583 IAW AMM 53-00-49-801-A01. FABRICATED NEW SEAT RAIL PER REO AND ECTC REO 670-53-00-343. INSTALLED NEW FABRICATED LT WALL SEAT RAIL FS 583 IAW AMM 53-00-49-400-801-A01. ALL DEFECTS CORRECTED.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

COCKPIT FLOOR PANEL 221 ALF AFT SUPPORT ANGLE CORRODED. REMOVED AND REPLACE COCKPIT FLOOR PANEL 221 ALF AFT SUPPORT ANGLE PN CC670-34095-1 WITH A SERVICEABLE PART IAW SRM 51-42-21-001-001-A01 & DRAWING CC670-34095.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

STR 23 RT CORRODED. REMOVED AND REPLACED STR 23 RT WITH SERVICEABLE PART PN SH670-32429-4 IAW 51-40-11-001-001-A01 &51-42-06-001-001-A01 & DRAWING SH670-32429.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

PAX DOOR LOWER SILL , LOWER ANGLE CORRODED. REMOVED AND INSTALLED SERVICEABLE LOWER ANGLE IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01 & DRAWING 670-31875.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

CORRODED INTERCOSTAL STR 20R BTW FRAMES 310 AND 319. REMOVED AND REPLACED INTERCOSTAL PN SH670-32047-1 IAW SRM 51-40-11-001-A01 & 51-42-06-001-A01 & 51-42-21-001-001-A01.

Part: RISER — CRACKED (PAX DOOR) · airframe 36,465 hrs · 27,168 cycles

UPON REMOVAL OF SEALANT, FOUND CRACK ON ASD FWD RISER PANEL AT TOP STEP. REPAIRED FWD RISER PANEL AT TOP STEP IAW SRM TR 52-0025 TASK 52-11-04-201-004-A01. THIS IS A MINOR REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

STRINGER 21R AND SPLICE CORRODED BETWEEN FS 319 TO FS 333. REMOVED AND REPLACED STR 21R SEGMENT AND STRINGER JOINT SPLICE BETWEEN FS 280 TO FS 333 PER SRM 53-00-03-201-001-A01 AND 51-42-06-001-001-A01. THIS IS A MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

FLOORBEAM LBL9, FS1031 HAS CORROSION DAMAGE. REMOVED DAMAGED SECTION, REPLACED WITH DOUBLER. ADDED SHIM TO SUPPORT CLEARANCE FOR POT WATER BRACKET PER ECTC EO 700-53-10-00053 AND ECTC REO 670-53-61-1366.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,465 hrs · 27,168 cycles

FLOORBEAM, LBL 27, FS 1047 HAS CORROSION DAMAGE. REMOVED AND REPLACED FLOORBEAM AT LBL 27 AND FS 1047 IAW SRM 51-251-06-001-001 A01, 53-61-43-101-001 A01, 53-61-43-201-001 A01 AND ECTC EO 700-53-10-00052 REV O.

Part: POST — CORRODED (COCKPIT DOOR) · airframe 36,465 hrs · 27,168 cycles

RIGHT COCKPIT DOOR POST HAS CORROSION AT THE BOTTOM. CUT OUT DAMAGED SECTION, FABRICATED A FILLER AND DOUBLER AND INSTALLED IAW ECTC EA 32-2017-099.

Part: FRAME — CORRODED (BS 295) · airframe 36,465 hrs · 27,168 cycles

FRAME BS 295 HAS CORROSION FWD & AFT SIDES BETWEEN STRINGERS 26R - 26L. CUT OUT DAMAGED SECTION, FABRICATED AND INSTALLED A NEW SECTION IAW ECTC REO 670-53-21-799 AND ECTC REO 670-53-21-1421 .

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 36,255 hrs · 27,008 cycles

PILOT REPORTED THE EMERGENCY LIGHTS INOPERATIVE. ALLOWED EMERGENCY LIGHTS TO CHARGE AND PERFORMED OPERATIONAL TEST, TESTED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — UNKNOWN (RT OVERWING) · airframe 34,984 hrs · 26,031 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. OPS CHECKED GOOD.IAW AMM 33-51-15.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING PREFLIGHT INSPECTION, NOTED TWO EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED & REPLACED EPSU BATTERY PACKS 2 & 3. OPS CHECKED GOOD IAW AMM 33-51-17.

Part: BOLT — SHEARED (CARGO DOOR) · airframe 33,929 hrs · 25,136 cycles

FWD CARGO DOOR FWD UPPER STOP ATTACHING BOLT SHEARED. COMPLIED WITH PERMANENT REPAIR TO FORWARD CARGO DOOR FWD UPPER STOP ATTACHMENT IAW STS EA 20-2016-048. RII FOR FWD CARGO DOOR ADJUSTMENT IAW AMM 52-35-00 COMPLIED WITH IAW GMM 3-3.

Part: STRINGER — CORRODED (BS 356) · airframe 33,529 hrs · 24,822 cycles

LONGERON AT STR 25R HAS CORROSION AT APPROXIMATELY FS356.00, LONGERON FS333.00-364, FOUND DURING ACCESS FOR FS 364.00 FRAME REPAIR. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED CORROSION FOUND TO BE OUT OF ALLOWBLE DAMGE LIMITS OF SRM 53-21-23-101-003-A01 AND SRM 53-21-03-11-006-A01, SERVERE CORROSION. R & R LONGERON IAW SRM 51-42-06-001-001-A01 AND DWG SH 670-320-50.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 33,529 hrs · 24,822 cycles

LT SIDE SEAT RAIL CORRODED IN SEVERAL PLACES FROM FS 708.00 TO FS 761.00. EVALUATED DAMAGE AND DETERMINED TO BE OUT OF LIMITS, REF: SRM 53-41-49-101-001-A01 AND SUPPLEMENT XJET 53-41-49. R & R LEFT SIDE SEAT RAIL FROM FS 708.00 TO FS 761.00 IAW AMM 53-00-49-000-801-A01 AND 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 33,529 hrs · 24,822 cycles

LT SIDE SEAT RAIL CORRODED IN SEVERAL PLACES FROM FS677.00 TO FS708.00 IAW SRM 53-41-49-101-001-A01 AND SRM SUPPLEMENT XJET 53-41-49, DAMAGE ON SEAT RAIL IS BEYOND ALLOWABLE LIMITS. R & R LT SIDE SEAT RAIL FS 677 TO FS 708 IAW AMM 53-00-49-000-801-A01 AND 53-00-49-400-801-A01. FABRICATED SERVICEABLE SEAT RAIL IAW EC/TC REO 670-53-00-343. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M, AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 923-985) · airframe 33,529 hrs · 24,822 cycles

LT SIDE SEAT RAIL CORRODED IN SEVERAL PLACES FROM FS923.00 TO FS985.00. EVALAUTED DAMAGE FURTHER AND DETERMINED DAMAGE UNREPAIRABLE REF: SRM 53-41-49-101-001-A01 AND SUPPLEMENT SJET 53-41-49. R & R SEAT TRACK FS923-FS985 IAW AMM 53-00-49-400-801-A01. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV M AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 830-863) · airframe 33,529 hrs · 24,822 cycles

RT SIDE SEAT RAIL CORRODED IN SEVERAL PLACES FROM FS830.40 TO FS863.00. EVALUATED DAMAGE AND DETERMINED TO BE OUT OF LIMITS REF: SRM 53-51-44-101-001-A01 AND SUPPLEMENT SJET 53-41-49. REMOVED RT SIDE SEAT RAIL BETWEEN FS830.40-FS863.00 IAW AMM 53-00-49-000-801-A01. INSTALLED NEW A SEAT TRACK AT FS830.40- FS863.00 IAW AMM 53-00-49-400-801-A01. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV M AS WRITTEN.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 33,529 hrs · 24,822 cycles

SERVICE DOOR SILL CORRODED IN SEVERAL AREAS. EVALUATED SERVICE DOOR SILL AND DETERMINED TO BE OUT OF LIMITS IAW SRM 53-21-23-001-001 A01. LOCATED HOLES IN NEW SERVICE DOOR SILL ANGLE AND STARTED INSTALLING IAW SRM 51-42-06-001-001 A01. LOCATED HOLES IN NEW WEB FLOOR PROTECTORS AND ANGLES IAW SRM 51-42-06-001-001 A01. FINISHED INSTALLING SILL ANGLE WEB FLOOR PROTECTORS & SERVICE DOOR SILL ANGLE IAW SRM 51-42-06-001-001 A01.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 33,529 hrs · 24,822 cycles

LT SIDE SEAT RAIL CORRODED IN SEVERAL PLACES FROM FS785.15 TO FS863.00. IAW SRM 53-41-49-101-001-A01 AND SRM SUPPLEMENT XJET 53-41-49 THIS SEAT RAIL IS NON-REPAIRABLE. REMOVED SEAT RAIL AT LT SIDE FS 785.15 TO FS 863.00 IAW AMM 53-00-49-000-801-A01 INSTALLLED IAW AMM 53-00-49-40-801 A01. FABRICATED SEAT RAIL IAW CEC/TC REO 670-53-00-343. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV M AS WRITTEN. PARTIALLY INSTALLED LT SIDE SEAT RAI FS 785 TO 863.00, 21 EA FASTENERS REMAINING IAW AMM 53-00-49-400-801 A01. INSTALLED 2 EA FASTENERS REMAINING IN LT SIDE SEAT RAIL IAW AMM 53-00-49-400-801 A01.

Part: SEAT TRACK — CORRODED (BS 863-923) · airframe 33,529 hrs · 24,822 cycles

RT SIDE SEAT RAIL CORRODED IN SEVERAL PLACES FROM FS 863.00 TO FS 923.00. EVALUATED DAMAGE AND DETERMINED DAMAGE TO BE UNREPAIRABLE. SRM 53-51-49-101-001 A01 AND SUPPLEMENT XJET 53-51-49. R & R SEAT TRACK BETWEEN FS 863.00 - FS 923.00 IAW AMM 53-00-49-400-801 A01. COMPLIED WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343, REV M AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 923-969) · airframe 33,529 hrs · 24,822 cycles

RT SIDE SEAT RAIL CORRODED IN SEVERAL PLACES FROM FS923.00 TO FS969.00. EVALUATED DAMAGE FURTHER AND DETERMINED DAMAGE UNREPAIRABLE, REF: SRM 53-51-44-101-001-A01 AND SUPPLMENT SJET 53-41-49. R & R SEAT TRACK IAW AMM 53-00-49-400-801-A01. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV M AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 863-923) · airframe 33,529 hrs · 24,822 cycles

LT SIDE SEAT RAIL CORRODED IN SEVERAL PLACES FROM FS863.00 TO FS923.00. EVALUATED FURTHER, FOUND CORROSION TO BE UNREPARABLE REF: SRM 53-51-49-101-001 A01 AND XJET SUPPLEMENT 53-51-49. REMOVED LT SIDE SEAT TRACK AT FS 863 - FS923 IAW AMM 53-00-49-000-801 A01. PARTIALLY INSTALLED LT SIDE SEAT RAIL FROM FS 863.00 TO FS 923. 5 EA FASTNERS REMAINING IAW AMM 523-00-49-400-801. FABRICATED SEAT RAIL IAW EC/TC REO 670-53-00-343. COMPLIED WITH ECTC REO 670-53-00-345 AND GREO 670-53-00-343, REV M AS WRITTEN. INSTALLED 5 EA REMAINING FASTENERS IN LT SIDE SEAT RAIL AT FS 863.00 TO FS 923.00 IAW AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 33,529 hrs · 24,822 cycles

LT SIDE SEAT TRACK CORRODED IN SEVERAL PLACES FROM FS 581.00 TO FS 677.00. EVALUATED DAMAGE AND DETERMINED TO BE OUT OF LIMITS, REF: SRM 53-31-49-101-001-A01 AND SUPPLEMENT 53-31-49. R & R SEAT RAIL W/SERVICEABLE SEAT RAIL IAW AMM 53-00-49-400-801. FABRICATED SERVICEABLE SEAT RAIL IAW EC/TC REO 670-53-00-343. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV M AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 785) · airframe 33,529 hrs · 24,822 cycles

CORROSION BELOW SEAT TRACK, SIDE, AT FS 785.15 ON RT ON EXTRUSION. BLENDED MINOR SURFACE CORROSION ON STRUCTURE BELOW SEAT RAIL AT FS 785 IN 2 LOCATIONS IN REF TO SRM 51-21-06-001-001-A01. DAMAGE TO SEAT RAIL MOUNTING STRUCTURE .010" DEEP EXCEEDS THE ALLOWABLE DAMAGE LIMIT OF 10 PERCENT GIVEN IN SRM 53-00-00-101-001 A01. RECEIVED AND COMPLIED WITH EA 32-2015-410.

Part: INTERCOSTAL — CORRODED (BS 349-365) · airframe 33,529 hrs · 24,822 cycles

INTERCOSTAL AT STR 27L BETWEEN FS 349-365 CORRODED. REMOVED CORROSION ON INTERCOSTAL AT STR 27L IN REF TO SRM 51-21-06-001-001-A01, TM51-21-06-001-001-A01. REMOVED INTERCOASTAL AT FS 349-365, STR 27L IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED HOLE IN NEW SERVICIBLE INTERCOASTAL AT FS 349-365, STR 27L IAW SRM 51-40-11-001-001-A01. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 785-830) · airframe 33,529 hrs · 24,822 cycles

RT SIDE SEAT RAIL CORRODED IN SEVERAL PLACES FROM FS785.15 TO FS830.40, APPROXIMATELY. REMOVED RT SIDE SEAT RAIL AND BLENDED CORROSION, FOUND TO BE OUT OF LIMITS IN REF TO SRM 53-41-49-101-001 A01 & 53-00-49-000-801 A02. INSTALLED NEW SERVICABLE SEAT RAIL RT SIDE BETWEEN FS 785-830 IAW AMM 53-00-49-400-801 A01. FABRICATED NEW SEAT RAIL. SEAT RAIL INSTALLED FOR PREFAB'D ORDERED PART.

Part: FRAME — CORRODED (BS 365) · airframe 33,529 hrs · 24,822 cycles

FS 365 FWD FACE BETWEEN 26L & 25L CORRODED. BEGAN REMOVAL OF CORROSION AT FWD FACE OF FRAME AT FS 365 BETWEEN STR 25L AND 26L IAW SRM 51-21-06-001-001-A01. PART WILL REQUIRE REPLACEMENT. REPLACED FRAME 365 IAW SRM 51-42-02-001-001-A01 GREO 670-53-21-687, MAINTENANCE DONE IAW REO 670-53-21-687 ND AMS 2770. COMPLIED WITH ECTC REO 670-53-21-687 AND GREO 670-53-21-687.

Part: STRINGER — CORRODED (BS 333) · airframe 33,529 hrs · 24,822 cycles

STRINGER 21R CORRODED AT APPROXIMATELY BS 333.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 33,529 hrs · 24,822 cycles

RT BS 280 FLOOR POST CORRODED AT BOTTOM INBD SIDE. REMOVED CORROSION OFF RT FLOOR POST FS 280 AT BOTTOM INBD SIDE IAW SRM TR 51-0050. COMPLIED WITH EA 32-2015-407. RECEIVED EC/TC AND ALL STEPS COMPLIED WITH ON EC/TC, EA 32-2015-407.

Part: STRAP — CORRODED (BS 280) · airframe 33,529 hrs · 24,822 cycles

CIRCUMFERENTIAL STRAP AT FS 280 INBD OF STR 26L AND INBD OF STR 25R CORRODED. REMOVED CORROSION OF STRAP AT FS 280 IAW SRM TR 51-0050. COMPLIED WITH EA 32-2015-404.

Part: FLOOR SUPPORT — CORRODED (BS 280-349) · airframe 33,529 hrs · 24,822 cycles

RT FLOOR SILL FROM FS 280 TO FS 349 CORRODED. BEGAN REMOVING CORROSION ON RT FLOOR SILL BETWEEN FS 280-319 IAW SRM 51-21-06-001-001-A01. REMOVED REPAIR AT RT FLOOR SILL FS 280 IAW SRM 51-42-06-001-001-A01. REMOVED RT FLOOR SILL AT FS 280-349 IAW SRM 51-42-13-001-001-A01. LOCATED HOLES ON NEW FLOOR SILL AND STARTED INSTALLING IAW SRM 51-42-06-001-001-A01 & 51-42-13-001-001-A01. FINISHED INSTALLING RT FLOOR SILL IAW SRM 51-42-06-001-001-A01 & 51-42-13-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 33,529 hrs · 24,822 cycles

AFT FACE OF FS 280 FLOORBOARD SUPPORT ANGLE CORRODED AT ALL 3 NUTPLATES. REMOVED CORROSION OF SUPPORT ANGLE IAW SRM TEMPORARY REV 51-0050. REMOVED ANGLE AND DRILLED SERIVCABLE ANGLE IAW SRM 51-42-06. 3 EA NUTPLATE HOLES ARE NOT DRILLED AND 51-40-11-001-001-A01. INSTALLED NEW FLOORBOARD SUPPORT ANGLE ON AFT FACE OF FS 280 IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 33,529 hrs · 24,822 cycles

SEAT TRACK AT FS 349 TO FS 485 LBL9 HAS CORROSION THROUGHOUT TRACK. UPON EVALUATION FOUND SEAT RAIL TO BE IN 2 SECTIONS BOTH FOUND TO BE OUT OF LIMITS IN REF TO SRM 53-21-49-101-001-A01. R & R SEAT RAILS W/ SERVICEABLE SEAT RAILS, 2EA IAW AMM 53-00-49-000-801, A01/53-00-49-400-801 A01. FABRICATED SERVICEABLE SEAT RAIL IAW EC/TC REO 670-53-00-343. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV M AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 33,529 hrs · 24,822 cycles

SEAT TRACK AT FS 349 TO 485 RBL9 HAS CORROSION THROUGHTOUT TRACK. UPON EVALAUTION FOUND SEAT TRACK AT FS 349 TO 485, RBL 9 TO BE OUT OF LIMITS IN REF RO SRM 53-21-49-101-001-A01. R & R SEAT TRACK AT FS 349 T OF S485, RBL 9 IAW AMM 53-00-49-000-801-A01 AND 53-00-49-400-801-A01.

Part: FRAME — CORRODED (BS 295) · airframe 33,529 hrs · 24,822 cycles

AFT FACE OF FS 295, RT OF STR 27 & OTBD OF 25R CORRODED. REMOVED CORROSION OF FRAME FS 295 FWD & AFT OF THE FRAME IAW SRM TR 51-0050. RECEIVED AND COMPLIED WITH EA 32-2015-406. RECEIVED AND COMPLIED WITH ECTC EA 32-2015-406.

Part: INTERCOSTAL — CORRODED (BS 349-365) · airframe 33,529 hrs · 24,822 cycles

INTERCOSTAL AT STR 26R BETWEEN FS 349-365 CORRODED. REMOVED INTERCOSTAL AT STG 26R BETWEEN FS 349-365 IAW SRM 51-42-21-001-001-A01. RE-INSTALLED INERCOSTAL AT STR 26R, FS 349-365 IAW SRM 51-42-21-001-001-A01 & 51-42-06-001-001-A01 & DWG SH 670-320-75. REMOVED CORROSION FROM INTERCOSTAL AT STR 26R BETWEEN FS 349 AND 364 IAW SRM 51-21-06-001-001-A01.

Part: STRINGER — CORRODED (BS 333-365) · airframe 33,529 hrs · 24,822 cycles

STR 26R, FS 333-365 CORRODED AND SPLICE AT BS 333 26R CORRODED. REMOVED CORROSION FROM STR 26R BETWEEN FS 333-365 IAW SRM 51-21-06-001-001-A01. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-21-03-101-000-A01. REMOVED CORROSION FROM STR 26R SPLICE AT FS 333 IAW SRM 51-21-06-001-001-A01. DAMAGE TO STR SPLICE FOUND TO BE OUT OF LIMITS IAW SRM 53-21-03-101-006-A01. REMOVED STR 26R BETWEEN FS 333-365 IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED HOLES IN NEW SERVICEABLE STR 26R BETWEEN FS 333-364 INSTALLED STR 26R IAW SRM 51-42-06-001-001-A01, SRM SH 670-31350. REMOVED STR 26R SPLICE AT FS 333 IAW DWG 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE SPLICE FOR STR 26R AT FS 333 IAW SRM 51-42-06-001-001-A01 DWG SH670-31350. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: INTERCOSTAL — CORRODED (BS 349-365) · airframe 33,529 hrs · 24,822 cycles

INTERCOSTAL AT STR 27R BETWEEN FS 349-365 CORRODED. REMOVED CORROSION ON INTERCOSTAL AT STR 7 BETWEEN FS 349-365 IN REF TO SRM 51-21-06-001-001-A01. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-140-003-A01. REMOVED INTERCOASTAL AT FS 349-365 STR 27R IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED HOLES IN NEW SERVICEABLE INTERCOASTAL AT FS 349-365, STR 27R IAW SRM 51-40-11-001-001-A01. INSTALLED NEW SERICEABLE INTERCOSTAL IAW SRM 51-42-06-001-001-A01 & DWG SH670-32075.

Part: FITTING — CORRODED (NOT REPORTED) · airframe 33,529 hrs · 24,822 cycles

INTERNAL FORWARD JACK FITTING CORRODED ALONG BOTH SIDES.

Part: STRINGER — CORRODED (BS 295-310) · airframe 33,529 hrs · 24,822 cycles

STR 25R BETWEEN FS 295-310 CORRODED AT HYD LINE STANDOFF CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001A01, DETERMINED OUT OF LIMITS IAW SRM 53-21-03-101-002-A01 10 PERCENT MATERIAL LOSS. BEGAN REMOVAL OF STR 25R BETWEEN FS 280-333 BY REMOVING RIVETS COMMON TO STR AND SKIN IAW SRM 51-42-06-001-001-A01 AND SPLICE AT FS 333. COMPLETED REMOVAL OF STR 25R BETWEEN FS280-333 IAW SRM 51-42-06-001-001 A01. BEGAN INSTALLATION OF STR 25R BETWEEN FS 280-333 BY INSTALLING RIVETS COMMON TO STR AND SKIN IAW SRM 51-42-06-001-001-A01. FOUND STRINGER SPLICE AT STR 25R, FS 333 CORRODED BEYOND LIMITS IAW SRM 53-21-03-101-002-A01. LOCATED HOLES AND INSTALLED NEW SERVCABLE STRIG SPLICES AT FS 333 STR 25R IAW SRM 51-42-06-001-001 A01 DWG SH670-32420. LOCATED AND DRILLED HOLES FOR STR TO FRAME CLIPS INTO STR 25R AT FS 295 AND 310 IAW SRM 51-40-11-001-001 A01. LOCATED HOLES AND INSTALLED STR CLIPS AT STR 25R, FS 319 AND 333 IAW SRM 51-42-06-001-001 A01 DWG SH670-32420. INSTALLATION OF STR 25R COMPLETE.

Part: STRINGER — CORRODED (BS 333) · airframe 33,529 hrs · 24,822 cycles

AFT FACE OF FS 333, STR 27 RT SIDE CORRODED. REMOVED CORROSION AFT SIDE FS 333 AT STR 27 IAW SRM 51-21-06-001-001 A01. COMPLIED WITH EA 26-2015-172. RECEIVED AND COMPLIED WITH ECTC EA 26-2015-172.

Part: FRAME — CORRODED (BS 319) · airframe 33,529 hrs · 24,822 cycles

FWD FACE FS 319, OTBD STR 26R INBD STR 26R INBD STR 26L OTBD STR 26L & INBD STR 25R CORRODED.

Part: FRAME — CORRODED (BS 319) · airframe 33,529 hrs · 24,822 cycles

FWD FACE OF FS 319 STR-27, RT SIDE, CORRODED.

Part: STRINGER — CORRODED (BS 310-319) · airframe 33,529 hrs · 24,822 cycles

FS 310-319, STR 25R CORRODED AROUND RIVET HEADS. REPAIRED IAW SRM 51-21-06-001-001-A01.

Part: DOOR SILL — CORRODED (CARGO DOORWAY) · airframe 33,529 hrs · 24,822 cycles

AFT CARGO DOOR LOWER SILL CORRODED.

Part: SKIN — CORRODED (PAX DOOR) · airframe 33,529 hrs · 24,822 cycles

PAX DOOR INNER SKIN CORRODED IN MULTIPLE AREAS. FWD TOP SECTION, MECHANICALLY REMOVED CORROSION ON AREAS ON PAX DOOR INNER SKIN, FWD TOP SECTION, IAW SRM 51-21-06-001-001-A01 1.1-1.3. RECEIVED AND COMPLIED WITH STS ENGINEERING EA 23-2015-171 PERMANENT REPAIR. RECEIVED AND COMPLIED WITH ECTC EA26-2015-171.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 33,410 hrs · 24,714 cycles

MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14, IPC REG 25-61-14, FIG 1A, ITEM 5. OPS CHECK GOOD.

Part: MECHANISM — FOULED (SERVICE DOOR) · airframe 33,393 hrs · 24,698 cycles

UNABLE TO OPEN SERVICE DOOR, DOORS AND OVERWING EMERGENCY EXITS. FOUND HARDWARE FROM ACCESS PANEL FALLEN OUT INTO INNER HANDLE MECHANISIM. REMOVED FOULED HARDWARE & REPLACED SCREW INTO PANEL. CW OPS CHECK OF SERVICE DOOR IAW AMM 52-41-00. OPS CHECK GOOD DEFER CLEAR.

Part: LIGHT — INOPERATIVE (CABIN ROW 6) · airframe 32,966 hrs · 24,341 cycles

ROW 6 CEILING EXIT LIGHT INOPERATIVE. R & R CEILING EXIT LIGHT IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 32,966 hrs · 24,341 cycles

12CD LOWER SIDEWALL EXIT SIGN HAVE 2 LIGHT BULBS BURNED. R & R 12 CD LOWER SIDEWALL EXIT SIGN LIGHT BULBS IAW 33-51-05. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 32,407 hrs · 23,890 cycles

12CD LOWER EXIT SIGN HAVE 2 BULBS BURNED. R & R 12CD LOWER EXIT SIGN LIGHT BULBS IAW AMM 33-51-05.

Part: SKIN — DAMAGED (BS 669-677) · airframe 31,157 hrs · 22,902 cycles

DENT WITH SCRATCH IN FUSELAGE BETWEEN WINDOWS 10 AND 11 ON LT SIDE. DAMAGE FOUND TO BE BETWEEN F/S 669.40 AND F/S 677 AND BETWEEN STRINGERS 10L AND 11L. THIS IS IN A NO DAMAGE ALLOWED AREA IAW SRM 53-41-01. DENT WITH GOUGE MEASURES 2.4" X 1.5" X .040". THIS IS CLASSIFIED A MAJOR REPAIR IAW GMM 5-3. RII COMPLIED WITH IAW GMM 3-3. BLENDED GOUGE OUT OF DAMAGED AREA BETWEEN F/S 669.40 AND F/S 677 AND BETWEEN STRINGERS 10L AND 11L IAW SRM 51-12-00. BLENDED AREA MEASURES 1.8" X .40" X .015". THIS IS CLASSIFIED A MAJOR REPAIR IAW GMM 5-3. RII COMPLIED WITH IAW GMM 3-3.

Part: RETAINER — GOUGED (CARGO DOOR SEAL) · airframe 30,989 hrs · 22,767 cycles

FWD CARGO DOOR SEAL RETAINER GAUGED AT BOTH FWD AND AFT BOTTOM CORNERS. COMPLIED WITH EC/TC REO 670-52-35-127 01, PERMANENT REPAIR. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,190 hrs · 22,144 cycles

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

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 29,302 hrs · 21,499 cycles

CRACK ON PAX DOOR AFT DRAG ANGLE. REPAIRED IAW SRM 52-11-04-201-002-A01.

Part: TRUNNION — DAMAGED (LT MLG) · airframe 29,302 hrs · 21,499 cycles

DURING REMOVAL OF LT TRUNNION STRAP AND AFT MLG DOOR HINGE, THREE HOLES OVERSIZED BEYOND SB670BA-57-020-01. COMPLIED REO 670-57-21-641, REV. P1. MAJOR REPAIR.

Part: STRINGER — GOUGED (BS 1154) · airframe 29,303 hrs · 21,501 cycles

STRINGER 6L GOUGED AT BS 1154. COMPLIED WITH REO 670-53-61-1021 AND REO 670-53-61-1021.

Part: STRINGER — GOUGED (BS 1154) · airframe 29,302 hrs · 21,499 cycles

STRINGER 7L GOUGED AT BS 1154. REPAIRED IAW REO 670-53-61-292 AND EC/TC REO 670-53-61-292. MAJOR REPAIR.

Part: SKIN — CORRODED (WING) · airframe 29,303 hrs · 21,501 cycles

DURING REMOVAL OF AFT DOOR HINGE FOUND CORROSION ON LOWER WING PLANK SURFACE AT WS 54.55. RECEIVED AND COMPLIED WITH REO 670-57-31-644. REPAIRED IAW REO 670-57-21-644 AND ECTC REO 670-57-21-644. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.

Part: BRACKET — CORRODED (MLG DOOR) · airframe 29,303 hrs · 21,501 cycles

AFT MLG DOOR FAIRING BRACKET CORRODED. REPAIRED IAW REO 670-57-21-644 AND ECTC REO 670-57-21-644. MAJOR REPAIR.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 29,302 hrs · 21,499 cycles

INTERCOSTAL HAS CORROSION AT BS 364, STR 27R. REMOVED INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21-001-001-A01. INSTALLED INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 29,303 hrs · 21,501 cycles

AFT SIDE OF PAX DOOR SIDEWALL HAS CRACK AT SECOND STEP DOWN FROM CABIN, NOT COUNTING FOLDING STEP. REPAIRED IAW REO 670-52-11-104 IAW ECTC REO 670-52-11-104. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 29,302 hrs · 21,499 cycles

FS 280 FLOORBEAM HAS CORROSION. FLOORBEAM REPLACED AT INCORPORATION OF SB670BA-53-041, REV C. MAJOR REPAIR

Part: LEAD — DAMAGED (ELECTRICAL) · airframe 29,302 hrs · 21,499 cycles

RT ENGINE IDG CABLE COVERING DAMAGED. INCORPORATED REO 670-24-21-001. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 29,303 hrs · 21,501 cycles

LT VERTICAL STAB DRAG ANGLE CRACKED. REPAIRED IAW 51-42-21-001-001-A01 AND 51-42-10-001-001-A01 AND SRM 51-42-11-001-001, SRM 51-42-06-001-001 AND DWG JBA670-35002. COMPLIED WITH REO 670-55-31-068. MAJOR REPAIR.

Part: LEAD — WORN (ELECTRICAL POWER) · airframe 29,302 hrs · 21,499 cycles

LT ENGINE IDE ELECTRICAL POWER LEADS PROTECTIVE SHEATHS WORN IN SEVERAL PLACES. INCORPORATED REO 670-24-21-001. REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,459 hrs · 20,873 cycles

AFT & FWD F/A`S CAN NOT TURN ON EMERGENCY LIGHTS. OPS CHECKED EMERGENCY LIGHTS IAW AMM 33-51-17. OPS GOOD NO DEFECTS NOTED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 28,134 hrs · 20,653 cycles

CRACKED PAX DOOR AFT DRAG ANGLE COMPLIED WITH REO 670-52-11-287, REV C.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 28,020 hrs · 20,568 cycles

EMERGENCY LIGHTS WILL NOT STAY ON. OPS CHECK EMERGENCY LIGHTS IAW AMM 33-50-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,783 hrs · 20,399 cycles

CENTER CEILING EMERGENCY LIGHT (4TH BACK FROM FRONT) IS INOPERATIVE. RELAMPED CENTER CEILING EMERGENCY LIGHT (4TH BACK FROM FRONT). OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,334 hrs · 20,046 cycles

NR 4 CABIN CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. LAMPED AND OPS CHECKED GOOD IAW AMM 33-51-00.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 26,116 hrs · 19,138 cycles

PHOTOLUMINESCENT STRIP NOT INSTALLED IN GALLEY AREA. INSTALLED PHOTOLUMINESCENT STRIPS IN GALLEY AREA IAW 33-51-01. ACFT OK FOR SERVICE. FERRY FLIGHT COMPLETE AND SATISFACTORY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,575 hrs · 18,760 cycles

CEILING EMERGENCY LIGHT IS OUT AT ROW 15. RELAMPED CEILING EMERGENCY LIGHT IAW AMM 33-51-09.

Part: PLACARD — MISSING (EMERGENCY EXIT) · airframe 25,540 hrs · 18,740 cycles

RT EMERGENCY EXIT EXTERIOR (PUSH IN FLAP) PLACARD IS MISSING. INSTALLED PLACARD IAW AMM 11-10-01.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 25,273 hrs · 18,553 cycles

FS 280 CROSSBEAM CORRODED. REPAIRED IAW REO 670-53-11-047, REV E.

Part: SEAT TRACK — CORRODED (BS 683-701) · airframe 25,273 hrs · 18,553 cycles

RT SEAT TRACK CORRODED FROM FS 683 TO 701. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A02. FABRICATED NEW TRACK IAW REO 670-53-00-343. INSTALLED RT FLOOR SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 25,273 hrs · 18,553 cycles

COCKPIT FLOOR SUPPORT AT FS 280.00 IS CORRODED. R & R FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01.

Part: BULKHEAD — CORRODED (BS 280) · airframe 25,273 hrs · 18,553 cycles

LT LOWER FS 280 BULKHEAD FOUND TO BE CORRODED. BULKHEAD WEB REPLACED IAW GREO 670-53-11-594.

Part: BULKHEAD — CORRODED (BS 280) · airframe 25,273 hrs · 18,553 cycles

RT LOWER FS 280 BULKHEAD FOUND TO BE CORRODED. BULKHEAD WEB REPLACED IAW GREO 670-53-11-594.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 25,273 hrs · 18,553 cycles

COCKPIT FLOORBEAM AT FS.280.00 IS CORRODED. R & R FLOORBEAM IAW SRM 51-42-06-001-001-A01.

Part: ANGLE — CRACKED (BS 280) · airframe 25,273 hrs · 18,553 cycles

ANGLES AT FS 280 AND LBL RBL 26.0 CRACKED OUT OF LOWER HOLE. REMOVED ANGLE IAW SRM 51-42-06-001-001-A01. FABRICATED NEW ANGLE IAW SRM 51-24-16-001-001-A01.

Part: BRACKET — CRACKED (FLOORBEAM) · airframe 25,309 hrs · 18,575 cycles

REMOVED BRACKETS FROM FS 280 FLOORBEAM AT LT AND RT BL 9. UPON REMOVAL FOUND LT & RT TEE BRACKET TO BE CRACKED REMOVED BY SRM 51-42-21-001-001-A01. DRILLED UP NEW TEE BRACKET LT & RT AND INSTALLED ON ACFT AFTER FS280 REPAIR IAW SRM 51-42-21-001-001-A01. THIS IS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 25,273 hrs · 18,553 cycles

RIGHT SEAT TRACK IS CORRODED IN NUMEROUS PLACES FROM FS 581 TO 677. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 379-483) · airframe 25,273 hrs · 18,553 cycles

LT SIDE SEAT TRACK CORRODED IN NUMEROUS PLACES FROM FS 379 TO 483. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 25,273 hrs · 18,553 cycles

RIGHT SEAT TRACK IS CORRODED IN NUMEROUS PLACES FROM FS 485 TO 581. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 713-763) · airframe 25,273 hrs · 18,553 cycles

RT SIDE SEAT TRACK IS CORRODED AT FS 738, TRACK 713 TO 763. REMOVED SEAT TRACK IAW AMM TASK 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 374-381) · airframe 25,273 hrs · 18,553 cycles

LT FLOOR SEAT TRACK IS CORRODED AT FS 374 TO FS 381. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A02. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 25,273 hrs · 18,553 cycles

RIGHT SEAT TRACK CORRODED IN NUMEROUS PLACES FROM FS 349 TO 485. CUT EXTRUSION TO LENGTH, DRILLED HOLES & COUNTER SUCK HOLES FOR SCREWS IAW REO 670-53-00-343 ALSO ALODINE, PRIME & PAINT SRM 51-25-16. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 379-483) · airframe 25,273 hrs · 18,553 cycles

RIGHT SEAT TRACK IS CORRODED IN NUMEROUS PLACES FROM FS 379 TO 483. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED RT SIDE SEAT TRACK IAW AMM 53-00-49-400-801 A01.

Part: SEAT TRACK — CORRODED (BS 683-701) · airframe 25,273 hrs · 18,553 cycles

RIGHT SEAT TRACK IS CORRODED IN NUMEROUS PLACES FROM FS 683 TO 701. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A02. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 573-661) · airframe 25,273 hrs · 18,553 cycles

RT SIDE SEAT TRACK IS CORRODED IN NUMEROUS PLACES FROM FS 573-661. REMOVED SEAT TRACK SECTION BETWEEN FS 573 AND 661 IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 675-713) · airframe 25,273 hrs · 18,553 cycles

RT SIDE SEAT TRACK CORRODED IN NUMEROUS PLACES FS 675-713. REMOVED SEAT TRACK IAW REO 670-53-00-343 CUT, DRILLED COUNTER SUNK, ALODINED, PRIMED & PAINT SEAT TRACK. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 25,273 hrs · 18,553 cycles

RIGHT SEAT TRACK IS CORRODED IN NUMEROUS PLACES FROM FS 485 TO 581. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 381-485) · airframe 25,273 hrs · 18,553 cycles

LEFT SEAT TRACK IS CORRODED IN NUMEROUS PLACES FROM FS 381 TO 485. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 25,273 hrs · 18,553 cycles

LEFT SEAT TRACK IS CORRODED IN NUMEROUS PLACES FROM FS 485 TO 581. REMOVED LT FLOOR SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 581-683) · airframe 25,273 hrs · 18,553 cycles

LEFT SEAT TRACK IS CORRODED IN NUMEROUS PLACES FROM FS 581 TO 683. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 25,273 hrs · 18,553 cycles

FS 280.00 CROSSBEAM CORRODED. R & R CROSSBEAM IAW SRM 51-42-06-001-001, 51-42-21-001-001 & REO 670-53-11-047.

Part: PAN — CRACKED (BS 193) · airframe 25,273 hrs · 18,553 cycles

FWD FUSELAGE, TRU FLOOR PAN CRACKED FROM AFT CORNER CUT OUT AT FS 193.00 AND STR 20R, GOING UNDER ADG PUMP PAN RT SIDE. REMOVED ADG ACTUATOR PAN IAW ARM 51-41-02. INSTALLED NEW PAN IAW SRM 51-41-02.

Part: SKIN — CORRODED (FUSELAGE) · airframe 25,273 hrs · 18,553 cycles

FWD FUSELAGE UPPER VHF ANTENNA PAINT PEELING AND SURFACE SKIN CORRODED. R & R VHF-1 ANTENNA IAW AMM 23-11-05-000-801 AND AMM 23-11-05-400-801.

Part: PAN — CRACKED (BS 193 S20L) · airframe 25,273 hrs · 18,553 cycles

FWD FUSELAGE, TRU FLOOR PAN CRACKED FROM AFT CORNER CUTOUT AT FS 193.00 AND STR 20L, (UNDER AREA OF BRAKE GAUGES) LT SIDE. REPAIRED IAW AMM 24-31-01-000-801-A01.

Part: STEP — CRACKED (PAX DOOR) · airframe 25,273 hrs · 18,553 cycles

ASD BOTTOM STEP CRACKED AT ROD END. R & R WITH SERVICEABLE STEP IAW AMM TASK 52-11-04-000-806 AND 52-11-04-400-806.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 24,303 hrs · 17,878 cycles

MEGA PHONE INOP. TURNED VOL UP. OPS CHECKED OK IAW 25-60-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,778 hrs · 17,505 cycles

EMERGENCY LIGHTS WILL NOT TEST. FOUND EMERGENCY BATTERIES DISCHARGED AND COULD NOT CHARGE. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERIES. OPS. CHECKED GOOD IAW AMM 33-51-17.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,778 hrs · 17,505 cycles

EMERGENCY LIGHTS WILL NOT TEST. FLT 5394. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-17.

Part: SLAT SYSTEM — FAILED · airframe 23,647 hrs · 17,417 cycles

SLATS FAIL CAUTION MESSAGE ON APPROACH. SYSTEM RESET IAW FIM 27-81-00. OPS CHECK GOOD IAW AMM 27-50-00.

Part: DOOR FRAME — CORRODED (BS 327.7-338.9) · airframe 22,118 hrs · 16,203 cycles

C CHECK - CORROSION FOUND ON INNER PAX DOOR LOWER FRAME UNDER REMOVED RESIN BETWEEN DOOR FRAME 327.7 - 338.9. REMOVED RIVETS TO ALLOW ACCESS IAW SRM 51-42-06-001-001-A01. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. DAMAGE FOUND TO BE WITHIN LIMITS IAW SRM 52-11-01-101-001-A01. INSTALLED 10 RIVETS IAW SRM 51-42-06-001-001-A01. TREATED, PRIMED, AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, AND 51-25-16-001-001-A01.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · airframe 22,120 hrs · 16,203 cycles

INNER PAX DOOR CLIPS AT FRAME 320 AND 358 ARE CORRODED (4 TOTAL). MADE NEW CLIP MATERIAL FROM 2075-T6. OLD CLIPS BEYOND LIMITS, INSTALLED AND PRIMED AND PAINTED 4 NEW CLIPS.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 22,120 hrs · 16,203 cycles

FOUND CORROSION ON INNER DOUBLER OF THE LOWER TCAS ANTENNA. REMOVED FASTENERS TO GAIN ACCESS AND BLENDED CORROSION. NDT AND MEASURED WITHIN LIMITS BLENDED AREAS. REINSTALLED HARDWARE.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 22,118 hrs · 16,203 cycles

C-CHECK - FLOOR SUPPORT ANGLE FOR PANEL 141ALF HAS CORROSION AT FS 280. DRILLED OFF FLOOR SUPPORT ANGLE. ANGLE IS CORRODED BEYOND LIMITS IAW SRM 51-42-06-001-001-A01 AND TASK 53-21-43-101-001-A01 AND 53-21-43-001-A01 PG 103. LOCATED FASTENER HOLES IN NEW PART IAW SRM 51-40-11-001-001-A01. INSTALLED NEW ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. TOPCOATED IAW SRM 51-25-16-001-001-A01. APPLIED CORROSION INHIBITOR IAW SRM 51-21-11-001-001-A01.

Part: DOOR — STIFF (MAIN PAX) · airframe 21,219 hrs · 15,565 cycles

MAIN CABIN DOOR HARD TO OPEN AND CLOSE. INSPECTED MCD FOR OBVIOUS DEFECTS, NONE NOTED. CYCLED DOOR SEVERAL TIMES, DOOR OPERATES NORMALLY. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: HOLDER — ARCED (COKCPIT) · airframe 21,179 hrs · 15,536 cycles

CAPTAIN'S SIDE CHART HOLDER ARCED AND IS INOP. DEACTIVATED AND PLACED ON MEL 33-11-1. RETURNED TO SERVICE.

Part: SKIN — CHAFED (LT TE FLAP) · airframe 21,118 hrs · 15,491 cycles

GROUND STRAP IS CHAFING SKIN IN LT INBD FLAP AT APPROX WS 60. BLENDED DAMAGED AREA. HFEC INSPECTED BLEND FOR CRACK IAW NDTM PART 6, 53-00-000-250-A01. NO CRACKS NOTED. HT THICKNESS CHECK IAW NDTM PART 1, 51-20-004. WITHIN LIMITS IAW SRM 57-52-01-101-001-A01. ALODINED AND PRIMED AREA.

Part: SKIN — CHAFED (TE FLAP) · airframe 21,118 hrs · 15,491 cycles

GROUND STRAP IS CHAFING SKIN AND RIVETS IN LT INBD FLAP AT APPROX WS 102. FOUND DAMAGE TO BE THROUGH PAINT ONLY ON SKIN. REPLACED DAMAGED RIVET IAW SRM 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (E/E BAY DOOR) · airframe 20,914 hrs · 15,343 cycles

DURING INSP FOUND CORROSION ON AVIONICS BAY DOOR INTERCOSTAL 27R AT FS 364.00, AFT PART OF ATTACH FLANGE ON BOTH SIDES OF WEB. REMOVED CORROSION, REMAINING MATERIAL THICKNESS FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23. REMOVED INTERCOASTAL IAW SRM 51-21-06-001-001-A01 AND 51-42-06-001-001-A01 PG 9. PREPARED NEW INTERCOSTAL IAW SRM 51-40-11-001-001-A01. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (BS 310-319 S26R) · airframe 20,914 hrs · 15,343 cycles

CORROSION FOUND AT FS 310-319 STR 26R. FOUND S26R FS 280-333 TO BE DAMAGED GREATER THAN 30 PERCENT LENGTH IAW SRM 53-21-03-101-002-A01. REMOVED STR IAW SRM 51-42-06-001-001-A01. PERFORMED LPI ON STR 26R, NO CRACKS FOUND IAW LPI NDTM 51-20-008. INSTALLED STRINGER 26R IAW REO 670-53-21-514. PRIMED AND PAINTED IAW SRM 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. COMPLETED REPAIR IAW REO 670-53-21-514. TOPCOATED AND APPLIED CORROSION INHIBITING COMPOUND IAW 51-25-00-001-001-A01 AND 51-21-11-001-001-A01.

Part: STRUCTURE — CORRODED (BS 280-364) · airframe 20,914 hrs · 15,343 cycles

CORROSION FOUND BETWEEN FS 280.00 THRU FS 364.0. COMPLIED WITH REPAIRS IAW REO 670-53-21-513, 670-53-21-514 AND 670-53-21-517.

Part: STRINGER — CORRODED (BS 295-310 S26R) · airframe 20,914 hrs · 15,343 cycles

CORROSION FOUND FS 295.0 TO FS 310.0 SRT 26R. DAMAGE FOUND TO BE GREATER THAN 30 PERCENT LENGTH IAW SRM 53-21-03-101-002-A01. REMOVED STRINGER IAW REO 670-53-21-514. PERFORMED LPI IAW LPI NDTM 51-20-008. PREPARED NEW STR IAW REO 670-53-21-514, INSTALLED NEW STRINGER IAW REO 670-53-21-514. PRIMED AND PAINTED RIVETS IAW SRM 51-26-06-001-001-A01 AND 51-25-16-001-001-A01. COMPLETED REPAIR IAW REO 670-53-21-514. TOPCOATED AND APPLIED CORROSION INHIBITING COMPOUND IAW 51-25-00-001-001-A01 AND 51-21-11 -001-001-A01.

Part: STRINGER — CORRODED (BS 282-295 S26R) · airframe 20,914 hrs · 15,343 cycles

FOUND CORROSION ON STR 26R FROM FS 282.00 TO FS 295.00. BLENDED OUT ALL CORROSION IAW SRM 51-21-06-001-001-A01, REMAINING MATERIAL IS OUT OF LIMITS IAW SRM 51-21-03. SENT TO MFG FOR AN REO REPAIR. REMOVED STR IAW SRM 51-42-06-001-001-A01. PERFORMED LPI ON NEW STRINGER IAW LPI NDTM 51-20-008. PREPARE NEW STRINGER IAW REO 670-53-21-514. INSTALLED NEW STR IAW REO 670-53-21-514. PRIMED AND PAINTED RIVETS IAW SRM 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. COMPLETED REPAIR IAW REO 670-53-21-514, TOPCOATED AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-25-00-001-001-A01 AND 51-21-11-001-001-A01.

Part: STRINGER — CORRODED (BS 319-333 S26R) · airframe 20,914 hrs · 15,343 cycles

CORROSION FOUND AT FS 319-333.00 STR 26R. FOUND STR 26R FS 280-333 TO BE DAMAGED GREATER THAN 30 PERCENT LENGTH IAW SRM 53-21-03-101-002-A01. REMOVED STRINGER IAW SRM 51-42-06-001-001-A01. PERFORMED LPI ON STR 26R, NO CRACKS FOUND IAW LPI NDTM 51-20-008. INSTALLED STR 26R IAW REO 670-53-21-514. PRIMED AND PAINTED IAW SRM 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. COMPLETED REPAIR IAW REO 670-53-21-514. TOPCOATED AND APPLIED CORROSION INHIBITING COMPOUND IAW 51-25-00-001-001-A01 AND 51-21-11-001-001-A01.

Part: STRINGER — CORRODED (BS 310-319 S26L) · airframe 20,914 hrs · 15,343 cycles

CORROSION FOUND FS 310.00 THRU 319.00 STR 26L. BLENDED OUT CORROSION IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-03. SENT TO MFG FOR REO. PERFORMED ECI ON STR 26L IAW ECI NDTM 51-20-006. PERFORMED LPI ON STR 26L IAW LPI NDTM 51-20-008. ATTACHED NEW STRINGER IAW SRM 51-42-06-001-001-A01. PRIMED AND PAINTED RIVET HEADS IAW SRM 51-25-16-001-001-A01. COMPLETED REPAIR IAW REO 670-53-21-514. TOP COATED AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-25-00-001-001-A01 AND 51-21-11-001-001-A01.

Part: DOOR — DAMAGED (CARGO BAY) · airframe 20,914 hrs · 15,343 cycles

DURING INSP FOUND DAMAGE TO INBD EDGES OF AFT BAGGAGE BAY DOOR SURROUND LWR COATING. BLENDED IAW CRJ700 SRM 51-12-00-001-001-A01. NO DAMAGE ALLOWED IN AREA. SENT TO BOMBARDIER FOR REO. PERFORMED LPI IAW NDTM LPI 51-20-008. REPAIRED DAMAGE IAW REO 670-53-61-532. TREATED PRIMED AND PAINTED IAW CRJ700 SRM 51-21-16-001-001-A01.

Part: SILL — CORRODED (FUSELAGE) · airframe 20,914 hrs · 15,343 cycles

DURING INSP FOUND CORROSION ON AFT BAGGAGE BAY CUTOUT LWR SILL. BLENDED OUT CORROSION, NO ALLOWABLE DAMAGE IAW SRM 51-21-06-001-001-A01. MAPPED AND SENT TO MFG FOR ENGINEERING. PERFORMED ECI IAW ECI 51-20-006. REPAIRED CORRODED AREA IAW REO 670-53-61-533. TREATED, PRIMED AND PAINTED REPAIR IAW SRM 51-21-11-001-001-A01, 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: STRINGER — CORRODED (BS 282 S26L) · airframe 20,914 hrs · 15,343 cycles

CORROSION FOUND INBD SIDE OF STR 26L ABOVE FS 282.00. BLENDED OUT CORROSION IAW SRM 51-21-06-001-001-A01, REMAINING MATERIAL THICKNESS FOUND TO BE OUT OF LIMITS IAW SRM 53-21-03-101-002-A01. SENT TO MFG FOR REO. PERFORMED ECI ON STR 26L, NO CRACKS FOUND IAW NDTM 51-20-006. PERFORMED LPI ON CUTLINE ON NEW STR 26L, IAW LPI NDTM 51-20-008. PREPARED NEW STRINGER FOR INSTALL, INSTALLED NEW STR 26L IAW SRM 51-42-06-001-001-A01 PRIMED AND PAINTED IAW SRM 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. COMPLETED REPAIR IAW REO 670-53-21-514. TOPCOATED AND APPLIED CORROSION INHIBITING COMPOUND IAW 51-25-00-001-001-A01 AND 51-21-11-001-001-A01.

Part: STRINGER — CORRODED (BS 319-333 S24R) · airframe 20,914 hrs · 15,343 cycles

CORROSION FOUND AT FS 319.-333 S24R. BLENDED OUT CORROSION AND FOUND BLENDS TO BE IN A NO DAMAGE ALLOWED AREA. SENT TO MFG FOR REO. PERFORMED ECI ON STR 24R, NO CRACKS FOUND IAW NDTM 51-20-006. PERFORMED LPI ON CUTLINE ON NEW S24R, IAW NDTM 51-20-008. INSTALLED STRINGER 24R AND COMPLETED REPAIR IAW REO 670-53-21-514. TOPCOATED AND APPLIED CORROSION INHIBITING COMPOUND IAW 51-25-00-001-001-A01 AND 51-21-11-001-001-A01.

Part: INTERCOSTAL — CORRODED (E/E BAY DOOR) · airframe 20,914 hrs · 15,343 cycles

DURING INSP FOUND CORROSION ON AVIONICS BAY DOOR INTERCOSTAL FWD 26R FS 364.00 ON AFT PART OF ATTACH FLANGE. BLENDED OUT CORROSION, REMAINING MATERIAL THICKNESS IS OUT OF LIMITS IAW SRM 51-21-23. SENT TO MFG FOR REO. PERFORMED LPI IAW NDTM 51-20-008. REMOVED STR 26R IAW SRM 51-42-06-001-001-A01. FABRICATED AND PREPARED NEW STR IAW REO 670-53-21-517, INSTALLED NEW STR IAW REO 670-53-21-517. PRIMED AND PAINTED RIVETS IAW SRM 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. COMPLETED REPAIR IAW REO 670-53-21-514, TOPCOATED AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-25-00-001-001-A01 AND 51-21-11-001-001-A01.

Part: STRINGER — CORRODED (BS 295-310 S26L) · airframe 20,914 hrs · 15,343 cycles

CORROSION FOUND AT FS 295-310 ON STR 26L. BLENDED OUT CORROSION IAW SRM 51-21-06-001-001-A01, REMAINING MATERIAL THICKNESS IS OUT OF LIMITS IAW SRM 53-23-03-101-002-A01. SENT TO MFG FOR REO. PERFORMED ECI, IAW ECI NDTM 51-20-006. PERFORMED LPI ON S26L IAW LPI NDTM 51-20-008 NO CRACKS FOUND. INSTALLED NEW STRINGER IAW SRM 51-42-06-001-001-A01. PRIMED IAW SRM 51-25-06-001-001-A01 PAINTED IAW SRM 51-25-16-001-001-A01. COMPLETED REPAIR IAW REO 670-53-21-514. PAINTED REPAIR AS REQUIRED AND APPLIED AV8 IAW SRM 51-25-00-001-001-A01 AND 51-21-11-001-001-A01.

Part: BUTTSTRAP — CORRODED (BS 282 S26R) · airframe 20,914 hrs · 15,343 cycles

CORROSION FOUND ON BUTTSTRAP AT FS 282.00 S26R. FOUND NO CORROSION ON BUTTSTRAP AFTER FURTHER CLEANING OF AREA IAW SRM 51-10-06. REMOVED CORROSION FOUND ON STR 26 IAW SRM 51-21-06, REMAINING MATERIAL THICKNESS IS OUT OF LIMITS IAW SRM 53-21-03. SENT TO MFG FOR REO. REMOVED STR 26R IAW SRM 51-42-06-001-001-A01. PERFORMED LPI, NO CRACKS FOUND IAW NDTM 51-20-008. PREPARED NEW STR FOR INSTALL, INSTALLED STR IAW REO 670-53-21-514. TOPCOATED AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-25-00-001-001-A01 AND 51-21-11-001-001-A01.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 20,914 hrs · 15,343 cycles

SEVERAL AREA OF CORROSION FOUND UNDER SERVICE DOOR SCUFF PLATE, FOUND ONE DENT AT FS 333.00 UNDER SCUFF PLATE. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. MAX MATERIAL REMOVED .008". SIZE OF BLENDS MEASURE .750 " WIDE, 1.000 LONG AND .800 WIDE BY 1.500 LONG, IAW SRM 51-21-06-001-001-A01. SENT TO ENGINEERING FOR REO. PERFORMED LPI IAW NDTM LPI 51-20-008. TREATED, PRIMED AND PAINTED IAW SRM 51-21-16-001-001-A01. ALL WORK DONE IN COMPLIANCE WITH REO 670-53-21-516.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,914 hrs · 15,343 cycles

FS 280 BEAM IS CORRODED RT AND LT. BEAMS CORRODED THROUGHOUT, REMOVED 280 BEAMS IAW SRM 51-42-06-001-001-A01. PERFORMED LPI ON CROSSBEAM CUTLINE IAW REO 670-53-11-047. LOCATED FASTENER HOLES IN NEW BEAMS IAW 51-40-11-001-001-A01. INSTALLED BEAMS IAW REO 670-53-11-047.

Part: UNKNOWN — CORRODED (BS 280-295 S23R) · airframe 20,914 hrs · 15,343 cycles

CORROSION FOUND FS 280.00 - 295.00 STR 23R. REMOVED CORROSION, WORK DONE IAW SRM 51-21-06-001-001-A01, 51-42-06-001-001-A01 PG 9 AND 53-21-03-002A-1 PG 104. REQUESTED REO REPAIR FROM MFG. PERFORMED ECI ON STR 23R FS 280-295.00, NO CRACKS OR CORROSION FOUND AT THIS TIME IAW ECI NDTM 51-20-008. TREATED, PRIMED AND PAINTED IAW SRM 51-21-16-001-001-A01. ALL WORK DONE IN CONFORMITY WITH REO-53-21-514. APPLIED HARDCOAT IAW SRM 51-21-11-001-001-A01.

Part: ANGLE — CORRODED (DOOR STRIKER) · airframe 20,914 hrs · 15,343 cycles

PAX DOOR LWR STRIKER ANGLE IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06. FOUND TO BE BEYOND LIMITS IAW SRM 53-21-23. REMOVED STRIKER ANGLE IAW SRM 51-42-06. LOCATED HOLES AND INSTALLED NUTPLATES ON NEW STRIKER ANGLE IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. INSTALLED NEW STRIKER ANGLE IAW SRM 51-42-06-001-001-A01.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 20,914 hrs · 15,343 cycles

PAX DOOR MID CAP ANGLE IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06. FOUND TO BE BEYOND LIMITS IAW SRM 53-21-23. REMOVED ANGLE IAW SRM 51-42-06. LOCATED HOLES AND INSTALLED NUTPLATES ON NEW ANGLE IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. INSTALLED NEW MID CAP ANGLE IAW SRM 51-41-00-001-001-A01 AND 51-42-21-001-001-A01.

Part: SKIN — CHAFED (LT WING SLAT) · airframe 20,914 hrs · 15,343 cycles

LT WING INBD SLAT LWR T/E CHAFED AT WING PICCILLO TUBE CONNECTION AND INBD ELECTRICAL CONNECTOR. BLENDED DAMAGED AREA IAW 51-21-00-001-001-A01. REQUESTED REO REPAIR FROM MFG. PERFORMED LPI, NO CRACKS OR CHAFING FOUND AT THIS TIME IAW LPI NDTM 51-20-006. TREATED, PRIMED AND PAINTED IAW 51-21-16-001-001-A01. ALL WORK PERFORMED IN CONFORMITY WITH REO 670-57-42-229.

Part: ANGLE — CORRODED (DOOR STRIKER) · airframe 20,914 hrs · 15,343 cycles

SERVICE DOOR STRIKER ANGLE IS CORRODED. BLENDED OUT CORROSION IAW SRM 51-21-06. FOUND WITHIN LIMITS IAW SRM 53-21-23. TREATED AND PRIMED IAW SRM 51-25-01-001-001-A01. PAINTED IAW SRM 51-25-16-001-001-A01.

Part: WEB — CORRODED (BS 280) · airframe 20,914 hrs · 15,343 cycles

FS 280 RT AND LT WEBBING IS CORRODED AT BEAM. BLENDED CORROSION FROM LT FS 280 WEB IAW SRM 53-11-10-003-A01. RT FS 280 WEB FOUND TO BE OUT OF LIMITS, DRILLED OFF RT WEB IAW SRM 53-11-10-003-A01 PAGE 201. LOCATED FASTENER HOLES IN NEW WEB IAW SRM 51-40-11-001-001-A01 AND 53-11-10-201-003-A01. INSTALLED RT WEB IAW SRM 51-42-06, 51-42-13. TREATED, PRIMED, AND PAINTED ALL AFFECTED AREAS ON LT WEB, PAINTED NEW RT WEB REF SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-00-001-001-A01.

Part: UNKNOWN — CORRODED (BS 280-295 S19L) · airframe 20,914 hrs · 15,343 cycles

CORROSION FOUND FS 280.00 THRU 295.00 STR 19L. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDED TO .009 DEEP BY .024 WIDE BY 2.0 LONG, NO ALLOWABLE DAMAGE IAW SRM 51-21-03-001-001-A01. PERFORMED ECI ON STR 19L FS 280 TO 295, NO CRACKS OR CORROSION FOUND AT THIS TIME IAW NDTM 51-20-006 ECI. REQUESTED REO FROM MFG. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, AND 51-25-00-001-001-A01. ALL WORK IAW REO 670-53-21-514 REV A.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 20,914 hrs · 15,343 cycles

SERVICE DOOR STRIKER SEAL HAS CORROSION ON INBD SIDE. BLENDED OUT CORROSION IAW SRM 51-21-06. PERFORMED ECI IAW 51-20-006, NO CRACKS OR CORROSION AT THIS TIME. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. APPLIED CORROSION INHIBITOR IAW SRM 51-21-11-001-001-A01.

Part: ANGLE — CORRODED (BS 310-314 S21L) · airframe 20,914 hrs · 15,343 cycles

CORROSION FOUND AT STR 21L BETWEEN FS 310 AND 314. REMOVED DIVERTER ANGLE IAW SRM 51-42-06. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23. REMOVED BACKUP SILL IAW SRM 51-42-06. INSTALLED NEW SILL IAW SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. REINSTALLED DIVERTER ANGLE IAW SRM 51-42-06-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,914 hrs · 15,343 cycles

COCKPIT FLOOR ANGLE CORRODED ON FWD SIDE OF FS 280 BEAM. REMOVED CORRODED CTR ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED NEW PART IAW REO 670-53-11-047 AND SRM 51-42-06-001-001-A01.

Part: MOUNT — CORRODED (DOOR SURROUND) · airframe 20,914 hrs · 15,343 cycles

FOUND DEEP PITTING CORROSION ON SERVICE DOOR SURROUND STRUCTURE MOUNTING PLATE AT FLOOR LEVEL FROM FS 331 TO FS 336.75. REMOVED ANGLE IAW SRM 51-42-06-001-001-A01. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND OUT OF LIMITS. INSTALLED NEW ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-25-16-001-001-A01. APPLIED IAW SRM 51-21-11-001-001-A01.

Part: INTERCOSTAL — CORRODED (E/E DOOR) · airframe 20,914 hrs · 15,343 cycles

DURING INSP FOUND CORROSION ON AVIONICS BAY DOOR INTERCOSTAL (FWD) 27L AT FS 364. REMOVED 8 RIVETS IAW SRM 51-42-06-001-A01. BLENDED OUT CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-003-A01. PERFORMED LPI IAW LPI NDTM 51-20-008. TREATED, PRIMED AND PAINTED WORKED AREA IAW SRM 51-21-06-001-001-A01. INSTALLED 8 RIVETS IAW SRM 51-42-06. PRIMED, PAINTED AND HARDCOATED IAW SRM 51-25-01-001-001-A01. WORK PERFORMED IN CONFORMITY WITH REO670-53-21-513.

Part: STRUCTURE — CORRODED (BS 333 S26-27L) · airframe 20,914 hrs · 15,343 cycles

DURING INSP, FOUND CORROSION ON FS 333.00 BETWEEN STR 27 AND STR 26L. REMOVED FASTENERS FOR ACCESS IAW SRM 51-42-06-001-001-A01 PG 9. BLENDED DAMAGED IAW SRM 51-21-06-001-001-A01. PERFORMED ECI IAW ECI NDTM 51-20-006. TREATED, PRIMED, INSTALLED RIVETS AS REQUIRED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, 51-42-06-001-001-A01 AND 51-25-16-001-001-A01. APPLIED CORROSION INHIBITOR IAW SRM 51-21-11-001-001-A01. ALL WORK IN CONFORMITY WITH REO 670-53-21-515.

Part: SILL — CORRODED (BS 280-319) · airframe 20,914 hrs · 15,343 cycles

DURING INSP, FOUND CORROSION ON RT SIDE FLOOR SILL AND BLANKING PLATE FROM FS 280-319.70. REMOVED FASTENERS FOR ACCESS IAW SRM 51-42-13-001-001-A01 & 51-42-06-001-001-A01. BLENDED DAMAGED IAW SRM 51-21-06-001-001-A01 & FOUND TO BE OUT OF LIMITS IAW 53-00-00-101-001-A01. REMOVED SILL IAW SRM 51-42-06. PREPARED NEW SILL FOR INSTALLATION IAW SRM 51-42-06. INSTALLED NEW SILL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. FABRICATED NEW .040 2024 T3 BLANKING PLATE IAW DRG SH670-33549-3. TREATED & PRIMED PART IAW SRM 51-21-11-001-001-A01 & 51-25-06-001-001-A01. INSTALLED BLANKING PLATE IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. TOP COATED RIVETS IAW SRM 51-25-16-001-001-A01.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 20,914 hrs · 15,343 cycles

FWD BAGGAGE BAY DOOR HAS CHAFE DAMAGE ON BOTH FWD AND AFT INBD INNER SKIN. REMOVED FASTENERS FOR ACCESS IAW SRM 51-42-13-001-001-A01. BLENDED SMOOTH IAW SRM 51-21-06-001-001-A01. FOUND OUT OF LIMITS, SENT TO ENGINEERING. BLENDED AND TRIMMED SKIN IAW REO 670-52-35-180. INSTALLED FASTENERS IAW SRM 51-42-13-001-001-A01. PRIMED AND PAINTED FASTENERS IAW SRM 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. PERFORMED LPI IAW LPI NDTM 51-20-008. TREATED, PRIMED, PAINTED REPAIR IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, AND 51-25-16-001-001-A01. ALL WORK IN CONFORMITY WITH REO 670-52-35-180.

Part: GUSSET — CORRODED (E/E BAY DOOR) · airframe 20,914 hrs · 15,343 cycles

DURING INSP FOUND CORROSION ON AVIONIC BAY DOOR FWD RT GUSSET AT FS 364.00. BLENDED OUT ALL CORROSION, FOUND WITHIN LIMITS IAW SRM 53-21-23. TREATED, PRIMED AND PAINTED IAW SRM 51-25-01-001-001-A01, AND 51-25-01-001-001-A01. APPLIED HARDCOAT IAW SRM 51-21-11-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 20,914 hrs · 15,343 cycles

LEFT SEAT TRACK FS 485 TO 565 HAS CORROSION. BLENDED AREAS OF CORROSION, FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED LT SEAT TRACK IAW 53-00-49-000-801. PREPARED NEW SEAT TRACK FOR INSTALL IAW SRM 51-40-11 AND 51-21-11. INSTALLED LT SIDE SEAT TRACK FS 485 TO 565 IAW AMM 53-00-49-400-801-A01.

Part: SKIN — CHAFED (LT AILERON) · airframe 20,914 hrs · 15,343 cycles

LT AILERON PANEL 589AB CHAFED. BLENDED IAW SRM 51-21-06-001-001-A01. REMOVED .005 MAX MATERIAL, WITHIN LIMITS IAW SRM 57-61-01-001-001-A01. TREATED, PRIMED, PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01.

Part: STRUCTURE — CORRODED (BS 517 S25L) · airframe 20,914 hrs · 15,343 cycles

CORROSION FOUND AT FS 517.00 STR 25L FWD CARGO. REMOVED 3 RIVETS IAW SRM 51-42-06. BLENDED IAW SRM 51-21-06, FOUND WITHIN LIMITS IAW SRM 53-31-06-003-A01. TREATED IAW SRM 51-21-11. PRIMED IAW SRM 51-25-06-001-001-A01. PAINTED AREA AND RIVETS IAW SRM 51-25-16-001-001-A01. APPLIED AV8 IAW SRM 51-21-11-001-001-A01.

Part: SKIN — CORRODED (FUSELAGE) · airframe 20,614 hrs · 15,343 cycles

CORROSION FOUND ON INNER SURFACE OF SKIN AT AVIONICS BAY DOOR CUT OUT. BLENDED CORROSION IAW REO 670-53-21-242. APPLIED FINISH COATING IAW SRM 51-21-16. PERFORM LPI ON CUT OUT IAW REO 670-53-21-242 NO DEFECTS NOTED. ALL WORK DONE IN CONFORMITY WITH REO 670-53-21-242.

Part: BUTTSTRAP — CORRODED (BS 282 S23-24L) · airframe 20,914 hrs · 15,343 cycles

CORROSION FOUND ON BUTTSTRAP AT FS 282.00 BETWEEN STR R23L TO STR R24L. REMOVED 20 RIVETS FOR ACCESS IAW SRM 51-42-06. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-01. PERFORMED ECI ON BUTTSTRAP IAW NDTM 51-20-006. TREATED PRIMED AND PAINTED IAW SRM 51-21-11, 51-25-06 AND 51-25-16-001-001-A01. INSTALLED 20 NEW RIVETS IAW SRM 51-42-06-001-001-A01. PRIMED RIVETS IAW SRM 51-25-06-001-001-A01, TOP COATED RIVETS IAW SRM 51-25-16-001-001-A01. APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: FITTING — GOUGED (RT MLG) · airframe 20,914 hrs · 15,343 cycles

RIGHT MLG SIDE STAY FITTING HAS GOUGE ON O/B UPPER FLANGE. BLENDED OUT CHAFE, FOUND DAMAGE TO BE WITHIN LIMITS IAW REO 670-57-11-043. PERFORMED LPI IAW REO 670-57-11-043. NO DEFECTS NOTED. PERFORMED ROTO PEEN IAW REO 670-57-11-043. TREATED, PRIMED AND PAINTED WORKED AREA IAW SRM 51-25-01-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 566-660) · airframe 20,914 hrs · 15,343 cycles

LT SIDE SEAT TRACK F/S 566 TO 660 HAS CORROSION. BLENDED AREAS OF CORROSION AND FOUND OUT OF LIMITS IAW REO 670-53-00-013. REMOVED LT SIDE SEAT TRACK F/S 566 TO F/S 660 IAW AMM 53-00-49-000-801. PREPARED NEW SEAT TRACK FOR INSTALLATION IAW SRM 51-40-11. ETCHED AND ALODINED NEW SEAT TRACK IAW SRM 51-21-11. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 785-830) · airframe 20,914 hrs · 15,343 cycles

RT SIDE SEAT TRACK F/S 785 TO 830 HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. PREPARED NEW SEAT TRACK FOR INSTALLATION IAW AMM 51-40-11. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 785-830) · airframe 20,914 hrs · 15,343 cycles

LT SIDE SEAT TRACK F/S 785 TO 830 HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED LT SIDE SEAT TRACK IAW AMM 53-00-49-000-801. PREPARED NEW SEAT TRACK FOR INSTALLATION IAW SRM 51-40-11. ETCHED AND ALODINED NEW SEAT TRACK IAW SRM 51-21-11. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A01.

Part: SKIN — CHAFED (BS 977 S27) · airframe 20,914 hrs · 15,343 cycles

BELLY CHAFE AT FS 977.00 STRINGER 27 OUTSIDE SKIN. BLENDED IAW REO 670-53-00-014. PERFORMED LPI IAW REO 670-53-00-014, NO DEFECTS NOTED. REMOVED 3 DAMAGED LOCK FASTENERS AND 2 RIVETS IAW SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. INSTALLED NEW LOCK FASTENERS AND RIVETS IAW SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. TREATED PRIMED AND PAINTED IAW SRM 51-21-16-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 20,914 hrs · 15,343 cycles

LEFT SEAT TRACK FS 708 TO 761 HAS CORROSION. REMOVED CORROSION IAW REO 670-53-00-013, FOUND TO BE WITHIN LIMITS. APPLIED ALODINE IAW SRM 51-21-11.

Part: SKIN — CHAFED (FUSELAGE) · airframe 20,914 hrs · 15,343 cycles

CHAFE BELOW AFT POTABLE WATER FILL PORT FUSELAGE SKIN. BLENDED IAW SRM 51-12-00, FOUND TO BE OUT OF LIMITS IAW SRM 53-51-01-003-A01. PERFORMED LPI IAW REO 670-53-51-042, NO DEFECTS NOTED. TREATED, PRIMED AND PAINTED IAW SRM 51-25-01-001-001-A01. ALL WORK DONE IN CONFORMITY WITH REO 670-53-51-042.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 20,914 hrs · 15,343 cycles

CHAFE DAMAGE TO SKIN DOUBLER AT LAV SERVICE AREA ADJACENT TO ELECTRICAL CONNECTOR PL118J1. REMOVED 1 RIVET IAW SRM 51-42-06. BLENDED OUT CHAFE IAW SRM 51-12-00, FOUND TO BE WITHIN LIMITS PER SRM 53-000-01-001-A01 PG 10. TREATED, PRIMED, AND PAINTED IAW SRM 51-25-01-001-001-A01. INSTALLED 1 RIVET IAW SRM 51-42-06-001-001-A01. PRIMED, PAINTED RIVET IAW SRM 51-25-06-001-001-A01 AND 51-25-16-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 831-865) · airframe 20,914 hrs · 15,343 cycles

LEFT SEAT TRACK FS 831 TO 865 HAS CORROSION AND DENT. REMOVED CORROSION FROM LT SIDE SEAT TRACK FS 831.00 TO FS 865.00. REMOVED .013 MATERIAL, MAX ALLOWABLE IS .035. FOUND TO BE WITHIN LIMITS IAW REO 670-53-00-013. TREATED BLENDED AREA IAW REO 670-53-00-013, COMPLETED TO STEP 9 IAW REO 670-53-00-013, NO FURTHER ACTION REQUIRED.

Part: SEAT TRACK — CORRODED (BS 831-863) · airframe 20,914 hrs · 15,343 cycles

RIGHT SEAT TRACK FS 831 TO 863 HAS CORROSION. REMOVED CORROSION FROM SEAT TRACK FS 831 TO 863. REMOVED TOTAL .014 FROM MAX .035. FOUND TO BE WITHIN LIMITS IAW REO 670-53-00-013.

Part: SMOKE DETECTOR — INTERMITTENT (ZONE 200) · airframe 19,990 hrs · 14,635 cycles

PDX- FIRE SYST FAULT STATUS MESSAGE, MESSAGE IS INTERMITTENT. PLACED ON MEL 26-00-1. RETURNED TO SERVICE. MEL CLEARED ON 7/16 BY REPLACING THE FORWARD SMOKE DETECTOR 2. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FIRE WARNING — FALSE ACTIVATION · airframe 19,701 hrs · 14,412 cycles

ONT- FIRE SYS FAULT MESSAGE. PLACED SYSTEM ON MEL 26-00-1. RETURNED TO SERVICE. MEL CLEARED ON 6/9. PERFORMED OPERATIONAL TEST OF THE FIDEEX SYSTEM PER AMM TASK 26-10-00-710-801. OPS TEST GOOD. NO FAULTS PRESENT. CLEAR MEL. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: PSEU — FAILED (MLG) · airframe 17,227 hrs · 12,310 cycles

PDX - FLIGHT 2590 - FOLLOWING GEAR RETRACTION, RECEIVED A GEAR DISAGREE MESSAGE. NOSE GEAR APPEARED SLOW TO RETRACT. MAINTENANCE ADJUSTED PX-22 IAW 32-61-05-820-804-A01. REPLACED PSEU AS PRECAUTION. RETURNED TO SERVICE. (A)

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 16,018 hrs · 11,429 cycles

PSP - FLIGHT 2610 - ELECTRICAL ODOR FROM ROW 4. MAINTENANCE COMPLIED WITH A INSPECTION OF THE SYSTEM AND WIRING AND FOUND NO DEFECTS. REPLACE THE LAMPS AND THE PS50 BALLAST. AIRCRAFT RETURNED TO SERVICE.

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 16,020 hrs · 11,431 cycles

BOI - FLIGHT 2553 - AFTER LEAVING, THE CEILING LIGHT ON FOR A FEW HOURS, A ELECTRICAL ODOR WAS NOTICED AT ROW 4. MAINTENANCE DISCONNECTED THE BALLAST AT ROW 4 (PS50) AND PLACED THE SYSTEM ON MEL 33-21-1. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — DAMAGED (ECU) · airframe 15,689 hrs · 11,204 cycles

PDX - AFTER ENGINE START, THE APU FAULT CAUTION ILLUMINATED FOLLOWED BY A APU SHUTDOWN. COMPLIED WITH CHECKLIST AND MESSAGE WENT AWAY. MAINTENANCE FOUND A UNDERSPEED FAULT AND ECU BUSS FAULT IN THE MDC. RESEATED AND CLEANED THE ECU PINS. OPERATIONAL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: ALTIMETER — MALFUNCTIONED · airframe 15,383 hrs · 11,001 cycles

SEA - FLIGHT 2503. ON TAXI RECEIVED A GLD UNSAFE MESSAGE. RETURNED TO THE GATE. MAINTENANCE PLACED THE RADIO ALTIMETER SYSTEM ON MEL 34-41-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE REPLACED THE CAPTAIN'S RADIO ALTIMETER R/T. OPERATIONAL CHECKS GOOD. MEL CLEARED AND AIRCRAFT RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — MALFUNCTIONED (DOOR) · airframe 15,105 hrs · 10,806 cycles

BOI - FLIGHT 4276 - DURING PUSHBACK RECEIVED A PROX SYSTEM FAULT 1 STATUS MESSAGE. RETURNED TO THE GATE. MAINTENANCE FOUND NO CURRENT FAULTS IN MDC. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WARNING LIGHT — FALSE ACTIVATION (TE FLAPS) · airframe 14,893 hrs · 10,661 cycles

ONT- FLIGHT 2567, RECEIVED A FLAPS FAIL CAUTION MESSAGE WHEN ATTEMPTING TO SELECT FLAPS TO 20 DEGREES. THE SYNOPTIC PAGE SHOWED THE FLAPS AND SLATS TO BE AT THE 1 DEGREE POSITION. ACCOMPLISHED THE CHECKLIST AND THE CAUTION CLEARED. ACCOMPLISHED A NORMAL LANDING. MAINTENANCE PERFORMED TASK 27-50-00-710-801-A01 OPERATIONAL CHECKS OF THE FLAPS AND SLATS WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CONTROL HANDLE — LACK OF LUBE (TE FLAPS) · airframe 14,893 hrs · 10,661 cycles

ONT- FLIGHT 2568, ON TAXI TO THE RUNWAY, RECEIVED A FLAP HALFSPEED MESSAGE AND A SLATS HALFSPEED MESSAGE. RETURNED TO THE GATE. MAINTENANCE CYCLED SHIPS POWER AND THE FLAP CONTROL HANDLE, AND LUBED THE FLAP CONTROL HANDLE. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DOOR — OPEN (CARGO BAY) · airframe 14,609 hrs · 10,451 cycles

SFO- FLIGHT 2524, AFTER TAKEOFF, DURING CLIMB RECEIVED A CABIN ALTITUDE MESSAGE. DIVERTED AIRCRAFT TO OAKLAND AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE FOUND THE AFT CARGO DOOR NOT PROPERLY CLOSED, AFT SECTION OF DOOR NOT SECURE. PERFORMED OPERATIONAL CHECK OF DOOR WITH NO DEFECTS FOUND. PERFORMED PRESSURIZATION CHECK WITH NO DEFECTS FOUND. AIRCRAFT RETURNED TO SERVICE WITH NO PARTS REPLACEMENTS.

Part: UNKNOWN — NONE (SLAT) · airframe 14,243 hrs · 10,199 cycles

DEN - WHEN FLAPS SELECTED TO 20 DEGREES RECEIVED A SLAT FAIL CAUTION MESSAGE. PER THE CHECKLIST, SELECTED THE PREVIOUS FLAP SETTING AND OPERATION WAS NORMAL. MAINTENANCE INSPECTED AIRCRAFT AND FOUND NO FAULT OR MESSAGES IN THE MDC. CYCLED SLATS SEVERAL TIMES WITH NO DEFECTS. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: UNKNOWN — MALFUNCTIONED (LT ENGINE) · airframe 13,897 hrs · 9,930 cycles

SEA - LEFT ENGINE WOULD NOT START. FUEL FLOW, IGNITION, AND ROTATION ALL NORMAL. NO ITT RISE. RETURNED TO THE GATE. MAINTENANCE PERFORMED 2 STARTS WITH NO PROBLEMS NOTED. NO FAULTS FOUND. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DOOR — OPEN (CARGO BAY) · airframe 13,143 hrs · 9,424 cycles

LIT- FLIGHT 4324, AFTER ROTATION CARGO DOOR OPENED. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE DOOR AND FOUND NO DEFECTS. COMPLIED WITH TEST OF DOOR AND PRESSURIZATION WITH NO DEFECTS. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: TRANSDUCER — FAULTED (ANTI-SKID SYS) · airframe 13,143 hrs · 9,424 cycles

SFO- FLIGHT 4166 (DEN-SJC) DURING CRUISE FLIGHT RECEIVED A ANTI-SKID FAULT STATUS MESSAGE. DUE TO THE RUNWAY LENGTH AT SJC, DIVERTED TO SFO AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE NR 2 WHEEL SPEED TRANSDUCER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LANDING GEAR — LOOSE (LEFT) · airframe 12,746 hrs · 9,161 cycles

C3 PDX - LEFT MAIN LANDING GEAR OUTBOARD SIDE STAY ATTACH POINT HAS RADIAL PLAY AT PINTLE PIN. REPAIRED IAW SRM 32-11-12.

Part: FRAME — CHAFED (LT FAN COWL) · airframe 12,746 hrs · 9,161 cycles

C3 PDX - LEFT ENGINE LOWER FAN COWL TORQUE BOX FRAME IS CHAFED AT 9:00 O'CLOCK POSITION. REPAIRED IAW SRM 51-12-00 AND REO670-54-21-735.

Part: BULKHEAD — CORRODED (BS 280) · airframe 12,746 hrs · 9,161 cycles

C3 PDX - FOUND RIGHT LOWER BULKHEAD AT STATION X280 IS CORRODED. REPAIRED IAW REO670-53-11-052.

Part: ANGLE — CRACKED (AIRSTAIR) · airframe 12,746 hrs · 9,161 cycles

C3 PDX - AFT MAIN CABIN DOOR AIRSTAIR CORNER ANGLE IS CRACKED FROM AFT EDGE OF DOOR AND 36" FROM TOP WITH DOOR OPEN. REPAIRED IAW REO670-52-11-072 AND SRM 51-25-01.

Part: SKIN — CORRODED (FUSELAGE) · airframe 12,746 hrs · 9,161 cycles

C3 PDX - LOWER TCAS ANTENNA HAS SMALL AMOUNT OF CORROSION AROUND CONNECTOR OF FUSELAGE. REPAIRED IAW SRM 51-21-16.

Part: FRAME — CHAFED (LT FAN COWL) · airframe 12,746 hrs · 9,161 cycles

C3 PDX - LEFT ENGINE UPPER FAN COWL TORQUE BOX FRAME HAS CHAFE AT 11:00 O'CLOCK POSITION. REPAIRED IAW SRM 51-12-00 AND REO670-78-34-378.

Part: FRAME — CHAFED (LT FAN COWL) · airframe 12,746 hrs · 9,161 cycles

C3 PDX - LEFT ENGINE UPPER FAN COWL TORQUE BOX FRAME IS CHAFED AT 9:00 O'CLOCK POSITION. REPAIRED IAW SRM 51-12-00 AND REO670-54-21-735.

Part: MANIFOLD — LEAKING (FUEL SYSTEM) · airframe 12,725 hrs · 9,149 cycles

PDX - DURING A DAILY CHECK, FOUND A FUEL LEAK AT THE NR 2 NACELLE. MAINTENANCE REPLACED THE HEAD END MANIFOLD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL VALVE — MALFUNCTIONED (LT PACK TEMP) · airframe 12,386 hrs · 8,920 cycles

FLIGHT 4205, RECEIVED A LT PACK CAUTION. RETURNED TO THE GATE. MAINTENANCE REPLACED THE TEMP CONTROL VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL VALVE — MALFUNCTIONED (THRUST REVERSER) · airframe 11,421 hrs · 8,262 cycles

BOI - ON TAKEOFF ROLL, RECEIVED A RIGHT THRUST REVERSER UNSAFE MESSAGE. ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE RELAY AND CONTROL VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCPIT) · airframe 11,411 hrs · 8,254 cycles

OKC - ON TAKEOFF ROLL, RECEIVED A RIGHT THRUST REVERSER CAUTION MESSAGE. ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE PERFORMED FUNCTIONAL TEST OF THRUST REVERSER SYSTEM IAW AMM 78-30-00-720-801-A01, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CONTROL VALVE — LEAKING (APU) · airframe 10,854 hrs · 7,861 cycles

DEN - FLIGHT 4299 - AFTER LANDING DURING APU START RECEIVED AN "APU LCV CLSD" CAUTION MESSAGE AND A OIL SMELL IN THE BLEED AIR. REMOVED AND REPLACED APU LOAD CONTROL VALVE IAW AMM TASK 49-51-05-000-801-A01 AND 49-51-05-400-801-A01. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — FAILED (MLG) · airframe 10,692 hrs · 7,755 cycles

DEN - ON FLIGHT 4310, RETURNED TO FIELD. GEAR DIAGREE WARNING MESSAGE ON TAKEOFF WHEN GEAR SELECTED UP FOLLOWED BY PROX SYSTEM FAULT STATUS MESSAGE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REALIGNED CENTERING CAM RETAINER AND REPACKED NOSE LANDING STRUT. OPERATIONAL CHECK OF EXTENSION AND RETRACTION GOOD. NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: VALVE — MALFUNCTIONED (APU) · airframe 10,375 hrs · 7,559 cycles

DEN - ON PUSHBACK FOR FLIGHT 4277 RECEIVED A -L FADEC FAULT 2- STATUS MESSAGE AND ENGINE WOULD NOT START. RETURNED, FOUND APU LOAD CONTROL VALVE CLOSED, NOT ENOUGH AIR FOR START. RECONFIGURED VALVES, ENGINE STARTED MESSAGE CLEARED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WARNING LIGHT — ILLUMINATED (A/C PACK) · airframe 10,354 hrs · 7,547 cycles

DEN - ON TAXI FOR FLIGHT 4430 LEFT PACK OFF WHITE STATUS MESSAGE AND MOMENTARY LEFT PACK OFF CAUTION MESSAGE. RETURNED TO THE GATE. PLACED ON MEL REF 21-51-1(A) RSI 356422. AIRCRAFT RETURNED TO SERVICE. ON 2/7 PERFORMED OPERATIONAL TEST OF AIR CONDITIONING DISTRIBUTION SYSTEM IAW CRJ-700 AMM 21-51-00-710-801-A01. TEST GOOD, AIRCRAFT RETURNED TO SERVICE AND MEL CLOSED. NO PARTS REPLACED.

Part: MOUNT — BINDING (SERVO) · airframe 10,135 hrs · 7,408 cycles

ON APPROACH FOR LANDING ON FLIGHT 2505, ROLL CONTROL REMAINS STUCK IN THE NEUTRAL POSITION FOR SEVERAL SECONDS AFTER THE AUTOPILOT IS DISENGAGED; AFTER SEVERAL SECONDS, HOWEVER, THE ROLL CONTROL WORKS NORMALLY. FOUND AP AILERON SERVICE MOUNT/CLUTCH BINDING. REPLACED MOUNT/CLUTCH AND SERVO PER CRJ700 (TR 22-0021/22) 22-11-11-000-801-A01, 22-11-11-400-801-A01, 22-11-21-000-801-A01, 22-11-21-400-801-A01. ALL CLOSEOUT TESTS CHECK GOOD. PERFORMED VISUAL INSPECTION OF AILERON CABLE CIRCUIT ACCESSABLE IN FIELD ENVIRONMENT FOR INTERFERENCE, BINDING, ROUGH BEARINGS. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: GENERATOR — WARNING LIGHT (NR 1) · airframe 9,906 hrs · 7,260 cycles

DEN - ON PUSHBACK FOR FLIGHT 4327, RECEIVED A NR 1 GENERATOR OFF CAUTION MESSAGE. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PLACED THE SYSTEM ON MEL 24-11-1B. AIRCRAFT RETURNED TO SERVICE. IN BOI MAINTENANCE REPLACED THE NR 1 IDG WITH NO HELP, ALSO THE NR 1 GCU WITH NO HELP. MEL CONTINUED. AIRCRAFT RETURNED TO SERVICE.

Part: SENSOR — MALFUNCTIONED (PITCH FEEL) · airframe 9,566 hrs · 7,036 cycles

FAT- ON FLIGHT 4299, PITCH FEEL FAULT STATUS MESSAGE ILLUMINATED. AIRCRAFT RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE HTSA SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (AILERONS) · airframe 9,430 hrs · 6,942 cycles

EN ROUTE TO SEA ON FLIGHT 2478 (FAT-SEA), OVER SMF, RECEIVED A FLT CONTROL AILERON MALFUNCTION MESSAGE. FLIGHT DIVERTED TO SMF AND ACCOMPLISHED A UNEVENTFUL LANDING. MTX IN SMF PERFORMED A DETAILED INSPECTION OF THE AILERON CONTROL SYSTEM AND A RIGGING CHECK OF THE SYSTEM WITH NO DEFECTS NOTED. REPLACED THE AILERON SERVO MOUNT/CLUTCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SPRAYER — MALFUNCTIONED (RAM AIR) · airframe 9,325 hrs · 6,874 cycles

DEN - NOTICEABLE SMELL IN THE CABIN AND COCKPIT WITH THE AIR CONDITIONING PACKS ON. INCREASED IN INTENSITY AT IDLE DESCENT AND WITH THE APU ON. MAINTENANCE REMOVED AND REPLACED THE RAM AIR WATER SPRAYERS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED SERVICE.

Part: CONTROL PANEL — SMOKE (FUEL) · airframe 8,665 hrs · 6,406 cycles

SMOKE AND ELECTRICAL ODOR COMING FROM FUEL CONTROL PANEL, RT WING ROOT. REPLACED REFUEL/DEFUEL PANEL IAW 28-25-00-801-A01. AIRCRAFT RETURNED TO SERVICE.

Part: FAN BLADE — VIBRATION (LT ENGINE) · airframe 8,504 hrs · 6,269 cycles

ON CLIMBOUT, LEFT ENGINE VIB OF 1.9 INDICATION, REDUCED N1 TO CLIMB THRUST IN ORDER TO MAINTAIN A GREEN VIB INDICATION WITHIN .05. IT WAS NECESSARY TO REDUCE N1 TO 67.5 TO MAINTAIN A GREEN INDICATION (A 3 THRUST LEVER KNOB WIDTH SPLIT) RETURNED TO DEN. DESCENT, REDUCED THRUST SETTINGS. LEFT ENGINE REMAINED OUT OF YELLLOW ON TOUCHDOWN, WITH REVERSE THRUST DEPLOYED, ENGINE VIB INDICATION WAS A YELLOW 2.6. MX REPLACED NR 1 ENGINE FAN BLADES. OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 8,503 hrs · 6,288 cycles

PITCH FEEL FAULT STATUS MESSAGE. MESSAGE DISAPPEARED WHEN TERMINATING CHECKLIST WAS COMPLETED. REPLACED NR 2 SSCU IAW CRJ-700 AMM 27-61-05-000-801-A01 AND 400-801-A01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED · airframe 8,024 hrs · 5,943 cycles

RECEIVED LT AND RT WING ANTI-ICE CAUTION MESSAGE ON 5 MILE FINAL. RAN CHECKLIST FOR WING ANTI-ICE CAUTION. CAUTION REMOVED. CAUTION RETURNED ON SHORT FINAL WITH BLEED AIR CROSS BLEED SET TO FROM RT. MX INTERROGATED MDC. REPORTS AFLC INTERNAL FAULT. LOSS OF A AND B CHANNELS TO DCU'S. REPLACED AILC IAW CRJ AMM 30-12-400-801-A01. OPS CHECK GOOD. ACFT RETURNED TO SERVICE.

Part: HINGE PIN — CORRODED (ZONE 300) · airframe 7,771 hrs · 5,750 cycles

YYC - VERTICAL STABILIZER HINGE PIN FOR HORIZONTAL STABILIZER HAS EVIDENCE OF CORROSION COMING FROM BEARINGS. REPAIRED IAW REO 670-55-11-021 AND CRJ700 SRM 51-21-16.

Part: HANDLE — CRACKED (ZONE 800) · airframe 7,771 hrs · 5,750 cycles

YYC - SERVICE DOOR INNER HANDLE HOUSING IS CRACKED. REPAIRED IAW CRJ700 SRM 52-41-00-801-A01, SRM 51-41-21-001-001-A01 AND SRM 52-41-00-710-801-A01.

Part: ACCESS PANEL — CORRODED (ZONE 500) · airframe 7,771 hrs · 5,750 cycles

YYC - LEFT HAND, FUEL PANEL 55100 REBATE IS CORRODED. REPAIRED IAW REO 670-57-00-010, CRJ700 SRM 51-24-11-001-001-A01, AND HORIZON AIR EA R-57-96.

Part: ACCESS PANEL — CORRODED (ZONE 500) · airframe 7,771 hrs · 5,750 cycles

YYC - LEFT HAND WING, FUEL PANEL 551BB REBATE IS CORRODED. REPAIRED IAW REO 670-57-00-010, CRJ700 SRM 51-24-11-001-001-A01, AND HORIZON AIR EA R-57-96.

Part: ACCESS PANEL — CORRODED (ZONE 500) · airframe 7,771 hrs · 5,750 cycles

YYC - LEFT HAND, FUEL PANEL 551EB REBATE IS CORRODED. REPAIRED IAW CRJ700 SRM 51-24-11-001-001-A01, REO 670-57-00-010, AND HORIZON AIR EA R-57-96.

Part: STRINGER — CORRODED (ZONE 100) · airframe 7,771 hrs · 5,750 cycles

YYC - FUSELAGE INTERIOR STRINGER AT FS 280 TO FS 333 STRINGER 25R HAS SEVERAL SPOTS OF CORROSION ALONG RIVET ROW. REPAIRED IAW CRJ700 SRM 53-21-03-101-002-AA1, SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC - LEFT HAND INBOARD SEAT RAIL AT STATION X663 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND HORIZON AIR EA R-53-083.

Part: STRINGER — CRACKED (ZONE 800) · airframe 7,771 hrs · 5,750 cycles

YYC - PASSENGER DOOR AFT SIDE STRINGER CRACKED AT TOP STEP RISER AT HANDRAIL STOWAGE BRACKET. REPAIRED IAW CRJ700 REO 670-52-11-102 AND HORIZON AIR EA R-52-228.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC - RIGHT HAND INBOARD SEAT RAIL AT STATION X399 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC - RIGHT HAND INBOARD SEAT RAIL AT STATION X430 HAS PITTING CORROSION AND WEARING MARKS ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC - RIGHT HAND OUTBOARD SEAT RAIL AT STATION X421 TO X426 HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC - RIGHT HAND INBOARD SEAT RAIL AT STATION X461 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND REO 670-53-00-013.

Part: SKIN — SCRATCHED (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC - FUSELAGE EXTERIOR FORWARD BAY DOOR CUTOUT, HAS SCRATCHES ON FORWARD EDGE OF DOOR CUTOUT FS 310, WL 80. REPAIRED IAW REO 670-53-21-081 AND HORIZON AIR EA R-53-276 AND CRJ700 SRM 51-25-01-001-001-A01.

Part: CHANNEL — CHAFED (ZONE 100) · airframe 7,771 hrs · 5,750 cycles

YYC - FUSELAGE TO WING BODY FAIRING STIFFENER CHANNEL HAS CHAFFING DAMAGE AT THE AFT END. REPAIRED IAW CRJ700 SRM 51-21-16-001-001-A01 AND REO 670-53-61-155 AND HORIZON AIR EA R-53-284.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC - RIGHT HAND INBOARD SEAT RAIL AT STATION X479.5 HAS PITTING CORROSION ON INSIDE SURFACE AROUND SCREW HOLE. REPAIRED IAW CRJ700 51-21-06-001-001-A01 AND REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC - RIGHT HAND INBOARD SEAT RAIL AT STATION X350 TO X355 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 REO 670-53-00-013.

Part: STRINGER — CRACKED (PAX DOOR) · airframe 7,771 hrs · 5,750 cycles

YYC - PASSENGER DOOR FORWARD SIDE STRINGER CRACKED AT TOP STEP RISER AT STOWAGE BRACKET. REPAIRED IAW REO 670-52-11-102 AND HORIZON AIR EO R-52-228.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC - RIGHT HAND INBOARD SEAT RAIL AT STATION X363 HAS PITTING CORROSION ON TOP SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND REO 670-53-00-013.

Part: SKIN — CHAFED (ZONE 100) · airframe 7,771 hrs · 5,750 cycles

YYC - FUSELAGE EXTERNAL BELLY SKIN HAS CHAFFING DAMAGE FROM FAIRING STIFFENER AT FS 974 AND LBL 1. REPAIRED IAW CRJ700 SRM 51-21-16-001-001-A01, HORIZON AIR EA R-53-284 AND REO 670-53-61-155.

Part: SKIN — GOUGED (ZONE 100) · airframe 7,771 hrs · 5,750 cycles

YYC - FUSELAGE EXTERNAL BELLY SKIN HAS A GOUGE FROM FAIRING SCREW AT FS 983 AND LBL 1.5 AND A DAMAGED HILITE FASTENER AT STRINGER 27. REPAIRED IAW REO 670-53-61-155 AND HORIZON AIR EA R-53-284.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC - RIGHT HAND INBOARD SEAT RAIL AT STATION X677 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND HORIZON AIR EA R-53-285.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC - LEFT HAND OUTBOARD SEAT RAIL AT STATION X707 TO X713 HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND HORIZON AIR EO R-53-281.

Part: RETAINER — GOUGED (ZONE 800) · airframe 7,771 hrs · 5,750 cycles

YYC - FORWARD CARGO DOOR SEAL RETAINER IS GOUGED AND BENT AT TWO CORNERS. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 52-35-07-400-802-A01.

Part: SKIN — TOOL DAMAGE (ZONE 800) · airframe 7,771 hrs · 5,750 cycles

YYC - CENTER FUSELAGE, FORWARD BAGGAGE BAY DOOR, DOOR SKIN PANEL HAS TOOLING MARK. REPAIRED IAW REO-679-52-35-059 AND HORIZON AIR EAR-52-225.

Part: SKIN — WORN (ZONE 600) · airframe 7,771 hrs · 5,750 cycles

YYC - RIGHT HAND AILERON, UPPER LEADING EDGE HAS THREE AREAS OF WEARING FROM TRAILING EDGE SEALS. REPAIRED IAW CRJ700 SRM 57-61-01-101-001-A01 AND SRM 51-12-00-001-001-A01.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC - RIGHT HAND INBOARD SEAT RAIL AT STATION X647 HAS PITTING CORROSION ON INSIDE SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND HORIZON AIR EA R-53-285.

Part: ACCESS PANEL — SCRATCHED (ZONE 600) · airframe 7,771 hrs · 5,750 cycles

YYC - RIGHT HAND LOWER WING LEADING EDGE ACCESS PANEL 622DB FORWARD SECTION, SKIN HAS A SCRATCH AND CHAFE MARK. REPAIRED IAW CRJ700 SRM 57-41-01-101-001-A01, SRM 51-12-00-001-001-A01, AND SRM 51-25-16-001-001-A01.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC - RIGHT HAND INBOARD SEAT RAIL AT STATION X603 HAS PITTING CORROSION ON TOP SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND HORIZON AIR EA R-53-285.

Part: SKIN — DAMAGED (ZONE 600) · airframe 7,771 hrs · 5,750 cycles

YYC - RIGHT HAND INBOARD FLAP LOWER SURFACE HAS GRAVEL DAMAGED. REPAIRED IAW CRJ700 SRM 57-52-01-101-001-A01, SRM 51-12-00-001-001-A01, AND SRM 51-25-16-001-001-A01.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC - LEFT HAND INBOARD SEAT RAIL AT STATION X461 HAS PITTING CORROSION ON TOP SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND HORIZON AIR EA R-53-282.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC - LEFT HAND INBOARD SEAT RAIL AT STATION X616 HAS PITTING CORROSION ON TOP SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND HORIZON AIR EA R-53-283.

Part: SKIN — CHAFED (ZONE 600) · airframe 7,771 hrs · 5,750 cycles

YYC - RIGHT HAND FLAP LOWER SURFACE INBOARD HINGE AREA HAS CHAFED MARKS FROM FAIRING. REPAIRED IAW CRJ700 SRM 57-52-01-101-001-A01, SRM 51-25-01-001-001-A01.

Part: PANEL — CHAFED (ZONE 400) · airframe 7,771 hrs · 5,750 cycles

YYC - LEFT HAND PYLON PANEL 412JB END EDGE HAS CHAFE MARK. REPAIRED IAW CRJ700 SRM 51-21-16-001-001-A01, REO 670-54-52-013 AND HORIZON AIR EA R-54-76.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC - LEFT HAND INBOARD SEAT RAIL AT STATION X677 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND HORIZON AIR EA R-53-283.

Part: SKIN — WORN (ZONE 500) · airframe 7,771 hrs · 5,750 cycles

YYC - LEFT AILERON, UPPER INBOARD LEADING EDGE HAS TWO AREAS OF WEARING FROM TRAILING EDGE SEALS. REPAIRED IAW CRJ700 SRM 57-61-01-101-001-A01 AND SRM 51-12-00-001-001-A01.

Part: FASTENER — LOOSE (ZONE 800) · airframe 7,771 hrs · 5,750 cycles

YYC - LEFT HAND WING UPPER SURFACE TRAILING EDGE HAS LOOSE FASTENERS AT STATION 170 AND 232. REPAIRED IAW CRJ7, SRM 51-25-01-001-001-A01 AND SRM 51-42-06-001-001-A01.

Part: VANE — CHAFED (ZONE 600) · airframe 7,771 hrs · 5,750 cycles

YYC - RIGHT HAND INBOARD FLAP VANE INBOARD LEADING EDGE PANEL 684ET HAS CHAFED MARK. REPAIRED IAW CRJ700 SRM 57-52-02-101-001-A01 AND SRM 51-12-00-001-001-A01.

Part: STIFFENER — CRACKED (ZONE 800) · airframe 7,771 hrs · 5,750 cycles

YYC - PASSENGER DOOR INTERNAL Z STIFFENER CRACKED BELOW ASSIST MOTOR OUTER BOTTOM BOLT. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: VANE — CHAFED (ZONE 600) · airframe 7,771 hrs · 5,750 cycles

YYC - RIGHT HAND INBOARD FLAP VANE LEADING EDGE HAS CHAFE MARK AT WS 88. REPAIRED IAW CRJ700 SRM 57-53-02-101-001-A01 AND SRM 51-25-01-001-001-A01.

Part: SKIN — CHAFED (ZONE 500) · airframe 7,771 hrs · 5,750 cycles

YYC - LEFT HAND WING LEADING EDGE SKIN HAS CHAFFED MARK FROM LEADING EDGE AT STATION 22. REPAIRED IAW CRJ700 SRM 57-41-01-101-001-A01 AND SRM 51-12-00-001-001-A01.

Part: VANE — CHAFED (ZONE 500) · airframe 7,771 hrs · 5,750 cycles

YYC - LEFT HAND WING INBOARD FLAP VANE, INBOARD LEADING EDGE PANEL 584ET HAS CHAFED MARK. REPAIRED IAW CRJ700 SRM 57-52-02-101-001-A01 AND SRM 51-25-01-001-001-A01.

Part: SKIN — DAMAGED (ZONE 500) · airframe 7,771 hrs · 5,750 cycles

YYC - LEFT HAND INBOARD FLAP LOWER SURFACE HAS GRAVEL DAMAGE. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, SRM 51-25-01-001-001-A01, AND SRM 57-52-01-101-001-A01.

Part: VANE — CHAFED (ZONE 500) · airframe 7,771 hrs · 5,750 cycles

YYC - LEFT HAND WING INBOARD FLAP VANE HAS CHAFFED MARK AT LEADING EDGE MID SECTION. REPAIRED IAW CRJ700 SRM 57-52-02-101-001-A01 AND SRM 51-25-01-001-001-A01.

Part: CROSSBEAM — CORRODED (ZONE 100) · airframe 7,771 hrs · 5,750 cycles

YYC - FUSELAGE INTERIOR FLOOR SUPPORT CROSSBEAM AT FS280 IS CORRODED. REPAIRED IAW REO 670-53-11-047.

Part: SKIN — WORN (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC - FUSELAGE EXTERIOR AFT BAGGAGE DOOR CUTOUT, HAS WEAR DAMAGE TO AFT SKIN AT FS 1047 WL 88. REPAIRED IAW HORIZON AIR EA R-53-277 AND REO 670-53-61-152.

Part: BULKHEAD — CORRODED (ZONE 100) · airframe 7,771 hrs · 5,750 cycles

YYC - FUSELAGE INTERIOR FS 280 BULKHEAD RIGHT HAND LOWER WEB IS CORRODED ALONG FLOOR LEVEL. REPAIRED IAW REO 670-53-11-052.

Part: PANEL — CRACKED (ZONE 800) · airframe 7,771 hrs · 5,750 cycles

YYC - PASSENGER DOOR AFT SIDE OF STAIR AT DOOR PANEL ANGLE IS CRACKED .75 INCH AT ASSIST MOTOR OUTER Z ATTACH. REPAIRED IAW REO 670-52-11-072.

Part: BULKHEAD — CORRODED (ZONE 100) · airframe 7,771 hrs · 5,750 cycles

YYC - FUSELAGE INTERIOR FS 280 BULKHEAD LEFT HAND LOWER WEB IS CORRODED AT FLOOR LEVEL. REPAIRED IAW REO 670-53-11-052.

Part: ACCESS PANEL — CHAFED (ZONE 600) · airframe 7,771 hrs · 5,750 cycles

YYC - RIGHT HAND INBOARD FLAP LOWER ACCESS PANEL 684BB HAS CHAFFED MARK FROM HINGE FAIRING. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01 AND SRM 57-52-01-101-001-A01.

Part: ARM — GOUGED (ZONE 400) · airframe 7,771 hrs · 5,750 cycles

YYC - LEFT HAND NACELLE LATCH DOOR HINGE ARMS ARE GOUGED. REPAIRED IAW CRJ700 SRM 51-25-00*-001-001-A01, SRM51-12-00-001-001-A01, AND SRM 54-21-00-101-001-A01.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 7,771 hrs · 5,750 cycles

YYC - FUSELAGE INTERIOR COCKPIT FLOOR SUPPORT ANGLE IS CORRODED AT FS 280. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-23-00-001-001-A01.

Part: ACCESS PANEL — CORRODED (ZONE 400) · airframe 7,771 hrs · 5,750 cycles

YYC - LEFT HAND COWL LATCH ACCESS PANEL 433AL HAS FRETTING CORROSION AT INTERNAL EDGE. REPAIRED IAW CRJ700 SRM 54-21-00-101-001-A01, SRM 51-12-00-001-001-A01, AND SRM 51-25-06-001-001-A01.

Part: PLATE — CORRODED (ZONE 800) · airframe 7,771 hrs · 5,750 cycles

YYC - GALLEY SERVICE DOOR CUTOUT INNER PROTECTOR PLATE HAS CORROSION ON UNDERSIDE. REPAIRED IAW CRJ700 SRM 51-21-23-101-002-A01 AND SRM 51-25-01-001-001-A01.

Part: RIVET — LOOSE (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC -FUSELAGE EXTERIOR HAS LOOSE RIVETS AT FS800 BETWEEN STRINGER 16 RT AND STRINGER 17 RT, AT WING TO BODY FAIRING ATTACH. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: SKIN — GOUGED (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC - AFT FUSELAGE BAGGAGE BAY DOOR LOWER AFT COWLING GOUGED. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01.

Part: FASTENER — LOOSE (ZONE 600) · airframe 7,771 hrs · 5,750 cycles

YYC - RIGHT HAND WING UPPER SURFACE TRAILING EDGE HAS LOOSE FASTENERS AT STATION WS 170 INBOARD OF MULTIFUNCTION SPOILERS. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01, SRM 51-25-01-001-001-A01.

Part: VENT — GOUGED (ZONE 800) · airframe 7,771 hrs · 5,750 cycles

YYC - FORWARD CARGO DOOR VENT FLAP HAS TWO GOUGES ON INSIDE FACE. REPAIRED IAW CRJ700 SRM 52-35-06-101-001-A01 AND SRM 51-12-00-001-001-A01.

Part: RIVET — LOOSE (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC - FUSELAGE EXTERIOR HAS LOOSE RIVETS AT FS800 BETWEEN STRINGER 16 LT AND STRINGER 17 LT, AT WING TO BODY FAIRING ATTACH. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: SKIN — SCRATCHED (ZONE 400) · airframe 7,771 hrs · 5,750 cycles

YYC - LEFT HAND NACELLE AFT CORE COWL SCRATCHED ON OUTBOARD SIDE. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, SRM 54-13-00-101-001-A01, AND SRM 51-21-11-001-001-A01.

Part: SKIN — GOUGED (ZONE 400) · airframe 7,771 hrs · 5,750 cycles

YYC - LEFT HAND NACELLE LIP SKIN GOUGED BETWEEN 7 AND 8 O'CLOCK POSITION. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND SRM 54-11-05-101-001-A01.

Part: PLATE — GOUGED (ZONE 200) · airframe 7,771 hrs · 5,750 cycles

YYC - CENTER UPPER FUSELAGE, OVERWING EXITS, RIGHT HAND OVERWING EXIT LOWER SILL PLATE GOUGED. REPAIRED IAW CRJ700 SRM 53-41-06-101-003-A01, SRM 51-12-00-001-001-A01, AND SRM 51-25-01-001-001-A01.

Part: SILL — CORRODED (ZONE 100) · airframe 7,771 hrs · 5,750 cycles

YYC - FUSELAGE INTERNAL AFT, LEFT HAND, FS 1000 TO FS 1047 SURROUND STRUCTURE, AFT BAGGAGE BAY DOOR, LOWER SILL IS CORRODED AROUND ANCHOR NUTS. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01.

Part: CONTROL VALVE — FAILED (ZONE 200) · airframe 7,569 hrs · 5,596 cycles

FLT RETURNED TO THE GATE WHEN DURING THE TAXI OUT THE CREW RECEIVED A RT PACK MASTER CAUTION. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RT PACK TEMPERATURE CONTROL VALVE. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUT — BINDING (RT MLG) · airframe 7,517 hrs · 5,559 cycles

ON LIFT-OFF, THE CREW RECEIVED A WOW INPUT CAUTION MESSAGE. THE OVERRIDE WAS USED TO RAISE THE GEAR. WHEN THE GEAR WAS RAISED, THE WOW INPUT CAUTION WAS EXTINGUISHED FOLLOWED BY A GEAR DISAGREE CAUTION WHICH REMAINED ILLUMINATED FOR APPROXIMATELY 5 SECONDS. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RIGHT MAIN LANDING GEAR STRUT AFTER DETERMINING THAT THE STRUT WAS BINDING. OPERATIONAL CHECKS WERE PERFORMED AND WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INTERCOSTAL — CRACKED (ZONE 400) · airframe 6,939 hrs · 5,125 cycles

PDX - RIGH HAND NACELLE, RIGHT HAND SIDE, ZONE 423 STATION XN198.00 ABOVE FLAP TRACK, INTERCOSTAL IS CRACKED. REPAIRED IAW SRM 51-42-05-330-001 AND SRM 51-40-15-400-001.

Part: SENSOR — OUT OF ADJUST (ZONE 700) · airframe 6,226 hrs · 4,596 cycles

DEN - FLIGHT 4167 - THE FLIGHT RETURNED TO FIELD WHEN AFTER TAKEOFF, THE CREW RECEIVED A PROX SYSTEM FAULT 1 INCH STATUS MESSAGE ACCOMPANIED BY GEAR AND FLAP INDICATIONS FAILING TO DISAPPEAR AFTER CLEANUP. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE LANDING GEAR WEIGHT OFF WHEELS NR 2 PROXIMITY SENSOR UNREASONABLY FAR. THE SENSOR WAS ADJUSTED AND THE OPERATONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FILTER — CLOGGED (ZONE 200) · airframe 5,653 hrs · 4,207 cycles

"DISPLAY COOL" CAUTION LIGHT ILLUMINATED AFTER TAKEOFF. EXTINGUISHED PER CHECKLIST. REILLUMINATED AFTER LANDING AND EXTINGUISHED AFTER CHECKLIST. FOUND DISPLAY FAN FILTER CLOGGED. REMOVED AND REPLACED FILTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FIRE WARNING — FALSE INDICATION (COCKPIT) · airframe 5,346 hrs · 3,984 cycles

BUR - FLIGHT 2555 - THE CREW RECEIVED AN INTERMITTENT FIRE WARNING FAULT STATUS MESSAGE. MAINTENANCE FOUND A MAINTENANCE DIAGNOSTIC COMPUTER FAULT: APU BOTTLE FAILED WIRING, LOW PRESSURE DETECTED. THE SYSTEM WAS PLACED ON MEL. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE APU FIRE EXTINGUISHER CONTAINER PRESSURE GAUGE, AND PERFORMED AN EXTINGUISHER WEIGHT CHECK. ALL CHECKS WERE GOOD. NO DISCREPANCIES NOTED. ALL OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FAN BLADE — WORN (NR 1 ENGINE) · airframe 5,238 hrs · 3,905 cycles

MFR - FLIGHT 2557 ON FLIGHT FROM PDX TO ONT AIRCRAFT DIVERTED TO MFR DUE TO NR 1 ENGINE VIBRATION. REPLACED FAN BLADES SERIAL NUMBERS, IHI3069N, IHI3130N, IHI3140N, IHI3144N, IHI3149N, IHI3150N, IHI3156N, IHI3158N, IHI3160N, IHI3178N, IHI3180N, IHI3182N, IHI3186N, IHI3188N, IHI3190N, IHI3191N, IHI3192N, IHI3193N, IHI3194N, IHI3195N, IHI3196N, IHI3198N, IHI3200N, IHI3202N, IHI3203N, IHI3204N, IHI3206N, AND IHI3208N. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CHIMNEY — DAMAGED (ZONE 200) · airframe 4,787 hrs · 3,580 cycles

PDX- CHIMNEY AT FORWARD ENRTY WAY TO BAGGAGE COMPARTMENT HAS DAMAGED WEBBING. REMOVED AND REPLACED CHIMNEY.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 3,800 hrs · 2,851 cycles

PDX- AFT CARGO PIT RIGHT HAND SIDE STRUCTURE AT INTERCOSTAL CRACKED FORWARD OF FEED THROUGH OF NR 2 CASE DRAIN RETURN LINE. REPAIRED IAW CRJ SRM 51-42-06.

Part: SKIN — GOUGED (FUSELAGE) · airframe 3,800 hrs · 2,851 cycles

PDX- FUSELAGE SKIN IS GOUGED AFT OF BAGGAGE BAY DOOR SURROUND INNER EDGE FIVE INCHES ABOVE LOWER FORWARD STOP FITTING. REPAIRED IAW CRJ SRM 53-61-01, 51-12-11 AND 51-25-01.

Part: SKIN — GOUGED (PAX DOOR) · airframe 3,800 hrs · 2,851 cycles

PDX- PASSENGER MAIN CABIN DOOR EXTERIOR SKIN HAS THREE GOUGES ON UPPER AFT CORNER EDGE OF DOOR. REPAIRED IAW CRJ SRM 51-20-06, 51-21-11, 51-25-01 AND AMM TASK 51-26-00-100-801-A01.

Part: AILERON — CHAFED (LT WING) · airframe 3,800 hrs · 2,851 cycles

PDX- LEFT AILERON BOTTOM FORWARD HAS CHAFE 12 INCHES FROM INBOARD EDGE. REPAIRED IAW CRJ SRM 51-20-06, 51-25-01 AND 51-21-11.

Part: SCREEN — DAMAGED (ZONE 200) · airframe 3,009 hrs · 2,264 cycles

BOI- FORWARD CARGO BAY CENTER CHIMNEY SCREEN IS DAMAGED. REPAIRED IAW REO 670-53-32-001. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BLADE — MISSING (ZONE 400) · airframe 2,576 hrs · 1,965 cycles

NR 1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND TWO BLADES MISSING. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THE MODIFICATION TO THE HPT1 DAMPNER (ALONG WITH RE-WORK OF THE ACCELERATOR) IS THE CORRECTIVE ACTION FOR THE REMOVED ENGINE. A PLAN HAS BEEN DEVISED TO INCORPORATE THIS MOD IN THE NEXT FEW QUARTERS.

Part: SWITCH — FAILED (FUEL SYSTEM) · airframe 2,355 hrs · 1,805 cycles

BOI ON FLIGHT 2447- CENTER WING SECTION HAS FUEL DRIPPING OUT. REMOVED AND REPLACED ENGINE FUEL PRESSURE SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: TUBE — CRACKED (FUEL SYSTEM) · airframe 2,257 hrs · 1,732 cycles

FAT - AIRPLANE IS TRANSFERRING FUEL FROM THE RIGHT WING TANK TO THE CENTER TANK ON GROUND. THE AIRCRAFT WAS DEFUELED, PANELS WERE OPENED, AND THE CENTER TANK WAS INSPECTED. MAINTENANCE FOUND A CRACK IN THE FUEL FEED TUBE AND REPLACED SAME. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACTUATOR — FAILED (L/E SLAT) · airframe 2,830 hrs · 2,356 cycles

PDX - CREW REPORTED A INTERMITTENT SLAT FAULT MESSAGE DURING DESCENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RIGHT NR 6 SLAT ACTUATOR. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TUBE — CHAFED (FUEL SYSTEM) · airframe 2,127 hrs · 1,641 cycles

PDX- LEFT HAND FUEL TUBE IS CHAFFED BEYOND LIMITS. REPAIRED IAW CRJ MM 28-21-00-790-802.

Part: TUBE — CHAFED (FUEL SYSTEM) · airframe 2,127 hrs · 1,641 cycles

PDX- LEFT AND RIGHT EJECTORS, RIGHT HAND LOWER CHECK VALVE, AND LEFT HAND UPPER CHECK VALVE TUBES CHAFED. REPAIRED IAW HORIZON AIR EO R-28-82 "A".

Part: WIRE HARNESS — DAMAGED (RT ENGINE) · airframe 1,886 hrs · 1,473 cycles

PDX- FIRE SYSTEM FAULT STATUS MESSAGE ON THE RIGHT HAND ENGINE FIRE LOOP A. REPAIRED WIRE HARNESS IAW AMM TASK 26-11-07-000-802-A01. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CAGE — DAMAGED (CARGO BAY) · airframe 1,640 hrs · 1,293 cycles

PDX- CAGE ABOVE AND JUST INSIDE FORWARD CARGO DOOR HAS SOME BROKEN MESH. REMOVED AND REPLACED CAGE IN FORWARD CARGO PIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PRESSURE SWITCH — LEAKING (FUEL SYSTEM) · airframe 1,408 hrs · 1,113 cycles

SEA - CREW REPORTS FUEL LEAK AT CENTER FUSELAGE. MAINTENANCE REPLACED THE PRIMARY EJECTOR PRESSURE SENSOR. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACM — DAMAGED (ACM BAY) · airframe 1,241 hrs · 981 cycles

PDX-LOUVER MISSING FROM LEFT HAND AIR CYCLE MACHINE EXHAUST AND ONE LOUVER IS CRACKED. REPAIRED IAW CRJ-700 SRM 51-42-06 AND HORIZON AIR EA R-21-13A.

Part: WARNING LIGHT — FALSE INDICATION (FWD CARGO DOOR) · airframe 1,218 hrs · 964 cycles

SJC - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKE-OFF THE CREW RECEIVED A CAUTION LIGHT FOR THE FORWARD CARGO DOOR. MAINTENANCE INSPECTED THE AIRCRAFT AND THE FORWARD CARGO DOOR PROXIMITY SENSORS. NO DISCREPANCIES WERE NOTED AND THE MDC VERIFIED CORRECT SENSOR STATUS. THE DOOR HANDLE RESET BUTTON WAS RESET AND A OPERATIONAL CHECK WAS COMPLIED WITH. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SENSOR — OVERHEATED (BRAKE ASSY) · airframe 1,062 hrs · 847 cycles

FLIGHT BETWEEN EUG - LAX WAS DIVERTED TO SMF. LEVEL AT FL370. BRAKE OVERHEAT WARNING MESSAGE ILLUMINATED. TEMPERATURE FLUXUATED BETWEEN 0-20, AFTER GEAR EXTENTION, TEMP WENT DOWN TO 0 WITH OCCASIONAL FLUXUATION. BACK TO 20 WITH ACCOMPANING WARNING. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT HAND BRAKE TEMP SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 537 hrs · 456 cycles

SEA- AFTER DEPARTURE, AN ACRID ODOR WAS REPORTED FROM CABIN. RECIRCULATING FAN CIRCUIT BREAKER WAS FOUND TO BE POPPED. TURNED RECIRCULATING FAN OFF, ODOR WENT AWAY. MAINTENANCE REPLACED THE NR 2 RECIRCULATION FAN, OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE.