N725PS

Part: TRUNNION — CORRODED (ZONE 500)

HN150978 DISCREPANCY: FOUND CORROSION ON L/H INBD FLAP VANE ACTUATOR FWD TRUNNION BODY (FLS24.00) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE FLAP VANE ACTUATOR TRUNNION BODY P/N 601R14261-1.

Part: SEAT TRACK — CORRODED (ZONE 200)

HN154917 DISCREPANCY: RBL 9 SEAT RAIL IS CORRODED BETWEEN FS 1033 AND FS 1061 CORRECTIVE ACTION: REMOVED AND REPLACED RBL 9 SEAT RAIL IAW CRJ-700 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-400-802-A03

Part: SEAT TRACK — CORRODED (ZONE 200)

HN154912 DISCREPANCY: FOUND SEAT RAIL @LBL 9 F.S 988-1005 HAS CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT RAIL P/N BA670-45074-3 @ LBL 9 F.S 988-1005 IAW CRJ 700 AMM 53-00-49-400-802 CONFIG A03

Part: PRESSURE PANEL — CHAFED

HN146636 DISCREPANCY: LOW PRESSURE BLEED PANEL PLATE HAS 4 CHAFED LOCATIONS IN THE SKIN AROUND THE BLEED ASSY CUTOUT. CORRECTIVE ACTION: REMOVED AND REPLACED LP BLEED PANEL PLATE IAW CRJ-700 SRM 51-42-06-001-001-A01, 51-42-22-001-001-A01, AND REO 670-53-61-2253 REV-- DATED 2024-04-02

Part: CRADLE — CORRODED (ZONE 600)

FOUND CORROSION ON R/H INBD FLAP VANE ACTUATOR CRADLE ASSY (FLS 140.40) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE CRADLE ASSY P/N CC670-14301-9 BN 309137

Part: FLOOR SUPPORT — CORRODED (ZONE 200)

HN00147959 DISCREPANCY: LBL 9 FLOOR BEAM IS CORRODED BETWEEN F.S. 1051.30 TO F.S. 1069.85. CORRECTIVE ACTION: REMOVED DAMAGED FLOOR BEAM LBL9 FROM FACTORY SPLICE TO MARKED CUT LINE. IAW CRJ-700 SRM 53-00-41-201-001-A01. FABRICATED REPAIR PARTS AND SPLICE PLATES FOR FLOOR BEAM, - B0501230BA – EXTRUSION, LBL 9 IAW CRJ 700 SRM 53-00-41-201-001-A01 AND REO 670-53-61-2254 REV -- DATED 2024-04-05

Part: WINDOW POST — CRACKED (ZONE 200)

HN146514 DISCREPANCY: FOUND WINDSHIELD POST CRACKED ON CAPTAIN SIDE BETWEEN WINDOW AND WINDSHIELD. CORRECTIVE ACTION: REMOVED AND REPLACED PILOT SIDE WINDSHIELD POST IAW CRJ-700 SRM 51-42-21-001-001-A01 AND 51-40-11-001-001-A01

Part: SKIN — CORRODED (PAX DOOR)

HN148465 DISCREPANCY: PAX DOOR INNER SKIN FOUND CORRODED. CORRECTIVE ACTION: REMOVED PAX DOOR INNER SKIN. SERVICEABLE INNER SKIN LOCATED AND DRILLED IAW CRJ700 SRM 51-40-11-001-001-A01

Part: FLOORBEAM — CORRODED (ZONE 200)

HN00147598 DISCREPANCY: LBL 27 FLOOR BEAM IS CORRODED AT F.S. 1031. CORRECTIVE ACTION: REPAIRED/REPLACED CORRODED SECTIONS OF FLOOR BEAM AT LBL 27 IAW CRJ 700 SRM 53-00-41-201-001-A01 AND REO 670-53-61-2254 REV -- DATED 2024-04-05.

Part: SEAT TRACK — CORRODED (ZONE 200)

HN154916 DISCREPANCY: FOUND SEAT RAIL AT RBL 9.00, FS 977-1005 TO BE CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED RBL 9 SEAT RAIL IAW CRJ-700 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-400-802-A03.

Part: SEAT TRACK — CORRODED (ZONE 200)

E HN154922 DISCREPANCY: RBL 27 SEAT RAIL IS CORRODED BETWEEN FS 1033 AND FS 1061 CORRECTIVE ACTION: REMOVED AND REPLACED RBL 27 SEAT RAIL IAW CRJ-700 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-400-802-A03

Part: FLOORBEAM — CRACKED (ZONE 200)

HN148550 DISCREPANCY: LBL9 FLIGHT COMPARTMENT FLOOR BEAM IS CRACKED ON THE FWD SIDE OF F.S. 280. CORRECTIVE ACTION: REPAIRED FLIGHT COMPARTMENT FLOOR BEAM IAW CRJ 700 SRM 53-11-43-201-003-A01

Part: BRACKET — CRACKED (PAX DOOR)

HN153304 DISCREPANCY: PAX DOOR BRACKET AT FWD CAM LATCH ASSY. FOUND TO BE CRACKED. CORRECTIVE ACTION: REMOVED BROKEN BRACKET. INSTALLED NEW SERVICEABLE PAX DOOR BRACKET AT FWD CAM LATCH ASSY IAW CRJ700 SRM 51-41-02-001-001-A01 AND CRJ700 AMM 52-70-04-400-806 (CONFIG A02)

Part: TRUNNION — CORRODED (ZONE 600)

HN150974 DISCREPANCY: FOUND CORROSION ON R/H INBD FLAP VANE ACTUATOR FWD TRUNNION BODY (FLS24.00) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE FLAP VANE ACTUATOR TRUNNION BODY P/N 601R14261-1.

Part: DOOR FRAME — CRACKED (ZONE 200)

HN147025 DISCREPANCY: LH OVERWING EMERGENCY EXIT DOOR TOP EDGE MEMBER IS CRACKED AT THE BASE OF THE AFT ALIGNMENT FITTING. CORRECTIVE ACTION: COMPLIED WITH MHIRJ REO 670-52-21-096 REV-- DATED 2024-04-01

Part: TRUNNION — CORRODED (ZONE 600)

HN150971 DISCREPANCY: FOUND CORROSION ON R/H INBD FLAP VANE ACTUATOR FWD TRUNNION BODY (FLS102.90) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE FLAP VANE ACTUATOR TRUNNION BODY P/N 601R14261-1. REFERENCE HR393982 FOR INSTALLATION. CERTS ATTACHED

Part: FLOORBEAM — CORRODED (ZONE 200)

HN00147488 DISCREPANCY: FS 280 FWD FLOOR SUPPORT ANGLE IS CORRODED AT LBL 9. CORRECTIVE ACTION: REMOVED J-ANGLE @ FS 280 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE J-ANGLE PN/ CC670-34095-1SB - ASSY, ANGLE IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01

Part: FLOORBEAM — CORRODED (BS 280)

HN148582 DISCREPANCY: FS 280 FRAME AFT AVIONICS BAY FLOORBOARD SUPPORT ANGLE IS CORRODED BETWEEN LBL 26 AND RBL 26. CORRECTIVE ACTION: REMOVED UNSERVICEABLE FLOORBOARD SUPPORT ANGLE IAW CRJ700 SRM 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE ANGLE PN/ CC670-34256-3 , IAW CRJ700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE ANGLE PN / CC670-34256-3 IAW CRJ700 SRM 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (ZONE 200)

HN154914 DISCREPANCY: LBL 9 SEAT RAIL IS CORRODED BETWEEN FS 1033 AND FS 1061 CORRECTIVE ACTION: REMOVED AND REPLACED LBL 9 SEAT RAIL IAW CRJ-700 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-400-802-A03

Part: SEAT TRACK — CORRODED (ZONE 200)

HN154920 DISCREPANCY: RBL 27 SEAT RAIL IS CORRODED BETWEEN FS 977 AND FS 1005 CORRECTIVE ACTION: REMOVED AND REPLACED RBL 27 SEAT RAIL IAW CRJ-700 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-400-802-A03

Part: INTERCOSTAL — CORRODED (ZONE 200)

HN00149798 DISCREPANCY: FWD INTERCOSTAL DD5 FOUND TO BE CORRODED. CORRECTIVE ACTION: PAX DOOR DD5 NEW SERVICEABLE INTERCOSTAL LOCATED AND DRILLED IAW CRJ700 SRM 51-40-11-001-001-A01. INSTALLED FWD INTERCOSTAL DD5 IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: DOOR FRAME — CORRODED (ZONE 200)

HN148697 DISCREPANCY: PAX DOOR FRAME AT FS320.00 FOUND TO BE CORRODED. CORRECTIVE ACTION: REMOVE CORRODED FRAME. LOCATED, DRILLED AND INSTALLED NEW PAX DOOR FRAME. PN# 601R318032-5 IAW CRJ700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: TRUNNION — CORRODED (ZONE 600)

HN150973 DISCREPANCY: FOUND CORROSION ON R/H INBD FLAP VANE ACTUATOR FWD TRUNNION BODY (FLS65.50) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE FLAP VANE ACTUATOR TRUNNION BODY P/N 601R14261-1. REFERENCE HR393982 FOR INSTALLATION. CERTS ATTACHED

Part: SKIN — CHAFED (ZONE 100)

HN00147837 DISCREPANCY: FUSELAGE OUTER SKIN IS CHAFED UNDER AFT LAV. RINSE/FILL PORT. CORRECTIVE ACTION: FOUND AN EXTERNAL REINFORCING DOUBLER AROUND CANNON PLUG PL118J1 TO BE CHAFED. NOT THE EXTERNAL SKIN. COMPLIED WITH REMAINING STEPS OF REO 670-53-51-281 REV - DATED 2024-04-05

Part: TRUNNION — CORRODED (ZONE 500)

HN150977 DISCREPANCY: FOUND CORROSION ON LH I/B FLAP VANE ACTUATOR FWD TRUNNION BODY. (FLS65.50) CORRECTIVE ACTION: RECEIVED SERVICEABLE TRUNNION BODY (P/N: 601R14261-1),

Part: INTERCOSTAL — CORRODED (FWD DOOR AREA)

HN00148680 DISCREPANCY: FWD INTERCOSTAL DD2 FOUND TO BE CORRODED. CORRECTIVE ACTION: REMOVED DAMAGED DD2 INTERCOSTAL. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE FWD INTERCOSTAL DD2 IAW CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01

Part: FLOOR SUPPORT — CRACKED (ZONE 200)

HN149314 DISCREPANCY: FOUND LH COCKPIT FLOOR BOARD SUPPORT ANGLE @ LBL 12 ON THE ATTACH FLANGE NEXT TO THE BULKHEAD POST TO BE CRACKED. CORRECTIVE ACTION: REMOVED LH COCKPIT FLOOR BOARD SUPPORT ANGLE @ LBL 12 ON THE ATTACH FLANGE NEXT TO THE BULKHEAD POST IAW CRJ700 SRM 51-42-06-001-001-A01 , SRM 51-42-21-001-001-A01. LOCATED AND INSTALLED NEW SERVICEABLE ANGLE PN/ CC670-33199-3S IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: FLOORBEAM — CORRODED (ZONE 200)

HN147962 DISCREPANCY: RBL 9.00 FLOOR BEAM IS CORRODED AT F.S. 1031.00. CORRECTIVE ACTION: REPAIRED DAMAGE I.A.W. BOMBARDIER CRJ700 SRM REPAIR 53-41-201-001-A01 AND MHIRJ REO 670-53-61-2254 REV.--, DATED 2024-04-05

Part: WEB — CRACKED

HN148432 DISCREPANCY: PAX DOOR AFT WEB FOUND CRACKED AND CORRODE. REQUIRES REPLACEMENT. CORRECTIVE ACTION: REMOVED CORRODED/CRACKED WEB. LOCATED AND DRILLED NEW AFT WEB PN 601R317071-11 IAW CRJ700 51-40-11-001-001-A01. REFERENCE TASK CARD HN00148068 FOR INSTALLATION OF AFT WEB.

Part: CRADLE — CORRODED (ZONE 500)

HN150967 DISCREPANCY: FOUND CORROSION ON THE L/H INBOARD FLAP VANE ACTUATOR CRADLE ASSY. (FLS140.00) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE CRADLE ASSY P/N CC670-14301-9 BN 309137.

Part: CRADLE — CORRODED (ZONE 500)

HN00150964 DISCREPANCY: FOUND CORROSION ON L/H INBD FLAP VANE ACTUATOR CRADLE ASSY (FLS102.90 CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE CRADLE ASSY P/N CC670-14301-9 BN 309137.

Part: MOUNT FITTING — NICKED (TRIM ACTUATOR)

HN00149690 DISCREPANCY: FOUND TRIM ACTUATOR FITTING HAS NICKS ON LH I/B LUG FWD AND AFT SIDES AND RH I/B LUG FWD SIDE. CORRECTIVE ACTION: COMPLIED WITH REO 670-55-31-171 REV-- DATED 4-12-24

Part: SEAT TRACK — CORRODED (ZONE 200)

HN154909 DISCREPANCY: LBL 27 SEAT RAIL IS CORRODED BETWEEN FS 977 AND FS 1005. CORRECTIVE ACTION: REMOVED AND REPLACED LBL 27 SEAT RAIL IAW CRJ-700 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-400-802-A03

Part: FORMER — CORRODED (PAX DOOR)

"HN148462 DISCREPANCY: PAX DOOR FWD FORMER FOUND CORRODED. CORRECTIVE ACTION: REMOVED PAX DOOR FWD FORMER IAW CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01 INSTALLED PAX DOOR FWD FORMER IAW CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01 .

Part: SEAT TRACK — CORRODED (ZONE 200)

HN154910 DISCREPANCY: LBL 27 SEAT RAIL IS CORRODED BETWEEN FS 1033 AND FS 1061. CORRECTIVE ACTION: REMOVED AND REPLACED LBL 27 SEAT RAIL IAW CRJ-700 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-400-802-A03

Part: WEB — CRACKED (DOOR STAIR)

HN149932 DISCREPANCY: PAX DOOR FWD STAIR WEB FOUND TO BE CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED PAX DOOR FWD STAIR WEB IAW CRJ-700 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, AND 51-42-21-001-001-A01.

Part: INTERCOSTAL — CORRODED (PAX DOOR)

HN148463 DISCREPANCY: PAX DOOR INTERCOSTAL DD6 MID FOUND CORRODED INSIDE PAX DOOR. CORRECTIVE ACTION: REMOVED PAX DOOR DD6 MID INTERCOSTAL IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR DD6 MID INTERCOSTAL P/N:601R318057-1 IAW CRJ700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: FLOORBEAM — CORRODED (ZONE 200)

HN148044 DISCREPANCY: RBL 27 FLOOR BEAM IS CORRODED FROM 1007 TO FS 1024. CORRECTIVE ACTION: REPAIRED RBL 27 FLOOR BEAM IAW CRJ-700 SRM 53-00-41-201-001-A01 AND MHIRJ REO 670-53-61-2254 REV-- DATED 2024-04-05.

Part: TRUNNION — CORRODED (ZONE 600)

HN150970 DISCREPANCY: FOUND CORROSION ON R/H INBD FLAP VANE ACTUATOR FWD TRUNNION BODY (FLS140.40) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE FLAP VANE ACTUATOR TRUNNION BODY P/N 601R14261-1.

Part: FORMER — CORRODED (PAX DOOR)

HN148941 DISCREPANCY: PAX DOOR AFT FORMER FOUND CORRODED. CORRECTIVE ACTION: REMOVED CORRODED FORMER AND INSTALLED PAX DOOR AFT FORMER P/N 601R318034-5 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01

Part: CRADLE — CORRODED (ZONE 600)

HN150969 DISCREPANCY: FOUND CORROSION ON THE R/H INBOARD FLAP VANE ACTUATOR CRADLE ASSY. (FLS24.00) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE CRADLE ASSY P/N CC670-14301 BN 30917.

Part: BRACKET — DAMAGED (ZONE 200)

HN00149834 DISCREPANCY: FWD INTERCOSTAL DD2 BRACKET FOUND TO HAVE ELONGATED HOLE. CORRECTIVE ACTION: DD2 BRACKET LOCATED AND DRILLED AND INSTALLED IAW CRJ700 51-40-11-001-001-A01 AND 51-42-06-001-001-A01

Part: BRACKET — CRACKED (SERVICE DOOR)

HN146956 DISCREPANCY: GALLEY SERVICE DOOR UPPER STABILIZER BRACKET IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED STABILIZER-BAR BRACKET IAW CRJ-700 AMM 52-41-27-400-801-A01 AND SRM 51-40-11-001-001-A01

Part: ACM — ODOR · airframe 14,709 hrs · 37,622 cycles

FLIGHT ATTENDANT REPORTED SEEING LIGHT SMOKE IN AFT CABIN PRIOR TO PUSH. CREW DEPLANED AIRCRAFT FOR INSPECTION. CREW DID NOT NEED MASKS, NO FIRE SUPPRESSION SYSTEMS USED. NO PASSENGER COMPLAINTS OR INJURIES FROM INHALATION. NO EMERGENCY DECLARED. RH PACK BLOWING SMOKE IN CABIN / DEFERRED RH PACK PER MEL 21-51-1-2 CAT C. / REMOVED AND REPLACED RH PACK ACM IAW CRJ 700 AMM 21-51-08-000/400-801.

Part: ACTUATOR — FAULTED (PITCH CONTROL) · airframe 37,825 hrs · 36,713 cycles

RECIEVED PITCH CONTROL MESSAGE ENROUTE TO SGF, THEY HAD TO LAND FLAPS 20 AND THEY DECLARED AN EMERGENCY. LANDED WITH NO FURTHER ISSUES. REMOVED AND REPLACED LINEAR PITCH-FEEL ACTUATOR (A140) IAW CRJ 700 AMM 27-31-23-000/400-801 A01. OPERATIONAL TEST OF THE PITCH FEEL SYSTEM CHECKS GOOD.

Part: SEAT TRACK — CORRODED (BS 477-581 LBL 9) · corrosion level 2 · airframe 37,454 hrs · 36,370 cycles

R/H SEAT AT RBL 9 FROM FS 477.0 TO FS 581 IS CORRODED (TRACK). INSTALLED NEW SERVICEABLE SEAT TRACK AT RBL 9 BETWEEN FS 477.0 TO 581 IAW CRJ 700 AMM 53-00-49-400-801-A03.

Part: FRAME — CORRODED (BS 379 S23-25R) · corrosion level 2 · airframe 37,454 hrs · 36,370 cycles

FS 379 FRAME IS CORRODED FROM STR 23R-25R. REMOVED FRAME AT FS 379 IAW CRJ 700 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. INSTALLED SERVICEABLE FRAME FS 379 RH IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 581-677 RBL 9) · corrosion level 2 · airframe 37,454 hrs · 36,370 cycles

R/H FLOOR SEAT TRACK FROM FS 581 - FS 677 AT RBL 9 IS CORRODED. FROM FS 581 - FS 677 IAW CRJ 700 AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 581-667 LBL 9) · corrosion level 2 · airframe 37,454 hrs · 36,370 cycles

L/H FLOOR SEAT TRACK FROM FS 581 - FS 677 AT LBL9 IS CORRODED. INSTALLED NEW RAIL, SEAT PN SH670-33425-3 IAW CRJ 700 AMM 53-00-49-400-801-A03.

Part: STRINGER — CORRODED (BS 364-394 S21R) · corrosion level 2 · airframe 37,454 hrs · 36,370 cycles

STGR 21 RH HAS MULTIPLE AREAS OF CORROSION AT FS 364.00 TO FS 394.00 AND ON PIECE JOINT. INSTALLED SERVICEABLE STRINGER AND REPAIR SPLICE IAW CRJ 700 SRM 53-00-03-991-905.

Part: SEAT TRACK — CORRODED (BS 677-830) · corrosion level 2 · airframe 37,454 hrs · 36,370 cycles

R/H FLOOR SEAT TRACK FROM FS 677 TO FS 830 AT RBL 9 IS CORRODED. INSTALLED NEW SERVICEABLE SEAT TRACK AT FS 677 TO FS 830 AT RBL 9 IAW CRJ 700 AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 677-830) · corrosion level 2 · airframe 37,454 hrs · 36,370 cycles

L/H FLOOR SEAT TRACK FROM FS 677 TO FS 830 AT LBL 9 IS CORRODED. LOCATED, DRILLED AND INSTALLED NEW SEAT TRACKS P/N 20275-288-0-0A FOR LH FROM 677 TO FS 830 LBL 9 IAW CRJ 700 REO 670-53-00-343 REV:L DATED 2015-05-05

Part: SEAT TRACK — CORRODED (BS 477-581 LBL9) · corrosion level 2 · airframe 37,454 hrs · 36,370 cycles

L/H FLOOR SEAT TRACK FROM FS 477 TO FS 581 AT LBL 9 IS CORRODED. REMOVED AND REPLACED SEAT RAIL IAW CRJ 700 AMM 53-00-49-400-801-A03.

Part: PANEL — CRACKED (PAX DOOR) · airframe 37,454 hrs · 36,370 cycles

CRACK ON LOWER CORNER OF SIDE PANEL FWD, LOCATED ON THE PASSENGER DOOR, P/N:601R317071-8. PERFORMED REPAIR AT LOWER CORNER OF SIDE PANEL FWD PASSENGER DOOR IAW CRJ 700 SRM 52-11-04-201-004-A01

Part: SEAT TRACK — CORRODED (BS 830-977) · corrosion level 2 · airframe 37,454 hrs · 36,370 cycles

R/H FLOOR SEAT TRACK FROM FS 830 TO 977 AT RBL 9 IS CORRODED. REPLACED CORRODED SEAT TRACK WITH NEW SERVICEABLE SEAT TRACK AT FS 830 TO FS 977 IAW CRJ 700 AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 830-977 LBL9) · corrosion level 2 · airframe 37,454 hrs · 36,370 cycles

L/H FLOOR SEAT TRACK FROM FS 830 TO FS 977 AT LBL 9 IS CORRODED. NEW RAIL, SEAT PN SH670-37420-5 WAS INSTALLED IAW CRJ 700 AMM 53-00-49-400-801-A03.

Part: RELAY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,604 hrs · 34,746 cycles

EMERGENCY LIGHTS ON STATUS MSG AND ILLUMINATION OF EMERGENCY LIGHTS INTERMITTENT THROUGHOUT THE FLIGHT. REMOVED AND REPLACED K135 RELAY IAW CRJ 700 AMM. OPS CHECK GOOD.

Part: LIGHT — DAMAGED (ROWS 16-18) · airframe 35,424 hrs · 34,589 cycles

EMERGENCY FLOOR PATH LIGHTING ON RH SIDE ROWS 16-18 DAMAGED. REMOVED AND REPLACED EMERGENCY FLOOR PATH LIGHTING ON THE RH SIDE AT ROWS 16-18 IAW CRJ 700 AMM 33-51-01-000/400-801-A11-PSA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,503 hrs · 33,762 cycles

L/H FWD EMERGENCY LIGHT INOP REMOVED AND REPLACED LH FWD EMERGENCY LIGHT OPS CHECK GOOD.

Part: ACTUATOR — FAILED (TE FLAP) · airframe 33,825 hrs · 33,133 cycles

ON APPROACH INTO CLT THE CREW RECEIVED A FLAPS FAIL MSG, DECLARED AN EMERGENCY AND LANDED SAFELY. MX REPLACED RT NR 4 FLAP ACTUATOR OPS CHECK GOOD.

Part: UNKNOWN — ODOR (A/C PACKS) · airframe 30,855 hrs · 30,352 cycles

SHORTLY AFTER TAKEOFF, THE CREW NOTICED A FOUL ODOR COMING FROM THE PACKS. THERE WAS NO EMERGENCY DECLARED AND THE AIRCRAFT RETURNED TO THE FIELD. MAINTENANCE COMPLIED WITH ENGINE RUNS AND OPS CHECK OF THE AIR CONDITIONING SYSTEM WITH NO DEFECTS AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CORRODED (BS 280) · corrosion level 2 · airframe 29,582 hrs · 29,252 cycles

FRAME AT BS 280 CORRODED BETWEEN STRINGER 26 AND 27L. PERFORMED A MAJOR REPAIR TO THE FRAME.

Part: BULKHEAD WEB — CORRODED (BS 280) · corrosion level 2 · airframe 29,582 hrs · 29,252 cycles

LEFT AND RIGHT BULKHEAD WEBS FOUND CORRODED AT BS 280. PERFORMED A MAJOR REPAIR TO THE BULKHEAD LOWER WEB.

Part: FRAME — CORRODED (BS 319) · corrosion level 2 · airframe 29,582 hrs · 29,252 cycles

FUSELAGE FRAME CORRODED AT BS 319.7 BETWEEN STRINGERS 25L AND 25R; PERFORMED A MAJOR REPAIR TO THE FUSELAGE FRAME.

Part: FRAME — DAMAGED (BS 333) · airframe 29,582 hrs · 29,252 cycles

FRAME DAMAGED AT FS333 BETWEEN STRINGER 26L AND 26R.

Part: WARNING MESSAGE — ACTIVATED (NLG STEERING) · airframe 29,204 hrs · 28,913 cycles

NOSEWHEEL STEERING INOPERATIVE CAUTION MESSAGE.

Part: WARNING MESSAGE — ACTIVATED (NLG STEERING) · airframe 29,204 hrs · 28,913 cycles

NOSEWHEEL STEERING INOPERATIVE CAUTION MESSAGE.

Part: WARNING MESSAGE — ILLUMINATED (NLG STEERING) · airframe 29,032 hrs · 28,751 cycles

NOSE WHEEL STEERING INOPERATIVE CAUTION MESSAGE DURING TAKEOFF.

Part: LIGHT — DETACHED (CABIN) · airframe 28,475 hrs · 28,191 cycles

LEFT HAND FORWARD EMERGENCY FLOOR PATH MARKING DETACHED FROM FLOOR. MAINTENANCE INSPECTED, RESECURED THE LEFT HAND FORWARD EMERGENCY FLOOR PATH MARKING AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (SPOILERS) · airframe 27,474 hrs · 27,289 cycles

INBD FLIGHT SPOILERS, AND INBD SPOILERONS, AMBER MESSAGE DISPLAYED IN FLIGHT. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, RESET THE SYS IAW MEL MANAUAL SYSTEM RESET, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 27,283 hrs · 27,118 cycles

CREW REPORTED A CRACK IN THE CAPTAIN’S SIDE WINDSHIELD AT FL280 AT 280 KTS. THEY DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE LT WINDSHIELD, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: CONTROLLER — FAULTY (WINDOW HEAT) · airframe 27,283 hrs · 27,118 cycles

CREW REPORTED A CRACK IN THE CAPTAIN’S SIDE WINDSHIELD AT FL280 AT 280 KTS. THEY DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE LT WINDSHIELD TEMPERATURE CONTROLLER, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,480 hrs · 26,376 cycles

EMERGENCY FLOODLIGHT, NR 6 IN CABIN OVERHEAD INOPERATIVE. RELAMPED EMERGENCY FLOODLIGHT IAW AMM. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (YAW DAMPING) · airframe 25,848 hrs · 25,801 cycles

CREW REPORTED UNCOMMANDED RUDDER INPUTS AT 34,000 FT. CREW DECLARED AN EMERGENCY AND DIVERTED. BEGAN DESCENT AND PROBLEM PERSISTED. COMING THROUGH APPROXIMATELY 10,000 FT, YD2 INOPERATIVE WHITE STATUS MESSAGE APPEARED. UNCOMMANDED RUDDER INPUTS CONTINUED TO SHORT FINAL, ALTHOUGH LESS PRONOUNCED. MAINTENANCE TROUBLESHOT, R & R NR 2 YAW DAMP ACTUATOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 25,750 hrs · 25,697 cycles

CREW REPORTED OTBD SPOILERON AND OTBD FLIGHT SPOILER CAUTION MESSAGES IN FLIGHT. CREW LANDED WITHOUT INCIDENT. SYSTEM RESET COMPLIED WITH IAW MINIMUM EQUIPMENT LIST MANUAL. ACFT RETURNED TO SERVICE.

Part: ANGLE — CORRODED (FS 319-349) · corrosion level 2 · airframe 25,621 hrs · 25,577 cycles

FS 319 TO FS 349 SERVICE DOOR LOWER SILL STRIKER HAS FILIFORM CORROSION. R & R SERVICE DOOR LOWER SILL STRIKER IAW SRM.

Part: DOOR SILL — CORRODED (BS 1015-1047) · corrosion level 2 · airframe 25,621 hrs · 25,577 cycles

FS 1015 TO FS 1047 AFT CARGO DOOR FLOOR SILL HAS FILIFORM CORROSION. R & R AFT CARGO DOOR FLOOR SILL IAW SRM.

Part: INTERCOSTAL — CORRODED (FS 278) · corrosion level 2 · airframe 25,621 hrs · 25,577 cycles

FS 278, JACK FITTING INTERCOSTALS HAVE FILIFOM CORROSION BL 0. R & R FS 278, JACK FITTING INTERCOSTALS IAW SRM.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 25,621 hrs · 25,577 cycles

RIGHT VERTICAL STAB FORWARD DRAG ANGLE CRACKED. REPAIRED DRAG ANGLE IAW REO.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 25,621 hrs · 25,577 cycles

BS 280, BULKHEAD LT LOWER WEB HAS CORROSION AT 3 LOCATIONS BETWEEN LBL 12 AND LBL 22. REPAIRED THE BULKHEAD LOWER WEB IAW SRM.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 25,621 hrs · 25,577 cycles

LEFT VERTICAL STABILIZER FWD DRAG ANGLE CRACKED. REPAIRED IAW REO.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 25,621 hrs · 25,577 cycles

BS 280 BULKHEAD RT LOWER WEB HAS CORROSION AT MULTIPLE LOCATIONS BETWEEN RBL 12 AND RBL 40. REPAIRED THE BULKHEAD IAM SRM.

Part: FRAME — CORRODED (BS 280) · airframe 25,621 hrs · 25,577 cycles

BS 280, J-CHANNEL HAS CORROSION BETWEEN LBL 12 AND RBL 12. REMOVED MINOR CORROSION AT FS 280.00, J-CHANNEL BETWEEN LBL 12 AND RBL 12 IAW SRM.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 25,621 hrs · 25,577 cycles

FS 280.00 CROSSBEAM ON UPPER FLANGE HAS FILIFORM CORROSION AT LBL 12 AND RBL 13. REPAIRED MINOR CORROSION AT FS 280.00 CROSSBEAM ON UPPER FLANGE IAW SRM.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED SYS) · airframe 24,054 hrs · 24,050 cycles

AT 27,000 FT, CREW REPORTED RT BLEED DUCT MASTER WARNING. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW FAULT ISOLATION MANUAL (FIM), INTERROGATED MAINTENANCE DIAGNOSTIC COMPUTER AND FOUND RT BLEED DUCT TO BE FLAGGED. MAINTENANCE PERFORMED VISUAL AND LEAK CHECK OF BLEED AIR DISTRIBUTION SYS AMM. NO DEFECTS NOTED. ACFT RELEASED FOR SERVICE.

Part: SEAT TRACK — CORRODED (BS 669-855) · corrosion level 2 · airframe 22,994 hrs · 22,941 cycles

DURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND ON SEAT TRACK BS 669 - 855. SEAT TRACK REPLACED IAW AMM. ACFT WAS RELEASED FOR SERVICE.

Part: STIFFENER — CRACKED (BS 202) · airframe 22,994 hrs · 22,941 cycles

DURING SCHEDULED MAINTENANCE, BS 202.75 FORWARD STIFFENERS WERE CRACKED AT LBL 30 AND RBL 30. AREA INSPECTED AND REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 22,344 hrs · 22,323 cycles

CREW REPORTED A BIRDSTRIKE TO NOSE OF AIRCRAFT. MAINTENANCE TROUBLESHOT, R & R THE RADOME USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 20,818 hrs · 20,775 cycles

CREW REPORTED SLATS FAIL CAUTION MESSAGE IN FLIGHT AFTER TAKEOFF. CREW COMPLIED WITH QRH (QUICK REFERENCE HANDBOOK) WITH SUCCESSFUL RETRACTION. CREW CONTINUED FLIGHT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. MESSAGE DID NOT RETURN. AIRCRAFT RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 19,490 hrs · 19,460 cycles

CREW REPORTED A SLATS FAIL MESSAGE. AIRCRAFT RETURNED TO AIRPORT LANDING WITHOUT ISSUE. MAINTENANCE USING THE AIRCRAFT MANUALS INSPECTED THE SYSTEM WITH NO DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE.

Part: SLAT — JAMMED (WING) · airframe 19,349 hrs · 19,315 cycles

CREW REPORTED SLATS FAIL AMBER CAS MESSAGE WITH FLAPS SELECTED TO EIGHT (8) DEGREES ON DESCENT. SLATS INDICATED ZERO DEGREES. CREW LANDED AT DESTINATION WITHOUT INCIDENT WITH FLAPS AT 45 DEGREES AND SLATS AT ZERO DEGREES. MAINTENANCE TROUBLESHOT SLAT SYSTEM, INTERROGATED MDC (MAINTENANCE DIAGNOSTIC COMPUTER) AND FOUND SLATS INHIBITED BY MECHANICAL JAM. MAINTENANCE CLEARED INHIBITS AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: SLAT — JAMMED (WING) · airframe 19,342 hrs · 19,309 cycles

CREW REPORTED SLATS FAIL CAUTION MESSAGE. MAINTENANCE TROUBLESHOT SLAT SYSTEM, INTERROGATED MDC (MAINTENANCE DIAGNOSTIC COMPUTER) AND FOUND SLATS INHIBITED DUE TO MECHANICAL JAM. MAINTENANCE CLEARED INHIBITS AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: TRANSDUCER — FAILED (HYDRAULIC SYSTEM) · airframe 19,108 hrs · 19,076 cycles

CREW REPORTED HYD 3 HIGH TEMP AMBER CAS MESSAGE IN FLIGHT. TEMPERATURE WENT FROM 96 DEGREES TO 108 DEGREES. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED NUMBER THREE (3) HYDRAULIC RESERVOIR AND NUMBER THREE (3) HYDRAULIC SYSTEM TRANSDUCER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 18,984 hrs · 18,955 cycles

CREW REPORTED RIGHT BLEED DUCT RED WARNING MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT AND PERFORMED OPERATIONAL TEST OF BLEED AIR LEAK DETECTION AND WARNING SYSTEM USING AIRCRAFT MAINTENANCE MANUALS. OPERATIONAL TEST GOOD. NO DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE.

Part: VALVE — FAILED (AC BAY) · airframe 18,828 hrs · 18,812 cycles

CREW REPORTED THE CABIN TEMPERATURE COULD NOT BE CONTROLLED AFTER TAKEOFF. AIRCRAFT RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE CROSS BLEED VALVE. THE LEFT HOT AIR SHUT OFF VALVE WAS ALSO REMOVED AND REPLACED. OPERATION CHECKS WERE PERFORMED USING MAINTENANCE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,415 hrs · 18,420 cycles

CREW REPORTED EMERGENCY FLOOD LIGHT AT ROW NINE (9) INOPERATIVE. MAINTENANCE INSPECTED, REMOVED AND REPLACED CEILING EMERGENCY FLOOD LIGHT NUMBER FOUR (4) LAMP AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: SKIN — DENTED (LE SLAT) · airframe 17,871 hrs · 17,892 cycles

CREW REPORTED BIRD STRIKE ON LEADING EDGE OF RIGHT WING DURING APPROACH. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE COMPLIED WITH BIRD STRIKE INSPECTION AND FOUND DENT IN RIGHT NUMBER ONE SLAT WITHIN LIMIT PER SRM (STRUCTURAL REPAIR MANUAL). NO FURTHER DEFECTS FOUND. AIRCRAFT RELEASED FOR SERVICE.

Part: RADAR — NOISY (NOSE) · airframe 17,161 hrs · 17,148 cycles

CREW REPORTED RADAR WAS MAKING A GRINDING SOUND WHEN CHANGING TILT. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MINTENANCE REMOVED AND REPLACED THE RADAR ANTENNA. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND OPERATIONAL CHECKED THE RADAR ANTENNA USING AIRCRAFT MANUALS.

Part: WINDOW — CRACKED (COCKPIT) · airframe 16,444 hrs · 16,420 cycles

CREW REPORTED AT CRUISE THAT THE LEFT SIDE WINDOW CRACKED. AIRCRAFT RETURNED TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE WINDOW. INSPECTION, REMOVAL, REPLACEMENTS, AND OPERATIONAL CHECKS WERE ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACM — SEIZED (NR 1) · airframe 16,162 hrs · 16,112 cycles

CREW REPORTED ON TAXI FOR DEPARTURE A SMOKE SMELL IN CABIN AND COCKPIT. AIRCRAFT WAS EVACUATED. MAINTENANCE TROUBLESHOT, REMOVED, AND REPLACED THE NR 1 AIR CYCLE MACHINE. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND PERFORMED OPERATIONAL CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DENTED (TE FLAP) · airframe 15,805 hrs · 15,743 cycles

DURING SCHEDULED MAINTENANCE REPAIRS WERE MADE TO A DENT ON THE LEFT INBOARD FLAP SKIN AT WS 55. INSPECTION AND REPAIR WAS ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,805 hrs · 15,743 cycles

DURING SCHEDULED MAINTENANCE THE FS 280 WEB AND FLOOR SUPPORT WERE CORRODED. INSPECTION AND REPAIR WAS ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FAN — DEFECTIVE (NR 2) · airframe 14,345 hrs · 14,332 cycles

CREW REPORTED STRONG ELECTRICAL FUMES COMING FROM THE AFT CABIN IN FLIGHT EN ROUTE FROM CLT TO TLH. CREW DIVERTED TO SAV AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE CIRCUIT BREAKER FOR THE NR 2 RECIRCULATION FAN WAS POPPED AND WOULD NOT RESET. MAINTENANCE REMOVED AND REPLACED THE NR 2 RECIRCULATION FAN AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RADOME — BURNED (FUSELAGE) · airframe 14,142 hrs · 14,109 cycles

CREW REPORTED A LIGHTNING STRIKE ON NOSE OF AIRCRAFT. MAINTENANCE USING THE AIRCRAFT MAINTENANCE MANUALS FOUND BURN MARKS ON THE RADOME. THE RADOME WAS REMOVED AND REPLACED. CHECKS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED.

Part: HANDLE — LACK OF LUBE (CARGO DOOR) · airframe 11,047 hrs · 10,878 cycles

CREW REPORTED AFT CARGO DOOR INDICATION INOP AFTER T/O IN CLT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HANDLE TO BE STIFF AND STICKS. MAINTENANCE TROUBLESHOT AND LUBED HANDLE PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WIRE — BROKEN (ANTI-ICE SYS) · airframe 10,314 hrs · 10,102 cycles

CREW REPORTED WING A/I SENSOR CAUTION MESSAGE IN FLIGHT. AIRCRAFT RETURNED TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE INSP AND FOUND 1 WIRE ON RT OUTBOARD TEMP SENSOR AND 3 WIRES ON LT OUTBOARD TEMP SENSOR TO BE PULLED OUT OR BROKEN. REPAIRS AND CHECKS WERE PERFORMED PER THE AIRCRAFT MAINTENANCE MANUAL WITH NO OTHER DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STALL WARNING — MALFUNCTIONED (COCKPIT) · airframe 10,010 hrs · 9,802 cycles

CREW REPORTED ON TAKEOFF A 'STALL FAIL' CAS MSG. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPS CHECK OF SPS AND FOUND NO DEFECTS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DOOR — OPEN (COMMS) · airframe 8,581 hrs · 8,403 cycles

CREW REPORTED AFTER TAKEOFF A LOUD WHINING NOISE COMING FROM THE NOSE OF THE AIRCRAFT. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE EXTERNAL COMM DOOR OPEN. MAINTENANCE SECURED THE DOOR CLOSED. NO DEFECTS OR DAMAGE NOTED AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DOOR — OPEN (EXTERNAL POWER) · airframe 8,342 hrs · 8,176 cycles

CREW REPORTED AN EXTERNAL POWER DOOR LEFT OPEN DURING FLIGHT. CREW ELECTED TO RETURN TO TLH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND SECURED THE DOOR CLOSED. NO DAMAGE NOTED AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 7,046 hrs · 6,904 cycles

CREW REPORTED A STRONG ODOR OF FUEL IN THE CABIN SHORTLY AFTER TAKEOFF AT APPROXIMATELY 4,000 FEET. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE RAN THE PACKS OFF THE ENGINE AND APU AND COULD NOT DUPLICATE THE PROBLEM ON THE GROUND. AIR CONDITIONING SYSTEM OPS CHECKS GOOD IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. SUSPECT ODOR CAME FROM PREVIOUS AIRCRAFT THAT TOOK OFF PRIOR TO THIS ONE. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DOOR — OPEN (GROUND POWER) · airframe 5,500 hrs · 5,345 cycles

CREW REPORTED A LOUD NOISE COMING FROM THE RT SIDE ON CLIMBOUT. CREW RETURNED TO GSO AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE GROUND POWER SERVICE DOOR OPEN. MAINTENANCE CLOSED AND SECURED DOOR. NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACTUATOR — FAILED (STICK PUSHER) · airframe 5,448 hrs · 5,291 cycles

CREW REPORTED A STALL FAIL CAS MESSAGE AFTER TAKEOFF. CREW RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE STICK PUSHER ACTUATOR IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ENGINE — VIBRATION (NR 2) · airframe 5,079 hrs · 4,956 cycles

CREW REPORTED A RIGHT HAND ENGINE VIBRATION AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NR 2 ENGINE AND PERFORMED AN ENGINE GROUND RUN. MAINTENANCE FOUND ALL VIBRATION INDICATIONS TO BE WITHIN LIMITS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DOOR — OPEN (EXTERNAL POWER) · airframe 4,976 hrs · 4,856 cycles

CREW REPORTED AN EXTERNAL POWER DOOR OPEN AFTER TAKEOFF. CREW RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CLOSED DOOR. NO DAMAGE OR DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DOOR — OPEN (EXTERNAL POWER) · airframe 4,838 hrs · 4,717 cycles

CREW REPORTED A LOUD SQUEAL IN COCKPIT ON CLIMBOUT. CREW RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE EXTERNAL POWER DOOR OPEN. MAINTENANCE CLOSED THE DOOR, INSPECTED AND FOUND NO DEFECTS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 1,348 hrs · 1,254 cycles

THE CREW REPORTED A HYD EDP 2A CAUTION MESSAGE EN ROUTE TO DTW. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE DRIVEN HYDRAULIC PUMP IAW CRJ700 AMM 29-11-01-000-801-A01 & 29-11-01-400-801-A01. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: AUTOTHROTTLE SYS — MALFUNCTIONED (COCKPIT) · airframe 814 hrs · 771 cycles

DURING TAKEOFF ROLL THE FLEX SETTING ON THE NR 1 ENGINE WAS LOST. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. THE FLEX SYSTEM WAS OPERATIONALLY CHECKED IAW CRJ 700 AMM 71-00-00-710-803-A01. THE SYSTEM OPS CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SENSOR — FAILED (LT ELEVATOR) · airframe 67 hrs · 62 cycles

DURING CRUISE (CLT TO TLH) THE ELEVATOR SPLIT CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2245 FOLLOWED THE QRH, DIVERTED TO JAX, AND MADE AN UNEVENTFUL LANDING. THE AIRCRAFT WAS INSPECTED BY CONTRACT MAINTENANCE AND THE DISCREPANCY WAS DETERMINED TO BE INDICATION ONLY. THE AIRCRAFT WAS THEN FERRIED TO DAY WHERE PSA MAINTENANCE REMOVED AND REPLACED THE RH ELEVATOR POSITION TRANSMITTER WITH A SERVICEABLE UNIT IAW CRJ 700 AMM 27-34-10-000-801-A02 AND 27-34-10-400-801-A02. THE TRANSMITTER WAS ADJUSTED IAW CRJ 700 AMM 27-34-10-820-801-A01 AND RIL 0194. THE SYSTEM OPERATIONALLY CHECKED GOOD IAW CRJ 700 AMM 27-34-10-710-801-A01. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: TRANSMITTER — OUT OF POSITION (RT ELEVATOR) · airframe 59 hrs · 53 cycles

DURING CLIMBOUT (IAD TO CLT) THE ELEVATOR SPLIT CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2231 FOLLOWED THE QRH, RETURNED TO IAD, AND MADE AN UNEVENTFUL LANDING. THE AIRCRAFT WAS INSPECTED BY CONTRACT MAINTENANCE AND THE DISCREPANCY WAS DETERMINED TO BE INDICATION ONLY. THE AIRCRAFT WAS THEN FERRIED TO DAY WHERE PSA MAINTENANCE FOUND THE RT ELEVATOR POSITION TRANSMITTER OUT OF ADJUSTMENT. THE RT TRANSMITTER WAS ADJUSTED IAW CRJ 700 AMM 27-34-10-820-801-A01. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: TRANSMITTER — OUT OF POSITION (RT ELEVATOR) · airframe 52 hrs · 46 cycles

AFTER DEPARTURE (CLT TO TLH) THE ELEVATOR SPLIT CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2232 FOLLOWED THE QRH, RETURNED TO CLT, AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE AT CLT REPOSITIONED THE RT ELEVATOR POSITION TRANSMITTER IAW CRJ 700 AMM 27-34-10-400-801-A02. THE SYSTEM OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.