N915EV

Part: WARNING MESSAGE — ILLUMINATED (LT ANTI-ICE) · airframe 43,922 hrs · 40,576 cycles

CREW DIVERTED TO PIT DUE TO ANTI ICE DUCT WARNING MSSG. (FLIGHT 5113 - FILED CLOSED) APR 15, 2025 STATION: PIT--PLEASE REFERENCE AML 1582914, PLEASE REFERENCE AML 1582036 PLEASE REFERENCE AML 1582037 FOR MAINTENANCE COMPLIED WITH. TROUBLESHOT ANTI ICE DUCT WARNING MSSG IN REFERENCE TO FIM 36-20-00. ARRIVED AT A/C AND PERFORMED OPERATIONAL TEST OF THE BLEED-AIR LEAK DETECTION AND WARNING SYSTEM IN REFERENCE TO CRJ 200 AMM 36-21-01. FOUND THE LH WING WOULD NOT TEST. PERFORMED RESISTANCE CHECK OF THE LH WING THERMAL SWITCHES IN REFERENCE TO CRJ 200 WM 36-21-00 AND ESPM 20-00-02. FOUND RESISTANCE TO BE MUCH HIGHER THAN EXPECTED. ISOLATED THE LH WING THERMAL SWITCHES. LH WING MOST OTBD WING SECTION TO BE AT FAULT. REMOVED AND REPLACED THERMAL SWITCHES AT LH WING STATIONS WS267.00, WS285.00, WS300.00, WS320.00, WS338.00, WS359.00 AND WS377.00 IN REFERENCE TO CRJ 200 AMM 36-21-07. REPERFORMED RESISTANCE CHECK OF LH WING. WING IS NOW READING AS EXPECTED. PERFORMED OPERATIONAL TEST OF THE BLEED-AIR LEAK DETECTION AND WARNING SYSTEM IN REFERENCE TO CRJ 200 AMM 36-21-01. OPS CHECK GOOD AT THIS TIME. R

Part: WARNING MESSAGE — ACTIVATED (ANTI-ICE SYS) · airframe 43,880 hrs · 40,536 cycles

CREW DIVERTED TO PIT DUE TO ANTI ICE DUCT WARNING MSSG. (FLIGHT 5113 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS

Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 43,691 hrs · 40,347 cycles

WINDSHIELD CRACKED IN FLIGHT. QRH EXECUTED AND DIVERTED TO KCOS (FLIGHT 5213 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 29693854 WITH THE FOLLOWING CORRECTIVE ACTION: REMOVED AND REPLACED LEFT WINDSHEILD IAW AMM 56-11-00 AND TASK CARD 56-220-1000-SKY. LEAK CHECK GOOD, OPS CHECK GOOD AT THIS TIME.

Part: OXYGEN BOTTLE — LOW PRESSURE (CREW) · airframe 42,077 hrs · 38,635 cycles

OXY LO PRESS DURING CRUISE. (FLIGHT 4634 FILED CLOSED)SERVICED CREW O2 TO PROPER LEVEL REF CRJ200 AMM 12-16-35. MCI IS ALREADY IN PLACE FOR TROUBLESHOOTING ON CREW O2 SYSTEM AND A POTENTIAL LEAK.

Part: STRUCTURE — DAMAGED (ZONE 500) · airframe 40,090 hrs · 36,662 cycles

FOUND HOLE IN UNDERLYING STRUCTURE IN THE FOOTPRINT OF PANEL 594UB TO BE DAMAGED REPAIRED THE STRUCTURE IAW REO 601R-57-51-1003, REV-.

Part: SKIN — CORRODED (BS 455) · airframe 40,090 hrs · 36,662 cycles

VHF ANTENNA CUT OUT AT F.S. 455.8 STGR 0 AFT O/B DOME NUTPLATE HAS A HOLE CORRODED. COMPLIED WITH REO 601R-53-41-3091 REV-. MAJOR REPAIR.

Part: HINGE — GOUGED (PAX DOOR) · airframe 40,090 hrs · 36,662 cycles

PAX DOOR HINGE LUGS ON FUSELAGE SIDE ARE GOUGED AT MID HINGE. REMOVED AND REPLACED THE DOOR HINGE IAW SRM 53-21-23.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 40,090 hrs · 36,662 cycles

RIGHT FLOOR SUPPORT BETWEEN BS 409+128 & 559 FOUND CORRODED AT MULTIPLE LOCATIONS. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-41-666, REV -C. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 40,090 hrs · 36,662 cycles

LEFT FLOOR SUPPORT BETWEEN BS 409+128 & 559. FOUND CORRODED AT MULTIPLE LOCATIONS. COMPLIED WITH REO 601R-53-41-666 REV -C. MAJOR REPAIR.

Part: STRINGER — CRACKED (BS 379 S3L) · airframe 40,090 hrs · 36,662 cycles

STRINGER 3L CRACKED, BS 379. REPAIRED THE STRINGER IAW SRM 53-00-03. MAJOR REPAIR.

Part: LANDING — CORRODED (LT WING PANEL) · airframe 40,090 hrs · 36,662 cycles

LEFT WING PLANK HAS SEVERAL AREAS OF CORROSION AROUND FUEL PANEL 540BB OPENING. REPAIRED THE WING PANEL LANDING IAW 601R-57-21-0030 REV-, MAJOR REPAIR TASK CARD 51-900-1003-SKY.

Part: PAN — CORRODED (SERVICE DOOR) · airframe 40,090 hrs · 36,662 cycles

SERVICE DOOR LOWER PAN IS CORRODED FORWARD AND AFT SIDES. REMOVED LOWER AFT SERVICE DOOR PAN IAW CRJ 200 SRM 51-42-06. INSTALLED SERVICEABLE LOWER AFT SERVICE DOOR PAN IAW CRJ 200 SRM 51-42-06. MAJOR REPAIR.

Part: FRAME — CORRODED (BS 310 S27L) · airframe 40,090 hrs · 36,662 cycles

FRAME SECTOR F.S.310 IS CORRODED AT STRINGER 27L. REMOVED THE FRAME SECTION, REINFORCMENT STRAP, AND SPLICES IAW SRM 51-42-21 AND 51-42-06. INSTALLED A FRAME NEW SECTION IAW SRM 51-42-21 AND 51-42-06. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 409-424) · airframe 40,090 hrs · 36,662 cycles

LBL 9 FLOOR SUPPORT UPPER CAP WAS FOUND CORRODED BS 409+123 - 424. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-41-3085, REV-.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 40,090 hrs · 36,662 cycles

LBL 9 FLOOR SUPPORT UPPER CAP INBD FLANGE HAD MULTIPLE AREAS OF CORROSION BETWEEN BS 409 - 409+112. REMOVED AND REPLACED THE FLOOR SUPPORT IAW REO 601R-53-31-1248 REV-. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 409-424) · airframe 40,090 hrs · 36,662 cycles

RBL 9 FLOOR SUPPORT UPPER CAP FOUND CORRODED BETWEEN BS 409+123 TO 424. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-41-3087, REV -.

Part: FRAME — CRACKED (BS 718 S11-12L) · airframe 40,090 hrs · 36,662 cycles

BS 718 FRAME FOUND CRACKED BETWEEN STRINGERS 11L & 12L. REPAIRED THE FRAME IAW REO 601R-53-61-193, REV A.

Part: FRAME — CRACKED (BS 718) · airframe 40,090 hrs · 36,662 cycles

FS 718 FRAME IS CRACKED BETWEEN STGR 11R AND 12R. REPAIRED THE FRAME IAW REO 601R-53-61-193, REV A, AND SRM 51-42-06 REV-39.

Part: SKIN — CHAFED (RT WING) · airframe 40,090 hrs · 36,662 cycles

RIGHT WING LOWER SKIN IS CHAFED ALONG BL 45 WHERE FAIRING CONTACTS SKIN. REPAIRED THE SKIN IAW REO 601R-57-21-880, REV-D.

Part: SKIN — CHAFED (LT WING) · airframe 40,090 hrs · 36,662 cycles

L/H WING LOWER SKIN IS CHAFED FROM BL 0 TO LBL. 45. REPAIRED THE SKIN IAW REO 601R-57-21-880 REV-D.

Part: STRUCTURE — DAMAGED (ZONE 500) · airframe 40,090 hrs · 36,662 cycles

FOUND ONE ELONGATED SCREW HOLE ON PANEL 572AL THROUGH INTO STRUCTURE. REPAIRED THE STRUCTURE IAW REO 601R-57-31-1403 REV-.

Part: SKIN — DAMAGED (ZONE 100) · airframe 40,090 hrs · 36,662 cycles

SHANK UNDER PANEL 192BB. REPAIRED FUSELAGE SKIN UNDER PANEL 192BB IAW REO 601R-53-31-1246 REV -.

Part: NONE — FAILED · airframe 39,693 hrs · 36,304 cycles

ON T/O WE RECEIVED A NOSE GEAR DISAGREE WITH NOSE GEAR DOWN AND GEAR LEVER UP ALSO RECEIVED A CAUTION WOW OUTPUT AND NOSE STEERING INOP CAUTION MSG ASSOCIATED WITH THE MASTER WARNING RAN QRH AND RECEIVED 3 GREEN ON GEAR INDICATION (FLIGHT 5367 - FILED CLOSED)JACKED AIRCRAFT AT NOSE LANDING GEAR. NOTED THAT NLG STRUT EXTENDED VERY SLOW, AND NEEDED TO BE PUSHED MANUALLY TO REACH FULL EXTENSION. LOWERED AIRCRAFT BACK DOWN AND PERFORMED A FULL NLG STRUT SERVICE IAW TASK CARD 12-710-002. JACKED NOSE OF AIRCRAFT AGAIN AND STRUT EXTENDED NORMALLY, AND LOCKED INTO PLACE WITHOUT ANY NEED TO MANUALLY PUSH IT TO FULL EXTENSION. PERFORMED GEAR SWING AT NLG PER AMM 32-33-00. AND ALL CHECKS GOOD.

Part: STOP FITTING — CRACKED (PAX DOOR FRAME) · airframe 37,320 hrs · 34,233 cycles

PAX DOOR CUTOUT, UPPER/FWD STOP-FITTING IS CRACKED FILED CLOSED REMOVED AND REPLACED PASSENGER DOOR CUTOUT UPPER FORWARD STOP FITTING REFERENCING APPLICABLE STEPS OF CRJ200 SRM 51-42-20.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 35,561 hrs · 32,328 cycles

LT PRESSURE FLOOR SILL AND SILL ANGLE ARE CORRODED BETWEEN FS 484 TO FS 499. (C-CHECK) RO: 09/12/2019 REPAIRED LT PRESSURE FLOOR SILL AND ANGLE IAW REO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,561 hrs · 32,328 cycles

LOWER FRAME SECTOR FS 574.00 CORRODED BETWEEN STR 25L TO 25R. (C-CHECK) RO: 09/12/2019 REPLACED LOWER FS 574 FRAME SECTOR IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,561 hrs · 32,328 cycles

FRAME CRACKED AT FS333.00 BETWEEN STR 0 AND STR 2L. (C-CHECK) RO: 09/12/2019 REMOVED AND REPLACED FS 333 TOP FRAME SECTOR P/N: 601R32004-41 IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 35,561 hrs · 32,328 cycles

STRAP AT FS 559.00 LBL 27.0 TO LBL 45.0 FLOOR LEVEL IS CORRODED ON UPPER SURFACE. (C-CHECK) RO: 09/12/2019 REMOVED & REPLACED LT 559.00 LBL UPPER SURFACE STRAP P/N 601R31025-29 IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 35,561 hrs · 32,328 cycles

AVIONICS DOOR SURROUND STRUCTURE, INTERCOSTAL CORRODED AT STR 27R BETWEEN FS349.00 AND FS364.00. (C-CHECK) RO: 09/12/2019 INSTALLED INTERCOSTAL BETWEEN FS349.00 AND FS364.00 AT STR 27R IAW SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 35,561 hrs · 32,328 cycles

AVIONICS DOOR SURROUND STRUCTURE FRAME CORRODED AT FS394.00 BETWEEN STR 27 AND 26L. (C-CHECK) RO: 09/12/2019 COMPLIED WITH REPAIR OF AVIONICS DOOR SURROUND STRUCTURE FRAME CORRODED AT FS394.00 BETWEEN STR 27 AND 26L REMOVE AND REPLACE FRAME SEGMENT IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 35,561 hrs · 32,328 cycles

AVIONICS DOOR SURROUND STRUCTURE INTERCOSTAL CORRODED BETWEEN FS349.00 AND FS364.00 AT STR 27. (C-CHECK) RO: 09/12/2019 INSTALLED INTERCOSTAL BETWEEN FS 349.00 AND FS 364.00 AT STR 27R IAW SRM.

Part: SKIN — CHAFED (FUSELAGE) · airframe 35,561 hrs · 32,328 cycles

EXTERIOR SKIN IS CHAFED AT AFT EDGE OF APU EXHAUST CUTOUT. (C-CHECK) RO: 09/12/2019 REPAIRED AREA IAW REO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 35,561 hrs · 32,328 cycles

EXTERIOR SKIN IS CORRODED BETWEEN FS 559.00+32 TO FS 574.00, STR 26R TO STR 26L. (C-CHECK) RO: 09/12/2019 C/W REMOVAL OF EXTERIOR SKIN CORROSION BETWEEN FS 559.00+32 TO FS 574.00, STR 26R TO STR 26L IAW REO.

Part: PANEL — CORRODED (FUSELAGE) · airframe 35,561 hrs · 32,328 cycles

RT PRESSURE FLOOR SILL PANEL IS CORRODED AT FS501. (C-CHECK) RO: 09/12/2019 REMOVED AREA OF CORROSION AT FS 501.0 IAW REO.

Part: PANEL — CORRODED (FUSELAGE) · airframe 35,561 hrs · 32,328 cycles

RT PRESSURE FLOOR SILL PANEL IS CORRODED AT FS441. (C-CHECK) RO: 09/12/2019 REPAIRED AREA OF CORROSION IAW REO.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 35,561 hrs · 32,328 cycles

PAX DOOR INTERCOSTAL DD3 CORRODED AT APPROX FS 333.00. (C-CHECK) RO: 09/12/2019 REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD3 CORRODED AT APPROX FS 333.00 IAW SRM.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 34,255 hrs · 30,883 cycles

ON GO AROUND, GEAR DISAGREE, SLOW RETRACTION. GEAR CAME UP ON ITS OWN. (FLT 3907) FO: 10/15/2018 WORK IN PROGRESS.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 32,388 hrs · 28,808 cycles

LEFT THRUST REVERSE UNLOCK IN FLIGHT. DIVERTED.

Part: FRAME — CORRODED (BS 574) · airframe 32,123 hrs · 28,527 cycles

FRAME BS 574 CORRODED. REPAIRED THE FRAME IAW SRM.

Part: FLAP — DAMAGED (RT WING TE FLAP) · airframe 32,123 hrs · 28,527 cycles

RIGHT OTBD FLAP REPAIR FAILED. REPLACED THE REPAIR IAW SRM.

Part: CHANNEL — CORRODED (LT WING) · airframe 32,123 hrs · 28,527 cycles

CHANNEL ALONG THE LT WING AFT SPAR CORRODED. REMOVED AND REPLACED THE CHANNEL IAW SRM.

Part: CHANNEL — CORRODED (RT WING) · airframe 32,123 hrs · 28,527 cycles

CHANNEL ALONG THE RT WING AFT SPAR CORRODED. REMOVED AND REPLACED THE CHANNEL IAW SRM.

Part: FAIRING — CHAFED (RT WING TE FLAP) · airframe 32,123 hrs · 28,527 cycles

RIGHT FLAP STUB-FAIRING CHAFED. REPAIRED THE FLAP IAW SRM.

Part: FAIRING — CHAFED (LT WING TE FLAP) · airframe 32,123 hrs · 28,527 cycles

LEFT FLAP STUB-FAIRING CHAFED. REPAIRED THE FLAP IAW SRM.

Part: BRACKET — CORRODED (LT WING) · airframe 32,123 hrs · 28,527 cycles

LEFT WING AFT SPAR BRACKET CORRODED. REMOVED AND REPLACED THE BRACKET IAW SRM.

Part: BRACKET — CORRODED (RT WING) · airframe 32,123 hrs · 28,527 cycles

RT WING AFT SPAR BRACKET CORRODED. REMOVED AND REPLACED BRACKET IAW SRM.

Part: FORMER — CORRODED (PAX DOOR) · airframe 32,123 hrs · 28,527 cycles

PASSENGER DOOR FORMER CORRODED. REPLACED THE FORMER IAW DWG.

Part: SUPPORT ANGLE — CORRODED (PAX DOOR) · airframe 32,123 hrs · 28,527 cycles

PASSENGER DOOR SUPPORT ANGLE CORRODED. REPAIRED DOOR SUPPORT ANGLE IAW SRM.

Part: FORMER — CORRODED (PAX DOOR) · airframe 32,123 hrs · 28,527 cycles

PASSENGER DOOR FORMER CORRODED. REPLACED THE FORMER IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 32,123 hrs · 28,527 cycles

FWD FACE OF THE BS 621 BULKHEAD IS CRACKED. REPAIRED THE BULKHEAD IAW REO. PRESSURE CHECKED GOOD.

Part: PANEL — CORRODED (PAX DOOR) · airframe 32,123 hrs · 28,527 cycles

PAX DOOR TOP PANEL CORRODED. REPLACED THE PANEL IAW SRM.

Part: FRAME ANGLE — CORRODED (BS 621) · airframe 32,123 hrs · 28,527 cycles

FRAME ANGLE AT BS 621 CORRODED. REMOVED AND REPLACED THE FRAME ANGLE IAW SRM.

Part: FRAME — CORRODED (BS 605) · airframe 32,123 hrs · 28,527 cycles

FRAME BS 605 CORRODED. REPLACED THE FRAME.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 32,123 hrs · 28,527 cycles

LT INBOARD FLAP VANE CHAFED. REPAIRED IAW REO.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 28,481 hrs · 24,611 cycles

RETURN TO FIELD DUE TO CARGO SMOKE WARNING MESSAGE. R & R THE CARGO AFT SMOKE DETECTOR.

Part: FRAME — CORRODED (BS 349) · airframe 28,467 hrs · 24,598 cycles

CORROSION ON AFT SIDE OF FRAME BS 349 BETWEEN STRINGERS 26L-26R. R & R FRAME IAW SRM.

Part: FRAME — CORRODED (BS 333) · airframe 28,467 hrs · 24,598 cycles

CORROSION ON AFT SIDE OF FUSELAGE FRAME BS 333, BELOW FLOOR, BETWEEN STRINGERS 25L AND 25R. R & R SECTION OF FRAME IAW SRM.

Part: SKIN — CHAFED (LT AILERON) · airframe 25,058 hrs · 21,142 cycles

LT AILERON UPPER LE SKIN DUE TO CHAFFED BEYOND ALLOWABLE LIMITS. C-CHECK REPLACED THE LT AILERON UPPER LE SKIN IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 25,058 hrs · 21,142 cycles

SERVICE DOOR SILL AREA KICK ANGLE HAS CORROSION BETWEEN FS 325 & FS 348. C-CHECK REPLACED SERVICE DOOR SILL ANGLE PN 601R38303-167 IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,058 hrs · 21,142 cycles

FLOOR BEAM CORRODED BEYOND ALLOWABLE LIMITS AT RBL27 BETWEEN FS589 TO FS605. C-CHECK REPLACED FLOOR BEAM AT RBL27 BETWEEN FS589 TO FS605 IAW REO.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 25,058 hrs · 21,142 cycles

LT INBD FLAP VANE LE SKIN CHAFED ON DOUBLER AT CENTER. C-CHECK BLENDED CHAFED AREA ON DOUBLER CAP LT INBD FLAP VANE AT CENTER OF LE IAW REO.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,058 hrs · 21,142 cycles

FLOOR SUPPORT STRUCTURE, FS559.0 TO FS559.0+80 CORROSION LT FLOOR SILL AT FS559.00-FS559.00+16. C-CHECK REMOVED CORROSION & BLENDED LT FLOOR SILL AT FS559.00 TO FS559.00+80 IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,058 hrs · 21,142 cycles

BAGGAGE FLOOR BEAM AT LBL27 FROM FS589 TO FS615 CORRODED. C-CHECK REPLACED BAGGAGE FLOOR BEAM AT LBL27 FROM FS589 TO FS615 IAW REO.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 25,058 hrs · 21,142 cycles

LT INBD FLAP VANE LE SKIN CHAFED ON DOUBLER AT INBD END. C-CHECK REPLACED WITH NEW DOUBLER CAP PN K601R14302-9S ON LT INBD FLAP VANE AT INBD END IAW SRM.

Part: SILL — CORRODED (FUSELAGE) · airframe 25,058 hrs · 21,142 cycles

CORROSION RT FLOOR SILL AT FS559.00+16 TO FS559.00+26 NUTPLATES. C-CHECK REMOVED & BLENDED CORROSION ON RT FLOOR SIL AT FS 559 TO 559+80 IAW REO.

Part: CONTROL CABLE — BROKEN (AUTOPILOT SYS) · airframe 25,058 hrs · 21,142 cycles

ELEVATOR AUTOPILOT SERVO CONTROL CABLE IS CORRODED & HAS BROKEN STRANDS AT THE SERVO CAPSTAN. C-CHECK REPLACED ELEVATOR AUTOPILOT SERVO CONTROL CABLE IAW AMM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 25,058 hrs · 21,142 cycles

MAIN AVIONICS COMPARTMENT DOOR STRUCTURE CUTOUT, FOUND SEVERAL AREAS AROUND THE STRUCTURE THAT HAS SURFACE CORROSION. C-CHECK BLENDED CORROSION FROM MAIN AVIONICS BAY DOOR STRUCTURE CUTOUT IAW REO.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 25,058 hrs · 21,142 cycles

LT INBD FLAP VANE LE SKIN CHAFED ON DOUBLER AT OTBD END. C-CHECK BLENDED CHAFED AREA ON DOUBLER CAP ON LT INBD FLAP VANE ON LE AT OTBD END IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,058 hrs · 21,142 cycles

RBL 27 FS 605 AFT HAS CORROSION AT NUTPLATE HOLES. C-CHECK TREATED CORROSION ON RT FLOOR BEAM AT RBL27 FROM FS589 TO FS605 IAW REO. CORROSION EXCEEDED LIMITS. REPLACED IAW REO.

Part: SKIN — CHAFED (RT MLG DOOR) · airframe 25,058 hrs · 21,142 cycles

RT MLG DOOR INNER LE SKIN CHAFED AT OTBD END. C-CHECK REMOVED DAMAGED AREA & FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR FILLER & RESTORED TOP COAT IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,058 hrs · 21,142 cycles

LBL 27 FS 589 TO JUST AFT OF FS 605 HAS CORROSION AT NUTPLATES. C-CHECK TREATED CORROSION ON LT FLOOR BEAM AT LBL27 FROM FS589 TO FS615 IAW REO. CORROSION EXCEEDED LIMITS. REPLACED IAW REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,058 hrs · 21,142 cycles

RBL 27 FS 484 INBD CLIP IS CRACKED RT SIDE. C-CHECK REPLACED INBD CLIP PART NR 601R31171-9 AT RBL 27 FS 484 IAW REO.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 25,058 hrs · 21,142 cycles

RBL 36 FS 484 INTERCOSTAL HAS CRACK AT UPPER RADIUS. C-CHECK REPLACED THE FS484 RBL36 CLIP IAW REO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 25,058 hrs · 21,142 cycles

LBL 36 FS 621 AFT LOWER FLOOR SUPPORT IS CRACKED AT RADIUS. C-CHECK REPLACED CRACKED FLOOR SUPPORT AT LBL 36 FS 621 IAW REO.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 25,058 hrs · 21,142 cycles

LT WING UPPER ACCESS PANEL 540AT HAS FRETTING AROUND PERIMETER. C-CHECK BLENDED LT WING UPPER ACCESS PANEL 540AT IAW SRM & REO.

Part: POST — CRACKED (FUSELAGE) · airframe 25,058 hrs · 21,142 cycles

CRACK IN FS409+128 VERTICAL POST AT RBL18, INBD C-CHANNEL IN THE AFT RADIUS. C-CHECK REPLACED OTBD & INBD C-CHANNEL AT VERTICAL POST FS409+128 AT RBL18 IAW REO.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 25,058 hrs · 21,142 cycles

RT WING WING ACCESS PANEL AREA 640AT HAS FRETTING AROUND PERIMETER. C-CHECK BLENDED WING ACCESS PANEL AREA 640AT IAW SRM & REO.

Part: PRINTER — MALFUNCTIONED (ACARS) · airframe 24,946 hrs · 21,036 cycles

ACARS PRINTER FAILED, THEN NOTICED A FAINT BURNING SMELL. SEEMS TO BE COMING FROM THE PRINTER. FLT#4580 INSPECTED COCKPIT FOR BURNING SMELL. NO DEFECTS NOTED. VERIFIED ACARS PRINTER INOPERATIVE. INSTALLED NEW ACARS PRINTER. PRINTER OPERATES NORMALLY. PN 8055515-4507, SN ON PTA458-06873, SN OFF PTA45B-06776.

Part: CHARGER — FAILED (CABIN) · airframe 24,335 hrs · 20,405 cycles

PASSENGER DOOR LOWER EMERGENCY FLOOD LIGHT DOES NOT ILLUMINATE. (SERVICE) REPLACED NR 2 EMERGENCY LIGHT CHARGER ASSEMBLY.

Part: WIRE — BROKEN (CABIN) · airframe 24,307 hrs · 20,372 cycles

MAIN CABIN DOOR FLOOR LEVEL EMERGENCY FLOOD LIGHT DOES NOT ILLUMINATE. (FLT 4645) REPAIRED BROKEN WIRE GOING TO MAIN CABIN DOOR EMERGENCY FLOOD LIGHT CONNECTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,307 hrs · 20,372 cycles

SERVICE DOOR EMERGENCY EXIT FLOOD LIGHT NR 4 BULB IS BURNED OUT. (FLT 4645) RELAMPED EMERGENCY LIGHT.

Part: UNKNOWN — SMOKE (CABIN) · airframe 24,148 hrs · 20,211 cycles

AFTER APPLYING BLEED AIR SMOKE WAS COMING OUT OF THE AIR VENTS. SMOKE TOILET CAUTION MESSAGE. OPENED MAIN CABIN DOOR. MESSAGE AND SMOKE CLEARED. (FLT 4553) INSPECTED BOTH PACKS FOR LEAKS AND PROPER OPERATION. OPERATED BOTH PACKS OFF OF THE APU IAW AMM. NO DEFECTS NOTED. INSPECTED THE LAV AREA AND NO EVIDENCE OF SMOKE AND SMOKE DETECTOR SYSTEM OPERATING NORMALLY.

Part: UNKNOWN — SMOKE (CABIN) · airframe 23,987 hrs · 20,041 cycles

SMOKE TOILET CAUTION MESSAGE APPEARED AFTER TRANSFERRING BLEEDS TO APU DURING APPROACH. AFTER TURNING OFF PACKS, MESSAGE CLEARED. AIRCRAFT HAD BEEN DEICED PRIOR TO DEPARTURE. (FLT 7430) PERFORMED OPERATIONAL CHECK OF AIR CONDITIONING SYSTEM USING BOTH APU AND ENGINE BLEEDS AS A SOURCE. COULD NOT DUPLICATE SMOKE IN CABIN. POSSIBLY GLYCOL INGESTED DURING DEICING. OPERATIONAL CHECK GOOD.

Part: AHRS — FAILED (NR 1) · airframe 23,653 hrs · 19,727 cycles

STALL FAIL CAUTION IN FLIGHT ON APPROACH AND AIRCRAFT INITIATED SHARP LEFT ROLL MOVEMENT. (FLT 4486) REPLACED NR 1 AHRS IAW AMM P/N: 622-9815-904 S/N: 1BWYC S/N OFF: 02GY AND NR 2 FCC P/N: 622-9336-400 S/N: FTLH S/N OFF: 12PRN

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,582 hrs · 19,656 cycles

LEFT FORWARD WING EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 7755) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,546 hrs · 19,617 cycles

NR 1 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 4736) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,271 hrs · 19,310 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4777) RELAMPED AND REPLACED NR 3 ELBP IN REFERENCE TO AMM. P/N: AD-2013-1A S/N OFF: 43078

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,160 hrs · 19,192 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4653) RELAMPED EMERGENCY LIGHT.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 22,951 hrs · 18,987 cycles

DURING DESCENT SMELLED FAINT BURNING SMELL. DURING TAXI LEFT PACK PUT OUT 120° AIR WHILE AT COLDEST SETTING. (FLT 4802) REPLACED LEFT AIR CYCLE MACHINE. P/N: 782790-15 S/N OFF: 200305035

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,780 hrs · 18,823 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4686) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,536 hrs · 18,568 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4503) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,321 hrs · 18,365 cycles

FORWARD OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7808) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,185 hrs · 18,225 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4594) RELAMPED EMERGENCY LIGHT.

Part: BEARING — CORRODED (ENGINE MOUNT) · airframe 22,144 hrs · 18,185 cycles

RIGHT ENGINE AFT MOUNT THRUST SHAFT HOUSING IS PITTED. REPLACED RIGHT ENGINE AFT THRUST MOUNT BEARING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,025 hrs · 18,055 cycles

LEFT AFT OVERWING EMERGENCY LIGHT IS OUT. (FLT 4681) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,014 hrs · 18,045 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4522) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,580 hrs · 17,646 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4551) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,494 hrs · 17,575 cycles

NR 6 & NR 7 EXTERIOR EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,392 hrs · 17,470 cycles

LEFT OVERWING AFT AND RIGHT OVERWING MIDDLE EXTERIOR LIGHTS ARE OUT. (SERVICE) RELAMPED EXTERIOR LIGHTS.

Part: SKIN — CRACKED (PAX DOOR) · airframe 21,354 hrs · 17,436 cycles

PAX DOOR LOWER INNER SKIN CRACKED. (C-CHECK) REPAIR PER REO.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 21,354 hrs · 17,436 cycles

PAX DOOR FORWARD AND AFT LOWER INTERCOSTAL CRACKED. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,321 hrs · 18,365 cycles

FS 559 BULKHEAD CRACKED. (C-CHECK) REPAIR PER REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 22,321 hrs · 18,365 cycles

RIGHT AILERON LOWER LEADING EDGE IS CHAFED AT OUTBOARD END OF AILERON. (C-CHECK) REPLACED RIGHT AILERON LOWER LEADING EDGE SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,194 hrs · 17,300 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4804) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,067 hrs · 17,185 cycles

LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4747) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,793 hrs · 16,941 cycles

RIGHT OVERWING FORWARD EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 4483) RELAMPED RT FWD EMERGENCY LIGHT. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,310 hrs · 16,531 cycles

AFT EMERGENCY CEILING LIGHT IS OUT. (FLT 4479) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,280 hrs · 16,502 cycles

EXTERIOR EMERGENCY LIGHT JUST FORWARD OF THE MAIN CABIN DOOR IS OUT. (FLT 4697) RELAMPED EMERGENCY LIGHT.

Part: MOUNT — CORRODED (LT ENGINE) · airframe 19,008 hrs · 15,396 cycles

LEFT ENGINE FORWARD MOUNT LINK PITTED. (ENG CHANGE) REPLACED LEFT ENGINE MOUNT LINK PER AMM.

Part: ACTUATOR — MALFUNCTIONED (STALL WARNING) · airframe 18,297 hrs · 14,754 cycles

ON ROTATION AND FLARE, EXCESSIVE ELEVATOR BACK-PRESSURE REQUIRED. (FLT 4686) PERFORMED OPERATIONAL CHECK OF THE ELEVATOR CONTROL SYSTEM, INSPECTED CABLES AND ELEVATOR AND FOUND NO DEFECTS. PERFORMED FORCE GAUGE CHECK OF THE RIGHT AND LEFT ELEVATORS FORCES AND FOUND FORCE GAUGE CHECK TO BE WITHIN LIMITS. REPLACED STICK PUSHER ACTUATOR.

Part: UNKNOWN — MALFUNCTIONED (ELEVATOR) · airframe 18,238 hrs · 14,701 cycles

EXCESSIVE FORCE REQUIRED FOR FULL AFT ELEVATOR DEFLECTION. (FLT 4946) ALL FORCES WITHIN LIMITS PER FTP F601R2730 ATA PAGE 102.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,156 hrs · 14,634 cycles

FURTHEST AFT CEILING EMERGENCY LIGHT INOP. (FLT 4567) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 16,874 hrs · 13,604 cycles

FS 202 BULKHEAD BRAKE CABLE PASS THROUGH CRACKED. (C CHECK) REPAIR PER REO IN PROGRESS.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 16,858 hrs · 13,590 cycles

UPPER CORNER LINTEL FITTING FS 621 BULKHEAD WEB INTERFACE CRACKED. (C CHECK) REPAIRED PER REO.

Part: FLANGE — CRACKED (FUSELAGE) · airframe 17,065 hrs · 13,746 cycles

FS 280 LEFT LOWER FLANGE CRACKED. (C CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,065 hrs · 13,746 cycles

FS 559 BULKHEAD WEB CRACKED. (C CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,065 hrs · 13,746 cycles

FS 621 BULKHEAD WEB CRACKED. (C CHECK) REPAIRED PER REO.

Part: FITTING — CRACKED (CARGO BAY) · airframe 17,065 hrs · 13,746 cycles

FS 621 CARGO DOOR TRACK FITTING CRACKED. (C CHECK) REPAIRED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,065 hrs · 13,746 cycles

FS 280 CLIPS CRACKED. (C CHECK) REPLACED PER REO.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 17,065 hrs · 13,746 cycles

FS 280 BULKHEAD GOUGED. (C CHECK) REPAIRED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,065 hrs · 13,746 cycles

FS 621 LINTEL FITTINGS CRACKED. (C CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,807 hrs · 13,547 cycles

FORWARD EMERGENCY FLOOD LIGHT INOP. (FLT 4391) RELAMPED EMERGENCY LIGHT.

Part: FLANGE — CRACKED (FUSELAGE) · airframe 16,860 hrs · 13,592 cycles

FS 280 LEFT LOWER FLANGE CRACKED. REPAIRED PER REO.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 15,246 hrs · 12,344 cycles

FLT 4577 - THE SECOND OVERHEAD EMERGENCY LIGHT INOP. RELAMPED.

Part: FRAME — CRACKED (BS 640) · airframe 15,117 hrs · 12,245 cycles

VISUALLY INSPECTED THE LEFT AND RIGHT SIDE FRAMES AS REQUIRED BY AD 2008-06-10/01. BOTH SIDE FRAME DOUBLERS AT FS 640 INDICATE CRACKS. (AD INSP) REPAIRED PER SB 601R-53-065 REV B.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 13,208 hrs · 10,753 cycles

FLT 3986 - LEFT WINDSHIELD OUTER PLY IS CRACKED. REPLACED PILOT'S WINDSHIELD IAW 56-11-01, P/N: NP-139321-B, S/N OFF: 02298H8774.

Part: WARNING MESSAGE — ILLUMINATED (LAVATORY) · airframe 13,080 hrs · 10,657 cycles

RECEIVED SMOKE TOILET CAUTION MESSAGE AFTER TAKEOFF, FLIGHT NR 3843. INSPECTED AND OPERATED BOTH PACKS WITH NO DISCREPENCIES NOTED. OPS CHECK GOOD.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,171 hrs · 10,722 cycles

RIGHT SIDE OF STA 280 LOWER FLOORBEAM IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIR ON LOWER BEAM PER CRJ200 REO 601R-53-11-171 REV D DATED 13-FEB-07.

Part: SUPPORT BEAM — CRACKED (RT ENGINE) · airframe 13,171 hrs · 10,722 cycles

RIGHT LOWER WEB AT FORWARD CORNER OF ACCESS OPENING ON ENGINE SUPPORT BEAM IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REO 601R-53-01-358 REV B TO REPAIR WEB.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,171 hrs · 10,722 cycles

STA 280 LEFT UPPER FLOORBEAM ANGLE IS CRACKED AT STA 280 AND LBL9, FOUND AT C-CHECK. COMPLIED WITH REPAIR TO FLOORBEAM ANGLE PER CRJ200 REO 601R-53-11-138.

Part: HANDLE — CORRODED (ESCAPE HATCH) · airframe 13,171 hrs · 10,722 cycles

CREW ESCAPE HATCH OUTER HANDLE ASSEMBLY HAS SIGNS OF CORROSION, FOUND AT C-CHECK. REMOVED LIGHT CORROSION ON OUTER HANDLE ASSEMBLY PER SRM CRJ200 51-21-06 PG 1 TO PG 5.

Part: FLOOR SUPPORT — CRACKED (BS 621) · airframe 13,171 hrs · 10,722 cycles

RIGHT SIDE OF FS 621 FLOOR SUPPORT ANGLE IS CRACKED, FOUND AT C-CHECK. REPLACED FLOOR SUPPORT PER CRJ200 REO 601R-53-61-117 REV A.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 13,171 hrs · 10,722 cycles

PAX DOOR EXTERIOR HANDLE IS CRACKED, FOUND AT C-CHECK. REPLACED PAX DOOR OUTSIDE HANDLE PER CRJ200 AMM 52-11-03-020-007.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 12,415 hrs · 10,171 cycles

FOUND FORWARD CEILING EMERGENCY POD LIGHT INOP. RELAMPED FORWARD CEILING EMERGENCY LIGHT. OPS CHECK GOOD.

Part: ADC — FAILED (COCKPIT) · airframe 10,681 hrs · 8,878 cycles

IN FLIGHT, LEFT ALTIMETER AND VERTICAL SPEED BECAME INOP ALONG WITH "MACH TRIM". REPLACED ADC NR 1 IAW ST34-220-1016 AND MM 34-13-01. OPERATIONAL CHECKS GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 10,298 hrs · 8,610 cycles

EMERGENCY LIGHT PACK ON CEILING IS BURNED OUT. REPLACED LAMP IN CEILING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD, PN 1317.

Part: LIGHT — FAILED (CABIN) · airframe 9,889 hrs · 8,306 cycles

CENTER OVERHEAD EMERGENCY LIGHT NON-FUNCTIONING. RELAMPED CENTER OVERHEAD EMERGENCY LIGHT.

Part: SWITCH — INOPERATIVE (NLG STEERING)

ON APPROACH, THE CREW RECEIVED A STEERING INOP CAUTION MESSAGE WHEN THE GEAR WAS SELECTED TO THE DOWN POSITION. THE CREW TRIED TO RESET THE NOSE WHEEL STEERING SWITCH, BUT THE SWITCH WOULD NO RESET. THE QRH WAS FOLLOWED. AN EMERGENCY WAS NOT DECLARED, BUT EMERGENCY TRUCKS WERE ROLLED OUT AS A PRECAUTION. AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT FEEDBACK RVDT AND ADJUSTED THE RT RVDT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING AN A-CHECK, THE FS 640 RT DOUBLER AT STRINGER 10 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 640 RT DOUBLER AT STRINGER 10. (K)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING AN OVERNIGHT SERVICE CHECK IN CAE, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CLAMP — DAMAGED (LANDING GEAR)

FLT 4773 - DURING TAKEOFF ROLL FROM FNT-CVG, AT APPROXIMATELY 130 KNOTS THE RIGHT MAIN LANDING GEAR MLG STRUCK A COYOTE. GEAR RETRACTION AND SUBSEQUENT TAKEOFF WERE NORMAL. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN CVG. MAINTENANCE FOUND ANIMAL REMAINS AND DAMAGE TO TWO BAND CLAMPS ON THE RIGHT MLG WHICH WERE REPLACED. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CIRCUIT BREAKER — TRIPPED (STAB TRIM)

FLT 4491 - DURING CLIMB-OUT FROM DFW-MSY, WHEN PASSING THROUGH 21,000 FEET THE CREW RECEIVED A STAB TRIM AND MACH TRIM CAUTION MESSAGE ON EICAS 1. QRH PROCEDURES WERE COMPLIED WITH AND ATTEMPTS TO REENGAGE THE STAB TRIM AND MACH TRIM WERE UNSUCCESSFUL, WITH THE MESSSAGE PERSISTING. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO AEX, LANDING SAFELY. MAINTENANCE RESET THE CIRCUIT BREAKERS FOR THE HORIZONTAL STABILIZER TRIM ACTUATOR SYSTEM AND ALSO PERFORMED A STABILIZER TRIM SYSTEM TEST IAW AMM 27-00. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE AFT EQUIPMENT BAY SPIDER DUCT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT EQUIPMENT BAY SPIDER DUCT BRACKET. (M)

Part: CLIP — CRACKED (BULKHEAD)

DURNG A C-CHECK IN MCN, THE AFT EQUIPMENT BAY PRESSURE BULKHEAD RT CLIP AT FS 625, NEAR STRINGERS 14 L/R WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AFT EQUIPMENT BAY PRESSURE BULKHEAD RT CLIP AT FS 625, NEAR STRINGERS 14 L/R IAW ASA EO 600-53-0174. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

FLT 4912 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY CEILING LIGHT AT ROW TWO WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW TWO. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ACTUATOR — INOPERATIVE (PAX DOOR)

FLT 4399 - DURING A GROUND INSPECTION IN JAX, THE PASSENGER DOOR WOULD NOT CLOSE OR OPEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: O-RING — LEAKING (APU FUEL SYS)

FLT 4772 - DURING CRUISE FROM MOB-DFW, AT APPROXIMATELY 31,000 FT, A STRONG FUEL ODOR OCCURRED IN THE COCKPIT. THE CREW INITIATED DESCENT OT 24,000 FEET AND SELECTED THE LEFT PACK OFF WHICH ELIMINATED THE FUEL ODOR. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED AN O-RING AT THE FUEL FLOW ELBOW ON THE AUXILIARY POWER UNIT. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LINE — LOOSE (APU FUEL SYS)

FLT 4628 - DURING TAKEOFF FROM VLV-ATL, A FUEL ODOR OCCURRED PRIMARILY IN THE COCKPIT WITH A SLIGHT ODOR IN THE GALLEY. THE ODOR DISSIPATED DURING FLIGHT AND REAPPEARED DURING LANDIING ROLL OUT. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE TIGHTENED A LEAKING FUEL LINE ON THE AUXILIARY POWER UNIT. OPERAIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)