N455SW
Registered owner: SKYWEST AIRLINES INC, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
141 reports on file, 2003-06-20 – 2024-08-06.
Part: GAUGE — FLUCTUATES (OIL PRESSURE) · airframe 41,483 hrs · 37,131 cycles
L ENG OIL PRESS MASTER WARNING AT CRUISE ALTITUDE. OIL PRESS GAUGE CYCLED IN AN OUT OF LOW PRESSURE. COMPLETED QRH, WITH ENG AT IDLE MASTER WARNING CONTINUED AND OIL PRESS GAUGE CONTINUED TO CYCLE IN AND OUT OF LOW PRESS INDICATION. DIVERTED TO KRAP. NO OTHER INDICATION OR ABNORMALITIES ON ENG 1. (FLIGHT 4663 - FILED CLOSED) PLEASE REFERENCE AML 1404605 PLEASE REFERENCE AML 1404617
Part: WINDOW FRAME — CRACKED (SEAT 13BC) · airframe 40,911 hrs · 36,532 cycles
CRACKED FRAME AROUND WINDOW BY SEAT 13BC: DEFERRED SEAT 13B WINDOW TRIM USING NEF-CAB-6D. SHARP EDGES COVERED WITH TAPE. NO FURTHER DISCREPANCIES FOUND. PLACARD PLACEDCAT: CDUE DATE: 11 APRIL 2024CRACKED FRAME AROUND WINDOW BY SEAT 13B (FILED CLOSED)REMOVED AND REPLACED WINDOW REVEAL BY SEAT 13B IN REF TO CMM 25-23-02. DMI CLEARED AND PLACARDS REMOVED
Part: FLOOR SUPPORT — DAMAGED (BS 349-449) · airframe 40,874 hrs · 36,494 cycles
NUTPLATE RIVET HOLES DAMAGED IN PRESSURE FLOOR SILL ASSEMBLY BETWEEN FS349.00 - FS449.85 AND LBL36.00 0 LBL45.00. (C-CHECK RO 3/24/2024) REPAIRED DAMAGE TO PRESSURE FLOOR SILL BETWEEN FS349.00 - FS449.85 AND LBL36.00 0 LBL45.00 IN REF TO REO 601R-53-41-3219,REV--, DATED 2024-03-14. COMPLETED TASK CARD 51-900-1003-SKY AND M-337.
Part: SKIN — DENTED (BS 640 S25R) · airframe 40,874 hrs · 36,494 cycles
2 SMALL DENTS WITH GOUGES/CREASES NOTED JUST AFT OF FS 640.00 AND ADJACENT TO STRINGER 25R. (C-CHECK RO 3/24/2024) REPAIRED DENT / GOUGE DAMAGE TO FUSELAGE SKIN BETWEEN FS621.00 - FS654.50 AND BETWEEN STR23R - STR26R IN REF TO REO 601R-53-61-8167 REV--, DATED 2024-03-10. COMPLETED TASK CARD 51-900-1003-SKY AND M-337.
Part: FLOOR SUPPORT — CORRODED (BS 435-559) · airframe 40,874 hrs · 36,494 cycles
SURFACE CORROSION FOUND AT SEVERAL FS LOCATIONS ON THE L/H PRESSURE FLOOR SILL ASSY ADJACENT TO LBL 36.00. LOCATIONS ARE AS FOLLOWS: FS 435, FS 439, FS 447, FS 451, 6 BETWEEN FS 473-FS 479, FS 500, FS 505, FS 522, FS 531, FS 537, FS 540, FS 544, FS 559 (C-CHECK RO 3/24/2024) BLENDED AND TREATED CORROSION DAMAGE ON THE LH PRESSURE FLOOR SIL ASSEMBLY BETWEEN FS424.00 - FS559.00 IN REF TO REO 601R-53-41-3218 REV--, DATED 2024-03-15. COMPLETED TASK CARD 51-900-1003-SKY AND M-337.
Part: BRACKET — CRACKED (BS 621 RBL36) · airframe 40,874 hrs · 36,494 cycles
AFT SIDE OF FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGER 15R, INTERCOSTAL CRACKED. (C-CHECK RO 3/24/2024) REMOVED AND REPLACED INTERCOSTAL ON THE AFT SIDE OF FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGER 15R IN REF TO SRM 51-42-21. COMPLETED 51-900-1003-SKY.
Part: ANGLE — CORRODED (PAX DOOR) · airframe 40,874 hrs · 36,494 cycles
FOUND CORROSION ON THE PAX DOOR ANGLE OF THE FUSELAGE PAX DOOR CUT OUT SURROUND STRUCTURE.-REF. SRM 53-21-23-00 PAGE 5 ITEM #56B PN: 601R31527-221 (C-CHECK RO 3/24/2024) REMOVED AND REPLACED PAX DOOR SILL ANGLE IN REF TO SRM 51-42-06 AND 51-42-21. APPLIED PRIMER / TOP COAT IN REF TO SRM 51-25-16. COMPLETED TASK CARD 51-900-1003-SKY AND M-337.
Part: PRESSURE BLKHD — GOUGED (BS 621) · airframe 40,874 hrs · 36,494 cycles
AFT PRESSURE BULKHEAD (FS621.00) FWD FACE HAS 6 GOUGES AND 7 GOUGED RIVET HEADS IN THE WEB DOUBLERS AT RBL 36.20, RBL 27.50, RBL 18.00, RBL9.50, LBL 9.50, LBL 18.00, LBL 27.50, AND LBL 36.20. (C-CHECK RO 3/24/2024) BLENDED 6 GOUGES AND REPLACED 7 GOUGED RIVETS IN THE WEB DOUBLERS AT RBL 36.20, RBL 27.50, RBL 18.00, RBL9.50, LBL 9.50, LBL 18.00, LBL 27.50, AND LBL 36.20 IN REF TO REO 601R-53-61-8168, REV--, DATED 2024-03-07. COMPLETED TASK CARD 51-900-1003.
Earlier reports · 2003–2022 · 133 reports
2022
Part: NONE — FAILED · airframe 40,419 hrs · 36,088 cycles
D:GEAR DISAGREE. NOSE GEAR WOULD NOT RETRACT. WOW INPUT CAUTION MESSAGE. STEERING INOP MESSAGE. LANDED OVER WEIGHT AT 49500 LBS TOUCH DOWN AT LESS THAN 100FT/MIN / C:MEL 32-30-1 / CAT A DUE WITHIN 1 FLIGHT DAY / NOTE:MX ACTION C/W / ***** REPEAT ODI **** REQUIRES MANAGEMMENT APPROVAL FOR RTS / GEAR DISAGREE. NOSE GEAR WOULD NOT RETRACT. WOW INPUT CAUTION MESSAGE. STEERING INOP MESSAGE. LANDED OVER WEIGHT AT 49500 LBS TOUCH DOWN AT LESS THAN 100FT/MIN (FLIGHT 5322 - FILED CLOSED) MAY 21, 2022 STATION: DEN-- PLEASE REFERENCE AML 911993 PLEASE REFERENCE AML 911995. DEFER LANDING GEAR RETRACTION SYSTEM PER CRJ 200 MEL 32-30-1 CAT II DOWNGRADED PLACARDS INSTALLED MX ACTION COMPLIED WITH GEAR PIN FLAGS ZIPTIED TO GEAR PIN RACK AUTHORIZED BY MCC.
Part: NONE — FAILED · airframe 40,419 hrs · 36,088 cycles
RECEIVED GEAR DISAGREE WARNING MESSAGE. BOTH MAINS RETRACTED BUT NOT THE NOSE GEAR. COMPLETED QRH PROCEDURE. LANDED BACK IN DEN WITHOUT ANY PROBLEMS. (FLIGHT 5111 - FILED CLOSED) PLEASE REFERENCE AML 911332 REMOVED AND REPLACED NLG SELECTOR VALVE PER AMM 32-33-10. PLEASE REFERENCE AML 911429 PLEASE REFERENCE AML 911430 PLEASE REFERENCE AML 911431 FOR OPS AND LEAK CHECKS A/C OK FOR SERVICE
2021
Part: HYDRAULIC SYSTEM — LEAKING · airframe 38,147 hrs · 34,065 cycles
UPON GEAR EXTENSION, GEAR DISAGREE WARNING MESSAGE AND HYD 3 LO PRESS CAUTION MESSAGE WITHIN 6 SECONDS. NOSE GREEN, MAINS YELLOW WITH XS. ATTEMPTED TO CYCLE GEAR WITHIN ABOUT 30 SECONDS, SAME RESULT. MANUALLY EXTENDED GEAR. THREE GREEN GEAR. HYD 3 SYSTEM SHOWED ZERO QUANTITY. DECLARED EMERGENCY AND LANDED AFTER COMPLETING QRH. DURING WALK-AROUND FOUND FLUID LEAK APPEARS TO BE FROM LEFT MAIN GEAR. NOT SURE HOW LONG HYD 3 PUMPS RAN DRY. PLEASE REFERENCE AML 554909. PLEASE REFERENCE AML 554971. PLEASE REFERENCE AML 554972 FOR REMOVAL AND REPLACEMENT OF HYD PUMP 3A AND 3B, LEAKING PRESSURE HOSES AND SWINGING OF LANDING GEAR AND OTHER WORK PERFORMED. AIRCRAFT GOOD FOR CONTINUED SERVICE AFTER WORK COMPLETED.
2019
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 36,486 hrs · 32,242 cycles
SPLICE STRAP AT STR 23R AND BETWEEN FS 310 AND FS 333 IS CORRODED. (C-CHECK) RO: 09/10/2019 COMPLIED WITH PERMANENT REPAIR IAW REO.
Part: FRAME — CORRODED (FUSELAGE) · airframe 36,486 hrs · 32,242 cycles
FRAME AT FS 310 , STR 23R CORRODED AT LOWER SPLICE. (C-CHECK) RO: 09/10/2019 REWORKED FRAME 310 AT STR 23 AND COMPLIED WITH ALL STEPS IAW REO. LEAK CHECKS GOOD.
Part: FRAME — CORRODED (FUSELAGE) · airframe 36,486 hrs · 32,242 cycles
FS 310 FRAME BETWEEN STR 26R- 26L CORRODED. (C-CHECK) RO: 09/10/2019 REWORKED 310 FRAME AND COMPLIED WITH ALL STEPS IAW REO. LEAK CHECKS GOOD.
Part: FRAME — CORRODED (FUSELAGE) · airframe 36,486 hrs · 32,242 cycles
FRAME AT FS319, STR23R CORRODED. (C-CHECK) RO: 09/10/2019 INSTALLED NEW FRAME SPLICE PN 601R32003-25 AT FS 310.0 & STRINGER 23R IAW SRM.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,486 hrs · 32,242 cycles
BL9R FLOOR BEAM INBOARD & OUTBOARD FLANGES HAVE CORROSION FS569.00 - FS608.00. (C-CHECK) RO: 09/10/2019 REMOVED AND REPLACED NEW FLOOR BEAM CAP IAW REO AND SRM.
Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 36,486 hrs · 32,242 cycles
BUTT STRAP AT FS 333 FROM STR 23L TO STR 23R PN#601R31022-9 CORRODED AT MULTIPLE LOCATIONS. (C-CHECK) RO: 09/10/2019 REMOVED AND INSTALLED NEW BUTT STRAP AT FS 333, BETWEEN STR 23L TO STR 23R IAW REO AND SRM.
Part: TRUNNION — DAMAGED (LT MLG) · airframe 36,486 hrs · 32,242 cycles
HOLE #14 LT MLG TRUNNION OVERSIZED AT .340". (C-CHECK) RO: 09/10/2019 COMPLIED WITH PERMANENT REPAIR HOLE #14 IAW REO.
Part: TRUNNION — DAMAGED (RT MLG) · airframe 36,486 hrs · 32,242 cycles
HOLE #14 ON RT MLG TRUNNION OVERSIZED AT .340". (C-CHECK) RO: 09/10/2019 REPAIRED RT TRUNNION HOLE #14 IAW REO.
Part: STRAP — CORRODED (FUSELAGE) · airframe 36,486 hrs · 32,242 cycles
CORROSION ON STRAP FS559.00, BL27L - BL42L. (C-CHECK) RO: 09/10/2019 REMOVED AND REPLACED STRAP P/N 601R31025-29 IAW AMM.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,486 hrs · 32,242 cycles
CORROSION ON THE INNER & OUTER FLANGES OF THE BL27L FLOORBEAM FS559.00+80 - FS569.00. (C-CHECK) RO: 09/10/2019 REPAIRED FLOORBEAM IAW SRM AND REO.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 36,486 hrs · 32,242 cycles
LEFT HAND FLOOR SILL MULTIPLE AREAS OF CORROSION, FS559.00+84 - FS562.00. (C-CHECK) RO: 09/10/2019 REPLACED LEFT FLOOR IAW REO.
Part: FRAME — CORRODED (FUSELAGE) · airframe 36,486 hrs · 32,242 cycles
FS 349 CORROSION ON FRAME BETWEEN STR 26L-27. (C-CHECK) RO: 09/10/2019 COMPLIED WITH STEPS OF PERMANENT REPAIR IAW REO.
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 36,486 hrs · 32,242 cycles
DOUBLER ON RIGHT FLOOR SILL CORRODED, FS310.00 - FS319.00. (C-CHECK) RO: 09/10/2019 INSTALLED NEW DOUBLER AT RT FLOOR SILL AT FS 310.00 - FS 319.00 IAW SRM.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 36,486 hrs · 32,242 cycles
RIGHT FLOOR SILL CORRODED, FS310.00 - FS319.00. (C-CHECK) RO: 09/10/2019 REMOVED AND INSTALLED NEW RT SILL PLATE AT FS310 TO FS319 IAW SRM.
Part: PIN — FAILED (NLG LOCK) · airframe 35,900 hrs · 31,569 cycles
RECEIVED GEAR DISAGREE WARNING MSG ON APPROACH. (FLT#7418) CLOSED REMOVED AND REPLACED NLG UP LOCK PIN AND BRACKET IAW AMM. PERFORMED OPS CHECK GOOD AT THIS TIME.
2017
Part: FRAME — CORRODED (BS 605) · airframe 33,071 hrs · 28,420 cycles
FRAME SECTOR AT BS 605 BETWEEN STRINGERS 20L AND 20R HAS OUT OF LIMITS CORROSION. REMOVED AND INSTALLED A NEW LOWER FRAME SECTOR IAW SRM. NO LEAKS NOTED.
Part: WEB — CORRODED (PAX DOOR) · airframe 33,071 hrs · 28,420 cycles
PAX DOOR AFT WEB HAS CORROSION. REMOVED AND REPLACED THE WEB IAW SRM. OPS TESTED GOOD.
Part: WEB — CORRODED (PAX DOOR STAIR) · airframe 33,071 hrs · 28,420 cycles
PAX DOOR FWD STAIR WEB HAS CORROSION. REMOVED AND REPLACED THE STAIR WEB IAW SRM. OPS TESTED GOOD.
Part: HINGE — GALLED (PAX DOOR) · airframe 33,071 hrs · 28,420 cycles
PAX DOOR FUSELAGE SIDE HINGE HAS GALLING BETWEEN EACH LUG. REMOVED AND INSTALLED NEW PASSENGER DOOR HINGE IAW SRM.
Part: ANGLE — BENT (PAX DOOR) · airframe 33,071 hrs · 28,420 cycles
PASSENGER DOOR BOTTOM ANGLE FOUND BENT. REPLACED THE BOTTOM ANGLE IAW SRM.
Part: DOOR — CHAFED (AFT CARGO) · airframe 33,071 hrs · 28,420 cycles
AFT CARGO DOOR LOWER SURROUND, HAS A DEEP CHAFE AND WEAR MARKS AT FWD SIDE. REMOVED AND INSTALLED A NEW UPPER AND UPPER DOOR COAMING IAW SRM. NO LEAKS NOTED.
2015
Part: FRAME — CORRODED (BS 319) · airframe 29,439 hrs · 24,581 cycles
AVIONICS BAY, FS 319.70, FRAME FLANGE HAS CORROSION AT STR 27. BELOW AVIONICS BAY FLOORBOARD. REPLACED LOWER FRAME AT FS 319 IAW SRM. LEAK CHECK GOOD.
Part: FRAME — CORRODED (BS 349) · airframe 29,439 hrs · 24,581 cycles
FS 349.0, AVIONICS BAY, FRAME FLANGE AT STR 27 HAS CORROSION. BELOW FLOORBOARD. REPLACED FS 349, FRAME FROM STR 23L-STR 23R WITH NEW FRAME AND INSTALLED NEW FRAME IAW SRM. LEAK CHECK GOOD.
2014
Part: WIRE HARNESS — FAILED (MLG) · airframe 27,635 hrs · 22,799 cycles
WOW INPUT CAUTION MESSAGE AFTER GEAR RETRACTION ALONG WITH LT OTBD BTMS INDICATOR DASHED. DURING GEAR EXTENSION, ANTI-SKID OTBD CAUTION MESSAGE AND PROX SYSTEM FAULT STATUS MESSAGE. R & R LT MLG OTBD HARNESS SUB ASSY, ANTI-SKID SUB HARNESS, AND ANTI SKID HARNESS. PERFORMED ANTI-SKID OPS CHECK. OPS CHECK GOOD IAW AMM. BTMS BRAKE TEMP ON NR 1 MLG WHEEL ASSY. OPS CHECK GOOD. ALL INDICATIONS NORMAL. WOW OPS CHECK GOOD IAW AMM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,330 hrs · 22,515 cycles
NR 3 EMERGENCY LIGHT POD IS INOPERATIVE. REPLACED THE LAMP.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,681 hrs · 21,898 cycles
EMERGENCY LIGHT AT PASSENGER INTERIOR WALL DOES NOT ILLUMINATE. REPLACED NR 2 EMERGENCY LIGHT BATTERY CHARGER IAW AMM.
2013
Part: PLATE — DAMAGED (TE FLAP) · airframe 25,875 hrs · 21,088 cycles
BLENDED AREA FOUND OUT OF LIMITS ON INBD SIDE PLATE ON RT INBD FLAP, INBD HINGE ARM. C-CHECK REPLACED INBD SIDE PLATE ON RT INBD FLAP ON INBD HINGE ARM IAW SRM.
Part: SILL — CORRODED (FUSELAGE) · airframe 25,875 hrs · 21,088 cycles
SERVICE DOOR LOWER SILL CORRODED IN SEVERAL AREAS, FOUR EACH WITH ONE LARGE PATCH OF CORROSION AROUND DOOR LUGS. C-CHECK REPLACED SERVICE DOOR LOWER SILL IAW SRM.
Part: SKIN — CHAFED (LT AILERON) · airframe 25,875 hrs · 21,088 cycles
LT AILERON UPPER LE CHAFED BEYOND ALLOWABLE LIMITS. C-CHECK REPLACED LT AILERON UPPER LE SKIN IAW SRM.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 25,875 hrs · 21,088 cycles
FLOOR AT FWD LT SIDE EQUIPMENT COMPARTMENT CRACKED AT FS193.0. C-CHECK REPAIRED FWD LT SIDE EQUIPMENT COMPARTMENT CRACKED AT FS 193 IAW REO.
Part: SKIN — CORRODED (LT WING) · airframe 25,875 hrs · 21,088 cycles
CORROSION ON LT WING, WING PLANK ON ACCESS 540BB. C-CHECK BLENDED WING PLANK ON ACCESS 540BB IAW REO.
Part: VANE — CHAFED (TE FLAP) · airframe 25,875 hrs · 21,088 cycles
LT INBD FLAP VANE CENTER LE IS CHAFED BEYOND LIMITS & NEEDS TO BE REPLACED. C-CHECK REPLACED WITH NEW LT INBD FLAP VANE CENTER LE, PN 601R14303-51S IAW SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 25,875 hrs · 21,088 cycles
FS 280 FLOOR BEAM WEB CRACKED AT RBL 9. C-CHECK REPAIRED FS 280 FLOOR BEAM WEB IAW REO.
Part: AILERON — CHAFED (RT WING) · airframe 25,875 hrs · 21,088 cycles
RT AILERON LE CHAFING WS. 312.50 TO 317.50. C-CHECK BLENDED CHAFING ON THE RT AILERON UPPER LE WS 312.5 TO 317.5 IAW REO.
Part: FITTING — CRACKED (FUSELAGE) · airframe 25,875 hrs · 21,088 cycles
FS 484 LBL 36 OTBD CLIP IS CRACKED AT RIVET HEAD. C-CHECK REPLACED FS 484 LBL 36 OTBD CLIP IAW REO.
Part: SKIN — CORRODED (FUSELAGE) · airframe 25,875 hrs · 21,088 cycles
AVIONICS BAY DOOR SURROUND HAS CORROSION AT FWD SECTION LT SIDE. C-CHECK REMOVED CORROSION FROM AVIONICS BAY DOOR CUTOUT INNER SKIN FWD SECTION LT SIDE IAW SRM & REO.
Part: AILERON — CHAFED (RT WING) · airframe 25,875 hrs · 21,088 cycles
RT AILERON, LE CHAFING WS 321.00 TO 331.00. C-CHECK BLENDED CHAFING ON THE RT AILERON UPPER LE WS 321 TO 331 IAW REO.
Part: SKIN — CHAFED (CARGO DOOR) · airframe 25,875 hrs · 21,088 cycles
AFT CARGO DOOR EXTERIOR SKIN HAS CHAFE MARK AT THE TOP CENTER AREA OF THE DOOR. C-CHECK BLENDED CHAFED AREA IAW REO.
Part: AILERON — CHAFED (RT WING) · airframe 25,875 hrs · 21,088 cycles
RT AILERON LE CHAFING FROM WS 343.50 TO 353.00. C-CHECK BLENDED CHAFING ON THE RT AILERON UPPER LE WS 343.50 TO 353.00 IAW REO.
Part: FITTING — CRACKED (FUSELAGE) · airframe 25,875 hrs · 21,088 cycles
FS 484 LBL 27 INBD CLIP CRACKED. C-CHECK REPLACED FS 484 LBL 27 INBD CLIP, PN 601R31171-17 IAW REO.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,875 hrs · 21,088 cycles
LT FS 202.0 BULKHEAD CRACKED AT THE PARKING BRAKE CABLE CUTOUT. C-CHECK REPAIRED LT FS 202.0 BULKHEAD CRACK AT THE PARKING BRAKE CUTOUT IAW REO.
Part: AILERON — CHAFED (RT WING) · airframe 25,875 hrs · 21,088 cycles
RT AILERON LE CHAFING WS 333.50 TO 343.50. C-CHECK BLENDED CHAFFING ON THE RT AILERON UPPER LE WS 333.50 TO 353.50 IAW REO.
Part: VANE — CHAFED (TE FLAP) · airframe 25,875 hrs · 21,088 cycles
LT INBD FLAP VANE HAS CHAFING ON INBD LE. C-CHECK BLENDED CHAFFING ON THE LT INBD FLAP VANE ON INBD LE IAW REO.
Part: VANE — CHAFED (TE FLAP) · airframe 25,875 hrs · 21,088 cycles
LT INBD FLAP VANE HAS CHAFING ON OTBD LE. C-CHECK REPLACED LT INBD FLAP VANE CAP PN 601R14303-43 IAW SRM.
Part: VANE — CHAFED (TE FLAP) · airframe 25,875 hrs · 21,088 cycles
LT INBD FLAP VANE HAS CHAFING ON MIDDLE OF LE. C-CHECK CHAFING ON THE LT INBD FLAP VANE CENTER LE SECTION WAS IAW REO.
Part: VANE — CHAFED (TE FLAP) · airframe 25,875 hrs · 21,088 cycles
RT INBD FLAP VANE HAS CHAFING ON OTBD LE. C-CHECK BLENDED CHAFING ON THE RT INBD FLAP VANE ON OTBD LE IAW REO.
Part: VANE — CHAFED (TE FLAP) · airframe 25,875 hrs · 21,088 cycles
RT INBD FLAP VANE HAS CHAFING IN MIDDLE OF LE. C-CHECK BLENDED CHAFING ON THE RT INBD FLAP VANE ON CENTER LE IAW REO.
Part: HINGE FITTING — CHAFED (AILERON) · airframe 25,875 hrs · 21,088 cycles
AILERON HINGE FITTING HAS EDGE CHAFING AT AILERON STATION 344.1665 OTBD HINGE FITTING LT SIDE. C-CHECK BLENDED OTBD HINGE FITTING EDGE TO A SMOOTH CONTOUR USING TYPE 1 REPAIR, SHEET 7 AT AILERON STATION 344.1665 PCU ATTACHMENT LUG IAW REO.
Part: VANE — CHAFED (TE FLAP) · airframe 25,875 hrs · 21,088 cycles
RT INBD FLAP VANE HAS CHAFING ON INBD LE. C-CHECK BLENDED CHAFFING ON THE RT INBD FLAP VANE ON INBD LE IAW REO.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,812 hrs · 21,032 cycles
EMERGENCY EXIT SIGN IN AISLE BURNED OUT. FLT#4815 REPLACED ELBP. PN 2013-1A, SN 113599, PN OFF AD-2013-1A & SN OFF 73196
Part: INVERTER — FAILED (CABIN) · airframe 25,779 hrs · 21,004 cycles
EXIT LIGHT BURNED OUT AT ROW 8. FLT#4460 REPLACED EMERGENCY LIGHTING INVERTER NR 1 IAW AMM. PN 5925-7
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,604 hrs · 20,835 cycles
FARTHEST AFT EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT#4676)RELAMPED.
Part: RESERVOIR — LOW (HYDRAULIC SYS) · airframe 25,448 hrs · 20,683 cycles
RECEIVED GEAR DISAGREE WHEN LANDING GEAR HANDLE WAS PUT DOWN. AFTER ONE MINUTE, RT MAIN CAME DOWN. FLT#7416 BLED AIR & SERVICED NR 3 RESERVOR AMM. PERFORMED SERVICES EXTENSION/RETRACTION OF LEADING GEAR & EMERGENCY FREEFALL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,448 hrs · 20,683 cycles
OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLT#4559 RELAMPED.
Part: BATTERY — DISCHARGED (CABIN) · airframe 25,373 hrs · 20,614 cycles
OVERHEAD CABIN EMERGENCY LIGHT DOES NOT ILLUMINATE. FLT#4606 BATTERY CHARGED & LIGHTS WORKED.
Part: SCREW — LOOSE (EMERGENCY LIGHT) · airframe 25,373 hrs · 20,614 cycles
MAIN CABIN DOOR EMERGENCY LIGHT DOES NOT ILLUMINATE. FLT#4811 TIGHTENED MOUNTING SCREWS & LIGHT ILLUMINATES.
Part: RESERVOIR — LEAKING (HYD SYSTEM) · airframe 25,300 hrs · 20,540 cycles
RECEIVED GEAR DISAGREE MASTER WARNING. RAN QRH. GEAR SHOWED THREE DOWN AND LOCKED AFTER FIRST CYCLE OF GEAR. RETURNED TO LAND WITH NO OTHER ISSUES. THE INITIAL GEAR THAT DIDN'T EXTEND WAS THE LT MAIN. REPLACED NR 3 HYD RESERVOIR DUE TO A LEAKING WEEP HOLE ON AFT SIDE OF RESERVOIR.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 25,195 hrs · 20,439 cycles
RIGHT FLOOD LIGHTS IN EMERGENCY EXIT SIGN ABOVE ROW 8 ARE BURNED OUT, RELAMPED.
Part: ACTUATOR — MALFUNCTIONED (RT MLG) · airframe 25,096 hrs · 20,329 cycles
A GEAR DISAGREE WARNING AND THE RIGHT MAIN GEAR WAS NOT DOWN, AFTER CYCLING THE LANDING GEAR, ALL THREE WERE DOWN AND LOCKED. LANDED WITHOUT INCIDENT. (FLT 4564) REPLACED RIGHT MLG SIDESTAY ACTUATOR IAW AMM. OPS CHECK GOOD. MANUAL GEAR RELEASE CHECKS GOOD IAW AMM. P/N: 17008-109 S/N: 01223 P/N OFF: 17008-115 S/N OFF: 01188 / P/N: 17014-3 S/N: 1698 S/N OFF: 1662 P/N: 17027-7 S/N: 7724 S/N OFF: 7194 P/N: 17028-3 S/N: 1238 S/N OFF: 1171
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,047 hrs · 20,279 cycles
PASSENGER DOOR FLOOR LEVEL EMERGENCY LIGHT BURNED OUT. (FLT 4546) RELAMPED EMERGENCY LIGHT.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 24,620 hrs · 19,839 cycles
WINDSHIELD CRACKED IN FLIGHT. (FLT 4765) REPLACED F/O'S WINDSHIELD IAW AMM. P/N: NP139321-14 S/N ON: 12347H9938 SN OFF: 07295H8489
2012
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,040 hrs · 19,257 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4634) RELAMPED EMERGENCY LIGHT.
Part: CONNECTOR — UNSECURE (SELECTOR VALVE) · airframe 23,978 hrs · 19,203 cycles
RECEIVED GEAR DISAGREE MESSAGE. (FLT 4460) FOUND CONNECTOR P5GA ON MLG SELECTOR VALVE NOT SECURED ALL THE WAY DUE TO THE SAFETY WIRE ON VALVE. ADJUSTED SAFETY WIRE AND SECURED CONNECTOR TO THE BAYONETS ON THE VALVE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,467 hrs · 18,720 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7812) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,409 hrs · 18,665 cycles
NR 2 AND NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4466) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,268 hrs · 18,533 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4750) RELAMPED EMERGENCY LIGHT.
Part: WHEEL — FAILED (NLG STEERING) · airframe 23,254 hrs · 18,521 cycles
WITH AIRCRAFT CENTERED ON THE RUNWAY THRUST WAS ADDED AND AIRCRAFT PULLED TO THE RIGHT. (FLT 7811) REPLACED STEERING HANDWHEEL IN REFERENCE TO MM. PN: 16650-101 SN OFF: DCL720/01
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,228 hrs · 18,499 cycles
TWO OVERWING EXTERIOR EMERGENCY LIGHTS ARE OUT, 1 ON THE LEFT SIDE AND 1 ON THE RIGHT SIDE. (FLT 4821) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,184 hrs · 18,454 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4788) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,046 hrs · 18,316 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: BUSHING — CORRODED (LT ENGINE) · airframe 22,655 hrs · 17,931 cycles
LEFT ENGINE FORWARD MOUNT LINK ASSEMBLY AND CLAMP UP BUSHING PITTED AND SCORED. INSTALLED SERVICEABLE LEFT ENGINE FORWARD MOUNT LINK ASSEMBLY AND CLAMP UP BUSHING.
Part: BUSHING — CORRODED (LT ENGINE) · airframe 22,655 hrs · 17,931 cycles
LEFT ENGINE AFT THRUST MOUNT SPHERICAL BUSHING PITTED. INSTALLED SERVICEABLE LEFT ENGINE AFT THRUST MOUNT SPHERICAL BUSHING.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,480 hrs · 17,771 cycles
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4764) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,451 hrs · 17,745 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4672) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,427 hrs · 17,725 cycles
RIGHT FORWARD OVERWING EMERGENCY LIGHT IS BURNED OUT. (FLT 4551) RELAMPED EMERGENCY LIGHT.
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,292 hrs · 17,607 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 4 IS OUT. (FLT 4531) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,247 hrs · 17,565 cycles
RIGHT EMERGENCY EXIT SIDE WALL EMERGENCY LIGHT HAS A BULB OUT. (FLT 4539) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,218 hrs · 17,541 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4666) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,114 hrs · 17,441 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4547) RELAMPED EMERGENCY LIGHT.
Part: VANE — CHAFED (TE FLAP) · airframe 22,247 hrs · 17,565 cycles
LEFT AND RIGHT INBOARD FLAP MIDDLE VANE LEADING EDGE CHAFED. (C-CHECK) REPAIRED PER SRM.
Part: VANE — CHAFED (TE FLAP) · airframe 23,046 hrs · 18,316 cycles
RIGHT INBOARD FLAP VANE INBOARD LEADING EDGE CHAFED. (C-CHECK) REPAIRED PER CRJ 200 SRM.
Part: VANE — CHAFED (TE FLAP) · airframe 23,046 hrs · 18,316 cycles
RIGHT INBOARD FLAP VANE OUTBOARD LEADING EDGE CHAFED. (C-CHECK) REPAIRED PER CRJ200 SRM.
Part: VANE — CHAFED (TE FLAP) · airframe 23,046 hrs · 18,316 cycles
RIGHT INBOARD FLAP VANE LEADING EDGE CHAFED, MID VANE. (C-CHECK) REPAIRED PER CRJ200 SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,139 hrs · 17,465 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4539) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,802 hrs · 17,153 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4559) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,670 hrs · 17,037 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4446) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,250 hrs · 16,659 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4779) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,212 hrs · 16,619 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4811) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,842 hrs · 16,311 cycles
NR 2 CEILING EMERGENCY LIGHT IS OUT. (FLT 4560) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,764 hrs · 16,248 cycles
RIGHT WING AFT EMERGENCY EXIT AND SERVICE DOOR LIGHTS ARE OUT. (FLT 4570) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,564 hrs · 16,078 cycles
AFT CEILING EMERGENCY LIGHT IS OUT. (FLT 4468) RELAMPED EMERGENCY LIGHT.
2010
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 20,187 hrs · 15,746 cycles
MIDDLE SECTION OF EXIT PATHWAY LIGHTING INOPERATIVE. (FLT 4884) REPLACED NR 3 EMERGENCY LIGHT BATTERY PACK.
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 20,187 hrs · 15,746 cycles
FORWARD FLOOR EMERGENCY LIGHT STRIP INOPERATIVE. (FLT 4854) RECONNECTED FLOOR LIGHT CONNECTION AT ROW 5.
Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 19,063 hrs · 14,751 cycles
FLOOR EMERGENCY ESCAPE PATH LIGHTING STRIP INOP. (FLT 4456) REPLACED CONNECTOR.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,204 hrs · 14,035 cycles
FIRST CEILING LEVEL EMERGENCY FLOODLIGHT INOP. (FLT 4629) RELAMPED EMERGENCY LIGHT.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,784 hrs · 13,691 cycles
RIGHT WING CENTER EMERGENCY EXIT LIGHT INOP. (FLT 4697) RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,726 hrs · 13,647 cycles
SECOND FROM AFT EMERGENCY LIGHT INOP. (FLT 4681)RELAMPED.
Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 17,898 hrs · 13,781 cycles
FS280 BULKHEAD GOUGED. (C CHECK)REPAIRED PER REO.
Part: CONNECTOR — LOOSE (CABIN) · airframe 17,260 hrs · 13,280 cycles
FLOOR LEVEL EMERGENCY LIGHTS INOP. (FLT 4421) RESEATED CONNECTOR.
2008
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 15,648 hrs · 12,055 cycles
FLT 4425 - CEILING LEVEL EMERGENCY FLOODLIGHT OVER ROW 2 INOP. RELAMPED.
Part: CARBON SEAL — LEAKING (LT ENGINE) · airframe 15,423 hrs · 11,873 cycles
FLT 3799 - AFTER TAKEOFF AIRCRAFT FILLED WITH SMOKE AND WE RECEIVED THE TOILET SMOKE CAUTION. FOUND NR 3 CARBON SEAL LEAK LEFT ENGINE. REPLACED ENGINE.
2007
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,510 hrs · 10,384 cycles
FLT 3994 - FLOOR EMERGENCY LIGHT IS INOP. REPLACED NR 3 ELBP INVERTER IAW MM 33-51-07. OPS CHECK GOOD.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 14,030 hrs · 10,772 cycles
FOUND AT C-CHECK, STA 280 RIGHT UPPER FLOORBEAM ANGLE IS CRACKED AT RBL9. COMPLIED WITH REPAIRS IAW REO 601-53-11-136.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 14,030 hrs · 10,772 cycles
FOUND AT C-CHECK, BS 280 AT LBL 9 LOWER FLOORBEAM IS CRACKED. COMPLIED WITH REPAIRS PER CRJ200 REO 601R-53-11-171.
Part: LIGHT — BROKEN (CABIN) · airframe 14,030 hrs · 10,772 cycles
FOUND AT C-CHECK, PASSENGER DOOR EMERGENCY EXIT BETA LIGHT IS BROKEN. REPLACED EMERGENCY EXIT BETA LIGHT PER CRJ200 AMM 33-51-09-400-801.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 14,030 hrs · 10,772 cycles
FOUND AT C-CHECK, FLOORBEAM IS CRACKED AT BS 280 AND LBL9. INSTALLED REPAIR PARTS IAW REO 601R-53-11-136.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 14,030 hrs · 10,772 cycles
FOUND AT C-CHECK, EMERGENCY TRACK LIGHTING CENTER SECTION IS INOP. SECURED CENTER SECTION LIGHT STRIP CONNECTOR PER CRJ WDM 31-51-00.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 14,030 hrs · 10,772 cycles
FOUND AT C-CHECK, FLOORBEAM STA 280 AND RBL9, LOWER FLOORBEAM IS CRACKED. COMPLIED WITH REPAIR PER REO 601R-53-11-1305 AND REO 601R-53-11-171.
Part: STRUCTURE — DAMAGED (RT WING) · airframe 13,235 hrs · 10,177 cycles
RIGHT WINGLET UPPER LEADING EDGE IS DAMAGED FROM BIRD STRIKE. INSTALLED NEW UPPER WINGLET LEADING EDGE IAW SRM 51-42-06.
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 11,902 hrs · 9,147 cycles
THIRD AND FOURTH OVERHEAD EMERGENCY FLOOD LIGHT IS INOP. REPLACED NR 3 ELBP WITH A SERVICEABLE UNIT. OPS CHECK GOOD.
Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 11,902 hrs · 9,147 cycles
AFT PORTION OF CENTER OVERHEAD EXIT LIGHT IS INOP. REPLACED BULB IN EXIT SIGN, OPS CHECKS GOOD.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 11,091 hrs · 8,578 cycles
CABIN EMERGENCY LIGHT INOP. RELAMPED OVERHEAD EMERGENCY LIGHT AT ROW 1. OPERATIONAL CHECKS GOOD.
Part: APU — ODOR · airframe 10,934 hrs · 8,473 cycles
ON CLIMB-OUT, BURNING SMELL IN COCKPIT AND CABIN FOLLOWED BY APU OVERTEMP MESSAGE AND SHUT DOWN. RETURNED TO FIELD. REPLACED APU ASSY IAW RII 49-310-1004 AND AMM 49-00-00. OPERATIONAL CHECKS GOOD.
2006
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 10,725 hrs · 8,324 cycles
FIRST OVERHEAD EMERGENCY LIGHT INOP. RELAMPED FIRST OVERHEAD EMERGENCY LIGHT WITH A NEW BULB. OPERATIONAL CHECKS GOOD.
Part: WINDOW — CRACKED (COCKPIT) · airframe 10,121 hrs · 7,865 cycles
LEFT COCKPIT SIDE WINDOW HAS A SMALL CRACK ON BOTTOM CORNER PART OF THE WINDOW. REPLACED LEFT COCKPIT SIDE WINDOW IAW CRJ MM 56-12-01 AND RII 56-220-1000, SN OFF: 2304H9217.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 9,484 hrs · 7,390 cycles
SMALL CRACK STARTING IN UPPER LEFT HAND CORNER OF CAPTAIN'S WINDSHIELD. REPLACED LEFT WINDSHIELD IAW CRJ 200 MM 56-11-01, AND RII 56-402. OPERATIONAL CHECKS GOOD, PN OFF NP-139321-003 SN OFF 02267H6510.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 9,026 hrs · 7,046 cycles
CEILING MOUNTED EMERGENCY LIGHT ABOVE ROW 2 DOES NOT ILLUMINATE. RELAMPED CEILING EMERGENCY FLOOD LIGHT AT ROW 2. OPERATIONAL CHECK GOOD.
Part: TRIM SWITCH — MALFUNCTIONED (COCKPIT) · airframe 8,378 hrs · 6,546 cycles
FO'S SIDE TRIM CONTROLS SWITCH STICKS TO ONE SIDE. REPLACED TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD IAW MM 27-40-00.
2005
Part: LIGHT — INOPERATIVE (ROW 5) · airframe 7,314 hrs · 5,747 cycles
EMERGENCY OVERHEAD POD AT ROW 5 IS OUT. REPLACED ROW 5 EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 7,002 hrs · 5,492 cycles
FWD CABIN CEILING EMERGENCY POD LIGHT BULB BURNED OUT. REPLACED BULB AT OVERHEAD EMERGENCY LIGHT IAW MM 33-00-00. OPERATIONAL CHECK GOOD.
Part: TRANSMITTER — MALFUNCTIONED (RUDDER CONTROL) · airframe 6,759 hrs · 5,300 cycles
ON PUSHBACK LOST RUDDER INDICATION ON EICAS. REPLACED RUDDER POSITION CONTROL TRANSMITTER IAW MM 27-24-05 OF THE MAINTENANCE MANUAL. OPERATIONAL CHECK GOOD.
Part: MANIFOLD — MALFUNCTIONED (GROUND SPOILER) · airframe 6,495 hrs · 5,086 cycles
INBOARD GROUND SPOILER FAULT STATUS MSG. REMOVED AND REPLACED INBOARD GROUND SPOILER MANIFOLD IAW AMM 27-63-05. OPERATIONAL CHECK GOOD.
Part: MANIFOLD — MALFUNCTIONED (GROUND SPOILER) · airframe 6,475 hrs · 5,072 cycles
INBOARD GROUND SPOILER FAULT ON TAXI IN. INSTALLED SERVICEABLE MANIFOLD ASSY FOR INBOARD GROUND SPOILERS. REPLACED SECU NR 1 AND NR 2 IAW MM 27-61-04. OPS CK GOOD. P/N OFF 49-164-06 S/N OFF 01786, 01787.
Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 6,379 hrs · 4,988 cycles
CARGO SMOKE WARNING ON GROUND IN SLC. REPLACED FWD & AFT SMOKE DETECTOR IAW 06-15-01. P/N 473597-19; S/N OFF 2274, S/N OFF 2275.
Part: SENSOR — MALFUNCTIONED (BRAKE POSITION) · airframe 5,483 hrs · 4,303 cycles
FLAPS FAIL MSG. REMOVED AND REPLACED BOTH LEFT AND RIGHT BPSU'S IAW MM CH 27-51-10. OPERATIONAL CHECK GOOD. P/N 855D100-11, S/N OFF 2019, 1944.
2004
Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 4,407 hrs · 3,444 cycles
FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED; FS 280.00, RBL 9.0 INBOARD AND OUTBOARD. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-25-16, AND 51-21-11.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 4,407 hrs · 3,444 cycles
CARGO PIT AFT BULKHEAD FLOOR ANGLE CRACKED; FS 621.00 RBL 38.0. ITEM FOUND AT C-CHECK INSPECTION. INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 REV "A".
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,407 hrs · 3,444 cycles
FUSELAGE PULLEY INTERCOSTAL HAS A CRACK ON OUTBOARD RETURN FLANGE; LEFT SIDE FS 484.00 LBL 36.0. ITEM FOUND AT C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601R-53-61-117. REV "B".
2003
Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 1,146 hrs · 915 cycles
STAB TRIM INDICATOR SHOWING ERRATIC INDICATIONS. REMOVED AND REPLACED HSTA IAW MM 27-40-00.
Part: GROUND WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 940 hrs · 749 cycles
EMERGENCY LIGHTS COME ON WITH SWITCH IN OFF POSITION AND AC POWER ON THE AIRCRAFT. FOUND GROUND STUD N1011 LOOSE. TIGHTENED GROUND STUD N1011, SYSTEM OPS CHECK GOOD.