N919SW
Registered owner: CORPORATE FLIGHT MANAGEMENT INC DBA, TN (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.
166 reports on file, 2004-02-03 – 2021-07-24.
Part: RETAINER — DAMAGED (CARGO DOOR SEAL) · airframe 46,212 hrs · 39,580 cycles
CARGO DOOR LOWER AFT SEAL RETAINER DAMAGED (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR LOWER AFT SEAL RETAINER IN REFERENCE TO CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY AND FORM M-337.
Part: TRACK — GOUGED (AFT CARGO DOOR) · airframe 46,212 hrs · 39,580 cycles
CARGO DOOR AFT TRACK GOUGED AT TOP. (FILED CLOSED) REMOVED AND REPLACED THE CARGO DOOR AFT TRACK IN REFERENCE WITH THE CRJ-200 SRM 51-42-06 AND 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY AND M-337.
Part: RETAINER — GOUGED (CARGO DOOR SEAL) · airframe 46,212 hrs · 39,580 cycles
CARGO DOOR UPPER AFT SEAL RETAINER GOUGED. (FILED CLOSED) REMOVED AND REPLACED THE UPPER AFT CARGO DOOR SEAL RETAINER IN REFERENCE TO CRJ 200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY AND M-337.
Part: DOOR FRAME — CORRODED (E/E BAY DOOR) · airframe 46,212 hrs · 39,580 cycles
AVIONICS DOOR LANDING HAS CORROSION AROUND WHOLE PERIMETER. (FILED CLOSED) REMOVED AVIONICS DOOR LANDING DOUBLER/PACKERS IN REF. TO SRM 51-42-06. FABRICATED REPLACEMENT DOUBLER/PACKERS AND INSTALLED PER REO 601R-53-21-26-31 REV "--" DATED 2015-06-23. COMPLETED TASK CARD 51-900-1003-SKY AND M-337.
Part: SERVICE DOOR — CORRODED · airframe 46,212 hrs · 39,580 cycles
SERVICE DOOR UNDERSIDE OF LOWER FORWARD AND AFT PAN CORRODED IN MULTIPLE LOCATIONS. REFER TO SRM 52-41-14 ITEM 2. (FILED CLOSED) REMOVED BOTTOM SERVICE DOOR FORWARD AND AFT SPIGOT FITTINGS, LOWER FORWARD AND AFT TRACK FITTINGS, ALONG WITH LOWER FORWARD AND AFT SERVICE DOOR SEAL RETAINERS WITH REFERENCE TO AMM 20-21-00, SRM 51-42-21 AND SRM 51-42-06. / BLENDED CORROSION FOUND ON SERVICE DOOR UNDERSIDE OF LOWER FORWARD AND AFT PAN IN REFERENCE TO SRM 51-21-06. LOWER FORWARD SERVICE DOOR PAN BLENDING FOUND TO BE WITHIN ACCEPTABLE LIMITS PER SRM 52-41-14 / SRM 52-00-00. APPLIED ALODINE, PRIMER, AND RESTORED TOPCOAT TO LOWER FORWARD SERVICE DOOR PAN WITH REFERENCE TO SRM 51-25-06 AND SRM 51-25-16. / SERVICE DOOR LOWER AFT PAN FOUND TO BE OUT OF LIMITS. REMOVED SERVICE DOOR LOWER AFT DOWNLOCK ROLLER AND ASSOCIATED BRACKETS WITH REFERENCE TO SRM 51-43-00 AND SRM 51-42-21. REMOVED AND REPLACED LOWER AFT SERVICE DOOR PAN WITH REFERENCE TO SRM 51-42-06, SRM 51-42-13, SRM 51-42-24, SRM 51-23-00, AND SRM 52-41-14. / INSTALLED LOWER FORWARD AND AFT SERVICE DOOR SEAL RETAINERS, LOWER FORWARD AND AFT DOOR SPIGOTS, AFT DOWNLOCK ROLLER, ALONG WITH
Part: ENGINE — POWER LOSS (NR 2) · airframe 45,506 hrs · 38,930 cycles
ON DEPARTURE, LOST POWER IN ENGINE 2. N2 VIB. COMPLIED WITH QRC AND QRH. RETURNED TO LAND FLIGHT 5431 - FILED CLOSED. INTERROGATED MDC. FOUND RT ENGINE TO HAVE HIGH N1 VIBE AND HIGH ITT. ITT WAS REPORTED THROUGH MDC TO BE 1076C FOR 3.7 SECONDS. PER AMM 71-00-00, RT ENGINE REQUIRES REPLACEMENT. PLEASE REFERENCE AML 571281 FOR REPLACEMENT OF THE RT ENGINE.
Earlier reports · 2004–2019 · 160 reports
2019
Part: VERTICAL BEAM — GOUGED (BS 621 BULKHEAD) · airframe 43,081 hrs · 36,816 cycles
AFT PRESSURE BULK HEAD AFT SIDE, VERTICAL BEAM BL0 GOUGED APROX 12 INCHES FROM TOP. LOCATED BEHIND CROSS BLEED VALVE. (C-CHECK) RO: 08/22/2019 PERFORMED ALL STEPS OF REPAIR IAW REO.
Part: ATTACH FITTING — WORN (LT WING TE FLAP) · airframe 43,081 hrs · 36,816 cycles
CENTER HINGE ARM ATTACH FITTING ON LH OTBD FLAP HAS WORN BOLT ATTACH POINTS. REMOVED AND INSTALLED LH OUTBOARD FLAP IAW AMM. OPERATIONAL TEST OF THE FLAPS GOOD. NO DEFECTS NOTED.
Part: ANGLE — CORRODED (BS 605) · airframe 43,081 hrs · 36,816 cycles
FS 605 LOWER FRAME REINFORCING ANGLE FOUND TO BE CORRODED. (C-CHECK) RO: 08/22/2019 REMOVED, REPLACED AND INSTALLED NEW FS605 LOWER FRAME REINFORCING ANGLE P/N 601R36026-35S IAW SRM AND REO.
Part: LONGERON — CORRODED (PAX DOOR) · airframe 43,081 hrs · 36,816 cycles
UPON REMOVAL OF THE PAX DOOR HINGE FOUND CORROSION ON PAX DOOR LOWER LONGERON PN 600-31528-9. (C-CHECK) RO: 08/22/2019 REMOVED CORROSION ON PAX DOOR LOWER LONGERON, VERIFIED ALL REPAIR STEPS WERE COMPLIED WITH IAW REO. LEAK CHECK GOOD.
Part: FRAME — CRACKED (BS 333) · airframe 43,081 hrs · 36,816 cycles
FRAME FS333.00 CRACKED BETWEEN STR0 AND LH STR1. (C-CHECK) RO: 08/22/2019 REPAIRED FRAME FS333.00 BETWEEN STRG 0 TO STGR 2L IAW REO AND SRM. LEAK CHECK GOOD.
Part: DOOR FRAME — CORRODED (BS 349) · airframe 43,081 hrs · 36,816 cycles
DOUBLER ATTACHED PASSENGER DOOR FRAME FS 349.00 AT FLOOR LEVEL HAS CORROSION ON I/B SIDE AT TOP. (C-CHECK) RO: 08/22/2019 COMPLETED ALL STEPS OF REPAIR IAW REO.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 43,081 hrs · 36,816 cycles
FOUND CORROSION AT PAX DOOR LOWER MID INTERCOSTAL DD6 P/N 601R318057-1. (C-CHECK) RO: 08/22/2019 REMOVED AND INSTALLED NEW INTERCOSTAL IAW SRM. LEAK CHECK GOOD.
Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 43,081 hrs · 36,816 cycles
R/H FLOOR SILL HAS SPOTS OF CORROSION FROM APPROX. 409+100 TO 409+128. (C-CHECK) RO: 08/22/2019 REPAIRED RH FLOOR SILL IAW SRM AND REO.
Part: FRAME — CORRODED (BS 310) · airframe 43,081 hrs · 36,816 cycles
FRAME AT FS310 IS CORRODED BETWEEN STR25L & STR22R. (C-CHECK) RO: 08/22/2019 REMOVED AND INSTALLED NEW LOWER FRAME SECTION P/N 601R32002-69 AT FS 310 IAW SRM. LEAK CHECK GOOD.
Part: HINGE — DAMAGED (PAX DOOR) · airframe 43,081 hrs · 36,816 cycles
PASSENGER DOOR - PIANO HINGE HALF ON FUSELAGE SIDE , HINGE PIN HOLES ARE ELONGATED. (C-CHECK) RO: 08/22/2019 REMOVED AND INSTALLED NEW PAX DOOR PIANO HINGE ON THE FUSELAGE SIDE IAW SRM AND REO. LEAK CHECK GOOD.
Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 43,081 hrs · 36,816 cycles
CORROSION FOUND ON R/H FLOOR BEAM CAP AT RBL9 FROM APPROX FS559+48 TO 559+112. (C-CHECK) RO: 08/22/2019 REPLACED RH FLOOR BEAM CAP AT RBL9 FROM APPROX. FS559+48 TO FS559+112 IAW REO.
Part: FLOOR SUPPORT — CORRODED (BS 559-569) · airframe 43,081 hrs · 36,816 cycles
CORROSION FOUND ON L/H FLOOR SILL FROM APPROX FS559+86 TO FS569. REPAIRED CORROSION AT LH FLOOR SILL FROM APPROX. FS559+86 TO FS569 AND FS559+95 TO FS559+104 IAW REO.
Part: FLOOR SUPPORT — CORRODED (BS 569-621) · airframe 43,081 hrs · 36,816 cycles
CORROSION FOUND ON L/H FLOOR BEAM CAP AT LBL27 FROM APPROX FS569 TO FS621. (C-CHECK) RO: 08/22/2019 PERFORMED REPAIR ON LH FLOOR BEAM CAP AT LBL27 AT APPROX. FS569 TO FS621 IAW REO.
Part: PRESSURE DECK — CRACKED (BS 461) · airframe 43,081 hrs · 36,816 cycles
PRESSURE FLOOR SKIN HAS 2 CRACKS AT FS461, BL0 TO RBL9. (C-CHECK) RO: 08/22/2019 PERFORMED PRESSURE FLOOR SKIN REPAIR AT FS461, BL0 TO RBL9, IAW REO. LEAK CHECK GOOD.
Part: FLOOR SUPPORT — DENTED (BS 503) · airframe 43,081 hrs · 36,816 cycles
R/H PRESSURE FLOOR SILL PANEL HAS A DENT WITH CREASE AT APPROX. FS503, RBL45. (C-CHECK) RO: 08/22/2019 PERFORMED REPAIR TO DENTED AREA IAW REO. LEAK CHECK GOOD.
Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 43,081 hrs · 36,816 cycles
L/H PRESSURE FLOOR ANGLE BETWEEN APPROX FS 409.00 + 128 THRU APPROX FS 559.00 HAS AREAS OF CORROSION. (C-CHECK) RO: 08/22/2019 BLENDED OUT CORROSION ON L/H PRESSURE FLOOR ANGLE BETWEEN APPROX FS 409.00 + 128 THRU APPROX FS 559.00 IAW REO. LEAK CHECK GOOD.
2017
Part: SELECTOR VALVE — FAILED (NLG) · airframe 39,304 hrs · 33,438 cycles
DURING APPROACH, SELECTED LANDING GEAR DOWN AND RECEIVED A GEAR DISAGREE WARNING. COMPLIED WITH QRH AND PERFORMED MANUAL FREEFALL OF LANDING GEAR FOLLOWED BY THREE DOWN AND GREEN INDICATIONS. REMOVED AND REPLACED THE NOSE LANDING GEAR DOOR SELECTOR VALVE AND THE NLG GEAR SELECTOR VALVE IAW AMM. SWUNG GEAR. SYSTEM OPS CHECKED GOOD.
Part: TARGET — LOOSE (LT MLG) · airframe 38,876 hrs · 32,999 cycles
AIRCRAFT RETURNED TO THE FIELD DUE TO A LEFT MAIN GEAR NOT RETRACTED. GEAR DISAGREE MESSAGE. SECURED THE LT MLG UPLOCK PROXIMITY SENSOR TARGET & REPLACED LT MLG SIDE STAY ACTUATOR. OPS & LEAK CHECKED GOOD.
Part: ANGLE — DAMAGED (BS 574) · airframe 38,686 hrs · 32,828 cycles
FOUND ANGLE AT BS 574 DAMAGED. REMOVED, AND REPLACED THE ANGLE IAW SNIEO AND SRM.
Part: SKIN — DENTED (BS 672.2) · airframe 38,686 hrs · 32,828 cycles
PROTRUDING DENT 2 INCHES AFT OF BS 672.2 BETWEEN STRINGERS 250R AND 26R, APPROXIMATELY .004 DEEP. REPAIRED IAW REO.
Part: SKIN — DENTED (BS 672.5) · airframe 38,686 hrs · 32,828 cycles
PROTRUDING DENT 5 INCHES FWD OF BS 672.5 BETWEEN STRINGERS 26 AND 27L APPROXINATELY .014 DEEP. REPAIRED THE DENT IAW REO.
Part: BULKHEAD — DAMAGED (BS 621) · airframe 38,686 hrs · 32,828 cycles
BS 621 BULKHEAD BELOW FLOOR, BACKSIDE DOUBLERS AT RBL 9.50, , LBL 9.50 , LBL 18.0 AND BL 0.0 DAMAGED. REPAIRED THE BULKHEAD IAW REO.
Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 38,686 hrs · 32,828 cycles
REAR PRESSURE BULKHEAD WEB HAS 9 AREAS WITH MULTIPLE CRACK INDICATIONS NOTED. ALL 9 AREAS FAILED NDT. REPAIRED THE REAR PRESSURE BULKHEAD WEB IAW SRM.
Part: SKIN — DENTED (BS 589-605) · airframe 38,686 hrs · 32,828 cycles
MULTIPLE DENTS AFT OF GROUND AC DOOR BS 589 - 605. REPAIRED THE DENTS IAW REO.
Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 38,655 hrs · 32,807 cycles
APPROXIMATELY 10,000FT MSL LOST CABIN PRESSURIZATION, BEGAN DESCENT @ 11700 TO 10000FT NO INDICATIONS ON ECS PAGE OF ABNORMAL CONDITIONS, DOOR PAGE NORMAL. (FLT#5445) FO: 06/22/2017 CLOSED REMOVED AND REPLACED THE THROTTLE QUADRANT IAW AMM AND THE OUTFLOW VALVE PNEUMATIC LINES WERE DISCONNECTED AND RE-INSTALLED. AIRCRAFT PRESSURIZATION SYSTEM OPS CHECK GOOD IAW AMM. NO FURTHER DEFECTS NOTED.
Part: HOSE — LEAKING (HYD SYSTEM) · airframe 38,138 hrs · 32,367 cycles
NR 2 HYD LOW PRESSURE MESSAGE DURING CLIMB OUT, RETURNED TO FIELD. REMOVED AND REPLACED INBD GROUND RETRACT HOSE ASSY.
2016
Part: ADC — MALFUNCTIONED (NR 1) · airframe 36,055 hrs · 30,467 cycles
DIVERTED DUE TO AN EFIS COMP MON WITH ASSOCIATED IAS FLAG ON THE NR 1 PFD. THE MACH TRIM AND A/P DISCONNECTED. CREW DECLARED AN EMERGENCY. R & R NR 1 ADC IAW AMM. OPS CHECK AND LEAK CHECKED IAW AMM.
Part: LANDING GEAR — SLOW · airframe 35,920 hrs · 30,349 cycles
EMERGENCY DECLARED HYD 3B LOW PRESSURE WHEN SELECTING GEAR DOWN, GEAR DISAGREE MSG AND NOSE GEAR DOOR WARNING. AFTER SECOND ATTEMPT GEAR DID COME DOWN AND LOCKED. PERFORMED EXTENSION AND RETRACTION OF THE NLG AND MLG IAW AMM. OPS CHECK GOOD. FLAP SYSTEM OPS CHECK GOOD IAW AMM. VISUAL INSPECTION OF GEAR DOORS AND FLAPS, NO DAMAGE NOTED.
2015
Part: SELECTOR VALVE — FAILED (MLG) · airframe 34,769 hrs · 29,368 cycles
GEAR DISAGREE ON GEAR EXTENSION. GEAR WOULD NOT COME DOWN. CREW HAD TO MANUALLY EXTEND THE GEAR. R & R MLG SELECTOR VALVE. OPS GOOD.
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 34,052 hrs · 28,736 cycles
CENTER CAP OF LT INBD FLAP VANE CHAFED. R & R THE LT INBD FLAP MOVEABLE VANE CENTER CAP IAW SRM AND STS EA.
2014
Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 32,544 hrs · 27,404 cycles
"EXIT" SIGNS AT BULKHEAD & GALLEY SERVICE DOOR DO NOT ILLUMINATE. REMOVED BATTERY AND REINSTALLED. OPS CHECKED GOOD.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,473 hrs · 26,512 cycles
FLOOR LEVEL FLOOD LIGHT AT HAS ONE LAMP INOPERATIVE.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,490 hrs · 26,524 cycles
FLOOR LEVEL FLOOD LIGHT AT MAIN CABIN DOOR HAS ONE LAMP INOPERATIVE. REPLACED THE LAMP IAW AMM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,310 hrs · 26,394 cycles
RIGHT FUSELAGE AFT EXTERIOR EMERGENCY LIGHT IS INOPERATIVE, REPLACED THE LAMP.
Part: SKIN — DENTED (FUSELAGE) · airframe 31,310 hrs · 26,394 cycles
AFT LOWER CORNER OF BAGGAGE BAY DOOR CUTOUT IS DENTED IN AND OUT OF LIMITS IAW SRM. CUT-OUT DAMAGE, FABRICATED DOUBLERS AND LOCATED FASTENER HOLES, PERFORMED FINAL CUT ON 3 DOUBLERS AND COUNTERSUNK FASTENER HOLES. INSTALLED SEALANT AND DOUBLERS AND COMPLETED INSTALLATION OF REPAIR IAW REO AND SRM.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 31,310 hrs · 26,394 cycles
NR 2 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. REPLACED THE LAMP IAW AMM.
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 31,278 hrs · 26,362 cycles
MAIN CABIN DOOR EMERGENCY LIGHT DOES NOT ILLUMINATE. SECURED CONNECTOR TO FWD DOOR EMERGENCY LIGHT INDICATION SIGN AT FLOOR LEVEL.
Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 30,872 hrs · 26,066 cycles
EMERGENCY EXIT SIGNS NEAR MAIN CABIN DOOR AND SERVICE DOOR DO NOT ILLUMINATE. CYCLED POWER OF EMERGENCY LIGHT INVERTER IAW AMM.
Part: HOLDER — FAULTY (CABIN) · airframe 30,499 hrs · 25,784 cycles
SEVERAL SIDEWALL LIGHTS ARCING. FLT 5407 REPLACED FAULTY SIDEWALL LIGHT HOLDER IAW AMM.
2013
Part: RESERVOIR — FAULTY (HYDRAULIC SYS) · airframe 30,217 hrs · 25,577 cycles
GEAR DISAGREE, GEAR RETRACTED AFTER ABOUT 15 SECONDS. FLT 5382 REPLACED NR 3 HYDRAULIC SYSTEM RESERVOIR IAW AMM, PN 7303-1, SN 1063A & SN OFF 1044A.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,144 hrs · 25,515 cycles
THE NR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. REPLACED LAMP.
Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 3) · airframe 30,109 hrs · 25,492 cycles
RECEIVED HYD 3 LOW PRESS CAUTION MESSAGE FOLLOWED BY A GEAR DISAGREE & NOSE DOOR OPEN WARNING. MESSAGES THE GEAR DID COME UP & ALL MESSAGES CLEARED. ENROUTE HYDRAULIC 3 SYSTEM PRESSURE READ 100% CONTINUOUSLY UNTIL THE GEAR WAS LOWERED. NO ISSUES WITH LOWERING THE LANDING GEAR, SYSTEM OPERATED NORMALLY. FLT 5361 BLEED & INSPECTED NR 3 SYS HYD IAW AMM. JACKED AIRCRAFT & COMPLIED WITH GEAR SWINGS FOLLOWED BY A FREEFALL CHECK. ALL OPERATIONS CHECKED GOOD.
Part: ANTI-ICE VALVE — FAULTY (LT WING) · airframe 30,081 hrs · 25,471 cycles
WING ANTI-ICE CAUTION MESSAGE APPEARED, THEN COCKPIT & CABIN FILLED WITH SMOKE. SMOKE DISSIPATED WHEN THE WING ANTI-ICE WAS TURNED OFF. FLT 5246 REPLACED LT WING ANTI-ICE VLV IAW AMM, PN 3214442-4 SN ON 2923 SN OFF 2558.
Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 3) · airframe 30,016 hrs · 25,405 cycles
RECEIVED HYD 3A LOW PRESSURE MESSAGE FOLLOWED BY GEAR DISAGREE MESSAGE. MESSAGES CLEARED AFTER AN EXTENDED GEAR RETRACTION. FLT5241 BLEED NR 3 HYD SYSTEM AS REQUIRED IAW AMM. SWING GEAR SEVERAL TIMES INCLUDING FREE FALL, NO MESSAGES NOTED. OPERATIONS CHECKED GOOD.
Part: SKIN PANEL — DENTED (RT WING) · airframe 29,903 hrs · 25,317 cycles
RT WING CENTER LE PANEL 630JL DENTED. C-CHECK REPLACED RT WING LE PANEL 630JL SKIN WITH SERVICEABLE SKIN PN 601R12057-4 IAW SRM.
Part: VANE — CHAFED (TE FLAP) · airframe 29,903 hrs · 25,317 cycles
LT INBD FLAP VANE LE CHAFED ON OTBD SIDE. C-CHECK LT INBD FLAP VANE LE CHAFE ON OTBD SIDE WAS BLENDED, NDT & FINISH RESTORED IAW REO.
Part: VANE — CHAFED (TE FLAP) · airframe 29,903 hrs · 25,317 cycles
RT INBD FLAP VANE LE CHAFED ON INBD SIDE. C-CHECK RT INBD FLAP VANE LE CHAFE ON INBD SIDE WAS BLENDED, NDT & FINISH RESTORED IAW REO.
Part: VANE — CHAFED (TE FLAP) · airframe 29,903 hrs · 25,317 cycles
RT INBD FLAP VANE LE CHAFED ON MID AREA. C-CHECK RT INBD FLAP VANE LE CHAFE ON MID AREA WAS BLENDED, NDT & FINISH RESTORED IAW REO.
Part: VANE — CHAFED (TE FLAP) · airframe 29,903 hrs · 25,317 cycles
RT INBD FLAP VANE LE CHAFED ON OTBD SIDE. C-CHECK RT INBD FLAP VANE LE CHAFE ON OTBD SIDE WAS BLENDED, NDT & FINISH RESTORED IAW REO.
Part: VANE — CHAFED (TE FLAP) · airframe 29,903 hrs · 25,317 cycles
LT INBD FLAP VANE LE CHAFED ON INBD SIDE. C-CHECK LT INBD FLAP VANE LE CHAFE ON INBD SIDE WAS BLENDED, NDT & FINISH RESTORED IAW REO.
Part: VANE — CHAFED (TE FLAP) · airframe 29,903 hrs · 25,317 cycles
LT INBD FLAP VANE LE CHAFED ON MID AREA. C-CHECK LT INBD FLAP VANE LE CHAFE ON MID AREA WAS BLENDED, NDT & FINISH RESTORED IAW REO.
Part: AILERON — CHAFED (RT WING) · airframe 29,903 hrs · 25,317 cycles
RT AILERON UPPER LE FOUND TO BE CHAFED OUT OF LIMITS. C-CHECK R & R RT AILERON UPPER LE IAW SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,903 hrs · 25,317 cycles
621 BULKHEAD SPLICE WEB AT BL 0.00 WL 139.50-137.50 CRACK INDICATION NOTED. C-CHECK REPAIRED 621 BULKHEAD SPLICE WEB AT BL 0.00, WL 139.50-137.50 IAW REO.
Part: PANEL — CHAFED (RT AILERON) · airframe 29,903 hrs · 25,317 cycles
RT AILERON PANEL 699BB ON LOWER LE IS CHAFED THROUGH PAINT FROM CONTACT WITH RUB SEAL. C-CHECK BLENDED OUT CHAFE IAW REO.
Part: LUG — CHAFED (RT AILERON) · airframe 29,903 hrs · 25,317 cycles
RT AILERON OTBD PCU LINK LUG IS CHAFED ON LOWER SIDE. C-CHECK REPAIRED CHAFED DAMAGE ON RT AILERON OTBD PCU LINK LUG IAW REO.
Part: CONNECTOR — UNSECURE (CABIN) · airframe 29,807 hrs · 25,247 cycles
AFT PORTION OF FLOOR LEVEL EMERGENCY LIGHT STRIP DOES NOT ILLUMINATE. FLT#6203 SECURED AFT LIGHTING STRIP PLUG. OPERATIONS CHECKED GOOD.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,572 hrs · 25,059 cycles
SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT BURNED OUT. FLT#6420 RELAMPED.
Part: BATTERY — DISCHARGED (CABIN) · airframe 29,461 hrs · 24,966 cycles
LT MIDDLE EMERGENCY EXIT LIGHT BURNED OUT. MIDDLE EMERGENCY EXIT LIGHT BURNED OUT. FLT#6236 REPLACED LT MIDDLE EMERGENCY BATTERY. PN AD-2013-1A , SN 64276 & SN OFF 40201
Part: COVER — UNSECURE (CABIN) · airframe 29,449 hrs · 24,950 cycles
EXIT ROW LIGHT COVER FELL OFF. FLT#5230 REPLACED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,818 hrs · 24,457 cycles
OVERHEAD EMERGENCY LIGHT IS OUT ABOVE ROW 8. RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,263 hrs · 23,999 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. (FLT 5514) RELAMPED EMERGENCY LIGHT.
Part: COOLING FAN — FAILED (E&E BAY) · airframe 27,988 hrs · 23,783 cycles
COOL EXHAUST FAIL STATUS MESSAGE ILLUMINATED, CIRCUIT BREAKER POPPED AND AN ACRID AROMA WAS NOTICED. (FLT 6537) REPLACED AVIONIC COOLING FAN IAW AMM. P/N: AE1410CA1 S/N ON: 00719 S/N OFF: L0125
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,739 hrs · 23,604 cycles
LEFT WING AFT EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 5592) RELAMPED EMERGENCY LIGHT.
2012
Part: BALLAST — INOPERATIVE (LAVATORY) · airframe 27,272 hrs · 23,230 cycles
LAVATORY LIGHT BALLAST BURNED OUT. (FLT 6227) REPLACED BALLAST.
Part: SIGN — INOPERATIVE (CABIN) · airframe 26,663 hrs · 22,769 cycles
EMERGENCY EXIT SIGN NEXT TO MAIN CABIN DOOR IS INOPERATIVE. LIGHT DOES NOT ILLUMINATE. (FLT 5631) REPLACED EMERGENCY EXIT SIGN IN REFERENCE TO AMM.
Part: WIRE — UNSECURE (CABIN) · airframe 26,607 hrs · 22,723 cycles
LOWER EMERGENCY LIGHT ON LEFT SIDE OF GALLEY IS OUT. (FLT 5387) RE-SECURED WIRES TO LIGHT ASSEMBLY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,285 hrs · 22,493 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6306) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,176 hrs · 22,415 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5583) RELAMPED EMERGENCY LIGHT.
Part: DRAIN MAST — OVERHEATED (POTABLE WATER) · airframe 25,915 hrs · 22,199 cycles
AFT POTABLE WATER DRAIN MAST WAS OVERHEATING AND CAUSING BURNING SMELL AROUND CARGO AREA. (FLT 6407) REPLACED AFT POTABLE WATER DRAIN MAST IN REFERENCE TO AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,808 hrs · 22,114 cycles
NR 3 OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT# 5377) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,340 hrs · 21,756 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6416) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,100 hrs · 21,565 cycles
RIGHT AFT EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 5226) RELAMPED EMERGENCY LIGHT.
2011
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,374 hrs · 20,943 cycles
FLOOR LEVEL EMERGENCY LIGHT STRIP FROM ROW 6 FORWARD ARE OUT. (FLT 6523) REPLACED NR 2 EMERGENCY LIGHT BATTERY PACK. P/N OFF: 2013-1A S/N OFF: 83163.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,251 hrs · 20,842 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6420) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,081 hrs · 20,710 cycles
LOWER EMERGENCY EXIT SIGN AT LEFT EMERGENCY EXIT NOT ILLUMINATING. (FLT 6235) INSTALLED SERVICEABLE ORDINANCE EXIT LIGHT AND FORWARD FLOOR LIGHTING POWER STRIP.
Part: INVERTER — INOPERATIVE (CABIN) · airframe 23,755 hrs · 20,454 cycles
EMERGENCY LIGHT AT LEFT EXIT ROW NOT WORKING. (FLT 5615) REPLACED NR 2 INVERTER.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,627 hrs · 20,342 cycles
RIGHT FORWARD EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 6439) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,983 hrs · 19,804 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. (FLT 6400) RELAMPED EMERGENCY LIGHT.
Part: CONNECTOR — DIRTY (CABIN) · airframe 22,884 hrs · 19,724 cycles
LEFT SIDE FORWARD FLOOR EMERGENCY LIGHTS ARE OUT. (FLT 6581) CLEANED CONNECTOR ON FORWARD FLOOR LEVEL STRIP LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,575 hrs · 19,468 cycles
LEFT AFT EMERGENCY LIGHT IS OUT. (FLT 5807) RELAMPED EMERGENCY LIGHT.
Part: SWITCH — DIRTY (CABIN DOOR) · airframe 22,327 hrs · 19,257 cycles
MCD WOULD NOT OPEN UPON ARRIVAL. (FLT 6927) CLEANED DOOR ASSIST PUSHBUTTON SWITCH OF GRIT AND GRIME.
2010
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,143 hrs · 19,096 cycles
NR 3 OVERHEAD EMERGENCY LIGHT OUT. (FLT 6533) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,126 hrs · 19,084 cycles
NR 2 CEILING EMERGENCY LIGHT INOP. (FLT 6767) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,928 hrs · 18,038 cycles
NR 2 OVERHEAD EMERGENCY LIGHT INOP. (FLT 6271) RELAMPED EMERGENCY LIGHT.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 20,777 hrs · 17,904 cycles
FS 280 FLOOR MEMBER CRACKED AT LBL 9.0. (C CHECK) REPAIRING PER REO.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,777 hrs · 17,904 cycles
FS 559 PRESSURE BULKHEAD CRACKED AT CAP ANGLE RADIUS. (C CHECK) REPAIRED PER REO.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,182 hrs · 18,265 cycles
PRESSURE BULKHEAD CRACKED AT FS 559.0. (C-CHECK) REPAIRED PER REO.
Part: HINGE — CRACKED (DOOR STEP) · airframe 21,182 hrs · 18,265 cycles
CRACKED HINGE AT DOOR STEP 832FT. (C-CHECK) REPAIRED PER SRM.
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 21,182 hrs · 18,265 cycles
CORRODED STRUCTURE AT FS 559+112 TO FS 605.0. REMOVED CORROSION PER SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,182 hrs · 18,265 cycles
BULKHEAD CRACKED AT FS 621. (C-CHECK) REPAIRED PER REO.
Part: BULKHEAD — CRACKED · airframe 19,750 hrs · 17,025 cycles
SVC CHECK, FORWARD PRESSURE BULKHEAD CRACKED AT EMERGENCY BRAKE CABLE ACCESS PORT. REPAIRED PER REO.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,303 hrs · 16,681 cycles
OVERHEAD EMERGENCY FLOOD LIGHT INOP. (FLT 6485) RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,174 hrs · 16,571 cycles
TWO EMERGENCY EXTERIOR LIGHTS INOP. (FLT 5990) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,895 hrs · 16,344 cycles
LEFT WING AFT EMERGENCY EXIT LIGHT INOP. (FLT 6640) RELAMPED EMERGENCY LIGHT.
Part: WIRE HARNESS — FAULTY (NLG) · airframe 18,072 hrs · 15,708 cycles
GEAR DISAGREE MESSAGE ON GEAR RETRACTION. (FLT 6664) REPLACED NR 1 NLG DOWNLOCK HARNESS AND SENSOR.
Part: PRIORITY VALVE — FAILED (NLG) · airframe 17,919 hrs · 15,583 cycles
FLT 6546 - GEAR DISAGREE WARNING DISPLAYED. REPLACED NLG PRIORITY VALVE.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 17,919 hrs · 15,583 cycles
FLT 6025 - OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED.
Part: HANDLE — BINDING (CARGO DOOR) · airframe 17,522 hrs · 15,254 cycles
FLT 6164 - MCD DIFFICULT TO OPEN. LUBRICATED MAIN CABIN DOOR INNER HANDLE ASSEMBLY.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,486 hrs · 15,225 cycles
FLT 5859 - CEILING EMERGENCY LIGHT. RELAMPED.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,312 hrs · 15,091 cycles
FLT 5877 - MCD EMERGENCY EXIT SIGN INOP. RELAMPED.
2008
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 16,412 hrs · 14,371 cycles
FLT 6717 - NR 2 CEILING LEVEL EMERGENCY FLOODLIGHT INOP. RELAMPED.
Part: SUPPORT BRACKET — CRACKED (BS 280) · airframe 16,662 hrs · 14,588 cycles
DURING C-CHECK, FS 280 SUPPORT BRACKET RADIUS CRACKED. REPLACED PER SRM.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 16,662 hrs · 14,588 cycles
DURING C-CHECK, FS 280 LBL9 OUTBOARD WEB CRACKED. REPAIRED PER REO.
Part: ANGLE — CRACKED (BS 280) · airframe 16,662 hrs · 14,588 cycles
DURING C-CHECK, FS 280 RBL 11 ANGLE CRACKED. REPAIRED PER REO.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 16,662 hrs · 14,588 cycles
DURING C-CHECK, FS 280 LBL9 FLOORBEAM CRACKED. REPAIRED PER REO.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 16,662 hrs · 14,588 cycles
C-CHECK, FS 280 RBL9 CLIPS CRACKED. REPAIRED PER REO.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,902 hrs · 13,945 cycles
F/A REPORTS AN EMERGENCY LIGHT POD IS INOPERATIVE. (FLIGHT NR 5946) RELAMPED LIGHT IAW AMM 33-51-16. OPS CHECK GOOD AT THIS TIME.
Part: WIRE — CHAFED (EMERGENCY LIGHTS) · airframe 15,131 hrs · 13,290 cycles
FLT 6423 - CEILING EMERGENCY LIGHT IS INOP. REPAIRED A CHAFED WIRE TO NR 4 ELBP CONNECTOR IAW MM 20-00-00. OPS CHECK GOOD.
Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,131 hrs · 13,290 cycles
CABIN EMERGENCY LIGHTS AT ROW 5 ARE INOP. REPLACED NR 3 INVERTER ASSEMBLY PER CRJ 200 WDM 33-51-00. ALL EMERGENCY LIGHTS CHECK GOOD.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,066 hrs · 13,236 cycles
FLT 6055 - EMERGENCY FLOOD LIGHT IS INOP. REPLACED NR 4 ELBP BATTERY CHARGER IAW CRJ MM 33-51-05. OPS CHECK GOOD.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,066 hrs · 13,236 cycles
FLT 6643 - FLOOR LEVEL EMERGENCY LIGHTS AFT OF ROW 10 WILL NOT ILLUMINATE. REPLACED NR 4 BATTERY PACK WITH SERVICEABLE UNIT AS REQUIRED PER AMM 33-51-04, PN AD-2013-1A, S/N OFF 87601.
2007
Part: SELECTOR VALVE — MALFUNCTIONED (MLG DOOR) · airframe 13,243 hrs · 11,612 cycles
GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES APPEARED, FLIGHT NR 6208. REPLACED NOSE LANDING GEAR SELECTOR VALVE. OPS CHECK GOOD PER CRJ MM 32-33-00, PN: 750006000, SN ON: 0584T SN OFF: 1949.
Part: UPLOCK — MALFUNCTIONED (NLG) · airframe 12,948 hrs · 11,346 cycles
FLT 6533 - WHEN THE GEAR WAS SELECTED DOWN, THE NOSE GEAR DID NOT EXTEND. AFTER PULLING THE LANDING GEAR MANUAL RELEASE HANDLE, THE NOSE GEAR EXTENDED AND INDICATED DOWN AND LOCKED. REPLACED THE NOSE GEAR UPLOCK ASSY IAW MM 32-33-05. OPS CHECK GOOD, PN 11600-103, SN/OFF NGL/0673/02.
Part: WINDOW — CRACKED (COCKPIT) · airframe 12,911 hrs · 11,314 cycles
FLT 5937 - LEFT SIDE WINDOW CRACKED AT FL340. REPLACED LEFT WINDOW AS REQUIRED IAW CRJ 200 MM 56-12-01, PN ON NP-139322-5, SN OFF, 02056H9385.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 12,033 hrs · 10,597 cycles
CABIN EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.
2006
Part: BRACKET — CRACKED (BS 484) · airframe 11,491 hrs · 10,092 cycles
RT 484 BRACKET AND ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIP P/N 601R31171-9 AT FS 4841 RBL27 AND ANGLE RT-2 PER CRJ200 REO 601R-53-41-059 REV.
Part: FRAME — CRACKED (BS 280) · airframe 11,491 hrs · 10,092 cycles
RBL 9 LOWER FRAME CRACKED STA 280, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FABRICATED PARTS AND I/B CLIP P/N 601R3113-58 AT STA 280, RBL 9.0 LOWER PER CRJ200 REO 601R-53-11-171 REV C.
Part: FRAME — CRACKED (BS 280) · airframe 11,491 hrs · 10,092 cycles
LBL9 UPPER FRAME CRACKED AT FS 280, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FABRICATED PARTS AND ANGLES PER CRJ200 REO 601R-53-11-138 REV NC.
Part: BRACKET — CRACKED (BS 484) · airframe 11,491 hrs · 10,092 cycles
LT 484 BRACKET AND ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED LT O/B GUIDE ROLLER BRACKET AT FS 484 PER CRJ200 SRM 51-41-02 PG 5-7.
Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 11,491 hrs · 10,092 cycles
AFT CARGO DOOR THRESHOLD FLOOR STRUCTURE HAS CRACKED STRUCTURE WHERE HINGE PLATE PIN BRACKET IS LOCATED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER AND FILLER PER CRJ200 REO 601R 53-61-1741.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 11,491 hrs · 10,092 cycles
PAX DOOR AFT DRAG ANGLE IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED 601R-52-11-513-1 ANGLE SECTION 2 AND 3 SPLICE ANGLE PER CRJ200 REO 601R-52-11-513 (REV A) SHEET 2.
Part: FRAME — CRACKED (BS 280) · airframe 11,491 hrs · 10,092 cycles
LBL9 LWR FRAME HAS CRACK AT STA280, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FABRICATED PARTS, 2 CLIPS IAW CRJ 200 REO 601R-53-11-171, REV C, REPAIR SCHEME B.
Part: BRACKET — CRACKED (MLG) · airframe 11,491 hrs · 10,092 cycles
RT MAIN GEAR, JUST FWD OF TRANSDUCER BRACKET WAS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED BRACKET P/N 601R75265-153 PO NR 70856 PER SRM 51-42-06 PGS 1-17.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 9,455 hrs · 8,314 cycles
CEILING EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT. OPERATIONAL CHECK GOOD PER MM 33-51-00.
Part: PDU — MALFUNCTIONED (TE FLAP) · airframe 9,400 hrs · 8,266 cycles
FLAPS FAILED AT 8 DEGREES WITH FLAP FAIL CAUTION MSG. REPLACED FLAP POWER DRIVE UNIT IAW MM 27-52-01. OPERATIONAL CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,937 hrs · 7,851 cycles
FWD CEILING EMERGENCY LIGHT INOP. REPLACED CEILING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD IAW AMM 33-51-00.
2005
Part: TRANSMITTER — FAULTY (RUDDER) · airframe 8,492 hrs · 7,453 cycles
UNABLE TO GET FULL RUDDER TRAVEL INDICATION IN EITHER DIRECTION. REPLACED RUDDER POSITION TRANSMITTER IAW MM 27-24-05. OPERATIONAL CHECK GOOD.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 8,475 hrs · 7,435 cycles
1 CEILING LEVEL EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED NR 3 ELBP IAW 33-51-04. OPERATIONAL CHECK GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,382 hrs · 7,343 cycles
EMERGENCY LIGHT IN CEILING AT ROW 10 IS INOPERATIVE. REPLACED EMERGENCY LIGHT (CEILING) AT ROW 10. OPERATIONAL CHECK GOOD.
Part: DETECTOR — MALFUNCTIONED (TE FLAPS) · airframe 8,106 hrs · 7,089 cycles
FLAP FAIL CAUTION MESSAGE, AFTER T/O. REPLACED SKEW DETECTOR UNIT, OPERATIONAL CHECK GOOD.
Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 7,766 hrs · 6,781 cycles
SPOILERON FAULT MESSAGE UPON LANDING. REPLACED PCU SPOILERON RT OUTBOARD. OPERATIONAL CHECK GOOD IAW MM 27-60-00.
Part: SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 7,665 hrs · 6,702 cycles
"FLAPS FAIL" CAUTION MSG. REMOVED AND REPLACED RT BPSU IAW CRJ MM 27-51-10 AND READJUSTED LT AND RT BPSU IAW M/M 27-51-10. READJUSTEMENT OF FECU POTENTIOMETER NR 5 AND NR 8. OPERATIONAL CHECK GOOD IAW CRJ M/M 27-51-10.
Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 7,594 hrs · 6,631 cycles
FLAPS FAIL IN FLIGHT. REPLACED AND RERIGGED LEFT AND RIGHT BPSU AND FECU IAW 27-50-00. OPERATIONAL CHECK GOOD.
Part: LEVER — MALFUNCTIONED (FLAP CONTROL) · airframe 7,575 hrs · 6,617 cycles
"FLAP FAIL" CAUTION MESSAGE. REPLACED FLAP SELECTOR LEVER IAW MM 27-50-00. OPERATIONAL CHECK GOOD, PN 7-45500-1, SN/OFF 764.
Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 7,568 hrs · 6,613 cycles
UPON LANDING AT LAX "SPOILERON FAULT" MESSAGE. NO MESSAGES PRIOR TO LANDING IN OAK. REMOVED AND REPLACED NR 1 SPOILER CONTROL UNIT WITH SERVICEABLE UNIT. FAULT D-7 ON UNIT, PN 49-164-05, SN/OFF 3149.
Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 7,490 hrs · 6,547 cycles
DURING CLEAN UP ON OUR CLIMB OUT, WE RECEIVED "FLAPS FAIL" MESSAGE ON ED 1. REPLACED FLAP ELECTRONIC CONTROL UNIT IAW 27-50-01. OPERATIONAL CHECK OK.
Part: BPSU — OUT OF RIG (TE FLAPS) · airframe 7,406 hrs · 6,459 cycles
AFTER DEPARTURE FLAPS WOULD NOT RETRACT PAST FLAPS 8. RIGGED BPSU'S IAW CRJ MM 27-51-10. OPERATIONAL CHECK GOOD.
Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 7,392 hrs · 6,444 cycles
ON FLAP RETRACTION, FLAPS FAILED AT 8 DEGREES. RIGGED RT BPSU IAW CRJ MM 27-51-10. OPERATIONAL CHECK GOOD.
Part: CLIP — CRACKED (FUSELAGE) · airframe 7,356 hrs · 6,412 cycles
FS 280 LEFT FLOORBEAM LBL 9.0 INBOARD AND OUTBOARD ATTACH CLIPS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,356 hrs · 6,412 cycles
AFT EQUIPMENT BAY INTERCOSTAL CLIP CRACKED FS 625.00 STR 14L. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ REO 601R-53-61-100 REV NC.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 7,356 hrs · 6,412 cycles
CARGO PIT FLOOR SUPPORT ANGLE CRACKED AT FS 621.0 RBL 42.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV "B".
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 8,176 hrs · 7,155 cycles
PAX DOOR; AIRSTAIR AFT DRAG ANGLE IS CRACKED BESIDE DOOR ASSIST PULLEY BRACKET; FS 357.00, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED DRAG ANGLE IAW CRJ REO 601R-52-11-513.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 7,356 hrs · 6,412 cycles
CARGO PIT FLOOR SUPPORT ANGLE CRACKED AT FS 621.0 LBL 38.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV "B".
Part: CLIP — CRACKED (FUSELAGE) · airframe 7,356 hrs · 6,412 cycles
FS 280 RT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH CLIPS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13 & 51-23-00.
Part: SKIN — DAMAGED · airframe 8,176 hrs · 7,155 cycles
FUSELAGE SKIN AT PASSENGER DOOR CUTOUT STR 18 LT LOWER FORWARD CORNER SKIN DENTED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED DAMAGE IAW REO 601R-53-00-030 REV "D".
Part: CLIP — CRACKED (FUSELAGE) · airframe 7,356 hrs · 6,412 cycles
AFT EQUIPMENT BAY INTERCOSTAL CLIP CRACKED FS 625.00 STR 14R. FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ REO 601R-53-61-100 REV NC.
Part: FITTING — CRACKED (FUSELAGE) · airframe 7,356 hrs · 6,412 cycles
FS 460 RT FLOOR RBL 9.0 OUTBOARD FITTING CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ SRM 51-40-11, 51-42-06 & 51-42-21.
Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 7,307 hrs · 6,376 cycles
FLAPS FAIL IN 20 DEGREE POSITION UPON TAKEOFF. RIGGED LEFT BPSU IAW MM 27-51-10. OPERATIONAL CHECK GOOD.
Part: CONTROL UNIT — MALFUNCTIONED (TE FLAP) · airframe 6,633 hrs · 5,753 cycles
SELECTED FLAPS TO 8 DEGREES, THEN FLAPS FAIL CAUTION MESSAGE. REMOVED AND REPLACED FECU IAW CRJ 200 MM CHAPTER 27-51-05, OPERATIONAL CHECK GOOD.
Part: SENSOR — MALFUNCTIONED (SPOILERS) · airframe 6,633 hrs · 5,753 cycles
"FLAPS FAIL" MSG WHEN SELECTING FLAPS OUT OF 0 DEGREES. REMOVED AND REPLACED RIGHT BPSU IAW CRJ27-51-10, OPERATIONAL CHECK GOOD.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 6,426 hrs · 5,598 cycles
EMERGENCY LIGHT CEILING AT ROW 5 INOPERATIVE. REPLACED LAMP IAW AMM 33-51-16. OPERATIONAL CHECK GOOD.
2004
Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 6,160 hrs · 5,362 cycles
ON TAXI OUT FLIGHT SPOILER STATUS MESSAGE. REPLACED NR 1 AND NR 2 SECU IAW AMM 27-60-00, REPLACED LEFT INBOARD FLIGHT SPOILER PCU IAW 27-61-00. OPERATIONAL CHECK GOOD. P/N 49-164-06, S/N OFF 01533, P/N 49-164-06, S/N OFF 01598, P/N 27000-7, S/N OFF 5494.
Part: ECU — MALFUNCTIONED (SPOILERON) · airframe 6,211 hrs · 5,408 cycles
SPOILERON FAULT STATUS MSG ON ED2 DURING TAXI OUT. REPLACED SECU NR 2 IAW 27-60-00. REPLACED LEFT INBOARD FLIGHT SPOILER PCU IAW 27-61-00, OPERATIONAL CHECK GOOD.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 4,755 hrs · 4,093 cycles
RIGHT AFT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RIGHT AFT EXTERIOR EMERGENCY LIGHT BULB, OPERATIONAL CHECK GOOD.
Part: SWITCH — FAILED (STAB TRIM) · airframe 4,251 hrs · 3,659 cycles
STAB CHANNEL NR 2 WILL NOT ENGAGE. REPLACED STAB DISCONNECT SWITCH ON F/O'S YOKE. REPLACED HSTCU. OPS CHECKS GOOD IAW MM 27-41-00. S/N OFF: 1384.
Part: SENSOR — MALFUNCTIONED (LT ENG TAILPIPE) · airframe 4,218 hrs · 3,631 cycles
WHILE ON APPROACH TO DEN LEFT JETPIPE OVERHEAT WARNING CAME ON. SHUTDOWN LEFT ENGINE AS PER THE QRH. REMOVED AND REPLACED LEFT ENGINE JETPIPE OVERHEAT SENSING ELEMENTS ON BOTH A AND B SYSTEMS IAW CRJ MM ATA CHPT 26-11-00 AND 26-11-01. P/N: 26212000.
Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB) · airframe 4,128 hrs · 3,564 cycles
STAB CHANNEL 1 WOULD NOT ENGAGE. REMOVED AND REPLACED HSTCU IAW CL600 MM 27-41-01, OPS CHECK GOOD.
Part: ATTACH ANGLE — CRACKED (FLOORBEAM) · airframe 3,981 hrs · 3,448 cycles
DURING C-CHECK INSPECTION, MAIN FUSELAGE FLOORBEAM AT LBL 9.0 HAS OUTBOARD ATTACH ANGLE CRACKED AT FS 280.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM.
Part: ATTACH ANGLE — CRACKED (FLOORBEAM) · airframe 3,981 hrs · 3,448 cycles
DURING C-CHECK INSPECTION, MAIN FUSELAGE FLOORBEAM AT RBL 9.0 HAS INBOARD AND OUTBOARD ATTACH ANGLES CRACKED AT FS 280.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM.
Part: ATTACH ANGLE — CRACKED (FLOORBEAM) · airframe 3,981 hrs · 3,448 cycles
DURING C-CHECK INSPECTION, MAIN FUSELAGE FLOORBEAM AT LBL 9.0 HAS A CRACKED INBOARD ATTACH ANGLE AT FS 280.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM.