N910EV
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.
151 reports on file, 2004-04-15 – 2025-11-04.
Part: DOOR SILL — CORRODED (ZONE 100) · airframe 41,507 hrs · 38,215 cycles
AFT CARGO DOOR LOWER SILL, CORRODED IN MULTIPLE LOCATIONS AND BENT, EVAL REQUIRED. REMOVED AND REPLACED CARGO DOOR LOWER SILL IAW SRM 51-42-21, 51-40-11, 51-42-06, 51-42-13, REV. 39B, AND REO 601R-53-61-8412, REV--. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 41,507 hrs · 38,215 cycles
TRANSVERSE FLOOR BEAM @ FS. 589 FOUND TO BE CRACKED IN MULTIPLE LOCATIONS WHERE AFT CARGO DOOR LOWER SILL SITS. REPAIRED TRANSVERSE BEAM AT FS 589.00 IAW MHIRJ REO 601R-53-61-8412 REV--. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUE CARD FOR WORK PERFORMED.
Part: SPAR — DAMAGED (ZONE 500 AILERON) · airframe 41,507 hrs · 38,215 cycles
LEFT AILERON AFT SPAR MOST OUTBOARD BORES ARE OVERSIZED. REPAIRED R/H AILERON AFT SPAR MOST OTBD AND INBD BORE ON WING IAW GREO 601R-57-51-015 REV NC.
Part: DRAIN — MISREPAIRED (ZONE 100) · airframe 41,507 hrs · 38,215 cycles
WHILE WORKING SB 601R-57-054 INADVERTENTLY REAMED SATELLITE HOLES FOR WATER DRAINS AT BL 0 ON LT & RT SIDES BETWEEN STRINGERS 14-15. REPAIRED SATELLITE HOLES FOR WATER DRAINS AT BL 0 ON LT AND RT SIDE BETWEEN STRS 14-15 IAW REO 601R-57-21-3982 REV -.
Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 41,507 hrs · 38,215 cycles
INTERCOSTAL FOUND TO BE SEVERELY CORRODED ON MORE THAN ONE ELEMENT REQUIRING REPLACEMENT LOCATED AT BS 364, S25L - 25R. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
Part: MOUNT BRACKET — DAMAGED (ZONE 100) · airframe 41,507 hrs · 38,215 cycles
UPON INSTALLATION OF THE A/C POWER RECEPTACLE BRACKET MOUNT FOUND 1 EA FASTENER HOLE TO BE ELONGATED ON AFT O/B SIDE IN CORNER MARKED WITH RED TAPE. REPAIRED A/C POWER RECEPTACLE BRACKET MOUNT IAW MHIRJ REO 601R-53-11-4026 REV -. COMPLETED SKYCARD 51-900-1003-SKY AND MAJOR REPAIR FORM M-337.
Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 41,507 hrs · 38,215 cycles
INTERCOSTALS FOUND TO BE SEVERELY CORRODED ON MORE THAN ONE ELEMENT REQUIRING REPLACEMENT. REMOVED AND REPLACED THE INTERCOSTALS IAW SRM 51-42-06, AND 51-42-21 06. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
Part: SPAR — DAMAGED (ZOEN 600 AILERON) · airframe 41,507 hrs · 38,215 cycles
R/H AILERON AFT SPAR MOST OUTBOARD BORES ARE OVERSIZED. REPAIRED R/H AILERON AFT SPAR MOST OTBD AND INBD BORE ON WING IAW GREO 601R-57-51-015 REV NC.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 41,507 hrs · 38,215 cycles
LEFT PRESSURE FLOOR SUPPORT IS CORRODED AT BS 549. REPAIRED THE CORROSION ON THE LT PRESSURE FLOOR SUPPORT AT FS 549 IAW REO 601R-53-41-666, REV C, AND SKY CARD 51-900-1003-SKY.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 41,507 hrs · 38,215 cycles
PAX DOOR DD7A FWD INTERCOSTAL FOUND TO BE CORRODED. REQUIRES REPLACEMENT. REPLACED PAX DOOR DD7A FWD INTERCOSTAL IAW SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 41,507 hrs · 38,215 cycles
PAX DOOR INTERCOSTAL DD3 MID CORRODED. REQUIRES REPLACEMENT. REMOVED AND REPLACED THE PAX DOOR MID INTERCOSTAL DD3 IAW SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 41,507 hrs · 38,215 cycles
PAX DOOR INTERCOSTAL DD2 MID FOUND TO BE CORRODED. REQUIRES REPLACEMENT. REMOVED AND REPLACED THE PAX DOOR MID INTERCOSTAL DD2 IAW SRM 51-42-06 AND 51-42-21, COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. CONTINUATION CARD FOR WORK PERFORMED
Part: FORMER — CORRODED (ZONE 800) · airframe 41,507 hrs · 38,215 cycles
PAX DOOR MID FORMER, FS329.41 BETWEEN DD5 AND DD6 FOUND TO BE CORRODED REQUIRED REPLACEMENT. REPLACED PAX DOOR MID FORMER AT FS329.41 IAW SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
Part: RIB — CRACKED (ZONE 600) · airframe 41,507 hrs · 38,215 cycles
RIGHT MLG BATTERY RIB IS CRACKED AT WS 53.60 FWD O/B SIDE. REMOVED AND REPLACED RT BATTERY RIB AT WS 53.60 IAW SRM 51-42-06 AND 51-42-21 COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
Part: SKIN — CRACKED (ZONE 100) · airframe 41,507 hrs · 38,215 cycles
LEFT FORWARD FUSELAGE SKIN IS CRACKED AT THE AFT LATCH CUTOUT OF THE TRU DOOR. REPLACED LT FORWARD FUSELAGE SKIN IAW SRM 51-42-06, 51-42-13, & 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY.
Part: SKIN — CRACKED (ZONE 100) · airframe 41,507 hrs · 38,215 cycles
RIGHT FORWARD FUSELAGE SKIN IS CRACKED AT THE AFT LATCH CUTOUT OF THE TRU DOOR. REPLACED RT FORWARD FUSELAGE SKIN IAW SRM 51-42-06, 51-42-13, AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY.
Part: DRIP TRAY — DAMAGED (ZONE 100) · airframe 41,507 hrs · 38,215 cycles
DRIP TRAY AT LBL 27, FS 409 IS DAMAGED. REPAIRED DRIP TRAY AND MOUNTING STRUCTURE IAW MHIRJ REO 601R-53-31-1351 REV-, AND REO 601R-53-31-1353, REV-. COMPLETED TASK CARD 51-900-1003-SKY. REF CONTINUATION CARD FOR WORK PERFORMED.
Part: FRAME — CORRODED (ZONE 100) · airframe 41,507 hrs · 38,215 cycles
BS 319 FRAME IS CORRODED BETWEEN S18L AND 20L. REMOVED AND REPLACED THE STUB FRAME AT IAW SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 41,507 hrs · 38,215 cycles
RBL 9 FLOOR SUPPORT TOP INBD FLANGE IS CORRODED FROM BS 409+5 TO BS 409+118. REMOVED AND REPLACED THE FLOOR SUPPORT CAP AT RBL9 FROM FS409+5-409+118 IAW SRM 51-42-06, 51-42-21, AND REO 601R-53-31-1350, REV-- DATED 2025-09-25. REF CONTINUATION CARD FOR ALL WORK PERFORMED.
Part: DOOR SILL — CORRODED (ZONE 200) · airframe 41,507 hrs · 38,215 cycles
PAX DOOR SILL LOWER FLOOR SUPPORT ANGLE IS CORRODED. REMOVED AND REPLACED PAX DOOR LOWER SILL FLOOR SUPPORT ANGLE IAW SRM 51-42-06, 51-42-13, AND 51-42-13. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 41,507 hrs · 38,215 cycles
FS280 CROSSBEAM LBL9 IB ANGLE IS CRACKED. (C-CHECK RO 12/17/2025)FABRICATED 1 EA CLAP AT FS 280 CROSSBEAM LBL 9IAW CRJ 200 SRM 51-40-06, 51-40-11, 51-25-00, 51-42-22 AND 51-42-21 REV. 39B, DATED 06-NOV-11. REFERENCING REO 601R-53-11-171 REV D DATED 13 FEB 07 FOR MATERIAL TYPE AND SPECIFICATIONS INSTALLED 1 EA FABRICATED CLIP IAW CRJ 200 SRM 51-42-21 REFERENCING REO 601R-53-11-171 REV D DATED 13 FEB 07 AND IAW SKY CARD 51-900-1003-SKY ATTACHED COMPLETED M-337 NOT WEIGHT CHANGE
Part: FITTING — CRACKED (ZONE 200) · airframe 41,507 hrs · 38,215 cycles
FS 460.00 FITTING IS CRACKED ON THE OTBD SIDE OF LBL 9, FLOORBEAM. REMOVED AND INSTALLED SERVICEABLE FITTING AT BS 460 IAW REO 601R-53-41-3353, REV-. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
Part: ANGLE — CRACKED (ZONE 500) · airframe 41,507 hrs · 38,215 cycles
LEFT WING, BATTERY RIB AT WS 53.60 ANGLE ON INBD SIDE OF WEB IS CRACKED AND WEB IS CRACKED AS WELL. REMOVED AND REPLACED LT WING BATTERY RIB IAW SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
Part: ANGLE — CRACKED (ZONE 500) · airframe 41,507 hrs · 38,215 cycles
LEFT WING, BATTERY RIB AT WS 48.30 ANGLE IS CRACKED. REMOVED AND REPLACED THE LT UPPER BATTERY RIB ANGLE IAW SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
Part: POST — FAILED INSP (ZONE 200) · airframe 41,507 hrs · 38,215 cycles
BS 409+128 BL 0 VERTICAL POST RT & LT SIDES HAS INDICATIONS .3" LONG BY 100% FSH IN THE AFT RADIUS AT WL69. FAILED NDT INSPECTION. REMOVED AND REPLACED BS 409+128 BL 0 VERTICAL POST IAW REO 601R-53-41-889 REV-D, COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
Part: SKIN — MISALIGNED (ZONE 800) · airframe 41,507 hrs · 38,215 cycles
SERVICE DOOR INNER SKIN HAS SEVERAL JO-BOLTS THAT ARE NOT PROPERLY INSTALLED. REPAIRED OVERSIZED HOLES AND INSTALLED FASTENERS IAW REO 601R-52-41-537 REV--. COMPLETED TASK CARD 51-900-1003-SKY.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 41,507 hrs · 38,215 cycles
PAX DOOR INTERCOSTAL DD 1A BETWEEN FS 323.361 AND FS 336.961 IS CORRODED. REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD1A IAW CRJ 200 SRM 51-42-06, 51-42-21 AND 51-42-11 COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337 NO WEIGHT CHANGE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED
Part: FORMER — CORRODED (ZONE 800) · airframe 41,507 hrs · 38,215 cycles
PAX DOOR FWD FORMER IS CORRODED ON THE INSIDE. REMOVED AND REPLACED PAX DOOR FWD FORMER IAW SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 41,507 hrs · 38,215 cycles
PAX DOOR INTERCOSTAL BETWEEN FS 320.163 AND FS 329.130 IS CORRODED. REMOVED AND REPLACED PAX DOOR MID INTERCOSTAL DD4 IAW CRJ 200 SRM 51-42-06 AND 51-42-21 COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337 NO WEIGHT CHANGE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 41,507 hrs · 38,215 cycles
PAX DOOR INTERCOSTAL DD 6 BETWEEN FS 320.163 AND FS 336.961 IS CORRODED. REMOVED AND REPLACED PAX DOOR MID INTERCOSTAL DD6 IAW SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 41,507 hrs · 38,215 cycles
PAX DOOR INTERCOSTAL DD 1 BETWEEN FS 323.361 AND FS 336.961 IS CORRODED. REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD1 MID BETWEEN FS323.61 AND FS336.961 IAW SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
Part: FORMER — CORRODED (ZONE 800) · airframe 41,507 hrs · 38,215 cycles
PAX DOOR AFT FORMER IS CORRODED ON THE INSIDE. REMOVED AND REPLACED PAX DOOR AFT FORMER IAW SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED
Part: SKIN — DENTED (ZONE 100) · airframe 41,507 hrs · 38,215 cycles
SEVERAL DENTS FROM BS 589 - 621 BETWEEN S22R AND 27R. REPAIRED THE DENTS IAW 601R-53-61-8395, REV-. COMPLETED TASK CARD 51-900-1003-SKY . REFERENCE CONTINUATION CARD FOR WORK PERFORMED
Part: SKIN — CHAFED (ZONE 600) · airframe 41,507 hrs · 38,215 cycles
RIGHT LOWER WING PLANK CHAFED ON TRAILING EDGE AT RWS 45.0 FROM CONTACT WITH PANEL 193AB. REPAIRED THE RT LOWER WING PLANK IAW REO 601R-57-21-880 REV-D. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
Part: SKIN — CHAFED (ZONE 500) · airframe 41,507 hrs · 38,215 cycles
LEFT LOWER WING PLANK CHAFED ON TRAILING EDGE AT LWS 45.0 FROM CONTACT WITH PANEL 193AB. REPAIRED THE LT LOWER WING PLANK ON TRAILING EDGE IAW REO 601R-57-21-880, REV-D. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. COMPLETED AND ATTACHED MAJOR REPAIR SKYCARD 51-900-1003-SKY.
Part: DOOR FRAME — CORRODED (ZONE 100) · airframe 41,507 hrs · 38,215 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: RA93189-601R-53-61-8212 MXCODEID77004-PR - FRAME FS574.00 AT CARGO DOOR FWD OPENING HAS CORROSION AT APPROX. WL 75.00. BLENDED CORROSION ON FRAME BS 574 AT CARGO DOOR FWD OPENING AT WL 75 IAW SRM 51-21-06 AND COMPLIED WITH REO 601R-53-61-8212 REV-.
Part: OIL SYSTEM — LEAKING (LT ENGINE) · airframe 41,033 hrs · 37,707 cycles
MASTER WARNING LH OIL PRESSURE ON CLIMB OUT, THEN N1 AND N2 AND ITT SPOOLED DOWN ON ITS OWN TO ZERO. RAN QRH ATTEMPTED RESTART TWICE - BOTH TIMES FAILED. COMING OUT OF XWA DIVERTED TO RAP. DECLARED AN EMERGENCY. NO EXTERNAL DAMAGE NOTED ON WALKAROUND POSTFLIGHT, BUT OIL IS LEAKING FROM LH ENGINE. (FLIGHT 4704 - FILED OPEN) PLEASE REFERENCE AML 1581433THIS IS CURRENTLY A WORK IN PROGRESS
Part: ENGINE — FAULTED (LEFT) · airframe 41,056 hrs · 37,731 cycles
MASTER WARNING LH OIL PRESSURE ON CLIMB OUT, THEN N1 AND N2 AND ITT SPOOLED DOWN ON ITS OWN TO ZERO. RAN QRH ATTEMPTED RESTART TWICE - BOTH TIMES FAILED. COMING OUT OF XWA DIVERTED TO RAP. DECLARED AN EMERGENCY. NO EXTERNAL DAMAGE NOTED ON WALKAROUND POSTFLIGHT, BUT OIL IS LEAKING FROM LH ENGINE. (FLIGHT 4704 - FILED CLOSED) PLEASE REFERENCE AML 1581433 THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 29982988 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED LH ENG IN REFERENCE TO TASK CARD 71-900-1000-SKYON TASK CARD 71-900-1000-SKY, THE FOLLOWING TOOL WAS ENTERED: TORQUE WRENCH SN- 0918106886 EXPIRATION- 11/25/25.ON TASK CARD 71-900-1000-SKY, THE FOLLOWING TOOL WAS ENTERED: TORQUE WRENCH SN- 0918106886/X050033 EXPIRATION- 11/01/25.ON TASK CARD 71-900-1000-SKY, THE FOLLOWING TOOL WAS ENTERED: -- SN- -- EXPIRATION- 04/16/25.ON TASK CARD 71-900-1000-SKY, THE FOLLOWING TOOL WAS ENTERED: TORQUE WRENCH SN- 0918106886 EXPIRATION- 11/01/25.ON TASK CARD 71-900-1000-SKY, THE FOLLOWING TOOL WAS ENTERED: - SN- - EXPIRATION- 04/01/25.ON TASK CARD 71-900-1000-SKY, THE FOLLOWING TOOL WAS ENTERED: TORQUE WRENCH SN- X050033 EXPIRATION- 03/01/26."
Earlier reports · 2004–2024 · 113 reports
2024
Part: FRAME — CORRODED (ZONE 100) · airframe 39,982 hrs · 36,623 cycles
FRAME FS574.00 AT CARGO DOOR FWD OPENING HAS CORROSION AT APPROX. WL75.00. (FILED - CLOSED)BLENDED CORROSION ON FRAME FS574.00 AT CARGO DOOR FWD OPENING AT APPROX WL75.00 WITH REFERENCE TO SRM 51-21-06 AND COMPLIED WITH REO 601R-53-61-8212 REV "--" DATED 2024-08-13. SEE CHILD CAMP FOR EDDY CURRENT INSPECTION. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT. THE SUBJECT REWORKED CONDITION IN STRUCTURALLY ACCEPTABLE FOR 1650 FLIGHT HOURS OR UNTIL NEXT 'C' CHECK WHICHEVER IS EARLIER. VISUALLY INSPECT REPAIRED AREA FOR ANY DAMAGE PROPAGATION AT INTERVALS NOT TO EXCEED 600 FLIGHT HOURS.
Part: FRAME ANGLE — CORRODED (ZONE 100) · airframe 39,982 hrs · 36,623 cycles
CORROSION ON FRAME ANGLE AT FS 605.00 BETWEEN STGR 18R AND 19R (FILED - CLOSED)REMOVED CORROSION FROM FRAME ANGLE AT FS 605.00 BETWEEN STGR 18R AND 19R WITH REFERENCE TO SRM 51-21-06 AND DISCOVERED CRACK. REPAIRED FRAME ANGLE AT FS 605.00 WITH REFERENCE TO REO 601R-53-61-8210 REV "--" DATED 2024-08-12. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT. SEE CHILD CAMP FOR EDDY CURRENT INSPECTION.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 39,982 hrs · 36,623 cycles
LH PRESSURE FLOOR SILL HAS NUMEROUS AREAS OF CORROSION LOCATED @ APPROX. FS460-465, 470.00-474.00, 485.5, 506.00, 513.00 AND 530.50. (FILED - CLOSED)BLENDED AND REPAIRED ALL OF THE CORROSION AREAS ON THE LH PRESSURE FLOOR SILL FROM APPROX FS409 + 128 TO FS559.00 PER REO 601R-53-41-666 DATED: 2012-11-06 REV- C. PERFORMED A UT THICKNESS MEASUREMENT OF THE BLENDED AREAS IN REFERENCE WITH NDTM PART 4 51-00-001 AND FOUND TO BE WITHIN LIMITS PER REO 601R-53-41-666. PERFORMED AN EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND PART 6 53-00-096 WITH NO CRACKS FOUND AT THIS TIME. APPLIED FINISHING AS STATED IN REO. COMPLETED CORROSION FINDINGS REPORT. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 39,982 hrs · 36,623 cycles
RH PRESSURE FLOOR SILL HAS SURFACE CORROSION LOCATED AT APPROX. FS 555.00, 513.00 AND 447.00. (FILED - CLOSED)BLENDED AND REPAIRED ALL OF THE CORROSION AREAS ON THE RH PRESSURE FLOOR SILL FROM APPROX FS409 + 128 TO FS559.00 PER REO 601R-53-41-666 DATED: 2012-11-06 REV- C. PERFORMED A UT THICKNESS MEASUREMENT OF THE BLENDED AREAS IN REFERENCE WITH NDTM PART 4 51-00-001 AND FOUND TO BE WITHIN LIMITS PER REO 601R-53-41-666. PERFORMED AN EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND PART 6 53-00-096 WITH NO CRACKS FOUND AT THIS TIME. APPLIED FINISHING AS STATED IN REO. COMPLETED CORROSION FINDINGS REPORT. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337.
Part: TRACK — CRACKED (ZONE 800) · airframe 39,982 hrs · 36,623 cycles
CARGO DOOR FORWARD TRACK LOWER CHANNEL CRACKED. (FILED - CLOSED)REMOVED AND REPLACED THE CARGO DOOR FORWARD TRACK LOWER CHANNEL WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337.
Part: STIFFENER — CRACKED (ZONE 100) · airframe 39,982 hrs · 36,623 cycles
CRACK INDICATION LOCATED FS409 + 128 BL0.00 ON VERTICAL BEAM/STIFFENER, FORWARD LEFT ANGLE AFT FACE, PROPAGATING OUTBOARD/AIRCRAFT LEFT FROM UPPER LEFT FASTENER (REFERENCE SRM 53-41-19 ITEM 6, FIGURE 1, SHEET 1 AND 3). (FILED - CLOSED)COMPLIED WITH REO 601R-53-41-3244 DATED: 2024-07-30 REV -- TEMPORARY REPAIR TO VERTICAL STIFFENER AT THE PRESSURE BULKHEAD FS409.00 + 128 AND BL 0.00. COMPLETED THE MAJOR REPAIR FORM (M-337). COMPLIED WITH TASK CARD 51-900-1003-SKY. REFERENCE CHILD FOR MCO FOR THIS AREA TO BE VISUALLY INSPECTED TO NOT EXCEED 800 FLIGHT HOURS
Part: PRESSURE BLKHD — CRACKED (ZONE 100) · airframe 39,982 hrs · 36,623 cycles
AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGER 14R, CLIP/ANGLE CRACKED. (FILED - CLOSED)REMOVED AND REPLACED CLIP/ANGLE ON AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGER 14R WITH REFERENCE TO SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337.
Part: PRESSURE BLKHD — GOUGED (ZONE 100) · airframe 39,982 hrs · 36,623 cycles
REAR PRESSURE BULKHEAD (FS621.00) FWD FACE HAS RIVET HEAD DAMAGE AND GOUGES ON DOUBLERS, LOCATED APPROX. LBL 18.00, 27.50, RBL 36.20, 27.50, 18.00 @ WL 87.50 AND WL 94.50. (FILED - CLOSED)UPON FURTHER INSPECTION FOUND 6 GOUGES LOCATED FS 621 BULKHEAD TOP DOUBLERS LOCATED AT LBL 18.00 & 27.50 AND RBL9.50, 18.00, 27.50 & 36.20 BELOW WL 106.17 AND EIGHT DAMAGED FASTENERS LOCATED LBL 9.50, 18.00, 27.50 & 36.20 AND RBL 9.50, 18.00, 27.50 & 36.20. REPAIRED DAMAGE WITH REFERENCE TO REO 601R-53-61-8209 REV "--" DATED 2024-07-26. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337.
Part: PRESSURE BLKHD — CRACKED (ZONE 100) · airframe 39,982 hrs · 36,623 cycles
AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH STRINGER 14L, CLIP/ANGLE CRACKED. (FILED - CLOSED)REMOVED AND REPLACED CLIP/ANGLE ON AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH STRINGER 14L WITH REFERENCE TO SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337.
2021
Part: NONE — NONE · airframe 38,738 hrs · 35,526 cycles
TRANSFER FROM EAML 763411 : QTY 07 MIS-DRILLED HOLES RH H/STAB LOWER SKIN O/B RIB NO 9. REF REO601R-55-11-699 DATED 2021-10-22 REV -- (FLIGHT 5459 - FILED CLOSED) REPAIRED MIS-DRILLED HOLES IN RH HORZONTAL STAB LOWER SKIN BETWEEN RIB #7 - RIB #9 AND F/SPAR 20% - R/SPAR 65% IN REF TO REO 601R-55-11-700, REV--, DATED 2021-11-03. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH FORM M-337. REF CP 23766729 FOR SPECIFIC AIRWORTHINESS LIMITATIONS.
Part: ENGINE — FAILED (RIGHT) · airframe 38,370 hrs · 35,222 cycles
RIGHT ENGINE FAILURE AFTER DEPARTING KBIS THROUGH 7000Ãâ¬â¢. PERFORMED QRC, QRH PROCEDURES, RETURNED TO KBIS. (FLIGHT 5729 - FILED CLOSED) REF AML 703489 FOR CORRECTIVE. MORE INFORMATION WAS ADDED TO AML 703489 BUT BOTH ARE THE SAME DISCREPANCY. THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 23277520 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE ML 23277518 FOR CORRECTIVE ACTION. ENGINE CHANGE."
Part: STOP FITTING — BROKEN (PAX DOOR) · airframe 38,318 hrs · 35,178 cycles
PAX DOOR (A/C SIDE) FWD UPPER BRACKET STOP FITTING FOUND BROKEN (FILED CLOSED) REMOVED AND REPLACED FWD UPPER BRACKET STOP FITTING ON PAX DOOR SURROUND PER AMM 53-21-23 OPS CHECK GOOD AT THIS TIME
2016
Part: TARGET — LOOSE (RT MLG UPLOCK) · airframe 30,958 hrs · 27,154 cycles
GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF. RETURNED TO FIELD. FOUND THE RT MLG UPLOCK TARGET LOOSE. TORQUED AND ADJUSTED THE UPLOCK TARGET IAW AMM. PERFORMED GEAR EXTENSION & RETRACTION TEST IAW AMM. OPS GOOD.
2014
Part: UNKNOWN — ODOR (CABIN) · airframe 26,356 hrs · 22,437 cycles
SMOKE ODOR IN CABIN WITH ENGINE & APU RUNNING.
Part: ACM — SMOKE (LEFT) · airframe 26,448 hrs · 22,529 cycles
OILY SMOKE ODOR DETECTED IN ACFT ALONG WITH A WHISTLE FROM OUTSIDE WHILE LT PACK IS ON APU. R & R LT PACK ACM, IAW AMM.
2013
Part: FRAME — CORRODED (FUSELAGE) · airframe 25,687 hrs · 21,784 cycles
FOUND CORROSION AT TWO FUSELAGE FRAMES JUST FWD OF THE AVIONICS BAY DOOR. CORROSION IS LOCATED ON THE FWD & AFT SIDES OF THE FRAME AT FS 349.0 BETWEEN STRINGER 26 & STRINGER 27 LT OF BL 0.0 & THE FWD AFT SIDES OF THE FRAME AT FS 333.0 BETWEEN STRINGER 26 & STRINGER 27 LT OF BL 0.0. C-CHECK REPLACED LOWER SECTION OF FRAMES AT FS 349.00 & FS 333.00 IAW SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,400 hrs · 21,479 cycles
AFT EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT 4674 RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,388 hrs · 21,469 cycles
NR 4 OVERHEAD EMERGENCY LIGHT POD BURNED OUT. FLT 4648 RELAMPED, PN ON 1317.
Part: HANDLE — UNSECURE (SERVICE DOOR) · airframe 25,267 hrs · 21,356 cycles
OVERBOARD COOL CAUTION MESSAGE, WOULD NOT PRESSURIZE. FLT#4531 SECURED INNER HANDLE ON SERVICE DOOR. PERFORMED OPERATIONAL CHECK OF AVIONICS EXHAUST VALVES & PRESSURIZATION IAW AMM. OPERATIONS CHECKED GOOD.
Part: O-RING — DAMAGED (APU) · airframe 25,266 hrs · 21,354 cycles
WITH APU RUNNING THERE IS A STRONG SMELL OF JET FUEL IN COCKPIT & CABIN. FLT#4511 REPLACED FCU O-RING, PN M25988-2-904.
Part: SKIN — CORRODED (WING) · airframe 25,158 hrs · 21,257 cycles
LOWER WING PLANK ACCESS HOLE NR 540BB HAS CORROSION. C-CHECK REPAIRED FUEL ACCESS PANEL, ACCESS HOLE NR 540BB IAW REO.
Part: SKIN — CORRODED (WING) · airframe 25,158 hrs · 21,257 cycles
LOWER WING PLANK ACCESS HOLE NR 640BB HAS CORROSION AS MARKED. C-CHECK REPAIRED IAW REO.
Part: SKIN — CORRODED (WING) · airframe 25,158 hrs · 21,257 cycles
LOWER WING PLANK ACCESS HOLE NR 550HB HAS CORROSION. CORRODED REPAIRED FUEL ACCESS HOLE NR 550HB IAW REO.
Part: SKIN — CORRODED (WING) · airframe 25,158 hrs · 21,257 cycles
LOWER WING PLANK ACCESS HOLE NR 640CB HAS CORROSION AS MARKED. C-CHECK REPAIRED IAW REO.
Part: SKIN — CORRODED (WING) · airframe 25,158 hrs · 21,257 cycles
LOWER WING PLANK ACCESS HOLE NR 540AB HAS CORROSION. C-CHECK REPAIRED FUEL ACCESS PANEL CUTOUT NR 540AB IAW REO.
Part: SKIN — CORRODED (WING) · airframe 25,158 hrs · 21,257 cycles
FUEL ACCESS HOLE FOR PANEL 650AB HAS FRETTING CORROSION & FOUR CRACKS. C-CHECK REPAIRED FRETTING CORROSION & FOUR CRACKS ON FUEL ACCESS HOLE FOR PANEL 650AB IAW REO.
Part: SKIN — CORRODED (WING) · airframe 25,158 hrs · 21,257 cycles
LOWER WING PLANK ACCESS HOLE NR 540FB HAS CORROSION. C-CHECK REPAIRED FUEL ACCESS PANEL CUTOUT HOLE NR 540FB IAW REO.
Part: SKIN — CORRODED (WING) · airframe 25,158 hrs · 21,257 cycles
LOWER WING PLANK ACCESS HOLE NR 650EB HAS CORROSION AS MARKED. C-CHECK REPAIRED IAW REO.
Part: SKIN — CORRODED (WING) · airframe 25,158 hrs · 21,257 cycles
LOWER WING PLANK ACCESS HOLE NR 650GB HAS CORROSION AS MARKED. C-CHECK REPAIRED IAW REO.
Part: SKIN — CORRODED (WING) · airframe 25,158 hrs · 21,257 cycles
LOWER WING PLANK ACCESS HOLE NR 650HB HAS CORROSION AS MARKED. C-CHECK REPAIRED IAW REO.
Part: SKIN — CORRODED (WING) · airframe 25,158 hrs · 21,257 cycles
LOWER WING PLANK ACCESS HOLE NR 610AB HAS CORROSION AS MARKED. C-CHECK REPAIRED IAW REO.
Part: SKIN — CORRODED (WING) · airframe 25,158 hrs · 21,257 cycles
LOWER WING PLANK ACCESS HOLE NR 550CB HAS CORROSION AS MARKED. C-CHECK REPAIRED FUEL ACCESS PANEL CUTOUT HOLE NR 550CB IAW REO.
Part: SKIN — CORRODED (WING) · airframe 25,158 hrs · 21,257 cycles
LOWER WING PLANK ACCESS HOLE NR 510AB HAS CORROSION. C-CHECK REPAIRED FUEL ACCESS PANEL CUTOUT 510AB IAW REO.
Part: SKIN — GOUGED (FUSELAGE) · airframe 25,158 hrs · 21,257 cycles
RT SIDE OF FS JUST AFT OF APU EXHAUST TWO SMALL GOUGES IN SKIN. C-CHECK REPAIRED TWO SMALL GOUGES IN SKIN ON RT SIDE OF FS JUST AFT OF APU EXHAUST, IAW STS EA.
Part: SKIN — CORRODED (WING) · airframe 25,158 hrs · 21,257 cycles
LOWER WING PLANK ACCESS HOLE NR 550FB HAS CORROSION. C-CHECK REPAIRED FUEL ACCESS PANEL CUTOUT HOLE IAW REO.
Part: SKIN — CORRODED (WING) · airframe 25,158 hrs · 21,257 cycles
LOWER WING PLANK ACCESS HOLE NR 540DB HAS CORROSION. C-CHECK REPAIRED ACCESS PANEL CUTOUT HOLE NR 540DB IAW REO.
Part: SKIN — CORRODED (WING) · airframe 25,158 hrs · 21,257 cycles
LOWER WING PLANK ACCESS HOLE NR 650CB HAS CORROSION AS MARKED. C-CHECK REPAIRED IAW REO.
Part: SKIN — CORRODED (WING) · airframe 25,158 hrs · 21,257 cycles
LOWER WING PLANK ACCESS HOLE NR 650FB HAS CORROSION AS MARKED. C-CHECK BLENDED OUT CORROSION IAW REO.
Part: SKIN — CORRODED (WING) · airframe 25,158 hrs · 21,257 cycles
LOWER WING PLANK ACCESS HOLE NR 50AB HAS CORROSION. C-CHECK REPAIRED FUEL ACCESS CUTOUT HOLE NR 550AB IAW REO.
Part: SKIN — CORRODED (WING) · airframe 25,158 hrs · 21,257 cycles
LOWER WING PLANK ACCESS HOLE NR 650DB HAS CORROSION AS MARKED. C-CHECK REPAIRED IAW REO.
Part: SKIN — CORRODED (WING) · airframe 25,158 hrs · 21,257 cycles
LOWER WING PLANK ACCESS HOLE NR 550BB HAS CORROSION AS MARKED. C-CHECK REPAIRED FUEL ACCESS PANEL CUTOUT HOLE NR 550BB IAW REO.
Part: AILERON — CHAFED (LT WING) · airframe 25,158 hrs · 21,257 cycles
LT AILERON LE UPPER SECTION HAS CHAFING ALONG THE INBD SIDE TO THE OTBD SIDE OF THE AILERON. C-CHECK BLENDED & RESTORED FINISH ON LT AILERON LE UPPER SECTION IAW REO.
Part: SKIN — GOUGED (FUSELAGE) · airframe 25,158 hrs · 21,257 cycles
MAIN AVIONICS DOOR CUTOUT SURROUND STRUCTURE AT APPROXIMATELY FS 364.00 TO 394.00 HAS NICKS & GOUGES FROM FWD TO AFT SECTIONS OF CUTOUT. C-CHECK REMOVED DAMAGE FROM SKIN AT AVIONICS DOOR CUTOUT IAW REO.
Part: BATTERY PACK — FAILED (CABIN) · airframe 24,648 hrs · 20,735 cycles
EMERGENCY LIGHTS CAME ON FOR A FEW SECONDS AND THEN SHUTOFF. REPLACED ALL 4 ELBPS IAW AMM, PN: AD-2013-1A, SN ON: 6483, 71068, 60182, 84024, SN OFF: 6872, 66820, 77179, 71081.
2012
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,709 hrs · 19,743 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4642) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,523 hrs · 19,538 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4628) RELAMPED EMERGENCY LIGHT.
Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 23,349 hrs · 19,366 cycles
HYDRAULIC 1 LOW PRESSURE CAUTION WITH PUMP 1B SELECTED ON. (FLT 7812) REPLACED NR 1B HYDRAULIC ELECTRIC PUMP IN REFERENCE TO CRJ 200 AMM. PART OFF: 848847 S/N: MX659234
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,304 hrs · 19,318 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4547) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,954 hrs · 18,991 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4536) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,754 hrs · 18,798 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4740) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,534 hrs · 18,581 cycles
NR 1 AND NR 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,522 hrs · 18,569 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4698) RELAMPED EMERGENCY LIGHT.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,292 hrs · 18,361 cycles
ALL EMERGENCY LIGHTS GO DIM AFTER A FEW SECONDS. (SERVICE) REPLACED ALL 4 ELBP'S.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,292 hrs · 18,361 cycles
EMERGENCY LIGHTS LEFT ON AND ARE NO LONGER WORKING. (FLT 4745) CHARGED EMERGENCY BATTERIES PER AMM AND RELAMPED NR 1 AND NR 3 OVERHEAD EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,155 hrs · 18,236 cycles
THREE EXTERIOR EMERGENCY LIGHTS ON LEFT SIDE OF AIRCRAFT ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,155 hrs · 18,236 cycles
NR 2 AND 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4809) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,130 hrs · 18,213 cycles
TWO OVERHEAD EMERGENCY LIGHTS AT ROW 2 AND 10 ARE OUT. (FLT 4553) RELAMPED EMERGENCY LIGHTS.
2011
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,324 hrs · 17,440 cycles
(C-CHECK) FS 559 BULKHEAD CRACKED AT RIGHT SIDE. REPAIRED PER REO.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,324 hrs · 17,440 cycles
FS 621 BULKHEAD WEB FORWARD FACE ABOVE UPPER CARGO DOOR TRACK CRACKED. (C-CHECK) REPAIR PER REO.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,990 hrs · 18,072 cycles
FS 559.0 PRESSURE BULKHEAD CRACKED AT RT SIDE. (C-CHECK) REPAIRED PER REO.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,896 hrs · 17,054 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4619) RELAMPED EMERGENCY LIGHT.
Part: APU — MALFUNCTIONED (APU BAY) · airframe 20,841 hrs · 17,004 cycles
EVIDENCE OF SMOKE WHEN RIGHT PACK IS TURNED ON. (FLT 4449) REPLACED APU ASSEMBLY. P/N 3800488-3, S/N ON P-1196, S/N OFF P-1064.
2010
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,319 hrs · 15,688 cycles
FORWARD PRESSURE BULKHEAD AROUND PARK BRAKE CABLE ROUTING HOLE CRACKED. (SERVICE CHECK) REPAIRED PRESSURE BULKHEAD PER REO.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,712 hrs · 15,137 cycles
EXTERIOR EMERGENCY LIGHT ON RIGHT SIDE BY SERVICE DOOR INOP. (FLT 4800) RELAMPED EMERGENCY LIGHT.
Part: WIRE HARNESS — BURNED (HYDRAULIC PUMP) · airframe 18,141 hrs · 14,626 cycles
HYDRAULIC PUMP 3A WIRE HARNESS WIRES BURNT. (FLT 4527) REPLACED WIRING HARNESS.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,603 hrs · 14,195 cycles
NR 1 AND NR 3 CABIN CEILING EMERGENCY LIGHTS INOP. (FLT 4657)RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,247 hrs · 13,904 cycles
NR 2 OVERHEAD EMERGENCY LIGHT INOP. (FLT 4717) RELAMPED EMERGENCY LIGHT.
Part: FITTING — CRACKED (FUSELAGE) · airframe 17,014 hrs · 13,715 cycles
FS 621 BULKHEAD LINTEL FITTING CRACKED. (C CHECK) REPAIR PER REO IN PROGRESS.
Part: FITTING — CRACKED (FUSELAGE) · airframe 17,259 hrs · 13,916 cycles
FS 621 LINTEL FITTING CRACKED. (C-CHECK) REPAIRED PER REO 601R-53-61-1230.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 17,259 hrs · 13,916 cycles
FS 484 RIVETS AND BRACKET CRACKED. (C CHECK) REPAIRED PER SRM.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 17,259 hrs · 13,916 cycles
FS 621 FLOOR SUPPORTS AND CLIPS CRACKED. (C CHECK) REPAIRED PER SRM.
Part: SUPPORT — CRACKED (FUSELAGE) · airframe 17,259 hrs · 13,916 cycles
FS 280 SUPPORT AND CLIPS CRACKED. (C CHCECK) REPAIRED PER REO.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,760 hrs · 13,525 cycles
FLT 4458, CABIN EMERGENCY LIGHTS INOP. RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,557 hrs · 13,354 cycles
AFT MOST EMERGENCY CEILING LIGHT INOP. (FLT 4605) RELAMPED EMERGENCY LIGHT.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 16,376 hrs · 13,214 cycles
FLT 4426 - EMERGENCY FLOODLIGHT INOP. RELAMPED.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,718 hrs · 12,718 cycles
FLT 4407 - CEILING EMERGENCY FLOODLIGHT AT ROW 10 INOPERATIVE. RELAMPED.
2008
Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,458 hrs · 12,517 cycles
FLT 4502 - EMERGENCY LIGHT FORWARD CABIN INOP. RELAMPED.
Part: BUSHING — CORRODED (RT ENGINE MOUNT) · airframe 15,275 hrs · 12,363 cycles
RIGHT ENGINE FORWARD MOUNT YOKE UPPER LINK BUSHINGS CORRODED, AD INSP, REPLACED.
Part: BUSHING — CORRODED (LT ENGINE MOUNT) · airframe 15,275 hrs · 12,363 cycles
LEFT ENGINE FORWARD MOUNT YOKE UPPER LINK BUSHINGS CORRODED. AD INSP, REPLACED.
Part: STRINGER CLIP — CRACKED (BS 624 S14L) · airframe 15,275 hrs · 12,363 cycles
STRINGER CLIP AT FRAME 624 TO STRINGER 14 LEFT SIDE CRACKED. AD INSP, REPLACED.
Part: STRINGER CLIP — CRACKED (BS 624 S14R) · airframe 15,275 hrs · 12,363 cycles
STRINGER CLIP AT FRAME 624 TO STRINGER 14 RIGHT SIDE CRACKED. AD INSP, REPLACED.
Part: SUPPORT BEAM — CRACKED (ENGINE) · airframe 15,275 hrs · 12,363 cycles
ENGINE SUPPORT BEAM CRACKED. AD INSP, REPAIRED PER REO.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,219 hrs · 12,318 cycles
LAST OVERHEAD EMERGENCY LIGHT INOP. (FLT 4416)RELAMPED.
Part: LINE — FAILED (RT A/C PACK) · airframe 15,129 hrs · 12,248 cycles
FLT 3766 - AT 300 AGL RECEIVED "SMOKE TOILET" CAUTION MESSAGE. FOUND OVERBOARD DRAIN RESTRICTOR LINE ON RIGHT PACK CAUSING LARGE BLEED AIR LEAK INTO APU BAY. RAN RIGHT ENGINE AND PACK, NO SMOKE NOTED. REPLACED DRAIN RESTRICTOR LINE.
Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 14,809 hrs · 11,991 cycles
RECEIVED A CARGO SMOKE INDICATION ON TAXI IN AND BOTH BOTTLES DISCHARGED. INSPECTED SYSTEM AND REPLACED NR 2 SMOKE DETECTOR IAW AMM 26-15-01. REMOVED AND REPLACED BOTH CARGO FIRE BOTTLE ASSEMBLIES IAW AMM 26-25-01. OPS CHECK GOOD. P/N 473547-19, S/N OFF 1861.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,704 hrs · 11,901 cycles
FWD CEILING EMERGENCY EXIT LIGHT IS INOP. (FLIGHT NR 4096) REPLACED NR 2 CHARGER ASSEMBLY IAW MM 33-51-00. OPS CHECK GOOD.
Part: COALESCER BAG — DIRTY (CABIN AIR) · airframe 14,054 hrs · 11,382 cycles
FLT 3758 - RECEIVED A "SMOKE TOILET" MESSAGE ON ROTATION. REPLACED RIGHT ACM IAW CRJ MM 21-51-10 AND REPLACED BOTH COALESCER BAGS AS REQUIRED. NO DISCREPANCIES NOTED.
Part: GEARBOX — STUCK (THROTTLE CONTROL) · airframe 13,945 hrs · 11,300 cycles
FLT 3921 - LEFT THRUST LEVER WOULD NOT RETURN TO FLIGHT IDLE. REPLACED LEFT ENGINE THROTTLE CONTROL CABLE IAW MM 76-11-09 AND REPLACED LEFT ENGINE THROTTLE GEARBOX IAW 76-11-17.
Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 13,407 hrs · 10,905 cycles
RECEIVED A SMOKE TOILET MESSAGE AFTER TAKE OFF, FLIGHT NR 3942. INSPECTED AREA AND OPERATIONALLY CHECKED LAVATORY SMOKE DETECTOR. NO DISCREPENCIES NOTED.
2007
Part: BRACKET — CRACKED (BRAKE XDUCER) · airframe 13,309 hrs · 10,833 cycles
RIGHT FORWARD BRAKE TRANSDUCER BRACKET IS CRACKED, FOUND AT C-CHECK. REPLACED BRAKE TRANSDUCER BRACKET PER CRJ200 SRM REF 51-42-06.
Part: STIFFENER — CRACKED (DOOR FRAME) · airframe 13,309 hrs · 10,833 cycles
FORWARD LOWER CARGO DOOR FRAME STIFFENERS ARE CRACKED, FOUND AT C-CHECK. REPLACED FORWARD LOWER CARGO DOOR TRACK CHANNEL AS PER CRJ200 SRM 51-41-02 PGS 1-18 AND 51-40-02 PGS 1-18.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,309 hrs · 10,833 cycles
LEFT SIDE OF FS 280 UPPER FLOORBEAM ANGLE IS CRACKED AT LBL12, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO 601R-53-11-138 STEP 7.
Part: BOX BEAM — CRACKED · airframe 13,309 hrs · 10,833 cycles
RIGHT SIDE OF ENGINE BOX BEAM SHOWS SIGNS OF CRACK AT ACCESS HOLE, FOUND AT C-CHECK. INSTALLED REPAIR PARTS IAW REO 601R-53-61-358 PG 1-4 REV A.
Part: PUMP — LEAKING (HYD SYSTEM) · airframe 10,771 hrs · 8,925 cycles
HYDRAULIC SYSTEM LOST ALL QUANTITY EN ROUTE. REPLACED LEFT ENGINE EDP IAW 29-13-00 AND CARBON SEALS ON EDP, AIR TURBINE STARTER AND IDG IAW RII 72-900-1000 AND MM 25-61-00. OPERATIONAL AND LEAKS CHECKS GOOD, S/N OFF MX-574191.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 10,520 hrs · 8,746 cycles
RIGHT WINDSHIELD CRACKED. REPLACED RIGHT WINDSHIELD IAW CRJ MM 56-11-01 AND RII 56-220-1000. OPS CHECKS GOOD. P/N OFF: NP139321-003 S/N OFF: 02248H5152.
2006
Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,699 hrs · 8,141 cycles
OVERHEAD EMERG EXIT LIGHT (FORWARD) INOP. REPLACED FLOOR LEVEL ENTRY FLOOD LIGHT IAW MM 33-51-19. OPERATIONAL CHECKS GOOD, P/N:BR9279-232.
Part: CHARGER — FAILED (CABIN) · airframe 9,699 hrs · 8,141 cycles
OVERHEAD EMERGENCY LIGHT IN MID CABIN DOES NOT ILLUMINATE. REPLACED NR 2 BATTERY CHARGER IAW 33-57-05. OPERATIONAL CHECKS GOOD, P/N ON: 11-0049.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 9,326 hrs · 7,857 cycles
CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED NR 2 EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECKS GOOD IAW MM 33-51-05, PN 11-0049, SN OFF 19746.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,949 hrs · 7,563 cycles
LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BULB. OPERATIONAL CHECKS GOOD, PN 1317.
Part: WARNING MESSAGE — FALSE ACTIVATION (THRUST REVERSER) · airframe 8,459 hrs · 7,185 cycles
RIGHT REV UNLOCKED MESSAGE INFLIGHT. EMERGENCY STOW AND SHUT RIGHT ENGINE DOWN PER QRH SINGLE ENGINE PROCEDURES. PERFORMED FUNCTIONAL TEST ON RIGHT THRUST REVERSER AND PDU WITH SHOP AIR AND AIRCRAFT SYSTEM IAW 78-30-00, OPERATIONAL CHECK GOOD.
Part: FITTING — CRACKED (FLOORBEAM) · airframe 9,231 hrs · 7,781 cycles
STA 280 RBL 9 BOTH FLOORBEAM CLIPS CRACKED RT SIDE I/B AND O/B, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED 2 ANGLE BRACKETS P/N 601R3113-58 IAW CRJ200 SRM 51-42-13;52-42-21 AND STANDARD REPAIR 601R 53-0057A.
Part: FITTING — CRACKED (FUSELAGE) · airframe 9,231 hrs · 7,781 cycles
FS 484.0 LBL27 INBD CLIP ON INTERCOSTAL IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED P/N 601R 31171-17 CLIP ON INTERCOSTAL AT FS484 LBL27 IAW 601R 53-41-059.
Part: SUPPORT BEAM — CRACKED (LT ENGINE) · airframe 9,231 hrs · 7,781 cycles
LT ENGINE SUPPORT BEAM FS 625.30 LBL 36.20 WL 111.09 LOWER WEB INBD FWD CORNER AT ACCESS PANEL CRACKED. FABRICATED AND INSTALLED 601R-53-61-358-1 REPAIR DOUBLER FROM 2024-T3 .071' PO 59134 IAW CRJ200 REO 601R-53-61-358.
Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 8,295 hrs · 7,055 cycles
LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED LEFT OVERWING EMERGENCY EXIT FWD LIGHT IAW 33-21-01.
Part: SWITCH — INOPERATIVE (COCKPIT) · airframe 8,166 hrs · 6,963 cycles
CAPTAINS STAB TRIM DISCONNECT SWITCH INOP. REPLACED THE CAPTIANS DISCONNECT SWITCH ASSY. OPERATIONAL CHECK GOOD.
2005
Part: FLAP SYSTEM — WARNING LIGHT (TE FLAPS) · airframe 7,598 hrs · 6,532 cycles
FLIGHT 5901 - FLAPS FAIL CAUTION. RESEST FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
Part: CONTROL LEVER — FAULTY (COCKPIT) · airframe 7,598 hrs · 6,532 cycles
FLIGHT 5114- FLAPS FAIL CAUTION. REPLACED THE FLAP CONTROL LEVER.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 7,490 hrs · 6,430 cycles
FLIGHT 5208 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
Part: ACTUATOR — LACK OF LUBE (TE FLAPS) · airframe 7,248 hrs · 6,215 cycles
FLIGHT 5711 - FLAPS FAIL CAUTION. LUBRICATED THE RIGHT WING FLAP ACTUATORS.
Part: COUPLING — WORN (TE FLAPS) · airframe 7,235 hrs · 6,203 cycles
FLIGHT 5228 - FLAPS FAIL CAUTION. REPLACED 5 FLEX DRIVE CABLES ON LT WING AND 3 FLEX DRIVE CABLES ON RT WING.
Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 7,171 hrs · 6,145 cycles
FLIGHT 5023 - FLAPS FAIL CAUTION. REPLACED THE FECU.
Part: ACTUATOR — FAILED (T/E FLAP)
FLT 4573 - DURING APPROACH INTO YYZ FROM ATL, THE CREW RECEIVED A FLAPS FAIL MESSAGE WITH THE LEFT FLAP AT THREE DEGREES AND THE RIGHT FLAP AT FOUR DEGREES. THE QRH WAS COMPLIED WITH AND EMERGENCY EQUIPMENT WAS REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN YYZ. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT INBOARD AND OUTBOARD FLAP ACTUATORS. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT LANDED SAFELY IN YYZ. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT INBOARD AND OUTBOARD FLAP ACTUATORS. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
2004
Part: LIGHT — INOPERATIVE (CABIN)
DURING A (C) CHECK, THE FORWARD 3 SECTIONS OF EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD 3 SECTIONS OF EMERGENCY FLOOR LIGHT STRIPS. OPERATIONAL CHECKS GOOD.