N898SK
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.
118 reports on file, 2013-08-01 – 2026-07-21.
Part: UNKNOWN — ODOR (CABIN) · airframe 32,674 hrs · 26,081 cycles
AFT FLIGHT ATTENDANT REPORTED STARTING TO SMELL A BURNING ODOR DURING FINAL APPROACH COMING FROM LAVATORY. DESCRIBED IT AS SIMILAR TO OIL BURNING AND SAID IT DID NOT SMELL LIKE VAPING OR CIGARETTE SMOKE. SMOKE DETECTOR DID NOT ACTIVATE. UPON REACHING GATE, HE OPENED THE LAV DOOR AND SAW SOME WHITISH VAPOR NEAR CEILING, WHICH RAPIDLY DISSIPATED. NOTHING WAS FOUND IN THE TRASH RECEPTACLE AND NO OBVIOUS SOURCE. (FLIGHT 3651)
Part: FIRE DETECTOR — FAULTED (ZONE 400) · airframe 32,190 hrs · 25,516 cycles
IN FLIGHT RECEIVED RT ENGINE FIRE WARNING MESSAGE, COMPLIED WITH QRC AND QRH. ENGINE WAS SHUTDOWN IN FLIGHT. (FLIGHT 3500) PERFORMED AN INSPECTION OF THE RT ENGINE THAT HAVE SALT WATER OR FIRE EXTINGUISHANT CONTAMINATION IAW AMM 72-00-00, NO DEFECTS NOTED. PERFORMED A FUEL OIL LEAK CHECK IAW AMM 71-00-00, NO LEAKS NOTED AT THIS TIME. PERFORMED A DETAILED INSPECTION OF THE RIGHT ENGINE FIRE-DETECTION SENSING ELEMENTS IAW AMM 26-11-00, AND FOUND NO DEFECTS NOTED. REFERENCE AML 1868377 FOR PARTS, LABOR, TROUBLESHOOTING AND THE REPLACEMENT OF THE RH ENGINE LOOP B A238. WHILE TROUBLESHOOTING RH ENGINE FIRE DETECTION LOOP B, ALSO FOUND RT ENGINE FIRE DETECTION LOOP A OPEN. RESECURED RT ENGINE LOOP A A234 CONNECTION 6 IAW AMM 26-11-05. PERFORMED AN OPERATIONAL CHECK OF THE FIREX DETECTION SYSTEM IAW AMM 26-10-00, OPS CHECK GOOD AT THIS TIME.
Part: PSEU — FAULTED (ZONE 700) · airframe 32,082 hrs · 25,402 cycles
GEAR UP DISAGREE FOR NLG UPON RE-TRACTION. RAN QRH, GEAR DEPLOYED AND LOCKED WITH ALL INDICATIONS GREEN. RETURNED TO FIELD. (FLIGHT 4081) FOUND THE FOLLOWING B1 CODES AT TIME OF EVENT 007451 065387 065386 007427 007432. TROUBLESHOT GEAR DISAGREE IAW FIM 32-21-00. PERFORMED FAULT ISOLATION ACTIONS PER FIM. PERFORMED MULTIPLE GEAR SWINGS & ALTERNATE RELEASE, IAW AMM 32-30-00 & AMM 32-34-00, COULD NOT DUPLICATE FAULT & OPS CHKD GOOD. OPS CHKD PRIORITY VALVE IAW AMM 29-12-05, OPS CHKD GOOD. NO REPEAT FAULT HISTORY IN ACFT LOGS OR MDC FOUND. DUE TO MULTIPLE PROX SENSORS FLAGGED DURING FAULT, R & R PSEU IAW AMM 32-61-01, OPS CHKD GOOD. PERFORMED ADDITIONAL GEAR SWINGS, OPS CHKD GOOD & NO DEFECTS NOTED.
Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 900) · airframe 32,063 hrs · 25,380 cycles
GEAR UP DISAGREE FOR NLG UPON RETRACTION. RAN QRH, GEAR DEPLOYED & LOCKED WITH ALL INDICATIONS GREEN. RETURNED TO FIELD. FOUND THE FOLLOWING B1 CODES AT TIME OF EVENT 007451 065387 065386 007427 007432. DEFERRED MLG RETRACTION SYSTEM IAW MEL 32-30-1 MX ACTIONS C/W PLACARDS INSTALLED.
Earlier reports · 2013–2025 · 114 reports
2025
Part: LINTEL — DAMAGED (ZONE 800) · airframe 31,709 hrs · 24,999 cycles
COMPLY WITH REO 670-53-21-493 REV -D 2015-07-10 REPAIRS TO PAX DOOR LINTEL (STR.3L) BTW FS 280 & 295 (C-CHECK) COMPLIED WITH REPAIRS TO PAX DOOR LINTEL (STR.3L) BTW FS 280 & 295 IAW ALL STEPS OF REO 670-53-21-493 REV-D, DATED 2015-07-10. COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK TEST GOOD.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
CORROSION ON STRINGER SPLICE 25L BTWN BS 333 AND 319.70. (C-CHECK) REMOVED AND INSTALLED NEW STRINGER SPLICE 25L AT FS 333 IAW SRM 51-42-06-001-001-A01 AND DRAWING SH670-32420, REV E, SHEETS 1, AND 3. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
CORROSION ON STRG 19R BTWN STA 597.00 AND ASTA 613.00 (C-CHECK) COMPLIED WITH DISPOSITION FOR STRINGER SPLICE REPAIR ON STR19R BTWN FS581.00 & FS613.00 (DEVIATION TO SRM 53-00-03-201-001-A02) IAW REO 690-53-31-1032 REV -- DATED 2025-07-14 CRJ900 SRM 53-00-03-201-001-A02, CRJ900 SRM 51-42-06-001-001-A01, AND CRJ900 SRM 51-42-21-001-001-A01. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY. LEAK CHECK GOOD.
Part: STRINGER — CORRODED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
CORROSION ON STRINGER 26R BTWN BS 295 & 310. (C-CHECK) REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG SH670-31630 REV. K SHEET 1.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. MAJOR REPAIR.
Part: CHANNEL — CORRODED (ZONE 200) · airframe 31,709 hrs · 24,999 cycles
CORROSION ON INTERNAL TCAS LOWER CHANNEL BETWEEN BS 295 AND 310 AND BTWN S26R - 26L. (C-CHECK) REMOVED AND INSTALLED NEW TCAS CHANNEL IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG SH670-30023, REV G. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY.
Part: FRAME — CORRODED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
UPON REMOVAL FRAME SECTION AT FS969 BETWEEN STGR19R AND STRG24R FOUND MULTIPLES SPOTS OF CORROSION ON FRAME. (C-CHECK) COMPLIED WITH REPAIR FOR CORROSION DAMAGE ON LOWER FRAME FS969.00 BETWEEN STR20R-STR25R. REF REO 690-53-51-487 REV -- DATED: 2025-07-28. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY. LEAK CHECK GOOD.
Part: DRAG ANGLE — CRACKED (ZONE 200) · airframe 31,709 hrs · 24,999 cycles
DURING RH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE REMOVAL FIND CRACK ON RH VERT STAB-TO-FUSELAGE FWD DRAG ANGLE #30352476 (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 31,709 hrs · 24,999 cycles
DURING RH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE REMOVAL FIND CRACK ON RH VERT STAB-TO-FUSELAGE FWD DRAG ANGLE #30352476 (C-CHECK RO 08/29/2025)BLENDED CORRODED AREA OF LH WING FUEL ACCESS PANEL LANDING 510AB IN REFERENCE WITH REO 601R-57-21-030 REV. -L, DATED 2014-02-05. PERFORMED UT REMAINING THICKNESS INSPECTION WITH REFERENCE TO NDTM PART 4 51-00-001 AND FOUND TO BE WITHIN LIMITS OF 601R-57-21-030 REV. -L, DATED 2014-02-05. PERFORMED ROTO PEENING IN REF WITH REO 601R-57-21-030 REV. -L, DATED 2014-02-05. APPLIED SURFACE FINISH AS REQUIRED PER REO. COMPLETED CORROSION FINDINGS REPORT. REFERENCE CP 30350391 FOR EDDY CURRENT INSPECTION.
Part: FRAME — CORRODED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
SECTION FRAME AT FS 319.70 BETWEEN STGR 18L - STGR 21L HAS CORROSION TRANS #30300252 (C-CHECK) REMOVED AND INSTALLED NEW FRAME FS 319.70 STGR 18L -STGR 21L REF CRJ900 SRM 51-42-06-001-001-A01 DWG SH670-31810 REV AE COMPLIED WITH 51-900-1002-SKY
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 31,709 hrs · 24,999 cycles
RIGHT FLOOR SUPPORT ANGLE OF CENTER COCKPIT FLOOR IS CRACKED. (C-CHECK) REMOVED AND REPLACED RT FLOOR SUPPORT ANGLE OF CENTER COCKPIT FLOOR IAW SRM 53-11-10-201-006-A01.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY MAJOR REPAIR.
Part: BRACKET — BENT (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
S/N 0755AFT BAGGAGE BAY UNDERFLOOR, BS 1031 - 1047, STRINGER 27L. THEIRS A BENT BRACKET. (C-CHECK) REMOVED AND REPLACED WITH NEW NEW BRACKET ON AFT BAGGAGE BAY UNDERFLOOR, IAW SRM 51-42-06-001-001-A01, REV 38 AND DWG MM670-36084, REV D. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 31,709 hrs · 24,999 cycles
LH FLOOR SUPPORT ANGLE OF CENTER COCKPIT FLOOR IS CRACKED. (C-CHECK) REMOVED AND REPLACED LT FLOOR SUPPORT ANGLE OF CENTER COCKPIT FLOOR IAW SRM 53-11-10-201-006-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. MAJOR REPAIR.
Part: HINGE — GOUGED (ZONE 200) · airframe 31,709 hrs · 24,999 cycles
FUSELAGE SIDE AFT LUG LANDING ON PIANO HINGE IS GOUGED. (C-CHECK) REMOVED PAX DOOR PIANO HINGE FUSELAGE SIDE IAW SRM 53-21-23-201-007-A01, AND INSTTALLED NEW PAX DOOR PIANO HINGE OF FUSELAGE SIDE IAW SRM 53-21-23-201-007-A01, SRM 51-42-21-001-001-A01, AND DWG SH670-31810 REV Y. LEAK TESTED GOOD IAW AMM 21-31-00-910-801 (A02). COMPLIED WITH 51-900-1002-SKY.
Part: SKIN — CHAFED (ZONE 600 AILERON) · airframe 31,709 hrs · 24,999 cycles
RIGHT WING AILERON HAS CHAFING ON THE LOWER LEADING EDGE, (C-CHECK) REMOVED AND WET INSTALLED NEW REPLACEMENT INBD & OUTBD L/E LOWER PANELS AT RT AILERON REF. SRM TASK 51-42-06-001-001-A01 & SRM TASK 51-42-21-001-001-A01 AND DWG CC670-13000 REV. D. COMPLIED WITH 51-900-1002-SKY.
Part: FRAME — CRACKED (ZONE 200) · airframe 31,709 hrs · 24,999 cycles
BS 333 CRACKED AT APPROXIMATELY STRINGER 0. (C-CHECK) REPAIRED FRAME AT BS 333 AT APPROXIMATELY STR 0 IAW REO 690-53-21-1972, REV-. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.
Part: FLOOR SKIN — CRACKED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
LEFT SIDE FWD EQUIPMENT COMPARTMENT TRU BAY FLOOR WEB IS CRACKED IN THE RADIUS. (C-CHECK). REPAIRED LHS FWD EQUIPMENT COMPARTMENT TRU BAY FLOOR WEB IAW GREO 670-53-11-509, REV -E. ALL APPLICABLE STEPS OF GREO COMPLETED FOR A LEFT REPAIR.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 31,709 hrs · 24,999 cycles
INTERNAL STRUCTURE OF THE REAR FUSELAGE - FLOOR CROSS BEAM FS1047 LT HAS PITTING CORROSION. FLAGGED (C-CHECK) REMOVED CORROSION ON FLOOR CROSS BEAM FS1047 BETWEEN LBL27 AND LBL35 REF CRJ900 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS REF CRJ900 SRM 53-61-43-101-001-A02. REPAIRED FLOOR CROSS BEAM FS1047 LH SIDE REF REO 690-53-61-1643 REV -- DATED 2025-07-04. COMPLIED WITH ALL STEPS OF REO 690-53-61-1643 REV -- DATED 2025-07-04. COMPLIED WITH 51-900-1002-SKY
Part: TIE DOWN — CORRODED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
TIEDOWN FITTING AT BS 565 BETWEEN STR 22L - 23L IS CORRODED. (C-CHECK) REMOVED AND REPLACED TIEDOWN FITTING AT BS 565 BETWEEN S22L AND 23L. IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01, AND DWG SH690-33600, REV AH. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. MAJOR REPAIR.
Part: SHAFT — DENTED (ZONE 600 FLAP) · airframe 31,709 hrs · 24,999 cycles
RIGHT INBD FLAP, OTBD VANE ACTUATOR SHAFT HAS INDENT. (C-CHECK) BLENDED OUT THE DAMAGE ON RT INBD FLAP, OTBD VANE ACTUATOR SHAFT IAW REO 670-57-52-257, REV A. FOUND TO BE IN LIMITS IAW REO 670-57-52-257, REV. A. COMPLIED WITH ALL STEP OF REO 670-57-52-257 REV. A. OPS CHECKED GOOD. COMPLIED WITH 51-900-1002-SKY
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 31,709 hrs · 24,999 cycles
INTERNAL STRUCTURE OF THE REAR FUSELAGE - FLOOR SUPPORT BS 985 TO 1098.20, RBL 9, FLOOR SUPPORT HAS CORROSION PITTING. (C-CHECK) REPAIRED CORROSION ON FLOOR SUPPORT AT FS 985 TO1098.2 & RBL 9. IAW SRM 51-42-21-01-01-A01, SRM 53-00-41-201-001-A03 , REO 690-53-61-1632 REV-, AND DWG MM690-35041, REV AB. COMPLIED WITH SKY CARD 51-900-1002-SKY.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 31,709 hrs · 24,999 cycles
INTERNAL STRUCTURE OF THE REAR FUSELAGE - FLOOR SUPPORT FS1015.00 TO FS1098.20 LBL27 FLOOR SUPPORTHAS CORROSION PITTING. (C-CHECK) REMOVED CORROSION AT FLOOR SUPPORT FS1051.00 TO FS1098.20 & LBL27 REF CRJ900 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE FOUND IAW SRM 56-61-43-101-001-A02. RECEIVED AND COMPLIED WITH STEPS 1-6 OF REO 690-53-61-1634, REV-. COMPLIED WITH 51-900-1002-SKY.
Part: SHAFT — DENTED (ZONE 600 FLAP) · airframe 31,709 hrs · 24,999 cycles
RIGHT INBD FLAP, SECOND FROM OTBD VANE ACTUATOR SHAFT HAS A DENT. (C-CHECK) REMOVED, REPAIRED, AND REINSTALLED RT INBD FLAP OTBD VANE ACTUATOR SHAFT IAW SRM 51-41-02-001-001-A01, ALL STEPS (1-5) OF REO 670-57-52-257, REV -A,, & DRAWING CC670-14303, REV -B. OPS TEST OF THE FLAP AND SLAT SYS COMPLETED IAW AMM 27-50-00-710-801-A02. OPS TESTED BAD. WHEN FLAPS/SLATS RETURNED TO THE FULLY RETRACTED POSITION A FLAP HALF-SPEED INDICATION WAS DISPLAYED ON EICAS. COMPLETED SKYWEST TASKCARD 51-900-1002-SKY.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 31,709 hrs · 24,999 cycles
INTERNAL STRUCTURE OF THE REAR FUSELAGE - FLOOR SUPPORT FS985.00 TO FS1098.20, LBL9. FLOOR SUPPORT HAS CORROSION PITTING. (C-CHECK) REMOVED AND INSTALLED NEW FABRICATED FLOOR SUPPORT SECTION LBL 9.0 FROM BS 977 TO BS 1080 AND REPAIR PARTS REF SRM 53-00-41-201-001-A03, STEPS 5.B. 10 &14 & 16 & 19, REO 690-53-61-1632, REV -. AND DWG MM690-35041, REV AB. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY.
Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
R/H SIDE FWD EQUIPMENT COMPARTMENT AFT DOOR LATCH CUTOUT HAS A SUSPECTED CRACK ON THE DOOR LANDING. (C-CHECK RO 11/25/2025)REMOVED AND INSTALLED NEW RT SIDE FWD EQUIPMENT COMPARTMENT AFT DOOR LANDING IAW CRJ900 SRM 51-42-06-001-001-A01 AND REO 690-53-11-2033 REV -- DATE 2025-07-01. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY.
Part: FLOORBEAM — CORRODED (ZONE) · airframe 31,709 hrs · 24,999 cycles
FLOORBEAM BS 985 TO 1098.20, RBL 27 HAS CORROSION PITTING. CIRCLE WITH BLACK GREASE PENCIL. (C-CHECK) COMPLIED WITH DISPOSITION FOR BLENDED CORROSION DAMAGE TO RBL 27.FLOORBEAM BETWEEN BS 1069.75 & 1088.20 IAW SRM 53-00-41-201-001-A03, REV 38. AND REO 690-53-61-1644 REV-. COMPLIED WITH 51-900-1002-SKY.
Part: STRIKER — DENTED (ZONE 200) · airframe 31,709 hrs · 24,999 cycles
BS 310 SEAL STRIKER DENTED.UPPER FWD FITTING. (C-CHECK) REPAIRED PAX DOOR FWD UPPER SEAL STRIKER BS 310 IAW SRM 53-21-23-201-006-A01. COMPLIED WITH 51-900-1002-SKY.
Part: SHAFT — DENTED (ZONE 600 FLAP) · airframe 31,709 hrs · 24,999 cycles
RIGHT INBD FLAP, INBD VANE ACTUATOR SHAFT HAS A DENT. (C-CHECK) REMOVED, REPAIRED, AND REINSTALLED RT INBD FLAP INBD VANE ACTUATOR SHAFT IAW SRM 51-41-02-001-001-A01, ALL STEPS (1-5) OF REO 670-57-52-257, REV -A, AND DRAWING CC670-14303, REV -B. OPS TEST OF THE FLAP AND SLAT SYSTEM COMPLETED REF AMM 27-50-00-710-801-A02. OPS TESTED BAD. WHEN FLAPS/SLATS RETURNED TO THE FULLY RETRACTED POSITION A FLAP HALF-SPEED INDICATION WAS DISPLAYED ON EICAS. COMPLETED SKYWEST TASKCARD 51-900-1002-SKY.
Part: SKIN — DAMAGED (ZONE 600 SLAT) · airframe 31,709 hrs · 24,999 cycles
RIGHT WING, UNDER PANEL 631BZ HAS TOOLING DAMAGE. (C-CHECK) COMPLIED WITH DISPOSITION FOR BLENDED TOOL DAMAGE TO RT NR 2 SLAT AFT SKINS BETWEEN SS 261.25, TRACK 2-2, AND BETWEEN SS 315.75, TRACK 2-3 IAW REO 690-57-42-1237, REV-. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY.
Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 31,709 hrs · 24,999 cycles
RIGHT VERT STAB-TO-FUSELAGE AFT DRAG ANGLE, THE AFT END POSSIBLE CRACKED. (C-CHECK) REMOVED AND REPLACED WITH NEW RT VERT STAB-TO-FUSELAGE AFT DRAG ANGLE. IAW DWG BA670-35002, REV -F, SRM 51-42-21-001-001-A01, SRM 51-42-13-001-001-A01 AND SRM 51-42-22-001-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.
Part: SKIN — DAMAGED (ZONE 600 SLAT) · airframe 31,709 hrs · 24,999 cycles
RIGHT WING, UNDER PANEL 622CZ HAS TOOLING DAMAGE, (C-CHECK) REPAIRED RIGHT WING SLAT NR 1 AFT SKIN, UNDER PANEL 622CZ REF. REO 690-57-42-1238 REV-.
Part: SKIN — CRACKED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
LEFT TRU BAY ACCESS, LOWER AFT CORNER OF THE FUSELAGE SKIN POSSIBLE CRACK IN RADIUS. (C-CHECK) REPAIRED LT TRU BAY ACCESS THE LOWER AFT CORNER OF THE FUSELAGE SKIN IAW REO 690-53-11-2023 REV-. COMPLIED WITH ALL STEPS OF REO 690-53-11-2023 REV-. COMPLIED WITH 51-90-1002-SKY
Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 31,709 hrs · 24,999 cycles
LH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE, THE FWD END POSSIBLE CRACK (MARKED) (C-CHECK RO 11/25/2025)REMOVED AND INSTALLED NEW AFT DRAG ANGLE PN# AV670-21186-003 ON LH VERTICAL STABILIZER REF CRJ900 SRM 51-42-13-001-001-A01, CRJ900 SRM 51-42-22-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG BA670-35002 REV -F, COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY, AND M-337
Part: FRAME — CORRODED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
BS 969 FRAME WEB ON THE FWD SIDE AT STRINGER 26R AND THE ATTACHED FLANGE BETWEEN STRINGER 26 - 27R ARE CORRODED. (C-CHECK) PERFORMED CUT-AWAY OF DAMAGED FRAME SECTION ON FRAME BS 969 FROM STR 25R TO STR 25L. IAW SRM 53-00-06-201-001-A03, FIGURE 53-00-06-991-879. INSTALLED FABRICATED REPAIR SPLICE FRAMES AND CLEATS (2 EA) ON REWORKED AREA AT FRAME BS 969 FROM STR 25R TO STR 25L. IAW SRM 53-00-06-201-001-A03 FIGURE 53-00-06-991-879 AND DWG# SH690-37060 REV. AC. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY. LEAK CHECK GOOD.
Part: SKIN — DAMAGED (ZONE 600 SLAT) · airframe 31,709 hrs · 24,999 cycles
RIGHT WING, UNDER PANEL 631CZ HAS TOOLING DAMAGE, (C-CHECK) COMPLIED WITH DISPOSITION FOR BLENDED TOOL DAMAGE TO RT NR 2 SLAT AFT SKINS BETWEEN SS261.25 - TRACK 2-2, AND BETWEEN SS315.75 - TRACK 2-3 IAW REO 690-57-42-1237 REV- AND SRM 51-12-00-001-001-A01. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY.
Part: FRAME — CORRODED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
BS 942 FRAME WEB ON THE FWD AND AFT SIDES BETWEEN STR 25L &26L AND THE ATTACHED FLANGE BETWEEN STR 25L ̉‰ 25R ARE CORRODED. (C-CHECK) REMOVED AND INSTALLED NEW FRAME SECTION & SPLICES ON BS.942, BETWEEN STGR 25L & 25RT. REF CRJ900 SRM 53-00-06-201-001-A03. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY. LEAK CHECK GOOD.
Part: STRINGER — CORRODED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
STR 20L IS CORRODED BETWEEN FS954 - 969. (C-CHECK) BLENDED CORROSION AT STR 20 AT FS954 TO 969 IAW SRM 51-21-06-001-001-A01. FOUND OUT OF LIMITS. IAW SRM 53-51-03-101-002-A04. REPAIRED STR 20L REF REO 690-53-51-483 REV-. COMPLIED WITH ALL STEPS OF REO 690-53-51-483 REV-. COMPLIED WITH 51-900-1002-SKY
Part: STIFFENER — CHAFED (ZONE) · airframe 31,709 hrs · 24,999 cycles
AFT PRESSURE BULKHEAD STIFFENER LBL 9, AT THE BOTTOM INNER CHAFFED HOLE (MARKED) (C-CHECK). REPAIRED AFT PRESSURE BULKHEAD STIFFENER LBL 9 AT THE BOTTOM INNER CHAFE HOLE. REF REO 690-53-61-1640 REV-. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD.
Part: ATTACH ANGLE — CORRODED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
PANEL 542AZ IN THE LT GEAR WELL, THE ATTACH ANGLE ON THE AFT SIDE OF THE AFT WING SPAR, IS CORRODE ON TOP AND BOTTOM. (C-CHECK) REPLACED NEW ATTACH ANGLE TO LT WHEEL WELL ANGLE COMMON TO PANEL 542AZ IAW SRM, 51-42-21-001-001-A01 AND DWG CC670-10320 REV- F. COMPLIED WITH TASK CARD 51-900-1002-SKY, LEAK CHECKS GOOD.
Part: ATTACH ANGLE — CORRODED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
PANEL 642AZ IN THE RH GEAR WELL, THE ATTACH ANGLE ON THE AFT SIDE OF THE AFT WING SPAR, IS CORRODE ON TOP AND BOTTOM (MARKED) (C-CHECK RO 11/25/2025)REPLACED NEW ATTACH ANGLE TO RH WHEEL WELL ANGLE COMMON TO PANEL 642AZ REF. CRJ-900 SRM, 51-42-21-001-001-A01 AND DWG CC670-10320 REV-F. COMPLIED WITH TASK CARD 51-900-1002-SKY, LEAK CHECKS GOOD.
Part: DOOR FRAME — CRACKED (ZONE 800) · airframe 31,709 hrs · 24,999 cycles
LEFT FWD OVERWING EMERGENCY DOOR UPPER STOP FITTING, POSSIBLE CRACKED ON THE DOOR FRAME. (C-CHECK) REPAIRED CRACK FROM LT FWD OVERWING EMERGENCY DOOR UPPER STOP FITTING, ON THE DOOR FRAME IAW REO 670-52-21-103, REV--, NOTES 1-17. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
Part: STRINGER — CORRODED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
STRINGER 27 AT BS 280 (ADJACENT TO BUTT STRAP) IS CORRODED, AND APPERS TO HAVE MISSING PIECES ALONG EDGE (C-CHECK) REMOVED AND INSTALLED NEW STRINGER 27 BETWEEN FS280 AND FS299. IAW SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01 AND DWG SH670-31630, REV K, SHEET 1.
Part: STOP FITTING — CRACKED (ZONE 800) · airframe 31,709 hrs · 24,999 cycles
LEFT AFT OVERWING EMER DOOR UPPER STOP FITTING, POSSIBLE CRACK ON THE DOOR FRAME. (C-CHECK) REPAIRED CRACK FROM LH AFT OVERWING EMERGENCY DOOR UPPER STOP FITTING, ON THE DOOR FRAME IAW REO 670-52-21-103, REV. --, COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 31,709 hrs · 24,999 cycles
RIGHT FLOOR SILL IS CORRODED AND SCRATCHED FS280 - 319. (C-CHECK) REMOVED AND REPLACED RT FLOOR SILL IAW SRM 51-42-06-001-001-A01, DWG SH670-32170, REV. V & EDRN SH670-32172 REV D . COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY. LEAK CHECK GOOD,
Part: STOP FITTING — CRACKED (ZONE 800) · airframe 31,709 hrs · 24,999 cycles
RIGHT AFT OVERWING EMER DOOR UPPER STOP FITTING, POSSIBLE CRACK ON THE DOOR FRAME. (C-CHECK) REPAIRED CRACK FROM RT AFT OVERWING EMERGENCY DOOR UPPER STOP FITTING, ON THE DOOR FRAME IAW 670-52-21-103, REV -, NOTES 1-17 SEE CONTINUATION CARD FOR WORK DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
Part: SUPPORT — CORRODED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
BACKUP SILL BETWEEN FS310.00 -319.00 STGR21L IS CORRODED. (C-CHECK) REMOVED AND REPLACED WITH NEW BACKUP SILL AT BS 310 - 319, STGR 21L IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31810 REV AECOMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
Part: SKIN — GOUGED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
GOUGE ON OUTER SKIN STGR27 BETWEEN FS913.00 & 927.00. (MARKED) (C-CHECK) COMPLIED WITH REPAIR TO FUSELAGE SKIN AT FS913.00 AND STR 27 REF REO 690-53-51-484 REV -- AND REO 670-53-00-290 REV -F . COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY. LEAK CHECK GOOD.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 31,709 hrs · 24,999 cycles
AFT SIDE OF FS280.00 CROSS BEAM, THE OUTBD ATTACH ANGLE FOR RBL9 FLOOR BEAM CRACKED. (C-CHECK). REMOVED AND REPLACED ATTACH ANGLE P/N CC670-34099-2 AT BS 280, RBL9. IAW SRM 51-42-21-001-001-A01, AND DWG KBA670-30026 REV. J, SHEET 5, 7 AND 9. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. MAJOR REPAIR.
Part: STRIKER — CORRODED (ZONE 800) · airframe 31,709 hrs · 24,999 cycles
SERVICE DOOR LOWER SEAL STRIKER IS CORRODED. (C-CHECK) REMOVED AND REPLACED SERVICE DOOR LOWER NEW SEAL STRIKER P/N: SH670-31412-7 REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG SH670-31950 REV: Y. COMPLIED WITH TASK CARD 51-900-1002-SKY. SERVICE DOOR LEAK CHECK GOOD.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 31,709 hrs · 24,999 cycles
RIGHT COCKPIT FLOORBEAM, RBL 12 POSSIBLE CRACK AT THE AFT END WHERE IT ATTACHES TO BS 280 FLOORBEAM. (C-CHECK) REMOVED AND REPLACED FLOORBEAM SECTION -34 WITH NEW FLOORBEAM SECTION FWD OF BS 280, RBL12. IAW SRM 53-11-43-201-003-A01, REPAIR TYPE 4.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 31,709 hrs · 24,999 cycles
LH COCKPIT FLOOR BEAM LBL12 POSSIBLE CRACK AT THE AFT END WHERE IT ATTACHES TO FS280.00 CROSS BEAM. (C-CHECK) REMOVED AND INSTALLED NEW FLOOR BEAM LBL 12 REF. SRM 53-11-43-201-003-A01 TYPE 4 REPAIR. COMPLIED WITH 51-900-1002-SKY.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 31,709 hrs · 24,999 cycles
FS280.00 COCKPIT FLOOR PANEL AFT ATTACH ANGLE CORRODED (MARKED) (C-CHECK5) REMOVED AND REPLACED FS280 COCKPIT FLOOR PANEL AFT ATTACH ANGLE P/N CC670-34095-1. REF. CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DRAWING CC670-33052 REV. G SHEET 2. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY, STRUCTURAL MAJOR REPAIR.
Part: SUPPORT — CORRODED (ZONE 200) · airframe 31,709 hrs · 24,999 cycles
BACKUP SILL BETWEEN BS 319 -349, S21L IS CORRODED. (C-CHECK) REMOVED AND REPLACED WITH NEW BACKUP SILL BS 319 - 349, S21L IAW SRM 51-42-06-001-001-A01, AND DWG SH670-31810, REV AE. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY, MAJOR REPAIR.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 31,709 hrs · 24,999 cycles
AFT SIDE OF BS 280 CROSSBEAM, THE OUTBD ATTACH ANGLE FOR LBL9 FLOORBEAM CRACKED. (C-CHECK) REMOVED AND REPLACED ATTACH ANGLE AT BS 280, LBL 9. IAW SRM 51-42-21-001-001-A01 AND DWG KBA670-30026, REV. J SHEET 5, 7 AND 9. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
Part: DOOR FRAME — DAMAGED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
MAIN AVIONICS BAY DOOR SURROUND STRUCTURE HAS PITTING AROUND THE PERIMETER OF THE LAND. (MARKED IN RED) (C-CHECK) REMOVED DAMAGE IN MAIN AVIONICS BAY DOOR SURROUND STRUCTURE IAW SRM 51-12-00-001-001-A01. FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE AROUND DOOR CUT OUT IAW CRJ900 SRM 53-21-01-101-006-A04 AND CRJ900 SRM 53-21-01-001-006-A02. RECEIVED AND COMPLIED WITH REO 690-53-21-032, REV.--, DATED 2008/03/07COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY, STRUCTURAL MAJOR REPAIR.
Part: DOOR FRAME — CHAFED (ZONE 200) · airframe 31,709 hrs · 24,999 cycles
CREW ESCAPE HATCH SURROUND STRUCTURE CHUTE BOLT FITTINGS, ON THE FORWARD FRAME, ARE LIGHTLY CHAFED AT THE BOTTOM OF THE FITTING. (C-CHECK) COMPLIED WITH DISPOSITION FOR BLENDED CHAFE DAMAGE TO CREW ESCAPE HATCH FORWARD ALIGNMENT FITTINGS, LT SIDE AND RT SIDE IAW REO 690-53-11-2026, REV-. OPS CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY
Part: SCREW — DAMAGED (ZONE 400) · airframe 31,709 hrs · 24,999 cycles
LEFT UPPER TRANSCOWL HAS 1 EA SHANKED SCREW AT LOCKOUT (C-CHECK) REPAIRED 1 EA. FASTENER HOLE AT LOCKOUT ON LT UPPER TRANSCOWL IAW REO 690-54-21-575, REV-, COMPLIED WITH SKYWEST TASK CARD 51-900-1002 SKY.
Part: TRANSCOWL — CRACKED (ZONE 400) · airframe 31,709 hrs · 24,999 cycles
L/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK) REMOVED AND REPLACED INBD STANDOFF WITH NEW STANDOFF P/N CN624-2082-S0701 REF. REO 670-54-21-971 REV. B, 2023-11-28 AND EO CN624-2005 SNIEO-S07 DATED 2025-06-12 AND ENSURED ALL OTHER DRAWING REQUIREMENTS WERE MET. COMPLIED WITH SKY CARD 51-900-1002-SKY.
Part: STAND OFF — CRACKED (ZONE 400) · airframe 31,709 hrs · 24,999 cycles
RIGHT LWR TRANSCOWL OTBD -A- BRACKET STANDOFF IS CRACKED. (C-CHECK) REMOVED AND REPLACED OUTBD -A- BRACKET ON THE RT LOWER TRANSCOWL. IAW REO 670-54-21-971, REV B, AND DRAWING CN624-2005 SNIEO S08. COMPLIED WITH 51-900-1002 SKY.
Part: STAND OFF — CRACKED (ZONE 400) · airframe 31,709 hrs · 24,999 cycles
R/H LWR TRANSCOWL INBD -A- BRACKET STANDOFF IS CRACKED. (C-CHECK) REMOVED AND REPLACED INBD -A- BRACKET ON THE RT LOWER TRANSCOWL IAW REO 670-54-21-971, REV B, AND DRAWING CN624-2005 SNIEO S08. COMPLIED WITH 51-900-1002 SKY.
Part: STAND OFF — CRACKED (ZONE 400) · airframe 31,709 hrs · 24,999 cycles
LEFT LWR TRANSCOWL OTBD A BRACKET STANDOFF IS CRACKED. (C-CHECK) REMOVED AND REPLACED OTBD STANDOFF WITH NEW STANDOFF IAW REO 670-54-21-971, REV B, AND EO CN624-2005 SNIEO-S07 DATED 2025-06-12 AND ENSURED ALL OTHER DRAWING REQUIREMENTS WERE MET. COMPLIED WITH SKY CARD 51-900-1002-SKY.
Part: HANDLE — CHAFED (ZONE 800) · airframe 31,709 hrs · 24,999 cycles
SERVICE DOOR EXTERNAL HANDLE HOUSING IS CHAFED. (C-CHECK) REMOVED AND INSTALLED NEW SERVICE DOOR EXTERNAL HOUSING IAW SRM 51-42-06-001-001-A01 AND DWG CC670-38103, REV-C, COMPLIED WITH 51-900-1002-SKY
Part: ROLLER — EXPIRED (ZONE 500) · airframe 31,709 hrs · 24,999 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: SIDE ROLLER SLAT TRACK 2-2 900 LT - LT SIDE ROLLER ASSY 0.750 DIA. SLAT TRACK (QTY 2) AND SIDE ROLLER ASSY 0.875 DIA. SLAT TRACK (QTY 2) ARE DUE LIFE LIMIT. REMOVED, DISCARDED, & REPLACED WITH SERVICEABLE PARTS IAW 27-530-815, MRB 27-81-43-702, 27-81-43-707. (C-CHECK)
Part: ROLLER — EXPIRED (ZONE 500) · airframe 31,709 hrs · 24,999 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: SIDE ROLLER SLAT TRACK 1-2 900 LT - LT SIDE ROLLER ASSY 0.750 DIA. SLAT TRACK (QTY 2) AND SIDE ROLLER ASSY 0.875 DIA. SLAT TRACK (QTY 2) ARE DUE LIFE LIMIT. . REMOVE AND DISCARD. REPLACE WITH SERVICEABLE PARTS IAW 27-520-804, MRB 27-81-43-702, 27-8143-713, (C-CHECK).
Part: STRINGER — CORRODED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: RA33248-STS EA 30-2016-196-DTI - REMOVED CORROSION ON STRINGER 23RT FROM STA FS954 TO FS969 REPAIRED STRINGER REF STS EA 30-2016-196 REV̉‰, NDT PERFORM LFEC INSP OF REPAIRED AREA PER STS EA 30-2016-196 REV A SEC II DTIR., (C-CHECK) REMOVED PREVIOUS REPAIR AND COMPLIED WITH PERMANENT REPAIR ON STRINGR 23R BETWEEN BS 954 TO 969. REF. MHIRJ REO 690-53-51-485 REV-- 2025-07-28. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.
Part: LENS — DAMAGED (ZONE 500) · airframe 31,709 hrs · 24,999 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: RA66312-690-57-21-384 898SK MXCODEID54688-PR - LEFT WING LEADING EDGE AT INBOARD SIDE OF NAV LIGHT LENS COVER STRUCK BY FORKLIFT. COMPLIED WITH TEMPORARY REPAIR PER REO 690-57-21-384 REV.-- DATED 2021-02-04. PERMANENT REPAIR DUE WITHIN 2700 FLT HRS WITH ESCALATION PROVIDED BY REO 690-57-21-384 REV D. DUE BY 31785.6 TAT, PART NUMBER: - , SERIAL NUMBER: 15110, POSITION: (C-CHECK) PERFORMED PERMANENT REPAIR FOR DAMAGE TO LEFT WING LEADING EDGE AT INBOARD SIDE OF NAV LIGHT LENS COVER; REF REO 690-57-21-531, REV.-- DATED: 2025-07-20; COMPLIED WITH 51-900-1002-SKY
Part: ROLLER — EXPIRED (ZONE 600) · airframe 31,709 hrs · 24,999 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: SIDE ROLLER SLAT TRACK 2-2 900 RT - RT SIDE ROLLER ASSY 0.750 DIA. SLAT TRACK (QTY 2) AND SIDE ROLLER ASSY 0.875 DIA. SLAT TRACK (QTY 2) ARE DUE LIFE LIMIT. REMOVED, DISCARDED, & REPLACED WITH SERVICEABLE PARTS IAW 27-630-815, MRB 27-81-43-702, & 27-81-43-707. (C-CHECK)
Part: ROLLER — OUT OF LIMITS (ZONE 600) · airframe 31,709 hrs · 24,999 cycles
TRACK ROLLER SLAT 1-2 900 RT - COMPLY WITH TASK CARD 27-630-809 RT TRACK ROLLER SEALED, TRACK 1-2, TOP FORWARD - SLAT 1, (C-CHECK) REMOVED AND REPLACED TRACK TOP FWD SEALED ROLLER IAW AMM 27-81-43-000-801-A01. OP TEST OF THE FLAP AND SLAT SYSTEM COMPLETED IAW AMM 27-50-00-710-801-A02. OPS TESTED BAD. WHEN FLAPS/SLATS RETURNED TO THE FULLY RETRACTED POSITION A FLAP HALF-SPEED INDICATION WAS DISPLAYED ON EICAS.. COMPLIED WITH SKYWEST TASK CARD: 27-630-809-A01.
Part: ROLLER — OUT OF LIMITS (ZONE 500) · airframe 31,709 hrs · 24,999 cycles
TRACK ROLLER SLAT 1-3 900 LT - COMPLY WITH TASK CARD 27-530-809 LT. TRACK ROLLER SEALED, TRACK 1-3, TOP FORWARD - SLAT 1. (C-CHECK) REMOVED AND REPLACED LT SLAT TRACK SEALED ROLLER TOP FORWARD 1-3 IAW AMM 27-81-43-400-801-A01. OP TEST OF THE FLAP AND SLAT SYS COMPLETED IAW AMM 27-50-00-710-801-A02. OPS TESTED BAD. WHEN FLAPS/SLATS RETURNED TO THE FULLY RETRACTED POSITION A FLAP HALF-SPEED INDICATION WAS DISPLAYED ON EICAS.
Part: STRINGER — DAMAGED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: RA33058-STS EA 40-2016-209-DTI - COMPLIED WITH REPAIR OF STR21 RH FROM FS954 TO FS969 REF STS EA 40-2016-209 REV--, PERFORM NDT LFEC PER STS EA 40-2016-209 REV A SEC II DTIR, PART NUMBER: - , SERIAL NUMBER: 15110, POSITION: (C-CHECK) REMOVED PREVIOUS REPAIR AND COMPLIED WITH PERMANENT REPAIR ON STGR 21RH BETWEENFS954 TO FS969. REF. MHIRJ REO 690-53-51-485 REV-- 2025-07-28. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.
Part: ROLLER — EXPIRED (ZONE 600) · airframe 31,709 hrs · 24,999 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: SIDE ROLLER SLAT TRACK 1-2 900 RT - RT SIDE ROLLER ASSY 0.750 DIA. SLAT TRACK (QTY 2) AND SIDE ROLLER ASSY 0.875 DIA. SLAT TRACK (QTY 2) ARE DUE LIFE LIMIT. REMOVE, DISCARD & REPLACED WITH SERVICEABLE PARTS IAW 27-620-804 & MRB 27-81-43-702, 27-81-43-707. (C-CHECK).
Part: ROLLER — OUT OF LIMITS (ZONE 500) · airframe 31,709 hrs · 24,999 cycles
TRACK ROLLER SLAT 1-2 900 LT - COMPLY WITH TASK CARD 27-530-809 LT TRACK ROLLER SEALED, TRACK 1-2, TOP FORWARD - SLAT 1 (C-CHECK) REMOVED AND REPLACED LH SLAT TRACK 1-2 SEALED ROLLER (TOP FORWARD) IAW AMM 27-81-43-400-801-A01. OPS TEST OF THE FLAP AND SLAT SYSTEM COMPLETED IAW AMM 27-50-00-710-801-A02. OPS TESTED BAD. WHEN FLAPS/SLATS RETURNED TO THE FULLY RETRACTED POSITION A FLAP HALF-SPEED INDICATION WAS DISPLAYED ON EICAS.
Part: ROLLER — OUT OF LIMITS (ZONE 600) · airframe 31,709 hrs · 24,999 cycles
TRACK ROLLER SLAT 1-3 900 RT - COMPLY WITH TASK CARD 27-630-809 RH TRACK ROLLER SEALED, TRACK 1-3, TOP FORWARD - SLAT 1. (C-CHECK) REMOVED AND REPLACED RT SLAT TRACK SEALED ROLLER TOP FORWARD 1-3 IAW AMM 27-81-43-400-801-A01. OPS TEST OF THE FLAP AND SLAT SYS COMPLETED IAW AMM 27-50-00-710-801-A02. OPS TESTED BAD. WHEN FLAPS/SLATS RETURNED TO THE FULLY RETRACTED POSITION A FLAP HALF-SPEED INDICATION WAS DISPLAYED ON EICAS.
Part: ROLLER — EXPIRED (ZONE 600) · airframe 31,709 hrs · 24,999 cycles
SIDE ROLLER SLAT TRACK 3-2 900 RT - RT SIDE ROLLER ASSY 0.750 DIA. SLAT TRACK DUE LIFE LIMIT. (C-CHECK) REMOVED AND REPLACED THE RT SLAT TRACK 3-2 SIDE ROLLERS. IAW AMM 27-81-44-400-803-A01. GAP CHECKS GOOD.
Part: ROLLER — EXPIRED (ZONE 500) · airframe 31,709 hrs · 24,999 cycles
SIDE ROLLER SLAT TRACK 3-2 900 LT - LT SIDE ROLLER ASSY 0.750 DIA. SLAT TRACK DUE LIFE LIMIT. REMOVED, DISCARDED & REPLACED WITH SERVICEABLE PARTS IAW 27-530-816 & MRB 27-81-43-702, (C-CHECK)
Part: SKIN — DAMAGED (ZONE 100) · airframe 31,709 hrs · 24,999 cycles
DAMAGE FOUND ON FUSELAGE AFT OF GROUND AIR CONNECTION DOOR DUE TO CONNECTION COVER SMACKING SIDE OF FUSELAGE DURING FLIGHT. COMPLIED WITH TEMPORARY REPAIR REO 690-53-61-1044 REV-A DATED 2021-11-07. PERMANENT REPAIR DUE WITHIN 4750 FLT HRS BY 35218.3 TAT, (C-CHECK) COMPLIED WITH PERMANENT REPAIR OF AFT FUSELAGE SKIN AROUND THE GROUND AIR CONNECTION REF REO 690-53-61-1645 REV -- DATED 2025-07-15, COMPLIED WITH 51-900-1002-SKY, LEAK CHECK PASSED.
Part: ROLLER — OUT OF LIMITS (ZONE 500) · airframe 31,709 hrs · 24,999 cycles
TRACK ROLLER SLAT 2-2 900 LT - COMPLY WITH TASK CARD 27-530-809 LT TRACK ROLLER SEALED, TRACK 2-2, TOP FORWARD - SLAT 2. (C-CHECK) REMOVED AND REPLACED LT SLAT TRACK SEALED ROLLER TOP FORWARD 2-2 IAW AMM 27-81-43-400-801-A01. OP TEST OF THE FLAP & SLAT SYSTEM COMPLETED IAW AMM 27-50-00-710-801-A02. OP TESTED BAD. WHEN FLAPS/SLATS RETURNED TO THE FULLY RETRACTED POSITION A FLAP HALF-SPEED INDICATION WAS DISPLAYED ON EICAS.
Part: ROLLER — OUT OF LIMITS (ZONE 600) · airframe 31,709 hrs · 24,999 cycles
TRACK ROLLER SLAT 2-2 900 RT - COMPLY WITH TASK CARD 27-630-809 RT TRACK ROLLER SEALED, TRACK 2-2, TOP FORWARD - SLAT 2. (C-CHECK) REMOVED AND REPLACED RT SLAT TRACK SEALED ROLLER TOP FORWARD 2-2 IAW AMM 27-81-43-400-801-A01. OPS TEST OF THE FLAP AND SLAT SYSTEM COMPLETED IAW AMM 27-50-00-710-801-A02. OPS TESTED BAD. WHEN FLAPS/SLATS RETURNED TO THE FULLY RETRACTED POSITION A FLAP HALF-SPEED INDICATION WAS DISPLAYED ON EICAS.
2022
Part: NONE — CRACKED · airframe 31,066 hrs · 24,433 cycles
L WINDSHIELD HEAT FAILED IN CRUSE. THE WINDSHIELD CRACKED SHORTLY AFTER. (FLIGHT 4131- FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
2019
Part: FLOOR SUPPORT — CORRODED (BS 985-1088) · airframe 27,208 hrs · 21,249 cycles
RIGHT-HAND FLOOR SILL AT BS 985 TO 1088.2 HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND INSTALLED NEW RT FLOOR SILLS IAW SRM.
Part: FLOOR SUPPORT — CORRODED (BS 985-1088) · airframe 27,208 hrs · 21,249 cycles
LEFT-HAND, AFT CARGO FLOOR BEAM AT FS985.00 TO FS1088.20, LBL27, HAS MULTIPLE SPOTS OF CORROSION, CORRODED THROUGH THE BEAM. (C-CHECK) RO: 08/15/2019 REPLACED AFT CARGO FLOOR BEAM LOCATED AT LBL27 BETWEEN FS985 - FS1098.2 WITH NEW BEAM IAW SRM. ALL CHECKS GOOD.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 27,208 hrs · 21,249 cycles
PAX DOOR INTERCOSTAL DD4 HAS CORROSION. REMOVED CORRODED PAX DOOR INTERCOSTAL DD4 AND REPLACED WITH NEW IAW SRM. LEAK CHECK GOOD.
Part: DRAIN MAST — CORRODED (BS 1031-1051) · airframe 27,208 hrs · 21,249 cycles
DRAIN MAST DOUBLER BETWEEN FS1031 AND FS1051 CORRODED. REMOVED CORRODED DRAIN MAST DOUBLER BETWEEN FS1031 AND FS1051 AND REPLACED WITH NEW IAW SRM. LEAK AND OPERATIONAL TESTS GOOD.
Part: FRAME — CORRODED (BS 295) · airframe 27,208 hrs · 21,249 cycles
FS 295 LOWER FUSELAGE FRAME CORRODED BETWEEN STR 26L AND STR 26R. (C-CHECK) RO: 08/15/2019 PERFORMED FRAME SPLICE REPAIR TO FS295 LOWER SECTOR BETWEEN STR26L-26R IAW REO. LEAK CHECK GOOD.
Part: FRAME — CORRODED (BS 319) · airframe 27,208 hrs · 21,249 cycles
FS319 LOWER FUSELAGE FRAME CORRODED BETWEEN STR 26L AND STR 26R. PERFORMED FRAME SPLICE REPAIR TO FS319 LOWER SECTOR BETWEEN STR26L-26R IAW REO. LEAK CHECK GOOD.
Part: FRAME — CORRODED (BS 310) · airframe 27,208 hrs · 21,249 cycles
FS 310 LOWER FUSELAGE FRAME CORRODED BETWEEN STR 26L AND STR 26R. (C-CHECK) RO: 08/15/2019 PERFORMED FRAME SPLICE REPAIR TO FS310 LOWER SECTOR BETWEEN STR26L-26R IAW REO. LEAK CHECK GOOD.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 27,208 hrs · 21,249 cycles
FLOOR PANEL SUPPORT ANGLE CORRODED FROM RBL9 TO LBL9 AT FS 280. (C-CHECK) RO: 08/15/2019 REMOVED AND REPLACED COCKPIT FLOOR SUPPORT AT FS 280 IAW SRM.
Part: SEAL — TORN (HORIZONTAL STAB) · airframe 27,208 hrs · 21,249 cycles
TORN SEAL ON LEFT HAND HORIZONTAL STABILIZER LEADING EDGE ACCESS PANEL 331AL. REPLACED L/H SEAL P/N: AV670-21486-001 FOR HORIZONTAL STABILIZER LEADING EDGE ACCESS PANEL 331AL,
Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 27,208 hrs · 21,249 cycles
THE AFT CARGO DOOR SURROUND'S FLOOR SILL IS CORRODED AND CHAFED IN MULTIPLE AREAS. REMOVED AND REPLACED DAMAGED THE AFT CARGO DOOR FLOOR SILL. LEAK CHECK GOOD.
Part: HINGE — GOUGED (PAX DOOR) · airframe 27,208 hrs · 21,249 cycles
THE PAX DOOR HINGE, FUSELAGE SIDE, HAS A GOUGE IN THE AFT MOST LUG LAND. (C-CHECK) RO: 08/15/2019 BLENDED OUT DAMAGE AT PAX DOOR HINGE, FUSELAGE SIDE AT THE AFT MOST LUG LAND AND COMPLIED WITH ALL STEPS OF REO.
2018
Part: HINGE — DAMAGED (PAX DOOR) · airframe 24,976 hrs · 19,768 cycles
THE PASSENGER DOOR PIANO HINGE DAMAGED AND REQUIRES REPLACEMENT. REPLACED THE PASSENGER DOOR PIANO HINGE IAW REO. PRESSURE CHECKED GOOD.
Part: DCU — FAILED (NR 2) · airframe 24,654 hrs · 19,575 cycles
OUTBOARD FLIGHT SPOILER CAUTION MESSAGE, ELEVATOR SPLIT CAUTION MESSAGE, AND CAS MISCOMPARE MESSAGE. NO CONTROL ISSUES NOTED. EMERGENCY DECLARED. REMOVED AND REPLACED THE NR 2 DCU IAW AMM. OPS CHECKED GOOD.
2016
Part: STRINGER — CORRODED (BS 954-969) · airframe 19,686 hrs · 16,389 cycles
STRINGER 21R FROM BS 954 - 969 HAS CORROSION. REPAIRED THE STRINGER IAW EA AND DWG. LEAK CHECKED GOOD.
Part: STRINGER — CORRODED (BS 954-969) · airframe 19,686 hrs · 16,389 cycles
STRINGER 23R FROM BS 954 - 969 HAS CORROSION. REPAIRED THE STRINGER IAW EA. LEAK CHECKED GOOD.
Part: FRAME — CORRODED (BS 847) · airframe 19,686 hrs · 16,389 cycles
FRAME AT BS 847+16 HAS CORROSION BETWEEN STRINGERS 26L AND 26R. REPAIRED THE FRAME IAW EA. LEAK CHECKED GOOD.
Part: FRAME — CORRODED (BS 1047) · airframe 19,686 hrs · 16,389 cycles
FRAME AT BS 1047 HAS CORROSION BETWEEN STRINGERS 25 - 26L. REPAIRED THE FRAME IAW SRM.
Part: RETAINER — CHAFED (PAX DOORWAY) · airframe 19,686 hrs · 16,389 cycles
PAX DOOR BOTTOM AFT CORNER SEAL RETAINER IS CHAFED. REMOVED & REPLACED THE SEAL RETAINER IAW SRM. LEAK CHECKED GOOD.
Part: LONGERON — CORRODED (BS 333-349) · airframe 19,686 hrs · 16,389 cycles
CORROSION ON LONGERON 25R BETWEEN BS 333 - 349. REMOVED AND REPLACED THE LONGERON IAW SRM AND DWG. LEAK CHECKED GOOD IAW SRM.
Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 19,686 hrs · 16,389 cycles
CORROSION AROUND FASTENER HOLES ON STRINGER SPLICE 25R, AFT OF THE FRAME AT BS 333. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM. LEAK CHECKED GOOD.
Part: TIRE — FAILED (NR 3) · airframe 18,762 hrs · 15,832 cycles
NR 3 MAIN TIRE BURST ON T/O. DAMAGE TO RT FLAP, AND POSSIBLE ENGINE DAMAGE. CONTINUED TO DESTINATION, EMERGENCY LANDING DECLARED. REPLACED NR 3 TIRE. R & R RT INBD FLAP. OPS CHECK GOOD.
2014
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,942 hrs · 12,939 cycles
AFT CEILING EMERGENCY OVERHEAD LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,899 hrs · 12,896 cycles
AFT CEILING EMERGENCY LIGHT IS INOPERATIVE. REPLACED THE LAMP IAW AMM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,842 hrs · 12,843 cycles
LEFT FUSELAGE AFT MOST EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM.
Part: HINGE — GOUGED (PAX DOOR) · airframe 14,693 hrs · 12,687 cycles
PASSENGER DOOR PIANO HINGE HAS GOUGES AT FORWARD LUG, MARKED. C-CHECK, BLENDED GOUGE REF REO.
Part: HINGE — GOUGED (PAX DOOR) · airframe 14,693 hrs · 12,687 cycles
PASSENGER DOOR PIANO HINGE HAS GOUGES AT AFT LUG NR 5, MARKED. C-CHECK, BLENDED GOUGES, REF REO.
Part: AXLE — CORRODED (RT MLG) · airframe 14,693 hrs · 12,687 cycles
RT MLG 4 AXLE IS CORRODED. C-CHECK, REMOVED CORROSION IAW REO 670-32-11-235.
Part: AXLE — CORRODED (RT MLG) · airframe 14,693 hrs · 12,687 cycles
RIGHT MLG NR 3 AXLE IS CORRODED. C-CHECK, REMOVED CORROSION IAW REO.
Part: AXLE — CORRODED (LT MLG) · airframe 14,693 hrs · 12,687 cycles
LEFT MLG NR 2 AXLE IS CORRODED. C-CHECK, REMOVED CORROSION IAW REO.
Part: AXLE — CORRODED (LT MLG) · airframe 14,693 hrs · 12,687 cycles
LEFT MLG NR 1 AXLE IS CORRODED. C-CHECK, REMOVED CORROSION IAW REO.
Part: SEAT TRACK — CORRODED (BS 364-379) · airframe 14,693 hrs · 12,687 cycles
RIGHT FLOOR SEAT TRACK HAS CORROSION AT BS 364-379 APPROXIMATELY. C-CHECK, BLENDED OUT CORROSION IAW REO.
Part: WEB — UNKNOWN (BS 280) · airframe 14,693 hrs · 12,687 cycles
RT WEB AT F/S 280 IAW REO. C-CHECK, REPLACED RT WEB AT FS 280 IAW REO.
Part: WEB — UNKNOWN (BS 280) · airframe 14,693 hrs · 12,687 cycles
REPLACE LT WEB AT F/S 280 IAW REO. C-CHECK, REPLACED LT WEB AT FS 280 IAW REO.
2013
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,538 hrs · 11,594 cycles
OVERHEAD EMERGENCY LIGHT NR 6 IS BURNED OUT. FLT 2937 RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,175 hrs · 11,244 cycles
2ND TO LAST EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#2985 RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,975 hrs · 11,046 cycles
EMERGENCY OVERHEAD LIGHT IN CABIN IS BURNED OUT. FLT#2974 RELAMPED.