N558GJ
Registered owner: SKY WEST 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.
64 reports on file, 2021-11-28 – 2026-03-26.
Part: WARNING MESSAGE — ILLUMINATED (ZONE 700) · airframe 45,138 hrs · 34,542 cycles
GEAR DISAGREE WARNING UPON GEAR UP RETRACTION ASSOCIATED WITH A PROX SYSTEM FAULT 1 STATUS MESSAGE. QRH RESOLVED THE ISSUE AND MESSAGES CLEARED AND GEAR INDICATED DOWN 3 GREEN (FLIGHT 5610) REFERENCE CP 31990225 (R/R PX08 NLG CENTERING PROXIMITY SENSOR TARGET AND ATTACHING HARDWARE), CP 31990253(R/R PX37 NLG CENTERING PROXIMITY SENSOR TARGET AND ATTACHING HARDWARE),CP 31984486, AND CP 31969289 REV. -B COMPLIANCE FOR CORRECTIVE ACTIONS PERFORMED OPS TEST OF THE MLG EXTENSION, RETRACTION SYS IAW AMM 32-30-00, OPS CHECKS GOOD AT THIS TIME NO GEAR DISAGREE WARNING CASS MESSAGE POPULATED DURING OPS CHKS,
Part: SENSOR — FAULTED (ZONE 700 WOW) · airframe 45,133 hrs · 34,537 cycles
GEAR DISAGREE ON TAKEOFF. GEAR DID NOT COME UP. FLIGHT 5428, WIRING CHKD LANDING GEAR CONTROL HANDLE, LANDING GEAR SELECTOR VALVE & PSEU, ADJUSTED OF PX37 BRACKET HARDWARE. RIGGED SENSORS PX24, PX11, & PX37, INSPECTED NLG AFT DOOR DRIVE BRACKET. REPLACED RT MLG WOW SENSOR PX09. ADJUSTED SENSOR PX10 & INSPECTED THE PSEU FOR DAMAGED PINS. OPS CHECKS OF THE PROXIMITY SENSOR SYS WITH WOW. PROX SYS HEALTH CHKD. LANDING GEAR HYD & MECHANICAL HEALTH CHK. LANDING GEAR EXTENSION/RETRACTION OPS CHKD GOOD. PSS SYSTEM. OPS CHKD GOOD . RETURNED TO SERVICE.
Part: PROXIMITY SENSOR — FAULTED (ZONE 700) · airframe 45,124 hrs · 34,528 cycles
GEAR DISAGREE UPON GEAR UP LEVER BEING PLACED IN THE UP POSITION. (FLIGHT 5565) TROUBLESHOT GREAR DISAGREE REFERENCING APPLICABLE STEPS OF FIM 32-21-00. FOUND NLG PROXIMITY SENSOR PX37 SHOWING FAR (UNREADABLE). ATTEMPTED TO ADJUST SENSOR PX37 REFERENCING APPLICABLE STEPS OF AMM 32-61-05 AND FOUND THE SENSOR FAULTY AND UNRESPONSIVE TO ADJUSTMENT. SEE CP'S 31934202 AND 31934188 FOR REPLACEMENT OF THE RH NLG NLG, WOW, CENTERED AND LVDT PROXIMITY-SENSOR HARNESS ASSEMBLY. PERFORMED OPERATIONAL TEST OF THE LANDING-GEAR EXTENSION/RETRACTION SYSTEM REFERENCING APPLICABLE STEPS OF AMM 32-30-00. OPS CHECK GOOD AT THIS TIME. GEAR DISAGREE MESSAGE NEVER RETURNED. AIRCRAFT GOOD FOR CONTINUED SERVICE."
Part: SKIN — MECHANIC ERROR (ZONE 200) · airframe 44,852 hrs · 34,278 cycles
DURING STARLINK INSTALLATION A STRINGER RIVET WAS MISDRILLED AT FWD RIGHT SKIN, STRINGER 2R, BS 437. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR, COMPLIED WITH MAJOR REPAIR OF FWD RIGHT SKIN, STRINGER 2R, BS 437 IAW STARLINK EO SPX-00011260. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Earlier reports · 2021–2025 · 60 reports
2025
Part: STRINGER — CORRODED (ZONE 100) · airframe 44,635 hrs · 34,074 cycles
WHILE REMOVING STRINGER 21R FOUND CORROSION ON THE STRINGER CIRCUMFERENTIAL JOINT SPLICE AT BS 477. REPLACED STRINGER 21R JOINT SPLICE IAW SRM 51-40-11-001-001-A01, & 51-42-06-001-001-A01, REV 38.
Part: STRINGER — CORRODED (ZONE 100) · airframe 44,635 hrs · 34,074 cycles
STRINGER 20R FOUND TO BE CORRODED BETWEEN BS 319.70 - 333, BEHIND ELECTRICAL CONNECTOR BRACKET. REMOVED THE STRINGER IAW SRM 51-42-06-001-001-A01, REV OA, AND 51-42-21-001-001-A01, REV OA. FABRICATED LOCATED AND DRILLED A NEW STRINGER IAW DRAWING SH670-32428-3 AND SAMPLE IAW SRM 51-24-16-001-001-A01 AND 51-40-11-001-001-A01, REV OA. INSTALLED NEWLY FABRICATED STRINGER BETWEEN BS 319 - 333 IAW SRM 51-42-06-001-001-A01, REV OA.
Part: FRAME — NO DISCREPANCY (ZONE 100) · airframe 44,635 hrs · 34,074 cycles
FRAME BS 319 BETWEEN STGR 18L - STGR 21L REQUIRES REMOVAL TO FOM. REMOVED AND REINSTALLED FS319 STUB FRAME 18L-21L IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01AND 51-25-16-001-001-A01 REV 38.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 44,635 hrs · 34,074 cycles
FOUND CORROSION ON STRINGER SPLICE 23R, BS 333. REPLACED THE STRINGER SLICE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 53-00-00-101-001-A01, 51-25-16-001-001-A01, AND 51-23-00-001-001-A01 REV 38.
Part: STRINGER — CORRODED (ZONE 100) · airframe 44,635 hrs · 34,074 cycles
STRINGER 24R FOUND CORRODED BETWEEN BS 349 TO 364. REPAIRED THE STRINGER IAW SRM 51-23-00-001-001-A01, 51-24-36-001-001-A01, 51-25-06-001-001-A01, 51-25-16-001-001-A01, 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-20-001-001-A01, 51-42-21-001-001-A01, 53-00-03-201-001-A01, AND 53-21-03-101-006-A01 REV 38.
Part: SUPPORT PLATE — CORRODED (ZONE 100) · airframe 44,635 hrs · 34,074 cycles
CORROSION FOUND ON SUPPORT PLATE AT BS 333, S20R. REPLACED SUPPORT PLATE IAW SRM 51-40-11-001-001-A01, 51-24-36-001-001-A01, AND 51-42-21-001-001-A01, REV 38.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 44,635 hrs · 34,074 cycles
PAX DOOR AFT DD5 INTERCOSTAL FOUND TO BE CORRODED, REQUIRES REPLACEMENT. REPLACED THE PAX DOOR AFT DD5 INTERCOSTAL IAW SRM 51-42-06-001-001-A01, AND 51-40-11-01-001-001-A01, REV 38.
Part: SKIN — DENTED (ZONE 100) · airframe 44,635 hrs · 34,074 cycles
FUSELAGE SKIN HAS PROTRUDING DENTS AT FS 299 BETWEEN STRS 20R AND 21R. REPAIRED FUSELAGE SKIN FS299 STGR 20R-21R IAW REO# 670-53-21-2667 REV - AND SRM 51-23-00-001-001-A01 REV 38
Part: FORMER — CORRODED (ZONE 800) · airframe 44,635 hrs · 34,074 cycles
PAX DOOR FORMER,FS329.41, BETWEEN DD5 AND DD6 FOUND BE CORRODED REQUIRE REPLACEMENT (C-CHECK RO 12/09/2025)INSTALLED PAX DOOR NEW SERVICEABLE FORMER PN 601R318078-3 AT FS 329.41 IAW CRJ 550 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01 REV 38 JUL 25/2020
Part: FRAME — NO DISCREPANCY (ZONE 100) · airframe 44,635 hrs · 34,074 cycles
STRUCTURES ACCESS FOR STRINGER 23R BETWEEN BS 333 TO 379. REMOVED AND REINSTALLED FRAME AT BS 333 STRINGER 25R IAW SRM 53-00-06-201-006-A01, 51-42-21-001-001-A01, AND 51-42-06-001-001-A01, REV 38
Part: FRAME — NO DISCREPANCY · airframe 44,635 hrs · 34,074 cycles
FRAME 469 REQUIRES REMOVAL FOR STRINGER REPAIRS. (C-CHECK RO 12/09/2025)REMOVED AND REINSTALLED/SPLICED FRAME AT FS469 MHIRJ REO# 670-53-21-2665 REV. -- DATED 2025-09-15 AND CRJ 550 SRM 51-42-20-001-001-A01 AND 51-42-06-001-001-A01 REV 38 JUL 25/2020. REFERENCE CONTINUATION CARD FOR WORK PERFORMED
Part: FRAME — NO DISCREPANCY · airframe 44,635 hrs · 34,074 cycles
FRAME BS 295 REQUIRES REMOVAL FOR AVI BAY STRINGER REPLACEMENT. INSTALLED FRAME AND SPLICE IAW SRM 53-00-06-201-A03, SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01, 51-25-16-001-001-A01, 51-25-06-001-001-A01, 51-23-00-001-001-A01, REV 38. AND REO 670-53-21-2663, REV-.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 44,635 hrs · 34,074 cycles
FOUND EVIDENCE OF CORROSION ON STRINGER SPLICE 21L, BS 333. REMOVED THE STRINGER SPLICE, BS 333 IAW SRM 51-42-06-001-001-A01, REV OA. INSTALLED THE STRINGER SPLICE IAW SRM 51-42-06-001-001-A01, REV OA.
Part: STRINGER — CORRODED (ZONE 100) · airframe 44,635 hrs · 34,074 cycles
EVIDENCE OF CORROSION FOUND ON STRINGER 20R BETWEEN BS 280 AND 295. INSTALLED STRINGER 20R FROM BS 280 TO 319 IAW SRM 51-42-06-001-001-A01, & SRM 51-42-21-001-001-A01, REV 38.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 44,635 hrs · 34,074 cycles
PAX DOOR INTERCOSTAL DD5 CORRODED BETWEEN BS 311.75 AND 320. INSTALLED NEW SERVICEABLE FWD DD5 IAW SRM 51-42-06-001-001-A01, REV 38 AND REO 670-52-11-1492, REV -.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 44,635 hrs · 34,074 cycles
PAX DOOR INTERCOSTAL DD6 CORRODED BETWEEN BS 320 AND 338. REPLACED PAX DOOR INTERCOSTAL IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01, REV 38.
Part: FORMER — CORRODED (ZONE 800) · airframe 44,635 hrs · 34,074 cycles
PAX DOOR AFT FORMER AT FS347.27 CORRODED BETWEEN DD4 AND DD7. REPLACED PAX DOOR AFT FORMER AT BS 347.27 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-001-001-A01 REV 38.
Part: FORMER — CORRODED (ZONE 800) · airframe 44,635 hrs · 34,074 cycles
PAX DOOR FWD FORMER BS 311.75 BETWEEN DD4 AND DD7 CORRODED. REMOVED AND REPLACED PAX DOOR FWD FORMER IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01, REV 38.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 44,635 hrs · 34,074 cycles
LBL 9 FLOOR SUPPORT IS CORRODED BETWEEN BS 863 AND 879 ON THE UPPER INBD FLANGE. REMOVED CORROSION BY BLENDING IAW REO 670-53-51-353, REV -. COMPLETED TASK CARD 51-900-1002- SKY.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 44,635 hrs · 34,074 cycles
LBL 9 FLOOR SUPPORT IS CORRODED ON THE UPPER INBD FLANGE BETWEEN BS 645 & 693. REPAIRED THE FLOOR SUPPORT ON THE UPPER FLANGE IAW REO 670-53-31-1068 REV-. COMPLETED TASK CARD 51-900-1003-SKY.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 44,635 hrs · 34,074 cycles
RBL 9 FLOORBEAM IS CORRODED AT BS 661, ON THE UPPER INBD FLANGE. COMPLIED WITH REO 670-53-31-1067, REV -.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 44,635 hrs · 34,074 cycles
RBL 9 FLOOR SUPPORT IS CORRODED BETWEEN BS 469 & 485 ON THE UPPER INBD FLANGE. COMPLIED WITH REO 670-53-31-1066 REV-.
Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 44,635 hrs · 34,074 cycles
FOUND CORROSION ON INTERCOSTAL AT STRINGER 20R BETWEEN BS 349-364. UPON FURTHER INVESTIGATION FOUND INSTERCOSTAL AT STGR 20R BETWEEN FS349-FS364 TO HAVE DAMAGE IN MORE THAN ONE ELEMENT AT A GIVEN CROSSSECTION INSTERCOSTAL IS OUT OF LIMITS 100% MATERIAL LOSS REQUIRES REPLACEMENT IAW SRM 53-00-00-101-001-A01. INSTALLED NEW SERVICEABLE INTERCOSTAL AT STGR 20R BETWEEN FS349-FS364 IAW SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01.
Part: ANTENNA — CORRODED · airframe 44,635 hrs · 34,074 cycles
ADF ANTENNA HAS CORROSION AROUND FASTENER HOLES. REPAIRED AREA AROUND ADF ANTENNA FASTENER HOLES IAW REO 670-53-31-1065 REV -. INSTALLED 4EA LOCK FASTENERS IAW SRM 51-42-21-001-001-A01, REV 38.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 44,635 hrs · 34,074 cycles
PAX DOOR INTERCOSTAL IS CORRODED BETWEEN BS 333 TO 349, STRINGER 20L. INSTALLED THE INTERCOSTAL BETWEEN IAW SRM 51-42-06-001-001-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 44,635 hrs · 34,074 cycles
STRINGER 21R IS CORRODED BETWEEN BS 409 TO 421. INSTALLED STRINGER 21R FROM BS 394 - 477 IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-21-001-001-A01, 53-21-03-101-002-A01, AND 53-21-03-101-006-A01, REV 38 .
Part: STRINGER — CORRODED (ZONE 100) · airframe 44,635 hrs · 34,074 cycles
STRINGER 23R CORRODED BETWEEN BS 364 TO 379. INSTALLED NEW SERVICEABLE STRINGER BETWEEN BS 333 - 379 IAW SRM 51-42-06-001-001-A01, AND 51-40-11-001-001-A01, REV 38.
Part: STRINGER — CORRODED (ZONE 100) · airframe 44,635 hrs · 34,074 cycles
STRINGER 21R IS CORRODED BETWEEN BS 280 TO 295. REPLACED THE STRINGER 21R, BS 280-333 IAW SRM 51-42-21-001-001-A01, 51-40-11-001-001-A01, 51-42-20-001-001-A01, 51-42-06-001-001-A01, AND 53-21-03-101-001-A01, REV 38.
Part: SPLICE — CORRODED (ZONE 100) · airframe 44,635 hrs · 34,074 cycles
H SPLICE AT BS 581, STRINGER 26L IS CORRODED. COMPLIED WITH REO 670-53-31-1064, REV-. INSTALLED SIX JO-BOLTS IAW SRM 51-42-22-001-001-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 44,635 hrs · 34,074 cycles
STRINGER 20R IS CORRODED BETWEEN BS 437 TO 453. REPAIRED THE STGR IAW REO 670-53-21-2662, REV -.
Part: STRINGER — CORRODED · airframe 44,635 hrs · 34,074 cycles
STRINGER 18L IS CORRODED BETWEEN BS 319 TO 333. REMOVED CORROSION FROM STRINGER 19L IAW SRM 51-21-06-001-001-A01, FOUND TO BE OUT OF LIMITS DUE TO DAMAGE BEING IN MORE THAN ONE ELEMENT AT A GIVEN CROSS SECTION IAW SRM 53-21-03-101-001-A01. INSTALLED A NEW SERVICEABLE STRINGER 19L, BS 310 - 333 IAW SRM 51-42-06-001-001-A01, PAINTED SKIN RIVETS S19L, BS 319 - 349 IAW SRM 51-25-01-001-001-A01 REV 38.
Part: STRINGER — CORRODED (ZONE 100) · airframe 44,635 hrs · 34,074 cycles
STRINGER 20R CORRODED BETWEEN BS 349 TO 364. REPAIRED THE STRINGER IAW REO 670-53-21-2661 REV-, SRM 51-21-06-001-001-A01, 51-21-16-001-001-A01, 51-42-02-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 53-21-03-101-006-A01, REV 38.
Part: SLIDER — CHAFED (ZONE 400) · airframe 44,635 hrs · 34,074 cycles
RIGHT TRANSCOWL LOWER INBD SLIDER IS CHAFED. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1751 REV -.
Part: SLIDER — CHAFED (ZONE 400) · airframe 44,635 hrs · 34,074 cycles
RIGHT TRANSCOWL LOWER OTBD SLIDER IS CHAFED. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1751 REV -.
Part: SLIDER — CHAFED (ZONE 400) · airframe 44,635 hrs · 34,074 cycles
RIGHT TRANSCOWL UPPER INBD SLIDER IS CHAFED. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1750 REV -.
Part: SLIDER — CHAFED (ZONE 400) · airframe 44,635 hrs · 34,074 cycles
LEFT TRANSCOWL LOWER OTBD SLIDER IS CHAFED. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1749 REV -.
Part: SLIDER — CHAFED (ZONE 400) · airframe 44,635 hrs · 34,074 cycles
LEFT TRANSCOWL LOWER IB SLIDER IS CHAFED. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1749 REV -.
Part: SLIDER — CHAFED (ZONE 600) · airframe 44,635 hrs · 34,074 cycles
RIGHT TRANSCOWL UPPER OB SLIDER IS CHAFED. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1750 REV -.
Part: SLAT TRACK — CHAFED (ZONE 600) · airframe 44,635 hrs · 34,074 cycles
RIGHT SLAT TRACK 1-1 IS CHAFED. REPAIRED RT SLAT TRACK 1-1 IAW REO 670-57-42-2148, REV -.
Part: SLAT TRACK — CHAFED (ZONE 500) · airframe 44,635 hrs · 34,074 cycles
LEFT SLAT TRACK 1-1 IS CHAFED. COMPLIED WITH REO 670-57-42-2144, REV -.
Part: SLAT TRACK — CHAFED (ZONE 500) · airframe 44,635 hrs · 34,074 cycles
LEFT SLAT TRACK 1-3 IS CHAFED. COMPLIED WITH REO 670-57-42-2145, REV -.
Part: SLAT TRACK — CHAFED (ZONE 600) · airframe 44,635 hrs · 34,074 cycles
RIGHT SLAT TRACK 2-1 IS CHAFED. REPAIRED THE RT SLAT TRACK 2-1 IAW REO 670-57-42-2150 REV -.
Part: SLAT TRACK — CHAFED (ZONE 500) · airframe 44,635 hrs · 34,074 cycles
LEFT SLAT TRACK 2-3 IS CHAFED. COMPLIED WITH REO 670-57-42-2147 REV -.
Part: SLAT TRACK — CHAFED (ZONE 600) · airframe 44,635 hrs · 34,074 cycles
RIGHT SLAT TRACK 2-3 IS CHAFED. REPAIRED RT SLAT TRACK 2-3 IAW REO 670-57-42-2151, REV -.
Part: SLAT TRACK — CHAFED (ZONE 600) · airframe 44,635 hrs · 34,074 cycles
RIGHT SLAT TRACK 1-3 IS CHAFED. REPAIRED THE RT SLAT TRACK 1-3 IAW REO 670-57-42-2149, REV -.
Part: SLAT TRACK — CHAFED (ZONE 500) · airframe 44,635 hrs · 34,074 cycles
LEFT SLAT TRACK 2-1 IS CHAFED. COMPLIED WITH REO 670-57-42-2146 REV-.
Part: HINGE FITTING — GOUGED (ZONE 500 FLAP) · airframe 44,635 hrs · 34,074 cycles
LEFT OTBD FLAP, MID. HINGE AFT FLAP ATTACH FITTING, INBD LUG GOUGED. REMOVED DAMAGE FROM LT OTBD FLAP MID HINGE FLAP ATTACH FITTING IAW SRM 51-12-00-001-001-A01. PERFORMED HFEC OF LT OTBD FLAP ATTACH FITTING INBD LUG REWORKED AREA IAW PART 1 51-20-006-250-A01 WITH NO INDICATIONS NOTED AT THIS TIME. MECHANICAL MEASUREMENTS FOR WS 220.00 HINGE FITTING ORIGINAL MATERIAL THICKNESS: 0.250" MRT: 0.168" MAX MATERIAL REMOVED 0.082" NO DAMAGE LIMITS GIVEN. REPAIRED LT OTBD MID HINGE AFT FALP ATTACH FITTING IAW REO 670-57-53-417, REV -.
Part: WINDOW — CRACKED (ZONE 200) · airframe 44,321 hrs · 33,755 cycles
R WINDOW HEAT CAUTION ON INITIAL CLIMB OUT AFTER TAKEOFF LEAVING APPROXIMATELY 5000. NOTICED A CRACK ON THE RIGHT WINDOW. (FLIGHT 5289 - FILED CLOSED)INSPECTED RH WINDOW REF AMM 56-12-01, FOUND ARCING ON LOWER AFT BOTTOM OF WINDOW AND POSSIBLE CRACK ON MIDDLE PANE OR CONDUCTIVE FILM, MORE TROUBLESHOOTING REQUIRED. PLEASE REFERENCE AML 1578646
2024
Part: STEERING SYS — WARNING MESSAGE (ZONE 700) · airframe 43,693 hrs · 33,066 cycles
STEERING INOP CAUTION MESSAGE IN FLIGHT. (FLIGHT 6973 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 29022551 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE FOLLOWING CAMPS FOR TROUBLESHOOTING AND CORRECTIVE ACTIONSOF STEERING INOP CAUTION.CP 29030865 FOR TAXI CHECKCP# 29025712: TROUBLESHOOTING OF STEERING INOP CAUTION.CP# 29025998: INSPECTED CONNECTORS ASSOCIATED TO NWS SYSTEM ON NLG FOR CONDITION AND SECURITYCP# 29026957: MEGGER/WIRING CHECKSCP# 29027067: NWS ECU REPLACEMENTCP# 29030865: TAXI CHECK"
2022
Part: WEB — CRACKED (ZONE 100) · airframe 43,449 hrs · 32,820 cycles
CRACK FOUND APPROX 1.0" ON FUSELAGE WEB AFT LOWER CORNER RADIUS. STA 909 BL 20L WL 50. AS MARKED. REPAIR ON FUSELAGE WEB L/H AFT LOWER CORNER IAW EO C550-53MIR-002-O
Part: TRACK — NONE (ZONE 200) · airframe 43,449 hrs · 32,820 cycles
STA 459 TRANSITION PANELS WILL NOT FIT IN TRACK LEFT HAND SIDE25. REMOVED FABRICATED AND INSTALLED REPLACEMENT BRACKETS IAW CRJ 700 SRM 51-24-21, AND EO C550-25MR-019-O, AND AEROSPACE DRAWING GJ0012526N31 REV H
Part: DRAIN — CRACKED (ZONE 800) · airframe 43,449 hrs · 32,820 cycles
R/H FWD AVIONICS BAY, SILL IS CRACKED BY FWD AND AFT DOOR LATCH POINTS. REMOVED AND REPLACED R/H FWD AVIONICS BAY, SILL IAW CRJ 700 SRM 51-42-13, 51-25-06, 51-25-01.
Part: TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,449 hrs · 32,820 cycles
FWD CARGO BAY, AFT #3 TRACK HAS CORROSION. REMOVED AND REPLACED FWD CARGO BAY, AFT #3 TRACK IAW CRJ 700 AMM 25-51-02.
Part: SUPPORT BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,449 hrs · 32,820 cycles
CORROSION ON BELLY AVIONICS COMP FLOORBOARD , FWD SUPPORT BRACKET AT FS280
Part: TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,449 hrs · 32,820 cycles
FWD CARGO BAY, FWD #4 TRACK HAS CORROSION. REMOVED AND REPLACED FWD CARGO BAY, FWD #4 TRACK IAW CRJ 700 AMM 25-51-02.
Part: TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,449 hrs · 32,820 cycles
FWD CARGO BAY, FWD #3 TRACK HAS CORROSION. REMOVED AND REPLACED FWD CARGO BAY, FWD #3 TRACK IAW CRJ 700 AMM 25-51-02.
Part: CONNECTOR — LOOSE (ZONE 700) · airframe 43,426 hrs · 32,796 cycles
STEERING INOP MASTER CAUTION IN FLIGHT. TROUBLESHOOT AND FOUND CONNECTORS AT STEERING MANIFOLD WERE LOOSE. RECONNECTED CONNECTORS IAW CRJ550 AMM 32-51-50. PERFORMED OPS CHECK OF STEERING IAW CRJ550 AMM 32-51-00. OPS CHECK GOOD AT THIS TIME AND NO EICAS MSG.
2021
Part: LANDING GEAR — FALSE INDICATION · airframe 43,163 hrs · 32,530 cycles
GEAR DISAGREE WARNING MSG. PERFORMED GVI OF ALL THREE GEARS IAW CRJ-AMM-05-21-00. NO DEFECTS NOTED. DEFERRED LG RETRACTION ON OCN 70076166 PER MEL 32-30-01 CAT A AUTH BY MXC.
Part: DOOR LATCH — NONE (PAX DOOR) · airframe 43,160 hrs · 32,527 cycles
PAX DOOR LATCH CAUTION MSG. DEFERRED PER MEL 52-70-01 CAT A OCN 70076122 AUTH BY MXC
Part: WATER SYSTEM — LEAKING (GALLEY) · airframe 43,117 hrs · 32,489 cycles
PITCH FEEL FAULT CAUTION MSG// INB GROUND SPOILER/IB SPOILERON CAUTION MSG. INSPECTED AND FOUND WATER IN AVIONICS BAY, REMOVED WATER AND DRIED AREA, SWAPPED SSCU1 AND 2 IAW CRJ 550 AMM 27-61-05, OPS CHECK GOOD AND ALL MESSAGES CLEARED