N454SW
Registered owner: SKYWEST AIRLINES INC, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SKYWEST AIRLINES, INC. (SWIA) | Operator | 2010-11-02 – 2010-11-02 | Operator named in NTSB report |
| SKYWEST AIRLINES INC | Operator | 2010-11-02 – 2010-11-02 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
DURING INSPECTION OF PANELS FOUND DENT IN RT AILERON UPPER SKIN, NEAR THE INBD EDGE. REPAIRED RH AILERON UPPER SKIN NEAR THE INBD EDGE IAW REO 601R-57-61-887 REV -, AND COMPLIED WITH TASK CARD 51-900-1003-SKY.
UPON REMOVAL OF FRAME BS 574 BETWEEN S20R AND S20L FOUND REINFORCING ANGLE CORRODED AT MULTIPLE LOCATION. REMOVED AND REPLACED BY NEW REINFORCING ANGLE AT BS 574 BETWEEN S24L TO S20L IAW SRM 51-42-06 AND SRM 51-42-21 REV. 39, AND DWG 601R36024 REV. N. PERFORMED LEAK CHECK GOOD,
UPON REMOVAL OF LOW-PRESSURE GROUND AIR DOOR STRUCTURES FOUND FRAME SECTION AT BS 589 CORRODED. REMOVED AND REPLACED BY NEW FRAME SECTION AT BS 589, S21-20L IAW SRM 51-42-06, SRM 51-42-21 REV. 39, DWG 601R36025 REV. P, AND DWG 601R35005 REV AG,
UPON REMOVAL OF LOW-PRESSURE GROUND AIR DOOR STRUCTURES FOUND REINFORCING ANGLE CORRODED. REMOVED CORRODED REINFORCING ANGLE IAW SRM 51-42-06 AND INSTALLED NEW REINFORCING ANGLE IAW SRM 51-42-06 AND DWG 601R36025 REV. P AND COMPLIED WITH TASK 51-900-1003-SKY.
UPON REMOVAL OF LOW PRESSURE GROUND AIR DOOR AFTANGLE FOUND LANDING ANGLE CORRODED. REMOVED LOW-PRESSURE GROUND AIR DOOR AFT ANGLE LANDING IAW SRM 51-42-06 AND INSTALLED NEW LOW-PRESSURE GROUND AIR DOOR AFT ANGLE LANDING IAW SRM 51-42-06 AND DWG 601R35226 REV. P COMPLIED WITH TASK CARD 51-900-1003-SKY. PERFORMED LEAK CHECK GOOD, NO LEAKS NOTED.
LOW PRESSURE GROUND AIR DOOR FWD LANDING ANGLE IS CORRODED. REMOVED FWD LANDING ANGLE IAW SRM 51-42-06 AND INSTALLED NEW FWD LANDING ANGLE IAW SRM 51-42-06 AND DWG 601R35226 REV. P AND COMPLIED WITH TASK CARD 51-900-1003-SKY.
LOW PRESSURE GROUND AIR DOOR MOUNTING PLATE IS CORRODED. REMOVED AND REPLACED BY NEW MOUNTING PLATE AT LOW PRESSURE GROUND AIR DOOR, REF. SRM 51-42-06, REV. 39, AND DWG 601R35226 REV. P. COMPLIED WITH TASK CARD 51-900-1003-SKY. PERFORMED LEAK CHECK GOOD, NO LEAKS NOTED.
LOW PRESSURE GROUND AIR DOOR AFT INTERNAL STRUCTURE ANGLE IS CORRODED. REMOVED AFT ANGLE IAW SRM 51-42-06 AND INSTALLED NEW AFT ANGLE IAW SRM 51-42-06 AND IAW DWG 601R35226 REV. P. PERFORMED LEAK CHECK GOOD,
LOW PRESSURE GROUND AIR DOOR FWD INTERNAL STRUCTURE IS CORRODED. REMOVED FWD ANGLE IAW SRM 51-42-06 AND INSTALLED NEW FWD ANGLE IAW SRM 51-42-06. PERFORMED LEAK CHECK GOOD.
BS 625.30, S14L, ATTACHING ANGLE FROM THE FRAME TO THE INTERCOSTAL ON THE REAR PRESSURE BULKHEAD, IS CRACKED. INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL IAW DWG 601-35012 REV D, REO 601R-53-61-422 REV NC, SRM 51-42-21, AND SKYWEST TASK CARD 51-900-1003-SKY.
LEFT WING LOWER SKIN CHAFFED AT WS127.25 WHERE FLAP FAIRING MAKE CONTACT. REPAIRED LT WING LOWER SKIN WS127.25 IAW REO 601R-57-21-3992 REV -.
LEFT WING LOWER SKIN CHAFED AT WS 264 WHERE FLAP FAIRING MAKE CONTACT. REPAIRED LH WING LOWER SKIN WS 264 IAW REO 601R-57-21-3988, REV-, & SKYWEST TASK CARD 51-900-1003-SKY.
RIGHT WING LOWER SKIN FRETTING AND GOUGED AT TRAILING EDGE BL45.00 WHERE FAIRING MAKES CONTACT. REPAIRED RT WING LOWER SKIN FRETTING AND GOUGE AT TRAILING EDGE BL45.00 WHERE FAIRING MAKES CONTACT REF REO 601R-57-21-880 REV-D, , DWG# 601R10046 REV. V, SRM 51-12-00 REV 39.
FRAME AT BS 605 AND BETWEEN S20L-18L HAS SEVERAL CORROSION AND CRACKED AT S18L. REMOVED AND REPLACED BY NEW FRAME SECTION AT BS 605 BETWEEN S20L-S18L AND WL 73 REF. DWG 601R36026 REV. AF, SRM 51-42-06 AND SRM 51-42-21, REV. 39. COMPLIED WITH TASK CARD 51-900-1003-SKY. PERFORMED LEAK CHECK GOOD, NO LEAKS NOTED.
THE LT HORIZONTAL STAB ELEVATOR HINGE NR 1 IS CHAFED/GOUGED. REPAIRED LT HORIZONTAL STAB ELEVATOR HINGE NR 1 IAW REO 601R-55-11-807 REV -. AND COMPLIED WITH TASK CARD 51-900-1003-SKY.
RIGHT PRESSURE FLOOR SILL HAS MULTIPLE AREAS OF CORROSION BETWEEN FS409+128 AND FS559. REMOVED CORROSION ON RT FLOOR SILL BETWEEN FS409+128 AND FS559 AND FOUND TO BE WITHIN LIMITS. REF. GREO 601R-53-41-666, REV. C, DISPOSITION 1.2. COMPLIED WITH TASK CARD 51-900-1003-SKY.
LEFT HAND PRESSURE FLOOR SILL HAS MULTIPLE AREAS OF CORROSION BETWEEN FS409 +128 AND FS559. REMOVED CORROSION ON LT FLOOR SILL BETWEEN FS409+128 AND FS559.00 AND FOUND TO BE WITHIN LIMITS. REF. GREO 601R-53-41-666, REV. -C, DISPOSITION 1.2. COMPLIED WITH TASK CARD 51-900-1003-SKY.
LEFT WING REAR SPAR WS 130.00 RIB IS BENT. REMOVED AND REPLACED BY NEW LH WING REAR SPAR RIB, REF. DWG 601R10339, REV. D, SRM 51-42-21, REVISION 39, AND SRM 51-42-06 REVISION 39, COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.
2EA FASTENER HOLES WITH NOTED CORROSION ON THE HORIZONTAL STABILIZER, UNDER ACCESS PANEL 333AL (MARKED). (C-CHECK RO 01/03/2026)REMOVED CORROSION ON 2EA FASTENER HOLES ON THE HORIZONTAL STABILIZER, UNDER ACCESS PANEL 333AL. REF 601R-55-11-812 REV. --, DATED: 2025-11-24. STEPS 3-5. REMAINING REO STEPS COMPLIED WITH ON CAMP # 31014392. SEE CONTINUATION CARD FOR DETAILS. M-337 AND SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH.
LEFT FLAP HINGE BOX AT WS220 AFT HINGE ATTACH FITTING CHAFED. REPAIRED LH FLAP HINGE BOX AT WS 220 AFT HINGE ATTACH FITTING IAW REO 601R-57-21-3984 REV -. AND COMPLIED WITH TASK CARD 51-900-1003-SKY.
11EA OBLONG HOLES ON THE HORIZONTAL STABILIZER, UNDER ACCESS PANEL 333AL REPAIRED ELONGATED SCREW HOLES ON THE HORIZONTAL STABILIZER, UNDER ACCESS PANEL 333AL. REF REO 601R-55-11-812 REV. --,
FWD UPPER RETAINING PLATE FOR LT WING STUB FAIRING CHAFING AGAINST FUSELAGE EXTERNAL SKIN. REPAIRED FWD UPPER RETAINING PLATE FOR LH WING STUB FAIRING (APRON SKIN) IAW REO 601R-53-41-3365 REV -. COMPLIED WITH TASK CARD 51-900-1003-SKY.
CHAFING ON RT INBD FLAP OTBD FLAP VANE ACTUATOR BODY. REPAIRED RH INBD FLAP OTBD FLAP VANE ACTUATOR BODY IAW REO 601R-57-52-2533 REV.-.
LEFT INBD FLAP VANE LEADING EDGE IS CHAFED IN MULTIPLE LOCATIONS. LT INBOARD FLAP VANE LEADING EDGE 2 EA. AREAS BLENDED AND REPAIRED TO BE WITHIN LIMITS. REF REO 601R-57-52-004, REV -D, 2012-12-19. 1 EA. BLEND ON SKIN PANEL 601R14303-51 FOUND TO BE OUT OF LIMITS, REPLACED OUT OF LIMITS LEADING EDGE SKIN AS PER DWG 601R14302 REV. -E AND CRJ200 SRM 51-42-13 REV. 39.
LEFT INBD FLAP OTBD HINGE ARM CHAFED ON FWD PIVOT FITTING 3EA. LOCATIONS. REPAIRED LH INBD FLAP OTBD HINGE ARM CHAFE IAW ALL STEPS OF REO REO 601R-57-54-379 REV -. SKYWEST TASK CARD 51-900-1002-SKY COMPLIED WITH.
LH INBD FLAP INBD HINGE ARM CHAFFED ON FWD PIVOT FITTING. COMPLIED WITH REPAIR AT LH IB FLAP HINGE ARM REF. CRJ-200 REO 601R-57-54-382 REV-. ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1003-SKY.
AFT CARGO FLOOR SUPPORT, RBL 9, BETWEEN BS 559+64 AND BS.559+80 HAS SPOTS OF CORROSION. BLENDED REPORTED CORROSION ON THE FLOOR SUPPORT INNER CAP FLANGE BETWEEN BS 559+64 AND BS 559+80 IAW SRM 51-21-06. BLENDED AREA WAS FOUND OUT OF LIMITED IAW SRM 53-31-43 AND SRM 53-00-00 FIG 10, ACCOMPLISHED A FLOOR SUPPORT INNER CAP FLANGE REPAIR IAW SRM 53-00-43, REPAIR 01, FIG 203, SHEET 2, SRM 51-42-13, & SRM 51-42-06, REV 39. SKYWEST TASK CARD 51-900-1003-SKY.
FRAME TO LONGERON CLEAT AT WL73.00, LH FS461.50 IS GOUGED ON UPPER FORWARD SIDE. REMOVED AND REPLACED BY NEW FRAME TO LONGERON CLEAT AT WL73.00, LT FS461.50 REF. DWG 601R31145 REV. -P, DWG 601R31034 REV. -F AND SRM 51-42-21, REV. 39, PERFORMED LEAK CHECK GOOD,
FRAME TO LONGERON CLEAT AT WL73.00, RH FS484.00 IS GOUGED ON AFT SIDE AT FLOOR (C-CHECK RO 01/03/2026)BLENDED GOUGED AREA ON FRAME TO LONGERON CLEAT AT WL73.00 RH FS 484.00 REF REO 601R-53-41-3366 REV -- DATED 2025-11-04 STEPS 1 THROUGH 4. ORIGINAL THICKNESS =0.150", REMAINING =0.139", MATERIAL LOSS =0.011. SEE CONTINUATION CARD FOR WORK DETAILS. COMPLIED WITH SKYWEST M-337 AND COMPLIED WITH SKYWEST CARD NO. 51-900-1003-SKY.
AFT CARGO DOOR LOWER SILL HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 01/03/2026)AFT CARGO DOOR LOWER SILL IS REMOVED AND REPLACED WITH NEW IAW DWG 601R35011 REV. -R, SRM 51-42-06, SRM 51-42-21 AND REO 601R-53-61-593, REV. -A,
FS559.00 ON RT SIDE JUST ABOVE SILL CORRODED ON STRAP OF INNER FACE OF FRAME. REPLACED WITH NEW STRAP P/N: 601R32026-321 AT BULKHEAD ON RH SIDE @FS559.00 IAW DWG 601R32026 REV. -T, REF SRM 51-42-06, APPLIED FILLET SEAL TO PARTS REF AMM 51-23-00 AND RESTORED FINISH TO PARTS REF SRM 51-21-16 AND COMPLIED WITH TASK CARD 51-900-1003-SKY
RBL9 HAS MULTIPLE SPOTS OF CORROSION ON TOP PLATE BETWEEN BS 409 TO BS 409+64. REPAIRED MULTIPLE SPOTS OF CORROSION ON TOP PLATE OF FLOORBEAM CAP REF SRM 53-00-43, REPAIR 2, STEP 5 A (7) FIG. 203 , REO. 601R-53-31-1354, REV--, STEPS 1 - 9, ALL OTHER REQUIREMENTS IAW DWG 601R31117, REV E & DWG 601R31030, REV. N . COMPLIED WITH TASK CARD 51-900-1003-SKY.
CORROSION ON TOP OF RBL9 BETWEEN FS513.00 TO FS529.00. REPAIRED RBL9 BETWEEN FS513 TO FS529 FLOOR SUPPORT EXTRUSION AT RBL 9.00 FS409.00+128-FS529.00. REF. REO 601R-53-41-3361 REV -, DWG 601R31005 REV. B, DWG 601R31118 REV. L, LEAK CHECK GOOD, NO LEAKS NOTED
RIGHT CARGO FLOOR SILL FROM BS.559+85 TO BS 559+115, RBL 36 HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND INSTALL A NEW RT CARGO FLOOR SILL, BS 559+85 - 559+115 IAW SRM 51-42-21, SRM 51-42-06, SRM 51-45-00 AND DWG 601R31133, REV J. COMPLIED WITH TASK CARD 51-900-1003-SKY.
CORROSION ON THE LOWER SUPPORT ANGLE AT FS409.00 BETWEEN STGR26L - 26R. REMOVED AND REPLACED BY NEW LOWER SUPPORT ANGLE P/N 601R32200-17 AT FS409.00 BETWEEN STGR26L - 26R REF. DWG 601R31057 REV. -J, DWG 601R32200 REV. -V, CRJ-200, SRM 51-42-06 AND CRJ-200, SRM 51-42-21 REV. 39.
LH AILERON LOWER LEADING EDGE CHAFFED. )REMOVED AND INSTALLED NEW LH AILERON INBOARD LOWER LEADING EDGE SKIN SHROUD P/N CC670-13053-1 REF. DWG CC670-13000 REV. -D, CRJ200 SRM 51-42-21 AND CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.
LEFT AILERON UPPER LEADING EDGE CHAFED. REMOVED DAMAGED LH AILERON UPPER LEADING EDGE SKIN REF. SRM 51-42-06, SRM 51-42-21 AND SRM 51-42-22 AND INSTALLED NEW LH AILERON UPPER LEADING EDGE SKIN REF. DWG CC670-13000 REV. -D, SRM 51-42-06, SRM 51-42-21 AND SRM 51-42-22.
1EA ELONGATED HOLE NOTED UNDER FUSELAGE FAIRING 191BB, BETWEEN STR18L-STR19L AT FS409+96. REPAIRED 1EA ELONGATED HOLE UNDER FUSELAGE FAIRING 191BB, BETWEEN STR18L-STR19L AT FS409+96, REF. REO REO 601R-53-31-1356 REV -.
RH OVERWING EMERGENCY EXIT HAS DENT ON EXTERNAL SKIN LOWER FWD CORNER (MARKED) (C-CHECK RO 01/03/2026)REPAIRED RH OVERWING EMER EXIT DENT IAW ALL STEPS OF REO 601R-52-21-172 REV -A DATED 2025-11-20. M-337 AND SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH.
RIGHT WING LEADING EDGE HAS A FASTENER MISSING AT OTBD JOINT SEAM AT APPROX WS 353. REPAIRED RH WING LEADING EDGE ELONGATED HOKES AT OTBD JOINT SEAM @ APROX WS353.00 IAW REO 601R-57-41-1206 REV. --,
PERMANENT DISPOSITION FOR BLENDED SKIN AND MISDRILL DAMAGE TO FUSELAGE SKIN BETWEEN FS559+112 ̉‰ FS574.00 & STR15L ̉‰ STR16L., COMPLIED WITH PERMANENT REPAIR ON FUSELAGE SKIN BETWEEN FS559+112-FS574.00, STGR15L-STGR16L, REF. REO 601R-53-61-8417, REV. --, DATE 2025-12-17. COMPLIED WITH TASK CARD 51-900-1003-SKY. PERFORMED FUSELAGE PRESSURIZATION LEAK CHECK OF REPAIR AREA, NO LEAKS NOTED AT THIS TIME. SEE CONTINUATION CARD FOR DETAILS.
PERFORMED TEMPORARY REPAIR TO 4 DAMAGED RIVETS AND 1 BURN MARK ON RH SIDE OF FUSELAGE BETWEEN FS409+16 AND FS409+32, ALSO BETWEEN STR23R AND STR24R. WORK DONE IN ACCORDANCE WITH REO 601R-53-31-1134 REV A DATED: 2020-08-19. COMPLIED WITH EDDY CURRENT INSPECTION OF REWORKED AREA IN REFERENCE TO REO 601R-53-31-1134 REV A DATED: 2020-08-19 AND REO 601R-53-00-115 REV E
COMPLY WITH SCHEDULED MAINTENANCE CODE: RA92210-601R-53-61-8197 N454SW MXCODEID76131-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 92210CORROSION DAMAGE ON AFT WEB OF FS 574.00 BETWEEN STR20L - 21L. PERFORMED TEMPORARY REPAIR OF CORROSION DAMAGE ON AFT WEB OF FRAME BS 574 BETWEEN S20L - 21L WITH REFERENCE TO REO 601R-53-61-8197 REV A. REMOVED AND REPLACED BY NEW FRAME SECTION AT BS 574 BETWEEN S20L TO 20R IAW SRM 51-42-06, REV 39, AND DWG 601R36024, REV N. COMPLIED WITH TASK CARD 51-900-1003-SKY. PERFORMED LEAK CHECK GOOD, NO LEAKS NOTED AT THIS TIME.
COMPLY WITH SCHEDULED MAINTENANCE CODE: RA92498-601R-53-61-8196 MXCODEID76417-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 92498THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 1700 FLIGHT HOURS FROM INCORPORATION OF REO 601R-53-61-8196., PART NUMBER: - , SERIAL NUMBER: 7749, POSITION: (C-CHECK RO 01/03/2026)PERFORMED PERMANENT REPAIR ON RA ID: 92498 AT BULKHEAD AT FS621.00 BETWEEN LBL 18.00-LBL27.50, REF. REO 601R-53-61-8413 REV. --, DATED: 2025-11-14. COMPLIED WITH TASK CARD 51-900-1003-SKY. PERFORMED LEAK CHECK GOOD, NO LEAKS NOTED AT THIS TIME. SEE CONTINUATION CARD FOR DETAILS.
BURNING SMELL FOR 1-2 MINUTES COMING FROM CAPTAINS SIDE COCKPIT VENT. ONCE WE IDENTIFIED IT WAS COMING FROM CA SIDE VENT, SMELL STARTED TO GO AWAY ON ITS OWN WITHOUT ANY INTERVENTION. REFER TO ML 30434357 FOR REMOVAL AND REPLACEMENT OF THE LH AIR CYCLE MACHINE (ACM). NO BURNING SMELLS WERE DETECTED IN THE FLIGHT STATION WHILE PERFORMING OPERATIONAL CHECKS OF THE AIR CONDITIONING SYSTEM.
D: GEAR DISAGREE WARNING MESSAGE, SHOWED THE RIGHT LANDING GEAR WAS NOT RETRACTED. RAN QRH AND FIXED THE PROBLEM. GOT THREE GREEN LIGHTS AND RETURNED TO PRC.C: MEL 32-30-1CAT: A DUE DATE: 1 FC TAC NOT EXCEED: 36090. ODI EVENT REQUIRES UPPER MANAGEMENT APPROVAL TO CLEAR MEL. GEAR DISAGREE WARNING MESSAGE, SHOWED THE RIGHT LANDING GEAR WAS NOT RETRACTED. RAN QRH AND FIXED THE PROBLEM. GOT THREE GREEN LIGHTS AND RETURNED TO PRC. (FLIGHT 5071) DEFERRED LANDING GEAR RETRACTION SYSTEM PER MEL 32-30-1, MX ACTION COMPLIED WITH. PLACARDS INSTALLED, CAT 2 DOWNGRADED
PUNCTURE ON THE R/H FUSELAGE BETWEEN FS 559+96 AND 559+112 AND BETWEEN STGR 16R AND 17R MEASURING APPROX 3.5" H X 4" L. THIS IS CLASSIFIED AS A MAJOR REPAIR. FORM M-337 INITIATED. (FILED CLOSED) PERFORMED PERMANENT REPAIR ON R/H FUSELAGE BETWEEN FS 559+96 AND 559+112 AND BETWEEN STGR 16R AND 17R IAW REO 601R-53-51-679 REV -- DATED 2024-08-13.. PERMANENT REPAIR COMPLETED BY MHIRJ MRT AS STATED IN THE STATEMENT OF WORK. COMPLIED WITH STRUCTURAL MAJOR REPAIR TASK CARD 51-900-1003-SKY. COMPLETED FORM M-337. A/C OKAY FOR SERVICE AT THIS TIME.REFERENCE CP 28664057 FOR STEP 3 OF REO 601R-53-51-679, REFERENCE CP 28664063 FOR STEP 4 OF REO 601R-53-51-679. REFERENCE CP 28672239 FOR PRESSURIZATION CHECK OF REPAIRS.
CORROSION DAMAGE ON AFT WEB OF FS 574.00 BETWEEN STR20L - 21L (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
CORROSION DAMAGE ON AFT WEB OF FS 574.00 BETWEEN STR20L - 21L (FILED CLOSED) PERFORMED TEMPORARY REPAIR OF CORROSION DAMAGE ON AFT WEB OF FRAME FS 574.00 BETWEEN STR20L - 21L WITH REFERENCE TO REO 601R-53-61-8197 REV A DATED 07/11/2024. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND NDTM PART 6 53-00-096 WITH NO CRACKS FOUND. COMPLETED CORROSION FINDINGS REPORT. COMPLIED WITH TASK CARD 53-900--1003-SKY. COMPLIED WITH M-337. THIS DISPOSITION IS VALED FOR 1700 FLIGHT HOURS AND REQUIRES VISUAL INSPECTION OF REPAIRED AREA FOR ANY DAMAGE PROPAGATION AT INTERVALS NOT TO EXCEED 600 FLIGHT HOURS.
DENT LOCATED 1.5" FORWARD OF FS 605.00 BETWEEN STR 19L AND STR 20L. (FILED CLOSED)REPAIRED DENT LOCATED 1.5" FORWARD OF FS 605.00 BETWEEN STR 19L AND STR 20L IN REF TO REO 601R-53-61-8202, REV--, DATED 2024-07-18. COMPLETED TASK CARD 51-900-1003-SKY AND M-337.
R/H PRESSURE FLOOR SILL AT BL 36.00 HAS 8 SMALL, SURFACE SPOTS OF CORROSION LOCATED ABOUT 3" FOWARD OF FS439.00 AND EXTENDING TO FS 484.00. (FILED CLOSED) REPAIRED ALL 8 SMALL CORROSION DAMAGE ON R/H PRESSURE FLOOR SILL AT FS436.00 THROUGH FS 484.00 ON RBL 36.00 WITH REFERENCE TO REO 601R-53-41-666 REV -C DATED 2012-11-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE TO CRJ-200 NDTM PART 4 51-00-001 AND FOUND WITHIN LIMITS OF REO 601R-53-41-666. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO CRJ-200 NDTM PART 1 51-20-06 AND PART 6 53-00-096 WITH NO DEFECTS FOUND. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS.
R/H PRESSURE FLOOR SILL AT BL 36.00 HAS 8 SMALL, SURFACE SPOTS OF CORROSION LOCATED ABOUT 3" FOWARD OF FS439.00 AND EXTENDING TO FS 484.00.THIS IS CURRENTLY A WORK IN PROGRESS
MULTIPLE AREAS OF CORROSION ON THE LH PRESSURE FLOOR SILL BETWEEN FS 424.00 AND FS 473.00 ON LBL 36.00. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
MULTIPLE AREAS OF CORROSION ON THE LH PRESSURE FLOOR SILL BETWEEN FS 424.00 AND FS 473.00 ON LBL 36.00. (FILED CLOSED) BLENDED CORROSION DAMAGE ON THE LH PRESSURE FLOOR SILL BETWEEN FS 424.00 AND FS 473.00 ON LBL 36.00 WITH REFERENCE TO REO 601R-53-41-3240 REV -- DATED 2024-07-02 AND REO 601R-53-41-666 REV -C DATED 2012-11-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE TO NDTM PART 4 51-00-001 AND FOUND WITHIN LIMITS OF REO 601R-53-41-3240 AND REO 601R-53-41-666. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND PART 6 53-00-096 WITH NO DEFECTS FOUND. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS.
CORROSION ON PRESSURE FLOOR SILL AT FS 461.00 ON RBL 36.00 (FILED - CLOSED) REPAIRED CORROSION DAMAGE ON PRESSURE FLOOR SILL AT FS 461.00 ON RBL 36.00 WITH REFERENCE TO REO 601R-53-41-666 REV -C DATED 2012-11-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE TO NDTM PART 4 51-00-001 AND FOUND WITHIN LIMITS OF REO 601R-53-41-666. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND PART 6 53-00-096 WITH NO DEFECTS FOUND. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS.
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 INTERCOSTAL ON AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGER 14R IN REF TO SRM 51-42-21.COMPLETED TASK CARD 51-900-1003-SKY AND M-337.
CORROSION ON FWD SIDE OF FS 574.00 BETWEEN STGR 23R AND 24R (FILED CLOSED)PERFORMED TEMPORARY REPAIR OF CORROSION DAMAGE ON FWD SIDE OF FRAME FS 574.00 BETWEEN STR23R - 24R WITH REFERENCE TO REO 601R-53-61-8197 REV A DATED 07/11/2024. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND NDTM PART 6 53-00-096 WITH NO CRACKS FOUND. COMPLETED CORROSION FINDINGS REPORT. COMPLIED WITH TASK CARD 53-900--1003-SKY. COMPLIED WITH M-337. THIS DISPOSITION IS VALED FOR 1700 FLIGHT HOURS AND REQUIRES VISUAL INSPECTION OF REPAIRED AREA FOR ANY DAMAGE PROPAGATION AT INTERVALS NOT TO EXCEED 600 FLIGHT HOURS.
CORROSION ON FWD SIDE OF FS 574.00 BETWEEN STGR 26L AND 27 (CENTER) (FILED CLOSED)PERFORMED TEMPORARY REPAIR OF FRAME FS 574.00 BETWEN STGR26L AND STGR27 WITH REFERENCE TO SRM 53-00-15 REPAIR 2, PG 204 AND REO 601R-53-61-8197 REV "A" DATED 07/10/2024. THIS DISPOSITION IS VALID FOR 1700 FLIGHT HOURS. COMPLETED CORROSION FINDINGS REPORT. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. SEE CHILD CAMP FOR EDDY CURRENT INSPECTION.TEMP REPAIR VALID FOR 1700 FH.
CORROSION ON AFT SIDE OF FS 574.00 BETWEEN STGR 21L AND 22L (FILED CLOSED)PERFORMED TEMPORARY REPAIR OF FRAME FS 574.00 BETWEN STGR21L AND 22L WITH REFERENCE TO SRM 53-00-15 REPAIR 2, PG 204 AND REO 601R-53-61-8197 REV "A" DATED 07/11/2024. THIS DISPOSITION IS VALID FOR 1700 FLIGHT HOURS. COMPLETED CORROSION FINDINGS REPORT. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. SEE CP 28480469 FOR EDDY CURRENT INSPECTION.TEMP REPAIR VALID FOR 1700 FH.
D: APU DID NOT START DURING DESCENT BELOW 15000. TRIED AGAIN AFTER TWO MIN APU STARTED BUT A STRONG FUEL SMELL CAME THROUGH. SHUTDOWN APU. DID NOT ATTEMPT A RESTART. / C: MEL 49-10-1A / CAT C DUE 5/12/22 / APU DID NOT START DURING DESCENT BELOW 15000. TRIED AGAIN AFTER TWO MIN APU STARTED BUT A STRONG FUEL SMELL CAME THROUGH. SHUTDOWN APU. DID NOT ATTEMPT A RESTART. (FLIGHT 4760 - FILED CLOSED) MAY 02, 2022 STATION: ATW--UPON INSPECTION FOUND VERY SMALL RESIDUAL PUDDLE OF FUEL IN THE APU ENCLOSURE. CLEANED THE FUEL OUT OF THE APU ENCLOSURE AND THE RAN THE APU TO INVESTIGATE THE SMELL OF FUEL. RAN BOTH THE LEFT AND RIGHT PACK'S TO SEE IF WE COULD MAKE THE SMELLS COME BACK. COULD NOT DUPLICATE THE ODOR THROUGHOUT THE AIRCRAFT. DID THIS A COUPLE OF TIMES WITH THE SAME RESULTS. NO ODORS TO BE FOUND. WHILE RUNNING THE APU THE EGT WOULD SPIKE INTO THE YELLOW RANGE AND THEN DROP BACK DOWN INTO THE NORMAL GREEN. ALL WORK DOWN WAS DONE IN REFERENCE WITH FIM 21-21-00. NEEDS TO BE FURTHER TROUBLESHOOT AT THE NEXT OVERNIGHT DEFERRED THE APU PER CRJ 200 MEL 49-10-1A. COMPLIED WITH MX ACTIONS . PLACARDS INSTALLED.
GEAR DISAGREE AFTER TO, NOSE GEAR FAILED TO RETRACT. SOUNDED LIKE GEAR WAS STILL DOWN AND LOCKED WITH NO ATTEMPT TO RAISE. QRH FOLLOWED, SECURED LANDING GEAR DOWN AND RETURNED TO FIELD WITHOUT FURTHER ISSUE. GEAR PINS ALL ON BOARD, NO ABNORMAL PUSHBACK WAS NOTICED (FLIGHT 5506 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24663841 WITH THE FOLLOWING CORRECTIVE ACTION: "PERFORMED LANDING GEAR EXTENSION AND RETRACTION IAW AMM 32-30-00. OPS CHECK GOOD AT THIS TIME. COULD NOT DUPLICATE FAULT. / REFERENCE CP 24666809 FOR REPLACEMENT OF THE NLG EXTENDED/CENTERING HARNESS BRACKET. / REFERENCE CP 24666855 FOR REPLACEMENT OF THE NLG EXTENDED/CENTERING HARNESS. / REFERENCE CP 24666871 FOR DAMAGE ON THE NLG OUTER CYLINDER. / "
ON CLIMB OUT AFTER PASSING SOMEWHERE BETWEEN 13-14,000 FT WE RECEIVED A Ãâ¬ÅR 14TH DUCTÃâ¬? MASTER WARNING MESSAGE. THE AIRCRAFT HAD NORMAL CLIMB POWER APPLIED AT THE TIME. WE ELECTED TO RETURN TO 15,000FT TO RUN THE QRC/QRH, AND BEGAN TO RETURN TO CHICAGO. WE COMPLIED WITH THE QRH PROCEDURE AND THE MESSAGE REMAINED UNTIL WE WERE INSTRUCTED PER THE QRH TO BRING THE THRUST LEVER TO IDLE AT WHICH POINT THE MESSAGE CLEARED. THE MESSAGE THEN INTERMITTENTLY APPEARED AND DISAPPEARED SEVERAL TIMES UNTIL LANDING. NO OTHER ABNORMALITIES WERE NOTED AT THE TIME. (FLIGHT 5040 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24452629 WITH THE FOLLOWING CORRECTIVE ACTION: "TROUBLESHOT IN REFERENCE TO WM 36-21-00 AND FIM 36-20-00. CHECKED FOR CONTINUITY FROM PIN 23 TO PIN 38 ON 2P1WK. READING WAS 5 OHMS. PERFORMED RESISTANCE CHECK OF PIN 23 AND 38 TO GROUND ON 2P1WK. BOTH READINGS WERE OPEN ( 30 M ). NO OPENS OR SHORTS TO GROUND FOUND. COMPLIED WITH FIM 36-20-00. REMOVED AND REPLACED THE RIGHT BLEED LEAK CONTROL UNIT IN REFERENCE TO AMM 36-21-10. SYSTEM OPS CHECK GOOD AT THIS TIME."
RH WING IB FLAP WELL, "RACETRACK" GROMMET DISPLACED AT WS140. ( AGING AIRCRAFT INSP RO 1/16/2022) INSTALLED RH WING IB FLAP WELL, "RACETRACK" GROMMET AT WS140 IN REFERENCE TO AMM 27-11-00.
RBL27 IB VERTICAL POST AT FS409+128 APPEARS CRACKED IN THE RADIUS. ( AGING AIRCRAFT INSP RO 1/16/2022) REPAIRED RBL27 FS409+128 VERTICAL POST IN ACCORDANCE WITH REO 601R-53-41-056
LH IB GROUND SPOILER PCU LINK HARDWARE APPEARS WORN AND CORRODED ( AGING AIRCRAFT INSP RO 1/16/2022) REMOVED AND REPLACED LH IB GROUND SPOILER PCU LINK HARDWARE IN REFERENCE TO AMM 27-62-01
RH IB FLAP VANE LEADING EDGE APPEARS CHAFFED AT APPROX WS104. ( AGING AIRCRAFT INSP RO 1/16/2022) REMOVED AND REPLACED RH IB FLAP IN REFERENCE TO AMM 27-54-01 AND IN REFERENCE TO AMM 57-52-08. VERFIFIED CORRECT RIG OF LH AND RH FLAPS IN REFERENCE TO AMM 27-54-01.
RH INBOARD FLAP VANE LEADING EDGE APPEARS CHAFFED AT WS56 ( AGING AIRCRAFT INSP RO 1/16/2022) REMOVED AND REPLACED RH IB FLAP IN REFERENCE TO AMM 27-54-01 AND IN REFERENCE TO AMM 57-52-08. VERFIFIED CORRECT RIG OF LH AND RH FLAPS IN REFERENCE TO AMM 27-54-01.
LH OB GROUND SPOILER PCU LINK HARDWARE APPEARS WORN AND CORRODED WS120. ( AGING AIRCRAFT INSP RO 1/16/2022) REMOVED AND REPLACED LH OB GROUND SPOILER PCU LINK HARDWARE IN REFERENCE TO AMM 27-62-01
RH WING IB FLAP WELL, "RACETRACK" GROMMET DISPLACED IN TWO LOCATIONS. WS97 AND WS140. ( AGING AIRCRAFT INSP RO 1/16/2022) INSTALLED NEW RACETRACK GROMMET ON THE RH WING AT WS97 IN REFERENCE TO AMM 27-11-00. FOR WS 140 GROMMET PLEASE SEE CP 24163284-1.
RH OB FLAP CAM FOLLOWER BEARING APPEARS SEIZED. WS163. ( AGING AIRCRAFT INSP RO 1/16/2022) REMOVED AND REPLACED RH OB FLAP CAM FOLLOWER BEARING IN REFERENCE TO AMM 20-21-00. / NEW BEARING SPINS FREELY.
RH WING IB FLAP WELL, "RACETRACK" GROMMET DAMAGED AND LOOSE WS120. ( AGING AIRCRAFT INSP RO 1/16/2022) INSTALLED RH WING IB FLAP WELL, "RACETRACK" GROMMET AT WS120 IN REFERENCE TO AMM 27-11-00.
LBL18 OB VERTICAL POST AT FS409+128 APPEARS CRACKED IN THE RADIUS. ( AGING AIRCRAFT INSP RO 1/16/2022) REPAIRED LBL 18 FS409+128 VERTICAL POST IN ACCORDANCE WITH REO 601R-54-41-056
MACH TRIM AND STAB TRIM MESSAGE, 200 FEET AFTER TAKEOFF. FLIGHT 5141-FILED CLOSED. THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22160283 WITH THE FOLLOWING CORRECTIVE ACTION: "TROUBLESHOT PER CRJ200 FIM 27-40-00 PG 28,29 LABEL 273 BIT 16 AND 17. REMOVED AND REPLACED THE MCU, REF CRJ200 AMM 27-42-05. NO DEFECTS NOTED AT THIS TIME. COMPLIED WITH TASK CARD 34-220-1008-SKY. AIRCRAFT OKAY FOR SERVICE AT THIS TIME. FOUND NO HISTORY OF STAB TRIM/MACH TRIM ISSUES IN THE PAST 3 MONTHS, REF CP 22160446 FOR PARTS INFORMATION AND TASK CARD COMPLIANCE.
CAPT SIDE WINDOW CRACKED FLIGHT 4259. REMOVED AND REPLACED LEFT SIDE WINDOW WITH A SERVICEABLE UNIT IAW AMM. COMPLETED TASK CARD PRESSURE CHECK GOOD AND NO LEAKS NOTED AT THIS TIME.
RIGHT THRUST REVERSER UNLOCKED CAUTION ON TAKE OFF ROLL. PERFORMED STATIC TAKE OFF ROLL AND MESSAGE CAME ON ABOUT 60 KNOTS. FOUND STOW SWITCH TO BE OUT OF RIG. RIGGED RH TR STOW SWITCH IAW AMM. OPS CHECK GOOD AT THIS TIME.
LT UPPER SKIN ASSY SEAL RETAINER CRACKED. (C-CHECK) RO: 07/18/2019 REMOVED AND REPLACED LT UPPER SKIN ASSY SEAL RETAINER IAW SRM.
LT MLG TRUNNION REQUIRES REPLACEMENT DUE TO CRACK AT FASTENER HOLE #20. (C-CHECK) RO: 07/18/2019 LT MLG TRUNNION HOLE REPAIRED IAW SRM AND REO.
ONE ELONGATED HOLE ON 409+128 RBL 18.00 OUTBD POST. (C-CHECK) RO: 07/18/2019 REPAIRED ELONGATED HOLE IAW REO.
FLOOR SUPPORT STRAP FS 559.00 RBL 36.0 TO RBL 45.0 WL 72.5 HAS MINOR CORROSION ON UPPER SURFACE. (C-CHECK) RO: 07/18/2019 REMOVED AND REPLACED THE FLOOR SUPPORT STRAP IAW SRM.
FLOOR SUPPORT STRAP FS 559.0 LBL 36.0 TO LBL 45.0 WL 72.5 HAS CORROSION ON UPPER SURFACE. (C-CHECK) RO: 07/18/2019 REMOVED AND REPLACED FLOOR SUPPORT STRAP IAW SRM.
RT FLOOR SILL AT FS 409.00+128 RBL 42 IS CORRODED. (C-CHECK) RO: 07/18/2019 REPAIRED CORROSION DAMAGE ON RT FLOOR SILL AT FS 409.00+128 RBL 42 IAW REO.
RT FLOOR SILL AT FS 484.00 RBL40 IS CORRODED. (C-CHECK) RO: 07/18/2019 REPAIRED CORROSION DAMAGE ON RT FOOR SILL AT FS 484.00 RBL 40 IAW REO.
RT FLOOR SILL BETWEEN FS 449.85 AND FS 451.00 RBL42 IS CORRODED. (C-CHECK) RO: 07/18/2019 REPAIRED RT FLOOR SILL BETWEEN FS 449.85 AND FS 451.00 RBL 42 IAW REO.
BOLT HOLE DOUBLER AT FS 349 BETWEEN LBL 27 AND LBL41 IS CORRODED. (C-CHECK) RO: 07/18/2019 REMOVED AND REPLACED AFFECTED FASTENERS, AND REPLACED P/N 601R38673-43 ANGLE IAW SRM.
SERVICE DOOR LOWER SILL FLOOR SUPPORT ANGLE IS CORRODED BETWEEN FS 319 AND FS 349. (C-CHECK) RO: 07/18/2019 REMOVED AND REPLACED P/N 601R38303-253 IAW SRM.
RT FLOOR SILL AND DOUBLER ARE CORRODED BETWEEN FS 310 AND FS 319. (C-CHECK) RO: 07/18/2019 REMOVED AND REPLACED P/N 601R38669-49 IAW SRM.
PAX DOOR INTERCOSTAL DD4 CORRODED BETWEEN FS320.00 TO FS338.90. (C-CHECK) RO: 07/18/2019 REMOVED AND INSTALLED NEW SERVICEABLE PAX DOOR INTERCOSTAL DD4 IAW SRM.
FOUND INDICATIONS ON FS 409+128 RBL18 BOTH INBD & OTBD POSTS AT JOGGLE APPROX. .5 LONG. (C-CHECK) RO: 07/18/2019 REMOVED CRACKED POSTS AND INSTALLED NEW SERVICABLE INBD AND OTBD POST IAW SRM.
RT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT / RIVNUT LOCATIONS. (C-CHECK) RO: 07/18/2019 REPAIRED RT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIVNUT LOCATIONS IAW SRM AND REO.
REPAIR LT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT / RIVNUT LOCATIONS. (C-CHECK) RO: 07/18/2019 REPAIRED LT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT / RIVNUT LOCATIONS IAW SRM AND REO.
RECEIVED GEAR DISAGREE WARNING MESSAGE ON APPROACH. FOLLOWED QRH PROCEDURE AND AFTER FIRST CYCLE OF THE GEAR HANDLE, ALL GEAR WENT DOWN AND LOCKED. LANDED AND TAXIED TO GATE WITH NO FURTHER INCIDENTS. (FLT#3702) REMOVED AND REPLACED NLG UPLOCK ROLLER AND MOUNT BRACKET WITH A SERVICABLE UNIT IAW CMM. PERFORMED GEAR SWING IAW AMM, OPS CHECK GOOD AT THIS TIME.
GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF. NOSE GEAR DID NOT RETRACT. RAN QRH PROCEDURE. EXTENDED GEAR AND RETURNED TO FIELD. (FLT#3628) FO: 03/11/2019 CLOSED REMOVED AND REPLACED MLG PRIORITY VALVE P/N 4619-3 S/N 14748 IAW AMM. REMOVED AND REPLACED MLG SLECTOR VALVE P/N 750005000 S/N 0263T. PERFORMED GEAR EXTENSION/RETRACTION AND LEAK CHECK OF MLG PRIORITY VALVE AND MLG SELECTOR VALV IAW AMM. OPS CHECK GOOD NO LEAKS NOTED.
THRUST REVERSER UNLOCK. DECLARED EMERGENCY.
FRAME BS 394 BETWEEN STRINGERS 26L TO 26R IS CORRODED. REPAIRED IAW REO.
CARGO FLOOR SUPPORT OTB OF LBL 9 BETWEEN BS 589 AND 621 HAS CORROSION AT NUTPLATES. REPLACED THE FLOOR SUPPORT IAW SRM.
CARGO FLOOR SUPPORT INBD AND OTBD OF LBL 27 BETWEEN BS 589 AND 621 HAS CORROSION AT NUTPLATES. REMOVED AND INSTALLED A NEW SERVICABLE FLOOR SUPPORT IAW SRM.
CARGO DOOR SILL HAS CORROSION AT NUTPLATES. REMOVED AND REPLACED THE DOOR SILL IAW SRM. LEAK CHECKED GOOD.
CARGO BAY RT FLOOR SUPPORT BETWEEN BS 559 +112 AND 621 HAS CORROSION AT NUTPLATES. REMOVED AND REPLACED THE FLOOR SUPORT IAW SRM.
CARGO BAY RT FLOOR SUPPORT OTBD OF RBL 27 BS 589 TO 621 HAS CORROSION AT NUTPLATES. REPAIRED THE FLOOR SUPPORT IAW REO.
LEFT INBD FLAP, INBD VANE CAP CHAFED. INSTALLED A NEW FLAP VANE CAP. IAW SRM.
LEFT INBD FLAP, OTBD VANE CAP CHAFED. INSTALLED A NEW FLAP VANE CAP IAW SRM.
RIGHT INBD FLAP, INBD VANE CAP CHAFED. REPLACED THE FLAP VANE CAP IAW SRM.
AFT FUSELAGE FRAME BELOW FLOOR, BS 574 BETWEEN STRINGERS 25L AND 25R HAS CORROSION. COMPLIED WITH PERMANENT REPAIR OF THE FRAME IAW REO.
AFT FUSELAGE FRAME BELOW FLOOR, BS 589 AT STRINGER 27 HAS CORROSION. REMOVED AND REPLACED THE FRAME SECTION IAW REO AND SRM LEAK CHECKED GOOD.
AFT FUSELAGE BELOW FLOOR, BS 605 BETWEEN STRINGERS 26 AND 27L FRAME HAS CORROSION. REMOVED AND REPLACED THE FRAME SECTION IAW SRM. LEAK CHECKED GOOD.
RIGHT INBD FLAP, OTBD VANE CAP CHAFED. INSTALLED A NEW FLAP VANE CAP IAW SRM.
CORROSION FOUND ON BS 310 FRAME AFT SIDE OF WEB BETWEEN STRINGERS 26L AND 26R. REPLACED THE FRAME SECTION IAW SRM. LEAK CHECKED GOOD.
CORROSION ON FLOORBEAM STRAP BS 559, RBL36. REMOVED AND INSTALLED A NEW STRAP IAW SRM.
FLOORBEAM BS 409.00 IS CORRODED. REMOVED AND REPLACED FLOORBEAM IAW SRM. LEAK CHECKED GOOD.
AILERON PANEL 599BB HAS CHAFING. PANEL 599BB REPLACED IAW SRM.
AILERON PANEL 599AB HAS CHAFING. THE PANEL 599AB REPLACED IAW SRM.
FRAME BS 349 CORRODED STRINGERS 26L TO 26R. REMOVED AND REPLACED THE FRAME IAW SRM. LEAK CHECKED GOOD.
AILERON L/E PANEL 6994B HAS CHAFED. REMOVED AND REPLACED AILERON PANEL 699AB IAW SRM.
CHAFING ON CENTER DIVIDER OF PANEL 422DB. REMOVED AND INSTALLED NEW SEPARATORS IAW SRM.
FLAP HINGE FAIRING 692BB BOTH GUIDE PLATES ARE CHAFED. REMOVED AND INSTALLED THE GUIDE PLATES IAW SRM.
FLAP HINGE FAIRING 697BB THE GUIDE PLATE IS CHAFED. REMOVED AND INSTALLED NEW GUIDE PLATE ON PANEL 697BB IAW SRM.
AILERON L/E PANEL 699BB HAS CHAFING. THE PANEL WAS REPLACED IAW SRM.
DIVIDERS ON PANEL 412DB ARE CHAFED. FWD AND AFT SEPARATORS ON PANEL 412DB REPLACED IAW SRM.
DENT BS 700, STRINGER 18L. REPAIRED IAW REO.
DENT AT BS 621 BELOW STRINGER 20L. REPAIRED IAW REO.
RIGHT ENGINE FLAMEOUT 1800-2000 FT ITT WAS EXCEEDED 1170, HEARD LOUD THUMP, EMERGENCY DECLARED. RETURNED TO FIELD. R & R THE RT ENGINE ASSY IAW AMM. RIG AND LEAK CHECKS ARE GOOD.
BS 605 FRAME CRACKED ABOVE AND BELOW STR 9. REPAIRED THE FRAME IAW REO.
PAX DOOR PANEL 832AL HAS CORROSION AROUND FASTNER HOLES. C-CHECK, REMOVED CORROSION FROM PANEL IAW EA.
RT INBD FLAP VANE T/E INBD UPPER EDGE CHAFED. COMPLIED WITH PERMANENT REPAIR ON RT INBD FLAP VANE T/E INBD UPPER EDGE IAW STS EA.
RIGHT WING T/E CHANNEL FRAME HAS CORROSION APPROXIMATELY. INBD HINGE, INBD GROUND SPOILER. C-CHECK, REPAIRED CORROSION ON RT WING T/E CHANNEL FRAME APPROXIMATELY INBD HINGE ON INBD GROUND SPOILER IAW STS EA.
CARGO DOOR EXTERIOR SKIN HAS A CHAFE AT THE TOP OF DOOR. REPAIRED CHAFE TO CARGO DOOR EXTERIOR SKIN AT THE TOP OF THE DOOR IAW REO.
LEFT INBD FLAP OTBD ACTUATOR AFT HINGE HAS ELONGATED HOLE AT LOWER OTBD CORNER. COMPLIED WITH PERMANENT REPAIR TO LT INBD FLAP, OTBD HINGE FAIRING ATTACHMENT BRACKET ASSY AT WS 127.25 AND THE RETURN LIP EDGE OF THE LIGHTNING HOLE IAW REO.
OVERHEAD EMERGENCY EXIT SIGN, AFT SIDE FIXTURE HAS MULTIPLE BULBS BURNED OUT, REPLACED THE BULBS.
BULB IN EMERGENCY LIGHT ON BULKHEAD NEAR MAIN CABIN DOOR IS BURNED OUT. REPLACED BULB.
VERTICAL STIFFENER AT BL 0.0 AFT FACE OF FS 621 CHAFED. C-CHECK REPAIRED IAW REO.
VERTICAL STIFFENER AT BL 0.0 AFT FACE OF FS 621 CHAFED. C-CHECK REPAIRED IAW REO.
FS 621.0 BULKHEAD FWD FACE HAS SEVEN CHAFED AREAS AT WL 105.0. RBL 36.20, RBL 27.50, RBL 18.0, RBL 9.50, LBL 9.50, LBL 18.0, LBL 27.50, ALL APPROXIMATELY .004" DEEP. C-CHECK REPAIRED IAW REO.
LT INBD FLAP VANE LE CAPS AT FLAP STATION 57 & 110 CHAFED. C-CHECK REPLACED LT INBD FLAP VANE LE CAPS AT FLAP STATION 57 & 110 IAW SRM.
RT INBD FLAP VANE LE CAPS AT FLAP AT FS 110 & 139 ARE CHAFED. C-CHECK REPLACED RT INBD FLAP VANE LE CAPS AT FLAP AT FS 110 & 139 IAW SRM
LT INBD FLAP VANE LE CAPS AT FLAP STATION 57 & 110 ARE CHAFED. C-CHECK REPLACED LT INBD FLAP VANE LE CAPS AT FLAP STATION 57 & 110 IAW SRM.
RT INBD FLAP VANE LE CAPS AT FLAP STATIONS 1109 & 139 ARE CHAFED BEYOND LIMITS. C-CHECK REPLACED FLAP VANE IAW SRM.
FS409+128 VERTICAL POST AT BL0 AFT LT UPPER RADIUS FAILED NDT. C-CHECK REPAIRED IAW REO.
RT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED AT RBL 42. C-CHECK REPAIRED IAW REO.
FS 409+128 VERTICAL POST AT BL 0 AFT LT UPPER RADIUS HAS INDICATION 50 % SCREEN HEIGHT APPROXIMATELY .2 INCHES LONG. C-CHECK REPAIRED IAW REO.
RT FS621.00 FLOOR SUPPORT ANGLE IS CRACKED AT RBL42. C-CHECK REPAIRED IAW REO.
RIGHT REAR EXTERIOR EMERGENCY LIGHT IS BURNED OUT. (FLT 4551) RELAMPED EMERGENCY LIGHT.
GALLEY SERVICE DOOR WILL NOT OPEN. (FLT 4505) LUBRICATED DOOR AS NEEDED AND OPERATED SEVERAL TIMES. OPS CHECK GOOD AT THIS TIME.
GALLEY SERVICE DOOR EMERGENCY EXIT LIGHT IS FALLING OUT. (FLT 4865) REPLACED SERVICE DOOR EMERGENCY EXIT LIGHT.
AFT EMERGENCY CEILING OVERHEAD LIGHT BURNED OUT. (FLT 7766) RELAMPED EMERGENCY LIGHT.
STR 16 RIGHT, BETWEEN FS 349 AND FS 364 IS CRACKED. (SERVICE) REPLACED DAMAGED SECTION OF STRINGER 16 RIGHT IAW SRM.
OVERHEAD AISLE EMERGENCY LIGHT INOP. (FLT 4727) RELAMPED EMERGENCY LIGHT.
NR 2 OVERHEAD EMERGENCY LIGHT IS NOT WORKING. (FLT 4516) RELAMPED EMERGENCY LIGHT.
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4624) RELAMPED EMERGENCY LIGHT.
NR 2 AND NR 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4516) RELAMPED EMERGENCY LIGHTS.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4745) RELAMPED EMERGENCY LIGHT.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4506) RELAMPED EMERGENCY LIGHT.
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4624) RELAMPED EMERGENCY LIGHT.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4828) RELAMPED EMERGENCY LIGHT.
LEFT AFT EXTERIOR OVERWING EMERGENCY LIGHT IS OUT. (FLT 4824) RELAMPED EMERGENCY LIGHT.
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
OVERHEAD EMERGENCY LIGHT AT ROW 10 IS OUT. (FLT 4686) RELAMPED EMERGENCY LIGHT.
NR 3 OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 4468) RELAMPED EMERGENCY LIGHT.
MAIN CABIN DOOR FLOOR LEVEL EMERGENCY EXIT RIGHT SIDE COVER FELL OFF IS BROKEN. (FLT 4522) REPLACED BASE OF FIXTURE FOR MAIN CABIN DOOR FLOOR EMERGENCY LIGHT.
AIRCRAFT ROLLS TO THE LEFT WITH FLAPS SELECTED TO 45 DEGREES. (FLT 1301) REMOVED ROUGH EDGES OF PAINT FROM ALL 4 FLAP ASSEMBLIES IN REFERENCE TO AMM.
FS 559 PRESSURE BULKHEAD CRACKED AT LEFT SIDE. (C-CHECK) REPAIR PER REO.
FS 621 PRESSURE BULKHEAD FORWARD WEB FACE ABOVE UPPER CARGO DOOR TRACK FITTING IS CRACKED. (C-CHECK) REPAIR PER REO.
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4677) RELAMPED EMERGENCY LIGHT.
LEFT OVERWING EXTERIOR AFT EMERGENCY LIGHT IS OUT. (FLT 4689) RELAMPED EMERGENCY LIGHT.
RIGHT FORWARD AND AFT EXTERIOR EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.
AFT OVERHEAD EMERGENCY LIGHT BURNED OUT. (FLT 4656) RELAMPED EMERGENCY LIGHT.
NR 1 AND NR 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4777) RELAMPED EMERGENCY LIGHTS.
AFT CEILING EMERGENCY LIGHT BURNED OUT. (FLT 4474) RELAMPED EMERGENCY LIGHT.
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4615) RELAMPED EMERGENCY LIGHT.
NR 4 CEILING EMERGENCY LIGHT IS OUT. (FLT 4503) RELAMPED EMERGENCY LIGHT.
EXTERIOR LEFT REAR OVERWING EMERGENCY LIGHT IS OUT. (FLT 4672) RELAMPED EMERGENCY LIGHT.
AFT EMERGENCY CEILING LIGHT OUT. (FLT 4459) RELAMPED EMERGENCY LIGHT.
GALLEY SERVICE DOOR WILL NOT OPEN FROM THE OUTSIDE. (FLT 4880) OPERATION CHECK NORMAL.
FLOOR EMERGENCY LIGHTING NEAR MAIN CABIN DOOR INOP. (FLT 4828) REPLACED HARNESS ASSEMBLY PER AMM.
FLT 4572 - NR 3 CEILING EMERGENCY LIGHT INOP. RELAMPED.
FLOOR EMERGENCY LIGHTS AFT OF ROW 9 INOP. (FLT 4675) RESEATED AFT AISLE FLOOR LIGHT STRIP.
FLOOR LEVEL EMERGENCY LIGHTS FROM ROW 8 AFT INOP. (FLT 4505) REPLACED CABLE ASSEMBLY.
FS 559 BULKHEAD CRACKED. (C CHECK) REPAIRED PER REO.
FS 559 PRESSURE BULKHEAD CRACKED. (C CHECK) REPAIRED PER REO.
FS 559 PRESSURE BULKHEAD CRACKED. (C-CHECK) REPAIRED PER REO.
FLOOR SUPPORT STRUCTURE AT FS 484 INTERCOSTAL CRACKED. (C-CHECK) REPAIRED PER SRM AND REO.
CREW ESCAPE HATCH OUTER HANDLE CORRODED. (C-CHECK) REPLACED HANDLE PER SRM AND AMM.
FLT 4540 - AFT SECTION OF EMERGENCY FLOOR LIGHTING INOP. RESECURED LOOSE CONNECTION.
AFT SECTION OF FLOOR LEVEL EMERGENCY LIGHTS INOP. (FLT 4681) DOWN POWERED AND REPOWERED AIRCRAFT, LIGHT OPERATIONS NORMAL.
EMERGENCY LIGHTS AFT OF THE EXIT DOOR INOP. (FLT 4479) REPLACED BATTERY PACK.
FLT 9407 - NLG GEAR DISAGREE WARNING. PERFORMED NOSE GEAR SWINGS, CHECKS GOOD.
FLT 4672 - FLOOR EMERGENCY EXIT LIGHTS AFT OF EXIT ROW INOP. RESEATED CONNECTOR.
FLT 4400 - GEAR DISAGREE ON APPROACH. REPLACED NOSE LANDING GEAR SELECTOR VALVE, PN 750006000 SN OFF 0058T.
FLT 4529 - NOSE GEAR DIDN'T RETRACT ON TAKEOFF AND NOSE STEERING INOP ON LANDING. ACCOMPLISHED FULL SERVICE OF NOSE STRUT.
FLT 4483 - AFT EMERGENCY CEILING FLOOD LIGHT INOP. RELAMPED.
RECEIVED A GEAR DISAGREE MASTER WARNING. MANUALLY EXTENDED GEAR. (FLIGHT NR 3856) REPLACED NOSE DOOR SELECTOR VALVE IAW MM 33-22-20 AND LANDING GEAR CONTROL HANDLE IAW MM 32-31-01. PN 750006000 S/N OFF 0034I P/N OFF 7-45502-5 S/N OFF 1182.
RECEIVED A "GEAR DISAGREE WARNING" ON APPROACH. GEAR EXTENDED NORMALLY ON NEXT APPROACH. (FLIGHT NR 3940) REPLACED NOSE GEAR SELECTOR VALVE IAW MM 32-33-10. INSPECTED LANDING GEAR SYSTEM AND SWUNG GEAR SEVERAL TIMES. OPS CHECK GOOD.
SELECTED GEAR DOWN AND THE NOSE GEAR WOULD NOT EXTEND AND RECEIVED GEAR DISAGREE WARNING MESSAGE. GEAR THEN EXTENDED NORMALLY. (FLT 3845) INSPECTED AND PERFORMED OPERATIONAL CHECKS OF NOSE GEAR EXTENSION AND RETRACTION IAW MM 32-33-00 AND 32-32-00. ALL CHECKS GOOD.
LAST HALF OF FLOOR EMERGENCY LIGHTS DO NOT WORK. (FLT 3857) RESECURED WIRE CONNECTORS. OPS CHECK GOOD.
FLT 3773 - OUTBOARD, RIGHT FLAP WAS DAMAGED BY BIRD STRIKE. REPLACED RIGHT, OUTBOARD FLAP IAW MM 27-54-05. OPS CHECK GOOD.
FLT 3790, AFTER TAKEOFF WITH BLEEDS OPEN CABIN FILLED WITH SMOKE. RAN BOTH ENGINES AT TAKEOFF POWER AND WITH APU ONLY. OPS CHECK GOOD.
AFT SMOKE DETECTOR GIVES ERRONEOUS SMOKE MESSAGE. REPLACED AFT CARGO SMOKE DETECTOR IAW MM 26-15-01. OPS CHECK GOOD.
FOUND AT C-CHECK, STA 280 AT LBL 9 UPPER FLOORBEAM IS CRACKED. COMPLIED WITH REPAIRS IAW CRJ200 REO 601R-53-11-138.
EMERGENCY LIGHT FLOOR TRACK IS INOP, FOUND AT C-CHECK. REPAIRED WIRING FOR EMERGENCY LIGHTS PER CRJ200 ECSPM 20-17-80 PG 2-5.
STA 280 AT RBL 9 LOWER FLOORBEAM IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH FLOORBEAM REPAIR PER 601R -53-11-1305/601R 53-11-171.
NUMBER 2 CARGO FIRE TEST IS INOP, FOUND AT C-CHECK. REPLACED NR 2 SMOKE DETECTOR PER CRJ200 AMM 26-15-00-440-801.
FLT 3981 - JUST AFTER LIFTOFF, SMOKE APPEARED IN THE COCKPIT. INSPECTED CENTER PEDESTAL WITH NO EVIDENCE OF DAMAGED WIRES. INSPECTED ALL ELECTRICAL COMPONENTS AND RELAY CONTACTORS IN AVIONICS BAY WITH NO DISCREPANCIES NOTED. REPLACED NR 2 RTU FOR PRECAUTIONS. OPS CHECK GOOD.
FLT 3845 - RIGHT COWL ANTI-ICE CAUTION MESSAGE CAME ON DURING CLIMB-OUT. RETURNED TO FIELD. FOUND BLEED SOURCE LINE ON THRUST REVERSER PDU DISCONNECTED. RECONNECTED LINE IAW MM 78-32-03. REPLACED RIGHT LOWER COWLING, COWL ANTI-ICE PRESSURE SWITCH, AND COWL ANTI-ICE VALVE IAW MM 30-22-01. OPS CHECK GOOD.
PASSENGERS AND FLIGHT ATTENDANT REPORTED SMOKE IN ROW 12, RETURNED TO TULSA. FOUND TO BE CONDENSATION FROM RIGHT PACK SYSTEM DUE TO HIGH HUMIDITY.
NOSE WHEEL WOULD NOT RETRACT, NOSE DOOR OPEN WARNING. RETURNED TO FIELD. REPLACED O-RINGS AND PACKINGS ON NLG FLOATING STRUT PISTON IAW CMM 32-20-04 AND IAW CRJ 200 MM 32-21-25 AND C/W ST12-710-1002. OPERATIONAL CHECKS GOOD.
"CARGO SMOKE" WARNING ON APPROACH INTO PHX, DISCHARGED BOTH BOTTLES. NO EVIDENCE OF ANY FIRE PRESENT. REPLACED BOTH CARGO DETECTOR IAW 26-15-00. SYSTEM OPERATIONALLY CHECKS GOOD IAW 26-25-00, P/N - 473597-19.
AFT STRIP OF FLOOR LEVEL EMERGENCY LIGHTING NOT ILLUMINATED. RECONNECTED PINS FOR THE AFT SECTIONS OF FLOOR LIGHT STRIP. OPERATIONAL CHECKS GOOD.
SHUTDOWN NR 2 ENG IN FLIGHT DUE TO LOW OIL PRESSURE. REMOVED AND REPLACED IDG SPLINE SHAFT O-RING IAW AMM 24-11-01. OPERATIONAL CHECKS GOOD.
AFT FLOOR EMERGENCY LIGHTING IS NOT ILLUMINATING APPROXIMATELY 8 FEET OF AFT SECTION. OPERATIONAL CHECKS GOOD. ALL SEGMENTS ILLUMINATED.
MAIN DOOR CRACKED ON TOP RIGHT SIDE 4' FROM DOOR HINGE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED 601R 52-11-279-1 REPAIR ANGLE PER CRJ200 REO 601R 52-11-279. RII 52-401 COMPLETE.
ENGINE BEAM CRACKED RIGHT SIDE ACCESS CUTOUT (INBOARD FORWARD RADIUS), DISCOVERED DURING C-CHECK INSPECTION. INSTALLED PN 601R 53-61-358-3;601R 53-61-358-6; PER REO 601R 53-61-358.
CRACK ON RT FS 640.00 SUPPORT ANGLE BETWEEN STR 9-12, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED RT ENGINE BEAM REINFORCEMENT ANGLE PER 51-42-06 AND SKYWEST RII 53-401 PN 601R 36002-4/SB.
CRACK ON LEFT FS 640.00 SUPPORT ANGLES; BETWEEN STR 9 TO 12, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW SUPPORT ANGLE AT FS 640 LT SIDE PN 601R 36002-3/SB PER CRJ200 SRM 51-42-06 PG 11 PARA 9 AND SRM 51-42-21 PG 7 PARA 9.
CRACKED SUPPORT FOR RIGHT ACM SUPPORT STRUCTURE, DISCOVERED DURING C-CHECK INSPECTION. REPLACED WITH NEW SUPPORT PART NR 601R-95159-35; PER SRM 51-42-06 PG NR 4 ITEM B.
MAIN DOOR HAS CRACK IN ANGLE ON AFT SIDE 1' FROM DOOR MOTOR PULLEY, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED 601R 52-11-513-1 ANGLE SECTION AND 601R 52-11-513-2 AND -3 SPLICE ANGLE ON PAX DOOR.
CRACKED CLIP AT FS 625 RBL 40 WL 79, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW INTERCOSTAL RT SIDE STA 625 RBL 40 WL79 P/N 601-35012-52 PER SRM 51-42-21 PAGE 1-7.
LEFT STA 621 FLOOR ANGLE CRACKED AT CORNER, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED LT STA 621 FLOOR ANGLE REPAIR IAW CRJ200 REO 601R-53-61-117 REV B; SRM 51-42-06 FIG 8 PG 15.
MAIN DOOR CRACK ON TOP LEFT SIDE C 4' FROM DOOR HINGE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED 601R 52-11-279-1 REPAIR ANGLE PER CRJ200 REO 601R 52-11-279. RII 52-101 COMPLETE.
ARRIVAL INTO SLC FLIGHT SYSTEM AND GROUND SPOILER FAULT STATUS MESSAGE. REPLACED NR 1 SECU PER CRJ MM 27-61-05, OPERATIONAL CHECK GOOD.
FLAPS FAIL MESSAGE DURING TAXI-OUT. REPLACED RIGHT BPSU IAW 27-50-10. RIGGED FLAPS AND ACTUATORS IAW AMM 27-54-00. OPERATIONAL CHECK GOOD.
FLAPS FAIL CAUTION MESSAGE WITH FLAPS AT ZERO. RIGGED FLAPS AND ACTUATORS IAW AMM 27-54-00, OPERATIONAL CHECK GOOD.
AFTER LANDING WHILE RETRACTING FLAPS, RECEIVED AND FLAPS FAIL CAUTION MSG. REPLACED RT BPSU. OPERATIONAL CHECK GOOD IAW 27-51-10.
FLAPS FAIL CAUTION AT 30 DEG AFTER LANDING. REPLACED THE FLAP SELECTOR LEVER AND FECU IAW CRJ AMM 27-51-01AND MM 27-51-05. OPERATIONAL CHECK GOOD. PN 1 OFF 7-45500-1 SN 1 OFF 0560 PN 2 OFF 860D100-18ABCD SN 2 OFF 1217
STAB TRIM CH 1 INOP STATUS MSG CAME ON IN FLIGHT. REPLACED BOTH HSTCU AND MCU IAW MM 27-42-01 AND 27-42-05. OPERATIONAL CHECK GOOD. P/N: 7062-3 S/N OFF: 1043
MAIN CABIN DOOR WON'T OPEN FROM OUTSIDE. LUBED INNER DOOR ASSY AND OUTER DOOR HANDLE ASSY. OPERATIONAL CHECK GOOD.
AFT EMERGENCY LIGHT DAMAGED. INSTALLED NEW EMERGENCY LIGHT SOCKET IAW CRJ MM 20-00-00. OPERATIONAL CHECK GOOD.
AT 280 BULKHEAD, BL 9.00 & BR 9.00 2 ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED THE NEW ANGLES AT FS 280 L & R BL 9 UNDER FLOORBEAMS IAW EO 601R-53-11-136.
ON 625 BULKHEAD STRINGER 13L AND 13R CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED 2 REPLACEMENT BRACKETS PER RJ200 SRM 51-42-21 PG 13.
CORROSION FOUND ON LONGITUDINAL FLOOR SUPPORT AT RBL 27 APPROX FS 559 + 110 IN AFT BAGGAGE COMPARTMENT AT FLOORBOARD LOCATIONS 282 FRF AND 282 HRF. ITEM FOUND AT C-CHECK INSPECTION. REMOVED CORROSION IAW SRM 51-21-06 PG 1 & PG 2. CORROSION DID NOT PENETRATE PROTECTIVE LAYER.
FLAPS FAIL MESSAGE APPEARED AFTER SELECTING FLAPS 30 DEGREES. REMOVED AND REPLACED R3 AND R4 FLAP ACTUATOR IAW 27-53-05. OPS CHECK GOOD. REF RII 27-412. P/N: 854D100-20, S/N 2274.
FLAPS FAIL MESSAGE APPEARED AFTER SELECTING FLAPS 30 DEGREES. REMOVED AND REPLACED R3 AND R4 FLAP ACTUATOR IAW 27-53-05. OPS CHECK GOOD. REF RII 27-412. P/N: 854D100-20, S/N 2274.
FLIGHT SPOILER AND INBOARD GROUND SPOILER FAULT STATUS MESSAGE CAME UP ON SHORT FINAL. REMOVED AND REPLACED NR 2 SECU PER MM 27-61-05. OPS CHECK GOOD.
ON CLIMBOUT, FLAPS FAIL AT 8 DEGREES. RETURN TO SLC. RE-RIGGED FLAPS IAW 27-54-00. OPS CHECK GOOD.
FLAP HALFSPEED MESSAGE DURING FLAP EXTENSION. REMOVED AND REPLACED FLAP PDU IAW 27-52-01. OPS CHECK GOOD.
CAPTAIN'S STICK SHAKER NOT WORKING, BOTH WIRES ARE PULLED FROM UNIT ON CAPTAIN'S COLUMN. REINSTALLED PINS ONTO CAPT'S STICK SHAKER PER MM 20-00-00. OPS CHECK GOOD PER MM 27-00-00.
FLAPS FAIL CAUTION MESSAGE AFTER TAKEOFF WHILE RETRACTING FLAPS FROM 20 DEGREES TO 8 DEGREES. PERFORMED QRH AND RETURNED TO MEM FOR 8 DEGREE LANDING. REMOVED AND REPLACED RIGHT FLAP BPSU IAW MM 27-51-10. OPS CHECK GOOD.