N936EV
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.
162 reports on file, 2006-11-07 – 2021-11-02.
Part: NONE — DAMAGED · airframe 30,234 hrs · 30,697 cycles
LH & RH TRUNNION REPLACEMENT REQUIRES INCORPORATION OF SB 601R-57-048, REV C. (COLD WORK HOLES ON WEB MLG TRUNNION) (C-CHECK RO 12-4-2021) COLD WORKED HOLES IN MLG TRUNNION WEB LHS AND RHS PER REO 601R-57-21-3542 REV -A DATE 2021-12-01 ALL STEPS C/W AND REO 601R-57-21-3541 REV -- DATE 2021-11-15 ALL STEPS C/W. / COMPLIED WITH 51-900-1003 SKY
Part: NONE — CRACKED · airframe 30,234 hrs · 30,697 cycles
BAT ANGLE AT WS:48.3 RH SIDE IS CRACKED (C-CHECK RO 12-4-2021) REMOVED R/H BATT ANGLE AT WS 48.3 AND INSTALLED NEW R/H BATT RIB ANGLE P/N 600-10204 AT WS 48.3, REF: DWG 600-10204, REV: M, CRJ200 SRM 51-42-06. COMPLIED WITH 51-900-1003-SKY
Part: NONE — CHAFED · airframe 30,234 hrs · 30,697 cycles
APRON SKIN ON RH SIDE IS CHAFED (C-CHECK RO 12-4-2021) REPAIRED APRON SKIN ON RH SIDE REF REO 601R-53-41-115 REV -A DATE 2005-07-20. COMPLIED WITH ALL STEPS OF REO 601R-53-41-115 REV -A DATE 2005-07-20 COMPLIED WITH 51-900-1003-SKY
Part: NONE — CHAFED · airframe 30,234 hrs · 30,697 cycles
APRON SKIN ON LH SIDE IS CHAFED (C-CHECK RO 12-4-2021) REPAIRED APRON SKIN ON LH SIDE REF REO 601R-53-41-115 REV -A DATE 2005-07-20. COMPLIED WITH ALL STEPS OF REO 601R-53-41-115 REV -A DATE 2005-07-20 COMPLIED WITH 51-900-1003-SKY
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
FS333 FRAME CORRODED ON AFT FACE AT STGR27. (C-CHECK RO 12-4-2021) REPLACED FS333.0 LWR FRAME SECTOR BETWEEN STR 23L AND 23R. REF BOMBARDIER DWG 601R31022 REV B, CRJ200 SRM 51-42-06 & CRJ200 SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD.]
Part: NONE — CRACKED · airframe 30,234 hrs · 30,697 cycles
L/H CNTR FUEL TANK BL0 WATER DRAIN VALVE (COLLECTOR TANK) HOUSING FWD MOUNT HOLE IS CRACKED (MARKED). SEE CAMP# 23458922 JOB# 2803885 OP# 5122 FOR NDT REPORT. (C-CHECK RO 12-4-2021) COMPLIED WITH REO 601R-57-21-3537 REV-- DATED 2021-11-03. LEAK CHECK GOOD. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH 51-900-1003-SKY.
Part: NONE — CHAFED · airframe 30,234 hrs · 30,697 cycles
* PAX DOOR SURROUND - AFT PULL IN LEVER CAM WORN/CHAFED (C-CHECK RO 12-4-2021) REMOVED PAX DOOR SURROUND UPPER AFT CAM FITTING AND INSTALLED A NEW FITTING 600-31688-18 REF CRJ 200 SRM 51-42-21 AND DRAWING 600-31687 REV C.
Part: NONE — CRACKED · airframe 30,234 hrs · 30,697 cycles
WHILE COMPLYING WITH SB 601R-57-046 REV C PART F (RHS) !EA 2ND O/S FASTENER (HST411-10) WAS FOUND IN HOLE #14, HOLE DIA. IS .3400 WITH NO DEFECTS, HOLE #16, HOLE #19 AND HOLE #21 SHOWS CRACK INDICATIONS. (C-CHECK RO 12-4-2021) / COMPLIED WITH REPAIR TO WING ASSY AT WS 65.75 BETWEEN R/S & AUX SPAR, RHS, REF MHIRJ REO 601R-57-21-3534 REV -- DATED 2021-11-15 AND RIL 3690 REV NC. / COMPLIED WITH TASK CARD 51-900-1003-SKY / LEAK CHECK GOOD
Part: NONE — CRACKED · airframe 30,234 hrs · 30,697 cycles
* STGR3L ANGLE CRACKED AT APPROXIMATELY FS282 (C-CHECK RO 12-4-2021) REMOVED AND INSTALLED NEW ANGLE AT STGR3L APPROXIMATELY FS282.00. REF CRJ 200 SRM 51-42-06 AND DWG 600-31057 REV P / PERFORMED PRESSURIZATION LEAK CHECK REF CRJ200 AMM 21-32-00-863-801. NO LEAKS DETECTED / COMPLIED WITH TASK CARD 51-900-1003-SKY
Part: NONE — CRACKED · airframe 30,234 hrs · 30,697 cycles
WHILE COMPLYING WITH SB 601R-57-046 REV C PART E (LHS) !EA 2ND O/S FASTENER (HST411-10) WAS FOUND IN HOLE #14, HOLE DIA. IS .3400 WITH NO DEFECTS NOTED, HOLE #16 AND HOLE #18 SHOWS CRACK INDICATIONS. (C-CHECK RO 12-4-2021) COMPLIED WITH MHIRJ REO 601R-57-21-3533 REV -- DATED 2021-11-15 AND RIL 3690 REV NC. / COMPLIED WITH TASK CARD 51-900-1003-SKY / LEAK CHECK GOOD
Part: NONE — CRACKED · airframe 30,234 hrs · 30,697 cycles
*CLIP ATTACHING INTERCOSTAL TO FRAME AT FS 625 ON THE R/H SIDE IN THE AFT EQUIPMENT COMP IS CRACKED. CLIP IS FLAGED. (C-CHECK RO 12-4-2021) REMOVED AND INSTALLED NEW CLIP PART # 601R350126-2 ATTACHING INTERCOSTAL TO FRAME AT FS625.00 ON THE R/H SIDE IN THE AFT EQUIPMENT REF. CRJ200 SRM 51-42-06, CRJ200 SRM 51-21-11, REF. CRJ200 SRM 51-25-06, AND CRJ200 SRM 51-25-16 AND CANADAIR DWG 601-35012 REV. B COMPLIED WITH 51-900-1003-SKY
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
*EVIDENCE OF CORROSION EXIST ON FLOOR SILL @STRG 17R BTW FS 559.00 +64 AND FS 559.00 +112. (C-CHECK RO 12-4-2021) BLENDED OUT CORROSION ON R/H FLOOR SILL BETWEEN FS559.00+64 AND FS559.00+112. REF. REO 601R-53-00-526 REV.-- DATED 05/22/2013. FOUND TO BE OUT OF LIMITS REF REO 601R-53-00-526 REV.-- DATED 05/22/2013. REMOVED AND REPLACED NEW FLOOR SILL AT FS559+64 AND FS559+112 REF. CRJ200 SRM 51-42-06 AND SRM 51-42-21 AND DWG 601R31133 REV-J. COMPLIED WITH 51-900-1003-SKY
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
*EVIDENCE OF CORROSION EXIST IN MULTIPLE AREA @FS574.00 BTW STRG 24R AND 24L. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED FS574 FRAME SECTION BETWEEN STR 25R TO STR 20L WITH A SPLICE REPAIR. REF REO 601R-53-61-7733 REV -- DATED 2021-10-28 & CRJ200 SRM 51-42-06. COMPLIEDE WITH TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD.
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
*EVIDENCE OF CORROSION EXIST ON FLOOR SILL @STRG 17R BTW FS 589.00 AND FS 605.00. (C-CHECK RO 12-4-2021) BLENDED OUT CORROSION ON R/H FLOOR SILL BETWEEN FS589.00 AND FS605.00. REF. REO 601R-53-00-526 REV.-- DATED 05/22/2013 .FOUND TO BE IN LIMITS REF REO 601R-53-00-526 REV.-- DATED 05/22/2013. COMPLIED WITH ALL STEPS OF REO 601R-53-00-526 REV.-- DATED 05/22/2013
Part: NONE — DAMAGED · airframe 30,234 hrs · 30,697 cycles
FABRICATE SEAT RAIL P/N 601R38312-115 FOR INSTALLATION ON JOB 2803881 OP. 249 CAMP #23640844. (C-CHECK RO 12-4-2021) FABRICATED AND INSTALLED SIDE SEAT RAIL P/N 601R38312-115 FROM EXTRUSION P/N 20276-288-0-0A, PO# T-59810. REF. REPAIR B OF REO 601R-53-00-055 REV -C, DATED 2017-03-21. COMPLIED WITH ALL STEPS OF REO 601R-53-00-055 REV -C, DATED 2017-03-21.
Part: NONE — DAMAGED · airframe 30,234 hrs · 30,697 cycles
FABRICATE SEAT RAIL P/N 601R38312-25 TO BE INSTALLED ON JOB 2803881 OP.251 CAMP # 23640869 (C-CHECK RO 12-4-2021) FABRICATED AND INSTALLED SIDE SEAT RAIL P/N 601R38312-25 FROM EXTRUSION P/N 20276-288-0-0A, PO# T-59810. REF. REPAIR B OF REO 601R-53-00-055 REV -C, DATED 2017-03-21.SEE CONTINUATION CARD FOR DETAILS.
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
INTERCOSTAL CORRODED BTWN FS'S 349/364 AND STGRS 27/26R (C-CHECK RO 12-4-2021) REMOVED AND REPLACED INTERCOSTAL WITH NEW SERVICABLE P/N 601R31049-10 REF CRJ-200 SRM 51-42-21, SRM 51-42-06 AND DWG. 601R31049 REV NC / COMPLIED WITH TASK CARD 51-900-1003-SKY / LEAK CHECK GOOD
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
* R/H SIDE SEAT RAIL SECTION AT APPROX. FS 449.85 TO FS 499.00 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) REMOVED CORROSION FOR RH SIDE SEAT RAIL PER REFENCE CRJ 200 SRM 51-21-06. FOUND SEAT RAIL TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW RH SIDE SEAT RAILL FROM FS 449.85 TO FS 499 PER REFERENCE CRJ 200 AMM 53-01-11-400-802 AND CRJ 200 AMM 53-01-11-000-802
Part: NONE — CRACKED · airframe 30,234 hrs · 30,697 cycles
* CLIP CRACKED ON INTERCOSTAL AT FS 484.00 LBL 36. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED LBL36 INTERCOSTAL CLIP @ FS484. REF REO 601R-53-41-059 REV -C DATED 2020-03-11. COMPLIED WITH TASK CARD 51-900-1003-SKY.
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
* R/H SIDE SEAT RAIL MOUNTING CHANNEL SECTION AT APPROX. FS 364.00 TO FS 409.00 + 16 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) BLENDED OUT CORROSION ON RH SIDE SEAT RAIL RETAINER FROM FS 364 TO 409+16 AS MARKED REF CRJ 200 SRM 51-21-06 AND FOUND IN LIMITS REF CRJ 200 SRM 53-00-00.
Part: NONE — DAMAGED · airframe 30,234 hrs · 30,697 cycles
* R/H SIDE SEAT RAIL MOUNTING CHANNEL SECTION AT APPROX. FS 443.00 TO FS 495.00 HAS CLIP-NUT HOLE BROKEN OUT AT LOWER EDGE OF CHANNEL. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED RH SIDE SEAT RAIL MOUNTING CHANNEL SECTION FROM APPROX FS 443 TO FS 495 PER REFERENCE CRJ 200 AMM 53-01-11-000-802 AND CRJ 200 AMM 53-01-11-400-802
Part: NONE — CRACKED · airframe 30,234 hrs · 30,697 cycles
* CLIP CRACKED ON INTERCOSTAL AT FS 484.00 LBL 27. (C-CHECK RO 12-4-2021) RE MOVED AND REPLACED CLIP ON INTERCOSTAL AT FS 484.00 LBL 27 PART NUMBER .601R31171-17 REF. PREVIOUSLY INCORPERATED REO 601R-53-41-059 REV-C DATE 2020-03-11. COMPLIED WITH 51-900-1003-SKY
Part: NONE — CRACKED · airframe 30,234 hrs · 30,697 cycles
* CARGO NET SUPPORT BEAM AFT LOWER ATTACHMENT BRACKET AT FS 621.00 BULKHEAD CRACKED. (C-CHECK RO 12-4-2021) INSTALLED NEW BRACKET AT FS 621.00 BULKHEAD CARGO NET SUPPORT BEAM AFT LOWER ATTACHMENT. REF CRJ-200 SRM 51-42-21 AND DWG 601R35050 REV Y. COMPLIED WITH TASK CARD 51-900-1003. LEAK CHECK SATISFACTORY.
Part: NONE — WORN · airframe 30,234 hrs · 30,697 cycles
R/H INBD FLAP #1 (INBD) FLAP VANE ACTUATOR HAS ABRASION DAMAGE ON THE BOTH GUIDE TRACKS, TWO WORN CARRIAGE BEAM BUSHINGS, AS WELL AS A CORRODED INBD SPRING AND HARDWARE. (C-CHECK RO 12-4-2021) BLENDED R/H INBD FLAP #1 (INBD) FLAP VANE ACTUATOR HAS ABRASION DAMAGE ON THE BOTH GUIDE TRACKS AND TWO WORN CARRIAGE BEAM BUSHINGS REF. REO . FOUND TO BE IN LIMITS. COMPIED WITH ALL STEPS OF REO 601R-57-52-1989 REV -- DATED 22-NOV-2012. SEE CONTINUATION CARD FOR DETAILS OPS CHECKS GOOD
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
* L/H SIDE SEAT RAIL MOUNTING CHANNEL SECTION AT APPROX. FS 443.00 TO FS 495.00 HAS CLIP-NUT HOLE BROKEN OUT AT LOWER EDGE OF CHANNEL. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED DAMAGED SIDE SEAT RAIL MOUNTING CHANNEL AND INSTALLED NEW LH SIDE SEAT RAIL MOUNTING RETAINER CHANNEL FROM APPROX. FS 449.95 TO FS 499.00 REF. CRJ200 AMM 53-01-11-400-802 STEP 3 SEE CONTINUATION CARD FOR DETAILS.
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
* R/H SIDE SEAT RAIL SECTION AT APPROX. FS 409.00 + 16 TO FS 409.00 + 112 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) BLENDED OUT CORROSION ON R/H SIDE SEAT RAIL SECTION AT APPROX. FS 409.00 + 16 TO FS 409.00 + 112 IAW CRJ-200 SRM 51-21-06. / ORIGINAL THICKNESS AT BLENDED LOCATION "U" IS 0.370" WITH REMAINING THICKNESS 0.345" AND MATERIAL LOSS 0.025", MAX. PERMISSIBLE IS 0.020", THEREFORE FOUND TO BE OUT OF LIMITS. REF: CRJ-200 SRM 53-21-49 AND MHIRJ STANDAR CM0560002 REV -A / REMOVED AND REPLACED RH SIDE SEAT RAIL FROM FS.409.00+16 TO FS.409.00+112 REF CRJ200 AMM 53-01-11-400-802.
Part: NONE — DAMAGED · airframe 30,234 hrs · 30,697 cycles
* R/H SIDE SEAT RAIL MOUNTING CHANNEL SECTION AT APPROX FS 495.00 TO FS 535.00 HAS CLIP-NUT HOLE BROKEN OUT AT LOWER EDGE OF CHANNEL. (C-CHECK RO 12-4-2021) ORDERED AND RECEIVED 1EA NEW RETAINER P/N: 601R38828-2 / REMOVED DAMAGED R/H SIDE SEAT RAIL RETAINER P/N: 601R38828-2 REF CRJ-200 AMM 53-01-11-000-802 / INSTALLED NEW R/H SIDE SEAT RAIL RETAINER P/N: 601R38828-2 REF CRJ-200 AMM 53-01-11-400-802 USED CALIBRATED TORQUE WRENCH TUC8607 CAL DUE DATE: 28-FEB-22 / DRILLED/ LOCATED WIRING STAND OFFS ON NEW RETAINER LOWER FLANGE REF CRJ-200 SRM51-40-11 AND INSTALLED STAND OFFS REF CRJ-200 SRM 51-42-13
Part: NONE — DAMAGED · airframe 30,234 hrs · 30,697 cycles
* R/H SIDE SEAT RAIL MOUNTING CHANNEL SECTION AT APPROX FS 559.00 + 28 TO FS 559.00 + 80 HAS CLIP-NUT HOLE BROKEN OUT AT LOWER EDGE OF CHANNEL. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED R/H SIDE SEAT RAIL MOUNTING CHANNEL SECTION AT APPROX FS 559.00 + 28 TO FS 559.00 + 80. REF: CRJ-200 SRM 51-41-00. SEE CONTINUATION CARD FOR DETAILS.
Part: NONE — CRACKED · airframe 30,234 hrs · 30,697 cycles
* L/H WHEEL WELL HAS WS48.30 CAP ANGLE ATTACHED TO LOWER SIDE OF UPPER WING SKIN CRACKED. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED WITH NEW CAP ANGLE AT LH SIDE WS48.30 PN:600-10389-1 REF CRJ200 SRM 51-42-21 AND DWG:600-10212, REV -D. COMPLIED WITH 51-900-1003-SKY
Part: NONE — WORN · airframe 30,234 hrs · 30,697 cycles
R/H INBD FLAP #2 (MID) FLAP VANE ACTUATOR HAS ABRASION DAMAGE ON THE BOTH GUIDE TRACKS AND TWO WORN CARRIAGE BEAM BUSHINGS. (C-CHECK RO 12-4-2021) / BLENDED R/H INBD FLAP #2 (MID) FLAP VANE ACTUATOR HAS ABRASION DAMAGE ON BOTH GUIDE TRACKS AND TWO WORN CARRIAGE BEAM BUSHINGS REF. REO 601R-57-52-1989 REV -- DATED 22-NOV-2012. FOUND TO BE IN LIMITS. COMPIED WITH ALL STEPS OF REO 601R-57-52-1989 REV -- DATED 22-NOV-2012. SEE CONTINUATION CARD FOR DETAILS
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
* L/H SIDE SEAT RAIL SECTION AT APPROX. FS 449.95 TO FS 499.00 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED LH SIDE SEAT RAIL FROM APPROX. FS 449.95 TO FS 499.00 REF: CRJ-200 AMM 53-01-11-400-802. SEE CONTINUATION CARD FOR DETAILS.
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
* L/H SIDE SEAT RAIL SECTION AT APPROX. FS 409.00 + 112 TO FS 449.95 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) BLENDED L/H SIDE SEAT RAIL SECTION AT APPROX. FS 409+112 TO FS 449.95 CRJ 200 SRM 51-21-06.FOUND TO BE OUT OF LIMITS REF CRJ-200 SRM 53-21-49. REMOVED AND REPLACED LH SIDE SEAT RAIL FROM APPROX. FS 409+112 TO FS 449.95 REF: CRJ-200 AMM 53-01-11-400-802. SEE CONTINUATION CARD FOR DETAILS
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
* R/H SIDE SEAT RAIL SECTION AT APPROX. FS 499.00 TO FS 548.00 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED R/H SIDE SEAT RAIL SECTION AT APPROX. FS 499.00 TO FS 548.00 REF: CRJ-200 AMM 53-01-11-000-802 & CRJ200 AMM 53-01-11-400-802. SEE CONTINUATION CARD FOR DETAILS
Part: NONE — WORN · airframe 30,234 hrs · 30,697 cycles
R/H INBD FLAP #3 (OTBD) FLAP VANE ACTUATOR HAS ABRASION DAMAGE ON THE BOTH GUIDE TRACKS AND TWO WORN CARRIAGE BEAM BUSHINGS. (C-CHECK RO 12-4-2021) BLENDED R/H INBD FLAP #3 (OTBD) FLAP VANE ACTUATOR HAS ABRASION DAMAGE ON THE BOTH GUIDE TRACKS AND TWO WORN CARRIAGE BEAM BUSHINGS REF. REO 601R-57-52-1989 REV -- DATED 22-NOV-2012. FOUND TO BE IN LIMITS. COMPIED WITH ALL STEPS OF REO 601R-57-52-1989 REV -- DATED 22-NOV-2012. SEE CONTINUATION CARD FOR DETAILS
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
* L/H SIDE SEAT RAIL SECTION AT APPROX. FS 499.00 TO FS 548.00 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) BLENDED OUT CORROSION ON LH SIDE SEAT RAIL AS MARKED FS499.00 TO FS 548.00 REF CRJ 200 SRM 51-21-06.NO ALLOWABLE LIMITS GIVEN FOR SIDE SEAT RAIL REF CRJ 200 SRM 53-21-49, REPLACE SIDE SEAT RAIL.REMOVED AND REPLACED LH SIDE SEAT RAIL FS 499.00 TO FS 548.00 REF CRJ 200 AMM 53-01-11-400-802.
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
* L/H SIDE SEAT RAIL SECTION AT APPROX. FS 364.00 TO FS 409.00 + 16 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) BLENDED OUT CORROSION ON LH SIDE SEAT RAIL AS MARKED FS 364 TO 409+16 REF CRJ 200 SRM 51-21-06.NO ALLOWABLE LIMITS GIVEN FOR SIDE SEAT RAIL REF CRJ 200 SRM 53-21-49, REPLACE SIDE SEAT RAIL.REMOVED AND REPLACED LH SIDE SEAT RAIL FS 364 TO 409+16 REF CRJ 200 AMM 53-01-11-400-802.
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
* L/H SIDE SEAT RAIL SECTION AT APPROX. FS 409.00 + 16 TO FS 409.00 + 112 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) BLENDED OUT CORROSION ON LH SIDE SEAT RAIL AS MARKED FS 409+16 TO FS 409+112 REF CRJ 200 SRM 51-21-06.NO ALLOWABLE LIMITS GIVEN FOR SIDE SEAT RAIL REF CRJ 200 SRM 53-21-49, REPLACE SIDE SEAT RAIL.REMOVED AND REPLACED LH SIDE SEAT RAIL FS 409+16 TO 409+112 REF CRJ 200 AMM 53-01-11-400-802.
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
* R/H SIDE SEAT RAIL SECTION AT APPROX. FS 409.00 + 112 TO FS 449.95 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED R/H SIDE SEAT RAIL SECTION AT APPROX. FS 409.00+112 TO FS 449.95 REF: CRJ-200 AMM 53-01-11-000-802 & CRJ200 AMM 53-01-11-400-80. SEE CONTINUATION CARD FOR DETAILS
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
* L/H SIDE SEAT RAIL SECTION AT APPROX. FS 548.00 TO FS 559.00 + 80 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) REMOVED LH SIDE SEAT RAIL FROM APPROX. FS 548.00 TO FS 559.00+80. REF: CRJ-200 AMM 53-01-11-000-802 AND INSTALLED NEW L/H SIDE SEAT RAIL FORM APPROX. FS548-FS559+80 REF. CRJ200 AMM 53-01-11-400-802,
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
#1 RH OUTB FLAP HINGE BOX SPRING HAS EVIDENCE OF CORROSION. (C-CHECK RO 12-4-2021) REMOVED BUTE DOOR ACTUATOR ON HINGE BOX AT WS178.00 TO FOM. REF. CRJ200 AMM 27-54-25-000-801 AND REINSTALLED BUTE DOOR ACTUATOR ON HINGE BOX AT WS178.00. REF. CRJ200 AMM 27-54-25-400-801. OPS CHECKS GOOD
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
#1 RH OUTB FLAP HINGE BOX 3 EA ATTACHING HARDWARE TO AIRFRAME HAS EVIDENCE OF CORROSION. (FLAGGED) (C-CHECK RO 12-4-2021) REMOVED 3 EA. CORRODED NUTS AND WASHERS AT MOUNT BOLTS ON OUTBOARD FLAP HINGE BOX ASSEMBLY AT WS178.00 AND REPLACED WITH NEW HARDWARE (3 EA. NUTS AND WASHERS). REF. CRJ200 SRM 51-41-02. USED TORQUE WRENCH TUC1260, CAL DUE 31 AUG 21
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
RH OUTB FLAP, OUTB HINGE ARM ASSY HAS EVIDENCE OF CORRODED HARDWARE AT FWD ATTACH BOLT STOP PLATES, LEFT AND RIGHT SIDES. (FLAGGED) (C-CHECK RO 12-4-2021) REMOVED 4 EA. CORRODED BOLTS ON OUTBOARD FLAP HINGE ARM ATTACH POINT LH & RH STOP PLATES AND REPLACED WITH NEW BOLTS. REF. CRJ200 SRM 51-41-02.
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
#2 LEFT INB FLAP HINGE, FWD LUG CASTLE NUT SHOWING SIGNS OF CORROSION. (FLAGGED) (C-CHECK RO 12-4-2021) REMOVED AND REPLACED LH INBOARD #2 FLAP HINGE FWD HARDWARE (NUT AND COTTER PIN) REF: CRJ200 SRM 51-41-02. TUC1260 DUE: 31-AUG-22
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
#1 LEFT INB FLAP HINGE, FWD LUG CASTLE NUT SHOWING SIGNS OF CORROSION. (FLAGGED) (C-CHECK RO 12-4-2021) REMOVED AND REPLACED LH INBOARD #1 FLAP HINGE FWD HARDWARE (NUT AND COTTER PIN) REF: CRJ200 SRM 51-41-02. TUC1260 DUE: 31-AUG-22
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
#2 RH INB FLAP HINGE ARM HAS ALL 4 EA CASTLE NUTS SHOWING EVIDENCE OF CORROSION. (FLAGGED) (C-CHECK RO 12-4-2021) REMOVED CORRODED CASTLE NUTS AND INSTALLED NEW CASTLE NUTS RIGHT INBOARD FLAP HINGE ARM WS127.25 REF CRJ 200 AMM 57-52-08-400-802. TORQUE WRENCH TUC4200 CAL DUE 30 SEPT 2022.
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
#2 LEFT OUTBOARD FLAP HINGE BOX AFT, OUTBOARD, ATTACHED CASTLE NUT HARDWARE SHOWING EVIDENCE OF CORROSION. (FLAGGED) (C-CHECK RO 12-4-2021) REMOVED CORRODED AFT OUTBOARD CASTLE NUT LEFT FLAP HINGE BOX WS220.00 AND INSTALLED NEW CASTLE NUT REF CRJ 200 AMM57-21-35-400-802 STEPS 3. A. (4) THRU (6) TORQUE WRENCH TUC1260 CAL DUE 31 AUG 2022
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
#1 LH OUTBOARD FLAP HINGE BOX, AFT MOUNT CASTLE NUTS SHOWING EVIDENCE OF CORROSIN. (FLAGGED) (C-CHECK RO 12-4-2021) REMOVED 2 EA. CORRODED NUTS AT AFT MOUNT BOLTS ON LH OUTBOARD FLAP HINGE BOX ASSEMBLY AT WS178.00 AND REPLACED WITH NEW HARDWARE (2 EA. NUTS AND COTTER PINS). REF. CRJ200 SRM 51-41-02. USED TORQUE WRENCH TUC1260, CAL DUE 31 AUG 21.
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
#1 LEFT OUTBOARD FLAP HINGE BOX SPRING, FORWARD ATTACH HARDWARE HAS CASTLE NUT SHOWING EVIDENCE OF CORROSION. (C-CHECK RO 12-4-2021) REMOVED CORRODED CASTLE NUT AND INSTALLED NEW CASTLE NUT LEFT OUTBOARD FLAP HINGE BOX SPRING/ACTUATOR ASSEMBLY WS178.00 REF CRJ 200 AMM 27-54-25-400-801 STEPS 3. A. (5) THRU (6)
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
* L/H AND R/H, INB AND OBD ELEVATOR FLUTTER DAMPERS HAVE CORRODED ATTACHMENT HARDWARE NUTS AT ROD END. (C-CHECK RO 12-4-2021) REPLACED CORRODED NUTS (4 EA.) AT LH AND RH INBD AND OTBD ELEVATOR FLUTTER DAMPER RODENDS WITH NEW NUTS. (4 EA.). REF. CRJ200 AMM 27-34-05-400-801. OP TEST GOOD. SEE CONTINUE CARD FOR DETAILS.
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
#1 LEFT OUTBOARD FLAP HINGE BOX SPRING SHOWING EVIDENCE OF CORROSION. (C-CHECK RO 12-4-2021) REMOVED L/H BUTE DOOR ACTUATOR ON HINGE BOX ASSEMBLY AT WS178.00 TO FOM. REF. CRJ 200 AMM 27-54-25-000-801.AND REINSTALLED L/H BUTE DOOR ACTUATOR ON HINGE BOX ASSEMBLY AT WS178.00. REF. CRJ 200 AMM 27-54-25-400-801. OPS CHECKS GOOD
Part: NONE — DENTED · airframe 30,234 hrs · 30,697 cycles
L/H INBD FLAP (P/N: 601R14002-1 S/N: SBRJ1075) LWR SKIN IS DENTED IN 5 LOCATIONS IN ADDITION TO A PREVIOUS REPAIR. REPAIR L/H INBD FLAP LWR SKIN DAMAGE. (C-CHECK RO 12-4-2021) REMOVED & REPLACED LOWER I/B SKIN P/N 601R14008-45S & LOWER O/B SKIN P/N 601R14008-47SP ON L/H I/B FLAP, REF. CRJ200 SRM 51-42-10, CRJ200 SRM 51-42-22 & DWG. 601R14002, REV. K. / COMPLIED WITH 51-900-1003-SKY
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
LH INBOARD GROUND SPOILER PCU HAVE RUSTED HARDWARE FOR MOUNTING AND HINGE POINTS (C-CHECK RO 12-4-2021) REPLACED RUSTY HARDWARE WITH NEW HARDWARE LEFT INBOARD GROUND SPOILER PCU FORK END AND HINGE LINK REF CRJ 200 AMM 27-63-01-400-801 STEP 2. B. (3) THRU (4)
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
LH OUTBOARD GROUND SPOILER PCU HAVE RUSTED HARDWARE FOR MOUNTING AND HINGE POINTS (C-CHECK RO 12-4-2021) REPLACED RUSTED HARDWARE WITH NEW HARDWARE LEFT OUTBOARD GROUNG SPOILER PCU FORK END AND HINGE LINK REF CRJ 200 AMM 27-63-01-400-801 STEP 2. B. (3) THRU (4).
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
LH SPOILERON PCUS HAS RUSTED HARDWARE AT MOUNTING POINTS (C-CHECK RO 12-4-2021) REPLACED RUSTED HARDWARE WITH NEW HARDWARE LEFT SPOILERON PCU MOUNT POINTS REF CRJ 200 AMM 27-62-01-400-801 STEPS 2. B. (6) THRU (7) TORQUE WRENCH TUC5659 CAL DUE 28 FEB 2022
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
LH FLIGHT SPOILER PCUS HAS RUSTED HARDWARE AT MOUNTING POINTS (C-CHECK RO 12-4-2021) REPLACED RUSTY HARDWARE WITH NEW HARDWARE LEFT FLIGHT SPOILER PCU MOUNT POINTS REF CRJ 200 AMM 27-62-01-400-801 STEP 2. B. (6) THRU (7). TORQUE WRENCH TUC5689 CAL DUE 28 FEB 2022.
Part: NONE — CHAFED · airframe 30,234 hrs · 30,697 cycles
RH AILERON UPPER AND LOWER FIXED LEADING-EDGE SKIN IS CHAFED IN NUMEROUS LOCATIONS AS MARKED. (C-CHECK RO 12-4-2021) REMOVED AND INSTALLED NEW RH AILERON UPPER FIXED LEADING-EDGE SKIN. REF: CRJ200 SRM 51-42-22, CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DRWG. #CC670-13000 REV D. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
L/H AILERON INBD AND OTBD PCU ATTACH POINT HDWR HAS CORRODED COTTER PINS (C-CHECK RO 12-4-2021) REMOVED 2 EACH RUSTED COTTER PINS AND INSTALLED 2 EACH NEW COTTER PINS AT THE LH AILERON INBD/OTBD PCU ATTACH POINT HARDWARE. REF - CRJ 200 AMM 20-24-00-910-801. PERFORMED AN OPERATIONAL TEST OF THE AILERON CONTROL SYSTEM. REF - CRJ 200 AMM 27-11-00-710-801. OPERATIONAL TEST GOOD. NO DEFECTS NOTED.
Part: NONE — DAMAGED · airframe 30,234 hrs · 30,697 cycles
LEFT OVERWING EMER EXIT DOOR - FWD AND AFT HINGE FITTINGS AND ADJACENT LOWER DOOR SKIN EDGES DAMAGED (C-CHECK RO 12-4-2021) REPAIRED L/H OVERWING EMER EXIT DOOR - FWD AND AFT HINGE FITTINGS AND ADJACENT LOWER DOOR SKIN EDGES REF REO 601R-52-21-128 REV --, DATED 2021-10-18. COMPLIED WITH 51-900-1003-SKY. CHECKS GOOD.
Part: NONE — DENTED · airframe 30,234 hrs · 30,697 cycles
*RH INBD FLAP LOWER SKIN HAS 3EA DENTS (MARKED) (C-CHECK RO 12-4-2021) FOUND THE DENT ON RH INBD FLAP LOWER SKIN HAS 3EA DENTS OUT OF LIMITS REF CRJ 200 SRM57-52-00 . REPAIR RIGHT I/B FLAP REF: REO 601R-57-52-678 REV-C DATE 2012/10/19 . COMPLIED WITH ALL STEPS REO 601R-57-52-678 REV-C DATE 2012/10/19. COMPLIED WITH 51-900-1003-SKY.
Part: NONE — CRACKED · airframe 30,234 hrs · 30,697 cycles
* SUSPECTED CRACK IN FUSELAGE SKIN AT L/H FWD EQUIPMENT BAY DOOR AFT LATCH CUTOUT, LOWER AFT CORNER. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED CRACKED FUSELAGE SKIN WITH NEW P/N 600-33052-145. REF. CRJ200 SRM 51-42-06 AND SRM 51-42-13 AND DWG# 600-33052 REV. AB. COMPLIED WITH 51-900-1003-SKY
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
* GALLEY SERVICE DOOR LOWER FWD PAN CORRODED ON LOWER SIDE. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED THE GALLEY SERVICE DOOR LOWER FWD PAN REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21,CRJ 200 SRM 51-42-13, & DWG 601R38304 REV BM. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.CHECKS GOOD.
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
* GALLEY SERVICE DOOR LOWER AFT PAN CORRODED ON LOWER SIDE. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED THE GALLEY SERVICE DOOR LOWER AFT PAN REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21,CRJ 200 SRM 51-42-13, & DWG 601R38304 REV BM. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.CHECKS GOOD.
Part: NONE — DAMAGED · airframe 30,234 hrs · 30,697 cycles
D: R WINDOW HEAT CAUTION MESSAGE ENROUTE TO DESTINATION. PERFORMED QRH PROCEDURE AND CLEARED FOR 5 MINUTES THEN RETURNED. (RESET NO HELP) / C: 30-41-1B / CAT: C DUE 08OCT21 / R WINDOW HEAT CAUTION MESSAGE ENROUTE TO DESTINATION. PERFORMED QRH PROCEDURE AND CLEARED FOR 5 MINUTES THEN RETURNED. (C-CHECK RO 12-4-2021) REMOVED AND INSTALLED NEW WINDOW. SEE MXTRANS 23564863, JOB 2803885, OP 13 FOR MAINTENACE AND CORRECTIVE ACTION. / FOLLOWING C CHECK AND WINDOW REPLACEMENT PERFORMED OPERATIONAL TEST OF THE WINDSHIELD TEMPERATURE CONTROLLERS, REF CRJ-200 AMM 30-41-01-710-801, CHECKED GOOD
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
REMOVE AND REPLACE BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK RO 12-4-2021) REMOVED AND INSTALLED 8 EACH NEW SERVICEABLE BEARINGS ON THE RH AILERON WING AFT SPAR. REF - CRJ 200 AMM 20-26-00-910-802 AND CRJ 200 AMM 20-26-00-910-804.
Part: NONE — CORRODED · airframe 30,234 hrs · 30,697 cycles
REMOVE AND REPLACE BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK RO 12-4-2021) REMOVED AND INSTALLED 8 EACH NEW SERVICEABLE BEARINGS ON THE LH AILERON WING AFT SPAR. REF - CRJ 200 AMM 20-26-00-910-802 AND CRJ 200 AMM 20-26-00-910-804.
Part: NONE — DAMAGED · airframe 30,234 hrs · 30,697 cycles
ROUTE RH AILERON TO BACK SHOP TO REMOVE AND REPLACE SWEDGED BEARINGS AND BUSHINGS AT HINGE POINTS (INBD, MID, OUTBD) ON RH AILERON PER AMM (C-CHECK RO 12-4-2021) REMOVED AND REPLACED WORN BUSHINGS AND BEARINGS ON R/H AILERON REF. CRJ 200 AMM 20-26-00-910-804 FOR BUSHINGS AND CRJ 200 AMM 20-26-00-910-808 FOR BEARINGS
Part: NONE — DAMAGED · airframe 30,234 hrs · 30,697 cycles
ROUTE LH AILERON TO BACK SHOP TO REMOVE AND REPLACE SWEDGED BEARINGS AND BUSHINGS AT HINGE POINTS (INBD, MID, OUTBD) ON LH AILERON PER AMM (C-CHECK RO 12-4-2021) REMOVED AND REPLACED WORN BUSHINGS AND BEARINGS ON L/H AILERON REF. CRJ 200 AMM 20-26-00-910-804 FOR BUSHINGS AND CRJ 200 AMM 20-26-00-910-808 FOR BEARINGS
Earlier reports · 2006–2020 · 95 reports
2020
Part: LINER — CRACKED (CABIN) · airframe 28,834 hrs · 28,897 cycles
SERVICE DOOR SURROUND AFT LINER 232EZ, P/N 3864126N501 CRACKED MULTIPLE PLACES (48 MONTH) RO 5/28/2020. REMOVED AND REPLACED SERVICE DOOR SURROUND AFT LINER 232EZ REF AMM. SEE CONTINUE CARD FOR DETAILS.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,834 hrs · 28,897 cycles
SPOTS OF POSSIBLE CORROSION FOUND IN MULTIPLE LOCATIONS ALONG RBL 9 BETWEEN FS 409 - FS 409+128 (48 MONTH) RO 5/28/2020. REMOVED AND REPLACED FLOORBEAM CAP SECTION AT RBL 9 BETWEEN FS409.00-FS409+112. REF REO AND DWG. SEE CONTINUE CARD FOR DETAILS.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,834 hrs · 28,897 cycles
SPOTS OF POSSIBLE CORROSION FOUND IN MULTIPLE LOCATIONS ALONG LBL 9 BETWEEN FS 409 - FS 409+128 (48 MONTH) RO 5/28/2020. REMOVED AND REPLACED FLOORBEAM CAP BETWEEN LBL9 FS409 TO FS409+128 REF REO AND DWG.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,834 hrs · 28,897 cycles
RBL 9 FWD SEAT TRACK, SECTION EXTENDING JUST AFT OF FS 409 CORRODED (48 MONTH) RO 5/28/2020. REMOVED CORROSION ON RBL 9 SEAT TRACK, JUST FWD OF FS409, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK WITH NEW HARDWARE REF AMM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,834 hrs · 28,897 cycles
CORROSION FOUND IN MULTIPLE LOCATIONS ALONG RBL9, BETWEEN FS409+128 AND FS559.00 (48 MONTH) RO 5/28/2020. REPLACED PRESSURE FLOORBEAM CAP PER REO DWG SRM. COMPLETED TASK CARD.
Part: FITTING — CRACKED (FUSELAGE) · airframe 28,834 hrs · 28,897 cycles
LEFT OUTBD CLIP CRACKED AT FS280 AND LBL 9.0 (48 MONTH) RO 5/28/2020. REMOVED AND REPLACED LBL9 FLOORBEAM OTBD CLIP AT FS280 WITH NEW SERVICEABLE CLIP P/N 601R-53-11-171-2 AND FILLER P/N 601R-53-11-171-3 REF SRM, DWG AND PREVIOUSLY INCORPORATED REO.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,834 hrs · 28,897 cycles
LBL 9 SEAT TRACK JUST FWD OF FS 409 CORRODED (48 MONTH) RO 5/28/2020. REMOVED CORROSION ON LBL 9 SEAT TRACK JUST FWD OF FS409. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK WITH NEW HARDWARE. REF AMM TUC8416 CAL DUE 31-OCT-20.
Part: FITTING — CRACKED (FUSELAGE) · airframe 28,834 hrs · 28,897 cycles
LEFT INBD CLIP CRACKED AT FS280 AND LBL 9.0 (48 MONTH) RO 5/28/2020. REMOVED AND REPLACED LBL9 FLOORBEAM INBD CLIP AT FS280 WITH NEW SERVICEABLE CLIP P/N 601R-53-11-171-2 AND FILLER P/N 601R-53-11-171-3 REF SRM, DWG AND REO.
Part: WEB — CRACKED (FUSELAGE) · airframe 28,834 hrs · 28,897 cycles
FS 280 WEB MEMBER CRACKED JUST OTBD OF LBL 9 (48 MONTH) RO 5/28/2020. CUT OUT CRACKED AREA OF FS280 WEB MEMBER OTBD OF LBL9. COMPLIED WITH REO REPAIR BY CUTTING OUT DAMAGE, INSTALLING REPAIR DOUBLER/FILLER AND FAB/INSTALL 2 EA NEW FLOORBEAM SUPPORT CLIPS WITH FILLERS.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,834 hrs · 28,897 cycles
FS 349 LBL 27 CRACK IN VERTICAL BRACE ON OTBD AFT PORTION OF INTERSECTION (48 MONTH) RO 5/28/2020. REMOVED AND REPLACED THE INTERCOSTAL AT FS349 LBL27 WITH NEW FABRICATED PART REFERENCE REO.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,834 hrs · 28,897 cycles
CORROSION FOUND IN MULTIPLE LOCATIONS ALONG LBL9, BETWEEN FS409+128 AND FS559.00 (48 MONTH) RO 5/28/2020. REPLACED PRESSURE FLOORBEAM CAP PER REO. COMPLETED TASK CARD.
Part: NUT PLATE — CORRODED (FUSELAGE) · airframe 28,834 hrs · 28,897 cycles
NUTPLATE CORRODED RT FLOOR SILL JUST FWD OF FS 310. (48 MONTH) RO 5/28/2020. REMOVED AND REPLACED AND INSTALLED NEW NUTPLATE AT RT FLOOR SILL JUST FWD OF FS310.00 REF SRM.
Part: FITTING — CRACKED (FUSELAGE) · airframe 28,834 hrs · 28,897 cycles
RIGHT INBD CLIP CRACKED AT FS280 AND RBL 9.0 (48 MONTH) RO 5/28/2020. REMOVED AND REPLACED RBL9 FLOOR SUPPORT BEAM INBD CLIP AT FS280 WITH NEW SERVICEABLE P/N 601R31113-58 REF SRM AND DWG.
Part: FITTING — CRACKED (FUSELAGE) · airframe 28,834 hrs · 28,897 cycles
RIGHT OUTBD CLIP CRACKED AT FS280 AND RBL 9.0 (48 MONTH) RO 5/28/2020. REMOVED AND REPLACED RBL9 FLOOR SUPPORT OTBD CLIP AT FS280 WITH NEW SERVICEABLE P/N 601R-53-11-171-5 AND FILLER P/N 601R-53-11-171-6 REF SRM. DWG AND PREVIOUSLY INCORPORATED REO.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,834 hrs · 28,897 cycles
FLOOR SUPPORT BEAM FROM FS 559.0 TO FS 559+80 AT LBL 9 HAS SEVERAL AREAS OF CORROSION (MARKED) (48 MONTH) RO 5/28/2020. REPAIRED FLOOR SUPPORT BEAM FROM FS 559.0 TO FS 559+80 AT LBL 9, AREAS OF CORROSION (MARKED) REF REO AND REO. COMPLIED WITH 51-900-1003-SKY.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,834 hrs · 28,897 cycles
LEFT SIDE SEAT TRACK FROM FS 559.0 TO FS 559+80 AT LBL 9 HAS CORROSION (48 MONTH) RO 5/28/2020. SEAT TRACK BETWEEN FS559 AND FS559+80 LBL9, REMOVED AND REPLACED REF REO AND AMM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,834 hrs · 28,897 cycles
RIGHT SIDE SEAT TRACK FROM FS 559.0 TO FS 559+80 RBL 9 HAS CORROSION (48 MONTH) RO 5/28/2020. SEAT TRACK BETWEEN FS559 AND FS559+80 RBL9 REMOVED AND REPLACED REF REO AND AMM.
Part: SUPPORT CHANNEL — CRACKED (CARGO DOOR) · airframe 28,834 hrs · 28,897 cycles
FORWARD CARGO DOOR TRACK ATTACH SUPPORT U- CHANNEL IS CRACKED UNDER RIVET (AS MARKED) (48 MONTH) RO 5/28/2020. REMOVED AND REPLACED WITH NEW SUPPORT U- CHANNEL PN601R35020-25 AT AFT CARGO DOOR FWD TRACK REF SRM.
Part: FRAME — CHAFED (FUSELAGE) · airframe 28,834 hrs · 28,897 cycles
FRAME 718 BETWEEN STR16L AND STR17L, FREE FLANGE CHAFED THROUGH AND INTO FRAME WEB BY HYDRAULIC SUCTION HOSE (MARKED), (48 MONTH) RO 5/28/2020. PERFORMED SPLICE REPAIR TO FS718 FRAME BETWEEN STR20L AND STR13L REF REO. COMPLETED TASK CARD.
Part: FLOORBOARD — DELAMINATED (CARGO BAY) · airframe 28,834 hrs · 28,897 cycles
CARGO FLOORBOARD PNL281CLF IS DELAMINATED (48 MONTH) RO 5/28/2020. EVALUATED AND FOUND CARGO FLOORBOARD 281CLF TO BE BEYOND REPAIRABLE LIMITS PER REPAIR MANUAL. ORDERED AND RECEIVED REPLACEMENT FLOORBOARD P/N 601R31668-459 PO T-52072
Part: FLOORBOARD — DELAMINATED (CARGO BAY) · airframe 28,834 hrs · 28,897 cycles
CARGO FLOORBOARD PNL282MRF IS DELAMINATED (48 MONTH) RO 5/28/2020. EVALUATED AND FOUND CARGO FLOORBOARD 282MRF TO BE BEYOND REPAIRABLE LIMITS PER REPAIR MANUAL. ORDERED AND RECEIVED REPLACEMENT FLOORBOARD P/N 601R31668-477 PO T-52608.
Part: FLOORBOARD — DELAMINATED (CARGO BAY) · airframe 28,834 hrs · 28,897 cycles
CARGO FLOORBOARD PNL281FLF IS DELAMINATED (48 MONTH) RO 5/28/2020. EVALUATED AND FOUND CARGO FLOORBOARD 281FLF TO BE BEYOND REPAIRABLE LIMITS PER REPAIR MANUAL. ORDERED AND RECEIVED REPLACEMENT FLOORBOARD P/N 601R31668-455 PO T-50686.
Part: PLATE — CHAFED (TE FLAP) · airframe 28,834 hrs · 28,897 cycles
LEFT INBOARD FLAP VANE INBOARD LEADING EDGE CHAFED APPROXIMATELY 6Ãâ¬? FROM INBOARD END. (48 MONTH) RO 5/28/2020. REMOVED AND REPLACED LT FLAP VANE SACRIFICIAL PLATE REF SRM.
Part: PLATE — CHAFED (TE FLAP) · airframe 28,834 hrs · 28,897 cycles
RIGHT INBOARD FLAP VANE INBOARD LEADING EDGE CHAFED APPROXIMATELY 6Ãâ¬? FROM INBOARD END. (48 MONTH) RO 5/28/2020. REMOVED AND REPLACED RT FLAP VANE SACRIFICIAL PLATE REF SRM.
2018
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,947 hrs · 25,646 cycles
LBL27 SEAT RAIL BEAM FS559+80 TO FS574.00 HAS CORROSION. (C-CHECK) RO: 09/09/2018. LBL 27 SEAT RAIL BEAM REPLACED FROM FS569 TO FS559+52 IAW SRM.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 25,947 hrs · 25,646 cycles
CARGO DOOR FLOOR SILL FS574.00 - FS621.00 HAS CORROSION. (C-CHECK) RO: 09/09/2018. CARGO DOOR FLOOR SILL FS574 TO FS621 REMOVED AND REPLACED IAW REO.
Part: SKIN PANEL — CHAFED (LT AILERON) · airframe 25,947 hrs · 25,646 cycles
THE LT AILERON'S LOWER INBOARD LEADING EDGE SKIN/PANEL IS CHAFED IN MULTIPLE AREAS. (C-CHECK) RO: 09/09/2018. REPLACED LT AILERON LOWER INBOARD LEADING EDGE SKIN (SHROUD) IAW SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,947 hrs · 25,646 cycles
RBL9 SEAT RAIL BEAM FS559+80 - FS559+96 HAS CORROSION. (C-CHECK) RO: 09/09/2018. REMOVED AND INSTALLED RBL9 SEAT RAIL BEAM FS559+80 - FS559+96 IAW SRM AND REO.
Part: DOOR SILL — GOUGED (FUSELAGE) · airframe 25,947 hrs · 25,646 cycles
FOUR GOUGE MARKS ON PASSENGER DOOR UPPER SILL FITTING BETWEEN FS310.00 & FS349.00. (C-CHECK) RO: 09/09/2018. REPAIRED 4 GOUGE MARKS ON PASSENGER DOOR UPPER SILL FITTING BETWEEN FS310.00 & FS349.00, IAW REO.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 25,947 hrs · 25,646 cycles
RIGHT PRESSURE FLOOR SILL FS409.0+128 TO FS559.0 HAS CORROSION. (C-CHECK) RO: 09/09/2018. REPAIRED RT PRESSURE FLOOR SILL FS409.0+128 TO FS559.0 IAW REO.
2017
Part: STRINGER — DAMAGED (BS 582-621) · 24,087 cycles
STRINGER 21L FROM BS 582 TO 621 HAD ELONGATED HOLES. REMOVED AND REPLACED THE STRINGER SECTION IAW SRM.
Part: SKIN — DAMAGED (BS 589) · 24,087 cycles
FOUND SEVERAL ELONGATED HOLES IN SKIN BS 589. REPAIRED THE SKIN IAW REO.
Part: FLOOR SUPPORT — CORRODED (BS 349) · 24,087 cycles
FLOOR SUPPORT AT BS 349 AT STRINGER 17R IS CORRODED. REPAIRED IAW REO.
Part: FRAME — CORRODED (BS 589) · 24,087 cycles
FRAME BS 589 IS CORRODED BETWEEN STRINGERS 26 AND 27L. REPAIRED THE FRAME IAW REO.
Part: FRAME — CORRODED (BS 605) · 24,087 cycles
FRAME BS 605 IS CORRODED BETWEEEN STRINGERS 26 AND 27L. REMOVED AND REPLACED THE FRAME SECTION IAW SRM.
Part: SKIN — DENTED (LT WING TE FLAP) · 24,087 cycles
LEFT INBOARD FLAP TOP AND BOTTOM SKIN DENTED. TOP DENT APPROX 1.5" X .5" X .10". BOTTOM DENT APPROX 4" X 1.5" X .10". REPAIRED THE SKIN IAW SRM.
Part: SKIN — DENTED (BS 251) · 24,087 cycles
DENT ON FUSELAGE SKIN BS 251, STRINGER 23L. REPAIRED IAW REO.
Part: SKIN — DENTED (LT WING TE FLAP) · 24,087 cycles
LEFT INBD FLAP HAS A DENT ON UNDERSIDE JUST INBD OF WS 120.382. REPAIRED THE FLAP SKIN IAW SRM.
2016
Part: DOOR — OUT OF ADJUST · airframe 22,576 hrs · 21,932 cycles
ASD IS HARD TO OPEN FROM OUTSIDE. REMOVED THE ASD DOOR POWER ASSIST MOTOR IAW AMM 52-11-08-000-802. INSTALLED NEW SERIVCABLE ASD DOOR ASSIST MOTOR IAW AMM 52-11-08-400-802. ADJUSTED COUNTER BALACNE IAW AMM 52-11-17-820-802. OPS CHECKED GOOD.
Part: DOOR — OUT OF RIG · airframe 22,576 hrs · 21,932 cycles
DURING OPS TEST, THE PASSENGER DOOR FAILED OPS TEST & REQUIRES ADJUSTMENT. REPAIRED IAW AMM TASK 52-11-17-820-802, & 52-11-00-400-802.
Part: ACCESS PANEL — DAMAGED (FUSELAGE) · airframe 22,576 hrs · 21,932 cycles
LT CHEEK PANEL, 131AL CUTOUT HAS 1 DAMAGE SCREW HOLE APPROXIMATELY 12 O`CLOCK. REPAIRED DAMAGED FASTENER HOLES IN FORWARD FUSELAGE ACCESS PANEL DOOR SURROUND DOUBLER FS 228, STR 19-20 IAW REO 601R-53-11-162, REV C.
Part: FITTING — CRACKED (COCKPIT) · airframe 22,576 hrs · 21,932 cycles
LEFT WINDSHIELD SIDE POST LOWER AFT CLIP IS CRACKED. REMOVED LT WINDSHIELD SIDE POST LOWER AFT FITTING, CLIP IAW SRM 51-42-21. LOCATED AND DRILLED NEW FITTING AT LT WINDSHIELD SIDE POST LOWER AFT IAW SRM 51-40-11. INSTALLED IAW SRM, 51-42-21.
Part: FITTING — CRACKED (COCKPIT) · airframe 22,576 hrs · 21,932 cycles
RT WINDSHIELD SIDE POSE LOWER AFT CLIP IS CRACKED. REMOVED RT WINDSHIELD SIDE POST LOWER AFT FITTING, CLIP, IAW SRM 51-42-21. LOCATED AND DRILLED NEW FITTING AT RT WINDSHIELD SIDE POST LOWER AFT IAW SRM 51-40-11 INSTALLED IAW SRM, 51-42-21.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 22,576 hrs · 21,932 cycles
CARGO SEAT TRACK CORRODED OUT OF LIMITS AT LBL 9 BETWEEN 559+112-574. REMOVED CARGO SEAT TRACK, LBL9, FS 559+112-FS 574 IAW AMM 53-00-49-00-801. INSTALLED NEW FABRICATED SEAT RAIL AT LBL9, FS 559+12 -FS 574 IAW AMM 53-00-49-400-801. COMPLIED WITH EC/TC EO 601R-53-00-485 AND GREO 601R-53-00-485 REV B.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 22,576 hrs · 21,932 cycles
CARGO SEAT TRACK CORRODED OUT OF LIMITS AT RBL9 BETWEEN 559+112-574. REMOVED CARGO SEAT TRACK, RBL9, FS 559+112-FS 574 IAW AMM 53-00-49-00-801. INSTALLED NEW FABRICATED SEAT RAIL AT RBL9, FS 559+112-FS 574 IAW AMM 53-00-49-400-801. COMPLIED WITH EC/TC EO 601R-53-00-485 AND GREO 601R-53-00-485, REV B.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 22,576 hrs · 21,932 cycles
LT CARGO FLOOR SILL CORRODED BETWEEN 574-621. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526, REV.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 22,576 hrs · 21,932 cycles
CARGO SEAT TRACK CORRODED OUT OF LIMITS AT LBL9, BETWEEN 559+80-559+96. REMOVED CARGO SEAT TRACK, LBL9, FS 559+80-559+96 IAW AMM 53-00-49-000-801. INSTALLED NEW FABRICATED CARGO SEAT TRACK AT LBL9, FS 559+80-559+96 IAW AMM 53-00-49-400-801. COMPLIED WITH EC/TC REO 601R-53-00-485 AND GREO 601R-53-00-485, REV B, DATED 04/01/2016.
Part: CARGO TRACK — CORRODED (BS 559) · airframe 22,576 hrs · 21,932 cycles
CARGO TRACK IS CORRODED OUT OF LIMITS AT LBL 27 BETWEEN 559+80 & 559+96. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-00-49-00-801 & AMM 53-00-49-400-801.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,576 hrs · 21,932 cycles
LBL 27 FLOORBEAM CORRODED BETWEEN 570-621. EVALUATED FLOORBEAM AT LBL27, FS 570-620, FOUND TO BE OUT OF LIMITS IAW SRM 53-61-43. R & R FLOORBEAM AT FS 570-621, LBL27 IAW SRM 51-42-06 AND 51-42-21 LOCATED AND DRILLED NEW FLOORBEAM IAW SRM 51-40-41. COMPLIED WITH ECTC REO 601R-523-61-3778 AND GREO 601R-53-61-3778, REV A.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 22,576 hrs · 21,932 cycles
CARGO SEAT TRACK CORRODED OUT OF LIMITS AT RBL27 BETWEEN 559+80-559+96. REMOVED CARGO SEAT TRACK RB 27, FS 559+80-FS 559+96 IAW AMM 53-00-49-00-801. INSTALLED NEW FABRICATED SEAT RAIL AT RBL 27, FS 559+80-FS 559+96 IAW AMM 53-00-49-400-801. COMPLIED WITH EC/TC EO 601R-53-00-485 AND GREO 601R-53-00-485, REV B.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 22,576 hrs · 21,932 cycles
CARGO SEAT TRACK CORRODED OUT OF LIMITS AT RBL 9 BETWEEN 559+80-559+96. REMOVED CARGO SEAT TRACK, RBL9 FS 559+80- 559+96 IAW AMM 53-00-49-000-801. INSTALLED CARGO SEAT TRACK AT RBL9 FS 559+80-559+96 IAW AMM 53-00-49-400-801. COMPLIED WITH EC/TC REO 601R-53-00-485 AND GREO 601R-53-00-485, REV B.
Part: ANGLE — CORRODED (BS 310-349) · airframe 22,576 hrs · 21,932 cycles
DISBONDED NUT PLATES WITH SLIGHT CORROSION AT ATTACHMENT POINT AT ASD LOWER SILL ANGLE BETWEEN BS 310 - 349, WL 73.50. REMOVED THE CORROSION & FOUND TO BE OUT OF LIMIT IAW SRM 53-00-00. REMOVED AND REPLACED THE LOWER SILL ANGLE IAW SRM 51-42-13, 51-52-06, 51-42-21, SRM 51-40-11, AND 51-42-6.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 22,576 hrs · 21,932 cycles
RT FLOOR SILL CORRODED AROUND NUTPLATE BETWEEN 559+80-559+112 COMPLIED WITH EC/TC REO 601R-53-000-526 01 AND GREO 601R-53-00-526, REV.
Part: HINGE — GOUGED (PAX DOOR) · airframe 22,576 hrs · 21,932 cycles
PAX DOOR PIANO HINGE LUGS 7 AND 27 ON DOOR SIDE GOUGE. REPAIRED PAX DOOR HINGE DOORSIDE IAW EC/TC REO 601R-52-11-1347 & REO 601R-52-11-1347. MAJOR REPAIR.
Part: BRACKET — CRACKED (BS 202) · airframe 22,576 hrs · 21,932 cycles
IN FWD HYD BAY BS 202 SKIN IS CRACKED WHERE BRAKE CONTROL PUSH PULL MECHANISM ROD PASSES THROUGH SKIN. COMPLIED WITH EC/TC REO 601R-53-11-563 AND REO 601R-53-11-563 REV C. LOCATED, DRILLED AND INSTALLED NEW BRACKET IAW SRM 51-40-11 AND SRM 51-42-06.
2014
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,049 hrs · 18,246 cycles
CABIN CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-16. OPS CHECKED GOOD.
2013
Part: SCREW — MISSING (EMERGENCY LIGHT) · airframe 17,977 hrs · 17,131 cycles
LT AFT EXTERNAL EMERGENCY LIGHT LENS MISSING ONE SCREW. R & R LIGHT LENS IAW AMM 33-51-21.
Part: LIGHT — DAMAGED (CABIN) · airframe 17,977 hrs · 17,131 cycles
CENTER CABLE CEILING EMERGENCY LIGHTS, DAMAGED. R & R LIGHT ASSY IAW AMM 33-51-14. OPS CHECKED GOOD.
Part: ANGLE — CRACKED (BS 559) · airframe 17,758 hrs · 16,893 cycles
FOUND FS 559 CAP ANGLES AT LBL AND RBL 18 HAVE INDICATIONS NOTED APPROX .3" IN LENGTH 50 PERCENT FSH, BOTH FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-41-260 & REO 601R-53-41-260, REV E, AND REO 601R-53-41-1704.
Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 17,758 hrs · 16,893 cycles
FS 621 FWD SIDE FIVE ISOLATORS BROKEN OR MISSING. REMOVED BROKEN ISOLATORS AND REPLACED WITH NEW PARTS IAW SRM 51-42-13 .
Part: FLOOR SUPPORT — DAMAGED (BS 484) · airframe 17,758 hrs · 16,893 cycles
FS 484, LBL 27, FLOOR SUPPORT ANGLE IS CRACKED. REMOVED FS 484, LBL 27, FLOOR SUPPORT ANGLE IAW SRM 51-42-21. LOCATED & DRILLED NEW SUPPORT ANGLE & INSTALLED NEW ANGLE IAW SRM 51-40-11 & 51-42-21.
Part: POST — CRACKED (BS 409) · airframe 17,758 hrs · 16,893 cycles
FOUND FS 409+128 BL 0 LT AND RT VERTICAL POSTS HAVE INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL 69 BOTH APPROX .250" X 60 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW SRM 51-42-06 AND REO 601R-53-41-889.
Part: POST — CRACKED (BS 409) · airframe 17,758 hrs · 16,893 cycles
FOUND FS 409+128, LBL 18 INBD AND OTBD VERTICAL POSTS HAVE INDICATIONS NOTED IN AFT FLANGE RADIUS AT WL 69, BOTH APPROX .250" X 50 PERCENT FSH, FAILED NDT INSPECTION. REMOVED INBD AND OTBD VERTICAL POSTS AT STA FS 409+128 LBL 18 IAW SRM 51-42-06. INSTALLED INBD AND OTBD VERT POSTS AT FS 409+128 LBL 18 IAW REO 601R-53-41-889 AND SRM 51-42-06. LOCATED AND DRILLED INBD AND OTBD VERTICAL POST IAW 51-40-11.
Part: POST — CRACKED (BS 409) · airframe 17,758 hrs · 16,893 cycles
FOUND FS 409+128, RBL 18 INBD VERTICAL POSTS HAVE INDICATIONS NOTED IN AFT FLANGE RADIUS AT WL 69, BOTH APPROX .250" X 50 PERCENT FSH, FAILED NDT INSPECTION. REPAIRED IAW SRM 51-42-06 & REO 601R-53-41-889.
Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 17,758 hrs · 16,893 cycles
CARGO DOOR AREA FLOOR SUPPORT IS CORRODED FROM BS 574-621 . REMOVED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-06 AND 51-42-21 AND REO 601R-53-61-1574.
Part: ANGLE — CRACKED (BS 280) · airframe 17,758 hrs · 16,893 cycles
FS 280, ANGLE AT RBL 9 OTBD SIDE IS CRACKED. REMOVED ANGLE AT FS 280, RBL 9 OTBD, LOCATED NEW CLIP, PN 601R31113-58 IAW SRM 51-40-11 AND INSTALLED IAW SRM 51-42-21.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 17,758 hrs · 16,893 cycles
PAX DOOR AFT DRAG ANGLE IS CRACKED ABOVE PAX DOOR ASSIST MOTOR PULLEY. REPAIRED IAW REO 601R-52-11-513.
Part: ANGLE — CRACKED (BS 625) · airframe 17,758 hrs · 16,893 cycles
RT UPPER BS 625 OBLIQUE ANGLE IS CRACKED. R & R ANGLE IAW SRM 51-42-06.
2012
Part: UNKNOWN — SMOKE (CABIN) · airframe 16,531 hrs · 15,608 cycles
SMOKE ODOR IN COCKPIT ON BASE LEG, F/A REPORTS SMOKE AND ODOR IN THE CABIN. EMERGENCY DECLARED AS A PRECAUTION. PERFORMED OPS CHECK OF BOTH PACKS IAW AMM 21-51-00. NO DEFECTS NOTED AT THIS TIME.
2011
Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,192 hrs · 11,908 cycles
FS 280 WEB CRACKED OTBD OF RBL 9 APPROX .250", FLOORBEAM CLIPS INBD OF LBL 9 & RBL 9 ARE CRACKED AND J-ANGLE OTBD OF LBL 9 CRACKED. OPS CHECK GOOD IAW AMM 27-11-00-710-801. FOUND TO BE SATISFACTORY. (CLOSED)
Part: INTERCOSTAL — CRACKED (BS 484) · airframe 13,192 hrs · 11,908 cycles
FS 484.00 INTERCOSTAL IS CRACKED AT RBL 36. REPAIR TO INTERCOSTALS AT FS 484 BETWEEN BL 27.00 AND BL 36 IS COMPLETED IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS. FOUND TO BE SATISFACTORY.
Part: PLACARD — WORN (CABIN) · airframe 13,192 hrs · 11,908 cycles
EMERGENCY EXIT 831, CLOSED DECAL WORN & PAINT WORN ON PANEL 831. PAINTED PANEL 831 IAW SRM 51-25-01 AND APPLIED SILKSCREENS TO PANEL IAW MM 11-10-03-400-801.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,192 hrs · 11,908 cycles
FS 280 WEB CRACKED OTBD OF RBL 9 APPROX .250". FLOORBEAM CLIPS INBD OF LBL 9 AND RBL 9 ARE CRACKED. OTBD OF LBL 9 CRACKED.
Part: INTERCOSTAL — CRACKED (BS 484) · airframe 13,192 hrs · 11,908 cycles
FS 484 INTERCOSTAL ANGLE IS CRACKED RBL 27. REPAIRED TO THE INTERCOSTAL IAW REO 601R-53-41-059.
Part: INTERCOSTAL — CRACKED (BS 484) · airframe 13,192 hrs · 11,908 cycles
FS 484 INTERCOSTAL IS CRACKED AT RBL 36. REPAIRED INTERCOSTAL IAW REO 601R-53-41-059.
Part: SEAT TRACK — CORRODED · airframe 13,192 hrs · 11,908 cycles
AISLE SEAT TRACK HAS CORRODED FWD SEGMENT. REMOVED THE CORROSION ON THE LT AND RT AISLE SEAT TRACKS. FOUND THE LT SIDE FWD 2 AREAS .5" W X .5" L AND .014" DEEP TO BE WITHIN ALLOWABLE LIMITS OF THE SRM 53-00-49 AND 53-21-49. FOUND THE RT SIDE FWD END TO HAVE 4 AREAS OF CORROSION. THE AFT 2 AREAS ARE 1.5" X .4" AND .005" DEEP. THE FWD 2 AREAS ARE 2" X .4" AND APPROX .017" DEEP AND ARE WITHIN ALLOWABLE LIMITS OF THE SRM 53-00-49 AND 53-21-49. BLENDED AREAS IAW SRM 51-12-00.
2010
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 12,846 hrs · 11,499 cycles
FED CABIN CEILING EMERGENCY LIGHT INOP. RELAMPED FWD CABIN CEILING EMERGENCY LIGHT IAW AMM 33-23-04, OPS CK GOOD. (CLOSED)
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 12,776 hrs · 11,411 cycles
SERVICE DOOR EXIT LENS MISSING. C/W MISSING SERVICE EXIT LENS. REF AMM 33-51-00. (CLOSED)
Part: FIRE LOOP — FALSE INDICATION (APU BAY) · airframe 11,879 hrs · 10,347 cycles
ON TAKEOFF AFTER FLAP RETRACTION RECVD RED APU FIRE L JETPIPE OVERHEAT. RED PARKING BRAKE MSG AND SEVERAL YELLOW CAUTION MSGS. DISCHAGED APU FIRE BOTTLE IAW QRH AND RETURNED TO LAND. LANDED OVERWEIGHT. EMERGENCY DECLARED -- ACFT RETURNED TO DEPARTURE AFTER T/O) PERFORMED A/C WOW CONFIG IAW AMM 32-61-00. INTERRIGATED MDC. NO FAULTS FOUND. PSCU HAD NO CODES STORED. COULD NOT DUPLICATE. OK FOR SERVICE. (CLOSED)
2009
Part: WARNING SYSTEM — MALFUNCTIONED (MLG) · airframe 10,596 hrs · 8,892 cycles
FLT 5564. GEAR DISAGREE WARNING AFTER GEAR SELECTED UP ON CLIMB OUT, COMPLIED WITH QRH, GOT GEAR DOWN & LOCKED. [EMERGENCY DECLARED -- AIRCRAFT RETURNED TO ATL AFTER T/O]. ( NOSE GEAR INDICATED UP & BOTH MAINS DIDN'T)
Part: DOOR — STUCK (MAIN PAX) · airframe 10,470 hrs · 8,756 cycles
PAX DOOR WILL NOT OPEN (PASSENGER DOOR POWER ASSIST SYSTEM).
Part: DOOR — MALFUNCTIONED (ENTRY DOOR) · airframe 10,124 hrs · 8,380 cycles
F/A REPORTS ENTRANCE DOOR NOT OPENING PROPERLY.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 9,307 hrs · 7,587 cycles
JOB 8803811 OPERATION 199 / CARGO DOOR SUPPORT FS 621 LOWER SUPPORT ANGLE CRACKED.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 9,307 hrs · 7,587 cycles
JOB 8803811 OPERATION 209 / FS 280 OUTBOARD RBL & LBL 9 CUPS ARE CRACKED.
Part: WEB — CRACKED (PAX DOOR) · airframe 9,307 hrs · 7,587 cycles
PAX DOOR AFT WEB IS CRACKED IN 2 LOCATIONS, BOTH IN CORNERS, FOR MID FIXED STEP AND 832CT. REPAIRED PAX DOOR AFT WEB IAW REO 601R-52-11-702, REV A.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 9,307 hrs · 7,587 cycles
JOB 8803811 OPERATION 151 / PAX DOOR AFT DRAG ANGLE IS CRACKED NEAR ASSIST MOTOR PULLEY BRACKET. REPAIRED PAX DOOR AFT DRAG ANGLE IAW BOMBARDIER REO 601R-52-11-513, REV A. C/W EC/TC REO 601R-52-11-513 IAW REO 601R-52-11-513, REV A. NO FURTHER ACTION REQUIRED.
Part: PLACARD — TORN (PAX DOOR) · airframe 9,307 hrs · 7,587 cycles
JOB 8803811 OPERATION 147 / PAX DOOR EXIT PLACARD IS TORN.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 9,307 hrs · 7,587 cycles
JOB 8803811 OPERATION 88 / THE LT UPPER FS 621 TO FS 625 INTERCOSTAL ANGLE IS CRACKED.
2008
Part: ANCHOR FITTING — CORRODED (AIRSTAIR DOOR) · airframe 8,121 hrs · 6,522 cycles
AFT ASD ANCHOR FITTING HAS CORROSION DAMAGE ON SERRATED SIDE. REMOVED AND REPLACED ANCHOR FITTING SERRATED PLATE IAW SB 601R-52-093. (S)
Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 8,120 hrs · 6,521 cycles
AFT ASD ANCHOR FITTING SERRATED PLATE SHOWS SIGNS OF CORROSION. REMOVED AND REPLACED ANCHOR FITTING IAW SB 601R-52-093. NO DEFECTS NOTED AT THIS TIME. RII COMPLIED WITH SATISFACTORILY ON ADJUSTMENT AND RIG OF AFT ASD ANCHOR FITTING PER SP 607. (S)
Part: ANCHOR FITTING — CRACKED (AIRSTAIR DOOR) · airframe 8,120 hrs · 6,521 cycles
FWD ASD ANCHOR FITTING CRACKED. REMOVED AND REPLACED FWD ASD ANCHOR FITTING. ALL WORK ACCOMPLISHED IAW SB 601R-52-093. OPS CHECK GOOD. TK 7025453. RII COMPLIED WITH SATISFACTORILY ON ADJUSTMENT AND RIG OF FWD ASD ANCHOR FITTING PER SP 607. (S)
Part: DOOR — OUT OF ADJUST · airframe 7,746 hrs · 6,201 cycles
SERVICE DOOR WILL NOT OPEN FROM THE OUTSIDE. ADJUSTED SERVICE DOOR PER MM REF 52-41-00 OPS CHECK OK. (B)
2007
Part: YOKE — BINDING · airframe 6,293 hrs · 4,968 cycles
FELT A POP AND BINDING WHEN TURNING YOKE TO THE LEFT. EXCESSIVE FORCE OR STRENGTH NEEDED TO TURN YOKE LEFT ALSO. A/C RETURNED TO DAY AFTER T/O. EMERGENCY DECLARED. FLT 4434 DEL 61 MINS. NC FLT 4434 CX.
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 5,671 hrs · 4,486 cycles
LEFT MLG DISAGREE. A/C RETURNED TO OMA AFTER T/O. EMERGENCY DECLARED. LANDING GEAR RETRACTION SYSTEM.
2006
Part: ANCHOR FITTING — CRACKED (AIRSTAIR DOOR) · airframe 3,858 hrs · 3,163 cycles
ASD AFT CABLE COUNTER BALANCE ANCHOR BRACKET CRACKED.