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.
201 reports on file, 2006-11-07 – 2026-07-08.
Part: TRUNNION — GOUGED (ZONE 700) · airframe 32,312 hrs · 33,399 cycles
RIGHT MLG TRUNNION HAS GOUGES. REPAIRED THE GOUGES ON RT MLG TRUNNION IAW REO 601R-57-21-4118, REV --, COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 32,312 hrs · 33,399 cycles
FOUND PAX DOOR INTERCOSTAL MID DD3 SEVERAL CORRODED. REPLACED WITH NEW PAX DOOR INTERCOSTAL MID DD3 IAW DWG 601R31702, REV-N, & SRM 51-42-06, REV 39. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. LEAK CHECKED GOOD WITH NO DEFECTS NOTED.
Part: FORMER — CORRODED (ZONE 800) · airframe 32,312 hrs · 33,399 cycles
FOUND CORROSION ON PAX DOOR FORMER BS 329.76. INSTALLED NEW PAX DOOR FORMER BS 329.76 IAW DWG 601R31702, REV-N, AND SRM 51-42-06, REV 39. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY. LEAK CHECKED GOOD WITH NO DEFECTS NOTED.
Part: CLEAT — CORRODED (ZONE 800) · airframe 32,312 hrs · 33,399 cycles
FOUND PAX DOOR CLEAT AT INTERCOSTAL MID DD4 COMMON TO FORMER BS 338.963 SEVERAL CORRODED. REPLACED PAX DOOR CLEAT AT INTERCOSTAL MID DD4 COMMON TO FORMER BS 338.963 IAW DWG 601R31702, REV-N, & SRM 51-42-06.COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.
Part: CLEAT — CORRODED (ZONE 800) · airframe 32,312 hrs · 33,399 cycles
FOUND PAX DOOR CLEAT AT INTERCOSTAL MID DD4 COMMON TO FORMER BS 323.963 SEVERAL CORRODED. REPLACED PAX DOOR CLEAT AT INTERCOSTAL MID DD4 COMMON TO FORMER IAW DWG 601R31702, REV-N, & SRM 51-42-06.COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.
Part: CLEAT — CORRODED (ZONE 200) · airframe 32,312 hrs · 33,399 cycles
FOUND PAX DOOR CLEAT AT INTERCOSTAL MID DD6 COMMON TO FORMER BS 329.76 SEVERAL CORRODED. REPLACED PAX DOOR CLEAT AT INTERCOSTAL MID DD6 COMMON TO FRAME BS 329.76 AIW DWG 601R31702, REV-N, & SRM 51-42-06.COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.
Part: CLEAT — CORRODED (ZONE 800) · airframe 32,312 hrs · 33,399 cycles
FOUND PAX DOOR CLEAT AT INTERCOSTAL MID DD6 COMMON TO FRAME BS 338.963 SEVERAL CORRODED. REPLACED PAX DOOR CLEAT AT INTERCOSTAL MID DD6 COMMON TO FRAME BS 338.963 IAW DWG 601R31702, REV-N, & SRM 51-42-06.COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.
Part: ANGLE — CRACKED (ZONE 800) · airframe 32,312 hrs · 33,399 cycles
FOUND A CRACK ON PAX DOOR INTERCOSTAL DD7 AFT ANGLE. REPLACED PAX DOOR INTERCOSTAL DD7 AFT ANGLE IAW DWG 601R31702, REV-N, &SRM 51-42-06 REV. 39 DATED MAR 10/21.COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.LEAK CHECKED GOOD WITH NO DEFECTS NOTED.
Part: FLOOR SUPPORT — UNKNOWN (ZONE 100) · airframe 32,312 hrs · 33,399 cycles
AS PER REO 601R-53-61-8559, REV -, REINCORPORATE REPAIR TO CARGO BAY FLOOR SUPPORT, BS 562.72 - 589 IAW REO 601R-53-61-690, REV -D, FABRICATED AND INSTALLED NEW REPAIR DOUBLERS AND FILLER IAW REO 601R-53-61-690 REV-D. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.
Part: TRACK — CHAFED (ZONE 800) · airframe 32,312 hrs · 33,399 cycles
AFT CARGO DOOR, AFT TRACK HAS ONE BEND MID LOCATION AND MULTIP[LE CHAFE LOCATIONS. INSTALLED A NEW AFT CARGO AFT TRACK IAW SRM 51-42-06, AND DWG 601R35207, REV W. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.
Part: DOUBLER — CRACKED (ZONE 800) · airframe 32,312 hrs · 33,399 cycles
SUSPICIOUS CRACK ON PAX DOOR PULL IN CAM DOUBLER AT APPROX. FRAME BS 338. REPLACED THE PAX DOOR AFT PULL IN CAM DOUBLER AT BS 338 IAW DWG 601R31702, REV-N, SRM 51-42-06, & SRM 51-42-21.COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 32,312 hrs · 33,399 cycles
FOUND CORROSION ON PAX DOOR INTERCOSTAL DD4 AFT. INSTALLED NEW PAX DOOR INTERCOSTAL AFT DD4 IAW DWG 601R31702, REV-N, & SRM 51-42-06, REV 39. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY. PERFORMED PRESSURE LEAK CHECK ON REWORKED AREA WITH NO DEFECTS NOTED.
Part: HINGE FITTING — CORRODED (ZONE 300) · airframe 32,312 hrs · 33,399 cycles
DURING REMOVAL OF BEARING ON LT ELEVATOR INBD HINGE FITTING, FOUND BEARING BORES TO BE CORRODED AND PITTED. REPLACED THE HINGE FITTING ASSY AT I/B ES16.52 ON LT ELEVATOR, IAW SRM 51-42-06, SRM 51-42-21 AND ELEVATOR ASSY DWG. 601R24025, REV. G. SKYCARD 51-900-1003-SKY,
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 32,312 hrs · 33,399 cycles
FOUND CORROSION ON PAX DOOR INTERCOSTAL MID DD2. REMOVED CORROSION ON THE PAX DOOR INTERCOSTAL, MID DD2, & EVALUATED AS OUT-OF-LIMITS. INSTALLED A NEW PAX DOOR INTERCOSTAL DD2. IAW DWG 601R31702, REV-N, SRM 51-42-06, AND SRM 51-42-21, REVISION 39. COMPLIED WITH TASK CARD 51-900-1003-SKY. PRESSURE CHECKED GOOD. NO LEAKS DETECTED.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 32,312 hrs · 33,399 cycles
FOUND CORROSION ON PAX DOOR INTERCOSTAL FWD DD1. REMOVED CORROSION ON THE PAX DOOR INTERCOSTAL, FORWARD DD1, AND EVALUATED AS OUT-OF-LIMITS. INSTALLED A NEW PAX DOOR INTERCOSTAL DD1 IAW DWG 601R31702, REV-N, AND SRM 51-42-06, REV. 39. COMPLIED WITH TASK CARD 51-900-1003-SKY. PRESSURE CHECKED GOOD. NO LEAKS DETECTED.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 32,312 hrs · 33,399 cycles
FOUND CORROSION ON PAX DOOR INTERCOSTAL AFT DD1. REMOVED CORROSION ON THE PAX DOOR INTERCOSTAL, AFT DD1, AND EVALUATED AS OUT-OF-LIMITS. INSTALLED A NEW PAX DOOR INTERCOSTAL DD1 IAW DWG 601R31702, REV -N, & SRM 51-42-06 REV 39. COMPLIED WITH TASK CARD 51-900-1003-SKY. PRESSURE CHECK GOOD. NO LEAKS DETECTED.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 32,312 hrs · 33,399 cycles
FOUND CORROSION ON PAX DOOR INTERCOSTAL MID DD1. INSTALLED NEW PAX DOOR INTERCOSTAL MID DD1 IAW DWG 601R31702, REV-N, SRM 51-42-06, REV 39, AND SRM 51-42-21, REV 39. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY. LEAK CHECKED GOOD WITH NO DEFECTS NOTED.
Part: HINGE FITTING — CORRODED (OZNE 300) · airframe 32,312 hrs · 33,399 cycles
DURING REMOVAL OF BEARING ON RT ELEVATOR, INBD HINGE FITTING WAS FOUND TO BE PITTED AND CORRODED. REMOVAL AND REPLACED THE RT ELEVATOR INBD HINGE FITTING IAW DWG 601R24025, REV G. COMPLIED FULLY W/SKYCARD 51-900-1003SKY.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 32,312 hrs · 33,399 cycles
FOUND CORROSION ON PAX DOOR INTERCOSTAL MID DD1A. REMOVED CORROSION ON THE PAX DOOR INTERCOSTAL, MID DD1, AND EVALUATED AS OUT-OF-LIMITS. INSTALLED A NEW PAX DOOR INTERCOSTAL DD1 IAW DWG 601R31702, REV-N, SRM 51-42-06, REV 39. & SRM 51-42-21, REV 39. COMPLIED WITH TASK CARD 51-900-1003-SKY. PRESSURE CHECK GOOD. NO LEAKS DETECTED.
Part: DOUBLER — CRACKED (ZONE 800) · airframe 32,312 hrs · 33,399 cycles
PAX DOOR LOWER INTERNAL DOUBLER ATTACHED TO INTERNAL FRAME AT BS 320 WAS CRACKED AT FWD UPPER CORNER. REPLACED PAX DOOR FWD PULL IN CAM DOUBLER IAW DWG 601R31702, REV-N, SRM 51-42-06, & SRM 51-42-21. COMPLETED SKYTRACK TASK CARD 51-900-1003-SKY.
Part: INTERCOSTAL — CRACKED (ZONE 800) · airframe 32,312 hrs · 33,399 cycles
SUSPICIOUS CRACK ON PAX DOOR INTERCOSTAL DD7 AFT. REPLACED PAX DOOR INTERCOSTAL DD7 AFT IAW DWG 601R31702, REV-N, AND SRM 51-42-06, REV 39. COMPLETED SKYTRACK TASK CARD 51-900-1003-SKY.LEAK CHECKED GOOD WITH NO DEFECTS NOTED.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 32,312 hrs · 33,399 cycles
FLOORBEAM ANGLE AT BS 621 LT IS CRACKED. REPAIRED FLOORBEAM ANGLE IAW REO 601R-53-61-117, REV -E, COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 32,312 hrs · 33,399 cycles
FOUND CORROSION ON PAX DOOR INTERCOSTAL DD6 MID. REPLACED PAX DOOR INTERCOSTAL MID DD6 IAW DWG 601R31702, REV-N, SRM 51-42-06, REV 39 & SRM 51-42-21, REV 39. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY. LEAK CHECKED GOOD WITH NO DECFECTS NOTED.
Part: LUG — GOUGED (ZONE 600) · airframe 32,312 hrs · 33,399 cycles
RWS 178 AFT INBD AND OTBD FLAP HINGE BOX LUG FITTING GOUGED. REPAIRED GOUGED DAMAGES IAW REO 601R-57-21-4108, REV -. COMPLIED WITH SKY CARD 51-900-1003-SKY STRUCTURAL MAJOR REPAIR.
Part: INTERCOSTAL — CRACKED (ZONE 500) · airframe 32,312 hrs · 33,399 cycles
LEFT WING BATT RIB INTERCOSTAL AT APPROX. WS 50 HAS POSSIBLE CRACK. INSTALLED NEW LT WING AFT BATT RIB WS 53.60. IAW SRM 51-42-06, SRM 51-42-21, REO 601R-57-21-4117, REV -. & DWG 601R10203, REV -G. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.
Part: BUSHING — MIGRATED (RT TRUNNION) · airframe 32,312 hrs · 33,399 cycles
RIGHT MLG AFT TRUNNION BUSHING SHOWS SIGNS OF MIGRATION. REMOVED THE MIGRATED BUSHING ON THE AFT RT MLG TRUNNION AND REPLACED WITH A NEW BUSHING IAW REO 601R-57-21-4110, REV -, AND COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.
Part: SUPPORT ANGLE — CRACKED (ZONE 600) · airframe 32,312 hrs · 33,399 cycles
RIGHT WING BATT RIB ACCESS PANEL SUPPORT ANGLE AT APPROX. WS 50 HAD A POSSIBLE CRACK. REPLACED BATT RIB SUPPORT ANGLE. IAW DWG 601R10203, REV G. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.
Part: PRESSURE DECK — CORRODED (ZONE 200) · airframe 32,312 hrs · 33,399 cycles
RIGHT PRESSURE FLOOR PANEL, BTWN BS 409+128, & BS 559 HAS MULTIPLE AREAS OF CORROSION. REMOVED CORROSION FROM RT PRESSURE FLOOR PANEL BTWN BS 409+128 & BS 559, 16EA SPOTS. IAW REO 601R-53-41-666, REV-C. DISPOSITION 1.2 STEP.A. FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO 601R-53-41-666, REV-C. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. PRESSURE CHKD GOOD. NO LEAKS DETECTED.
Part: PRESSURE DECK — CORRODED (ZONE 200) · airframe 32,312 hrs · 33,399 cycles
LEFT PRESSURE FLOOR PANEL, BTWN FS 409+128 & BS 559 HAS MULTIPLE AREAS OF CORROSION. REPAIRED CORROSION DAMAGE ON LT PRESSURE FLOOR PANEL, IAW REO 601R-53-41-666, REV-C, COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 32,312 hrs · 33,399 cycles
PASSENGER DOOR MID INTERCOSTAL DD4 HAS CORROSION. INSTALLED NEW PAX DOOR INTERCOSTAL MID DD4 IAW DWG 601R31702, REV-N, SRM 51-42-06, REV 39, & SRM 51-42-21, REV 39, COMPLETED SKYWEST TASK CARD 51-900-1003-SKY. LEAK CHECKED GOOD, NO DEFECTS NOTED.
Part: STIFFENER — BENT (ZONE 500 AILERON) · airframe 32,312 hrs · 33,399 cycles
LEFT AILERON CENTER HINGE FITTING OTBD STIFFENER RIB BENT. COMPLIED WITH ALL STEPS IN PERMANENT REPAIR OF DRESS BACK TO STIFFENER ON LT AILERON, CENTER ACTUATOR HINGE FITTING ASSY BETWEEN, AILERON STA 343-534 - STA 351.539. IAW REO 601R-57-61-899, REV-, AND REO 601R-51-00-309, REV-B. C/W TASK CARD 51-900-1003-SKY.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 32,312 hrs · 33,399 cycles
FLOORBEAM BS 559 BETWEEN LBL 27 AND SILL, CORRODED. INSTALLED A NEW STRAP IAW SRM 51-42-06, REV 39, SRM 51-42-15, REV 39, SRM 51-21-16, REV 39, & DWG 601R31025, REV N. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. LEAK CHECKS GOOD.
Part: DOOR SILL — CORRODED (ZONE 100) · airframe 32,312 hrs · 33,399 cycles
AFT BAGGAGE DOOR OPENING SILL BETWEEN BS 574 - 605 WAS CORRODED. REPLACED AFT BAG BAY DOOR SILL IAW REO 601R-53-61-8559, REV--. & GREO 601R-53-61-690, REV D. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.
Part: FLOOR SUPPORT — DENTED (ZONE 200) · airframe 32,312 hrs · 33,399 cycles
FLOOR SUPPORT LBL 9 BTWN BS 559 TO 559+16 DENTED. R & R THE FLOOR SUPPORT BS.559+10 - 568 IAW REO 601R-53-51-749, REV-, STEPS.1-4. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 32,312 hrs · 33,399 cycles
FLOOR SUPPORT RBL 9, BTWN BS 559 - 559.00+32 CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06, SRM 51-42-21, DWG 601R31119, REV H, & REO 601R-53-51-747, REV-. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.
Part: CHANNEL — CORRODED (ZONE 100) · airframe 32,312 hrs · 33,399 cycles
CHANNEL ASSY OF FWD DRAIN MAST CORRODED. REMOVED THE DAMAGE FROM CHANNEL ASSY OF FWD DRAIN MAST, & EVALUATED AS OUT-OF-LIMITS. REPLACED CHANNEL WITH SERVICEABLE CHANNEL IAW DWG 601R43210, REV D, SRM 51-42-06-00 & SRM 51-42-10, REV 39. COMPLIED WITH TASK CARD 51-900-1003-SKY. PRESSURE LEAK CHKD GOOD. NO LEAKS DETECTED.
Part: PRESSURE BLKHD — DAMAGED (ZONE 100) · airframe 32,312 hrs · 33,399 cycles
COMPLY WITH THE LATEST REVISION OF REO 601R-53-61-1240 PART A AND B, REPAIR AND MODIFICATION TO BS 621 PRESSURE BULKHEAD WEB ON ACFT WITH A TOTAL TAC OF 30000 CYCLES OR MORE IAW REO 601R-53-61-1240, DETERMINED TO BE NOT EFFECTIVE TO ACFT SERIAL NR 8038. REPAIRED THE HOLES ON BS 621 BULKHEAD WEB IAW REO 601R-53-61-8564, REV --. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY. PRESSURE LEAK CHECK GOOD. NO LEAKS DETECTED.
Part: SKIN — CORRODED · airframe 32,312 hrs · 33,399 cycles
AIRCRAFT SKIN AT PANEL 195BB HAS CORROSION AT FASTENER HOLES. REPAIRED CORROSION DAMAGE ON AIRCRAFT SKIN AT PANEL 195BB AT FASTENER HOLES IAW REO 601R-53-61-8546, REV--, SEE CONTINUE CARD FOR WORK PERFORMED, COMPLIED WITH 51-900-1003-SKY. LEAK CHKD OK.
Part: FLOORBEAM — ABNORMAL (ZONE 200) · airframe 32,312 hrs · 33,399 cycles
COMPLY WITH REO 601R-53-41-1116, REPAIR & REINFORCEMENT FOR BS 559 LWR CAP ANGLES BL 9.00 & 18.00 LT & RT. COMPLIED WITH REO 601R-53-41-1116, REV- C. REPAIR AND REINFORCEMENT FOR BS 559 LWR CAP ANGLES, BL 9.AND 18. LT & RT. COMPLIED WITH TASK CARD 51-900-1003-SKY. PRESSURE LEAK CHECK GOOD. NO LEAKS DETECTED.
Earlier reports · 2006–2021 · 162 reports
2021
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 — 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 — 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 — 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 — 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 — 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 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 601R38312-25 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 — 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 — 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
* 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 — 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 — 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 — 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 — 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 — 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 — 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
* 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
* 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 — 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 #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
* 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 — 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 — 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 — 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
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
#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
#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 — 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
#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
#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
#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 — 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
* 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 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
#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
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 — 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
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 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 — 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
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 — 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 — 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 — 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 — 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
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 — 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.
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 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: 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: 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: 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: 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: 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: 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
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: 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: 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: 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 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
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: 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: 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 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: 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: 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.
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.
2018
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: 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
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: 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.
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.
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 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: 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: 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: 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: 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
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: 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 (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 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 (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: 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.
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.
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: 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: 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: 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, 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: 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: 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: 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: 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: 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: 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: 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: 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.
Part: PLACARD — TORN (PAX DOOR) · airframe 9,307 hrs · 7,587 cycles
JOB 8803811 OPERATION 147 / PAX DOOR EXIT PLACARD IS TORN.
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 — 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: 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: 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.