N755EV
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.
255 reports on file, 2005-07-04 – 2026-08-10.
Part: MOTOR — WARNING MESSAGE (HYD PUMP) · airframe 42,921 hrs · 31,901 cycles
HYD 3 LOW PRESSURE DURING CLIMB OUT. RAN QRH. MESSAGE REMAINED. (FLIGHT 6481) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 32805095. REF CP 32808417 FOR CORRECTIVE ACTION AND WORK PERFORMED.
Part: WARNING MESSAGE — ILLUMINATED (ZONE 800) · airframe 41,643 hrs · 30,817 cycles
PASSENGER DOOR WARNING RECEIVED IN FLIGHT. RAN QRH PROCEDURE. FLIGHT ATTENDANT REPORTED A POPPING NOISE FROM THE MCD IN FLIGHT BEFORE WARNING RECEIVED. (FLIGHT 4957) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 31562889 WITH THE FOLLOWING CORRECTIVE ACTION: "FOUND LOWER STOP BOLT FOR THE PAX DOOR INNER HANDLE LOOSE AND OBSTRUCTING FULL TRAVEL OF THE PAX DOOR INNER HANDLE. ADJUSTED AND RE-SECURED LOWER STOP BOLT FOR THE PAX DOOR INNER HANDLE REFERENCING APPLICABLE STEPS OF AMM 52̉‰11̉‰02. PERFORMED OPERATIONAL CHECK OF PAX DOOR REFERENCING APPLICABLE STEPS OF AMM 52-11-00. OPS CHECK GOOD AT THIS TIME. ALSO FOUND THE PAX DOOR SEAL ON THE AFT PORTION OF THE DOOR APPROXIMENTLY 3 FEET DOWN FROM THE TOP STEP WITH A 1 INCH SECTION THAT HAD COME OUT OF THE RETAINER. INSTALLED THE PAX DOOR SEAL THAT HAD COME OUT REFERENCING APPLICABLE STEPS OF AMM 52-11-07. PERFORMED PRESSURIZATION OF THE AIRCRAFT REFERENCING APPLICABLE STEPS OF AMM 21̉‰31̉‰00. NO POPPING NOISE OCCURED DURING PRESSURIZATION OF THE AIRCRAFT. LEAK CHECK GOOD AT THIS TIME. PASSENGER DOOR WARNING WAS NOT PRESSENT DURING PRESSURIZATION."
Part: WARNING MESSAGE — ACTIVATED (ZONE 800) · airframe 41,643 hrs · 30,816 cycles
PASSENGER DOOR WARNING RECEIVED IN FLIGHT. RAN QRH PROCEDURE. FLIGHT ATTENDANT REPORTED A POPPING NOISE FROM THE MCD IN FLIGHT BEFORE WARNING RECEIVED. (FLIGHT 4957) OPEN
Earlier reports · 2005–2024 · 252 reports
2024
Part: LATCH — CRACKED (TRU BAY) · airframe 39,161 hrs · 28,696 cycles
RH AFT TRU BAY LATCH RECESS APPEARS TO BE CRACKED IN TWO LOCATION. (C-CHECK RO 11/6/2024) STOP DRILLED CRACK AT RH AFT TRU BAY LATCH AND COMPLIED WITH ALL STEPS OF REO 670-53-11-2044 REV--, DATED 2024-11-01. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 39,161 hrs · 28,696 cycles
GALLEY 1 MOST FWD INBD FLOOR STRUCTURE MOUNT IS CORRODED. (MARKED) MX # 28984538. (C-CHECK RO 11-6/2024) REMOVED AND REPLACED NEW PLATE FITTING ON GALLEY 1 MOST FWD INBD FLOOR STRUCTURE MOUNT AT FS485 RBL15 REF CRJ700 SRM 51-42-21-001-001-A01 AND DRW# SH690-32120 REV -AL. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR DETAILS
Part: SLIDER — DAMAGED (ZONE 400) · airframe 39,161 hrs · 28,696 cycles
COMPLY WITH REO 670-54-22-088 REV A, FOR DAMAGE TO LH ENGINE UPPER C-DUCT TRANSCOWL SLIDER MOUNT HOLE. (C-CHECK RO 11/6/2024) COMPLIED WITH ALL STEPS OF REO 670-54-22-088 REV A DATED 2024-10-02 , FOR DAMAGE TO LH ENGINE UPPER C-DUCT TRANSCOWL SLIDER MOUNT HOLE. COMPLIED WITH SKYCARD 51-900-1002-SKY
Part: DUCT — GOUGED (THRUST REVERSER) · airframe 39,161 hrs · 28,696 cycles
LH LOWER THRUST REVERSER C-DUCT GOUGED NEAR FLOATING TIE BAR ATTACHING POINTS (C-CHECK RO 11-6/2024) BLENDED-OUT GOUGED AND RESTORED FINISH REWORKED AREA ON LH LOWER THRUST REVERSER C-DUCT NEAR FLOATING TIE BAR ATTACHING POINTS, COMPLIED TO ALL STEPS PROVIDED REF REO 670-54-22-089 REV -- DATE 2024-09-30COMPLIED WITH 51-900-1002-SKY
Part: DUCT — GOUGED (THRUST REVERSER) · airframe 39,161 hrs · 28,696 cycles
LH UPPER THRUST REVERSER C-DUCT, GOUGED NEAR FLOATING TIE BAR ATTACHING POINTS (C-CHECK RO 11-6/2024) BLENDED-OUT GOUGED AND RESTORED FINISH TO REWORKED AREA ON LH UPPER THRUST REVERSER C-DUCT NEAR FLOATING TIE BAR ATTACHING POINTS, COMPLIED TO ALL STEPS PROVIDED REF REO 670-54-22-091 REV -- DATE 2024-09-30 AND COMPLIED WITH TASK CARD 57-900-1002-SKY
Part: FRAME — CORRODED (ZONE 100) · airframe 39,161 hrs · 28,696 cycles
AFT CARGO BELOW FLOOR HAS CORROSION ON FRAME FS1051.30 RBL2 MX# 28848636 (C-CHECK RO 11/6/2024) PERFORMED SPLICE REPAIR FOR CORROSION DAMAGE TO FS1051.30 LOWER FRAME SECTOR BETWEEN STR26L-STR25R REF REO 670-53-61-2372,REV --, DATED 2024-09-24, CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 REV 38 JUL 25/2020, AND DRW MM670-35007, REV. W. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY. LEAK CHECK GOOD.
Part: FRAME — CRACKED (ZONE 200) · airframe 39,161 hrs · 28,696 cycles
FRAME FS333.00 BETWEEN STGR 1R-2R CRACKED CAMP 28807442 (C-CHECK RO 11/6/2024) COMPLIED WITH ALL STEPS 1-20. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS AT FS333- STGR1R - STGR2R REF REO 670-53-21-2457 REV -A DATE 2024-09-25. COMPLIED WITH 51-900-1002-SKY. SEE CONTINUE CARD FOR DETAILS.
Part: SKIN — DAMAGED (ZONE 800) · airframe 39,161 hrs · 28,696 cycles
AFT CARGO DOOR EXTERNAL SKIN HAS EDGE DAMAGE ON THE LWR AFT CORNER (C-CHECK RO 11/6/2024) REPAIRED AFT CARGO DOOR EXTERNAL SKIN DAMAGE REF REO 670-52-31-147 REV.--, DATED 2024-09-12. COMPLIED WITH AALL STEPS OF REO 670-52-31-147 REV.--, DATED 2024-09-12. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR DETAILS. OPS CHECK ON CARGO DOOR CHECK GOOD.
Part: SKIN — CORRODED (ZONE 100) · airframe 39,161 hrs · 28,696 cycles
FUSELAGE SKIN UNDER AFT DRAIN MAST IS CORRODED. CAMP# 28804960 (C-CHECK RO 11-6/2024) REMOVED CORROSION FROM FUSELAGE SKIN UNDER AFT DRAIN MAST, COMPLIED TO ALL THE STEPS REF REO 670-53-61-2365 REV-- DATED 2024-09-12. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: COAMING — CHAFED (ZONE 400) · airframe 39,161 hrs · 28,696 cycles
L/H LOWER TRANSCOWL LATCH COAMING CHAFED AT FWD EDGE BY FWD LATCH. (C-CHECK RO 11-6/2024) COMPLIED W/FINAL VERSION OF MHIRJ REO 670-54-21-1660, REV --, DATED 9/24/24. ALL STEPS OF REO COMPLETED IN THEIR ENTIRETY. SEE CONTINUATION STEPS FOR MORE DETAILS. ALL CHECKS GOOD. AND COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: SLIDER — CHAFED (ZONE 400) · airframe 39,161 hrs · 28,696 cycles
L/H LOWER TRANSCOWL INBD SLIDER CHAFED AT FWD END. (C-CHECK RO 11-6/2024) COMPLIED WITH CRJ 700 REO# 670-54-21-1659, REV --, DATED 9/11/24. COMPLIED WITH MANUAL EXTENSION/RETRACTION OF THE LH ENGINE THRUST REVERSER REF CRJ 700 AMM TASK 78-30-00-980-801-A01 AND CRJ 700 AMM TASK 78-30-00-980-802-A01. OPS CHECK IS GOOD, NO DAMAGES NOTED AT THIS TIME. COMPIED WITH TASK CARD 51-900-1002 SKY
Part: BRACKET — CRACKED (ZONE 400) · airframe 39,161 hrs · 28,696 cycles
L/H UPPER TRANSCOWL INBD "A" BRACKET STIFFENER CRACKED. (C-CHECK RO 11-6/2024) REMOVED AND REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51-900-1002-SKY.
Part: SLIDER — CHAFED (ZONE 400) · airframe 39,161 hrs · 28,696 cycles
L/H LOWER TRANSCOWL OUTBD SLIDER CHAFED AT FWD END. (C-CHECK RO 11-6/2024) COMPLIED WITH CRJ 700 REO# 670-54-21-1659, REV --, DATED 9/11/24 FOR L/H LOWER TRANSCOWL OUTBD SLIDER . COMPLIED WITH MANUAL EXTENSION/RETRACTION OF THE LH ENGINE LOWER THRUST REVERSER REF CRJ 700 AMM TASK 78-30-00-980-801-A01 AND CRJ 700 AMM TASK 78-30-00-980-802-A01. OPS CHECK IS GOOD, NO DAMAGES NOTED AT THIS TIME. COMPLIED WITH TASK CARD 51-900-1002
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 39,161 hrs · 28,696 cycles
R/H RBL 9 FLOOR BEAM CORRODED ON TOP FROM APROX FS 477- FS 570 MARKED (C-CHECK RO 11-6/2024) REPAIRED RH RBL9 FLOOR BEAM FROM APPROX FS477-FS570 REF-CRJ 700 REO 670-53-31-937 REV -- DATED 2024-09-12, EO NO: CL-600-2C10-53-L08306 REV.IR DATED 10/3/2024, CRJ 700 SRM 53-00-41-201-001-A01 REV. 38, DATED JULY 25, 2020. CRJ 700 SRM 51-42-21-001-001-A01 REV. 38, DATED JULY 25, 2020. CRJ 700 SRM 51-42-06-001-001-A01 REV. 38, DATED JULY 25, 2020. COMPLIED WITH TASK 51-900-1002-SKY
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 39,161 hrs · 28,696 cycles
R/H RBL 9 FLOOR BEAM CORRODED ON TOP FROM APROX FS 570 TO FS 680 MARKED (C-CHECK RO 11-6/2024) REPAIRED RBL 9 FLOOR BEAM APROX FS 570 TO FS 680. COMPLIED WITH ALL STEPS OF CRJ 700 SRM 53-00-41-201-001-A01, AND REO 670-53-31-950 REV:-A DATE: 2024-10-07, AND REO 670-53-31-938 REV:-- DATE:2024-09-12, AND REO 670-53-41-687 REV:-- DATE:2024-09-26. COMPLIED WITH TASK 51-900-1002-SKY. SEE CONTINUE CARD FOR DETAILS.
Part: SLAT TRACK — WORN (ZONE 500) · airframe 39,161 hrs · 28,696 cycles
LH WING SLAT TRACK 1-1 HAS WEAR GROVES ON LOWER SURFACE (C-CHECK RO 11-6/2024) BLENDED OUT WEAR GROVES, AT LH WING SLAT TRACK 1-1, ON LOWER SURFACE, 3EA SPOTS, REF. CRJ-700, SRM 51-12-00-001-001-A01. AND FOUND NO LIMITS IN SRM AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1730 REV -- DATE 2024-09-13. AND COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: SLAT TRACK — WORN (ZONE 500) · airframe 39,161 hrs · 28,696 cycles
LH WING SLAT TRACK 3-3 HAS WEAR GROVES ON LOWER SURFACE (C-CHECK RO 11-6/2024) BLENDED OUT WEAR GROVES, AT LH WING SLAT TRACK 3-3, ON LOWER SURFACE, 4EA SPOTS, REF. CRJ-700, SRM 51-12-00-001-001-A01. AND FOUND NO LIMITS IN SRM AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1731 REV-- DATED 2024-09-20 AND TASK CARD 51-900-1002-SKY
Part: FRAME SPLICE — CORRODED (ZONE 200) · airframe 39,161 hrs · 28,696 cycles
FRAME SPLICE STRAP IS CORRODED AT FS319 APPROX. WL72 (RH SIDE) (C-CHECK RO 11-6/2024) REMOVED AND REPLACED NEW FRAME SPLICE BRACKET LOCATED AT FS319.00 APPROX. WL72, R/H SIDE, FLOOR LEVEL REF CRJ 700 SRM 51-42-21-001-001-A01 AND SRM 51-42-13-001-001-A01 AND DWG SH670-31950 REV. Y. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: GUIDE — CHAFED (ZONE 800) · airframe 39,161 hrs · 28,696 cycles
AFT CARGO DOOR SURROUND GUIDE FITTINGS CHAFED (MARKED). (C-CHECK RO 11-6/2024) REPAIRED DAMAGE TO AFT CARGO DOOR SURROUND GUIDE FITTINGS REF REO-670-53-61-2361 REV -- DATE 2024-09-10, BY COMPLYING WITH ALL STEPS. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR DETAILS
Part: DOUBLER — GOUGED (ZONE 100) · airframe 39,161 hrs · 28,696 cycles
AFT LOWER SKIN DOUBLER REPAIR HAS SEVERAL GOUGES FROM WING TO BODY FAIRING (C-CHECK RO 11-6/2024) REMOVED AND REPLACED EXISTING DOUBLER REPAIR AT AFT LOWER SKIN WING TO BODY FAIRING REF REO 670-53-00-290, REV -F, DATED 2019/04/26. PRESSURE LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY. SEE CONTINUE CARD FOR DETAILS.
Part: DOOR FRAME — CORRODED (ZONE 100) · airframe 39,161 hrs · 28,696 cycles
FORWARD BAGGAGE BAY SURROUND STRUCTURE - AFT INNER JOINT PLATE HAS MULTIPLE AREAS OF CORROSION FS578.00 STGR25L. (MARKED IN RED) (C-CHECK RO 11-6/2024) REMOVED AFT INNER JOINT PLATE (LOWER EXTERNAL), FROM FORWARD BAGGAGE BAY SURROUND STRUCTURE, FS578.00 STGR25L, REF. CRJ-700, SRM 51-42-22-001-001-A01 & INSTALLED NEW AFT INNER JOINT PLATE (LOWER EXTERNAL), ON FORWARD BAGGAGE BAY SURROUND STRUCTURE, FS578.00 STGR25L, REF. DRAWING SH670-33750, REV. Y, CRJ-700, SRM 51-42-22-001-001-A01, AND SRM 51-42-21-001-001-A01.COMPLIED WITH TASK 51-900-1002-SKY
Part: TRACK — GOUGED (ZONE 100) · airframe 39,161 hrs · 28,696 cycles
AFT CARGO DOOR FWD TRACK ASSY HAS MULTIPLE AREAS GOUGED (C-CHECK RO 11-6/2024) REMOVED AND REPLACED AFT BAGGAGE BAY DOOR FWD TRACK ASSEMBLY REF. CRJ 700 SRM 53-61-58-001-001-A01 AND CRJ 700 SRM 53-61-58-201-002-A01. OPS TEST GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: DRAIN MAST — CORRODED (ZONE 100) · airframe 39,161 hrs · 28,696 cycles
AFT CARGO BELOW FLOOR DRAIN MAST CHANNEL HAS CORROSION (C-CHECK RO 11-6/2024) EVALUATED CORROSION AND FOUND TO BE BEYOND LIMITS PER CRJ700 SRM 53-61-04-101-003-A01. FABRICATED AND INSTALLED NEW CHANNEL AT AFT CARGO BELOW FLOOR DRAIN MAST REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG# MM670-43200 REV. N. OPS TEST AND LEAK TEST GOOD.
Part: DOOR FRAME — DAMAGED (ZONE 100) · airframe 39,161 hrs · 28,696 cycles
FORWARD CARGO DOOR SURROUND STRUCTURE - INNER SKIN BETWEEN THE FORWARD AND AFT JOINT PLATES HAS DAMAGE ON THE EDGE BEHIND THE FORWARD AND AFT DOOR HINGES. (MARKED IN RED) (C-CHECK RO 11-6/2024) REPAIRED FORWARD CARGO DOOR SURROUND STRUCTURE - INNER SKIN BETWEEN THE FORWARD AND AFT JOINT PLATES REF REO 670-53-31-935 REV:-- DATE: 2024-09-09 STEPS 1-4. ALL STEPS COMPLIED WITH. SKYCARD 51-900-1002-SKY COMPLIED WITH.
Part: TRACK — GOUGED (ZONE 800) · airframe 39,161 hrs · 28,696 cycles
AFT CARGO DOOR AFT TRACK ASSY HAS MULTIPLE AREAS GOUGED (C-CHECK RO 11-6/2024) REMOVED AND REPLACED AFT BAGGAGE BAY DOOR AFT TRACK ASSEMBLY REF. CRJ 700 SRM 53-61-58-201-002-A01 AND CRJ 700 SRM 53-61-58-201-002-A01. OPS TEST GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: DOOR FRAME — CORRODED (ZONE 100) · airframe 39,161 hrs · 28,696 cycles
FORWARD BAGGAGE BAY SURROUND STRUCTURE - FORWARD INNER UPPER JOINT PLATE HAS MULTIPLE AREAS OF CORROSION. (MARKED IN RED) (C-CHECK RO 11-6/2024) REMOVED AND REPLACED WITH NEW FWD BAGGAGE BAY SURROUND FWD INNER JOINT PLATE REF CRJ700 SRM 51-42-21-001-001-A01 AND 51-42-22-001-001-A01 AND DWG SH670-33750, REV AA.COMPLIED WITH TASK CARD 51-900-1002-SKY (CL600-2C10)
Part: SKIN — CORRODED (ZONE 100) · airframe 39,161 hrs · 28,696 cycles
INNER CLOSING SKIN HAS CORROSION IN MULTIPLE AREAS FS536.00 - 578.00 STGR25L. (MARKED IN RED) (C-CHECK RO 11-6/2024) REMOVED CORROSION FROM INNER CLOSING SKIN IN MULTIPLE AREAS FS536.00 - 578.00 STGR25L PER CRJ700 SRM 51-21-06-001-001-A01 AND FOUND TO BE OUT OF LIMITS AND COMPLY WITH ALL STEPS OF REO 670-53-31-939 REV.--, DATED 2024-09-13 AND TASK CARD 51-900-1002-SKY
Part: ANGLE — CORRODED (ZONE 100) · airframe 39,161 hrs · 28,696 cycles
SPLICE ANGLE ON STGR26R BETWEEN FS333.00 & FS349.00 HAS AREAS OF CORROSION. (C-CHECK RO 11-6/2024) BLENDED OUT CORROSION ON SPLICE ANGLE, STGR26R BETWEEN FS333.00 AND FS349.00. REF CRJ 700 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW SPLICE AT STRG 26R AND SHIM IAW CRJ 700 SRM 51-42-21-001-001-A01 AND REO 670-53-21-966 REV C DATED 2022-04-29. COMPLIED WITH TASK CARD 51-900-1002-SKY. RESTORED FINISH AND LEAK CHECK GOOD. SEE CONTINUE CARD FOR DETAILS.
Part: STRINGER — CORRODED (ZONE 100) · airframe 39,161 hrs · 28,696 cycles
CORROSION ON STGR26R BETWEEN FS349.00 & 364.00. (MARKED IN RED) (C-CHECK RO 11-6/2024) BLENDED OUT CORROSION ON STGR 26R BETWEEN FS349.00 & FS364.00. REF CRJ 700 SRM 51-21-06-001-001-A01 AND FOUND DAMAGE ALLOWED IN AREA. REPAIRED USING REO 670-53-21-2459 REV -- DATE: 2024-09-23 LEAK CHECK GOOD SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: SKIN — GOUGED (ZONE 800) · airframe 39,161 hrs · 28,696 cycles
FWD BAG BAY DOOR INNER SKIN AND STRUCTURE GOUGED AND CHAFFED AT R/H FWD CORNER (MARKED) (C-CHECK RO 11-6/2024) REPAIRED CHAFFE ON FWD BAGGAGE BAY DOOR, INNER SKIN AND STRUCTURE AT R/H FWD CORNER AND COMPLIED ALL STEPS REF REO 670-52-35-503 REV.--, DATED 2024-09-10, COMPLIED WITH TASK 51-900-1002-SKY
Part: SKIN — GOUGED (ZONE 800) · airframe 39,161 hrs · 28,696 cycles
FWD BAG BAY DOOR INNER SKIN AND STRUCTURE GOUGED AND CHAFFED AT R/H AFT CORNER (MARKED) (C-CHECK RO 11-6/2024) REPAIRED FWD CARGO DOOR INNER SKIN AND EDGE FRAMES IAW REO 670-52-35-503 REV. -- DATED 2024-09-10 ALL STEPS 1 THRU 5. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: PANEL — CORRODED (ZONE 500) · airframe 39,161 hrs · 28,696 cycles
PANEL 541DB HAS FRETTING CORROSION AT MULTIPLE POINTS ON THE PANEL (MARKED) MX#28736038 (C-CHECK RO 11-6/2024) REMOVED CORROSION ON INNER MATTING SURFACE AT PANEL 541DB REF CRJ700 SRM 51-21-06-001-001-A01 AND FOUND TO BE OUT OF LIMITS AND REPAIR REF REO 670-57-22-114 REV -- DATED 2024-09-03. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: HINGE — DAMAGED (ZONE 800) · airframe 39,161 hrs · 28,696 cycles
PAX DOOR HINGE (PAX SIDE) ROLL PIN INSERT HOLE ELONGATED (C-CHECK RO 11-6/2024) OPENED SPRING HOLE ON PASSENGER DOOR HINGE HALF TO 0.1285", RESTORED FINISH AND INSTALLED A NEW RETENTION SPRING PIN REF REO 670-52-11-1404 REV -- DATED 2024-09-10. ALL STEPS OF REO COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: NUT PLATE — MISSING (ZONE 300) · airframe 39,161 hrs · 28,696 cycles
R/H ELEVATOR PANEL HINGE 342BB HAS A MISSING NUT-PLATE WHERE MARKED. MX # 28730250. (C-CHECK RO 11-6/2024) REPAIRED R/H ELEVATOR PANEL HINGE 342BB RIB REF . EO NO: CL-600-2C10-55-L08260 REV: A DATE: 9/19/2024 AND CRJ 700 SRM 51-42-06-001-001-A01. SEE CONTINUE CARD FOR DETAILSCOMPLIED WITH TASK 51-900-1002-SKY
Part: STRUCTURE — DAMAGED (ZONE 600) · airframe 39,161 hrs · 28,696 cycles
RH WING JACK PAD DOES NOT GO INTO THREADS TRANS#28722388 (C-CHECK RO 11-6/2024) REPLACED RH WING JACK PAD WITH A SERVICEABLE UNIT REF CRJ 700 SRM 51-42-21-001-001-A01 REV. 38, DATED JULY 25, 2020, DWG CC670-10004 REV.-F, DWG CC670-10038 REV.NC. LEAK CHECK GOOD BOND CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY AND TASK CARD 28-900-1000-SKY. SEE CONTINUE CARD FOR DETAILS.
Part: PAD — DAMAGED (ZONE 600) · airframe 39,161 hrs · 28,696 cycles
RH WING JACK PAD DOES NOT GO INTO THREADS TRANS#28722388 (C-CHECK RO 11-6/2024) REPLACED RH WING JACK PAD WITH A SERVICEABLE UNIT REF CRJ 700 SRM 51-42-21-001-001-A01 REV. 38, DATED JULY 25, 2020, DWG CC670-10004 REV.-F, DWG CC670-10038 REV.NC. LEAK CHECK GOOD BOND CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY AND TASK CARD 28-900-1000-SKY. SEE CONTINUE CARD FOR DETAILS.
Part: NONE — NONE (NONE) · airframe 39,161 hrs · 28,696 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: RA74310-670-54-22-037 N787SK MXCODEID59647-PR - ENLARGED HOLES, LOG NUMBER 56115, LINE NO. 11. PERFORMED TEMPORARY REPAIR OF ENLARGED HOLES BY ACCOMPLISHING INSTRUCTIONS IN REO 670-54-22-037,. FINAL HOLE IS 0.354. INSTALLED SLIDER TRACK INSERT REPAIR IS ACCEPTABLE FOR 8000 FLIGHT HOURS AND REQUIRES DETAILED VISUAL INSPECTION PER NDTM 51-20-009 AT EVERY 1000 FLIGHT HOURS. , PART NUMBER: CN624-0101-003 - REVERSER GA-THRUST UPR LH, SERIAL NUMBER: SB1096, POSITION: ONLY (C-CHECK RO 11-6/2024) ENSURED FREEZE PLUG IS INTACT ON FWD HOLE AT LH TR I/B UPPER SLIDER TRACK AND COMPLIED TO ALL THE STEPS PROVIDED REF REO 670-54-22-037 REV -A DATE: 2024-10-01 PERMANENT REPAIR PROCEDURE. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR DETAILS.
Part: NONE — NONE (NONE) · airframe 39,161 hrs · 28,696 cycles
COMPLY WITH: 670BA-53-040 - FUSELAGE - CENTER FUSELAGE, PRIMARY STRUCTURE FS280.00 TO FS295.00 - INSPECTION AND REINFORCEMENT OF LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR REV C PART(S) B (C-CHECK RO 11-6/2024) COMPLIED WITH: 670BA-53-040 - FUSELAGE - CENTER FUSELAGE, PRIMARY STRUCTURE FS280.00 TO FS295.00 - INSPECTION AND REINFORCEMENT OF LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR REV CSERVICE BULLETIN 670BA-53-040, REVISION C, FUSELAGE - CENTER FUSELAGE, PRIMARY STRUCTURE FS280.00 TO FS295.00 - INSPECTION OF LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR, PART A, INCORPORATEDSERVICE BULLETIN 670BA-53-040, REVISION C, FUSELAGE - CENTER FUSELAGE, PRIMARY STRUCTURE FS280.00 TO FS295.00 - INSPECTION AND REINFORCEMENT OF LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR, PART B, INCORPORATEDCOMPLIED WITH SKYCARD 51-900-1002PRESSURE CHECK GOOD, NO LEAKS NOTED AT THIS TIMECOMPLIED WITH ALL STEPS OF REO 670-53-21-493 REV -D DATED 2015/07/16.
2021
Part: ANGLE — CRACKED (BS 333) · airframe 37,680 hrs · 27,589 cycles
AFTER REMOVAL OF F.S 333 FRAME AT STRINGER 21L, FOUND F.S 333 FRAME REINFORCEMENT ANGLE CRACKED. (C-CHECK RO 8/16/2021) REMOVED AND REPLACED CRACKED REINFORCEMENT ANGLE WITH NEW SERVICEABLE ANGLE AT FS333.00 L/H BETWEEN STGR'S 18L AND 21L USING ALL NEW HARDWARE.REF BOMBARDIER DWG# SH670-31810 REV Y AND CRJ700 SRM'S 51-42-06-001-001 A01 AND 51-42-21-001-001 A01. SEE CONTINUATION CARD FOR FURHTER DETAILS. / SKYCARD 51-900-1002-SKY COMPLIED WITH.
Part: STRUCTURE — CHAFED (RT NACELLE) · airframe 37,680 hrs · 27,589 cycles
RH LOWER TRANSCOWL SPIGOT HOLE CHAFED/WORN. (C-CHECK RO 8/16/2021) REPLACED DAMAGED RH LOWER TRANSCOWL SPIGOT HOLE/DOOR LATCH COAMING WITH NEW (P/N: CN624-2060-207) REF REO 670-54-21-1207, REV A DATED 2015-08-27. COMPLIED WITH ST 51-900-1002-SKY.
Part: DUCT — DAMAGED (THRUST REVERSER) · airframe 37,680 hrs · 27,589 cycles
RH ENGINE LOWER THRUST REVERSER C-DUCT, NYLON INSERT MOUNTING SCREW HOLES THROUGH METAL STRUCTURE ARE OBLONG / DAMAGED. (C-CHECK RO 8/16/2021) PERFORMED REPAIR OF RH ENGINE LOWER THRUST REVERSER C-DUCT NYLON ENLONGATED HOLES IAW REO 670-78-30-921 REV-B, DATED 2014-07-02. THRUST REVERSER FUNCTIONAL TEST GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: STIFFENER — CORRODED (BS 280 S23L-R) · airframe 37,680 hrs · 27,589 cycles
LOWER FS250.00 STIFFENER CORRODED AT MULTIPLE AREAS (MARKED) BETWEEN STGR 23R TO STGR 23L. (C-CHECK RO 8/16/2021) LOWER FS250.00 STIFFENER CORROSION EVALUATED AS OUT-O-LIMITS WITH 100% MATERIAL LOSS. REMOVED STIFFENER AT FS250.00 BETWEEN STGR23R - STGR23L, AND INSTALLED NEW STIFFENER, AND ANGLES. REF. CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, BOMBARDIER DWG CC670-34120 REV. NC. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: ANGLE — CRACKED (LT NACELLE) · airframe 37,680 hrs · 27,589 cycles
LH UPPER TRANSCOWL "Z" ANGLE APPEARS TO BE DISBONDED. (C-CHECK RO 8/16/2021) LH UPPER TRANSCOWL Z ANGLE FOUND TO BE CRACKED. PERFORMED REPAIR TO LH UPPER TRANSCOWL "Z" ANGLE IAW ALL STEPS OF REO 670-54-21-1460 REV--, DATED 2021-08-02 AND CRJ700 SRM 51-42-13-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: ANGLE — CRACKED (RT NACELLE) · airframe 37,680 hrs · 27,589 cycles
RH LOWER TRANSCOWL "Z" ANGLE DISBONDED. (C-CHECK RO 8/16/2021) RH UPPER TRANSCOWL Z ANGLE FOUND TO BE CRACKED. PERFORMED REPAIR TO RH UPPER TRANSCOWL "Z" ANGLE IAW ALL STEPS OF REO 670-54-21-1461 REV--, DATED 2021-08-02 AND CRJ700 SRM 51-42-13-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: STRUCTURE — CHAFED (LT NACELLE) · airframe 37,680 hrs · 27,589 cycles
LH UPPER TRANSCOWL SPIGOT HOLE CHAFED/WORN. (C-CHECK RO 8/16/2021) REMOVED DAMAGE AND INSTALLED NEW LH UPPER TRANSCOWL DOOR LATCH COAMING AND SPIGOT DOUBLER PER REO 670-54-21-1207 REV-A, DATED 2015-08-27. COMPLIED WITH ST 51-900-1002-SKY
Part: WINDOW POST — CRACKED (LT WINDSHIELD) · airframe 37,680 hrs · 27,589 cycles
LH WINDSHIELD SIDE POST, CRACK RADIATING FORWARD OUT OF THE TOP BARREL NUT HOLE. (C-CHECK RO 8/16/2021) REMOVED AND REPLACED LH WINDSHIELD SIDE POST, REF. CRJ700 SRM 51-42-21-001-001-A01 AND DRAWING 601R3307 REV. U. PRESSURIZATION LEAK CHEAK GOOD. SEE CONTINUATION CARD FOR MORE DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
Part: WINDOW POST — CRACKED (RT WINDSHIELD) · airframe 37,680 hrs · 27,589 cycles
RH WINDSHIELD SIDE POST, CRACK RADIATING FORWARD OUT OF THE TOP BARREL NUT HOLE. (C-CHECK RO 8/16/2021) REMOVED AND REPLACED RH WINDSHIELD SIDE POST, REF. CRJ700 SRM 51-42-21-001-001-A01 AND DRAWING 601R33007 REV. U. PRESSURIZATION LEAK CHEAK GOOD. SEE CONTINUATION CARD FOR MORE DETAILS. COMPLIED WITH SKYCARD 51-900-1002-SKY / NO DEFECTS NOTED.
Part: DRAG ANGLE — DEFORMED (PAX DOOR) · airframe 37,680 hrs · 27,589 cycles
PAX DOOR AFT DRAG ANGLE DEFORMED AND PREVIOUSLY REPAIRED. REQUIRES REPLACEMENT. (C-CHECK RO 8/16/2021) REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR AFT DRAG ANGLE REF CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-13-001-001-A01.
Part: SKIN — DAMAGED (BS 333 S26-27R) · airframe 37,680 hrs · 27,589 cycles
ELONGATED HOLE IN FUSELAGE SKIN JUST FWD OF FS333.00 BETWEEN STGR 27 AND STGR 26R FROM REMOVAL OF RIVET SECURING DRAIN DOUBLER. (C-CHECK RO 8/16/2021) UPSIZED HOLE TO 0.225", FABRICATED AND INSTALLED NEW DOUBLER REF REO 670-53-21-2072 REV -A DATED 2021-07-05. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1002-SKY. PRESSURE CHECK GOOD.
Part: SKIN — CRACKED (BS 202) · airframe 37,680 hrs · 27,589 cycles
LH FUSELAGE EXTERIOR SKIN HAS CRACK AT APPROXIMATELY FS202 WL79.50 (C-CHECK RO 8/16/2021) REMOVED AND INSTALLED NEW LH FUSELAGE EXTERIOR SKIN PN CC670-33106-1 REF BOMBARDIER DWG CC670-33040 REV G & DWG CC670-32010 REV C AND CRJ 700 SRM 51-42-06-001-001-A01 & SRM 51-42-10-001-001-A01 / .COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: INTERCOSTAL — CORRODED (BS 310-333 S21L) · airframe 37,680 hrs · 27,589 cycles
INTERCOSTAL 21L BETWEEN FS310 AND FS333 HAS EXFOLIATED CORROSION AROUND A FASTENER HOLES AND REQUIRES A REPLACEMENT (C-CHECK RO 8/16/2021) REMOVED AND REPLACED INTERCOSTAL IN FWD CABIN BETWEEN FS310.00 TO FS333.00 STRINGER21L IAW CRJ 700 SRM 51-42-06-001-001-A01 / 51-42-21-001-001-A01 AND DRAWING #SH670-31810 REV AE. ( SEE CONTINUATION SHEET FOR FURTHER DETAILS). COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: ATTACH ANGLE — BENT (BS 333 S21L) · airframe 37,680 hrs · 27,589 cycles
INTERCOSTAL CLIP AT FS333 COMMON TO STRINGER 21L IS BENT AND HAS OVER SIZE FASTENER HOLES AND REQUIRES REPLACEMENT (C-CHECK RO 8/16/2021) REMOVED AND REPLACED INTERCOSTAL CL[P/ANGLE IN FWD CABIN AT FS333.00 STRINGER21L IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. (SEE CONTINUATION SHEET FOR FURTHER DETAILS)
Part: STRINGER SPLICE — CORRODED (BS 333 S21L) · airframe 37,680 hrs · 27,589 cycles
STRINGER SPLICE AT FS333 STRINGER 21L HAS EXFOLIATED CORROSION AROUND A FASTENER HOLE AND REQUIRES REPLACEMENT (C-CHECK RO 8/16/2021) REPLACED STR 21L REF. CRJ 700 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV E / C/W TASK CARD 51-900-1002-SKY
Part: STRINGER — CORRODED (BS 333-347 S21L) · airframe 37,680 hrs · 27,589 cycles
STRINGER 21L BETWEEN FS333 AND FS347 HAS EXFOLIATED CORROSION AROUND A FASTENER HOLE AND REQUIRES A REPAIR (C-CHECK RO 8/16/2021) REPAIRED AND REPLACED STR 21L BETWEEN FS 333-347 PER REO 670-53-21-2089 REV -- DATED 2021-07-19, CRJ 700 SRM 51-42-06-001-001-A01, DWG SH670-32420 REV E AND DWG SH670-31350 REV A / C/W TASK CARD 51-900-1002-SKY
Part: FORMER — CORRODED (PAX DOOR) · airframe 37,680 hrs · 27,589 cycles
CORROSION FOUND ON PASSENGER DOOR AFT FORMER. (C-CHECK RO 8/16/2021) REPLACED THE PASSENGER DOOR AFT FORMER REF. CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND DWG 601R31702 REV N / C/W TASK CARD 51-900-1002-SKY
Part: STRINGER CLIP — CORRODED (BS 265 S27) · airframe 37,680 hrs · 27,589 cycles
STGR 27 CLIP COMMON TO FS265.00 IS CORRODED. (C-CHECK RO 8/16/2021) INSTALLED NEW STGR 27 CLIP COMMON TO FS265.00. REF CRJ700 SRM 51-42-06-001-001-A01. RESTORED FINISH TO STGR CLIP COMMON TO FS265.00 REF CRJ700 SRM 51-25-06-001-001-A01, AND 51-25-16-001-001-A01
Part: HINGE — GOUGED (PAX DOOR) · airframe 37,680 hrs · 27,589 cycles
* PAX DOOR HINGE ( DOOR SIDE ) HAS SEVERAL LUGS WITH SCRATCHES / GOUGES. (C-CHECK RO 8/16/2021) BLENDED OUT SRATCHES AND GOUGES ON HINGE LUG LAND (TYPE IV) AND HINGE FLANGES (TYPE I). REF CRJ700 SRM 52-11-01-201-007-A01. RESTORED FINISH IAW CRJ700 SRM 5125-06-001-001-A01, 51-25-16-001-001-A01, AND51-21-11 -001-001-A01 SW 2512A DATED 10/7/2020. BLEND REPAIR ONLY NO WEIGHT REMOVED /INSTALLED.COMPLIED WITH TAS CARD 51-900-1002-SKY AND M-337 ATTACHED.
Part: HINGE — GOUGED (PAX DOOR) · airframe 37,680 hrs · 27,589 cycles
* PAX DOOR HINGE ( FUSELAGE SIDE ) AFT LUG LAND IS GOUGED. (C-CHECK RO 8/16/2021) BLENDED OUT GOUGE ON AFT LUG LAND PAX DOOR HINGE TO A COMBINED REPAIR DEPTH OF 0.070". FOUND TO BE WITHIN LIMITS. REF CRJ700 SRM 53-21-23-201-001-A01. RESTORED FINISH TO A023 AND A044 REF CRJ700 SRM 53-21-23-201-001-A01 / . / SKYCARD 51-900-1002-SKY COMPLIED WITH
Part: BOLT — SEIZED (RT WING) · airframe 37,680 hrs · 27,589 cycles
RIGHT-HAND WING, FLUTTER DAMPENER, FORWARD BOLT IS SIEZED. (C-CHECK RO 8/16/2021) REMOVED SIEZED BOLT FROM THE RIGHT-HAND WING, FLUTTER DAMPENER, BY REMOVING FLUTTER DAMPENER BRACKET. REF. CRJ700 SRM 51-42-21-001-001-A01. INSTALLED NEW FLUTTER DAMPENER BRACKET. REF. DWG. CC670-10174 REV. E DATE: 2019-JAN-28, CRJ700 SRM 51-42-21-00-001-001-A01. RESTORED FINISH. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: FLOORBEAM — CORRODED (BS 250 S26L/R) · airframe 37,680 hrs · 27,589 cycles
* UNDER COCKPIT FLOOR FS250.00 IS CORRODED APPROX. SRTG 26LH AND 26RH. FLAGGED (C-CHECK RO 8/16/2021) REPLACED THE LOWER ATTACH FLANGE FRAME BETWEEN STR 25L-25R PER REO 670-53-11-1707 REV -A DATED 2021-07-30, DWG CC670-34030 REV -B, CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01 / C/W TASK CARD 51-900-1002-SKY
Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 37,680 hrs · 27,589 cycles
* RIGHT SIDE SEAT RAIL IS CORRODED FROM APPROX. FS 379.00 TO FS 485.00. (C-CHECK RO 8/16/2021) CORROSION IS OUT OF LIMITS OF CRJ 700 SRM 53-21-49-101-001-A01. REMOVED AND REPLACED WITH A SERVICEABLE UNIT REF CRJ 700 AMM 53-00-49-400-801-A17.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,680 hrs · 27,589 cycles
CORROSION FOUND ON PASSENGER DOOR AFT DD4 INTERCOSTAL P/N 601R31902-317 (C-CHECK RO 8/16/2021) REPLACED PASSENGER DOOR AFT DD4 INTERCOSTAL REF CRJ700 SRM 51-42-06-001-001-A01 DWG# 601R31702 REV-N / C/W TASK CARD 51-900-1002-SKY
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 37,680 hrs · 27,589 cycles
* LEFT SIDE SEAT RAIL IS CORRODED FROM APPROX. FS 485.00 TO FS 581.00. (C-CHECK RO 8/16/2021) CORROSION IS OUT OF LIMITS OF CRJ 700 SRM 53-21-49-101-001-A01. REMOVED AND REPLACED WITH A SERVICEABLE UNIT REF CRJ 700 AMM 53-00-49-400-801-A17.
Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 37,680 hrs · 27,589 cycles
* LEFT SIDE SEAT RAIL IS CORRODED FROM APPROX. FS 677.00 TO FS 708.00. (C-CHECK RO 8/16/2021) CORROSION OUT OF LIMITS REF CRJ 700 SRM 53-21-49-101-001-A01. REMOVED AND REPLACED WITH A SERVICEABLE UNIT REF CRJ 700 AMM 53-00-49-400-801-A17.
Part: ANGLE — CORRODED (PAX DOOR) · airframe 37,680 hrs · 27,589 cycles
CORROSION FOUND ON PASSENGER DOOR DD7A ANGLE P/N 601R317052-1 (C-CHECK RO 8/16/2021) REPLACED PASSENGER DOOR DD7A ANGLEL REF CRJ700 SRM 51-42-21-001-001-A01 DWG# 601R31702 REV-N / C/W TASK CARD 51-900-1002-SKY
Part: ANGLE — CORRODED (PAX DOOR) · airframe 37,680 hrs · 27,589 cycles
* PAX DOOR SURROUND MID- CAP ANGLE HAS CORROSION. (C-CHECK RO 8/16/2021) EVALUATED PAX DOOR MID CAP ANGLE CORROSION AS OUT-OF-LIMITS DUE TO EXFOLIATION WITH 100% MATERIAL LOSS. REMOVED CORRODED PAX DOOR MID CAP ANGLE, AND INSTALLED NEW MID CAP ANGLE. REF. BOMBARDIER DWG SH670-31810 REV. Y., AND CRJ700 SRM 51-41-02-001-001-A01. OPS CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,680 hrs · 27,589 cycles
CORROSION FOUND ON PASSENGER DOOR FWD DD3 INTERCOSTAL P/N 601R318054-1 (C-CHECK RO 8/16/2021) REPLACED PASSENGER DOOR FWD INTERCOSTAL DD3 REF CRJ700 SRM 51-42-06-001-001-A01 DWG# 601R31702 REV-N / C/W TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD
Part: SEAT TRACK — CORRODED (BS 349-485 LBL27) · airframe 37,680 hrs · 27,589 cycles
* LH BL 27 FLOOR SEAT RAILS GOUGED AND CORRODED FROM FS 349 TO FS 485 (C-CHECK RO 8/16/2021) REPLACED LH BL 27 FLOOR SEAT RAIL FROM FS349.00 TO FS485.00 PER CRJ 700 AMM 53-00-49-400-801-A17
Part: SEAT TRACK — GOUGED (BS 349-485 RBL 9) · airframe 37,680 hrs · 27,589 cycles
* RH BL 9 FLOOR SEAT RAILS GOUGED AND CORRODED FROM FS 349 TO FS 485 (C-CHECK RO 8/16/2021) REMOVED & REPLACED FLOOR SEAT TRACKS AT RBL9 FS 349-485 REF. CRJ 700 AMM 53-00-49-400-801-A17 . REPLACED HARDWARE AS REQUIRED
Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 37,680 hrs · 27,589 cycles
* RH FLOOR SILL HAS CORROSION FROM FS 280 TO FS 319 MARKED (C-CHECK RO 8/16/2021) REMOVED AND REPLACED NEW RIGHTHAND CABIN FLOOR SILL BETWEEN FS280.00 TO FS319.00 STRINGER17R IAW CRJ 700 SRM 51-42-06-001-001-A01 / 51-42-21-001-001-A01 / 51-42-13-001-001-A01 AND DRAWING #SH670-32170 REV G. ( SEE CONTINUATION SHEET FOR FURTHER DETAILS) PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: DOOR SILL — CORRODED · airframe 37,680 hrs · 27,589 cycles
* PAX DOOR SILL UPPER ANGLE IS CORRODED AROUND MULTIPLE NUTPLATE HOLES. (C-CHECK RO 8/16/2021) REMOVED AND REPLACED PAX DOOR SILL UPPER ANGLE CRJ700 SRM 51-42-06-001-A01, SRM 51-42-21-001-A01 AND DRAWING # SH670-31810 REV. Y. PRESSURIZATION LEAK CHECK GOOD. SEE CONTINUATION CARD FOR MORE DETAILS.COMPLIED WITH TASK CARD 51-900-1002-SKY AND M-337.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,680 hrs · 27,589 cycles
CORROSION FOUND PASSENGER DOOR DD6 INTERCOSTAL P/N 601R318057-1 (C-CHECK RO 8/16/2021) REPLACED PAX DOOR DD6 INTERCOSTAL 601R318057-1 REF. CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01 AND DWG 601R31702 REV N / C/W TASK CARD 51-900-1002-SKY
Part: INTERCOSTAL — CORRODED (BS 333 S21L) · airframe 37,680 hrs · 27,589 cycles
* INTERCOSTAL 21L AT APPROX. FS 333.00 IS CORRODED. (C-CHECK RO 8/16/2021) REMOVED AND REPLACED INTERCOSTAL IN FWD CABIN BETWEEN FS333.00 TO FS347.00 STRINGER21L IAW CRJ 700 SRM 51-42-06-001-001-A01 / 51-42-21-001-001-A01 AND DRAWING #SH670-31810 REV AE. ( SEE CONTINUATION SHEET FOR FURTHER DETAILS) COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: FLOORBEAM — CORRODED (BS 797 RBL 9) · airframe 37,680 hrs · 27,589 cycles
* FLOORBEAM UPPER FLANGE RBL9 AT APPROX. FS797.00 IS CORRODED. (C-CHECK RO 8/16/2021) REPAIRED FLOORBEAM UPPER FLANGE RBL9 APPROX. FS797.00 REF. REO 670-53-41-538 REV - - DATED 2021-7-15. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
Part: FORMER — CORRODED (PAX DOOR) · airframe 37,680 hrs · 27,589 cycles
CORROSION FOUND ON PASSENGER DOOR FWD FORMER FS311.75 P/N 601R318031-3. (C-CHECK RO 8/16/2021) REMOVED AND INSTALLED NEW PAX DOOR FWD FORMER AT FS311.75 REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND DWG 60131702 REV-N. COMPLIED WITH TASK CARD 51-900-1002-SKY. PRESSURE CHECK GOOD.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,680 hrs · 27,589 cycles
CORROSION FOUND PASSENGER DOOR AFT DD5 INTERCOSTAL P/N: 601R31902-317 (C-CHECK RO 8/16/2021) REMOVED AND INSTALLED NEW PASSENGER DOOR AFT DD5 INTERCOSTAL REF CRJ700 SRM 51-42-06-001-001-A01 DWG# 601R31702 REV-N. COMPLIED WITH TASK CARD 51-900-1002-SKY. PRESSURE CHECK GOOD.
Part: FORMER — CRACKED (PAX DOOR) · airframe 37,680 hrs · 27,589 cycles
CRACK FOUND ON PASSENGER DOOR FS335.00 FORMER P/N 601R318036-7 (C-CHECK RO 8/16/2021) REPLACED THE PASSENGER DOOR FORMER AT FS 335 REF. CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01 ALONG WITH DWG 601R31702 REV N. C/W TASK CARD 51-900-1002-SKY
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,680 hrs · 27,589 cycles
CORROSION FOUND PASSENGER DOOR AFT DD3 INTERCOSTAL P/N 601R318055-1 (C-CHECK RO 8/16/2021) REMOVED AND INSTALLED NEW PASSENGER DOOR AFT DD3 INTERCOSTAL REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG# 601R31702 REV-N. COMPLIED WITH TASK CARD 51-900-1002-SKY. PRESSURE CHECK GOOD.
Part: FLOORBEAM — CORRODED (BS 814 LBL 9) · airframe 37,680 hrs · 27,589 cycles
* FLOORBEAM UPPER FLANGE LBL9 AT APPROX. FS813.70 IS CORRODED. (C-CHECK RO 8/16/2021) BLENDED CORROSION ON FLOORBEAM, UPPER FLANGE AT APPROX. LBL9 FROM FS699.40 - FS855.40 REF. CRJ700 SRM 51-21-06-001-001-A01. EVALUATED BLEND AS OUT-OF-LIMITS. RECIEVED AND COMPLIED WITH ALL STEPS OF MHIRJ REO 670-53-41-537 REV -- DATE: 2021-06-27. RESTORED FINISH. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: DOOR FRAME — CORRODED (BS 328) · airframe 37,680 hrs · 27,589 cycles
CORROSION FOUND PASSENGER DOOR FRAME FS327.763 P/N: 601R318062-3. (C-CHECK RO 8/16/2021) REMOVED AND INSTALLED NEW PAX DOOR FRAME AT FS327.763 REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, AND DWG 601R31702 REV-N. COMPLIED WITH TASK CARD 51-900-1002-SKY. PRESSURE CHECK GOOD.
Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 37,680 hrs · 27,589 cycles
CRACK FOUND ON PASSENGER DOOR FWD DD1 INTERCOSTAL P/N 600-31902-259 (C-CHECK RO 8/16/2021) REMOVED AND INSTALLED NEW FWD DD1 INTERCOSTAL REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG# 601R31702 REV-N. COMPLIED WITH TASK CARD 51-900-1002-SKY. PRESSURE CHECK GOOD.
Part: DOUBLER — CRACKED (PAX DOOR) · airframe 37,680 hrs · 27,589 cycles
CRACK FOUND ON PASSENGER DOOR AFT DOUBLER, PULL IN CAM P/N 601R318094-2 (C-CHECK RO 8/16/2021) REMOVED AND REPLACED PASSENGER DOOR AFT PULL IN CAM DOUBLER REF CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01, DWG#601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 37,680 hrs · 27,589 cycles
CRACK FOUND ON PASSENGER DOOR AFT DD1 INTERCOSTAL P/N 601R31902-318 (C-CHECK RO 8/16/2021) REMOVED AND INSTALLED NEW AFT DD1 INTERCOSTAL REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG# 601R31702 REV-N. COMPLIED WITH TASK CARD 51-900-1002-SKY. PRESSURE CHECK GOOD.
Part: SLAT TRACK — CORRODED (LT WING) · airframe 37,680 hrs · 27,589 cycles
L/H 2-2 SLAT TRACK FWD I/B AND FWD O/B SIDE ROLLERS SHOWS SIGNS OF CORROSION (C-CHECK RO 8/16/2021) REMOVED AND INSTALLED NEW LH 2-2 SLAT TRACK FWD I/B AND FWD O/B SIDE ROLLERS PER CRJ 700 AMM 27-81-44-400-802-A01. ALL CHECKS GOOD.
Part: SLAT TRACK — CORRODED (LT WING) · airframe 37,680 hrs · 27,589 cycles
L/H SLAT TRACK 1-2 AFT I/B AND FWD O/B SIDE ROLLERS SHOWS SIGNS OF CORROSION (C-CHECK RO 8/16/2021) REMOVEDAND INSTALLED NEW SERVICEABLE L/H SLAT TRACK 1-2 AFT I/B AND FWD O/B SIDE ROLLERS REF CRJ 700 AMM 27-81-44-400-801 (CONFIG A01). ALL CHECKS GOOD
Part: SLAT TRACK — CORRODED (LT WING) · airframe 37,680 hrs · 27,589 cycles
L/H SLAT TRACK 3-2 AFT I/B AND FWD O/B SIDE ROLLERS SHOWS SIGNS OF CORROSION (C-CHECK RO 8/16/2021) REMOVED AND REPLACED L/H SLAT TRACK 3-2 AFT I/B AND FWD O/B SIDE ROLLERS PER CRJ 700 AMM 27-81-44-400-803-A01. ALL CHECKS GOOD
Part: STRAP — CRACKED (BS 909 S24L) · airframe 37,680 hrs · 27,589 cycles
LH DIAPHRAGM STRAP IS CRACKED FS 909 STRG 24L LOWER CORNER AS MARKED. (C-CHECK RO 8/16/2021) REPAIRED LEFTHAND DIAPHRAGM STRAP AT FS909.00 STRINGER24L TO COMPLY WITH REO 670-53-82-478 REV -A DATE 2014-11-12 STEPS1-10. ( SEE CONTINUATION SHEET FOR FURTHER DETAILS ) COMPLIED WITH 51-900-1002-SKY.
Part: SKIN — OUT OF LIMITS (LT WING TE FLAP) · airframe 37,680 hrs · 27,589 cycles
THE LH INBD FLAP, THE INBD LOWER SKIN IS OUT OF LIMITS AND REQUIRES REPAIR (C-CHECK RO 8/16/2021) PERFORMED REPAIR ON LH INBD FLAP LOWER SKIN IAW ALL STEPS OF CRJ700 SRM 57-52-01-201-005-A01 SPLICE REPAIR FROM FLS42.00 TO FLS48.00 FIGURE 57-52-01-995-802. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: SKIN — OUT OF LIMITS (RT WING TE FLAP) · airframe 37,680 hrs · 27,589 cycles
THE RH INBD FLAP, THE INBD LOWER SKIN IS OUT OF LIMITS AND REQUIRES REPAIR (C-CHECK RO 8/16/2021) WET INSTALLED NEW -4 EXTERNAL STRAP, -20 INTERNAL STRAP, -30 FILLER, -40 INTERNAL STRAP & -52 LOWER SKIN INSERT ON R/H I/B FLAP I/B LOWER SKIN, REF. CRJ700 SRM 57-52-01-201-005-A01 & COMPLIED WITH SKY CARD 51-900-1002-SKY.
Part: WEB — CORRODED (PAX DOOR) · airframe 37,680 hrs · 27,589 cycles
* PAX DOOR FWD WEB CORRODED ON LOWER OB CORNER (MARKED). (C-CHECK RO 8/16/2021) REMOVED AND REPLACED PAX DOOR FWD WEB WITH NEW REF. CRJ-700 SRM 51-40-11-001-001-A01. PAX DOOR FWD WEB REMOVED AND INSTALLED ON JOB#71018594 OP#15 MX TRANS#22939547.
Part: SLAT TRACK — CHAFED (LT WING) · airframe 37,680 hrs · 27,589 cycles
* LH SLAT TRACK AT THE 1-1 POSITIOIN CHAFED. (C-CHECK RO 8/16/2021) REPAIRED BY COMPLETING WITH ALL STEPS OF REO 670-57-42-1118, REV-- ,DATE 2021-06 -28. DAMAGE FOUND TO BE STRUCTURALLY ACCEPTABLE. COMPLIED WITH TASK CARD 51-900-1002-SKY. ALL CHECKS GOOD.
Part: SLAT TRACK — CHAFED (RT WING) · airframe 37,680 hrs · 27,589 cycles
* RH SLAT TRACK AT THE 1-1 POSITIOIN CHAFED ON BOTTOM SIDE. (C-CHECK RO 8/16/2021) PEFORMED REPAIR ON RH SLAT TRACK AT THE 1-1 IAW ALL STEPS OF REO 670-57-42-1123 REV--, DATED 2021-07-06. COMPLIED WITH TASK CARD 51-900-1002-SKY. OPS TEST GOOD.
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 37,680 hrs · 27,589 cycles
* LH INBD FLAP VANE CHAFED AT APPROXIMATELY WS88 (C-CHECK RO 8/16/2021) REMOVED AND REPLACED LH IB FLAP VANE CAP AT WS88 REF CRJ700 SRM 51-42-13-001-001-A01 & DWG NO: CC670-14010 REV E. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: DRAG ANGLE — CRACKED (VERT TO FUSE) · airframe 37,680 hrs · 27,589 cycles
* RH VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE HAS SUSPECTED CRACK (C-CHECK RO 8/16/2021) INSTALLED NEW RH AFT DRAG ANGLE ON VERTICAL STAB TO FUSELAGE IAW DWG BA670-35002, REV D, REF CRJ700 SRM 51-42-10-001-01-A01, CRJ700 SRM 51-42-21-001-001-A01 AND CRJ700 SRM 51-42-27-001-001-A01
Part: DRAG ANGLE — CRACKED (VERT TO FUSE) · airframe 37,680 hrs · 27,589 cycles
* LH VERTICAL STAB TO FUSELAGE FWD DRAG ANGLE HAS SUSPECTED CRACK (C-CHECK RO 8/16/2021) REPAIRED LEFT-HAND VERTICAL STAB. TO FUSELAGE FWD DRAG ANGLE. REF. REO 670-55-31-018 REV -A DATED 2016-11-10. / SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: DRAG ANGLE — CRACKED (VERT TO FUSE) · airframe 37,680 hrs · 27,589 cycles
* LH VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE HAS SUSPECTED CRACK (C-CHECK RO 8/16/2021) PERFORMED REPAIR PER REO 670-55-31-018 REV - A 2016-11-10. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: BUTTON — STUCK (AUTOPILOT) · airframe 36,918 hrs · 27,068 cycles
CAPTAIN SIDE AUTOPILOT DISENGAGE BUTTON ON YOKE DID NOT DISENGAGE THE AUTOPILOT ON APPROACH. AURAL WARNING FOR DISENGAGEMENT OF AUTOPILOT WAS AUDIBLE, BUT HAD TO GET THE YOKE UNSTUCK. FLIGHT 3294-FILED CLOSED. TROUBLESHOT PER CRJ700FIM 27-32-00-810-801 "ELEVATOR STIFF/HEAVY". REMOVED AND REPLACED ELEVATOR SERVO ACTUATOR WITH SERVICEABLE UNIT, IAW CRJ700AMM 24-11-24. ALL OPERATIONAL CHECKS GOOD. PERFORMED OPERATIONAL CHECK OF AUTOPILOT SYSTEM, IN REF TO CRJ700AMM 22-11-07. ALL OPERATIONAL CHECKS GOOD. PERFORMED OPERATIONAL CHECKS OF AUTOPILOT CONTROL WHEEL DISCONNECT SWITCHES, IN REF TO CRJ700AMM 22-11-00. ALL OPERATIONAL CHECKS GOOD. CAT II RETURN TO SERVICE TASK CARD HAS BEEN LOGGED. TORQUE WRENCH SN 0716807133 CAL DUE DATE 03/21. PLEASE REFERENCE AML 563141.
2019
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 34,902 hrs · 25,507 cycles
LEST WINDSHIELD CRACKED IN FLIGHT. FLIGHT 3289 CLOSED THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 19994297 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED LH WINDSHIELD IAW TASK CARD. OPS CHECK GOOD NO LEAKS NOTED."
2018
Part: FRAME — CRACKED (FUSELAGE) · airframe 32,357 hrs · 23,387 cycles
LT FS235 FRAME HAS AN INDICATION .15" LONG AT THE INBD FASTENER HOLE ABOVE STGR13A. (C-CHECK) 10/20/2018 REMOVED AND REPLACED THE FS 235 FRAME PN CC670-34133-9 IAW AMM. NO LEAKS NOTED AT THIS TIME.
Part: FRAME — CRACKED (FUSELAGE) · airframe 32,357 hrs · 23,387 cycles
RT FS220 FRAME HAS AN INDICATION .1" LONG AT THE 3RD FASTENER HOLE DOWN FROM STGR13A. (C-CHECK) 10/20/2018 REMOVED, DRILLED AND LOCATED, AND INSTALLED THE RT F. S. 220 UPPER FRAME SECTOR IAW SRM. NO LEAKS NOTED AT THIS TIME.
Part: POST — CRACKED (FUSELAGE) · airframe 32,357 hrs · 23,387 cycles
ONE CRACK INDICATION NOTED ON LBL30 POST ON FWD SIDE OF FS202 AT THE TOP OF I-BEAM (AFT WEB-FLANGE INTERSECTION) .400" LONG. (C-CHECK) 10/20/2018 REPAIRED ONE CRACK NOTED ON LBL30 POST ON FWD SIDE OF FS202 AT THE TOP OF I-BEAM (AFT WEB-FLANGE INTERSECTION) .400" LONG IAW SRM. LEAK CHECKS NO DEFECTS NOTED AT THIS TIME.
Part: NOT REPORTED — DENTED (FUSELAGE) · airframe 32,357 hrs · 23,387 cycles
FIVE (5) DENTS FROM FS1162 TO 1181 BETWEEN STR 23L AND 25L. (C-CHECK) 10/20/2018 REPAIRED 5 DENTS FROM FS 1162 TO FS 1181 BETWEEN STR 23L AND 25L IAW REO.
Part: PANEL — GOUGED (NOT REPORTED)
PANELS 443BB AND 443BT ARE GOUGED ON AFT END. REPAIRED PANELS 443BB AND 443BT IAW EC/TC EO CL600-2C-10-54-L05664 AND EO CL600-2C10-54-L05665.
Part: STRAP — CRACKED (FS 909)
JOINT BS 909 AND AFT WING TO FUSELAGE FAIRING STRAP WAS CRACKED. FABRICATED A JOINT AND AFT WING TO FUSELAGE FAIRING STRAP IAW SNIEO CC670-39171 S01.
Part: PANEL — GOUGED (RIGHT NACELLE)
PANELS 443BB AND 443BT ARE GOUGED ON AFT END. REPAIRED PANELS 443BB AND 443BT IAW EXPRESS JET EC/TC`S EO CL600-2C10-54 L05664 AND EO CL6002C10-54-L05565.
Part: SKIN — DAMAGED (BS 1015-1027)
RIGHT EXTERNAL FUSELAGE SKIN SCRATCHED AN GOUGED BETWEEN FS 1015 AND FS 1027, STRINGERS 23R AND 26R. REPAIRED EXTERNAL SKIN IAW STS ENGINEERING SOLUTIONS, ENGINEERING AUTHORIZATION 43-2018-068.
Part: STRINGER — CORRODED (FUSELAGE)
STRINGER 26L, FS 349 TO FS 364 CORRODED BEYOND REPAIRABLE LIMITS. REMOVED AND REPLACED STRINGER 26L, FS 349 TO FS 364 IAW SRM TASKS 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-21-001-001-A01, 51-21-11-001-001-A01, 51-25-01-001-001-A01.
Part: INTERCOSTAL — CORRODED (FUSELAGE)
INTERCOSTAL BETWEEN FS 349 TO FS 364 STRINGER 27L CORRODED ON FLANGE. NO DAMAGE ALLOWED IAW SRM 53-21-23-101-003-A01. REMOVED AND REPLACED INTERCOSTAL 27L BETWEEN FS 349 TO FS 364 IAW SRM TASKS 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-21-001-001-A01.
Part: FRAME — CORRODED (FUSELAGE)
CORROSION ON FRAME AT FS319.70 BETWEEN STRINGER 27 AND 26L. REPAIRED FS 319 IAW REO 670-53-21-799 REV A BY COMPLYING WITH EC/TC REO670-53-21-799 02.
Part: INTERCOSTAL — CORRODED (FUSELAGE)
INTERCOSTAL BETWEEN FS 349 AND FS 364 IS CORRODED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: FRAME — CORRODED (FUSELAGE)
FS 310 FRAME IS CORRODED BETWEEN STRINGERS 25L AND 25R. REPAIRED FRAME STA 310 IAW REO 670-53-21-799 BY COMPLYING WITH EC/TC REO 670-53-21-799-01.
Part: FRAME — CORRODED (FUSELAGE)
FRAME 349 HAS CORROSION BETWEEN STRINGER 27 AND 26R AND BETWEEN 26L AND 25L. REMOVED AND REPLACED FRAME349, PN SH 670-30357-5 IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: INTERCOSTAL — CORRODED (FUSELAGE)
INTERCOSTAL BETWEEN FS 340 - FS 364 STRINGER 26L IS CORRODED ON FLANGE. REMOVED AND REPLACED INTERCOSTAL BETWEEN FS 349 - FS 364 AT STRINGER 26L IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-23-00-001-001-A01, 51-25-16-001-001-A01 AND 51-21-11-001-001-A01.
2017
Part: RELAY — BROKEN (EMERGENCY LIGHTS) · airframe 29,990 hrs · 21,539 cycles
EMERGENCY LIGHTS COME ON WHEN IN THE ARM POSITION. REMOVED AND REPLACED THE RELAY K135 PCB5 (JB11) IAW ESPM 20-39-00, AND AMM 24-06-11, OPS CHECKED GOOD.
2015
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 26,601 hrs · 18,869 cycles
SOME EMERGENCY LIGHT WILL NOT TURN OFF REGARDLESS OF EMERGENCY LIGHT SWITCH IN COCKPIT OR CABIN. AFTER BEING ONBOARD FOR 10 MINTS THEY NOW WOULDN'T STAY ON. MORE THAN 15 SECONDS. CHARGED EMERGENCY LIGHT & PERFORMED OPS CHECK IAW MM 33-51-00, OPS CHECK GOOD AT THIS TIME. ACFT RETURNED TO SERVICE.
Part: FLOOR PANEL — CRACKED (BS 280) · airframe 25,768 hrs · 18,212 cycles
RT COCKPIT FLOOR AT FS280, RBL36, APPROX, WAS FOUND TO BE CRACKED UPON REMOVAL OF RT 280. REPAIRED IAW ECTC EA 32-2015-217.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 25,768 hrs · 18,212 cycles
LEFT COCKPIT FLOORBEAM CRACKED AT LBL 12. REPAIRED IAW ECTC REO 670-53-11-896 AND RERO 670-53-11-896, REV.
Part: STRUCTURE — CORRODED (BS 333) · airframe 25,768 hrs · 18,212 cycles
CORROSION FOUND AT BS 333, RBL 9. REMOVED PACKER IAW 51-42-06-001-001-A01. REPLACED IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-25-126-001-001-A01.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 25,768 hrs · 18,212 cycles
LT BS 280 BULKHEAD WEB CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. REMOVED AND REPLACED THE BULKHEAD WEB IAW SRM 53-11-10-201-003-A01, & DWG CC670-34170.
Part: SLIDER — GOUGED (THRUST REVERSER) · airframe 25,782 hrs · 18,224 cycles
LT UPPER TRANSCOWL INBD & OTBD SLIDERS GOUGED. REMOVED SLIDERS, GOUGED AT LT UPPER INBD AND OTBD SIDES OF TRANSCOWL AND ALL SHARP EDGES AND SMOOTH AREAS IAW SRM 54-21-00-101-001-A01. COMPLIED WITH STS EA 32-2015-222, REV A DATED 6/2/2015, SECTION I PERMANAMET REPAIR. VERIFIED ALL STEPS OF EA 32-2015-222 ARE COMPLETE. COMPLIED WITH ECTC EA 32-2015-222.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 25,768 hrs · 18,212 cycles
RT BS 280, BULKHEAD WEB CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. REMOVED AND REPLACED THE BULKHEAD WEB, IAW SRM 53-11-10-201-003-A01, AND DWG CC67034170.
Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 25,768 hrs · 18,212 cycles
RIGHT SIDE SEAT TRACK BS 581-677 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AND 53-00-49-400-801-A03.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 25,768 hrs · 18,212 cycles
BS 280 FLOORBEAM CORRODED. THE FLOORBEAM WAS R & R IAW SB670BA-53-041.
Part: SEAT TRACK — CORRODED (BS 761-724) · airframe 25,768 hrs · 18,212 cycles
LT SIDE SEAT TRACK BS 761.85-724.08 HAS CORROSION. REPAIRED IAW EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV L.
Part: SEAT TRACK — CORRODED (BS 724-761) · airframe 25,768 hrs · 18,212 cycles
RIGHT SIDE SEAT TRACK BS 724.08-761.85 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED, FABRICATED, AND INSTALLED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AMM 53-00-49-000-801-A03, AND AMM 53-00-49-400-801, A03.
Part: SEAT TRACK — CORRODED (BS 830-953) · airframe 25,768 hrs · 18,212 cycles
SEAT TRACK, RBL 9 BS 830.40 - 953 FOUND CORRODED. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 25,768 hrs · 18,212 cycles
RT SIDE SEAT TRACK BS 485-581 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AND 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 25,768 hrs · 18,212 cycles
LT SIDE SEAT TRACK BS 785.15-863 HAS CORROISON. REPAIRED IAW EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV L.
Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 25,768 hrs · 18,212 cycles
SEAT TRACK, RBL 9, BS 581-677 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AND 53-00-49-400-801-A03.
Part: FRAME — CORRODED (BS 549) · airframe 25,782 hrs · 18,224 cycles
549 FRAME HAS CORROSION BETWEEN STR 18LT AND 19LT, JUST BELOW FLOOR. BLENDED AREA IN FRAME BS 549 BETWEEN STR 18 LT AND 19 LT IAW SRM 51-21-06-001-001-A01. FINISHED REMOVING CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-06-101-002-A01. COMPLIED WITH REO 670-53-31-344 P1 DATED 06/03/2015. VERIFIED STEPS OF REO 670-53-31-344 HAVE BEEN COMPLETED WITH ECTC REO 670-53-31-344.
Part: SEAT TRACK — CORRODED (BS 364-485) · airframe 25,768 hrs · 18,212 cycles
SEAT TRACK AT LBL9 BS 364-485 HAS CORROSION. REPAIRED IAW EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV L.
Part: SEAT TRACK — CORRODED (BS 677-830) · airframe 25,768 hrs · 18,212 cycles
SEAT TRACK RBL 9 BS 677 - 830.40 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AMM 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 25,768 hrs · 18,212 cycles
SEAT TRACK AT LBL 9 BS 581-677 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AND 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 25,768 hrs · 18,212 cycles
SEAT TRACK AT LBL 9 BS 485-581 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, & AMM 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 863-985) · airframe 25,768 hrs · 18,212 cycles
LEFT SIDE SEAT TRACK AT BS 863 - 985 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AND AMM 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 830-953) · airframe 25,768 hrs · 18,212 cycles
LT SIDE SEAT TRACK BS 830.4 - 953 HAS CORROSION. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A01.
Part: FRAME — CORRODED (BS 565) · airframe 25,768 hrs · 18,212 cycles
BS 565 FRAME HAS CORROSION BETWEEN STRINGERS 18 AND 19LT, JUST BELOW FLOOR. REPAIRED IAW SRM 51-42-06-001-001-A01, SRM 53-37-06-101-002-AO1 AND SRM 51-21-16-001-001-AO1.
Part: ANGLE — CORRODED (BS 565) · airframe 25,768 hrs · 18,212 cycles
ANGLE HAS CORROSION THAT ATTACHES TO FRAME BS 565, BETWEEN STRINGERS 18 AND 19 LEFT. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06-0041-001-A01 AND 51-42-22-001-001-A01, SRM 51-42-06-001-001-A01 & SRM 51-42-22-001-001-A01.
Part: FRAME — CORRODED (BS 549) · airframe 25,768 hrs · 18,212 cycles
FRAME BS 549 HAS CORROSION BETWEEN STRS 26L AND 25L, FWD CARGO UNDER FLOOR. REPAIRED IAW SRM 51-21-06-001-001-AO1, 51-31-00-101-003-A01 AND 51-21-16-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 565-677) · airframe 25,768 hrs · 18,212 cycles
LT SIDE SEAT TRACK 565-677 HAS CORROSION. REPAIRED IAW EC/TE REO 670-53-00-343 AND GREO 670-53-00-343, REV L.
Part: SEAT TRACK — CORRODED (BS 785-969) · airframe 25,768 hrs · 18,212 cycles
RT SIDE SEAT TRACK BS 785.15-969 HAS CORROSION. REPLACED IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 25,768 hrs · 18,212 cycles
SEAT TRACK RBL 9 BS 485-581 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AND 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 677-830) · airframe 25,768 hrs · 18,212 cycles
SEAT TRACK AT LBL 9 677-830.4 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, & AMM 53-00-49-400-801-A03.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 25,768 hrs · 18,212 cycles
AFT FLOORBEAM ANGLE AT FS 280, CORRODED. R & R IAW SRM 42-06-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 349-495) · airframe 25,768 hrs · 18,212 cycles
SEAT TRACK, RBL 9, BS 349-495, CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.
Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 25,768 hrs · 18,212 cycles
AVIONICS FLOOR SUPPORT ANGLE CORRODED AT 280.00. R & R AVIONICS FLOOR SUPPORT IAW DWG CC670-34010, REV J, SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-25-06-001-001-A01, 51-25-16-001-A01, 51-21-11-001-001-A01.
Part: SKIN — CHAFED (NOT REPORTED) · airframe 25,768 hrs · 18,212 cycles
PANEL 443BB HAS CHAFE DAMAGE. BLENDED CHAFE DAMAGE TO A SMOOTH CONTOUR ON PANEL 443BB IN REF TO SRM 51-12-00-001-001-A01. BLENDED AREA IS OUT OF ALLOWABLE LIMITS IAW SRM 54-12-01-101-001-A01.
Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 25,768 hrs · 18,212 cycles
SERVICE DOOR EMERGENCY EXIT SIGN HAS CRACKED LENS. REMOVED AND INSTALLED SERVICABLE EMERGENCY EXIT SIGN LENS FOR SERVICE DOOR IAW AMM'S 33-51-05-000-801-A01 AND 33-51-05-400-801-A01.
Part: RIVET — LOOSE (LT WING TE FLAP) · airframe 25,782 hrs · 18,224 cycles
SEVERAL LOOSE RIVETS ON TOPSIDE OF LT OTBD FLAP. COMPLIED WITH EA 32-2015-218, SECTION I, PERMANENT REPAIR ORIGINAL ISSUE DATE 6-2-2015, REV A. VERIFIED ALL STEPS OF EA 32-2015-218, REV A IS COMPLETE. COMPLIED WITH ECTC EA 32-2015-218.
Part: SKIN — DENTED (RT WING SLAT) · airframe 25,782 hrs · 18,224 cycles
DENT FOUND ON RT WING NR 2 SLAT BS 325 JUST INBD SLAT TRACK 2-3. COMPLIED WITH EC/TC EA 32-2015-225 PERMANENT REPAIR REFER TO W/O 368037, N/R 00019. RECEIVED AND VERIFIED ALL STEPS OF EA32-2015-225 ARE DOCUMENTED AND COMPLETE. COMPLIED WITH ECTC EA 32-2015-225. REMOVED INNER SKIN NR 2 SLAT RT WING IAW SRM 51-42-06-001-001-A01 AND 51-42-10-001-001-A01. INSTALLED RIVETS AT ACCESS, OPENS BETWEEN SLAT STATIC 306-75 AND SLAT TRACK 2-3 IAW SRM 51-42-06-001-001A-01 AND DWG CC670-12700. INSTALLED RIVETS, ON RT SLAT INNER SKIN IAW SRM 51-42-06-001-001-A01. INSTALLED RIVETS AND NUTPLATES ON NR 2 RT SLAT INNER SKIN IAW SRM 51-42-06-001-001, SRM 51-42-13-001-001 AND SRM 51-42-15-001-001.
Part: RUB STRIP — DETERIORATED (LT AILERON) · airframe 25,768 hrs · 18,212 cycles
LEFT AILERON RUB STRIP PEELING UP. COMPLIED WITH PERMANENT REPAIR OF LT AILERON RUB STRIP IAW EC/TC REO 670-57-61-006 01. CURE CHECKED GOOD IAW AMM 51-23-00-390-804-A01. COMPLIED WITH ECTC REO 670-57-61-0016-01 AND 670-57-61-006, REV E 09/10/2014, PERMAMEMT REPAIR, AS WRITTEN.
Part: STRUCTURE — DENTED (FWD CARGO DOOR) · airframe 25,768 hrs · 18,212 cycles
FWD CARGO DOOR DENTED AT BOTTOM CENTER EDGE. REPAIRED IAW EC/TC EA 32-2015-226.
Part: LIGHT — MISSING (CABIN) · airframe 25,425 hrs · 17,941 cycles
PHOTO LUMINESCENT STRIP MISSING FWD AND AFT OF SERVICE DOOR. REPLACED PHOTO LUMINESCENT STRIP AROUND SERVICE DOOR IAW AMM 33-50-00.
2014
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 24,318 hrs · 17,105 cycles
EMERGENCY LIGHTS "ON" WITH FLT DECK AND CABIN SWITCHES IN ARM POSITIONS, RESPECTIVELY AND OFF. RACKED PCB5 CARD ON JB11. EMERGENCY LIGHTS OPS CHECKED GOOD IAW AMM 33-50-00. ACFT OK FOR SERVICE.
Part: LIGHT — MISSING (CABIN) · airframe 23,363 hrs · 16,381 cycles
EMERGENCY LIGHT MISSING FROM LOWER LT AREA AT SERVICE DOOR, R & R EMERGENCY LIGHT IAW AMM 11-30-03. NO FURTHER DEFECT NOTED. ACFT OK FOR SERVICE.
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 22,987 hrs · 16,106 cycles
MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,890 hrs · 16,039 cycles
RIGHT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS IAW AMM 33-51-15, OPS CHECKED GOOD.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,890 hrs · 16,039 cycles
NR 5 INTERIOR CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED LAMPS IAW AMM 33-51-09, OPS CHECKED GOOD.
2013
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,137 hrs · 15,504 cycles
LEFT OVERWING EMERGENCY EXIT LOWER EXIT LIGHT HAS SEVERAL BULBS INOPERATIVE. REPLACED BULBS. OPS CHECKED GOOD.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 21,506 hrs · 15,033 cycles
SERVICE DOOR FWD EMERGENCY LIGHT HAS SEVERAL INOPERATIVE BULBS. 07-22-2013 RELAMPED SERVICE DOOR FWD EMERGENCY LIGHT IAW AMM 33-51-19, OP'S CHECKED GOOD.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 21,431 hrs · 14,978 cycles
RT LOWER COCKPIT BULKHEAD REAR WEB CORRODED AT BS 280. REPAIRED RT LOWER WEB IAW GREO 670-53-11-594, REV, AND EC/TC REO 670-53-11-594 01, REV A.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 21,431 hrs · 14,978 cycles
LT LOWER COCKPIT BULKHEAD REAR WEB CORRODED AT BS 280. REPAIRED LT LOWER WEB IAW GREO 670-53-11-594 REV, AND EC/TC REO 670-53-11-594, REV A.
Part: STIFFENER — CRACKED (BS 280) · airframe 21,431 hrs · 14,978 cycles
STIFFENER BEHIND BS 280 FLOORBEAM WEB CRACKED. R & R STIFFENER IAW SRM 51-42-10.
Part: STRINGER — CORRODED (BS 340) · airframe 21,431 hrs · 14,978 cycles
STRINGER 26R AT BS 340 HAS CORROSION AROUND FASTENERS. R & R STRINGER 26R IAW REO 670-53-21-966 AND SRM 51-42-06, 51-24-36, 51-25-06 AND 51-25-21.
Part: SEAT TRACK — CORRODED (BS 675-713) · airframe 21,431 hrs · 14,978 cycles
SEAT TRACK BS 675 -713 HAS SIGNS OF CORROSION. REPLACED LT SIDE SEAT TRACK BS 675-713 IAW AMM 53-00-49.
Part: SEAT TRACK — CORRODED (BS 374-485) · airframe 21,431 hrs · 14,978 cycles
SEAT TRACK BS 374 -485 HAS SIGNS OF CORROSION. REPLACED SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.
Part: INTERCOSTAL — CORRODED (DOOR FRAME) · airframe 21,431 hrs · 14,978 cycles
INTERCOSTAL FWD OF AVIONICS DOOR SURROUND (RT OF CENTER LINE) HAS CORROSION. R & R INTERCOSTAL IAW AMM 52-70-08, 52-42-00-710-801 AND SRM 51-42-06, 51-40-11, 51-42-21, AND 51-25-16.
Part: SEAT TRACK — CORRODED (BS 724) · airframe 21,431 hrs · 14,978 cycles
SEAT TRACK CORRODED AT BS 724.08. R & R RT SEAT TRACK IAW AMM 53-00-49.
Part: SKIN — WORN (LT AILERON) · airframe 21,431 hrs · 14,978 cycles
FOUND WEAR ON LT AILERON UPPER L/E SKIN TO BE WORN OUT OF LIMITS ESTABLISHED IN SRM 57-61-01. R & R SKIN IAW SRM 51-42-21, 51-42-06 AND 51-40-11.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,431 hrs · 14,978 cycles
BS 280 FLOORBEAM CORRODED. REPLACED IAW SRM 51-42-10, 51-42-06, AND 51-42-21, SRM 53-11-41, SRM 51-40-11, SRM 51-21-11, SRM 51-21-16.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,431 hrs · 14,978 cycles
RT BS 280 FLOORBEAM WEB CORRODED. COMPLIED WITH EC/TC REO 670-53-11-594 01 AND GREO 670-53-11-594 REV, DATED 04/27/2011.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,431 hrs · 14,978 cycles
BS 280 FLOORBEAM CORRODED. REPLACED IAW SRM 51-40-11, 51-42-06, 51-21-16, 51-21-11.
Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 21,431 hrs · 14,978 cycles
RT FLOOR SUPPORT AT FS 280.00 CORRODED. R & R FLOOR SUPPORT IAW SRM 51-42-13.
Part: BULKHEAD — CORRODED (BS 279) · airframe 21,431 hrs · 14,978 cycles
CORROSION ON BS 279 RT INNER BULKHEAD PANEL. REPAIRED BULKHEAD IAW REO 670-53-11-842.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,431 hrs · 14,978 cycles
FS 280 FLOORBEAM CORRODED. REPLACED FLOORBEAM IAW SRM 51-42-06, 51-42-10 AND 51-42-21.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,431 hrs · 14,978 cycles
FS 280 FLOORBEAM LT WEB CORRODED. COMPLIED WITH EC/TC REO 670-53-11-594 AND GREO 670-53-11-594, DATED 04-27-2011.
Part: SEAT TRACK — CORRODED (BS 349) · airframe 21,431 hrs · 14,978 cycles
SEAT TRACK AT BS 349 CORRODED. REPLACED SEAT TRACK IAW AMM 53-00-49.
Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 20,407 hrs · 14,234 cycles
FWD F/A FLASHLIGHT INOPERATIVE. R & R FORWARD FLASHLIGHT BATTERIES IAW AMM 25-61-00-710-801. OPS CHECKED GOOD. ACFT RETURN TO SERVICE.
2012
Part: SOCKET — BROKEN (EMERGENCY LIGHT) · airframe 19,247 hrs · 13,391 cycles
PAX DOOR FLOOR EMERGENCY FLOODLIGHT HAS MISSING COVER AND BROKEN LIGHT SOCKET. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHT ON WARDROBE IAW AMM 33-51-11. OPS CHECK GOOD. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHT ON WARDROBE IAW AMM 33-51-11. OPS CHECK GOOD. SDR CLOSED.
Part: GLOWSTRIP — DETERIORATED · airframe 18,614 hrs · 12,910 cycles
RT SIDE FWD OF EMERGENCY EXIT PHOTOLLUMINESCENT DAMAGED. R & R THE DAMAGED SECTION OF PHOTOLUMINESCENT IAW AMM 33-51-01. OPS CHECKED GOOD.
Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 18,522 hrs · 12,835 cycles
RT SIDE AFTMOST EMERGENCY LIGHT LENS COVER IS CRACKED. R & R EMERGENCY LIGHT LENS COVER IAW AMM 33-51-15. NO FURTHER DEFECTS NOTED.
Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 18,415 hrs · 12,760 cycles
EMERGENCY LIGHT LENS COVER AFT OF LT WING, CRACKED. R & R LENS IAW 33-51-01.
2011
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,002 hrs · 12,462 cycles
NR 3 CABIN CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED NR 3 CABIN CEILING LIGHT IAW AMM 33-51-09. OPS CHECKED GOOD.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,002 hrs · 12,462 cycles
EMERGENCY EXIT FLOOR FLOOD LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM 33-51-11. OPS CHECKED GOOD.
Part: WIRE — DAMAGED (EMERGENCY LGIHTS) · airframe 16,901 hrs · 11,718 cycles
RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRING IAW ESPM 20-24-00. OPS CHECKED GOOD.
Part: WIRE HARNESS — MISWIRED (EMERGENCY LIGHT) · airframe 16,901 hrs · 11,718 cycles
RT OVERWING EMERGENCY LIGHT. REPAIRED WIRING AT SIDEWALL 12C AND 12D IAW ESPM 20-24-00. OPS CHECK OF EMERGENCY LIGHTING TEST, OPS CHECKED GOOD. DEFER CLEARED, PLACARD REMOVED.
Part: INTERCOSTAL — CORRODED (BS 346) · airframe 16,575 hrs · 11,510 cycles
BOTH INTERCOSTALS AT FS 364.00 AND STR 27 CORRODED. REMOVED INTERCOSTAL, DRILLED NEW INTERCOSTAL & INSTALLED IAW SRM 51-42-06-001-001.
Part: CROSSBEAM — CORRODED (BS 280) · airframe 16,575 hrs · 11,510 cycles
FS 280 CROSSBEAM CORRODED. REMOVED AND REPLACED IAW REO 670-53-11-047.
Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 16,575 hrs · 11,510 cycles
FLOOR PANEL, 141ALF FWD "SUPPORT ANGLE" WHICH IS MOUNTED TO THE FS 280 FRAME IS CORRODED. R & R CORRODED ANGLE UNDER FLOOR PANEL 141ALF ATTACHED TO AFT SIDE OF 280 FRAME IAW SRM 51-42-06-001-001 AND 51-42-21-001-001. THIS IS A MINOR REPAIR.
Part: WEB — CORRODED (BS 280) · airframe 16,575 hrs · 11,510 cycles
FS 280, LEFT WEB CORRODED. REMOVED CORROSION ORIGINAL THICKNESS =.035" MATERIAL REMOVED =.0045" DEEP X18"X.75". REMAINING MATERIAL THICKNESS = .0305" WITHIN ALLOWABLE LIMITS.
Part: ATTACH FITTING — CORRODED (BS 321) · airframe 16,575 hrs · 11,510 cycles
(2 EA) CLIPS CORRODED INSIDE ASD AT FS 321 AT HINGE AREA. R & R (1 EA) CLIPS INSIDE ASD AT FS.321 AT HINGE AREA IAW SRM 51-42-06-001-001. THIS IS A MINOR REPAIR.
Part: WEB — CORRODED (BS 280) · airframe 16,575 hrs · 11,510 cycles
FS 280, RIGHT WEB CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. ORIGINAL MAT THICKNESS OF WEB .040 MAX MAT. REMOVED .012 MAT REMAINING .028 WEB IS OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. R & R L WEB IAW 53-11-10-201-003-A01.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 16,817 hrs · 11,668 cycles
ASD ASSIST MOTOR FWD STIFFNER CRACKED. R & R ASD ASSIST MOTOR FWD STIFFENER IAW SRM 51-42-06-001-001. THIS IS A MINOR REPAIR.
Part: CROSSBEAM — CORRODED (BS 280) · airframe 16,575 hrs · 11,510 cycles
FS 280, CROSSBEAM CORRODED. REMOVED CROSSBEAM IAW REO 670-53-11-047. CUT CROSSBEAM IAW REO 670-53-11-047, STEP 1, 3, & PART OF STEP 4. NDT IAW STEP 2 OF REO 670-53-11-047. COMPLIED WITH STEP 2 OF REO 670-53-11-047 NDRM PART 1, 51-20-006 NO INDICATIONS NOTED AT THIS TIME. ISTALLED CROSSBEAM IAW REO 670-53-11-047.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 16,575 hrs · 11,510 cycles
REMOVE COCKPIT FLOORBEAM FROM FS280 FLOOR SUPPORT BEAM. REMOVED COCKPIT FLOORBEAM IAW SRM 51-42-06-001-001 AND 51-42-21-001-001. INSTALLED SERVICEABLE COCKPIT FLOOR SUPPORT PN CC670-33292-13 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01.
Part: HINGE FITTING — CORRODED (BS 339.75) · airframe 16,575 hrs · 11,510 cycles
TWO CLIPS CORRODED INSIDE ASD AT FS 339.75 ON HINGE SIDE. REMOVED CLIPS IAW SRM 51-42-06-001-001. INSTALLED NEW CLIPS IN ASD AT FS 339.75 IAW SRM 51-42-06-001-001.
Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 16,575 hrs · 11,510 cycles
SEAT TRACK SEGMENT FROM FS 581.00-677.00 HAS CORROSION. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-319. REMOVED OLD SEAT TRACK AND INSTALLED NEW SEGMENT IAW AMM 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 790) · airframe 16,575 hrs · 11,510 cycles
SEAT TRACK AT FS 790.00 HAS CORROSION. REMOVED SEAT TRACK IAW AMM 53-00-49-00-801-A03. FABRICATED NEW TRACK IAW REO 670-53-00-319. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-00-801-A03.
Part: SEAT TRACK — CORRODED (BS 724.08) · airframe 16,575 hrs · 11,510 cycles
SEAT TRACK AT FS 724.08 HAS CORROSION. REMOVED SEAT TRACK SEGMENT IAW AMM 53-00-49-00-801-A03. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-319. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 597-677) · airframe 16,575 hrs · 11,510 cycles
SEAT TRACK SEGMENT AT FS 597.00-677.00 CORRODED BEYOND REPAIR. REMOVED SEAT TRACK SEGMENT IAW AMM 53-00-49-00-801-A03. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-319. INSTALLED SERVICABLE SEAT TRACK IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 863-977) · airframe 16,575 hrs · 11,510 cycles
RIGHT SEAT TRACK CORRODED FROM FS 863.00-977.00. REMOVED SEAT TRACK IAW AMM 53-00-40-000-801. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-319. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 581-669) · airframe 16,575 hrs · 11,510 cycles
LEFT SIDE SEAT TRACK CORRODED FROM FS 581.00-669.00. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-319. INSTALLED NEW SERVICABLE SIDEWALL SEAT TRACK IAW AMM 53-00-49.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 16,684 hrs · 11,584 cycles
CRACK ON FLOOR IN LT FWD EQUIPMENT COMPARTMENT ADJACENT TO BRAKE ACCUMULATOR GAUGES. PERFORMED EDDY CURRENT INSP OF CUTLINE AND UNDERLYING STRUCTURE IAW REO 670-53-11-509 NDTM PART 1. NO INDICATIONS NOTED AT THIS TIME.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 16,575 hrs · 11,510 cycles
RIGHT SEAT TRACK IS CORRODED FROM FS 485.00-581.00. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-319. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 16,575 hrs · 11,510 cycles
RIGHT SEAT TRACK CORRODED FROM FS 785.00-863.00. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-319. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 16,575 hrs · 11,510 cycles
LEFT SEAT TRACK CORRODED FROM FS 485.00-581.00. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-319. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 669-708) · airframe 16,575 hrs · 11,510 cycles
RIGHT SEAT TRACK CORRODED FROM FS 669.00-708.00. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-319. INSTALLED SEAT TRACK IAW AMM TASK 53-00-49-400-801-A03.
Part: FLOOR PANEL — CRACKED · airframe 17,390 hrs · 12,053 cycles
CRACK ON FLOOR IN RT FWD EQUIPMENT BAY ADJACENT TO ADG PUMP. COMPLY WITH ECTC REO 670-53-11-509. COMPLIED WITH ECTC REO 670-53-11-509 AND GENERIC REO 670-53-11-809.
Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 16,575 hrs · 11,510 cycles
RIGHT SEAT TRACK CORRODED FROM FS 708.00-761.00. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED SEAT TRACK IAW REO 670-53-00-319. INSTALLED NEW SERVICABLE SEAT TRACK IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 16,575 hrs · 11,510 cycles
LEFT SEAT TRACK CORRODED FROM FS 785.00-863.00. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-319. INSTALLED NEW SERVICABLE SEAT TRACK IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 863-977) · airframe 16,575 hrs · 11,510 cycles
LEFT SEAT TRACK CORRODED FROM FS 863.00-977.00. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-319. INSTALLED NEW SEAT TRACK.
Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 16,575 hrs · 11,510 cycles
LEFT SEAT TRACK CORRODED FROM FS 708.00-761.00. REMOVED AND FABRICATED SEAT TRACK IAW REO 670-53-00-319. INSTALLED SERVICABLE SEAT TRACK IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 581-669) · airframe 16,575 hrs · 11,510 cycles
RIGHT SEAT TRACK CORRODED FROM FS 581.00-669.00. REMOVED SEAT TRACK IAW AMM 53-00-49-00-801-A03. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-319 INSTALLED SERVICABLE SEAT TRACK IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 669-708) · airframe 16,575 hrs · 11,510 cycles
LEFT SEAT TRACK CORRODED FROM FS 669.00-708.00. REMOVED AND FABRICATED SEAT TRACK IAW REO 670-53-00-319, AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM TASK 53-00-49-400-801-A03.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 16,575 hrs · 11,510 cycles
AFT DRAG ANGLE CRACKED ON AIRSTAIR DOOR. FABRICATED NEW DRAG ANGLE IAW SRM 51-42-06-001-001. INSTALLED DRAG ANGLE IAW SRM 51-42-13-001-001.
2009
Part: ANTI-ICE SYSTEM — MALFUNCTIONED (WING) · airframe 13,017 hrs · 8,933 cycles
DURING FLIGHT LEVEL 270 IN ICING CONDITIONS WING ANTI-ICE DUCT WARNING RED MESSAGE FOLLOWED QRH IAW TURNED OFF WING ANTI-ICE AND DIVERTED. (EMERGENCY DECLARED -- ENROUTE, ACFT DIVERTED DUE TO MX)
Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,874 hrs · 8,832 cycles
AT ROW 14CD THE LWR EMERGENCY EXIT SIGN HAS MULTIPLE LIGHTS INOP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,565 hrs · 8,593 cycles
FWD EMERGENCY EXIT LIGHT ARE INOP.
Part: UNKNOWN — SMOKE (CABIN) · airframe 12,248 hrs · 8,365 cycles
FLT 5377, DURING TAXI NR 2 ENG ONLY, NO APU, CABIN BEGAN FILLING WITH SMOKE. EVACUATED ALL PAX, NO INJURIES. AIRPORT FIRE DEPT DETECTED "HOT SPOT" AT ROW 6 ON CEILING AB SIDE OF CABIN. EMERGENCY DECLARED -- GATE RETURN.
Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 12,241 hrs · 8,360 cycles
EMERGENCY LIGHT COVER AT GALLEY SERVICE DOOR MISSING
Part: LIGHT — CRACKED (CABIN) · airframe 11,578 hrs · 7,851 cycles
LT EMERGENCY FLOOR PATH LIGHTING ASSY IS CRACKED AT FWD END. REMOVED BROKEN E-LIGHT ASSY PER 33-51-01. INSTALLED LT FWD END EMERGENCY FLOOR PATH LIGHT ASSY PER MM 33-51-01.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 11,578 hrs · 7,851 cycles
FS 280 FLOOR SUPPORT CROSSBEAM CORRODED AT LBL9 AND RBL9. ALL WORK DONE IAW REO 670-53-11-047.
Part: BULKHEAD — CORRODED (BS 280) · airframe 11,578 hrs · 7,851 cycles
LT LWR FS 280 BULKHEAD WEB CORRODED. WORK DONE IAW SRM 53-11-10-201-003.
Part: FAIRING — CRACKED (FUSELAGE) · airframe 11,578 hrs · 7,851 cycles
RT L/E TRANS FAIRING IS CRACKED PN CC670-15356-2. REMOVED UNSERVICEABLE RT TRANS FAIRING. LOCATED SERVICEABLE TRANS FAIRING P/N CC670-15356-2 IAW SRM 51-40-11.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 11,578 hrs · 7,851 cycles
FLT DECK FLOOR SUPPORT ANGLE AT FS 280 CORRODED. REMOVED FLT DECK FLOOR SUPPORT ANGLE IAW SRM 51-42-21. INSTALLED FLT DECK SUPPORT ANGLE IAW SRM 51-42-06, 51-42-21.
Part: BULKHEAD — CORRODED (BS 280) · airframe 11,578 hrs · 7,851 cycles
RT LWR FS 280 BULKHEAD WEB CORRODED. WORK ACCOMPLISHED IAW SRM 53-11-10-201-003.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,209 hrs · 7,555 cycles
RT OVERWING EMERGENCY EXIT LOWER EMERGENCY LIGHT HAS SEVERAL INOP BULBS.
Part: CHARGER — FAILED (CABIN) · airframe 11,060 hrs · 7,438 cycles
EMERGENCY LIGHT BATTERY CHARGER NR 2 FAILED.
2008
Part: MECHANISM — BINDING (PAX DOOR) · airframe 10,790 hrs · 7,243 cycles
F/A REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE AND FEELS AS THOUGH LOCKING MECHANISM IS BINDING.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,585 hrs · 6,350 cycles
EMERGENCY LIGHTS INOPERATIVE. RESET SYSTEM OPS OK PER 33-51-01. (S)
Part: UNKNOWN — MALFUNCTIONED (HYDRAULIC SYS) · airframe 9,350 hrs · 6,188 cycles
HYD NR 3 HI TEMP FOLLOWED BY HYD NR 3 LO PRESS. QRH COMPLIED WITH. HYD NR 3 PRESS RETURNED TO NORMAL WHEN GEAR EXTENDED ON FINAL APPROACH. TOWER DECLARED AN EMERGENCY TRUCKS ROLLED. REMOVED AND REPLACED PRESSURE MANIFOLD ON HYD NR 3 IAW CRJ-700 AMM 29-10-01. NO HELP. NEEDS MORE TROUBLESHOOTING. [SDR CLOSED](B)
Part: PLACARD — PEELING (CABIN) · airframe 9,350 hrs · 6,188 cycles
EMERGENCY MEDICAL KIT PLACARD PEELING REMOVED AND REPLACED EMERGENCY MEDICAL KIT PLACARD IAW AMM 11-30-02. (B)
Part: STEP — CRACKED (AIRSTAIR DOOR) · airframe 8,253 hrs · 5,417 cycles
ASD LOWER STEP CRACKED.
2007
Part: GLOWSTRIP — MISSING (CABIN) · airframe 8,192 hrs · 5,372 cycles
PHOTO LUMINESCENT TAPE MISSING NEAR GALLEY CART STORAGE AREA.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,497 hrs · 4,914 cycles
CEILING EMERGENCY LIGHT THIRD FROM FRONT INOP.
Part: WEB — CORRODED (FUSELAGE) · airframe 7,204 hrs · 4,713 cycles
RIGHT LOWER FS 280 WEB HAS CORROSION. REMOVED LITE SURFACE CORROSION, .0035 INCH DEEP IAW CRJ SRM 51-21-06. RIGHT LOWER FS 280 WEB AREA UNDER BEAM (BLENDED AREA) IS WITHIN SERVICEABLE LIMITS IAW REO 67053-11-052. OK TO ALODINE AND PRIME BARE METAL. ALODINED AND PRIMED BARE METAL ON THE RIGHT LOWER FS 280 WEB IAW CRJ SRM 51-21-11 AND 51-25-06. OK TO PAINT. PAINTED IAW CRJ SRM 51-25-16. SUPPLEMENTAL - SDR CLOSED 08/14/07.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,204 hrs · 4,713 cycles
LEFT SIDE SEAT RAIL HAS CORROSION IN ONE PLACE AFT OF EMERGENCY DOOR (MARKED IN RED).
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 7,204 hrs · 4,713 cycles
LEFT FS 280 CROSSBEAM CRACKED ON UPPER FLANGE O/B OF LBL 9.0. REMOVED LEFT FS 280 DAMAGED BEAM. LOCATED NEW LEFT FS 280 FLOORBEAM, P/N CC670-304175-7, IAW CRJ SRM 51-42-21. OK TO INSTALL. INSTALLED LEFT FS 280 BEAM, IAW CRJ SRM 51-42-06 AND 51-42-21. OK TO TOPCOAT. PAINTED, IAW CRJ SRM 51-25-16. SUPPLEMENTAL - SDR CLOSED 08/14/07.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,204 hrs · 4,713 cycles
RIGHT SIDE SEAT RAIL HAS CORROSION IN TWO PLACES AFT OF EMERGENCY DOOR (MARKED IN RED).
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 7,204 hrs · 4,713 cycles
RIGHT FS 280 CROSSBEAM CRACKED ON UPPER FLANGE O/B OF RBL 9.0. REMOVED RIGHT FS 280 DAMAGED BEAM. LOCATED NEW RIGHT, FS 280 FLOORBEAM, P/N CC670-34175-7, IAW CRJ 700 SRM 51-40-11. OK TO INSTALL. INSTALLED RIGHT FS 280 BEAM, IAW CRJ SRM 51-42-06 AND 51-42-21. OKAY TO TOPCOAT PAINTED IAW CRJ SRM 51-25-16. SUPPLEMENTAL - SDR CLOSED 08/14/07.
Part: WEB — CORRODED (FUSELAGE) · airframe 7,204 hrs · 4,713 cycles
LEFT LOWER FS 280 WEB HAS CORROSION. REMOVED LITE SURFACE CORROSION .004" DEEP IAW CRJ SRM 51-21-06. LEFT LOWER FS 280 WEB AREA UNDER BEAM (BLENDED AREA) IS WITHIN SERVICEABLE LIMITS IAW REO 670-53-11-052. OK TO ALODINE AND PRIME BARE METAL. ALODINED AND PRIMED BARE METAL ON THE LT LOWER FS 280 WEB, IAW CRJ SRM 51-21-11 AND 51-25-06. OKAY TO PAINT. PAINTED IAW CRJ SRM 51-25-16. SUPPLEMENTAL - SDR CLOSED 08/14/07.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,204 hrs · 4,713 cycles
PAX DOOR AFT DRAG ANGLE AND PULLEY CRACKED.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 7,204 hrs · 4,713 cycles
FS 280 FWD CENTER FLOOR SUPPORT ANGLE CORRODED.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 6,325 hrs · 4,136 cycles
F/O`S FLASHLIGHT INOP.
Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 6,308 hrs · 4,123 cycles
CAPT'S FLASHLIGHT INOP.
Part: UNKNOWN — SMOKE (CABIN) · airframe 5,885 hrs · 3,838 cycles
AFTER TAKEOFF FROM MCN CABIN FILLED WITH BURNING OIL SMELL AND HAZE. FWD LAV SMOKE CAME ON. CABIN CLEARED OF SMELL. WHEN POWER REDUCED TO DESCEND INTO ATL, SMOKE CAME BACK, WENT AWAY ON APU BLEED. EMERGENCY DECLARED.
2006
Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,635 hrs · 3,030 cycles
AFT CEILING 1EA EMERGENGY LIGHT INOP.
Part: DOOR — MALFUNCTIONED (CABIN) · airframe 3,974 hrs · 2,626 cycles
PAX DOOR WILL NOT OPEN, CABLE OFF PULLY.
Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 3,889 hrs · 2,567 cycles
PILOTS FLASHLIGHT INOP. REPLACED PILOTS FLASHLIGHT IAW M/M 25-60. (CLOSED)
Part: SIGN — MISSING (CABIN)
DURING A GROUND INSPECTION IN ATL, THE EXIT SIGN, ON THE PASSENGER DOOR, WAS FOUND MISSING. MAINTENANCE REPLACED THE EXIT SIGN, ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
2005
Part: STEP — CRACKED (PAX DOOR)
DURING AN A-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR IAW CRJ700 MM 52-00. OPERATIONAL CHECKS GOOD. (M)
Part: STEP — CRACKED (PAX DOOR)
DURING AN A-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ASSEMBLY ON THE PASSENGER DOOR. (M)