N741EV
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
STRONG BURNT PLASTIC SMELL ROWS 11-15 IN THE BACK OF THE CABIN (FLIGHT 6337) TROUBLESHOT STRONG BURNT PLASTIC SMELL ROWS 11-15 IN THE BACK OF THE CABIN, IAW FIM 21-22-00-810-806, IT WAS DISCOVERED THAT THE NR 2 HYD SYSTEM RESERVOIR HAD BEEN LEAKING HYD FLUID ALL OVER THE AFT EQUIPMENT BAY INCLUDING THE PACK DUCTS. SEE CP 32510369 FOR WORK COMPLETED AND PARTS REPLACEMENT. NO ABNORMAL SMELLS PRESENT AT THIS TIME.
LOSS OF CABIN PRESSURE AT F200. EMERGENCY DESCENT. MASKS DEPLOYED. CREW OXYGEN MASKS USED (FLIGHT 6269 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 29962820 WITH THE FOLLOWING CORRECTIVE ACTION: "CARRIED FORWARD FOR RESCHEDULING. NOT SCHEDULED FOR THIS MX BASE."
TRANSFER FROM EAML 1512385 : FO RIGHT SIDE WINDOW SHATTERED (SPIDER WEB) DURING TAXI IN (FLIGHT 6500) REMOVED AND REPLACED RH WINDOW IN REF. TO AMM 56-12-01. INSTALLED UP TO STEP 28 IN AMM 56-12-01. FINAL TORQUE HAS BEEN COMPLIED WITH ON SIDE WINDOW. SIDE POST STILL NEEDS INSTALLATION.
TRANSFER FROM EAML 1512385 : FO RIGHT SIDE WINDOW SHATTERED (SPIDER WEB) DURING TAXI IN (FLIGHT 6500 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
INTERCOSTAL FWD OF AVIONICS DOOR LEFT OF STGR27 HAS SIGNS OF CORROSION ON INBD WEB (C-CHECK RO 10/6/2024) (FILED CLOSED)REMOVED AND REPLACED INNER COSTAL FWD AVIONICS DOOR AT STGR 27 IB WEB IAW CRJ700 SRM 51-42-06, 51-42-21, 51-40-11, 51-21-11, 51-25-06, 51-42-13, 51-25-16, 51-41-02, 53-21-23, AMM 52-70-08, 52-42-00, 21-31-00.
SIGNS OF CORROSION FOUND UNDER RAM AIR FAIRING ON FUSELAGE FASTENERS BETWEEN FS1144.00-1162.00 BETWEEN STR 0-1L (C-CHECK RO 10/6/2024) (FILED CLOSED)INSTALLED EWIS PROTECTION ABOVE AND BELOW RAM AIR FAIRING IAW CRJ700 AMM 20-70-00. REMOVED FASTENERS BETWEEN FS. 1144.00 AND FS. 1162.00 STR-0 AND STR-1L IAW CRJ700 SRM 51-42-06. EVALUATED CORROSION NO DAMAGE ALLOWED IN AREA IAW CRJ700 SRM 53-61-01. REMOVED CORROSION IAW CRJ700 SRM 51-21-06. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D REPORT# S090924-7 P.O.# 173562 DATE OF INSPECTION 09SEP2024. NO DEFECTS NOTED AT TIME OF INSPECTION. SEE REPORT FOR DETAILS. APPLIED ALODINE PRIMER AND INSTALLED FASTENERS IAW REO 670-53-61-2364 REV.-- AND SRM 51-21-11,51-25-06.
RBL9 FLOOR BEAM HAS SIGNS OF CORROSION AT FS581. EVALUATED CORROSION AT RBL9 FS. 581.FOUND TO BE WITHIN LIMITS IAW REO 670-53-31-921 AND AMM 53-00-49. APPLIED ALODINE, PRIMER AND TOPCOAT IAW CRJ700 SRM 51-21-11, SRM 51-25-06 AND SRM 51-25-16. REINSTALLED SEAT TRACK AT RBL 9 FS.565 RO FS. 677 IAW CRJ700 SRM 51-41-02. APPLIED CIC IAW SRM 51-21-11.
LH SIDE SEAT RAIL HAS SIGNS OF CORROSION FROM FS909.00 - FS911.00 (C-CHECK RO 10/6/2024) (FILED CLOSED)REPAIRED DAMAGE AT LH SIDE SEAT RAIL FROM FS909.00-FS911.00 IAW CRJ700 SRM 53-51-49CAL TOOL DEPTH GAUGE AV7277 DUE-AUG2024
LH FLOOR SEAT TRACK (LBL9) HAS SIGNS OF CORROSION AT FS517-FS553.00. (C-CHECK RO 10/6/2024) (FILED CLOSED)EVALUATED LH FLOOR SEAT TRACK (LBL9) BETWEEN AT FS 517.00 TO FS 553.00 AND DAMAGE WAS FOUND 80% OF THE MATERIAL THEREFORE IT IS OUT LIMITS IAW CRJ 700 SRM 53-31-49REMOVED AND REPLACED LH FLOOR SEAT TRACK (LBL9) BETWEEN FS 469.00 TO FS 565.00 IAW CRJ 700 AMM 53-00-49CALIBRATED TOOL: TORQUE DRIVE AV-BX100 DUE 31-JAN-25
LH SIDE SEAT RAIL HAS SIGNS OF CORROSION FROM FS708.00 - FS761.85 (C-CHECK RO 10/6/2024) (FILED CLOSED)OK TO INSTAL BJ910267REMOVED AND REPLACED LH SIDE SEAT RAIL FS708.00 - FS 761.85 IAW CRJ 700 AMM 53-41-49, CRJ700 AMM 53-00-49P/N- SH670-37509-1 S/N- UNKCAL TOOL: TORQUE DRIVER AVBX100 CAL DUE 1/2025
LH SIDE SEAT RAIL HAS SIGNS OF CORROSION FROM FS677.00 TO FS708.00 (C-CHECK RO 10/6/2024) (FILED CLOSED)EVALED AND FOUND TO BE OUT OF LIMITS. REPLACED LH SIDE SEAT RAIL FROM FS 677.00 TO 708.00 IAW CRJ 700 AMM 53-00-49, SRM 53-41-49 AND SRM 51-42-34.CAL TOOL:TQ DRIVER AV-BX100DUE: JAN 2025
LBL 9 FLOOR SEAT TRACK HAS SIGNS OF CORROSION AT FS379.00 (C-CHECK RO 10/6/2024) (FILED CLOSED)REMOVED CORROSION ON SEAT TRACK AT LBL 9 FS. 379 IAW CRJ700 SRM 51-21-06 AND SRM 53-21-49 SRM 51-21-11. CORROSION REMOVED WITHIN LIMITS IAW CRJ700 SRM 51-21-06CAL TOOL: DIGITAL CALIPER ID:AV-7805 CAL DUE: JAN-2025
RH FLOOR SEAT TRACK (RBL9) HAS SIGNS OF CORROSION FROM FS349.00-FS485.00. (C-CHECK RO 10/6/2024) (FILED CLOSED)REPAIRED CORRODED RH FLOOR SEAT TRACK (RBL9) FROM FS 349.00 - FS 485.00 (2) PLACES.POST BLEND DIMENSIONS ARE L=5.00" W=0.90" D=0.0083" (2) L=1.6" W=0.90" D= 0.0095". FOUND TO BE WITHIN LIMITS IAW CRJ700 SRM 53-21-49 & SRM 51-21-11.CAL TOOL:DEPTH GAUGE USED AV-7277CAL DUE AUG2024
RH FLOOR SEAT TRACK (RBL9) HAS SIGNS OF CORROSION FROM FS581.00-FS683.00 (C-CHECK RO 10/6/2024) (FILED CLOSED)OK TO INSTALL BJ 910267REMOVED AND REPLACED RH FLOOR SEAT TRACK (RBL9) FROM FS 581.00-FS 683.00 IAW CRJ 700 AMM 53-00-49 AND SRM 53-31-49.CAL TOOL: TORQUE DRIVER AV-BX100 CAL DUE: JAN 2025
LH FLOOR SEAT TRACK (LBL9) HAS SIGNS OF CORROSION AT FS629.00-FS632.00 (C-CHECK RO 10/6/2024) (FILED CLOSED)REMOVED AND REPLACED LH FLOOR SEAT TRACK BETWEEN FS 565.00 TO 632.00 IAW CRJ 700 AMM 53-00-49BLENDED LH FLOOR SEAT TRACK BETWEEN FS 565.00 TO 632.00 MATERIAL LOSS 0.032 FOUND TO BE OUT LIMITS IAW CRJ 700 SRM 51-21-06 AND SRM 53-31-49CALIBRATED TOOL: TORQUE DRIVE AV-BX100 DUE 31-JAN-25DIGITAL CALIPER AV-7803 DUE 31-JAN-25
LH INBD FLAP VANE CHAFFED AT INBD HINGE LOCATION (C-CHECK RO 10/6/2024) (FILED CLOSED)REMOVED AND REPLACED LH INBD FLAP VANE. NDT PERFORMED BY BARRON NDT LLC, FAA CRS #5NDR545D, REPORT #S072924-5 P.O. #173177 DATE OF INSPECTION 29JUL2024, SEE REPORT FOR DETAILS. IAW CRJ700 SRM 57-52-01, SRM 51-42-10, SRM 51-40-11, SRM 51-21-11, SRM 51-25-06, AND SRM 51-25-01
THE REPAIR LOCATED AT FS969.00 STR 27, HAS CHAFFING ON FASTENERS AND CHAFFING ON THE TRIPLER. PERFORMED REPAIR LOCATED AT FS969.00 STR 27 IAW REO 670-53-00-290 REV-F DATE: 2019-04-26, CRJ700 SRM 25-82-06, 53-61-01, 51-25-01, AMM 25-08-06, 21-31-00, NDT PERFORMED BY BARON NDT, LLC FAA CRS# 5NDR545D REPORT# S081324-1 PO# 173177 DATE INSPECTION 13-AUG-2024, SEE REPORT FOR DETAILS.
LH TRANS COWL INBD SLIDER GOUGED (C-CHECK RO 10/6/2024) (FILED CLOSED)PERFORMED REPAIR ON CHAFE DAMAGE AT L/H TRANSCOWL INBD SLIDER IAW REO 670-78-34-384 REV D DATED 2018-11-27CAL TOOL: DIGITAL CALIPER ID: AV-7805 CAL DUE: JAN-2025PERFORMED NDT PT INSPECTION BY BARON NDT,LLC FAA CRS# 5NDR545D REPORT# S072924-9 P.O# 173177 DATE OF INSPECTION 29-JUL-2024.SEE REPORT FOR DETAILS
ON THE LH INBOARD FLAP VANE, THERE IS CHAFFING ON THE CENTER LEADING EDGE OF THE VANE. (C-CHECK RO 10/6/2024) (FILED CLOSED)REMOVED AND REPLACED L/H INBD FLAP VANE CENTER LEADING EDGE CAP VANE IAW CRJ700 SRM 51-42-13, SRM 51-21-11, SRM 51-25-06, SRM 51-25-16, SRM 51-40-11, SRM 57-52-01.
PASSENGER DOOR SKIN AT FS310.00 UPPER SECTION GOUGED EVAL (C-CHECK RO 10/6/2024) (FILED CLOSED)REMOVED DAMAGE AND EVALUATED AREA AT PASSENGER DOOR SKIN AT FS 310.00 UPPER SECTION,DIMENSIONS L=1.710" W=0.325",REMAINING THICKNESS 0.125",FOUND TO BE WITH IN LIM ITS IAW REO 670-53-21-2456 REV -- DATED 2024-09-09,CRJ 700 SRM 51-26-01,SRM 53-21-01CAL TOOLS: DEPTH GOUGE ID: AJ-1511 CAL DUE:FEB-2025,DIGITAL CALIPER ID: AV-7806 CAL DUE: AUG-2024PERFORMED NDT ET/UT INSPECTION BY BARON NDT,LLC FAA CRS #5NDR545D,REPORT #S090424-7,P.O #173562,DATE OF INSPECTION 04-SEP-2024,
FRAME FS1144.00 DAMAGED NEAR STR 9R BY WATER INJECTION LINE (C-CHECK RO 10/6/2024) (FILED OPEN)EVALUATED DAMAGE ON FRAMS FS. 1144.00 NEAR SRT 9RH FOUND TO BE OUT OF LIMITS IAW CRJ700 SRM 53-61-06. FABRICATED REPAIR ANGLE ON FRAME FS 1144.00 NEAR STR 9RH BY WATER INJECTION LINE IAW MHIRJ REO 670-53-61-2342 REV--(P1) DATE: 2024-08-07 AND REO 670-53-61-2342 REV.-- DATE: 2024-09-09PERFORMED NDT INSPECTION BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S090424-6, P.O# 173562 DATE: 04-SEP-2024, NO DEFECTS NOTED AT TIME OF INSPECTION, SEE REPORT FOR DETAILS CAL TOOLS USED DIGITAL SCALE ID: AV-8473 CAL DUE: AUG-2025
FRAME FS1144.00 DAMAGED NEAR STR 9R BY WATER INJECTION LINE (C-CHECK RO 10/6/2024) (FILED CLOSED)EVALUATED DAMAGE ON FRAMS FS. 1144.00 NEAR SRT 9RH FOUND TO BE OUT OF LIMITS IAW CRJ700 SRM 53-61-06. FABRICATED REPAIR ANGLE ON FRAME FS 1144.00 NEAR STR 9RH BY WATER INJECTION LINE IAW MHIRJ REO 670-53-61-2342 REV--(P1) DATE: 2024-08-07 AND REO 670-53-61-2342 REV.-- DATE: 2024-09-09PERFORMED NDT INSPECTION BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S090424-6, P.O# 173562 DATE: 04-SEP-2024, NO DEFECTS NOTED AT TIME OF INSPECTION, SEE REPORT FOR DETAILS CAL TOOLS USED DIGITAL SCALE ID: AV-8473 CAL DUE: AUG-2025
PASSENGER DOOR SKIN AT FS.310.00 LOWER SECTION HAS A DENT EVAL (C-CHECK RO 10/6/2024) (FILED OPEN)PERFORMED DRESS BACK ON PASSENGER DOOR SKIN AT FS 310.00 LOWER SECTION IAW BOMBARDIER REO 670-51-00-085 REV-A DATE: 2017-08-23, MHIRJ REO 670-53-21-2455 REV-- DATE: 2024-09-07 AND IAW CRJ 700 SRM 53-00-01, SRM 51-26-01, SRM 51-42-06 AND SRM 51-42-21 AND AMM 21-31-00.PERFORMED NDT INSPECTION BY BARON NDT, LLC FAA CRS# 5NDR545D, REPORT# S090924-8, P.O# 173562 DATE OF INSPECTION: 09-SEP-2024 NO DEFECTS NOTED AT TIME OF INSPECTIONCAL TOOLS USED DEPTH GAUGE ID: AJ-1511 DUE: FEB-2025 DEPTH GAUGE ID: AV-7277 CAL DUE: AUG-2025 DIGITAL CALIPERID: AV-7806 CAL DUE: AUG-2024
PASSENGER DOOR FRAME SKIN AT FS349.00 UPPER SECTION GOUGED EVAL (C-CHECK RO 10/6/2024) (FILED OPEN)PERFORMED BLEND OUT REPAIR ON PASSANGER DOOR FRAME SKIN AT FS349.00 UPPER SECTION , FOUND WITHIN LIMITS IAW REO 670-53-21-2460 REV-- DATE: 2024-09-12, CRJ700 SRM 53-21-01, 51-12-00, USED TOOL DEPTH GOUGE ID: AJ-1511 DUE: FEB-2025PERFOMED NDT BY BARON NDT, LLC FAA CRS# 5NDR545D REPORT# S091624-6 PO# 173562 DATE INSPECTION: 16-SEP-2024, SEE REPORT FOR DETAILS
FRAME FS1144.00 DAMAGED NEAR STR 9R BY WATER INJECTION LINE (C-CHECK RO 10/6/2024) (FILED CLOSED)EVALUATED DAMAGE ON FRAMS FS. 1144.00 NEAR SRT 9RH FOUND TO BE OUT OF LIMITS IAW CRJ700 SRM 53-61-06. FABRICATED REPAIR ANGLE ON FRAME FS 1144.00 NEAR STR 9RH BY WATER INJECTION LINE IAW MHIRJ REO 670-53-61-2342 REV--(P1) DATE: 2024-08-07 AND REO 670-53-61-2342 REV.-- DATE: 2024-09-09PERFORMED NDT INSPECTION BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S090424-6, P.O# 173562 DATE: 04-SEP-2024, NO DEFECTS NOTED AT TIME OF INSPECTION, SEE REPORT FOR DETAILS CAL TOOLS USED DIGITAL SCALE ID: AV-8473 CAL DUE: AUG-2025
PASSENGER DOOR SKIN AT FS.310.00 LOWER SECTION HAS A DENT EVAL (C-CHECK RO 10/6/2024) (FILED CLOSED)PERFORMED DRESS BACK ON PASSENGER DOOR SKIN AT FS 310.00 LOWER SECTION IAW BOMBARDIER REO 670-51-00-085 REV-A DATE: 2017-08-23, MHIRJ REO 670-53-21-2455 REV-- DATE: 2024-09-07 AND IAW CRJ 700 SRM 53-00-01, SRM 51-26-01, SRM 51-42-06 AND SRM 51-42-21 AND AMM 21-31-00.PERFORMED NDT INSPECTION BY BARON NDT, LLC FAA CRS# 5NDR545D, REPORT# S090924-8, P.O# 173562 DATE OF INSPECTION: 09-SEP-2024 NO DEFECTS NOTED AT TIME OF INSPECTIONCAL TOOLS USED DEPTH GAUGE ID: AJ-1511 DUE: FEB-2025 DEPTH GAUGE ID: AV-7277 CAL DUE: AUG-2025 DIGITAL CALIPERID: AV-7806 CAL DUE: AUG-2024
PASSENGER DOOR FRAME SKIN AT FS349.00 UPPER SECTION GOUGED EVAL (C-CHECK RO 10/6/2024) (FILED CLOSED)PERFORMED BLEND OUT REPAIR ON PASSANGER DOOR FRAME SKIN AT FS349.00 UPPER SECTION , FOUND WITHIN LIMITS IAW REO 670-53-21-2460 REV-- DATE: 2024-09-12, CRJ700 SRM 53-21-01, 51-12-00, USED TOOL DEPTH GOUGE ID: AJ-1511 DUE: FEB-2025PERFOMED NDT BY BARON NDT, LLC FAA CRS# 5NDR545D REPORT# S091624-6 PO# 173562 DATE INSPECTION: 16-SEP-2024, SEE REPORT FOR DETAILS
CHAFFING NOTED ON LH INBOARD FLAP LOWER SKIN WHERE CANOE FAIRING IS INSTALLED, INBOARD FAIRING. (C-CHECK RO 10/6/2024) (FILED CLOSED)REPAIRED ON LH IB FLAP LWR SKIN(PN CC670-14061-3, BATCH# 173054) WHERE CANOE FAIRING AT IB FAIRING IAW CRJ700 SRM 57-52-01, 51-42-10, 51-40-11, 51-21-11, 51-25-06, 51-25-01, USED TOOL DEPTH GOUGE ID: AV-7277 DUE: JAN-2025, D. COUNTING SCALE AV-4800 DUE: DEC-2023NDT PERFORMED BY BARON NDT, LLC FAA CRS# 5NDR545D REPORT# S080824-2, S090324-1 PO# 173177 DATE INSPECTION: 03-SEP-2024, SEE REPORT FOR DETAILS.
SIGNS OF CORROSION NOTED ON COCKPIT AND CABIN FLOOR LANDINGS ON THE FS280.00 BEAM, LBL9 -RBL9. (C-CHECK RO 10/6/2024) (FILED CLOSED)REMOVED AND REPLACE NEW ANGLE P/N CC670-34095-3S ON COCKPIT FS280.00 BEAM, LBL9 TO RBL9 AND EVALUATED AREA ON CABIN FLOOR LANDINGS FOUND TO BE IN THE PAINT ONLY, WITH NO MATERIAL LOSS NOTED IAW CRJ 700 SRM 51-42-06, 51-42-21, 51-11-00, 51-26-00, 51-21-11, 51-25-06, 51-25-16, 20-70-00, 51-40-11. CAL TOOL: COUNTING SCALE ID: AV-4800 DATE: DEC-2024.
L/H VERTICAL STABLIZER DRAG ANGLES CRACKED FWD AND AFT. (C-CHECK RO 10/6/2024) (FILED CLOSED)REPAIRED L/H VERTICAL STABILIZER DRAG ANGLES FWD AND AFT IAW REO 670-55-31-018 REV-- DATE: 2024-08-29, REO 670-55-31-018 REV-A DATE: 2016-11-10, CRJ700 SRM 51-26-01, NDT PERFORMED BY BARON NDT,LLC FAA CRS# 5NDR545D REPORT# S082924-7 PO# 173562 DATE INSPECTION: 29-AUG-2024, SEE REPORT FOR DETAILS.
LH AILERON LOWER LEADING EDGE CHAFFING DAMAGE. (C-CHECK RO 10/6/2024) (FILED CLOSED)REPAIRED DAMAGE LH AILERON LOWER LEADING EDGE IAW CRJ700 SRM 51-42-06, SRM 57-61-01, SRM 51-21-11, SRM 51-25-06, & SRM 51-25-16. NDT PERFORMED BY BARRON NDT, LLC FAA CRS #5NDR545D, REPORT #S072424-2 P.O. #173177 DATE OF INSPECTION 24JUL24. NO DEFECTS NOTED AT TIME OF INSPECTION. SEE REPORT FOR DETAILS.
L/H VERTICAL STABLIZER DRAG ANGLES CRACKED FWD AND AFT. (C-CHECK RO 10/6/2024) (FILED OPEN)REPAIRED L/H VERTICAL STABILIZER DRAG ANGLES FWD AND AFT IAW REO 670-55-31-018 REV-- DATE: 2024-08-29, REO 670-55-31-018 REV-A DATE: 2016-11-10, CRJ700 SRM 51-26-01, NDT PERFORMED BY BARON NDT,LLC FAA CRS# 5NDR545D REPORT# S082924-7 PO# 173562 DATE INSPECTION: 29-AUG-2024, SEE REPORT FOR DETAILS.TOOL USED DIGITAL COUNTING SCALE ID: AV-4800 DUE: DEC-2024
R/H VERTICAL STABLIZER DRAG ANGLES CRACKED FWD AND AFT. (C-CHECK RO 10/6/2024) (FILED OPEN)REPAIRED R/H VERTICAL STABILIZER AFT DRAG ANGLE IAW BOMBARDIER REO 670-55-31-177 REV.-- DATE:2024/08/22, REO 670-55-31-018 REV.-A DATE: 2016-11-10, CRJ700 SRM 51-26-01, 51-40-11, 51-42-22, 51-21-11, 51-25-06, 51-25-16NDT PERFORMED BY BARON NDT, LLC FAA CRS# 5NDR545D REPORT# S082024-2 P.O# 173562 DATE OF INSPECTION 20AUG2024. PERFORMED SPECIAL ET ISPECTION OF CUT LINE EDGES ON R/H VERTICAL STABILIZER AFT DRAG ANGLE. PERFORMED SPECIAL DETAILED ET INSPECTION OF R/H VERTICAL STABILIZER FWD DRAG ANGLE AND FOUND TO BE CRACK FREE.NO DEFECTS NOTED AT TIME OF INSPECTION.TOOL USED: DIGITAL SCALE TOOL ID# AV4800 CAL DUE DEC2024
PAX DOOR FWD CORNER SKIN PNL DENTED WITH A DAMAGED RIVET. (C-CHECK RO 10/6/2024) (FILED CLOSED)REMOVED AND REPLACED DAMAGED PASSENGER DOOR FWD CORNER PANEL IAW CRJ700 SRM 51-21-11, SRM 51-25-06, SRM 51-42-06, SRM 51-42-13, SRM 51-25-16, SRM 51-40-11, AND SRM52-11-01.DEPTH GAGE AV-6696 JAN 2025
COMPLY WITH: 670BA-32-056 - LANDING GEAR - NOSE LANDING GEAR (NLG) AND DOORS - INSTALLATION OF A NEW HINGE FOR THE NLG AFT DOOR ASSEMBLY REV A PART(S) 0 (C-CHECK RO 10/6/2024) (FILED CLOSED)PERFORMED DOUBLER REPAIR ON NOSE LANDING GEAR AT LH DOOR AFT HINGE FITTING IAW MHIRJ REO 670-53-11-2013 REV-P1 DATE: 2024-09-06, MHIRJ REO 670-53-11-2013 REV-- DATE: 2024-10-02, IAW CRJ 700 AMM 32-22-01, CRJ 700 ESPM 20-12-00. COMPLIED WITH SERVICE BULLETIN# 670BA-32-056 REV-A DATE: 04-17-2017. NDT PERFORMED BY BARON NDT, LLC FAA CRS# 5NDR545D REPORT# S091224-5 P.O# 173562 DATE OF INSPECTION: 12-SEP-2024 NO DEFECTS NOTED AT TIME OF INSPECTION.TORQUE DRIVER: AV-BX101 SEP25, TORQUE WRENCH: AV-BX102 AUG25, MILLIOHMETER: AJ-1448 JAN25.CAL TOOL USED TORQUE WRENCH ID:AV-BX102 CAL DUE: 31-AUG-2025 TORQUE DRIVE ID: AV-BX101 CAL DUE: SEP-2025 MILLIOHM METER ID: AJ-1448 CAL DUE: JAN-2025
LEFT SIDE WINDSHIELD CRACKED. (FLT 3164 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
LEFT SIDE WINDSHIELD CRACKED. (FLT 3164 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26542290 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED LH SIDE WINDOW REFERENCE APPLICABLE STEPS IN AMM 56-12-01TASK CARD 56-220-1000-SKY COMPLIED WITH."
FLOOR SUPPORT STRUCTURE SUPPORT ANGLE LOCATED AT LBL27 BETWEEN FS349 - FS364 IS BENT/DEFORMED. (FILED- OPEN) REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE SUPPORT ANGLE AT LBL27 BETWEEN FS349 - FS364 IN REFERENCE TO SRM 51-42-13.
FLOOR SUPPORT STRUCTURE SUPPORT ANGLE LOCATED AT LBL27 BETWEEN FS333 - FS349 IS BENT/DEFORMED. (FILED- OPEN) REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE SUPPORT ANGLE AT LBL27 BETWEEN FS333 - FS349 IN REFERENCE TO SRM 51-42-13.
FLOOR SUPPORT STRUCTURE SUPPORT ANGLE LOCATED AT LBL27 BETWEEN FS310 - FS333 IS BENT/DEFORMED. (FILED- OPEN) REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE SUPPORT ANGLE AT LBL27 BETWEEN FS310 - FS333 IN REFERENCE TO SRM 51-42-13.
BACKUP SILL BETWEEN FS 310.00 TO 333.00 AND STGR 21L CORRODED. (FILED- OPEN) REMOVED AND REPLACED BACKUP SILL BETWEEN FS 310.00 TO 333.00 AND STR 21L WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1002-SKY. COMPLETED M-337.
DURING THE INCORPORATION OF SB 670SH-53-042 THE BULKHEAD BEAM @ FS693 LBL 18 PN SH670-35886-5 WAS DAMAGED. (FILED- CLOSED) REMOVED AND REPLACED BULKHEAD BEAM @ FS693 LBL 18, IN REF. TO 670BA-53-036 AND 670SH-53-042, COMPLETED 51-900-1002-SKY AND M337. REF. CP 23852492 FOR LEAK CHECK
DURING THE INCORPORATION OF SB 670SH-53-042 THE BULKHEAD BEAM @ FS693 LBL 9 PN SH670-35885-5 WAS DAMAGED. (FILED - OPEN) REMOVED AND REPLACED BULKHEAD BEAM @ FS693 LBL 9, IN REF. TO 670BA-53-036 AND 670SH-53-042, COMPLETED 51-900-1002-SKY AND M337. REF. CP 23852492 FOR LEAK CHECK
DURING THE INCORPORATION OF SB 670SH-53-042 THE BULKHEAD BEAM @ FS693 LBL 27 PN SH670-35884-7 WAS DAMAGED. (FILED- OPEN) REMOVED AND REPLACED BULKHEAD BEAM @ FS693 LBL 27, IN REF. TO 670BA-53-036 AND 670SH-53-042, COMPLETED 51-900-1002-SKY AND M337. REF. CP 23852492 FOR LEAK CHECK
FOUND CRACKED DIAPHRAGM PN SH670-36115-1 @ FS735, AND LBL36. REPLACE AS NECESSARY. (FILE - CLOSED) REMOVED AND REPLACED DIAPHRAGM @ FS735 AND LBL36 IN REF. SRM 51-42-21, COMPLETED 51-900-1002-SKY AND COMPLETED M-337, REF. CP 23852492 FOR LEAK CHECK
COMPLY WITH: 670BA-53-036 - FUSELAGE - CENTER FUSELAGE, FS669.40 TO FS855.40 - REPLACEMENT OF THE BEAMS AF LBL36 AND RBL36, AND THE FLOOR ASSEMBLY BETWEEN FS693.00 AND FS847.00 WITH BEAMS INSTALLED AT BL0, LBL9, LBL18, LBL27, RBL9, RBL18 AND RBL27 REV D PART(S) 0 (FILED - CLOSED) COMPLIED WITH SB 670BA-53-036 REV-D DATED 09/09/2014, FUSELAGE - CENTER FUSELAGE, FS669.40 TO FS855.40 - REPLACEMENT OF THE BEAMS AF LBL36 AND RBL36, AND THE FLOOR ASSEMBLY BETWEEN FS693.00 AND FS847.00 WITH BEAMS INSTALLED AT BL0, LBL9, LBL18, LBL27, RBL9, RBL18 AND RBL27 REV D / COMPLETED TASK CARD 51-900-1002-SKY AND FORM M-337 FOR MAJOR STRUCTURAL REPAIR. / REFERENCE REO 670-53-41-579 REV-- DATED 2021-12-20, SB DEVIATION FOR OVERSIZE FASTENER INSTALLATION AT LBL36 AT FS 797.00.
AIRCRAFT SUSTAINED DAMAGE TO LHS SKIN PANEL BETWEEN FS 193.00 - FS 202.75 AND STR BL22.00 - STR 14L FROM BIRDSTRIKE. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR. REF CAMP'S ML 23603273, 23603274, 23603275 AND 23603276. (FILED CLOSED) REMOVED AND REPLACED LH SIDE SKIN ASSY BETWEEN FS193.00 - FS202.75 AND BL00.00 - BL22.00 IN REF TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1002-SKY. COMPLIED WITH M-337. PRIMED AND PAINTED IN REF TO SRM 51-25-01.
FLOOR SUPPORT STRUCTURE - ENTRANCE STORAGE FWD AMOUNT BRACKETS HAVE CORROSION AROUND AND IN THE BOLT HOLES. REMOVED AND REPLACED FLOOR SUPPORT NEW ENTRANCE STORAGE FWD MOUNT BRACKETS IAW SRM.
RBL 9 FLOORBEAM AT BS 581 WAS CORRODED. COMPLIED WITH ALL STEPS OF REO.
LBL 9 FLOOR BEAM, FS533 TO FS565 WAS CORRODED. COMPLIED WITH ALL STEPS OF REO.
L/H 280.0 CROSSBEAM AS A CRACK ON UPPER FLANGE LBL39.0 RADIUS AREA. REMOVED AND REPLACED CRACKED L/H FS 280.00 CROSSBEAM WITH NEW CROSSBEAM (P/N CC670-34094-1S) IAW SRM AND DWG. RESTORED FINISH TO REWORK AREA IAW SRM AND APPLIED CIC.
CORRODED BS 333, STRINGER CLIP 26L. INSTALLED A NEW STRINGER CLIP IAW SRM AND DWG.
CLEAT COMMON TO STRINGER 23R, FRAME 319 WAS CORRODED. THE STRINGER CLIP HAD INTERGRANULAR CORROSION, OUT OF LIMITS IAW SRM, REPLACED IAW DWG, AND SRM.
STRINGER SPLICE 24R, BS 333 WAS CORRODED. REPLACED THE STRINGER SPLICE IAW SRM AND DWG .
STRINGER SPLICE 23R, BS 333 WAS CORRODED. REPLACED THE STRINGER SPLICE WITH NEW IAW SRM AND DRAWING.
FOUND CORROSION ON STRINGER SPLICE AT FS333.00 STR21R. REPLACED THE STRINGER SPLICE IAW SRM AND DRAWING, RESTORED FINISH AND LEAK CHECK GOOD.
FOUND CORROSION ON STRINGER CLEAT AT FS333.00 STR21R. REMOVED DAMAGED CLEAT PER SRM 51-42-06-001-001-A01, LOCATED AND DRILLED NEW CLEAT PN SH670-32605-1 , PER SRM, INSTALLED NEW CLEAT PER SRM .
FOUND CORROSION ON STRINGER CLEAT AT FS319.00 STR21R. INSTALLED NEW STRINGER CLEAT IAW SRM AND DRAWING RESTORED FINISH COMPLIED WITH.
CLEAT @ STGR21R FS349.00 IS CORRODED. REPLACED THE CLEAT WITH NEW IAW SRM AND DWG.
GALLEY 2 FLOOR MOUNT ATTACHED TO SEAT TRACK HAS EVIDENCE OF CORROSION. REPLACED 2 EA GALLEY2 FLOOR MOUNT FITTINGS WITH NEW. REF CRJ-700 SRM.
DENT ON FUSELAGE SKIN LOCATE BEWEENT FS280 & FS295 AND STRG25R & STRG26R. REPAIRED THE SKIN, COMPLIED WITH ALL STEPS OF REO.
4EA DENTS ON FUSELAGE SKIN LOCATED BETWEEN FS310 & FS333 AND STRG24R & STRG26R. CUT OUT DAMAGE, DRESSED BACK DENTS, AND INSTALLED DOUBLER REF REO.
DENT LOCATEDON ON FUSELAGE SKIN BETWEEN FS333 & FS349 AND STRG25R & STRG26R. ) / CUT OUT DAMAGE, DRESSED BACK DENT, AND INSTALLED DOUBLER REF REO COMPLIED WITH SKY CARD
DENT ON FUSELAGE SKIN LOCATED AT APPROXIMATELY AT FS348 STRG24L. REPAIRED DENT AREA PER WITH REO.
INTERCOSTAL AT 20R, FS310 - FS319 FOUND TO BE CORRODED. REMOVED AND REPLACED NEW INTERCOSTAL IAW SRM.
STRINGER 24R AT FS280 IS CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REPLACED STRINGER 24R AT FS280.00 REF SRM AND DWG.
STRINGER 22R AT FS280 IS CORRODED. REMOVED CORROSION AND FOUND REWORKED AREA TO BE OUT OF LIMITS. REPLACED STRINGER AT STGR 22R, FS280 - FS333 REF SRM.
STRINGER 3L, BS 280, AFT OF THE BULKHEAD IS CRACKED. COMPLIED WITH REPAIRED IAW SERVICE BULLETIN, REVISION C.
* A BAY DOOR STRUCTURE - FS 349 - STGR 25R - FRAME CORRODED AFT OTBD QUAD . REMOVED AND REPLACED NEW FS 349.00 LOWER SECTOR P/N SH670-31357-5S REF CRJ 700 SRM. COMPLIED WITH TASK CARD. LEAK CHECK GOOD
STGR 19R BETWEEN FS280-FS333 IS CORRODED. REPLACED THE STRINGER IAW DWG AND SRM.
NLG AFT DOOR HINGE L/H SIDE ON THE AIRCRAFT STRUCTURE HAS EVIDENCE OF CORROSION. REPAIR NLG AFT DOOR HINGE LH SIDE OF AIRCRAFT STRUCTURE REF REO.
LEFT FLOOR SUPPORT AT BS 280 TO 310 WAS CRACKED ON THE LOWER FLANGE TO HOLE LOCATED ON TOP OF THE SILL. REPLACED THE FLOOR SUPPORT IAW SRM AND DWG.
ANGLE @ FS280.00 LOWER WEB RBL26.00 IS CRACKED INSTALLED NEW ANGLE IAW SRM AND DRAWING.
* A BAY - FS 280 - FLOORBOARD BRKT ON 280 FACING AFT CORRODED @ MULTIPLE LOCATIONS AS MARKED (C-CHCECK 8/23/2020) / REPLACED A BAY - FS 280 - FLOORBOARD BRKT ON 280 FACING AFT REF CRJ700SRM.
STRINGER 23R AT FS280 IS CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS REPLACED THE STRINGER IAW DWG, AMM, AND SRM.
STRINGER 21R AT FS280 IS CORRODED. REMOVED AND REPLACED NEW STRINGER IAW SRM.
STRINGER 20R AT FS280 IS CORRODED . REPLACED STRINGER AT 20R FROM FS280-FS319.00 REF DWG AND SRM.
280 FRAME HAS MULTIPLE AREAS OF CORROSION ON THE LOWER AFT SIDE BETWEEN STRG25L & STRG25R, COMPLIED WITH CORROSION REPAIR OF 280 FRAME AFT SIDE BETWEEN STRINGER 25L AND STRINGER 25R AS PER SRM AND REO.
*PRESSURE FLOOR ̉‰ FLOOR SUPPORTAT BL0 HAS WIRING SUPPORTS IMPROPERLY RIVETED FROM FS693 TO FS847, WITH UNACCEPTABLE BUCKTAILS AND AT LEAST 4 HOLES APPEARING ELONGATED. PERFORMED REPAIR OF PRESSURE FLOOR SUPPORT AT BL0 FS693.00 TO FS847.00 REF REO.
PRESSURE FLOOR AT FLOOR ANGLE UNDER THE RT EMERGENCY EXIT HAD SEVERAL SPOTS OF CORROSION. REMOVE CORROSION UNDER FLOOR BY RH EMERGENCY EXIT,COMPLIED WITH REO FOUND TO BE WITHIN LIMITS
*STRINGER SPLICE, STGR26L, AT FS333 JOINT HAS CORROSION. (C-CHCECK 8/23/2020) / REMOVED CORROSION FOUND TO BE OUT OF LIMITS REPLACED NEW STRINGER P/N SH670-3249-3 26L AT FS333.00 REF CRJ 700 SRM AND BOMBARDIER DWG.LEAK CHECK GOOD
STRINGER 26L, BETWEEN FS333 AND FS349 WAS CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REPLACED THE STRINGER IAW SRM AND DWG.
STRINGER 25R, BETWEEN FS333 AND FS349 WAS CORRODED. REPLACED THE STRINGER IAW SRM, AND DWG.
FLOOR SUPPORT STRUCTURE AT THE GALLEY 1 MOUNT BRACKETS: BOTH FWD LOCATIONS HAVE CORROSION AROUND AND IN THE BOLT HOLES. REMOVED AND REPLACED NEW FITTINGS AT GALLEY 1 MOUNT BRACKETS IAW SRM.
FS280.00 RH LOWER WEB HAS CORROSION. REPLACED RH LOWER WEB AS PER CRJ 700 SRM. SKYWEST TASK CARD AND M-337 COMPLIED WITH.
* A BAY DOOR STRUCTURE - FS'S 394/409 - INTERCOSTAL CORRODED AT SKIN JUST RIGHT OF STGR27. REMOVED CORROSION FROM AVIONICS BAY DOOR CUT OUT INTERNAL STRUCTURE AT FS394 - FS409, STGR 27 AND FOUND REWORKED AREA TO BE WITHIN LIMITS REF SRM.
A BAY DOOR STRUCTURE - FS'S 349/379 - STGR 21R CORRODED. REPLACED STG21R FROM FS349-FS379 WITH NEW. REF SRM AND DWG, NO LEAKS NOTED
* A BAY DOOR STRUCTURE - STGR 25L JUST FWD OF FS 421 CORRODED. COMPLIED WITH ALL STEPS OF REO.
* A BAY DOOR STRUCTURE - FS 364 - STGR JUST RIGHT OF CENTER - AREA AROUND RIVETS CORRODED. REPLACED STGR26R FROM FS364-FS333 WITH NEW REF CRJ-700 SRM DWG.COMPLIED WITH TASK CARD, LEAK CHECK GOOD.
* A BAY DOOR STRUCTURE - FS 364 - STGR 26L - FRAME CORRODED AT SKIN. REMOVED CORROSION FROM FRAME AT FS364 LOWER SECTOR AND FOUND REWORKED AREA TO BE OUT OF LIMITS. REPAIRED FRAME REF SRM. NO LEAKS NOTED
* A BAY DOOR STRUCTURE - FS 349/364 - 26R-25R SKIN CORRODED. COMPLIED WITH ALL STEPS OF REO RESTORED FINISH. COMPLIED WITH.
* A BAY DOOR STRUCTURE - FS'S 349/364 - 26R - INTERCOSTAL CORRODED. INSTALLED NEW INTERCOSTAL 26R FROM FS349-FS364 REF SRM AND DRAWING RESTORED FINISH COMPLIED WITH
* A BAY - FS 319 - FRAME CORRODED ON AFT SIDE OF STGR 26R. REMOVED CORROSION ON FRAME AT FS319 BETWEEN 25L & 25R. FOUND REWORKED AREA TO BE ACCEPTABLE AS IS REF REO.
* A BAY - FS'S 295/310 - STGR 27 - TCAS ANTENNA DOUBLER CORRODED. REMOVED AND REPLACED LOWER TCAS CHANNEL P/N SH670-32364-7 REF SRM. LEAK CHECK GOOD
* A BAY - FS'S 295/310 - STGR 26R CORRODED (C-CHCECK 8/23/2020) / REPLACED STRINGER 26R REF CRJ700 SRM AND DRAWING. COMPLIED WITH TASK CARD. NO LEAKS NOTED. M-337 FORM ATTACHED
* A BAY - FS'S 295/310 - STGR 25R CORRODED. REPLACED STRINGER 25R REF CRJ700 SRM AND DRAWING.
A BAY - FS'S 319/333 - STGR 25L CORRODED. REMOVED CORROSION FROM STGR25 BETWEEN FS31- & FS333, WITHIN LIMITS,
A BAY - FS'S 295/310 STGR 26L CORRODED. INSTALLED NEW STRINGER REF CRJ 700 SRM, AND DWG.
A BAY - FS 295 - STGR 27 CORRODED. REPLACED STRINGER 27 FROM FS280-310 REF SRM AND DWG
A BAY - FS 295 - FRAME CORRODED BOTH SIDES OF STGR 27. REPAIRED FRAME 295.00 FROM STRG 25L TO STRG 25R REF SRM.COMPLIED WITH TASK CARD. NO LEAKS NOTED.
A BAY - FS 280 LONGITUDINAL SPLICE CORRODED MULTIPLE PLACES FROM 26L TO 19R. REMOVED CORROSION FROM FS280 LOWER BUTTSTRAP AND FOUND REWORKED AREA TO BE ACCEPTABLE AS IS REF REO. PRESSURE LEAK CHECK GOOD.
FWD FUSELAGE - BELOW FLOOR - BETWEEN FS 280 & 265 - STGR 25R - POLYFAB BAG DEGRADED BEYOND USE AND CONTAMINATING ABAY - WASN'T ABLE TO REMOVE. REPLACED FWD FUSELAGE BELOW FLOOR BETWEEN FS280-265 STGR 25R INSULATION WITH NEW. IAW AMM.
* FWD FUSELAGE - BELOW FLOOR - FS 250 FRAME CORRODED @ STGR 26R. REPAIRED DAMAGE REF REO.
* A BAY - FS'S 319/333 - STGR 25R CORRODED. REMOVED CORROSION AND FOUND REWORKED AREA TO BE OUT OF LIMITS. REPLACED STINGER SPLICE AT STGR25R, FS333 REF SRM & DWG.
NLG APEX BUSHINGS OUT OF LIMITS. REPLACED WITH NEW NLG APEX BUSHINGS IAW CMM 32-21-06. MAXIMUM GAP 0.012", MEASURED GAP 0.005", GAP IS WITHIN LIMITS
R/H FLOOR SILL @ STR 17R FUS 985 - 1000 HAS CORRSOIN. REPAIRED CORRODED FLOOR SILL AT STR 17R FS 985-1000 AS PER CRJ 700 SRM.
LEFT FS274 CRACKED LEFT OF LBL9.00. REPAIRED CRACKED LEFT FLOORBEAM LBL9.00 AT FS280.00 TO FS265.00 REF CRJ700 SRM.COMPLIED WITH STRUCTURAL MAJOR REPAIR AND FORM M-337 ATTACHED.
*CRACK BETWEEN FRAME AND DIAPHRAGM AT FS909 BELOW WL97.50 ON WING-TO-BODY SUPPORT STRUCTURE. REPAIRED CRACK BETWEEN FRAME AND DIAPHRAGM AT FS909 BELOW WL97.50 REFERENCING REO.
LEFT HAND SIDE SEAT RAIL HAS CORROSION ON MULTIPLE FASTENERS, FS573.00 669.00. REPLACED L/H SIDE SEAT RAIL BETWEEN F.S. 573.00 TO F.S.675.00 REF. CRJ 700 AMM. / FABRICATED NEW SEAT TRACK IAW SRM.
LEFT HAND SIDE SEAT RAIL HAS CORROSION AND CORROSION ON FASTENERS AT MULTIPLE AREAS, FS378.00 483.00. (MARKED) (C-CHECK 8/23/2020) / INSTALLED NEW SEAT RAIL ON L/H SIDE BETWEEN FS378.00 TO S483.00 REF CRJ700 AMM.
RIGHT HAND SIDE SEAT RAIL HAS CORROSION ON MULTIPLE FASTENERS, FS573.00 669.00. (MARKED) (C-CHECK 8/23/2020) INSTALLED NEW SEAT RAIL ON R/H SIDE BETWEEN FS573.00-FS669.00 / REF CRJ700 AMM.
RIGHT HAND SIDE SEAT RAIL HAS CORROSION AND DAMAGE AT MULTIPLE AREAS, FS483.00 FS573.00. REPLACED THE R/H SIDE SEAT RAIL BETWEEN F.S 483.00 TO F.S. 573.00 REF. CRJ 700 AMM. FABRICATED SEAT TRACK IAW SRM.
RIGHT HAND SIDE SEAT RAIL HAS CORROSION AND DAMAGE AT MULTIPLE AREAS, FS378.00 - 483.00. INSTALLED NEW SEAT RAIL ON R/H SIDE BETWEEN FS378.00-FS483.00 / REF CRJ700 AMM.
LEFT HAND SIDE SEAT RAIL HAS CORROSION AND CORROSION ON FASTENERS AT MULTIPLE AREAS, FS785.00 - 854.00. REPLACED R/H SIDE SEAT RAIL BETWEEN F.S. 784.00 TO F.S. 861.00 REF. AMM. FABRICATED SEAT TRACK IAW SRM.
LEFT HAND SIDE SEAT RAIL HAS CORROSION AND DAMAGE AT MULTIPLE AREAS, FS869.00 961.00. REPLACED L/H SIDE SEAT TRACK BETWEEN F.S. 861.00 TO F.S. 961.00 IAW AMM. FABRICATED SEAT TRACK IAW SRM.
RIGHT HAND SIDE SEAT RAIL HAS CORROSION AND DAMAGE AT MULTIPLE AREAS, FS869.00 961.00. REPLACED R/H SIDE SEAT RAIL BETWEEN F.S. 861.00 TO F.S. 961.00 REF. CRJ 700 AMM. FABRICATED SEAT TRACK IAW SRM.
RIGHT HAND SIDE SEAT RAIL HAS CORROSION AT MULTIPLE AREAS, FS854.00 869.00. REPLACED R/H SIDE SEAT TRACK BETWEEN F.S. 855.00 TO F.S. 861.00 REF. CRJ 700 AMM. FABRICATED SEAT TRACK IAW SRM.
CORROSION MULTIPLE AREAS ON SEAT RAIL FS349.00 FS485.00, BL9R. (MARKED) (C-CHECK 8/23/2020) / REPLACED SEAT RAIL BETWEEN F.S. 374.00 TO F.S. 485.00 REF. CRJ 700 AMM. FABRICATED SEAT FROM P/N 20276-288-0-0 PO# T55037 REF. CRJ 700 SRM.
CORROSION MULTIPLE AREAS ON SEAT RAIL FS349.00 FS485.00, BL9L. REPLACED SEAT TRACK BETWEEN F.S. 349.00 TO F.S.485.00 AT LBL 9 REF. CRJ 700 AMM. FABRICATED NEW SEAT TRACK FROM P/N 20276-228-0-0 PO#T55627 REF. CRJ 700 SRM.
CORROSION MULTIPLE AREAS ON SEAT RAIL FS485.00 FS581.00, BL9R. INSTALLED NEW SEAT RAIL ON R/H SIDE RBL9.00 BETWEEN FS 485.00 - FS581.00 / REF CRJ700 AMM.
CORROSION MULTIPLE AREAS ON SEAT RAIL FS581.00 FS670.00, BL9L. REPLACED SEAT TRACK BETWEEN F.S. 581.00 TO F.S. 677.00 AT LBL 9 REF. AMM. FABRICATED NEW SEAT TRACK FROM P/N 20276-288-0-0 IAW SRM.
CORROSION MULTIPLE AREAS ON SEAT RAIL FS581.00 FS670.00, BL9R. (MARKED) (C-CHECK 8/23/2020) REMOVED CORROSION FROM RH FLOOR SEAT RAIL FS581 - FS670. FOUND REWORKED AREA OUT OF LIMITS. REPLACE SEAT RAIL REF CRJ-700 SRM.
RIGHT WHEEL WELL - ATTACH ANGLE, ON THE RIGHT WING REAR SPAR, FOR TIRE BURST PANEL (642BZ) IS CORRODED. (MARKED) (C-CHECK 8/23/2020) / REMOVED CORROSION R/H WHEEL WELL ATTACH ANGLE ON THE RIGHT WING REAR SPAR FOR THE TIRE BURTS PANEL 642BZ FOUND TO BE WITHIN LIMITS REF CRJ 700 SRM / SEE CONTINUATION CARD FOR DETAILS
PASSENGER STAIR WIRE HARNESS TUBE AT DOOR LOWER SILL HAS EVIDENCE OF CORROSION. REPLACED PAX DOOR HARNESS TUBE ASSY REF ESPM AND EM.
AFT CARGO DOOR SURROUND STRUCTURE LOWER BRACKET IS CRACKED. FS1047. REPLACED AFT CARGO DOOR SURROUND BRACKET PN: MM670-35552-005 WITH NEW IAW SRM.
LEFT WHEEL WELL - ATTACH ANGLE, ON THE LEFT WING REAR SPAR, FOR TIRE BURST PANEL (542BZ) IS CORRODED. REPLACED WITH NEW LH WHEEL WELL ATTACH ANGLE P/N CC670-10338-1 ON THE LEFT WING REAR SPAR FOR THE TIRE BURTS PANEL 542BZ REF SRM.
CORROSION - BAGG DOOR - FWD UPPER ROLLER ASSY MOUNT BRACKET - LWR OTBD MOUNT BOLT CORRODED. REPLACED BOLT COMMON TO THE AFT BAGGAGE BAY FWD UPPER ROLLER ASSY MOUNT BRACKET. REF CRJ-700 SRM.
PAX DOOR FRAME320 IS CORRODED, APPOX STGR 13. REPAIRED PASSENGER DOOR FRAME FS320.00. REF REO ALL STEPS COMPLIED WITH
RH ENGINE LOWER INNER CORE COWL INNER SKIN CHAFFED ON REPAIR. REMOVED AND FABRICATED NEW REPAIR DOUBLER PER CRJ 700 SRM, FABRICATED DOUBLER OUT OF AISI 321 CRES STAINLESS STEEL .010, LOCATED DRILLED AND INSTALLED WET WITH RED RTV -106 / AND RESTORED FINISH ON FASTENERS. PER SRM.
RH OVERWING EMER EXIT STEP PLATE HAS CORROSION AROUND NUT CLIP HOLES AND ALONG INNER BOTTOM EDGE. REMOVED CORROSION ON RH OVERWING EMER EXIT STEP PLATE AS PER SRM. DAMAGE FOUND TO BE WITHIN LIMITS
CORROSION NOTED ON COCKPIT ENTRY FLOOR SUPPORT. REMOVED AND REPLACED COCKPIT FLOOR SUPPORT ANGLE SRM, AND DRAWING .
LH OVERWING EMER EXIT STEP PLATE HAS CORROSION AROUND AFT SCREW ON TOP. REMOVED CORROSION ON LH OVERWING EMER EXIT STEP PLATE AS PER SRM. DAMAGE FOUND TO BE WITH IN ALLOWABLE LIMITS.
CORROSION NOTED ON FS280 CROSSBEAM, RH SIDE. REMOVED AND REPLACED RH FS280.00 CROSSBEAM REF: SRM DRAWING AND WITH TASK CARD.
L/H WING OUTBOARD FLAP, INBOARD HINGE ARM SPRING ACTUATOR IS CORRODED. (C-CHECK 8/23/2020) REMOVED CORRODED AND INSTALLED NEW LH WING OB FLAP IB HINGE ARM SPRING ACTUATOR REF CRJ700 AMM. / OPS TEST GOOD SEE CONTINUATION FOR WORK ACCOPLISHED
L/H WING INBOARD AILERON PCU ROD END HAS EVIDENCE OF CORROSION. REPLACED LH WING IB AILERON PCU REF CRJ 700 AMM. OPS CHECK GOOD.
L/H WING OUTBOARD AILERON PCU ROD END HAS EVIDENCE OF CORROSION. REPLACED WITH NEW L/H WING OUTBOARD AILERON PCU REF CRJ 700 AMM A02. OPS CHECK GOOD.
RH ENGINE UPPER OUTB CASCADE IS CHAFED AT THE OUTBD ATTACH AREA. REPAIRED RH ENGINE UPPER OTBD CASCADE IS CHAFED AT THE OUTBD ATTACH AREA. REF REO.
THE RH FUSELAGE SKIN HAS 1 DENT BETWEEN FS 409 AND FS 421 AND BETWEEN STR 15R AND STR 16R. REPAIRED RH FUSELAGE SKIN DENT BETWEEN FS 409 AND FS 421 AND BETWEEN STR 15R AND STR 16R AS PER REO.
THE RH FUSELAGE SKIN HAS 1 DENT BETWEEN FS 394 AND FS 409 AND BETWEEN STR 15R AND STR 16R. REPAIRED DENT AREA REF COMPLIED WITH REO
THE RH FUSELAGE SKIN HAS 1 DENT BETWEEN FS 349 AND FS 364 AND BETWEEN STR 15R AND STR 16R. COMPLIED WITH REO DISPOSITION FOR DENT DAMAGE TO FUSELAGE SKIN BETWEEN FS 349-364AND STR 15R-16R.
* THE LH SIDE FUSELAGE SKIN PANEL BETWEEN FS 169 AND FS 173, JUST FWD OF THE TRU ACCESS DOOR, HAS 2 DENTS NEXT TO ONE ANOTHER. REPAIRED DENT LOCATED AT LH SIDE FUSELAGE SKIN PANEL FS 169-FS 173 JUST FWD OF THE TRU ACCESS DOOR. REF REO.
THE RH AILERON'S UPPER LEADING EDGE SHROUD IS CHAFED IN MULTIPLE AREAS. REMOVED AND REPLACED UPPER SKIN OF RH AILERON LEADING EDGE PN CC670-13052-4 ,DUE TO BEING OUT OF LIMITS PER SRM AND FASTENER INSTALLATION DRAWING CC670-13000
THE LH WING OUTBOARD FLAP'S UPPER SKIN PANEL HAS 3 "SMOKING RIVETS" ALONG ITS TRAILING EDGE, NEAR THE INBOARD END. REMOVED DAMAGED FASTENERS PER SRM. REQUESTED ENGINEERING TO REWORK FATENER HOLES, REO. WAS RECEIVED , OPENED HOLES TO 5/32, INSTALLED FASTENERS CR3224-5-2 AND RESTORED FINISH PER REO.
THE RH FUSELAGE SKIN HAS 3 DENTS BETWEEN FS 409 AND FS 421 AND BETWEEN STR 16R AND STR 17R. REPAIRED RH FUSELAGE SKIN 3 EA. DENTS BETWEEN FS 409 AND FS 421 AND BETWEEN STR 16R AND STR 17R AS PER REO.
* THE RH FUSELAGE SKIN HAS 1 DENT BETWEEN FS 394 AND FS 409 AND BETWEEN STR 16R AND STR 17R. (MARKED WITH BLACK GREASE PENCIL) (C-CHECK 8/23/2020)REPAIRED DENT ON RH FUSELAGE SKIN BETWEEN FS 394 AND 409 AND BETWEEN STR 16R AND 17R AS PER MHIRJ REO.
OVAL SHAPED DENT THAT IS 2 IN LONG BY 1 INCH WIDE LOCATED AT APPROX. FS 1162, STRINGER 23L. MAP EVALUATE AND REPAIR AS REQUIRED. IF FOUND WITHIN LIMITS, ELIMINATE DENT USING AIRCRAFT STANDARD PRACTICES/PROCEDURES. REPAIRED OVAL SHAPED DENT AT APPROX FS1162 STGR 23L WITH DOUBLER. REF SRM.
PASSENGER DOOR DD6 INTERCOSTAL BETWEEN FS323.363 AND FS338.963 HAS CORROSION. (C-CHECK) RO: 12/31/2018 REPLACED PAX DOOR INTERCOSTAL DD6 BTW FS323.363 - FS338.963 WITH NEW IAW SRM AND REO.
LT WING ̉‰ SLAT TRACK CANISTER FOR SLAT TRACK 1-3 ̉‰ WELDED BRACKET CRACKED. (C-CHECK) RO: 12/31/2018 REPAIRED LT WING SLAT TRACK CANISTER FOR SLAT TRACK 1-3 IAW REO.
FWD CARGO DOOR SEAL RETAINER BENT AND CRACKED ON I/B FWD SIDE. (C-CHECK) RO: 12/31/2018 REMOVED AND REPLACED FWD CARGO DOOR I/B LOWER SEAL RETAINER WITH NEW SEAL RETAINER P/N LE670-39644-1 IAW SRM AND AMM.
RT WING INBD SLAT HAS CORROSION AT TELESCOPIC DUCT CONNECTION POINT. FOUND DURING GASKET REPLACEMENT. COMPLIED WITH EA 43-2017-041 AND EA 43-2017-041 FOR REPAIR OF RT INBD SLAT RIB.
RT ENGINE IDG POWER LEAD CONDUIT DAMAGED. COMPLIED WITH EC/TC REO 670-24-21-001 AND REO 670-24-21-001 FOR REPAIR OF RT ENGINE IDG CONDUIT.
PAX DOOR LOWER FWD FORMER CORRODED AROUND LOWER TENSION TIE AREA. COMPLIED WITH EC/TC EA 20-2017-059 AND EA 20-2017-059. FOR REPAIR OF PAX DOOR.
PASSENGER DOOR AFT SIDE FRAME NEAR TOP STEP BUCKLED. REMOVED AND REPLACED AFT RISER P/N 601R317071-11 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, & DRAWING 601R317071.
FS 319.7 FRAME HAS CORROSION DAMAGE (FWD & AFT SIDES) STR 26L -26R. COMPLIED WITH ECTC REO 670-53-21-1407.
FWD RISER ON PAX DOOR FOUND 2 EA. CRACKS. REPAIRED FWD RISER IAW SRM TR 52-0025, 52-11-04--201-004-A01.
ASD MOTOR LOWER STIFFENER CRACKED. REMOVED AND REPLACED PAX DOOR STIFFENER PER SRM 51-42-06-001-001-A01,51-40-06-001-001-A01 AND 51-40-11-001-001-A01.
AVI BAY DOOR SEAL RETAINER FOUND TO BE CORRODED. REMOVED AND REPLACED AVI DOOR SEAL RETAINER PER SRM 51-42-06-001-001-A01, 51-23-00-001-001-A01.
RT SIDE SEAT RAIL SEGMENT FROM FS 785.15-852 HAS CORROSION DAMAGE. REMOVED AND REPLACED WITH SERVICEABLE SEAT RAIL AT RT SIDE FS 785.15-852 IAW AMM 53-00-49-000-801 A17 & 53-00-49-400-801 A17 COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M AS WRITTEN.
RT SIDE SEAT RAIL HAS CORROSION DAMAGE FS 712-761.85. REMOVED AND REPLACED WITH SERVICEABLE SEAT RAIL AT RT SIDE FS 712-761.85 IAW AMM 53-00-49-000-801 A17 & 53-00-49-400-801 A17 COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M AS WRITTEN.
FLOOR SEAT RAIL 686.00-838.00 RBL 9 HAS CORROSION DAMAGE. REMOVED AND REPLACED WITH SERVICEABLE SEAT RAIL AT FS 686.00-838.00 AT RBL 9 IAW AMM 53-00-49-000-801 A17 & 53-00-49-400-801 A17 COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M AS WRITTEN.
RT SIDE SEAT RAIL SEGMENT FROM FS 570 - 677 HAS CORROSION DAMAGE. REMOVED AND REPLACED WITH SERVICEABLE SEAT RAIL AT RT SIDE FS 570-677 IAW AMM 53-00-49-000-801 A17 & 53-00-49-400-801 A17 COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M AS WRITTEN.
FLOOR SEAT RAIL FS 830.40-985 RBL 9 HAS CORROSION DAMAGE. REMOVED AND REPLACED WITH SERVICEABLE SEAT RAIL AT FS 830.40-985 AT RBL 9 IAW AMM 53-00-49-000-801 A17 & 53-00-49-400-801 A17 COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M AS WRITTEN.
RT SIDE FLOOR SEAT RAIL FS 677-712 HAS CORROSION DAMAGE. REMOVED AND REPLACED WITH SERVICEABLE SEAT RAIL AT RT SIDE FS 677-712 IAW AMM 53-00-49-000-801 A17 & 53-00-49-400-801 A17 COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M AS WRITTEN.
FLOOR SEAT RAIL FS 830.40-985 LBL 9 HAS CORROSION DAMAGE. REMOVED AND REPLACED WITH SERVICEABLE SEAT RAIL AT FS 830.40-985 AT LBL 9 IAW AMM 53-00-49-000-801 A17 & 53-00-49-400-801 A17 COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M AS WRITTEN.
FLOOR SEAT RAIL 686.00-838.00 LBL 9 HAS CORROSION DAMAGE. REMOVED AND REPLACED WITH SERVICEABLE SEAT RAIL AT FS 581.00-686.00 AT RBL 9 IAW AMM 53-00-49-000-801 A17 & 53-00-49-400-801 A17 COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M AS WRITTEN.
FLOOR SEAT RAIL 581.00-686.00 RBL 9 HAS CORROSION DAMAGE. REMOVED AND REPLACED WITH SERVICEABLE SEAT RAIL AT FS 581.00-686.00 AT RBL 9 IAW AMM 53-00-49-000-801 A17 & 53-00-49-400-801 A17 COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M AS WRITTEN.
ASD HINGE LUGS DOOR SIDE 3 DAMAGED LUGS 6,20,23. COMPLIED WITH EC/TC REO 670-52-91-511 AND REO 670-52-91-511.
REFER TO CO#10155817 JOB 71015587 OP 43. ASD HINGE LUGS DOOR SIDE 3 DAMAGED LUGS 6,20,23 - MTC - COMPLIED WITH EC/TC REO 670-52-91-511 AND REO 670-52-91-511.
FLOOR SILL AFT OF SERVICE DOOR HAS CORROSION. COMPLIED WITH EC/TC REO 670-53-00-390 AND REO 670-53-00-390. FOR REPAIR OF FLOOR SILL.
FLOOR SEAT RAIL FOUND CORRODED AT 581.00-686.00 AND LBL 9. REMOVED AND REPLACED SEAT RAIL IAW AMM 53-00-49-001-001-A03 AND EC/TC REO 670-53-00-343 AND REO 670-53-00-343.
FRAME CLIP CORRODED AT STR 19L FS 1015. REMOVED AND REPLACED FS 1015, STR 19L CLIP IAW SRM 51-42-06-001-001 A01, AND DRW MM670-36080.
PILOT REPORTED LEFT ENG BETWEEN 16,000 AND FL220 ENGINE WILL ROLLBACK FROM 87.2 TO 85.9. THE ENGINE WILL ROLL UP AND DOWN TILL FL220 THEN IT STABILIZES. MX REMOVED AND REPLACED FUEL PUMP ASSY ON LEFT ENGINE WITH OPERATIONAL AND LEAK CHECKS GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
THE CREW REPORTED DURING CLIMB BETWEEN 18000-21000 FT, THE LEFT ENGINE N1 ROLLED BACK FROM 86.7% TO 83.9% 5 TIMES. ALL OTHER ENGINE INDICATIONS WERE NORMAL. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE FADEC AND THE NR 1 ENGINE FUEL METTERING UNIT,AND THE NR 1 ENGINE N1 PROBE. OPERATIONAL CHECKS WERE GOOD.
LEFT SIDE EXTERIOR EMERGENCY LIGHT LENS COVER IS BROKEN. REMOVED AND REPLACED THE LENS COVER IAW AMM 33-51-15, OPS CHECKED GOOD.
GALLEY LOWER AFT EXIT, COURTESY LIGHT HAVE 2 LIGHT BULBS BURNED. RELAMPED GALLEY AFT EXIT SIGN IAW GMM 3-8, OPS CHECKED GOOD.
12 AB LOWER EXIT SIGN HAVE 2 LIGHT BULBS BURNED. RELAMPED 2 BULBS AT 12 AB EXIT SIGN IAW GMM 3-8. OPS CHECKED GOOD.
ISLE OVERHEAD EMERGENCY LIGHT INOPERATIVE AT SEATS 10B,C. REMOVED INOPERATIVE BULB AND INSTALLED NEW BULB IAW AMM 33-51-09, OPS CHECK GOOD.
CAPTAIN'S FLASHLIGHT INOPERATIVE. REPLACED BATTERIES IN CAPTAIN'S FLASHLIGHT AND OPS CHECK GOOD IAW AMM 25-61-00. ACFT OK FOR SERVICE.
SMOKE AFT LAV WARNING AFTER TAKEOFF. A DISTINCT ODOR WAS NOTICED THROUGHOUT THE ENTIRE ACFT WHICH SMELLED LIKE SOMETHING WAS BURNING. ACFT RETURNED TO DEPARTURE AFTER T/O. PERFORMED ENGINE DRYOUT IAW AMM 72-00-00 TO DRY COMPRESSOR WASH FLUID.
STRINGER 7R BS 1144 IS CHAFED. BLENDED OUT DAMAGE IAW SRM 51-12-00-001-001-A01AND SRM 5-51-16. MAJOR REPAIR.
STRINGER 18R CORRODED FROM BS 280-287. . REMOVED SECTION OF STRINGER IAW SRM 51-42-06-001-001 & SRM 51-42-21-001-001. REPAIRED IAW EA 12-2014-167 REV A2. MAJOR REPAIR.
CHAFE DAMAGE ON WEB OF INTERCOSTAL BETWEEN BS 1144 - 1154.48. DRILLED UP NEW INTERCOSTAL IAW SRM 51-40-11001-001-DWG MM670-360-86. MAJOR REPAIR.
STRINGER SPLICE 25R AT BS 333 CORRODED OUT OF LIMITS. REMOVED AND REPLACED IAW SRM 51-42-06-001-001-A01, 51-42-06-001-001-A01 AND DWG SH670-32420.
RIGHT NR 7 EMERGENCY LIGHT TRACK DELAMINATED. REMOVED AND REPLACED THE EMERGENCY LIGHT TRACK IAW AMM 33-51-01, REV A.
STRINGER SPLICE 18R CORRODED BS 284 - 292. REPAIRED IAW EA 12-2014-167.
STRINGER 27 CORRODED BS 295. REMOVED STRINGER BETWEEN BS 280 - 295 IAW SRM 51-42-06-001-001-A01. INSTALLED NEW STRINGER IAW SRM 51-42-06-001-001-A01. MAJOR REPAIR.
STRINGER 26R FWD SPLICE FOUND TO BE CORRODED BETWEEN BS 329-333. BLENDED CORROSION, AND FOUND TO BE IN A NO DAMAGE ALLOWED AREA IN REF TO SRM 53-21-03-101 & 51-21-06-001-001. INSTALLED NEW STRINGER SPLICE IAW SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.
STRINGER 26L CORRODED BS 282. CUT & REMOVED SECTION OF STRINGER BETWEEN BS 280 - 302.5 IAW SRM 53-00-03-201-001, SRM 53-00-53-201-001 AND SRM 53-00-003-201-001-A01. INSTALLED NEW SECTION OF STRINGER IAW SRM 53-00-03-201-001-A01 AND EA 32-2014-040 REV A.
SERVICE DOOR FLOOR PROTECTOR ANGLE CORRODED. REPLACED ANGLE IAW SRM 51-42-06-001-001, SRM 51-42-02-001, 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
STRINGER 25R CORRODED BS 282. REPAIRED IAW SRM 53-00-03-201-001-A01. MAJOR REPAIR.
SERVICE DOOR LOWER SILL ANGLE CORRODED. REMOVED LOWER SILL ANGLE ON SERVICE DOOR IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW LOWER SILL ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED LOWER SILL ANGEL AND UPPER SILL ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31996.
CORROSION AROUND NUTPLATES IN ASD INNER SKIN UNDER ACCESS PANEL 832AB. REMOVED CORROSION AROUND NUTPLATES ON ASD INNER SKIN IAW SRM 51-21-06-001-001. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.
RIGHT CABIN FLOOR SUPPORT CORRODED FROM BS 286-319.7. COMPLIED WITH REO 670-53-00-390.
RIGHT FS 280 WEB CORRODED. INSTALLED RT STRAP TO RT WEB IAW REO 670-53-11-594. COMPLIED WITH REO 670-53-11-594, REV-DATED 2011/04/27 AS NEEDED.
FOUND THE RT COCKPIT FLOOR SUPPORT ANGLE TO BE CRACKED AT FS 278. R & R RT COCK PIT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01, SRM TR-53-0057 & DWG CC670-33199.
FOUND THE LT COCKPIT FLOORBEAM ANGLE TO BE CRACKED AT FS 278. R & R THE SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01, SRM TR-53-005 & DWG CC670-33199, REV B.
LT SIDE SEAT TRACK AT FS 785 - 863 CORRODED. REMOVED THE SEAT TRACK IAW AMM 53-00-49-000-801. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.
LT INBD SEAT TRACK BS 379-485 HAS CORROSION. R & R SEAT TRACKIAW SRM 53-00-49-001-001-A001 & AMM 53-00-49-400-801.
STRINGER 26R, BS 333-349 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01 & DWG SH670-31350.
FRAME STRAP BS 333 CORRODED BETWEEN 25-26R. REMOVED CORROSION IAW SRM 51-21-00-001-001-A01. COMPLIED WITH EA 32-2014-021.
RIGHT FS 280, WEB CORRODED. COMPLIED WITH ECTC REO 670-53-11-597 01 AND GREO 670-53-11-594, REV.
COCKPIT FLOOR AFT SUPPORT ANGLE CORRODED. REMOVED CORRODED COCKPIT FLOOR SUPPORT ANGLE AND REPLACED WITH SERVICEABLE COCKPIT FLOOR AFT SUPPORT ANGLE AS NEEDED IAW SB 670BA-53-041, REV D DATED 12 MAR 14.
RIGHT & LEFT 280 FLOORBEAM CORRODED. REMOVED RT 280 CORRODED FLOORBEAM AND REPLACED WITH SERVICEABLE RT 280 FLOORBEAM AS NEEDED IAW SB670BA-53-041, REV D. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.
ASD PULL IN LEVER DOUBLER CRACKED INSIDE ACCESS PANEL, 832AR. R & R ASD PULL IN LEVER DOUBLER IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01 AND AMM 51-42-21-001-001-A01 IAW DWG 601R318097. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.
RT SEAT TRACK BS 349-485 HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001, 51-21-00-001-001. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.
LT INBD SEAT TRACK BS 677-830 HAS CORROSION. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.
LEFT INBD SEAT TRACK BS 581-677 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.
RT SIDE SEAT TRACK BS 711-761 HAS CORROSION. R & R SEAT TRACK IAW AMM 53-00-49-400-801 AND 53-00-49-000-801.
RT SIDE SEAT TRACK BS 677-711 HAS CORROSION. FOUND TO BE OUT-OF-LIMITS IAW SRM 53-41-49-11-001-A01. R & R THE SEAT TRACK IAW AMM 53-00-49-001-801/53-00-49-400-801.
RT SIDE SEAT TRACK AT BS 485-578 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SR, 53-31-49-101-001-A01. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801, AND 53-00-49-400-801.
LT SIDE SEAT TRACK AT BS 573-708 HAS CORROSION. REMOVED & INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-000-801 & 53-00-49-400-801.
LT SIDE SEAT TRACK AT BS 677-708 HAS CORROSION. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801 & 53-00-49-400-807.
LT SIDE SEAT TRACK BS 708-752 HAS CORROSION. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.
ASD HINGE ACFT SIDE GOUGED AT AFT END BY ROLL PIN. ALL WORK ACCOMPLISHED IAW REO 670-53-21-582. RESTORED FINISH TO ASD HINGE IAW REO 670-53-21-582 AND ECTC REO 670-53-21-582. REPAIRED PASSENGER DOOR HINGE, FUSELAGE SIDE, IAW REO 670-53-21-582, REV A. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.
ASD INTERCOSTAL CRACKED INSIDE ACCESS PANEL 832BR. R & R ASD INTERCOSTAL IAW SRM 51-42-06-001-001-A01, SRM 51-42-06-13-001-001-A01 AND 51-42-21-001-001-A01 IAW DWG 601R31902. RESTORED FINISH IAW SRM 51-21-16-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.
RT SIDE FWD SUPPORT JUST AFT OF BS 280 HAS CORROSION. CLEANED CORROSION AND FOUND AREA OUT OF LIMITS IAW SRM 51-21-06-001-001-A01. CUT AWAY DAMAGE IAW SRM 53-21-43-201-002-A01. MAJOR REPAIR.
ASD SILL KICK PLATE ANGLE CORRODED. FOUND OUT OF LIMITS IAW SRM 53-21-23-101-001-A01 AND 52-06-00-101-001-A01. REMOVED KICKPLATE ANGLE IAW SRM 51-42-06-001-001. DRILLED KICKPLATE ANGLE IAW SRM 51-40-11-001-001-A01.
FRAME AT BS 310 CORRODED BETWEEN STRINGERS 25L-25R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.
INTERCOSTAL CORRODED BETWEEN BS 310-319.70 STRINGER 20R. REMOVED CORROSION IAW SRM 51-21-03-001-001-A01.
INTERCOSTAL CORRODED BETWEEN BS 349-364 AT STRINGER 26 RT. FOUND TO BE OUT OF LIMITS. REMOVED THE INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND INSTALLED A NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND DWG NR SH670.32050, 10 CAT. MAJOR REPAIR.
FS 280 FRAME CORRODED BETWEEN STRINGERS 23RT-23LT. REMOVED CORROISON FROM FRAME IAW SRM 57-21-06-001-001-A01. MAJOR REPAIR.
CORRODED ANGLE AT BS 349, STR 20 RT. REMOVED CORROSION FROM ANGLE IAW SRM 53-21-101-002-A01. FOUND DAMAGE IS BEYOND THE ALLOWABLE LIMITS OF SRM 53-00-00-101-001-A01, ANGLE REPLACED.
SERVICE DOOR UPPER SEAL STRIKER CORRODED AT DRAIN HOLES. R & R CORRODED SERVICE DOOR LOWER SEAL STRIKER IAW SRM 51-42-06. LOCATED AND DRILLED NEW STRIKER SEAL IAW SRM 51-40-11-001-001-A01.
TCAS DOUBLER CORRODED BETWEEN FRAMES 295-310 AT STR 27. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED CORRODED DOUBLER IAW SRM 51-42-06-001-001-A01. TRANSFERED HOLES TO NEW DOUBLER IAW SRM 51-42-06-001-001-A01. INSTALLED TCAS DOUBLER IAW SRM 51-42-06-001-001-A01 AND DWG SH670-30023.
TWO STAND OFFS ARE UNSECURE ON FRAME BS 265 BETWEEN S24L-24R. BONDED THE STAND OFFS IAW SRM 51-22-00-001-001-A01. MAJOR REPAIR.
FRAME BS 333 CORRODED AFT SIDE BETWEEN S26L-26R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.
FWD FLOORBEAM ANGLE CORRODED AT BS 280. REMOVED FWD FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. INSTALLED NEW FLOORBEAM ANGLE IAW DWG PL CC670-34256 AND SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
SERVICE DOOR UPPER ANGLE CORRODED. REMOVED ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-15-001-001-A01. INSTALLED ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31996. MAJOR REPAIR.
FWD EQUIPMENT BAY FLOOR PANEL CRACKED RT SIDE BY ADG STOW PUMP APPROXIMATELY BS 193. REPAIRED IAW REO 670-53-11-509. MAJOR REPAIR.
FWD EQUIPMENT BAY FLOOR PANEL CRACKED LT SIDE APPROXIMATELY, BS 193. REPAIRED IAW EC/TC REO-670-53-11-509 AND GRO 670-53-11-509, REV B. MAJOR REPAIR.
LEFT ENGINE INLET COWL DENTED AT BOTTOM. FOUND DENTS TO BE OUT OF LIMITS IAW 54-11-01-101-A01. FINISHED MAPPING AND SUBMITTED FOR PERMANMENT REPAIR TO STS ENGINEERING. RECEIVED AND COMPLIED WITH EC/TC AND EA 32-2014-014.
RT AILERON OTBD RUB STRIP REQUIRES PERMANENT REPAIR. PERMANENT REPAIR TO RT AILERON OTBD RUB STRIP IAW SRM 51-22-00. COMPLIED WITH REO 670-57-61-006, REV D FOR PERMANAENT REPAIR TO RT AILERON RUB STRIP.
LT AILERON OTBD RUB STRIP REQUIRES PERMANENT REPAIR. COMPLIED WITH EC/TC, REO 670-57-61-006 PERMANENT REPAIR. COMPLIED WITH REO 670-57-61-006, REV D OF PERMANENT REPAIR. RECEIVED AND COMPLIED WITH ECTC REO 670-57-61-006-01.
MEGAPHONE SCREW RETAINERS DAMAGED. R & R THE MEGAPHONE IAW AMM 25-61-14 AND AIPC 25-61-14, FIG 1C, ITEM 5.
PAX DOOR DRAG ANGLE CRACKED AT ASSIST PULLEY. REMOVED DAMAGED DRAG ANGLE (AFT SIDE) ON PAX DOOR IAW SRM 51-42-06 AND 51-42-13. DRILLED UP AND INSTALLED NEW DRAG ANGLE IAW SRM 51-42-13 AND 51-42-22.
EMERGENCY LIGHTS LEFT ON, AND WILL NOT POWER UP. CHARGED BATTERY PACKS WITH APU POWER.
AFT F/A FLASHLIGHT INOPERATIVE. R & R BATTERIES IAW AMM 25-60-00. OPS CHECKED GOOD AT THIS TIME.
CEILING EMERGENCY LIGHT AT ROW 15 INOPERATIVE. RELAMPED EMERGENCY LIGHT IAW AMM 33-51-09, OPS CHECKED GOOD.
FLOOR LIGHT STRIP AT ROW 14 UNSECURE. R & R FLOOR LIGHT STRIP AT ROW 14 A & B IAW AMM 33-51-01.
PHOTOLUMINESCENT PLACARD ON THE RT SIDE OF GALLEY EMERGENCY EXIT DOOR IS MISSING INSTALLED PHOTOLUMINECENT PLACARD ON GALLEY SERVICE DOOR IAW AMM 11-30-00.
G-1 GALLEY EMERGENCY LIGHT INOPERATIVE. TROUBLESHOT AN FOUND WIRE AT FORWARD EDIT LIGHT AT FWD SERVICE DOOR IS BROKEN. REPAIRED IAW ESPM 20-33-00. OPS TESTED GOOD IAW AMM 33-51-00-710-801.
FRAME 320.10 CRACKED. LOCATED, DRILLED, AND INSTALLED IAW SRM 51-42-06-001-001-A01.
LEFT FS 280.00 WEB AFT FACE HAS CORROSION. REPLACED WEB IAW EC/TC REO 670-53-11-594.
CABIN LT FLOOR SUPPORT JUST AFT OF FS 280.00 IS CORRODED. REMOVE CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED CORROSION AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 53-21-43-101-001-A01. ALODINED, PRIMED AND PAINTED TREATED AREA AS REQUIRED IAW SRM 51-21-06-001-001-A01.
RT FLOOR SUPPORT JUST AFT OF FS 349.00 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT 3. FOUND OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. REPAIRED REO 670-53-21-854.
VERTICAL ANGLE AT PAX DOOR IS CORRODED AROUND NUTPLATES ON INBD AND OTBD SIDES. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND IT TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01 AND 51-21-06-001-001-A01. REMOVED ANGLE ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED SERVICEABLE PART IAW SRM TASKS 51-42-06-001-001 & 51-42-21-001-001-A01.
SEAT TRACK RBL 9, FS 835 TO 980 IS CORRODED. R & R SEAT TRACK IAW AMM'S 53-00-49-000-801 AND 53-00-49-400-801.
SEAT TRACK LBL 9, FS 835 TO 990 IS CORRODED. R & R WITH NEW FLOOR SEAT TRACK IAW AMM 53-00-49-000-801-A01 AND 53-00-49-400-801-A03.
AFT CARGO DOOR LOWER SILL ANGLE CORRODED FROM BS 1000.00 - 1051.30. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. MIN MATERIAL REMAINING IS .034", ORIGINAL IS .063" MATERIAL REMOVED IS .029". REPAIRED IAW REO 670-53-61-872.
AFT CARGO BAY, LT FLOOR SILL SCREW HOLES CORRODED FROM FS 985 TO 1000. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURES UT 3. MIN MATERIAL REMAINING IS .061" ORIGINAL IS .063" MATERIAL REMOVED IS .002". REPAIRED IAW REO 670-53-61-871.
AFT CARGO BAY, RT FLOOR SILL SCREW HOLES CORRODED FROM 1000 TO 1051.3. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. MIN MATERIAL REMAINING IS .058" ORIGINAL IS .063" MATERIAL REMOVED IS .005".
AFT CARGO BAY RT FLOOR SILL SCREW HOLES CORRODED FROM FS 1051.3 TO 1088.2. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURES UT 3. MIN MATERIAL REMAINING IS .057" ORIGINAL IS .063" MATERIAL REMOVED IS .006". REPAIRED IAW REO 670-53-61-871.
AFT CARGO BAY , LT FLOOR SILL SCREW HOLES CORRODED FROM FS 1051.3 TO 1088.2. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLENDED AREA IAW MAC NDT INSPECTION PROCEDURE UT 3. MIN MATERIAL REMAINING IS .061" ORIGINAL IS .063" MATERIAL, REMOVED IS .002". REPAIRED IAW REO 670-53-61-871.
SEAT TRACK RBL 27.00, FS 978 TO 1005 IS CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-802 AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-802.
SEAT TRACK RBL 9.0, FS 978 TO 1005 IS CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-802, INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-802.
RT FS 280.00 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. MATERIAL REMOVED 0.002" LESS 10 PERCENT IN LIMITS. PERFORMED LPI TYPE1 METHOD C ON BLEND AREA IAW SRM 51-12-00-001-001-A01 IAW MAC NDT PROCEDURE PT-1. NO INDICATIONS NOTED. RESTORED FINISH AS NEEDED AT REPAIR AREA IAW SRM 51-42-06-001-001-A01 AND SRM 51-21-11-001-001-A01.
RT FS 280.00 WEB AFT FACE HAS CORROSION. REPLACED BS 280 WEB IAW EC/TC REO 670-53-11-594 01.
COCKPIT CENTER FLOORBOARD AFT SUPPORT FWD OF FS 280.00 HAS CORROSION. REMOVED FLOOR SUPPORT AND INSTALLED SERVICEABLE SUPPORT IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
FS 280.00 CROSSBEAM HAS CORROSION. REPLACED 280 CROSSBEAM IAW EC/TC REO 670-53-11-047.
CORROSION FOUND ON INTERCOSTAL AT FS 364 AND S26L. REMOVED INTERCOSTAL IAW SRM 51-42-06-001-001. LOCATED & DRILLED SERVICEABLE INTERCOSTAL IAW SRM TASK 51-40-11-001-001. TREATED & PRIMED HOLES IAW SRM 51-21-16-001-001. INSTALLED INTERCOSTAL IAW SRM TASKS DWG SH670-32050, 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
SEAT TRACK LBL 9.0 FS 898 TO 1005 IS CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-802.
AFT CARGO COMPT, RT FLOOR SILL SCREW HOLES CORRODED FROM FS 985 TO 1000. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURES UT 3. MIN MATERIAL REMAINING IS .061" ORIGINAL IS .063" MATERIAL REMOVED IS .002". REPAIRED IAW REO 670-53-61-871.
CORROSION FOUND ON INTERCOSTAL AT FS 349-364 BETWEEN AND S26 AND 27R. REMOVED INTERCOSTAL IAW SRM 51-42-06-001-001. LOCATED & DRILLED SERVICEABLE INTERCOSTAL IAW SRM TASK 51-40-11-001-001. TREATED & PRIMED HOLES IAW SRM 51-21-16-001-001. INSTALLED INTERCOSTAL IAW DWG SH670-32050, SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
EMERGENCY LIGHT AT SERVICE DOOR EXIT, INOPERATIVE. FOUND BROKEN WIRE AT CONNECTOR BEHIND PANEL 232JZ. REPAIRED IAW ESPM 20-12-00. OPS TESTED GOOD IAW AMM 33-51-00-710-801.
EMERGENCY EXIT SIGN ON LT WINDSCREEN INOPERATIVE. CONNECTED CONNECTOR FOR THE EMERGENCY LIGHT IAW AMM 25-24-01. OPS CHECKED GOOD.
RT OVERWING EMERGENCY EXIT DOOR LOWER EXIT SIGN HAS SEVERAL LIGHTS BURNED OUT. RELAMPED RT OVERWING EMERGENCY DOOR EXIT SIGN IAW AMM 33-51-11.
RT AFT MOST EXTERNAL EMERGENCY LIGHT INOPERATIVE. RELAMPED RT AFT MOST EXTERNAL EMERGENCY LIGHT. OPS CHECKED GOOD IAW AMM 33-51-15.
AFT MOST CABIN CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED AFT MOST CABIN CEILING EMERGENCY LIGHT. OPS CHECKED GOOD.
FWD STOP BRACKET CRACKED ON MAIN CABIN DOOR. REINSPECTED FWD STOP BRACKET ON MAIN CABIN DOOR IAW REO 670-53-21-765. NO FURTHER DEFECTS NOTED AT THIS TIME.
EMERGENCY FLOOD LIGHT COVER MISSING. REPLACED LIGHT COVER IAW AMM 33-51-11.
CEILING EMGENCY LIGHT AT ROW 4 OUT. REPINNED CONNETOR P357 IAW ESPN 20-26-00 OPS CHECKED GOOD. ACFT OK FOR SERVICE.
NR 2 CABIN CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED NR 2 CABIN CEILING EMERGENCY LIGHT IAW AMM 33-51-09, OP'S CHECKED GOOD.
RT SIDE AFT EXTERNAL EMEGENCY LIGHT IS OUT. RELAMPED RT SIDE AFT EXTERNAL EMEGENCY LIGHT. OPS CHECK GOOD IAW AMM 33-51-02. ACFT OK FOR SERVICE.
NUMEROUS EMERGENCY LIGHTS OUT, INTERIOR/EXTERIOR. R & R THE NR 3 EPSU BATTERY PACK IAW AMM 33-51-17. OPS CHECKED GOOD.
FS 280 CROSSBEAM CORRODED IN SEVERAL PLACES. INSTALLED TEE BRACKETS AND COMPLIED WITH STEPS 9 TO 17 OF REO 670-53-11-047. ALL WORK DONE IAW REO 670-53-11-047. COMPLIED WITH EC/TC REO 670-53-11-047 AND REO 670-53-11-047, REV E.
RT SIDE SEAT RAIL BETWEEN FS 785.00 AND FS 863.00 HAS CORROSION. INSTALLED SIDE SEAT RAIL IAW 53-00-49-400-801.
SUPPORT ANGLE FOR RT WEB AT FS 280, RBL26 FOUND CRACKED. R & R SUPPORT ANGLE FOR RT WEB AT FS280, RBL 26 IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. (CLOSED)
TEE ANGLES AT 280 RBL9 & LBL9 FWD FLOORBEAM TO 280 ATTACHED ANGLES CORRODED. REMOVED UNSERVICEABLE TEE ANGLES AND REPLACED WITH SERVICEABLE TEE ANGLES. ALL WORK DONE IAW SRM 51-42-21-001-001-A01 AND SRM 51-42-22-001-001-A01.
COCKPIT FLOOR SUPPORT CORRODED BEYOND LIMITS. REMOVED COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
LT FS 280 WEB CORRODED AT LBL 12. REMOVED DAMAGED WEB IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. DRILLED NEW WEB IAW SRM 51-40-11-001-001-A01. WEB. INSTALL LT FS280, AT INSTALLED WEB IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01. RESTORED FINISH ON FASTENERS AND WEB IAW SRM 51-21-16-001-001-A01.
FS 280, CROSSBEAM CORRODED IN SEVERAL PLACES. REMOVED DAMAGED CROSSBEAM IAW SRM 51-42-06 AND 51-42-21. CUT NEW CROSSBEAM IAW SRM 51-40-11-001-001-A01. COMPLIED WITH STEP 2 OF REO 670-53-11-047. NO INDICATIONS NOTED. COMPLIED WITH STEPS 3-7 OR REO 670-53-11-047. COMPLIED WITH STEP 8 EXCLUDING FASTENERS THROUGH TEE BRACKETS. ALL WORK DONE FOR REO 670-53-11-047.
RT FS 280 WEB CORRODED AT RBL 12. REMOVED WEB DAMAGED FROM CORROSION IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. DRILLED NEW WEB IAW SRM 51-40-11-001-001-A01. INSTALLED WEB IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01. RESTORED FINISH ON FASTENERS AND WEB IAW SRM 51-21-16-001-001-A01.
ANGLE HAS CORROSION AT FS 364.00 AND STR 26R. REMOVED CORROSION FROM ANGLE IAW SRM 51-21-00-001-A01, SRM 51-42-06-001-A01. BLENDED AREA WITHIN ALLOWABLE DAMAGE LIMITS SRM 53-21-23-101-003-A01.
CORROSION ON INTERCOSTAL AT FS 364 AND STR 27RT. REMOVED CORROSION FROM INTERCOSTAL IAW SRM 51-21-00-001-A01, SRM 51-42-06-001-A01. BLENDED AREA FS 364 & STR 27R IS WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-21-23-101-003-A01.
CORROSION ON INTERCOSTAL AT FS 364 AND STR 27L. REMOVED CORROSION FROM INTERCOSTAL IAW SRM 51-21-00-001-A01, SRM 51-42-06-001-A01.
CORROSION AT FS 280 ON FLOORBEAM ANGLE THAT SECURES THE FWD END OF FLOOR BOARD PANEL 131 ALF. REMOVED CORRODED SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01 FOR SOLID RIVETS, IAW SRM 51-42-20-001-001-A01 FOR LOCK FASTENER, REMOVED NUT PLATES FROM CORRODED SUPPORT ANGLE AND INSTALLED THEM ON NEW SUPPORT ANGLE IAW SRM 51-42-10-001-001-A01, INSTALLED NEW SUPPORT IAW SRM 51-42-06-001-001-A01 FOT SOLID RIVETS, IAW SRM 51-42-20-001-001-A01 FOR LOCK FASTENER, PAINTED ASSY IAW SRM 51-21-16-001-001-A01 FINISH CODE A025 JR161745 10/19/10 2. APPLIED CORROSION INHIBITOR TO NEW SUPPORT ANGLE IAW SRM 51-21-11 7 D(1). REMOVED FOD FROM SURROUNDING AREA.
SEAT TRACK HAS CORROSION FROM FS680-693 LBL 9.00 ON THE INSIDE AND OUTSIDE OF TRACK. REMOVED SEAT TRACK. TRIMMED NEW SEAT TRACK TO DIMENTIONS OF OLD SEAT TRACK & MATCH DRILLED SEAT TRACK IAW REO 670-53-00-074. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.
SEAT TRACK HAS CORROSION ON INSIDE AND OUTSIDE OF SEAT TRACK FROM FS 485-FS 581 RBL 9.00. REMOVED SEAT TRACK. FITTED, TRIMMED, DRILLED & COUNTERSUNK IAW REPAIR EO 670-53-00-074, PARA 3. INSTALLED SEAT TRACK AT FS 485-FS 581 IAW AMM 53-00-49-000-801.
SEAT TRACK HAS CORRSION FROM FS581-680 LBL 9.00 ON INSIDE AND OUTSIDE OF TRACK. REMOVED SEAT TRACK. TRIMMED TO FIT NEW SEAT TRACK AND CUT BACK SCALLOP FLANGE IAW THE ORIGINAL TRACK. LOCATED, DRILLED AND COUNTERSTRUCK. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.
SEAT TRACK HAS CORROSION ON INSIDE AND OUTSIDE OF SEAT TRACK FROM FS 581-693.00 RBL 9.00. REMOVED SEAT TRACK. TRIMMED TO FIT NEW SEAT TRACK AND, CUT BACK SCALLOP FLANGE IAW THE ORIGINAL TRACK. LOCATED, DRILLED AND COUNTERSUNK. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.
STRINGER 26R CORRODED AT FS 303. REMOVED COATING. MEASURED CORROSION DAMAGE WITH DEPTH GUAGE (.033" MATERIAL LOSS) AND FOUND CORRODED AREA OUT OF LIMITS IAW SRM 51-21-00-AND SRM 53-00-00-101-001-A01. R & R STRINGER 26 RT FS 303.00 IAW SRM 51-42-06-002-001-A01.
SEAT TRACK HAS CORROSION ON INSIDE AND OUTSIDE OF TRACK AT FS 349.00, RBL 9.00. REMOVED & INSTALLED SEAT TRACK AT FS 350-485, RBL 9.00 IAW AMM 53-00-49-400-801.
SEAT TRACK HAS CORRISON AT FS 364.00, RBL 9.00. SEAT TO BE REPLACED. (CLOSED)
FRAME HAS CORROSION AT FS 310 AND BETWEEN STR 27 AND 26L. REMOVED COATINGS AND CORROSION IAW SRM 51-21-00-001-A01. BLENDED CORRODED AREAS IAW SRM 51-21-00-001-A01. PERFORMED UT THICKNESS MEASUREMENT ON BLEND AREA IAW MAC NDT INSP PROCEDURE UT-3 MINIMUN MATERIAL REMAINING IS .048". APPLIED A023 FINISH TO AREA BETWEEN STR 26L & 26R AT FS 310 ON FRAME FLANGE REF SRM 51-21-16-001-001-A01.
LT SIDE SEAT RAIL BETWEEN FS 863.00 AND FS 969.00 HAS CORROSION. CORROSION ON SEAT TRACK IS NOT WITHIN LIMITS IAW SRM 53-31-49. REMOVED & INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A03.
LT SIDE SEAT RAIL BETWEEN FS 677.00 AND FS 712.00 HAS CORROSION. CORROSION NOT WITHIN LIMITS IAW SRM 53-31-49 3(B)1. REMOVED SEAT TRACK IAW AMM 53-06-49-000-801. INSTALLED NEW SEAT TRACK AT FS 677 - 712 IAW AMM 55-00-49-400-801.
RT SIDE SEAT RAIL BETWEEN FS 485.00 AND FS 573.00 HAS CORROSION. CORROSION NOT WITHIN LIMITS IAW SRM 53-31-49 PARA 3(B) 1. REMOVED RT SIDE SEAT RAIL IAW AMM 53-00-49-000-801. INSTALLED RT SIDE SEAT RAIL BETWEEN FS 485.00 AND FS 573.00 IAW AMM 53-00-49-400-801.
RT SIDE SEAT RAIL BETWEEN FS 573.00 AND FS 677.00 HAS CORROSION. DAMAGE NOT WITHIN LIMITS IAW SRM 53-31-49, PARA 3(B)1. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-287 & REO 670-53-00-074-A. INSTALLED NEW SIDEWALL SEAT TRACK IAW AMM 53-00-49-400-801.
LT SIDE SEAT RAIL BETWEEN FS 573.00 AND FS 677.00 HAS CORROSION. MINOR GRANULAR AND PITTING FOUND, RECOMEND CORROSION REMOVAL AND TREATMENT. CONTINUE CLEANING SEAT TRACK. UPON FUTHER CORROSION REMOVAL THE FREQUENCY OF THE MINOR PITTING ON THE SEAT TRACK IS NOT WITHIN LIMITS IAW SRM 53-31-49, PARA.3(B). REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SENT TRACK BETWEEN FS 573.00 AND FS 677.00. IAW AMM 53-00-49-400-801-A03.
LT SIDE SEAT RAIL BETWEEN FS 485.00 AND FS 573.00 HAS CORROSION. MINOR PITTING AND SOME EXCEEDS .010 BUT NO LESS THAN 3" BETWEEN DAMAGE CORROSION REMOVAL AND TREATMENT REQUIRED IAW SRM 51-21-00 CONTINUE CLEANING SEAT TRACK. UPON FURTHER CORROSION REMOVAL THE FREQUENCY OF THE MINOR PITTING ON THE SEAT TRACK IS NOT WITHIN LIMITS IAW SRM 53-31-49, PARA 3(B)1 BETWEEN FS 485 TO 573. REMOVED SEAT TRACK AT LT SIDEWALL FS485 TO 573. REPLACED SEAT TRACK AT LT SIDEWALL FS 485 TO 573 IAW AMM CH 53-00-49-400-801.
RT SIDE SEAT RAIL BETWEEN FS 677.00 AND FS 712.00 HAS CORROSION. CORROSION NOT WITHIN LIMITS IAW SRM 53-31-49, PARA 3(B)1. REMOVED & INSTALLED NEW SEAT TRACK 51-670-37509-1 IAW AMM 53-00-49-400-801.
RT SIDE SEAT RAIL BETWEEN FS 712.00 AND FS 761.00 HAS CORROSION. CORROSION NOT WITHIN LINITS IAW SRM 53-31-49. REMOVED SEAT TRACK & INSTALLED AT RT FS 712-FS 761 IAW AMM 53-49-400-801.
RT SIDE SEAT RAIL BETWEEN FS 785.00 AND FS 863.00 HAS CORROSION. CORROSION NOT WITHIN LIMITS IAW SRM 53-31-49 PARA 3(B). REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-000-801.
RT SIDE SEAT RAIL BETWEEN FS 863.00 AND FS 969.00 HAS CORROSION. CORROSION NOT WITHIN LIMITS IAW SRM 53-31-49, PARA 3(B) I. REPLACE SEAT TRACK IAW AMM 53-00-49-000-801.
LEFT SIDE SEAT RAIL BETWEEN FS 785.00 AND FS 863.00 HAS CORROSION. CORROSION NOT WITHIN LIMITS IAW SRM 53-31-49, PARA 3 (B) REMOVED LT SIDE SEAT RAIL AND REPLACED IAW AMM 53-00-49-400-801.
LT SIDE SEAT RAIL BETWEEN FS 712.00 AND FS 761.00 HAS CORROSION. REMOVED & INSTALLED SEAT RAIL AT FS 712- 761 IAW AMM 53-00-49-400-801.
FLOOR PANEL 221ALF LT SUPPORT ANGLE CRACKED. REMOVED LT FLOOR SUPPORT ANGLE FOR FLOOR PANEL 221ALF IAW SRM 51-42-06-001-001-A01. NEW FLOOR SUPPORT ANGLE NEEDS TO BE INSTALLED. DRILLED NEW SERVICEABLE FLOOR SUPPORT ANGLE, INSTALLED CAM LOC RECEPTICALS IAW SRM 51-42-06-001-001-A01. NEW FLOOR SUPPORT ANGLE READY TO BE INSTALLED. OK TO INSTALL NEW FLOOR SUPPORT ANGLE. FLOOR SUPPORT ANGLE REQUIRES INSTALLATION. INSTALLED NEW SERVICEABLE FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01.
EMERGENCY LIGHT ON STATUS MESSAGE INTERMITTANTLY ILLUMINATES IN FLIGHT. CYCLE COCKPIT AND CABIN SWITCH, NO HELP. R & R NR 5 PCBP IN JB11 CONTAINING RELAY K135 IAW AMM 24-06-11. OPS CHK GOOD. (SDR CLOSED)
EMERGENCY LIGHT OVER THE RT EXIT EMERGENCY DOOR INOP. REPLACED BATTERY PACK IAW ASA AMM 33-51-17. OPS CK OK.
R & R BATTERY PACK IAW ASA AMM 33-51-17 OPS CK OK. (CLOSED)
FLT 5046. SLAT FAIL CAUTION MSG. LANDED FLAPS AT 45 SLATS AT ZERO [TOWER DECLARED AN EMERGENCY].
EMERGENCY EXIT ROWS EXIT SIGNS HAVE INOP BULBS.
OUTBOARD SPOILERON MESSAGE, O/B FLT SPOILER CAUTION MESSAGE. EMERGENCY DECLARED. FLT 5610 DEL 107 MINS.
RIGHT OVERWING EMERGENCY EXIT LIGHT INOP.
CABIN CEILING SECOND EMERGENCY LIGHT DO NOT ILLUMINATE.
VERTICAL ANGLE RIGHT STA 280 RBL 18 APPROX 18 IS CRACKED.
COCKPIT FLOOR LAND, AFT SIDE BADLY CORRODED. ALL WORK BEING COMPLIED WITH ON TASK CARD N/R-00099 IAW EO 670-53-11-047.
THE 280 BEAM CORRODED LBL 9-14. REMOVED AND REPLACED 280 CROSSBEAM IAW IS67053110026 AND REO 670-53-11-047.
RIGHT 280 WEB CORRODED. PREVIOUSLY BLENDED ON. REMOVED AND REPLACED RIGHT 280 WEB IAW CRJ 700 SRM 51-24-21 AND REO670-53-11-052. SUPPLEMENTAL - SDR CLOSED 04/13/07.
LEFT 280 WEB CORRODED. PREVIOUSLY BLENDED ON. REMOVED AND REPLACED LEFT 280 WEB IAW CRJ 700 SRM 51-42-00 AND REO 670-53-11-052. SUPPLEMENTAL - SDR CLOSED 04/13/07.
AFT MOST CEILING EMERGENCY LIGHT INOP.
EMERGENCY LIGHT ABOVE ROW 19 INOP. (CLOSED)
DURING A GROUND INSPECTION, THE OVERHEAD EMERGENCY LIGHT, AT ROW 4, WAS FOUND TO BE INOPERATIVE. (K)
DURING A C-CHECK IN MCN, THE PASSENGER DOOR TOP STEP HINGE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP HINGE IAW CRJ 200 AMM 52-10. (M)
DURING AN (A) CHECK, THE OVERHEAD EMERGENCY CEILING LIGHT AT ROW 4 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE UNDER THE CEILING PANEL TO THE NR 2 EMERGENCY CEILING LIGHT AT CONNECTOR J357. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)