N582CA
Registered owner: DELTA AIR LINES INC, GA (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.
174 reports on file, 2009-01-03 – 2024-10-06.
Part: PRESSURE DECK — MISALIGNED (ZONE 200) · airframe 35,389 hrs · 24,875 cycles
WHILE INCORPORATING SB 670SH-53-043 REV C, WE HAVE ENCOUNTERED MISMATCHED FACTORY PILOT HOLES @FS 843 LBL 18 COMMON TO THE LBL18 FLOOR BEAM AND PRESSURE BOX EXISTING HOLES. REPAIRED BY INSTALLING A FREEZE PLUG IAW MHIRJ REO 690-53-41-502 REV -- DATED 2024-10-11.
Part: BRACKET — NONE · airframe 35,389 hrs · 24,875 cycles
WHILE INCORPORATING SB 670SH-53-043 REV C, WE ARE UNABLE TO GET PROPER EDGE DISTANCE ON BOTH VOLUMETRIC FUSE BRACKETS SH698-75359-1S AND SH698-75355-1S DUE TO EXISTING AIRCRAFT FASTENER PITCH. FABRICATED AND INSTALLED BRACKETS IAW MHIRJ SNIEOS KSH670-35829-S88, SH698-75355-S11 AND SH698-75359-S10.
Part: FITTING — UNKNOWN · airframe 35,389 hrs · 24,875 cycles
WHILE PERFORMING SB 670BA-53-044 REVISION G DATED JUL05/2022 FOUND LH AND RH FITTINGS PN CC670-33562-001SB AND CC670-33563-001SB AT STR12A CANNOT BE INSTALLED IN ACCORDANCE WITH SERVICE BULLETIN INSTRUCTIONS DUE TO EXISTING RIVET PATTERN ON THE AIRCRAFT. TRIMMED FITTINGS AND INSTALLED IAW MHIRJ REOS 690-53-11-1868 REV - - DATED 2024-10-04 AND 690-53-11-1867 REV -- DATED 2024-10-9.
Part: BEAM — FAILED INSP (ZONE 200) · airframe 35,389 hrs · 24,875 cycles
LBL 9 BULKHEAD BEAM, I/B SIDE @ FS 693 HAS A PREVIOUS REPAIR ON TOP FLANGE COMMON TO THE FLOOR BEAM AND FLOORBOARD MOUNTING STRUCTURE. THIS REPAIR WAS DISCOVERED WHILE REMOVING STRUCTURE TO INCORPORATE SB 670SH-53-043 AND WILL REQUIRE A DEVIATION FROM ENGINEERING TO INSTALL TO COMPLY WITH SB REQUIREMENTS. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-21-001-001-A01, AND 51-42-06-001-001-A01, REFERENCING SB 670SH-53-043 REV C INSTALLATION FIGURE 105 SHEET 5 AND SHEET 7.
Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 34,949 hrs · 24,498 cycles
R/H AFT EMERGENCY EXIT DOOR, UPPER AFT FITTING IS CRACKED. REPAIRED DAMAGE I.A.W. ENDEAVOR AIR EA # CRJ952-16440 REV.IR, DATED 04/20/2024.
Part: HOUSING — CRACKED (ZONE 800) · airframe 34,949 hrs · 24,498 cycles
WHILE PERFORMING SDI OF MAIN AVIONICS COMPARTMENT DOOR HANDLE FOUND MULTIPLE INDICATIONS 50%FSH, FAILED NDT INSTALLED AVIONICS BAY DOOR HANDLE HOUSING AND FASTENERS IAW CRJ900 SRM 51-42-06-001-001-A01
Part: STRINGER — CORRODED (ZONE 200) · airframe 34,949 hrs · 24,498 cycles
STRINGER 19R FROM F.S.280.00 TO F.S.316.00 IS CORRODED AT MULTIPLE FASTENER LOCATIONS. INSTALLED NEW SERVICEABLE STRG 19R PN SH670-31632-1 FOR FS 280 - FS 316 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
Part: STRINGER — CORRODED (ZONE 100) · airframe 34,949 hrs · 24,498 cycles
STRINGER 20R CORRODED BETWEEN FS280 AND FS333. INSTALLED STRG 20R (PN SH670-31208-3) BETWEEN FS 280 - FS 316 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 34,949 hrs · 24,498 cycles
LBL 12.00 COCKPIT FLOOR BEAM IS CRACKED IN RADIUS AT FS280.00. REMOVED CRACKED BEAM AT LBL 12 FS280. FABRICATED AND INSTALLED NEW L/H FLOOR BEAM P/N CC670-33202-21 IAW CRJ 900 SRM 53-11-43-201-003-A01.
Part: STRINGER — CORRODED (ZONE 200) · airframe 34,949 hrs · 24,498 cycles
STRINGER 19RH IS CORRODED BETWEEN FS437-453 REMOVED AND INSTALLED NEW SERVICEABLE STRINGER 19R BETWEEN FS349 TO FS477 (PN# SH670-31103-4S) IAW CRJ900 51-42-06-001-001-A01.
Part: ANGLE — CORRODED (BS 379-394 S21R) · airframe 34,949 hrs · 24,498 cycles
"WATER WASTE SERVICE DOOR SURROUND DIAPHRAGM P/N SH670-32285-13 IS CORRODED ON OUTER SURFACE BETWEEN FS379.00 AND FS394.00, STR 21R. INSTALLED NEW SERVICEABLE SURROUND DIAPHRAGM PN SH670-32285-15 IAW CRJ 900 SRM 51-42-06-001-001-A01.EVALUATE AND BLEND CORROSION ON WASTE WATER SERVICE DOOR UPPER SURROUND DIAPHRAGM. CORRECTIVE ACTION: BLENDED CORROSION ON UPPER SURROUND DIAPHRAGM PN SH670-32285 WITH A NOMINAL THICKNESS OF 0.080"" AND MAX ALLOWABLE LIMIT OF 0.008"" IAW CRJ 900 SRM 51-21-06-001-001-A01 AND SRM 53-21-23-101-005-A02. MRT IS 0.052"" IS OUT OF LIMITS AND WILL REQUIRE REPLACEMENT. TOOL USED WVACT 203808 CAL DUE 30SEP24.LOCATE AND DRILL NEW SERVICEABLE SURROUND DIAPHRAGM PN SH670-32285-15. CORRECTIVE ACTION: LOCATED AND DRILLED NEW SERVICEABLE SURROUND DIAPHRAGM PN SH670-32285-15 IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALL 6 DOME NUTPLATES AROUND HOLE FOR VENT LINE ON SURROUND DIAPHRAGM. CORRECTIVE ACTION: INSTALLED 6 DOME NUTPLATES AROUND HOLE FOR VENT LINE ON SURROUND DIAPHRAGM IAW CRJ 900 SRM 51-42-06-001-001-A01. APPLY ""VENT"", ""DRAIN"", AND ""T-HANDLE"" DECALS. CORRECTIVE ACTION: INSTALLED ""DRAIN"" DECAL P/N: S7640-1 AND ""T-HANDLE"" DECAL P/N: S30318-1 IAW CJ900 AIPC 11-20-02-01M. LINE 4A CAN NOT BE SIGNED OFF TO A IPC CORRECTIVE ACTION: WORK PERFORMED IN TASK 4A IAW CRJ 900 AMM 20-60-04-400-801-A01.APPLY ""VENT"" DECAL. CORRECTIVE ACTION: INSTALLED VENT DECAL P/N S7201-1 IAW CRJ 900 AMM 20-60-04-400-801-A01.APPLY EDGE SEALANT, AND SEAL AROUND DOME NUTPLATES. CORRECTIVE ACTION: SEALED REWORKED AREAS AND DOME NUTPLATES IAW CRJ900 SRM 51-23-00-001-001-A01.APPLY PROTECTIVE SURFACE FINISH. CORRECTIVE ACTION: APPLIED PROTECTIVE SURFACE FINISH IAW CRJ 900 SRM 51-25-16-001-001-A01.303.6 LINE 5 IS INCORRECT CORRECTIVE ACTION: CORRECTED LINE 5 OF 303.6INTERCOSTAL LOCATED AT FS 349-364 AT RBL 37 WAS REMOVED FOR ACCESS IAW CRJ 900 SRM 51-42-21-001-001-A01. CORRECTIVE ACTION: REINSTALLED INTERCOSTAL LOCATED AT FS 349-364 AT RBL 37 IAW CRJ 900 SRM 51-42-21-001-001-A01.CABIN PRESSURIZATION LEAK TEST REQUIRED. CORRECTIVE ACTION: COMPLIED WITH LEAK TEST OF WASTE WATER SERVICE DOOR UPPER SURROUND DIAPHRAGM IAW CRJ900 AMM 52-00-00-790-801 (A01). LEAK TEST GOOD AT THIS TIME."
Part: ANGLE — CORRODED (ZONE 200) · airframe 34,949 hrs · 24,498 cycles
PAX DOOR MID SILL ANGLE IS CORRODED. REMOVED PAX DOOR MID SILL PN: SH670-31875-7 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICABLE PAX DOOR MID SILL PN: SH670-31875-7 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 34,949 hrs · 24,498 cycles
VERTICAL STAB., R/H FORWARD DRAG ANGLE IS CRACKED. REPAIRED DAMAGE I.A.W. CRJ900 SRM 55-31-00-201-001-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 34,949 hrs · 24,498 cycles
AFT CARGO STR 26R HAS CORROSION BETWEEN FS 1031 AND FS 1047. COMPLIED WITH ENDEAVOR EA CRJ953-16613 REV.IR DATED 5-7-2024.
Part: FLOOR SUPPORT — CORRODED (BS 1025-1037) · airframe 34,949 hrs · 24,498 cycles
PREVIOUS FLOOR BEAM REPAIR AT L.B.L 27.00 HAS CORROSION ON THE CAP AT F.S. 1025.00 TO F.S. 1037.00. REPAIRED DAMAGE I.A.W. BOMBARDIER CRJ900 SRM 53-00-41-201-001-A03.
Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 34,949 hrs · 24,498 cycles
VERTICAL STAB., L/H FORWARD DRAG ANGLE IS CRACKED. REPAIRED DAMAGE I.A.W. CRJ900 SRM 55-31-00-201-001-A01.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 34,949 hrs · 24,498 cycles
PAX DOOR FORWARD INTERCOSTAL DD5 IS CORRODED. REPLACED INTERCOSTAL I.A.W. CRJ900 SRM 51-40-1-001-001-A01 AND 51-42-06-001-001-A01.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 34,949 hrs · 24,498 cycles
PAX DOOR INTERCOSTAL DD7A MID CORRODED AND REQUIRES REPLACEMENT. INSTALLED NEW PAX DOOR INTERCOSTAL DD7 MID C ANGLE P/N 601R317052-1 IAW CRJ 900 SRM 52-42-21-001-001-A01
Part: INTERCOSTAL — CORRODED (BS 310-320 S20R) · airframe 34,949 hrs · 24,498 cycles
INTERCOSTAL BETWEEN FS 310 AND FS 319.70 ON STRG 20R IS CORRODED. UPON FURTHER INVESTIGATION FOUND STGR 20R INTERCOSTAL AT FS 310 TO FS 319.70 (PN SH670-32047-1) TO BE CORRODED BEYOND ALLOWABLE LIMITS IAW CRJ 900 SRM 53-21-23-101-002-A02 AND REQUIRES REPLACEMENT. RECEIVED, LOCATED, AND DRILLED SERVICEABLE STGR 20R INTERCOSTAL AT FS 310 TO 319.70 IAW CRJ 900 SRM 51-40-11-001-001-A01. REF. BARCODE IDENTIFIER HN00156280 FOR INSTALL.
Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 34,949 hrs · 24,498 cycles
PAX DOOR INTERCOSTAL DD4 FWD CORRODED AND REQUIRES REPLACEMENT. INSTALLED NEW PAX DOOR FWD INTERCOSTAL DD4 P/N 601R318093-1 IAW CRJ 900 SRM 51-42-06-001-001-A01
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 34,949 hrs · 24,498 cycles
PAX DOOR INTERCOSTAL DD3 FWD CORRODED AND REQUIRES REPLACEMENT. INSTALLED NEW PAX DOOR FWD INTERCOSTAL DD3 IAW CRJ 900 SRM 51-42-06-001-001ÿ½A01
Part: DOOR — CORRODED (LT OVERWING) · airframe 34,949 hrs · 24,498 cycles
L/H AFT OVERWING EMERGENCY EXIT DOOR S/N B1394 TOP FORMER IS CRACKED. RECEIVED ENDEAVOR AIR EA CRJ952-16638 REV IR (P1) DATED 5/12/2024. COMPLIED WITH STEPS 1,2,4-7 OF ENDEAVOR AIR EA CRJ952-16638 REV IR (P1) DATED 5/12/2024. REMOVED DOOR LINING IAW CRJ900 AMM 25-26-09-000-801-A01. INSTALLED DOOR LINING IAW CRJ900 AMM 25-26-09-400-801-A01. INCORRECT REFERENCE USED IN STEP 1B FOR INSTALL OF DOOR LINING. CORRECT REFERENCE FOR INSTALL OF DOOR LINER PANEL IS IAW CRJ 900 AMM 25-26-09-000-801 (CONFIG A02). PERFORMED EDDY CURRENT ON L/H AFT EMERGENCY EXIT UPPER FORMER CUTLINE EDGES IAW ENDEAVOR AIR EA CRJ 952-16638 REV-- (P1) DATED 5-12-2024 STEP 3. NO INDICATIONS NOTED AT THIS TIME. C/W HFEC ON LH AFT O/W EXIT DOOR FORMER NEWLY FABRICATED REPAIR PARTS IAW ENDEAVOR AIR CRJ952-16638 REV IR DATED 5/12/2024 STEP 8. NO INDICATIONS NOTED AT THIS TIME. COMPLY WITH STEPS 9-11 (NDT RII BUYBACK, INSTALLATION, AND PAINT) OF ENDEAVOR AIR EA CRJ952-16638 REV IR (P1) DATED 5/12/2024. COMPLIED WITH STEPS 9-11 (NDT RII BUYBACK, INSTALLATION, AND PAINT) OF ENDEAVOR AIR EA CRJ952-16638 REV IR (P1) DATED 5/12/2024. CONFIRM RIGGING IS WITHIN AMM LIMITS IAW STEP 12 OF ENDEAVOR AIR EA CRJ952-16638 REV IR (P1) DATED 5/12/2024. COMPLIED WITH STEP 12 OF ENDEAVOR EA CRJ952-16638 REV IR DATED 5/12/24. RIG CHECK GOOD. DEFER IAW STEP 13 OF ENDEAVOR AIR EA CRJ952-16638 REV IR (P1) DATED 5/12/2024. COMPLIED WITH STEP 13 OF ENDEAVOR EA CRJ952-16638 REV IR DATED 5/12/24. FINAL REV REQUIRED IAW STEP 14 OF ENDEAVOR AIR EA CRJ952-16638 REV IR (P1) DATED 5/12/2024. RECEIVED FINAL EA. REPAIRED LH AFT EMERGENCY EXIT DOOR IAW ENDEAVOR EA CRJ952-16638 REV IR DATED 5/12/24
Part: STRINGER SPLICE — CORRODED (BS 469-485 S19R) · airframe 34,949 hrs · 24,498 cycles
STGR 19R SPLICE IS CORRODED BETWEEN F.S. 469 TO F.S. 485. STGR 19R SPLICE IS CORRODED BETWEEN F.S. 469 TO F.S. 485. DAMAGE REQUIRES EVALUATION. FOUND STRINGER SPLICE PN: SH670-33264-1 AT STR 19R AND FS 477.40 TO BE CORRODED OUT OF LIMITS IAW CRJ-900 SRM 53-00-00-101-001-A01 DUE TO DEPTH OF CORROSION AND CORROSION DAMAGE ACROSS MULTIPLE ELEMENTS. DEEPEST DAMAGE DEPTH IS .021. STRINGER SPLICE PN: SH670-33264-1 AT STR 19R AND FS 477.40 REQUIRES ENGINEERING OR REPLACEMENT. REMOVED SPLICE (SH670-33264-1) STRINGER #19R/H BETWEEN F.S.477 TO 485 IAW CRJ900 SRM 51-42-06-001-001-A01. REMOVED 6EA CLIPS (P/N: SH670-35625-1), 1EA CLIP (P/N: SH670-35625-2) BETWEEN F.S.333 TO F.S. 477.40, STGR #19, IAW CRJ900SRM 51-42-06-001-001-A01. FOR ACCESS. INSTALLED 6EA CLIPS (P/N: SH670-35625-1), 1EA CLIP (P/N: SH670-35625-2) BETWEEN F.S.333 TO F.S. 477.40, STGR #19, IAW CRJ900SRM 51-42-06-001-001-A01. REMOVED CABIN DISTRIBUTION (GG670-95616-2) IAW CRJ900 AMM 21-23-04-000-801-A06. FOR ACCESS. INSTALLED ABOVE FLOOR BOTTOM DUCT FS469 TO FS485 IAW CRJ 900 AMM 21-23-04-400-801-A06 LEAK CHECK REQUIRED LEAK CHECK OF THE ABOVE FLOOR BOTTOM DUCT FS469-FS485 GOOD IAW CRJ900 AMM 21-23-00-790-801-A01 STRINGER SPLICE REQUIRES ENGINEERING OR REPLACEMENT REMOVED STRINGER SPLICE IAW CRJ900 SRM 51-42-06-001-001-0A01. LOCATE AND DRILL NEW STRINGER SPLICE (P/N:SH670-33264-1). LOCATED AND DRILLED NEW STRINGER SPLICE (P/N:SH670-33264-1) IAW CRJ900 SRM 51-40-11-001-001-A01 NEW STRINGER SPLICE (P/N:SH670-33264-1) REQUIRES INSTALL. INSTALLED NEW STRINGER SPLICE (P/N:SH670-33264-1) IAW CRJ900 SRM 51-42-06-001-001-A01. REQUIRES FINISH SURFACE. COMPLETED FINISH SURFACE IAW CRJ900 SRM 51-41-16-001-001-A01.
Part: FRAME — CORRODED (BS 847 S26L&R) · airframe 34,949 hrs · 24,498 cycles
FRAME CORRODED AT FS 847+32 BETWEEN STRINGERS 26L AND 26R. REPAIRED DAMAGE I.A.W. CRJ 900 SRM 53-00-06-201-001-A01.
Part: FRAME — CRACKED (ZONE 200) · airframe 34,949 hrs · 24,498 cycles
RH FRAME FS333 CRACKED BETWEEN STGR1R AND STGR2R REPAIRED DAMAGE RH FRAME FS333 BETWEEN STGR1R AND STGR2R IAW EA NO. CRJ953-16546 DATED: 5/10/2024 REV IR
Part: FORMER — CORRODED (PAX DOOR) · airframe 34,949 hrs · 24,498 cycles
PAX DOOR FS329.41 FOUND TO BE CORRODED REQUIRES REPLACEMENT REMOVED FORMER AT FS 329.14 IAW CRJ900 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. INSTALLED NEW FORMER AT F/S 329.14 BETWEEN DD4 AND DD5 P/N 601R318088-3 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. NEW SERVICEABLE FORMER AT FS 329.41 LOCATED AND DRILLED IAW CRJ900 SRM 51-40-11-001-001-A01.
Part: FLOOR SUPPORT — CORRODED (BS 693-752) · airframe 34,949 hrs · 24,498 cycles
RBL 9 FLOOR BEAM CAP CORRODED AROUND NUTPLATE HOLES FROM FS693 TO FS752.50 REPAIRED RBL9 FLOOR BEAM CAP IAW MHIRJ REO 690-53-41-470 REV -- DATED 2024-06-13.
Part: STRINGER — CORRODED (BS 549-565 S20R) · airframe 34,949 hrs · 24,498 cycles
STRINGER20RH @ FS549-565 IS CORRODED. S20R @ FS 549-565 IS CORRODED REQUIRES EVAL BLENDED OUT DAMAGE IAW CRJ900 SRM 51-21-06-001-001-A01 NO DAMAGE ALLOWED IN AREA PER CRJ900 SRM 53-31-03-101-003-A04 REPAIR REQUIRED STGR 20R FROM FS 477-613 REQUIRES INSTALL INSTALLED STGR 20R FROM FS 477- 613 IAW CRJ 900 SRM 51-42-06-001-001-A01 STGR 20R SPLICE AT FS 477 REQUIRES INSTALL INSTALLED STGR 20R SPLICE AT FS 477 IAW CRJ900 SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01. BRACKET ON STGR 20R BETWEEN FS 597-613 REQUIRES INSTALL INSTALLED BRACKET ON STGR 20R BETWEEN FS 597-613 IAW CRJ 900 SRM 51-42-13-001-001-A01. CRJ 900 SRM STRINGER SPLICE REPAIR DOES NOT APPLY TO STRINGER 20, ENGINEERING DISPOSITION REQUIRED FOR PERMANENT REPAIR. COMPLIED WITH EA CRJ953-16637 REV IR DATED 5/12/2024DISPLACED STRINGER 20R CLIPS FROM FS 501 TO FS 613 FOR ACCESS, IAW CRJ -900 SRM 51-42-06-001-001-A01. INSTALLED STRINGER CLIPS COMMON TO STR 20R BETWEEN F.S 501 TO F.S 613 IAW CRJ900 SRM 51-42-06-001-001-A01. DISPLACED 6EA WIRE LOOMS BETWEEN RH BELOW FLOOR FS661 - FS661+90 BY REMOVING 12EA SCREWS AND 12 WASHERS INSTALLED 6 WIRE LOOMS ON RH SIDE UNDERFLOOR BETWEEN FS661 - FS661+90 12 SCREWS AND 12 WASHERS IAW CRJ900 AMM 20-21-00-910-801-A01. INSTALLED EWIS PROTECTION BETWEEN RH BELOW FLOOR FS661 - FS661+90 IAW CRJ900 AMM 20-70-00-910-801-A01 REMOVED EWIS PROTECTION BETWEEN RH BELOW FLOOR FS661 - FS661+90 IAW CRJ900 AMM 20-70-00-910-801-A01. REMOVED EWIS WIRE LOOMS BETWEEN FS477 TO FS693 IAW CRJ900 SRM 51-41-02-001-001-A01 INSTALLED EWIS WIRE LOOMS FS477 TO FS693 IAW CRJ900 AMM 20-21-00-910-801-A01 NDT REQUIRED PERFORMED AN EDDY CURRENT INSPECTION ON FS549-FS565 STRINGER 20R CUTLINE EDGES, REPAIR PARTS, AND AFFECTED FASTENER HOLES IAW ENDEAVOR AIR EA CRJ953-16637 REV--(IR) DATED 5/12/2024 STEPS 3, 8, AND 10. NO INDICATION NOTED AT THIS TIME
Part: STRINGER — CORRODED (BS 985 S21L) · airframe 34,949 hrs · 24,498 cycles
AFT CARGO STR 21L HAS CORROSION AFT OF FS 985.00. AFT CARGO STR 21L HAS CORROSION AFT OF FS 985.00. REMOVED CORROSION AFT CARGO STR 21L, AFT OF FS 985.00, IAW CRJ 900 SRM 51-21-06-001-001-A01. REQUIRE UT FOR CHECK THICKNESS (NDT) PERFORMED UT THICKNESS OF STRINGER 21L FS985 REWORKED AREA IAW CRJ 900 NDTM PART 1 51-20-004-270-A01 REV 36 DATED 2/8/22. FOUND LOWEST REMAINING THICKNESS TO BE 0.049"" OR GREATER UT MEASUREMENTS REQUIRE EVALUATION. NO DAMAGE ALLOWED IN ATTACHED FLANGE OF STGR IAW CRJ900 SRM 53-61-03-101-003-A02. ENGINEERING DISPOSITION REQUIRED. REPAIR STGR 21L CRJ900 SRM 53-00-03-201-001-A02 INSTALLED STRINGER REPAIR AT STGR 21L BETWEEN FS 1000 FS 1015 IAW CRJ900 SRM 53-00-03-201-001-A02. REF TO TASK 9A FOR STRINGER SEGMENT REPLACEMENT. INSTALLED NEW SERVICEABLE STR 21L SEGMENT P/N MM670-35151-031 BETWEEN FRAME STATION 977 AND 1007.5 IAW CRJ 900 SRM 51-42-06-001-001-A01. REMOVED/ INSTALLED STR 21L CLIP COMMON TO 1007.5 AND PARTIALLY REMOVED CLIP COMMON TO FS 997 TO FACILITATE STR 21 REMOVAL IAW CRJ 900 SRM 51-42-06-001-001-A01. REMOVED / INSTALLED SPLICE N/P MM670-36418-001 AT FS 985.00, IAW CRJ 900 SRM 51-42-06-001-001-A01. RECEIVED NEW STGR 21 P/N: MM670-35151-031 REQUIRES LOCATED AND DRILLED. LOCATED DRILLED AND DEBURRED NEW STGR 21 P/N: MM670-35151-031 IAW CRJ900 SRM 51-40-11-001-001-A01. APPLIED CIC IN WORKED AREA IAW SRM 51-21-11-001-001 A01 "
Part: INTERCOSTAL — CORRODED (BS 865-881 S21R) · airframe 34,949 hrs · 24,498 cycles
INTERCOSTAL AT FS865.00-FS881.00 @STGR21R IS CORRODED. INSTALLED NEW SERVICEABLE INTERCOSTAL (PN: SH690-37121-1S) AT STRG 21R BETWEEN FS 865 TO FS 881 IAW CRJ900 SRM 51-42-06-001-001-A01
Part: STRINGER — CORRODED (ZONE 100) · airframe 34,949 hrs · 24,498 cycles
AFT CARGO STRINGER 26L HAS CORROSION BETWEEN FS1069-FS1088. REPAIRED DAMAGE I.A.W. CRJ900 SRM 53-00-03-201-001-A02.
Part: HANDLE — CRACKED (PAX DOOR) · airframe 34,949 hrs · 24,498 cycles
PAX DOOR INNER HANDLE CRACKED. REMOVED AND REPLACED HANDLE I.A.W. 51-40-11-00-001-001-A01 AND 51-43-00-001-001-A01.
Part: DOOR FRAME — CORRODED (ZONE 800) · airframe 34,949 hrs · 24,498 cycles
PAX DOOR F.S. 320 FRAME IS CORRODED BETWEEN INTERCOSTAL DD4 AND DD5. REMOVED PAX DOOR FS320 FRAME IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. RECEIVED NEW F/S 320 FRAME P/N 601R318032-5 , LOCATED AND DRILLED IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW PAX DOOR F/S320 FRAME P/N 601R318032-5 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
Part: BRACKET — CORRODED (ZONE 800) · airframe 34,949 hrs · 24,498 cycles
PAX DOOR BRACKET ON FWD INTERCOSTAL DD5 CORRODED REQUIRES REPLACEMENT PAX DOOR BRACKET ON FWD INTERCOSTAL DD5 INSTALLED IAW CRJ900 SRM 51-42-06-001-001-A01
Part: ANGLE — CORRODED (DOOR SILL) · airframe 34,949 hrs · 24,498 cycles
PAX DOOR MID SILL ANGLE IS CORRODED AROUND SCREW HOLES. UPON FURTHER INVESTIGATION, FOUND PAX DOOR MID CAP ANGLE P.N. SH670-31825-7 TO BE OUT OF LIMITS DUE TO CORROSION ON MULTIPLE ELAMENTS AND IN EXCESS OF OVER 40% OF MATERIAL THICKNESS IAW CRJ900SRM TASK 53-21-23-101-001-A02. LOCATED AND DRILL SILL SH670-31825-9 IAW CRJ900 SRM 51-40-11-001-001-A01. REPLACED PAX DOOR MID CAP ANGLE P.N. SH670-31825-7 IAW CRJ 900 SRM 51-41-02-001-001-A01.
Part: BRACKET — CRACKED (ZONE 800) · airframe 34,949 hrs · 24,498 cycles
GALLEY SERVICE DOOR STABILIZER BAR IS CRACKED. GALLEY SERVICE DOOR STABILIZER BAR BRACKET REQUIRES REPLACEMENT. REMOVED GALLEY SERVICE DOOR STABILIZER BAR BRACKET IAW CRJ 900 AMM 52-41-27-400-801-A01. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE BRACKET PN: CC670-38380-1 IAW CRJ 900 AMM 52-27-400-801-A01 AND CRJ 900 SRM 51-40-11-001-001-A01. GALLEY DOOR OPS CHECK REQUIRED. PERFORMED OPS CHECK OF GALLEY SERVICE DOOR IAW CRJ 900 AMM 52-41-00-710-801-A01, OPS CHECK GOOD AT THIS TIME.
Earlier reports · 2009–2020 · 138 reports
2020
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,026 hrs · 20,468 cycles
ON PREFLIGHT EMERGENCY LIGHTS IN ROW 13 DO NOT WORK-SIDE WALL & OVERHEAD LIGHTS. R & R NR 2 BATTERY PACK, IAW CRJ 900 AMM 33-51-17. OPERATIONS CHECK GOOD NO FURTHER DEFECTS NOTED.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,007 hrs · 20,450 cycles
REAR FACE OF CEILING EMERGENCY EXIT LT AND ROW 13 LOWER EMERGENCY EXIT LIGHTS NOT ILLUMINATED DURING TEST. REMOVED AND REPLACED BATTERY ASSEMBLY PS 37. P/N OFF: AD-2013-1A SN: 71935; P/N ON: 2013-1ASMI SN: 10096. OPERATIONS CHECK GOOD, IAW CRJ-900 33-51-17.
2019
Part: HINGE FITTING — CORRODED · airframe 28,468 hrs · 19,028 cycles
CORROSION FOUND ON THE LT & RT HINGE FITTINGS AT THE NLG STRUCTURE. THE FITTINGS WERE REPLACED IAW SRM 51-42-20-001-001-A01.
Part: PLATE — CORRODED (CARGO DOOR) · airframe 28,468 hrs · 19,028 cycles
CORROSION ON PLATE LOWER AT FWD BAGGAGE BAY DOOR, THE PLATE WAS REPLACED IAW AMM 52-35-07-400-802 ( CONFIG. A02 ) FIGURE 410.
Part: STRINGER — CORRODED (BS 280-327) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION ON STRINGER 25L, BS 280 - 327 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND 51-42-20-001-001-A01. "
Part: RECEPTACLE — CRACKED (FUSELAGE) · airframe 28,468 hrs · 19,028 cycles
CRACK FOUND IN RECEPTACLE PLATE AT FUSELAGE. THE RECEPTACLE PLATE WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-20-001-001-A01.
Part: CANISTER — CRACKED (RT WG FUEL CELL) · airframe 28,468 hrs · 19,028 cycles
CRACK IN CANISTER, WELDED NO.3 IN STA. WS148 AT RH MAIN FUEL TANK. REPAIRED PER REO 670-57-42-577 REV--. AND FUEL LEAK CHECK WAS PERFORMED PER AMM 28-11-00-790-801-A01 AND NO LEAK WAS FOUND.
Part: CANISTER — CRACKED (LT WG FUEL CELL) · airframe 28,468 hrs · 19,028 cycles
CRACK FOUND IN CANISTER, WELDED NR 3 AT LWS 148 IN THE LT MAIN FUEL TANK. REPAIRED IAW REO 670-57-42-577 REV--. AND FUEL LEAK CHECK WAS PERFORMED PER CRJ-900 AMM 28-11-00-790-801-A01 AND NO LEAK WAS FOUND "
Part: COAMING — WORN · airframe 28,468 hrs · 19,028 cycles
WEAR FOUND ON LOWER COAMING AT THE AFT BAGGAGE DOOR CUT-OUT. THE LOWER COAMING WAS REPLACED IAW SRM 51-41-02-001-001-A01 PAR 6.
Part: DRAIN — CORRODED (BS 649-409) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION ON SILLS IN STA. FS= 349 TO FS= 409 BETWEEN 41RBL TO 46RBL AT PAX CABIN FWD WET AREA. ON SILLS IN STA. FS= 349 TO FS= 409 BETWEEN 41RBL TO 46RBL AT PAX CABIN FWD WET AREA WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-20-001-001-A01,CRJ900 SRM 51-42-13-001-001-A01
Part: INTERCOSTAL — CORRODED (BS 349-364) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION FOUND ON INTERCOSTAL, BS 349 TO 364 NEAR STRINGER 27 IN THE MAIN AVIONICS COMPARTMENT. INTERCOSTAL WAS REPLACED IAW SRM 51-42-06-001-001-A01 PAR. 6.C, AND SRM 51-42-20-001-001-A01 PAR. 6.
Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION FOUND ON FLOORBEAM ANGLE AT BS 280 BETWEEN LBL 11TO RBL 11. FLOORBEAM ANGLE WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-20-001-001-A01.
Part: STRINGER — CORRODED (BS 337-364) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION FOUND ON STRINGER 24R, BS 337 TO 394 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPAIRED RM 53-00-03-201-001-A02, FIG. 53-00-03-995-807.
Part: SUPPORT ANGLE — CORRODED (BS 346) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION ON PROTECTION PLATE SUPPORT ANGLE AT BS 346 BETWEEN RBL 41 TO 44 AT THE GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. THE SUPPORT ANGLE WAS REPLACED IAW SRM 51-42-06-001-001-A01 PAR 6C.
Part: FLOOR SUPPORT — CRACKED (BS 279) · airframe 28,468 hrs · 19,028 cycles
CRACK ON THE LONGITUDUNAL FLOOR SUPPORT RBL 12, BS 279. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-11-43-201-003-A01, AND FIGURE 53-11-43-995-819.
Part: DOUBLER — CORRODED (BS 333-349) · airframe 28,468 hrs · 19,028 cycles
CORROSION WAS FOUND ON THE C CHANNEL DOUBLER AT BS 333 TO 349 BETWEEN STRINGERS 24R & 25R IN THE MAIN AVIONICS COMPARTMENT. THE DOUBLER WAS REPLACED IAW SRM 51-42-06-001-001-A01 PAR 6.C.
Part: DIAPHRAGM — CRACKED (BS 797-807) · airframe 28,468 hrs · 19,028 cycles
DURING REMOVAL OF THE MLG WHEEL BINS RELATED WITH TASK 900-27-900-112 STEP 5, A CRACK IN THE FAIRING SUPPORT DIAPHRAGM BS 797 - 807, LBL 35 - RBL 35. THE FAIRING SUPPORT DIAPHRAGM WAS REPLACED IAW SRM 51-41-06-001-001-A01, PAR 6.C, AND SRM 51-42-20-001-001-A01, PAR. 6.C.
Part: STRINGER SPLICE — CORRODED (BS 327-337) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION WAS FOUND ON STRINGER SPLICE 26R, BS 327 TO 337, IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER SPLICE WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-20-001-001-A01.
Part: FRAME — CORRODED (BS 349) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION ON FRAME BS 349 BETWEEN STRINGERS 25L TO 25R IN THE MAIN AVIONICS COMPARTMENT. THE FRAME WAS REPLACED IAW SRM 51-42-06-001-001-A01 PAR. 6.C, AND SRM 51-42-20-001-001-A01 PAR. 6.
Part: STRINGER — CORRODED (BS 337-394) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION FOUND ON STRINGER 26R, BS 337 TO 394 IN THE MAIN AVIONICS COMPARTMENT. STRINGER WAS REPAIRED IAW SRM 51-42-06-001-001-A01 PAR. 6.C, AND SRM 51-42-0-001-001-A01 PAR. 6.
Part: STRINGER SPLICE — CORRODED (BS 327-337) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
DURING REPLACEMENT OF DRY LINERS RELATED WITH TASK R25120, CORROSION WAS FOUND ON STRINGER SPLICE 23R, BS 327 TO 337 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER SPLICE WAS REPLACED IAW SRM 51-42-06-001-001-A01 PAR 6. AND SRM 51-42-20-001-001-A01 PAR 6.C
Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 28,468 hrs · 19,028 cycles
CORROSION FOUND ON THE FLOOR SUPPORT BS 280 TO 319, BETWEEN RBL 41 TO RBL 46 IN THE PAX CABIN FWD WET AREA. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND 51-42-10-001-001-A01.
Part: ANGLE — CORRODED (BS 349-364) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION FOUND ON ANGLE ATTACHED TO STRINGER 26R, BS 349 TO 364 IN THE MAIN AVIONICS COMPARTMENT. THE ANGLE WAS REPLACED IAW SRM 51-42-06-001-001-A01 PAR. 6.C.
Part: STRINGER — CORRODED (BS 337-394) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION FOUND ON STRINGER 27, BS 337 TO 354 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-20-001-001-A01.
Part: STRINGER SPLICE — CORRODED (BS 327-337) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION WAS FOUND ON THE STRINGER SPLICE 25L, BS 327 TO 337 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER SPLICE WAS REPLACED IAW SRM 51-42-06-001-001-A01, PAR 6.C, AND SRM 51-42-20-001-001-A01, PAR. 6.
Part: STRINGER SPLICE — CORRODED (BS 327-337) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
DURING REPLACEMENT OF DRY LINERS RELATED WITH TASK R25120, CORROSION WAS FOUND ON STRINGER SPLICE 22R, BS 327 TO 337 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER SPLICE WAS REPLACED IAW SRM 51-42-06-001-001-A01 PAR 6. AND SRM 51-42-20-001-001-A01 PAR 6.C.
Part: SUPPORT ANGLE — CORRODED (BS 339) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION WAS FOUND ON THE PROTECTION PLATE SUPPORT ANGLE AT BS 339 BETWEEN RBL 41 TO 44 AT THE GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. THE SUPPORT ANGLE WAS REPLACED IAW SRM 51-42-06-001-001-A01, PAR 6C.
Part: STRINGER — CORRODED (BS 280-327) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION FOUND ON STRINGER 26R, BS 280 TO 327 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01, PAR. 6.C, AND SRM 51-42-20-001-001-A01, PAR. 6
Part: STRINGER — CORRODED (BS 337-394) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION FOUND ON STRINGER 25R, BS 337 TO 394 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPAIRED IAW SRM 51-42-06-001-001-A01 PAR. 6.C, AND SRM 51-42-20-001-001-A01 PAR. 6.
Part: SUPPORT PLATE — CORRODED (BS 329) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION WAS FOUND ON THE PROTECTION PLATE SUPPORT AT BS 329 BETWEEN RBL 41 TO 44, AT THE GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. THE SUPPORT WAS REPLACED IAW SRM 51-42-21-001-001-A01, PAR 6C.
Part: STRINGER — CORRODED (BS 337-394) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION FOUND ON STRINGER 25L, BS 337 TO 394 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01 PAR. 6.C, AND SRM 51-42-20-001-001-A01 PAR. 6.
Part: STRINGER SPLICE — CORRODED (BS 327-337) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION WAS FOUND ON STRINGER SPLICE 24R, BS 327 TO 337 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER SPLICE WAS REPLACED IAW SRM 51-42-06-001-001-A01 PAR. 6.C, AND SRM 51-42-20-001-001-A01 PAR. 6.
Part: SUPPORT PLATE — CORRODED (BS 339) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION WAS FOUND ON THE PROTECTION PLATE SUPPORT BS 339 BETWEEN RBL 41 TO 44, AT THE GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. THE SUPPORT WAS REPLACED IAW SRM 51-42-21-001-001-A01, PAR 6C.
Part: STRINGER SPLICE — CORRODED (BS 327-337) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION FOUND ON STRINGER SPLICE 25R, BS 327 TO 337 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER SPLICE WAS REPLACED IAW SRM 51-42-06-001-001-A01 PAR. 6.C, AND SRM 51-42-20-001-001-A01 PAR. 6.
Part: STRINGER SPLICE — CORRODED (BS 327-337) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION WAS FOUND ON STRINGER SPLICE 27, BS 327 TO 337, IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER SPLICE WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-20-001-001-A01.
Part: STRIKER — CORRODED (BS 319-349) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION FOUND ON THE LOWER STRIKER, BS 319 TO 349, RBL44 AT THE GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. THE STRIKER WAS REPLACED IAW SRM 51-42-06-001-001-A1 PAR 6C.
Part: STRINGER SPLICE — CORRODED (BS 327-337) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION WAS FOUND ON STRINGER SPLICE 26L, BS 327 TO 337 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER SPLICE WAS REPLACED IAW SRM 51-42-06-001-001-A01 PAR. 6.C, AND SRM 51-42-20-001-001-A01 PAR. 6.
Part: STRINGER — CORRODED (BS 319-333) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION WAS FOUND ON STRINGER 27, BS 319 TO 333 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-20-001-001-A01.
Part: DOUBLER — CORRODED (BS 295-310) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION WAS FOUND ON THE INTERNAL PRODUCTION DOUBLER AT BS 295 - 310, BETWEEN STRINGERS 26L TO 26R IN THE MAIN AVIONICS COMPARTMENT. THE DOUBLER WAS REPLACED IAW SRM 51-42-06-001-001-A01.
Part: STRINGER — CORRODED (BS 280-327) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION FOUND ON STRINGER 25R, BS 280 TO 327 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-20-001-001-A01.
Part: STRINGER — CORRODED (BS 280-327) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION ON STRINGER 26L, BS 280 - 327 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-20-001-001-A01. "
Part: CHANNEL — CRACKED (FAIRING) · airframe 28,468 hrs · 19,028 cycles
CRACKED AFT FAIRING PANEL C CHANNEL AT PANEL 195DL . THE CHANNEL WAS REPLACED IAW SRM 51-42-13-001-001-A01 PAR.6 AND E.O R53573 REV DATE: 22/FEB/18 "
Part: FLOORBEAM — CORRODED (BS 280) · airframe 28,468 hrs · 19,028 cycles
CORROSION ON FLOORBEAM AT BS 280 BETWEEN STRINGERS 26L TO 26R IN THE MAIN AVIONICS COMPARTMENT. THE CORROSION WAS REMOVED IAW SRM 51-21-06-001-001-A01, PAR 5D, AND THE REWORKED AREA WAS MEASURED AND FOUND OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-42-06-001 001-A01, PAR 6D, AND SRM 51-42-20-001-001-A01, PAR 6A.
Part: SUPPORT PLATE — CORRODED (BS 346) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION WAS FOUND ON THE PROTECTION PLATE SUPPORT AT BS 346 BETWEEN RBL 41 TO 44, AT THE GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. THE SUPPORT WAS REPLACED IAW SRM 51-42-21-001-001-A01, PAR 6C.
Part: SUPPORT ANGLE — CORRODED (BS 319-349) · airframe 28,468 hrs · 19,028 cycles
CORROSION ON SUPORT ANGLE AT BS 319 - 349, RBL 41 AT THE GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. THE SUPPORT ANGLE WAS REMOVED IAW SRM 51-21-06-001-001-A01, PAR 5D.
Part: SUPPORT ANGLE — CORRODED (BS 329) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION WAS FOUND ON THE PROTECTION PLATE SUPPORT ANGLE, BS 329 BETWEEN RBL 41 TO 44 IN THE GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. THE PROTECTION PLATE SUPPORTS ANGLE WAS REPLACED IAW SRM 51-42-06-001-001-A01 PAR 6C.
Part: SUPPORT ANGLE — CORRODED (BS 319-349) · airframe 28,468 hrs · 19,028 cycles
CORROSION FOUND ON THE SUPPORT MOUNTING ANGLE AT BS 319 TO 349, RBL 41, AT THE GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. THE CORROSION WAS REMOVED IAW SRM 51-21-06-001-001-A01, PAR 5D.
Part: ANGLE — CORRODED (BS 310-349) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION WAS FOUND ON THE MID CAP ANGLE, BS 310 TO 349, LBL 41 AT THE MAIN ENTRANCE DOOR LOWER SILL, FWD WET AREA. THE CAP ANGLE WAS REPLACED IAW SRM 51-41-02-001-001-A01 PAR.6, A.
Part: SUPPORT PLATE — CORRODED (BS 322) · corrosion level 2 · airframe 28,468 hrs · 19,028 cycles
CORROSION ON PROTECTION PLATE SUPPORT AT BS 322 BETWEEN RBL 41 TO 44, AT THE GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. THE SUPPORT WAS REPLACED IAW SRM 51-42-06-001-001-A01, PAR 6C.
Part: SUPPORT ANGLE — CORRODED (BS 322) · airframe 28,468 hrs · 19,028 cycles
CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR 6C.
Part: RETAINER — DAMAGED (CARGO DOOR) · airframe 28,468 hrs · 19,028 cycles
BENT AND WORN LOWER PRESSURE SEAL RETAINER ON THE CORNER OF THE FWD CARGO DOOR. THE SEAL RETAINER WAS REPLACED IAW SRM 51-42-06-001-001-A01, PAR 6 C.
Part: RETAINER — WORN (CARGO DOOR) · airframe 28,468 hrs · 19,028 cycles
BENT AND WEAR ON LOWER PRESSURE SEAL RETAINER ON THE FWD/AFT CORNER AT CENTRAL CARGO BAY DOOR. LOWER PRESSURE SEAL RETAINER IN FWD/AFT CORNER AT CENTRAL BAGGAGE BAYDOOR WAS REPLACED IAW SRM 51-42-06-001-001-A01, PAR 6 C.
2018
Part: OXYGEN MASK — LEAKING (FIRST OFFICER'S) · airframe 24,975 hrs · 16,406 cycles
FIRST OFFICER`S OXYGEN MASK HAD A LEAK. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12, OPS CHECKED GOOD.
Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 24,961 hrs · 16,393 cycles
OBSERVER`S OXYGEN MASK LEAKING WHEN PUSH TO TEST WAS USED. REPLACED THE OBSERVER`S OXYGEN MASK IAW AMM 35-11-12, REPLACED THE STOWAGE BOX IAW AMM 35-11-15.
Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 24,961 hrs · 16,393 cycles
AFT RT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED & REPLACED THE EMERGENCY LIGHT AND LENS IAW AMM 33-51-15.
2017
Part: CONNECTOR — LOOSE (CARGO BAY) · airframe 22,641 hrs · 14,709 cycles
AFTER TAKE OFF RECEIVED FWD CARGO SQUIB 1 CAUTION MESSAGE. RETURNED TO LAND PER QRH. FOUND CONNECTOR ON FWD CARGO SQUIB LOOSE, RE SECURED IAW AMM 26-25-04.
Part: DOOR — BINDING (EMERGENCY EXIT) · airframe 22,107 hrs · 14,354 cycles
RIGHT AFT EMERGENCY ESCAPE DOOR WILL NOT OPEN UNDER NORMAL OPERATION OR DURESS.
2016
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,672 hrs · 14,053 cycles
EMERGENCY EXIT LIGHTS OUT IN GALLEY AND MID CABIN. REMOVED AND REPLACED BATTERY PACK ASSY PER AMM 33-51-04, OP'S CK GOOD.
Part: CONTACT — BROKEN (EMERGENCY LIGHT) · airframe 20,855 hrs · 13,528 cycles
THE RT OUTBD AFT OVERWING EMERGENCY LIGHT INOPERATIVE. FOUND A BROKEN CONTACT ON GROUND WIRE. REMOVED AND REPLACED CONTACT IAW ESPM 20-16-05, OPS TESTED GOOD.
Part: STRINGER — CORRODED (BS 349-364) · airframe 20,855 hrs · 13,528 cycles
STRINGER 26L CORRODED BS 364-349. REMOVED & REPLACED THE STRINGER IAW SRM 51-42-06-001-001 A01.
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 20,855 hrs · 13,528 cycles
THE MEGAPHONE WAS FOUND TO BE INOPERATIVE DURING LINE CHECK. REMOVED AND REPLACED THE MEGAPHONE IAW AMM 25-61-14-000/400-801-A01. OPS CHECKED GOOD.
Part: SEAT TRACK — CORRODED (BS 374-485) · airframe 20,855 hrs · 13,528 cycles
RBL 9 CABIN SEAT TRACK SEGEMNT BS 374 - 485 CORRODED AT SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A07, AND AMM 53-00-49-400-801 A07.
Part: DOOR SILL — CORRODED (PAX DOORWAY) · airframe 20,855 hrs · 13,528 cycles
PASSENGER DOOR SILL LOWER MID CAP IS CORRODED. FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-21-23-101-001A-02. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-41-02-001-001-A01, AND SRM 51-40-11-001-001-A01.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 20,855 hrs · 13,528 cycles
RIGHT BS 280 WEB CORRODED. REPAIRED IAW EC/TC REO 670-53-11-594 01 AND GENERIC REO 670-53-11-594 REV.
Part: FLOOR SUPPORT — CORRODED (BS 761-785) · airframe 20,855 hrs · 13,528 cycles
CUSTOMER NOTED CORROSION ON RT FLOOR SUPPORT BS 761-785. REMOVED CORROSION IAW SRM 51-21-06-001-001 A01.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 20,855 hrs · 13,528 cycles
LEFT BS 280 BULKHEAD WEB CORRODED. REPAIRED IAW EC/TC REO 670-53-11-594 AND GENERIC REO 670-53-11-594 REV A.
Part: FRAME — CORRODED (BS 310) · airframe 20,855 hrs · 13,528 cycles
FRAME BS 310 IS CORRODED FROM STRINGERS 26L - 25R. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-21-06-001-001-A01, AND 53-21-06-101-002-A02. REPAIRED IAW REO 670-53-21-799.
Part: FLOORBEAM — CORRODED (BS 1031) · airframe 20,855 hrs · 13,528 cycles
FLOORBEAM LBL 27, BS 1031 HAS SURFACE CORROSION UNDER FILLER STRIP. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-43-101-001-A02.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,855 hrs · 13,528 cycles
RT BS 280 FLOORBEAM ANGLE IS CORRODED BEYOND ALLOWABLE LIMITS . REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06-001-001 A01, 51-42-21-001-001 A01, AND 54-41-02-001-001 A01.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,855 hrs · 13,528 cycles
LEFT BS 280 FLOORBEAM ANGLE CORRODED. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06-001-001 A01, AND 51-42-21-001-001 A01.
Part: STRINGER — CORRODED (BS 333-349) · airframe 20,855 hrs · 13,528 cycles
STRINGER 26R AND SPLICE BS 333-349 IS CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A-01, AND 51-42-21-001-001-A01.
Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 20,855 hrs · 13,528 cycles
AFT COCKPIT FLOOR SUPPORT CORRODED. REMOVED AND REPLACED THE COCKPIT FLOOR SUPPORT IAW SRM 51-42-20-001-001 A01 & 51-42-06-001-001-A01. .
Part: STRINGER — CORRODED (BS 280-333) · airframe 20,855 hrs · 13,528 cycles
STRINGER 25R, BS 280 - 333 IS CORRODED. REMOVED AND REPLACED THE STRINGER AND SPLICE IAW SRM 51-42-06-001-001-S01, 51-42-21-001-001-A01, 51-40-11-001-001-A01 AND DWG SH670-37420 REV D.
Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 20,855 hrs · 13,528 cycles
RIGHT SIDE SEAT TRACK BS 785 - 847+16 IS CORRODED. FOUND TO BE BEYOND ALLOWABLE LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND AMM 53-00-49-400-801-A07.
Part: DOOR SILL — CORRODED (PAX DOOR) · airframe 20,855 hrs · 13,528 cycles
PAX DOOR LOWER STRIKER SILL CORRODED AT BS 325. LOWER SILL IS BEYOND ALLOWABLE LIMITS IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
Part: DOUBLER — CORRODED (BS 316) · airframe 20,855 hrs · 13,528 cycles
BS 316, STRINGER 27 DOUBLER IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-01-101-002-A01. REMOVED AND REPLACED THE DOUBLER IAW AMM 34-43-07-000-801-A01, SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, SRM 51-42-06-001-001-A01, AND AMM 34-43-07-400-80A9A01.
Part: INTERCOSTAL — CORRODED (BS 310-319) · airframe 20,855 hrs · 13,528 cycles
INTERCOSTAL AT STRINGER 20R, BS 310 - 319 CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 53-21-23-201-002-A01, 51-42-06-001-A01, & 51-42-21-001-001-A01.
Part: FRAME — CORRODED (BS 295) · airframe 20,855 hrs · 13,528 cycles
FRAME BS 295, STRINGERS 26L-24R IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001 A01. REPAIRED IAW REO 690-53-21-834.
Part: FRAME — CORRODED (BS 333) · airframe 20,855 hrs · 13,528 cycles
BS 333 FRAME, STRINGERS 25L-25R CORRODED. BLENDED THE CORROSION IAW SRM 51-21-06-001-001 A01 AND REPAIRED IAW REO 670-53-21-799.
Part: SEAT TRACK — CORRODED (BS 681-661) · airframe 20,855 hrs · 13,528 cycles
RIGHT SEAT TRACK IS CORRODED AT BS 581 - 661+46. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001 A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A07, AND AMM 53-00-49-400-801 A07.
Part: FRAME — CORRODED (BS 319) · airframe 20,855 hrs · 13,528 cycles
BS 319 FRAME, STRINGERS 26L-26R CORRODED. REMOVED CORROISON AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-06-101-002A-02. REPAIRED THE FRAME IAW 670-53-21-799.
Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 20,855 hrs · 13,528 cycles
LEFT SIDE SEAT TRACK BS 744 - 761 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-01-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 765-847) · airframe 20,855 hrs · 13,528 cycles
LEFT SIDE SEAT TRACK BS 765 - 847+16 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49--000-801-A07, AND AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 667-720) · airframe 20,855 hrs · 13,528 cycles
RIGHT SIDE SEAT TRACK BS 667 - 720 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-01-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND AMM 53-00-49-400-801-A07.
Part: FLOOR SUPPORT — CORRODED (BS 280-310) · airframe 20,855 hrs · 13,528 cycles
FLOOR SUPPORT BS 280 - 310 CORRODED AT MULTIPLE AREAS. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED AND REPLACE THE FLOOR SUPPORT IAW SRM 51-42-00-001-001-A01, 51-47-21-001-001-A01, AND SRM 51-40-11-001-001-A01.
Part: ANGLE — CORRODED · airframe 20,855 hrs · 13,528 cycles
FWD MID AND AFT LOWER SILL ANGLES ON SERVICE DOOR ARE CORRODED. REMOVED AND REPLACED IAW SRM 51-42-06-001-001 A01, & 51-42-20-001-001 A01.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 20,855 hrs · 13,528 cycles
RIGHT SEAT TRACK BS 485 - 581 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001 A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 661) · airframe 20,855 hrs · 13,528 cycles
RIGHT SIDE SEAT TRACK BS 661+16 - 661+90 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001 A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND AMM 53-00-49-400-801-A07.
Part: INTERCOSTAL — CORRODED (BS 364) · airframe 20,855 hrs · 13,528 cycles
INTERCOSTAL BS 364 STRINGER 26L IS CORRODED. REMOVED THE INTERCOSTAL IAW SRM 51-42-21-001-01-A01, 51-42-06-001-001A-01.
Part: SEAT TRACK — CORRODED (BS 477-565) · airframe 20,855 hrs · 13,528 cycles
RIGHT SIDE SEAT TRACK BS 477 - 565 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001 A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A07, AND AMM 53-00-49-400-801 A07.
Part: FRAME — CORRODED (BS 280) · airframe 20,855 hrs · 13,528 cycles
FRAME AT BS 280 STRINGER 26L-26R CORRODED. REMOVED CORROSION IAW SRM 51-12-00-001-001-A01, AND 51-21-06-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 20,855 hrs · 13,528 cycles
RIGHT SEAT TRACK IS CORRODED BS 661+46 - 693. FOUND TO BE BEYOUND ALLOWABLE LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 661) · airframe 20,855 hrs · 13,528 cycles
RIGHT SIDE SEAT TRACK BS 661+16 - 661+90 CORRODED. FOUND TO BE BEYOND ALLOWABLE LIMITS. INSTALLED A SERVICABLE SEAT TRACK IAW AMM 53-00-49-400-801-A07.
Part: FRAME — CORRODED (BS 349) · airframe 20,855 hrs · 13,528 cycles
BS 349 FRAME, STRINGER 25L-24R FOUND CORRODED. REMOVED CORROSION ON FRAME AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001-A01, AND 53-21-06-101-006-A02. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG SH690-31350.
Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 20,855 hrs · 13,528 cycles
LEFT SEAT TRACK BS 581 - 661+46 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 20,855 hrs · 13,528 cycles
SEAT TRACK RBL 9, BS 349 - FS 485 CORRODED IN MULTIPLE AREAS. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND AMM 53-00-49-400-801-A07.
Part: ANGLE — CORRODED (DOOR SILL) · airframe 20,855 hrs · 13,528 cycles
CORROSION FOUND ALONG PAX DOOR CUTOUT (LOWER SIDE. REPAIRED IAW SRM 51-40-11-001-001-A01. .
Part: RETAINER — DENTED (CARGO DOOR) · airframe 20,855 hrs · 13,528 cycles
CENTER CARGO DOOR SEAL RETAINER IS DENTED AT THE AFT RT CORNER. REPAIRED IAW EC/TC REO 690-52-35-013 & REO 690-52-35-013 REV B.
Part: WIRE — DAMAGED (MEGAPHONE) · airframe 20,571 hrs · 13,323 cycles
MEGAPHONE WIRING DAMAGED. R & R MEGAPHONE IAW AMM 25-61-14. AIPC REF 25-61-14, FIG 1G, ITEM 5.
Part: RETAINER — CRACKED (CARGO DOOR SEAL) · airframe 20,142 hrs · 12,999 cycles
FWD CARGO DOOR LOWER AFT CORNER SEAL RETAINER DAMAGE, CRACKED, NEEDS REPAIR. PERFORMED PERMANENT REPAIR TO FWD CARGO DOOR SEAL RETAINER IAW EC/TC REO 690-52-35-013, REV C. REF EC/TC FOR ALL WORK ACCOMPLISHED.
2015
Part: MEGAPHONE — FAILED (CABIN) · airframe 19,508 hrs · 12,552 cycles
F/A MEGAPHONE DOES NOT WORK. R & R MEGAPHONE IAW AMM 25-61-14 REF; IPC 25-61-14, ITEM 5, OPS CHECK GOOD.
Part: GLOWSTRIP — MISSING (GALLEY) · airframe 18,455 hrs · 11,778 cycles
PHOTOILLUMINESCENT STRIP MISSING IN THE GALLEY. INSTALLED NEW PHOTOILLUMINESCENT STRIP IN GALLEY IAW AMM 33-51-11.
Part: BRAKE — FAILED (MLG) · airframe 18,269 hrs · 11,645 cycles
SMOKE COMING FROM INBD RIGHT BRAKE . TEMP HOLDING AT 7. EMERGENCY DECLARED. R & R RT INBD BRAKE IAW AMM 32-43-26, ITEM 5. ACFT OK FOR SERVICE.
Part: MEGAPHONE — UNKNOWN (CABIN) · airframe 17,978 hrs · 11,427 cycles
MEGAPHONE DAMAGED REQUIRES REPLACMENT. REPLACED MEGAPHONE IAW AMM 25-61-14, AIPC 25-61-14, FIG 1X, ITEM 5. OPS CHECK GOOD NO DEFECTS NOTED.
2014
Part: STRAP — CRACKED (BS 882) · airframe 15,163 hrs · 9,573 cycles
AFT BELLY FAIRING STRAP JOINT CRACKED AT BS 882. REPAIRED IAW REO 690-53-82-052.
Part: ANGLE — CORRODED (DOOR FRAME) · airframe 15,163 hrs · 9,573 cycles
FOUND UPPER DOOR FRAME ANGLE CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. LOCATED AND DRILL NEW ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-10-001-001-A01 AND INSTALLED.
Part: ANGLE — CORRODED (DOOR SILL) · airframe 15,163 hrs · 9,573 cycles
FOUND LOWER SERVICE DOOR SILL ANGLE CORRODED. FOUND TO BE MORE THAN 30 PERCENT OF THE AREA OF THE LENGTH OF ANGLE. FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-21-23-101-002-A01 NOTE 1. REMOVED ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED, DRILLED AND DEBURRED AS REQUIRED ON REPLACEMENT SERVICE ANGLE IAW SRM 51-42-11-001-001 AND DWG SH670-31950. INSTALLEDANGLE, IAW DWG SH670-31950, SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
Part: ANGLE — CORRODED (DOOR FRAME) · airframe 15,163 hrs · 9,573 cycles
FOUND UPPER SERVICE DOOR FRAME ANGLE CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REMOVED ANGLE IAW SRM 51-42-06-001--001-A01. LOCATED, DRILLED, AND DEBURRED IAW SRM 51-40-11-001-001, 51-42-06-001-001 AND DWG SH670-31950. INSTALLED ANGLE IAW DWG SH670-31950 AND SRM 51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 349) · airframe 15,163 hrs · 9,573 cycles
SEAT TRACK AT RBL 9 BS 349 CORRODED. FOUND OUT OF LIMITS IAW 53-21-49-101-001-A01. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.
Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 15,162 hrs · 9,572 cycles
RT COCKPIT FLOORBEAM CRACKED. REPAIRED IAW REO 690-53-11-663. MAJOR REPAIR.
Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 15,163 hrs · 9,573 cycles
LT COCKPIT FLOORBEAM CRACKED. COMPLIED WITH EC/TC REO 690-53-11-663 AND REO 690-53-11-663 & FABRICATED NEW SERVCEABLE REPAIR ANGLE. MAJOR REPAIR.
Part: SUPPORT ANGLE — BROKEN (BS 1144-1162) · airframe 15,162 hrs · 9,572 cycles
SUPPORT ANGLE BETWEEN BS 1144 & 1162 STRINGER 7R IS BROKEN. REMOVED BROKEN ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED NEW ANGLE IAW 51-42-21-001-001.
Part: ANGLE — CRACKED (UNKNOWN) · airframe 15,163 hrs · 9,573 cycles
NDT DETECTED A CRACK ON ANGLE. REWORKED IAW EC/TC SB670BA-53-041, REV D ITEM NR 258-273, 275. COMPLIED WITH EC/TC 670BA-53-041 01 AND REO 670BA-53-041 01. MAJOR REPAIR.
Part: SUPPORT ANGLE — BROKEN (BS 1144-1162) · airframe 15,162 hrs · 9,572 cycles
SUPPORT ANGLE BETWEEN BS 1144 & 1162 AT STRINGER 9R IS BROKEN. REMOVED BROKEN ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED NEW ANGLE IAW SRM 51-42-06-001-001.
Part: SEAT TRACK — CORRODED (BS 785.15) · airframe 15,162 hrs · 9,572 cycles
RT SIDE SEAT TRACK CORRODED AT FS 785.15. REMOVED SEAT TRACK FROM BS 784 - 847 IAW AMM 53-00-49-000-801-A07. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 785.15) · airframe 15,162 hrs · 9,572 cycles
LT SIDE SEAT TRACK AT FS 785.15 CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013 AND SRM 51-21-06. REMOVED AND INSTALLED NEW SEAT TRACK FROM BS 784 - 847 IAW AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 761.85) · airframe 15,162 hrs · 9,572 cycles
RT SIDE SEAT TRACK CORRODED AT BS 761.85. R & R SEAT TRACK IAW AMM 53-00-49-400-801 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 720) · airframe 15,162 hrs · 9,572 cycles
LT SIDE SEAT TRACK CORRODED AT BS 720.85. R & R SEAT TRACK IAW AMM 53-00-49-000-801 & 53-00-49-400-801 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 720.85) · airframe 15,162 hrs · 9,572 cycles
RT SIDE SEAT TRACK CORRODED AT BS 720.85. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801 AND REO 670-53-00-013.
Part: SKIN — GOUGED (BS 942) · airframe 15,162 hrs · 9,572 cycles
SKIN DAMAGED AT BS 942. COMPLIED WITH REO 670-53-00-290 AND EC/TC REO 670-53-00-290. MAJOR REPAIR.
Part: FAIRING — DAMAGED (THRUST REVERSER) · airframe 15,162 hrs · 9,572 cycles
THRUST REVERSER UPPER HINGE LINE FAIRING 443BT, RT ENGINE, HAS A GOUGE AND IS CRACKED. REMOVED UPPER THRUST REVERSER HINGE LINE FAIRING 443BT ON RT ENGINE IAW AMM 54-12-01-000-802-A02. THIS REPAIR IS CLASSIFIED AS A REPAIR IAW SOP 5702. CRACK AND GOUGE IS OUT OF LIMITS SRM 54-12-01-101-001-A01. LOCATED AND DRILLED NEW HINGE FAIRING STAN RT AND TRANSFERED HARDWARE IAW SRM 51-40-11 51-42-06 AND 51-42-13. INSTALLED NEW RUB STRIP AND SEAL RETAINER TO HINGE FAIRING IAW SRM 51-42-06-001-001-A01 AND DWG CN624-4265. INSTALLED NEW UPPER THRUST REVERSER HINGE LINE FAIRING (443BT) TO RT ENGINE IAW AMM 54-12-01-400-802.
Part: WEB — CRACKED · airframe 15,162 hrs · 9,572 cycles
FLOOR WEB CRACKED AT ADG STOW PUMP. COMPLIED WITH REO 670-53-11-509.
2013
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,721 hrs · 8,669 cycles
PAX DOOR EMERGENCY LIGHT AT FWD SIDE OF ENTRANCE HAS SEVERAL LIGHTS OUT. REPAIRED.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,716 hrs · 8,666 cycles
PAX DOOR EMERGENCY LIGHT AT FWD SIDE OF ENTRANCE HAS SEVERAL LIGHTS OUT. REPLACED LAMPS IAW GMM 3-8-9. OPS CHECKED IAW 33-51-00-710-802. OPS NORMAL.
Part: SKIN — DAMAGED (LT WING LE SLAT) · airframe 13,314 hrs · 8,399 cycles
LEFT SLAT T/E DAMAGED SS 142.25. REPAIRED IAW REO 670-57-41-254. MAJOR REPAIR IAW GMM 5-3.
Part: SKIN — DAMAGED (LT WING SLAT) · airframe 13,305 hrs · 8,393 cycles
LEFT SLAT AND L/E DAMAGED AT SS 142.25 AND WS144.95. REPAIRED IAW SRM 51-13-01 AND REO 670-57-41-109. MAJOR REPAIR IAW GMM 5-3.
Part: LIGHT — DAMAGED (CABIN) · airframe 12,422 hrs · 7,846 cycles
EMERGENCY LIGHT AT SEAT 13B IS DAMAGED. SECURED EMERGENCY LIGHT AT 13B IAW AMM 33-51-01. NO FURTHER DEFECTS NOTED. ACFT OK FOR SERVICE.
2012
Part: SLAT SYSTEM — MALFUNCTIONED (WING) · airframe 11,235 hrs · 7,091 cycles
ON APPROACH INTO MSP RECEIVED SLAT FAIL CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY. RESET SLAT CONTROL SYSTEM AND CLEARED INHIBITS IN MDC. PERFORMED OPS CHECK OF SLATS, OPS CHECK GOOD.
Part: SKIN — DENTED (FUSELAGE) · airframe 10,591 hrs · 6,666 cycles
FUSELAGE SKIN DENTED AND PUNCTURED ABOVE AND AFT OF AFT LAV SERVICE PANEL. CUT OUT DAMAGED SKIN AND INSTALLED A DOUBLER IAW BOMBARDIER REO 690-53-61-269.
Part: WARNING SYSTEM — FALSE ACTIVATION (LE SLAT) · airframe 10,210 hrs · 6,409 cycles
ON APPROACH INTO MSP RECEIVED SLAT FAIL MSG, PREFORMED QRH. EMERGENCY DECLARED, A/C LANDED SAFELY. INSPECTED SLATS, NO DEFECTS FOUND. PERFORMED ELECTRICAL RIGGING OF SLAT SYSTEM, CLEARED INHIBITS OF BOTH CHANNELS, PERFORMED SFECU SELF TEST, NO DEFECTS. OPS CHECK OF SLAT AND FLAP SYSTEM GOOD.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 9,907 hrs · 6,207 cycles
ON DESCENT INTO BHM RECEIVED SLAT FAIL CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY IN BHM. CLEARED INHIBITS FOR SLAT CH 1 AND CH 2. OPS CHECK GOOD.
Part: SKIN — DENTED (FUSELAGE) · airframe 9,821 hrs · 6,152 cycles
FUSELAGE SKIN DENTED ABOVE FWD LAV SERVICE DOOR. CUT OUT DAMAGED SKIN AND INSTALLED A DOUBLER IAW BOMBARDIER REO 690-53-21-338.
Part: SILL — CORRODED (BS 280-319.7) · corrosion level 3 · airframe 9,820 hrs · 6,152 cycles
RIGHT SIDE FLOOR SILL, FS 280.00 TO 319.70 CORRODED BEYOND ALLOWABLE LIMITS. INSTALLED NEW SILL IAW SRM 51-42-06, 51-42-13,51-42-20.
2010
Part: CONTROLLER — INTERMITTENT (BLEED AIR SYS) · airframe 5,847 hrs · 3,612 cycles
ON CLIMBOUT FROM DTW RECEIVED BLEED AIR DUCT WARNING MSG. EMERGENCY DECLARED, A/C RETURNED TO DTW LANDED SAFELY. REMOVED AND REPLACED ANTI-ICE LEAK CONTROLLER.
Part: ENGINE — VIBRATION (LEFT) · airframe 5,331 hrs · 3,265 cycles
ON CLIMBOUT FROM RDU LEFT ENGINE FAN VIB AT 2.6. EMERGENCY DECLARED, A/C DIVERTED TO GSO LANDED SAFELY. TRANSFERRED TO DEFERRED LIST PER MEL GMM 5-2 CAT 1.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 23,575 hrs · 20,519 cycles
AFT PRESSURE BULKHEAD CRACKED AT FS 621.00 LBL 27.50 ABOVE CARGO DOOR TRACK. REPAIRED AFT PRESSURE BULKHEAD FS 621.00 LBL 27.50 IAW REO 601R-53-61-1541.
2009
Part: SLAT SYSTEM — MALFUNCTIONED · airframe 1,872 hrs · 1,201 cycles
ON APPROACH, RECEIVED SLAT FAIL CAUTION MSG. QRH PROCEDURES ACCOMPLISHED, EMERGENCY DECLARED. FLAPS EXTENDED ACFT LANDED SAFELY. RESET SSCU AND SLAT SYS, OPS CHECK GOOD. NO DEFECTS NOTED.
Part: COMPUTER — MALFUNCTIONED (SLATS) · airframe 1,829 hrs · 1,170 cycles
ON APPROACH, RECEIVED SLATS FAIL CAUTION MSG AP ON CONFIGURING THE ACFT FOR LANDING. FOLLOWED QRH, EMERGENCY DECLARED. ACFT LANDED SAFELY WITH FUNCTIONAL FLAPS. CLEARED SLAT FAULTS FROM MDC, PERFORMED OPS CHECK OF SLAT SYSTEM, NO DEFECTS NOTED.