N668CA
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.
238 reports on file, 2004-12-15 – 2025-07-26.
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 40,280 hrs · 30,852 cycles
CEILING EMERGENCY FLOOD LIGHT FOUND INOP REMOVED AND REPLACED CEILING EMERGENCY FLOOD LIGHT BULB IAW CRJ 700 AMM 33-51-09. OPS CHECK GOOD.
Earlier reports · 2004–2024 · 237 reports
2024
Part: FRAME — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
FRAME FS863 BETWEEN STRINGER 27 AND 26R IS CORRODED. REPAIRED FRAME F.S.863 IAW ENDEAVOR AIR EA CRJ753-17338 REV IR DATED 10/9/2024
Part: ANGLE — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
FOUND JOINT ANGLE AT FS333.00 & STR 21L TO BE CORRODED. REMOVED CORROSION FOR FS 333.00 JOINT ANGLE @ STR 21L IAW CRJ 700 SRM 51-21-06-001-001-A01. UPON FURTHER INVESTIGATION FOUND NO ALLOWED DAMAGE IN THIS AREA & 20% MATERIAL LOST ON JOINT ANGLE, REQUIRE REPLACEMENT. LOCATED AND DRILLED NEW SERVICEABLE STRINGER SPLICE P/N SH670-35055-1 AT STGR 21L F.S. 333 IAW CRJ-700 SRM 51-40-11-001-001-A01. INSTALLED SERVICEABLE FS 333.00 JOINT ANGLE PN SH670-35055-1 @ STR 21L IAW CRJ 700 SRM 51-21-06-001-001-A01 AND SRM 51-42-21-001-001-A01
Part: REPAIR — NONE · airframe 39,291 hrs · 29,803 cycles
PER ENDEAVOR, REMOVE FS 409-426, S14R-17R, EXISTING REPAIR DOUBLER & SHIMS, NDT SKIN FASTENER HOLES AND CUT-OUTS TO ENSURE THERE ARE NO CRACKS. FABRICATE NEW SHIMS & DOUBLER AND INSTALL IAW SRM OR SUBMIT TO ENGINEERING IF REQUIRED. REMOVED PREVIOUS REPAIR DOUBLER LOCATED AT FS 409-426, S14R-17R OUTER FUSELAGE SKIN. IAW CRJ700 SRM 51-42-06-001-001-A01. INSTALLED NEW REPAIR DOUBLER IAW CRJ700 SRM 51-42-06-001-001-A01. AND CRJ700 SRM 53-00-01-201-0 REMOVED PREVIOUS REPAIR SHIM LOCATED AT FS 409-426, S14R-17R OUTER FUSELAGE SKIN. IAW CRJ700 SRM 51-42-06-001-001-A01. INSTALLED NEW REPAIR SHIM IAW CRJ700 SRM 51-42-06-001-001-A01. AND CRJ700 SRM 53-00-01-201-001.AHFEC PERFORMED ON FUSELAGE SKIN CUT-OUT AND FASTENER HOLES AT FS 409-426, S14R-17R IAW CRJ 700 NDTM PART 1 51-20-006-250-A01 NO INDICATIONS NOTED AT THIS TIME01.01-A01.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
"SPLICE AT FS333 & STR24R IS CORRODED REMOVED CORROSION ON FS 333.00 SPLICE P/N SH670-32429-4 AT STR 24R IAW CRJ 700 SRM 51-21-06-001-001-A01. MATERIAL REMOVED 0.035"", NOMINAL THICKNESS OF 0.063"". BLENDS ARE BEYOND THE ALLOWABLE DAMAGE LIMITS AS PER CRJ700 SRM 53-00-00-101-001-A01.SPLICE REQUIRES REPLACEMENT. LOCATED AND DRILLED NEW SERVICEABLE JOINT SPLICE P/N SH670-32429-4 AT FS333 AND STR 24R IAW CRJ700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE JOINT SPLICE P/N SH670-32429-4 AT FS333 AND STR 24R IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01"
Part: ANGLE — CRACKED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
UPON REMOVAL FOUND FS 364 FACTORY SPLICE (P/N: SH670-32460-1) TO BE CRACKED AND REQUIRES REPLACEMENT. LOCATED AND DRILLED SERVICEABLE FS 364.00 @ STGR 20L IB FACTORY SPLICE (P/N: SH670-32460-1) IAW CRJ 700 SRM 51-40-11-001-001-A01.REF. BARCODE IDENTIFIER HN00185608 LINE ITEM 5A FOR INSTILLATION OF FS 364.00 @ STGR 20L IB FACTORY SPLICE (P/N: SH670-32460-1).
Part: SPLICE — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
"CORROSION ON JOINT SPLICE (PN SH670-32429-3) FROM STR 26L AND FS 333. REMOVED CORROSION ON FS 333.00 JOINT PIECE P/N SH670-32429-3 AT STR 26L PER CRJ 700 SRM 51-21-06-001-001-A01. REMOVED .029"" MATERIAL FROM A NOMINAL THICKNESS OF .063"". BLENDS ARE BEYOND THE ALLOWABLE DAMAGE LIMITS SPECIFIED BY CRJ 700 SRM 53-00-00-101-001-A01. JOINT PIECE REQUIRES REPLACEMENT. REMOVED AND REPLACED 1EA JOINT SPLICE (PN SH670-32429-3) FROM STR 26L AND FS 333 FOR ACCESS IAW CRJ700 SRM 51-42-06-001-001-01. LOCATE AND DRILLED NEW SERVICEABLE JOINT SPLICE (PN SH670-32429-3) IAW CRJ 700 SRM 51-40-11-001-001-A01."
Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
STGR 26R SPLICE IS CORRODED AT F.S. 333 ON THE FWD SIDE. REMOVED STGR 26R JOINT SPLICE AT FS 333 IAW CRJ-700 SRM 51-42-06-001-001-A01. INSTALLED STGR 26R JOINT SPLICE AT FS 333 IAW CRJ 700 SRM 51-42-06-001-001-A01
Part: STRINGER — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
STGR 19R IS CORRODED BETWEEN F.S. 280 TO F.S. 310. REMOVED STGR 19R (P\N SH670-31632-1) BETWEEN F.S. 280 TO F.S. 319 IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE STR 19R P/N SH670-31632-1 IAW CRJ-700 SRM 51-42-06-001-001-A01
Part: STRINGER — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
STRINGER 25R AT FS280 IS CORRODED. REMOVED STR 25R P/N SH670-31212-2 FROM FS 280 TO FS 333 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE STR 25R, P/N SH670-31212-2, FROM FS 280 TO FS 333 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
STRINGER 21R AT FS280 IS CORRODED. REMOVED STR 21R FROM FS 280 TO FS 333 IAW CRJ 700 SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01. INSTALLED NEW STR 21R (PN SH670-31636-1) FROM FS 280 TO FS 333 IAW CRJ 700 SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01.
Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
AVI DOOR FWD INTERCOSTAL IS CORRODED BETWEEN STGR 27 TO STGR 26R. REMOVED CORROSION ON INTERCOSTAL BETWEEN STGR 27 AND STGR 26R AND BETWEEN FS 349-364 IAW CRJ 700 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS DUE TO BEING IN A NO DAMAGE ALLOWED AREA IAW CRJ 700 SRM 53-21-23-101-003-A01. REMOVED AND REPLACED AVI BAY DOOR FWD INTERCOSTAL BETWEEN STGR 27-26R (PN: SH670-32075-4) IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. REMOVED 2EA RIVETS FROM INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01. INSTALLED 2EA RIVETS FROM INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01. REMOVED GUSSET FROM FS 364 BETWEEN STGR 27-26R IAW CRJ 700 SRM 51-42-21-001-001-A01. INSTALLED GUSSET FROM FS 364 BETWEEN STGR 27-26R IAW CRJ 700 SRM 51-42-21-001-001-A01. REMOVED AVI COMPARTMENT DOOR PROXIMITY SENSOR 41 IAW CRJ 700 AMM 52-70-08-000-801-A02. INSTALLED AVI COMPARTMENT DOOR PROXIMITY SENSOR 41 IAW CRJ 700 AMM 52-70-08-400-801-A02. LOCATE AND DRILL REQUIRED FOR AVI DOOR FWD INTERCOSTAL BETWEEN STGR 27-26R. LOCATED AND DRILLED NEW AVI BAY DOOR FWD INTERCOSTAL BETWEEN STGR 27-26R (PN: SH670-32075-4) IAW CRJ 700 SRM 51-40-11-001-001-A01. APPLIED EDGE SEAL AND TOP COAT ON AVI BAY DOOR FWD INTERCOSTAL BETWEEN STGR 27-26R IAW CRJ 700 SRM 51-23-00-001-001-A01 AND 51-25-16-001-001-A01.
Part: DOOR SILL — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
"AFT CARGO DOOR SILL PLATE F.S. 1000-1051 LBL 34 CORRODED INCLUDING NUT PLATES AND HOLES BLENDED CORROSION ON AFT CARGO LOWER DOOR SILL PLATE PN MM670-35655-001 IAW CRJ 700 SRM 53-61-23-201-001-A01, AND 51-12-00-001-001-A01. MEASURED BLEND AREA MATERIAL REMOVED 0.036"" MAX ALLOWABLE IS 0.016"" IS OUT OF LIMITS AND REQUIRES REPLACEMENT. TOOL USED 205492 CAL DUE 31DEC24. REMOVED AFT CARGO LOWER DOOR SILL PN MM670-35655-003 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE LOWER SILL PN# MM670-35655-003 IAW CRJ-700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE LOWER SILL PN MM670-35655-003 IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED 24 EA MISSING RIVETS ON NEW SERVICEABLE LOWER SILL PN# MM670-35655-003 IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. REMOVED AND REPLACED MULTIPLE FASTENERS ON LOWER SILL PN: MM670-35655-003 IAW CRJ-700 SRM 51-42-06-001-001-A01. COMPLETED FINISH SURFACE IAW CRJ-700 SRM 51-21-16-001-001-A01. INSTALLED MISSING NUT PLATE TO LOWER SILL IAW CRJ 700 SRM 51-42-15-001-001-A01. REMOVED LOWER COAMING (P/N: MM670-35698-003) AND INTERCOSTAL (P/N: MM670-35324-003) IAW CRJ700 SRM 51-42-06-001-001-A01. AND SRM 51 51-42-21-001-001-A01. FOR ACCESS. REINSTALLED LOWER COAMING (P/N: MM670-35698-003) AND INTERCOSTAL (P/N: MM670-35324-003) IAW CRJ700 SRM 51-42-06-001-001-A01. AND SRM 51-42-21-001-001-A01, SRM 51-23-00-001-001-A01. REMOVED 2EA STOP FITTING IAW CRJ700 SRM 51-41-02-001-001-A01. FOR ACCESS. REINSTALLED AND FINISH SURFACE ON 2EA STOP FITTING IAW CRJ700 SRM 51-41-02-001-001-A01, SRM 51-21-16-001-001-A01, SRM 51-23-00-001-001-A01. REMOVED 3EA INNER CORDS AND 2EA CLIPS FROM FS 1000 TO FS 1047 AND 1EA SHIM AT FS 1047 IAW CRJ 700 SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. INSTALLED 3EA INNER CORDS AND 2EA CLIPS FROM FS 1000 TO FS 1047 AND 1EA SHIM AT FS 1047 IAW CRJ 700 SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01."
Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
UPON EVAL DETERMINED THAT CIRCUMFERENTIAL JOINT AT FS333, STR 21R REQUIRES REPLACEMENT DUE TO CORROSION. PON FURTHER INVESTIGATION, IT WAS FOUND THAT THE STRINGER JOINT SPLICE AT STR 21R AT FS 333 IS WHAT REQUIRES REPLACEMENT DUE TO CORROSION IAW CRJ700 SRM 53-21-03-101-006-A01.LOCATED AND DRILLED NEW STRINGER JOINT SPLICE AT STR 21R AT FS 333 (PN SH670-31197-1) IAW CRJ700 SRM 51-40-11-001-001-A01.INSTALLED NEW STRINGER JOINT SPLICE AT STR 21R AT FS 333 (PN SH670-31197-1) IAW CRJ700 SRM 51-42-06-001-001-A01 COMPLETED THE INSTALL OF THE NEW SERVICEABLE STRINGER JOINT P/N SH670-31197-1 AT STR 21R AND FS 333 IAW CRJ 700 SRM 51-42-21-001-001-A01
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 39,291 hrs · 29,803 cycles
PAX DOOR INTERCOSTAL MID DD2 FOUND CORRODED REMOVED PAX DOOR INTERCOSTAL MID DD2 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR INTERCOSTAL MID DD2 P/N:601R318053-3 IAW CRJ700 SRM 51-40-11-001-001-A01 INSTALLED NEW SERVICEABLE PAX DOOR INTERCOSTAL DD2 MID IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 39,291 hrs · 29,803 cycles
PAX DOOR MID DD3 FOUND TO BE CORRODED REMOVED PAX DOOR MID INTERCOSTAL DD3 IAW CRJ700 SRM 51-42-006-001-001-A01 AND 51-42-21-001-001-A01 LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR MID DD3 INTERCOSTAL P/N:601R318056-1 IAW CRJ700 SRM 51-40-11-001-001-A01INSTALLED SAME SERVICEABLE PAX DOOR FORMER AT FS 329.50 BETWEEN DD3 AND DD2 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 INSTALLED NEW SERVICEABLE PAX DOOR INTERCOSTAL MID DD3 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 39,291 hrs · 29,803 cycles
PAX DOOR AFT INTERCOSTAL DD5 FOUND CORRODED REQUIRES REPLACEMENT REMOVED PAX DOOR AFT INTERCOSTAL DD5 IAW CRJ700 SRM 51-42-06-001-001-A01. THEN LOCATED DRILLED AND INSTALLED NEW SERVICEABLE AFT INTERCOSTAL DD5 P/N: 601R31902-317A IAW CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01
Part: FORMER — DAMAGED (ZONE 800) · airframe 39,291 hrs · 29,803 cycles
PAX DOOR AFT FORMER REQUIRES REPLACEMENT DUE TO PREVIOUS REPAIR REMOVED PAX DOOR AFT FORMER IAW CRJ700 SRM 51-42-06-001-001-A01 AND THEN INSTALLED NEW SERVICEABLE PAX DOOR AFT FORMER IAW CRJ700 SRM 51-42-06-001-001-A01
Part: SUPPORT — CORRODED (ZONE 200) · airframe 39,291 hrs · 29,803 cycles
SERVICE DOOR HAS 4EA FLOOR PROTECTOR SUPPORTS AND 4EA ANGLES WITH CORROSION. REMOVED AND REPLACED FWD WEB FLOOR PROTECTOR AND 2 EA AFT WEB FLOOR PROTECTOR IAW CRJ700 SRM 51-41-02-001-001-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
STGR 19L IS CORRODED BETWEEN F.S. 280 TO F.S. 295. INSTALLED NEW SERVICEABLE STGR 19L (PN: SH670-31207-1)
Part: FRAME SPLICE — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
STR 25R CIRCUMFERENTIAL JOINT AT FS333 REQUIRES REPLACEMENT DUE TO CORROSION LOCATED AND DRILLED STR 25R CIRCUMFERENTIAL JOINT AT FS333 IAW CRJ 700 SRM 51-40-11-001-001-A01. NEW SERVICEABLE PART, P/N SH670-32429-4S. REFERENCE HN00184967, TASK 6A, FOR THE INSTILLATION OF STR 25R CIRCUMFERENTIAL JOINT, P/N SH670-32429-4S, AT FS333.
Part: SKIN — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
FUSELAGE SKIN IS CORRODED BETWEEN F.S. 280 TO F.S. 295 AND BETWEEN STGR 26R TO STGR 25R. REPAIRED IAW ENDEAVOR AIR EA CRJ753-17310, DATE: 9/16/2024, REV IR.
Part: FRAME — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
F.S. 310 IS CORRODED BETWEEN STGR 26R TO STGR 26L. REPAIRED IAW CRJ 700 SRM 53-00-06-201-006-A01.
Part: FRAME — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
F.S. 295 FRAME IS CORRODED BETWEEN STGR 19L TO STGR 20L. REPLACED FRAME PER SRM.
Part: STRINGER — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
STGR 26L IS CORRODED BETWEEN F.S. 295 TO F.S. 310. REMOVED STRINGER 26L (PN: SH670-31634-1) FROM FS 280 TO FS 333 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE STRINGER 26L (PN: SH670-31634-1) FROM FS 280 TO FS 333 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: CUP — CORRODED (DOOR HANDRAIL) · airframe 39,291 hrs · 29,803 cycles
PAX DOOR FWD AND AFT HANDRAIL CUPS ARE CORRODED. UPON FURTHER INVESTIGATION PAX DOOR FWD HANDRAIL CUPS P/N SH670-31840-3 HAS SEVERE CORROSION BEYOND OUT OF LIMITS IAW CRJ 700 SRM 53-00-00-101-001-A01. REMOVED PAX DOOR FWD HANDRAIL CUPS P/N SH670-31840-3 IAW CRJ 700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-41-02-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR FWD HANDRAIL CUP P/N SH670-31840-3S IAW CRJ 700 SRM 51-42-06-001-001-A01 AND SRM 51-41-02-001-001-A01
Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
AVI DOOR FWD INTERCOSTAL IS CORRODED AT STGR 26R. INSTALLED NEW SERVICEABLE INTERCOSTAL(DIAPHRAGM) IAW CRJ-700 SRM 51-42-06-001-001-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
STGR 19L IS CORRODED BETWEEN F.S. 349 TO F.S. 394. REPAIRED IAW CRJ700 SRM 53-00-03-201-201-001-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
"STRINGER 26R IS CORRODED BETWEEN F.S. 349 TO F.S. 364. REMOVED REMAINING FASTENERS THROUGH SKIN ON STGR 26R BETWEEN FS 333 TO FS 364 IAW CRJ-700 SRM 51-42-06-001-001-A01. REMOVED CORROSION ON STGR 26R BETWEEN FS 349-364 IAW CRJ 700 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS WAS .070, MATERIAL REMOVED WAS .015, REMAINING THICKNESS IS .055 AND IS OUT OF ALLOWABLE DAMAGE LIMITS IAW CRJ 700 SRM 53-21-03-101-006-A01 RECEIVED NEW SERVICEABLE STGR 26R (P/N SH670-31372-4S) BTW FS 333 TO FS 364. NEW STGR REQUIRES LOCATE AND DRILL. LOCATED AND DRILLED NEW SERVICEABLE STGR 26R (P/N SH670-31372-4S) BTW FS 333 TO FS 364 THROUGH THE ATTACHMENT ANGLE IAW CRJ-700 SRM 51-40-11-001-001-A01. INSTALLED STR 26R FS 333-364 IAW CRJ-700 SRM 51-42-06-001-001-A01 INSTALLED REMAINING FASTENERS COMMON TO STRINGER SPLICE IAW CRJ-700 SRM 51-42-06-001-001-A01 PRIME AND TOP COATED IAW CRJ-700 SRM 51-25-16-001-001-A01 APPLIED SEALANT ON THE EDGES OF STRINGER 26R (P/N SH670-31372-4S) BTW FS 333 TO FS 364. IAW CRJ-700 51-23-00-001-001-A01. "
Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
AVI DOOR FWD INTERCOSTAL IS CORRODED BETWEEN STGR 27 TO STGR 26L. REMOVED CORROSION ON INTERCOSTAL BETWEEN STGR 27 AND STGR 26L AND BETWEEN FS 349-364 IAW CRJ 700 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS DUE TO BEING IN A NO DAMAGE ALLOWED AREA IAW CRJ 700 SRM 53-21-23-101-003-A01. REMOVED 7EA RIVETS FROM INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01. REMOVED GUSSET FROM FS 364 BETWEEN STGR 27-26L IAW CRJ 700 SRM 51-42-21-001-001-A01. REMOVED INTERCOASTAL BETWEEN STGR 27-26L IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW AVI BAY DOOR FWD INTERCOSTAL BETWEEN STGR 27-26L (PN: SH670-32075-3) IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED NEW AVI BAY DOOR FWD INTERCOSTAL BETWEEN STGR 27-26L (PN: SH670-32075-3) IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED GUSSET FROM FS 364 BETWEEN STGR 27-26L IAW CRJ 700 SRM 51-42-21-001-001-A01. INSTALLED 7EA RIVETS IN AVI DOOR FWD INTERCOSTAL BETWEEN STGR 27-26L IAW CRJ 700 SRM 51-42-06-001-001-A01. APPLIED EDGE SEAL AND TOP COAT ON AVI BAY DOOR FWD INTERCOSTAL BETWEEN STGR 27-26L IAW CRJ 700 SRM 51-23-00-001-001-A01 AND 51-25-16-001-001-A01.
Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
SERVICE DOOR INTERCOSTAL IS CORRODED BETWEEN F.S. 310 TO F.S. 319 STGR 20R. EVALUATED AND FOUND TO BE OUT OF LIMITS IAW CRJ-700 SRM 53-21-23-101-002-A01, NOTE 2, THE CORROSION EXCEEDS 30% THE LENGTH OF A MEMBER. REMOVED INTERCOSTAL (PN# SH670-32047-1) FROM FS 310 TO FS 319 AT STR 20 IAW CRJ700 SRM 51-42-06-001-001-A01. LOCATED AND DRILL NEW SERVICEABLE INTERCOSTAL (PN# SH670-32047-1) BETWEEN F.S. 310 TO F.S.319, STR 20R IAW CRJ700 SRM 51-40-11-001-001-A01. REMOVED 1EA CLEAT (PN# SH670-32046-3) AND 1EA GUSSET (PN# SH670-31126-1) FROM FS 310 AND STR 20R IAW CRJ700 SRM 51-42-06-001-001-A01. REMOVED 1EA GUSSET (PN# SH670-31998-1) FROM FS 319 AND STR 20R IAW CRJ700 SRM 51-42-21-001-001-A01. DISCONNECTED GROUND STUD GS1844 AND GROUND STUD GS1842 FROM INTERCOSTAL AT STR 20R BETWEEN FS 310 TO FS 319 IAW CRJ700 SRM 51-41-02-001-001-A01 INSTALLED NEW SERVICEABLE INTERCOSTAL PN# SH670-32047-1 FROM FS 310-319 AT STR 20R IAW CRJ-700 SRM 51-42-06-001-001-A01. REINSTALLED 1 CLEAT PN# SH670-32046-3 AND 1 GUSSET PN# SH670-31126-1 FROM STA 310 STR 20R IAW CRJ-700 SRM 51-42-06-001-001-A01. REINSTALLED 1EA GUSSET (PN# SH670-31998-1) FROM FS 319 AND STR 20R IAW CRJ700 SRM 51-42-21-001-001-A01. CONNECTED GROUND STUD GS1844 AND GROUND STUD GS1842 FROM INTERCOSTAL AT STR 20R BETWEEN FS 310 TO FS 319 IAW CRJ700 SRM 51-41-02-001-001-A01
Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
SERVICE DOOR INTERCOSTAL IS CORRODED BETWEEN F.S. 349 TO F.S. 364. REMOVED INTERCOSTAL FROM FS 349 TO FS 364 (P/N: SH670-31749-3) FOR ACCESS IAW CRJ700 SRM 51-42-21-001-001-A01. REMOVED UNSERVICEABLE INTERCOSTAL FROM FS 349 TO FS 364 P/N: SH670-31994-1 IAW CRJ700 SRM 51-42-06-001-001-A01 UPON FURTHER INVESTIGATION THE SERVICE DOOR INTERCOSTAL IS LOCATED ON STR 20R BETWEEN FS 349 TO FS 364 AND IS FOUND TO BE OUT OF LIMITS IAW CRJ-700 SRM 53-21-23-101-002-A01, NOTE 2, THE CORROSION EXCEEDS 30% THE LENGTH OF A MEMBER. LOCATED AND DRILLED NEW INTERCOSTAL P/N: SH670-31994-1 IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE INTERCOSTAL FROM FS 349 TO FS 364 P/N: SH670-31994-1 IAW CRJ700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. INSTALLED SAME INTERCOSTAL FROM FS 349 TO FS 364 (P/N: SH670-31749-3) IAW CRJ700 SRM 51-42-21-001-001-A01.
Part: FRAME — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
"F.S. 333 IS CORRODED BETWEEN STGR 25L TO STGR 27. REMOVED CORROSION ON FS 333 BETWEEN STGR 25L-27 IAW CRJ 700 SRM 51-21-06-001-001-A01. MINIMUM REMAINING THICKNESS AT ALL BLEND LOCATIONS TO FS333.00 FRAME SEGMENT FROM STR 25L TO STR 26L AND STR 27 TO STR 26R IS .044"", (.006"" MATERIAL LOSS) AND ARE WITHIN THE ALLOWABLE BLEND DEPTH LIMITS OF CRJ 700 SRM 53-00-06-201-005-A01. REFERENCE TASK 11A FOR REPAIR OF FS333.00 FRAME SEGMENT ATTACHED FLANGE BETWEEN STR 26L AND STR 27 THAT HAS AN MRT OF .037"" AND IS BEYOND THE ALLOWABLE BLEND LIMITS OF CRJ 700 SRM 53-00-06-201-005-A01. PERFORMED CUTOUT ON FS 333 BETWEEN STRINGER 26L AND STRINGER 27 REQUIRES NDT IAW CRJ 700 SRM 53-00-06-201-004-A01. FABRICATED, LOCATED AND DRILLED FALSE FLANGE REPAIR FOR FS 333 BETWEEN STRINGER 26L AND STRINGER 27 IAW CRJ 700 SRM 53-00-06-201-004-A01. INSTALLED FALSE FLANGE REPAIR AT FS333 BETWEEN STR 26L TO STR27 IAW CRJ 700 SRM 53-00-06-201-004-A01. COMPLIED WITH REMAINING STEPS IAW CRJ 700 SRM 53-00-06-201-004-A01. REMOVED AND REINSTALLED 2 EA HYDRAULIC LINES TO BRACKETS WITH CORRECT CLAMPS BETWEEN FS 319 AND FS 349 ON STRINGER 27 IAW CRJ 700 SRM 51-41-04-001-001-A01."
Part: STRINGER — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
STRINGER 26L CORRODED ON UPPER SURFACE OF ATTACHED FLANGE BETWEEN FS333.00 AND FS349.00. REPAIRED IAW ENDEAVOR AIR EA NO. CRJ753-17445 ISSUE DATE: 10/2/2024 REV. IR.
Part: STRINGER — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
STGR 21R IS CORRODED BETWEEN F.S. 319 TO F.S. 364. UPON INVESTIGATION FOUND STR 21R FROM FS 333 TO FS 379 (P/N SH 670-31383-1) FREE AND ATTACHED FLANGE TO BE HEAVILY CORRODED BETWEEN FS364.00 TO FS379.00 AND BEYOND THE ALLOWABLE DAMAGE LIMITS OF CRJ700 SRM 53-21-03-101-006-A01 DUE TO CORROSION DEPTH. STRINGER REQUIRES REPLACEMENT FROM FS 333 TO FS 379. REFERENCE MWC HN00184963, SN 665 FOR REPLACEMENT OF STR 21R FROM FS 280 TO FS 333. REMOVED AND REINSTALLED CLEAT FROM STR 21R AND FS 364, BRACKET FROM STGR21R BETWEEN FS364-379, CABLE SUPPORT FROM STGR21R BETWEEN FS364-FS379, BRACKET AND GUSSET ON STGR 21R ON FS 364, WIRE BRACKET ASSY P/N SH670-41539-1 ON STR 21R AND STR 20R BETWEEN FS 364 AND FS 379 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-13-001-001-A01 APPLIED EDGE SEAL ON STR 21R FS280-FS379 IAW CRJ 700 SRM 51-23-00-001-001-A01. RESTORED INTERIOR AND EXTERIOR SURFACE FINISH IAW CRJ 700 SRM 51-25-16-001-001-A01. REMOVED AND REPLACED STRINGER (PN SH670-31383-1S) 21R BETWEEN F.S. 319 TO F.S. 364 REQUIRES IAW CRJ700 SRM 51-42-06-001-001-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
STGR 22R IS CORRODED BETWEEN F.S. 333 TO F.S. 349. INSTALLED NEW SERVICEABLE P/N: SH670-31379-1 AT STR22R BETWEEN FS333 AND FS349 IAW CRJ700 SRM 51-42-06-001-001-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
STGR 24R IS CORRODED BETWEEN F.S. 280 TO F.S. 310. EVALUATE CORROSION ON STR 24R FROM FS 280 TO FS 310 UPON FURTHER INVESTIGATION STR 24R FROM FS 280 TO FS 333 HAS DEEP CORROSION ON ATTACHED FLANGE STR 24R THERE IS NO DAMAGE ALLOWED IAW CRJ700 SRM 53-21-03-101-002-A01. STR 24R FROM FS 280 TO FS 333 REQUIRES REPLACEMENT. STRINGER 24R (PN SH670-31212-2) FROM FS 280 TO FS 333 REQUIRES REPLACE. REMOVED STRINGER 24R (PN SH670-31212-2) FROM FS 280 TO FS 333 IAW CRJ-700 SRM 51-42-06-001-001-A01 NEW SERVICEABLE STRINGER 24R (PN SH670-31212-2) FROM FS 280 TO FS 333 REQUIRES LOCATED DRILLED AND INSTALLED LOCATED AND DRILLED NEW SERVICEABLE STRINGER 24R P/N SH670-31212-2 FROM FS 280 TO FS 333 IAW CRJ700 SRM 51-40-11-001-001-A01. NEW SERVICEABLE STRINGER REQUIRE INSTALL. INSTALLED NEW SERVICEABLE STRINGER 24R P/N SH670-31212-2 FROM FS 280 TO FS 333 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. REQUIRE APPLY SEALANT AND PAINT. APPLIED PAINT AND SEALANT IAW CRJ700 SRM 51-25-16-001-001-A01 AND 51-23-00-001-001-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
STGR 20L IS CORRODED BETWEEN F.S. 379 TO F.S. 394. EVALUATED S20L FOUND 50% MATERIAL LOSS AND NO DAMAGE ALLOWED IN AREA FOUND TO BE OUT OF LIMITS IAW CRJ700 SRM 53-21-03-101-006-A01. REMOVED AND REPLACE STGR 20L SH670-31405-1 AT F.S. 349 - F.S. 477 BY FABRICATING FROM B0530021BF EXTRUSION. LOCATED AND DRILLED NEW SERVICEABLE STGR 20L , BETWEEN F.S. 379 - 469, FROM B0530021BF EXTRUSION PO 5-5780 IAW CRJ-700 SRM 51-40-11-001-001-A01. REMOVED AND REINSTALLED 01 AIR CONDITIONING SUPPORT ON STGR 20L, BETWEEN F.S. 437 - 453. IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. APPLIED EDGE SEAL, PAINTED AND CIC AT STGR 20L BETWEEN F.S. 349 - F.S. 477 IAW CRJ-700 SRM 51-25-16-001-001-A01, 51-21-11-001-001-A01 AND 51-23-00-001-001-A01.
Part: FRAME — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
F.S. 295 FRAME IS CORRODED BETWEEN STGR 19L TO STGR 20L LOCATED AND DRILLED NEW SERVICEABLE SUB FRAME P/N SH670-31941-3 AT FS295 BETWEEN STR18L AND 20L IAW CRJ700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE SUB FRAME P/N SH670-31941-3 AT FS 295 BETWEEN STGR 18L AND STGR 20L IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 39,291 hrs · 29,803 cycles
SERVICE DOOR INTERCOSTAL IS CORRODED BETWEEN F.S. 319 TO F.S. 333 STGR 20R. LOCATED AND DRILLED NEW INTERCOSTAL P/N: SH670-32004-1 BETWEEN FS 319.70 - FS 349 AT STGR 20 RH IAW CRJ 700 SRM 51-40-11-001-001-A01
Part: FRAME — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
F.S. 364 FRAME IS CORRODED ON THE FWD AND AFT SIDE BETWEEN STGR 19L TO STGR 20L. NEW SEGMENT OF FRAME P/N:SH670-31158-3 WAS INSTALLED IAW CRJ700 SRM TASK 51-42-06-001-001-A01.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 39,291 hrs · 29,803 cycles
FLOOR BEAM LBL9 FROM FS 549 TO FS 570 AREAS OF CORROSION REPAIRED IAW CRJ-700 SRM 53-00-41-201-001-A01 AND REO 670-53-31-943 REV -- DATED 09-20-2024.
Part: STRIKER — CORRODED (ZONE 800) · airframe 39,291 hrs · 29,803 cycles
AFT SIDE OF THE SERVICE DOOR SEAL STRIKER IS CORRODED AT THE BOTTOM OF THE DOOR ENTRY WAY. REMOVED CORRODED SEAL STRIKER AND INSTALLED NEW SERVICEABLE SERVICE DOOR LOWER SEAL STRIKE P/N:SH670-31412-7. IAW CRJ700 SRM 51-42-06-001-001-A01.
Part: SPLICE — CORRODED · airframe 39,291 hrs · 29,803 cycles
STR 25R CIRCUMFERENTIAL JOINT AT FS333 REQUIRES REPLACEMENT DUE TO CORROSION LOCATED AND DRILLED STR 25R CIRCUMFERENTIAL JOINT AT FS333 IAW CRJ 700 SRM 51-40-11-001-001-A01. NEW SERVICEABLE PART, P/N SH670-32429-4S. REFERENCE HN00184967, TASK 6A, FOR THE INSTILLATION OF STR 25R CIRCUMFERENTIAL JOINT, P/N SH670-32429-4S, AT FS333.
Part: STRINGER — CORRODED (ZONE 200) · airframe 39,291 hrs · 29,803 cycles
STGR 19L IS CORRODED BETWEEN F.S. 349 TO F.S. 394. REPAIRED IAW CRJ700 SRM 53-00-03-201-201-001-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
STRINGER 26R BETWEEN FS280 AND FS295 IS CORRODED LOCATED AND DRILLED AND INSTALLED NEW SERVICEABLE STGR 26R (P/N SH670-31634-2S) BTW FS 280 TO FS 333 THRU THE ATTACHMENT ANGLE IAW CRJ-700 51-40-11-001-001-A01 AND CRJ-700 SRM 51-42-06-001-001-A01.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 39,291 hrs · 29,803 cycles
FLOORBEAM RBL9 IS CORRODED AT FS549 PERFORMED PERMANENT REPAIR AT FLOOR BEAM RBL9 AT FS 549, IAW CRJ-700 SRM 53-00-41-201-001-A01, FIGURE 53-00-41-991-829.
Part: FRAME — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
FRAME FS517 CORRODED BETWEEN STRINGERS 18L AND 19L REMOVED STUB FRAME TO BLEND DAMAGE AREA AT FS517 BETWEEN STR18L TO STR19L, IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.EVALUATED AND FOUND TO BE OUT OF LIMITS DUE TO THE DAMAGE IS ON TWO ELEMENT AND MORE THAN20% MATERIAL LOSS, IAW CRJ-700 SRM 51-31-06-001-002-A01. LOCATED AND DRILLED NEW SERVICEABLE TOP STUB FRAME, P/N SH670-33177-1, IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE TOP STUB FRAME, P/N SH670-33177-1 AT FS517 BETWEEN STR18L TO STR19L, IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: STRINGER — CORRODED (ZONE 200) · airframe 39,291 hrs · 29,803 cycles
STRINGER 19R IS CORRODED BETWEEN FS549 AND FS565 RECEIVED AND COMPLIED WITH EA NO. CRJ753-17406. DATED: 10/1/2024. REV IR.
Part: STRINGER — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
STRINGER 19L IS CORRODED BETWEEN FS485 AND FS501 LOCATED AND DRILLED NEW STRINGER 19L FOR FS469-FS501 PN SH670-33143-1A IAW CRJ700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE STR 19L, PN SH670-33143-1A, FROM FS 469 TO FS 501 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01
Part: STRINGER — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
STRINGER 22R AT FS280 IS CORRODED INSTALLED NEW SERVICEABLE P/N: SH670-31210-2U STR22R BETWEEN FS280 AND FS333 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 39,291 hrs · 29,803 cycles
FLOOR BEAM CORRODED AT LBL 27 F.S. 985-1031 REPAIRED IAW CRJ700 SRM 53-00-41-201-001-A01 AND MHIRJ REO 670-53-61-2382 REV -- DATED 2024-10-03.
Part: STRINGER — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
STRINGER 23R AT FS280 IS CORRODED INSTALLED NEW SERVICEABLE STRINGER 23R PN SH670-31211-4U FROM FS 280 TO FS 333 IAW CRJ-700 SRM 51-42-06-001-001-A01.
Part: ANGLE — CRACKED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
FRAME F.S. 295 REINFORCEMENT ANGLE STR18L IS CRACKED. REPLACED REINFORCEMENT ANGLE PER SRM
Part: TIE DOWN — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
3 EA AFT CARGO TIE DOWN MOUNTING TILES CORRODED F.S. 1000-1047 LBL 34 BLENDED OUT CORROSION ON THE FOWARD AND AFT CARGO MOUNTING TILES P/N MM67035-35329-011 AT FS 1000 - FS 1047 @ LBL 34 AS NEEDED IAW CRJ 700 SRM 51-21-06-001-001-A01REPLACED MIDDLE AFT CARGO TIE DOWN MOUNTING TILE WITH NEW SERVICEABLE MOUNTING TILE P/N MM670-35329-011 IAW CRJ 700 SRM 51-42-06-001-001-A01RECEIVED AND COMPLIED WITH ENDEAVOR AIR EA # CRJ753-17372 REV IR DATED 9/21/2024 AND ENDEAVOR AIR EA # CRJ753-17373 REV IR DATED 9/21/2024
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 39,291 hrs · 29,803 cycles
FLOOR BEAM LBL9 IS CORRODED. REPAIRED PER MHIRJ REO 670-53-31-945/947.
Part: STRINGER — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
STRINGER 20R AT FS280 IS CORRODED RPLACED STRINGER 20R (PN# SH670-31208-3) FROM FS 280 TO FS 310 IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001- A01.
Part: FRAME — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
FS280 CIRCUMFERENTIAL JOINT INTERFACE IS CORRODED BETWEEN STRINGERS 18L AND 18R. REPAIRED F.S. 280 CIRCUMFERENTIAL BUTTSTRAP AT F.S. 280 BETWEEN STGR 18R TO STGR 18L IAW ENDEAVOR AIR EA CRJ 753-17298, DATED 11/20/2024, REV IR.
Part: FRAME — CORRODED (ZONE 100) · airframe 39,291 hrs · 29,803 cycles
FRAME F.S. 1015 STR21L-23R FWD SIDE OF STATION IS CORRODED REPAIRED PER EA CRJ753-17405
Part: INTERFACE UNIT — CORRODED (ZONE 800) · airframe 39,291 hrs · 29,803 cycles
PAX DOOR INTERCOSTAL DD6 PN601R31902-323 IS CORRODED. SEE SRM 52-11-06-001-001-A01 ITEM 75 FOR LOCATION. REMOVED PAX DOOR AFT INTERCOSTAL DD6 IAW CRJ700 SRM 51-42-06-001-001-A01 AND THEN LOCATED DRILLED AND INSTALLED NEW SERVICEABLE AFT INTERCOSTAL DD6 P/N:601R31902-323 IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01
Part: BRACKET — CORRODED (ZONE 800) · airframe 39,291 hrs · 29,803 cycles
PAX DOOR INTERCOSTAL DD5 BRACKET FOUND TO BE CORRODED REQUIRES REPLACEMENT PN: 601R31902-461 CRJ700 SRM 52-11-06-001-001-A01 ITEM 81 PAX DOOR FWD INTERCOSTAL BRACKET REPLACED AND INSTALLED IAW CRJ700 SRM 51-42-06-001-001-A01 PN: 601R31902-461
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 39,291 hrs · 29,803 cycles
PAX DOOR FORWARD INTERCOSTAL DD6 PN601R31902-485 IS CORRODED SEE SRM52-11-06-001-001-A01 ITEM 82 FOR LOCATION. REMOVED PAX DOOR FWD INTERCOSTAL DD6 IAW CRJ700 SRM 51-42-06-001-001-A01 NEW SERVICEABLE PAX DOOR FWD INTERCOSTAL DD6 HAS BEEN LOCATED AND DRILLED IAW CRJ700 SRM 51-40-11-001-001-A01 PN: 601R31902-485 INSTALLED PAX DOOR FWD INTERCOSTAL DD6 IAW CRJ700 SRM 51-42-06-001-001-A01
2022
Part: LAMP — INOPERATIVE · airframe 38,834 hrs · 29,372 cycles
EXTERIOR EMERGENCY LIGHT (LEFT AFT) BURNT OUT. R/R'D BULB AT LH AFT EMERGENCY LIGHT (EXTERIOR) IAW CRJ 700 AMM 33-51-15. OPC NORMAL P/N OFF/ON: 8GH002473-08
2020
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,192 hrs · 26,972 cycles
PAX DOOR INTERCOSTAL DD4 P/N 601R318081-1 FOURTH FROM HINGE BETWEEN FS 320.163 TO FS 338.96 IS CORRODED. REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD4, IAW CRJ700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,192 hrs · 26,972 cycles
PAX DOOR INTERCOSTAL DD2 P/N 601R-318052-1 THIRD FROM BOTTOM AFT BETWEEN FS 338.963 TO FS 347.25 IS CORRODED. REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD2, IAW CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,192 hrs · 26,972 cycles
PAX DOOR INTERCOSTAL DD6 P/N #601R318057-1 2ND FROM HINGE BETWEEN FS 328.163 TO FS 338.963 IS CORRODED. REMOVED AND REPLACED INTERCOSTAL DD6, IAW CRJ700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
2019
Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,716 hrs · 25,736 cycles
EMERGENCY CEILING FLOOD LIGHT INOP ON ROW 4. R&R LIGHT BULB IAW AMM 33-51-09. OPS CHECK GOOD AT THIS TIME. P/N ON/OFF: 1317 S/N ON/OFF: NSN
Part: WEB — CRACKED (PAX DOOR) · airframe 33,726 hrs · 24,924 cycles
PASSENGER DOOR AFT WEB IS CRACKED AT TOP STEP. CORRECTIVE ACTION: REMOVED AND REPLACED AFT WEB(PN:601R317071-11) IAW CRJ 700 SRM 51-42-06..
2018
Part: DOUBLER — CRACKED (PAX DOOR) · airframe 33,726 hrs · 24,924 cycles
PASSENGER DOOR PULLIN CAM DOUBLER IS CRACKED. CORRECTIVE ACTION: REMOVED CRACKED DOUBLER FABRICATED AND INSTALLED NEW DOUBLER IAW CRJ 700 SRM 52-11-06, 52-11-02, 51-42-06, 51-42-02, 51-21-11, 51-25-06
Part: STRINGER — CORRODED (BS 280-333) · airframe 33,726 hrs · 24,924 cycles
STRINGER 25R IS CORRODED BETWEEN F.S. 280-F.S.333. CORRECTIVE ACTION: REMOVED CORRODED AREA FABRICATED AND INSTALLED REPAIR PARTS IAW GO JET ENGINEERING ORDER C700-53MR-005-0 DATED 08 NOV 2018.
Part: FRAME — CORRODED (BS 295) · airframe 33,726 hrs · 24,924 cycles
FRAME 295 IS CORRODED BETWEEN STGR 25L AND 25R. CORRECTIVE ACTION: REMOVED CORRODED FRAME AREA AND INSTALLED REPAIR PARTS IAW GO JET ENGINEERING ORDER C700-53MR-004-R1 DATED 26 NOV 2018.
Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 33,726 hrs · 24,924 cycles
VERTICAL STABILIZER L/H FWD DRAG ANGLE IS CRACKED. CORRECTIVE ACTION REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW BOMBARDIER REO 670-5531-098 REV.-- DATED 2017-06-28, AND 670-55-31-018 REV. A DATED 2016-11-10
Part: RETAINER — CORRODED (E/E BAY DOOR) · airframe 33,726 hrs · 24,924 cycles
MAIN AVIONICS DOOR AFT OB SEAL REATINER IS CORRODED. CORRECTIVE ACTION REMOVED AND REPLACE SEAL RETAINER(PN:CC670-38662-5S) IAW CRJ 700 SRM 51-40-11, AND 51-42-06
Part: RETAINER — CORRODED (E/E BAY DOOR) · airframe 33,726 hrs · 24,924 cycles
MAIN AVIONICS DOOR AFT OB SEAL REATINER IS CORRODED. CORRECTIVE ACTION REMOVED AND REPLACE SEAL RETAINER(PN:CC670-38675-3) IAW CRJ 700 SRM 51-40-11, AND 51-42-06
Part: RETAINER — CORRODED (E/E BAY DOOR) · airframe 33,726 hrs · 24,924 cycles
MAIN AVIONICS DOOR FWD IB SEAL REATINER IS CORRODED. CORRECTIVE ACTION REMOVED AND REPLACE SEAL RETAINER(PN:CC670-38674-3) IAW CRJ 700 SRM 51-40-11, AND 51-42-06
Part: RETAINER — CORRODED (E/E BAY DOOR) · airframe 33,726 hrs · 24,924 cycles
MAIN AVIONICS DOOR FWD OB SEAL REATINER IS CORRODED. CORRECTIVE ACTION REMOVED AND REPLACE SEAL RETAINER(PN:CC670-38675-3S) IAW CRJ 700 SRM 51-40-11, AND 51-42-06
Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 33,726 hrs · 24,924 cycles
RIGHT HAND FLOOR SILL AT F.S. 280.00-F.S. 319.00 IS CORRODED. CORRECTIVE ACTION REMOVED AND REPLACED THE R/H SILL(PN:SH670-32172-5) IAW BOMBARDIER REO 670-53-00-390 REV.-- DATED 22 JAN 2014.
Part: POST — CRACKED (COCKPIT) · airframe 33,726 hrs · 24,924 cycles
RT WINDSHIELD SIDE POST CRACKED. REMOVED AND REPLACED RT WINDSHIELD SIDE POST IAW SRM 51-42-21.
Part: ANGLE — CORRODED (PAX DOOR) · airframe 33,726 hrs · 24,924 cycles
PAX DOOR MID CAP HAS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED MID CAP ANGLE IAW CRJ 700 SRM 51-42-06, 51-41-02.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 33,726 hrs · 24,924 cycles
INTERCOSTAL BELOW PAX DOOR STRUCTURE HAVE SIGNS OF CORROSION BETWEEN FS 319.00 AND FS 333.00. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-11, 51-42-06, 51-42-21.
Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 33,726 hrs · 24,924 cycles
LT FWD FUSELAGE TO VERTICAL DRAG ANGLE HAS SIGNS OF CRACKING AT FS 1200. REPAIRED LT FWD FUSELAGE TO VERTICAL DRAG ANGLE AT FS 1200 IAW REO 670-55-31-018, REV A, 2016-11-10 AND REO 670-55-31-098, 2017-06-28.
Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 33,726 hrs · 24,924 cycles
RT, AFT FUSELAGE TO VERTICAL DRAG ANGLE HAS SIGNS OF CRACKING AT FS 1200. REPAIRED RT AFT FUSELAGE TO VERTICAL DRAG ANGLE AT FS 1200 IAW REO 670-55-31-018, REV A, 2016-11-10.
Part: DETECTION SYS — MALFUNCTIONED (ANTI-ICE) · airframe 32,532 hrs · 23,802 cycles
ANTI-ICE DUCT MESSAGE. PERFORMED A RESET AND OPS CHECKED THE BLEED LEAK DETECTION AND WARNING IAW AMM 36-21-00. ALL CHECKED GOOD. ACFT OK FOR SERVICE.
2017
Part: COVER — UNSECURE (EMERGENCY EXIT) · airframe 31,937 hrs · 23,294 cycles
RT SIDE EMERGENCY EXIT HANDLE WILL NOT STAY CLOSED. SECRURED THE HANDLE COVER IAW AMM 51-22-61. OK FOR SERVICE.
Part: COVER — UNSECURE (EMERGENCY EXIT) · airframe 31,937 hrs · 23,294 cycles
RT SIDE EMERGENCY EXIT HANDLE WILL NOT STAY CLOSED. SECRURED THE HANDLE COVER IAW AMM 51-22-61. OK FOR SERVICE.
Part: WARNING MESSAGE — FALSE ACTIVATION (PAX DOOR HANDLE) · airframe 30,400 hrs · 21,915 cycles
PAX DOOR OUTER HANDLE CAUTION INTERMITTENT IN FLIGHT. PERFORMED OPS TEST OF PAX DOOR OUTER HANDLE IAW AMM 52-11-03, OPS TESTED GOOD. NO DEFECTS. OK FOR SERVICE. PERFORMED A TEST OF THE DOOR WARNING SYS IAW AMM 52-70-00, OPS TESTED GOOD. NO DEFECTS NOTED.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 30,085 hrs · 21,673 cycles
FUSELAGE FS202.75 FWD SIDE OF BULKHEAD RBL30 STIFFENER HAS INDICATION .25 LONG IN THE UPPER EDGE OF FLANGE, FAILED NDT.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,031 hrs · 21,627 cycles
SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-17. OPS CHECKED GOOD, NO DEFECTS NOTED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,026 hrs · 21,623 cycles
FWD STOWAGE EMERGENCY LIGHTS INOPERATIVE.
2016
Part: TRANSITION PANEL — DAMAGED · airframe 30,018 hrs · 21,618 cycles
TRANSITION PANEL DAMAGED. REMOVED AND REPLACED THE LEFT FWD TRANSITION PANEL IAW SRM 53-21-23, 51-42-21, 51-42-06, 51-24-36, 51-40-11, 51-25-16, 51-42-22, 51-11-00, 51-21-11, AND AMM 52-11-05,20-70-00.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 30,018 hrs · 21,618 cycles
PASSENGER DOOR AFT DRAG ANGLE IS CRACKED. REPLACED THE DRAG ANGLE IAW REO 670-52-11-072 REV. G.
Part: SKIN — CORRODED (PAX DOOR) · airframe 30,018 hrs · 21,618 cycles
PASSENGER DOOR HAS AREAS OF CORROSION ON INNER SKIN. REMOVED AND REPLACED THE DOOR SKIN IAW SRM5 1-40-11, 51-42-06, 51-25-16, AMM 51-26-00, 51-42-10, 51-42-11, 51-42-12, 51-42-13 AND 51-42-22.
Part: SEAL — DIRTY (ESCAPE HATCH) · airframe 29,712 hrs · 21,381 cycles
ESCAPE HATCH SEAL IS LEAKING SEVERLY. CLEANED THE ESCAPE HATCH. OPENED AND CLOSED THE ESCAPE HATCH IAW 52-22-00. NO LEAKS NOTED.
Part: WARNING MESSAGE — ILLUMINATED (PAX DOOR LATCH) · airframe 29,619 hrs · 21,309 cycles
PAX DOOR LATCH CAUTION MESSAGE.
Part: WARNING MESSAGE — MALFUNCTIONED (PAX DOOR) · airframe 29,604 hrs · 21,297 cycles
PAX DOOR WARNING MESSAGE WILL NOT SHOW CLOSED. PERFORMED OPS CHECK OF DOOR IAW AMM 52-11-00 OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,504 hrs · 21,226 cycles
PASSENGER DOOR SKIN CUTOUT DAMAGED ON LOWER FWD CORNER. CUT OUT DAMAGE, FABRICATED AND INSTALLED A REPAIR IAW REO 670-53-21-1330 AND REO 670-53-21-001.
Part: FRAME — CORRODED (BS 310) · airframe 29,504 hrs · 21,226 cycles
FRAME BS 310 BETWEN STRINGERS 25 AND 26L IS CORRODED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW REO 670-53-21-799.
Part: STRUCTURE — GOUGED (LT ELEVATOR) · airframe 29,504 hrs · 21,226 cycles
LEFT ELEVATOR T/E HAS A GOUGE BETWEEN RIBS 4 AND 5. REMOVED DAMAGE FROM LT ELEVATOR T/E BETWEEN RIBS 4 AND 5, AND FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 55-21-01-991-815, SHEET 1. NDT PERFORMED WO A16-1084.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,504 hrs · 21,226 cycles
LEFT FLOOR SEAT TRACK 34 COUNTINUING AFT IS CORRODED. R & R LT FLOOR SEAT TRACK 34, PN:SH670-RPA0045 COUNTINUING AFT IAW AMM 53-00-49, 51-21-01, AND REO 670-53-00-074.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 29,504 hrs · 21,226 cycles
INTERCOSTAL DD2 ON PASSENGER DOOR IS CORRODED. R & R INTERCOSTAL DD2 ON PASSENGER DOOR IAW SRM 51-42-06, 51-42-21.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 29,504 hrs · 21,226 cycles
PASSENGER DOOR HAS CORRODED INTERCOSTAL. R & R INTERCOSTAL DD6 IAW SRM 51-42-21, 51-42-06.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,504 hrs · 21,226 cycles
RIGHT FORWARD COUNT AFT NR 6 SIDE SEAT RAIL CORRODED. R & R RT FORWARD COUNTING AFT NR 6 SIDE SEAT RAIL IAW AMM 53-00-49, REO 670-53-00-74, REV A 2009/3/05, AMM 51-21-01, AND SRM 51-40-11.
Part: FORMER — CORRODED (PAX DOOR) · airframe 29,504 hrs · 21,226 cycles
PASSENGER DOOR CENTER FORMER IS CORRODED. R & R PASSENGER DOOR CENTER FORMER IAW SRM 51-42-06, 51-42-21, 51-25-16.
Part: STRAP — CORRODED (FUSELAGE) · airframe 29,504 hrs · 21,226 cycles
AFT BELLY FAIRING CENTER STRAP IS MISSING RIVETS, AND SHOWING SIGNS OF CORROSION. FABRICATED AND INSTALLED CENTER STRAP, A670-39171, IAW SRM 51-42-15, 51-42-06, 51-25-06, 51-21-11, 51-42-13, 51-40-11, 51-24-36, 51-25-16, AND PLCC670-39171.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,504 hrs · 21,226 cycles
LEFT FWD COUNTING AFT NR 5 SIDE SEAT RAIL CORRODED. R & R LT SEAT RAIL IAW AMM 53-00-49.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 29,504 hrs · 21,226 cycles
INTERCOSTAL DD4 ON PASSENGER DOOR IS CORRODED. R & R INTERCOSTAL DD4 ON PASSENGER DOOR IAW SRM 51-42-21, 51-42-06.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,504 hrs · 21,226 cycles
LEFT FORWARD COUNTING AFT NR 6 SIDE SEAT RAIL CORRODED FS 790.0. R & R LT FORWARD COUNTING AFT NR 6 SIDE SEAT RAIL AT FS 790.00 IAW AMM 53-00-49, REO 670-53-00-074, REV A.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,504 hrs · 21,226 cycles
RIGHT FLOOR SEAT TRACK BETWEEN FS 581.00 AND 677.00 IS CORRODDED. R & R FLOOR SEAT TRACK, PN:SH670-33425-1, BETWEEN FS 581.00 AND FS 677.00 IAW AMM 53-00-49.
Part: SEAT TRACK — CORRODED (BS 677-761) · airframe 29,504 hrs · 21,226 cycles
RIGHT SIDE SEAT TRACK, BS 761.85 - 677 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49, REO 670-53-00-074 REV A, SRM 51-42-13, 51-42-21, AND AMM 53-00-49,
Part: SEAT TRACK — CORRODED (BS 863-969) · airframe 29,504 hrs · 21,226 cycles
LEFT SIDE SEAT TRACK CORRODED AT BS 863-969. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-074 REV. A, AND AMM 53-00-49 AND 51-21-01.
Part: SEAT TRACK — CORRODED (BS 517-581) · airframe 29,504 hrs · 21,226 cycles
LEFT SEAT TRACK BETWEEN BS 517 - 581 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.
Part: SEAT TRACK — CORRODED (BS 677-693) · airframe 29,504 hrs · 21,226 cycles
RIGHT SEAT TRACK BETWEEN BS 677 - 693 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.
Part: FLOOR SUPPORT — CORRODED (BS 280-310) · airframe 29,504 hrs · 21,226 cycles
RIGHT FLOOR SUPPORT AT BS 280 - 310 CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-11, 51-42-13, 51-42-06, 51-25-16, AND 51-21-11.
Part: STRINGER — CORRODED (BS 295-310) · airframe 29,504 hrs · 212,226 cycles
STRINGER 25R BETWEEN BS 295 - 310 FOUND TO BE CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06, 51-42-02, AND 51-42-21.
Part: ANGLE — CORRODED (ZONE 200) · airframe 29,504 hrs · 21,226 cycles
GALLEY SERVICE DOOR MIDCAP CORRODED. REMOVED, LOCATED, DRILLED, AND INSTALLED NEW SERVICE DOOR MIDCAP IAW SRM 51-71-00, 51-42-06, AND 51-42-21.
Part: FIRESHIELD — GOUGED (RT NACELLE) · airframe 29,504 hrs · 21,226 cycles
RIGHT LOWER COWLING FIRESHIELD GOUGED. REPAIRED THE FIRESHIELD IAW REO 670-54-23-459 REV B.
Part: SKIN — DENTED (TE FLAP) · airframe 29,504 hrs · 21,226 cycles
LEFT INBD FLAP LOWER SKIN BETWEEN WS 30.00-36.00 HAS A DENT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-57-52-3536, DATED 29, AUG 2016 AND SRM 51-42-13, NDT PERFORMED WO A16-1082, DATED 31 AUG 2016.
Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 29,504 hrs · 21,226 cycles
FS 280 BEAM LT IS CRACKED. REPAIRED FS 280 CROSSBEAM LT SIDE IAW SB 670BA-53-026, REV B DATE 5DEC2006, SRM 53-11-41. NDT PERFORMED PO 135885, WO A16-1462. NO CRACK INDICATIONS NOTED.
Part: FRAME — CORRODED (BS 295) · airframe 29,504 hrs · 21,226 cycles
FRAME BS 295 BETWEEN STRINGERS 25 - 26L CORRODED OUT OF LIMITS. REPAIRED THE FRAME IAW REO 670-53-21-1281. NDT PERFORMED. NO CRACK INDICATIONS NOTED.
Part: SEAT TRACK — CORRODED (BS 675-713) · airframe 29,504 hrs · 21,226 cycles
RIGHT SEAT TRACK AND ATTACHING HARDWARE FROM BS 675 - 713 IS CORRODED. REPLACED THE SEAT TRACK IAW AMM 53-00-49.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,847 hrs · 20,732 cycles
ROW 9 CEILING EMER FLOOD LIGHT INOPERATIVE. DEFERRED ROW 9 EMER FLOOD LIGHT IAW MEL 33-51-01B CAT C.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,766 hrs · 20,671 cycles
EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 EPSU BATTERY PACK IAW AMM 33-51-17.
Part: FLOOR SUPPORT — CORRODED (BS 1015-1031) · airframe 28,481 hrs · 28,481 cycles
CORROSION ON FLOORBEAM AT LBL 9.0 BETWEEN FS 1015.00 AND FS 1031.00. COMPLIED WITH REO 670-53-00-029, REV -A.
2015
Part: LIGHT — MISSING (CABIN) · airframe 26,733 hrs · 19,108 cycles
EMERGENCY SIGN LIGHT NEAR FWD PAX DOOR IS MISSING LIGHTS. DEFERRED ON MEL 33-51-01E CAT C.
Part: WHEEL — MALFUNCTIONED (CABIN DOOR) · airframe 26,699 hrs · 19,080 cycles
MAIN CABIN DOOR WHEEL DID NOT DEPLOY. CHECKED DOOR & FUSELAGE FOR ANY DAMAGE, NO DAMAGE NOTED. PERFORMED OPERATIONS CHECK OF SUPPORT WHEEL IAW AMM 52-11-13. OPERATIONS CHECKED GOOD.
Part: CABLE — OUT OF ADJUST (CABIN DOOR) · airframe 26,699 hrs · 19,080 cycles
GROUND WHEEL ON MAIN CABIN DOOR DID NOT DEPLOY WHEN DOOR WAS OPENED. INSPECTED & ADJUSTMENT OF SUPPORT WHEEL CABLE IAW AMM 52-11-13. OPERATIONS CHECKED GOOD.
Part: GLOWSTRIP — WORN (CABIN) · airframe 26,643 hrs · 19,038 cycles
PHOTO LUMINESCENT STRIP WORN AT 4 CD. DEFERRED PHOTO LUMINESCENT STRIP IAW MEL 33-51-01G CAT C.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 26,454 hrs · 18,895 cycles
EXIT SIGN ON RT EMER EXIT HAS TWO LIGHTS OUT, LOWER RT EXIT SIGN. DETERMINED 50% OF THE LOWER RT EXIT SIGN TO BE OPERATIVE. DEFERRED RT LOWER EXIT SIGN IAW MEL 33-51-01F CAT C.
Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 26,448 hrs · 18,891 cycles
NOSE WHEEL STEERING INOPERATIVE, CAUTION MSG. RESET NOSE WHEEL STEERING IAW SOP CH 5-1 8. NOSE WHEEL STEERING OPERATIONAL CHECKED GOOD.
Part: COVER — UNSECURE (EMERGENCY EXIT) · airframe 25,843 hrs · 17,548 cycles
RIGHT EMER EXIT COVER IS FALLING DOWN. SECURED RT EMER OVERWING EXIT COVER IAW AMM 51-22-61.
Part: WHEEL — MALFUNCTIONED (PAX DOOR) · airframe 26,138 hrs · 18,660 cycles
PASSENGER DOOR SUPPORT WHEEL DID NOT DEPLOY. PERFORMED OPERATIONS CHECK ON PAX DOOR IAW AMM 52-11-00. COULD NOT DUPLICATE EVENT. OPERATIONS CHECKED GOOD AT THIS TIME.
2014
Part: POWER UNIT — INOPERATIVE (PAX DOOR) · airframe 25,674 hrs · 18,288 cycles
PASSENGER DOOR POWER ASSIST INOPERATIVE. DEFERRED PAX DOOR POWER ASSIST IAW MEL 52-11-01A CAT C.
Part: STEP — CRACKED (PAX DOOR) · airframe 25,252 hrs · 17,955 cycles
PAX DOOR STEP NR 3 HAS DENT WITH A CRACK. REPAIRED DAMAGE TO PAX DOOR STEP NR 3 IAW REO 670-52-11-791 REV DATED 2014-09-13.
Part: SKIN — CORRODED (PAX DOOR) · airframe 25,252 hrs · 17,955 cycles
PAINT BUBBLING UNDER PAX DOOR PANELS 832JL, 832HL, 832DL, 832AB, 832GL & 832DR. REPAIRED DOOR INNER SKIN UNDER PANELS IAW 700 SRM 52-11-01. REPAIRED PAX DOOR INNER SKIN UNDER PANEL 832BL IAW REO 670-52-11-790 REV DATED 2014-09-14. SEE WORK ORDER 80245 WC 8045.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 25,252 hrs · 17,955 cycles
FLOORBEAM AT FS 280 IS CRACKED & CORRODED. R & R FLOORBEAM WITH NEW PN CC670-34175-7S IAW SRM 51-42-06 & SB 670BA-53-026. WORK ORDER 80245 WC 1053.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 25,252 hrs · 17,955 cycles
FLIGHT COMPARTMENT FLOOR QUARTER TURN ANGLE AT FS 280, LBL12 & RBL12 IS CORRODED. R & R QUARTER TURN ANGLE IAW SRM 51-42-06. WORK ORDER 80245 WC 1052.
Part: MECHANISM — JAMMED (PAX DOOR) · airframe 25,252 hrs · 17,955 cycles
PAX DOOR INNER HANDLE RETENTION MECHANISM JAMMED & ROLLER ASSEMBLY HAS EXCESSIVE PLAY. REPAIRED INNER HANDLE DETENT ASSEMBLY BY REPLACING ROLLER PN 600-38109-7, BEARING PN M8193411-04A008, BEARING PN 600-38040-33, COMPRESSION SPRING PN LC-063F-6M, PIN PN MS20392-3C17 & WASHER PN BO202026U1616-20 IAW AMM 52-11-02 & CMM 52-11-00. WORK ORDER 80245 WC 8044.
Part: ATTACH BRACKET — CRACKED (PAX DOOR) · airframe 25,252 hrs · 17,955 cycles
PAX DOOR PULLEY ATTACHMENT CLIP IS CRACKED. R & R PAX DOOR PULLEY BRACKET IAW SRM 51-42-10. WORK ORDER 80245 WC 8042.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 25,252 hrs · 17,955 cycles
RIGHT FLOOR SILL AT FS 280 TO 319 IS CORRODED. R & R SILL IAW SRM 51-42-06. WORK ORDER 80245 WC 1051.
Part: FITTING — CRACKED (FUSELAGE) · airframe 25,252 hrs · 17,955 cycles
FS 280 LT & RT BACKING ANGLES FITTING CRACKED AT LBL 9 & RBL 9. R & R LT PN BA670-30068-1, & RT PN BA670-30068-2 FITTINGS IAW SRM 51-42-21. WORK ORDER 80245 WC 1054.
Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 25,252 hrs · 17,955 cycles
LEFT & RIGHT BULKHEAD LOWER WEBS CORRODED AT FS 280. REMOVED WEBS, FABRICATED NEW WEBS & INSTALLED IAW REO 670-53-11-594 REV DATED 27 APR 2011. WORK ORDER 80245 WC 1050.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 25,252 hrs · 17,955 cycles
AFT BODY FAIRING SUPPORT WEB & ANGLE ARE CORRODED. REPAIRED SUPPORT STRUCTURE BY REMOVING LIGHT SURFACE CORROSION & TREATING IAW SRM 51-21-06 & 51-25-06. R & R ANGLE IAW SRM 51-42-06. WORK ORDER 80245 WC 1074.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 25,252 hrs · 17,955 cycles
CRAWLWAY ANGLE AT FS 280 IN AVIONICS BAY CORRODED. R & R CRAWLWAY ANGLE IAW SRM 51-42-06.
Part: ATTACH FITTING — CORRODED (FA SEAT) · airframe 25,252 hrs · 17,955 cycles
FLIGHT ATTENDANT SEAT COMPARTMENT FOOT ATTACHMENT CORRODED. REPLACED FOOT ATTACHMENT TO FWD FLIGHT ATTENDANT SEAT IAW AMM 20-21-00.
Part: PLACARD — WORN (PAX DOOR) · airframe 24,692 hrs · 17,521 cycles
PASSENGER DOOR, OPEN, PLACARD IS WORN. PLACED PLACARD ON NEF 25-500-0 CAT 5.
Part: HOOK AND LOOP — WORN (EMERGENCY EXIT) · airframe 24,345 hrs · 17,246 cycles
LEFT EMERGENCY EXIT COVER WON'T STAY UP. REPLACED HANDLE COVER VELCRO IAW AMM 25- 06-09, AT THIS TIME ACFT OK FOR SERVICE.
Part: CONTROL CABLE — FOD (RUDDER) · airframe 24,304 hrs · 17,214 cycles
RUDDER PEDALS HARD TO MOVE. LEFT WILL NOT CENTER. INSPECTED RUDDER CABLES & FOUND FOD ON RUDDER CABLES IN THE AFT EQUIPMENT BAY. REMOVED FOD, PERFORMED OPERATIONS TEST IAW AMM 27-21-00, OPERATIONS TESTED GOOD.
Part: HOOK AND LOOP — UNSECURE (EMERGENCY EXIT) · airframe 24,304 hrs · 17,214 cycles
EMERGENCY OVERWING EXIT HANDLE COVER FELL OFF. SECURED HOOK AND LOOP ON LT OVERWING EXIT DOOR AS REQUIRED. OK FOR SERVICE IAW AMM 52-70-10.
Part: WHEEL — MALFUNCTIONED (PAX DOOR) · airframe 24,187 hrs · 17,128 cycles
PASSENGER DOOR STRUCK RAMP, WHEEL DID NOT DEPLOY. PERFORMED GVI & OPERATIONAL CHECK OF DOOR. NO MSG OR DOOR INTERFERENCE. ACFT SAFE FOR A ONE TIME FLIGHT FROM DTW TO LGA.
Part: UNKNOWN — MALFUNCTIONED (PAX DOOR) · airframe 24,020 hrs · 17,005 cycles
PASSENGER DOOR FELL TO THE GND, WHEEL DID NOT DEPLOY, DOOR DID NOT HIT THE GND. DEACTIVATED PAX DOOR ASSIST MOTOR & DEFERRED SYS IAW MEL 52-11-01 CAT C.
Part: CABLE — OUT OF POSITION (PAX DOOR) · airframe 23,898 hrs · 16,906 cycles
PASSENGER DOOR FREE FELL. REPOSITION PAX DOOR CABLE IAW CRJ700 AMM 52-11-00. PERFORMED OPERATIONS CHECK OF PAX DOOR IAW CRJ700 AMM 52-11-00. OPERATIONS CHECKED GOOD AT THIS TIME.
2013
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,712 hrs · 16,767 cycles
OVERHEAD EMERGENCY LIGHTS OUT AT ROWS 4 & 15. R & R EMERGENCY LIGHT BULB AT ROW 4 & 15 IAW CRJ700 AMM 33-51-09. OPERATIONS CHECKED GOOD AT THIS TIME.
Part: WARNING SYSTEM — FALSE ACTIVATION (PAX DOOR) · airframe 23,592 hrs · 16,978 cycles
PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE & PROX SYS 2 STATUS MESSAGE. PERFORMED OPERATION CHECK OF PROX SYS FAULT 2 IAW FIM 32-60-00-810-808-AO1, OPERATIONS CHECKED GOOD AT THIS TIME.
Part: INDICATOR — FAULTY (PAX DOOR) · airframe 23,506 hrs · 16,616 cycles
PASSENGER DOOR OUTER HANDLE CAUTION. DEFERRED PAX DOOR INDICATOR ON DMI 303460000 IAW MEL 52-70-01 CAT C.
Part: WARNING SYSTEM — FALSE ACTIVATION (PAX DOOR) · airframe 23,498 hrs · 16,610 cycles
OUTER PAX DOOR HANDLE CAUTION MESSAGE IN FLIGHT. OPERATION & FUNCTIONAL CHECKED GOOD AT THIS TIME IAW CRJ700 AMM 52-11-00.
Part: WARNING MESSAGE — ILLUMINATED (RT A/C PACK) · airframe 23,486 hrs · 16,596 cycles
ABORTED TAKEOFF DUE TO RT PACK FAULT STATUS MESSAGE BELOW 60KTS.
Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 23,472 hrs · 19,646 cycles
LEFT EMERGENCY DOOR CAUTION MESSAGE. PERFORMED ADJUSTMENT TEST OF OVERWING EMERGENCY EXIT IAW AMM 52-70-10. OPS CHECKED GOOD AT THIS TIME.
Part: WARNING MESSAGE — FALSE ACTIVATION (PAX DOOR) · airframe 223,456 hrs · 16,576 cycles
PAX DOOR HANDLE CAUTION MESSAGE INTERMITTENT IN FLIGHT. CYCLED PAX DOOR THROUGH SEVERAL TIMES, NO DEFECTS NOTED, OPS CHECKED GOOD IAW AMM 52-70-04.
Part: DOOR — UNSECURE (EMERGENCY EXIT) · airframe 23,429 hrs · 16,555 cycles
LEFT EMERGENCY EXIT OVERWING DOOR INDICATION INTERMITTENTLY ON DURING TAXI. INSPECTED AND RESEATED LT EMERGENCY EXIT DOOR AND PERFORMED OP'S CHECK IAW AMM 52-21-00, OPS CHECK GOOD.
Part: WARNING MESSAGE — FALSE ACTIVATION (STABILATOR) · airframe 23,328 hrs · 16,474 cycles
STABILATOR FAULT STATUS MESSAGE. PERFORMED SPOST 1 AND SPOST 2 TESTS AMM 27-40-00, MESSAGE CLEARED.
Part: WARNING MESSAGE — MULTIPLE FAIL · airframe 23,259 hrs · 16,416 cycles
DURING TAKEOFF, CAUTION MESSAGES DISPLAYED. PERFORMED OP'S CHECK OF STALL PROTECTION SYS IAW AMM 27-35-01, OPS CHECKED GOOD, OPS CHECK OF ANTI-ICE AND PITOT SYS IAW AMM 30-12-00 & 30-31-00, OPS CHECKED GOOD.
Part: DOOR — LACK OF LUBE (EMERGENCY EXIT) · airframe 23,047 hrs · 16,248 cycles
LEFT EMERGENCY DOOR CAUTION MESSAGE. LUBRICATED EMERGENCY DOOR IAW AMM 52-21-06. OP'S CHECKED GOOD AT THIS TIME.
Part: WARNING MESSAGE — ILLUMINATED (LT A/C PACK) · airframe 22,950 hrs · 16,178 cycles
LEFT PACK FAULT MESSAGE.
Part: WARNING LIGHT — FALSE ACTIVATION (OVERWING DOOR) · airframe 22,931 hrs · 16,163 cycles
ABORTED TAKEOFF FOR LT OVERWING EMERGENCY DOOR CAUTION MESSAGE WHEN ADDED POWER FOR TAKEOFF. INSPECTED DOOR FOR SECURITY, FOUND TO BE SECURE, DEFERED DOOR INDICATION ON MEL 52-70-03.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,729 hrs · 16,001 cycles
CEILING EMERGENCY FLOODLIGHT INOPERATIVE AT ROW 4. R & R FLOOD LIGHT AT ROW 4 IAW AMM 33-51-09, OP'S CHECKED GOOD AT THIS TIME.
Part: WARNING MESSAGE — ILLUMINATED (EMERGENCY EXIT) · airframe 22,248 hrs · 15,626 cycles
LEFT EMERGENCY DOOR CAUTION MESSAGE.
Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 22,085 hrs · 15,500 cycles
EMERGENCY EXIT COVER AT 12A FALLING DOWN. SECURED EMERGENCY EXIT HANDLE COVER AT 12A IAW AMM 25-26-09.
Part: LIGHT — BURNED OUT (CABIN) · airframe 21,662 hrs · 15,187 cycles
OVERHEAD CEILING EMERGENCY LIGHTS BURNED OUT. R & R OVERHEAD CEILING LIGHT, IAW AMM 33-51-09, OP'S CHECKED GOOD AT THIS TIME.
2012
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,458 hrs · 15,044 cycles
MID CABIN EMERGENCY LIGHT INOPERATIVE. R & R CABIN EMERGENCY LIGHT BULB IAW 33-51-07.
Part: WARNING LIGHT — ILLUMINATED · airframe 20,931 hrs · 14,656 cycles
ANTI-ICE DUCT MASTER CAUTION, ANTI-ICE MASTER CAUTION. APPLIED DC4 ON MT165 IN THE RIGHT WING SUPPLY BLEED AIR LEAK DETECTION LOOPS IAW AMM 36-21-07. PERFORMED OPS CHECK OF BLEED AIR DETECTION LOOP IAW AMM 36-21-00.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,846 hrs · 14,591 cycles
CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. R & R EMERGENCY LIGHT AT ROW 17 OVERHEAD IAW AMM 33-51-09.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,818 hrs · 14,572 cycles
CEILING EMERGENCY FLOOD LIGHT ROW 17 INOPERATIVE.
Part: CONTROLLER — DEFECTIVE (A/C PACK) · airframe 20,773 hrs · 14,534 cycles
BOTH PACKS 1 & 2 CYCLING ON AND OFF IN FLIGHT. R & R AIR CONDITIONING CONTROLLER, OP'S CHECKED GOOD, IAW AMM 21-61-00. NO FURTHER DEFECTS NOTED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,740 hrs · 14,511 cycles
CEILING EMERGENCY LIGHT AT ROW 4-5 IS OUT.
Part: WARNING MESSAGE — ILLUMINATED · airframe 20,740 hrs · 14,511 cycles
COOL MESSAGE DISPLAYED .
Part: ANGLE — CORRODED (PAX DOOR) · airframe 20,734 hrs · 14,505 cycles
PASSENGER DOOR KICK ANGLE IS CORRODED. R & R PASSENGER DOOR KICK ANGLE IAW SRM 51-42-06, 51-40-11, 51-25-01, 52-70-04, AND 52-11-04.
Part: DIAPHRAGM — CRACKED (WING TO BODY) · airframe 20,734 hrs · 14,505 cycles
CRACK IN LT WING TO FUSELAGE DIAPHRAGM AT BS 909.0. REPAIRED IAW REO 670-53-82-436, AN EDDY CURRENT INSPECTION WAS COMPLIED WITH AND NO REJECTABLE INDICATIONS IAW NDTM 51-20-06, REO 670-52-35-127, SRM 51-21-11,51-22-00, AND 51-42-06.
Part: SUPPORT — CORRODED (ZONE 100) · airframe 20,734 hrs · 14,505 cycles
FORWARD JACK SUPPORT AT S27R, BS 265 - 280 CORRODED. R & R JACK SUPPORT IAW SRM 51-42-06 AND 51-42-21.
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 20,734 hrs · 14,505 cycles
AFT CARGO BAY RT FLOOR SUPPORT BETWEEN FS 1030.0 AND 1051.0. REMOVED THE CORROSION, MAPPED AND MEASURED DAMAGE IAW SRM 51-21-06 AND REO 670-53-61-894. AN EDDIE CURRENT INSPECTION COMPLIED WITH IAW NDTM 51-20-006 NO REJECTABLE INDICATIONS, ALODINED, PRIMED, AND PAINTED IAW SRM 51-25-06.
Part: SUPPORT — CORRODED (ZONE 100) · airframe 20,734 hrs · 14,505 cycles
FORWARD JACK SUPPORT, BS 265 TO 280 AT S27L IS CORRODED. R & R JACK SUPPORT IAW SRM 51-42-06 AND 51-42-21.
Part: FRAME — CORRODED (BS 265) · airframe 20,734 hrs · 14,505 cycles
FRAME FS 265.0 CORRODED BETWEEN STR 26L AND 26R. R & R FRAME IAW SRM 51-42-06 AND 51-42-21.
Part: BULKHEAD — CORRODED (BS 280) · airframe 20,734 hrs · 14,505 cycles
RT BULKHEAD LOWER WEB AT FS 280.0 IS CORRODED. R & R RT BULKHEAD LOWER WEB AT FS 280.0 IAW REO 670-53-11-594, SRM 51-42-06, AND 51-40-11.
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 20,734 hrs · 14,505 cycles
RT FORWARD LOWER FLOOR SUPPORT IS CORRODED. R & R FLOOR SUPPORT IAW EO DWG NR SH670-32170, REV R, SRM 51-42-06, AND 51-42-00.
Part: SHAFT — BENT (DOOR HANDLE) · airframe 20,734 hrs · 14,505 cycles
PASSENGER INNER DOOR HANDLE ROLLER SHAFT IS BENT (DETENT SHAFT). R & R PASSENGER INNER DOOR HANDLE ROLLER SHAFT (DETENT SHAFT) IAW AMM 52-11-02.
Part: ANGLE — CORRODED (PAX DOOR) · airframe 20,734 hrs · 14,505 cycles
PASSENGER DOOR MID CAP ANGLE IS CORRODED. R & R PASSENGER MID CAP ANGLE IAW SRM 51-42-06 AND 51-25-01.
Part: ANGLE — CORRODED (THRESHOLD) · airframe 20,734 hrs · 14,505 cycles
PASSENGER DOOR THRESHOLD AFT CAP IS CORRODED. R & R PASSENGER DOOR AFT CAP IAW SRM 51-42-06 AND 51-25-01.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,734 hrs · 14,505 cycles
FS 280.0 FLOORBEAM IS CORRODED. R & R FS 280.0 FLOORBEAM IAW REO 670-53-11-047, REO 690-53-11-032, SRM 51-42-21,51-42-10, AND 51-42-06.
Part: FITTING — CORRODED (THRESHOLD) · airframe 20,734 hrs · 14,505 cycles
PASSENGER DOOR THRESHOLD FORWARD CLOSING FITTING IS CORRODED. R & R FORWARD CLOSING FITTING IAW SRM 51-42-06, 51-40-11,51-42-21, AND 51-21-11.
Part: BULKHEAD WEB — CORRODED (ZONE 100) · airframe 20,734 hrs · 14,505 cycles
LOWER BULKHEAD WEB AT FS 280.0 IS CORRODED. R & R LT LOWER BULKHEAD WEB IAW REO 670-53-11-594, SRM 51-42-06,51-40-11, AND 51-21-11.
Part: FITTING — CORRODED (ZONE 100) · airframe 20,734 hrs · 14,505 cycles
RIGHT OTBD INTERCOSTAL FLOORMOUNT MACHINE FITTING IS CORRODED. R & R OTBD INTERCOSTAL FLOORMOUNT MACHINE FITTING IAW SRM 51-40-11 AND 51-42-21.
Part: WEB — CORRODED (ZONE 100) · airframe 20,734 hrs · 14,505 cycles
AFT SERVICE DOOR FLOOR PROTECTOR CORRODED OUT OF LIMITS. R & R FLOOR PROTECTOR AT SERVICE DOOR IAW SRM 51-42-06,51-45-00, AND 51-42-21.
Part: FLOOR SUPPORT — CORRODED (BS 1051-1069) · airframe 20,734 hrs · 14,505 cycles
AFT CARGO BAY RT FLOOR SUPPORT BETWEEN FS 1051.0 AND FS 1069.0 IS CORRODED. R & R REPAIR DOUBLER AND FLOOR SUPPORT SECTION IAW REO 670-53-61-894, SRM 51-21-06, 51-24-21, 51-21-11,51-12-00, 51-21-16, AND 51-42-06.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,538 hrs · 14,366 cycles
ROW 17 CEILING EMERGENCY FLOOD LIGHT INOPERATIVE.
Part: LIGHT — INOPERATIVE (ROW 15) · airframe 17,934 hrs · 12,154 cycles
CEILING EMERGENCY FLOOD LIGHT INOP AT ROW 15. DEFERRED CEILING EMERGENCY FLOODLIGHT AT ROW 15 IAW MEL 33-51-01B, CAT C.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,990 hrs · 13,947 cycles
ROW 7 CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED BULB.
Part: SEAL — CONTAMINATED (EMERGENCY EXIT) · airframe 19,929 hrs · 13,907 cycles
SQUEAL FROM LT OVERWING EMEGENCY EXIT DOOR WHILE IN FLIGHT. REMOVED DOOR AND INSPECTED SEAL, CLEANED DEBRIS, AND REINSTALLED DOOR IAW AMM 52-21-00.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,898 hrs · 13,884 cycles
EMERGENCY CEILING FLOOD LIGHT ABOVE ROW 15 INOPERATIVE. R & R CEILING FLOOD LIGHT IAW AMM 33-51-09.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,709 hrs · 13,751 cycles
ROW 17, CEILING EMERGENCY FLOOD LIGHT INOPERATIVE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,489 hrs · 13,574 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4785) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,364 hrs · 13,486 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 7 IS OUT. (FLT 4560) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,348 hrs · 13,477 cycles
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT4676) RELAMPED EMERGENCY LIGHT.
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,098 hrs · 13,320 cycles
OVERHEAD EMERGENCY LIGHT ABOVE ROW 15 IS OUT. (FLT 4578) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,900 hrs · 13,182 cycles
THE 2ND TO LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4558) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,610 hrs · 12,993 cycles
NR 6 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,564 hrs · 12,971 cycles
THE 2ND FROM AFT CEILING EMERGENCY LIGHT IS OUT. (FLT 4707) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,495 hrs · 12,919 cycles
NR 5 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4635) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,414 hrs · 12,857 cycles
SECOND TO LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4680) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,283 hrs · 12,777 cycles
NR 5 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4684) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,920 hrs · 12,528 cycles
THE 2ND FROM BACK CEILING EMERGENCY LIGHT IS OUT. (FLT 4681) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,674 hrs · 12,366 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 15 IS OUT. (FLT 4533) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — UNSECURE (CABIN) · airframe 17,188 hrs · 12,032 cycles
THE 2ND TO LAST CEILING LEVEL EMERGENCY LIGHT IS OUT. (FLT 4587) FOUND BULB NOT SECURED. RE-SECURED BULB.
2010
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,580 hrs · 10,967 cycles
FS 280 FLOORBEAM CRACKED AND CORRODED. (C-CHECK) REPAIR PER REO.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,690 hrs · 11,047 cycles
FS 280.00 FLOORBEAM HAS CRACK AND CORROSION LT & RT SIDES. (C-CHECK) REPLACED FS 280 FLOORBEAM PER SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,922 hrs · 10,523 cycles
EMERGENCY CEILING LIGHT JUST PAST EXIT ROW INOP. (FLT 4594) RELAMPED EMERGENCY LIGHT.
Part: MOUNT — CORRODED (RT ENGINE) · airframe 14,738 hrs · 10,377 cycles
RIGHT ENGINE MOUNT LINK AND BUSHING CORRODED. (ENG CHANGE) REPLACED MOUNT LINK AND BUSHING.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,360 hrs · 10,076 cycles
SECOND TO LAST EMERGENCY CEILING LIGHT INOP. (FLT 4494) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,197 hrs · 9,950 cycles
NR 3 OVERHEAD EMERGENCY LIGHT INOP. (FLT 4737) RELAMPED EMERGENCY LIGHT.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,109 hrs · 9,191 cycles
SECOND TO LAST OVERHEAD EMERGENCY LIGHT INOP. (FLT 4656) RELAMPED EMERGENCY LIGHT.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 12,596 hrs · 8,805 cycles
FLT 4694 - OVERHEAD EMERGENCY LIGHT AT ROW 4 INOP. RELAMPED.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 11,830 hrs · 8,262 cycles
FLT 4853 - OVERHEAD EMERGENCY LIGHT NR 5 INOP. RELAMPED.
2008
Part: FLOORBEAM — CORRODED (BS 280) · airframe 10,865 hrs · 7,604 cycles
C-CHECK - FS 280 BEAM CORRODED. REPAIRED PER REO.
Part: STRUCTURE — CRACKED · airframe 11,098 hrs · 7,766 cycles
C-CHECK, RADIUS CRACKED ON STRUCTURE NEXT TO ADG PUMP. REPAIRED PER SRM.
Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 11,098 hrs · 7,766 cycles
C-CHECK, PASSENGER DOOR AFT INTERCOSTAL CRACKED. REPLACED PER SRM.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 11,098 hrs · 7,766 cycles
C-CHECK, PASSENGER DOOR AFT DRAG ANGLE CRACKED. REPAIRED PER REO.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 11,098 hrs · 7,766 cycles
C-CHECK, FS 280 BEAM CORRODED. REPAIRED PER REO.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 9,156 hrs · 6,472 cycles
FLT 4052 - EMERGENCY POD LIGHT IS INOP. RELAMPED POD LIGHT. OPS CHECK GOOD.
2007
Part: STEP — CRACKED (PAX DOOR) · airframe 7,370 hrs · 5,330 cycles
PAX DOOR UPPER MID STEP IS CRACKED ON AFT SIDE, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES AND DOUBLER PER CRJ700 REO 670-52-11-104 AND SRM 51-12-06.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 7,370 hrs · 5,330 cycles
COCKPIT FLOORBEAM AT FS 280 CORRODED, DISCOVERED AT C-CHECK. INSTALLED NEW COCKPIT FLOOR SUPPORT ANGLE P/N:CC670-33292-13 IAW CRJ700 SRM TASK 51-42-06-001-001-A01.
Part: STEP — CRACKED (PAX DOOR) · airframe 7,370 hrs · 5,330 cycles
PAX DOOR UPPER MID STEP IS CRACKED ON FORWARD SIDE, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES AND DOUBLER PER CRJ700 REO 670-52-11-104 AND SRM 51-42-06.
Part: BULKHEAD — CRACKED (BS 280) · airframe 7,370 hrs · 5,330 cycles
LEFT WEB AT FS 280 BULKHEAD IS CORRODED, DISCOVERED AT C-CHECK. INSTALLED REPLACEMENT WEB IAW CRJ700 SRM TASK 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 7,370 hrs · 5,330 cycles
LEFT ELEVATOR WAS STRUCK BY LIGHTNING ON TRAILING EDGE BETWEEN 9TH AND 10TH RIB, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS PER REO 670-55-21-038.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 7,370 hrs · 5,330 cycles
FS 280 FLOORBEAM CRACKED AT RIGHT AND LEFT BUTTLINE 9, DISCOVERED AT C-CHECK. INSTALLED CROSS BEAM SPLICE AT FS 280 PER REO 670-53-11-047. INSTALLED INTERCOSTALS PER CRJ700 SRM 51-42-21.
Part: BULKHEAD — CRACKED (BS 280) · airframe 7,370 hrs · 5,330 cycles
RIGHT WEB AT STA 280 BULKHEAD IS CORRODED, DISCOVERED AT C-CHECK. INSTALLED REPLACEMENT WEB IAW CRJ700 SRM TASK 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: DOOR — UNKNOWN (EMERGENCY EXIT) · airframe 6,737 hrs · 4,900 cycles
FLIGHT 5032 - ON TAKEOFF ROLL RIGHT EMERGENCY DOOR MESSAGE CAME ON. ABORTED TAKEOFF AND RETURNED TO GATE. TRANSFERRED TO DMI LIST 52-70-03.
2006
Part: ACM — SEIZED (RIGHT) · airframe 5,576 hrs · 4,083 cycles
FLIGHT 5606 - DURING TAXI-OUT SMOKE WAS EMANATING FROM THE RIGHT COCKPIT GASPERS AND WAS ALSO EVIDENT IN THE CABIN. CREW DECLARED AN EMERGENCY AND FLIGHT RETURNED TO THE GATE. REPLACED THE RIGHT AIR CYCLE MACHINE.
Part: LIGHT — MELTED (COCKPIT) · airframe 4,456 hrs · 3,389 cycles
FLIGHT 5039 - DURING TAXI, THE F/O'S RIGHT FORWARD FLOOD LIGHT SHORTED CAUSING FIRE AND SMOKE, CREW DECLARED AN EMERGENCY AND UTILIZED FIRE EXTINGUISHER. REPLACED FLOOD LIGHT ASSEMBLY.
2005
Part: OIL FILTER — DIRTY (RT ENGINE) · airframe 2,401 hrs · 1,939 cycles
RT ENGINE OIL PRESSURE IN AMBER DASHES. REPLACED THE OIL FILTER.
2004
Part: SHUTOFF VALVE — MALFUNCTIONED (RT WING ANTI ICE) · airframe 851 hrs · 684 cycles
FLIGHT 4975 RIGHT ENGINE BLEED CAUTION MESSAGE. REPLACED THE RIGHT WING ANTI-ICE SOV.