N146PQ
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.
191 reports on file, 2009-07-13 – 2026-06-10.
Part: LANDING — CRACKED · airframe 41,814 hrs · 31,366 cycles
SECONDARY NRC FROM TC 900-57-580-503: AFTER REMOVING THE 584FB ACCESS PANEL, ELONGATED HOLE WAS FOUND IN THE SETTLEMENT AREA. SETTLEMENT AREA OF 584FB ACCESS PANEL WAS REPAIRED PER REO 690-57-52-595 REV: - -
Part: HANDLE — CRACKED (ZONE 800) · airframe 41,814 hrs · 31,366 cycles
CRACK OUTER HANDLE OF PASSENGER DOOR. OUTER HANDLE OF PASSENGER DOOR WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
Part: FITTING — CRACKED (ZONE 200) · airframe 41,814 hrs · 31,366 cycles
CRACK ON AFT LOWER FITTING SIDE POST LH/RH SIDE BTW WINDSHIELD AND SIDE WINDOWS. AFT LOWER FITTING SIDE POST LH/RH SIDE BTW WINDSHIELD AND SIDE WINDOWS WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01
Part: FITTING — CRACKED (ZONE 200) · airframe 41,814 hrs · 31,366 cycles
CRACK ON AFT LOWER FITTING SIDE POST LT/RT SIDE BTW WINDSHIELD AND SIDE WINDOWS. AFT LOWER FITTING SIDE POST LH/RH SIDE BTW WINDSHIELD AND SIDE WINDOWS WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01
Part: ANGLE — CORRODED · airframe 41,814 hrs · 31,366 cycles
SECONDARY NRC FROM NRC 00099 AND 00100: AFTER REMOVAL, CORROSION ON ANGLE SUPPORTS (2EA) OF ACCESS PANELS 542AZ AND 642AZ. CORROSION ON ANGLE SUPPORTS (2EA) OF ACCESS PANELS 542AZ AND 642AZ WAS REMOVED PER SRM 51-21-06-001-001-A01 AND ANGLE SUPPORT (1EA) OF ACCESS 642AZ WAS EVALUATED OUT LIMITS AND REPLACED PER SRM 51-10-06-001-001-A01 AND ANGLE SUPPORT (1EA) OF ACCESS PANELS 542AZ WAS EVALUATED WITHIN LIMITS PER SRM 53-00-00-101-001-A01.
Part: DOOR FRAME — CORRODED (ZONE 100) · airframe 41,814 hrs · 31,366 cycles
SECONDARY NRC FROM NRC 290: CORROSION ON INNER CHORD (3EAS) BTW FS1000 TO FS1047 AT AFT BAGGAGE DOOR SURROUND STRUCTURE LOWER SIDE. CORROSION ON INNER CHORD (2EAS) BTW FS1000 TO FS1047 AT AFT BAGGAGE DOOR SURROUND STRUCTURE LOWER SIDE WAS REMOVED PER CRJ/900 SRM 51-21-06-001-001-A01 AND WERE EVALUATED WITHIN LIMITS PER CRJ 900 SRM 53-00-00-101-001-A01 AND INNER CHORD (1EA) WAS EVALUATED OUT LIMITS PER CRJ/900 SRM 51-10-06-001-001-A01 THEREFORE WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 41,814 hrs · 31,366 cycles
CRACK ON CLIP THAT ATTACH AFT FACE OF PRESSURE BULKHEAD TO INTERCOSTAL, FS=1098.20 AND SGTR 24LH AT AFT EQUIPMENT COMPARMENT. CLIP THAT ATTACH AFT FACE OF PRESSURE BULKHEAD TO INTERCOSTAL, FS=1098.20 AND SGTR 24LH AT AFT EQUIPMENT COMPARMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-10-001-001-A01
Part: RIB — CRACKED (ZONE 500) · airframe 41,814 hrs · 31,366 cycles
CRACK ON MACHINED RIB OF LEADING EDGE SS27.16 AT LEFT WING MACHINED RIB OF LEADING EDGE SS27.16 AT LEFT WING WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01, CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-10-001-001-A01
Part: SUPPORT FITTING — CORRODED (ZONE 200) · airframe 41,814 hrs · 31,366 cycles
CORROSION ON SUPPORT FITTINGS OF GALLEY/LAVATORY AS FOLLOW; (6/A) BTW FS280 AND FS310 BTW LBL45 AND RBL45 AND (2E/A) BTW FS364 AND FS394 BTW RBL9 AND RBL45 AT PAX CABIN FLOOR STRUCTURE. DUE TO EXCESSIVE CORROSION ON SUPPORT FITTINGS (2 EA) BTW FS280 BTW RBL45 RBL0 AND (1E/A) BTW FS364 AND RBL45 WERE REPLACED PER CRJ-900 SRM 51-10-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 41,814 hrs · 31,366 cycles
CORROSION ON FLOOR CROSSBEAM FS333 BTW RBL7 AND RBL45 AT PAX CABIN FLOOR STRUCTURE. CORROSION ON FLOOR CROSSBEAM FS333 BTW RBL7 AND RBL45 AT PAX CABIN FLOOR STRUCTURE WAS REPAIRED PER EA NO. CR953-22493 REV IR
Part: ANGLE — CORRODED (ZONE 200) · airframe 41,814 hrs · 31,366 cycles
CORROSION ON FWD, MID AND AFT CAP ANGLES (PASSENGER FLOOR SILL AREA) AT PAX CABIN FLOOR STRUCTURE DUE TO EXCESSIVE CORROSION ON FWD, MID AND AFT CAP ANGLES (PASSENGER FLOOR SILL AREA) AT PAX CABIN FLOOR STRUCTURE WERE REPLACED PER CRJ-900 SRM 51-10-06-001-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-41-02-001-001-A01
Part: ANGLE — CORRODED (ZONE 200) · airframe 41,814 hrs · 31,366 cycles
CORROSION ON FWD, MID AND AFT CAP ANGLES (PASSENGER FLOOR SILL AREA) AT PAX CABIN FLOOR STRUCTURE DUE TO EXCESSIVE CORROSION ON FWD, MID AND AFT CAP ANGLES (PASSENGER FLOOR SILL AREA) AT PAX CABIN FLOOR STRUCTURE WERE REPLACED PER CRJ-900 SRM 51-10-06-001-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-41-02-001-001-A01
Part: ANGLE — CORRODED (ZONE 200) · airframe 41,814 hrs · 31,366 cycles
CORROSION ON FWD, MID AND AFT CAP ANGLES (PASSENGER FLOOR SILL AREA) AT PAX CABIN FLOOR STRUCTURE DUE TO EXCESSIVE CORROSION ON FWD, MID AND AFT CAP ANGLES (PASSENGER FLOOR SILL AREA) AT PAX CABIN FLOOR STRUCTURE WERE REPLACED PER CRJ-900 SRM 51-10-06-001-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-41-02-001-001-A01
Part: FITTING — CORRODED (ZONE 200) · airframe 41,814 hrs · 31,366 cycles
CORROSION FLOOR FITTING IN AFT AND FWD ACCESS 205 (2EAS) ON GALLEY 2. SUMMARY OF NRC 00336:NEW FLOOR FITTING IN FWD ACCESS 205 (1EA) ON GALLEY 2 WAS REPLACED PER SAFRAN CMM 25-32-84 AND NEW FLOOR FITTING IN AFT (1EA) ON GALLEY 2 WAS FABRICATED PER EA NO: CRJ953-22393 REV IR AND INSTALLED PER SAFRAN CMM 25-32-84
Part: FITTING — CORRODED (ZONE 200) · airframe 41,814 hrs · 31,366 cycles
CORROSION FLOOR FITTING IN AFT AND FWD ACCESS 205 (2EAS) ON GALLEY 2. SUMMARY OF NRC 00336:NEW FLOOR FITTING IN FWD ACCESS 205 (1EA) ON GALLEY 2 WAS REPLACED PER SAFRAN CMM 25-32-84 AND NEW FLOOR FITTING IN AFT (1EA) ON GALLEY 2 WAS FABRICATED PER EA NO: CRJ953-22393 REV IR AND INSTALLED PER SAFRAN CMM 25-32-84
Part: FITTING — CORRODED (ZONE 200) · airframe 41,814 hrs · 31,366 cycles
CORROSION FLOOR FITTING IN FWD ACCESS 109 (1EA) ON GALLEY 1. SUMMARY OF NRC 00333:NEW FLOOR FITTING IN FWD ACCESS 109 (1EA) ON GALLEY 1 WAS FABRICATED PER EA NO: CRJ953-22394 REV IR AND INSTALLED PER SAFRAN CMM 25-33-67
Part: FITTING — CORRODED (ZONE 200) · airframe 41,814 hrs · 31,366 cycles
CORROSION FLOOR FITTING IN FRONT PAPER CONTAINER ON FWD LAV (1EA). SUMMARY OF NRC 00338: FLOOR FITTING IN FRONT PAPER CONTAINER ON FWD LAV (1EA) WAS FABRICATED PER EA NO: CRJ953-22392 REV IR AND INSTALLED PER SAFRAN CMM 25-40-76
Part: FITTING — CORRODED (ZONE 200) · airframe 41,814 hrs · 31,366 cycles
CORROSION FLOOR FITTING IN FWD AND AFT ACCESS 306 (2EAS) ON GALLEY 3. SUMMARY OF NRC 00337: FLOOR FITTING IN FWD AND AFT ACCESS 306 (2EAS) ON GALLEY 3 WERE REPLACED PER ZODIAC AEROSPACE CMM 25-33-18 REV. NO 5 DATED MAY 15/15
Part: FITTING — CORRODED (ZONE 200) · airframe 41,814 hrs · 31,366 cycles
CORROSION FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1. SUMMARY OF NRC 00335: FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-67 REV NO 10 DATED JUN 20/22
Part: FITTING — CORRODED (ZONE 200) · airframe 41,814 hrs · 31,366 cycles
CORROSION FLOOR FITTING IN AFT ACCESS 108 (1EA) ON GALLEY 1. SUMMARY OF NRC 00334: FLOOR FITTING IN AFT ACCESS 108 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-67 REV. 10 DATED JUN 20/22
Part: ANGLE — CORRODED (ZONE 200) · airframe 41,814 hrs · 31,366 cycles
CORROSION ON KICKPLATE ANGLE (PASSENGER FLOOR SILL AREA) AT PAX CABIN FLOOR STRUCTURE. DUE TO EXCESSIVE CORROSION ON KICKPLATE ANGLE (PASSENGER FLOOR SILL AREA) AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER CRJ 900 SRM 53-00-00-101-001-A01 , SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
Part: SUPPORT FITTING — CORRODED (ZONE 200) · airframe 41,814 hrs · 31,366 cycles
CORROSION ON SUPPORT FITTINGS OF GALLEY/LAVATORY AS FOLLOW; (6/A) BTW FS280 AND FS310 BTW LBL45 AND RBL45 AND (2E/A) BTW FS364 AND FS394 BTW RBL9 AND RBL45 AT PAX CABIN FLOOR STRUCTURE. DUE TO EXCESSIVE CORROSION ON SUPPORT FITTINGS (2 EA) BTW FS280 BTW RBL45 RBL0 AND (1E/A) BTW FS364 AND RBL45 WERE REPLACED PER CRJ-900 SRM 51-10-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
Part: FAIRING — CRACKED (ZONE 400) · airframe 41,814 hrs · 31,366 cycles
CRACKED HINGE FAIRING 443BT HINGE FAIRING 443BT WAS REPAIRED PER EA CRJ954-22614 REV. A
Part: STRINGER — CORRODED (ZONE 100) · airframe 41,814 hrs · 31,366 cycles
CORROSION ON STGR19R BTW FS 295 AND FS 310 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STGR19R BTW FS 295 AND FS 310 AT MAIN AVIONICS COMPARTMENT WAS REMOVED AND EVALUATED OUT OF LIMITS, THEREFORE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND CRJ 900 SRM 51-21-06-001-001-A01
Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 41,814 hrs · 31,366 cycles
CORROSION ON STGR19R, BTW FS 437 AND FS 453 AND BTW FS 469 AND FS 485 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STGR19R, BTW FS 437 AND FS 453 AND BTW FS 469 AND FS 485 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT LIMITS PER CRJ900 SRM 53-21-03-101-007-A01 THEREFORE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
Part: STRINGER — CORRODED (ZONE 100) · airframe 41,814 hrs · 31,366 cycles
INITIAL INSPECTION: CORROSION ON STGR20R (LONGITUDINAL JOINT AREA); FROM FS485 TO FS533, FROM FS565 TO FS581 AND FROM FS597 TO FS613 AT FWD BAGGAGE BAY COMPARTMENT. CORROSION ON STGR20R (LONGITUDINAL JOINT AREA); FROM FS485 TO FS533, FROM FS565 TO FS581 AND FROM FS597 TO FS613 AT FWD BAGGAGE BAY COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-31-03-101-001-A01 THEREFORE WAS REPLACED PER REO 690-53-31-1142 REV.--
Part: STRINGER — CORRODED (ZONE 100) · airframe 41,814 hrs · 31,366 cycles
INITIAL INSPECTION: CORROSION ON STGR18R FROM FS629 TO FS661 AND FROM FS661+62 TO FS661+90 AT FWD BAGGAGE BAY COMPARTMENT. CORROSION ON STGR18R FROM FS629 TO FS661 AND FROM FS661+62 TO FS661+90 AT FWD BAGGAGE BAY COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-31-03-101-004-A02 THEREFORE WAS REPAIRED PER EA NO: CRJ953-22525 REV. A
Part: DOOR SILL — CORRODED (ZONE 100) · airframe 41,814 hrs · 31,366 cycles
CORROSION ON LOWER SILL AT AFT BAGGAGE BAY DOOR CUT OUT. CORROSION ON LOWER SILL AT AFT BAGGAGE BAY DOOR CUT OUT WAS EVALUATED OUT LIMITS PER SRM 51-10-06-001-001-A01 THEREFORE WAS REPLACED PER SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01
Part: PLATE — CORRODED (ZONE 100) · airframe 41,814 hrs · 31,366 cycles
CORROSION ON FWD AND AFT GUSSET PLATES ALSO CORROSION ON PLATES (BTW STGR24L AND STGR26L) OF FWD AND CTR DOOR LOWER SURROUND STRUCTURE AT FWD BAGGAGE BAY COMPARTMENT. DUE TO NOT ALLOWABLE CORROSION ON FWD AND AFT GUSSET PLATES ALSO CORROSION ON PLATES (BTW STGR24L AND STGR26L) OF FWD AND CTR DOOR LOWER SURROUND STRUCTURE AT FWD BAGGAGE BAY COMPARTMENT PER CRJ-900 SRM 53-31-23-101-001-A02 WAS REPAIRED PER EA NO.: CRJ953-22510 REV. IR, PER EA NO.: CRJ953-22479 REV. A, PER EA NO.: CRJ953-22508 REV. IR, PER EA NO.: CRJ953-22509 REV. IR AND PER EA NO.: CRJ953-22495 REV. A.
Part: BRACKET — CORRODED (ZONE 100) · airframe 41,814 hrs · 31,366 cycles
CORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/RH MAIN WHEEL WELL. CORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/RH MAIN WHEEL WELL WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND SUPPORT PLATE LH WAS EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND SUPPORT PLATE RH WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 41,814 hrs · 31,366 cycles
CORROSION ON RH SIDE SEAT RAIL (4 EAS) FROM FS 379.00 TO FS 669.40 ON STGR 15R AT PAX CAB. RH SIDE SEAT RAIL (3 EAS) FROM FS 485.00 TO FS 669.40 ON STGR 15R AT PAX CAB WAS CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND NO DAMAGE WAS FOUND, DUE TO EXCESSIVE CORROSION ON RH SIDE SEAT RAIL (1 EA) FROM FS 379.00 TO FS 485.00 ON STGR 15R AT PAX CABIN WAS REPLACED PER CRJ-900 SRM 51-10-06-001-001-A01 AND PER CRJ900 AMM 53-00-49-000-801 (CONFIG A07) & AMM 53-00-49-400-801 (CONFIG A07).
Part: SUPPORT — CRACKED · airframe 41,814 hrs · 31,366 cycles
CRACK ON FWD EDGE LT & RT OF SUPPORT AT JB6. SUPPORT AT JB6 WAS REPLACED PER SRM 51-42-06-001-001-A01.
Part: THRUST REVERSER — CRACKED (RIGHT) · airframe 41,814 hrs · 31,366 cycles
DEGRADATED AFT EDGE OF INBD BIFURCATION PANELS ON UPPER AND LOWER CORE COWL AT RH ENGINE SUMMARY: PAINT WAS REMOVED ON LOWER CORE COWL AT RH ENGINE PER CRJ-900 SRM 51-26-01-001-001-A01 AND DAMAGE WAS NOT FOUND AND ON UPPER BIFURCATION PANEL AT RH ENGINE WAS REPAIRED PER EA CRJ954-22288 REV. A.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 41,814 hrs · 31,366 cycles
CORROSION ON STGR-19R (2EA) FIRST LOCATED BTW FS469 AND FS485 AND SECOND LOCATED ON FS597 TO FS613. CORROSION ON STGR-19R (2EA) FIRST LOCATED BTW FS469 AND FS485 AND SECOND LOCATED ON FS597 TO FS613 WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 51-10-06-001-001-A01 THEREFORE WAS REPAIRED PER CRJ-900 SRM 53-00-03-201-001-A01
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 41,814 hrs · 31,366 cycles
CORROSION ON LT SIDE SEAT TRACK (4 EAS) FROM BS 379.00 TO BS 669.40 ON STR 15L AT PAX CAB. SEAT TRACK (3 EAS) FROM BS 485.00 TO BS 669.40 ON STR 15L AT PAX CAB WAS CLEANED PER IAW SRM 51-26-00-001-001-A01 & NO DAMAGE WAS FOUND. LT SIDE SEAT TRACK (1 EA) FROM BS 379.00 TO BS 485 ON STR 15L AT PAX CAB WAS REPLACED PER AMM 53-00-49.
Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 41,814 hrs · 31,366 cycles
CRACK AT FWD SUPPORT ANGLES (2EA) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARTMENT INTERNAL STRUCTURE (INSIDE ACCESS PANEL 121AL). FWD SUPPORT ANGLES (2EA) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARTMENT INTERNAL STRUCTURE (INSIDE ACCESS PANEL 121AL) WERE REPLACED PER SRM 51-42-21-001-001-A01 AND SRM 51-41-02-001-001-A01 .
Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 41,814 hrs · 31,366 cycles
CRACK AT FWD SUPPORT ANGLES (2EA) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARTMENT INTERNAL STRUCTURE (INSIDE ACCESS PANEL 121AL). FWD SUPPORT ANGLES (2EA) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARTMENT INTERNAL STRUCTURE (INSIDE ACCESS PANEL 121AL) WERE REPLACED PER CRJ 900 SRM 51-42-21-001-001-A01 AND SRM 51-41-02-001-001-A01 .
Part: STRAP — CORRODED (ZONE 100) · airframe 41,814 hrs · 31,366 cycles
CORROSION SEVERAL PLACES ON METAL STRIP AT FAIRING PANEL 193AB INNER AND OUTER FACE STRAPS ON FAIRING PANEL 193AB WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01.
Part: STRAP — CORRODED (ZONE 100) · airframe 41,814 hrs · 31,366 cycles
CORROSION SEVERAL PLACES ON METAL STRIP AT FAIRING PANEL 193AB INNER AND OUTER FACE STRAPS ON FAIRING PANEL 193AB WERE REPLACED IAW SRM 51-42-10-001-001-A01.
Part: HINGE — CRACKED (ZONE 200) · airframe 41,814 hrs · 31,366 cycles
PAX PASSENGER DOOR WAS REPAIRED PER EA CRJ952-22490 REV.IR
Part: HINGE — CRACKED (ACCESS PANEL) · airframe 41,814 hrs · 31,366 cycles
SECONDARY NRC: AFTER STEP PANEL 832FT REMOVAL IN REF NRC 046, CRACK ON HINGE WAS FOUND. HINGE ON ACCESS PANEL 832FT WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01
Part: RIB — CRACKED (ZONE 500) · airframe 41,814 hrs · 31,366 cycles
INITIAL INSPECTION': CRACK ON MACHINED RIB LEADING EDGE SS57.16 AT LEFT WING. MACHINED RIB LEADING EDGE SS57.16 AT LEFT WING WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01
Part: TEE ANGLE — CORRODED (ZON E100) · airframe 41,814 hrs · 31,366 cycles
CORROSION ON ANGLE SETTLEMENT AREA OF FAIRING PANEL STA=693 RBL=45 TO LBL=45 /// CORROSION ON ANGLE SETTLEMENT OF FAIRING PANEL FS= 661+90 LBL=40 TO RBL=40 /// CORROSION ON ANGLE SETTLEMENT OF FAIRING FS=661+62 RBL=45 TO LBL=45 ALSO CORROSION ON ANGLE SETTLEMENT AREA OF FAIRING PANEL LBL=0 BTW STA=661+90 TO STA= 661+62 SUMMARY: CORROSION ON ANGLE SETTLEMENT AREA OF FAIRING PANEL BTW STA=693 RBL=45 TO LBL=45 , FS= 661+90 LBL=40 TO RBL=40 , AND FS=661+62 RBL=45 TO LBL=45 WAS REMOVED AND EVALUATED WITHIN OF LIMITS PER CRJ-900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-82-55-101-001-A01 AND ON ANGLE SETTLEMENT BTW LBL=0 BTW STA=661+90 TO STA= 661+62 IS OUT OF LIMITS THEREFORE ANGLE SETTLEMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
Part: DOOR FRAME — CORRODED (ZONE 100) · airframe 41,814 hrs · 31,366 cycles
CORROSION ON ANGLES STA= 847+32 BTW STG 17RH TO 17 LH. CORROSION ON ANGLES BTW STA= 847+32 AND 847+64 AND RBL=18 AND LBL=18. CORROSION ON ANGLE STA= 794 BOTTOM SIDE AND RBL=46 LBL=46 ANGLES STA= 847+32 BTW STG 17RH TO 17 LH, ANGLES, STA= 847+32 AND 847+64 AND RBL=18 AND LBL=18, & ANGLE STA= 794 BOTTOM SIDE AND RBL=46 LBL=46 WAS REMOVED IAW SRM 51-42-10-001-001-A01 AND STA= 847+32 BTW STG 17RH TO 17 LH 847+32 EVALUATED OUT LIMITS IAW SRM 53-82-55-101-002-A02, REPLACED IAW SRM 51-42-10-001-001-A01, ANGLES STA= 847+32 AND 847+64 EVALUATED WITHIN OF LIMITS IAW SRM 53-82-55-101-002-A02 & STA= 794 (FRAME ASSY) EVALUATED OUT LIMITS IAW SRM 53-00-01-101-001-A01. REPLACED IAW SRM 51-42-21-001-001-A01.
Part: DOOR FRAME — CORRODED (ZONE 100) · airframe 41,814 hrs · 31,366 cycles
CORROSION ON ANGLES BS 847+32 BTW STG 17R TO 17L. CORROSION ON ANGLES BTW BS 847+32 & 847+64 AND RBL 18 LBL 18. CORROSION ON ANGLE BS 794 BOTTOM SIDE AND RBL 46 LBL 46. CORROSION ON ANGLES BS 847+32 BTW S17R TO 17L. CORROSION ON ANGLES BTW BS 847+32 & 847+64, RBL 18 & LBL 18. CORROSION ON ANGLE BOTTOM SIDE, & RBL 46, LBL 46, REMOVED IAW SRM 51-42-10-001-001-A01, BS 847+32 BTW S17R TO 17L, 847+32 (DOOR LANDING) EVALUATED OUT LIMITS IAW SRM 53-82-55-101-002-A02. REPLACED IAW SRM 51-42-10-001-001-A01, ANGLES BTW BS 847+32, & 847+64 EVALUATED WITHIN OF LIMITS IAW SRM 53-82-55-101-002-A02, & SETTLEMENT OF FAIRING PANEL BS 794 (FRAME ASSY) EVALUATED OUT LIMITS IAW SRM 53-00-01-101-001-A01, REPLACED IAW SRM 51-42-21-001-001-A01
Part: THRUST REVERSER — CRACKED (ZONE 400) · airframe 41,814 hrs · 31,366 cycles
CRACK ON RH LOWER THRUST REVERSER TORQUE BOX FRAME AT LH ENGINE CRACK ON RH LOWER THRUST REVERSER TORQUE BOX FRAME AT LH ENGINE WAS REPAIRED PER REO 690-54-22-130REV. - -
Part: RIB — CRACKED (ZONE 600) · airframe 41,814 hrs · 31,366 cycles
CRACKED BAT RIB AT WS 14.50 OUTER WING, RT MLG WHEEL WELL TRUNNION AREA. BAT RIB AT WS 14.50 OUTER WING, RT MLG WHEEL WELL TRUNNION AREA WAS REPLACED PER SRM 51-42-21-001-001-A01, SRM 51-41-02-001-001-A01, AND SRM 51-42-10-001-001-A01.
Part: RIB — CRACKED (ZONE 500) · airframe 41,814 hrs · 31,366 cycles
CRACKED BAT RIB AT WS 14.50 OUTER WING, LH MLG WHEEL WELL TRUNNION AREA. BAT RIB AT WS 14.50 OUTER WING, LH MLG WHEEL WELL TRUNNION AREA WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01, SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01
Part: LATCH — BROKEN (FUEL PANEL) · airframe 41,814 hrs · 31,366 cycles
BROKEN SPRING LATCH (2 EAS) OF REFUEL/DEFUEL CONTROL PANEL 192AR SPRING LATCH (2 EAS) OF REFUEL/DEFUEL CONTROL PANEL 192AR WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01
Part: ACCESS PANEL — CORRODED (MLG WW) · airframe 41,814 hrs · 31,366 cycles
CORROSION ON MLG WHEEL WELL ACCESS PANELS NO. 542AZ, 542BZ, 642AZ AND 642BZ CORROSION ON MLG WHEEL WELL ACCESS PANELS NO. 542BZ, 642AZ AND 642BZ WAS REMOVED PER SRM 51-21-06-001-001-A01 AND WERE FOUND WITHIN LIMITS PER SRM 53-00-00-101-001-A01. NEW MLG WHEEL WELL ACCESS PANEL NO. 542AZ WAS VERIFIED AND REPLACED PER CRJ900 IPC 57-52-32 AND WILL BE INSTALLED WITH OPENING/CLOSING OF ACCESS CRJ-900-500-OPEN/CLOSE.
Part: CHANNEL — CHAFED (ZONE 800) · airframe 41,814 hrs · 31,366 cycles
OUT OF SCOPE: WEAR ON BEAM OF AFT BAGGAGE-BAY CARGO DOOR STRUCTURE (INTERFERENCE WITH AFT/FWD BALANCE SPRING CABLE) BEAM OF AFT BAGGAGE-BAY CARGO DOOR STRUCTURE (INTERFERENCE WITH AFT/FWD BALANCE SPRING CABLE) WAS BLENDED OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND WAS REPAIRED PER EA NO. CRJ953-22395 REV IR
Part: FITTING — WORN · airframe 41,814 hrs · 31,366 cycles
"INITIAL INSPECTION': WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE. FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND PER CRJ900 SRM 51-41-02-001-001-A01"
Part: PLATE — WORN · airframe 41,814 hrs · 31,366 cycles
"INITIAL INSPECTION': WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE. FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND PER CRJ900 SRM 51-41-02-001-001-A01"
Part: SKIN — CHAFED (ZONE 800) · airframe 41,814 hrs · 31,366 cycles
WEAR PREVIOUS REPAIR OF OUTER SKIN UPPER EDGE AT AFT BAGGAGE DOOR OUTER SKIN UPPER EDGE AT AFT BAGGAGE DOOR PER EA CRJ952-15060 REV.IR
Part: PLATE — WORN · airframe 41,814 hrs · 31,366 cycles
"INITIAL INSPECTION': WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE. FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND PER CRJ900 SRM 51-41-02-001-001-A01"
Part: FITTING — WORN · airframe 41,814 hrs · 31,366 cycles
"INITIAL INSPECTION': WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE. FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND PER CRJ900 SRM 51-41-02-001-001-A01"
Part: DOOR SILL — CRACKED (ZONE 200) · airframe 41,814 hrs · 31,366 cycles
CRACK ON AFT RT DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR). AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, CRJ-900 SRM 51-42-21-001-001-A01 AND CRJ-900 SRM 51-42-10-001-001-A01
Earlier reports · 2009–2023 · 134 reports
2023
Part: LIGHT — INOPERATIVE (UNKNOWN) · airframe 35,294 hrs · 25,883 cycles
OVERWING EMERGENCY LIGHT UNDER AFT EMER. EXIT DOOR IS NOT WORKING - DS 102 POSITION. R/R OVERWING EMERGENCY LIGHT UNDER AFT EMER. EXIT DOOR IAW AMM 33-51-1 5 OPS CHECK GOOD PN ON/OFF - 2LA006954-00
Part: FLOORBEAM — CORRODED · airframe 35,089 hrs · 25,677 cycles
L/H F.S. 280.00 CROSSBEAM IS CORRODED BETWEEN LBL 12.00 AND B.L. 0.00. REMOVED AND REPLACED BEAM I.A.W. BOMBARDIER CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01.
Part: ANGLE — CORRODED · airframe 35,089 hrs · 25,677 cycles
"J"" ANGLE @ FS280 IS CORRODED INSTALLED FS 280 J ANGLE PN CC670-34095-3S IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01."
Part: FLOORBEAM — CORRODED · airframe 35,089 hrs · 25,677 cycles
R/H FS 280 CROSSBEAM IS CORRODED BETWEEN RBL 12 ABD BL 0. REMOVED RH FS 280 CROSSBEAM IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01 LOCATED AND DRILLED NEW SERVICEABLE R/H FS 280 CROSSBEAM P/N CC670-34094JP-2S IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED RH FS 280 CROSSBEAM IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01. EDGE SEALED RH FS. 280 IAW CRJ900 SRM 51-23-00-001-A01PAINTED RH FS 280 CROSSBEAM IAW CRJ 900 SRM 51-25-21-001-001-A01CIC RH FS 280 CROSSBEAM IAW CRJ 900 SRM 51-21-11-001-001-A01
Part: ANGLE — CRACKED · airframe 35,089 hrs · 25,677 cycles
STIFFENING ANGLE ON FS280 BULKHEAD AT LBL 26 IS CRACKED. REMOVED, LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE STIFFENING ANGLE PN: CC670-34117-5 AT LBL 26 FS 280 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
2019
Part: STRAP — CORRODED (BS 319) · airframe 28,690 hrs · 20,273 cycles
"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON "CORROSION LEVEL 2, ON FRAME STRAP IN FS= 319 BETWEEN STGR 17RH TO 18RH AND 41RBL AT PAX CABIN FWD WET. THE FRAME STRAP WAS REPLACED PER CRJ-900 SRM 51-42-20-001-001-A01 " FRAME STRAP IN FS= 319 BETWEEN STGR 17RH TO 18RH AND 41RBL AT PAX CABIN FWD WET AREA. (W1) (CPAX) "
Part: SEAL — TORN (NACELLE) · airframe 28,690 hrs · 20,273 cycles
"PART RACK: TORN SEAL AT FORWARD FACE OF THE AFT CORE-COWL RH/LH ENGINE. (MOT1)(MOT2) " "SEAL AT FORWARD FACE OF THE AFT CORE-COWL RH/LH ENGINE. (MOT1)(MOT2) WERE REPAIRED PER CRJ-900 SRM 54-13-00-201-007-A "
Part: FRAME — CORRODED (BS 333) · airframe 28,690 hrs · 20,273 cycles
"[ IN REFERENCE NRC 00131 & 00134 ]: INITIAL INSPECTION: CORROSION ON FRAME FS= 333 BETWEEN STRG 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 " "CORROSION LEVEL 2. CORROSION ON FRAME FS= 333 BETWEEN STRG 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER EA CRJ953-09738 REV.IR "
Part: SUPPORT PLATE — CORRODED (BS 339) · corrosion level 2 · airframe 28,690 hrs · 20,273 cycles
"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 339 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "SUMMARY: CORROSION LEVEL 2. PROTECTION PLATE SUPPORT IN STA. FS= 339 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA WAS REPLACED PER CRJ-900 SRM 51-42-20-001-001-A01 PAR 6E "
Part: SUPPORT PLATE — CORRODED (BS 346) · corrosion level 2 · airframe 28,690 hrs · 20,273 cycles
"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "SUMMARY: CORROSION LEVEL 2.PROTECTION PLATE SUPPORT IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA WAS REPLACED PER CRJ-900 SRM 51-42-20-001-001-A01 PAR 6E "
Part: BRACKET — CRACKED · airframe 28,690 hrs · 20,273 cycles
"PARTS RACK: CRACK IN INNER BRACKET AT RH AFT CORE COWL. (MOT2) " "SUMMARY INNER BRACKET AT RH AFT CORE COWL. WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 "
Part: COUNTERBALANCE — WORN (CARGO DOOR) · airframe 28,690 hrs · 20,273 cycles
"INITIAL INSPECTION : WEAR ON COUNTER BALANCE ARM BOTH SIDE AT FWD CARGO DOOR (SM) ""WEAR WAS BLEND OUT ON COUNTER BALANCE ARMS, BOTH SIDE OF THE FWD CARGO DOOR PER CRJ-900 SRM 52-35-09-201-001-A01 , FIGURE 52-35-09-995-806. AREA REWORKED WAS MEASSURED AND FOUND IN THE FOWOLLOWING CONDITIONS:ORIGINAL THICKNESS .300"" , MAXIMUM DEPTH .260"", TH EREFORE : ITS WITHIN "
Part: HELICOIL — MISSING (RAIL) · airframe 28,690 hrs · 20,273 cycles
"INITIAL INSPECTION: MISSING HELICOIL INSERT IN FITTING ATTACHED TO AFT RIGHT RAIL AND MISSING BOLT OF HIS FITTING AT FWD BAGGAGE BAY. (CCD) " "NEW FITTING AFT RIGHT RAIL AT FWD BAGGAGE BAY WILL BE INSTALLED UNDER CARD 900-53-900-125 STEP 29. "
Part: SCUFF PLATE — WORN (CARGO BAY) · airframe 28,690 hrs · 20,273 cycles
"INITIAL INSPECTION: WAVINESS SCUFF PLATES AT FWD BAGGAGE BAY CUT-OUT.(CCD) "SCUFF PLATES AT FWD BAGGAGE BAY CUT-OUT WERE REMOVED, PER EXCESSIVE DAMAGE WILL BE REPLACED AND NEW SCUFF PLATES AT FWD BAGGAGE BAY CUTOUT WILL BE INSTALLED UNDER CARD 900-53-900-125 STEP 28 " "
Part: BOLT — MISSING (RAIL) · airframe 28,690 hrs · 20,273 cycles
"INITIAL INSPECTION: MISSING FITTING ATTACHED TO FWD RIGHT RAIL AND MISSING BOLTS OF HIS FITTING AT FWD BAGGAGE BAY. (CCD) " "NEW FITTING FWD RIGHT IN RAILAT FWD BAGGAGE BAY WILL BE INSTALLED UNDER CARD 900-53-900-125 STEP 29. "
Part: FAIRING — WORN (RT PYLON) · airframe 28,690 hrs · 20,273 cycles
"INITIAL INSPECTION: WEAR ON LOWER FAIRING AFT RH PYLON (MOT 2). " "SUMMARY: LOWER FAIRING AFT RH PYLON WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 "
Part: STRIKER — WORN (FWD CARGO DOOR) · airframe 28,690 hrs · 20,273 cycles
"INITIAL INSPECTION: WEAR ON FWD/AFT SEAL STRIKER AT FWD BAGGAGE BAY DOOR CUT-OUT. (CCD) " "WEAR ON AFT SEAL STRIKER AT FWD BAGGAGE BAY DOOR CUT-OUT WAS BLENDED OUT PER CRJ/900 SRM 51-12-00-001-001-A01. AREA WAS MEASURED WHIT FOLLOW DIMENSIONS : MAX DEPTH IS: 0.002"" THEREFORE IT IS WITHIN LIMITS FOUND PER CRJ/900 SRM 53-31-23-101-001-A02. FWD SEAL STRIKER AT FWD BAGGAGE BAY DOOR WAS REPLACED PER CRJ/900 SRM 51-41-02-001-001-A01 "
Part: ANGLE — CORRODED (BS 310-349) · airframe 28,690 hrs · 20,273 cycles
"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON MID CAP ANGLE [ JUMPER/PROX-SENSOR/CONNECTOR-WIRING ANGLE ] IN STA. FS= 310 TO FS= 349 AND 41LBL AT MAIN ENTRANCE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "CORROSION LEVEL 2. CORROSION ON MID CAP ANGLE [ JUMPER/PROX-SENSOR/CONNECTOR-WIRING ANGLE ] IN STA. FS= 310 TO FS= 349 AND 41LBL AT MAIN ENTRANCE DOOR LOWER SILL, FWD WET AREA.WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 P6 A "
Part: STEP — CORRODED · corrosion level 2 · airframe 28,690 hrs · 20,273 cycles
"AWR: OUT OF LIMITS: [ DURING EVALUATION/MEASURE OF LH FWD/AFT SILL STEP PLATE RELATED WITH NRC 00324 ]: CORROSION ON SILL STEP PLATE AT LH FWD/AFT EMERGENCY EXIT SURROUNDING STRUCTURE. (CPAX)TCI: 53-20-258 " "CORROSION LEVEL 2. SILL STEP PLATE AT LH FWD/AFT EMERGENCY EXIT SURROUNDING STRUCTURE WERE REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01 PAR6. "
Part: ANGLE — CORRODED (BS 310-349) · airframe 28,690 hrs · 20,273 cycles
"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON KICKPLATE ANGLE IN STA. FS= 310 TO FS= 349 AND 41LBL AT MAIN ENTRANCE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "CORROSION LEVEL 2. KICKPLATE ANGLE IN STA. FS= 310 TO FS= 349 AND 41LBL AT MAIN ENTRANCE DOOR LOWER SILL, FWD WET AREA WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 PAR 6,C "
Part: STRINGER — CORRODED (BS 280-327) · corrosion level 2 · airframe 28,690 hrs · 20,273 cycles
"[ IN REFERENCE NRC 00131 & 00134 ]: INITIAL INSPECTION: CORROSION ON STRINGER 26RH IN STA. FS= 280 TO FS= 327 AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 ""CORROSION LEVEL 2. STRINGER 26RH IN STA. FS= 280 TO FS= 327 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR 6.D AND CRJ-900 SRM 51-42-20-001-001-A01 PAR 6.E "
Part: SUPPORT ANGLE — CORRODED (BS 346) · airframe 28,690 hrs · 20,273 cycles
"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "CORROSION LEVEL 1. ON SUPPORT ANGLE IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL WAS MEASURED AND FOUND WHIT FOLLOWING DIMENCSIONS: OT:0.063"" AND RT:0.057"" THEREFORE IS WITHIN LIMITS IS WITHIN LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 "
Part: FRAME — CORRODED (BS 319) · corrosion level 2 · airframe 28,690 hrs · 20,273 cycles
"[ IN REFERENCE NRC 00131 & 00134 ]: INITIAL INSPECTION: CORROSION ON FRAME FS= 319 BETWEEN STRG 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 " "SUMMARY:CORROSION LEVEL 2, ON FRAME FS= 319 BETWEEN STRG 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER CRJ-900 SRM 53-00-06-201-006-A01. "
Part: STRINGER — CORRODED (BS 280-327) · airframe 28,690 hrs · 20,273 cycles
"[ IN REFERENCE NRC 00131 & 00134 ]: INITIAL INSPECTION: CORROSION ON STRINGER 26LH IN STA. FS= 295 TO FS= 319 AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 " "CORROSION LEVEL 2. STRINGER 26LH IN STA. FS= 280 TO FS= 327 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR 6.D AND CRJ-900 SRM 51-42-20-001-001-A01 PAR 6.E. "
Part: SUPPORT ANGLE — CORRODED (BS 280 FLOORBEAM) · airframe 28,690 hrs · 20,273 cycles
"[ IN REFERENCE NRC 00131 & 00134 ]: INITIAL INSPECTION: CORROSION ON FLOOR SUPPORT IN STA. FS= 280 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 " "CORROSION LEVEL 2. FLOOR SUPPORT IN STA. FS= 280 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ900 51-42-20-001-001-A01-PAR 6A AND CRJ900 SRM 51-42-06-001-001-A01 PAR 6D "
Part: SUPPORT — DAMAGED (BS 797-807) · airframe 28,690 hrs
"AWR; PER MTC REQUEST: [ DURING REMOTION OF MLG WHEEL BINS RELATED WITH TASK 900-27-900-112 STEP 5 ]: ELONGATED HOLE IN RH FAIRING SUPPORT IN STA. FS= 797 TO FS= 807 AND 35RBL AT RH MLG WHEEL WELL. (FYT) " "SUMMARY: FAIRING SUPPORT IN STA. FS= 797 TO FS= 807 AND 35RBL AT RH MLG WHEEL WELL WAS REPLACED PER CRJ-900 SRM 51-42-20-001-001-A01. "
Part: STRINGER — CORRODED (BS 295-310) · airframe 28,690 hrs · 20,273 cycles
"[ IN REFERENCE NRC 00131 & 00134 ]: INITIAL INSPECTION: CORROSION ON STRINGER 24RH IN STA. FS= 295 TO FS= 310 AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 " "CORROSION LEVEL 2. STRINGER 24RH IN STA. FS= 295 TO FS= 310 WAS REPLAED PER CRJ 900 SRM 51-42-06-001-001-A01 PAR. 6. .AND CRJ-900 SRM 51-4-20-001-001-A01 PAR 6. "
Part: STRINGER — CORRODED (BS 310-327) · corrosion level 2 · airframe 28,690 hrs · 20,273 cycles
"[ IN REFERENCE NRC 00131 & 00134 ]: INITIAL INSPECTION: CORROSION ON STRINGER 27 IN STA. FS= 310 TO FS= 327 AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 ""CORROSION LEVEL 2. STRINGER 27 IN STA. FS= 310 TO FS= 327 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR6.D AND CRJ-900 SRM 51-42-20-001-001-A01 PAR 6.E "
Part: STRINGER — CORRODED (BS 280-327) · corrosion level 2 · airframe 28,690 hrs · 20,273 cycles
"[ IN REFERENCE NRC 00131 & 00134 ]: INITIAL INSPECTION: CORROSION ON STRINGER 25LH IN STA. FS= 295 TO FS= 327 AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 " "CORROSION LEVEL 2. STRINGER 25LH IN STA. FS= 280 TO FS= 327 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR 6.D AND CRJ-900 SRM 51-42-20-001-001-A01 PAR 6.E "
Part: STRIKER — CORRODED (BS 319-349) · airframe 28,690 hrs · 20,273 cycles
"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON LOWER STRIKER IN STA. FS= 319 TO FS= 349 AND 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "CORROSION LEVEL 2.LOWER STRIKER IN STA. FS= 319 TO FS= 349 AND 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA WAS REPLACED PER CRJ-900,SRM 51-42-06-001-001-A01 "
Part: STRINGER — CORRODED (BS 337-364) · airframe 28,690 hrs · 20,273 cycles
"[ IN REFERENCE NRC 00131 & 00134 ]: INITIAL INSPECTION: CORROSION ON STRINGER 26LH IN STA. FS= 337 TO FS= 364 AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 " "CORROSION LEVEL 2. STRINGER 26LH IN STA. FS= 337 TO FS= 364 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR 6.D AND CRJ-900 SRM 51-42-20-001-001-A01 PAR 6.E. "
Part: SUPPORT ANGLE — CORRODED (BS 329) · airframe 28,690 hrs · 20,273 cycles
"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 329 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "CORROSION LEVEL 2. PROTECTION PLATE SUPPORT ANGLE IN STA. FS= 329 BETWEEN 41RBL TO 44RBL WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 "
Part: SUPPORT ANGLE — CORRODED (BS 329) · airframe 28,690 hrs · 20,273 cycles
"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 329 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "CORROSION LEVEL 2, ROTECTION PLATE SUPPORT ON RBL 44 AND STA. FS= 329 WAS REPLACED PER CRJ-900 SRM 51-42-20-001-001-A01 PAR 6E "
Part: SUPPORT ANGLE — CORRODED (BS 322) · airframe 28,690 hrs · 20,273 cycles
"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "CORROSION LEVEL 2,PROTECTION PLATE SUPPORT IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA WAS REPLACE: PER CRJ-900 SRM 51-42-20-001-001-A01 PAR 6E "
Part: CHANNEL — CORRODED (LAV SERV PANEL) · airframe 28,690 hrs · 20,273 cycles
"INITIAL INSPECTION: CORROSION ON ANGLE IMPACT CHANNEL AT FWD LAVATORY SERVICE PANEL. (FUS) (TCI: 100-16) " "SUMMARY: ANGLE IMPACT CHANNEL AT FWD LAVATORY SERVICE PANEL WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01. PAR.6A. "
Part: SUPPORT — CRACKED (BS 797-807) · airframe 28,690 hrs · 20,273 cycles
"AWR; PER MTC REQUEST: [ DURING REMOTION OF MLG WHEEL BINS RELATED WITH TASK 900-27-900-112 STEP 5 ]: CRACK IN LH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35LBL AT LH MLG WHEEL WELL. (FYT) " "FAIRING SUPPORT DIAPHRAGM LH IN STA. FS= 797 TO FS= 807 AND 35LBL AT LH MLG WHEEL WELL WAS REPLACED PER CRJ/900 SRM 51-41-02-001-001-A01 PAR D1 "
Part: SUPPORT ANGLE — CORRODED (BS 339) · airframe 28,690 hrs · 20,273 cycles
"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 339 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "CORROSION LEVEL 1. CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 339 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA WAS REMOVED PER CRJ 900 SRM 51-21-06-001-A01 PAR 5 D AND AREA WAS MEASURED AND FOUND WHIT FOLLOWING DIMENCSIONS: OT:0.063"" AND RT:0.058"" THEREFORE IS WITHIN LIMITS PER CRJ-900 SRM 53-21-23-101-001-A0 "
Part: SUPPORT PLATE — CORRODED (BS 322) · airframe 28,690 hrs · 20,273 cycles
"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) "
Part: COVER — CRACKED (PAX DOOR) · airframe 28,690 hrs · 20,273 cycles
"AWR; HIDDEN CRACK:[DURING REMOTION OF FASTENERS, RELATED WITH NRC 0465 ] CRACK IN AFT UPPER CORNER AT MAIN PASSENGER DOOR. (L1) (PTAS) " "SUMMARY: AFTER CORNER WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6. (C). AND SRM 51-42-13-001-001-A01 PAR. 6. (C). "
Part: ANGLE — CORRODED (BS 319-349) · airframe 28,690 hrs · 20,273 cycles
"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON SUPORT MOUNTING ANGLE IN STA. FS= 319 TO FS= 349 AND 41RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "SUMMARY: SUPORT MOUNTING ANGLE ON RBL 44 BTW STA FS=319 TO FS=349 WAS REPLACED PER CRJ-900,SRM 51-42-06-001-001-A01 "
Part: SKIN — CRACKED (NOT REPORTED) · airframe 28,690 hrs · 20,273 cycles
INITIAL INSPECTION: CRACK IN RECEPTACLE PLATE AT FUSELAGE. (FUS) "SUMMARY: RECEPTACLE PLATE AT FUSELAGE WAS REPLACE PER CRJ/900 SRM 51-42-20-001-001-A01 PAR.6A "
Part: PIN — OUT OF POSITION (CABIN DOOR) · airframe 28,168 hrs · 19,868 cycles
ON ARRIVAL TO BNA MAIN CABIN DOOR WOULD NOT OPEN. IT FEELS JAMMED CLOSED. FOUND PAX STAIRS STOR PIN LANYARD JAMMED IN DOOR. INSPECTED DOOR AND STOWED PINS. FOUND NO APPARANT DAMAGE. OPS CHK GOOD IAW AMM 52-11-00. OK FOR SVC.
2018
Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 26,353 hrs · 18,522 cycles
CREW O2 LOW 1010, FOUND OBSERVERS MASK LEAKING. REMOVED AND REPLACED CREW O2 MASK IAW AMM 35-11-12. OPS CHECK GOOD. ALL MX PROCEDURES COMPLIED WITH.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,151 hrs · 18,376 cycles
FA REPORTED BULBS OUT ON THE EMERGENCY LIGHT. R & R THE BULBS IAW AMM 33-51-11. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
Part: HANDLE — CRACKED (PAX DOOR) · airframe 24,948 hrs · 17,495 cycles
PAX DOOR INNER HANDLE IS CRACKED. REMOVED AND REPLACED THE PAX DOOR INNER HANDLE IAW AMM 52-11-02, CONFIG A02. OPS CHECKED GOOD.
Part: HOUSING — CRACKED (E/E DOOR HANDLE) · airframe 24,948 hrs · 17,495 cycles
MAIN AVIONICS DOOR HANDLE HOUSING IS CRACKED AROUND THE BASE OF THE HANDLE SHAFT. NDT HAS VERIFIED. REMOVED AND REPLACED MAIN AVIONICS BAY DOOR HANDLE HOUSING IAW AMM 52-42-03.
Part: HINGE — WORN (PAX DOOR) · airframe 24,948 hrs · 17,495 cycles
PAX DOOR HINGE DOOR WORN. REMOVED AND REPLACED THE PAX DOOR HINGE DOOR IAW SRM 51-42-21.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 24,948 hrs · 17,495 cycles
PAX DOOR AFT DRAG ANGLE IS CRACKED. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 51-42-06, AND 51-42-13.
Part: FRAME — CORRODED (PAX DOOR) · airframe 24,948 hrs · 17,495 cycles
PAX DOOR FWD UPPER FRAME IS CORRODED AROUND LOCK. REMOVED AND REPLACED THE PAX DOOR FRAME IAW SRM 51-42-06, AND 51-42-21.
Part: ESCAPE ROPE — FRAYED (MAIN CABIN) · airframe 24,948 hrs · 17,495 cycles
LEFT OVERWING ESCAPE ROPE IS FRAYED AND CARABINER LOCK DOES NOT SPRING CLOSED. REMOVED AND REPLACED ESCAPE ROPE AND CARABINER IAW AMM 25-63-04-000-801, AND 25-63-04-400-801.
Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 24,948 hrs · 17,495 cycles
MAIN CABIN CENTER OVERWING EXITS AFT EMERGENCY LIGHT LENS IS CRACKED. REMOVED AND REPLACED LENS IAW AMM 33-51-07-000-802-A01, PARA 4A, STEP 3, AND 33-51-07-400-802-A01, PARA 4A, STEP 5.
Part: BRACKET — CRACKED (WHEEL WELL) · airframe 24,948 hrs · 17,495 cycles
MLG BAY, CENTER FAIRING ATTACH BRACKET BETWEEN WHEEL WELL BINS BROKEN. FASTENERS MISSING. REMOVED AND REPLACED THE ATTACH BRACKET IAW SRM 51-42-06.
Part: COVER — CRACKED (CARGO DOOR) · airframe 24,948 hrs · 17,495 cycles
FWD CARGO BAY FWD LOWER HINGE HARNESS PROTECTOR CRACKED. REMOVED AND REPLACED THE FWD HINGE COVER IAW SRM 51-41-02.
Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 24,948 hrs · 17,495 cycles
G2 GALLEY LOWER FLOOR EMERGENCY LIGHT LENS CRACKED. REMOVED AND REPLACED THE LENS IAW AMM 33-51-11-000-801, STEP 4.B(1), AND 33-51-11-400-801, STEP 4.B.4.
Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 24,948 hrs · 17,495 cycles
WHILE REMOVING PAX DOOR INNER SKIN FOUND AFT UPPER INTERCOSTAL CRACKED. REMOVED AND REPLACED THE PAX DOOR INTERCOSTAL IAW SRM 51-42-21, & 51-42-06.
2017
Part: DOUBLER — CORRODED (BS 295-310) · airframe 23,411 hrs · 16,370 cycles
TCAS ANTENNA DOUBLE AT STRINGER 27, BS 280 & 298 CORRODED. REMOVED AND REPLACE CORRODED TCAS ANTENNA DOUBLER IAW SRM 51-42-06-001-001-A10, & DWG SH 670-32364
2015
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 20,127 hrs · 14,074 cycles
WHILE COMPLYING WITH EO 700-25-0166, FOUND MEGAPHONE TO BE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14.
2014
Part: SKIN — DENTED (CARGO DOOR) · airframe 17,473 hrs · 12,237 cycles
DENT ON AFT CARGO DOOR LOWER AFT CORNER. REPAIRED IAW EA 32-2014-202. MAJOR REPAIR2.
Part: ANGLE — GOUGED · airframe 17,471 hrs · 12,234 cycles
DURING REMOVAL OF RT OTBD LONGITUDAL BEAM TO BS 280 FLOORBEAM AT RBL9, ANGLE WAS FOUND GOUGED AND BONDED IN GOUGES. REMOVED GOUGED ANGLE TO PERFORM SB 670BA-53-041-01 IAW SRM 51-42-03-001-001. LOCATED & DRILLED NEW SERVICEABLE FITTING IAW SB 670BA-53-041-01 & SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE ANGLE RT OTBD AT RBL 9, FS 280 IAW SRM 51-42-21-001-001 A01 & SB 670BA-53-041-01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.
Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 17,473 hrs · 12,237 cycles
COCKPIT FLOORBEAM IS CRACKED. REPAIRED IAW REO 690-53-11-410, REV B. MAJOR REPAIR.
Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 17,473 hrs · 12,237 cycles
COCKPIT FLOORBEAM IS CRACKED. REPAIRED IAW REO 690-53-11-410, REV B. MAJOR REPAIR.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 17,471 hrs · 12,234 cycles
BS 280 LOWER BULKHEAD WEB CORRODED. REPAIRED IAW GREO 670-53-11-594.
Part: SEAT TRACK — CORRODED (BS 364-379) · airframe 17,471 hrs · 12,234 cycles
SEAT TRACK CORRODED BETWEEN BS 364 - 379 LBL9. FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A01 & 53-00-49-400-801-A07. MAJOR REPAIR.
Part: FITTING — CHAFED (RT WING TE FLAP) · airframe 17,471 hrs · 12,234 cycles
RT OTBD FLAP ROLLER GUIDE FITTING CHAFED INBD SIDE. COMPLIED WITH REO 670-57-51-036. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REPAIR OF THE WEAR DAMAGE ON OTBD FLAP ROLLER GUIDE FITTING IS COMPLETED IAW REO 670-57-51-036 AND MEETS WITH ALL ITS REQUIREMENTS.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 17,473 hrs · 12,237 cycles
CORRODED INTERCOSTAL BETWEEN BS 349 - 364 STRINGER 27L. FOUND BEYOND ALLOWABLE LIMITS, REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: SKIN — CORRODED (FUSELAGE) · airframe 17,471 hrs · 12,234 cycles
AVIONICS BAY DOOR CUTOUT INTERNAL SKIN CORRODED. BLENDED TO A SMOOTH CONTOUR IAW ITEM 6 OF ECTC REO 690-53-21-032. COMPLIED WITH GREO 690-53-21-032.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 17,471 hrs · 12,234 cycles
CORRODED INTERCOSTAL FRAMES 349 - 364 STR 27R. CORROSION IS FOUND BEYOND ALLOWABLE LIMITS, NO DAMAGE AREA IAW SRM 53-21-23-101-003-A01. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06-001-001-A01, 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 17,471 hrs · 12,234 cycles
DURING REMOVAL OF THE BS 280 FLOORBEAM CAP ANGLE. THE FLOORBEAM WAS FOUND CORRODED AND CRACKED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-06-001-001, SRM 51-40-11-001-001-A01 & DWG 670-53-11-594.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 17,471 hrs · 12,234 cycles
CORRODED INTERCOSTAL BETWEEN BS 349 - 364 S26L. CORROSION FOUND BEYOND ALLOWABLE LIMITS, NO DAMAGE AREA, IAW SRM 53-21-23-101-003-A01. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06-001-001-A01, 51-42-06-001-001-A01, SRM 51-42-06-001-001-A01 AND 51-42-21-001-A01.
Part: FRAME — CORRODED (BS 349) · airframe 17,471 hrs · 12,234 cycles
FRAME AT BS 349, CORRODED BETWEEN STRINGERS 26L & 26R. CORROSION REMOVED IAW SRM 53-21-06-101-004-A02.
Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 17,471 hrs · 12,234 cycles
RIGHT FLOOR SUPPORT CORRODED AT BS 349. R & R THE FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01.
Part: DOUBLER — CORRODED (BS 295-310) · airframe 17,473 hrs · 12,237 cycles
INTERNAL SKIN DOUBLER CORRODED AT TCAS ANTENNA CONNECTOR STRINGER 27, BETWEEN BS 295 & 310. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01-001-001-A01. REMOVED AND REPLACED THE DOUBLER IAW SR M51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG SH670-30023. MAJOR REPAIR.
Part: FITTING — CHAFED (LT WING TE FLAP) · airframe 17,471 hrs · 12,234 cycles
LT OTBD FLAP ROLLER GUIDE FITTING CHAFED ON INBD SIDE. REPAIRED IAW REO 670-57-51-036. MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (BS 669-720) · airframe 17,471 hrs · 12,234 cycles
LT SIDE SEAT TRACK SEGMENT FROM BS 669.40 - 720.85 HAS ONE SPOT OF CORROSION. FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A01, SRM 51-40-11-001-001-A01 & GREO 670-53-00-343 AND 53-00-49-400-801.
Part: STRUCTURE — CORRODED (BS 280-282) · airframe 17,471 hrs · 12,234 cycles
CORROSION ON CIRCUMFERENTIAL JOINT FS280-282.86 BETWEEN STR 26 R-25R. REMOVED CORROSION AT STA 280 STRG25L-27 IAW SRM 51-21-06-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED CORROSION FROM CIRCUMFERENTIAL JOINT AT FS280-282-.86 BETWEEN STR 26L, 25L IAW SECTION I STEP 1 A & B OR EA 22-2014-337.
Part: SEAT TRACK — CORRODED (BS 669-720) · airframe 17,471 hrs · 12,234 cycles
SEAT TRACK SEGMENT BS 669.40 - 720.85 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW 53-00-49-000-801, CONF A07.
Part: SEAT TRACK — CORRODED (BS 661) · airframe 17,471 hrs · 12,234 cycles
LEFT SIDE SEAT TRACK SEGMENT CORRODED AT BS 661+32 & 661+46 AND 661+62. FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, CONFIG A07, SRM 51-40-11-001-001-A01 AND GREO 670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 635) · airframe 17,471 hrs · 12,234 cycles
RIGHT SIDE SEAT TRACK SEGMENT FROM FS 570 TO 661+16 IS CORRODED AT FS 635. EVALUATED AND FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013. REMOVED SEAT TRACK AT RT SIDE FS 570 TO 661+16 IAW AMM 53-00-49-000-801, CONFIG A07. FABRICATED NEW SEAT TRACK IAW SRM 51-40-11-001-001-A01 AND REO 670-53-00-343. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV G AS WRITTEN. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801, CONFIG A07, AT FS 570-661+16, RT SIDE. SDR CLOSED.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 17,471 hrs · 12,234 cycles
BS 280 FWD FLOORBEAM ANGLE CORRODED. REMOVED AND REPLACED IAW SRM 51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 17,471 hrs · 12,234 cycles
LEFT SIDE SEAT RAIL SEGMENT FROM FS 785.15 TO FS 847+16 IS CORRODED AND OUT-OF-LIMITS EVALUATED AND FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013. REMOVED LT SIDE SEAT RAIL SEGMENT FROM FS 785.15-847+16 IAW SRM 51-41-00-001-001-A01 AND AMM 53-00-49-000-801CONFIG A07. FABRICATED NEW SEAT RAIL IN REF TO SRM 51-40-11-001-001-A01 AND GREO 670-53-00-343. INSTALLED NEW FABRICATED SEAT RAIL IN FEF TO AMM 53-00-49-400-801, A07.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 17,471 hrs · 12,234 cycles
PAX DOOR SILL MID CAP ANGLE IS CORRODED FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001-A01 & 53-21-23-101-001-A02. REMOVED AND REPLACED IAW SRM 51-42-06-001-001-A01, 51-41-00-001-A01.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,471 hrs · 12,234 cycles
BS 280 FLOORBEAM CRACKED AND CORRODED. CAP ANGLE REMOVED IAW SRM 51-42-06-001-001-A01 AND DWG CC670-34010. INSTALLED A NEW CAP ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG CC670-34010.
Part: FLOOR SUPPORT — CORRODED (BS 280-310) · airframe 17,471 hrs · 12,234 cycles
RT FLOOR SUPPORT CORRODED FROM BS 280-310. REMOVED AND REPLACED THE FLOOR SUPPORTIAW SRM 51-42-06-001-001-A01, DWG SH690-32170, SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND DWG SH690-32170
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 17,471 hrs · 12,234 cycles
SERVICE DOOR SILL CORRODED. REPAIRED IAW SRM 51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 790-813) · airframe 17,471 hrs · 12,234 cycles
SEAT TRACK CORRODED BS 790 AND 813.70. REPAIRED IAW SRM 51-45-00-001-001-A01, SRM 51-21-06-01-001-001, AND 53-41-49-001-002.
Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 17,471 hrs · 12,234 cycles
RT COCKPIT FLOORBEAM ANGLE CRACKED. REMOVED THE ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. FABRICATED AND INSTALLED REPLACEMENT ANGLE.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 17,471 hrs · 12,234 cycles
LT FS 280 BULKHEAD WEB CORRODED INBD EDGE. CORRSOSION WAS FOUND TO GO THROUGH WEB AND IS OUT OF LIMITS . INSTALLED A NEW BULKHEAD WEB IAW GREO 670-53-11-594. T
Part: ANGLE — CORRODED (FUSELAGE) · airframe 17,471 hrs · 12,234 cycles
SERVICE DOOR SILL KICKPLATE ANGLE CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01, SRM 51-21-06+001-001-A01. LOCATED & DRILLED SERVICE NEW DOOR KICKPLATE ANGLE IAW SRM 51-40-11-001-001-A01. ASSEMBLED NEW ANGLE & INSTALLED SERVICE DOOR LOWER SILL IAW 51-42-06-001-001-A01.
Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 17,471 hrs · 12,234 cycles
LT COCKPIT FLOORBEAM ANGLE CRACKED. REMOVED THE ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. FABRICATED AND INSTALLED REPLACEMENT ANGLE.
Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 17,471 hrs · 12,234 cycles
RIGHT SEAT TRACK CORRODED, BS 349 - 485, RBL9. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, REO 670-53-00-343 AND REO 670-53-00-343, REV G.
Part: SEAT TRACK — CORRODED (BS 485-570) · airframe 17,471 hrs · 12,234 cycles
RIGHT SIDE SEAT TRACK SEGEMENT FROM FS485 TO FS570 IS CORRODED BEYOND ALLOWABLE LIMITS. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343. REMOVED SEAT TRACK AT STA485-570 RIGHT IAW AMM 53-00-49-000-801, CONFIG A07. INSTALLED SEAT TRACK SEGMENT FROM RT SIDE FS 485 TO FS 570 IAW AMM 53-00-49-400-801, CONFIG A07. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV G AS WRITTEN. THIS REPAIR IS CLASSIFIED AS A MAJOR ALTERATION IAW SOP 5702.
Part: SEAT TRACK — CORRODED (BS 597-665) · airframe 17,471 hrs · 12,234 cycles
LT SIDE SEAT TRACK CORRODED AT BS 597-665. FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, CONFIG A01, SRM 51-40-11-001-001-A01, GREO 670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 17,471 hrs · 12,234 cycles
SEAL TRACK SEGMENT BS 744.15 TO 761.85 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 -A070 AND AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 661-669) · airframe 17,471 hrs · 12,234 cycles
RH SIDE SEAT TRACK SEGMENT FROM BS 661+16 TO 669.40 HAS CORROSION AT SEVERAL SPOTS. EVALUATED FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013. REMOVED SEAT TRACK AT FS 661+16 TO 661.40 RT IAW AMM 53-00-49-000-801-A07. FABRICATED NEW SEAT TRACK IAW SRM 51-40-11-001-001-A01 AND GREO 670-53-00-343. RECEIVED AND COMPLIED WITH ECTC REO 670-53-00-343.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 17,471 hrs · 12,234 cycles
BS 280 FLOORBEAM ANGLE CORRODED. REMOVED THE ANGLE AND INSTALLED A NEW ANGLE IAW SRM 51-42-06-001-001-A01, DWG CC670-34-256.
Part: SUPPORT — CORRODED (BS 280-365) · airframe 17,471 hrs · 12,234 cycles
CORROSION ON RT SIDE OF NOSE JACK FITTING SUPPORT, FS 365-280. OUT OF LIMITS IAW SRM 53-00-101-001-A01. REMOVED AND REPLACED IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
Part: FITTING — CORRODED (BS 365) · airframe 17,471 hrs · 12,234 cycles
CORROSION ON LT SIDE OF NOSE JACK FITTING SUPPORT BS 365.280. FOUND AREAS TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-101-001-A01, NEW SERVICEABLE SUPPORT TO BE INSTALLED. REMOVED CORRODED SUPPORT FITTING, INTERCOSTAL, IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. LOCATED & DRILLED NEW SERVICEABLE LT SUPPORT IAW DWG CC670-32179. INSTALLED SOLID RIVETS THROUGH THE SKIN ON THE LT SIDE OF NOSE JACK FITTING SUPPORT IN REF TO SRM 51-42-06-001-001-A01.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 17,471 hrs · 12,234 cycles
PAX DOOR SILL FWD CAP ANGLE CORRODED. REMOVED CORROSION ON LOWER SILL FWD CAP ANGLE FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001-A01 & 53-21-23-101-001-A02. REMOVED FWD CAP ANGLE, PN SH670-31821-5 IAW SRM 51-42-06-001-001-A01. DRILLED UP FWD CAP ANGLE AND INSTALLED FWD CAP ANGLE IAW SRM 51-40-11-001-001-A01 AND SRM 51-42-06-001-001-A01 AND DWG SH670-31821.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 17,471 hrs · 12,234 cycles
SERVICE DOOR SILL CAP ANGLE CORRODED. EVALUATED SERVICE DOOR LOWER SILL CAP ANGLE - OUT OF LIMITS IAW SRM 51-21-06-001-001-A01 53-21-23-101-002-A01. LOCATED & DRILLED NEW SERVICE DOOR LOWER SILL CAP ANGLE IAW SRM 51-40-11-001-001 INSTALLED NUTPLATES & CLIPS IAW SRM 51-42-06-001-001-A01. ASSEMBLED NEW ANGLE & INSTALLED SERVICE DOOR SILL IAW SRM 51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 549) · airframe 17,471 hrs · 12,234 cycles
LT SIDE SEAT TRACK CORRODED AT BS 549. R & R SEAT RAIL AT IAW AMM 53-00-49-000-801 CONFIG A07 AND 53-00-49-400-801-A07 11/20/14, FS485-572.
Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 17,471 hrs · 12,234 cycles
LT VERTICAL AFT DRAG ANGLE CRACKED. REMOVED THE DRAG ANGLE AND INSTALLED A NEW DRAG ANGLE IAW SRM 51-42-10-001-01-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, 51-42-22-001-001-A01 AND DWG BA670-35002.
Part: HINGE — GOUGED (PAX DOOR) · airframe 17,471 hrs · 12,234 cycles
PAX DOOR, FUSELAGE SIDE, HINGE AFT LUG LAND GOUGED BY ROLL PIN. REPAIRED THE HINGE IAW REO 670-53-21-582-REV B.
Part: RETAINER — BENT (CARGO DOOR SEAL) · airframe 17,333 hrs · 12,138 cycles
FWD CARGO DOOR SEAL RETAINER BENT. REPAIRED IAW REO 690-52-35-013 MAJOR REPAIR IAW GMM 5-3.
Part: RETAINER — DAMAGED (CARGO DOOR SEAL) · airframe 16,483 hrs · 11,530 cycles
SEAL RETAINER OF FWD DOOR, FWD CARGO BIN, IS DAMAGED. PERFORMED PERMANENT REPAIR OPTION OF REO 690-52-35-013, REV "A" ON FWD DOOR OF FWD CARGO BIN.
Part: RETAINER — DAMAGED (CARGO DOOR) · airframe 16,483 hrs · 11,530 cycles
SEAL RETAINER OF AFT DOOR OF FWD CARGO BIN, IS DAMAGED ON UPPER AND LOWER RETAINERS. PERFORMED PERMANENT REPAIR OPTION OF REO 690-52-35-013 REV "A" ON AFT DOOR OF FWD CARGO BIN UPPER AND LOWER RETAINERS.
2013
Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 13,603 hrs · 9,700 cycles
FIRST FLIGHT OF DAY CHECK- EMERGENCY LIGHTS SWITCH SELECTED ON THE FORWARD HALF OF CABIN EMERGENCY LIGHTS COME ON THEN THEY GO OFF. AFT EMERGENCY LIGHTS STAY ON. RESET, CHARGED CABIN, EMERGENCY LIGHTS BATTERIES & OPS CHECKED GOOD, IAW AMM 33-51-01. ACFT OK FOR SERVICE.
Part: PROXIMITY SENSOR — FAULTY (LANDING GEAR) · airframe 12,643 hrs · 9,082 cycles
ON FLIGHT 3870 (TYS TO ATL) AFTER TAKEOFF GEAR UP DISAGREE, LEFT INITIALLY THEN INCLUDED THE NOSE & PROXIMITY SYSTEM 1 STATUS. COMPLETED QRH WITH GEAR DOWN AND LOCKED. FLIGHT CONTINUED TO ATL AND LANDED SAFELY. (AIRCRAFT WAS OUT OF SERVICE AND IN WORK FROM 1/24 UNTIL 1/28). REMOVED AND REPLACED PROXIMITY 20. OPS CHECKED GOOD PER AMM 32-61-05. OK FOR SERVICE.
Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 12,641 hrs · 9,078 cycles
7 EACH LIFE VEST HAS HOLES IN BAG. REMOVED AND REPLACED 7 LIFE VEST IAW AMM 25-61-03.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 12,517 hrs · 8,992 cycles
CREW REPORTS FLIGHT ATTENDANT FLASHLIGHT (FWD) INOPERABLE. REMOVED & REPLACED FWD FLIGHT ATTENDANT FLASHLIGHT BATTERY IAW CRJ900 AMM 25-61-02. OPS CHECK GOOD. OK FOR CONTINUED SERVICE.
2012
Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 12,013 hrs · 8,638 cycles
OBSERVER'S LIFE VEST HAS TEAR IN BAG. REMOVED AND REPLACED OBSERVERS LIFE VEST IAW AMM 25-61-03.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,540 hrs · 8,285 cycles
LEFT SIDE SEAT RAILS FWD AND AFT OF EMERGENCY EXITS CORRODED OUT OF LIMITS. REMOVED AND REPLACED IAW AMM 53-00-49.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,540 hrs · 8,285 cycles
RIGHT FLOOR NR 2 SEAT TRACK CORRODED OUT OF LIMITS. REMOVED AND REPLACED IAW AMM 53-00-49.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,540 hrs · 8,285 cycles
LEFT FLOOR SEAT TRACK NR 4 CORRODED OUT OF LIMITS. REMOVED AND REPLACED IAW AMM 53-00-49.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,540 hrs · 8,285 cycles
RIGHT SEAT TRACK CORRODED OUT OF LIMITS. REMOVED AND REPLACED IAW AMM 53-00-49.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 11,538 hrs · 8,285 cycles
RBL 12 FLOORBEAM CRACKED AT BACKUP FITTING BOSS. REPAIRED IAW BOMBARDIER REO 690-53-11-410.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 11,540 hrs · 8,285 cycles
LBL 12 FLOORBEAM CRACKED AT BACKUP FITTING BOSS. REPAIRED IAW REO 690-53-11-410.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,540 hrs · 8,285 cycles
LEFT SIDE NR 3 SEAT TRACK AND HARDWARE CORRODED. REPAIRED IAW SRM 51-21-06.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,540 hrs · 8,285 cycles
LEFT AISLE SEAT TRACK CORRODED AT FS 797. REPAIRED IAW BOMBARDIER REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,540 hrs · 8,285 cycles
LEFT NR 6 SEAT TRACK AND HARDWARE CORRODED. REPAIRED IAW BOMBARDIER REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,540 hrs · 8,285 cycles
LEFT SIDE NR 4 SEAT TRACK AND HARDWARE CORRODED. REPAIRED IAW SRM 51-21-06.
Part: DOOR — LEAKING · airframe 11,538 hrs · 8,285 cycles
FOUND EMERGENCY DOOR AT 12 AB SQUEALING AT DOOR FLAP. CLEANED AND APPLIED SEALANT AT GAP ON EMERGENCY DOOR FLAP RGF AMM 52-21-00. OK FOR SERVICE, LT WING FWD EMERGENCY DOOR.
Part: SEAL — LEAKING (EMERGENCY EXIT) · airframe 11,523 hrs · 8,274 cycles
LEFT EMERGENCY EXIT DOOR MAKES LOUD NOISE IN FLIGHT. REMOVED AND REPLACED LEFT EMERGENCY (LT WING) EXIT VENT PLATE SEAL IAW AMM 52-21-03.
Part: LIGHT — MISSING (CABIN) · airframe 11,523 hrs · 8,274 cycles
EMERGENCY LIGHT MISSING. REPLACED LIGHT IAW AMM 33-51-06 (12 A/B). AIRCRAFT OK FOR SERVICE.
Part: ACTUATOR — SATURATED (LE SLAT) · airframe 10,954 hrs · 7,807 cycles
SLATS FAIL CAUTION MSG ON DESCENT SLAT WOULD NOT EXTEND PAST 0. PERFORMED WATER CONTAMINATION CHECK OF ALL SLAT ACTUATORS PER SL 27-0080, REMOVED WATER FROM LEFT SLAT ACTUATORS 1-1, 2-1 AND RIGHT WING ACTUATORS 1-1, 2-2. RE-INSTALLED ACTUATORS AND OPS CHECKED GOOD PER CRJ-900 AMM # 27-81-09.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 10,813 hrs · 7,703 cycles
F/O FLASHLIGHT NOT BLINKING. REMOVED AND REPLACED FLASHLIGHT ON F/O SIDE IAW AMM 25-60-00. OK FOR SERVICE.
Part: BATTERY — DAMAGED (FLASHLIGHT) · airframe 10,813 hrs · 7,703 cycles
FLASHLIGHT BATTERY DAMAGED. REMOVED AND REPLACED F/O FLASHLIGHT BATTERY IAW AMM 25-60-00. OK FOR SERVICE.
Part: WIRE — DAMAGED (DOOR WARNING) · airframe 10,790 hrs · 7,688 cycles
AIR RETURN FOR PROXY SYS FAULTED ON AFTER BLOCK OUT WITH CTR CARGO DOOR MESSAGE ABLE TO GET MESAGE OUT WITH A RESET OF CTR CARGO DOOR ON CLIMBOUT RECEIVED B"PROX SYS FAULTED" STATUS MESSAGE AGAIN AFTER TALKING TO MX RETURN TO ATL. UPON TROUBLESHOOTING FOUND PX 13 SNSR WIRE OPEN, PERFORMED WIRE REPAIR IAW CMM 52-35-00 OPERATIONAL TEST OF DOOR INDICATION CONDITION TEST GOOD OK FOR SERVICE IAW CRJ 900 AMM 52-70-12 EWIS OBSERVED.
2011
Part: PUMP — INOPERATIVE (LT ENGINE) · airframe 10,051 hrs · 7,230 cycles
LT EDP INOP LOW HYDRAULIC PRESSURE MSG. EDP REMOVED AND DEFERRED.
Part: ANTI-ICE VALVE — MALFUNCTIONED (LT WING) · airframe 9,867 hrs · 7,092 cycles
MASTER WARNING ANTI DUCT IN FLIGHT WITH WINGS ANTI ICE ON AT AND ABOVE 65 PERCENT N2. REMOVED AND RE-INSTALLED LT ANTI ICE VALVE IAW AMM 30-12-02. OP CHECK AND LEAK CHECK GOOD. OK FOR SERVICE.
Part: O-RING — DAMAGED (AC BAY) · airframe 9,124 hrs · 6,529 cycles
L BLEED DUCT WARNING. FOUND PROTUDING O-RING IN LEFT ACM DUCT AND LEAKING AIR. REMOVED AND REPLACED O-RING IN L ACM AND LEAK TEST GOOD PER CRJ-900 AMM 21-51-00.
Part: SEAL — TORN (RT MLG FAIRING) · airframe 7,660 hrs · 5,568 cycles
FOLLOWING THE INSPECTIONS PER SB A670BA-32-030, OPERATOR HAS REPORTED DAMAGE TO THE RT MLG FAIRING AFT RUBBER SEAL. SEAL PIN CC670-39247-2 IS TORN AT 2 LOCATIONS WITH LENGTHS MEASURING 1.50" AND 0.50". TEMPORARY REPAIR IAW BOMBARDIER REO 690-53-83-017. REPEAT INSPECT EVERY 25 FH. REMOVE AND REPLACE SEAL IAW CRJ 900 AMM 53-83-85 WITHIN 150 FH.
2010
Part: STRIP — MISSING (FUSELAGE) · airframe 7,558 hrs · 5,494 cycles
THE CENTER (AISLE) FLOOR PANEL WAS REMOVED FOR MAINTENANCE AND THE JOINT STRIP (REFERENCE IPC 53-00-47, FIGURE 5B, ITEM 375) WAS NOT INSTALLED AT FUSELAGE STATION 693.3 (BETWEEN FLOOR PANELS 251BLF AND 261 AFL). THE JOINT STRIP PROVIDES A METHOD FOR THE FLOOR PANELS TO JOIN THE FORWARD / AFT ENDS OF FLOOR PANELS AND PROVIDE SUPPORT AT THESE JUNCTIONS. PERMANENT REPAIR IAW STS ENGINEERING EA 5-2010-318.
Part: WIRE HARNESS — SHORTED (BRAKE SYSTEM) · airframe 7,216 hrs · 5,260 cycles
LEFT MAIN INBOARD BRK MASTER WARNING IN FLIGHT BTMS 20 REMOVED AND REPLACED LT INBOARD MAIN GEAR HARNESS IAW CRJ900 AMM 32-61-05. OPS CHECKS GOOD. OK FOR SERVICE.
2009
Part: CONNECTOR — SHORTED (POTABLE WATER) · airframe 3,872 hrs · 2,912 cycles
IN CRUISE AT FL 310, HEARD A POP AND SAW SPARKS COME FROM ABOVE THE JUMP SEATERS HEAD IN GASPER AREA WITH SMOKE. QRH FOLLOWED, EMERGENCY DECLARED AND DIVERTED. LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND CONNECTOR FOR GALLEY POTABLE WATER SYSTEM SHORTED. REMOVED AND REPLACED CONNECTOR IAW C & D ZODIAC CMM. WIRE DESIGNATOR PL 114P1.