N709PS
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| PSA Airlines Inc. | Operator | 2017-02-15 – 2017-02-15 | Operator named in NTSB report |
| PSA AIRLINES, INC. (VNAA) | Operator | 2017-02-15 – 2017-02-15 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
LH WINDSHIELD SIDE POST P/N 601R33223 IS CRACKED APPROX. 6" FROM TOP AND 2" LONG AT 100% FSH FAILING NDT. REPAIRED BY CUTTING OUT DAMAGED PORTION AND SPLICING IN NEW REPAIR PARTS IAW MHIRJ REO 670-53-21-2465 REV-- DATED 10-21-24
FOUND R/H FLAP VANE ACTUATOR AT FLS 140.40 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE. CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIRJ REO 670-57-52-257 REV A DATED 2024-08-20.
FOUND R/H FLAP VANE ACTUATOR AT FLS 102.90 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE. CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIRJ REO 670-57-52-257 REV A DATED 2024-08-20.
FOUND R/H FLAP VANE ACTUATOR AT LWS 65.50 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE. CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIRJ REO 670-57-52-257 REV A DATED 2024-08-20.
FOUND L/H FLAP VANE ACTUATOR AT LWS 140.40 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE. CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIRJ REO 670-57-52-257 REV A DATED 2024-08-20.
FOUND L/H FLAP VANE ACTUATOR AT LWS 65.50 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE. CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIRJ REO 670-57-52-257 REVA DATED 2024-08-20.
FOUND L/H FLAP VANE ACTUATOR AT LWS 102.90 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE. CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIRJ REO 670-57-52-257 REV A DATED 2024-08-20.
FOUND L/H FLAP VANE ACTUATOR AT FLS 24.00 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIRJ REO 670-57-52-257 REVA DATED 2024-08-20.
PILOT RUDDER FEEL UNIT CHANNEL CC670-94223 REQUIRES REMOVAL DUE TO DOUBLE DRILLED HOLE. CORRECTIVE ACTION: REMOVED PILOT RUDDER FEEL UNIT LWR CHANNEL CC670-94223 IAW CRJ 700 AMM 27-21-05-000-801-A01 FABRICATED RUDDER PEDAL SUPPORT CHANNEL PN: CC670-94223-3 IAW CRJ-700 SRM 51-24-16-001-001-A01 AND 51-24-36-001-001-A01. REFERENCE DRAWING CC670-94223 FOR MATERIAL SPECIFICATIONS AND DIMENSIONS. INSTALLED RUDDER PEDAL SUPPORT CHANNEL P/N CC670-94223-3 IAW CRJ 700 SRM 51-42-02-001-001-A01
PAX DOOR INNER ANGLE ON VENT FLAP COVER FOUND CRACKED AND REQUIRES REPLACEMENT. CORRECTIVE ACTION: REMOVED CRACKED INNER ANGLE IAW CRJ 700 SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW INNER ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE INNER ANGLE P#601R318072-1 IAW CRJ 700 SRM 51-42-06-001-001-A01
PAX DOOR TOP STEP PANEL CRACKED REQUIRES REPLACEMENT CORRECTIVE ACTION: LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR TOP STEP PANEL P/N:601R317075-3 IAW CRJ700 SRM 51-40-11-001-001-A01. REFERENCE JOB CARD HN00189258 FOR REMOVAL AND INSTALL
R/H I/B SEAT TRACK @ FS 538 HAS SOME GOUGING AND MINOR CORROSION WHICH REQUIRES EVALUATION. REMOVED RBL 9 SEAT TRACK BETWEEN FS485 AND FS581 IAW CRJ-700 SRM 53-00-49-000-801-A03. FABRICATED NEW SEAT TRACK P/N SH690-33407-1 @ RBL 9 SEAT TRACK BETWEEN FS485 AND FS581 IAW CRJ 700 SRM 53-00-49-201-002-A01. INSTALLED SEAT TRACK P/N SH690-33407-1 @ RBL 9 BETWEEN FS485 AND FS581 IAW CRJ 700 AMM 53-00-49-400-801-A03.
PAX DOOR AFT DRAG ANGLE FOUND WITH CRACK AT UPPER END. CORRECTIVE ACTION: LOCATE, DRILL, AND INSTALLED NEW SERVICEABLE DRAG ANGEL P# 601R31772-5S IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
STR 26R @ FS. 333 + 6 FOUND TO HAVE PITTING/CORROSION ON ATTACH FLANGE. CORRECTIVE ACTION: REMOVED CORRODED STRINGER AND INSTALLED A NEW STGR26R BETWEEN FS 333 AND FS 364 (PN- SH670-31372-4S) IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-21-06-001-001-A0
PAX DOOR FWD STAIR WEB DRAG ANGLE FOUND CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
PAX DOOR FWD STAIR WEB DRAG ANGLE FOUND CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
PAX DOOR AFT CORNER COVER FOUND CRACKED UPON REMOVAL. REQUIRES REPLACEMENT. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-13-001-001-A01.
CLEAT LOCATED AT STR19L ON FWD SIDE OF FS1047 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-021-001-001-A01.
MAIN AVIONICS DOOR L/H FWD SEAL RETAINER IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
FS 909 RBL 2- RBL 22 WING TO FUSELAGE SUPPORT STRUCTURE FLANGE FAYING SURFACE (BOTTOM) IS CORRODED ALONG LENGTH. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-10-001-001-A01.
FS 909 RBL 2- RBL 22 WING TO FUSELAGE SUPPORT STRUCTURE FLANGE FAYING SURFACE (BOTTOM) IS CORRODED ALONG LENGTH. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-10-001-001-A01.
FS 939 ON CL WING TO FUSELAGE SUPPORT STRUCTURE FLANGE IS CORRODED AROUND 2 EA. FASTENER HOLES AND REQUIRES EVALUATION. CORRECTIVE ACTION: REMOVED AND REPLACED ANGLE P/N SH670-39189-1 IAW CRJ-700-SRM-51-40-11-001-001-A01 AND 51-42-06-001-001-A01
FS 879 LBL 10- RBL 28 WING TO FUSELAGE SUPPORT STRUCTURE FLANGE FAYING SURFACE (BOTTOM) IS CORRODED ALONG LENGTH AND REQUIRES EVALUATION CORRECTIVE ACTION: REMOVED CORRODED STRAPS AND INSTALLED (2) STRAPS P/N: (SH670-39333-9) ON FS 879 LBL 10- RBL 28 WING TO FUSELAGE SUPPORT STRUCTURE IAW CRJ700 SRM 51-45-00-001-001-A01, 51-42-10-001-001-A01, 51-42-06-001-001-A01, 51-23-00-001-001-A01, & 51-25-01-001-001-A01.
FS 333.00 FRAME IS CRACKED BETWEEN STRINGER 2R AND 3R. REPAIRED BY CUTTING OUT DAMAGED PORTION AND SPLICING IN NEW REPAIR PARTS IAW MHIRJ REO 670-53-21-2465 REV-- DATED 10-21-24
MAIN AVIONICS DOOR, R/H SEAL RETAINER IS CORRODED. REMOVED AND REPLACED RETIANER I.A.W. CRJ700 SRM 51-42-06-001-001-A01.
THE LEFT WING INBOARD FLAP LOWER SKIN IS DENTED 6 X 6 X .035 JUST AFT OF THE MLG TIRES. CORRECTIVE ACTION: REPAIRED IAW CRJ-700 SRM 57-52-01-201-005-A01.
F.S. 406-421 STR 19 CORRODED CORRECTIVE ACTION:STRINGER WAS REPAIRED IAW IAW CRJ700 SRM 53-00-03-201-001-A01
FOUND R/H SLAT TRACK 3-1 TO HAVE WEAR DAMAGE IN MULTIPLE LOCATIONS. CORRECTIVE ACTION: REPAIRED R/H SLAT TRACK 3-1 IAW REO 670-57-42-1745 REV-DATED 11-11-2024. SDIR IS BEING TRACKED UNDER RFTS-116974
RBL 9 FLOOR BEAM IS CORRODED AT FS 1031 CORRECTIVE ACTION: DAMAGE WAS REPAIRED IAW CRJ700 SRM 53-00-41-201-001-001-A01 AND REO 670-53-61-2395 REV-- DATED 2024-10-24
FS 280.00 J ANGLE CORRODED LBL 9 TO RBL 9 INCLUDING BOTH WALL CLIPS. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. BLENDED WALL CLIPS IAW CRJ 700 SRM 51-21-06-001-001-A01, WITHIN LIMITS IAW CRJ 700 SRM 53-00-00-101-001-A01.
MULTIPLE AREAS OF CORROSION R/H SILL PLATE F.S. 280 -333 RBL 34 CORRECTIVE ACTION: REMOVED AND REPLACED R/H SILL PLATE P/N SH670-32172-5 AT FS 280-333 RBL 34 IAW CRJ 700 SRM 51-42-13-001-001-A01
RIGHT INBD FWD GALLEY TIE DOWN CORRODED JUST AFT OF F.S.280 APPROX RBL 14. REMOVED CORRODED TIE DOWN. LOCATED AND REPLACED WITH NEW SERVICEABLE R/H INBD FWD GALLEY TIE DOWN P/N (SH670-32149-3) JUST AFT OF F.S.280 APPROX RBL 14 IAW CRJ-700 SRM 51-42-21-001-001-A01.
FS 280.00 J ANGLE CORRODED LBL 9 TO RBL 9 INCLUDING BOTH WALL CLIPS. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. BLENDED WALL CLIPS IAW CRJ 700 SRM 51-21-06-001-001-A01, WITHIN LIMITS IAW CRJ 700 SRM 53-00-00-101-001-A01.
3 EA TOOLING MARKS ON AFT BOTTOM SIDE OF L/H TORQUE BOX BELOW LOOKING UP F.S.295 APPOX LBL12. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-13-001-001-A01.
STR 25R CORRODED F.S. 280 -333. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
FS 632-655 WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE FLANGE IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
DISCREPANCY: FS 629 STGR 19L -27 ON WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE FLANGES FWD AND AFT HAVE MULTIPLE AREAS OF CORROSION AROUND THE FASTENER HOLES CORRECTIVE ACTION: INSTALLED NEW SERVICEABLE SPLICE JOINT PLATE P/N SH670-39054-3 WITH SOLID RIVETS IAW CRJ-700 SRM 51-42-06-001-001-A01.
R/H I/B SEAT TRACK @ FS 538 HAS SOME GOUGING AND MINOR CORROSION WHICH REQUIRES EVALUATION. CORRECTIVE ACTION: REMOVED RBL 9 SEAT TRACK BETWEEN FS485 AND FS581 IAW CRJ-700 SRM 53-00-49-000-801-A03. FABRICATED NEW SEAT TRACK P/N SH690-33407-1 @ RBL 9 SEAT TRACK BETWEEN FS485 AND FS581 IAW CRJ 700 SRM 53-00-49-201-002-A01. INSTALLED SEAT TRACK P/N SH690-33407-1 @ RBL 9 BETWEEN FS485 AND FS581 IAW CRJ 700 AMM 53-00-49-400-801-A03.
FRAME AT FS 661 BOTTOM CL AFT END OF FWD CARGO COMPARTMENT IS CORRODED COMPLETELY THROUGH TO THE SHEAR TIE ON THE FRONT SIDE WITH A HOLE APPROXIMATELY 1". CORRECTIVE ACTION: CUT AWAY DAMAGED PORTION OF FRAME AND INSTALLED REPAIR PARTS IAW MHIRJ REO 670-53-31-984 REV-- DATED 12-20-2024.
RH SIDE SEAT RAIL IS CORRODED BETWEEN FS 785.15 AND 863.00. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 AMMS 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.
UPON REMOVAL OF AFT CARGO DOOR SILL, FOUND THE CENTER INNER CHORD TO BE CORRODED AT NUTPLATE LOCATIONS. DAMAGE WAS REPAIRED BY INSTALLING A SERVICABLE INNER CHORD
UPON REMOVAL OF AFT CARGO DOOR SILL, FOUND THE CENTER INNER CHORD TO BE CORRODED AT NUTPLATE LOCATIONS. CORRECTIVE ACTION: DAMAGE WAS REPAIRED BY INSTALLING A SERVICABLE INNER CHORD
UPON REMOVAL OF AFT CARGO DOOR SILL, FOUND THE CENTER INNER CHORD TO BE CORRODED AT NUTPLATE LOCATIONS. CORRECTIVE ACTION: DAMAGE WAS REPAIRED BY INSTALLING A SERVICABLE INNER CHORD
UPON REMOVAL OF AFT CARGO DOOR SILL, FOUND THE FWD INNER CHORD TO BE CORRODED AT NUTPLATE LOCATIONS. CORRECTIVE ACTION: DAMAGE WAS REPAIRED BY INSTALLING A SERVICABLE INNER CHORD
DISCREPANCY: LH SIDE SEAT RAIL IS CORRODED BETWEEN FS863 AND FS969.00
RBL 9 SEAT TRACK IS CORRODED BETWEEN FS 985.00 AND 1015.00. CORRECTIVE ACTION: REMOVED SEAT TRACK ON RBL9 FROM FS985.00 TO FS1015.00 IAW CRJ-700 AMM 53-00-49-000-802 CONFIG A03. SEAT TRACK ON RBL9 FROM FS985.00 TO FS1015.00 WAS FABRICATED IN COMPLIANCE WITH REO 670-53-00-589, REV-C, DATE: 2022-12-19. INSTALLED NEW SERVICABLE SEAT TRACK P/N 670-53-00-589-1 IAW MHIRJ REO 670-53-00-589, REV-C, DATE: 2022-12-19
LBL 9 SEAT TRACK IS CORRODED BETWEEN FS 985.00 AND 1015.00. CORRECTIVE ACTION: REMOVED, FABRICATED, AND REPLACED SEAT TRACK IAW MHIRJ REO 670-53-00-589, REV-C, DATE: 2022-12-19.
RBL 27 SEAT TRACK IS CORRODED BETWEEN FS 1031.00 AND 1069.75. CORRECTIVE ACTION: REMOVED, FABRICATED, AND REPLACED SEAT TRACK IAW MHIRJ REO 670-53-00-589, REV-C, DATE: 2022-12-19.
RBL 9 SEAT TRACK IS CORRODED BETWEEN FS 1031.00 AND 1069.75. CORRECTIVE ACTION: REMOVED SEAT TRACK ON RBL 9 FROM FS 1031.00 TO FS 1069.75 IAW CRJ-700 AMM 53-00-49-000-802 CONFIG A03. RBL 9 SEAT TRACK FS 1031.00 - 1069.75.WAS FABRICATED IN COMPLIANCE WITH REO 670-53-00-589, REV-C, DATE: 2022-12-19. INSTALLED NEW SERVICABLE SEAT TRACK P/N 670-53-00-589-1 IAW MHIRJ REO 670-53-00-589, REV-C, DATE: 2022-12-19
LBL 9 SEAT TRACK IS CORRODED BETWEEN FS 1031.00 AND 1069.75. CORRECTIVE ACTION: REMOVED, FABRICATED, AND REPLACED SEAT TRACK IAW MHIRJ REO 670-53-00-589, REV-C, DATE: 2022-12-19.
DISCREPANCY: LBL 9 FLOOR BEAM IS CORRODED AT FS 1031.00 CORRECTIVE ACTION: DAMAGE WAS REPAIRED IAW REO 670-53-61-2395 REV-- DATED 2024-10-24 AND CRJ-700 SRM 53-00-41-201-001-A01
DISCREPANCY: AFT CARGO BAY SEAT TRACK ON LBL27 FROM FS978 TO FS1006 IS CORRODED CORRECTIVE ACTION: REMOVED CORRODED SEAT RAIL AND INSTALLED A SERVICABLE SEAT RAIL IAW CRJ-700 AMM 53-00-49-000/400-801-A03
CO # 101651424 BARCODE HN00190434 DISCREPANCY: LH SIDE SEAT RAIL IS CORRODED BETWEEN FS863 AND FS969.00
LH SIDE SEAT RAIL IS CORRODED BETWEEN FS 785.15 AND 863. REMOVED CORRODED SEAT RAIL AND INSTALLED A SERVICABLE SEAT RAIL
PAX DOOR AFT FORMER FOUND TO HAVE PREVIOUS REPAIR REQUIRES REPLACEMENT. CORRECTIVE ACTION: REMOVED AND REPLACED PAX DOOR AFT FORMER P/N 601R318034-5S IAW CRJ 700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01AND CRJ 700 SRM 51-42-22-001-001-A01.
PILOT WINDSHIELD LOWER LANDING IS GOUGED IN MULTIPLE LOCATIONS. CORRECTIVE ACTION: REPAIRED DAMAGED AREA IAW MHIRJ REO 670-53-11-2032 REV. -- DATED 2024-10-10.
FOUND PAX DOOR AFT DD1 TO BE CRACKED REQUIRES REPLACEMENT. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
LBL 27 FLOOR BEAM IS CORRODED BETWEEN FS 1000.00 AND 1031.00. CORRECTIVE ACTION: REPAIRED BY CUTTING OUT DAMAGED PORTION AND SPLICING IN NEW FABRICATED FLOOR BEAM IAW CRJ 700 SRM 53-00-41-201-001-A01.
CO-PILOT WINDSHIELD LOWER LANDING IS GOUGED IN MULTIPLE LOCATIONS. CORRECTIVE ACTION: REPAIRED DAMAGED AREA IAW MHIRJ REO 670-53-11-2032 REV. -- DATED 2024-10-10
RH SIDE SEAT RAIL IS CORRODED BETWEEN FS 708.00 AND 761.85. CORRECTIVE ACTION: REMOVED, FABRICATED, AND REPLACED SEAT TRACK IAW CRJ 700 SRM 53-00-49-201-002-A01 AND CRJ 700 AMM 53-00-49-400-801-A03.
RH SIDE SEAT RAIL IS CORRODED BETWEEN FS 677.00 AND 708.00. CORRECTIVE ACTION: REMOVED, FABRICATED, AND REPLACED SEAT TRACK IAW CRJ 700 SRM 53-00-49-201-002-A01 AND CRJ 700 AMM 53-00-49-400-801-A03.
RBL 9 SEAT TRACK IS CORRODED BETWEEN FS 830.40 AND 969.00. CORRECTIVE ACTION: REMOVED, FABRICATED, AND REPLACED SEAT TRACK IAW CRJ 700 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-400-801-A03.
LH SIDE SEAT RAIL IS CORRODED BETWEEN FS 708.00 AND 761.85. CORRECTIVE ACTION: REMOVED, FABRICATED, AND REPLACED SEAT TRACK IAW CRJ 700 SRM 53-00-49-201-002-A01 AND CRJ 700 AMM 53-00-49-400-801-A03
LH SIDE SEAT RAIL IS CORRODED BETWEEN FS 677.00 AND 708.00. CORRECTIVE ACTION: REMOVED, FABRICATED, AND REPLACED SEAT TRACK IAW CRJ 700 SRM 53-00-49-201-002-A01 AND CRJ 700 AMM 53-00-49-400-801-A03.
RH SIDE SEAT RAIL IS CORRODED BETWEEN FS 565.00 AND 677.00. CORRECTIVE ACTION: REMOVED R/H SIDE WALL SEAT TRACK (PN - SH670-33558-3) BETWEEN FS 565.00 TO FS 677.00 IAW CRJ700 AMM 53-00-49-000-801-A03. INSTALLED NEW SERVICEABLE R/H SIDE WALL SEAT TRACK (PN - SH670-33558-3) BETWEEN FS 565.00 TO FS 677.00 IAW CRJ700 AMM 53-00-49-400-801-A03
LBL 9 SEAT TRACK IS CORRODED BETWEEN FS 677.00 AND 830.40. CORRECTIVE ACTION: REMOVED SEAT TRACK LBL9 FS677-830.40 IAW CRJ700 AMM 53-00-49-000-801-A03, FABRICATED NEW SEAT TRACK P/N SH670-35864-3 @ LBL 9 BETWEEN F.S 677 AND F.S 830.40 IAW CRJ 700 SRM 53-00-49-201-002-A01, INSTALLED SEAT TRACK LBL9 FS677-830.40 IAW CRJ700 AMM 53-00-49-400-801-A03.
THE LOWER WING SKIN IS GOUGED AFT OF FUEL PANEL 611AB, APPROXIMATELY 0.25" LONG AND 0.018" DEEP. CORRECTIVE ACTION: REPAIRED IAW REO-670-57-21-997 REV-- DATED 10-17-24
THE LOWER WING SKIN IS GOUGED AFT OF FUEL PANEL 511AB, APPROXIMATELY 0.20" LONG AND 0.007" DEEP. CORRECTIVE ACTION REPAIRED IAW REO-670-57-21-997 REV-- DATED 10-17-24
RBL 9 SEAT TRACK IS CORRODED BETWEEN FS 677.00 AND 830.40. CORRECTIVE ACTION: FABRICATED NEW SEAT TRACK P/N SH670-35864-3 @ RBL 9 BETWEEN F.S 677 AND F.S 830.40 IAW CRJ 700 SRM 53-00-49-201-002-A01 INSTALLED SEAT TRACK RBL9 FS677-830.40 IAW CRJ700 AMM 53-00-49-400-801-A03
LBL 9 SEAT TRACK IS CORRODED BETWEEN FS 677.00 AND 830.40. CORRECTIVE ACTION: REMOVED SEAT TRACK LBL9 FS677-830.40 IAW CRJ700 AMM 53-00-49-000-801-A03, FABRICATED NEW SEAT TRACK P/N SH670-35864-3 @ LBL 9 BETWEEN F.S 677 AND F.S 830.40 IAW CRJ 700 SRM 53-00-49-201-002-A01, INSTALLED SEAT TRACK LBL9 FS677-830.40 IAW CRJ700 AMM 53-00-49-400-801-A03
RBL 9 SEAT TRACK IS CORRODED BETWEEN FS 581.00 AND 677.00. CORRECTIVE ACTION: FABRICATED NEW SEAT TRACK P/N SH670-33558-3 @ RBL 9 BETWEEN F.S 581 AND F.S 677 IAW CRJ 700 SRM 53-00-49-201-002-A01 INSTALLED SEAT TRACK RBL9 FS581-677 IAW CRJ700 AMM 53-00-49-400-801-A03
LBL 9 SEAT TRACK IS CORRODED BETWEEN FS 581.00 AND 677.00. CORRECTIVE ACTION: FABRICATED NEW SEAT TRACK P/N SH670-33425-3 @ LBL 9 BETWEEN F.S 584 AND F.S 677 IAW CRJ 700 SRM 53-00-49-201-002-A01. INSTALLED SEAT TRACK LBL9 FS581-677 IAW CRJ700 AMM 53-00-49-400-801-A03
AFT CARGO DOOR SILL IS CORRODED. CORRECTIVE ACTION: REMOVED DAMAGED AFT CARGO DOOR SILL AND INSTALLED A SERVICABLE AFT CARGO DOOR SILL IAW CRJ-700 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-15-001-001-A01 AND 51-42-21-001-001-A01.
AFT FUSELAGE PROTECTION PLATE AT FS 977.00 NOT IN PLACE. FUSELAGE GOUGED. 2 FASTNERS REQUIRE REMOVAL. CORRECTIVE ACTION: REPAIRED IAW BOMBARDIER REO 670-53-00-290 REV -F, DATED 2019/04/26, SOLUTION 2 (CRJ-700)
IB SPOILERON IB FLT SPOILER DEPLOYED ON T/O. TROUBLESHOT B1-007911 IAW CRJ 700 FIM 27-64-01-810-813. REMOVED AND REPLACED RH IB MFS PCU IAW CRJ 700 AMM 27-62-01-000/400-801-A01-PSA. LEAK CHECK GOOD, OPS CHECK GOOD.
IN CRUISE AT FL340, CREW RECEIVED AN EFIS COMP MON FAIL MESSAGE, FOLLOWED BY ADC1 FAIL AND FINALLY A STALL FAIL CAUTION MSG. PER QRH CREW DECLARE EMERGENCY AND DIVERTED TO MEM. INSPECTED MAIN PITOT / STAND BY PITOT DRAIN ASSY IAW CRJ 700 AMM 34-11-00-220-802/805-A01/A02. FOUND MOISTURE IN P3. REPLACED ADC 1 AND DRAINED PITOT STATIC DRAIN ASSEMBLIES IAW CRJ 700 AMM 34-13-01-000/400-801-A01-PSA AND CRJ 700 AMM 34-11-00-220-801 OPS CHECK GOOD. MODE C RETURN TO SERVICE CHECK REQUIRED. PERFORMED MODE C CHECK IAW CRJ 700 AMM 34-54-00-720-802-A01-PSA. OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME.
PASSING THROUGH FL170 ON DESCENT INTO PWM, THE CREW RECEIVED A PAX DOOR AMBER CAUTION MESSAGE. THE QRH WAS RAN, AND NOTHING APPEARED TO BE AFFECTING THE FLIGHT ADVERSELY. THE CAPTAIN INFORMED THE FA'S OF THE SITUATION, THEN DECLARED AN EMERGENCY WITH PWM APPROACH AS A PRECAUTION. PAX WERE NOT INFORMED TO BRACE. AT FL130, THE AMBER LIGHT WENT OUT, AND CABIN PRESSURIZATION CHECKED OK, SO THE CREW UNDECLARED THE EMERGENCY WITH ATC. THE FLIGHT LANDED SAFELY AT PWM. ON SITE MX IS INBOUND AT THE TIME OF REPORT TO ADD MEL'S. TROUBLESHOT THRU MDC FOUND SEVERAL ENTRIES FOR PAX DOOR SENSOR (PX25) OUT OF RIG B1CODE 007627. INSPECTED PX25 SENSOR FOUND TARGET BRACKET DEFORMED. REMOVED AND REPLACED TARGET AND BRACKET IAW CRJ 700 SRM 51-42-06/10-001-001-A01. PREFORMED OPS CHECK IAW CRJ 700 AMM 52-70-00-750-801-A01. OPS CHECK GOOD AT THIS TIME.
DURING CLIMB THE CREW RECIEVED A RIGHT WINDSHIELD HEAT CAUTION MESSAGE. SPARKS AND FLAMES OCCURRED AT WHICH TIME THE WINDSHIELD CRACKED AND THE DASH STARTED TO MELT. THE CA TURNED OFF THE WINDSHIELD HEAT AND THE FLAMES DISSAPATED. THEY DECLARED AN EMERGENCY AND RETURNED TO CAK WHERE THEY LANDED SAFELY AND TAXIED THE PASSENGERS TO THE GATE. R&R RH WINDSHIELD IAW CRJ 700 AMM 56-11-01-000/400-801. REMOVED AND REPLACED THE SEALANT AROUND THE WINDSHIELD STRAP IAW CRJ700 AMM 56-11-01-000/400-801
WHILE ENROUTE FROM DCA TO VPS, THE CAPTAIN'S SIDE WINDSHIELD SHATTERED. DISPATCHER AND CREW MADE THE DECISION TO DIVERT TO CLT. EMERGENCY WAS DECLARED. FLIGHT HAS LANDED SAFELY AND WILL SWAP TO A SPARE AIRPLANE WHEN A GATE IN CLT BECOMES AVAILABLE. R & R CA WINDSHIELDS, IAW CRJ 700 AMM 56-11-01-000/400-801-A01-PSA. OPERATIONS CHECK AND LEAK CHECK OK.
REMOVED AND REPLACED THE AFT FA FLASHLIGHT IAW CRJ 700 AMM 25-60-00-220-801-PSA. OPS CHECK GOOD AT THIS TIME THIS CLEARS MEL.
STRINGER 7L BETWEEN FS1144.00-FS1162.00 IS GOUGED DUE TO RAM AIR WATER SPRAYER BRACKET. REMOVED AND REPLACED STRINGER. P/N MM670-35119-049
ALL EMERGENCY LIGHTS GO OUT AFTER 3 SEC. R&R PCB05 IN JB1 IAW AMM 24-06-11-000/400-801. OPS CHECK GOOD. R&R PCB05 IN JB1 IAW AMM 24-06-11-000/400-801. OPS CHECK GOOD
LT SIDE SEAT RAILS LOCATED @ STR 15L FROM FS379 TO FS985 CORRODED. REMOVED AND REPLACED SEAT TRACKS.
SEAT TRACK AT LBL9 FROM FS 374 TO FS 485 IS CORRODED. REMOVED AND REPLACED SEAT TRACK.
SEAT TRACK AT LBL9 FROM FS 485 TO FS 581 IS CORRODED. REMOVED AND REPLACED SEAT TRACK.
FRAME AT FS 310.00 BETWEEN STRINGER 26L AND 26R IS CORRODED. PERFORMED REO 670-53-21-1281 REPAIR.
RT SIDE SEAT RAIL LOCATED @ STR 15R FROM FS379 TO FS973. REMOVED AND REPLACED SEAT TRACKS.
CREW REPORTED L PACK AUTO FAIL/SMOKE IN COCKPIT. MX INSPECTED AND DEFERRED THE LT PACK. MX REMOVED AND REPLACED LH ACM. OPS AND LEAK CHECKS GOOD.
CREW REPORTED AN INTERMITTENT BURNING ODOR IN THE GALLEY AREA ENROUTE. MX INSPECTED GALLEY LIGHT ASSEMBLIES AND COFFEEMAKER, PERFORMED AN OPS CHECK. NO DEFECTS NOTED. ALSO INSPECTED AVIONICS BAY WITH NO DEFECTS FOUND.
SEAT TRACK AT BS 693 - 977 CORRODED AT LBL 9. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND PERFORMED CHECKS IAW THE AMM.
RIGHT OUTBOARD FLOOR SUPPORT AT BS 319 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT AND PERFORMED CHECKS IAW THE AMM.
BS 280 CROSSBEAM CORRODED ON UPPER FLANGE BETWEEN RBL 14 AND LBL 11. MAINTENANCE REMOVED AND REPLACED F.S. 280 LEFT HAND CROSSBEAM, REMOVED LIGHT SURFACE CORROSION FROM TOP OF F.S. 280 RIGHT HAND CROSSBEAM AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT CONTINUES HEAVY MAINTENANCE CHECKS.
J ANGLE AT BS 280 BETWEEN LBL 12 AND RBL 12 IS CORRODED. MAINTENANCE REMOVED AND REPLACED THE J ANGLE AND PERFORMED CHECKS IAW THE AMM.
BS 280 LEFT SIDE BULKHEAD WEB IS CORRODED AT LBL 12. MAINTENANCE REPAIRED THE BULHEAD WEB AND PERFORMED CHECKS IAW THE AMM.
SEAT TRACK CORRODED AT BS 485 - 581 LBL9. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT CONTINUES HEAVY CHECK MAINTENANCE.
DURING CRUISE, THE LEFT ENGINE SHOWED ZERO OIL PRESSURE. THE CREW DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND CLEANED A CONNECTOR ON THE OIL PRESSURE TRANSMITTER; ALSO FOUND CIRCUIT BREAKER POPPED, RESET CIRCUIT BREAKER. TECHNICIANS PERFORMED ENGINE RUNS WITH CREW. LEFT HAND ENGINE OIL PRESSURE TRANSMITTER OPS CHECK GOOD. NO FURTHER DEFECT NOTED, AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED OTBD FLIGHT SPOILERS AND OTBD SPOILERONS CAUTION MESSAGES IN FLIGHT AND OBSERVED SPOILERS DID NOT DEPLOY. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED SPOST 2 SELF TEST IAW AMM. OPS CHECK WAS GOOD. ACFT RELEASED FOR SERVICE.
CREW REPORTED LT AND RT WING ANTI-ICE CAUTION MESSAGES IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R RT OTBD TELESCOPIC DUCT WIRING HARNESS AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
CREW REPORTED CABIN PRESSURE POPPING AND VERY UNCOMFORTABLE ON CLIMBOUT WITH APU OFF AND USING ENGINES AS BLEED SOURCE. LEFT PRESSURE REGULATING SHUTOFF VALVE CYCLING NONSTOP. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R LT ENGINE PRESSURE REGULATING SHUTOFF VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
DURING DEPLOYING FLIGHT SPOILERS FOR APPROACH, CREW REPORTED BOTH INBD FLIGHT SPOILERS AND INBD SPOILERONS AMBER MESSAGES DISPLAYED. CREW PERFORMED QRH, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. CREW PERFORMED SYSTEM RESET IAW MINIMUM EQUIPMENT LIST. PROBLEM DID NOT REOCCUR.
LEFT AND RIGHT VERTICAL STABILIZER LOWER FUSELAGE ATTACHMENT DRAG ANGLES AT 67.5 PERCENT REAR SPAR DATUM, ARE CRACKED. C/W REO 670-55-31-018, REV DATED 4/16/07.
SERVICE DOOR LOWER SILL IS CORRODED, FILIFORM, AROUND FORWARD FITTING. R & R SERVICE DOOR LOWER SILL ANGLE IAW SRM 51-42-06-001-001 AND 51-42-21-001-001-A01.
SERVICE DOOR LOWER SILL STRIKER FITTING IS CORRODED, FILIFORM, AROUND MULTIPLE FASTENER HOLES. R & R SERVICE DOOR LOWER SILL STIKER FITTING IAW SRM 51-42-06-001-001-A01.
LATCH PIN INTERCOSTAL AT STR 27R IS CORRODED, FILIFORM, AT FS 364. REPLACED INTERCOSTAL PN SH670-32075-4 AT FS 364, STR 27R, REAPPLIED CORROSION INHIBITING COMPOUND IAW SRM.
LATCH PIN INTERCOSTAL AT STR 27L IS CORRODED, FILIFORM, AT FS 364. REPLACED INTERCOSTAL PN SH670-32075-3 AT FS 364, STR 27L, REAPPLIED CORROSION INHIBITING COMPOUND IAW SRM.
FRAME SECTION BS 565 JUST ABOVE STRINGER 18L IS CORRODED. REPAIRED FRAME SECTOR IAW REO 670-53-31-339.
FRAME SECTION AT FS 549 JUST ABOVE STR 18L IS CORRODED. REPAIRED FRAME SECTOR IAW REO 670-53-31-339.
BS 280 CROSSBEAM IS CRACKED JUST OTBD OF LBL 9 AND RBL 9. PERFORMED A MAJOR REPAIR TO BS 280 CROSSBEAM LT AND RT SIDES IAW SRM 53-11-201-003-A01.
DURING REMOVAL OF RT BS 280 CROSSBEAM, FOUND CORROSION ON RT LOWER WEB. REPAIRED CORROSION AT FS280 LOWER WEB IAW REO670-53-11-594.
INTERCOSTAL BETWEEN BS 310 - 349 ON STRINGER 20 IS CORRODED. REPLACED INTERCOSTAL WITH A SERVICEABLE IAW SRM 51-42-21-001-A01.
CREW REPORTED LT WINDSHIELD HAD SPARKS AND MELTING GLOW. A LINE FORMED ON WINDSHIELD AND STOPPED WHEN WINDSHIELD HEAT TURNED OFF. CREW RETUNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R LT WINDSHIELD HEAT CONTROLLER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
CREW REPORTED LT WINDSHIELD HAD SPARKS AND MELTING GLOW. A LINE FORMED ON WINDSHIELD AND STOPPED WHEN WINDSHIELD HEAT TURNED OFF. CREW RETUNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R LT WINDSHIELD AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
CREW REPORTED EMERGENCY LIGHT STRIP MISSING IN ROW 12. INSTALLED LIGHT STRIP AT ROW 12 IAW AMM 33-51-01-400-801 PSA AND PERFORM CHECKED IAW AMM. ACFT RELEASE FOR SERVICE.
AFTER ENGINE START, AFTER PUSHBACK, CREW REPORTED RT PACK AUTOFAIL AMBER CAUTION MESSAGE FOLLOWED BY AND ODOR OF SMOKE AND BURNING PLASTIC. RETURNED TO GATE. MAINTENANCE TROUBLESHOT, AND R & R RT ACM AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
CREW REPORTED STRONG CHEMICAL ODOR IN CABIN ON DESCENT. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, FOUND PAPER, DEBRIS BENEATH COFFEEMAKER AND REMOVED DEBRIS. MAINTENANCE R & R COFFEEMAKER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
CREW REPORTED STRONG ELECTRICAL ODOR IN FLIGHT DECK. MX TROUBLESHOT, R & R RT DIRECT CURRENT POWER CENTER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
DURING SCHEDULED MX, STRINGER 3L BETWEEN BS 280-295 CRACKED. REPAIRED IAW AMM. ACFT RELEASED FOR SERVICE.
DURING SCHEDULED MX, BS 202.75, RBL 30 AND LBL 30 VERTICAL STIFFENER HAD AN INDICATED CRACK. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.
CREW REPORTED HYD 3 LOW PRESSURE CAUTION MESSAGE AND INBOARD GROUND SPOILERS CAUTION MESSAGE AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED SAFELY. AIRCRAFT TOWED FROM RUNWAY DUE TO INOPERABLE NOSE WHEEL STEERING AND PASSENGERS TAKEN BY BUS TO TERMINAL. MAINTENANCE INSPECTED AND FOUND LEFT AILERON NUMBER 3 PCU (POWER CONTROL UNIT) LEAKING. MAINTENANCE REMOVED AND REPLACED LEFT AILERON PCU FOR NUMBER 3 SYSTEM AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.
DURING SCHEDULED MAINTENANCE A DENT WAS FOUND ON RIGHT INBOARD FLAP SKIN. THE RIGHT INBOARD FLAP SKIN WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
AT CAK, FOUND EMERGENCY LIGHT ON LOWER AFT SIDE OF SERVICE DOOR ENTRANCE INOPERATIVE. MAINTENANCE TROUBLESHOT AND FOUND CONNECTOR BEHIND WARDROBE ASSEMBLY DISCONNECTED. MAINTENANCE RECONNECTED CONNECTOR AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED A STEERING INOP CAS MESSAGE ON GEAR RETRACTION ON DEPARTURE FROM MLB. CREW CONTINUED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, RESET STEERING SYSTEM AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
DURING SCHEDULED MAINTENANCE THE T-ANGLE AT FS 280.0 WAS FOUND CRACKED. REPAIRS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT RELEASED FOR SERVICE.
DURING SCHEDULED MAINTENANCE CORROSION WAS FOUND AT FS 280.0. REPAIRS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT RELEASED FOR SERVICE.
DURING SCHEDULED MAINTENANCE LIGHTNING DAMAGE WAS FOUND ON THE RIGHT INBOARD FLAP. REPAIRS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT RELEASED FOR SERVICE.
CREW REPORTED LIGHTNING STRIKE. MAINTENANCE PERFORMED EN ROUTE LIGHTNING STRIKE INSPECTION USING MM. DAMAGE FOUND. REMOVED AND REPLACED RIGHT WINGLET OUTBOARD TRAILING EDGE FAIRING, LEFT AFT HORIZONTAL STABILIZER TIP FAIRING, REAR ANTI-COLLISION LIGHT AND PRIMARY / SECONDARY NAV LIGHTS ON VERTICAL STABILIZER AND SEVERAL STATIC WICKS. MAINTENANCE PERFORMED STRUCTURAL REPAIR UNDER HORIZONTAL STABILIZER TIP PANEL, REPAIRED DAMAGED AREAS ON VERTICAL STABILIZER AND MADE REPAIRS FOR BURNT / DAMAGED SCREW HEADS AND COUNTERSINKS ON BOTH SIDES OF AFT FUSELAGE DORSAL FIN. CHECKS WERE PERFORMED AND AIRCRAFT RELEASED FOR SERVICE.
CREW REPORTED HYDRAULIC SYSTEM NR 3 LOW PRESSURE CAUTION MESSAGE WHILE ON APPROACH TO CLT. CREW LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE 3B HYDRAULIC PUMP OUTLET FITTING LEAKING. MAINTENANCE REMOVED AND REPLACED THE 3B HYDRAULIC PUMP OUTLET FITTING O-RING AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED A SLATS FAIL MESSAGE ON ARRIVAL INTO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE OUTBOARD ACTUATOR FOR THE RIGHT INBOARD (NR 1) SLAT AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED A SLATS FAIL AMBER CAS MESSAGE ON APPROACH INTO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, CHECKED CODES, CYCLED CIRCUIT BREAKER AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
AT CLT, CREW REPORTED A POSSIBLE LIGHTNING STRIKE ON THE NOSE CONE. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE RADOME, WEATHER RADAR ANTENNA AND BOTTOM VHF ANTENNA DUE TO BURN DAMAGE CAUSED BY LIGHTNING AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
AT CLT, CREW REPORTED AN EMERGENCY LIGHTS ON STATUS MESSAGE IN FLIGHT WHEN SWITCH WAS IN THE ARM POSITION. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED A RELAY AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED THAT RT HYDRAULIC QUANTITY INDICATION WENT TO ZERO. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM USING AIRCRAFT MAINTENANCE MANUALS. MAINTENANCE REMOVED AND REPLACED THE RT HYDRAULIC PUMP. SYSTEM WAS SERVICED AND CHECKED PER THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.
CREW REPORTED A NOSE WHEEL STEERING INOPERATIVE MESSAGE AFTER TAKEOFF FROM CLT. AIRCRAFT LANDED IN DAY WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED A NOSE WHEEL STEERING PRESSURE SWITCH AND A SOLENOID AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.
ON TAKEOFF FROM CLT, CREW REPORTED A SLATS FAIL MESSAGE ON FLAP RETRACTION. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. NO FAULTS WERE FOUND. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED HYD 2 LO PRESS MSG FOLLOWED BY RAPID LOSS OF SYSTEM 2 HYDRAULIC FLUID. AIRCRAFT DIVERTED TO ATL LANDING WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT USING AIRCRAFT MAINTENANCE MANUAL AND REMOVED AND REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP. CHECKS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED AFTER TAKEOFF FROM CLT THAT THE NOSE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NOSE GEAR AND FOUND THE NLG LOCK PIN INSTALLED. THE NLG LOCK PIN WAS REMOVED IAW THE AIRCRAFT MAINTENANCE MANUAL. NO FURTHER DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED LIGHTNING STRIKE IN CLT. MAINTENANCE FOUND AND REPAIRED BURNED RIVETS PER REO 670-53-00-045. NO OTHER DEFECTS WERE NOTED AFTER CHECKS BY AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED 'L ENG BLEED' CAUTION AFTER TAKEOFF FROM CLT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TESTED AND REMOVED AND REPLACED THE LT ENG PRSOV PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED A LT ENG BLEED CAUTION MESSAGE AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LT PRESSURE SHUT OFF VALVE AND THE LT BLEED TEMP SENSOR. MAINTENANCE REMOVED AND REPLACED THE LT BLEED TEMP SENSOR IN ACCORDANCE WITH THE ACFT MAINTENANCE MANUAL. ACFT WAS RELEASED FOR SERVICE. (S)
CREW REPORTED A LIGHTNING STRIKE. MAINTENANCE PERFORMED AN EN ROUTE AND A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE FOUND DAMAGE TO THE NR 2 VHF ANTENNA AND SEVERAL RIVETS. MAINTENANCE REPAIRED ALL DAMAGE IN ACCORDANCE WITH THE STRUCTURAL REPAIR MANUAL. ACFT WAS RELEASED FOR SERVICE. (S)
CREW REPORTED AN EXTERNAL POWER DOOR OPEN ON CLIMBOUT. CREW ELECTED TO RETURN TO MSY AND LAND WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE EXTERNAL POWER DOOR OPEN. MAINTENANCE CLOSED DOOR AND PERFORMED OPERATIONAL CHECKS IN ACCORDANCE WITH AMM 53-10-00-210-807-A01. NO DAMAGE NOTED AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED THE RIGHT HAND PACK CYCLED ON/OFF MULTIPLE TIMES AFTER TAKEOFF. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE RIGHT HAND PACK IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 21-51-00-710-801. NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED A SERVICE DOOR CAUTION MESSAGE ON CLIMBOUT. CREW FOLLOWED THE QRH AND RETURNED TO TLH WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE SENSOR CAP JAMMED. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY SWITCH CAP. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED A RIGHT HAND COWL ANTI ICE MESSAGE AFTER TAKEOFF. CREW RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE ANTI ICE VALVE. OPERATIONAL CHECKS WERE PERFORMED. THE AIRCRAFT WAS RELEASED FOR SERVICE.
THE CREW REPORTED AN I/B FLIGHT SPOILER AND I/B SPOILERONS AMBER CAS MESSAGE IN FLIGHT. MAINTENANCE PERFORMED A SPOST TEST OF THE SPOILER SYSTEM. NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.
DURING WALKAROUND INSPECTION THE CREW DISCOVERED A DENT IN THE LT FORWARD FUSELAGE AFT OF THE RADOME. MAINTENANCE FOUND THE DENT -ACCEPTABLE AS IS- AFTER INSPECTION IAW BOMBARDIER REO 670-53-11-141. THE AIRCRAFT WAS RELEASED FOR SERVICE.
DURING APPROACH THE CREW REPORTED A LIGHTNING STRIKE TO THE FUSELAGE NOSE SECTION AND THE RADAR FAILED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED EN ROUTE & DETAILED LIGHTNING STRIKE INSPECTIONS. DAMAGE WAS FOUND ON THE RADOME, LT HORIZ STAB TIP FAIRING, RT NLG DOOR, AND TWO ANTENNAS. ALL DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.
DURING TAKEOFF THE LEFT EMERGENCY DOOR CAUTION MESSAGE ILLUMINATED. THE CREW ABORTED THE TAKEOFF. MAINTENANCE VERIFIED THE DOOR WAS SECURED AND DEFERRED THE INDICATION SYSTEM PER MEL 52-70-03 CODE C. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. AFTER TROUBLESHOOTING THE LEVER ASSEMBLY WAS FOUND WORN MAKING POOR CONTACT WITH THE PROXY SENSOR. PART IS ON ORDER.
THE CREW REPORTED A LIGHTNING STRIKE TO THE RADOME. MAINTENANCE COMPLIED WITH EN ROUTE & DETAILED LIGHTNING STRIKE INSPECTIONS IAW CRJ700 AMM 05-51-07-210-801-A01 & AMM 05-51-07-220-801-A01. MINOR BURN DAMAGE TO BOTH WINGLET TIPS WAS REPAIRED IAW BOMBARDIER REO 690-57-31-002. NO OTHER DEFECTS WERE FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.
EN ROUTE (CLT TO GSO) A FLIGHT ATTENDANT NOTICED A NOISE COMING FROM THE RIGHT SIDE OF THE AIRCRAFT AT THE WING AREA. THE CREW WAS NOTIFIED. THE CREW OF FLIGHT 2249 HAD NO INDICATION OF MALFUNCTIONS AND CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. THE CREW INSPECTED THE AIRCRAFT AND REPORTED THAT THE REFUEL PANEL WAS LEFT OPEN BY THE FUELER. THE FUEL CAP WAS NOT SECURED AND CAUSED DAMAGE TO THE AREA UNDER THE REFUEL ACCESS DOOR. CONTRACT MAINTENANCE INSPECTED AND PERFORMED A TEMPORARY REPAIR TO THE WING TO FUSELAGE FAIRING IAW BOMBARDIER REO 670-53-82-028. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.