N509AE
Registered owner: AMERICAN AIRLINES INC, TX (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
CROSSFLOW PUMP CAUTION MESSAGE WITH AUTO CROSSFLOW INHIB STATUS IN FLT. PERFORMED GRAVITY CROSS QRH PROCEDURE FUEL BALANCED OUT. TURN GRAVITY CROSS FLOW SOV OFF FUEL INBALANCE CAME RT BACK IMMEDIATELY, INSTALLATION OF THE CARTRIDGE, CROSS FLOW PUMP HAS BEEN COMPLETED IAW AMM 28-13-47-400-801-A01. OPS TEST OF THE FUEL/DEFUEL PANEL WAS COMPLETED IAW AMM 28-25-00-710-801-A01 STEPS 4(A)(7) THROUGH 4(A)(24). OPS TEST GOOD. MAGNETIC LEVEL INDICATOR CHECK HAS BEEN COMPLETED IAW AMM 12-11-28-750-802-A01. OPS CHECK GOOD. CAPACITANCE CHECK OF THE FUEL QUANTITY PROBES IS COMPLETED IAW AMM 28-41-09-720-801-750-802-A02. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.
INBOARD FLT SPOILER AND SPOILERON CAUTION INFLIGHT. / REMOVED AND REPLACED THE INBOARD MFS PCU IAW CRJ 700 AMM 27-62-01-000/400-801. LEAKAGE TEST AND OPERATIONAL TEST GOOD AT THIS TIME.
RIGHT PACK TEMP CAUTION MSG IN FLIGHT. REMOVED AND REPLACED ACSC 2 PER AMM 21-61-04-000/400-801-A01.PERFORMED RT PACK TEMP CONTROL SYSTEM OPS TEST PER AMM 21-60-00-710-801. NO FAULTS FOUND.
STRONG SMELL OF KEROSENE IN FLIGHT AROUND ROWS 16-18. NO OTHERS SMELLS NOTED NO SMOKE NOTED. TROUBLESHOT SMELL OF KEROSENE? IN CABIN IAW FIM 21-22-00-810-806-A01. AFTER MULTIPLE ENGINE RUNS COULD NOT MANAGE TO DUPLICATE THE SMELL. DID NOT FIND ANY LEAKS OR FAULTS THAT WOULD CAUSE A SMELL TO EMANATE THROUGHOUT THE CABIN. AIRCRAFT IS OKAY FOR SERVICE.
LT PACK TEMP CAUTION AT 26,000 CLIMBING. RAN QRH AT 30,000. RT PACK TEMP CAUTION. BEGAN DESCENT AND RAN QRH. CABIN ALT CAUTION THEN WARNING. RAN QRC/QRH. CABIN O2 MASKS DEPLOYED IN FLIGHT. / REMOVED AND REPLACED LEFT ACSC IAW CRJ700 AMM 21-61-04-000/400-801-A01. OP CHECK GOOD. REMOVED AND REPLACED AIR CONDITIONING CONTROL PANEL IAW AMM 21-61-02-000/400-801-A02. OPS CHECKS GOOD.
LEFT PACK TEMP AN RT PACT TEMP CAUTION IN FLIGHT. UNPRESSURIZED CHECKLIST RTF. PERFORMED OPS CHECK OF TEMP CONTROL PANEL IN MANUAL MODE IAW AMM 21-61-02. OPS CHECKED GOOD. NO DEFECTS NOTED AT THIS TIME.
HN00200835 SN: 00369 DISCREPANCY: FS824.5 CL WING TO BODY FAIRING ANCHOR POINT IN THE CENTER OF THE MLG WHEEL WELL AREA FWD R/H NUTPLATE CLIP IS BROKEN AND 3 EACH REMAINING CLIPS ARE FRETTED AND CORRODED REQUIRING BLEND AND EVALUATION. CORRECTIVE ACTION: REMOVED INCORRECT SUPPORT ANGLES AND INSTALLED CORRECT ANGLES (2 EACH PN: SH670-39183-5 ANGLE ASSY, 1 EACH PN: SH670-39188-5 SUPPORT ASSY, AND 1 EACH PN: SH670-39188-3 ANGLE) IN THE CORRECT ORIENTATION ONTO WING TO BODY FAIRING ANCHOR POINT CENTER MLG WHEEL WELL AT FS824.5 IAW CRJ-700 SRM 51-42-06-001-001-A01.
HN00200808 DISCREPANCY: FS909 LBL16 TO RBL16 WING TO BODY SUPPORT STRUCTURE FAYING SURFACE STRAP BOTTOM SURFACE IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED NEW MIDSTRAP PN SH670-39338-1 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-45-00-001-001-A01
HN00200429 DISCREPANCY: FS553-558 R/H SIDE SEAT RAIL IS CORRODED. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW SERVICEABLE R/H SIDE SEAT RAIL (ALTERNATE PN- SH670-32234-3) IAW CRJ700 AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03
HN00198477 DISCREPANCY: PAX DOOR FWD FORMER IS CORRODED.. CORRECTIVE ACTION: LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR FWD FORMER FS311.75 P/N#601R31803-5 IAW CRJ-700 SRM TASK 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR FWD FORMER, FS311.75 IAW CRJ-700 SRM TASK 51-42-06-001-001-A01, AND TASK 51-42-21-001-001-A01.
HN00200937 DISCREPANCY: AFT BAGGAGE BAY DOOR AFT CROTCH FITTING IS CHAFED. CORRECTIVE ACTION: REPAIRED IAW REO 670-53-61-2420 REV-- DATED 2024-11-24. REFERENCE RFTS-117959 FOR TRACKING
HN00200936 DISCREPANCY: AFT BAGAGE BAY DOOR FWD CROTCH FITTING IS CHAFED. CORRECTIVE ACTION: REPAIRED IAW REO 670-53-61-2420 REV-- DATED 2024-11-24. REFERENCE RFTS-117959 FOR TRACKING
HN00200871 DISCREPANCY: AFT FAIRING 195BB ATTACHMENT STRUCTURE IS CORRODED AROUND MULTIPLE FASTENER HOLES. CORRECTIVE ACTION: REMOVED CORROSION ON 3 STRAPS BETWEEN F.S. 879 TO F.S. 909 AND FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 53-82-55-101-002-A01. REMOVED CORROSION ON ONE STRAP BETWEEN F.S. 879 TO F.S. 879 TO F.S. 909 AND FOUND TO BE OUT OF LIMITS IAW CRJ 700 SRM 53-82-55-101-002-A01. REMOVED UNSERVICEABLE STRAP AND INSTALLED SERVICEABLE STRAP P/N SH670-39344-3IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-10-001-001-A01
HN00200856 DISCREPANCY: MLG FAIRING 194AB FWD ATTACHMENT STRUCTURE IS CORRODED IN MULTIPLE AREAS AROUND FASTENER HOLES. CORRECTIVE ACTION: INSTALLED NEW SERVICEABLE RECEPTACLES (PN- CA1810C) IAW CRJ700 SRM 51-42-06-001-001-A01 AND INSTALLED NEW SERVICEABLE DOOR LANDING (PN- CC670-39151-3) ON MLG FAIRING 194AB IAW CRJ700 SRM 51-42-13-001-001-A01
HN00200849 DISCREPANCY: LBL45 WL 38 FS821 TO FS847 ON APRON SUPPORT STRUCTURE IS CORRODED AROUND 5 EA. NUT PLATE HOLES CORRECTIVE ACTION: REPAIRED CORRODED AREAS IAW MHIRJ REO 670-53-42-111 REV. -- DATED 2024-11-30.
HN00210032 SN: 00829 DISCREPANCY: CORROSION INDICATIONS ON FORWARD TRUNNION BODY RH WS24 FAILED NDT. . CORRECTIVE ACTION: LOCATED AND MACHINED 3EA HOLES ON RH FLAP VANE ACTUATOR ROD AT FLS 24.00 IAW CRJ 700 SRM 51-40-11-001-001-A01 REFERENCING DWG CC670-14303 FOR SIZES AND DIMENSIONS. FLAP VANE FORWARD TRUNNION BODY AT RH WS24.00 WAS REPLACED WITH FLAP VANE ACTUATOR ASSY PN CC670-14300-9-01 SN PR1942 REFER TO HR00493751 FOR INSTALL
HN00210031 SN: 00828 DISCREPANCY: CORROSION INDICATIONS ON FORWARD TRUNNION BODY LH WS140.4 FAILED NDT. CORRECTIVE ACTION: FABRICATED FWD TRUNNION BODY ON LH 140.4 (PN-CC670-14305-1) REFER TO HN00210363 FOR WORK PERFORMED. IAW MHIRJ SNIEO 601R14261-S19.
CORROSION INDICATIONS ON CRADLE ASSY LH WS102.9 FAILED NDT CORRECTIVE ACTION: BLENDED OUT CORROSION IAW EA AI-670-57-00093 REV -- DATED 1/5/2025 STEPS 1-4 HFEC PERFORMED ON REWORKED AREAS IAW PSA EA NO: A1-670-57-00093 REV - DATED 2025-01-05 STEP 5 NO INDICATIONS NOTED AT THIS TIME. REFER TO HN00205129 FOR THE REPLACEMENT OF LH FLAP VANE ACTUATOR ASSEMBLY AT WS102.9.
PAX DOOR FWD AND AFT ON FRAME FS320 (2EA) CLIPS AT HINGE FOUND TO BE CORRODED REQUIRE REPLACEMENT. REMOVED AND REPLACED NEW SERVICEABLE PAX DOOR FWD AND AFT CLIPS (2EA) AT HING P/N #601R319034-1,P/N#601R319043-2 IAW CRJ-700 SRM TASK 51-42-06-001-001-A01 AND TASK 51-40-11-001-001-A01
FURTHER INVESTIGATION FINDS CORROSION ON EXISTING REPAIR IN THE FS295.00 FRAME BETWEEN FRAME AND SKIN BETWEEN RH STGR 26-22 CORRECTIVE ACTION: REMOVED EXISTING REPAIR IN THE FS295.00 FROM STGR L26-R23 IAW CRJ700 SRM 51-42-21-001-001-A01 & 51-23-00-001-001-A01. LOCATED AND DRILLED NEW FS 295.00 FRAME PN# SH670-31353-1 BETWEEN STR 25L TO STRINGER 23R IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED NEW FS 295 FRAME BETWEEN STRINGER 25L TO STRINGER 23R IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
HN00205126 SN: 00703 DISCREPANCY: LH IB FLAP VANE ACTUATOR AT FLS65.50 UPPER TRUNNION HAS CORROSION CORRECTIVE ACTION: LOCATED AND MACHINED 3EA HOLES IN LH IB FLAP VANE ACTUATOR ROD AT FLS 65.50 IAW CRJ 700 SRM 51-40-11-001-001-A01 REFERENCING DWG CC670-14303 FOR SIZES AND DIMENSIONS. REFER TO HR00493692 FOR REPLACEMENT OF THE LH IB FLAP VANE ACTUATOR AT FLS65.50 (PN-CC670-14300-9-01 SN-PR1939
HN00204267 SN: 00670 DISCREPANCY: FOUND R/H SLAT TRACK 3-1 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS CORRECTIVE ACTION: REPAIRED RIGHT SLAT TRACK 3-1 IAW MHIRJ REO 670-57-42-1887 REV -- DATED 2024-12-16
HN00204265 DISCREPANCY:FOUND L/H SLAT TRACK 3-1 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION:BLENDED DAMAGED AREAS ON L/H SLAT TRACK 3-1 IAW CRJ700 SRM 51-12-00-001-001-A01. COMPLIED WITH MHI RJ REO 670-57-42-1886 REV -- DATED 2024-12-16
HN00204264 SN: 00668 DISCREPANCY: FOUND R/H SLAT TRACK 2-2 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS CORRECTIVE ACTION: REPAIRED RIGHT SLAT TRACK 2-2 IAW MHIRJ REO 670-57-42-1891 REV -- DATED 2025-02-21
HN00204261 DISCREPANCY:FOUND L/H SLAT TRACK 3-2 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS CORRECTIVE ACTION: REPAIRED DAMAGE BY BLENDING WEAR ON SLAT TRACK 3-2 IAW ENGINEERING REO 670-57-42-1889 REV -- (P1) DATED 2024-12-10.
HN00204260 SN: 00664 DISCREPANCY: FOUND R/H SLAT TRACK 2-1 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS CORRECTIVE ACTION: REPAIRED RIGHT SLAT TRACK 2-1 IAW MHIRJ REO 670-57-42-1883 REV -- DATED 2025-12-09
HN00204258 SN: 00662 DISCREPANCY: FOUND R/H SLAT TRACK 1-3 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS CORRECTIVE ACTION: REPAIRED RIGHT SLAT TRACK 1-3 IAW MHIRJ REO 670-57-42-1888 REV -- DATED 2025-02-19
HN00204547 SN: 00683DISCREPANCY:WHILE REPLACING THE LH AILERON FLUTTER DAMPER LINK SHEAR PIN FOUND THE LINK TO BE INTERNALLY CORRODED, AND, FROZEN. REQUIRES REPLACEMENTCORRECTIVE ACTION: FWD HALF OF NEW SERVICEABLE LINK PART NO.600-10177-7 AND AFT HALF PART NO.600-10178-5 HAVE BEEN ATTACHED USING SHEAR PIN PART NO. 601R10179-1 IAW CRJ700 AMM 27-15-05-400-804-A01. INSTALLED LH AILERON FLUTTER DAMPER LINK IAW CRJ700 AMM 27-15-05-400-802-A01
HN00204271 DISCREPANCY:FOUND R/H SLAT TRACK 3-3 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION:REPAIRED IAW MHIRJ REO 670-57-42-1885 REV -- DATED 2024-12-09.
HN00204268 DISCREPANCY:FOUND L/H SLAT TRACK 2-3 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: COMPLIED WITH MHIRJ.REO 670-57-42-1894 REV.-- DATED 2025-02-28.
HN00204257 DISCREPANCY:FOUND L/H SLAT TRACK 1-3 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: BLENDED DAMAGED AREAS ON L/H SLAT TRACK 1-3 IAW CRJ700 SRM 51-12-00-001-001-A01. COMPLIED WITH MHI RJ REO 670-57-42-1878 REV -- DATED 2024-12-05
HN:00204256 DISCREPANCY:FOUND R/H SLAT TRACK 1-1 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: BLENDED DAMAGED AREAS ON R/H SLAT TRACK 1-1 IAW CRJ700 SRM 51-12-00-001-001-A01. COMPLIED WITH MHI RJ REO 670-57-42-1879 REV -- (P1) DATED 2024-12-05.
HN00201660 SN: 00439 DISCREPANCY: RH SIDE SEAT RAIL BETWEEN FS863 TO FS969 IS CORRODED. CORRECTIVE ACTION: REPLACED SIDE SEAT RAIL BETWEEN FS863 TO FS969 PN SH670-37543-3 IAW CRJ 700 AMM 53-00-49-400-801-A03
HN00204255 DISCREPANCY:FOUND L/H SLAT TRACK 1-1 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: BLENDED DAMAGED AREAS ON L/H SLAT TRACK 1-1 IAW CRJ700 SRM 51-12-00-001-001-A01. COMPLIED WITH MHIRJ REO 670-57-42-1881 REV --(P1) DATED 2024-12-05
HN00214387 SN: 00876 DISCREPANCY: FLOOR SEAT TRACK LOCATED AT F.S.985-F.S.1000 RBL 9 FOUND TO BE CORRODED. CORRECTIVE ACTION: REMOVED FLOOR SEAT TRACK LOCATED AT F.S.985-F.S.1000 RBL 9 IAW CRJ 700 AMM 53-00-49-000-802-A06. INSTALLED NEW SERVICEABLE SEAT TRACK PN: BA670-45073-3 AT F.S.985 - F.S.1000 ON RBL 9 IAW CRJ-700 SRM 51-21-11-001-001-A01, 51-23-00-001-001-A01 AND 51-41-04-001-001-A01
HN00204263 DISCREPANCY:FOUND L/H SLAT TRACK 2-2 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: BLENDED DAMAGED AREAS ON L/H SLAT TRACK 2-2 IAW CRJ700 SRM 51-12-00-001-001-A01 COMPLIED WITH MHI RJ REO 670-57-42-1892 REV -- (P1) DATED 2024-12-17.
HN00200426 DISCREPANCY: FS555 L/H SIDE SEAT RAIL IS CORRODED CORRECTIVE ACTION: REMOVED LH SIDE SEAT RAIL P/N (SH670-32234-951) BETWEEN LH FS483.00-FS573.00CRJ700 AMM 53-00-49-000-801-A03. FABRICATED LH SEAT RAIL AT FS 555 IAW CRJ700 SRM 53-00-49-201-002-A01. INSTALLED NEW SERVICEABLE SEAT TRACK ON LH SIDE AT FS 555 IAW CRJ700 AMM 53-00-49-400-801-A03
HN00199778 DISCREPANCY: RH WING PANEL 698AT HAS AN ELONGATED SCREW HOLE. CORRECTIVE ACTION:COMPLIED WITH EA NO: A1-670-57-00075 REV.-- DATED 2024-11-24 REPAIR
HN00199472 DISCREPANCY: PANEL 326CT HAS DISBONDED LIGHTNING DIVERTER PLATE WITH POSSIBLE CORROSION NEEDS FURTHER EVALUATION. CORRECTIVE ACTION: FABRICATED SERVICEABLE REPLACEMENT BONDING PLATE PN: 670-55-32-025-1 IAW STEPS 1-4 OF BOMBARDIER REO 670-55-32-025, REV-A, DATED 2010-07-08. FABRICATION MATERIAL IS 202-T3, .032, PO: 5-5501. BONDED NEW SERVICEABLE BONDING PLATE (PN- 670-55-32-025-1) TO PANEL 326CT IAW STEP 5 OF BOMBARDIER REO 670-55-32-025, REV-A, DATED 2010-07-08. RESTORED FINISH OF WORKED AREA IAW BOMBARDIER REO 670-55-32-025 AND CRJ700 SRM 51-25-00-001-001-A01
HN00198891 SN: 00194 DISCREPANCY:DURING REMOVAL OF RH ENGINE BY PSA ENGINE REMOVAL TEAM BACKED LIFT INTO RIGHT SIDE OF FUSELAGE JUST AFT OF PYLON TRAILING EDGE AND TWO FOOT BELOW PYLON TRAILING EDGE. THE SKIN IS PUNCTURED. CORRECTIVE ACTION: REPAIRED PUNCTURED SKIN IAW MHIRJ REO 670-53-61-2404. REV.-- DATED 2024-12-23.
HN00198732 SN: 00166 DISCREPANCY: EXTERNAL FRAME IS DENTED @FS 280 BETWEEN 23R AND 24R CORRECTIVE ACTION: REPAIRED EXTERNAL FRAME AT FS 280 BETWEEN 23R AND 24R IAW REO 670-53-21-2514 REV -- DATED 2025-01-10
HN00212773 DISCREPANCY: AFT INTERCOSTAL OF AFT CARGO DOOR SILL HAS MINOR CORROSION. CORRECTIVE ACTION: REMOVED TIE DOWN ASSEMBLY PLATE FROM INTERCOSTAL IAW CRJ700 SRM 51-42-06-001-001-A01. INSTALLED NEW TIE DOWN ASSEMBLY PLATE PN# MM670-35329-011 IAW CRJ700 SRM 51-42-06-001-001-A01
HN00200904 DISCREPANCY: FWD WING TO BODY, PLATE, SPLICE JOINT LOCATED AT FS. 629 HAS MULTIPLE AREAS OF CORROSION FROM LBL28 TO RBL28. CORRECTIVE ACTION: .REMOVED CORRODED SPLICE JOINT. LOCATED AND INSTALLED A NEW SPLICE JOINT IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-15-001-001-A01.
HN00199235 DISCREPANCY: R/H WING TIRE BURST ACCESS PANEL 642BZ IS CORRODED. CORRECTIVE ACTION: LOCATED AND DRILLED NEW SERVICEABLE PART PN (CC670-10339-2) IAW CRJ 700 SRM 51-40-11-001-001-A01. REFERENCE BARCODE HR00493825 FOR INSTALL.
HN00202818 DISCREPANCY: PAX DOOR FWD INTERCOSTAL DD7A FOUND TO BE CORRODED. REQUIRES REPLACEMENT CORRECTIVE ACTION: LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR INTERCOSTAL DD7 MID P/N 601R318083-1 IAW CRJ-700 SRM TASK 51-40-11-001-001-A01 INSTALLED NEW SERVICEABLE PAX DOOR INTERCOSTAL DD7A MID IAW CRJ-700 SRM TASK 51-42-06-001-001-A01.
HN00202814 DISCREPANCY: PAX DOOR AFT FORMER FOUND TO BE CORRODED. REQUIRES REPLACEMENT CORRECTIVE ACTION: REMOVED PAX DOOR AFT FORMER IAW CRJ-700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.LOCATED AND DRILLED NEW PAX DOOR AFT FORMER (PART# 601R318034-5S) IAW CRJ-700-SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR AFT FORMER IAW CRJ-700 SRM TASK 51-42-06-001-001-A01 AND TASK 51-42-21-001-001-A01.
HN00204262 SN: 666 DISCREPANCY: FOUND R/H SLAT TRACK 3-2 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: REPAIRED R/H SLAT TRACK 3-2 WEAR DAMAGE IAW MHIRJ REO 670-57-42-1890 REV -- DATED 2025-02-21.
HN00198229 DISCREPANCY: FUSELAGE EXTERNAL SKIN IS DENTED BETWEEN F.S. 1015 TO F.S. 1031 STGR 26R TO STGR 25R. CORRECTIVE ACTION: REPAIRED THE EXTERNAL SKIN OF THE FUSELAGE BETWEEN FS1015 AND FS1031, STGR 25R TO STGR 26R IAW REO 670-51-00-085 REV: A DATED: 2017-08-23 AND IAW REO 670-53-61-2435 REV: -- DATED: 2024-12-16.
HN00205392 SN: 00600 DISCREPANCY: F.S. 333 FRAME IS CRACKED BETWEEN STGR 0 TO STGR 1R. CORRECTIVE ACTION: REPAIRED FRAME AT F.S.333 STRINGER 0 AND 2R IAW MHIRJ REO 670-53-21-2533 REV-- DATED 2025-01-20
BARCODE HN00204263 SN: 667 DISCREPANCY: FOUND L/H SLAT TRACK 2-2 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: REPAIRED R/H SLAT TRACK 2-2 WEAR DAMAGE MHIRJ REO 670-57-42-1892 REV-- DATED 2024-12-17. REPAIR IS ACCEPTABLE FOR 8000 FH FROM THE TIME OF INCORPORATION OF MHIRJ REO 670-57-42-1892 REV -- DATED 2024-12-17 OR UNTIL NEXT "C" CHECK. VISUALLY INSPECT SUBJECT SLAT TRACK AND ROLLERS FOR ANY DAMAGE AT INTERVALS NOT TO EXCEED 4000 FLIGHT HOURS PER REFERENCE AMM 27-81-00-220-805. NEXT INSPECTION DUE IN 4000 FH
HN00204261 SN: 665 DISCREPANCY: FOUND L/H SLAT TRACK 3-2 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: REPAIRED R/H SLAT TRACK 2-2 WEAR DAMAGE MHIRJ REO 670-57-42-1889 REV-- DATED 2025-02-28. REPAIR IS ACCEPTABLE FOR 8000 FH FROM THE TIME OF INCORPORATION OF MHIRJ REO 670-57-42-1892 REV -- DATED 2024-12-17 OR UNTIL NEXT "C" CHECK. VISUALLY INSPECT SUBJECT SLAT TRACK AND ROLLERS FOR ANY DAMAGE AT INTERVALS NOT TO EXCEED 4000 FLIGHT HOURS PER REFERENCE AMM 27-81-00-220-805. NEXT INSPECTION DUE IN 4000 FH
HN00203669 SN: 00600 DISCREPANCY: FWD BAGGAGE BAY CARGO NET RING ATTACHMENT BRACKET LBL 2.6 FS533 IS CORRODED IN MULTIPLE AREAS. SEE SRM 53-32-58-001-001-A01 ITEM 86 FOR REFERENCE. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW BRACKET P/N SH670-33389-1 IAW CRJ700 SRM 51-42-21-001-001-A01
HN00201645 SN: 00432 DISCREPANCY: LH SIDE SEAT RAIL BETWEEN FS781.15 TO FS863 IS CORRODED. CORRECTIVE ACTION: INSTALLED NEW LH SIDE SEAT RAIL FS 781.15 TO FS863 P/N SH670-36260-5 IAW CRJ-700 AMM 53-00-49-400-801-A03
HN00201654 SN: 00431 DISCREPANCY: LH SIDE SEAT RAIL BETWEEN FS710 TO FS761.85 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED L/H SIDE SEAT RAIL BETWEEN FS710-FS761.85 IAW CRJ-700 AMM 53-00-49-000-801-A03
HN00201643 SN: 00430 DISCREPANCY: LH SIDE SEAT RAIL BETWEEN FS667 TO FS710 IS CORRODED. CORRECTIVE ACTION: REMOVED, FABRICATED AND INSTALLED LH SIDE SEAT RAIL BETWEEN FS677 TO FS710 IAW CRJ700 AMM 53-00-49-400-801 (CONFIG A03)
HN00201642 SN: 00429 DISCREPANCY: LH SIDE SEAT RAIL BETWEEN FS570 TO FS667 IS CORRODED. CORRECTIVE ACTION: REMOVED DAMAGED SEAT RAIL PN (SH670-33558-3) IAW CRJ 700 AMM 53-00-49-000-801 (CONFIG A03) INSTALLED NEW SERVICEABLE SEAT RAIL PN (SH670-33558-3) IAW CRJ 700 AMM 53-00-49-400-801 (CONFIG A03)
HN00201640 SN: 00428 DISCREPANCY: LH SIDE SEAT RAIL BETWEEN FS379 TO FS485 IS CORRODED. CORRECTIVE ACTION: REMOVED L/H SIDE SEAT RAIL FS379-485 IAW CRJ700 AMM 53-00-49-000-801-A03 INSTALLED L/H SIDE SEAT RAIL FS379-485 IAW CRJ700 AMM 53-00-49-400-801-A03
HN00201298 SN: 00405 DISCREPANCY: SEAT TRACK LBL9 BETWEEN FS836 AND FS985 IS CORRODED IN MULTIPLE LOCATIONS CORRECTIVE ACTION: FABRICATED NEW SEAT TRACK P/N SH670-37420-5 LBL9 FS836-985 IAW CRJ700 SRM 53-00-49-201-002-A01. INSTALLED NEW SEAT TRACK [P/N SH670-37420-5] LBL 9 [FS 836-985] IAW CRJ 700 AMM 53-00-49-400-801-A03.
HN00201296 DISCREPANCY: SEAT TRACK LBL9 BETWEEN FS678 AND FS835 IS CORRODED/GOUGED IN MULTIPLE LOCATIONS CORRECTIVE ACTION: INSTALLED NEW SEAT TRACK P/N SH670-35864-3 LBL9 FS678-FS835 IAW CRJ700 AMM 53-00-49-400- 801-A03.
HN00201295 DISCREPANCY: SEAT TRACK LBL9 BETWEEN FS582 AND FS677 IS CORRODED/GOUGED IN MULTIPLE LOCATIONS. CORRECTIVE ACTION: EVALUATED CORRODED LBL9 SEAT TRACK SEGMENT BETWEEN FS 582 AND FS 677 AND FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW CRJ-700 SRM 53-31-49-101-001-A01. REMOVED DAMAGED SEAT TRACK IAW CRJ 700 AMM 53-00-49-000-801 (CONFIG A03). INSTALLED NEW SERVICEABLE SEAT TRACK PN (SH670-33425-3) IAW CRJ 700 AMM 53-00-49-400-801 (CONFIG A03).
HN00201291 DISCREPANCY: SEAT TRACK LBL9 BETWEEN FS364 AND FS485 IS CORRODED/GOUGED IN MULTIPLE LOCATIONS CORRECTIVE ACTION: EVALUATED CORRODED/GOUGED SEAT TRACK SEGMENT BETWEEN FS 364 AND FS 485 AND FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW CRJ-700 SRM 53-21-49-101-001-A01. NEW SERVICEABLE PART (LBL9 SEAT TRACK P/N (SH670-32249-3) WAS R&R IAW CRJ700 AMM 53-00-49-000-801(CONFIG A03), CRJ700 AMM 53-00-49-400-801(CONFIG A03), CRJ700 SRM 51-26-00-001-001-A01, CRJ700 SRM 51-23-00-001-001-A01, CRJ700 SRM 51-41-02-001-001-A01, AND CRJ700 SRM 51-41-04-01-001-A01.
HN00201137 DISCREPANCY: SEAT TRACK RBL9 BETWEEN FS830 AND FS985 IS CORRODED IN MULTIPLE LOCATIONS. CORRECTIVE ACTION: REMOVED SEAT TRACK P/N SH670-37411-3 RBL9 FS830-FS955 IAW CRJ700 AMM 53-00-49-000- 801-A03. INSTALLED NEW SEAT TRACK P/N SH670-37411-3 RBL9 FS830-FS955 IAW CRJ700 AMM 53-00-49-400- 801-A03
HN00201136 DISCREPANCY: SEAT TRACK RBL9 BETWEEN FS677 AND FS830 IS CORRODED IN MULTIPLE LOCATIONS. CORRECTIVE ACTION: INSTALLED NEW SEAT TRACK P/N SH670-35864-3 @ RBL9 FS677-830 IAW CRJ700 AMM 53-00-49-400- 801-A03
HN00201129 DISCREPANCY: SEAT TRACK RBL9 BETWEEN FS581 AND FS677 IS CORRODED IN MULTIPLE LOCATIONS. CORRECTIVE ACTION: SEAT TRACK P/N (SH670-33425-3) WAS BLENDED TO REMOVE CORROSION IAW CRJ700 SRM 51-12-00-001-001-A01, REMAINING THICKNESS IS OUT OF LIMITS IAW CRJ700 SRM 53-31-49-101-001-A01. SEAT TRACK P/N (SH670-33425-3) WAS BLENDED TO REMOVE CORROSION IAW CRJ700 SRM 51-12-00-001-001-A01, REMAINING THICKNESS IS OUT OF LIMITS IAW CRJ700 SRM 53-31-49-101-001-A01.REMOVED UNSERVICEABLE SEAT AT RBL9 BETWEEN F.S. 581 TO F.S. 677. INSTALLED A SERVICEABLE SEAT TRACK AT RBL9 BETWEEN F.S. 581 TO F.S. 677 IWA CRJ 700 SRM 51-26-00-001-001-A01, 51-23-00-001-001-A01, AND SRM 51-41-02-001-001-A01, AND 51-41-04-01-001-A01.
HN00204269 SN: 672 DISCREPANCY: FOUND R/H SLAT TRACK 2-3 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: REPAIRED R/H SLAT TRACK 2-3 WEAR DAMAGE MHIRJ REO 670-57-42-1895 REV-- DATED 2025-02-19. REPAIR IS ACCEPTABLE FOR 8000 FH FROM THE TIME OF INCORPORATION OF MHIRJ REO 670-57-42-1895 REV-- DATED 2025-02-19 OR UNTIL NEXT "C" CHECK. VISUALLY INSPECT SUBJECT SLAT TRACK AND ROLLERS FOR ANY DAMAGE AT INTERVALS NOT TO EXCEED 4000 FLIGHT HOURS PER REFERENCE AMM 27-81-00-220-805. NEXT INSPECTION DUE IN 4000 FH.
HN00201298 SN: 00393 DISCREPANCY: SEAT TRACK RBL9 BETWEEN FS485 AND FS581 IS CORRODED IN MULTIPLE LOCATIONS. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW SEAT TRACK P/N SH670-33426-1 @ RBL9 FS485-581 IAW CRJ700 AMM 53-00-49-400-801-A03
HN00203986 SN: 00640 DISCREPANCY: PASSENGER DOOR FUSELAGE HINGE VALLEYS ARE CHAFED 5TH FROM FWD SIDE, AND 2ND, 3RD, 4TH, 5TH, 6TH, 7TH, 8TH, 9TH, 10TH, 11TH, AND 12TH FROM THE AFT SIDE. CORRECTIVE ACTION: REMOVED AND REPLACE PASSENGER DOOR HINGE (FUSELAGE SIDE) IAW CRJ700 SRM 53-21-23-201-007-A01.
HN00203809 DISCREPANCY: UPON REMOVAL OF INTERCOSTAL DD7A FOUND CLIP TO BE CORRODED AND REQUIRES REPLACEMENT. CORRECTIVE ACTION: LOCATED AND DRILLED NEW SERVICEABLE DD7A CLIP PN: 601R318058-1 IAW CRJ700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE DD7A CLIP IAW CRJ700 SRM 51-42-06-001-001-A01.
HN00203800 SN: 00620 DISCREPANCY: PAX DOOR MID CAP ANGLE IS CORRODED, CENTER SECTION CORRECTIVE ACTION: REMOVED AND INSTALLED PAX DOOR MID CAP ANGLE IAW CRJ700 SRM 51-41-02-001-001-A01
HN00203764 SN: 00614 DISCREPANCY: PAX DOOR FORMER BETWEEN DD5, AND DD6 AT FS329.41 FOUND TO BE CORRODED AND REQUIRES REPLACEMENT. CORRECTIVE ACTION: INSTALLED NEW SERVICEABLE PAX DOOR FORMER BETWEEN DD5 AND DD6 P/N#601R31807-3 IAW CRJ-700 SRM TASK 51-42-06-001-001-A01
HN00201654 SN: 00435 DISCREPANCY: RH SIDE SEAT RAIL BETWEEN FS581 TO FS677 IS GOUGED IN MULTIPLE LOCATIONS. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW SERVICEABLE R/H SIDE SEAT RAIL BETWEEN FS581 AND FS677 IAW CRJ700 AMM 53-00-49-400-801-A03
HN00201647 SN: 00433 DISCREPANCY: LH SIDE SEAT RAIL BETWEEN FS863 TO FS985 IS CORRODED. CORRECTIVE ACTION: REMOVED L/H SIDE SEAT RAIL FS863-985 IAW CRJ700 AMM 53-00-49-000-801-A03 INSTALLED L/H SIDE SEAT RAIL FS863-985 IAW CRJ700 AMM 53-00-49-400-801-A03
HN00204254 DISCREPANCY: FOUND R/H SLAT TRACK 1-2 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: REPAIRED BY BLENDING R/H SLAT TRACK 1-2 IAW MHIRJ REO 670-57-42-1877 REV -- DATED 2025-02-27.
HN00204238 SN: 00654 DISCREPANCY: FOUND CORROSION ON FLOOR FITTING P/N SH670-32155-1 BETWEEN F.S. 310-319. CORRECTIVE ACTION: REMOVED AND INSTALLED FLOOR FITTING P/N SH670-32155-1 IAW CRJ 700 SRM 51-42-21-001-001-A01
HN00204234 SN: 00651 DISCREPANCY: FOUND MULTIPLE DENTS ON L/H INBOARD FLAP INNER SKIN INBOARD SIDE. CORRECTIVE ACTION: PREFORMED A MAJOR REPAIRED TO THE L/H INBOARD FLAP IAW CRJ 700 SRM 57-52-01-201-A01
HN00204220 DISCREPANCY: P/N SH670-31990-1 FITTING FS319.70 R/H STRGR 18R CORRODED OUT OF LIMITS DUE TO NO LIMITS GIVEN. CORRECTIVE ACTION: REMOVED AND REPLACED CORRODED FITTING WITH NEW SERVICEABLE FITTING (PN SH670-31990-1) IAW CRJ700 SRM 51-40-11-001-001-A01 & 51-42-21-001-001-A01
HN00201914 SN: 00471 DISCREPANCY: RUDDER EXTERNAL SKIN IS DENTED CORRECTIVE ACTION: REPAIRED RIGHT SIDE RUDDER SKIN IAW CRJ-700 SRM 55-41-01-201-001-A01.
HN00201657 SN: 00438 DISCREPANCY: RH SIDE SEAT RAIL BETWEEN FS781.15 TO FS863 IS CORRODED. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW SERVICEABLE R/H SIDE SEAT RAIL BETWEEN FS781.15 AND FS863 (PN- SH670-36260-5) IAW CRJ700 AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03
HN00201656 SN: 00437 DISCREPANCY: RH SIDE SEAT RAIL BETWEEN FS708 TO FS761.85 IS CORRODED. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW SERVICEABLE R/H SIDE SEAT RAIL BETWEEN FS708 AND FS761.85 (PN- SH670-37509-1) IAW CRJ700 AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03
HN00201655 SN: 00436 DISCREPANCY: RH SIDE SEAT RAIL BETWEEN FS677 TO FS708 IS CORRODED. CORRECTIVE ACTION: REMOVED, FABRICATED AND INSTALLED INSTALLED RH SIDE SEAT RAIL BETWEEN FS677 TO FS708 IAW CRJ700 AMM 53-00-49-400-801 (CONFIG A03)
HN00203627 SN: 00589 DISCREPANCY: INTERNAL ANTENNA DOUBLER BETWEEN FS 295.00 TO FS 310.00 STR 27 IS CORRODED CORRECTIVE ACTION: REMOVED CORRODED/UNSERVICEABLE TCAS OMNIDIRECTIONAL ANTENNA INTERNAL DOUBLER P/N SH670-32364-7S IAW CRJ 700 SRM 51-42-06-001-001-A01.LOCATED AND DRILLED UP NEW SERVICEABLE TCAS OMNIDIRECTIONAL ANTENNA DOUBLER P/N SH670-32364-7S IAW CRJ 700 SRM 51-40-11-001-001-A01.INSTALLED NEW SERVICEABLE TCAS OMNIDIRECTIONAL ANTENNA DOUBLER P/N SH670-32364-7S AT F.S. 295.00 TO F.S. 310 .00 AT STGR 27 IAW CRJ 700 SRM 51-42-06-001-001-A01.
HN00202633 SN: 00516 DISCREPANCY: RIGHT HAND WINDSHIELD SIDE POST HAS A DAMAGED BRACKET ON THE FORWARD/INBOARD LOWER SIDE. CORRECTIVE ACTION: FABRICATED BRACKET PN 601R41246-14 AS PER SAMPLE REFERENCING DWG 601R41246 FOR MATERIAL ID. INSTALLED NEW SERVICEABLE BRACKET PN 601R41246-14 IAW CRJ-700-AMM-20-21-00-910-801-A01.
HN00202627 SN: 00516 DISCREPANCY: LEFT HAND WINDSHIELD SIDE POST CRACKED IN FORWARD UPPER AREA. (MARKED WITH ORANGE TAPE.) CORRECTIVE ACTION: INSTALLED NEW L/H WINDOW POST PN: 601R33223-1 IAW CRJ700 SRM 51-42-21-001-001-A01.
HN00209676 SN: 00816DISCREPANCY:FOUND CORROSION ON STRINGER 23R BETWEEN FS 310 AND FS 319.CORRECTIVE ACTION:REMOVED AND INSTALLED NEW SERVICEABLE STRINGER 23R PN# SH670-31211-4 BETWEEN FS 280.00 AND FS 333.00 IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
HN00208950 SN: 00795 DISCREPANCY:UPON INSTALLATION OF WINDOW POST, SIDE POST LOWER, AFT FITTING PN: GC212-0045-3 FOUND TO BE GOUGED IN MULTIPLE LAVATIONS AND REQUIRES REPLACEMENT DUE TO NO ALLOWABLE LIMITS IN THIS AREA. CORRECTIVE ACTION: LOCATED, DRILLED, AND DEBURRED SIDE POST LOWER, AFT FITTING PN: GC212-0045-3 IAW CRJ700 SRM 51-40-11-001-001-A01 INSTALLED SIDE POST LOWER, AFT FITTING PN: GC212-0045-3 IAW CRJ700 SRM 51-42-21-001-0014-A01
HN00208858 SN: 00787 DISCREPANCY: FOUND CORROSION ON WATER WASTE DOOR SURROUND STRUCTURE BOTTOM DIAPHRAGM PN# SH670-32284-3 CORRECTIVE ACTION: REMOVED WATER WASTE DOOR SURROUND STRUCTURE BOTTOM DIAPHRAGM PN# SH670-32284-3 IAW CRJ 700 SRM 51-42-06-001-001-A01. INSTALLED NEW WATER WASTE DOOR SURROUND STRUCTURE BOTTOM DIAPHRAGM PN# SH670-32284-3 IAW CRJ 700 SRM 51-42-06-001-001-A01.
HN00208853 SN: 00785DISCREPANCY:FOUND CORROSION ON STRINGER 23R PN SH670-31380-1 BETWEEN FS 379 AND FS 333.CORRECTIVE ACTION: REMOVED UNSERVICABLE STRINGER 23R AND INSTALLED A SERVICEABLE STRINGER 23R IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01 AND 51-25-16-001-001-A01.
HN00208704 SN: 00782DISCREPANCY:FOUND PAX DOOR AFT DD2 TO BE CORRODED.CORRECTIVE ACTION: LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR AFT INTERCOSTAL DD2 P/N 601R318052-1 IAW CRJ-700 SRM TASK 51-40-11-001-001-A01. INSTALLED PAX DOOR AFT DD2 INTERCOSTAL IAW CRJ700 SRM 51-42-06-001-001-A01.
HN00208623 SN: 00781 DISCREPANCY: AFT CARGO DOOR FLOOR SILL HAS SEVERAL CHAFES AND AREAS OF CORROSION BETWEEN FS1000-FS1047 CORRECTIVE ACTION: REMOVED AND INSTALLED NEW FLOOR SILL P/N MM670-35655-003 IAW CRJ700 SRM TASK 51-42-20-001-001-A01, & TASK 51-42-06-001-001-A01 MM670-35655-003
FLOOR SEAT TRACK FS985-FS1000 FOUND TO BE CORRODED CORRECTIVE ACTION: REMOVED, FABRICATED SEAT TRACK AT FS985 - 1000 LBL9 IAW CRJ700 SRM 53-00-49-201-002-A01 AND INSTALLED IAW CRJ-700 SRM 51-41-02-001-001-A01,REO 670-53-00-768 REV-- DATE 2025-01-22
HN00207469 SN: 00754 DISCREPANCY: PAX DOOR AFT DAFT ANGLE FOUND TO BE CRACKED REQUIRE REPLACEMENT CORRECTIVE ACTION: LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR AFT WEB DRAG ANGLE P/N #601R31772-5S IAW CRJ-700 SRM TASK 51-40-11-001-001-A01. INSTALLED NEW AFT DRAG ANGLE IAW CRJ 700SRM 51-42-06-001-001-A01
HN00207465 SN: 00752 DISCREPANCY: PAX DOOR FWD WEB FOUND TO BE CRACKED REQUIRE REPLACEMENTT CORRECTIVE ACTION: LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR FWD WEB. P/N 601R317071-12. IAW CRJ-700 SRM TASK 51-40-11-001-001-A01.INSTALLED NEW FWD WEB IAW CRJ 700SRM 51-42-06-001-001-A01
HN00210292 SN: 00840 DISCREPANCY: FOUND CORROSION ON STRINGER 24R BETWEEN FS 295 AND FS 310. CORRECTIVE ACTION: LOCATED AND DRILLED NEW STRINGER 24R PN# SH670-31212-2 IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED NEW STRINGER 24R BETWEEN FS 280 TO FS 333 IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
BURNING RUBBER SMELL IN THE COCKPIT / FOUND FLOODLIGHT BELOW FO SIDE POST TO BE BURNT AND CAUSING THE SMELL. REMOVED AND REPLACED BURNT OUT BULBS IAW CR7 AMM 33-11-03-000/400-801-A01. PERFORMED OPS CHECK IAW CR7 AMM 33-11-00-710-801-A01. OPS CHECK GOOD AT THIS TIME.
IMMEDIATELY AFTER TAKEOFF, THE MAIN LANDING GEAR WOULD NOT RETRACT / REMOVED AND REPLACED HYD SYS 3 RESERVOIR IAW CRJ700 AMM 29-12-30-000/400-801-A01-PSA. PERFORMED EXTENSION/RETRACTION OF THE LANDING GEAR IAW CRJ 700 AMM 32-30-00-865-801. OPS CHECK GOOD AT THIS TIME.
PAX DOOR CRACKS ZONE 3. PERMANENT REPAIR C/W BY MHI TECH IAW FINAL REO 670-52-11-1324
NR-0009 NLG SHOCK STRUCT HAS SEVERAL AREAS OF CORROSION BENEATH STEERING COLLAR AND TENSION BOLT FITTING
DURING MX OPERATIONS IN CANTON OH, (CAK) MX REPORTS TWO DENTS LOCATED UNDER CAPTAIN'S WINDSHIELD ABOVE RVSM AREA. LOCATED ON L/H SKIN PANEL (FS202.75-FS280.00). BOTH DENTS ARE ABOVE STGR12A BETWEEN FS220.00 AND FS202.75. FWD DENT MEASURES .8125" LONG, .5937" WIDE, AND .0125" DEEP AND IS ON/TOUCHING A FASTENER. AFT DENT MEASURES 1.0625" LONG, .6562" WIDE, AND .016" DEEP WITH NEAREST FASTENER BEING .6875" AWAY FROM DENT. THE LH UPPER SKIN PANEL P/N CC670-33101-3 IS FABRICATED FROM .063Ãâ¬? 2024-T3. / COMPLIED WITH FINAL DVI OF FWD AND AFT DENTS IAW EA 21-C7-53-191 REV-A. NO DEFECTS NOTED AT THIS TIME. 337 FORM FILLED OUT AND FILED WITH AIRCRAFT PAPERWORK FOR FINAL REPAIR. DTE TO BE ACCOMPLISHED WITHIN 12 MONTHS OF THE RETURN TO SERVICE DATE FOR SECTION I REPAIR IN ACCORDANCE WITH AC 120-93 PER SECTION IV OF EA.
AFTER T/O DURING CLIMB THE CREW RECEIVED A L/H ENGINE OIL WARNING MESSAGE. CREW LEVELED OFF AT 4000 AND ALL INDICATIONS ON OIL PRESSURE NORMAL. CREW DECLARED EMERGENCY AND RETURNED TO TLH WITHOUT INCIDENT. MX R/R L ENGINE OIL PRESSURE SWITCH IAW CRJ 700 AMM AND PERFORMED FUEL AND OIL LEAK CHECK. NO LEAK FOUND. NO L ENGINE OIL PRESSURE WARNING INDICATION DISPLAYED.
FS 280 AVIONICS FLOOR BOARD SUPPORT ANGLE IS CORRODED. REPLACED SUPPORT ANGLE.
STR 26L IS CORRODED BETWEEN FRAMES 421 AND437. REPLACED STRINGER 26L.
FRAME 295 IS CORRODED BETWEEN STR23R AND STR26L. REPLACED FRAME295.
RH SIDE SEAT TRACK FROM APPROX FS 661 - FS 708 HAS MULTIPLE AREAS OF CORROSION. REPLACED SEAT TRACK
RH SIDE SEAT TRACK FROM APPROX FS 565 - FS 661 HAS MULTIPLE AREAS OF CORROSION.
STR24L IS CORRODED BETWEEN FS347 AND FS379.
FRAME 409 IS CORRODED AT STR 27.
STR26R IS CORRODED BETWEEN FS295 AND FS310. REPLACED STRINGER 26R.
FRAME 333 IS CORRODED BETWEEN STR25R AND STR24R. REPLACED FRAME 333.
RH SIDE SEAT TRACK FROM APPROX FS 785 TO FS 863 HAS MULTIPLE AREAS OF CORROSION. REPLACED SEAT TRACK.
RH SIDE SEAT TRACK FROM APPROX FS 708 TO FS 761 HAS MULTIPLE AREAS OF CORROSION.
EMERGENCY BATTERIES LEFT ON ALL NIGHT. REMOVED AND REPLACED EPSU BATTERY PACK IAW CRJ 700 AMM. OPS CHECK GOOD AT THIS TIME / #1 POWER SUPPLY BATTERY P/N AD2013-1A S/N 231815, #2 BATTERY P/N 2013-1A S/N 104602, #3 BATTERY P/N AD2013-1A S/N 68782, #4 BATTERY 2013-1A S/N 495310"
DURING CLIMB OUT OF HPN THE CREW RECEIVED A NOSE WHEEL STEERING INOP CAUTION MESSAGE. UPON ARRIVE INTO CLT THE CREW DECLARED AN EMERGENCY AND TRUCK ROLLED. THE AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE. B1 CODE 007464. PERFORMED SYSTEM RESET. PROBLEM DID NOT REOCCUR.
CREW RECEIVED A NOSE WHEEL STEERING INOPERATIVE CAUTION MESSAGE. CREW CYCLED SYSTEM CIRCUIT BREAKERS. MSG CLEARED.
CREW REPORTED RECEIVING A STEERING INOP CAUTION MSG JUST AFTER TAKEOFF. RAN THEIR QRH AND COULD NOT GET THE MESSAGE TO CLEAR. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO PHL FOR THE LONG RUNWAY. ON ARRIVAL THE CREW HAD THE CABIN PREPARED FOR AN EMERGENCY. ONCE ON THE GROUND THE AIRCRAFT WAS MET BY EMERGENCY EQUIPMENT AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. CW SYS RESET MSG DID NOT REOCCUR.
ON TAKEOFF ROLL, STALL FAIL CAUTION AND RUD LIMIT FAULT STATUS MSG PERFORMED INSP AND DRAIN MOISTURE ON STANDBY PITOT/STATIC DRAIN ASSY "P3" IAW AMM 34-11-00-220-801. OPS CHECK GOOD. NO FURTHER DEFECT NOTED AT THIS TIME.
OIL SMELL IN COCKPIT AND CABIN ON TAKE-OFF AND DECENT WITH APU OFF. INSPECTED AFT EQUIPMENT BAY AND DUCTING, NO DEFECTS FOUND. RAN BOTH ENGINES, NO SMELLS DETECTED. AIRCRAFT RETURNED TO SERVICE.
THE AIRCRAFT REPORTED A RIGHT BLEED DUCT WARNING FOLLOWED BY A BLEED DUCT CAUTION. THE AIR CONDITIONING PACKS AUTO SHUTDOWN THEN THE CREW RECEIVED A CABIN ALT CAUTION MESSAGE. THE OXYGEN MASKS DEPLOYED WITH PASSENGER USE. MAINTENANCE INSPECTED THE LOOPS AND INTERROGATED THE MDC AND REPOSITIONED BLEED LOOPS. THE AIRCRAFT FERRIED AND REPLACED THE USED OXYGEN GENERATORS AND THE AIRCRAFT WAS RETURNED TO SERVICE.
FLOORBEAM CAP CORRODED IN AFT BAGGAGE BAY AT BS 1031, LBL 27. REPLACED THE FLOORBEAM.
BS 280 FLOORBEAM IS CRACKED AT RBL 13. PERFORMED SB670BA-53-041, REV C.
FUSELAGE FRAME BS 349 IS CORRODED BETWEEN STRINGERS 26L AND 26R. REPLACED THE FRAME SECTION.
J-ANGLE IS CORRODED AT BS 280 BETWEEN LBL 12 AND RBL 12. PERFORMED SB670BA-53-041 REV C.
RH SIDE SEAT TRACK DAMAGED AT BS 436 - 872. REPLACED THE SEAT TRACK.
LEFT SEAT TRACK HAS DAMAGE AT BS 403 - 936. REPLACED THE SEAT TRACK
BS 280 RT BULKHEAD WEB IS CORRODED ON AFT FACE AT WL 73.5, RBL 14. REPAIRED THE BULKHEAD WEB IAW SRM 63-11-10-201-004-A01.
BS 280 FLOORBEAM IS CORRODED ALONG TOP AT MULTIPLE AREAS. PERFORMED SB 670BA-53-041, REV C.
LEFT AND RIGHT COCKPIT FLOOR SUPPORT ANGLES CRACKED. REMOVED AND INSTALLED THE FLOOR SUPPORT ANGLES.
BS 280 LBL AND RBL 9 FLOORBEAM CRACKED. REPLACED THE FLOORBEAM ANGLE.
RIGHT FLOORBEAML AT BS 280 HAS CORROSION. REPLACED THE FLOORBEAM ANGLE.
FLIGHT CREW REPORTED AC ESSENTIAL BUSS CAUTION MESSAGE AND A GENERATOR 1 FAULT IN FLIGHT. CREW RAN QRH AND ATTEMPTED TO START APU WHICH TOOK THREE ATTEMPTS. FLT DIVERTED AND DECLARED EMERGENCY. LANDED SAFELY. REPLACED APU GCU AND K117. OPS CHECKED GOOD.
PASSENGER DOOR SEAL RETAINER DAMAGED. REMOVED AND REPLACED SEAL RETAINER.
INBOARD FLIGHT SPOILER, INBOARD SPOILERON CAUTION MESSAGES. MAINTENANCE COMPLIED WITH SYSTEM RESET. MESSAGE SHOULD NOT APPEAR AGAIN. AIRCRAFT RELEASED FOR SERVICE.
LT ENGINE VIBE OF 4.7 AND AN INTENTIONAL ENGINE SHUTDOWN AFTER TAKEOFF. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FORWARD BLIND CAP, RETAINING RING, AFT SPINNER AND FORWARD SPINNER, AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.
AUTO PILOT, RT WING DOWN CAUTION MESSAGE IN FLIGHT. THE CREW CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. THE ACFT WAS FERRIED TO A REPAIR FACILITY. MAINTENANCE TROUBLESHOT, R & R THE RT FEEL UNIT QUADRANT AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
FRAME IS CORRODED AT FS 565 BELOW WL 72.5 WHERE THE FLOORBEAM ATTACHES AT THE LT SIDE. MAINTENANCE REPAIRED FRAME SECTOR AT FS 565 IAW REO 670-53-31-364, REV.
FRAME IS CORRODED FS 549 BELOW WL 72.5 WHERE THE FLOORBEAM ATTACHES AT THE LT SIDE. MAINTENANCE REPARED FRAME SECTOR AT FS 549 IAW REO 670-53-31-364 REV DATED 2016-04-14.
PASSENGER DOOR LOWER SILL ANGLE MOUNT STRUCTURE IS CORRODED WITH FILAFORM CORROSION. MAINTENANCE R & R PASSENGER DOOR LOWER SILL ANGLE MOUNT STRUCTURE AND CAP ANGLES IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-77-00-001-001-A01.
CREW REPORTED RECEIVING A DISPLAY COOL FAIL MESSAGE WHEN CLIMBING TO FL190. THE CREW INITIATED EMERGENCY PROCEDURES AND DIVERTED TO NEAREST FIELD. THE CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REPLACED THE LOW FLOW SENSOR AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
CREW REPORTED RECEIVING A DISPLAY COOL FAIL MESSAGE WHEN CLIMBING TO FL190. THE CREW INITIATED EMERGENCY PROCEDURES AND DIVERTED TO NEAREST FIELD. THE CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REPLACED FLIGHT COMPARTMENT FILTER AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
DURING ENGINE START, CREW REPORTED SMOKE HAZE IN CABIN WITH A BURNING ODOR. RETURNED TO GATE. MAINTENANCE RAN BOTH PACKS HOT AND COLD IN ALL BLEED CONFIGURATIONS AND PERFORMED OPS CHECKS IAW AMM. OPS CHECK GOOD. COULD NOT DUPLICATE DISCREPANCY. ACFT RELEASED FOR SERVICE.
RIGHT WING INBD FLAP LOWER SURFACE HAS A DENT, ONE FOOT FROM INBD EDGE. COMPLIED WITH ERS-CR-57MR-449.
MAIN AVIONICS UNDERFLOOR DOOR SURROUND RT WEB BETWEEN FS 349.00 & 364.00 IS CORRODED ON THE INBD & OTBD SIDES. INSTALLED WEB IAW SRM 51-42-06, 51--42-13 & 51-42-21.
MAIN AVIONICS UNDERFLOOR DOOR SURROUND LT WEB BETWEEN FS 349.00 & 364.00 IS CORRODED ON THE INBD & OTBD SIDES. INSTALLED WEB IAW SRM 51-42-06, 51--42-13 & 51-42-21.
FORWARD EQUIP BAY FLOOR CRACKED AT THE RT AFT CORNER. REPAIRED IAW ETN-CR-53-099.
RIGHT WING ANTI-ICE TELESCOPIC DUCT CLOSING PLATE HAS LOOSE MOUNT SCREWS & IS CRACKED 1/4 INCH. R & R RT WING ANTI-ICE TELESCOPIC DUCT PLATE INTERNAL BRACKET IAW SRM 51-42-00.
FORWARD EQUIP BAY FLOOR CRACKED AT THE LT CORNER UNDER THE ADG PUMP. REPAIRED FWD EQUIP BAY FLOOR IAW ETN-CR-53-099.
MAIN AVIONICS UNDERFLOOR STRINGER 26LT IS CORRODED BETWEEN FS 310.00 & 319.70. R & R STRINGER 26L IN MAIN AVIONICS UNDERFLOOR IAW SRM 51-42-06.
GALLEY G2 LOWER EMER SIGN LIGHT BULB BURNT OUT. R & R BULBS. OPERATIONS CHECKED GOOD IAW MM 33-51-00.
INTERCOSTAL AT FS 333 TO 349 IS CORRODED AT STRINGER 21L. INSTALLED NEW SERVICEABLE INTERCOSTAL AT FS 333.00 TO FS 349.00 AT STRINGER 21L IAW SRM 51-42-06.
EXTERIOR EMER LIGHTS INOPERATIVE ON LT SIDE SECOND ONE PAST OVERWING EMER EXIT LOOKING AFT & RT SIDE FIRST ON PAST OVERWING EMER EXIT LOOKING AFT. R & R 2 EA EXTERIOR EMER LIGHTS. LT SIDE SECOND ONE PAST OVERWING EMER EXIT LOOKING AFT & RT SIDE FIRST ONE PAST OVERWING EMER EXIT LOOKING AFT IAW AMM 33-51-15. OPERATIONS CHECKED GOOD.
EMERGENCY LIGHT ON GALLEY 1 LOWER CORNER HAS 2 BURNT OUT LIGHTS. R & R GALLEY 1 LOWER CORNER EMER LIGHT BULBS IAW MM 33-51-05.
RIGHT ANGLE AT BL 9.04 IS CRACKED AT FS 280.00. FABRICATED NEW ANGLES & SHIM. INSTALLED IAW SRM 53-11-41.
LEFT ANGLE AT BL 9.04 IS CRACKED AT FS 280.00. FABRICATED NEW ANGLES & SHIM. INSTALLED IAW SRM 53-11-41.
PASSENGER COMPARTMENT CEILING PANEL 273ALC EMER LIGHT BULB BURNT OUT. R & R BULB IAW MM 33-51-09. OPERATIONS CHECKED GOOD IAW MM 33-51-00.
INTERCOSTAL BETWEEN FS 319.70 & 333.00 IS CORRODED AT STRINGER 21L. R & R INTERCOSTAL BETWEEN FS 319.70 & 333.00 IAW SRM 51-42-06.
RIGHT OVERWING FWD EMER EXIT IS INOPERATIVE. R & R RT OVERWING FWD EMER EXIT BULB IAW AMM 33-51-15. OPERATIONS CHECKED GOOD.
RIGHT OVERWING EXIT IS HARD TO OPEN. CLEANED & LUBED RT EXIT SHOOT BOLTS & SOCKETS IAW AMM 12-20-52-640-802. PERFORMED FUNCTIONAL TEST IAW AMM 52-21-00-720-801, FOUND PULL TO BE 33 LBS AVERAGE AFTER 6 PULLS, MAX ALLOWED IS 40 LBS. FUNCTIONAL CHECK GOOD.
LEFT EMER EXIT, LOWER EMER SIGN LIGHT BULB BURNT OUT. R & R BULBS. OPERATIONS CHECKED GOOD IAW MM 33-51-00.
DURING APPROACH, 10 SECONDS AFTER DEPLOYING, FLIGHT SPOILERS INBD FLIGHT SPOILERS & INBD SPOILERONS MSG, CAUTION POSTED MSGS. CREW COMPLIED WITH AOM VOL 1 PROCEDURES, DECLARED AN EMER & LANDED WITHOUT INCIDENT. TRANSFERRED TO NRWC 509-DFW-02009. R & R RT WING MULTI-FUNCTION SPOILER INBD SIDE IAW AMM 27-62-01. OPERATIONS CHECK, LEAK CHECKED GOOD.
FORWARD SIDE OF BULKHEAD AT FS 202.75 FOUND INDICATION ON TOP OF STIFFENER AT RBL 30 APPROX 1/8 INCH LONG. STIFFENER FAILS NDT. REPAIRED STIFFENER IAW NCR-CR-53-089 & REO 670-53-11-1018.
WHILE PERFORMING SERVICE BULLETIN 670BA-53-040 FOUND LINTEL STRINGER 3 OF THE MAIN PAX DOOR CRACKED. SERVICE BULLETIN 670BA-53-040 REV C FUSELAGE CTR FUSELAGE, PRIMARY STRUCTURE FS 280.00 TO 295. INSPECTION & REINFORCEMENT OF THE LINTEL STRINGER 3 OF THE MAIN PAX DOOR PART B INCORPORATED, WHICH INCLUDES REPAIR IAW REO 670-53-21-493.
FS 693, RBL 9 VERTICAL POST HAS A CRACK IN RADIUS, FAILED NDT INSPECTION. REMOVED CRACKED VERTICAL POST & INSTALLED SERVICEABLE POST IAW SRM 51-40-11-001-A01, 51-45-010-001-001-A01, 51-42-06-001-A01 & SB670SH-53-042.
CAPTAIN`S FLASHLIGHT HOLDER CRACKED. R & R CAPTAIN`S FLASHLIGHT HOLDER IAW AMM 25-61-02. OPERATIONS CHECKED GOOD.
NUMBER 2 FMS FAILED. ITEM DEFERRED IAW MEL 34-41. R & R FMC NR 2 IAW MM 34-61-07. OPERATIONS TESTED GOOD IAW MM 34-61-01. MEL ITEM RESTORED.
EMERGENCY LIGHTS DID NOT ILLUMINATE DURING FLIGHT ATTENDANT PREFLIGHT CHECKS. PERFORMED CHARGE OF EMER BATTERY SYS IAW CMM 25-60-03. OPERATIONS CHECKED GOOD IAW AMM 33-51-15. ACFT OK FOR SERVICE.
FLIGHT ATTENDANT NR 1 FLASHLIGHT INOPERATIVE. R & R NR 1 FLIGHT ATTENDANT FLASHLIGHT IAW AMM 25-61-02.
CEILING EMER LIGHT ADJACENT TO ROW 16 IS OUT. CEILING EMER LIGHT NR 5 IAW MEL 33-34.
INBOARD SPOILERON & INBD FLIGHT SPOILER CAUTION MSG HYD SYS 2 PSI DROPPED TO 600 & FLUCTUATED. WHEN 71800 ACMP 2 ON IAW CHECKLIST DID NOT RECOVER PRESS. AFTER A FEW MOMENTS HYD SYS PRESS STABILIZED AT 3000 PSI ONCE POWER WAS MOVED FROM CRUISE RANGE TO CLIMB DETENT. UPON LANDING WITH ELEVATORS DEPLOYED & NORMAL BRAKE APPLICATION HYD SYS 2 PSI DROPPED TO 2200 PSI.
FIRST OFFICERS EMER FLASHLIGHT HOLDER IS BROKEN. R & R FIRST OFFICERS EMER FLASHLIGHT ASSEMBLY IAW AMM 25-61-02.
CEILING EMER LIGHT OVER ROW 5 INOPERATIVE. DEFERRED 2ND CEILING LEVEL FLOOD LIGHT IAW MEL 33-34. R&R CEILING EMER FLOOD LIGHT LAMP IAW AMM CRJ 33-51-09 OPERATIONS CHECKED GOOD MEL ITEM RESTORED.
DURING CLIMB, THE ACFT WOULD NOT PRESSURIZE. LEVELED AT 10,000 FEET, COMPLIED WITH AOM VOL 1 PROCEDURES. RETURNED TO DEPARTURE & LANDED WITHOUT INCIDENT. R & R CABIN PRESSURE CONTROL PANEL IAW AMM 21-33-01, OPS CHECKED GOOD, PRESSURIZED ACFT IN MM IAW AMM 21-31-00, ACFT HELD 3.8 DELTA PSI FOR OVER 3 MINUTES, NO LEAKS NOTED AT THIS TIME.
CABIN EMERGENCY LIGHT BETWEEN ROWS 10 &11 INOPERATIVE. SECURED LOOSE CONNECTOR. EMERGENCY LIGHTS NOW CK NORMAL IAW AMM 33-51-09. MEL IS RESTORED
FORWARD FLIGHT ATTENDANT`S EMERGENCY FLASHLIGHT SWITCH BROKEN. R & R FWD FLIGHT ATTENDANT`S EMERGENCY FLASHLIGHT & CRADLE ASSEMBLY IAW AMM 25-61-02, OPERATIONS CHECKED GOOD.
CABIN EMERGENCY LIGHTS INOPERATIVE. FLT CREW PLAC IAW MEL 33-32 AUTH 120434D-A MOC 686516.
THE CREW REPORTED THE FORWARD F/A FLASHLIGHT MISSING. INSTALLED FLASHLIGHT IAW AMM 25-61-02. THE OPS CHECKED GOOD. RETURNED TO SERVICE.
RT INBD BRAKE, SMOKING ALL OTHERS GREEN, COMPLETED AE BRAKE ASSY WORK CARD 32-007. BLEED COMPLETED, NO LEAKS, FOUND NR 3 BRAKE UPPER PISTON TO BE STICKING. REPLACED NR 3 BRAKE ASSY IAW WC 32-007 UP TO AND INCLUDING STEP 9. OPS CHECKED GOOD.
THE CREW REPORTED THE RT INBD MAIN TIRE WENT FLAT ON LANDING. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 3 MLG TIRE ASSY IAW W/C 32-002. R & R THE NR 4 MLG TIRE ASSY IAW W/C 32-002. THE ACFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE NR 4 CEILING EMERGENCY LIGHT FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY CHARGER AND BATTERY PACK IAW CRJ 700 AMM 33-51-17. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION 3C CHECK FOUND STRINGER 26 RIGHT CORRODED BETWEEN FS 319.70 AND FS 364.00. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED STRINGER IAW STRUCTURAL REPAIR MANUAL 51-42-06. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION 3C CHECK FOUND CROSSBEAM AT FS 280.00 TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CROSSBEAM IAW STRUCTURAL REPAIR MANUAL 51-42-13, 51-42-12, 51-42-06 AND 51-42-21. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND FRAME AT FS 319.70 IS CORRODED BETWEEN STRINGERS 25LT AND 25RT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME IAW EO CR-53MR-329. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE FLOOR PROXIMITY LIGHT STRIP AT PASSENGER SEATS 13B-15BC DISBONDED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR PROXIMITY LIGHT STRIP AT PASSENGER SEATS 13B-15BC IAW CRJ700 AMM 33-51-01-400-801. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3728 THE CREW REPORTED THE RIGHT WING EMERGENCY EXIT PATH ON TOP OF WING WAS PEELING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SAFETY TAPE IAW PT B OF EO-CR-5700-147. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 4663 THE CREW REPORTED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT HOLDER WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED FLASHLIGHT HOLDER TO MOUNT IAW STANDARD MAINTENANCE PRACTICES. THE FLASHLIGHT CHARGED PROPERLY. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3602 THE CREW REPORTED THE FORWARD FLASHLIGHT WAS MISSING. DEFERRED FORWARD FLASHLIGHT PER MEL 25-14 AUTH#110071-C (F/A FLASHLIGHT). M PROCEDURE COMPLY WITH. FORWARD FLASHLIGHT WAS FOUND BY FLIGHT CREW IN AN OVERHEAD BIN. INSTALLED FORWARD FLASHLIGHT IAW CRJ-700 AMM 25-61-02. MEL RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.
FLIGHT 3695, NR 2 FLIGHT ATTENDANT REPORTED A STRONG "BURNING" ODOR FROM THE VENTS OVER SEAT 18 A/B. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED PS62 BALLAST IAW MM 33-21.03. AIRCRAFT RETURNED TO SERVICE.
ON FLIGHT 3710 THE CREW REPORTED THE AFT MOST OVERHEAD EMERGENCY LIGHT INOPERABLE. RELAMPED AFT EMERGENCY CEILING LIGHT IAW AMM 33-51-09. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE AFT EMERGENCY CEILING LIGHT IS OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMEREGENCY FLOOD LIGHT BULB NR 6 IN CEILING IAW CRJ700 AMM 33-51-09. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3833 THE CREW REPORTED THAT WHILE CRUISING AT ALT.3700, THEY RECEIVED A CABIN ALT WARNING MESSAGE, MASK DROPPED, CABIN ALT MOMENTARILY WENT 23000 FT THEN BACK TO 6400FT NORMAL READING ON CABIN ALT AND CABIN PRESSURE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CABIN PRESSURE CONTROL PANEL IAW CRJ-700 AMM 21-33-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B-INSPECTION, FOUND NUMEROUS FORWARD SECTION EMERGENCY LIGHTS WOULD NOT ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 EMERGENCY BATTERY AND CHARGER IAW AMM 33-51-17. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
ON FLIGHT 3695 THE FLIGHT ATTENDANT REPORTED THE LIGHTS ON THE AFT PORTION OF THE EXIT SIGN IN THE CABIN WERE INOPERABLE. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK NR 4 IAW CRJ 700 AMM 33-51-17. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3850 THE FLIGHT ATTENDANT REPORTED THAT EMERGENCY EXIT AT 13 C/D WAS EMITTING A LOUD SQUEALING NOISE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED PRESSURE CHECK ON RIGHT OVERWING EXTIT IAW CRJ 700 AMM 21-31-00. THE OPERATIONAL CHECK WAS GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE VISIT FOUND THE LEFT SIDE PASSENGER ESCAPE ROPE AT THE EMERGENCY EXIT ROW COVER WILL NOT REMAIN IN PLACE. THE COVER NEEDS TO BE RESECURED. THE AIRCRAFT WAS REMOVED FROM SERIVCE. RE-SECURED LEFT SIDE PASSENGER ESCAPE ROPE COVER IAW STAND MAINTENANCE PRACTICES. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE NR 4 CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE 4 CEILING EMERGENCY LIGHT BULB IAW AMM 33-51-09. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT THE NR 4 CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 CEILING EMERGENCY LIGHT BULB IAW AMM 33-51-09. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 4623 THE CREW REPORTED THAT A LEFT MAIN BRAKE OVERHEAT MESSAGE OCCURRED IN CRUISE AT 30000 FEET. THE CREW FOLLOWED AOM VOL 1 LANDING PROCEDURES AND ELECTED TO DIVERT TO ALB. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE NR 1 BRAKE TEMPERATURE SENSOR IAW AMM 32-46-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 9300 THE CREW REPORTED THAT DURING CRUISE RECEVIED A PARKING BRAKE WARNING. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT AT DESTINATION. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH INSULATION REPAIR OF SHORTED WIRE FBH2416-22 ABOVE FRAME LOCATED BETWEEN ASCU AND JB10 IAW EEC SPM 20-33-00. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3815 THE CREW REPORTED A PARKING BRAKE AND ANTI-SKID MESSAGES APPEARED ON EICAS DURING DESCENT. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT PER CRJ FIM 32-45-19 AND FOUND THE PARKING BRAKE SWITCH OUT OF ADJUSTMENT. ADJUSTED THE SWITCH IAW AMM 32-45-16. NO PART REMOVED OR REPLACED. THE OPERATIONAL TEST WAS GOOD IAW AMM 32-45-00. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING THE MAINTENANCE BASE VISIT FOUND BEAM 28- CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED A NEW FRAME IAW EO CR53MR219. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT FOUND THE SERVICE DOOR ENTRANCE LOWER AFT SILL EDGE TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE CORROSION ISSUE IAW CR-53MR-236. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3844 DURING THE CLIMB THE CREW REPORTED A HYDRAULIC NR 2 LOAD CLOSE VALVE CLOSED AND OPENED INTERMITTINGLY. WHEN IN THE CLOSED POSITION INBOARD SPOILERON, THE INBOARD FLIGHT SPOILERON RIGHT REVERSER CAUTIONS ILLUMINATED WITH HYDRAULIC 2 SWITCH IN ON POSITION PER AIRCRAFT OPERATING MANUAL SYSTEM NORMAL. THE CREW ELECTED TO RETURN TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT ENGINE FIRE PUSHBUTTON IAW CRJ 700 AMM 26-21-01. THE OPERATIONAL CHECK WAS GOOD. REMOVED AND REPLACED THE FIRE DETECTION CONTROL UNIT IAW CRJ 700 AMM 26-10-01. THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3869 DURING THE APPROACH THE CREW REPORTED, RECEIVED A SLAT FAIL CAUTION MESSAGE POSTED ON ED-1. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESET SLAT CIRCUIT BREAKERS AND PERFORMED OPERATIONAL TEST OF THE FLAPS AND SLATS SYSTEM IAW CRJ700 AMM 27-50-00-710-801. THE OPERATIONAL CHECK WAS GOOD NO DEFECTS NOTED. ALSO REMOVED AND REPLACED THE LEFT WING SLAT ACTUATOR AT TRACK 1-3 IAW CRJMM 27-81-09. THE OPERATIONAL CHECK OF THE FLAPS/SLATS SYSTEM WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3716 DURING THE APPROACH THE CREW REPORTED THE SLATS FAILED TO EXTEND. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 5 SLAT ACTUATOR ON THE LEFT WING IAW M/M 27-81-09. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3880 ON APPROACH THE CREW REPORTED, RECEIVED SLAT FAIL CAUTION MESSAGE ON EICAS. THE CREW FOLLOWED THE PROCEDURE IN ACCORDANCE WITH CRJ 700 AIRCRAFT OPERATING MANUAL VOL 1. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED FAULT ISOLATION MANUAL TASK 27-81-00-810-802-A01 AND PERFORMED OPERATIONAL TEST OF FLAPS/SLATS IAW AMM 27-50-00. NO PARTS WERE REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT FOUND THE PORTABLE SAFETY MEGAPHONE TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MEGAPHONE BATTERY IAW CRJ-700 AMM 25-61-14. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING THE MAINTENANCE BASE VISIT FOUND THE FLIGHT ATTENDANTâS EMERGENCY FLASHLIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANTâS EMERGENCY FLASHLIGHT BATTERY IAW CMM 25-601-01. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3570 THE FLIGHT ATTENDANT REPORTED A NOISE/WHISTLE FROM THE RIGHT OVERWING EMERGENCY EXIT DURING FLIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DOOR SEAL ON THE RIGHT OVERWING EXIT IAW CRJ-700 AMM 52-21-07 AND 21-31-00. THE PRESSURE LEAK CHECK WAS GOOD.
ON FLIGHT 3582 IN ICING CONDITIONS AT 20,000 FEET THE CREW REPORTED THAT THEY GOT AN ANTI ICING MESSAGE. THE CREW RECEIVED DESCENT CLREARENCE TO 11,000 FEET WHEN A R BLEED DUCT WARNING CAME ON. THE CREW THEN RAN AN EMERGENCY CHECKLIST FOR THR R BLEED DUCT WARNING. THE FIRST OFFICER REPORTED A NOXIOUS ODOR WITH FUMES IN THE CABIN. THE CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN TO DFW. AFTER THE BLEED VALVES WERE CLOSED ALL INDICATIONS WENT AWAY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SIDEWALL POWER UNIT. ALSO REMOVED AND REPLACED 4 CEILING LAMP AT ROW 10 IAW AMM 33-21-01. P/N OF LAMPS: F18T5WW. OPERATIONAL CHECK GOOD. IAW AMM 33-21-00. AIRCRAFT RETURNED TO SERVICE.
ON FLIGHT 4113 CREW REPORTED CABIN EMERGENCY LIGHT SWITCH LEFT ON ALL LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REPLACED NR 1, 2, 3 AND AVIONICS BAY EMERGENCY LIGHT BATTERIES. OPERATION CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
ABORTED TAKEOFF FOR STANDBY INDICATED AIR SPEED. INDICATED FALSE READING COMPARED TO LEFT AND RIGHT INDICATED AIR SPEED INDICATION. MTX FOUND AND CLEANED P2 LINES OF MOISTURE CONTAMINATION IAW AMM 34-11-12. OPS CHECK GOOD LEAK TESTED. NO LEAKS IAW AMM 34-11-00. AIRCRAFT RETURNED TO SERVICE.
LT PACK TEMPERATURE CAUTION FOLLOWED BY LEFT PACK FAULT CAUTION, RECEIVED RIGHT BLEED DUCT CAUTION AT 20,000 FEET. RETURNED TO DFW. PERFORMED WORK SCOPE DEVELOPED BY AMERICAN EAGLE REPEATER DEPARTMENT WITH NO DEFECTS NOTED. PERFORMED FUNCTIONAL CHECK FLIGHT ACCOMPLISHED WITH NO DEFECTS. AIRCRAFT RETURNED TO SERVICE.
CHANNEL 2 FUEL FAIL MESSAGE, POST INSPECTION FOUND CIRCUIT BREAKER U11 POPPED. REMOVED AND REPLACED FUEL GAUGE QUANTITY GAUGING COMPUTER IAW CRJ AMM. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.
FOUND FAILED TO PRESSURIZE ON CLIMB-OUT, RETURNED TO ORD. PERFORMED FIM TASK 21-30-00-810-A01, AMM TASKS 45-45-00-970-801-A01 AND 21-31-00-910-801-A01 WITH NO DEFECTS. AIRCRAFT PRESSURIZED AND DEPRESSURIZED NORMALLY. AIRCRAFT RETURNED TO SERVICE.
SMOKE AND SPARKS OBSERVED COMING FROM THE GLARESHIELD AREA ABOVE THE TILLER WHEEL DURING AIRCRAFT BOARDING. AIRCRAFT POWER DOWN. REMOVED AND REPLACED FLOOD LIGHT ASSEMBLY IAW EMB AMM 33-11-05.
FOUND EMERGENCY LIGHT SWITCH ON FLIGHT ATTENDANT PANEL IN THE ON POSITION. REMOVED AND REPLACED NUMBER 1, 2, 3 AND 4 EMERGENCY LIGHT BATTERIES IAW CRJ AMM 33-51-17. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.
LT SIDEWALL EMERGENCY LIGHT FAILS TO TEST. REPLACED EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200600354) (K)
FLT 3639 - DFW - CABIN LEFT WING EMERGENCY EXIT LOWER LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
XNA - DURING SCHEDULED MAINTENANCE CHECK, EMERGENCY LIGHT AT FS 416 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY POWER SUPPLY UNIT IAW CRJ MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)