N645NN
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
STEERING INOP MSG IN FLIGHT. REMOVED AND REPLACED PILOT HAND TILLER IAW AMM 32-51-01-000/400-801-A01. OPS CHECKED GOOD.
CORROSION ON ACCESS PANELS 542AZ 542BZ 642AZ AND 642BZ CORRODED ON ACCESS PANELS WERE REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WERE EVALUATED OUT OF LIMITS IAW SRM 53-00-00-101-001-A01 AND ACCESS PANELS 542AZ, 542BZ, 642AZ AND 642BZ WERE REPLACED AND VERIFIED PER AIPC 57-52-32
IN REFERENCE TO: TASKCARD TRFKE00FCUS8, 8000FH PERM-REPAIR FUSELAGE SKIN LIGHTNING STRIKE DAMAGE ON SKIN ONLY (NO FASTENER AT DAMAGE LOCATION) WITHIN 8000FH, ACCOMPLISH PERMANENT REPAIR OF TEMP REPAIR PER 670-53-00-045 SECTION 1 PARAGRAPH B3. SEE ATTACHMENTS FOR DETAILS. PERM-REPAIR FUSELAGE SKIN LIGHTNING STRIKE DAMAGE ON SKIN ONLY (NO FASTENER AT DAMAGE LOCATION) WITHIN 8000FH WAS REPAIRED PER REO 690-53-21-2069 REV.-- AND REO 670-53-00-045 REV.-K
IN REFERENCE TO: TASKCARD TRFKE00FCUS8, 8000FH PERM-REPAIR FUSELAGE SKIN LIGHTNING STRIKE DAMAGE ON SKIN ONLY (NO FASTENER AT DAMAGE LOCATION) WITHIN 8000FH, ACCOMPLISH PERMANENT REPAIR OF TEMP REPAIR PER 670-53-00-045 SECTION 1 PARAGRAPH B3. SEE ATTACHMENTS FOR DETAILS. PERM-REPAIR FUSELAGE SKIN LIGHTNING STRIKE DAMAGE ON SKIN ONLY (NO FASTENER AT DAMAGE LOCATION) WITHIN 8000FH WAS REPAIRED PER REO 690-53-21-2069 REV.-- AND REO 670-53-00-045 REV.-K
CORROSION FLOOR FITTING ON ACCESS 104 (1EA) AISLE SIDE AND BEHIND ACCESS 105B (1 EA) ON GALLEY 1. FLOOR FITTING ON ACCESS 104 AISLE SIDE AND BEHIND ACCESS 105B ON GALLEY 1 WERE REPLACED PER SAFRAN CMM 25-32-02
CORROSION AROUND FASTENER HOLE ON AFT CORNER OF THE LOWER PLATE OF CENTER BAGGAGE-BAY DOOR SEAL. LOWER PLATE OF CENTER BAGGAGE-BAY DOOR SEAL WAS EVALUATE FOUND EXCESSIVE DAMAGE PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACE PER CRJ-900 SRM 51-41-02-001-001-A01 AND WITH NRC 00036
CORROSION WAS FOUND AT CENTER HINGE FITTING ASSY LUGS #L1, #L2, #L3, #L4, #L5 AND #L6 (6 EA´S). ALSO ON AILERON HINGE FITTING #1 (1EA). FITTING #1 (1EA) AND L3, L4 OF CENTER HINGE FITTING (2EAS) AT LH AILERON WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A0. L1 & L6 WERE REPAIRED PER REO 670-57-61-237 REV -- AND L2 & L5 WERE REPAIRED PER REO REO 690-57-61-464 REV. - -
AFTER BUSHINGS REMOVAL, CORROSION WAS NOTED ON RIGHT AILERON LUGS R1, R2, R5 AND R6. RIGHT AILERON LUGS R1, R2, R5 AND R6 WERE REPAIRED PER REO 670-57-61-237 REV. --
CORROSION AT SUPPORT STRUCTURE STRAP BTW FAIRING ACCESS PANEL 193AL & 193AR TO FAIRING ACCESSPANEL 193AB. SUPPORT STRUCTURE STRAP FAIRING ACCESS PANEL 193AL AND 193AR WERE REPLACED PER CRJ 900 SRM 51-42-10-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01
CORROSION ON INTERNAL ANGLES OF REFUEL/DEFUEL CONTROL PANEL SUPPORT STRUCTURE. CORROSION ON INTERNAL ANGLE P/N: CC670-39182-8 WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-00-01-101- 001-A01 AND ANGLE 1EA (BRACKET, P/N: CC670-39182-5) WAS FABRICATED PER DWG CC670-39182 REV: - A .
CORROSION ON INNER SKIN TRAILING EDGE OF LH WING BTW STA BL45 TO STA WS 38, AND CORROSION ON INTERCOSTAL (2EA) OF LH WING T. EDGE BTW STA BL45 TO STA WS 38. CORROSION ON INNER SKIN TRAILING EDGE OF LH WING BTW STA BL45 TO STA WS 38 WAS REPAIRED PER REO 690-57-21-548 REV - -,INTERCOSTAL CC670-10322-7 AND CC670-10321-3 OF LH WING T. EDGE BTW STA BL45 TO STA WS 38 WERE REPAIRED PER REO 690-57-22-118 REV. - - AND REO 690-57-22-117 REV. - -, BRACKET ASSY P/N: CC670-75269-3 WAS EVALUATED PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
CORROSION ON LH SIDE SEAT RAILS; (5E/A) FROM FS483 TO FS720, (1E/A) FROM FS744 TO FS761, (1E/A) FROM FS785 TO FS852 AND (2E/A) FROM FS847+19 TO FS969 AT PAX CABIN. LH SIDE SEAT RAILS (5E/A) FROM FA483 TO FS720, (1E/A) FROM FS744 TO FS761, (1E/A) FROM FS785 TO FS852 AND (2E/A) FROM FS847+19 TO FS969 AT PAX CABIN WERE EVALUATED AND FOUND EXCESSIVE DAMAGE PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ-900 AMM 53-00-49
CORROSION ON FITTINGS (2EA) BTW STA FS 280 TO STA FS 295 AND RBL 16 TO RBL 38.AND CORROSION ON FITTINGS (2EA) BTW STA 364 TO STA FS 379 AND LBL 13 TO LBL 40 APPROXIMATELY. FITTINGS (4EAS). BTW STA FS 280 TO STA FS 295 AND RBL 16 TO RBL 38 AND BTW STA 364 TO STA FS 379 AND LBL 13 TO LBL 40 WERE REPLACED PER CRJ900 SRM 51-42-20-001-001-A01
CORROSION ON FLOOR SEAT RAILS RBL9; (4E/A) FROM FS581 TO FS977 AT PAX CABIN. CORRECTIVE ACTION: WERE EVALUATED, DUE TO EXCESSIVE DAMAGE ON SEAT RAILS RBL9; (3E/A) FROM FS581 TO FS 847+16 AT PAX CABIN PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ-900 AMM 53-00-49 AND FLOOR SEAT RAILS(1EA) RBL9 FROM FS 847+16 TO FS977 AT PAX CABIN WAS CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND GVI WAS PERFORMED ON FLOOR SEAT RAILS RBL9 FROM FS 847+16 TO FS977 AT PAX CABIN PER CRJ-900 NDTM 51-20-009-210-A01 AND NO DAMAGE WAS FOUND
CRACK ON AFT RH DOOR LANDING AT FS 188.00 (LATCH HOUSING CUT OUT OF ACCESS DOOR 212AR). LATCH HOUSING ON AFT RH DOOR LANDING AT FS 188.00 (CUT OUT OF ACCESS DOOR 212AR) WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-42-10-001-001-A01
CORROSION ON FLOOR SEAT RAILS LBL9; (1E/A) FROM FS377 TO FS485, (1E/A) FROM FS581 TO FS661+32 AND (3E/A) FROM FS677 TO FS1000 AT PAX CABIN. DUE TO EXCESSIVE DAMAGE ON SEAT RAILS LBL9; (1E/A) FROM FS377 TO FS485, (1E/A) FROM FS581 TO FS661+32 AND (3E/A) FROM FS677 TO FS1000 AT PAX CABIN WERE REPLACED PER CRJ-900 AMM 53-00-49-000-801-A12 AND AMM 53-00-49-400-801-A12
CORROSION ON NO. 2 AND 3 HYDRAULIC TUBES-FITTING SUPPORT, AFT OF RIGHT OUTER WING REAR SPAR AT WS24.50. FITTING SUPPORT, AFT OF RIGHT OUTER WING REAR SPAR AT WS24.50 WAS EVALUATE PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ 900 SRM 51-42-06 001-001-A01
CORROSION ON RH SIDE SEAT RAILS; (4E/A) FROM FS379 TO FS661+14, (1E/A) FROM FS744 TO FS761, (1E/A) FROM FS785 TO FS852 AND(2E/A) FROM FS847+19 TO FS969 ATPAX CABIN. CORROSION ON RH SIDE SEAT RAILS; (4E/A) FROM FS379 TO FS661+14, (1E/A) FROM FS744 TO FS761, (1E/A) FROM FS785 TO FS852 AND(2E/A) FROM FS847+19 TO FS969 ATPAX CABIN WAS EVALUATE DUE TO EXCESSIVE DAMAGE PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ-900 AMM 53-00-49 .
CRACK ON FLOOR BEAM RBL 12.0 BTW FS221.73-FS229.00 AT FWD FUSELAGE INTERNAL STRUCTURE. FLOORBEAM RBL 12.0 BTW FS221.73-FS229.00 AT FWD FUSELAGE INTERNAL STRUCTURE WAS REPAIRED PER REO 690-53-11-2086 REV. - -
CORROSION ON SUPPORT LINES WS 38 AT LH TRUNNION AREA WAS FOUND. SUPPORT LINES WS 38 AT LH TRUNNION WAS EVALUATED PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01
CRACKED WING RIB FLS168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING. WING RIB FLS168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING WAS REPAIRED PER REO 690-57-51-492 REV - -
CORROSION ON DRAIN CHANNELS (2 EAS) FS281.00 LBL14.00 AND RBL14.00 AT PAX CABIN . CORROSION WAS REMOVED ON DRAIN CHANNEL RH (1 EA) ON FS281.00 AT PAX CABIN PER CRJ 900 SRM 51-21-06-001-001-A01 AND EVALUATED THEREFORE IT IS WITHIN LIMITS PER CRJ-900 SRM 53-21-43-101-001-A03 AND DRAIN CHANNEL LH (1 EA) ON FS281.00 AT PAX CABIN WAS EVALUATE FOUND EXCESSIVE DAMAGE PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01
CORROSION ON HINGE (1E/A) OF REFUEL ACCESS DOOR AT FWD LOWER FUSELAGE. HINGE (1E/A) OF REFUEL ACCESS DOOR AT FWD LOWER FUSELAGE WAS EVALUATED FOUND TO EXCESSIVE DAMAGE PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01 AND CRJ-900 AMM 52-45-21-400-801
CORROSION ON SHIMS OF DOOR HINGES OF LP GROUND CONNECTION ACCESS DOOR AT AFT FUSELAGE. SHIMS OF DOOR HINGES OF LP GROUND CONNECTION ACCESS DOOR AT AFT FUSELAGE WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
CORROSION ON ATTACHMENT POINT ANGLE OF SIDE STAY BONDING JUMPER AT LH MLG WHEEL WELL. ATTACHMENT POINT ANGLE OF SIDE STAY BONDING JUMPER AT LH MLG WHEEL WELL WAS EVALUATE FOUND TO EXCESSIVE DAMAGE PER CRJ900 SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
CORROSION ON NUT STRIPS (2 E/A'S) AT UPPER AREA OF LH/RH WHEEL WELL AREA (APROX. RBL/LBL 49). NUT STRIPS (2 E/A'S) AT UPPER AREA OF LH/RH WHEEL WELL AREA (APROX. RBL/LBL 49) WERE EVALUATED FOUND EXCESSIVE DAMAGE PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
CORROSION ON RH/LH FITTINGS SUPPORTS OF CONECTORS PX10J1/PX02J1, PX09J1/PX01J1 AT MLG WHEEL WELL. RH/LH FITTINGS SUPPORTS OF CONECTORS PX10J1/PX02J1, PX09J1/PX01J1 AT MLG WHEEL WELL WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01
CORROSION ON BRACKETS FS514.00, FS565.00, FS626.00, FS661.00 + 9.00 BTW STGR 26LH & 27 AND BTW STGR 22LH & STGR 23LH AND FS652.00 STGR 24RH & 25RH AT FWD/CENTER BAGGAGE BAY COMPARTMENT. BRACKETS FS514.00 BTW STGR 26LH & 27 AND FS514.00, FS565.00, FS626.00, FS661.00 + 9.00 BTW STGR 22LH & STGR 23LH AND FS652.00 STGR 24RH & 25RH AT FWD/CENTER BAGGAGE BAY COMPARTMENT WERE CLEANED PER CRJ-900 SRM 51-26-00-001-001-A01 AND NO DAMAGE WAS FOUND, BRACKETS FS565.00, FS626.00, FS661.00 + 9.00 BTW STGR 26LH & 27 WAS EVALUATED FOUND EXCESSIVE DAMAGE PER CRJ-900 SRM 53-32-58-101-001-A01 AND SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ900 SRM 53-32-58-001-001-A02, SRM 51-42-06-001-001-A01 , SRM 51-42-22-001-001-A01 , SRM 51-42-21-001-001-A01 AND SRM 51-42-10-001-001-A01
CORROSION ON SETTLEMENT ANGLE OF ACCESS PANEL642AZ AT RH WING. SETTLEMENT ANGLE OF ACCESS PANEL 642AZ AT RH WING WAS EVALUATED FOUND EXCESSIVE DAMAGE PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACED PER SRM 51-42-21-001-001-A01
CORROSION ON KICKPLATE ANGLE AND ON MID CAP ANGLE FROM FS310 TO FS 349 AT PASSENGER DOOR SURROUND STRUCTURE. KICKPLATE ANGLE AND ON MID CAP ANGLE FROM FS310 TO FS 349 AT PASSENGER DOOR SURROUND STRUCTURE WERE EVALUATED FOUND EXCESSIVE DAMAGE PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
CORROSION ON LOWER SILL AT AFT DOOR CARGO COMPARTMENT. LOWER SILL AT AFT DOOR CARGO COMPARTMENT WAS EVALUATE FOUND EXCESSIVE DAMAGE PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 , SRM 51-42-13-001-001-A01 AND SRM 51-42-21-001-001-A01
CORROSION ON INTERCOSTAL (STRINGER 26L, STGR 27L, STGR 27R) BTW F.S. 349.00 AND F.S. 364.00 AT AVIONICS COMPARTMENT. CORROSION ON INTERCOSTAL (STRINGER 26L, ) BTW F.S. 349.00 AND F.S. 364.00 AT AVIONICS COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS EVALUATE WITHIN LIMITS PER CRJ-900 SRM 53-21-23-101-003-A02 AND INTERCOSTAL'S (2 EAS) OF F.S. 349.00 TO F.S. 364.00 BTW STRINGER 26LH TO 26 RH WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
CRACK ON MACHINED RIB OF LEADING EDGE SS57.16 AT RH WING. MACHINED RIB OF LEADING EDGE SS57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV - -
CORROSION ON STGR AND STAND-OF ON 26LH BTW FS295.00 TO FS310.00 AT E&E BAY. :STRINGER AND STAND-OFF WAS EVALUATED AND FOUND TO EXCESSIVE DAMAGE CRJ-900 SRM 53-21-03-101-002-A04 AND SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ900 SRM 51-42-13-001-001-A01 AND CRJ 900 SRM 51-42-06-001-001-A01
CORROSION ON RH/LH MLG BIN SUPPORTS (6EA) BTW STA FS 693 TO STA FS847 AND CORROSION ON GUSSET (4EA) BTW STA FS 693 TO STA FS847,AND CORROSION ON FAIRING SUPPORT (4EAS) BTW STA FS 732 TO STA FS 752. CORROSION ON RH/LH MLG BIN SUPPORTS (3EA) BTW STA FS 693 TO STA FS847 AND CORROSION ON GUSSET (4EA) BTW STA FS 693 TO STA FS847 AND CORROSION ON FAIRING SUPPORT (4EAS) BTW STA FS 732 TO STA FS 752 WERE REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED THEREFORE ARE WITHIN OF LIMITS PER CRJ 900 SRM 53-82-55-101-001-A02 AND CRJ 900 SRM 53-42-02-101-001-A02,MLG BIN SUPPORTS (3 EAS) BTW STA FS 693 TO STA FS847 WAS EVAUATED FOUND EXCESSIVE DAMAGE PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-13-001-001-A01
CORROSION ON FAIRING SUPPORTS (SETTLEMENTS AREA, LOWER/UPPER) BTW STA FS847.00 TO STA FS881 BTW STR 18RH TO STR 18LH AND CORROSION ON FAIRING SUPPORT MEMBRANES BTW STA FS 847.00 TO STA FS881 AND BTW STR 25RH TO STR25LH . DUE TO EXCESSIVE DAMAGE ON ANGLE SUPPORT CENTER BTW FS.847 MUST BE REPLACED PER CRJ-900 SRM 51-10-06-001-001-A01 AND SRM 53-83-85-101-001-A01 AND PER CRJ900 SRM 51-40-11-001-001-A01 AND DUE TO EXCESSIVE DAMAGE ON FAIRING SUPPORTS SETTLEMENTS AREA (LOWER) BTW STA FS847 MUST BE REPLACED PER CRJ-900 SRM 51-10-06-001-001-A01 AND PER CRJ900 SRM 51-40-11-001-001-A01, AND SRM 53-83-85-101-001-A01, CORROSION ON FAIRING SUPPORTS (SETTLEMENTS AREA, LOWER/UPPER) BTW STA FS847.00 TO STA FS881 BTW STR18RH TO STR 18LH, AND CORROSION ON FAIRING SUPPORT MEMBRANES BTW STA FS 847.00 TO STA FS881 AND BTW STR 25RH TO STR25LH, CORROSION ON ANGLE SUPPORT RH UPPER AND ANGLE SUPPORT LH UPPER AT STA 847.00 REMOVED PER CRJ-900 SRM 51- 21-06-001-001-A01 AND AREAS WAS THEREFORE THEY ARE WITHIN OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01
CRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-2088 REV - -
CORROSION ON DIAPHRAGM FAIRINGS IN STA FS 797.00 AND RBL/LBL 34 AT RH/LH MLG WHEEL WELL. DIAPHRAGM FAIRINGS IN STA FS 797.00 AND RBL/LBL 34 AT RH/LH MLG WHEEL WELL WERE EVALUATE FOUND TO EXCESSIVE DAMAGE PER CRJ900 SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ900 SRM 51-41-02-001-001-A01
CORROSION ON MLG HYDRAULIC LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) AND ON CONNECTORS SUPPORT PLATE (PX33, PX17, PX34, PX19) AT RH/LH WHEEL WELL AREA. MLG HYDRAULIC LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) AND ON CONNECTORS SUPPORT PLATE (PX33, PX17, PX34, PX19) AT RH/LH WHEEL WELL AREA WERE REPLACED PER CRJ-900 SRM 51-42-20-001-001-A01 AND SRM 51-42-06 001-001-A01 AND SRM 51-41-02-001-001-A01
DENT ON EXTERNAL FUSELAGE SKIN BTW FS 477.40 TO FS 501.00 BTW STGR 17 LH TO STGR 18 LH. DENT ON EXTERNAL FUSELAGE SKIN BTW FS 477.40 TO FS 501.00 BTW STGR 17 LH TO STGR 18 LH WAS REPAIRED PER REO 670-51-00-085 REV - A AND REO 690-53-31-1091 REV - -
SEVERAL DENTS ON EXTERNAL FUSELAGE SKIN BTW FS 1015.00 TO FS 1031.00 BTW STGR 20 LH TO STGR 23 LH. SEVERAL DENTS ON EXTERNAL FUSELAGE SKIN BTW FS 1015.00 TO FS 1031.00 BTW STGR 20 LH TO STGR 23 LH WERE REPAIRED PER REO 670-51-00-085 REV - A AND REO 690-53-61-1702 REV - -