N678CA
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
214 reports on file, 2008-04-11 – 2026-05-27.
Part: CONTACT — INOPERATIVE (ZONE 200) · airframe 41,670 hrs · 30,120 cycles
AFT EMER CEILING LIGHT INOPERATIVE. REPINNED P361 IAW CRJ 900 ESPM 20-26-03. P# OFF/ON 350690-7. OPS CHECKS GOOD IAW AMM 33-51-00.
Part: STAND OFF — CRACKED (ZONE 400) · airframe 41,001 hrs · 29,593 cycles
PARTS RACK: CRACKED INNER SUPPORT ANGLE (STANDOFF 1 EA) ON LH LOWER TRANSCOWL. INNER SUPPORT ANGLE (STANDOFF 1 EA) ON LH LOWER TRANSCOWL WAS REPAIRED AND REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01, CRJ-900 SRM 51-42-28-001-001-A01, EA CRJ954-21413 REV A, CMAPS 188-001 REV. B, CMAPS 176-002 REV. - - ,CRJ-900 SRM 51-40-11-001-001-A01 ,CRJ-900 SRM 51-21-11-001-001-A01 AND CRJ-900 SRM 51-42-10-001-001-A01
Part: HINGE — CORRODED (ZONE 600) · airframe 41,001 hrs · 29,593 cycles
CORROSION AT INNER LUG BORES OF RH AILERON, CENTER HINGE FITTING AILS R1,R2,R5 AND R6 WAS FOUND LUGS BORES R1, R5 AND R6 RH AILERON WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 CLEANING AND NOT FOUND CORROSION & R2 WERE REPAIRED PER REO 670-57-61-107 REV - B
Part: PACKER — CORRODED (ZONE 100) · airframe 41,001 hrs · 29,593 cycles
AFTER FWD WASTE LAVATORY SERVICE PANEL DOOR REMOVAL, CORROSION ON PACKERS (2EAS) WERE FOUND PACKERS (2EAS) WERE REPLACED ON FWD WASTE LAVATORY SERVICE PANEL DOOR PER CRJ900 SRM 51-10-06-001-001-A01 AND INSTALLED WITH NRC 00030.
Part: HINGE — CORRODED (ZONE 100) · airframe 41,001 hrs · 29,593 cycles
SECONDARY NRC FROM RC 900-32-710-902ÿ½: AFTER HARDWARE REMOVAL, CORROSION ON LH/RH FITTING, NLG W/W AREA WAS FOUND LH/RH FITTING, NLG W/W WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01
Part: DIAPHRAGM — CRACKED (ZONE 100) · airframe 41,001 hrs · 29,593 cycles
AFTER CLEANING, CRACK IN LH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35LBL AT LH MLG WHEEL WELL WAS FOUND. FAIRING SUPPORT DIAPHRAGM LH IN STA. FS= 797 TO FS= 807 AND 35LBL AT LH MLG WHEEL WELL WAS REPLACED PER CRJ/900 SRM 51-41-02-001-001-A01
Part: SKIN — CHAFED (ZONE 100) · airframe 41,001 hrs · 29,593 cycles
WEAR ON FUSELAGE SKIN BTW STA FS=910 TO FS=930 AND BTW STGR 24 LH AND 24 RH. WEAR ON FUSELAGE SKIN BTW STA FS=910 TO FS=930 AND BTW STGR 24 LH AND 24 RH WERE BLEND OUT AND EVALUATED WITHIN LIMITS BTW FS913 TO FS930 , STRG 24L/24R PER CRJ900 SRM 51-12-00-001-001-A01 ,CRJ900 SRM 53-51-01-101-003-A04 , PER REO 670-53-00-290 REV -F AND BTW FS910 TO FS913 WAS REPAIRED PER EA CRJ953-19683 REV IR
Part: HINGE — CORRODED (ZONE 800) · airframe 41,001 hrs · 29,593 cycles
SECONDARY NRC FROM NRC 00129: AFTER REMOVAL OF FLAP STEP PLATE, CORROSION ON FLAP STEP PLATE HINGES (ALL) WAS FOUND. FLAP STEP PLATE HINGES (FWD,MID, AFT) WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND EA CRJ953-21415 REV, IR .
Part: SEAT TRACK — CORRODED (ZON E200) · airframe 41,001 hrs · 29,593 cycles
INITIAL INSPECTION: CORROSION ON SEAT TRACK LOCATED BTW FS349.00 TO FS379.00 AND RBL9.00. SEAT TRACK LOCATED BTW FS349.00 TO FS379.00 AND RBL9.00 WAS REPLACED PER CRJ-900 AMM 53-00-49-000-801-A07. AND AMM 53-00-49-400-801-A07.
Part: ANGLE — CRACKED (ZONE 100) · airframe 41,001 hrs · 29,593 cycles
OUT OF SCOPE: CRACKED INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE. INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE. WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01.
Part: HINGE — CORRODED (ZONE 800) · airframe 41,001 hrs · 29,593 cycles
SECONDARY NRC FROM NRC 00129: AFTER REMOVAL OF FLAP STEP PLATE, CORROSION ON FLAP STEP PLATE HINGES (ALL) WAS FOUND. FLAP STEP PLATE HINGES (FWD,MID, AFT) WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND EA CRJ953-21415 REV, IR .
Part: HINGE — CORRODED (ZONE 800) · airframe 41,001 hrs · 29,593 cycles
SECONDARY NRC FROM NRC 00129: AFTER REMOVAL OF FLAP STEP PLATE, CORROSION ON FLAP STEP PLATE HINGES (ALL) WAS FOUND. FLAP STEP PLATE HINGES (FWD,MID, AFT) WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND EA CRJ953-21415 REV, IR .
Part: FRAME — CRACKED (ZONE 200) · airframe 41,001 hrs · 29,593 cycles
CRACK ON FUSELAGE FRAME FS 533.00 BTW STGR 0/ STGR 1R CRACK ON FUSELAGE FRAME FS 533.00 BTW STGR 0/ STGR 1R WAS REPAIRED PER EA CRJ953-19684 REV IR
Part: HINGE — CRACKED (ZONE 500) · airframe 41,001 hrs · 29,593 cycles
INITIAL INSPECTION: CRACK ON HINGE OF THE BUTTER DOOR ACCESS PANEL 591LB AT LH WING. CRACK ON HINGE OF THE BUTTER DOOR ACCESS PANEL 591LB AT LH WING WAS REPAIRED PER EA NO: CRJ957-21363 REV. IR
Part: FITTING — CORRODED (ZONE 200) · airframe 41,001 hrs · 29,593 cycles
CORROSION FLOOR FITTING ON ACCESS 107 (1EA) AISLE SIDE AND ACCESS 109 (1EA) ON GALLEY 1. SUMMARY OF NRC 00251: FLOOR FITTING (1EA) AND DOUBLER FLOOR FITTING (1EA) AISLE SIDE ON ACCESS 107 AND FLOOR FITTING (1EA) ON ACCESS 109 AT GALLEY 1 WERE REPLACED PER SAFRAN CMM 25-33-67
Part: DOOR — CRACKED (ZONE 800) · airframe 41,001 hrs · 29,593 cycles
CRACKED TOP EDGE STRUCTURE OF LEFT FORWARD OVERWING EMERGENCY EXIT DOOR. TOP EDGE STRUCTURE OF LEFT FORWARD OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER REO 670-52-21-103 REV. --
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 41,001 hrs · 29,593 cycles
CRACKED FLOOR SUPPORT BTW FS=295.00 TO 319.70 AND RBL 27 AT PASSENGER FLOOR STRUCTURE FLOOR SUPPORT BTW FS=295.00 TO 319.70 AND RBL 27 AT PASSENGER FLOOR STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-13-001-001-A01 & SRM 51-42-06-001-001-A01
Part: FITTING — CORRODED (ZONE 200) · airframe 41,001 hrs · 29,593 cycles
CORROSION FLOOR FITTING ON ACCESS 107 (1EA) AISLE SIDE AND ACCESS 109 (1EA) ON GALLEY 1. SUMMARY OF NRC 00251: FLOOR FITTING (1EA) AND DOUBLER FLOOR FITTING (1EA) AISLE SIDE ON ACCESS 107 AND FLOOR FITTING (1EA) ON ACCESS 109 AT GALLEY 1 WERE REPLACED PER SAFRAN CMM 25-33-67
Part: LANDING — CRACKED (ZONE 800) · airframe 41,001 hrs · 29,593 cycles
CRACK ON SETTLEMENT AREA OF ACCESS PANEL 832DR AT PASSENGER DOOR. SETTLEMENT AREA OF ACCESS PANEL 832DR AT PASSENGER DOOR WAS REPAIRED PER EA NO. CRJ952-21312 REV. A.
Part: DOOR SILL — CRACKED (ZONE 200) · airframe 41,001 hrs · 29,593 cycles
INITIAL INSPECTION: CRACK ON AFT RH DOOR LANDING FS 188.0 (LATCH CUT OUT OF ACCESS DOOR 212AR) AT FWD EQUIPMENT COMPARTMENT. DOOR LANDING (LATCH CUT OUT OF ACCESS DOOR 212AR) AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER EA CRJ953-21314 REV. IR AND CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01.
Part: SKIN — CORRODED (ZONE 100) · airframe 41,001 hrs · 29,593 cycles
CORROSION ON INTERNAL SKIN FROM STA FS 364 TO 394 BTW STGR 25L-25R AT E/E COMPARTMENT DOOR CUTOUT INTERNAL SKIN FROM STA FS 364 TO 394 BTW STGR 25L-25R AT E/E COMPARTMENT DOOR CUTOUT WAS REPAIRED PER REO 690-53-21-032 REV. --
Earlier reports · 2008–2022 · 193 reports
2022
Part: BRACKET — CRACKED (BS 220) · airframe 34,388 hrs · 23,994 cycles
WHILE REMOVING ASSEMBLY MADE BRACKET, FOUND BRACKETS CRACKED ON TOP OF BS 220 LT & RT. REMOVED AND REPLACED THE BRACKETS IAW SRM 51-42-06-001-001-A01.
Part: SIGN — INOPERATIVE · airframe 33,645 hrs · 23,359 cycles
FWD OVER WING BOTTOM DOOR EXIT LIGHT INOP. R/R IDENTIFIER EXIT ASSEMBLY @ EXIT SING DS177 IAW AMM 33-51-05. OPS TEST GOOD. P/N ON/OFF: BR9279-013
Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 33,642 hrs · 23,357 cycles
RH OVERWING EMERGENCY LIGHTS ARE INOP.
Part: INTERCOSTAL — CORRODED · airframe 33,642 hrs · 23,357 cycles
INTERCOSTAL AT STRINGER 20R IS CORRODED BETWEEN F.S.333 TO F.S.349 REMOVED AND REPLACED INTERCOSTAL IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
Part: ANGLE — CRACKED · airframe 33,642 hrs · 23,357 cycles
R/H FWD VERT DRAG ANGLE IS CRACKED. REPAIRED R/H FWD DRAG ANGLE IAW CRJ 900 SRM 55-31-00-201-001-A01
Part: DOUBLER — CORRODED · airframe 33,642 hrs · 23,357 cycles
ANTENNA DOUBLER CORRODED AT STGR 27 BETWEEN FS 485.00 AND FS 501.00 REMOVED AND REPLACED DOUBLER (NUT PLATE SUB ASSEMBLY) I.A.W. CRJ 900 SRM'S #51-40-11-001-001-A01 AND51-42-06-0001-001-A01
Part: STRINGER — CORRODED · airframe 33,642 hrs · 23,357 cycles
STRINGER 25L BETWEEN FS 485.00 AND FS 517.00 IS CORRODED REPAIRED STRINGER IAW ENDEAVOR EA CRJ953-13740 REV A DATED 6/24/2022.
Part: FORMER — CORRODED · airframe 33,642 hrs · 23,357 cycles
FORMER ON PASSENGER DOOR AT FS329.41 BETWEEN DD5 AND DD6 IS CORRODED. REPLACED FORMER IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: FITTING — CORRODED · airframe 33,642 hrs · 23,357 cycles
FOUND CORROSION ON PAX DOOR FWD CLOSING FITTING AFTER REMOVING UPPER DOOR SILL ANGLE. REMOVED & REPLACED FITTING IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01.
Part: STRINGER — CORRODED · airframe 33,642 hrs · 23,357 cycles
STRINGER 24R CORRODED BETWEEN FS581.00 AND FS597.00 REPAIRED IAW ENDEAVOR EA CRJ953-13716 REV IR DATED; 5/27/2022
Part: FRAME — CRACKED · airframe 33,642 hrs · 23,357 cycles
LEFT FORWARD EMERGENCY EXIT DOOR TOP EDGE MEMBER HAS POSSIBLE CRACK AT DOOR SWITCH STOP. REPAIRED TOP EDGE MEMBER ON L/H FWD EMERGENCY EXIT DOOR IAW ENDEAVOR AIR EA CRJ952-13633 REV IR DATED 5-17-2022.
Part: STRINGER — CORRODED · airframe 33,642 hrs · 23,357 cycles
STGR 22R IS CORRODED BETWEEN FS 319.00 - FS 333.00. REMOVED, FABRICATED & REPLACED STRINGER IAW ENDEAVOR AIR EA CRJ953-13763.
Part: INTERCOSTAL — CORRODED · airframe 33,642 hrs · 23,357 cycles
INTERCOSTAL CORRODED BETWEEN FS 865 AND FS 881 @ STGR 21R. REPAIRED INTERCOSTAL IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 & ENDEAVOR AIR EA CRJ953-13700.
Part: ANGLE — CRACKED · airframe 33,642 hrs · 23,357 cycles
R/H AFT VERT DRAG ANGLE IS CRACKED. REMOVED & REPLACED R/H AFT DRAG ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-13-001-001-A01, 51-42-22-001-001-A01, 51-42-21-001-001-A01 & 51-25-01-001-001-A01.
Part: SEAT TRACK — CORRODED · airframe 33,642 hrs · 23,357 cycles
PASSENGER SEAT TRACK AT LBL 9 FS 977 - FS 1000 IS CORRODED. REMOVED, FABRICATED & REPLACED SEAT TRACK IAW CRJ 900 SRM 51-40-11-001-001-A01, 53-00-49-201-002-A01 & AMM 53-00-49-000/400-801-A07.
Part: NONE — CORRODED · airframe 33,642 hrs · 23,357 cycles
LH SIDE SEAT RAIL F.S. 673.- 720 HAS MULTIPLE SPOTS OF CORROSION REMOVED, FABRICATED AND REPLACED SIDE SEAT RAIL IAW CRJ SRM 53-00-49-201-002-A01 & AMM 53-00-49-000/400-801-A07
Part: STRINGER — CORRODED (FS 333-409) · airframe 33,642 hrs · 23,357 cycles
STGR 24R BETWEEN FS 333 TO FS409 FOUND 4 LOCATIONS AROUND FASTENERS CORRODED. REPAIRED STRINGER IAW ENDEAVOR EA CRJ953-13887 REV IR DATED 6/27/2022.
Part: DRAG ANGLE — CRACKED (LH AFT) · airframe 33,642 hrs · 23,357 cycles
LH AFT VERTICAL DRAG ANGLE CRACKED. REPLACED LH AFT DRAG ANGLE IAW CRJ 900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01.
Part: STRINGER — CORRODED (FS 295-310) · airframe 33,642 hrs · 23,357 cycles
STGR 24R BETWEEN FS 295 TO FS310 FOUND 2 LOCATIONS AROUND FASTENERS CORRODED. REPAIRED STRINGER IAW ENDEAVOR EA CRJ953-13804 REV IR DATED 6/24/2022.
Part: FRAME — CORRODED · airframe 33,642 hrs · 23,357 cycles
FRAME CORRODED @ FS 942 BETWEEN STGR 27 AND STGR 25R. SPLICE REPAIRED FRAME USING FRAME SECTOR PART NUMBER SH690-37073-5 IN LIEU OF P/N SH690-37095-3 IAW ENDEAVOR AIR EA CRJ953-13822.
Part: STRINGER — CORRODED · airframe 33,642 hrs · 23,357 cycles
STGR 21R IS CORRODED BETWEEN FS 333.00-349.00. REMOVED & REPLACED STRINGER IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01.
Part: SPLICE — CORRODED · airframe 33,642 hrs · 23,357 cycles
STGR SPLICE (JOINT PIECE) 21R IS CORRODED AT FS 333.00. REMOVED & REPLACED SPLICE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
Part: HINGE — WORN · airframe 33,642 hrs · 23,357 cycles
PAX DOOR HINGE, FUSELAGE SIDE FAILS INSPECTION. AFT 12 LUGS FAIL. REMOVED & REPLACED PAX DOOR FUSELAGE SIDE HINGE IAW CRJ 900 SRM 51-42-21-001-001-A01 & 53-21-23-201-007-A01.
Part: FRAME — CORRODED · airframe 33,642 hrs · 23,357 cycles
F.S.847+16 FRAME IS CORRODED FROM STGR 26L TO 26R. SPLICE REPAIRED FRAME IAW CRJ 900 SRM 53-00-06-201-001-A03.
Part: BEAM — CORRODED · airframe 33,642 hrs · 23,357 cycles
FRAME STA 1031, LBL9, FLOOR BEAM CORRODED TO FS 1051. SPLICE REPAIRED BEAM IAW CRJ 900 SRM 53-00-41-201-001-A03.
Part: FRAME — CORRODED · airframe 33,642 hrs · 23,357 cycles
FRAME CORRODED @ FS 927 BETWEEN STGR 27 AND STGR 25R. SPLICE REPAIRED FRAME IAW CRJ 900 SRM 53-00-06-201-001-A03
Part: STRIKER — CORRODED · airframe 33,642 hrs · 23,357 cycles
LOWER SERVICE DOOR SURROUND HAS MULTIPLE SPOTS OF CORROSION. REMOVED & REPLACED SEAL STRIKER FITTING IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01 & 51-42-06-001-001-A01.
Part: STRINGER — CORRODED · airframe 33,642 hrs · 23,357 cycles
STRINGER/SH670-31636-1/CORRODED/STRINGER/SH670-31636-1 STRINGER/SH670-31636-1/CORRODED
Part: SPLICE — CORRODED · airframe 33,642 hrs · 23,357 cycles
STGR SPLICE 24 R AT FS 333 IS CORRODED. INSTALLED NEW STGR SPLICE 24R IAW CRJ900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 53-21-03-101-002-A04, 51-42-21-001-001-A01.
Part: BEAM — CORRODED · airframe 33,642 hrs · 23,357 cycles
FLOOR BEAM CORRODED FS 1031 LBL 27. SPLICE REPAIRED BEAM IAW CRJ 900 SRM 53-00-41-201-001-A03.
Part: SEAT TRACK — CORRODED · airframe 33,642 hrs · 23,357 cycles
PASSENGER SEAT TRACK AT LBL 9 FS 849 - FS 977 IS CORRODED. REMOVED & REPLACED SEAT TRACK IAW CRJ 900 AMM 53-00-49-000/400-801-A07
Part: STRINGER — CORRODED · airframe 33,642 hrs · 23,357 cycles
STGR 20R IS CORRODED BETWEEN FS 319.00 - FS349.00 INSTALLED NEW STGR 20R I.A.W. CRJ 900 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, & #51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED · airframe 33,642 hrs · 23,357 cycles
PASSENGER SEAT TRACK AT LBL 27, FS 977 IS CORRODED. REMOVED & REPLACED SEAT TRACK IAW CRJ 900 AMM 53-00-49-000/400-801-A07.
Part: STRINGER — CORRODED · airframe 33,642 hrs · 23,357 cycles
STGR 20R IS CORRODED BETWEEN FS 295.00 - FS310.00 INSTALLED NEW STGR 20R I.A.W. CRJ 900 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, & #51-42-06-001-001-A01.
Part: ANGLE — CORRODED · airframe 33,642 hrs · 23,357 cycles
ANGLE CORRODED LEFT OF STGR27 BETWEEN FS 565.00 AND FS 581.00 INSTALLED NEW ANGLE I.A.W ENDEAVOR EA CRJ 953-13611 REV IR DATED 5-18-22 AND CRJ 900 SRM 51-42-06-001-001-A01.
Part: INTERCOSTAL — CORRODED · airframe 33,642 hrs · 23,357 cycles
INTERCOSTAL AT STGR27 R/H BETWEEN F.S.394 TO F.S.409 HAS CORROSION AT RIVETS. REMOVED & REPLACED INTERCOSTAL IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
Part: NONE — CORRODED · airframe 33,642 hrs · 23,357 cycles
L/H SIDE SEAT RAIL BETWEEN F.S.572 TO F.S.661+16 HAS MULTIPLE SPOTS OF CORROSION. REMOVED CORRODED L/H SIDE SEAT RAIL FROM F.S.572 TO F.S.661+16 AND INSTALLED NEW SERVICABLE SEAT RAIL IAW CRJ 900 AMM 53-00-49-400-801-A07 AND SRM 53-00-49-201-002-A01.
Part: NONE — CORRODED · airframe 33,642 hrs · 23,357 cycles
L/H SIDE SEAT RAIL BETWEEN F.S. 897 TO F.S. 913+8 IS CORRODED. REMOVED CORRODED L/H SIDE SEAT RAIL FROM F.S. 897 TO F.S. 913+8 AND INSTALLED NEW SERVICABLE SEAT RAIL IAW CRJ 900 SRM 53-00-49-201-002-A01 AMM 53-00-49-400-801-A07.
Part: STRINGER — CORRODED · airframe 33,642 hrs · 23,357 cycles
STR 23R BETWEEN FS280 AND FS295 FOUND 1 LOCATION AROUND FASTENER CORRODED JOB 81512551 OP 617 REPLACED STRINGER IAW CRJ SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 53-21-03-101-002-A04, 51-42-21-001-001-A01
Part: STRINGER — CORRODED · airframe 33,642 hrs · 23,357 cycles
STR 22 IS CORRODED BETWEEN FS333-FS349 JOB 81512555 OP 16 REPLACED STRINGER IAW CRJ SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01
Part: FRAME — CRACKED · airframe 33,642 hrs · 23,357 cycles
LEFT AFT EMERGENCY EXIT DOOR TOP EDGE MEMBER HAS POSSIBLE CRACK AT DOOR SWITCH STOP. REPAIRED TOP EDGE MEMBER ON L/H FWD EMERGENCY EXIT DOOR IAW ENDEAVOR AIR EA CRJ952-13605 REV IR DATED 5-27-2022.
Part: FRAME — CRACKED · airframe 33,642 hrs · 23,357 cycles
RIGHT AFT EMERGENCY EXIT DOOR TOP EDGE MEMBER HAS POSSIBLE CRACK AT DOOR SWITCH STOP. REPAIRED TOP EDGE MEMBER ON R/H AFT EMERGENCY EXIT DOOR IAW ENDEAVOR AIR EA CRJ952-13603 REV IR DATED 5-27-2022.
Part: FRAME — CRACKED · airframe 33,642 hrs · 23,357 cycles
RIGHT FORWARD EMERGENCY EXIT DOOR TOP EDGE MEMBER HAS POSSIBLE CRACK AT DOOR SWITCH STOP. REPAIRED TOP EDGE MEMBER ON R/H FWD EMERGENCY EXIT DOOR IAW ENDEAVOR AIR EA CRJ952-13604 REV IR DATED 5-27-2022.
Part: RETAINER — DAMAGED · airframe 33,642 hrs · 23,357 cycles
PAX DOOR, FWD LOWER CORNER SEAL RETAINER IS BENT. REMOVED BENT SEAL RETAINER FROM PAX DOOR FWD LOWER CORNER AND INSTALLED NEW SERVICABLE SEAL RETAINER IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01.
Part: INTERCOSTAL — CORRODED (PASSENGER DOOR) · airframe 33,642 hrs · 23,357 cycles
PASSENGER DOOR INTERCOSTAL AT DD3 IS CORRODED. REMOVED CORRODED PAX DOOR INTERCOSTAL, INSTALLED NEW SERVICABLE INTERCOSTAL IAW CRJ 900 SRM 51-42-06-001-001-A01
Part: NONE — CORRODED · airframe 33,642 hrs · 23,357 cycles
RH SIDE SEAT RAIL BETWEEN FS661+16 TO FS677.00 HAS MULTIPLE SPORTS OF CORROSION. REMOVED AND REPLACED RH SIDE SEAT RAIL FROM F.S. 661+16-677.00 IAW CRJ900 AMM 53-00-49-000/400-801-A07.
Part: FORMER — CORRODED · airframe 33,642 hrs · 23,357 cycles
PASS. DOOR AFT FORMER F.S. 347.27 CORRODED (601R318034-5). REPLACED PAX DOOR AFT FORMER IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01.
Part: SEAT TRACK — CORRODED · airframe 33,642 hrs · 23,357 cycles
R/H SIDE SEAT TRACK BETWEEN F.S. 379.00-469.00 HAS MULTIPLE SPOTS OF CORROSION. REPLACED RH SIDE SEAT TRACK F.S. 469.00-485.00 IAW CRJ900 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-000/400-801-A07.
Part: FRAME — CORRODED · airframe 33,642 hrs · 23,357 cycles
FRAME AT F.S. 349.00 BETWEEN STGR 26L-25R HAS MULTIPLE SPOTS OF CORROSION. REPLACED FRAME AT F.S. 349.00, STGR 26L-25R IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: INTERCOSTAL — CORRODED · airframe 33,642 hrs · 23,357 cycles
PASSENGER DOOR INTERCOSTAL AT DD4 IS CORRODED. REMOVED CORRODED PAX DOOR INTERCOSTAL P/N: 601R31902-317 AND ATTACH BRACKET P/N: 601R318084-2 AND INSTALLED NEW SERVICABLE INTERCOSTAL AND BRACKET IAW CRJ 900 SRM 51-42-06-001-001-A01
Part: WEB — CORRODED · airframe 33,642 hrs · 23,357 cycles
PAX DOOR FWD STAIR WEB IS CORRODED AT NUTPLATE HOLES. REPLACED PAX DOOR FWD STAIR WEB, I.A.W. CRJ SRM'S #51-40-11-001-001-A01, #51-42-06-001-001-A01,
Part: WEB — CORRODED · airframe 33,642 hrs · 23,357 cycles
PAX DOOR AFT STAIR WEB IS CORRODED AT NUTPLATE HOLES. REPLACED PAX DOOR AFT STAIR WEB, I.A.W. CRJ SRM'S #51-40-11-001-001-A01, #51-42-06-001-001-A01,
Part: INTERCOSTAL — CORRODED · airframe 33,642 hrs · 23,357 cycles
STGR 20R FS 349.00 - FS364.00, CORRODED AND GOUGED ON CORNER. REPLACED INTERCOSTAL I.A.W. CRJ 900 SRM'S #51-40-11-001-001-A01, 51-42-21-001-001-A01, & #51-42-06-001-001-A01.
Part: NONE — CORRODED · airframe 33,642 hrs · 23,357 cycles
R/H SIDE SEAT RAIL BETWEEN F.S.453 TO F.S.469 HAS MULTIPLE SPOTS OF CORROSION. REMOVED CORRODED R/H SIDE SEAT RAIL FROM F.S.453 TO F.S.469 AND INSTALLED NEW SERVICABLE SEAT RAIL IAW CRJ 900 AMM 53-00-49-400-801-A07 AND SRM 53-00-49-201-002-A01.
Part: INTERCOSTAL — CORRODED · airframe 33,642 hrs · 23,357 cycles
INTERCOSTAL BETWEEN F.S.349 TO F.S.369 AT STGR 26R TO 27 HAS MULTIPLE SPOTS OF CORROSION. REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW SERVICABLE INTERCOSTAL, I.A.W. CRJ 900 SRM'S, #51-40-11-001-001-A01, #51-42-06-001-001-A01 AND 51-42-21-001-001-A01. PROTECTIVE FINISHES REAPPLIED
Part: NONE — CORRODED · airframe 33,642 hrs · 23,357 cycles
R/H SIDE SEAT RAIL BETWEEN F.S.485 TO F.S.572 HAS MULTIPLE SPOTS OF CORROSION. REMOVED CORRODED R/H SIDE SEAT RAIL FROM F.S.485 TO F.S.572 AND INSTALLED NEW SERVICABLE SEAT RAIL IAW CRJ 900 AMM 53-00-49-400-801-A07.
Part: NONE — CORRODED · airframe 33,642 hrs · 23,357 cycles
L/H SIDE SEAT RAIL BETWEEN F.S.379 TO F.S.485 HAS MULTIPLE SPOTS OF CORROSION. REMOVED CORRODED L/H SIDE SEAT RAIL FROM F.S.379 TO F.S.485 AND INSTALLED NEW SERVICABLE SEAT RAIL IAW CRJ 900 AMM 53-00-49-400-801-A07.
Part: NONE — CORRODED · airframe 33,642 hrs · 23,357 cycles
R/H SIDE SEAT RAIL BETWEEN F.S.572 TO F.S.661+16 HAS MULTIPLE SPOTS OF CORROSION. REMOVED CORRODED R/H SIDE SEAT RAIL FROM F.S.572 TO F.S.661+16 AND INSTALLED NEW SERVICABLE SEAT RAIL IAW CRJ 900 AMM 53-00-49-400-801-A07 AND SRM 53-00-49-201-002-A01.
Part: INTERCOSTAL — CORRODED · airframe 33,642 hrs · 23,357 cycles
INTERCOSTAL BETWEEN F.S.349 TO F.S.369 AT STGR 26L TO 27 HAS MULTIPLE SPOTS OF CORROSION. REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW SERVICABLE INTERCOSTAL, I.A.W. CRJ 900 SRM'S, #51-40-11-001-001-A01, #51-42-06-001-001-A01 AND 51-42-21-001-001-A01. PROTECTIVE FINISHES REAPPLIED
Part: SKIN — CORRODED · airframe 33,642 hrs · 23,357 cycles
PASSENGER DOOR INNER SKIN IS CORRODED AT NUTPLATE HOLES FOR ACCESS PANEL. REMOVED UNSREVICEABLE PASSENGER DOOR INNER SKIN. INSTALLED A SERVICEABLE PASSENGER DOOR INNER SKIN IAW CRJ 900 SRM 51-20-11-001-001-A01, AND 51-42-06-001-001-A01.
Part: INTERCOSTAL — CORRODED · airframe 33,642 hrs · 23,357 cycles
PAX DOOR INTERCOSTAL DD7 , FWD SIDE IS CORRODED. REMOVED AND REPLACED INTERCOSTAL, I.A.W. CRJ 900 SRM'S #51-40-11-001-001-A01, #51-42-06-001-001-A01
Part: NONE — CORRODED · airframe 33,642 hrs · 23,357 cycles
PASSENGER DOOR INTERCOSTAL @ DD1A, AFT SIDE IS CORRODED REMOVED AND REPLACED INTERCOSTAL I.A.W. CRJ 900 SRM"S #51-40-11-001-001-A01, #51-42-06-001-001-A01.
Part: STRINGER — CORRODED · airframe 33,642 hrs · 23,357 cycles
STRINGER 22L CORRODED @FS 333.00 - 349.00 REMOVED AND REPLACED STRINGER 22L, I.A.W. CRJ 900 SRM'S #51-40-11-001-001-A01, @51-42-21-001-001-A01, 51-42-06-0001-001-A01.
Part: SUPPORT — CORRODED · airframe 33,642 hrs · 23,357 cycles
RH SIDE SEAT RAIL STRUCTURE F.S. 673-720 HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED SIDE SEAT RAIL STRUCTURE I.A.W. CRJ SRM'S # 51-40-11-001-001-A01, #53-00-49-201-002, AND AMM #53-00-49-400-801-A07
Part: SPLICE — CORRODED · airframe 33,642 hrs · 23,357 cycles
STGR SPLICE AT 26L, FS319.00 - FS333.00 CORRODED. REPLACED STRINGER SPLICE, I.A.W. CRJ 900 SRM'S, #51-40-11-001-001-A01, #51-42-06-001-001-A01. PROTECTIVE FINISHES REAPPLIED
Part: FRAME — CORRODED · airframe 33,642 hrs · 23,357 cycles
FRAME CORRODED, F S 847.00 +32, STGR 26L - STGR 26R. REPAIRED FRAME IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 & ENDEAVOR AIR EA CRJ953-13801, REV - IR, 06/17/2022.
Part: FRAME — CORRODED · airframe 33,642 hrs · 23,357 cycles
PAX DOOR FWD FRAME AT FS320.163 CORRODED. REMOVED AND REPLACED FRAME I.A.W. CRJ 900 SRM'S #51-40-11-0001-0001-A01, #51-42-06-001-001-A01.
Part: FRAME — CORRODED · airframe 33,642 hrs · 23,357 cycles
PAX DOOR FRAME CORRODED REMOVED AND REPLACED PAX DOOR FRAME, I.A.W. CRJ 900 SRM'S #51-40-11-001-001-A01, @51-42-21-001-001-A01, 51-42-06-0001-001-A01.
Part: FRAME — CORRODED · airframe 33,642 hrs · 23,357 cycles
FRAME CORRODED @FS 501.00, STGR 23L - 26R REMOVED AND REPLACED STUB FRAME, I.A.W. CRJ 900 SRM'S #51-40-11-001-001-A01, @51-42-21-001-001-A01, 51-42-06-0001-001-A01 AND REPAIRED REMAINING FRAME SEGMENT, I.A.W. ENDEAVOR AIR EA#CRJ953-13702,REV IR, 5/25/2022
2019
Part: BRACKET — DAMAGED · airframe 29,231 hrs · 19,560 cycles
"WHILE INCORP SB670BA-57-020, FOUND VISUAL DAMAGE IN AFT FAIRING BRACKET 7/16 FASTENERS HOLE ON RH & LH SIDE. " "C/W REO BOMBARDIER 690-57-21-329. REF ATTACHED REO FOR WORK PERFORMED . NO FURTHER ACTION REQUIRED. WVAC EMP #7195 "
Part: SKIN — DAMAGED (LT WING) · airframe 29,231 hrs · 19,560 cycles
"WHILE INCORP SB670BA-57-020, FUND 3 EA 2ND OVERSIZE HST+54 FASTENERS IN THE COLD WORK AREA. ""REPAIRED 4 EA 2ND OVERSIZE HOLES OT LHS LOWR WING ASSY AND AFT MLG DOOR HINGE AT WS 48.95 IAW REO 690-57-328 REV-- DATED 12-10-19. REF ATTACHED REO P1 & P2 FOR SIGNATURES. WVAC EMP 712 STAMP "
Part: SKIN — DENTED (RT WING TE FLAP) · airframe 29,231 hrs · 19,560 cycles
"RH IB FLAP LOWER T/E SKIN DENTED. MARKED WITH TAPE. ""C/W FALP REPAIR AT 2 LOCATIONS ON LOWER SURFACE OF RH IB FLAP IAW CRJ700 SRM 57-52-01-201-001-A01. WVAC EMP 712 STAMP "
Part: FITTING — DENTED · airframe 29,231 hrs · 19,560 cycles
TOOLING MARKS FOUND ON RH REAR SPAR NEAR REAR SPAR REINFORCEMENT FITTING "COMPLIED WITH BOMBARDIER REO# 690-57-21-330 REV.-- DATED 2019-12-10 FOR REPAIR. "
Part: HOUSING — CRACKED (E&E DOOR) · airframe 27,137 hrs · 17,963 cycles
INITIAL INSPECTION: CRACK WAS FOUND OF 2.500" LENGTH ON THE MAIN AVIONICS COMPARTMENT DOOR HANDLE HOUSING. ( REFERENCE: W.C 900-52-810-901) COMPLETE: SUMMARY OF NRC 00132:HANDLE HOUSING WAS REPLACED PER SRM 51-42-20-001-001-A01 PAR. 6.AND AMM 52-42-02-400-801 (CONFIG A01)
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 27,137 hrs · 17,963 cycles
HIDDEN DAMAGE: CORROSION WAS FOUND ON INTERCOSTAL OVER STRINGER 21L, BTW STA FS-310-349. IN REF JOB CARD R25120 STEP 10. COMPLETE: SUMMARY: INTERCOSTAL WAS REPLACED PER SRM 51-41-02-001-001-A01 PAR.6
2018
Part: ACM — ODOR (LEFT) · airframe 27,059 hrs · 17,911 cycles
ODOR OF BURNING PLASTIC FROM RECIRC VENTS IN CRUZ & CLIMB RAN ENGINE WITH CREW VERIFIED #1 PACK SOURCE OF SMELL REGARDLESS OF EN G. BLEED SELECTED. DEFERRED L/H PACK IAW MEL 21-51-1B. NOTIFIED MOC 98 628. ENTERED INTO MM02 PLACARD INSTALLED. JORDAN KIPP SKYSERVICE TROUBLESHOT WTH FIM TS#002737 OPS CHECK GOOD, NO DEFECTS FOUND, PLACAR D REMOVED MM02 UPDATED, MOC # 96183
Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,036 hrs · 17,894 cycles
EXIT ROWS BOTH SIDES EMERGENCY LIGHTS BULBS OUT. REMOVED AND REPLACE EXIT ROW EMERGENCY LIGHT BULBS IAW AMM 33-5 1-00.
Part: OXYGEN BOTTLE — LOW PRESSURE (PORTABLE) · airframe 25,489 hrs · 16,789 cycles
FWD PORTABLE OXYGEN BOTTLE HAD LOW PRESSURE. REMOVED & REPLACED THE PORTABLE OXYGEN BOTTLE IAW AMM 35-31-00.
Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 25,480 hrs · 16,783 cycles
FWD ENTRY CABIN EXIT SIGN IS BROKEN. REMOVED AND REPLACED THE EXIT SIGN IAW AMM 33-51-05.
2017
Part: ANGLE — CORRODED · airframe 24,461 hrs · 16,008 cycles
PAX DOOR SILL ANGLE HAS CORROSION AROUND SCREW HOLES. MAINTENANCE REPLACED SILL ANGLE.
Part: SEAT TRACK — CORRODED (BS 661) · airframe 24,461 hrs · 16,008 cycles
SEAT TRACK SEGMENT, STRINGER 15R, BS 661+16 - 661.90 CORRODED IN SEVERAL AREAS. MAINTENANCE REPLACED THE SEAT TRACK SEGMENT IAW EC/TC 670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 24,461 hrs · 16,008 cycles
CABIN SEAT TRACK SEGMENT, STRINGER 15L FROM BS 744.15 - 761.85 CORRODED IN SEVERAL AREAS. MAINTENANCE REPLACED THE SEAT TRACK SEGMENT IAW EC/TC 670-53-00-343.
Part: STRINGER SPLICE — CORRODED (BS 327-329) · airframe 24,461 hrs · 16,008 cycles
STRINGER SPLICE 25R, BS 329 - 327 FOUND CORRODED. MAINTENANCE REPLACED THE STRINGER SPLICE.
Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 24,461 hrs · 16,008 cycles
SEAT TRACK SEGMENT, LBL 9, BS 379 - 485 FOUND CORRODED. MAINTENANCE REPLACED THE SEAT TRACK SEGMENT IAW EC/TC 670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 785-844) · airframe 24,461 hrs · 16,008 cycles
CABIN SEAT TRACK SEGMENT, STRINGER 15R, BS 785.15 - 844 FOUND CORRODED. MAINTENANCE REPLACED THE SEAT TRACK SEGMENT IAW EC/TC 670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 24,461 hrs · 16,008 cycles
CABIN SEAT TRACK SEGMENT, STRINGER 15L FROM BS 744.15 - 761.85 CORRODED IN SEVERAL AREAS. MAINTENANCE REPLACED THE SEAT TRACK SEGMENT IAW EC/TC 670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 24,461 hrs · 16,008 cycles
CABIN SEAT TRACK SEGMENT, LBL 9, BS 661+32 - 693 CORRODED IN SEVERAL AREAS. MAINTENANCE REPLACED THE SEAT TRACK IAW EC/TC670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 785-844) · airframe 24,461 hrs · 16,008 cycles
CABIN SEAT TRACK SEGMENT, STRINGER 15L, BS 785.15 - 844 CORRODED. MAINTENANCE REPLACED THE SEAT TRACK IAW EC/TC 670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 24,461 hrs · 16,008 cycles
SEAT TRACK SEGMENT, LBL 9, BS 485 - 581 CORRODED. MAINTENANCE REPLACED THE SEAT TRACK SEGMENT IAW EC/TC 670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 485-571) · airframe 24,461 hrs · 16,008 cycles
CABIN SEAT TRACK SEGMENT CORRODED, STRINGER 15R, BS 485 - 571. MAINTENANCE REPLACED THE SEAT TRACK IAW EC/TC 670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 673-720) · airframe 24,461 hrs · 16,008 cycles
CABIN SEAT TRACK SEGMENT, STRINGER 15L, BS 673 - 720.85 CORRODED AT SEVERAL AREAS. MAINTENANCE REPLACED THE SEAT TRACK SEGMENT IAW EC/TC 670-53-00-343.
Part: ANGLE — CORRODED (BS 280 FLOORBEAM) · airframe 24,461 hrs · 16,008 cycles
FLOORBEAM ANGLE AT BS 280 IS CORRODED. MAINTENANCE REPLACED THE FLOORBEAM ANGLE.
Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 24,461 hrs · 16,008 cycles
CABIN SEAT TRACI SEGMENT, STRINGER 15R, BS 744.15 - 761.85 CORRODED IN SEVERAL AREAS. MAINTENANCE REPLACED THE SEAT TRACK SEGMENT IAW EC/TC 670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 673-720) · airframe 24,461 hrs · 16,008 cycles
CABIN SEAT TRACK SEGMENT STRINGER 15 FROM BS 673 - 720.85 FOUND CORRODED AT SEVERAL AREAS. MANTENANCE REPLACED THE SEAT TRACK IAW EC/TC 670-53-00-343
Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 24,461 hrs · 16,008 cycles
CABIN SEAT TRACK SEGMENT RBL 9, FROM BS 661+32 - 693 CORRODED IN SEVERAL AREAS. MAINTENANCE REPLACED THE SEAT TRACK SEGMENT IAW EC/TC 670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 24,461 hrs · 16,008 cycles
CABIN SEAT TRACK SEGMENT, LBL 9, BS 581 - 661+32 FOUND CORRODED IN SEVERAL AREAS. MAINTENANCE REPLACED THE SEAT TRACK SEGMENT IAW EC/TC 670-53-00-343.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 24,461 hrs · 16,008 cycles
CORRODED INTERCOSTAL AT LBL2 BETWEEN FRAMES 349 & 364. MAINTENANCE REPLACED INTERCOSTAL BETWEEN FRAMES 349 AND 364.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,461 hrs · 16,008 cycles
CABIN SEAT RAIL SEGMENT LBL 27 AND FROM FS 364-485 CORRODED IN SEVERAL AREAS. MAINTENANCE REPLACED SEAT RAIL SEGMENT WITH A NEW FABRICATED ONE IAW EC/TC 670-53-00-343.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 24,461 hrs · 16,008 cycles
CORRODED INTERCOSTAL AT RBL2 BETWEEN FRAMES 349 & 364. MAINTENANCE REPLACED INTERCOSTAL.
Part: FLOOR SUPPORT — CORRODED (BS 394-409) · airframe 24,461 hrs · 16,008 cycles
CORRODED FLOOR SUPPORT LBL 2, BS 394 AND 409. MAINTENANCE REPLACED THE FLOOR SUPPORT.
Part: SKIN — CRACKED (FUSELAGE) · airframe 23,307 hrs · 15,185 cycles
A/C EXTERNAL POWER RECEPTACLE BRACKET ASSY AND SURROUNDING STRUCTURE REQUIRES PERMANENT REPAIR. C/W EC/TC REO 670-53-11-029 01 AND EC/TC REO 670-53-11-844.
2016
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 21,816 hrs · 14,154 cycles
MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14, REF IPC 25-61-14, FIG 1, ITEM 5.
2015
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,847 hrs · 12,752 cycles
DURING CRJ LINE CHECK FOUND LT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. EXTERIOR EMERGENCY LIGHTS, ACFT NOT OPERATED AT NIGHT. LEFT AFT OVERWING EVERGENCY LIGHT OPS CHECKS GOOD IAW MM 33-51-00 PLACARD REMOVED.
Part: BATTERY PACK — INOPERATIVE (MEGAPHONE) · airframe 19,625 hrs · 12,604 cycles
MEGAPHONE DOES NOT WORK. R & R BATTERY IAW AMM 25-61-05.
Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 19,525 hrs · 12,532 cycles
PAX DOOR HARD TO OPERATE. LUBED AND OPS CHECKED PAX DOOR, OK FOR SERVICE, IAW AMM 52-11-00.
Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 19,515 hrs · 12,524 cycles
SERVICE DOOR EMERENCY EXIT LENS CRACKED. R & R EMERGENCY EXIT LENS ON SERVICE DOOR BY UNSNAPPING OLD LENS AND SNAPPING ON NEW LENS.
Part: SKIN — CORRODED (BS 302) · airframe 19,515 hrs · 12,524 cycles
EXTERNAL FUSELAGE SKIN CORRODED AT LOWER TCAS MOUNT AREA. REMOVED CORROSION AT LOWER TCAS ATENNA MOUNT AREA, FS 302 IAW SRM 51-21-06-001-001-A01. BLEND AREA IN A DAMAGE ALLOWED AREA REF SRM 53-21-01-101-002-A02, FIG 53-21-01-991-854. SUBMITTED TO STS ENGINEERING FOR PERMANENT DISPOSITION. COMPLIED WITH ECTC EA 32-2015-343.
Part: NUT PLATE — DAMAGED · airframe 19,515 hrs · 12,524 cycles
PANEL 323 AT HAS 2 DAMAGED NUTPLATES, AT THE AIR INLET. R & R 2 EA NUTPLATES AT THE AIR INLET IAW SRM 51-42-06-001-001-AO1 AND SRM 51-42-15-001-001-AO1. THIS REPAIR IS CLASSIFIED AS MAJOR/MINOR REPAIR IAW SOP 5702.
Part: SUPPORT ANGLE — CORRODED (DOOR FRAME) · airframe 19,515 hrs · 12,524 cycles
PAX DOOR FWD FRAME, SUPPORT ANGLE, CORRODED AT UPPER & LOWER CAM RECEPTACLES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001. REMOVED CORRODED FRAME IAW SRM 551-42-06-001-001. LOCATED, DRILLED AND INSTALLED NEW FRAME IAW SRM 51-42-06-001-001-A01.
Part: FLOORBEAM — CORRODED (BS 349) · airframe 19,515 hrs · 12,524 cycles
CORROSION ON CROSSBEAM AT FS 349 AND RBL9. R & R CORRODED PACKER C, FS349, RBL9 IAW SRM 51-42-06-001-001-A01.
Part: INTERCOSTAL — CORRODED (BS 310-349) · airframe 19,515 hrs · 12,524 cycles
CORROSION AT NUMEROUS POINTS ON INTERCOSTAL FROM BS 310-349 AND STR 20R. BLENDED CORROSION ON INTERCOSTAL FROM FS 310 TO FS 349 ON STR 20R IN REF TO SRM 51-21-06-001-001-A01. REMOVED INTERCOSTAL AND FWD GUSSET IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. CORROSION DAMAGE ON FWD INTERCOSTAL SECTION FROM FS 310 TO 319.70 FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED FASTENER LOCATIONS IN NEW INTERCOSTAL IAW SRM 51-40-11-001-001-A01. AFTER FURTHER EVALUATION FOUND DAMAGE ON INTERCOSTAL BETWEEN FS 319.70 TO FS 349 TO BE IN LIMITS. REMOVED 1 SUPPORT RAIL, PN SH670.50018-1 TO FOM IN REF TO SRM 51-42-06-001-001-A01. INSTALLED SUPPORT RAIL, PN SH670-50018-1 IAW SRM 51-42-06-001-001-A01 AND DWG NR SH670-31980. REMOVED FWD CLIP TO GAIN ACCESS TO THE INTERCOSTAL IN REF TO SRM 51-42-06-001-001-A01. INSTALLED FWD CLIP TO INTERCOSTAL AND FRAME IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31950. REMOVED OTBD RIVETS THAT ATTACH THE INTERCOSTAL TO STR 20 IN ORDER TO REMOVE INTERCOSTAL IN REF TO SRM 51-42-06-001-001-A01. INSTALLED OTBD RIVETS THAT ATTACH THE INTERCOSTAL TO STR (20) IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31950. REINSTALLED IAW DWG SH0670-31-950 AND SRM 51-42-06-001-001-A01. COMPLETED INSTALL OF INTERCOSTAL FS310-FS319.70 IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31950.
Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 19,515 hrs · 12,524 cycles
CORROSION ON RT FLOOR SILL BETWEEN FS349-364 AT THE FOLLOWING LOCATIONS: FS349, FS360 AND FS364. BLENDED CORROSION AT FS 349 -FS 360 + FS 364 IAW GREO 670-53-390. BLENDED AREA IS OUT OF ALLOWABLE LIMIT IAW REO 670-53-00-390. COMPLIED WITH EC/TC REO 670-53-00-390 AND REO 670-53-00-390, REV-DATED 01/22/2014 AS WRITTEN. COMPLIED WITH ECTC REO 690-53-21-770 AS REQUIRED.
Part: ANGLE — CORRODED (BS 280 FLOORBEAM) · airframe 19,515 hrs · 12,524 cycles
CORROSION ON MOUNTING ANGLE FOR PANEL 141ALF AT FS 280. BEYOND ALLOWABLE LIMITS IAW SRM 53-00-00-101-001-A01. REPLACED MOUNT ANGLE.
Part: DOOR — NO TEST (EMERGENCY EXIT) · airframe 19,515 hrs · 12,524 cycles
RIGHT FWD OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST. CLEANED AND LUBED RT FWD OVERWING EMERGENCY EXIT DOOR IAW AMM 12-20-52-640-815 A01. COMPLIED WITH FUNCTIONAL TEST OF THE RT FWD OVERWING EMERGENCY EXIT DOOR IAW AMM 52-21-00-720-803-A01.
Part: DOOR — NO TEST (EMERGENCY EXIT) · airframe 19,515 hrs · 12,524 cycles
LEFT FWD OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST. CLEANED AND LUBED LT FWD OVERWING EMERGENCY EXIT DOOR IAW AMM 12-20-52-640-815 A01. COMPLIED WITH FUNCTION TEST OF THE LT FWD OVERWING EMERGENCY EXIT DOOR IAW AMM 52-21-00-720-803-A10. FUNCTIONAL TEST GOOD.
Part: DOOR — NO TEST (EMERGENCY EXIT) · airframe 19,515 hrs · 12,524 cycles
LEFT AFT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST. CLEANED AND LUBED LT AFT OVERWING EMERGENCY EXIT DOOR IAW AMM 12-20-52-640-815-A01. COMPLIED WITH FUNCTIONAL TEST OF THE LT AFT OVERWING EMERGENCY EXIT DOOR IAW AMM 52-21-00-720-803-A01, FUNCTIONAL TEST GOOD.
Part: DOOR — NO TEST (EMERGENCY EXIT) · airframe 19,515 hrs · 12,524 cycles
RIGHT AFT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST. CLEANED AND LUBED RT AFT OVERWING EMERGENCY EXIT DOOR IAW AMM 12-20-52-640-815 A01. COMPLIED WITH FUNCTIONAL TEST OF THE RT AFT OVERWING EMERGENCY EXIT DOOR IAW AMM 52-21-00-720-803-A01.
Part: SEAT TRACK — CORRODED (BS 597-661) · airframe 19,515 hrs · 12,524 cycles
LT SIDE SEAT TRACK AT FS 597.00-661.00 IS CORRODED IN MULTIPLE AREAS. BLENDED LT SIDE SEAT RAIL AT FS597.00-661, FOUND TO BE OUT OF LIMITS IAW REO 670-53-000-013. REMOVED SEAT RAIL LT FS 597.00-661 IAW AMM 53-00-49-000-801. REMOVED AND INSTALLED NEW SERVICEABLE SIDE SEAT RAIL LT FS597.00-661.00 IAW AMM 53-00-49-000-801-A07 AND 63-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 19,515 hrs · 12,524 cycles
LT SIDE SEAT RAIL AT FS 485-581 IS CORRODED IN MULTIPLE AREAS. BLENDED IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SIDE SEAT RAIL AT FS485-581 IAW AMM 53-00-49-000-801. REMOVED SIDE SEAT RAIL AT FS485-581 IAW AMM 53-00-49-000-801-A07. RECEIVED ECTC REO INSTALLED NEW SERVICEABLE SEAT RAIL LT AT FS485-581 IAW AMM 53-00-49-400-801-A07. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343 REV L AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 865-977) · airframe 19,515 hrs · 12,524 cycles
RT SIDE SEAT TRACK IS CORRODED IN MULTIPLE AREAS FS 865-977. NO ALLOWABLE LIMITS ON RT SIDE SEAT RAIL FS 865-977 IAW REO 670-53-00-013 & SRM SUPPLEMENT 53-51-49. REMOVED RT SIDE SEAT RAIL FS 865 977 IAW AMM 53-00-49-000-801-A07. COMPLIED WITH ECTC/REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN. INSTALLED SEAT TRACK RT FS 865-977 IAW AMM 53-00-49-400-801-A07 MINUS 13 EA .2500" SCREWS AT FS 897-927. INSTALLED 13EA .2500" SCREWS IN RT SIDE SEAT RAIL AT FS 897-927 IAW AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 19,515 hrs · 12,524 cycles
SEAT TRACK RBL9 AT FS 349-485 IS CORRODED IN SEVERAL AREAS. REMOVED CORROSION ON SEAT TRACK RBL9 FS 349-485, SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. REMOVED SEAT TRACK RBL9, FS349-485 IAW AMM 53-00-49-000-801-807. COMPLIED WITH ECTC REO 670-53-1-343. GREO 670-53-00-343, REV L AS WRITTEN. INSTALLED SERVICABLE SEAT RAIL, RBL9 AT FS349-485 IAW 53-00-49-400-801-807.
Part: SEAT TRACK — CORRODED (BS 661) · airframe 19,515 hrs · 12,524 cycles
LT SIDE SEAT RAIL AT FS 661-00-661.00174 IS CORRODED IN MULTIPLE AREAS. BLENDED LT SIDE SEAT RAIL AT FS 661-661.00+74 AREA FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. RECEIVED ECTC/REO 670-53-00-343 AND COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN. REMOVED SEAT RAIL LT SIDE AT FS 661.00+661.00+74 IAW AMM 53-00-49-000-801-A07. INSTALLED NEW SEAT RAIL LT SIDE AT FS 661.00+ FS 661.00+74 IAW AMM 53-00-49-400-801-A07. FABRICATED LT SIDE SEAT RAIL AT FS 661.00-FS 661.00+74 IAW REO 670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 847-1000) · airframe 19,515 hrs · 12,524 cycles
SEAT TRACK, RBL 9 AT FS 847-1000 IS CORRODED IN MULIPLE AREAS. EVALUATED SEAT RAIL AT RBL 9, FS 847-FS 1000 & FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK AT RBL9, FS 847-1000 IAW AMM 53-00-49-000-801, A07. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN. INSTALLED SEAT TRACK AT RBL9, FS 847-1000 IAW AMM 53-00-49-400-801 A07.
Part: SEAT TRACK — CORRODED (BS 847-865) · airframe 19,515 hrs · 12,524 cycles
RT SIDE SEAT TRACK IS CORRODED IN MULTIPLE AREAS FS 847 - 865. RT SIDE SEAT RAIL AT FS 847.00+16-865, FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013 & SRM SUPPLEMENT 53-51-49. REMOVED RT SEAT RAIL AT FS 847+16-864 IAW AMM 53-00-49-000-801-A07. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN. INSTALLED SERVICEABLE SEAT RAIL IAW AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 847-897) · airframe 19,515 hrs · 12,524 cycles
LT SIDE SEAT RAIL AT FS 847 & 897 IS CORRODED IN MULTIPLE AREAS. BLENDED LT SIDE SEAT RAIL FS 847.0016-897 IAW SRM 51-21-06-001-001-A01. FOUND TO BE IN LIMITS IAW REO 670-53-00-013. AFTER FURTHER EVALATUION FOUND SEAT RAIL TO BE OUT OF LIMITS AT FS847.16-897 TO BE OUT OF LIMITS IAW RE 670-53-00-013. REMOVED SEAT RAIL FROM LT SIDE RAIL AT FS 847.16-897 IAW AMM 53-00-49-000-801-A07. INSTALLED NEW SERIVCEABLE SEAT RAIL LT FROM FS 847-907 IAW AMM 53-00-49-400-801-A07. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 19,515 hrs · 12,524 cycles
LT SIDE SEAT AT FS 744.15-761.85 IS CORRODED IN MULTIPLE AREAS. BLENDED LT SIDE SEAT RAIL FS 744.15-761.85 IAW SRM 51-21-06-001-001-A01 FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED LT SEAT RAIL AT FS 744-761 IAW AMM 53-0-49-000-801, A07. INSTALLED NEW SERVICEABLE SEAT RAIL LT AT FS 744-761 IAW AMM 53-00-49-400-801, A07.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 19,515 hrs · 12,524 cycles
SEAT TRACK IS CORRODED IN MULTIPLE AREAS RBL9 AT FS 485-581. BLENDED CORROSION AT RBL9 BS 485-581 FOUND TO BE OUT OF LIMITS IAW SRM SUPPLEMENT 53-31-49. REMOVED SEAT TRACK RBL9 AT FS 485-581 IAW AMM 53-00-49-000-801. FABRICATED SERVICEABLE SEAT RAIL IAW REO 670-53-00-343. INSTALLED SERVICEABLE SEAT RAIL RBL9 AT FS 485-581 IAW AMM 53-00-49-400-801. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 847-1000) · airframe 19,515 hrs · 12,524 cycles
SEAT TRACK, LBL 9 AT FS 847-1000 IS CORRODED IN MULTIPLE AREAS. BLENDED SEAT TRACK LBL9 FS 847.100 IAW SRM 51-21-06-001-001-A01. FOUND TO BE IN LIMITS IAW REO 670-53-00-013. UPON FURTHER EVALATUION FOUND SEAT TRACK AT LBL9, FS 847-1000 TO BE CORRODED OUT OF LIMITS IAW RE670-53-00-013. REMOVED SEAT RAIL AT FS 847-1000 AT LBL9 IAW AMM 53-00-49-000-801-A07. INSTALLED NEW SERIVCEABLE SEAT RAIL AT FS 847-FS1000 AT LBL9 IAW AMM 53-00-49-400-801-A07. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV C AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 661-720) · airframe 19,515 hrs · 12,524 cycles
RT SEAT TRACK IS CORRODED IN MULITIPLE AREAS FS 661.00+90-720.85. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. R & R SEAT TRACK ON RT SIDE BETWEEN FS 661.00+90 TO 720.85 IN REF TO AMM 53-00-49-000-801-A07 & 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 19,515 hrs · 12,524 cycles
LT SIDE SEAT RAIL AT FS 785.15-847.00 & 48 IS CORRODED IN MULTIPLE AREAS. BLENDED LT SIDE SEAT RAIL FS 785.15-847+48 IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT RAIL FROM LT SIDE RAIL AT FS 847.16-897 IAW AMM 53-00-49-000-801-A07. INSTALLED NEW SERVICEABLE SEAT RAIL LT FROM FS 847-907 IAW AMM 53-00-49-400-801-A07. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 693-847) · airframe 19,515 hrs · 12,524 cycles
SEAT TRACK, RBL9 AT FS 693.00-847 IS CORRODED IN MULITIPLE AREAS. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01, FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK RBL 9 FS 593-847 IAW AMM 53-00-49-000-801-A07. INSTALLED NEW SEAT RAIL AT RBL 9, FS 693-847 IAW AMM 53-00-49-400-801. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 19,515 hrs · 12,524 cycles
SEAT TRACK AT LBL9 IS CORRODED IN MULITIPLE AREAS FS 785-15 - 847+16. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01, FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK AT LBL9 FS 693-835 IAW AMM 53-00-49-000-801-A07. INSTALLED NEW SERVICEABLE SEAT RAIL AT LBL9 FS 693-835 IAW AMM 53-00-49-000-801. RECEIVED EC/TC REO 670-53-00-343. COMPLIED WITH EC/TC REO 670-53-00-343 & GREO 670-53-00-343, REV L AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 19,515 hrs · 12,524 cycles
RT SIDE SEAT RAIL IS CORRODED IN MULITIPLE AREAS FS 785-15 - 847+16. CORROSION OUT OF LIMITS ON SIDE SEAT RAIL RT BS 785.15-847+16 IAW SUPPLEMENT 53-31-49. REMOVED SIDE SEAT RAIL AT RT FS785.15-FS847+16 IAW AMM 53-00-49-000-801A-07. COMPLETED INSTALLATION OF SIDE SEAT RAIL RT AT FS785-847 IAW AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 19,515 hrs · 12,524 cycles
SEAT TRACK IS CORRODED IN MULITIPLE AREAS RBL9 AT FS 581-661.00+62. BLENDED CORROSION AT RBL 9, BS 581-661.00+62, FOUND TO BE OUT OF LIMITS IAW SRM SUPPLEMENT 53-31-49. REMOVED SEAT TRACK AT RBL9, FS 581-661.00+62, REF: AMM 53-00-49-000-801-A07. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN. INSTALLED SERVICEABLE SEAT TRACK AT RBL9 FS 581-661.00+62, REF: AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 897-1000) · airframe 19,515 hrs · 12,524 cycles
LT SIDE SEAT TRACK IS CORRODED IN MULTIPLE AREAS FS 897-1000. BEGAN TO BLEND CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. RECEIVED ECTC REO 670-53-00-343 COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN. REMOVED SIDE SEAT RAIL IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT RAIL FOR LT SIDE AT FS 897-1000 IAW REO 690-53-00-343, REV L. INSTALLED NEW SEAT RAIL LT SIDE AT FS 897-1000 IAW AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 785-820) · airframe 19,515 hrs · 12,524 cycles
LT SIDE SEAT TRACK AT FS 785.15-820 IS CORRODED IN MULTIPLE AREAS. BLENDED LT SEAT RAIL AT FS 785.15-820, FOUND TO BE OUT OF LIMITS IAW REO 670-53-000-013. DAMAGE IS OUT OF LIMITS OF ECTC REO 670-53-00-013. REMOVED LT SIDE SEAT RAIL AT FS 785.15-820 IAW AMM 53-00-49-000-801-A01. REMOVED SEAT RAIL AT FS 785.15-820 AT LT SIDE RAIL IAW AMM 53-00-49-000-801A-01. INSTALLED NEW SERVICEABLE SEATRAIL ON LT SIDE RAIL AT FS 785.15-FS820 IAW AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 19,515 hrs · 12,524 cycles
RT SIDE SEAT TRACK IS CORRODED IN MULTIPLE AREAS FS 485-581. EVALUATED SEAT RAIL AT RBL 9 BETWEEN FS 830.40 & 881 & FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT RAIL AT RBL9, FS 830.40-FS 881 IAW AMM 53-00-49-000-001-A07. REMOVED SEATRAIL AT RBL 9 FS 830.40 -FS 881 IAW AMM 53-00-49-000-001-A01-A07. COMPLIED WITH EC/TC 670-53-00-343 & GREO 670-53-00-343, REV L AS WRITTEN. INSTALLED NEW SERVICEABLE SEAT RAIL AT RBL9, FS 830.40, FS 881 IAW AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 19,515 hrs · 12,524 cycles
RT SEAT TRACK RAIL IS CORRODED IN MULITIPLE AREAS FS 581-661.00+16. CORROSION OUT OF LIMITS ON SEAT RAIL SIDE AT BS 581-661.00+16 IAW SRM SUPPLEMENT 53-31-49. REMOVED SIDE SEAT RAIL IAW AMM 53-00-49-000-801, CONFIG A07. COMPLIED WITH EC/TC 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN. INSTALLED NEW SEAT RAIL IAW AMM 53-00-49-400-801, CONFIG A07.
Part: FASTENER — MISSING (LIGHT RETAINER) · airframe 19,515 hrs · 12,524 cycles
LEFT LOGO LIGHT IS MISSING 1 FASTENER, CAMLOCK. REMOVED LOGO LIGHT RETAINER IAW CMM 33-43-70 PGS, ITEM 4B. INSTALLED NEW LOGO LIGHT RETAINER RING IAW CMM 33-43-70, PG 6, ITEM 8, D, SS. THIS REPAIR IS CLASSIFIED AS A MAJOR/MINOR REPAIR IAW SOP 5702.
Part: SKIN — CORRODED (PAX DOOR) · airframe 19,515 hrs · 12,524 cycles
PAX DOOR IS CORRODED UNDER PANEL 832AL, NUTPLATES. REMOVED OLD SKIN, LOCATED, DRILLED, INSTALLED NEW INNER SKIN IAW SRM 51-42-06-001-001, 51-42-13-001-001 & DWG 601R318024 & 601R31-702.
Part: LIGHT — MISSING (CABIN) · airframe 19,183 hrs · 12,288 cycles
PHOTOLUMINESCENT EMERGENCY STRIP IS MISSING NEAR FOYER IN FRONT OF CATERING CARTS. INSTALLED MISSING PHOTOLUMINESCENT STRIP IN GALLEY IAW AMM 33-13-01. ACFT OK FOR SERVICE.
Part: DOOR — ICED (MAIN PAX) · airframe 18,031 hrs · 11,522 cycles
MAIN CABIN DOOR WAS STUCK CLOSED. COULD MOVE THE HANDLE ABOUT 1/3 OPEN AND PARTIALLY OPERATE THE CAM LOCKS BUT THEN IT WOULD JAM. REMOVED ICE FROM PASSENGER DOOR AND PERFORMED OPS CHECK IAW AMM 52-11-00 AND PERFORMED OPS CHECK GOOD.
2014
Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 16,637 hrs · 10,591 cycles
MAIN CABIN DOOR HANDLE IS BINDING WHEN F/A ATTEMPS TO OPEN OR CLOSE THE DOOR. LUBED PAX DOOR HANDLE, DOOR OPS CHECKED GOOD IAW AMM 52-11-00. ACFT OK FOR SERVICE.
Part: MEGAPHONE — DAMAGED (CABIN) · airframe 16,252 hrs · 10,340 cycles
MEGAPHONE DAMAGED. R & R MEGAPHONE IAW AMM25-61-19, REF AIPC 25-61-19, ITEM5.
Part: ACM — SMOKE (LEFT) · airframe 15,465 hrs · 9,825 cycles
SMOKE IN THE CABIN WHEN LT PACK CAME ON LINE AND TEMP SPIKED TO 99 AND LT PACK AUTO FAIL CAUTION MESSAGE, AIR CONDITIONING PACKS, BOTH PACKS. R & R LT ACM IAW AMM 21-51-08. OPS CHECKED IAW 21-51-08, FIG 1, ITEM 10.
2013
Part: HANDLE — OUT OF ADJUST (PAX DOOR) · airframe 14,757 hrs · 9,390 cycles
FUNCTIONAL CHECK OF PAX DOOR FAILED. HANDLE EXCEEDED 16 POUNDS. ADJUSTED INNER HANDLE IAW AMM 52-11-02-820-801, STEPS 4B-3A-3E. OPS & FUNCTIONAL CHECKED GOOD.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 14,757 hrs · 9,390 cycles
AFTER REMOVING SERVICE DOOR MOUNTING ANGLE DUE TO CORROSION, FOUND SILL ANGLE CORRODED. REMOVED SILL ANGLE PN SH 670-31986-1 IAW SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01. DRILLED FASTENER LOCATIONS AND INSTALLED NEW SERVICABLE SILL ANGLE IAW SRM 51-42-06-001-001-A01 SRM 51-42-21-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-15-001-001-A01 IAW DWG SH670-31950. MAJOR REPAIR.
Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 14,757 hrs · 9,390 cycles
LT COCKPIT FLOORBEAM CRACKED. REPAIRED IAW SRM 51-24-21-001-001-A01 AND REO 690-53-11-576. MAJOR REPAIR.
Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 14,757 hrs · 9,390 cycles
RT COCKPIT FLOORBEAM CRACKED. FABRICATED REPAIR PARTS IAW SRM 51-24-21-001-001-A01. REPAIRED IAW ECTC REO 690-53-11-576. MAJOR REPAIR.
Part: FRAME — CORRODED (BS 295) · airframe 14,755 hrs · 9,389 cycles
CORROSION FOUND ON FRAME FS 295 AT STRINGER 25R. REPAIRED IAW SRM 53-00-01-101-001-A01 AND REO 690-53-61-402.
Part: STRINGER — CORRODED (BS 295-310) · airframe 14,757 hrs · 9,390 cycles
CORROSION FOUND ON STRINGER 26R BETWEEN BS 295 AND 310. REPAIRED IAW SRM 51-21-06-001-001-A01 & 63-21-03-201-002. MAJOR REPAIR.
Part: SILL — CORRODED (BS 319-349) · airframe 14,755 hrs · 9,389 cycles
CORROSION FOUND ON SERVICE DOOR SILL BETWEEN FS 319 - 349. REMOVED MOUNTING ANGLE AND LOWER SILL ANGLE IAW SRM 51-42-06-001-001-A01. DRILLED NEW SERVICEABLE MOUNTING ANGLE. INSTALLED NEW SERVICEABLE MOUNTING ANGLE IAW SRM 51-42-06-001-001-A01 & SRM 51-47-34-001-001-A01 IAW DWG SH670-31950. MAJOR REPAIR.
Part: SILL — CORRODED (BS 319-349) · airframe 14,755 hrs · 9,389 cycles
CORROSION FOUND ON PAX DOOR SILL BETWEEN BS 319 - 349. REMOVED PAX DOOR SILL IAW SRM 51-42-06-001-001-A01. REMOVED MID CAP ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED DEBURRED AND INSTALLED PAX DOOR SILL AND MIDCAP ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED DORRS SILL KICK PLATE IAW SRM 51-42-06-001-001-A01 SH670-31825 & SH670-3175. MAJOR REPAIR.
Part: SHEAR TIE — CORRODED (CORRODED) · airframe 14,749 hrs · 9,385 cycles
CORROSION AT FS 333 FRAME BETWEEN STRGS 27 AND 25R. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702. REPAIRED IAW SRM 53-21-06-001-001-A01 AND REO 690-53-21-544.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 14,744 hrs · 9,380 cycles
RT FS 280 FLOORBEAM CORRODED AND CRACKED AT RBL 11.5. REMOVED FLOORBEAM IAW SRM 51-42-06-001-001-A01. INSTALLED FLOORBEAM IAW SB670BA-53-041. REPAIR CLASSIFIED AS MAJOR.
Part: FLOOR SUPPORT — CRACKED · airframe 14,744 hrs · 9,380 cycles
FLOOR PANEL 195DL CHANNEL CRACKED, REMOVED CHANNEL IAW SRM 51-42-13-001-001-A01. LOCATED, DRILLED, DEBURED AND INSTALLED NEW SERVICEABLE CHANNEL IAW SRM 51-40-11-001-001-A01 AND DWG CC690-39302.
Part: STRUCTURE — CHAFED (BS 913) · airframe 14,744 hrs · 9,380 cycles
FUSELAGE HAS CHAFE DAMAGE AT APPROX BS 913.00 STR 27. REPAIRED IAW REO 670-53-00-290. REPAIR CLASSIFIED AS MAJOR.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 14,744 hrs · 9,380 cycles
FS 280 FLOORBEAM AT LBL 11.5 IS CRACKED. REMOVED LT FS 280 FLOORBEAM IAW SRM 51-42-06-001-001-A01 AND INSTALLED IAW SB670BA-53-041.
Part: FRAME — CORRODED (BS 349) · airframe 14,749 hrs · 9,385 cycles
CORROSION AT FS 349, FRAME BETWEEN LT INTERCOSTALS AT S26L. REPAIRED IAW SRM 51-21-06-001-001-A01 AND REO 690-53-21-544. MAJOR REPAIR.
Part: POST — CORRODED (DOOR FRAME) · airframe 14,744 hrs · 9,380 cycles
LT BOTTOM DOOR POST SKIN AT FS 280 IS CORRODED. REPAIRED IAW SRM 51-21-06-001-001-A01, SRM 53-00-00-101-001, AND REO 690-53-11-578. REPAIR CLASSIFIED AS MAJOR.
Part: FRAME — CORRODED (BS 319) · airframe 14,755 hrs · 9,389 cycles
CORROSION AT FS 319 FRAME BETWEEN S26L AND 26R. REMOVED CORROSION IAW SRM 51-42-06-001-001-A01; 51-21-06-001-001-A01 AND 53-21-06-101-002-A02.
Part: FRAME — CORRODED (BS 349) · airframe 14,749 hrs · 9,385 cycles
CORROSION AT FS 349 FRAME BETWEEN RT INTERCOSTALS AT S26R. REPAIRED IAW SRM 51-21-06-001-001-A01 AND REO 690-53-21-544.
Part: FRAME — CORRODED (BS 295) · airframe 14,755 hrs · 9,389 cycles
CORROSION AT BS 295 FRAME BETWEEN STRINGERS 26L AND 26R. REPAIRED IAW SRM 5-42-06-001-001-A01;51-21-06-001-001-A01;53-21-06-101-002-A02 AND REO 690-53-21-544.
Part: FLOOR SUPPORT — CRACKED (BS 278) · airframe 14,749 hrs · 9,385 cycles
PANEL 221ALF RT SIDE SUPPORT ANGLE IS CRACKED AT APPROX FS 278. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702. REMOVED RT SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED UP NEW SUPPORT ANGLE IAW SRM 51-40-11. INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG CC670-33199 AND CC670-33052.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,744 hrs · 9,380 cycles
FS 280, FLOORBEAM CORRODED. REPAIRED IAW SRM 53-21-43-201-002-A01. REPAIR CLASSIFIED AS MAJOR.
Part: FLOOR SUPPORT — CORRODED (BS 278) · airframe 14,749 hrs · 9,385 cycles
PANEL 221ALF LT SIDE SUPPORT ANGLE IS CRACKED AT APPROX FS 278. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702. REMOVED ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED UP NEW SUPPORT ANGLE IAW SRM 51-40-11. INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG CC670-33199 AND CC670-33052.
Part: POST — CORRODED (BS 280) · airframe 14,744 hrs · 9,380 cycles
RT BOTTOM DOOR POST SKIN AT FS 280 IS CORRODED. REPAIRED IAW SRM 51-21-06-001-001-A01, 53-00-00-101-001, AND REO 690-53-11-577. REPAIR CLASSIFIED AS MAJOR.
Part: FRAME — CORRODED (BS 310) · airframe 14,755 hrs · 9,389 cycles
CORROSION AT FS 310, FRAME BETWEEN STRINGERS 26L AND 25R. REPAIRED IAW SRM 5-42-06-001-001-A01;51-21-06-001-001-A01;53-21-06-101-002-A02 AND REO 690-53-21-544.
Part: SEAT TRACK — CORRODED (BS 708) · airframe 14,744 hrs · 9,380 cycles
LEFT SEAT TRACK AT FS 708 CORRODED. REMOVED SEAT TRACK BETWEEN FS 672 - 722 IAW AMM 53-00-49-000-801-A07. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801. REPAIR CLASSIFIED AS MAJOR.
Part: SEAT TRACK — CORRODED (BS 708) · airframe 14,744 hrs · 9,380 cycles
RIGHT SIDE SEAT TRACK AT BS 708 CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-000-801, 53-00-49-400-801 AND ECTC REO 670-53-00-343, REV D.
Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 14,744 hrs · 9,380 cycles
RT FLOOR SEAT RAIL FROM BS 349 - 485 HAS SEVERAL SPOTS OF CORROSION, OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-000-801.
Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 14,744 hrs · 9,380 cycles
RT FWD ELECTRIC BAY FLOOR IS CRACKED BY ADG STOW PUMP. REPAIRED IAW GREO 670-53-11-509. REPAIR CLASSIFIED AS MAJOR.
Part: FRAME — DENTED (BS 1108) · airframe 14,757 hrs · 9,390 cycles
FOUND DENT LOCATED ON THE AFT SIDE OF THE FRAME JUST ON FWD SIDE OF THE AFT EQUIP BAY DOOR OPENING. R & R DAMAGED FRAME FWD SIDE OF THE AFT EQUIP BAY DOOR AT FS 1108 IAW SRM 51-40-06, 51-42-11. REMOVED AND DRILLED ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01. INSTALLED NEW SERVICABLE ANGLE IAW SRM 51-42-06-001-001. MAJOR REPAIR
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 13,654 hrs · 8,660 cycles
GALLEY EXIT LIGHT COVER MISSING ON REAR OF GALLEY. INSTALLED FLOODLIGHT LENS COVER IAW AMM 33-51-11. OPS CHECK GOOD. NEF CLEARED ACFT OK FOR SERVICE.
2012
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 12,239 hrs · 7,734 cycles
EMERGENCY OVERWING LIGHT INOPERATIVE ON RT AND LT SIDE AND SOME INTERIOR LIGHTS INOPERATIVE. CHARGED EMERGENCY LIGHT BATTERIES, PERFORMED AN OPS CHECK OF THE EMERGENCY LIGHTS IAW AMM 33-51-00 AND FOUND NO DEFECT.
Part: DATA PLATE — MISSING (MEGAPHONE) · airframe 12,239 hrs · 7,734 cycles
MEGAPHONE DATA PLATE IS MISSING. R & R THE MEGAPHONE IAW AMM 25-61-14. OPS CHECKED GOOD. SDR CLOSED.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 11,910 hrs · 7,509 cycles
FS 280 FLOORBEAM CRACKED AT LBL 9.0. REPAIRED LEFT FS 280 CROSSBEAM BY REPLACING BEAM IAW REO 690-53-11-092.
2011
Part: WARNING SYSTEM — FALSE ACTIVATION (BLEED AIR SYS) · airframe 9,611 hrs · 5,938 cycles
EN ROUTE FROM MIA TO DCA RECEIVED LEFT BLEED DUCT WARNING MSG. EMERGENCY DECLARED, A/C DIVERTED TO MCO LANDED SAFELY. INSPECTED LEFT BLEED DETECTION LOOPS IN AFT EQUIPMENT BAY. NO DEFECTS NOTED, OPS CHECK GOOD.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 8,851 hrs · 5,457 cycles
FS 280 FLOORBEAM CORRODED LBL9 RBL 27. REMOVED AND REPLACED FS 280 FLOORBEAM IAW REO 690-53-11-092.
Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 3 · airframe 8,851 hrs · 5,457 cycles
FS 280 RT LOWER BULKHEAD WEB AT CABIN FLOOR LINE CORRODED. REMOVED LOWER SECTION OF FS 280 RT BULKHEAD WEB, FABRICATED AND INSTALLED NEW SECTION IAW SRM 53-11-10-201-003-A01.
Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 3 · airframe 8,851 hrs · 5,457 cycles
FS 280 LT LOWER BULKHEAD WEB AT CABIN FLOOR LINE CORRODED. REMOVED LOWER SECTION OF FS 280 LT BULKHEAD WEB, FABRICATED AND INSTALLED NEW SECTION IAW SRM 53-11-10-201-003-A01.
Part: SELECTOR VALVE — FAILED (MLG) · airframe 8,713 hrs · 5,372 cycles
ON APPROACH INTO BHM RECEIVED GEAR DISSAGREE MSG. EMERGENCY DECLARED, PERFORMED MANUAL GEAR EXTENSION. A/C LANDED SAFELY. REMOVED AND REPLACED MLG SELECTOR VALVE. OPS CHECK GOOD.
2010
Part: PANEL — CRACKED (PAX DOOR) · airframe 7,888 hrs · 4,862 cycles
PAX DOOR FWD SIDE PANEL CRACKED IN ZONE 2. REPAIRED PAX DOOR FWD SIDE ZONE 2 BY REMOVING DAMAGE AND INSTALLING DOUBLER IAW REO 670-52-11-104.
Part: SELECTOR VALVE — FAILED (LANDING GEAR) · airframe 7,602 hrs · 4,672 cycles
ON APPROACH INTO MEM RECEIVED GEAR DISAGREE MSG. FOLLOWED QRH, EMERGENCY DECLARED. A/C LANDED SAFELY. REMOVED AND REPLACED MAIN LANDING GEAR SELECTOR VALVE.
Part: PSEU — FAULTY (LANDING GEAR) · airframe 7,270 hrs · 4,455 cycles
ON APPROACH INTO JFK WHEN LANDING GEAR WAS SELECTED DOWN GEAR DID NOT EXTEND, RECEIVED GEAR DISAGREE. EMERGENCY DECLARED, FOLLOWED QRH ALL GEAR EXTENDED MANUALLY. A/C LANDED SAFELY. REMOVED AND REPLACED PSEU. NO FURTHER DEFECTS NOTED.
2009
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 4,421 hrs · 2,761 cycles
ON FINAL APPROACH INTO CVG RECEIVED FLAPS FAIL CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY. CLEARED INHIBITS PER FIM 27-50-00, MSG CLEARED. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED.
Part: SENSOR — FAULTY (BLEED AIR SYS) · airframe 4,167 hrs · 2,610 cycles
EN ROUTE FROM CHS TO ATL RECEIVED LEFT BLEED DUCT WARNING MSG. EMERGENCY DECLARED, A/C RETURNED TO CHS LANDED SAFELY. REMOVED AND REPLACED LEFT BLEED TEMP SENSOR.
Part: SENSING ELEMENT — FAULTY (BLEED AIR SYS) · airframe 4,144 hrs · 2,593 cycles
EN ROUTE FROM IAH TO JFK RECEIVED LEFT BLEED DUCT MSG. EMERGENCY DECLARED, A/C DIVERTED TO AEX LANDED SAFELY. REMOVED AND REPLACED SENSING ELEMENT MT 225.
Part: DOOR — OPEN (AC POWER) · airframe 13,830 hrs · 9,835 cycles
AC POWER DOOR LEFT OPEN, A/C RETURNED TO JFK LANDED SAFELY. INSPECTED AC POWER DOOR, NO DEFECTS NOTED. SECURED DOOR CLOSED.
2008
Part: DOOR — OPEN (EXTERNAL POWER) · airframe 2,460 hrs · 1,500 cycles
AFTER T/O LOUD NOISE COMING FROM NOSE AREA, SUSPECTED EXTERNAL ACCESS PANEL LEFT OPEN. EMERGENCY DECLARED, A/C RETURNED BACK TO IAH AND LANDED SAFELY. INSPECTED A/C AND FOUND EXT PWR RECEPTACLE DOOR OPEN. INSPECTED DOOR NO DEFECTS NOTED, CLOSED DOOR.
Part: LANDING GEAR — MALFUNCTIONED (NLG) · airframe 1,605 hrs · 1,030 cycles
FLIGHT 5099 - GEAR DISAGREE MESSAGE RECEIVED ON CLIMB. NOSE GEAR NOT RETRACTING. DECLARED EMERGENCY, FOLLOWED QRH, RETURNED TO CVG, ALL GEAR SHOWED GREEN, LANDED WITHOUT INCIDENT. VISUALLY INSPECTED NOSE GEAR, PERFORMED EXTENSION AND RETRACTION CHECKS. NO DEFECTS FOUND.
Part: LOOP — OUT OF POSITION (OVERHEAT SYS) · airframe 1,565 hrs · 1,005 cycles
FLIGHT 5056- ON CLIMB-OUT FROM AUS TO ATL, RECEIVED LEFT BLEED DUCT WARNING MESSAGE. EMERGENCY DECLARED AND A/C RETURNED BACK TO AUS AND LANDED SAFELY. REPOSITIONED INSULATION AND LOOPS AT HP GROUND DUCT. OPS CHECK GOOD.
Part: ECU — MALFUNCTIONED (NLG STEERING) · airframe 1,358 hrs · 882 cycles
FLIGHT 5210 - ON APPROACH INTO CVG RECEIVED NOSE WHEEL STEERING INOP CAUTION MESSAGE. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. RESET NOSE WHEEL STEERING SYSTEM C/B'S AND ECU. OPS CHECK GOOD.