N928XJ
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Endeavor Airlines | Operator | 2023-01-02 – 2023-01-02 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
PAX DOOR AFT GAS STRUT MOUNTING BRACKET IS CRACKED. REPLACED PAX DOOR AFT GAS STRUT MOUNTING BRACKET P/N 601R318011-1 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.
POSSIBLE CRACK ON FORWARD LUG OF THE DOOR SIDE OF THE PAX DOOR HINGE. REPLACEED PAX DOOR HINGE P/N 601R318073-5 IAW CRJ900 SRM 52-11-01-201-002-A01
FORWARD FORMER ON PAX DOOR IS CORRODED ON LOWER ATTACH FLANGE. REMOVED AND REPLACED PAX DOOR FWD FORMER ANGEL IAW CRJ900 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
L/H FWD AVIONICS EQUIPMENT COMPARTMENT DECK CRACKED AT FRAME CUTOUT AT FS193. REPAIRED IAW CRJ900 SRM 53-11-43-201-001-A01
PAX DOOR CUTOUT KICKPLATE SILL ANGLE IS CORRODED. REMOVED PAX DOOR KICKPLATE SILL ANGLE IAW CRJ-900 SRM 51-42-06-001-001-A01 51-42-21-001-001-A01 LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR KICKPLATE PN#SH670-31875-7S IAW CRJ-900 SRM 51-40-11-001-001-A01 INSTALLED PAX DOOR KICKPLATE IAW CRJ-900 SRM 51-42-06-001-001-A01 51-42-21-001-001-A01
VERTICAL STAB. LH AFT DRAG ANGLE IS CRACKED. REMOVED AND INSTALLED SERVICEABLE AFT DRAG ANGLE LH SIDE WITH PN: AV670-21186-003 IAW CRJ900 SRM 51-42-21-001-001-A01, 51-42-14-001-001-A01 AND 51-42-27-001-001-A01 :
FWD GALLEY EMERGENCY LIGHT MISSING INSTALLED GALLEY EMERGENCY LIGHT IAW CRJ 900 AMM 33-51-01, ALL CHECKS GOOD.
PERSISTANT SMELL IN GALLEY AND FIRST FOUR ROWS THROUGHT FLIGHT, IRRITTING BOTH FA'S AND CA'S THROAT AND NASAL PASSAGES, THOUGH IT WAS DE-ICE FLUID, BUT SMELL PERSISTED FOR OVER 2 HOURS, NO COMPLAINTS FROM PAX, FA'S WERE FINE TO CONTINUE TO DESTINATION, BUT WE DEFINITLEY CAN'T DO ANOTHER FLIGHT IN THOSE CONDITIONS GROUND RAW PACK SYSTEM, INSPECTED FWD AND AFT LAV'S INSPECTED GALLEY AND GALLEY HEATER, NO DISCREPANCYS NOTED, NO ODORS DETECTED, IAW AMM 21-51-00 OK FOR SERVICE PER MOC 96045
INITIAL INSPECTION : CRACK IN CANISTER, WELDED NO.3 IN STA WS148 AT RH MAIN FUEL TANK. (AD) CANISTER, WELDED NO.3 IN STA WS148 AT RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV."--" LEAK TEST WAS PERFORMED AND NO LEAK WAS FOUND PER CRJ900 AMM 28-11-00-- 790-801 (CONF A01).
HIDDEN DAMAGE [DURING REMOTION OF STIFFENER IN REF NRC 452: CRACK ON SKIN AT ACCESS 172CR AND 171CL. (FUS). SUMMARY: SKIN AT ACCESS 172CR AND 171CLL WAS REPAIRED PER REO 670-53-82-430 REV. --
PARTS RACK: CORROSION ON STRAPS LH/RH AT WING FAIRING 193AB. (FUS) SUMMARY: STRAPS LH/RH AT WING FAIRING 193AB WERE REPLACED FOR NEW ONES PER CRJ900 SRM 51-42-10-001-001-A01 (LEVEL CORROSION 2)
INITIAL INSPECTION. CORROSION ON FLOOR SEAT RAIL RBL9 BTW FS 691-836, 836-847+51, 847+51 -977. (TCI 100-20). FLOOR SEAT RAIL RBL9 BTW FS691-836, 836-847+51 AND 847+51-977 AT PAX CABIN FWD WET AREA WAS REPLACED PER CRJ-900 AMM 53-00-49-000-801 PAR. C (CONFIG.A07). CORROSION LEVEL 2.
AWR; [TASK R53520 STEP 7]; CORROSION ON FLOOR SEAT RAIL IN SECTIONS [FS= 375 TO FS= 409, 9LBL] AT PAX CABIN FWD WET AREA. (W1) (CPAX). FLOOR SEAT RAIL IN SECTIONS FS375 TO FS409 AND 9LBL AT PAX CABIN FWD WET AREA WERE REPLACED FOR NEW ONES PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A07). LEVEL CORROSION 2.
AWR; [TASK R53520 STEP 7]; CORROSION ON FLOOR SEAT RAIL IN SECTIONS [FS= 364 TO FS= 409, 27LBL] AT PAX CABIN FWD WET AREA. (W1) (CPAX). FLOOR SEAT RAIL IN SECTIONS FS364 TO FS409 AND 27LBL AT PAX CABIN FWD WET AREA WAS REPLACED PER CRJ-900 AMM 53-00-49-000-801 PAR. C (CONFIG.A07). CORROSION LEVEL 2.
INITIAL INSPECTION. CORROSION ON FLOOR SEAT RAIL LBL9 BTW FS 691-836, 836-847+51 AND 847+51 -985. (TCI 100-20). FLOOR SEAT RAIL LBL9 BTW FS691/836, FS836/847+51 AND FS847+51/985 WERE REPLACED FOR NEW ONES PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A07).
PART RACK. WEAR ON ACCESS PANEL 584ET, 684ET, 584EB, 684EB AT RH/LH FLAPS. WEAR ON ACCESS PANEL 584ET, 684ET, 584EB, 684EB AT RH/LH FLAPS WAS BLENDED PER CRJ-900 SRM 51-12-00-001-001-A01. ORIGINAL THICKNESS IS 0.090"" ON ACCESS PLATE 684 EB AND 584 EB MAXIMUM DEPTH REMOVED 0.003"" THEREFORE IT IS WITHIN LIMITS PER CRJ-900 SRM 57-52-01-101-001-A01. ORIGINAL THICKNESS IS 0.050"" ON ACCESS PLATE 584 ET AND 684 ET MAXIMUM DEPTH REMOVED IS 0.030"" THEREFORE IT IS OUT LIMITS PER CRJ-900 SRM 57-52-01-10 1-001-A01 (ACCESS PLATE 584 ET AND 684 ET WERE REPLACED WITH NEW ONES) PARTS: 584 ET AND 684ET WERE REPLACED)
AWR; [TASK R53520 STEP 7]; CORROSION ON FLOOR SEAT RAIL IN SECTIONS [FS= 349 TO FS= 409, 9RBL] AT PAX CABIN FWD WET AREA. (W1) (CPAX). SIDE SEAT RAIL BTW SECTIONS FS349 TO FS409 AND 9RBL WERE REPLACED FOR NEW ONES PER CRJ-900 AMM 53-00-49-000-801 (CONFIG A07). CORROSION LEVEL 2.
INITIAL INSPECTION: CORROSION ON FLOOR SUPPORT BEAM LBL27 BTWN. FS1015 AND FS1051.30 AT AFT BAGGAGE BAY COMPARTMENT. (CCT)(TCI 200-09). FLOOR SUPPORT BEAM LBL27 BTW FS 1015 AND FS 1051.30 AT AFT BAGGAGE COMPARTMENT WAS REPAIRED PER CRJ-900 SRM 53-00-41-201-001-A03 AND SRM 51-42-21-001-001-A01. (LEVEL CORROSION 2).
INITIAL INSPECTION: CORROSION ON FLOOR SUPPORT BEAM LBL9 BTWN. FS 1051.30 AND FS1000 AT AFT BAGGAGE BAY COMPARTMENT. (CCT)(TCI 200-09). FLOOR SUPPORT BEAM LBL9 BTW FS1051.30 AND FS1000 AT AFT BAGGAGE COMPARTMENT WAS REPAIRED PER CRJ-900 SRM 53-00-41-201-001-A03 AND SRM 51-42-21-001-001-A01. (LEVEL CORROSION 2).
INITIAL INSPECTION: CORROSION ON FRAME FS1015 BTWN. STGR. 25L AND 26L AT AFT BAGGAGE BAY COMPARTMENT.(CCT)(TCI 200-09). SUMMARY OF NRC S/N 00295: CORROSION ON FRAME FS1015 BTWN. STGR. 25L AND 26L AT AFT BAGGAGE BAY COMPARTMENT WAS REPAIRED WHIT EA NO: CRJ953-09842. REV. IR (LEVEL CORROSION 1)
INITIAL INSPECTION: CORROSION ON FRAME FS1031 BTWN. STGR. 22L AND 25L AT AFT BAGGAGE BAY COMPARTMENT.(CCT)(TCI 200-09). SUMMARY OF NRC S/N 00296: CORROSION ON FRAME FS1031 BTWN. STGR. 22L AND 25L AT AFT BAGGAGE BAY COMPARTMENT WAS REPAIRED PER EA NO: CRJ953-09841. REV. IR (LEVEL CORROSION 1)
INITIAL INSPECTION: CORROSION ON FRAME FS613 BTW STGR 26L-26R AT FWD BAGGAGE BAY COMPARTMENT. (C1)(TCI: 53-20-306). CORROSION ON FRAME FS613 BTW STGR 26L-26R AT FWD BAGGAGE BAY COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND BLENDED AREAS WERE MEASURED AND FOUND WHIT THE FOLLOWING DIMENTIONS: ORIGINAL THICKNESS: 0.063"", REMAINING THICKNESS IS 0.061"" THEREFORE IS WITHIN LIMITS PER CRJ-900 SRM 53-31-06-101-003-A04, LEVEL CORROSION 1.
INITIAL INSPECTION: CORROSION ON FRAME FS581 BTW STGR 26L-26R AT FWD BAGGAGE BAY COMPARTMENT. (C1)(TCI: 53-20-306). CORROSION ON FRAME FS581 BTW STGR 26L-26R AT FWD BAGGAGE BAY COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND BLENDED AREAS WERE MEASURED AND FOUND WHIT THE FOLLOWING DIMENTIONS: ORIGINAL THICKNESS: 0.063"", REMAINING THICKNESS IS 0.059"" THEREFORE IS WITHIN LIMITS PER CRJ-900 SRM 53-31-06-101-003-A04, LEVEL CORROSION 1.
INITIAL INSPECTION: CORROSION ON FRAME FS1047 BTWN. STGR. 27 AND 26L AT AFT BAGGAGE BAY COMPARTMENT. (CCT) (TCI 200-09). SUMMARY OF NRC S/N 000290: FRAME FS1047 BTWN. STGR. 27 AND 26L AT AFT BAGGAGE BAY COMPARTMENT WAS REPAIRED WHIT EA NO: CRJ953-09802. REV. IR
AWR: CORROSION ON SETTLEMENT OF TIRES BURST ACCESS PANELS 542AZ/542BZ AT LH MLG REAR SPAR. (FYT)(TCI:500-13E1). SUPPORT WAS REPLACED PER CRJ-900 SRM 51-42-10-001-001- A01
INITIAL INSPECTION: CORROSION ON FRAME FS501 BTW STGR 26L-26R AT FWD BAGGAGE BAY COMPARTMENT. (C1)(TCI: 53-20-306). CORROSION ON FRAME FS501 BTW STGR 26L-26R AT FWD BAGGAGE BAY COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-06, BLENDED AREAS WERE MEASURED AND FOUND WHIT THE FOLLOWING DIMENTIONS: ORIGINAL THICKNESS: 0.050"", REMAINING THICKNESS IS 0.047"" THEREFORE IS WITHIN LIMITS PER CRJ-900 SRM 53-31-06-101-003-A04. EQUIPMENT: DIAL INDICATOR P/N: 543-783, DUE DATE: 04/JUN/20, N/C 1252 RCG, LEVEL CORROSION 1.
INITIAL INSPECTION: CORROSION ON FRAME FS533 BTW STGR 26L-26R AT FWD BAGGAGE BAY COMPARTMENT. (C1)(TCI: 53-20-306). CORROSION ON FRAME FS533 BTW STGR 26L-26R AT FWD BAGGAGE BAY COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND BLENDED AREAS WERE MEASURED AND FOUND WHIT THE FOLLOWING DIMENTIONS: ORIGINAL THICKNESS: 0.050", REMAINING THICKNESS IS 0.046" THEREFORE IS WITHIN LIMITS PER CRJ-900 SRM 53-31-06-101-003-A04 (LEVEL CORROSION 1).
INITIAL INSPECTION: CORROSION ON FRAME FS549 BTW STGR 26L-26R AT FWD BAGGAGE BAY COMPARTMENT. (C1)(TCI: 53-20-306). CORROSION ON FRAME FS549 BTW STGR 26L-26R AT FWD BAGGAGE BAY COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND BLENDED AREAS WERE MEASURED AND FOUND WITH THE FOLLOWING DIMENTIONS: ORIGINAL THICKNESS: 0.050", REMAINING THICKNESS IS 0.047" THEREFORE IS WITHIN LIMITS PER CRJ-900 SRM 53-31-06-101-003-A04, LEVEL CORROSION 1.
INITIAL INSPECTION: CORROSION ON STGR 27 BTW FS556-581 AT FWD BAGGAGE BAY COMPARTMENT. (C1)(TCI: 53-20-306). CORROSION ON STGR 27 BTW FS556-581 AT FWD BAGGAGE BAY COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND AREAS WERE MEASURED AND FOUND WHIT THE FOLLOWING DIMENTIONS: ORIGINAL THICKNESS: 0.120", REMAINING THICKNESS IS 0.112" THEREFORE IS WITHIN LIMITS PER CRJ-900 SRM 53-31-03-101-003-A04. LEVEL CORROSION 1.
INITIAL INSPECTION: CORROSION ON FRAME FS661+32 BTW STGR 26L-26R AT FWD BAGGAGE BAY COMPARTMENT. (C1)(TCI: 53-20-306). CORROSION ON FRAME FS661+32 BTW STGR 26L-26R AT FWD BAGGAGE BAY COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 PAR 5D, BLENDED AREA WAS MEASURE AND FOUND WITH THE FOLLOWING DIMENTIONS: ORIGINAL TICKNESS 0.063", REMAINING TICKNESS: 0.059", THEREFORE ITS WITHIN LIMITS PER CRJ-900 SRM 53-31-06-101-003-A04 EQUIPMENT: DIAL INDICATOR, P/N:543-783, DUE DATE: 23/APR/20. LEVEL CORROSION 1.
INITIAL INSPECTION: CORROSION ON FRAME FS661 BTW STGR 26L-26R AT FWD BAGGAGE BAY COMPARTMENT. (C1)(TCI: 53-20-306). FRAME FS661 BTW STGR 26L-26R AT FWD BAGGAGE BAY COMPARTMENT WAS REPAIRED PER CRJ900 SRM 53-00-06-201-001-A03. (LEVEL CORROSION 2).
INITIAL INSPECTION: CORROSION ON FRAME FS597 BTW STGR 26L-26R AT FWD BAGGAGE BAY COMPARTMENT. (C1)(TCI: 53-20-306). CORROSION ON FRAME FS597 BTW STGR 26L-26R AT FWD BAGGAGE BAY COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-06, BLENDED AREAS WERE MEASURED AND FOUND WHIT THE FOLLOWING DIMENTIONS: ORIGINAL THICKNESS: 0.063", REMAINING THICKNESS IS 0.060" THEREFORE IS WITHIN LIMITS PER CRJ-900 SRM 53-31-06-101-003-A04. EQUIPMENT: DIAL INDICATOR P/N: 543-783, DUE DATE: 04/JUN/20, N/C 1252 RCG. LEVEL CORROSION 1.
INITIAL INSPECTION. CORROSION ON STRINGER SPLICE 26LH IN STA. FS= 329 TO FS= 339 AT MAIN AVIONICS COMPARTMENT. (E/E)(TCI:53-20-304). STRINGER SPLICE 26LH IN STA. FS= 329 TO FS= 339 WAS REPLACED PER CRJ-900 SRM 51-42-06. CORROSION LEVEL 2
INITIAL INSPECTION. CORROSION ON FLOOR SUPPORT IN STA. FS= 280 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT.(TCI:53-20-304) (E/E). FLOOR SUPPORT IN STA. FS= 280 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06 AND SRM 51-42-20 CORROSION LEVEL 2.
INITIAL INSPECTION: CORROSION ON FRAME IN STA. FS= 319 BETWEEN STRG 25 LH TO 27 AT MAIN AVIONIC COMPARTMENT. (E/E)(TCI:53-20-304. SUMMARY:CORROSION ON FRAME IN STA. FS= 319 BETWEEN STRG 25 LH TO 27 AT MAIN AVIONIC COMPARTMENT. FRAME WAS MEASURED AND FOUND WITHIN LIMITS PER CRJ 900 SRM 53-00-06-201-005-A01.
INITIAL INSPECTION: CORROSION ON FRAME IN STA. FS= 295 BETWEEN STRG 25 LH TO 26RH AT MAIN AVIONIC COMPARTMENT. (E/E)(TCI:53-20-304). SUMMARY: CORROSION ON FRAME IN STA. FS= 295 BETWEEN STRG 25LH TO 26RH WAS REMOVED PER CRJ900 SRM 51-21-06.FRAME WAS MEASURED AND FOUND WITHIN LIMITS PER CRJ 900 SRM 53-00-06-201-005-A01.
INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAIL BTWN. SECTIONS FS477 TO FS581, FS581 TO FS661.00+16, FS661.00+16 TO FS693.00 AT 9RBL , FS581 TO FS661.00+16, FS661.00+16 TO FS693.00 AT 9LBL ALSO FS477 TO FS581, FS581 TO FS661.00+16 AT 27LBL.(CPAX). TCI :(53-20-245). SEATS RAIL BTW SECTIONS FS477 TO FS581, FS581 TO FS661.00+16 AND FS661.00+16 TO FS693.00 AT 9RBL, FS581 TO FS661.00+16 AND FS661.00+16 TO FS693.00 AT 9LBL ALSO FS477 TO FS581 AND FS581 TO FS661.00+16 AT 27LBL WERE REPLACED FOR NEW ONES PER CRJ-900 AMM 53-00-49-000-801 (CONFIG A07). CORROSION LEVEL 2.
INITIAL INSPECTION. CORROSION ON INTERCOSTALS (2EAS) BTW FS349-364 AND (2EAS) FS394-411, STGR 26L-26R. (TCI 53-20-313) AFTER REMOVAL PAINT AND CLEANING INTERCOSTALS (2EAS) BTW FS349-364 WERE RE-INSPECTED PER CRJ 900 SRM 51-26-00-001-001-A01 STEP 3 E, AND NO CORROSION WAS NOTED, INTERCOSTALS (2EAS) BTW FS 394 TO FS 411, STGR 26L-26R WERE REPLACED PER CRJ-900 SRM 51-42-06 AND SRM 51-42-20 CORROSION LEVEL 2.
CRACK WAS FOUND WITH 0.456 OF LENGTH ON FLOOR BEAM FS 275 AND 12 RBL PREVIOUS REPAIR ON BEAM FS 275 AND 12RBL WAS REPLACED PER REO 690-53-11-1185 REV
INITIAL INSPECTION: CORROSION ON SIDE SEAT RAIL BTWN. SECTIONS FS677 TO FS720.85, FS744.15 TO FS761.85, FS785.15 TO FS847.00+8.40, FS847.00+8.40 TO FS881.00,FS881.00 TO FS977.00 AT STGR 15LH/15RH.(CPAX). (TCI: 53-20-233). SIDE SEAT RAIL BTW SECTIONS FS677 TO FS720.85, FS744.15 TO FS761.85, FS785.15 TO FS847.00+8.40, FS847.00+8.40 TO FS881.00 AND FS881.00 TO FS977.00 AT STGR 15LH/15RH WERE REPLACED FOR NEW ONES PER CRJ-900 AMM 53-00-49-000-801 (CONFIG A07). CORROSION LEVEL 2.
INITIAL INSPECTION: CORROSION ON SIDE SEAT RAIL BTWN. SECTIONS FS379 TO FS469, FS469 TO FS477, FS477 TO FS565, FS565 TO FS661, FS661 TO FS661.00+90,FS661.00+90 TO FS677 AT STGR 15LH/15RH.(CPAX) SIDE SEAT RAIL BTW SECTIONS FS379 TO FS469, FS469 TO FS477, FS477 TO FS565, FS565 TO FS661, FS661 TO FS661.00+90 AND FS661.00+90 TO FS677 AT STGR 15LH/15RH WERE REPLACED FOR NEW ONES PER CRJ-900 AMM 53-00-49-000-801 (CONFIG A07). CORROSION LEVEL 2.
INITIAL INSPECTION: WEAR ON DOUBLER AND TRIPLER REPARATION BTW FS913 AND FS927, STGR 26LH TO 26RH. (FUS). SUMMARY: DOUBLER AND TRIPLER BTW FS913 AND FS927, STGR 26LH TO 26RH WERE REPLACED AND FUSELAGE SKIN WAS REPAIRED PER REO 670-53-00-290 REV F
INITIAL INSPECTION: CORROSION ON ANGLE STRAPS SUPPORT STRUCTURE OF AFT WING-TO-FUSELAGE FAIRING AT FS847+32. (FUS)(TCI: 53-20-260). ANGLES STRAPS SUPPORT STRUCTURE OF AFT WING-TO-FUSELAGE FAIRING WERE REPLACED FOR A NEW ONES PER CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6C
INITIAL INSPECTION: FRETTING CORROSION ON BODY TO FUSELAGE FAIRING ANGLE SUPPORT AT FS847. (FUS). ANGLE SUPPORT WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-13-001-001-A01 PAR. 6C.
INITIAL INSPECTION. CORROSION ON ANGLE AT SERVICE DOOR LOWER SILL. (TCI 53-20-219) ANGLE AT SERVICE DOOR LOWER SILL WAS REPLACED PER CRJ-900 SRM 51-42-06. CORROSION LEVEL 2
INITIAL INSPECTION. CORROSION ON CLIPS (4EAS) AND PROTECTOR WEB FITTINGS (4EAS) ON SERVICE DOOR LOWER SILL PROTECTOR PLATE SUPPORTS. (TCI 53-20-219). CLIPS (4EAS) AND PROTECTOR WEB FITTINGS (4EAS) ON SERVICE DOOR LOWER SILL PROTECTOR PLATE SUPPORTS WERE REPLACED PER CRJ-900 SRM 51-42-06 AND SRM 51-42-21. CORROSION LEVEL 2.
INITIAL INSPECTION: CORROSION ON INTERCOSTAL DD6 BTW FORMER FS320.163 AND FS329.41 AT PASSENGER DOOR. (L1)(TCI: 52-10-301). SUMMARY LEVEL CORROSION 2.- INTERCOSTAL DD6 BTW FORMER FS320.163 AND FS329.41 AT PASSENGER DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-01-001-001-A01
INITIAL INSPECTION. CORROSION ON SEAL STRIKER AT SERVICE DOOR LOWER SILL. (TCI 53-20-219) SEAL STRIKER AT SERVICE DOOR LOWER SILL WAS REPLACED PER CRJ900 SRM 51-42-06. CORROSION LEVEL 2
AWR:IN REF EO R53582 WEAR ON LP GROUND CONNECTION PLATE.(SM)(FUS). LP GROUND CONNECTION PLATE WAS REPAIRED PER EA CRJ953-09785 RV: IR
INITIAL INSPECTION: WEAR ON FWD SEAL RETAINER AT FWD BAGGAGE BAY DOOR SURROUND STRUCTURE. (C1) SUMMARY: FWD SEAL RETAINER AT FWD BAGGAGE BAY DOOR SURROUND STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01 AND CRJ-900 SRM 51-42-06-001-001-A01
INITIAL INSPECTION: WORN HINGE PLATES ON LOWER CUT OUT ACCESS PANEL 122CR AND 122DR. (FUS). ACCESS PANEL 122CR WAS REPLACED PER EA CRJ953-09836 REV IR AND ACCES PANEL 122DR WAS REPLACED PER EA CRJ953-09806 REV IR.
INITIAL INSPECTION: CRACK ON SUPPORT OF AC GROUND POWER CONNECTION RECEPTACLE. (FUS). RECEPTACLE SUPPORT WAS REPLACED PER CRJ/900 SRM 51-42-13-001-001-A01
EMERGENCY LIGHTS OUT IN BETWEEN ROWS 7 THRU 11. FOUND CEILING EMERGENCY LIGHT ABOVE ROW 9 INOP. RECONNECTED CANNON PLUG OPS TEST GOOD IAW AMM 33-51-00.
FLIGHT ATTENDANT OBSERVED A STRONG ELECTRICAL ODOR COMING FROM THE GALLEY FORWARD AREA. THIS WAS FOLLOWED BY A GALLEY HEATER OVERHEAT LIGHT. CONFIRMED SMELL COMING FROM GALLEY HEATER, DEFERRING THE GALLEY HEATER IAW MEL 21-40-1. ALL MAINTENANCE PROCEDURES COMPLIED WITH. REMOVED AND REPLACED GALLEY HEATER IAW AMM 21-23-64. OPS CHECKS GOOD.
ELT FAILED THE G SWITCH TEST. INSTALLED A NEW ELT IAW AMM 25-62-02. OPS TESTED GOOD IAW 25310700. NO DEFECTS NOTED.
SMOKE FWD LAV WARNING JUST PRIOR TO PUSHBACK DEACTIVATED FWD LAV SMOKE DETECTOR IAW CRJ900 AMM 26-16-01. DEFERRED F OR LAV SMOKE DETECTOR IAW MEL 26-16-1. PLACARD INSTALLED ENTERED INTO MM02. M PROCEDURES C/W. PER MOC 96074. R AND R'D FWD LAV SMOKE DET IAW AMM 26-16-01. OPS CHECK GOOD. THIS CLEARS DM #3428015-1. MOC 96184. REMOVED FROM MM02 . PLACARD REMOVED
EXTERIOR EMERGENCY LIGHT BY THE SERVICE DOOR INOPERATIVE. REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY FOR BATTERY PACK NR 2 IAW AMM 33-51-17. OPS CHECKED NORMAL. LIGHT WORKS NORMALLY.
EMER FLASHLIGHT BY BOARDING DOOR INOP. R&R FLASHLIGHT HOLDER ASSY IAW AMM 25-61-02. OK FOR SVC.
PILOT SIDE OXYGEN MASK PURGE AND EMERGENCY MASK DOES NOT WORK. REMOVED CAPTAINS MASK IAW AMM 35-11-12. INSTALLED A NEW MASK IAW TA 001714-R1. OPS CHECKED GOOD, NO DEFECTS NOTED. OK FOR SERVICE.
BS 264 FRAME HAS CORROSION BETWEEN STRINGERS 26L AND 26R ON STIFFENER ANGLE. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06.
EXTERNAL SKIN BS 900, STRINGER 27 REPAIR DOUBLER AND RIVETS CHAFED. REPAIRED THE SKIN DOUBLER IAW REO 670-53-00-290.
INTERNAL FWD JACK FITTING AT BS 278 INBD AND OTBD LOWER FLANGES ARE CORRODED. REMOVED AND REPLACED THE SUPPORTS IAW SRM 51-42-06.
PASSENGER DOOR AFT DRAG ANGLE IS CRACKED. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 52-11-04.
LONGERON 21R HAS CORROSION JUST FWD OF BS 379. REMOVED AND REPLACED UPPER JOINT PIECE BETWEEN BS 364 AND 379 AT FWD WASTE AND WATER DOOR IAW IAW SRM 51-42-06 AND SRM 51-42-21. REPAIRED IAW EA 953-05800.
PAX DOOR CENTER FIXED STEP IS CRACKED IN CENTER OF TREAD. REMOVED & REPLACED PAX DOOR STEP IAW SRM 51-42-20.
PAX DOOR AFT WEB IS CRACKED UNDER COUNTER BALANCE. REMOVED & REPLACED THE PAX DOOR AFT WEB IAW SRM 51-42-06, & 51-42-13.
PAX DOOR AFT DRAG ANGLE IS CRACKED. REMOVED & REPLACED THE AFT DRAG ANGLE IAW SRM 51-42-06.
FOUND SUPPORT ANGLE ON THE RT BULKHEAD WEB FWD FACE CRACKED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-42-06, 51-42-13, & 51-42-21.
RBL 9 SEAT TRACK FROM BS 847+57 - 990 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-55-00-343, AND AMM 53-00-49.
STRINGER 20R INTERCOSTAL HAS CORROSION BETWEEN BS 349 AND 364. REMOVED & REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND 51-42-21.
STRINGER 26R HAS CORROSION BETWEEN BS 333 AND 349. REMOVED & REPLACED STRINGER IAW SRM 51-42-06, AND 51-42-21.
PAX DOOR FWD WEB IS BENT AROUND UPPER HANDRAIL. REPAIRED THE PAX DOOR FWD WEB IAW REO 670-52-11-848, REV A.
AFTER REMOVING THE FLOORBEAM ANGLE AT BS 280 FOUND CORROSION ON THE RT FLOORBEAM. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACE IAW SRM 51-42-06, 51-42-13, AND 51-42-21.
LEFT BS 280 BULKHEAD WEB IS CORRODED OUT OF LIMITS. REPAIRED IAW REO 670-53-11-594, REV A.
LBL 9 SEAT TRACK, BS 837 - 847+57 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-343, AND AMM 53-00-49.
RBL 9 SEAT TRACK, BS 837 - 847+57 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-343, AND AMM 53-00-49.
BS 280 FLOORBEAM HAS CORROSION UNDERNEATH TITANIUM UPPER CAP ANGLE BETWEEN LBL 12 AND LBL 16. REMOVED AND REPLACED IAW SRM 51-42-06, 51-42-13, & 51-42-21.
FLOORBEAM ANGLE AT BS 280 UPPER SURFACE HAS CORROSION BETWEEN RBL 12 AND LBL 12. REMOVED AND REPLACED IAW SRM 51-42-06, AND 51-42-21.
BS 280 RT BULKHEAD WEB HAS CORROSION, AND FOUND OUT OF LIMITS. REPAIRED IAW REO 670-53-11-594 REV A.
THE LOWER TCAS ANTENNA INTERNAL CHANNEL IS CORRODED. REMOVED & REPLACED THE ANTENNA INTERNAL CHANNEL IAW SRM 51-42-06.
FUSELAGE STRINGER 25R HAS CORROSION BETWEEN BS 333 AND 349. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-06.
FWD SERVICE DOOR EMER EXIT LIGHT PANEL NOT ILLUMINATING. REPAIRED BROKEN WIRE BEHIND THE LIGHT ASSEMBLY IAW AMM 33-51-05 AND 20 -10-01. OPS CHECK SATISFACTORY. A/C OK FOR SVC.
EICAS FOR EMERGENCY LIGHTS ON DISPLAYED. CABIN EMERGENCY LIGHT SWITCH CYCLED. BATTERY POWER AT ALL TIMES. APU ON WITH GENERATOR ON. SERVICE DOOR EMERGENCY LIGHT AND EXTERIOR LIGHTS ON. R & R THE NR 2 EMERGENCY LIGHT CHARGER AND POWER SUPPLY IAW AMM 33-51-17. OP CHECKED GOOD.
LEFT, FORWARD MOST SECTION OF EMERGENCY EXIT LIGHTING ALONG FLOOR IS MISSING. R&R EMERGENCY FLOOR TRACK IAW AMM 33-51-01. OPC GOOD, OK FOR SVC.
STALL FAIL CAUTION CAME ON DURING CLIMB LOW SPEED CUE CRAWLED TO 290KT S AND STICK SHAKER CAME ON AND OFF INTERMITTENTLY. REMOVED AND REPLACED THE RT ANGLE-OF-ATTACK TRANSDUCER IAW AMM 27-35-05. PERFORMED OPERATIONAL TEST OF THE RT ANGLE-OF-ATTACK TRANSDUCER IAW AMM 27-35-05-710-801. OPERATIONAL TEST PASSED.
FWD LAV SMOKE DETECTOR DOES NOT TEST. REMOVED AND REPLACED FWD LAV SMOKE DETECTOR IAW AMM 26-16-1, OPS CHECKED GOOD.
EMERGENCY LIGHT IN GALLEY NR 2, BULBS INOPERATIVE. REPLACED THE BULBS IAW AMM 33-51-11. OPS CHECKED GOOD.
DURING PREFLIGHT INSPECTION, FLIGHT ATTENDANT NOTIFIED THAT ROW 13 EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE. FOUND BATTERY PACK NR 5 WILL NOT TAKE A CHARGE. REMOVED CEILING PANEL & BATTERY PACK NR 5 IAW AMM 33-51-17. NR 5 BATTERY PACK INOPERATIVE. R & R BATTERY PACK PS 38, NO FIX. R & R BATTERY PACK PS 37 IAW JC 33-900-701. OPS CHECKED GOOD. INSTALLED ORIGINAL BATTERY PACK AT PS 38. OPS CHECKED GOOD IAW AMM 33-51-17.
LEFT & RIGHT OVERWING AFT EMER LIGHTS INOPERATIVE. REPAIRED RT OVERWING EXIT LIGHT BY RE-TORQUEING GND STUD IAW AMM 33-51-15-400-801-A08. INSTALLED A NEW CONTACT, PN 001104-200-02, ONTO THE WIRE FOR LT AFT EMER EXIT IAW ESPM 20-16-00. OPERATIONS TESTED GOOD.
FLOOR PHOTO LUMINESCENT TRACK LIGHTING HAS A BROKEN TRACK & TOP COVER MISSING. INSTALLED SERVICEABLE PHOTO LUMINESCENT TRACK LIGHT & TOP COVER IAW AMM 33-51-01-400-801 A21.
PASSENGER DOOR FLOOR SILL ANGLE IS CORRODED. CONTINUATION CARD 81519011 OP 61. R & R SILL ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 & 51-40-11-001-001-A01.
SUPPORT ANGLE FOR FLOORBOARD 141ALF AT FS 280 IS CORRODED. R & R FLOORBOARD SUPPORT ANGLE AT FS 280 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 & 51-42-15-001-001-A01.
PRE-DOCK & POST DOCK. LT WING JACK POINT HELI COIL INSERT & NYLON PLUG MISSING. JACK POINT FITTING REQUIRES REPLACEMENT. CONTINUATION CARD 81519016 OP 17. R & R JACK POINT FITTING IAW SRM 51-42-21-001-001-A01 & 51-40-11-001-001-A01.
COPILOT EMER FLASHLIGHT INOPERATIVE. R & R COPILOT'S FLASHLIGHT BATTERY IAW CMM 25-60-02. FLASHLIGHT OPERATIONS CHECKED OK IAW MM 25-61-00-710-801-A04.
TWO EACH INTERCOSTAL BELOW SERVICE DOOR, BETWEEN FS 319 - 349 ARE CORRODED. CONTINUATION CARD 81519011 OP 69. R & R DAMAGE INTERCOSTAL IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 & 51-40-11-001-001-A01.
FRAME SECTOR AT FS 533 IS CORRODED BELOW LT FLOOR SILL. CONTINUATION CARD 81519011 OPS 66 & 74. CUT OUT CORRODED SECTION IAW SRM 53-00-06-201-001-A03. PERFORMED EDDY CURRENT IAW SRM 53-00-06-201-001-A03 STEP 6C. INSTALLED REPAIR SECTION IAW SRM 53-00-06-201-001-A03.
FLOOR SUPPORT J ANGLE AT FS 280 IS CORRODED, BETWEEN RBL 12 TO LBL 12. R & R FS 280.00 FWD J ANGLE, PN CC670-34095-3 IAW SRM 51-42-06-001-001-A01.
SERVICE DOOR FLOOR SILL & SILL ANGLE HAVE AREAS OF CORROSION, BETWEEN FS 319 - 349. CONTINUATION CARD 81519011 OP 75. R & R THE SERVICE DOOR FLOOR SILL & SILL ANGLE IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
EMERGENCY TRACK LIGHTING LOCATED AT LT NR 1 EXIT IN THE FWD POSITION IS DAMAGED. REPLACED LT NR 1 FWD SECTION OF EMER TRACK LIGHTING IAW AM 33-51-01-400-801 A21.
SEAT TRACK SEGMENT HAS CORROSION, BETWEEN FS 661+46 TO FS 693 AT RBL 9. R & R SEAT TRACK IAW AMM 53-00-49-000 400-801-A07, SRM 51-40-11-001-001-A01 & REO 670-53-00-343 REV M DATED 2015 10 19.
FOUND CORROSION ON FRAME AT FS 349, BETWEEN STRINGERS 27 & 26R. CONTINUATION CARD 81519011 OP 68. REMOVED FRAME SECTION AT FS 349, STRINGER 23L & 24L IAW SRM 51-42-06-001-001-A01. INSTALLED FRAME SECTION IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 & 51-77-00-001-001-A01.
FS 280 LT BEAM CRACKED. REMOVED & INSTALLED NEW LT CROSSBEAM FS 280 IAW SRM 51-42-06-001-001-A01, 51-42-22-001-001-A01, 51-77-00-001-001-A01 & 51-40-11-001-001-A01.
CLIP IS CORRODED ATTACHING TO J ANGLE & SIDE POST AT FS 280 & RBL 11. REMOVED CORRODED RT & LT FWD J ANGLE ATTACH CLIPS. INSTALLED NEW SERVICEABLE CLIPS IAW SRM 51-42-06-001-001-A01.
SEAT TRACK SEGMENT AT LBL 9 IS CORRODED, BETWEEN FS 661+46 TO FS 693. R & R SEAT TRACK IAW AMM 52-00-49-000 400-801-A07, SRM 51-40-11-001-001-A01 & 670-53-00-343 REV REV M DATED 2015 10 19.
SEAT TRACK SEGMENT AT LBL 9 IS CORRODED, BETWEEN FS 581 TO FS 661+46. R & R SEAT TRACK IAW AMM 53-00-49-000 400-801-A07 & SRM 51-40-11-001-001-A01, REO 670-53-00-343 REV M DATED 2015 10 19.
FRAME SECTOR AT FS 645 IS CORRODED BELOW LT FLOOR SILL. CONTINUATION CARD 81519011 OP 65. CUT OUT CORRODED SECTION, BETWEEN STRINGER 16L - 14L IAW SRM 53-00-06-201-001-A03. PERFORMED EDDY CURRENT & INSTALLED REPAIR SECTION IAW SRM 53-00-06-201-001-A03 TO INCLUDE STEP 6C.
FIRST OFFICERS FLASHLIGHT, RED LIGHT NOT BLINKING. REPLACED BATTERY PACK IAW CMM 25-60-02. OPERATIONS CHECKED GOOD.
EMERGENCY FLOOR LIGHT STRIP MISSING IN GALLEY. REPLACED EMER FLOOR LIGHT STRIP IAW AMM 33-51-00.
PANEL 195AB, RT SIDE HINGE WORN. REPLACE THE WORN HINGE WITHIN 100FH IAW EA CRJ953-03841. HINGE PNA CC670-39111-3, BUSHING PN NAS76A4-009P. NO FURTHER ACTION REQUIRED.
FLOOR LUMINESCENT STRIP IN FRONT OF SEAT 12G COME OFF. SECURED IAW AMM 33-61-01. ALL CHECKED GOOD, OK FOR SVC.
PILOTS EMER FLASHLIGHT INOPERATIVE. REPLACED BATTERY PACK PN P4-01-0021 IAW CMM 25-60-11. OPERATIONS CHECKED GOOD.
EMERGENCY LIGHT FLOOR LIGHTING 12B LOOSE. ATTACHED EMER LIGHT FLOOR LIGHTING 12B IAW AMM 33-50-01.
TASK CARD 900-71-430-103 TOP SIDE OF NR 1 ENG PYLON PANEL 433BT IS CHAFED OTBD AFT. LOCATED & DRILLED NEW PANEL FASTENER HOLES. REMOVED STIFFENERS FROM OLD PANEL & INSTALLED ON NEW PNL IAW SRM 51-42-00-001-001-A01. PAINTED NEW PNL IAW SRM 51-25-01-001-001-A01.
TASK CARD CR FWD AVIONICS COMPARTMENT DOOR CRACKED ON INTERIOR CTR WHERE HANDLE CTR ROTATING ROD GOES INTO THE DOOR FRAME. IF YOU TAKE THE EXTERIOR HANDLE & WIGGLE IT LOOK AT THE BASE OF THE HANDLE FOR CRACK. R & R AVIONICS BAY DOOR HANDLE IAW AMM 52-42-03-000-801-A01 & AMM 52-42-03-400-801-A01. R & R AVIONICS BAY DOOR IAW AMM 52-420-000-801-A01 & AMM 52-42-00-400-801-A01. PERFORMED OPERATIONS CHECK OF AVIONIC BAY DOOR. OPERATIONS CHECKED GOOD IAW AMM 52-42-000-710-801-A01.
TASK CARD 900-26-430-100 LT ENG AFT CORE EXHAUST COWL HAS CHAFE SPOTS AT PYLON TO COWL. REPAIRED CHAFED AREAS ON LT CORE COWL IAW SRM 54-13-00-201-006-A01.
TASK CARD 900-26-440-100 RT ENG AFT CORE EXHAUST COWL HAS CHAFE MARKS AT THE PYLON TO COWL INTERFACE. REPAIRED CHAFED AREAS ON RT CORE COWL IAW SRM 54-13-00-201-006-A01.
TASK CARD 900-71-430-100 LT ENG LOWER CORE COWLING HAS CHAFE DAMAGE TO FIRE SEALS. REPAIRED AREA IAW EO R54090.
TASK CARD 900-53-900-106 RIVET PUSHED IN ON THE BOTTOM OF THE FUSELAGE BY 919.00 & SMALL DENT WHERE RIVET IS LOCATED. REPAIRED AREA IAW EO R53545.
TASK CARD 900-71-440-100 RT ENG LWR CORE COWL AFT Z FIRE SHIELD BENT ON CORNERS. REPAIRED IAW EA CRJ954-02612.
TASK CARD 900-71-440-100 RT ENG LOWER CORE COWLING HAS CHAFE DAMAGE ON FIRE SEAL. REPAIRED FIRE SHIELD IAW EO R54090.
TASK CARD 900-53-900-101 LT SEAT TRACK IN FRONT OF FWD LAVATORY HAS CORROSION ON FWD END. R & R LT SEAT TRACK IN FRONT OF FWD LAVATORY IAW AMM 53-00-49-000-801-A07 & AMM 53-00-49-400-801-A07.
RIGHT SEAT TRACK IN FRONT OF FWD LAVATORY HAS CORROSION ON FWD END. R & R RT SEAT TRACK FWD OF LAVATORY IAW AMM 53-00-49-000-801-A07 & 53-00-49-400-801-A07.
PAX DOOR ASSIST CABLE PULLEY BRACKET CRACKED. R & R PAX DOOR ASSIST CABLE PULLEY BRACKET IAW SRM 51-42-22-001-001-A01, STEPS 11 & 9.
TASK CARD 900-25-280-101 WIFI RACK SIDE COVER CRACKED. REPAIRED WIFI RACK SIDE COVER IAW ER NR CRJ946-02602 REV 1R.
TASK CARD 900-25-900-907 FIRST CLASS 1 EACH EMERGENCY LIGHT STRIP MISSING. REPLACED MISSING EMERGENCY LIGHT STRIP IAW AMM 33-51-01-400-801-A21.
FLOOR TRACK LIGHT DEGRADED ON LT SIDE OF ROWS 3 - 4. REPLACED EMERGENCY FLOOR TRACK LIGHT PN PL-88-900LH00 IAW AMM 33-51-01.
EMERGENCY FLOOR TRACK STRIP MISSING AT WINDOW EXIT 13DC. REPLACED FLOOR TRACK STRIP AT SEAT 13DC IAW CRJ 900 AMM 33-51-01.
EMERGENCY LIGHTING STRIP IN THE GALLEY AREA IS NO LONGER SECURE. STRIP LOCATED IN FRONT OF CARTS NR 305 & 306. SECURED STRIP LIGHTING IN FWD GALLEY IAW 33-51-00, ACFT OK TO CONTINUE.
MAIN PAX DOOR WOULD NOT FULLY OPEN UPON ARRIVAL. REMOVED CABLE BALL END AT DOOR FRAME ATTACHMENT. LOWERED DOOR, CABLE BACKLASHED ON DRUM, STOWED CABLE, STOWED MTR CONNECTOR, PULLED & COLLARED CBP 1 E1 VERIFIED DOOR OPEN & CLOSES FREELY WITHOUT INTERFERENCE & INDICATES CLOSED. ITEM CURRENTLY ON MEL 52-11-1A C IAW LOG PAGE 2462876 1 REMAINS DEFERRED.
CHARGER PS43P1 INOPERATIVE. R & R CHARGER IAW AMM 33-51-17. OPS CHECKED GOOD.
BATTERY AT PS35 BURNED. R & R EPSU BATTERY PACK AT PS35 IAW J/C 33-900-701.
EMERGENCY LIGHT MISSING IN GALLEY. REPLACED EMERGENCY LIGHT IAW AMM 33-51-01. OPS CHECKED GOOD.
FWD EQUIPMENT COMPARTMENT RT SKIN CRACKED UNDER ADG HAND PUMP. REPAIRED CRACKED RT SKIN AS REQUIRED IAW REO 670-53-11-509.
LEFT 280 BEAM HAS CORROSION. REMOVED AND REPLACED LEFT FS 280 BEAM IAW EO R53290 & EO R53117 AND EO R53127.
LBL 12 BEAM IN THE VERY FWD E & E BAY IS CRACKED. REMOVED AND REPLACED CRACKED SECTION OF LBL 12 BEAM IAW EO R53289.
SPLICE ON STGR 25R AT FRAME 333 HAS CORROSION, IN THE FWD E & E BAY. REMOVED AND REPLACED STGR 25R SPLICE AT FS 333 IAW CRJ 900 SRM 51-42-06.
STRINGER 26R HAS CORROSION BETWEEN FRAMES 333 AND 280, IN THE FWD E & E BAY. REMOVED AND REPLACED STGR 26R FROM FS 280 TO FS 333 IAW CRJ 900 SRM 51-42-06.
RBL 12 BEAM IN THE VERY FWD E & E BAY IS CRACKED. REMOVED AND REPLACED CRACKED PORTION OF RBL 12 BEAM IAW EO R53289. AAR SM-10.
RBL 12 BEAM IN THE VERY FWD E & E BAY IS CRACKED. REMOVED AND REPLACED CRACKED PORTION OF RBL 12 BEAM IAW EO R53289. AAR SM-10.
RIGHT 280 BEAM UPPER FREE FLANGE AT BL 0.00, UPPER RADIUS HAS CORROSION. REMOVED AND REPLACED RIGHT FS 280 BEAM IAW EO R53290 + EO 53127. P/N CC670-34094-2S.
FLT DECK FLOOR FLANGE AFT LANDING LOWER SURFACE HAS CORROSION NEW 280 BEAM. REMOVED AND REPLACED AFT FLOOR LANDING IAW CRJ 900 RM 51-40-11 & 51-42-06. P/N CC670-34095-35. AAR SM-10.
FOUND EMERGENCY BATTERY TO BE BAD. R & R BATTERY AT PS 43 IAW JOB CARD 33-900-701. OPS CHECKED GOOD.
WITH THE EMERGENCY LIGHT SWITCH IN THE ARMED POSITION THE EMERGENCY LIGHTS COME ON AND FLICKER OFF ON THEIR OWN. PERFORMED OPS TEST OF EMERGENCY LIGHTING IAW AMM 33-51.
FWD OVERWING EMERGENCY LIGHT & ROW 12 EMERGENCY LIGHTS ON WHEN ACFT POWER REMOVED. LIGHTS COME ON INTERMITTENTLY. REPLACED PS37 POWER SUPPLY/CHARGER P/C 11-0049, SN 23169, AND REPLACED BATTERY ASSY PN 2013-1A, SN 98024, IAW AMM 33-51-17. OPS CHECKED GOOD.
DURING RETURN TO GATE, NOTED ROW 12 EMERGENCY LIGHTS ILLUMINATED. REPLACED BATTERY PACK PS37 IAW AMM 33-51-17 PN ON/OFF 2013-1A, SN OFF 99445, SN ON 98024.
DURING CRUISE AT FL 340, THE EMERGENCY LIGHTS IN THE CABIN (ALL OF THEM) ALONG WITH THE ASSOCIATED "EMER LTS ON" EICAS STATUS MESSAGE BEGAN CYCLING ON AND OFF. ALL OTHER SYS APPEARED NORMAL. CONTINUED FOR REMAINDER OF FLIGHT AND WHILE PARKED AT THE GATE ON EXTERNAL POWER. R & R ACESS BUSS SENSE RELAY K198, PN M83536/17-002L IAW ESPM 20-39-00. OPS CHECK OF EMERGENCY LIGHTS GOOD IAW AMM 33-51-00.
DURING INSPECTION, NOTED LT SIDE GALLEY FLOOR TRACK LIGHT STRIP BROKEN/MISSING. INSTALLED NEW FLOOR TRACK LIGHT STRIP ON LT SIDE OF GALLEY.
EMERGENCY LIGHT STRIP IN GALLEY IS MISSING. REPLACED FLOOR TRACK LIGHTING.
GEAR EXTENSION FAILED ON APPROACH TO DTW. PERFORMED EMERGENCY LANDING GEAR EXTENSION AND LANDED IN DTW. (A)