N303PQ
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
FO SIDE MAP LIGHT SPARKED AND EMITTED SMOKE WHEN MOVED. REMOVED AND REPLACED FO SIDE MAP READING LIGHT IAW AMM 33-13-03. OPS CHECKS GOOD. NO SMOKE ODOR NOTED.
AT FL250 MLG BAY OVHT WARN RAN QRH WARN MSG DID NOT EXTINGUISH BTMS ALL 0000 LANDED W/O ISSUE WARN MSG PERSISTS AT GATE. R/R FIRE DETECTION CONTROL IAW AMM 26-14-01. MESSAGE DID NOT CLEAR. R/R L & R MLG BAY TEMPATURE SENSING ELEMENT IAW AMM 26-14-04. OPS TEST GOOD. MESSAGE CLEARED. NO OTHER DEFECTS NOTED AT THIS TIME.
RH REAR EXTERIOR EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED EXTERIOR EMEREGENCY LIGHT AT THE RIGHT AFT OVER WING SECTION OF THE FUSELAGE IAW AMM 33-51-15 OPS CHECK GOOD P/N ON/OFF:8GH002473-08
DURING INSP. FOUND ALL FOUR OVERWING EMER EXITS/ FORWARD FLOOR EMER EXITS AND MID CABIN FORWARD EMERGENCY LIGHTS INOP. TROUBLESHOT AND FOUND EMERGENCY BATTERY PS37 INCORRECTLY INSTALLED. R/R PS37 BATTERY AND WAS ABLE TO GET ONE O/W EXIT LIGHT WORKING AND BOTH FWD FLOOR EMER EXIT ROW LIGHTS WORKING. BOTH O/W RH EXIT LIGHTS AND FWD MID CABIN LIGHT STILL INOP. R/R PS35, PS36, PS38 BATTERYS IAW JOBCARDS 33-900-701. BOTH RH O/W AND FWD MID CABIN STILL INOP. R/R PS37 BATTERY CHARGER IAW AMM 33-51-17. R/R FWD LH O/W LIGHT BULB IAW AMM 33-51-15. OPS. CHECKS GOOD.
AFT LH EMERGENCY EXIT DOOR POSSIBLE CRACK NEAR BASE OF UPPER LUG. REPAIRED AFT LH EMERGENCY EXIT DOOR IAW ENDEAVOR AIR EA NO: CRJ952-16063 REV IR DATED 3/4/2024
LEFT FORWARD OVER-WING EMERGENCY EXIT 833 APPEARS TO BE CRACKED AT THE BASE OF THE AFT UPPER LUG. REQUIRES EVALUATION. REPAIRED AFT LH EMERGENCY EXIT DOOR IAW ENDEAVOR AIR EA NO: CRJ952-15922 REV IR DATED 3/6/2024
PAX DOOR FWD STAIR SIDE PANEL CORRODED AT APPROX DD7 AROUND HAND RAIL UPPER FWD POST ASSY. REPAIRED SIDE PANEL, FORWARD, PASSENGER DOOR STAIRS, P/N 601R317071-12 IAW ENDEAVOR AIR EA. CRJ952-16088 REV -- DATED 2-19-2024.
STIFFENING ANGLE AT FS 280 RBL26 PN:CC670-34117-6 IS CRACKED AND REQUIRES REPLACEMENT. REMOVED STIFFENING ANGLE AT FS 280 RBL 26 PN: CC670-34117-6 IAW CRJ 900 SRM 51-42-06-001-001-A01. INSTALLED NEW STIFFENING ANGLE PN CC670-31147-6 IAW CRJ900 SRM 51-42-06-001-001-A01
RH FLAP L/E ACCESS PANEL 684GB IS CHAFED. FOUND DAMAGE ON PANEL BEYOND REPAIR. LOCATED AND DRILLED NEW SERVICABLE PANEL 684GB IAW CRJ-900 SRM 51-40-11-001-001-A01.
EXTERNAL A/C POWER RECEPTICAL MOUNTING CHANNEL IS CRACKED. DISCONNECTED THE MAIN BATTERY IAW CRJ900 AMM 24-32-00-040-801-A01, CONNECTED MAIN BATTERY IAW CRJ 900 AMM 24-32-00-440-801-A01. REMOVED AND REINSTALLED EXTERNAL AC POWER RECEPTACLE USING PN NAS1149DD332K NUTS PO 5-8434 AND MS21042L3 WASHERS PO 5-10302 IAW CRJ900 AMM 24-41-03-400-801-A01. CONNECTING MAIN BATTERY, ENERGIZING GROUND SERVICE BUS FROM EXTERNAL AC AND RETRACTION OF THE ADG REQUIRED. REFER TO JOB HR00381925 FOR RETRACTION OF ADG. REMOVED AND REPLACED EXTERNAL A/C POWER RECEPTACLE MOUNTING CHANNEL PN CC670-33401-3 IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01. APPLIED PROTECTIVE SURFACE COATING IAW SRM 51-21-16-001-001-A01.
"L/H FWD EQUIPMENT BAY FLOOR WEB APPEARS TO BE CRACKED AT F.S.193. REMOVED DAMAGED AREA IN BAY FLOOR WEB LH SIDE AT FS193 IAW CRJ900 SRM 53-11-43-201-001-A01. FABRICATED, LOCATED DRILLED, DEBURRED AND INSTALLED REPAIR PARTS, DOUBLER AND SHIM 2024T3 0.040"" PO: 5-4713, CLEAT 2024T3 0.032"" PO: W81195 IAW CRJ900 SRM 53-11-43-201-001-A01. REMOVED AND REINSTALLED SYS#2 AND #3 BRAKE ACCUMULATOR GAUGES IAW CRJ 900 AMM 32-43-30-000-801-A01. REMOVED AND REINSTALLED NITROGEN LINES FOR BRAKE ACCUMULATOR GAUGES IAW CRJ 900 AMM 20-22-00-910-801-A01. REMOVED AND REINSTALLED SUPPORT (NP CC670-75600-1) TO GAIN ACCESS IAW CRJ-900 SRM 51-42-06-001-001-A01 SERVICED THE BRAKE ACCUMULATORS IAW CRJ 900 AMM 12-12-29-614-801-A01. PERFORMED OPS CHECK OF THE BRAKE ACCUMULATOR IAW CRJ 900 AMM 32-43-16-710-801-A01. OPS CHECK GOOD."
RH COCKPIT FLOOR BEAM (RBL12) IS CRACKED ON O/B AFT RADIUS. COMPLIED WITH MHIRJ REO# 690-53-11-1689 REV. -- DATED 2024-02-22 FOR RBL12 COCKPIT FLOOR BEAM.
LH COCKPIT FLOORBEAM IS CRACKED ON O/B AFT RADIUS. COMPLIED WITH MHIRJ REO# 690-53-11-1689 REV. -- DATED 2024-02-22 FOR RBL12 COCKPIT FLOOR BEAM.
LBL 12 FWD ATTACH ANGLE FOUND TO BE CRACKED. LOCATED AND DRILLED SERVICEABLE LBL 12 FWD ATTACH ANGLE P/N CC670-34099-1SB. INSTALLED SERVICEABLE LBL 12 FWD ATTACH ANGLE P/N CC670-34099-1SB IAW CRJ 900 SRM 51-42-21-001-001-A01.
RH FLOOR SILL BETWEEN FS 280 TO 319 IS CORRODED ON UPPER AND LOWER SURFACE. REMOVED AND REPLACED RH FLOOR SILL IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01
RBL 9 FWD OB ATTACH ANGLE FOUND TO BE CRACKED. LOCATED AND DRILLED SERVICEABLE RBL 9 FWD OB ATTACH ANGLE P/N CC670-34269-8 INSTALLED SERVICEABLE RBL 9 FWD OB ATTACH ANGLE P/N CC670-34269-8 IAW CRJ 900 SRM 51-42-21-001-001-A01.
RBL 12 FWD ATTACH ANGLE FOUND TO BE CRACKED. LOCATED AND DRILLED SERVICEABLE RBL 12 FWD ATTACH ANGLE P/N CC670-34099-2.INSTALLED SERVICEABLE RBL 12 FWD ATTACH ANGLE P/N CC670-34099-2 IAW CRJ 900 SRM 51-42-21-001-001-A01.
"FS 280 ""J"" ANGLE IS CORRODED BETWEEN LBL 9 AND RBL 9 REMOVED FS 280 ""J"" ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW ""J"" ANGLE PN: CC670-34095-1 IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW FS 280 ""J"" ANGLE PN: CC670-34095-1 IAW CRJ900 SRM 51-42-06-001-001-A01."""
LH FS 280 BULKHEAD LOWER WEB IS CORRODED. REPAIRED LH FS 280 BULKHEAD LOWER WEB IAW CRJ 900 SRM 53-11-10-201-004-A01.
RH FS 280 BULKHEAD LOWER WEB IS CORRODED. REPAIRED RH FS 280 BULKHEAD LOWER WEB IAW CRJ 900 SRM 53-11-10-201-004-A01.
RH FS 280 CROSSBEAM IS CORRODED REPLACED CROSS BEAM IAW SRM 51-40 AND 51-42
LH FS 280 CROSSBEAM IS CORRODED REMOVED AND REPLACED LH FS 280 CROSSBEAM IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-21-11-001-001-A01.
FS 280 DOOR CORNER POST IS CORRODED AT LBL9 FLOOR LEVEL REPAIRED FS 280 DOOR CORNER POST AT LBL9 FLOOR LEVEL IAW CRJ 900 SRM 53-11-10-201-006-A01. REMOVED AND REINSTALLED INSTALLED SAME SERVICEABLE GUSSET AND INSTALLED NEW SERVICEABLE ATTACH ANGLE AT LH FS 280 DOOR CORNER POST IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 53-11-10-201-006-A01. FABRICATED, LOCATED, AND DRILLED ATTACH ANGLE PN: CC670-34191-1 OUT OF S6144-4 IAW CRJ 900 SRM 53-11-10-201-006-A01. APPLIED PAINT TO LH FS 280 DOOR CORNER POST IAW CRJ 900 SRM 51-25-16-001-001-A01.
AT 29000 FT WE RECIEVED A CABIN ALT CAUTION THAT ESCALATED TO A CABIN ALT WARNING. THE CABIN ALT INCREASED TO 12,300 FT. WE RAN THE EMERGENCY CHECKLIST CARD WHICH DIRECTED US TO QRH 7-7. WE PREFORMED THE QRH PROCEDURE AS UNPRESSURIZED AND CONTINUED THE FLIGHT TO JFK. THE RIGHT PACK TURNED OFF BEFORE COMPLETION OF QRH AUTOMATICALLY. COMPLIED WITH FIM 21-31-00 INSPECTION AND CHECKS AND WORK SCOPE ISSUED MY MOTR. FOUND DAMAGED WIRE ON LPCP. REPAIRED WIRE (PER ESPM 20-44-11) AND REPLACED CPCP (PER AMM 21-33-01). ALSO FOUND DAMAGED PIN ON PSEU (PN 8-953-05, SN D3455). REPLACED PSEU (PER AMM 32-61-01). NO FURTHER ISSUES FOUND.
FA REPORTS FLOOR LEVEL EMRGENCY LIGHTED EXIT SIGNS ON BOTH SIDES IN ROW 13 ARE INOP. REMOVED AND REPLACED PS38 EPSU BATTERY PACK IAW AMM 33-51-17. OPS CHECK OK.
INITIAL INSPECTION: WEAR ON SETTLEMENT AREA OF THE WHEEL AT NLG PISTON/AXLE ASSEMBLY. (SM).IN REFERENCE NRC SN 461. SETTLEMENT AREA OF THE WHEEL AT NLG PISTON/AXLE ASSEMBLY WAS REPAIRED PER REO 690-32-21-117 REV --
EDV AIR: LH ENGINE TR COWL LOWER SEAL TORN.(MOT1)(AYP) SUMMARY: SEAL (P/N: G50483) LOWER TR COWL LH ENGINE WAS REPLACED PER CRJ 900 SRM 51-42-10-001-001-A01.
AWR IN REF NRC S/N 00523, AFTER BUSHING REMOVAL CORROSION WAS FOUND ON PCU HINGES FITTING LUGS (4EAS) OF LH AILERON . HINGES FITTING LUGS (4EAS) OF LH AILERON WERE REPAIRED PER REO 670-57-61-237 REV.--
AWR IN REF NRC S/N 00524, AFTER BUSHING REMOVAL CORROSION WAS FOUND ON PCU HINGES FITTING LUGS (4EAS) OF RH AILERON . HINGES FITTING LUGS (4EAS) OF RH AILERON WERE REPAIRED PER REO 670-57-61-237 REV. --
INITIAL INSPECTION. WEAR ON SEAL DEPRESSURE FS 517 AND 565, BTW STRG 23L-24L AT FWD CARGO BAY SURROUND. SEAL DEPRESSURE FS 517 BTW STRG 23L-24L AT FWD CARGO BAY SURROUND WAS REPLACED PER CRJ900 SRM 51-41-02 AND RETAINER SEAL SURROUND ON FS 565 WAS BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01 THEREFORE IT'S WITHIN LIMITS PER CRJ-900 SRM 53-31-23-101-001-A02
INITIAL INSPECTION: CORROSION ON SIDE SEAT RAIL 15RH BETWEEN FS847+16 TO FS897.70, FS897.70 TO FS913, FS913 TO FS969 AT PASSENGER CABIN.(SM)(CPAX)(TCI 53-20-301) SUMMARY. SIDE SEAT RAILS 15RH BETWEEN FS847+16 TO FS897.70, FS897.70 TO FS913, FS913 TO FS969 AT PASSENGER CABIN WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801-A12.
INITIAL INSPECTION : CRACK IN CANISTER, WELDED NO.3 IN STA WS148 AT LH MAIN FUEL TANK. (AI) CANISTER, WELDED NO. 3 IN WS148 AT LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. "-
INTIAL INSPECTION: CORROSION ON STRINGER 26RH BETWEEN FS 349 AND FS364 AT MAIN AVIONICS COMPARTMENT. (SM)(E/E)(CI 100-09E5) SUMMARY: STRINGER 26RH BTW FS=333 TO FS=364 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01.
INITIAL INSPECTION : WEAR ON RETAINER 8E/A OF LOWER AND UPPER RH ENGINE TRASCOWL (MOT 2) SUMMARY: RETAINER 8E/A OF LOWER AND UPPER RH ENGINE TRASCOWL WERE REPLACED PER CRJ900 SRM 51-42-20-001-001-A01.
INITIAL INSPECTION : BENT SEAL RETAINER LOWER EDGE OF AFT CARGO COMPARTMENT DOOOR (PTAS) SEAL RETAINER LOWER EDGE OF AFT CARGO COMPARTMENT DOOOR WAS REPAIRED PER EA NO: CRJ952-10646 REV. IR
INITIAL INSPECTION. CORROSION ON FRAME FS 549, STRG 18 AT FWD CARGO BAY. (TCI 53-20-333). FRAME FS 549, STRG 18 AT FWD CARGO BAY WAS REPAIRED PER EA CRJ953-10527 REV IR
"PARTS RACK: CORROSION ON HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT. (CCT). " "HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WERE REPLACED FOR NEW ONES PER CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6A."
INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS IN SECTIONS [ FS= 349 TO FS= 485, 9RBL/LBL ] [FS485 TO FS581 9RBL][ FS= 661+32 TO FS= 847+8.40, 9LBL/9RBL ] ALSO [27LBL FS954 TO FS 985 AND 9LBL FS977 TO FS 985] AT PAX CABIN. (CPAX) (TCI: 53-20-243) FLOOR SEAT RAILS IN SECTIONS [ FS= 349 TO FS= 485, 9RBL/LBL ] [FS485 TO FS581 9RBL][ FS= 661+32 TO FS= 847+8.40, 9LBL/ 9RBL ] ALSO [27LBL FS954 TO FS 985 AND 9LBL FS977 TO FS 985] AT PAX CABIN. WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801-A12.
INITIAL INSPECTION: CORROSION ON SEAT SIDE RAIL SECTIONS FS485 TO FS565, FS565 TO 661+16, FS 661+16 TO FS661+90 LH SIDE ALSO FS661 TO FS661+16,FS661+16 TO FS661+90 SECTION RH SIDE AT PASSENGER CABIN. (SM) (CPAX) (TCI 53-20-301) SEAT SIDE RAIL SECTIONS FS485 TO FS565, FS565 TO 661+16, FS 661+16 TO FS661+90 LH SIDE ALSO FS661 TO FS661+16,FS661+16 TO FS661+90 SECTION RH SIDE AT PASSENGER CABIN WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801-A12.
INITIAL INSPECTION: CORROSION ON SEAT SIDE RAIL SECTIONS FS677 TO FS720.85, FS744.15 TO FS761.85, FS785.15 TO FS847+FS8.40, FS847+8.40 TO FS847+16 SIDE RAIL LH/RH SECTIONS AT PASSENGER CABIN.(SM)(CPAX)(TCI 53-20-301) SEAT SIDE RAIL SECTIONS FS677 TO FS720.85, FS744.15 TO FS761.85, FS785.15 TO FS847 +FS8.40, FS847+8.40 TO FS847+16 SIDE RAIL LH/RH SECTIONS AT PASSENGER CABIN WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801-A12
INITIAL INSPECTION: CORROSION ON SEAT SIDE RAIL SECTION FS847+16 TO FS913, FS913 TO FS969 LH SIDE RAIL AT PASSENGER CABIN. (SM) (CPAX) (TCI 53-20-301) SEAT SIDE RAIL SECTION FS847+16 TO FS913, FS913 TO FS969 LH SIDE RAIL AT PASSENGER CABIN WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801-A12.
"AWR; [TASK R53520 STEP 7]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "SUMMARY: PROTECTION PLATE SUPPORTS ANGLE WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01. "
AWR; [TASK R53520 STEP 7]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 329 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY:PROTECTION PLATE SUPPORTS ANGLE WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01.
AWR; [TASK R53520 STEP 7]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY:CORROSION ON ANGLE, LOWER SILL WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01.ANGLE, LOWER SILL MUST BE REPLACED BECAUSE DAMAGE EXCEEDS THE 10 PERCENT OF ALLOWABLE LIMITS PER CRJ 900 SRM 53-21-23-101-002 A02.ANGLE, LOWER SILL WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01.
AWR; [TASK R53520 STEP 7]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY: PROTECTION PLATE SUPPORTS ANGLE WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01.
AWR; [TASK R53520 STEP 7]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) PROTECTION PLATE SUPPORTS ANGLE WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01.
AWR; [TASK R53520 STEP 7]; INITIAL INSPECTION: CORROSION ON SUPPORT MOUNTING ANGLE IN STA. FS= 319 TO FS= 349 AND 41RBL AT GALLEY SERVICEDOOR LOWER SILL,FWD WET AREA. (W1) (CPAX) SUMMARY: CORROSION ON ANGLE, LOWER SILL REMOVED PER CRJ900 SRM 51-21-0 6-001-001A01. ANGLE,MOUNTING MUST BE REPLACED BECAUSE DAMAGE EXCEEDS THE 10% OF ALLOWABLE LIMITS PER CRJ 900 SRM 53-21-23-101-002-A02. ANGLE MOUNTING WAS REPLACED PER CRJ900 51-42-21-001-001-A01.
INITIAL INSPECTION: CRACK ON BAFFLES 2E/A ON RH ENGINE LOWER THRUST REVERSER CASCADE FITTINGS.(MOT2) BAFFLES 2E/A ON RH ENGINE LOWER THRUST REVERSER CASCADE FITTINGS WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 ADDITIONAL PART CN624-2052-201
PARTS RACK: . CRACK ON CHANNEL 1E/A OF WING TO FUSELAGE FAIRING 196DR. (FUS) DAMAGED CHANNEL WAS REPLACED PER CRJ 900 SRM 51-42-10-001-001-A01
[IN REFERENCE NRC 0070]: INITIAL INSPECTION: CORROSION ON FRAME FS= 333 BETWEEN STRG 27 TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) [TASK 900-53-140-300 APPENDIX A] TCI: 100-09, 100-09E4, 100-09E5 FRAME FS= 333 BETWEEN STRG 27 TO 26RH AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER CRJ900 SRM 53-00-06-201-004-A01.
[IN REFERENCE NRC0070]: INITIAL INSPECTION. CORROSION ON INTERNAL PRODUCTION DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) [TASK 900-53-140-300 APPENDIX A] TCI: 100-09, 100-09E4, 100-09E5" INTERNAL PRODUCTION DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-20-001-001-A01.
[IN REFERENCE NRC 0070] : INITIAL INSPECTION: CORROSION ON STRINGER 26RH IN STA. FS= 280 TO FS=333 AT MAIN AVIONICS COMPARTMENT. (E/E) [TASK 900-53-140-300 APPENDIX A] TCI: 100-09, 100-09E4, 100-09E5 SUMMARY:STRINGER 26RH BTW FS 280 TO FS333 WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01.
INITIAL INSPECTION: CRACK ON CHANNEL OF AFT CARGO DOOR SURROUND STRUCTURE. (CCT) "CHANNEL OF AFT CARGO DOOR SURROUND STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01."
[ IN REFERENCE NRC 0070 ] : INITIAL INSPECTION: CORROSION ON INTERCOSTALS IN STA. FS= 349 TO FS= 364 NEAR STGR 27 (2 EA´S) AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 SUMMARY: NEW INTERCOSTALS IN STA. FS= 349 TO FS= 364 NEAR STGR 27 (2 EA´S) WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01.
[IN REFERENCE NRC 0070]: INITIAL INSPECTION: CORROSION ON FRAME FS= 319 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) [TASK 900-53-140-300 APPENDIX A] TCI: 100-09, 100-09E4, 100-09E5 FRAME FS= 319 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER EA NO: CRJ953-10454 REV IR
[IN REFERENCE NRC 0070]: INITIAL INSPECTION: CORROSION ON FRAME FS= 310 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) [TASK 900-53-140-300 APPENDIX A] TCI: 100-09, 100-09E4, 100-09E5 FRAME FS= 310 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) WAS REPAIRED PER EA CRJ953-10604 REV.IR.
INITIAL INSPECTION: CORROSION ON STRINGER SPLICE 22RH BETWEEN FS= 319.70 AND FS333 AT MAIN AVIONICS COMPARTMENT. (SM)(E/E)(TCI: 53-20-304) SUMMARY: STRINGER SPLICE 22RH BETWEEN FS319.70 AND FS333 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.
INITIAL INSPECTION: WEAR ON PAD WHERE SEATS THE LATCH OF LOWER/UPPER COWL BLOW-OFF DOOR AT RH ENGINE PADS WHERE SEATS THE LATCH OF LOWER/UPPER COWL BLOW-OFF DOOR AT RH ENGINE WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01.
INITIAL INSPECTION : BROKEN LATCH OF AC EXTERNAL POWER ACCESS DOOR ( 122DR) LATCH OF AC EXTERNAL POWER ACCESS DOOR ( 122DR) WAS INSTALLED PER CRJ900 SRM 51-42-06-001-001-A01.
INITIAL INSPECTION . CORROSION ON BONIDING JUMPER BRACKET AT FWD WATER WASTE SERVICE PANEL DOOR 142BR. BONDING JUMPER BRACKET AT FWD WATER WASTE SERVICE PANEL DOOR 142BR WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-06-001-001-A01
INITIAL INSPECTION: WEAR ON PAD WHERE SEATS THE LATCH OF UP/LWR COWL BLOW-OFF DOORS AT LH ENGINE (MOT) PADS WHERE SEATS THE LATCH OF UP/LWR COWL BLOW-OFF DOORS AT LH ENGINE WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01
INITIAL INSPECTION: CORROSION ON BRACKET OF GREEN LIGHT INDICATOR AT RINSE/FILL VALVE AFT LAVATORY (SM) BRACKET OF GREEN LIGHT INDICATOR AT RINSE/FILL VALVE AFT LAVATORY WAS REPLACED FOR A NEW ONE PER CRJ 900 SRM 51-41-02-001-001-A01 AND AMM 20-21-00-910-801-A01.
CA SIDE O2 MASK WILL NOT PURGE. REMOVED AND REPLACED CA O2 MASK IAW AMM 35-11-12-400-807. OPS CHECK GOOD.
FO 02 MASK SEEMS TO BE LEAKING. REMOVED AND REPLACED FO'S MASK IAW AMM 35-11-12. OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME.
PROXIMITY SYSTEM CAUTION MOMENTARILY ILLUMINATED, AND GEAR DISAGREE AS WELL DURING FLIGHT. R & R THE LANDING GEAR SELECTOR VALVE AND LANDING GEAR CONTROL LEVER IAW AMM 32-31-01 AND AMM 32-32-10. CHECKED GOOD.
EMERGENCY LIGHT STATUS MESSAGE. CABIN EMERGENCY LIGHTS COME ON AND OFF ON THEIR OWN WHILE ARMED. REMOVED AND REPLACED EMERGENCY LIGHT RELAY K198 IAW AMM 33-51-19. OPS CHECKED GOOD.
AFT FA FLASHLIGHT INOPERATIVE. R & R THE AFT FA FLASHLIGHT IAW AMM 25-61-02. OPS CHECKED GOOD. OK FOR SERVICE.
EMERGENCY FLASHLIGHT BY AFT LAVATORY INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 25-61-02. OPS CHECKED GOOD.
F/A REPORTED EMERGENCY LIGHT NOT CHARGING. REMOVED AND REPLACED THE EMERGENCY LIGHT. OPS CHECKED GOOD.
PAX DOOR AFT RISER IS CRACKED BEHIND HANDRAIL RECETACLE. REPAIRED PAX DOOR AFT RISER IAW SRM 52-11-04 TR52-0025. OPS TEST GOOD IAW AMM 52-11-04-710-801 AND 52-11-00-710-801.
MAIN AVI DOOR FORWARD SURROUND RIGHT LATCH PIN INTERCOSTAL CORRODED, FS 364 AT STGR 26R. OUT OF LIMITS. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-06 AND SRM 51-42-21.
MAIN AVIN DOOR FORWARD SURROUND LEFT LATCH PIN INTERCOSTAL CORRODED, FS364 AT STRINGER 26L. OUT OF LIMITS. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-06 AND SRM 51-42-21. PREFORMED OPS CHECK OF THE MAIN AVIONICS DOOR IAW AMM 52-42-00-710-801. OPS CHECK GOOD.
STGR25R SPLICE AT FS 333.00 CORRODED. REMOVED AND REPLACED STRINGER SPLICE IAW SRM 51-42-06 AND SRM 51-42-21.
PAX DOOR AFT RISER IS CRACKED AT TOP FIXED STEP. REPAIRED PAX DOOR AFT RISER AT TOP FIXED STEP IAW SRM 52-11-04.
PAX DOOR FWD RISER IS CRACKED BEHIND HANDRAIL RECETACLE. REPAIRED PAX DOOR FWD RISER BEHIND HANDRAIL RECETACLE IAW SRM 52-11-04.
MAIN AVI DOOR FORWARD SURROUND INTERCOSTAL AT STR 26R CORRODED, FS349 TO FS364. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-06.
DURING WAKE UP CHECK, NOTED GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. R & R THE FLASHLIGHT IAW AMM 25-61-02 .
CAPTAIN & FLIGHT ATTENDANTS LIFE VEST BAGS TORN. R & R CAPTAIN & FLIGHT ATTENDANTS LIFE VEST IAW AMM 25-61-03.
EMERGENCY EXIT ROW 13 CD, EXIT DOOR HAS A LOUD AIR NOSE THAT BOTHERS THE PAXS, LOUD WHISTLING SOUND. R & R RT AFT EMER EXIT VENT SEAL PN SH670-36576-1 IAW MM 52-21-03. PRESS CHECK IAW 52-00-00 GOOD.
ABOUT 2 MINUTES PRIOR TO LANDING, BOTH PILOTS SMELLED BURNING SMELL. FOUND CB PANEL 2 G7 OPEN, COPILOT MAP LIGHTS. BREAKER WAS PREVIOUSLY OPEN ON ACFT POWER UP. BURNING SMELL QUICKLY DISSIPATED. ALL OTHER INDICATIONS NORMAL. INSPECTED BEHIND CB PANEL 2 G7, CO-PILOT MAP LIGHT & SURROUNDING AREA. NO DEFECTS NOTED TO CB OR WIRING. DEFERRED FIRST OFFICERS MAP LIGHT IAW MEL 33-11-1A CAT C, ENTERED IN MM2. PLACARD INSTALLED. CB PANEL 2 G7 COLLARD. PERFORMED INSPECTION RESISTANCE & VOLTAGE CHECK OF FO MAP LIGHT WITH REFERENCE TO CRJ 900 SSM 33-13-00 AND WM 33-13-01, PERFORMED OPS CHECK OF FO MAP LIGHT IAW CRJ 900 AMM 33-13-03, OPS CHECK GOOD. CLEARED FROM MM02, PLACARD REMOVED, MXC NOTIFIED 95909."